N525MD
Registered owner: HAWAII PACIFIC AVIATION INC, HI (owner ≠ operator)
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.
12 reports on file, 1997-12-08 – 1998-02-19.
Part: PRSOV — INOPERATIVE (NR 2 ENGINE)
THE NR 2 PACK OVERHEATED WITH SMOKE ENTERING THE CABIN WHILE LEVELING OFF AT FL 280. THE AIRCRAFT WAS RETURNED TO DUS, WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE NR 2 ENGINE PRSOV WOULD NOT SHUT OFF ELECTRICALLY, CAUSING THE NR 2 PACK TO OVERTEMP AND TRIP. THE NR 2 PRSOV WAS LOCKED OUT MANUALLY AND THE NR 2 PNEUMATIC SYSTEM AND NR 2 PACK WERE PLACARDED INOPERATIVE. THE ENGINES WERE RUN AND ALL OPERATION CHECKED GOOD.
Part: SUPPORT — CORRODED (BS 1845)
INSPECTION FOUND FLOORBEAM SUPPORT ANGLE CORRODED AT STA 1845, RBL 25. THE SUPPORT WAS REMOVED AND A REPLACEMENT SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 53-16-0, AND 51-10-01.
Part: SPAR WEB — CRACKED (LT WING)
INSPECTION FOUND A 1.25 CRACK IN LT WING BOOST PUMP CUTOUT IN REAR SPAR AFT WEB ON PERIPHERY AND AFT FACE OF CUTOUT. THE CRACK WAS STOP DRILLED. DOUBLER, FILLER, AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 53 AND 51-31-01.
Part: SKIN — CRACKED (RT WING)
INSPECTION FOUND A 1.125 CRACK IN RT WING NR 9 SLAT TRACK CUTOUT NEAR FUELING PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 57-10-00. DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5710-01894 AND SRM 57-10-00.
Part: SKIN — CORRODED (RT RUDDER)
INSPECTION FOUND RT LOWER AFT RUDDER SKIN CORRODED ON BOTH TOP AND BOTTOM AREA. THE SKIN AND DOUBLER WERE REMOVED. NEW SKIN AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 55-42-0, 51-71-01, 51-21-01, AND 51-31-01.
Part: BRACKET — CRACKED (RT TE FLAP)
INSPECTION FOUND A 6 INCH CRACK IN RT INBOARD HINGE LOWER BULLET ATTACH BRACKET ON RT OUTBOARD FLAP. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 57-52-01 AND 51-21-01.
Part: LONGERON — CRACKED (CARGO COMPT)
INSPECTION FOUND A 21.5 CRACK IN AFT CARGO PIT LONGERON SPLICE. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 53-15-01.
Part: INTERCOSTAL — CRACKED (BS 1941-1951)
INSPECTION FOUND A 11 CRACK IN INTERCOSTAL OF AFT CARGO COMPARTMENT AT FS 1941 TO 1951, LONGERON 51R. THE INTERCOSTAL WAS REMOVED IAW SRM 53-31-01. A REPLACEMENT INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-15-01, 51-10-00, AND 51-31-01.
Part: SUPPORT — BROKEN (E/E COMPT)
INSPECTION FOUND FLOORBOARD SUPPORT BROKEN IN E AND E COMPARTMENT, LT AFT. THE ANGLE WAS REMOVED IAW SRM 51-31-01. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-37-01, 51-21-01, AND 51-31-01.
Part: BRACKET — CORRODED (BS 2033)
INSPECTION FOUND RT SIDE FAIRING SUPPORT BRACKET CORRODED AT STA 2033, LONGERON 24R. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-31-01, 53-17-01, FIGURE 5, AND 51-21-01.
Part: LONGERON — CORRODED (BS 1830)
INSPECTION FOUND LONGERON 45R CORRODED IN CENTER CARGO COMPARTMENT AT FS 1830. THE CORRODED SECTION WAS REMOVED IAW SRM 51-31-01. A NEW LONGERON SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-21-02 AND 51-31-01.
Part: SKIN — DENTED (BS 1007)
INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 1007, L41R. THE DENTED SECTION WAS REMOVED IAW SRM 53-50-00. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-50-00, FIGURE 8 SHEET 1 SRM 53-50-11 FIGURE 8 SHEET 1 AND SRM 51-33-01.