What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) N49811, a Cessna 152, was brought to its maintenance base (kpao) due to a squawk that complained the engine was running rich and not developing full power. The a&p/ia mechanic made the following engine logbook entry on 2/01/08: "removed carburetor to clear obstruction causing engine to run rich. Reinstalled carb iaw Cessna 152 mm." Shortly after takeoff on the ferry flight back to its operations base, N49811 experienced a loss of power causing the pilot to return to kpao. The engine lost power on short final. The airplane landed hard, causing substantial damage to the structure. Inspection of the aircraft after the accident revealed the following deficiencies: 1. Carburetor heat air valve seals were missing fore and aft preventing the valve to seal. 2. The carburetor fuel drain plug was not safety wired. 3. Water was found in the carburetor bowl assembly. 4. The number 1 cylinder had zero compression. This case has been referred to the airworthiness unit for investigation of these maintenance deficiencies.
As the FAA filed it
(-23) N49811, A CESSNA 152, WAS BROUGHT TO ITS MAINTENANCE BASE (KPAO) DUE TO A SQUAWK THAT COMPLAINED THE ENGINE WAS RUNNING RICH AND NOT DEVELOPING FULL POWER. THE A&P/IA MECHANIC MADE THE FOLLOWING ENGINE LOGBOOK ENTRY ON 2/01/08: "REMOVED CARBURETOR TO CLEAR OBSTRUCTION CAUSING ENGINE TO RUN RICH. REINSTALLED CARB IAW CESSNA 152 MM." SHORTLY AFTER TAKEOFF ON THE FERRY FLIGHT BACK TO ITS OPERATIONS BASE, N49811 EXPERIENCED A LOSS OF POWER CAUSING THE PILOT TO RETURN TO KPAO. THE ENGINE LOST POWER ON SHORT FINAL. THE AIRPLANE LANDED HARD, CAUSING SUBSTANTIAL DAMAGE TO THE STRUCTURE. INSPECTION OF THE AIRCRAFT AFTER THE ACCIDENT REVEALED THE FOLLOWING DEFICIENCIES: 1. CARBURETOR HEAT AIR VALVE SEALS WERE MISSING FORE AND AFT PREVENTING THE VALVE TO SEAL. 2. THE CARBURETOR FUEL DRAIN PLUG WAS NOT SAFETY WIRED. 3. WATER WAS FOUND IN THE CARBURETOR BOWL ASSEMBLY. 4. THE NUMBER 1 CYLINDER HAD ZERO COMPRESSION. THIS CASE HAS BEEN REFERRED TO THE AIRWORTHINESS UNIT FOR INVESTIGATION OF THESE MAINTENANCE DEFICIENCIES.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.