20100321031609A

Accident · Substantial damage

FAA accident report · Beech 95-B55 (T42 · Medford, NJ · March 21, 2010

Date
March 21, 2010 · 14:30 local
Place
Medford, NJ
Airport
Flying W Airport
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1572L
NTSB investigation
NTSBERA10LA193
Reported as
Beech 95-B55 (T42
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
25,000 total300 in this make and model6 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.

While performing VFR patterns and landing practice to runway 19 at the Flying W Airport the cabin door popped open on the downwind leg. The pilot who was the sole occupant lowered the gear and observed it as down and locked. The open door was distacting and caused turbulence and buffeting. The pilot elected to fly the approach at a slightly higher airspeed at 115 - 120 mph on final as opposed to the normal approach speed of 100 mph. The pilot stated that the landing was not hard and he touched down in a flat attitude. After touchdown on the runway numbers and approximately 500 feet into the rollout the gear collapsed with the nose gear first then the right gear and then the left gear. The aircraft slid approximately 1500 feet. The pilot brought all the power quadrant levers back and exited the aircraft uninjured.

As the FAA filed it

WHILE PERFORMING VFR PATTERNS AND LANDING PRACTICE TO RUNWAY 19 AT THE FLYING W AIRPORT THE CABIN DOOR POPPED OPEN ON THE DOWNWIND LEG. THE PILOT WHO WAS THE SOLE OCCUPANT LOWERED THE GEAR AND OBSERVED IT AS DOWN AND LOCKED. THE OPEN DOOR WAS DISTACTING AND CAUSED TURBULENCE AND BUFFETING. THE PILOT ELECTED TO FLY THE APPROACH AT A SLIGHTLY HIGHER AIRSPEED AT 115 - 120 MPH ON FINAL AS OPPOSED TO THE NORMAL APPROACH SPEED OF 100 MPH. THE PILOT STATED THAT THE LANDING WAS NOT HARD AND HE TOUCHED DOWN IN A FLAT ATTITUDE. AFTER TOUCHDOWN ON THE RUNWAY NUMBERS AND APPROXIMATELY 500 FEET INTO THE ROLLOUT THE GEAR COLLAPSED WITH THE NOSE GEAR FIRST THEN THE RIGHT GEAR AND THEN THE LEFT GEAR. THE AIRCRAFT SLID APPROXIMATELY 1500 FEET. THE PILOT BROUGHT ALL THE POWER QUADRANT LEVERS BACK AND EXITED THE AIRCRAFT UNINJURED.

NTSB investigation

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