20221221018329A

Accident · Destroyed

FAA accident report · Grumman American AA-5B · Reserve, LA · December 21, 2022

Date
December 21, 2022 · 19:54 local
Place
Reserve, LA
Airport
Port Of South Louisiana Execut
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N321GD
NTSB investigation
NTSBCEN23LA068
Reported as
Grumman American AA-5B
Reported engine
Lycoming O-360-AK4
People aboard
2
Fatal injuries
0
Other injuries
1
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,237 total657 in this make and model91 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

The aircraft, privacy data omitted, was refuelled to full tanks 2 days prior to the accident and kept in a heated hanger. The CFI and student had not flown the day of the accident. They conducted a comprehensive sortie brief for the instrument training flight, and recieved a weather brief before filing an IFR flight plan, with kmsy as their alternate. After conducting their preflight checks and run up, there was little delay in recieving their release from msy, and the aircraft took off at 7.52PM. The CFI noted that the carb temperature was 72°f on climb out. The aircraft was climbed at 90 KTS and went IMC at 450’. Shortly after, at approximately 500’, there was a marked power reduction felt and the RPM dropped to approximately 1400. The handling pilot heard the engine "cough and splutter" and noted an rom drop. The CFI took control and instigated a turn back to the left. As part of his troubleshooting he leaned the mixture, noting a rise in approximately 200 RPM as he did so. He did not apply carb heat, and the electrical fuel pump was on. When the aircraft emerged into VMC at approxiately 350’, the aircraft was approximately half was down the runway. In order to avoid overrunning the airfield and ending up in a ditch, the CFI put down full flap and conducted a forward slip, hoping to land the aircraft facing back up the parallel taxiway for runay 35. The student noted that by this point the propellor had stopped. At approximately 5’, the aircraft was felt to stall and the left wing and nosewheel hit the ground. The aircraft rapidly decelerated and then turned onto a heading of 241°. The CFI conducted an emergency engine shutdown and safely vacated the aircraft with his student, sustaining a mild facial abrasion as he did so. Subsequent investigation of the engine by FAA maintenance inspectors found no failure of any component within the engine. Given the conditions of flight, carburettor icing is considered to be the most likely cause of the engine failure.

As the FAA filed it

THE AIRCRAFT, ^PRIVACY DATA OMITTED^, WAS REFUELLED TO FULL TANKS 2 DAYS PRIOR TO THE ACCIDENT AND KEPT IN A HEATED HANGER. THE CFI AND STUDENT HAD NOT FLOWN THE DAY OF THE ACCIDENT. THEY CONDUCTED A COMPREHENSIVE SORTIE BRIEF FOR THE INSTRUMENT TRAINING FLIGHT, AND RECIEVED A WEATHER BRIEF BEFORE FILING AN IFR FLIGHT PLAN, WITH KMSY AS THEIR ALTERNATE. AFTER CONDUCTING THEIR PREFLIGHT CHECKS AND RUN UP, THERE WAS LITTLE DELAY IN RECIEVING THEIR RELEASE FROM MSY, AND THE AIRCRAFT TOOK OFF AT 7.52PM. THE CFI NOTED THAT THE CARB TEMPERATURE WAS 72°F ON CLIMB OUT. THE AIRCRAFT WAS CLIMBED AT 90 KTS AND WENT IMC AT 450’. SHORTLY AFTER, AT APPROXIMATELY 500’, THERE WAS A MARKED POWER REDUCTION FELT AND THE RPM DROPPED TO APPROXIMATELY 1400. THE HANDLING PILOT HEARD THE ENGINE "COUGH AND SPLUTTER" AND NOTED AN ROM DROP. THE CFI TOOK CONTROL AND INSTIGATED A TURN BACK TO THE LEFT. AS PART OF HIS TROUBLESHOOTING HE LEANED THE MIXTURE, NOTING A RISE IN APPROXIMATELY 200 RPM AS HE DID SO. HE DID NOT APPLY CARB HEAT, AND THE ELECTRICAL FUEL PUMP WAS ON. WHEN THE AIRCRAFT EMERGED INTO VMC AT APPROXIATELY 350’, THE AIRCRAFT WAS APPROXIMATELY HALF WAS DOWN THE RUNWAY. IN ORDER TO AVOID OVERRUNNING THE AIRFIELD AND ENDING UP IN A DITCH, THE CFI PUT DOWN FULL FLAP AND CONDUCTED A FORWARD SLIP, HOPING TO LAND THE AIRCRAFT FACING BACK UP THE PARALLEL TAXIWAY FOR RUNAY 35. THE STUDENT NOTED THAT BY THIS POINT THE PROPELLOR HAD STOPPED. AT APPROXIMATELY 5’, THE AIRCRAFT WAS FELT TO STALL AND THE LEFT WING AND NOSEWHEEL HIT THE GROUND. THE AIRCRAFT RAPIDLY DECELERATED AND THEN TURNED ONTO A HEADING OF 241°. THE CFI CONDUCTED AN EMERGENCY ENGINE SHUTDOWN AND SAFELY VACATED THE AIRCRAFT WITH HIS STUDENT, SUSTAINING A MILD FACIAL ABRASION AS HE DID SO. SUBSEQUENT INVESTIGATION OF THE ENGINE BY FAA MAINTENANCE INSPECTORS FOUND NO FAILURE OF ANY COMPONENT WITHIN THE ENGINE. GIVEN THE CONDITIONS OF FLIGHT, CARBURETTOR ICING IS CONSIDERED TO BE THE MOST LIKELY CAUSE OF THE ENGINE FAILURE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.