Thursday, March 14, 2019

Landing Gear Not Configured: Beech E-55 Baron, N15VK; accident occurred March 13, 2019 at Albert Whitted Airport ( KSPG), St Petersburg, Pinellas County, Florida













Aviation Accident Final Report - National Transportation Safety Board

The National Transportation Safety Board did not travel to the scene of this accident.

Additional Participating Entity: 
Federal Aviation Administration / Flight Standards District Office; Tampa, Florida

Investigation Docket - National Transportation Safety Board:


Location: St. Petersburg, Florida 
Accident Number: ERA19TA129
Date & Time: March 13, 2019, 16:17 Local 
Registration: N15VK
Aircraft: Beech E55
Aircraft Damage: Substantial
Defining Event: Landing gear not configured 
Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis

The pilot stated that he became distracted and did not extend the landing gear before landing at the airport. The airplane slid on the runway, which resulted in substantial damage to the left wing's rear spar. Although the airplane was equipped with a gear warning horn, both the pilot and the passenger said the horn did not sound. The gear warning horn had been functionally checked during the last annual inspection and was also tested after the accident with no anomalies noted; thus, the investigation could not determine why the pilot and passenger were unable to hear the horn.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's failure to extend the landing gear, which resulted in a gear-up landing.

Findings

Aircraft Main landing gear - Not used/operated
Personnel issues Forgotten action/omission - Pilot
Aircraft Gear position and warning - Inoperative

Factual Information

On March 13, 2019, at 1617 eastern daylight time, a Beech E55, N15VK, sustained substantial damage during a gear-up landing at the Albert Whitted Airport (SPG), St. Petersburg, Florida. The commercial pilot and the passenger were not injured. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight that departed Lakeland Linder International Airport (LAL) Lakeland, Florida, at 1515.

The pilot stated that became distracted and did not extend the landing gear before landing. The airplane slid on the runway resulting in substantial damage to the left wing's rear spar. The propellers and flaps were also damaged.

According the airplane's Pilot Operating Handbook (POH), page 6-10, "If either or both throttles are retarded below an engine setting sufficient to sustain flight with the landing gear retracted, a warning horn will sound intermittently." The airplane was equipped with a gear warning horn; however, both the pilot and the passenger said the horn did not sound. The horn was functionally checked during the last annual inspection with no deficiencies noted. The horn was also tested after the accident and it worked as designed.

The pilot held a commercial pilot certificate with ratings for airplane single-engine land and sea, multiengine land, and instrument airplane. He also held a certified flight instructor certificate with a rating for airplane single-engine land. The pilot's last Federal Aviation Administration (FAA) third-class medical certificate was issued on February 11, 2019. He reported a total of 3,706 hours, of which, 1,217 hours were in multi-engine aircraft.

Weather reported at SPG at 1653 included wind from 090° at 11 knots, visibility 10 miles, and clear skies.

History of Flight

Landing-landing roll Landing gear not configured (Defining event)

Pilot Information

Certificate: Commercial; Flight instructor; Private
Age: 63, Male
Airplane Rating(s): Single-engine land; Single-engine sea; Multi-engine land
Seat Occupied: Right
Other Aircraft Rating(s): None 
Restraint Used: 4-point
Instrument Rating(s): Airplane 
Second Pilot Present: No
Instructor Rating(s): Airplane single-engine
Toxicology Performed: No
Medical Certification: Class 3 With waivers/limitations
Last FAA Medical Exam: February 11, 2019
Occupational Pilot: No
Last Flight Review or Equivalent: September 18, 2018
Flight Time: 3706 hours (Total, all aircraft), 590 hours (Total, this make and model), 3504 hours (Pilot In Command, all aircraft), 26 hours (Last 90 days, all aircraft), 19 hours (Last 30 days, all aircraft), 0 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Beech 
Registration: N15VK
Model/Series: E55 UNDESIGNATED
Aircraft Category: Airplane
Year of Manufacture: 1970
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: TE-805
Landing Gear Type: 
Retractable - Tricycle 
Seats: 6
Date/Type of Last Inspection: September 1, 2018 Annual 
Certified Max Gross Wt.: 5300 lbs
Time Since Last Inspection: 
Engines: 2 Reciprocating
Airframe Total Time: 3996.6 Hrs as of last inspection
Engine Manufacturer: Continental Motors
ELT: C126 installed, not activated
Engine Model/Series: IO-520-C7B
Registered Owner:
Rated Power: 285 Horsepower
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC) 
Condition of Light: Day
Observation Facility, Elevation: SPG, 6 ft msl 
Distance from Accident Site: 0 Nautical Miles
Observation Time: 16:53 Local 
Direction from Accident Site: 0°
Lowest Cloud Condition: Clear 
Visibility 10 miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 11 knots / 
Turbulence Type Forecast/Actual: None / None
Wind Direction: 90°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 30.06 inches Hg 
Temperature/Dew Point: 27°C / 19°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Lakeland, FL (LAL)
Type of Flight Plan Filed: None
Destination: St. Petersburg, FL (SPG) 
Type of Clearance: VFR
Departure Time: 15:15 Local
Type of Airspace: Class D

Airport Information

Airport: Albert Whitted SPG 
Runway Surface Type: Asphalt
Airport Elevation: 6 ft msl 
Runway Surface Condition:
Runway Used: 18
IFR Approach: None
Runway Length/Width: 2864 ft / 150 ft
VFR Approach/Landing: Full stop

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries: 1 None 
Aircraft Fire: None
Ground Injuries: N/A 
Aircraft Explosion: None
Total Injuries: 2 None
Latitude, Longitude: 27,-82(est)
 

Location: St. Petersburg, FL
Accident Number: ERA19TA129
Date & Time: 03/13/2019, 1617 EDT
Registration: N15VK
Aircraft: Beech E55
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal 

On March 13, 2019, at 1617 eastern daylight time, a Beech E55, N15VK, sustained substantial damage during a gear-up landing at the Albert Whitted Airport (SPG), St. Petersburg, Florida. The commercial pilot and the passenger were not injured. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight that departed Lakeland Linder International Airport (LAL) akeland, Florida, at 1515.

The pilot stated that became distracted and did not extend the landing gear before landing. The airplane slid on the runway resulting in substantial damage to the left wing's rear spar. The propellers and flaps were also damaged. The airplane was equipped with a gear warning aural alert; however, it did not sound for unknown reasons.

The pilot held a commercial pilot certificate with ratings for airplane single-engine land and sea, multi-engine land, and instrument airplane. He also held a certified flight instructor certificate with a rating for airplane single-engine land. The pilot's last Federal Aviation Administration (FAA) third-class medical certificate was issued on February 11, 2019. He reported a total of 3,706 hours, of which, 1,217 hours were in multi-engine aircraft.

Weather reported at SPG at 1653 included wind from 090° at 11 knots, visibility 10 miles, and clear skies. 

Aircraft and Owner/Operator Information

Aircraft Make: Beech
Registration: N15VK
Model/Series: E55 UNDESIGNATED
Aircraft Category: Airplane
Amateur Built: No
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: SPG, 6 ft msl
Observation Time: 1653 EDT
Distance from Accident Site: 0 Nautical Miles
Temperature/Dew Point: 27°C / 19°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: 11 knots / , 90°
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 30.07 inches Hg
Type of Flight Plan Filed: None
Departure Point: Lakeland, FL (LAL)
Destination: St. Petersburg, FL (SPG)

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries: 1 None
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 2 None
Latitude, Longitude:  27.000000, -82.000000 (est)
















HOURS estimated from logbooks or other information - not guaranteed or warranted

AIRCRAFT:   
1970 BEECH E-55 N15VK, s/n: TE-805
Last Annual 09/01/18 at Hobbs 3996.6
Hobbs on 03/13/19 4067.5

ENGINES: 
(2) TCM IO-520-C7B;  Last Annual 09/01/18 at Hobbs 3996.6, ETT 980.6 

PROPELLERS: 
Right: McCauley 3AF32C75-NR, s/n: 780382, OH 07/14/11
Left:  McCauley 3AF32C75-NR, s/n: 751161
Last Annual Inspection on 09/01/18
                       
EQUIPMENT: 
Garmin G500
Garmin GTN 750
Garmin GTN 650
Garmin GTN-Integrated GTX3X5 transponder
Garmin GTN-Integrated Garmin Audio Panel
Garmin GDL 88
Avidyne TAS 600 traffic alert (integrated with Garmin)
L3 WX500 Stormscope (integrated with Garmin)
Sandia SAI-340 Quattro Standby Instrument
S-TEC 55x Autopilot with Autotrim
EDM-960 engine management system
Alpha Systems Angle of Attack Indicator
Artex ME406 ELT
Advanced Aero Low Thrust Detection System
MidContinent MD93 Digital Clock/USB charger
BAS Shoulder Harness (2)
GAMI fuel nozzles
Vortex Generators

DESCRIPTION OF ACCIDENT:
Gear up landing that resulted in double prop strike on 03/13/19 at Albert Whitted Airport, St Petersburg, Florida 

DESCRIPTION OF DAMAGES: 
The damage includes but may not be limited to:  Damage sustained to left wing (substantial), nose skins, and underbelly damaged.

LOCATION OF AIRCRAFT: 
Sheltair, Albert Whitted Airport, St Petersburg, Florida

REMARKS:  
Insurer reserves the right to reject any and all bids. 
Salvage is as is/where is. 
The posting information is the best to our knowledge. 
An inspection of the aircraft is recommended. 
Logbooks may not be complete.

Read more here: http://www.avclaims.com

Bell OH-58A, N519P: Accident occurred March 13, 2019 in Ponte Vedra Beach, St. Johns County, Florida

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. 

The National Transportation Safety Board did not travel to the scene of this accident.

Additional Participating Entity:

Federal Aviation Administration / Flight Standards District Office; Orlando, Florida


Location: Ponte Vedra Beach, FL

Accident Number: ERA19LA126
Date & Time: 03/13/2019, 1755 EDT
Registration: N519P
Aircraft: Bell OH 58A
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Public Aircraft - Local 

On March 13, 2019, about 1755 eastern daylight time, a Bell OH-58A, N519P, operated by the St. Johns County Sheriff's Office was substantially damaged during a forced landing after a total loss of engine power in Ponte Vedra Beach, Florida. The commercial pilot and mission crewmember were not injured. The aerial observation flight departed a designated landing zone at a local golf course at 1750, destined for the Northeast Florida Regional Airport (SGJ), St. Augustine, Florida. Visual meteorological conditions prevailed at the accident site, and a company flight plan was filed for the public-use flight.

According to the pilot, the accident occurred on the third flight of the day, and he had performed a preflight inspection prior to each flight. All three flights were part of an aerial surveillance mission over a local golf tournament. The first flight was 90 minutes, and the helicopter was refueled prior to the second flight, which was 30 minutes. The accident flight departed the golf course landing zone with an estimated 340 lbs. of fuel on board. About 5 minutes after takeoff while orbiting at 1,100 ft mean sea level, the helicopter suddenly yawed to the left and the "low rotor" horn sounded. The pilot reduced the collective pitch, the horn silenced, he noticed the "engine out" and "master caution" lights illuminated on the instrument panel, and the engine tachometer showed a decreasing rpm. He performed an autorotation to a fairway on the golf course. During touchdown, the helicopter began to violently shake as it moved forward across the soft ground. As the windscreen began to crack and separate from its frame, the pilot increased collective to reduce the vibration and the helicopter came to a stop.

Examination of the wreckage by a Federal Aviation Administration inspector revealed bending and buckling damage to the tail boom and the frame around the windscreen and doors. Fuel was present in the fuel tank and a sample taken from the tank was clear with no water present. No fuel or other fluid leaks were observed. A field examination of the engine by an NTSB investigator revealed that all the accessible fuel line "B" nuts had matching torque stripes and could not be loosened by hand. The engine components rotated freely by hand with no binding, and there were no visible indications of any components overheating. The starter operated normally. When the starter was engaged the first time, no fuel was present at the fuel spray nozzle supply line. After bleeding air from the fuel lines, operating the starter resulted in fuel flow at the spray nozzle. The airframe fuel lines were pressurized with shop air with no leaks detected. The engine was removed and retained for further examination.

The helicopter's most recent 100-hour inspection was performed on May 6, 2019, at an airframe total time of 8,209 flight hours. At that time the engine had accrued a total of 6,245 hours since new, and 638 hours since overhaul. Maintenance performed at the time of the inspection included a scheduled replacement of a bleed valve and replacement of an intermittent spark ignitor. The helicopter had flown about 21 hours since that inspection/maintenance.

The pilot held a commercial pilot certificate with ratings for rotorcraft-helicopter and airplane single- engine land. At the time of the accident he had accrued a total of 822 hours of flight experience, of which 698 were in the same make and model as the accident helicopter.

The 1753 weather conditions reported at the Jacksonville Executive Airport (CRG), located about 10 miles northwest of the accident site included wind from 130° at 7 knots with gusts to 15 knots, few clouds at 5,000 ft above ground level, visibility 10 (statute) miles. 

Aircraft and Owner/Operator Information

Aircraft Make: Bell
Registration: N519P
Model/Series: OH 58A No Series
Aircraft Category: Helicopter
Amateur Built: No
Operator: St Johns County Sheriffs Office
Operating Certificate(s) Held:None  

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KCRG, 41 ft msl
Observation Time: 1753 EDT
Distance from Accident Site: 10 Nautical Miles
Temperature/Dew Point: 22°C / 14°C
Lowest Cloud Condition: Few / 5000 ft agl
Wind Speed/Gusts, Direction: 7 knots / 15 knots, 130°
Lowest Ceiling:
Visibility:  10 Miles
Altimeter Setting: 30.19 inches Hg
Type of Flight Plan Filed: Company VFR
Departure Point: Ponte Vedra Bch, FL
Destination: St Augustine, FL (SGJ)

Wreckage and Impact Information

Crew Injuries: 2 None
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 2 None
Latitude, Longitude:  30.206111, -81.403333 (est)

Piper PA-28R-200, N33305: Accident occurred March 13, 2019 in Easton, Talbot County, Maryland -and- Incident occurred March 29, 2018 at Lee Airport (KANP), Edgewater, Anne Arundel County, Maryland








Aviation Accident Final Report - National Transportation Safety Board 

Additional Participating Entity: 
Federal Aviation Administration / Flight Standards District Office; Baltimore, Maryland

Investigation Docket - National Transportation Safety Board:

Aquila Aviation LLC


Location: Easton, Maryland 
Accident Number: ERA19LA160
Date & Time: March 13, 2019, 17:40 Local
Registration: N33305
Aircraft: Piper PA28R 
Aircraft Damage: Substantial
Defining Event: Loss of engine power (total) 
Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Instructional

Analysis

The flight instructor and pilot were on a flight to resume the pilot's instrument training. After performing maneuvers and several touch-and-go landings, the pilots elected to perform a practice instrument approach to the destination airport. While on the approach, they configured the airplane for landing. The flight instructor noted that the airplane was below the glideslope and asked the pilot to increase engine power; however, the engine did not respond to the throttle input. The flight instructor took the controls and attempted to restore engine power without success. The propeller continued to windmill, the pilot switched fuel tanks, and the engine did not restart. The flight instructor performed a forced landing in a nearby field, during which the fuselage was substantially damaged. During recovery from the field, fuel was drained from both fuel tanks, and no water or debris was noted in the fuel. An examination of the engine revealed crankshaft and valvetrain continuity throughout the engine. The propeller was rotated through 360° of motion, and compression and suction were noted on all cylinders. In addition, fuel was plumbed into the engine, and the engine was started and ran smoothly without hesitation. The engine power was decreased to idle power, and then the engine was shut down. There were no mechanical malfunctions or failures noted with the engine that would have precluded normal operation before the accident. The reason for the loss of engine power could not be determined.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The loss of engine power for reasons that could not be determined because postaccident engine examination and testing revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation.

Findings

Not determined (general) - Unknown/Not determined

Factual Information

On March 13, 2019, about 1740 eastern daylight time, a Piper PA-28R-200, N33305, was substantially damaged during a forced landing to a field near Easton, Maryland. The flight instructor and the private pilot were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the instructional flight that departed from the Cambridge-Dorchester Regional Airport (CGE), Cambridge, Maryland, about 1720. The flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91 and had an intended destination of Easton/Newnam Field (ESN), Easton, Maryland.

According to the flight instructor, the purpose of the flight was to reacquaint the pilot with the airplane and resume his instrument flight training. They departed Lee Airport (ANP), Annapolis, Maryland, about 1630, and flew to CGE and performed two landings. Then, they departed CGE and were cleared for the "ILS Rwy 4" approach with a circle to land clearance for runway 22 at ESN. While descending on the approach, they configured the airplane for landing by reducing engine power, moving the propeller control to the full forward position, setting the mixture to full rich, turning the electric fuel pump on, moving the landing gear selector to the down position, and extending the flaps "one notch." The airplane descended below the glideslope and the flight instructor told the pilot to add engine power, however, while advancing the throttle, the engine did not respond. The flight instructor took the controls and attempted to get the engine to respond without success. The propeller continued to windmill, the pilot switched the fuel tanks, and again, the engine did not restart. The flight instructor looked for a place to land and found a nearby field. They were about 1,000 ft mean sea level, so he extended the flaps, elected to retract the landing gear, and performed a forced landing to the muddy field. The airplane came to rest in the field, the two occupants turned "everything off" and egressed the airplane.

According to Federal Aviation Administration (FAA) airworthiness records, the airplane was manufactured in 1975. The airplane was equipped with a Lycoming IO-360-C1C, 200-horsepower engine. According to the engine maintenance logbook, the most recent annual inspection was completed on March 5, 2019, at 1,567.6 hours since major overhaul.

An examination of the wreckage by an FAA inspector revealed that a fuselage rib was substantially damaged during the accident sequence. Fuel was noted in both fuel tanks and during recovery was drained using the electric fuel pump, which pumped fuel into exterior containers. No water or contaminates were noted in the fuel. An examination of the fuel selector revealed that it moved
smoothly, and it could be clearly felt when the selector was in each respective detent.

Examination of the engine revealed that there was no damage to the crankcase. Crankshaft and valvetrain continuity were confirmed. Compression and suction were noted on all cylinders. The magneto timing was checked, the magnetos were sparked, and no anomalies were noted. The airbox was examined and not obstructed. Engine control cable continuity was confirmed from the propeller, mixture, and throttle control cables to their respective connections on the engine.

Later, the airplane was secured, fuel was plumbed into to the engine, and the engine was started. It ran smoothly, without hesitation, the engine power was decreased to idle power, and then the engine was shutdown. There were no anomalies noted with the engine.

History of Flight

Approach-circling (IFR) Loss of engine power (total) (Defining event)
Emergency descent Off-field or emergency landing
Landing-flare/touchdown Collision during takeoff/land

Flight instructor Information

Certificate: Commercial; Flight instructor; Private
Age: 29, Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied: Right
Other Aircraft Rating(s): None 
Restraint Used: 3-point
Instrument Rating(s): Airplane
Second Pilot Present: Yes
Instructor Rating(s): Airplane single-engine; Instrument airplane
Toxicology Performed: No
Medical Certification: Class 1 Without waivers/limitations
Last FAA Medical Exam: January 4, 2017
Occupational Pilot: Yes Last Flight Review or Equivalent: January 26, 2019
Flight Time: 855 hours (Total, all aircraft), 158 hours (Total, this make and model), 814 hours (Pilot In Command, all aircraft), 198 hours (Last 90 days, all aircraft), 67 hours (Last 30 days, all aircraft), 1 hours (Last 24 hours, all aircraft)

Pilot Information

Certificate: Commercial; Private
Age: 40, Male
Airplane Rating(s): Single-engine land 
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: 3-point
Instrument Rating(s): Airplane 
Second Pilot Present: Yes
Instructor Rating(s): None 
Toxicology Performed: No
Medical Certification: Class 1 With waivers/limitations
Last FAA Medical Exam: July 24, 2017
Occupational Pilot: No
Last Flight Review or Equivalent: October 26, 2018
Flight Time: 263 hours (Total, all aircraft), 21 hours (Total, this make and model), 190 hours (Pilot In Command, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Piper 
Registration: N33305
Model/Series: PA28R 200
Aircraft Category: Airplane
Year of Manufacture: 1975 
Amateur Built: No
Airworthiness Certificate: Normal 
Serial Number: 28R-7535131
Landing Gear Type: Retractable - Tricycle 
Seats: 4
Date/Type of Last Inspection: March 5, 2019 Annual 
Certified Max Gross Wt.: 2650 lbs
Time Since Last Inspection: 
Engines: 1 Reciprocating
Airframe Total Time: 4537.6 Hrs as of last inspection
Engine Manufacturer: Lycoming
ELT: Installed, not activated 
Engine Model/Series: IO-360-C1C
Registered Owner:
Rated Power: 200
Operator: 
Operating Certificate(s) Held: Pilot school (141)

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC)
Condition of Light: Day
Observation Facility, Elevation: ESN,72 ft msl 
Distance from Accident Site: 2 Nautical Miles
Observation Time: 17:57 Local
Direction from Accident Site: 31°
Lowest Cloud Condition:
Visibility:  10 miles
Lowest Ceiling: Broken / 6000 ft AGL
Visibility (RVR):
Wind Speed/Gusts: 8 knots / 
Turbulence Type Forecast/Actual:  /
Wind Direction: 160° 
Turbulence Severity Forecast/Actual:  /
Altimeter Setting: 30.3 inches Hg
Temperature/Dew Point: 13°C / -2°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Cambridge, MD (CGE)
Type of Flight Plan Filed: None
Destination: Easton, MD (ESN) 
Type of Clearance: None
Departure Time: 17:20 Local 
Type of Airspace: 

Airport Information

Airport: Easton/Newnam Field ESN
Runway Surface Type: Asphalt
Airport Elevation: 72 ft msl
Runway Surface Condition: Vegetation
Runway Used: 04
IFR Approach: ILS
Runway Length/Width: 5500 ft / 100 ft 
VFR Approach/Landing: Forced landing

Wreckage and Impact Information

Crew Injuries: 2 None 
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: N/A 
Aircraft Explosion: None
Total Injuries: 2 None 
Latitude, Longitude: 38.779724,-76.088058(est)

March 29, 2018: Aircraft landed gear up.

Date: 29-MAR-18
Time: 20:13:00Z
Regis#: N33305
Aircraft Make: PIPER
Aircraft Model: PA 28R 200
Event Type: INCIDENT
Highest Injury: UNKNOWN
Aircraft Missing: No
Damage: UNKNOWN
Activity: UNKNOWN
Flight Phase: LANDING (LDG)
Operation: 91
City: ANNAPOLIS
State: MARYLAND

Loss of Control on Ground: Cessna 182D Skylane, N8905X; accident occurred March 13, 2019 near Transylvania Community Airport (3NR3), Brevard, North Carolina















Aviation Accident Final Report - National Transportation Safety Board 

The National Transportation Safety Board did not travel to the scene of this accident.

Additional Participating Entity:

Federal Aviation Administration / Flight Standards District Office; Charlotte, North Carolina

Investigation Docket - National Transportation Safety Board:


Location: Brevard, North Carolina 
Accident Number: ERA19LA131
Date & Time: March 13, 2019, 18:10 Local
Registration: N8905X
Aircraft: Cessna 182
Aircraft Damage: Substantial
Defining Event: Loss of control on ground 
Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis

The pilot performed a preflight inspection after the airplane had undergone maintenance and no anomalies were noted. He boarded the airplane, adjusted the seat, and then verified that it was locked in position. Shortly after beginning the takeoff roll, his seat slid backward. He was unable to reach the rudder pedals, and the airplane departed the left side of the runway, nosed over, and came to rest inverted. Examination revealed that the pilot seat’s left front roller housing was disengaged from the seat rail. The seat rail exhibited scoring on top of the rail, which likely occurred during the accident sequence. No scoring was noted on the sides of the rail. The roller housing was not splayed or damaged, indicating that it did not pull off the rail during the accident sequence. Although the seat rail holes were slightly worn, the pin did not exhibit any anomalies.

The mechanic stated that he did not remove the pilot's seat to perform the maintenance that he completed before the accident flight; however, given the lack of side damage to the rails and the fact that the left front seat roller housing was not splayed, it is likely that the roller housing came off the rails during the maintenance and went unnoticed by both the mechanic and the pilot, which resulted in the seat sliding backward during takeoff.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The mechanic's failure to notice that the left front seat left front roller housing disengaged from the seat rail during recent maintenance, and the pilot's failure to detect the disengaged roller housing during the preflight inspection, which resulted in the seat sliding backward during takeoff and a subsequent loss of airplane directional control.

Findings

Personnel issues Replacement - Maintenance personnel
Personnel issues Preflight inspection - Pilot
Aircraft Seat/cargo attach fitting - Incorrect service/maintenance
Aircraft Directional control - Attain/maintain not possible
Personnel issues Aircraft control - Pilot

Factual Information

On March 13, 2019, about 1810 eastern daylight time, a Cessna 182D, N8905X, was substantially damaged after it impacted terrain during takeoff from Transylvania Community Airport (3NR3), Brevard, North Carolina. The private pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight, which was originating at the time of the accident. The
flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91.

According to the pilot, he completed a preflight inspection with no anomalies noted. When he boarded the airplane, the pilot seat was in its aft most position, since that was how he would typically exit the airplane. The pilot then slid the seat forward until he "could see 3 holes" in the rail, which was his typical seating position. He then "rocked the seat back and forth" to verify it was locked in position, and then proceeded to start the engine, taxi, and perform an engine runup. He then taxied onto the runway and began the takeoff roll. About 4-5 seconds into the takeoff roll, his seat slid backwards. At that point, he was unable to reach the rudder pedals, and the airplane departed the left side of the runway, nosed over, and came to rest inverted.

According to a Federal Aviation Administration (FAA) inspector who responded to the accident location, the airplane sustained substantial damage to the wings and fuselage.

According to FAA airworthiness records, the airplane was manufactured in 1961 and registered to the pilot in January 2019. The airplane's most recent annual inspection was completed on August 18, 2018, at a total time of 4,251.8 hours. In addition, the annual inspection maintenance log entry indicated that an inspection in accordance with airworthiness directive (AD) 2011-10-09, associated with a seat rail inspection, had been completed. At the time of the accident, the airplane had accumulated 4,265 total hours.

In an interview with the FAA inspector, a mechanic was working on the airplane the day before the accident to replace the transponder. He stated that sometimes he does have to remove the front seats to perform the work, however, he did not have the left front seat out of the airplane during the maintenance work, he only had the right front seat out of the airplane.

An examination of the left front seat rails revealed that the housings remained engaged on the seat rails except the left forward roller housing, which was disengaged from the seat rail. The housing tangs were not worn, distorted, or splayed. The pin that engaged into the track had no anomalies, the pin spring had positive engaging forces, and the holes were slightly worn. The seat rail was not damaged along the sides of the rail; however, the top of the rail had scoring marks.

According to the airplane owner's manual, the before engine start checklist stated, "Adjust seat to a comfortable position, check to see the seat locking mechanism is secure, and fasten safety belt."

History of Flight

Takeoff Miscellaneous/other
Takeoff Loss of control on ground (Defining event)

Pilot Information

Certificate: Private 
Age: 60, Male
Airplane Rating(s): Single-engine land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Unknown
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 3 With waivers/limitations 
Last FAA Medical Exam: July 6, 2017
Occupational Pilot: No
Last Flight Review or Equivalent: April 18, 2018
Flight Time: 294 hours (Total, all aircraft), 294 hours (Total, this make and model), 240 hours (Pilot In Command, all aircraft), 14 hours (Last 90 days, all aircraft), 1 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Cessna 
Registration: N8905X
Model/Series: 182 D 
Aircraft Category: Airplane
Year of Manufacture: 1961
Amateur Built: No
Airworthiness Certificate: Normal 
Serial Number: 18253305
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection: August 18, 2018 Annual
Certified Max Gross Wt.: 2348 lbs
Time Since Last Inspection: 13 Hrs
Engines: 1 Reciprocating
Airframe Total Time: 4265 Hrs at time of accident
Engine Manufacturer: Continental
ELT: Installed, activated, did not aid in locating accident
Engine Model/Series: O-470 SERIES
Registered Owner:
Rated Power: 230 Horsepower
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC)
Condition of Light: Day
Observation Facility, Elevation: AVL,2162 ft msl 
Distance from Accident Site: 11 Nautical Miles
Observation Time: 17:54 Local 
Direction from Accident Site: 45°
Lowest Cloud Condition: Clear 
Visibility: 10 miles
Lowest Ceiling: None 
Visibility (RVR): 
Wind Speed/Gusts: 8 knots / 
Turbulence Type Forecast/Actual:  /
Wind Direction: 140° 
Turbulence Severity Forecast/Actual: /
Altimeter Setting: 30.21 inches Hg 
Temperature/Dew Point: 14°C / 0°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Brevard, NC (3NR3) 
Type of Flight Plan Filed: None
Destination: Asheville, NC (AVL) 
Type of Clearance: None
Departure Time: 18:10 Local
Type of Airspace: Class G

Airport Information

Airport: Transylvania Community 3NR3 
Runway Surface Type: Asphalt
Airport Elevation: 2110 ft msl
Runway Surface Condition: Dry
Runway Used: 27 IFR 
Approach: None
Runway Length/Width: 2903 ft / 50 ft
VFR Approach/Landing: None

Wreckage and Impact Information

Crew Injuries: 1 None 
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None 
Latitude, Longitude: 35.269721,-82.643608(est)

Location: Brevard, NC
Accident Number: ERA19LA131
Date & Time: 03/13/2019, 1810 EDT
Registration: N8905X
Aircraft: Cessna 182
Injuries: 1 Minor
Flight Conducted Under: Part 91: General Aviation - Personal 

On March 13, 2019, about 1810 eastern daylight time, a Cessna 182D, N8905X, was substantially damaged after it impacted terrain during takeoff from Transylvania Community Airport (3NR3), Brevard, North Carolina. The private pilot incurred minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight, which was originating at the time of the accident. The flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91.

According to the pilot, he completed a preflight inspection with no anomalies noted. When he boarded the airplane, the pilot seat was in its aft most position, since that was how he would typically exit the airplane. The pilot then slid the seat forward until he "could see 3 holes" in the rail, which was his typical seating position. He then "rocked the seat back and forth" to verify it was locked in position, and then proceeded to start the engine, taxi, and perform an engine runup. He then taxied onto the runway and began the takeoff roll. About 4-5 seconds into the takeoff roll, his seat slid backwards. At that point, he was unable to reach the rudder pedals, and the airplane departed the left side of the runway, nosed over, and came to rest inverted.

According to a Federal Aviation Administration (FAA) inspector who responded to the accident location, the airplane sustained substantial damage to the wings and fuselage.

According to FAA records, the airplane was manufactured in 1961 and registered to the pilot in January 2019. The airplane's most recent annual inspection was completed on August 18, 2018. In addition, the annual inspection maintenance log entry indicated that the inspection an inspection in accordance with airworthiness directive (AD) 2011-10-09 had been completed.

The airplane was retained for further examination.

Aircraft and Owner/Operator Information

Aircraft Make: Cessna
Registration: N8905X
Model/Series: 182 D
Aircraft Category: Airplane
Amateur Built: No
Operator: Paul B Greene
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: AVL
Observation Time: 1754 EDT
Distance from Accident Site: 11 Nautical Miles
Temperature/Dew Point: 14°C / 0°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: 8 knots / , 140°
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 30.22 inches Hg
Type of Flight Plan Filed: Unknown
Departure Point: Brevard, NC (3NR3)
Destination:

Wreckage and Impact Information

Crew Injuries: 1 Minor
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 Minor
Latitude, Longitude:  35.269722, -82.643611 (est)

Runway Incursion - Aircraft: North American T-28B Trojan, N5440F and Cessna 152, N48962; fatal accident occurred March 13, 2019 at Compton-Woodley Airport (KCPM), Los Angeles County, California

Lukas Michael Swidzinski
~

Lukas Swidzinski, piano
~


Aviation Accident Final Report - National Transportation Safety Board

The National Transportation Safety Board traveled to the scene of this accident.

Additional Participating Entity: 

Federal Aviation Administration / Flight Standards District Office; Los Angeles, California

Investigation Docket - National Transportation Safety Board: 

Tomorrow's Aeronautical Museum


Long Beach Flying Club

Candace A Larned Enterprises LLC


Location: Compton, California
Accident Number: WPR19FA095
Date and Time: March 13, 2019, 18:50 Local
Registration: N5440F (A1); N48962 (A2)
Aircraft: North American T28 (A1); Cessna 152 (A2)
Aircraft Damage: Minor (A1); Destroyed (A2)
Defining Event: Runway incursion veh/AC/person
Injuries: 1 None (A1); 1 Fatal, 1 Serious (A2)
Flight Conducted Under: Part 91: General aviation - Personal (A1); Part 91: General aviation - Instructional (A2)

Analysis

The student pilot and flight instructor in the Cessna were landing at the non-tower-controlled airport when a North American T-28 collided with the Cessna from behind, fatally injuring the student. Radar data indicated that the T-28 overflew the airport before joining the downwind leg of the traffic pattern for the landing runway; about this time, the Cessna was on final approach. The pilot of the T-28 reported that the bright sun and the haze created a glare on the windscreen that obscured his forward vision, making it difficult for him to see directly ahead, and the glare became worse as he descended toward the runway on final approach. The T-28 pilot saw the Cessna ahead of him on the runway just before the collision occurred.

The instructor onboard the Cessna could not recall the details of the flight but reported that his student would have made radio calls on the airport's common traffic advisory frequency (CTAF) as they approached the airport for landing. The CTAF was not recorded, and the radio frequency settings of the Cessna could not be determined due to thermal damage. Examination of the T-28 revealed that its radio was not tuned to the airport's CTAF; therefore, the T-28 pilot was neither receiving position reports from other aircraft in the traffic pattern, nor was he broadcasting his position. The circumstances of the accident are consistent with the T-28 pilot's failure to see and avoid the Cessna while landing with reduced visibility due to sun glare, and it is likely that his failure to monitor and use the CTAF contributed to the accident.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The failure of the T-28 pilot to see and avoid the Cessna while landing with reduced visibility due to sun glare, which resulted in a collision on the runway. Contributing to the accident was his failure to use the airport's common traffic advisory frequency during the approach and landing.

Findings

Personnel issues (A1) Monitoring communications - Pilot
Environmental issues (A1) Bright light - Contributed to outcome
Personnel issues (A1) Monitoring other aircraft - Pilot
Environmental issues (A1) Glare - Effect on personnel
Personnel issues (A2) Attention - Pilot of other aircraft

Factual Information

History of Flight

Landing-landing roll (A1) Runway incursion veh/AC/person (Defining event)
Landing-landing roll (A2) Runway incursion veh/AC/person

On March 13, 2019, about 1850 Pacific daylight time, a Cessna 152 airplane, N48962, and a North American T-28 Trojan (T-28), N5440F, were involved in an accident near Compton, California. The T28 sustained substantial damage and the airline transport pilot onboard was not injured. The student pilot onboard the Cessna was fatally injured, and the flight instructor sustained serious injuries; the airplane was destroyed. The T-28 was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight; the Cessna was operated as a Title 14 CFR Part 91 instructional flight.

Review of radar data revealed two discrete secondary beacon code targets that were correlated to the two airplanes as they approached Compton/Woodley Airport (CPM); the Cessna from the south-southwest and the T-28 from the north/east. (See figure 1.) The instructor onboard the Cessna stated that he and the student were simulating a diversion to CPM. He was seriously injured during the accident and could not recall the details of the flight but stated that the student would have made all radio calls over the airport's common radio frequency. Radar indicated that the Cessna entered the airport traffic pattern on the downwind leg at an altitude about 950 ft above ground level (agl), then proceeded to fly the base and final legs of the traffic pattern for runway 25 left (25L). 

The T-28 pilot stated that he was returning the airplane to CPM following maintenance. As he approached the area at an altitude about 1,000 ft above ground level (agl), he began to become concerned, because the haze was extreme and the sun was low and bright, obscuring his forward vision. He was initially unable to find CPM but located an open area without buildings and thought that was likely the airport, which he confirmed as he got closer. In an effort to announce his presence at the airport, he overflew the runway from the southeast, crossing midfield then making left descending turns into the left traffic pattern for runway 25.

Radar data indicated that the T-28 approached CPM from the east, overflew the airport about 700 to 750 ft agl, then entered the left downwind leg of the traffic pattern for runway 25L. (See figure 2.)

The T-28 pilot stated that as he turned from the base to final legs, the bright sun and the haze created a glare on the windscreen that obscured his forward vision, making it difficult for him to see directly ahead. As he descended toward the runway, the glare became worse and he realized he was between runways 25L and 25R. He side-stepped to runway 25L and the airplane touched down on the runway surface. Several seconds later, the pilot saw the Cessna on the runway ahead of him. He applied hard braking and felt the impact with the other plane and resulting explosion immediately thereafter. The T28 continued about 1,000 ft before coming to rest off the right side of runway 25L. (See figure 3.)

Multiple video recordings captured the accident (see figure 4); review of the footage revealed that the Cessna touched down on runway 25L and continued its landing roll. The T-28 crossed the runway threshold about 10 seconds after the Cessna and subsequently touched down about 1850:36. On the landing roll, adjacent to the runway halfway point sign, the T-28 impacted the Cessna.

Pilot Information (A1)

Certificate: Airline transport; Commercial; Flight engineer; Flight instructor; Military 
Age: 84,Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied: Front
Other Aircraft Rating(s): None 
Restraint Used: 4-point
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s): Airplane single-engine
Toxicology Performed: No
Medical Certification: Class 3 With waivers/limitations 
Last FAA Medical Exam: December 5, 2018
Occupational Pilot: No 
Last Flight Review or Equivalent: March 15, 2017
Flight Time: 24000 hours (Total, all aircraft), 400 hours (Total, this make and model), 18000 hours (Pilot In Command, all aircraft), 3 hours (Last 90 days, all aircraft), 1 hours (Last 30 days, all aircraft), 1 hours (Last 24 hours, all aircraft)

Flight instructor Information (A2)

Certificate: Airline transport; Commercial; Flight instructor
Age: 34,Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied: Right
Other Aircraft Rating(s): None
Restraint Used: Unknown
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s): Airplane multi-engine; Airplane single-engine; Instrument airplane
Toxicology Performed: No
Medical Certification: Class 1 Without waivers/limitations
Last FAA Medical Exam: August 3, 2018
Occupational Pilot: Yes 
Last Flight Review or Equivalent:
Flight Time: (Estimated) 9542 hours (Total, all aircraft), 1674 hours (Total, this make and model), 9402 hours (Pilot In Command, all aircraft), 107 hours (Last 90 days, all aircraft), 55 hours (Last 30 days, all aircraft), 1 hours (Last 24 hours, all aircraft)

Student pilot Information (A2)

Certificate: Student
Age: 40, Male
Airplane Rating(s): None 
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Unknown
Instrument Rating(s): None 
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: Yes
Medical Certification: Class 1 With waivers/limitations
Last FAA Medical Exam: November 7, 2018
Occupational Pilot: No
Last Flight Review or Equivalent:
Flight Time: (Estimated) 22 hours (Total, all aircraft), 22 hours (Total, this make and model), 1 hours (Pilot In Command, all aircraft), 15 hours (Last 90 days, all aircraft), 5 hours (Last 30 days, all aircraft), 1 hours (Last 24 hours, all aircraft)

T-28 Pilot (A-1)

The 84-year-old pilot was issued a third-class special issuance Federal Aviation Administration (FAA) airman medical certificate with a limitation for glasses for near vision. On his most recent medical exam, his color vision and field of vision were normal, and his uncorrected distant vision was 20/30. At his November 2017 ophthalmology examination, the pilot was diagnosed with age-related cataracts that had both a nuclear and cortical component. He was noted to wear eyeglasses with prism correction, and his uncorrected distant vision was 20/30 in each eye. An ophthalmology exam on October 2019 found a worsening of his cataracts and distant vision.

Review of the pilot’s uncorrected vision results from exams spanning over thirty years for first or second-class medical certification showed some gradual decrement of distant vision with aging, which required him to wear corrective lenses when flying.

The T-28 pilot stated that he used his “Flight Guide” book for determining airport frequencies. Examination of the actual guide found at the airplane revealed that the page for CPM was missing; a paper note in place of the page read, “Pg 34, Aug 2017 Compton a/d removed.” 

Aircraft and Owner/Operator Information (A1)

Aircraft Make: North American
Registration: N5440F
Model/Series: T28 B 
Aircraft Category: Airplane
Year of Manufacture: 1956 
Amateur Built: No
Airworthiness Certificate: Experimental (Special)
Serial Number: 138294
Landing Gear Type: Retractable - Tricycle
Seats: 2
Date/Type of Last Inspection: Unknown
Certified Max Gross Wt.: 850 lbs
Time Since Last Inspection: 
Engines: 1 Reciprocating
Airframe Total Time:
Engine Manufacturer: Wright
ELT: Installed Engine Model/Series: R-1820-86B
Registered Owner: Rated Power: 1475 Horsepower
Operator: Operating Certificate(s)
Held: None

Aircraft and Owner/Operator Information (A2)

Aircraft Make: Cessna
Registration: N48962
Model/Series: 152 No Series
Aircraft Category: Airplane
Year of Manufacture: 1977
Amateur Built: No
Airworthiness Certificate: Normal 
Serial Number: 15281075
Landing Gear Type: Tricycle 
Seats: 2
Date/Type of Last Inspection: February 20, 2019 100 hour
Certified Max Gross Wt.: 1675 lbs
Time Since Last Inspection: 68 Hrs
Engines: 1 Reciprocating
Airframe Total Time: 20105 Hrs at time of accident
Engine Manufacturer: Lycoming
ELT: Installed, activated, did not aid in locating accident
Engine Model/Series: O-235-L2C
Registered Owner: 
Rated Power:
Operator:
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC) 
Condition of Light: Day
Observation Facility, Elevation: KHHR,63 ft msl
Distance from Accident Site: 5 Nautical Miles
Observation Time: 01:53 Local 
Direction from Accident Site: 293°
Lowest Cloud Condition: Clear
Visibility:  10 miles
Lowest Ceiling: None 
Visibility (RVR):
Wind Speed/Gusts: 11 knots / 16 knots
Turbulence Type Forecast/Actual:  /
Wind Direction: 270°
Turbulence Severity Forecast/Actual:  /
Altimeter Setting: 30.02 inches Hg 
Temperature/Dew Point: 17°C / 0°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Los Angeles, CA (WHP) (A1); Long Beach, CA (LGB) (A2)
Type of Flight Plan Filed: None (A1); None (A2)
Destination: Compton, CA (CPM) (A1); Long Beach, CA (LGB) (A2)
Type of Clearance: None (A1); None (A2)
Departure Time: 18:30 Local (A1); 18:30 Local (A2)
Type of Airspace:
The time of sunset was 1859:24. 

The sun’s azimuth at the time of the accident was 267° (see figure 5) and the elevation was slightly above the horizon at 0.50°. 


Airport Information

Airport: Compton/Woodley CPM 
Runway Surface Type: Asphalt
Airport Elevation: 98 ft msl
Runway Surface Condition: Dry
Runway Used: 25L 
IFR Approach: None
Runway Length/Width: 3322 ft / 60 ft 
VFR Approach/Landing: Traffic pattern

Wreckage and Impact Information (A1)

Crew Injuries: 1 None
Aircraft Damage: Minor
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: 
Aircraft Explosion: None
Total Injuries: 1 None 
Latitude, Longitude: 33.889446,-118.24083

Wreckage and Impact Information (A2)

Crew Injuries: 1 Fatal, 1 Serious
Aircraft Damage: Destroyed
Passenger Injuries:
Aircraft Fire: On-ground
Ground Injuries: 
Aircraft Explosion: On-ground
Total Injuries: 1 Fatal, 1 Serious 
Latitude, Longitude: 33.889446,-118.24083

The Cessna came to rest on the north side of runway 25L, about 150 ft west of the left outboard wing. The T-28 was 450 ft further west of the Cessna. The marks on runway revealed no indications of braking by the T-28 before the collision.

Additional Information

FAA Advisory Circular (AC) 90-66B, Non-Towered Airport Flight Operations, recommends that:

All traffic within a 10-mile radius of a non-towered airport or a part-time-towered airport when the control tower is not operating should continuously monitor and communicate, as appropriate, on the designated CTAF until leaving the area or until clear of the movement area. After first monitoring the frequency for other traffic present passing within 10 miles from the airport, self-announcing of your position and intentions should occur between 8 and 10 miles from the airport upon arrival. Departing aircraft should continuously monitor/communicate on the appropriate frequency from startup, during taxi, and until 10 miles from the airport, unless 14 CFR or local procedures require otherwise.

Communications

Neither pilot was in contact with an air traffic control facility, nor were they required to be. CPM's common traffic advisory frequency (CTAF) was not recorded.

The Cessna's radio settings could not be determined due to thermal damage. The T-28 was equipped with a Garmin GTR SL40 communications radio, located immediately below a Garmin 327 transponder mounted to the bottom of the panel. When the electrical system was powered on following the accident, the active radio frequency was 125.00 and the standby frequency was 121.50. The CPM CTAF was 123.05. Commonly referred to as "GUARD," 121.5 MHz is reserved for emergency communications for aircraft in distress, as well as the frequency utilized by earlier generation emergency locator transmitters as a means of locating downed aircraft.

When positioned in the pilot's seat in the T-28, investigators noted that the radio frequencies were partially obscured from the pilot’s field of vision. While in a normal flying position, an investigator of similar height of the T-28 pilot could only see the bottom half of the displayed frequencies.

Preventing Similar Accidents

See and Be Seen

Adequate visual lookout while flying in visual meteorological conditions is critical to avoiding other aircraft. While accidents can occur in high-traffic areas (near airports), they can also occur in cruise flight.

All pilots can be vulnerable to distractions in the cockpit, and the presence of technology has introduced challenges to the see-and-avoid concept. Aviation applications on portable electronic devices (PEDs) such as cell phones, tablets, and handheld GPS units, while useful, can lead to more head-down time, limiting a pilot's ability to see other aircraft.

Pilots need to be vigilant and use proper techniques to methodically scan for traffic throughout your flight, not only in high-volume traffic areas. Dividing attention inside and outside the aircraft and minimizing distractions (including nonessential conversations, photography or sightseeing activities, and PED use) that may degrade the ability to maintain awareness of other aircraft are two strategies that can help improve traffic scans. Passengers can help look for traffic and, during instructional flights, one pilot should always be responsible for scanning for traffic.

Aircraft visible to other aircraft can be improved by turning on available lights, including anti-collision lights, and using high-intensity discharge or LED lighting.

Pilots should clearly communicate intentions and use standard phraseology, known distances, and obvious ground references to alert other pilots of their location.

Some conditions make it harder to see other aircraft, such as operating in areas where aircraft could be masked by surrounding terrain or buildings and when sun glare is present. Effective use of on-board traffic advisory systems, when available, can help pilots visually acquire and avoid other aircraft but is not a substitute for an outside visual scan.

See http://www.ntsb.gov/safety/safety-alerts/documents/SA_045.pdf for additional resources.

The NTSB presents this information to prevent recurrence of similar accidents. Note that this should not be considered guidance from the regulator, nor does this supersede existing FAA Regulations (FARs).










Location: Compton, CA
Accident Number: WPR19FA095A
Date & Time: 03/13/2019, 1855 PDT
Registration: N5440F
Aircraft: North American T28
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Personal 

On March 13, 2019, about 1855 Pacific daylight time, a Cessna 152 airplane, N48962, and a North American T-28 Trojan, N5440F, collided while landing on runway 25L at the Compton/Woodley Airport, Compton, California. The student onboard the Cessna was fatally injured and the flight instructor sustained serious injuries; the Cessna was destroyed after being consumed by fire. The Airline Transport Pilot onboard the T-28 was not injured; the T-28 sustained minor damage. The T-28 was operated by Tomorrow's Aeronautical Museum and the Cessna was operated by the Long Beach Flying Club. Both airplanes were being operated under Title 14 Code of Federal Regulations Part 91 as personal flights. Visual meteorological conditions prevailed, and no flight plan was filed for either flight. The Cessna departed for a local instructional flight from the Long Beach Airport, Long Beach, California at an unknown time. The T-28 departed for a local personal flight from Whiteman Airport, Los Angeles, California about 1830 with a planned destination of Compton.

There were multiple video recordings that captured the accident. A review of the footage revealed that the Cessna touched down and continued on the landing roll out. The T-28 crossed over the runway threshold bar about 10 seconds after the Cessna and subsequently touched down. On the landing roll, adjacent to the "1/2" sign (indicates half of the runway remains), the T-28 impacted the Cessna resulting in an explosion.


The T-28 pilot stated that as he turned the airplane left from the base leg to final approach in the traffic pattern for runway 25L, he noticed a layer of haze on the horizon. The bright sun and the haze created a glare on the windscreen that obscured his forward vision making it difficult for him to see directly ahead. As he descended toward the runway, the glare became worse and he realized he was in between runway 25L and 25R. He side-stepped to runway 25L and the airplane touched down on the runway surface. Several seconds later, the pilot observed the Cessna on the runway ahead of him. He felt the impact with the other airplane and resulting explosion immediately thereafter. The T-28 continued about 1,000 ft before coming to rest off the right side of 25L (see figure 01).



Figure 01: Wreckage Distribution

Utilizing the National Oceanographic and Atmospheric Administration (NOAA) sunrise/sunset calculator and solar position calculator, the time of sunset was 1859:24. The sun's azimuth at the time of the accident was 267° (see figure 02) and the elevation was 0.50° (about 90 ft above the horizon).

Figure 02: Solar Position 

Aircraft and Owner/Operator Information


Aircraft Make: North American

Registration: N5440F
Model/Series: T28 B
Aircraft Category: Airplane
Amateur Built: No
Operator:
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan


Conditions at Accident Site: Visual Conditions

Condition of Light: Day
Observation Facility, Elevation: KHHR, 63 ft msl
Observation Time: 0153 UTC
Distance from Accident Site: 5 Nautical Miles
Temperature/Dew Point: 17°C / 0°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: 11 knots / 16 knots, 270°
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 30.02 inches Hg
Type of Flight Plan Filed: None
Departure Point: Los Angeles, CA (WHP)
Destination: Compton, CA (CPM)

Wreckage and Impact Information


Crew Injuries: 1 None

Aircraft Damage: Minor
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None
Latitude, Longitude: 33.889444, -118.240833


Location: Compton, CA
Accident Number: WPR19FA095B
Date & Time: 03/13/2019, 1855 PDT
Registration: N48962
Aircraft: Cessna 152
Injuries: 1 Fatal, 1 Serious
Flight Conducted Under: Part 91: General Aviation - Instructional 

On March 13, 2019, about 1855 Pacific daylight time, a Cessna 152 airplane, N48962, and a North American T-28 Trojan, N5440F, collided while landing on runway 25L at the Compton/Woodley Airport, Compton, California. The student onboard the Cessna was fatally injured and the flight instructor sustained serious injuries; the Cessna was destroyed after being consumed by fire. The Airline Transport Pilot onboard the T-28 was not injured; the T-28 sustained minor damage. The T-28 was operated by Tomorrow's Aeronautical Museum and the Cessna was operated by the Long Beach Flying Club. Both airplanes were being operated under Title 14 Code of Federal Regulations Part 91 as personal flights. Visual meteorological conditions prevailed, and no flight plan was filed for either flight. The Cessna departed for a local instructional flight from the Long Beach Airport, Long Beach, California at an unknown time. The T-28 departed for a local personal flight from Whiteman Airport, Los Angeles, California about 1830 with a planned destination of Compton.

There were multiple video recordings that captured the accident. A review of the footage revealed that the Cessna touched down and continued on the landing roll out. The T-28 crossed over the runway threshold bar about 10 seconds after the Cessna and subsequently touched down. On the landing roll, adjacent to the "1/2" sign (indicates half of the runway remains), the T-28 impacted the Cessna resulting in an explosion.

The T-28 pilot stated that as he turned the airplane left from the base leg to final approach in the traffic pattern for runway 25L, he noticed a layer of haze on the horizon. The bright sun and the haze created a glare on the windscreen that obscured his forward vision making it difficult for him to see directly ahead. As he descended toward the runway, the glare became worse and he realized he was in between runway 25L and 25R. He side-stepped to runway 25L and the airplane touched down on the runway surface. Several seconds later, the pilot observed the Cessna on the runway ahead of him. He felt the impact with the other airplane and resulting explosion immediately thereafter. The T-28 continued about 1,000 ft before coming to rest off the right side of 25L (see figure 01).


Figure 01: Wreckage Distribution

Utilizing the National Oceanographic and Atmospheric Administration (NOAA) sunrise/sunset calculator and solar position calculator, the time of sunset was 1859:24. The sun's azimuth at the time of the accident was 267° (see figure 02) and the elevation was 0.50° (about 90 ft above the horizon).

Figure 02: Solar Position 

Aircraft and Owner/Operator Information

Aircraft Make: Cessna

Registration: N48962
Model/Series: 152 No Series
Aircraft Category: Airplane
Amateur Built: No
Operator: Long Beach Flying Club
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan


Conditions at Accident Site: Visual Conditions

Condition of Light: Day
Observation Facility, Elevation: KHHR, 63 ft msl
Observation Time: 0153 UTC
Distance from Accident Site: 5 Nautical Miles
Temperature/Dew Point: 17°C / 0°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: 11 knots / 16 knots, 270°
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 30.02 inches Hg
Type of Flight Plan Filed: None
Departure Point: Long Beach, CA (LGB)
Destination:  Long Beach, CA (LGB)

Wreckage and Impact Information


Crew Injuries: 1 Fatal, 1 Serious

Aircraft Damage: Destroyed
Passenger Injuries: N/A
Aircraft Fire: On-Ground
Ground Injuries: N/A
Aircraft Explosion: On-Ground
Total Injuries: 1 Fatal, 1 Serious
Latitude, Longitude: 33.889444, -118.240833




Lukas, a friend, brother, son and mentor. 

Lukas has been fascinated with airplanes and had dreams to become a pilot himself. Unfortunately, last Wednesday Lukas and his flight instructor were involved in tragic plane accident and as a result Lukas did not survive. He was enthusiastic with everything he did in his life and he died doing one of the things he loved most. 

Lukas’ closest family, his mother Alicja and brother Mario, are making arrangements to come to the US from Europe to lay Lukas to rest. The funds raised here will help with funeral expenses, family’s travel expenses, and to be sure Lukas is taken care of and remembered well by the people he has touched throughout his life. 

There were many people that Lukas made an impact on in their lives, whether it was his students or people in the dive community, he was truly an amazing person. Lukas’ passion and talent for music inspired many young minds. Lukas was a kind and generous person who would do anything to help his friends. Lukas loved all animals and considered his cats family members. He had the most adventurous spirit, the biggest heart and the largest smile. From music, to motorcycles, to roller coasters, to scuba diving and flying Lukas lived his life with an enormous amount of enthusiasm.  He will be missed by family, friends, students and colleagues.  




Authorities Thursday identified a student pilot who was killed when two planes collided on a runway at Compton/Woodley Airport.

The crash occurred about 7 p.m. March 13 on Runway 25L on March 13, when a North American T-28B Trojan crashed into a Cessna 152 occupied by a flight instructor and a student pilot.

The fatally injured man was identified today by the coroner's office as 40-year-old Lukas Michael Swidinski of Long Beach.

"The Cessna landed first, trailed by the T28," Ian Gregor of the Federal Aviation Administration said in a statement. "The North American T-28B Trojan landed and ran into the Cessna 152, which was still on the runway, causing the Cessna 152 to explode. There were two people on the Cessna 152 and one on the North American T-28B Trojan."

The second man in the Cessna 152 was a flight instructor in his 30s. He was taken to a hospital in critical condition, the sheriff's department said.

The pilot of the North American T-28B Trojan was unhurt, according to the sheriff's department.

Personnel from the FAA and the National Transportation Safety Board were working to determine what caused the two planes to collide.

The North American T-28B Trojan is a military trainer first used by the U.S. Air Force and U.S. Navy in the 1950s, then was utilized as a counter-insurgency aircraft in the Vietnam War.

Anyone who may have witnessed the crash was asked to call the Los Angeles County Sheriff's Department's Aero Bureau at (562) 421-2701.


https://www.nbclosangeles.com




A flight instructor remained in critical condition Thursday after a fiery, two-plane crash at the Compton/Woodley Airport killed his student the previous evening.

The Los Angeles County Sheriff's Department described the surviving victim as a man in his 30s and the student as a man in his 40s. They were in a single-engine Cessna 152, which was struck by a single-engine North American T-28 on the runway around 7 p.m. Wednesday.

The pilot of the T-28 did not sustain any injuries in the incident, the Sheriff's Department said. That aircraft, which bears the U.S. Navy sign, appeared to be mostly intact as it sat at the airfield on Thursday morning.

Officials have yet to identify the three individuals involved.

The Cessna had just landed on the runway when the T-28 touched down and ran into it, causing the Cessna to explode, according to the Federal Aviation Administration.

"Like many general aviation airports, Compton does not have a control tower," FAA Public Affairs Manager Ian Gregor said. "Pilots communicate with each other on a common radio frequency."

The T-28 appeared to approach the Cessna from behind before landing on top of it, witnesses told KTLA on Wednesday night.

"It just sounded like the darnedest explosion you would imagine… I saw one of the airplanes involved in the crash dragging parts of the other airplane down the runway," pilot Billy Jackson said.

The Compton Fire Department responded to the scene and extinguished the blaze, the L.A. County Sheriff's Department said.

The FAA is helping the National Transportation Safety Board investigate the case.  The NTSB typically takes at least a year to determine what caused an incident, Gregor noted.

A 2015 crash at the county-owned Compton airport left a pilot dead when a single-engine plane that had been trying to tow an advertising banner crashed and burned on a runway, the Associated Press reported.

Story and video ➤ https://ktla.com














COMPTON, California (KABC) -- One person was killed when two small planes collided in a fiery crash at Compton/Woodley Airport Wednesday night. 

The crash was reported just before 7 p.m. It appeared to involve a vintage Vietnam-era T-28 aircraft and a small plane that appears to be a Cessna. 

The small plane was destroyed and burned up in the crash. One pilot was apparently ejected from one of the aircraft and killed. 

Pieces of the aircraft are littering the runway and the wing landed about 100 yards away from the main fuselage. 

Witnesses say it appeared the Cessna had already landed and was taxiing when the other pilot, possibly having trouble with the setting sun, also tried landing on the same runway and crashed into it. 

Firefighters and law enforcement officials were on the scene.  Paramedics transported another person from the scene in an ambulance. 

Story and video ➤https://abc7.com