19981103039929A

Accident · Substantial damage

FAA accident report · Piper STCPA12 · Willow, AK · November 3, 1998

Date
November 3, 1998 · 14:50 local
Place
Willow, AK
Airport
Willow
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5129Y
NTSB investigation
NTSBANC99LA011
Reported as
Piper STCPA12
Reported engine
Lycoming O320A2B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
77 total14 in this make and model4 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.

(.19) On November 3, 1998, about 1450 Alaska standard time, a wheel equipped Piper PA-12 airplane, N5129Y, sustained substantial damage following a loss of engine power and subsequent off airport forced landing about 15 miles northeast of Willow, Alaska. The airplane was being operated as a visual flight rules (VFR) local area personal flight under title 14, CFR part 91, when the accident occurred. The certificated private pilot, and the one passenger aboard were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. During a telephone conversation with the national transportation safety board investigator-in-charge on November 4, 1998, the pilot reported that while in cruise flight at 1,000 feet MSL, all engine power was lost. He stated that all attempts to restore engine power failed, forcing him to select an open meadow as an emergency landing area. During the ensuing landing roll, the airplane's main landing gear contacted soft tundra, and the airplane nosed over. The airplane sustained substantial damage to the wings, fuselage and tail. (.4) the certificated private pilot reported that while in cruise flight at 1,000 feet MSL, all engine power lost. He stated that all attempts to restore engine power failed, forcing him to select an open swampy meadow as an emergency landing area. During the ensuing landing roll, the airplane's main landing gear contacted soft tundra, and the airplane nosed over. The airplane sustained substantial damage to the wings, fuselage and tail. The NTSB investigator-in-charge did not have access to the airplane or engine after recovery, and was unable to perform a postaccident inspection. (-23) during flight cruise at an altitude of between 900 and 1000 feet, the engine lost power. Pilot switch from the right fuel tank which was 3/4 full to the left fuel tank which was full. The engine did not respond. Pilot then advanced the throttle to the maximum power setting with no response from the engine. Pilot then used the engine primer to try and restart the engine. The engine seemed to try to restart once, but did not actually restart. Engine primer would not buildup pressure even though there was fuel in both fuel tanks. Pilot landed the aircraft in a clearing. During the rollout the tires broke through the frozen ground causing the aircraft to flip over onto its back there were no injuries. The aircraft sustained substantial damage. Aircraft removed from the accident site by helicopter and is located at the Willow Airport.

As the FAA filed it

(.19) ON NOVEMBER 3, 1998, ABOUT 1450 ALASKA STANDARD TIME, A WHEEL EQUIPPED PIPER PA-12 AIRPLANE, N5129Y, SUSTAINED SUBSTANTIAL DAMAGE FOLLOWING A LOSS OF ENGINE POWER AND SUBSEQUENT OFF AIRPORT FORCED LANDING ABOUT 15 MILES NORTHEAST OF WILLOW, ALASKA. THE AIRPLANE WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) LOCAL AREA PERSONAL FLIGHT UNDER TITLE 14, CFR PART 91, WHEN THE ACCIDENT OCCURRED. THE CERTIFICATED PRIVATE PILOT, AND THE ONE PASSENGER ABOARD WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED. DURING A TELEPHONE CONVERSATION WITH THE NATIONAL TRANSPORTATION SAFETY BOARD INVESTIGATOR-IN-CHARGE ON NOVEMBER 4, 1998, THE PILOT REPORTED THAT WHILE IN CRUISE FLIGHT AT 1,000 FEET MSL, ALL ENGINE POWER WAS LOST. HE STATED THAT ALL ATTEMPTS TO RESTORE ENGINE POWER FAILED, FORCING HIM TO SELECT AN OPEN MEADOW AS AN EMERGENCY LANDING AREA. DURING THE ENSUING LANDING ROLL, THE AIRPLANE'S MAIN LANDING GEAR CONTACTED SOFT TUNDRA, AND THE AIRPLANE NOSED OVER. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE TO THE WINGS, FUSELAGE AND TAIL. (.4) THE CERTIFICATED PRIVATE PILOT REPORTED THAT WHILE IN CRUISE FLIGHT AT 1,000 FEET MSL, ALL ENGINE POWER LOST. HE STATED THAT ALL ATTEMPTS TO RESTORE ENGINE POWER FAILED, FORCING HIM TO SELECT AN OPEN SWAMPY MEADOW AS AN EMERGENCY LANDING AREA. DURING THE ENSUING LANDING ROLL, THE AIRPLANE'S MAIN LANDING GEAR CONTACTED SOFT TUNDRA, AND THE AIRPLANE NOSED OVER. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE TO THE WINGS, FUSELAGE AND TAIL. THE NTSB INVESTIGATOR-IN-CHARGE DID NOT HAVE ACCESS TO THE AIRPLANE OR ENGINE AFTER RECOVERY, AND WAS UNABLE TO PERFORM A POSTACCIDENT INSPECTION. (-23) DURING FLIGHT CRUISE AT AN ALTITUDE OF BETWEEN 900 AND 1000 FEET, THE ENGINE LOST POWER. PILOT SWITCH FROM THE RIGHT FUEL TANK WHICH WAS 3/4 FULL TO THE LEFT FUEL TANK WHICH WAS FULL. THE ENGINE DID NOT RESPOND. PILOT THEN ADVANCED THE THROTTLE TO THE MAXIMUM POWER SETTING WITH NO RESPONSE FROM THE ENGINE. PILOT THEN USED THE ENGINE PRIMER TO TRY AND RESTART THE ENGINE. THE ENGINE SEEMED TO TRY TO RESTART ONCE, BUT DID NOT ACTUALLY RESTART. ENGINE PRIMER WOULD NOT BUILDUP PRESSURE EVEN THOUGH THERE WAS FUEL IN BOTH FUEL TANKS. PILOT LANDED THE AIRCRAFT IN A CLEARING. DURING THE ROLLOUT THE TIRES BROKE THROUGH THE FROZEN GROUND CAUSING THE AIRCRAFT TO FLIP OVER ONTO ITS BACK THERE WERE NO INJURIES. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE. AIRCRAFT REMOVED FROM THE ACCIDENT SITE BY HELICOPTER AND IS LOCATED AT THE WILLOW AIRPORT.

NTSB investigation

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

Other reports on N5129Y · 2

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