20240318011109I

Incident · Minor damage

FAA incident report · Beech 35-C33A · Denison, TX · March 18, 2024

Date
March 18, 2024 · 18:14 local
Place
Denison, TX
Airport
North Texas Regional/Perrin Fld
Phase of flight
Takeoff: Departure Roll
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N488DD
Reported as
Beech 35-C33A
Reported engine
Continental IO-520 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
2,889 total140 in this make and model95 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.

Airman provided a written statement indicating that he had been practicing a power-off 180 maneuver and conducted a normal landing without incident with the intention of performing a touch-and-go. In the process of rolling out from the landing and resetting the aircraft the landing gear collapsed. The airman stated that during the process of resetting that he may have either bumped the landing gear switch, activated it, and quickly moved it back or he had some other mechanical issue. He stated that he was not 100% certain on what happened and while the landing was smooth he noticed a small bounce before the gear collapsed. The airman was asked what his normal reset procedure would be while performing a touch-and-go landing and he stated that he would typically retract the flaps, apply power, and lift back off the runway and once airborne with a positive rate of climb would retract the landing gear.

On scene investigation of the incident aircraft showed that it came to rest perpendicular to taxiway echo on runway 35R, approximately 2,750’ from the runway threshold. It was observed that the nose gear and nose gear door were completely retracted, the right main gear was partially retracted, and the left main gear was fully extended. The propeller tips were bent backward indicating the engine was running at the time of impact. It was also observed that the flaps were fully extended.

Propeller strike marks were observed on the runway centerline markings starting at approximately 340’ south of the aircraft location. Based on the distance between propeller strike marks on the ground it was estimated that the aircraft was traveling approximately 48-61KTS at the time of first impact.

Review of aircraft maintenance records showed aircraft was in compliance with inspection requirements and held a valid airworthiness & registration certificate. Review of pilot records and logbook showed pilot was in compliance with currency requirements and held the appropriate pilot certificate and medical to operate the aircraft.

As the FAA filed it

AIRMAN PROVIDED A WRITTEN STATEMENT INDICATING THAT HE HAD BEEN PRACTICING A POWER-OFF 180 MANEUVER AND CONDUCTED A NORMAL LANDING WITHOUT INCIDENT WITH THE INTENTION OF PERFORMING A TOUCH-AND-GO. IN THE PROCESS OF ROLLING OUT FROM THE LANDING AND RESETTING THE AIRCRAFT THE LANDING GEAR COLLAPSED. THE AIRMAN STATED THAT DURING THE PROCESS OF RESETTING THAT HE MAY HAVE EITHER BUMPED THE LANDING GEAR SWITCH, ACTIVATED IT, AND QUICKLY MOVED IT BACK OR HE HAD SOME OTHER MECHANICAL ISSUE. HE STATED THAT HE WAS NOT 100% CERTAIN ON WHAT HAPPENED AND WHILE THE LANDING WAS SMOOTH HE NOTICED A SMALL BOUNCE BEFORE THE GEAR COLLAPSED. THE AIRMAN WAS ASKED WHAT HIS NORMAL RESET PROCEDURE WOULD BE WHILE PERFORMING A TOUCH-AND-GO LANDING AND HE STATED THAT HE WOULD TYPICALLY RETRACT THE FLAPS, APPLY POWER, AND LIFT BACK OFF THE RUNWAY AND ONCE AIRBORNE WITH A POSITIVE RATE OF CLIMB WOULD RETRACT THE LANDING GEAR.

ON SCENE INVESTIGATION OF THE INCIDENT AIRCRAFT SHOWED THAT IT CAME TO REST PERPENDICULAR TO TAXIWAY ECHO ON RUNWAY 35R, APPROXIMATELY 2,750’ FROM THE RUNWAY THRESHOLD. IT WAS OBSERVED THAT THE NOSE GEAR AND NOSE GEAR DOOR WERE COMPLETELY RETRACTED, THE RIGHT MAIN GEAR WAS PARTIALLY RETRACTED, AND THE LEFT MAIN GEAR WAS FULLY EXTENDED. THE PROPELLER TIPS WERE BENT BACKWARD INDICATING THE ENGINE WAS RUNNING AT THE TIME OF IMPACT. IT WAS ALSO OBSERVED THAT THE FLAPS WERE FULLY EXTENDED.

PROPELLER STRIKE MARKS WERE OBSERVED ON THE RUNWAY CENTERLINE MARKINGS STARTING AT APPROXIMATELY 340’ SOUTH OF THE AIRCRAFT LOCATION. BASED ON THE DISTANCE BETWEEN PROPELLER STRIKE MARKS ON THE GROUND IT WAS ESTIMATED THAT THE AIRCRAFT WAS TRAVELING APPROXIMATELY 48-61KTS AT THE TIME OF FIRST IMPACT.

REVIEW OF AIRCRAFT MAINTENANCE RECORDS SHOWED AIRCRAFT WAS IN COMPLIANCE WITH INSPECTION REQUIREMENTS AND HELD A VALID AIRWORTHINESS & REGISTRATION CERTIFICATE. REVIEW OF PILOT RECORDS AND LOGBOOK SHOWED PILOT WAS IN COMPLIANCE WITH CURRENCY REQUIREMENTS AND HELD THE APPROPRIATE PILOT CERTIFICATE AND MEDICAL TO OPERATE THE AIRCRAFT.

Other reports on N488DD · 1

Matched to the same aircraft by N-number and date.