20210830017009A

Accident · Substantial damage

FAA accident report · Piper PA-24-400 · Fullerton, CA · August 30, 2021

Date
August 30, 2021 · 13:45 local
Place
Fullerton, CA
Airport
Fullerton Municipal
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8501P
NTSB investigation
NTSBWPR21LA343
Reported as
Piper PA-24-400
Reported engine
Lycoming IO-720
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
3,834 total2,633 in this make and model2 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.

On August 30, 2021 at 2045(zulu) / 1345 (local) PST, Piper comanche (PA-24-400), bearing registration mark N8501P and serial number 26-81 was being flown by pilot in command (PIC), privacy data omitted, privacy data omitted, whom holds a commercial pilot rating and held a third class (private) medical. The PIC was accompanied by a certified flight instructor (CFI) for the purpose of evaluating the PIC for continued insurance coverage (annual flight review). The aircraft and crew were involved in an accident at Fullerton Municipal Airport (kful), in Fullerton, California.

PIC richmond and the CFI were on final approach to runway 24, in a right closed traffic pattern at kful after departing chino (cno) at 2001 (zulu) / 12 noon (local) PST. The PIC was instructed by the Fullerton tower to go around and that the aircraft wheels appeared up. ATC stated that these instructions were not responded to by the PIC. The PIC stated that he heard the instructions from the tower, and extended the landing gear. The PIC stated the aircraft was setup for a straight in approach to runway 24 at kful, without any flap extension. The PIC stated that he was pulling the throttle back pretty FAR to keep his airspeed down. The CFI stated that he reminded the PIC that the landing gear was retracted but received neither verbal nor physical response. The CFI recalled ATC stating something to the effect that the aircraft wheels were not extended, and to go around. The CFI stated that the PIC then silently lowered the gear lever. At this point the CFI stated that the aircraft was pointing down towards the perimeter chain link fence on the approach end of runway 24. Rather than struggling with the PIC over the yoke, the CFI recalled that just before impacting the fence, he believes that he nudged the yoke back just enough to clear the fence.

N8501P?s propeller, undercarriage, and extended landing gear struck the top support tube of an 8 foot tall perimeter fence along artesia drive. The chain link fence showed evidence of propeller strikes and landing gear entanglement. The aircraft appeared to then move into a slightly nose down attitude and struck a medium intensity approach lighting system (malsr) which was immediately inside of the perimeter fence. The aircraft contacted the grassy area between the perimeter fence and runway 24?s threshold. The aircraft was in an uncontrolled status for 50 meters in the grass, prior to contacting runway marking lights at the edge of runway 24. The aircraft left an oil stain in the grass for 25 meters. The aircraft pitot tube, nose wheel assembly, and windshield plexiglas were scattered from the perimeter fence to the edge of runway 24. Perimeter fence material was likewise scattered in the grass area. This grass area is approximately 50 meters in length. After traveling approximately 50 meters in the grass on an azimuth of 240 degrees, the aircraft struck the runway marking lights at the approach end of runway 24, as evident by plexiglas and the runway light identification plate being torn off of the light base. The aircraft continued to skid until coming to a stop approximately 50 feet short of runway 24 threshold. The left hand main landing gear assembly separated from the aircraft and was located approximately 25 feet forward of the nose of the aircraft.

The PIC recalls turning off aircraft power switches, and removing the keys, prior to first responders arriving to render aid. The PIC and CFI were both transported to uci medical center for treatment. The PIC sustained abrasions to his left elbow and right hand. The CFI recalls being in a state of shock, and was able to crawl out of the aircraft, on to the right hand wing and await first responders. The CFI sustained bumps and bruises from the seatbelt.

As the FAA filed it

ON AUGUST 30, 2021 AT 2045(ZULU) / 1345 (LOCAL) PST, PIPER COMANCHE (PA-24-400), BEARING REGISTRATION MARK N8501P AND SERIAL NUMBER 26-81 WAS BEING FLOWN BY PILOT IN COMMAND (PIC), ^PRIVACY DATA OMITTED^, ^PRIVACY DATA OMITTED^, WHOM HOLDS A COMMERCIAL PILOT RATING AND HELD A THIRD CLASS (PRIVATE) MEDICAL. THE PIC WAS ACCOMPANIED BY A CERTIFIED FLIGHT INSTRUCTOR (CFI) FOR THE PURPOSE OF EVALUATING THE PIC FOR CONTINUED INSURANCE COVERAGE (ANNUAL FLIGHT REVIEW). THE AIRCRAFT AND CREW WERE INVOLVED IN AN ACCIDENT AT FULLERTON MUNICIPAL AIRPORT (KFUL), IN FULLERTON, CALIFORNIA.

PIC RICHMOND AND THE CFI WERE ON FINAL APPROACH TO RUNWAY 24, IN A RIGHT CLOSED TRAFFIC PATTERN AT KFUL AFTER DEPARTING CHINO (CNO) AT 2001 (ZULU) / 12 NOON (LOCAL) PST. THE PIC WAS INSTRUCTED BY THE FULLERTON TOWER TO GO AROUND AND THAT THE AIRCRAFT WHEELS APPEARED UP. ATC STATED THAT THESE INSTRUCTIONS WERE NOT RESPONDED TO BY THE PIC. THE PIC STATED THAT HE HEARD THE INSTRUCTIONS FROM THE TOWER, AND EXTENDED THE LANDING GEAR. THE PIC STATED THE AIRCRAFT WAS SETUP FOR A STRAIGHT IN APPROACH TO RUNWAY 24 AT KFUL, WITHOUT ANY FLAP EXTENSION. THE PIC STATED THAT HE WAS PULLING THE THROTTLE BACK PRETTY FAR TO KEEP HIS AIRSPEED DOWN. THE CFI STATED THAT HE REMINDED THE PIC THAT THE LANDING GEAR WAS RETRACTED BUT RECEIVED NEITHER VERBAL NOR PHYSICAL RESPONSE. THE CFI RECALLED ATC STATING SOMETHING TO THE EFFECT THAT THE AIRCRAFT WHEELS WERE NOT EXTENDED, AND TO GO AROUND. THE CFI STATED THAT THE PIC THEN SILENTLY LOWERED THE GEAR LEVER. AT THIS POINT THE CFI STATED THAT THE AIRCRAFT WAS POINTING DOWN TOWARDS THE PERIMETER CHAIN LINK FENCE ON THE APPROACH END OF RUNWAY 24. RATHER THAN STRUGGLING WITH THE PIC OVER THE YOKE, THE CFI RECALLED THAT JUST BEFORE IMPACTING THE FENCE, HE BELIEVES THAT HE NUDGED THE YOKE BACK JUST ENOUGH TO CLEAR THE FENCE.

N8501P?S PROPELLER, UNDERCARRIAGE, AND EXTENDED LANDING GEAR STRUCK THE TOP SUPPORT TUBE OF AN 8 FOOT TALL PERIMETER FENCE ALONG ARTESIA DRIVE. THE CHAIN LINK FENCE SHOWED EVIDENCE OF PROPELLER STRIKES AND LANDING GEAR ENTANGLEMENT. THE AIRCRAFT APPEARED TO THEN MOVE INTO A SLIGHTLY NOSE DOWN ATTITUDE AND STRUCK A MEDIUM INTENSITY APPROACH LIGHTING SYSTEM (MALSR) WHICH WAS IMMEDIATELY INSIDE OF THE PERIMETER FENCE. THE AIRCRAFT CONTACTED THE GRASSY AREA BETWEEN THE PERIMETER FENCE AND RUNWAY 24?S THRESHOLD. THE AIRCRAFT WAS IN AN UNCONTROLLED STATUS FOR 50 METERS IN THE GRASS, PRIOR TO CONTACTING RUNWAY MARKING LIGHTS AT THE EDGE OF RUNWAY 24. THE AIRCRAFT LEFT AN OIL STAIN IN THE GRASS FOR 25 METERS. THE AIRCRAFT PITOT TUBE, NOSE WHEEL ASSEMBLY, AND WINDSHIELD PLEXIGLAS WERE SCATTERED FROM THE PERIMETER FENCE TO THE EDGE OF RUNWAY 24. PERIMETER FENCE MATERIAL WAS LIKEWISE SCATTERED IN THE GRASS AREA. THIS GRASS AREA IS APPROXIMATELY 50 METERS IN LENGTH. AFTER TRAVELING APPROXIMATELY 50 METERS IN THE GRASS ON AN AZIMUTH OF 240 DEGREES, THE AIRCRAFT STRUCK THE RUNWAY MARKING LIGHTS AT THE APPROACH END OF RUNWAY 24, AS EVIDENT BY PLEXIGLAS AND THE RUNWAY LIGHT IDENTIFICATION PLATE BEING TORN OFF OF THE LIGHT BASE. THE AIRCRAFT CONTINUED TO SKID UNTIL COMING TO A STOP APPROXIMATELY 50 FEET SHORT OF RUNWAY 24 THRESHOLD. THE LEFT HAND MAIN LANDING GEAR ASSEMBLY SEPARATED FROM THE AIRCRAFT AND WAS LOCATED APPROXIMATELY 25 FEET FORWARD OF THE NOSE OF THE AIRCRAFT.

THE PIC RECALLS TURNING OFF AIRCRAFT POWER SWITCHES, AND REMOVING THE KEYS, PRIOR TO FIRST RESPONDERS ARRIVING TO RENDER AID. THE PIC AND CFI WERE BOTH TRANSPORTED TO UCI MEDICAL CENTER FOR TREATMENT. THE PIC SUSTAINED ABRASIONS TO HIS LEFT ELBOW AND RIGHT HAND. THE CFI RECALLS BEING IN A STATE OF SHOCK, AND WAS ABLE TO CRAWL OUT OF THE AIRCRAFT, ON TO THE RIGHT HAND WING AND AWAIT FIRST RESPONDERS. THE CFI SUSTAINED BUMPS AND BRUISES FROM THE SEATBELT.

NTSB investigation

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