N964CE
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
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.
4 reports on file, 2020-03-26 – 2022-05-25.
Part: LONGERON SPLICE — CORRODED (ZONE 100)
CORRODED LONGERON AND SPLICES FROM F/STA 1211 TO 1259. TO REMOVE AND REPLACE A CORRODED LONGERON SECTION (29L) AND ITS TWO CORRODED SPLICES AT F/STA 1211 AND 1259. REMOVED CORRODED SPLICES AND STRINGER SECTION, REPLACE WITH NEW. PERFORM ALL WORK FROM DC-9/MD-80 SRM 53-02 PAGES 43 FIGURE 16.
Part: NONE — NONE
CORRODED ZEE CHANNELS AROUND COCKPIT WINDSHIELD. TO REPLACE CORRODED ZEE CHANNELS AT THE BOTTOM CORNERS OF THE CENTER WINDSHIELD. REMOVE CORRODED ZEE ANGLES, AND INSTALL NEW ONES FOLLOWING STANDARD PRACTICES PER DC-9/MD-80 SRM. INSTALL NEW PARTS WITH SAME TYPE AND SIZES AS REMOVED, RIVETS AND HI-LOKS, AND USE SUBSTITUTE FASTENERS IF REQUIRED.
Part: PUMP — FAULTED (FUEL BOOST) · airframe 59,085 hrs · 31,263 cycles
CENTER FUEL PRESSURE LOW LIGHT ILLUMINATED/CENTER TANK FAILS TO FEED IN FLIGHT. RAN QRH PROCEDURE.(FOUND AFT CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKER OPEN)
Part: SKIN — CRACKED (FUSELAGE)
SKIN DENTED AND CRACKED LONGERON AT F/STA 263 LONGERON 22R. TO REPAIR A DENT WITH CREASE ON THE FUSELAGE, AND A CRACK IN THE LONGERON AT F/STA 263, LONGERON 22R. PERFORM FUSELAGE SKIN REPAIR PER DC-9/MD-80 SRM 53-04-3 (SHEET 1) CLASS 1 REPAIR. PERFORM LONGERON REPAIR PER DC-9/MD-80 SRM 53-02 PARA, 12, AND FIGURE 18 (SHEET 1). USE DC-9/MD-80 SRM 51-60-0 PARA 5. H. HI-LOK FASTERNERS (1) (USE HL-18PB6 IN STRINGER FLANGES).