What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On November 26, 2003 at approximately 1500 central standard time N8058L, a Cessna 172H aircraft, departed Wichita Falls valley airport (F14) on a maintenance test flight with two occupants on board. Shortly after departure the engine lost power and the pilot-in-command, privacy data omitted, attempted a right hand turn to another runway for an emergency landing. The aircraft stalled and struck the ground in a nose low attitude. The nose wheel and engine were torn from the fuselage and the tail section aft of the baggage compartment was torn almost in half with the aircraft coming to rest inverted. Both occupants sustained minor injuries and were hospitalized 24 hours for observation. On-scene investigation of the aircraft revealed the inner lining of the aerquip fuel supply line from the gascolator to the carburetor had been damaged during assembly of the fittings on each end of the hose. This caused a restriction in the hose which would not allow adequate fuel flow to sustain full throttle operation of the engine.
As the FAA filed it
(-23) ON NOVEMBER 26, 2003 AT APPROXIMATELY 1500 CENTRAL STANDARD TIME N8058L, A CESSNA 172H AIRCRAFT, DEPARTED WICHITA FALLS VALLEY AIRPORT (F14) ON A MAINTENANCE TEST FLIGHT WITH TWO OCCUPANTS ON BOARD. SHORTLY AFTER DEPARTURE THE ENGINE LOST POWER AND THE PILOT-IN-COMMAND, ^PRIVACY DATA OMITTED^, ATTEMPTED A RIGHT HAND TURN TO ANOTHER RUNWAY FOR AN EMERGENCY LANDING. THE AIRCRAFT STALLED AND STRUCK THE GROUND IN A NOSE LOW ATTITUDE. THE NOSE WHEEL AND ENGINE WERE TORN FROM THE FUSELAGE AND THE TAIL SECTION AFT OF THE BAGGAGE COMPARTMENT WAS TORN ALMOST IN HALF WITH THE AIRCRAFT COMING TO REST INVERTED. BOTH OCCUPANTS SUSTAINED MINOR INJURIES AND WERE HOSPITALIZED 24 HOURS FOR OBSERVATION. ON-SCENE INVESTIGATION OF THE AIRCRAFT REVEALED THE INNER LINING OF THE AERQUIP FUEL SUPPLY LINE FROM THE GASCOLATOR TO THE CARBURETOR HAD BEEN DAMAGED DURING ASSEMBLY OF THE FITTINGS ON EACH END OF THE HOSE. THIS CAUSED A RESTRICTION IN THE HOSE WHICH WOULD NOT ALLOW ADEQUATE FUEL FLOW TO SUSTAIN FULL THROTTLE OPERATION 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 N8058L · 1
Matched to the same aircraft by N-number and date.