DASSAULT-BREGUET FALCON 10 near Panama City, FL — 2023-06-07
- Date
- 2023-06-07
- Location
- Panama City, FL, USA
- Airport
- ECP
- Aircraft
- DASSAULT-BREGUET FALCON 10
- Registration
- N87RT
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Landing
Probable cause
The flight crew’s failure to appropriately configure the airplane for landing, which resulted in a failed attempt to utilize the thrust reversers during landing and the inability to stop the airplane using its brakes due to increased forward thrust. Contributing to the accident was the flight crew’s failure to utilize the appropriate checklist for the thrust reverser equipped airplane.
Contributing factors
Contributing to the accident was the flight crew’s failure to utilize the appropriate checklist for the thrust reverser equipped airplane.
NTSB narrative
Upon arriving at the destination airport, the business jet touched down about 2,500 ft beyond the threshold of the 10,000-ft-long runway. The pilot extended the airplane’s flight spoilers and attempted to activate the thrust reversers, but the airplane did not decelerate as expected and a warning horn sounded. The pilots then attempted to apply normal followed by emergency braking, both of which were ineffective in slowing the airplane. The airplane subsequently overran the runway and struck several approach lighting stanchions, coming to rest after the landing gear collapsed. The airplane’s occupants were uninjured, but the airplane was substantially damaged during the accident sequence. Following the accident, the captain noticed he had forgotten to move the thrust reverser emergency stow switches to their normal operating position after completing a preflight check. The warning horn heard during the landing was an indication of the stowed thrust reverser switches. The ineffective braking likely occurred because of the engines’ increased thrust output due to the attempted application of the thrust reversers with the switches in the stowed position. A postaccident examination of the wreckage confirmed that there was no evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. The airplane checklist found in the cockpit was marked “For Training Purposes Only” and for an airplane that was not equipped with thrust reversers.
Analysis
- Primary failure mode
- Human factors
- First missed decision gate
- Pilot did not check thrust reverser stow switches before landing.
NTSB coding
Evidence available
- CVR
- ADS-B / radar
- Photos
- 18 docket documents
Docket documents18
- COCKPIT VOICE RECORDER - SPECIALIST'S FACTUAL REPORTcvr
- PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT, NTSB FORM 6120.1form
- PIC STATEMENT AND INTERVIEW SUMMARYinterview
- SIC STATEMENTinterview
- EASA AFM SUPPLEMENT NO. 3other
- ECP AIRPORT DIAGRAMother
- ECP ILS OR LOCALIZER RUNWAY 16 INSTRUMENT APPROACH PROCEDUREother
- GRUMMAN THRUST REVERSERS - AIRPLANE FLIGHT MANUAL SUPPLEMENT NO.1other
- GRUMMAN THRUST REVERSERS - MAINTENANCE MANUAL SUPPLEMENTother
- GRUMMAN THRUST REVERSERS - OPERATIONAL LNSTRUCTIONS MANUAL SUPPLEMENTother
- INVESTIGATION PHOTOGRAPHSphotos
- ADS-B DATA (KMZ FORMAT)radar
- ADS-B DATA (TABULAR)radar
- ADS-B DATA PLOT (FINAL APPROACH, LANDING, AND OVERRUN)radar
- ADS-B DATA PLOT (ROUTE OF FLIGHT)radar
- ELECTRONIC DEVICES - SPECIALIST'S FACTUAL REPORTreport
- MEMORANDUM FOR RECORD - WRECKAGE EXAMINATION AND ONBOARD GUIDANCE DOCUMENTS REVIEWwreckage
- WRECKAGE RELEASE AND EVIDENCE CONTROLwreckage
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