N801HC
Registered owner: AIRLINE CONTRACT MAINTENANCE AND EQUIPMENT 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.
89 reports on file, 2013-10-18 – 2019-12-28.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION LT WINDOW NR 12 LOWER AREA BETWEEN FRAMES 29-30. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0087723_01...13704 ISSUE B, DATED 1/10/2020.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION AT NR 8 WINDOW UPPER AREA FRAMES 24-25. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0088003_01...13701 ISSUE B, DATED 1/1/2020.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION AT RT WING LOWER TRAILING EDGE BETWEEN RIBS 13-15. CORRECTIVE ACTION: REPAIR PER SRAS ES-609/16...9999 ISSUE F, DATED 1/10/2020.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION LT WINDOW NR 6 TOP AREA BETWEEN FRAMES 23-24. CORRECTIVE ACTION: REPAIR PER SRAS ES_0087717_01...13705 ISSUE B, DATED 1/10/2020.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION LT WINDOW 10 UPPER AREAS BETWEEN FRAMES 27-28. CORRECTIVE ACTION: REPAIR PER SRAS ES_0087717_01...13705 ISSUE B, DATED 1/10/2020.
Part: SUPPORT — CORRODED (RT WING) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION ON RT WING SCAN LIGHT ASSY/SUPPORT. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0087717_01...13705 ISSUE B, DATED 1/10/2020.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION LT WING LOWER TRAILING EDGE BETWEEN RIBS 21-22. CORRECTIVE ACTION: REPAIR PER SRAS ES-608/16...10011 ISSUE F, DATED 1/10/2020.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION FWD CARGO DOOR CUT OUT FWD UPPER AREA AT FRAME 14. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0087479_01...13687 ISSUE B, DATED 1/7/2020.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION LT WINDOW NR 9 BOTTOM AREA BETWEEN FRAMES 26-27. CORRECTIVE ACTION: REPAIR PER SRAS ES_0087717_01...13705 ISSUE B, DATED 1/10/2020.
Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: LEVEL 2 CORROSION AT RT UPPER WING RIB 5 AROUND PANEL 622CT. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112679_01...15741 ISSUE A, DATED 1/10/2020.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,762 hrs · 32,847 cycles
MINOR REPAIR: FUSELAGE SKIN LEVEL 2 CORROSION FRAME 13 BUTT JOINT BETWEEN STRINGERS 2-6 ON LT SIDE. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112469_01...15723 ISSUE A, DATED 1/10/2020.
Part: DOOR — OBSTRUCTED (COMMS) · airframe 22,713 hrs · 30,096 cycles
FLIGHT 625, ENROUTE LNY - HNL, AIR TURNBACK. DISCREPANCY: ON CLIMB OUT OF LNY, THE CREW NOTICED A LOUD AIR NOISE COMING FROM LEFT SIDE OF AIRCRAFT. CREW WAS UNABLE TO DETERMINE THE SOURCE OF THE NOISE, SO ELECTED TO RETURN TO LNY. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE FOUND AND REMOVED DEBRIS ON COCKPIT COMMUNICATIONS DOOR. PERFORMED FUSELAGE PRESSURIZATION LEAK TEST. CHECKS GOOD WITH NO FURTHER DEFECTS.
Earlier reports · 2013–2018 · 77 reports
2018
Part: KEELBEAM — CORRODED (FRAME 27A) · corrosion level 2 · airframe 22,653 hrs · 29,998 cycles
WO 188750 NR 100061 HEAVY CHECK COE/MINOR REPAIR: KEEL BEAM FWD OF FRAME 27A HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.
Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 22,653 hrs · 29,998 cycles
WO 188750 NR 500042 HEAVY CHECK COE/MINOR REPAIR: LH WING LOWER TRAILING EDGE DROP DOWN PANEL 531AB MIDDLE HINGE SUPPORT ATTACH PLATE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED HINGE WITH OEM PART.
Part: HINGE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 22,653 hrs · 29,998 cycles
WO 188750 NR 500041 HEAVY CHECK COE/MINOR REPAIR: LH WING LOWER TRAILING EDGE DROP DOWN PANEL 531AB INBOARD HINGE SUPPORT ATTACH PLATE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED HINGE WITH OEM PART.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 22,653 hrs · 29,998 cycles
WO 188750 NR 300025 HEAVY CHECK COE/MINOR REPAIR: RH HORIZONTAL LEADING EDGE HAS LEVEL 2 CORROSION ON THE ATTACH FLANGE MATING SURFACE. CORRECTIVE ACTION: REPLACED LEADING EDGE.
Part: SKIN — CORRODED (E/E BAY DOOR) · corrosion level 2 · airframe 22,653 hrs · 29,998 cycles
WO 188750 NR 800006 HEAVY CHECK COE/MINOR REPAIR: AVIONICS DOOR HAS LEVEL 2 CORROSION ON EXTERIOR SURFACE. CORRECTIVE ACTION: REPLACED DOOR ASSY. WITH OEM.
Part: SKIN — CORRODED (E/E BAY) · corrosion level 2 · airframe 22,653 hrs · 29,998 cycles
WO 188750 NR 800005 HEAVY CHECK COE/MINOR REPAIR: AVIONICS DOOR HAS LEVEL 2 CORROSION AT AFT END ON INTERIOR SURFACE. CORRECTIVE ACTION: REPLACED DOOR ASSY WITH OEM.
Part: ACCESS PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,653 hrs · 29,998 cycles
WO 188750 NR 100034 HEAVY CHECK COE/MINOR REPAIR: EXTERIOR FUSELAGE, ACCESS PANEL FOR FWD CARGO DOOR CONTROL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED PANEL WITH OEM.
Part: STRINGER — CORRODED (FRAMES 39-40) · corrosion level 2 · airframe 22,106 hrs · 28,584 cycles
STRINGER 15L HAD CORROSION BETWEEN FRAMES 39 - 40. REPLACED THE STRINGER.
Part: STRUCTURE — CORRODED (RT SERVICE DOOR) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
RIGHT SERVICE DOOR, OUTBOARD STRUCTURE HAD 2 CORROSION. REPLACED.
Part: FLOORBEAM — CORRODED (FRAME 40) · corrosion level 2 · airframe 22,106 hrs · 28,584 cycles
FLOORBEAM AT FRAME 40 WAS EXFOLIATED, JUST INBOARD OF THE LT CREASE BEAM WEB. PERFORMED A FLOORBEAM SPLICE REPAIR IAW SRM 530000-300-837-A01.
Part: WEB — CORRODED (THRESHOLD) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
INTERIOR FUSELAGE, SERVICE DOOR THRESHOLD WEB HAD CORROSION. REPLACED THE WEB.
Part: FLOORBEAM — CORRODED (FRAME 38) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
FLOORBEAM AT FRAME 38, TOP SURFACE HAD CORROSION. REPLACED THE FLOORBEAM.
Part: WEB — CORRODED (FRAMES 36-39) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
PASSENGER DOOR THRESHOLD WEB HAD CORROSION. REPLACED WITH THE THRESHOLD WEB.
Part: SUPPORT PLATE — CORRODED (FRAME 40) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
INTERIOR FUSELAGE, LAVATORY SUPPORT PLATE HAD CORROSION. REPLACED THE SUPPORT PLATE.
Part: SPAR — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
LEFT WING SLAT REAR SPAR STRIP HAD CORROSION BETWEEN RIBS 17 - 21. REPAIRED IAW SRAS PCE-1855/18.
Part: SPAR — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
LEFT WING SLAT REAR SPAR UPPER STRIP HAD CORROSION, BETWEEN RIBS 14 - 17. REPAIRED IAW SRAS PCE-1855/18.
Part: SEAT TRACK — CORRODED (FRAMES 41-42) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
RIGHT SEAT TRACK HAD CORROSION BETWEEN FRAMES 41 - 42. REPLACED THE SEAT TRACK.
Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 22,106 hrs · 28,584 cycles
LEFT WING REMOVABLE PANEL 521DT HAD FRETTING CORROSION. REPLACED THE PANEL.
Part: SKIN — CORRODED (RT WING LOWER) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
RIGHT WING LOWER SKIN, TRAILING EDGE AT RIB 23 HAD CORROSION. REPAIRED IAW ES-609/16.10000, ISSUE D.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
LT WING LOWER SKIN AT THE TRAILING EDGE HAD CORROSION BETWEEN RIBS 26 & 27. REPAIRED IAW SRAS ES-608/16.
Part: SKIN — CORRODED (LT WING LOWER) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
LEFT WING LOWER SKIN AT THE TRAILING EDGE, RIB 13 WAS CORRODED. REPAIRED IAW SRAS ES-608/16.
Part: FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
RIGHT WING LOWER SURFACE RIB 13 PIANO FITTING HAD CORROSION. REPAIRED IAW SRAS CE-564/16.
Part: SKIN — CORRODED (RT WING LOWER) · corrosion level 2 · airframe 22,106 hrs · 28,585 cycles
RIGHT WING, LOWER SKIN AT THE TRAILING EDGE HAD CORROSION BETWEEN RIBS 13 - 16. REPAIRED IAW SRAS ES-609/16.
2017
Part: PROBE — MALFUNCTIONED (RT WING)
NR ENGINE EXPERIENCED A FLAMEOUT DURING DESCENT. CREW DECLARED EMERGENCY. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER ISSUE. CREW REPORTED A LOW LEVEL FUEL LIGHT LOCAL ALERT ILLUMINATED ON CAP DURING CLIMB OUT. CREW STATED THE RIGHT ENGINE ELECTRIC FUEL PUMP TURNED ON. CREW REPORTED AN INDICATION OF OVER 2000 POUNDS TOTAL AND 1000 POUNDS OF FUEL IN TANK AND NO INDICATION OF A FUEL LEAK. DURING DESCENT WITH AN INDICATION OF 900 POUNDS OF FUEL REMAINING IN THE RIGHT FUEL TANK, THE RIGHT ENGINE FLAMEDOUT. MAINTENANCE PERSONNEL VERIFIED THE INCORRECT INDICATION OF FUEL QUANTITY IN THE RIGHT WING. MAINTENANCE REMOVED AND REPLACED THE FUEL PROBES IN RIGHT WING. OPS CHECKED GOOD. NR 3 FUEL PROBE WAS DETERMINED TO HAVE CAUSED THE INCORRECT QUANTITY INDICATION.
Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 21,654 hrs · 27,423 cycles
MAJOR REPAIR/DISCREPANCY: LEVEL 2 CORROSION ON RT LOWER WING BETWEEN RIBS 13-15 ON TRAILING EDGE. DETERMINED TO BE A MAJOR REPAIR ON 11/2/2017 PER SRAS. REPAIR PER SRAS ES-609/16...9999 ISSUE D.
Part: SHUTOFF VALVE — FAULTED (NR 2 BLEED AIR) · airframe 21,282 hrs · 26,435 cycles
NR 2 ENGINE BLEED FAULT DURING CLIMB OUT. CREW ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE BLEED AIR SHUTOFF VALVE.
Part: SWITCH — MALFUNCTIONED · airframe 20,663 hrs · 24,771 cycles
AIR TURNBACK, IDLE GATE FAILED ON CCAS IN FLIGHT. CREW ELECTED TO RETURN TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED SWITCH 150KR WITH SOLDER. ADJUSTED AND SECURED SWITCH. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
2016
Part: DOOR — DAMAGED (SERVICE)
SERVICE DOOR REMOVED FROM 801HC FOR AN AIR LEAK. DAMAGE TO LOWER FWD CORNER. REPAIRED IAW CETS-5119/16.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT WING, HINGE FOR LE PANEL 511 HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.
Part: SKIN PANEL — DAMAGED (RT WING) · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. RT WING LOWER SKIN PANEL HAS A DENT WITH A GOUGE & ADJACENT GOUGE OTBD OF RIB 10, BETWEEN STIFFENERS 9 - 10. REPAIR IAW SRAS ES-1000 16 100056 DATED 3 10 16.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT FRAME 6, FLANGE DAMAGED BELOW WL 2327.5. REPAIR IAW SRAS S531R0335 10057 DATED 3 10 2016.
Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & /MAJOR REPAIR. NOSE FUSELAGE LT LOWER FWD SKIN PANEL HAS PERFORATION & SURROUNDING DENT AT FRAME 6. REPAIRED IAW SRAS S531R0335 10057 DATED 3 10 2016.
Part: FITTING — CORRODED (CARGO DOOR) · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. FWD CARGO DOOR, FWD LATCH FITTING, FWD CTR HOLE HAS CORROSION INSIDE. REPAIRED IAW SRAS CE 964 16 10029 DATED 2 26 16.
Part: SKIN PANEL — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT HORIZONTAL STABILIZER LE PANEL 331 HAS LEVEL 2 CORROSION INSIDE AROUND FASTENER HOLES. REPAIR PER SRAS CE 524 16 10014 DATED 2 26 16.
Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE, RT LATERAL LOWER SKIN PANEL HAS LEVEL 2 CORROSION UNDER THE SERVICE DOOR SCUFF PLATE. REPAIR IAW SRAS CE 588 16 9955 DATED 2 17 16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. RT INBD SEAT TRACK HAS AREAS OF BARE METAL & LEVEL 2 CORROSION, BETWEEN FRAMES 34 - 36. REPAIR IAW SRM 530000-300-853-A01.
Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE, DROP DOWN PANEL 632AB, INBD ROLLER BRACKET HAS LEVEL 2 CORROSION. REPLACED BRACKET WITH OEM PART.
Part: GUIDE — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION ON LT OTBD FLAP RIB 11 CAM GUIDE. REPLACED CAM GUIDE WITH OEM PART.
Part: BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE DROP DOWN PANEL 632BB, MIDDLE ROLLER BRACKET HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE DROP DOWN PANEL 631AB, HINGE HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION ON AFT SECTION OF FRAME 45, UNDER FLANGE & BY MICRO SWITCH ON FWD SIDE OF FRAME. REPLACED WITH OEM PART.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION LOCATED ON AFT SECTION OF FRAME, UNDER FLANGE & BY MICRO SWITCH ON FWD SIDE OF FRAME 45 ON SHEAR TIE. REPLACED WITH OEM PART.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. RT WING OUTER LOWER SKIN HAS LEVEL 2 CORROSION ALONG THE TE, BETWEEN RIBS 22 - 23. REPAIRED IAW SRAS ES 609 16 10000 DATED 2 19 2016.
Part: SKATE ANGLE — CORRODED (LT NACELLE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT NACELLE INBD SKATE ANGLE AT TE, HAS LEVEL 2 CORROSION. REPAIR IAW BLEND SRM 571540-300-801-A01.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT WING LOWER SKIN HAS LEVEL 2 CORROSION AT TE, BETWEEN RIBS 6 - 8. REPAIR IAW SRAS ES 762 16 10015 DATED 2 25 16.
Part: RUB STRIP — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING UPPER OTBD TE, OTBD FLAP RUB STRIP HAS LEVEL 2 CORROSION. REPLACED STRIP WITH SRM PART.
Part: RUB STRIP — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING UPPER INBD TE FLAP RUB STRIP HAS LEVEL 2 CORROSION. REPLACED STRIP WITH SRM PART.
Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE, LOWER SKIN PANEL HAS LEVEL 2 CORROSION AROUND THE LT OUTFLOW VLV OUTLET. REPAIRED IAW SRAS CE 499 16 9956 DATED 2 17 16.
Part: SKIN — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. SERVICE DOOR EXTERIOR SKIN HAS LEVEL 2 CORROSION AROUND FWD & LOWER EDGES. REPAIRED IAW SRAS CE 584 16 9950 DATED 2 17 2016.
Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT WING LOWER SKIN TE HAS LEVEL 2 CORROSION, BETWEEN RIBS 21 - 22. REPAIR IAW SRAS ES 608 16 10011 2 23 2016.
Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT WING LOWER SKIN TE HAS LEVEL 2 CORROSION, BETWEEN RIBS 17 - 20. REPAIR IAW SRAS ES 608 16 10011 DATED 2 23 2016.
Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LEFT WING LOWER SKIN TE HAS LEVEL 2 CORROSION AT RIB 13. REPAIR IAW SRAS ES 608 16 10011 DATED 2 23 16.
Part: RUB STRIP — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING UPPER OTBD TE, INBD FLAP RUB STRIP HAS LEVEL 2 CORROSION. REPLACED WITH FABRICATED STRIPS.
Part: HINGE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. POTABLE WATER SERVICE DOOR HINGE HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. EXTERIOR FUSELAGE SKIN AFT OF SERVICE DOOR, HAS LEVEL 2 CORROSION STRINGER 14. REPAIRED IAW SRAS CE 588 16 9955 DATED 2 17 16.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. EXTERIOR FUSELAGE SKIN AROUND THE LAVATORY SERVICE, HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 499 16 9956 DATED 2 17 16.
Part: RUB STRIP — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LT WING UPPER OTBD TE FLAP RUB STRIP HAS LEVEL 2 CORROSION. REPLACED STRIP WITH SRM PART.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT WING LOWER SKIN TE HAS LEVEL 2 CORROSION, BETWEEN RIBS 26 - 27. REPAIR IAW SRAS ES 608 16 10011 DATED 2 23 16.
Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING PANEL 632AB HINGE HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. EXTERIOR FUSELAGE SKIN FWD OF SERVICE DOOR, STRINGER 14 HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 588 16 9955 DATED 2 17 2016.
Part: DOOR — CORRODED (LAVATORY SERVICE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
WO 153570 NR 100012 HEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION ON EXTERIOR SURFACE OF LAVATORY SERVICE DOOR PANEL. REPLACED LAVATORY SERVICE DOOR PANEL WITH OEM PART.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. RT WING LOWER SURFACE HAS LEVEL 2 CORROSION ALONG RIB 13. REPAIRED IAW SRAS CE 564 16 9976 DATED 2 15 16.
Part: RUB STRIP — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. RT WING UPPER OTBD TE FLAP RUB STRIP HAS LEVEL 2 CORROSION. REPLACED WITH FABRICATED STRIP.
Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE LOWER SKIN PANEL HAS LEVEL 2 CORROSION, AROUND LT AFT STATIC PORT. REPAIR IAW SRAS CE 499 16 9956 DATED 2 17 2016.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT LOWER WING HAS LEVEL 2 CORROSION ALONG RIB 13. REPAIR IAW SRAS CE 565 16 9959 DATED 2 11 2016.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LT WING PANEL 531AB, INBD, HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LT WING PANEL 531AB HINGE, OTBD, HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.
Part: RUB STRIP — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LT WING UPPER INBD TE FLAP RUB STRIP HAS LEVEL 2 CORROSION. REPLACED STRIP WITH SRM PART.
Part: RETAINER — CORRODED (TE FLAP) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LT WING UPPER OTBD TE RUB STRIP RETAINERS HAS LEVEL 2 CORROSION. REPLACED STRIPS WITH SRM PART.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. LT WING LOWER SKIN TE HAS LEVEL 2 CORROSION, BETWEEN RIBS 28 - 29. REPAIR IAW SRAS ES 608 16 10011 DATED 2 23 16.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. EXTERIOR FUSELAGE SKIN, AROUND THE POTABLE WATER SERVICE DOOR, HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 500 16 9949 DATED 2 25 16.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. EXTERIOR FUSELAGE SKIN BY THE FWD EDGE OF LT EMER EXIT HAS LEVEL 2 CORROSION STRINGER 8. REPAIR IAW SRAS CE 476 16 9942 DATED 2 11 16.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LT WING PANEL 532AB, HINGE, OTBD, HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MAJOR REPAIR. RT WING OUTER LOWER SKIN HAS LEVEL 2 CORROSION ALONG THE TE, BETWEEN RIB 13 - 15. REPAIR PER SRAS ES-609 16 9999 DATED 2 19 16.
Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 19,455 hrs · 21,880 cycles
HEAVY CHECK COE & MINOR REPAIR. LT WING PANEL 532AB HINGE, INBD, HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.
2015
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,228 hrs · 21,334 cycles
MAJOR REPAIR, LEVEL 2 CORROSION DAMAGE TO SKIN FWD OF AFT AVIONICS BAY DOOR. REPAIR IAW EO 5330-09 BASED ON SRI CE-5752 15-26296, SRAS TO FOLLOW AFTER REPAIR COMPLETE.
2013
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,320 hrs · 16,520 cycles
HEAVY CHECK, MAJOR REPAIR. UPPER FUSELAGE FWD ADF ANTENNA MOUNT AREA HAS LEVEL 2 CORROSION. REPAIR IAW SRAS DT S 6084 13 8058 11/19/2013.