N932CE
Registered owner: TATONDUK OUTFITTERS LTD, AK (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.
15 reports on file, 2012-05-21 – 2018-10-19.
Part: INSERT — MISSING (RT ENGINE) · airframe 56,261 hrs · 45,308 cycles
ENGINE SHUTDOWN AT 1945 LOSS OF OIL QUANTITY AND OIL TEMP RISING. FOUND TREAD INSERT AND STUD LOST FROM RT ENGINE ACCY DRIVE CASE.
Part: SKIN — CRACKED (CARGO DOOR)
MAIN CARGO DOOR CORNER REPAIRS. REPAIR OF FUSELAGE SKIN CRACKS AT THE UPPER, FORWARD AND AFT CORNERS OF THE MAIN CARGO DOOR. REPAIR FUSELAGE SKIN CRACKS AT THE UPPER FORWARD AND AFT CORNER OF THE MAIN CARGO DOOR PER BOEING ISSUED 8900-9 AND BOEING SKETCH -09C.
Earlier reports · 2012–2017 · 13 reports
2017
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,011 hrs · 44,087 cycles
SKIN CRACK AT RIGHT HAND FUSELAGE STATION 1143 STRINGER RIGHT 14. MAJOR REPAIR OF CRACK PER SRM REFERENCE. REPAIR PER SRM 53-01 FIGURE 2 (SHEET 3).
2015
Part: SKIN — CRACKED (FUSELAGE)
SKIN CRACK AT STATION 466 AROUND LOWER VHF ANTENNA. A CRACK WAS FOUND IN THE VICINITY OF THE LOWER VHF ANTENNA WHILE PERFORMING A VISUAL INSPECTION REQUIRED BY AD 85-03-08R1. STOP DRILL CRACK & ACCOMPLISH REPAIR IAW ATTACHED MSGS. TNK-TNKK-15-0026-01C DATED MAY 27 2015 & TNK-TNK-15-0026-05B DATED MAY 29 2015.
2012
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,608 hrs · 40,789 cycles
AFT CARGO COMPARTMENT FROM BS 897 TO BS 889, BETWEEN LONG 28 - 29R,WEB CORRODED. REPAIRED WEB SECTION BETWEEN BS 889 AND BS 897 IAW SRM 51-70-4 FIG 2.
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,608 hrs · 40,789 cycles
AFT CARGO COMPARTMENT FROM BS 937 TO 945, BETWEEN LONG 25R AND 26R, WEB WITH CORROSION. REPAIRED WEB AT AFT CARGO COMPARTMENT FROM YSTA 937 TO YSTA 945, BETWEEN LONG 25R AND 26R, IAW SRM 51-70-4, FIG 2.
Part: FITTING — CRACKED (MLG DOOR) · airframe 51,608 hrs · 40,789 cycles
LOWER FUSELAGE LT INBD MLG DOOR INBD FWD SECTION FITTING WITH A CRACK. REPAIRED LT MLG DOOR INBD FWD FITTING IAW EO COO-9-52-189-12,DTD JULY 03, 2012.
Part: DOOR — CRACKED (RT MLG) · airframe 51,608 hrs · 40,789 cycles
LOWER FUSELAGE RT INBD MLG INBD FWD SECTION FITTING WITH A CRACK. REPAIRED RT MLG DOOR INBD FWD FITTING IAW EO COO-9-52-190-12, DTD JULY 03, 2012.
Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 51,608 hrs · 40,789 cycles
RT WING INBD SPOILER DAMAGED . REPAIRED RT WING INBD SPOILER, IAW EO COO-CMP-9-57-182-12.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,608 hrs · 40,789 cycles
LOWER FUSELAGE AFT CARGO COMPARTMENT BS 996 -X2,-Z11. WEB ON AFT CARGO COMPARTMENT STA 996 BETWEEN -X5 AND +X5, IAW EO COO-9-53-192-12,DTD JULY 09,2012.
Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,608 hrs · 40,789 cycles
LOWER FUSELAGE FWD CARGO COMPARTMENT MAIN CARGO TRACK LOWER SIDE WITH CORROSION FROM YSTA 351 TO YSTA 370 AND +X20. CARGO SEAT TRACK SECTION FROM YSTA 334 TO YSTA 445 AT +X 20 WAS REPAIRED IAW SRM 53-05, FIG 4F.
Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,608 hrs · 40,789 cycles
LOWER FUSELAGE FWD CARGO COMPARTMENT, SEAT TRACK LOWER SIDE WITH CORROSION FROM 427 TO 455 ST +X 40. REPAIRED CARGO SEAT TRACK SECTION FROM BS 314 TO 462.5 IAW SRM 53-05, FIG 4F.
Part: FRAME — CRACKED (ZONE 200) · airframe 51,608 hrs · 40,789 cycles
UPPER FUSELAGE AT YSTA 699 CARGO DECK WHEEL WELL FRAME RT FWD FITTING LOWER POCKET AFT FACE LOWER FLANGE AND INBD RADIUS CRAKED. REPLACED MAIN CARGO WHEEL WELL FRAME FITTING AT BS 699 RT SIDE IAW S/B 53-131, OPTION 2, FIG 3, REV 4.
Part: DOUBLER — CRACKED (ZONE 600) · airframe 51,608 hrs · 40,789 cycles
RT WING, FIXED L/E SKIN DOUBLER CRACKED AT XRS 286. REPAIRED IAW EO COO-9-57-180-12,.
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 51,608 hrs · 40,789 cycles
COCKPIT WINDOW FRAME CRACKED. PERFORMED A PERMANENT REPAIR IAW SB 53-290 R1. ACCOMPLISHED COCKPIT ENCLOSURE WINDOW LOWER SILL FRAMES PERMANENT REPAIRS IAW SB 53-290, REV 01.