N961CE

MCDONNELL DOUGLAS DC-9-82(MD-82) · 1987 · Valid Registration

Registered owner: ARCTIC ONE LLC, 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

O · 2023-03-02 Matched by certificate designator
ATA 5300

CORRODED ZEE CHANNEL REPLACEMENT, COCKPIT F.O./CENTER WINDSHIELD. REQUESTING AUTHORIZATION TO REPLACE ZEE CHANNEL AT LOWER INTERSECTION OF F.O'S AND CENTER WINDOWS. REMOVE AND REPLACE CORRODED ZEE ANGLE IAW DC-9/MD-80 SRM STANDARD PRACTICES. NEW ANGLE IS SAME TYPE AND SIZE AS REMOVED. HI-LOKS WILL BE SUBSTITUTED FOR MS20426AD RIVETS PER THE SRM.

Source: SDR FXGA202303022302 · FAA SDRS
N · 2022-11-11 Matched by certificate designator
ATA 5500

MAIN CARGO DOOR LATCHES REPAIR. DURING TORQUE TUBE ISSUES ON ABOVE AIRCRAFT, ALL LATCHES RESULTED WITH GOUGES CAUSED BY THE LOCK PINS. IN ORDER TO CONTINUE WITH LATCHES EVALUATION, IT WILL BE REQUIRED TO BLEND OUT THE LATCHES AND PROVIDE THE THICKNESS OF REMAINING MATERIAL. REQUIRED TO BLEND OUT THE LATCHES AND STATIC ANALYSIS OF AE5003 LEVERS #4 AND #7 WERE FOUND TO BE OF NEGATIVE MARGIN AND WILL NEED TO BE REPLACED. SEE APPENDIX A FOR STATIC ANALYSIS NOTES.

Source: SDR FXGA202211112229 · FAA SDRS
O · 2022-06-21 Matched by certificate designator
ATA 5200

SEAL RETAINER INSTALLATION - DEVIATION. DAMAGED SEAL RETAINER PN: AE5660-11 MUST BE REPLACED WITH ALTERNATE PN: AE5738-16. DURING A VISUAL INSPECTION AROUND THE DOOR, IT WAS FOUND A CRACKED SEAL RETAINER PN: AE5660-11 (SEE FIGURE 1). THUS, A SECTION OF EXISTING SEAL RETAINER IS GOING TO BE TRIMMED OUT AND WILL BE SUBSTITUTED WITH A SECTION OF SEAL RETAINER PN: AE5738-16, PER THE INSTRUCTIONS OF THIS ENGINEERING ORDER.

Source: SDR FXGA202206212218 · FAA SDRS
O · 2020-09-24 Matched by certificate designator
ATA 5330

FUSELAGE SKIN DAMAGED AT F/STA 533 BETWEEN STRINGERS 10L AND 11L. TO REPAIR A GOUGED SKIN BEHIND THE CARGO DOOR AT F/STA 533 BETWEEN STRINGERS 10L AND 11L. REPAIR DAMAGED SKIN, PER AEI EO11598. PERFORM SUPPLEMENTAL INSPECTION AT 10,100 CYCLES (THRESHOLD AND INTERVAL).

Source: SDR FXGA202009242014 · FAA SDRS