NK11A

No registry detail on file · not in current registry

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.

7 reports on file, 2009-11-23 – 2020-07-26.

OTHER · 2020-07-26 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (BS 986-1006) · corrosion level 2 · airframe 52,308 hrs · 34,675 cycles

CORROSION ON INTERNAL SKIN BY #1 FASTENER HOLE OF REMOVED DRAIN MAST LOCATED @ STA 986-1006 BETWEEN STR 24L & 25L

Source: SDR K11A2020080300005
OTHER · 2019-04-27 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (BS 229-237) · corrosion level 2 · airframe 51,402 hrs · 62,857 cycles

FLOOR WEB CORRODED STA 229 - 237 RBL 50 - 60

Source: SDR K11A2019061991706
OTHER · 2016-08-07 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles

FLOOR WEB CORROSION.

Source: SDR K11A2016110291524
OTHER · 2016-07-20 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,789 hrs · 75,837 cycles

FUSELAGE EXTERIOR CORROSION JUST AFT OF THE AFT CARGO DOOR.

Source: SDR K11A2016110291517
OTHER · 2016-04-19 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,897 hrs · 20,509 cycles

STA 351, RBL 17 TO LBL 17 WEB CORD HAS CORROSION.

Source: SDR K11A2016062829007
OTHER · 2010-10-01 Matched by certificate designator
ATA 5720

Part: PIN — DAMAGED (RT WING) · airframe 39,939 hrs · 22,371 cycles

RT AFT BOTTLE PIN DAMAGED.

Source: SDR K11A2010121372611
OTHER · 2009-11-23 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,771 hrs · 33,411 cycles

MAIN DECK FLOORBEAM UPPER CHORD, AFT LWR FLANGE HAS CORROSION.

Source: SDR K11A2009112372504