Saturday, October 21, 2017

Gulfstream G-IV, N450KK: Accident occurred April 10, 2015 over the Caribbean Sea

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

Additional Participating Entities:
Federal Aviation Administration / Flight Standards District Office; Miramar, Florida
Gulfstream; Savannah, Georgia 

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

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

Registered Owner: Las Eugentas Aircraft Holdings LLC

Operator: La Venezolana de Seguros CA

http://registry.faa.gov/N450KK



NTSB Identification: ERA15LA328
14 CFR Part 91: General Aviation
Accident occurred Friday, April 10, 2015 in Caribbean Sea, Unknown
Aircraft: GULFSTREAM AEROSPACE G IV, registration: N450KK
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.

HISTORY OF FLIGHT

On April 10, 2015, about 1845 eastern daylight time, a Gulfstream Aerospace G-IV airplane, N450KK, experienced a cabin overpressurization event over the Caribbean Sea. The airline transport pilot and copilot were not injured, and the airplane sustained substantial damage. The airplane was being operated by a private company as a 14 Code of Federal Regulations Part 91 positioning flight. Day, visual meteorological conditions prevailed, and an instrument flight rules flight plan was filed. The flight originated at Simón Bolívar International Airport (SVMI), Maiquetia, Venezuela, about 1645 and was destined for Fort Lauderdale Executive Airport (FXE), Fort Lauderdale, Florida.

The pilot reported that the purpose of the flight was to fly the airplane to Boca Raton Airport (BCT), Boca Raton, Florida, for scheduled maintenance with a planned stop at FXE to clear US Customs. While approaching to start the descent to FXE, at flight level 430, the pilots observed a red "9.8 CABIN DFRN" warning message on the crew advisory system (CAS), indicating a maximum cabin differential pressure of 9.8 pounds per square inch differential (psid) or greater, followed by a red "DOOR MAIN" warning message. According to the digital flight data recorder (DFDR), this was preceded 21 seconds by the illumination of the amber Master Caution switch. The pilots then donned oxygen masks and referenced the airplane's quick reference handbook (QRH) for the emergency checklist. The pilots then heard a loud "bam" sound in the cabin and immediately initiated a descent in accordance with the QRH. The pilots manually opened the cabin pressure outflow valve and leveled the airplane at 12,000 ft mean sea level. The DFDR also showed that the 9.8 CABIN DFRN warning illuminated a second time, at 1858:38, and remained illuminated until 1904:14. This was not reported by the flight crew. The pilots continued the flight to FXE unpressurized and landed without further incident. Examination of the airplane the next day revealed structural airframe damage.

AIRPLANE INFORMATION

According to Gulfstream, "The pressurization system controls, regulates and monitors the amount of conditioned air within the pressure vessel to achieve and maintain a safe and comfortable cabin pressure (cabin altitude), up to the airplane's maximum operating altitude. While normally preprogrammed, cabin altitude can also be controlled manually. Cabin conditioned air is also exchanged at regular intervals for occupant comfort."

Normally, the cabin pressurization system limits the cabin pressurization differential to 9.55 +0.1 psid. As differential pressure reaches 9.55 psid, an amber "CABIN DFRN 9.6" caution message is displayed on the CAS. If the pressurization system malfunctions and cannot limit the maximum cabin pressurization differential to 9.55 +0.1 psid, the cabin pressurization relief/safety valve (CPRV) limits pressure differential to 9.7 +0.1 psid. As differential pressure reaches 9.8 psid, a red "CABIN DFRN 9.8" warning message is displayed on the CAS.

FLIGHT RECORDERS

The airplane was equipped with a digital flight data recorder (DFDR), and the entire accident flight was captured on the DFDR. The DFDR was not designed to record cabin pressure or cabin altitude; however, it recorded CAS messages associated with cabin differential pressure anomalies.

The following is a chronological sequence of events based on the DFDR data with estimated times:

1645:00 - Flight took off from SVMI.
1844:41 - Amber Master Caution switch illuminated (the DFDR did not record the type of message).
1845:02 - A red "9.8 CABIN DFRN" CAS warning message and red Master Warning switch illuminated; the CAS message remained on for 11 minutes 44 seconds.
1846:10 - Pilots acknowledged the amber and red CAS messages (89 seconds after the first CAS illumination).
1847:17 - The airplane began to descend.
1848:28 - Amber Master Caution switch illuminated (the DFDR did not record the type of message); pilots extinguished 5 seconds later.
1853:50 - Red Master Warning switch illuminated (the DFDR did not record the type of message); pilots extinguished 10 seconds later.
1855:18 - Amber Master Caution switch illuminated (the DFDR did not record the type of message); pilots extinguished 24 seconds later.
1856:46 - Red "9.8 CABIN DFRN" message extinguished. Airplane was level at 20,000 ft.
1857:55 - Amber Master Caution switch illuminated (the DFDR did not record the type of message); pilots extinguished 1 second later.
1858:38 - Red "9.8 CABIN DFRN" CAS warning message and red Master Warning switch illuminated.
1904:14 - Red "9.8 CABIN DFRN" extinguished and remained off for the remainder of flight.
1905:52 - "Cabin Pressure Low" CAS message illuminated and remained on for 27 minutes; airplane descended through 13,000 ft.
1905:53 - Red Master Warning switch illuminated (the DFDR did not record the type of message); pilots extinguished 45 seconds later.
1905:59 - Emergency checklist activated for Cabin Pressure Low.
1932:53 - Cabin Pressure Low message extinguished and stayed off for the remainder of flight.
1947:27 - Airplane landed at FXE, 62.7 minutes after the first amber CAS message illuminated in the cockpit.

POSTACCIDENT EXAMINATION

The day after the accident, the airplane was repositioned to BCT, about 20 miles from FXE, for scheduled maintenance. During the scheduled maintenance, several damaged floor beams on the left side of the fuselage and a damaged frame under the right galley door were noted. Gulfstream maintenance and engineering personnel then examined the airplane and found structural airframe damage, including a cracked floor beam, dimpled areas in the floor boards, damaged structure between ribs, and damaged wing links.

An examination of the outer fuselage revealed that the CPRV static port, located above the CPRV, was completely plugged with a foreign material resembling dried dirt from a mud dauber. According to Gulfstream, a blocked CPRV static port would render the CPRV inoperative due to its inability to measure the cabin-to-atmosphere pressure differential. However, the cabin pressure could still be controlled independently by manual operation of the outflow valve. The cabin could also be depressurized by using ram air, which would shut off bleed air for pressurization. No other mechanical anomalies were found with the pressurization system. The airplane was not repaired and returned to service.; therefore, the reason for the initial overpressurization event could not be determined. According to Gulfstream, an obstructed CPRV static port would be difficult to detect on a preflight walk-around inspection.

Examination of the aural warning system speaker showed evidence of deterioration, and the speaker volume was not functioning properly. An aural caution (double chime) and an aural warning (triple chime) should have accompanied the amber and red cabin differential pressure messages on the CAS. There was no evidence that the flight crew received any aural cautions or warnings.

Abnormal Procedures

The abnormal procedures in the G-IV QRH addressed both the 9.6- and 9.8-psid scenarios. The 9.6-psid procedure instructed the crew to raise cabin altitude and increase cabin climb rate, if required, and to switch to manual pressurization control in the event that automatic pressurization control was lost. The procedure cautioned the crew to closely monitor the cabin differential pressure and not allow it to exceed 9.8 psid. If cabin psid exceeded 9.8, then the ram air switch should be placed to "RAM" to use ram air, and air from both air conditioning packs should be shut off for pressurization.

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