19961111035049A

Accident · Destroyed

FAA accident report · Cessna 152 · Grand Canyon, AZ · November 11, 1996

Date
November 11, 1996 · 11:05 local
Place
Grand Canyon, AZ
Airport
Valle Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N714VX
NTSB investigation
NTSBLAX97LA037
Reported as
Cessna 152
Reported engine
Lycoming O235L2C
Fatal injuries
0
Pilot’s flight hours
138 total102 in this make and model5 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.

Witness reported that the aircraft wobbled and crashed nose first shortly after takeoff. (.4)according to the pilot, during initial climb, the engine gradually lost power. Subsequently, it crash landed on uneven/rocky terrain and came to rest against trees in an inverted attitude. Density altitude was computed to be about 7,300 feet. The pilot reported that prior to the flight, when he first started the engine, no indication of oil pressure was observed. He shut down the engine and purchased 1 quart of oil. No abnormal indications were observed during the subsequent ground check out or takeoff roll. However, during the initial climb, the oil pressure indicator dropped to zero pounds. A teardown examination of the engine was performed. The crankshaft assembly revealed signatures consistent with heat distress in the number 2 main journal area. The oil pump's drive shaft was found broken. A foreign metal object was observed wedged between the teeth of the pump's driving and driven gears, and the engagement end of the oil pump drive shaft was found sheared off. The foreign object resembled a small bolt or screw, which was not used in the manufacture of the engine.

As the FAA filed it

WITNESS REPORTED THAT THE AIRCRAFT WOBBLED AND CRASHED NOSE FIRST SHORTLY AFTER TAKEOFF. (.4)ACCORDING TO THE PILOT, DURING INITIAL CLIMB, THE ENGINE GRADUALLY LOST POWER. SUBSEQUENTLY, IT CRASH LANDED ON UNEVEN/ROCKY TERRAIN AND CAME TO REST AGAINST TREES IN AN INVERTED ATTITUDE. DENSITY ALTITUDE WAS COMPUTED TO BE ABOUT 7,300 FEET. THE PILOT REPORTED THAT PRIOR TO THE FLIGHT, WHEN HE FIRST STARTED THE ENGINE, NO INDICATION OF OIL PRESSURE WAS OBSERVED. HE SHUT DOWN THE ENGINE AND PURCHASED 1 QUART OF OIL. NO ABNORMAL INDICATIONS WERE OBSERVED DURING THE SUBSEQUENT GROUND CHECK OUT OR TAKEOFF ROLL. HOWEVER, DURING THE INITIAL CLIMB, THE OIL PRESSURE INDICATOR DROPPED TO ZERO POUNDS. A TEARDOWN EXAMINATION OF THE ENGINE WAS PERFORMED. THE CRANKSHAFT ASSEMBLY REVEALED SIGNATURES CONSISTENT WITH HEAT DISTRESS IN THE NUMBER 2 MAIN JOURNAL AREA. THE OIL PUMP'S DRIVE SHAFT WAS FOUND BROKEN. A FOREIGN METAL OBJECT WAS OBSERVED WEDGED BETWEEN THE TEETH OF THE PUMP'S DRIVING AND DRIVEN GEARS, AND THE ENGAGEMENT END OF THE OIL PUMP DRIVE SHAFT WAS FOUND SHEARED OFF. THE FOREIGN OBJECT RESEMBLED A SMALL BOLT OR SCREW, WHICH WAS NOT USED IN THE MANUFACTURE OF THE ENGINE.

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 N714VX · 1

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