What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) After takeoff, during climb at an altitude of 200 to 300 feet, the student pilot on his second solo flight reported that the engine began to sputter and lost significant RPM. The student pilot turned left 180 degrees back towards the airport for an emergency landing. During the turn, the airplane lost significant altitude and it could not clear a stand of trees in a semi-swampy area on the northwest corner of the airport. As the airplane contacted the trees, it was near stalling speed. The student pilot sustained minor injuries. A post-accident inspection was performed by an airworthiness inspector on 09/11/2003. He found the following discrepancies: 1. Shielding was separated on 5 of the 8 ignition leads; 2. No. 2 cylinder lower ignition lead was misfiring into the shielding; 3. Excessive play in the carburetor throttle shaft; 4. The point gap on both magnetos was minimal, .004 and .008 with pitting evident; 5. The contacts on the distributer blocks of both magnetos were burned and worn; and 6. The fuel screen was very dirty. He concluded that the lack of proper maintenance on this engine was a likely contributing factor in this accident.
As the FAA filed it
(-23) AFTER TAKEOFF, DURING CLIMB AT AN ALTITUDE OF 200 TO 300 FEET, THE STUDENT PILOT ON HIS SECOND SOLO FLIGHT REPORTED THAT THE ENGINE BEGAN TO SPUTTER AND LOST SIGNIFICANT RPM. THE STUDENT PILOT TURNED LEFT 180 DEGREES BACK TOWARDS THE AIRPORT FOR AN EMERGENCY LANDING. DURING THE TURN, THE AIRPLANE LOST SIGNIFICANT ALTITUDE AND IT COULD NOT CLEAR A STAND OF TREES IN A SEMI-SWAMPY AREA ON THE NORTHWEST CORNER OF THE AIRPORT. AS THE AIRPLANE CONTACTED THE TREES, IT WAS NEAR STALLING SPEED. THE STUDENT PILOT SUSTAINED MINOR INJURIES. A POST-ACCIDENT INSPECTION WAS PERFORMED BY AN AIRWORTHINESS INSPECTOR ON 09/11/2003. HE FOUND THE FOLLOWING DISCREPANCIES: 1. SHIELDING WAS SEPARATED ON 5 OF THE 8 IGNITION LEADS; 2. NO. 2 CYLINDER LOWER IGNITION LEAD WAS MISFIRING INTO THE SHIELDING; 3. EXCESSIVE PLAY IN THE CARBURETOR THROTTLE SHAFT; 4. THE POINT GAP ON BOTH MAGNETOS WAS MINIMAL, .004 AND .008 WITH PITTING EVIDENT; 5. THE CONTACTS ON THE DISTRIBUTER BLOCKS OF BOTH MAGNETOS WERE BURNED AND WORN; AND 6. THE FUEL SCREEN WAS VERY DIRTY. HE CONCLUDED THAT THE LACK OF PROPER MAINTENANCE ON THIS ENGINE WAS A LIKELY CONTRIBUTING FACTOR IN THIS ACCIDENT.
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 N5172B · 1
Matched to the same aircraft by N-number and date.