N750PA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PAN AMERICAN WORLD AWYS INC. | Operator | on 1979-09-30 | Operator named in NTSB report |
| PAN AMERICAN WORLD AWYS INC. | Operator | on 1971-02-07 | Operator named in NTSB report |
Accident & incident history
Operated by PAN AMERICAN WORLD AIRWAYS (per NTSB report)
Operated by PAN AMERICAN WORLD AWYS INC. (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
3 reports on file, 1998-11-10 – 2000-08-01.
Part: FUEL CONTROL — FAILED
DURING CRUISE, ENGINE WENT TO MAX POWER AND WAS UNCONTROLLABLE. ENGINE WOULD NOT RESPOND TO POWER LEVER OR EMERGENCY POWER LEVER. ENGINE WAS CONTINUOUSLY OVER TORQUE AND OVER TEMP LIMITS FOR 7 MINUTES. AIRCRAFT WAS FLOWN TO NEAREST AIRPORT BY CYCLING THE PROP IN AND OUT OF FEATHER. ALL ENGINE RIGGING WAS FOUND TO BE INTACT. SUBMITTER SUSPECTED FUEL CONTROL DRIVE SHAFT FAILURE. THIS EVENT IS STILL UNDER INVESTIGATION. (X)
Part: ROLL PIN — LOOSE (COCKPIT)
ROLL PIN SECURING AILERON TRIM CHAIN SPROCKET TO AILERON TRIM WHEEL ASSY WORKED OUT OF SHAFT RENDERING AILERON TRIM INOPERABLE. RE-INSTLALED ROLL PIN (ITEM 14 IN CESSNA 208 IPC CHAPTER 27-10-03 FIG 02). SAFETY WIRED ROLL PIN WITH .020 INCH SAFETY WIRE (ITEM 14) AND SAFETIED REMAINING ROLL PINS IN ASSY ITEMS 2, 12 (ITEM 12 IN TWO AREAS) TO PREVENT RECURRENCE.
Part: DUCT — DAMAGED (PRIMARY EXHAUST)
DURING A SCHEDULED INSPECTION, THE PRIMARY EXHAUST DUCT WAS FOUND TO HAVE A 2.5 BY 6.O INCH HOLE IN THE CENTER OF THE OUTBOARD SURFACE OF THE DUCT. THIS AREA IS LOCATED BEHIND THE OIL COOLER AND IS NOT VISIBLE WITH THE COWLING INSTALLED NO DAMAGE TO THE SURROUNDING COWLING WAS FOUND.