20010414006939A

Accident · Substantial damage

FAA accident report · Piper PA-28-235 · Flagstaff, AZ · April 14, 2001

Date
April 14, 2001 · 12:24 local
Place
Flagstaff, AZ
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8731W
NTSB investigation
NTSBLAX01LA147
Reported as
Piper PA28235
Reported engine
Lycoming O540B4B5
People aboard
1
Fatal injuries
0
Pilot’s flight hours
262 total20 in this make and model11 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 April 14, 2001, about 1224 hours MST a Piper PA-28-235, N8731W, sustained substantial damage when it made a hard, forced landing on a highway following a loss of engine power about 30 miles northwest of Flagstaff, AZ. The pilot was operating the borrowed airplane under the provisions of 14 CFR part 91. The private pilot, the sole occupant was not injured. The personal cross-country flight departed cedar city, Utah about 1130, enroute to deer valley, Arizona. Visual meteorological conditions prevailed. No flight plan had been filed. The FAA accident coordinator interviewed the pilot. The pilot said he completed a 2.5 hour flight from deer valley to cedar city. He started the return flight on the right wing tip tank. He switched to the left wing tip tank near page, AZ. About 20 minutes later the engine began to run rough, and then it lost all power. The pilot did not switch fuel tanks again. He made a hard landing on a road, which sheared all three landing gear from the airplane. (-23)on April 14, 2001, Piper aircraft N8731W was at cruise flight at 11,500 MSL near Flagstaff, AZ. When the engine quit. The pilot made several uns uccessful attempts to start the engine. The pilot attempted to land on a paved road but aborted due to auto traffic. The pilot made an emergency forced landing next to the paved road,thirty miles north of Flagstaff. The aircraft sustained damage to the propeller, engine, landing gear, underside fuselage, wings and empennage. The aircraft was operated by the pilot/owner as a personal flight under CFR part 91. Visual meteorological conditions prevailed at the time, the pilot was not injured. (.4) on April 14, 2001, about 1224 hours mountain standard time, a Piper PA-28-235, N8731W, sustained substantial damage when it made a hard, forced landing near a highway following a loss of engine power about 30 miles northwest of Flagstaff, Arizona. The pilot was operating the borrowed airplane under the provisions of 14 CFR part 91. The private pilot, the sole occupant, was not injured. The personal cross-country flight departed cedar city, Utah, about 1130, en route to deer valley, Arizona. Visual meteorological conditions prevailed. No flight plan had been filed. The federal aviation administration)accident coordinator interviewed the pilot. The pilot said he c ompleted a 2.5-hour flight from deer valley to cedar city in the morning and did not experience any problems with the airplane. He filled all four fuel tanks in cedar city. He started the return flight on the right wing tip tank. He switched to the left wing tip tank near page, Arizona. About 20 minutes later the engine began to run rough, and then it lost all power. The pilot did not switch fuel tanks again. In his statement to the safety board, the pilot stated he did not switch fuel tanks because he believed there was "ample fuel in left tip." The pilot set up to land on a highway, but a traffic conflict forced him to land in terrain alongside the road. He landed the airplane approximately 70 yards from the highway and all three landing gear sheared off.

As the FAA filed it

(.19) ON APRIL 14, 2001, ABOUT 1224 HOURS MST A PIPER PA-28-235, N8731W, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT MADE A HARD, FORCED LANDING ON A HIGHWAY FOLLOWING A LOSS OF ENGINE POWER ABOUT 30 MILES NORTHWEST OF FLAGSTAFF, AZ. THE PILOT WAS OPERATING THE BORROWED AIRPLANE UNDER THE PROVISIONS OF 14 CFR PART 91. THE PRIVATE PILOT, THE SOLE OCCUPANT WAS NOT INJURED. THE PERSONAL CROSS-COUNTRY FLIGHT DEPARTED CEDAR CITY, UTAH ABOUT 1130, ENROUTE TO DEER VALLEY, ARIZONA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. NO FLIGHT PLAN HAD BEEN FILED. THE FAA ACCIDENT COORDINATOR INTERVIEWED THE PILOT. THE PILOT SAID HE COMPLETED A 2.5 HOUR FLIGHT FROM DEER VALLEY TO CEDAR CITY. HE STARTED THE RETURN FLIGHT ON THE RIGHT WING TIP TANK. HE SWITCHED TO THE LEFT WING TIP TANK NEAR PAGE, AZ. ABOUT 20 MINUTES LATER THE ENGINE BEGAN TO RUN ROUGH, AND THEN IT LOST ALL POWER. THE PILOT DID NOT SWITCH FUEL TANKS AGAIN. HE MADE A HARD LANDING ON A ROAD, WHICH SHEARED ALL THREE LANDING GEAR FROM THE AIRPLANE. (-23)ON APRIL 14, 2001, PIPER AIRCRAFT N8731W WAS AT CRUISE FLIGHT AT 11,500 MSL NEAR FLAGSTAFF, AZ. WHEN THE ENGINE QUIT. THE PILOT MADE SEVERAL UNS UCCESSFUL ATTEMPTS TO START THE ENGINE. THE PILOT ATTEMPTED TO LAND ON A PAVED ROAD BUT ABORTED DUE TO AUTO TRAFFIC. THE PILOT MADE AN EMERGENCY FORCED LANDING NEXT TO THE PAVED ROAD,THIRTY MILES NORTH OF FLAGSTAFF. THE AIRCRAFT SUSTAINED DAMAGE TO THE PROPELLER, ENGINE, LANDING GEAR, UNDERSIDE FUSELAGE, WINGS AND EMPENNAGE. THE AIRCRAFT WAS OPERATED BY THE PILOT/OWNER AS A PERSONAL FLIGHT UNDER CFR PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME, THE PILOT WAS NOT INJURED. (.4) ON APRIL 14, 2001, ABOUT 1224 HOURS MOUNTAIN STANDARD TIME, A PIPER PA-28-235, N8731W, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT MADE A HARD, FORCED LANDING NEAR A HIGHWAY FOLLOWING A LOSS OF ENGINE POWER ABOUT 30 MILES NORTHWEST OF FLAGSTAFF, ARIZONA. THE PILOT WAS OPERATING THE BORROWED AIRPLANE UNDER THE PROVISIONS OF 14 CFR PART 91. THE PRIVATE PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. THE PERSONAL CROSS-COUNTRY FLIGHT DEPARTED CEDAR CITY, UTAH, ABOUT 1130, EN ROUTE TO DEER VALLEY, ARIZONA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. NO FLIGHT PLAN HAD BEEN FILED. THE FEDERAL AVIATION ADMINISTRATION)ACCIDENT COORDINATOR INTERVIEWED THE PILOT. THE PILOT SAID HE C OMPLETED A 2.5-HOUR FLIGHT FROM DEER VALLEY TO CEDAR CITY IN THE MORNING AND DID NOT EXPERIENCE ANY PROBLEMS WITH THE AIRPLANE. HE FILLED ALL FOUR FUEL TANKS IN CEDAR CITY. HE STARTED THE RETURN FLIGHT ON THE RIGHT WING TIP TANK. HE SWITCHED TO THE LEFT WING TIP TANK NEAR PAGE, ARIZONA. ABOUT 20 MINUTES LATER THE ENGINE BEGAN TO RUN ROUGH, AND THEN IT LOST ALL POWER. THE PILOT DID NOT SWITCH FUEL TANKS AGAIN. IN HIS STATEMENT TO THE SAFETY BOARD, THE PILOT STATED HE DID NOT SWITCH FUEL TANKS BECAUSE HE BELIEVED THERE WAS "AMPLE FUEL IN LEFT TIP." THE PILOT SET UP TO LAND ON A HIGHWAY, BUT A TRAFFIC CONFLICT FORCED HIM TO LAND IN TERRAIN ALONGSIDE THE ROAD. HE LANDED THE AIRPLANE APPROXIMATELY 70 YARDS FROM THE HIGHWAY AND ALL THREE LANDING GEAR SHEARED OFF.

NTSB investigation

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