N651PW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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, 2005-06-02 – 2008-07-03.
Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM)
HORIZ PITCH TRIM CONTROL ADVISORY UNIT WAS REPLACED AND OPERATIONALLY CHECKED GOOD IAW MM 27-40-01. AT PREFLIGHT, PILOT NOTICED TRIM INDICATION WAS NORMAL, THEN IT BEGAN INDICATING MOVEMENT WHILE TRIM SWITCHES WERE NOT ENGAGED. WITH TRIM INDICATION AT TAKEOFF THE PILOT PERFORMED A VISUAL INSPECTION OF HORIZONTAL STAB POSITION AND CONFIRMED STAB POSITION WAS IN FULL DOWN WHILE INDICATOR SHOWED GREEN T/O MARK. FLIGHT WAS CANCELLED AND ANOTHER TRIM ADVISORY UNIT WAS ORDERED, UNIT WAS REPLACED THE NEXT DAY. UNIT WAS RECENTLY REPAIRED ON WO NR 1199756 DATED FEB 18, 2008 AND BOUGHT ON JULY 2, 2008 AND INSTALLED THAT SAME DATE. (K)
Part: STATIC PORT — LEAKING · airframe 9,335 hrs · 7,473 cycles
FOUND RT SIDE LOWER STATIC PORT SLIGHTLY LOOSE. REMOVED BOTH RT SIDE STATIC PORTS, CLEANED AREA ON INSIDE AND OUTSIDE OF AC. APPLIED PRIMER TO AFFECTED AREAS. INSTALLED (2) STATIC PORTS P/N-CM2933-7 ON RT SIDE OF AC WITH (8) CM3827AD-4 RIVETS.
Part: WHEEL — BROKEN (MLG)
DURING WEEKLY INSPECTION ON AIRCRAFT, IT WAS DISCOVERED THAT ONE THROUGH BOLT ON LT MAIN WHEEL IN NR 1 POSITION WAS BROKEN. AFTER FURTHER INSPECTION NR 2 POSITION WHEEL ON SAME LT LANDING GEAR HAD 2 BROKEN THROUGH BOLTS ADJACENT TO EACH OTHER. ALL BOLTS RETAINED AND AVAILABLE UPON REQUEST. (K)