Friday, August 4, 2017

Half Moon Bay Airport (KHAF) to be named in honor of Eddie Andreini

Edward August Andreini




Eddie Andreini is remembered as a man whose feet were firmly rooted in the Coastside soil. After growing up in a farm family, his construction company would help develop countless public and private projects on the coast. His head, however, was always in the clouds.

And it is his love of flying that will be the focus of ceremonies later this month to rename the airfield at Half Moon Bay Airport in his honor. The renaming is the work of the San Mateo County Public Works Department, which manages the airport, and comes with the full support of an army of Andreini fans all around the coast.

The county plans a ceremony to unveil the new name at 1 p.m. on Aug. 26 at the 3-Zero Café. The public is welcome to attend. Andreini was a regular at the café, which overlooks the airport’s landing strips.

After becoming enamored with flight by watching the local crop dusters, Andreini got his first airplane — a Piper Super Cruiser — at the age of 14. Over time, he would become an expert pilot with a particular love for vintage aircraft. He performed in World War II-era equipment like his Stearman biplane and his P-51 and Yak-9 fighters.

Coastsiders could often hear his aircraft as he practiced maneuvers that would quicken the pulse of any pilot. In 2013, he was inducted into the International Council of Air Shows Hall of Fame.

Andreini died a year later, at the age of 77, while performing maneuvers during an air show at Travis Air Force Base.

Air-show announcer Bill Vasilovich spoke of Andreini at his funeral. He described why the pilot was beloved by many in the community.

“He was a true gentleman, a barnstormer,” Vasilovich told the Review at the time. “He made people look up into the skies and smile.”

Story and comments ► http://www.hmbreview.com

Cessna 180, N9455C: Accident occurred August 01, 2017 in Puntilla, Alaska

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Anchorage, Alaska

Aviation Accident Factual Report - National Transportation Safety Board: https://app.ntsb.gov/pdf


Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms

http://registry.faa.gov/N9455C

Location: Puntilla, AK
Accident Number: GAA17CA473
Date & Time: 08/01/2017, 1900 AKD
Registration: N9455C
Aircraft: CESSNA 180
Aircraft Damage: Destroyed
Defining Event: Loss of control on ground
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Personal 

According to the pilot, he made two passes over a dry creek bed to assess a potential landing site. The second pass was accomplished up creek into rising terrain. The airplane was configured with full power, with flaps at 20° and flying about 50ft AGL and 80 MPH.

The pilot reported that the airplane encountered a downdraft as the airplane transitioned from overflying the trees, to overflying the creek bed, which he attempted to correct, but the airplane aerodynamically stalled.

Following the stall, the pilot attempted to land on a dry creek bed. The airplane touched down on the creek bed, then bounced and descended into a "dry cut channel". The airplane came to rest nose down and the airplane in a near vertical position. The airplane was destroyed by a post-crash fire.

According to the National Transportation Safety Board's, Pilot Aircraft Accident Report, the pilot reported that the event could have been avoided by making the low pass along descending terrain at a higher airspeed.

The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. 

Pilot Information

Certificate: Commercial
Age: 26, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Lap Only
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 3 Without Waivers/Limitations
Last FAA Medical Exam: 06/25/2015
Occupational Pilot: No
Last Flight Review or Equivalent: 06/03/2017
Flight Time:  (Estimated) 305 hours (Total, all aircraft), 70 hours (Total, this make and model), 277 hours (Pilot In Command, all aircraft), 55 hours (Last 90 days, all aircraft), 30 hours (Last 30 days, all aircraft), 2 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Manufacturer: CESSNA
Registration: N9455C
Model/Series: 180 UNDESIGNATED
Aircraft Category: Airplane
Year of Manufacture: 1955
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 31853
Landing Gear Type: Tailwheel
Seats: 4
Date/Type of Last Inspection: 09/03/2016, Annual
Certified Max Gross Wt.: 2550 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 2883 Hours as of last inspection
Engine Manufacturer: CONT MOTOR
ELT: Installed, not activated
Engine Model/Series: O-470J
Registered Owner: On file
Rated Power: 225 hp
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: KPTI, 1858 ft msl
Observation Time:
Distance from Accident Site: 13 Nautical Miles
Direction from Accident Site: 39°
Lowest Cloud Condition: Scattered
Temperature/Dew Point:
Lowest Ceiling:
Visibility:  
Wind Speed/Gusts, Direction: 
Visibility (RVR):
Altimeter Setting:
Visibility (RVV):
Precipitation and Obscuration:
Departure Point: Wasilla, AK (PAWS)
Type of Flight Plan Filed: None
Destination:
Type of Clearance: None
Departure Time: 1745 AKD
Type of Airspace: Class G 

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Destroyed
Passenger Injuries: N/A
Aircraft Fire: On-Ground
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None
Latitude, Longitude:  61.923611, -153.023611 (est)



ANCHORAGE, Alaska (KTUU) A pilot was rescued by the Alaska Air National guard after his plane crashed 130 miles northwest of Anchorage.

On the morning of August 3rd the pilot’s brother contacted the Alaska Rescue Coordination Center with concerns about his brothers expected return on Tuesday, August 1st.

According to a press release today aircraft wreckage was found within a few hours of the call in the area of Ptarmigan Pass. The pilot did not appear to have sustained serious injuries.

“The pilot was traveling with a satellite tracking device that can be used to send emergency messages via text and also sends a signal of the aircraft location periodically,” said Lt. Col. Scot Milani, director of the RCC. “The last known coordinates provided by his brother assisted in identifying a general area where the plane was when it last submitted a transmission.”

The Alaska Rescue Coordination Center along with support from the Alaska National Guard’s 176th Wing were able to spot the wreckage in mountainous terrain at about 3,000 feet in elevation.

The survivor was helped into a helicopter, treated at the Mat-Su Regional Medical Center, and later released.

“It’s important for pilots to have a plan—letting someone know where they are going, their planned route, when they plan to depart and return—and be packed with food, gear and shelter,” said Milani. “They should be equipped to spend an extended period of time surviving until rescue forces are able to locate them in the event of an emergency.”

http://www.ktuu.com

Robinson R44 II, N4138M, registered to and operated by Bering Air Inc: Accident occurred August 03, 2017 in Solomon, Alaska

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

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Anchorage, Alaska

Aviation Accident Preliminary Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

Bering Air Inc:   http://registry.faa.gov/N4138M

NTSB Identification: ANC17LA040
Nonscheduled 14 CFR Part 135: Air Taxi & Commuter
Accident occurred Thursday, August 03, 2017 in Solomon, AK
Aircraft: ROBINSON HELICOPTER COMPANY R44, registration: N4138M
Injuries: 2 Uninjured.

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. NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On August 3, 2017, about 1032 Alaska daylight time, a Robinson R-44 Clipper II helicopter, N4138M, impacted water and sank while dropping mineral claim markers about 1 mile south of Solomon, Alaska. The commercial pilot and passenger sustained no injury, and the helicopter sustained substantial damage. The helicopter was registered to, and operated by, Bering Air, Inc., Nome, Alaska, as a visual flight rules flight under the provisions of 14 Code of Federal Regulations (CFR) Part 135 on-demand charter flight. Visual meteorological conditions prevailed at the time of the accident, and company flight following procedures were in effect. The flight originated from the Nome Airport, Nome, about 0845. 

The pilot reported that the purpose of the flight was to place mineral claim markers, which involved maneuvering the helicopter over a Global Positioning System (GPS) point where the passenger can drop the marker from the rear left seat of the helicopter. Some of the mineral claim corners are in water, and the placement of those markers must be offset to the nearest land mass. The pilot departed from the Nome Airport and arrived at the passenger's private residence about 4 miles east of Nome. The helicopter was shutdown, the pilot briefed the flight to the passenger, 23 markers were loaded onboard the helicopter, and the helicopter departed. 

With about half the markers left to drop, the helicopter was operating over a lagoon between the mainland and a sand barrier, at about 10 to 15 feet above the water. The pilot reported that he was lower than he should have been and lost situational awareness when he was working with the GPS unit. He inadvertently allowed the helicopter to descend into the water "in a more level or slight nose low attitude" and the helicopter was not maneuvering at the time. He further reported that he must have pushed forward on the cyclic as he leaned forward to manipulate the GPS unit. After the helicopter impacted water, the helicopter rolled, and came to rest on its right side in about 4 feet of water. The pilot and passenger egressed without further incident and waded to the shore with the helicopter occupant survival bag and satellite phone. The pilot contacted the operator with the satellite phone and a second company helicopter was dispatched to pick up the pilot and passenger about 1200.

The helicopter sustained substantial damage to the main rotor system, the fuselage, the tail boom, and the tail rotor system.

The pilot reported that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. 


At the time of the accident, the helicopter was not equipped with a Federal Aviation Administration (FAA) approved radio altimeter or a FAA approved device that incorporates a radio altimeter as required by 14 CFR Part 135.160 Radio Altimeters for Rotorcraft Operations. The operator was operating with a Letter of Deviation Authority approved by the FAA.

Eurocopter AS-350B-3, N351SH, Soloy Helicopters LLC: Accident occurred August 03, 2017 in Delta Junction, Alaska

Aviation Accident Final Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

NTSB Identification: ANC17CA041 
Nonscheduled 14 CFR Part 135: Air Taxi & Commuter
Accident occurred Thursday, August 03, 2017 in Delta Junction, AK
Probable Cause Approval Date: 09/22/2017
Aircraft: AIRBUS AS350, registration: N351SH
Injuries: 2 Uninjured.

NTSB investigators used data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator and did not travel in support of this investigation to prepare this aircraft accident report.

The helicopter pilot reported that he was transporting a passenger to a remote drilling site where a tracked drilling unit was stationed. He reported that he landed into the wind, which necessitated descending over bordering trees into the drilling site. The helicopter touched down on the dirt, and upon lowering the collective, he reported that he heard a “bang,” and the helicopter slowly started to “pick up a ground wobble.” The pilot shut down the helicopter, and both occupants exited without further incident. 

A postaccident inspection revealed that the blue and red main rotor blades sustained substantial damage from impacting a black 1.5-inch steel frame attached to the tracked drilling unit, which is used to mount a canvas weather shelter for the drilling crews. The pilot reported that the steel frame was not visible to him from above as he was descending into the drilling site. The pilot further reported that he had made multiple landings at the drilling site in the past 3 months and that, with the previous landings, he had landed farther past the tracked drilling unit, and the steel frame was always behind the helicopter.

The pilot reported that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. 

The Federal Aviation Administration Helicopter Flying Handbook (FAA-H-8083-21A, 2012) discusses high and low reconnaissance procedures and states, in part:
The purpose of conducting a high reconnaissance is to determine direction and speed of the wind, a touchdown point, suitability of the landing area, approach and departure axes, and obstacles for both the approach and departure.

A low reconnaissance is accomplished during the approach to the landing area. When flying the approach, verify what was observed in the high reconnaissance, and check for anything new that may have been missed at a higher altitude, such as wires and their supporting structures (poles, towers, etc.), slopes, and small crevices.

The National Transportation Safety Board determines the probable cause(s) of this accident as follows:
The pilot’s failure to maintain clearance from a steel frame attached to a tracked drilling unit. Contributing to the accident was the pilot’s failure to visually identify the steel frame during the reconnaissance process. 

Additional Participating Entities:
Federal Aviation Administration / Flight Standards District Office; Fairbanks, Alaska
Bureau d’Enquêtes et d’Analyses; Paris
Airbus Helicopters (Technical Advisor); Grand Prairie, Texas
Safran Helicopter Engines (Technical Advisor); Grand Prairie, Texas

Aviation Accident Factual Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms

Operator: Soloy Helicopters LLC

Operator Does Business As: Soloy Helicopters LLC

http://registry.faa.gov/N351SH

NTSB Identification: ANC17CA041
Nonscheduled 14 CFR Part 135: Air Taxi & Commuter
Accident occurred Thursday, August 03, 2017 in Delta Junction, AK
Aircraft: AIRBUS AS350, registration: N351SH
Injuries: 2 Uninjured.

NTSB investigators used data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator and did not travel in support of this investigation to prepare this aircraft accident report.

The helicopter pilot reported that he was transporting a passenger to a remote drilling site, where a tracked drilling unit was stationed. He reported that he landed into the wind, which necessitated descending over bordering trees into the drilling site. The helicopter touched down on the dirt, and upon lowering the collective, he reported he heard a "bang" and the helicopter slowly started to "pick up a ground wobble." The pilot shutdown the helicopter and both occupants exited without further incident.

A postaccident inspection revealed that the blue and red main rotor blades sustained substantial damage from impacting a black 1.5-inch steel frame attached to the tracked drilling unit, which is used to mount a canvas weather shelter for the drilling crews. The pilot reported that the steel frame was not visible to him from above as he was descending into the drilling site. The pilot further reported that multiple landings have been made to the drilling site in the past 3 months, and that with the previous landings he landed further past the tracked drilling unit and the steel frame was always behind the helicopter.

The pilot reported that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. 

The Federal Aviation Administration Helicopter Flying Handbook (FAA-H-8083-21A, 2012) discusses high and low reconnaissance procedures and states in part:

The purpose of conducting a high reconnaissance is to determine direction and speed of the wind, a touchdown point, suitability of the landing area, approach and departure axes, and obstacles for both the approach and departure.

A low reconnaissance is accomplished during the approach to the landing area. When flying the approach, verify what was observed in the high reconnaissance, and check for anything new that may have been missed at a higher altitude, such as wires and their supporting structures (poles, towers, etc.), slopes, and small crevices.

Enstrom F-28F, N503PD, Airwest Aviation Academy LLC: Incident occurred August 03, 2017 in Lake Pleasant, Arizona

Airwest Aviation Academy LLC: http://registry.faa.gov/N503PD

Emergency landing.

Date: 03-AUG-17
Time: 20:45:00Z
Regis#: N503PD
Aircraft Make: ENSTROM
Aircraft Model: F28
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: UNKNOWN
Activity: INSTRUCTION
Flight Phase: EN ROUTE (ENR)
Operation: 91
City: LAKE PLEASANT
State: ARIZONA

Phoenix, Arizona 
September 30, 2014

PRELIMINARY INFORMATION FROM FEDERAL AVIATION ADMINISTRATION OPS: PHOENIX, AZ/UAS INCIDENT/1215P/N503PD, ENSTROM EN28, REPORTED A UAS (QUAD-COPTER) HOVERING 300 FEET BELOW WHILE ORBITING AT 1,600 FEET, 3 WNW PHX. NO CONFLICT REPORTED.

9/30/14 12:15 phoenix arizona prelim info from faa ops: phoenix, az/uas incident/1215p/n503pd, enstrom en28, reported a uas (quad-copter) hovering 300 feet below while orbiting at 1,600 feet, 3 wnw phx. no conflict reported.

Cessna 172S Skyhawk, N1129K, registered to American Airplane Exchange and operated by Orange County Flight Center: Accident occurred July 29, 2017 at John Wayne-Orange County Airport (KSNA), Santa Ana, Orange County, California

Aviation Accident Final Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

Location: Santa Ana, CA
Accident Number: GAA17CA479
Date & Time: 07/29/2017, 1030 PDT 
Registration: N1129K
Aircraft: CESSNA 172
Aircraft Damage: Substantial
Defining Event: Hard landing
Injuries: N/A
Flight Conducted Under: Part 91: General Aviation - Personal

Analysis 

The Federal Aviation Administration aviation safety inspector reported that, during a preflight inspection, the student pilot and designated pilot examiner observed propeller damage. Further inspection by maintenance personnel revealed substantial damage to the firewall and fuselage consistent with a hard landing. The airplane was flown by numerous renter pilots before the damage was found, and none of them claimed responsibility for the damage. The time of the accident and the identification of the pilot(s) are unknown. 

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
A hard landing and propeller strike for reasons that could not be determined based on the available evidence. 

Findings

Aircraft
Landing flare - Not attained/maintained (Cause)

Personnel issues
Aircraft control - Other/unknown (Cause)

Factual Information

History of Flight

Landing-flare/touchdown
Hard landing (Defining event)
Abnormal runway contact 

Aircraft and Owner/Operator Information

Aircraft Manufacturer: CESSNA
Registration: N1129K
Model/Series: 172 S
Aircraft Category: Airplane
Year of Manufacture: 2006
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 172S10315
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection: 03/30/2017, Annual
Certified Max Gross Wt.: 2300 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 4500 Hours
Engine Manufacturer: LYCOMING
ELT: Installed, not activated
Engine Model/Series: IO-360-L2A
Registered Owner: AMERICAN AIRPLANE EXCHANGE
Rated Power: 180 hp
Operator: Orange County Flight Center
Operating Certificate(s) Held: Pilot School (141) 

Meteorological Information and Flight Plan

Conditions at Accident Site: Unknown
Condition of Light: Not Reported
Observation Facility, Elevation:
Observation Time:
Distance from Accident Site:
Direction from Accident Site:
Lowest Cloud Condition:
Temperature/Dew Point:
Lowest Ceiling:
Visibility:  
Wind Speed/Gusts, Direction:
Visibility (RVR):
Altimeter Setting:
Visibility (RVV):
Precipitation and Obscuration:
Departure Point:  Unknown, UN (NONE)
Type of Flight Plan Filed: Unknown
Destination: Unknown, UN (NONE)
Type of Clearance: Unknown
Departure Time: 
Type of Airspace: Unknown

Wreckage and Impact Information

Crew Injuries: N/A
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: N/A
Latitude, Longitude: 33.675556, -117.868333 (est)

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Long Beach, California

Aviation Accident Factual Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms

Operator: Orange County Flight Center

American Airplane Exchange dba American Aircraft Sales

http://registry.faa.gov/N1129K


NTSB Identification: GAA17CA479
14 CFR Part 91: General Aviation
Accident occurred Saturday, July 29, 2017 in Santa Ana, CA
Aircraft: CESSNA 172, registration: N1129K
Injuries: Unavailable

NTSB investigators used data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator and did not travel in support of this investigation to prepare this aircraft accident report.

The Federal Aviation Administration Aviation Safety Inspector reported that, during a preflight inspection, the student pilot and designated pilot examiner observed propeller damage during their preflight inspection. Subsequently, a further inspection by maintenance personnel revealed substantial damage to the firewall and fuselage. The airplane was flown by numerous renter pilots prior to the damage being found, and none of them claimed responsibility for the damage.

Beech D17S Staggerwing, N44562: Accident occurred August 03, 2017 at Colorado Springs Airport (KCOS), El Paso County, Colorado

Aviation Accident Final Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

NTSB Identification: CEN17LA301
14 CFR Part 91: General Aviation
Accident occurred Thursday, August 03, 2017 in Colorado Springs, CO
Probable Cause Approval Date: 11/14/2017
Aircraft: BEECH D17S, registration: N44562
Injuries: 2 Uninjured.

NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

The airline transport pilot was landing in the tailwheel-equipped airplane in right quartering tailwind conditions. After touchdown, with the tailwheel on the runway, the airplane drifted to the right and the pilot applied left brake. The right landing gear collapsed, and the airplane ground looped and came to rest upright near the right edge of the runway. The pilot stated there were no mechanical malfunctions with the airplane, and that, "it got away from me, I guess."

The National Transportation Safety Board determines the probable cause(s) of this accident as follows:
The pilot's failure to maintain directional control during the landing roll with a quartering tailwind.

On August 3, 2017, about 1130 mountain daylight time, a Beech D17S airplane, N44562, ground looped during landing at City of Colorado Springs Municipal Airport (COS), Colorado Springs, Colorado. The pilot and one passenger were not injured and the airplane sustained substantial damage. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident and no flight plan had been filed. The flight departed Gallup Municipal Airport (GUP), Gallup, New Mexico, about 0900. 

The pilot stated during landing the right quartering tailwind was 10 to 13 mph. He made a normal landing with a lot of left rudder application to keep the airplane straight. After touchdown, with the tailwheel on the runway, the airplane drifted to the right and he applied left brake. The right landing gear collapsed and the airplane continued to the right edge of the runway where it came to rest upright. The pilot stated there were no mechanical malfunctions with the airplane and that "it got away from me, I guess."

The responding Federal Aviation Administration (FAA) inspector reported that the airplane landed on runway 35L and ground looped during the landing roll. The right main landing gear collapsed (figure 1), the lower right wing struck the ground. A postaccident examination revealed no anomalies with the landing gear.

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

Additional Participating Entity:

Federal Aviation Administration / Flight Standards District Office; Denver, Colorado

Aviation Accident Factual Report - National Transportation Safety Board: https://app.ntsb.gov/pdf


Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms

http://registry.faa.gov/N44562

NTSB Identification: CEN17LA301
14 CFR Part 91: General Aviation
Accident occurred Thursday, August 03, 2017 in Colorado Springs, CO
Aircraft: BEECH D17S, registration: N44562
Injuries: 2 Uninjured.

NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On August 3, 2017, about 1130 mountain daylight time, a Beech D17S airplane, N44562, ground looped during landing at City of Colorado Springs Municipal Airport (COS), Colorado Springs, Colorado. The pilot and one passenger were not injured and the airplane sustained substantial damage. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident and no flight plan had been filed. The flight departed Gallup Municipal Airport (GUP), Gallup, New Mexico, about 0900.

The pilot stated during landing the right quartering tailwind was 10 to 13 mph. He made a normal landing with a lot of left rudder application to keep the airplane straight. After touchdown, with the tailwheel on the runway, the airplane drifted to the right and he applied left brake. The right landing gear collapsed and the airplane continued to the right edge of the runway where it came to rest upright. The pilot stated there were no mechanical malfunctions with the airplane and that "it got away from me, I guess."


The responding Federal Aviation Administration (FAA) inspector reported that the airplane landed on runway 35L and ground looped during the landing roll. The right main landing gear collapsed (figure 1), the lower right wing struck the ground. A postaccident examination revealed no anomalies with the landing gear.

NTSB Identification: CEN17LA301
14 CFR Part 91: General Aviation
Accident occurred Thursday, August 03, 2017 in Colorado Springs, CO
Aircraft: BEECH D17S, registration: N44562
Injuries: 2 Uninjured.

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. NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On August 3, 2017, about 1130 mountain daylight time, a Beech D17S airplane, N44562, ground looped during landing at City of Colorado Springs Municipal Airport (COS), Colorado Springs, Colorado. The pilot and one passenger were not injured and the airplane sustained substantial damage. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident and no flight plan had been filed. The flight departed Gallup Municipal Airport (GUP), Gallup, New Mexico, about 0900. 

The responding Federal Aviation Administration (FAA) inspector reported that the airplane landed on runway 35L and ground looped during the landing roll. The right main landing gear collapsed and the right wing struck the ground (figure 1). 

The airplane has been retained for further examination.

Cessna 152, N5276M, RE Airways Corp: Incident occurred August 02, 2017 in Miami, Florida

RE Airways Corp: http://registry.faa.gov/N5276M

Aircraft went off runway and back to taxiway.

Date: 02-AUG-17
Time: 23:28:00Z
Regis#: N5276M
Aircraft Make: CESSNA
Aircraft Model: C152
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: UNKNOWN
Activity: PERSONAL
Flight Phase: LANDING (LDG)
Operation: 91
City: MIAMI
State: FLORIDA

Diamond DA-20C-1 Eclipse, N634DC, Falcon Aviation Academy LLC: Incident occurred August 01, 2017 at Newnan–Coweta County Airport (KCCO), Georgia

Falcon Aviation Academy LLC: http://registry.faa.gov/N634DC

Hard landing.

Date: 01-AUG-17
Time: 19:45:00Z
Regis#: N634DC
Aircraft Make: DIAMOND
Aircraft Model: DA20
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: MINOR
Activity: INSTRUCTION
Flight Phase: LANDING (LDG)
Operation: 91
City: NEWNAN
State: GEORGIA

Autogyro MTO Sport, N571UJ: Accident occurred August 03, 2017 at Mentone Airport (C92), Kosciusko County, Indiana

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

Aviation Accident Factual Report - National Transportation Safety Board: https://app.ntsb.gov/pdf

Investigation Docket: - National Transportation Safety Board:
https://dms.ntsb.gov/pubdms

http://registry.faa.gov/N571UJ

NTSB Identification: CEN17LA302
14 CFR Part 91: General Aviation
Accident occurred Thursday, August 03, 2017 in Mentone, IN
Aircraft: JAMES F HAKE MTO SPORT, registration: N571UJ
Injuries: 1 Minor.

NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On August 3, 2017, about 0917 central daylight time, a Hake MTO Sport gyroplane, N571UJ, was substantially damaged when it tipped over on landing at Mentone Airport (C92), Mentone, Indiana. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 Code of Federal Regulations Part 91 without a flight plan. The pilot sustained minor injuries. The local flight originated about 0930.

According to the pilot's accident report, when he touched down on the main landing gear, he applied "moderate" right rudder to maintain runway alignment and to avoid slipping. He stated he should have raised the nose to reduce airspeed, but instead he lowered the nose and struck the runway. The pilot explained that on this particular gyroplane, the nose wheel and rudder are interconnected; that is, the nose wheel does not pivot on a caster. When the gyroplane touched down, it 'jerked" abruptly to the right and tipped over. The pilot concluded, "This accident was the result of pilot error. There was no malfunction [of the gyroplane, flight controls, or engine]."

NTSB Identification: CEN17LA302
14 CFR Part 91: General Aviation
Accident occurred Thursday, August 03, 2017 in Mantone, IN
Aircraft: JAMES F HAKE MTO SPORT, registration: N571UJ
Injuries: 1 Serious.

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. NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On August 3, 2017, about 0917 central daylight time, a Hake MTO Sport gyroplane, N571UJ, sustained minor damage when it tipped over on landing at Mantone Airport (C92), Mantone, Indiana. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of Title 14 Code of Federal Regulations Part 91 without a flight plan. The pilot sustained a serious injury. The local flight originated at an undetermined time.

Witnesses reported the pilot flared too high and landed hard on runway 36. The gyroplane bounced and tipped over. The pilot later told a Federal Aviation Administration FAA) inspector that he had applied right rudder on landing. The rudder pedals remain connected to the steerable nose gear. When the nose wheel touched down, the side load caused the gyrocopter to tip onto its side and the rotor and propeller both struck the ground. The pilot said the accident was due to pilot error and that there were no mechanical or weather issues.





MENTONE – A Michigan man was transported to a Rochester hospital this morning after his Autogyro MTO Sport tipped over while landing at the Mentone Airport.

James Hake, 71, had a compound fracture his wrist, according to Kosciusko County Sheriff’s Department Sgt. Rick Shepherd. Mentone Town Marshal Jim Eads said Hake had a broken left arm and lots of abrasions, but had a helmet on when he crashed before 10 a.m. today. Hake was the only person in the plane.

Based on the information Shepherd gathered at the scene, as Hake was landing his Autogyro MTO Sport a front wheel tilted and caused the whole plane to rollover.

Since there was a crash with injury, Eads said the Federal Aviation Administration had to be contacted. Popular Rotorcraft Association President Brent Drake said he made that contact. 

“It just tipped over. It is just a rollover accident,” Drake said, identifying the gyroplane as “an Autogyro MTO Sport.”

He said the association is having it's yearly convention at the Mentone Airport this weekend and will be there through Sunday. Drake expected 300 members to be in attendance, with people coming from all over, including as far away as Alabama and Tennessee. In 2016, a man came from China for the convention.

Shepherd said before the gyroplane could be moved from the runway, the FAA had to clear it. 

Along with KCSD and the Mentone Police Department, responding to the scene was the fire department. 

http://www.timesuniononline.com

Cessna 172R, N91966, registered to and operated by Beers Investment Group Inc: Accident occurred August 02, 2017 at Kearney Regional Airport (KEAR), Buffalo County, Nebraska

Additional Participating Entity: 
Federal Aviation Administration / Flight Standards District Office; Lincoln, Nebraska 

Aviation Accident Factual Report - National Transportation Safety Board: https://app.ntsb.gov/pdf 

Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms 

Beers Investment Group Inc: http://registry.faa.gov/N91966

Location: Kearney, NE
Accident Number: GAA17CA482
Date & Time: 08/02/2017, 1630 CDT
Registration: N91966
Aircraft: CESSNA 172
Aircraft Damage: Substantial
Defining Event: Loss of control on ground
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Instructional 

The pilot reported that just after touchdown, he lost directional control of the airplane. The airplane exited the right side of the runway and collided with a taxiway sign.

The airplane's lower right fuselage sustained substantial damage.

The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. 

Pilot Information

Certificate: Private
Age: 24, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: 3-point
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification:  Class 1 With Waivers/Limitations
Last FAA Medical Exam: 03/24/2016
Occupational Pilot: No
Last Flight Review or Equivalent: 01/14/2017
Flight Time:  (Estimated) 142 hours (Total, all aircraft), 142 hours (Total, this make and model), 52 hours (Pilot In Command, all aircraft), 18 hours (Last 90 days, all aircraft), 5 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Manufacturer: CESSNA
Registration: N91966
Model/Series: 172 R
Aircraft Category: Airplane
Year of Manufacture: 2012
Amateur Built: No
Airworthiness Certificate: Normal; Utility
Serial Number: 17281616
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection: 06/21/2017, Annual
Certified Max Gross Wt.: 2299 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 1568.3 Hours as of last inspection
Engine Manufacturer: LYCOMING
ELT: Installed, not activated
Engine Model/Series: IO-360-L2A
Registered Owner: BEERS INVESTMENT GROUP INC
Rated Power: 160 hp
Operator: BEERS INVESTMENT GROUP INC
Operating Certificate(s) Held: Pilot School (141) 

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KEAR, 2130 ft msl
Observation Time: 2056 UTC
Distance from Accident Site: 1 Nautical Miles
Direction from Accident Site: 178°
Lowest Cloud Condition: Clear
Temperature/Dew Point: 26°C / 17°C
Lowest Ceiling: None
Visibility: 10 Miles
Wind Speed/Gusts, Direction: Calm
Visibility (RVR):
Altimeter Setting: 30.11 inches Hg
Visibility (RVV):
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Salina, KS (KSLN)
Type of Flight Plan Filed: VFR
Destination: Kearney, MA (KEAR)
Type of Clearance: VFR
Departure Time: 1500 CDT
Type of Airspace: Class E 

Airport Information

Airport: KEARNEY RGNL (EAR)
Runway Surface Type: Asphalt
Airport Elevation: 2131 ft
Runway Surface Condition: Dry
Runway Used: 18
IFR Approach: None
Runway Length/Width: 7094 ft / 150 ft
VFR Approach/Landing: Full Stop; Traffic Pattern 

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None
Latitude, Longitude:  40.752222, -99.000833 (est)

CZAW SportCruiser, N777NG, registered to and operated by N M G Aviation LLC: Accident occurred August 03, 2017 at Rowan County Airport (KRUQ), Salisbury, North Carolina

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Charlotte, North Carolina

Aviation Accident Final Report - National Transportation Safety Board: https://app.ntsb.gov/pdf


Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms 


N M G Aviation LLC: http://registry.faa.gov/N777NG


Location: Salisbury, NC

Accident Number: GAA17CA465
Date & Time: 08/04/2017, 0800 EDT
Registration: N777NG
Aircraft: CZECH AIRCRAFT WORKS SPOL SRO SPORTCRUISER
Aircraft Damage: Substantial
Defining Event: Hard landing
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Instructional 

Analysis 

The student pilot reported that he had departed with the intent to perform touch-and-go takeoffs and landings. After takeoff, he realized that the canopy was not latched. He struggled to maintain airplane control in the pattern, but he was able to land normally.

The student pilot then checked the latch handle, and he believed that he had secured the canopy correctly. He took off and flew one pattern but just before landing, the canopy opened and obstructed the pilot's view of the runway.

The airplane landed hard and bounced, and the pilot aborted the landing.

The student pilot flew a third pattern and made an approach over the runway centerline, "slightly above stall airspeed." The airplane landed hard on the runway, and the right main landing gear (MLG) and the nose landing gear separated from the airplane. The airplane skidded to a stop on the runway.

The airplane sustained substantial damage to the right MLG attachment points and the right-wing spar.

The student pilot asserted that the canopy latch was down during the takeoffs but was not seated correctly. For the latch to seat correctly, "the canopy itself needed to be pushed up so that gravity seated the canopy."

The airplane was equipped with a full-width clear canopy, hinged in the front and tipped forward for entry to the cockpit.

The manually operated canopy was supposed to be closed by the pilot by reaching above their head and grabbing the handle identified by the manufacturer's illustrated parts catalogue as SF0730N. Per the photographs provided by Federal Aviation Administration (FAA) aviation safety inspectors, the handle was not installed on the canopy.

The canopy security latches consisted of two metal claw-type latches that were mechanically moved forward to secure the canopy to the fuselage. The canopy latches were moved forward to the secure position when the pilot lowered the canopy "T" handle. The "T" handle was affixed to the baggage compartment front wall in the cockpit between the left and right seats just above the arm rest and just below the pilot headset audio input jacks.

The student pilot's head set control unit was about 4 inches long by 1 inch in diameter. Photographs taken shortly after the accident and provided by FAA inspectors revealed that the control unit was lodged underneath the "T" handle.

The student pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The physical interference of the student pilot's headset control unit with the canopy, which prevented the canopy latches from seating properly and resulted in the canopy opening in flight and the subsequent hard landing. 

Findings

Aircraft
Interphone - Unintentional use/operation (Cause)

Personnel issues
Aircraft control - Student pilot (Cause)

Environmental issues
Access to equipment/controls - Effect on operation (Cause)

Factual Information

History of Flight

Landing-flare/touchdown
Hard landing (Defining event)

Takeoff
Loss of control in flight

Student Pilot Information

Certificate: Student
Age: 68, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: 3-point
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Sport Pilot Without Waivers/Limitations
Last FAA Medical Exam:
Occupational Pilot: No
Last Flight Review or Equivalent:
Flight Time:  (Estimated) 46 hours (Total, all aircraft), 46 hours (Total, this make and model), 7 hours (Pilot In Command, all aircraft), 11 hours (Last 90 days, all aircraft), 4 hours (Last 30 days, all aircraft) 

Aircraft and Owner/Operator Information

Aircraft Manufacturer: CZECH AIRCRAFT WORKS SPOL SRO
Registration: N777NG
Model/Series: SPORTCRUISER A
Aircraft Category: Airplane
Year of Manufacture: 2007
Amateur Built: No
Airworthiness Certificate: Special Light-Sport
Serial Number: 07SC059
Landing Gear Type: Tricycle
Seats: 2
Date/Type of Last Inspection:  06/01/2017, Annual
Certified Max Gross Wt.: 1320 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 2593 Hours at time of accident
Engine Manufacturer: ROTAX
ELT: C91A installed, not activated
Engine Model/Series: ROTAX 912S (4
Registered Owner: NMG AVIATION LLC
Rated Power: 100 hp
Operator: NMG AVIATION LLC
Operating Certificate(s) Held: None 

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: RUQ
Observation Time: 1145 UTC
Distance from Accident Site:
Direction from Accident Site:
Lowest Cloud Condition: Clear
Temperature/Dew Point: 19°C / 19°C
Lowest Ceiling: None
Visibility:  7 Miles
Wind Speed/Gusts, Direction: Calm
Visibility (RVR):
Altimeter Setting: 30.14 inches Hg
Visibility (RVV):
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Salisbury, NC (KRUQ)
Type of Flight Plan Filed: None
Destination: Salisbury, NC (KRUQ)
Type of Clearance: None
Departure Time: 0800 EDT
Type of Airspace: Class G

Airport Information

Airport: ROWAN COUNTY (KRUQ)
Runway Surface Type: Unknown
Airport Elevation: 772 ft
Runway Surface Condition: Dry
Runway Used: 20
IFR Approach: None
Runway Length/Width: 5500 ft / 100 ft
VFR Approach/Landing: Full Stop; Traffic Pattern

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None
Latitude, Longitude:  35.645833, -80.520278 (est)