20030909031169A

Accident · Substantial damage

FAA accident report · Cessna 152 · Kissimmee, FL · September 9, 2003

Date
September 9, 2003 · 09:05 local
Place
Kissimmee, FL
Airport
Kissimmee Municipal Airport
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5172B
NTSB investigation
NTSBMIA03LA179
Reported as
Cessna 152
Reported engine
Lycoming O235*
Fatal injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
18 total18 in this make and model16 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.

(-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.