N69602
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.
11 reports on file, 2000-02-07 – 2007-01-04.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,284 hrs · 19,088 cycles
INSPECTION FOUND FORWARD CARGO DOOR CUTOUT FORWARD FRAME WEB CRACKED AT DOOR STOP FITTING FWD/LWR AREA, STA 400, S24R, WL 160. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,284 hrs · 19,088 cycles
INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AROUND SCREW HOLES AT STA 986.5, RBL 19 TO RBL 46. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A TEE REPAIR ANGLE AND STRAP WERE INSTALLED IAW ECRA 5310-04494, REPAIR OPTION B.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,284 hrs · 19,088 cycles
INSPECTION FOUND FLOORBEAM CORRODED AROUND HOLE AT STA 967, RBL 30. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-51, FIGURE 201.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,284 hrs · 19,088 cycles
INSPECTION FOUND FLOORBEAM CORRODED AROUND HOLES AT STA 967, LBL 30. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51.
Part: SKIN — DENTED (CARGO DOOR) · airframe 29,738 hrs · 15,667 cycles
INSPECTION FOUND FORWARD BAGGAGE BIN DOOR OUTER SKIN DENTED 15 INCHES FROM TOP AND 18 INCHES FROM AFT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,738 hrs · 15,667 cycles
INSPECTION FOUND AFT MAIN CABIN FLOORBEAM CORRODED AT FS 986, LBL 46. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-31, FIGURE 203.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 24,873 hrs · 13,035 cycles
INSPECTION FOUND RT TIE DOWN TRACK IN FRONT OF AFT CARGO THRESHOLD CORRODED AT STA 767-870. A NEW TRACK SECTION WAS INSTALLED IAW SRM 53-00-53.
Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 24,873 hrs · 13,035 cycles
INSPECTION FOUND LT TIE DOWN TRACK IN AFT CARGO COMPARTMENT CORRODED AT STA 877-947. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,873 hrs · 13,035 cycles
INSPECTION FOUND FOUR 1 INCH CRACKS IN CABIN FLOOR SUPPORT BETWEEN STA 482B AND 520, BL 0. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 24,873 hrs · 13,035 cycles
INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 540, RBL 1. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: FRAME — GOUGED (BS 1040)
INSPECTION FOUND BELTFRAME GOUGED BY TAIL COMPARTMENT PNEUMATIC DUCT CLAMP AT STA 1040. A REPAIR WAS INSTALLED IAW ECRA 5310-03981.