19971126043249A

Accident · Destroyed

FAA accident report · Piper PA-32-300 · Obyan, Northern Mariana Islands · November 26, 1997

Date
November 26, 1997 · 07:22 local
Place
Obyan, Northern Mariana Islands
Airport
Saipan International
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Operator
PIVA
Damage
Destroyed
Aircraft
N1256H
NTSB investigation
NTSBLAX98LA046
Reported as
Piper PA32300
Reported engine
Lycoming IO540K1G5
Fatal injuries
0
Pilot’s flight hours
3,000 total50 in this make and model90 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.

Pilot reported left side engine cylinders seperated on a maintenance test flight for engine vibrations. Ditched. (.4)the pilot was conducting a maintenance test flight in the traffic pattern when the engine lost power and he made a forced landing. Two days before the accident test flight, a company pilot made an unscheduled landing due to a rough running engine with a vibration. A review of the aircraft inspection discrepancy logs and maintenance records revealed that maintenance personnel removed and cleaned the fuel injector nozzles, the servo unit screen was flushed, and a compression check was completed. Four engine ground runs were conducted with a rough running engine and vibrations noted in the first three runs. The fourth ground run did not note any anomalies. Review of the records found two operator's inspection discrepancy records for this aircraft. Examination of the documents disclosed that they are essentially the same, except for item number 3. On the first document the item 3 discrepancy stated that the no. 5 cylinder fuel injector nozzle needed replacement, with a further note that none were in stock. On the second docume nt item 3 said that the fuel injector nozzles were cleaned and reinstalled, and that a ground run-up was normal. The company dispatcher instructed the pilot to perform the test flight as the airplane scheduled to return to service the same day. The pilot performed the ground checklist, which included checking the magnetos and propeller. He did not note any discrepancies. After takeoff no engine performance malfunctions were noted; however, while on base leg, the aircraft engine banged three times and then parts flew through the engine colwing. The colwing separated and struck the empennage. The pilot subsequently ditched the aircraft in the ocean, where it sank and was not recovered. (-23)the aircrft sustained a catastrophic engine failure while performing a maintenance test flight. The aircraft was lost in water approxiamtely 200' deep and was not recovered. This investigation concluded that the cause of the accident was catastropic engine failure of unknown origin.

As the FAA filed it

PILOT REPORTED LEFT SIDE ENGINE CYLINDERS SEPERATED ON A MAINTENANCE TEST FLIGHT FOR ENGINE VIBRATIONS. DITCHED. (.4)THE PILOT WAS CONDUCTING A MAINTENANCE TEST FLIGHT IN THE TRAFFIC PATTERN WHEN THE ENGINE LOST POWER AND HE MADE A FORCED LANDING. TWO DAYS BEFORE THE ACCIDENT TEST FLIGHT, A COMPANY PILOT MADE AN UNSCHEDULED LANDING DUE TO A ROUGH RUNNING ENGINE WITH A VIBRATION. A REVIEW OF THE AIRCRAFT INSPECTION DISCREPANCY LOGS AND MAINTENANCE RECORDS REVEALED THAT MAINTENANCE PERSONNEL REMOVED AND CLEANED THE FUEL INJECTOR NOZZLES, THE SERVO UNIT SCREEN WAS FLUSHED, AND A COMPRESSION CHECK WAS COMPLETED. FOUR ENGINE GROUND RUNS WERE CONDUCTED WITH A ROUGH RUNNING ENGINE AND VIBRATIONS NOTED IN THE FIRST THREE RUNS. THE FOURTH GROUND RUN DID NOT NOTE ANY ANOMALIES. REVIEW OF THE RECORDS FOUND TWO OPERATOR'S INSPECTION DISCREPANCY RECORDS FOR THIS AIRCRAFT. EXAMINATION OF THE DOCUMENTS DISCLOSED THAT THEY ARE ESSENTIALLY THE SAME, EXCEPT FOR ITEM NUMBER 3. ON THE FIRST DOCUMENT THE ITEM 3 DISCREPANCY STATED THAT THE NO. 5 CYLINDER FUEL INJECTOR NOZZLE NEEDED REPLACEMENT, WITH A FURTHER NOTE THAT NONE WERE IN STOCK. ON THE SECOND DOCUME NT ITEM 3 SAID THAT THE FUEL INJECTOR NOZZLES WERE CLEANED AND REINSTALLED, AND THAT A GROUND RUN-UP WAS NORMAL. THE COMPANY DISPATCHER INSTRUCTED THE PILOT TO PERFORM THE TEST FLIGHT AS THE AIRPLANE SCHEDULED TO RETURN TO SERVICE THE SAME DAY. THE PILOT PERFORMED THE GROUND CHECKLIST, WHICH INCLUDED CHECKING THE MAGNETOS AND PROPELLER. HE DID NOT NOTE ANY DISCREPANCIES. AFTER TAKEOFF NO ENGINE PERFORMANCE MALFUNCTIONS WERE NOTED; HOWEVER, WHILE ON BASE LEG, THE AIRCRAFT ENGINE BANGED THREE TIMES AND THEN PARTS FLEW THROUGH THE ENGINE COLWING. THE COLWING SEPARATED AND STRUCK THE EMPENNAGE. THE PILOT SUBSEQUENTLY DITCHED THE AIRCRAFT IN THE OCEAN, WHERE IT SANK AND WAS NOT RECOVERED. (-23)THE AIRCRFT SUSTAINED A CATASTROPHIC ENGINE FAILURE WHILE PERFORMING A MAINTENANCE TEST FLIGHT. THE AIRCRAFT WAS LOST IN WATER APPROXIAMTELY 200' DEEP AND WAS NOT RECOVERED. THIS INVESTIGATION CONCLUDED THAT THE CAUSE OF THE ACCIDENT WAS CATASTROPIC ENGINE FAILURE OF UNKNOWN ORIGIN.

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 N1256H · 1

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