# N930FT: 1966 Boeing 727-23, registration cancelled 2006-08-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 8, 2006
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-23](https://openairdocs.org/model/boeing-727-23) (registry code 1384004)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 19387
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 16, 1984
- Certificate issued: August 22, 1995
- Last registry action: August 17, 2004
- Mode S code: ACE638
- Owner when cancelled: [Northern Air Cargo Inc](https://openairdocs.org/faa-owner/NORTHERN%20AIR%20CARGO%20INC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N930FT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=930FT
- Page: https://openairdocs.org/deregistered/N930FT-2006-08-08

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 727-23: https://openairdocs.org/model/boeing-727-23.md

## Service difficulty reports (21)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR NACA20030103](https://openairdocs.org/sdr/NACA20030103), Aug 6, 2003: PRESSURE SWITCH. FALSE INDICATION. NR 1 ENGINE OIL PRESSURE WARNING LIGHT(BYPASS), FLICKERING DURING CLIMB. INSPECTED NR 1 ENGINE MAIN OIL FILTER. NO METAL FOUND, INSTALLED NEW FILTER. DEFERRED O
- [SDR NACA20030101](https://openairdocs.org/sdr/NACA20030101), Aug 1, 2003: WARNING LIGHT. MALFUNCTIONED. AFTER TAKE-OFF THE WHEEL WELL FIRE WARNING ILLUMINATED AND BELL SOUNDED. BOTH EXTINGUISHED UPON GEAR EXTENSION. CREW REPORTED HEAVY BRAKING AT PAEN. INSPECTED W
- [SDR NACA20030096](https://openairdocs.org/sdr/NACA20030096), Jul 22, 2003: SWITCH. FALSE INDICATION. NR 2 SLAT INDICATES FORWARD AMBER LIGHT AND F.E. TRANSITE LIGHT WITH FLAPS UP. REPLACED NR 2 SLAT EXTEND SWITCH.
- [SDR NACA20030095](https://openairdocs.org/sdr/NACA20030095), Jul 21, 2003: ACTUATOR. FALSE INDICATION. NR 2 SLAT LIGHT ON IN FLT WITH FLAPS IN UP POSITION. REPLACED SLAT ACTUATOR.
- [SDR NACA20030085](https://openairdocs.org/sdr/NACA20030085), May 8, 2003: HINGE. CORRODED. LT WING KRUEGER FLAP MOUNT BRACKET HINGE ASSEMBLY CORRODED. REMOVED AND REPLACED HINGE ASSEMBLY.
- [SDR NACA20030082](https://openairdocs.org/sdr/NACA20030082), Apr 3, 2003: COUPLER. OSCILLATES. RIGHT ON TAKE-OFF, UPPER YAW DAMPER OSCILATE AUTO PILOT DISENGAGE, LIGHT STAYED ON, WIND SHEAR CAUTION LIGHT STAYS ON. REPLACED UPPER YAW DAMPER COUPLER AND TES
- [SDR NACA20030076](https://openairdocs.org/sdr/NACA20030076), Feb 11, 2003: ENGINE. SHORTED. DISCREPANCY: ABORTED TAKE OFF DUE TO #1 ENGINE OIL PRESSURE LIGHT ILLUMINATED.CORRECTIVE ACTION: REMOVED MOISTURE FROM OIL DIFFERENTIAL PRESSURE SWITCH CANNON P
- [SDR NACA20030073](https://openairdocs.org/sdr/NACA20030073), Feb 6, 2003: VOLT REGULATOR. TRIPPED. DISCREPANCY: ON TAKE OFF ROLL LOST #1 ENG GEN ESSENTIAL POWER WITH #3 ENGINE GENERATOR SELECTED.CORRECTIVE ACTION: REPLACED #1 VOLTAGE REGULATOR.
- [SDR NACA20020021](https://openairdocs.org/sdr/NACA20020021), May 21, 2002: SPAR CAP. CORRODED. DISCREPANCY: During "C" inspection, I.G. corrosion was discovered on the L/H wing aft spar lower chord, from w.s. 224.5 TO w.s. 241.0.CORRECTIVE ACTION: Lower s
- [SDR NACA20020036](https://openairdocs.org/sdr/NACA20020036), Mar 14, 2002: ATTACH FITTING. DURING "C" CHECK INSPECTION FOUND 2 EA STARTED DRILL HOLES IN THE ATTACH FITTING AT B.S. 1183, WL 278, AND RBL 27. CORRECTED BY INSTALLING 2 PIECE FREEZE PLUG, 
- [SDR NACA20010038](https://openairdocs.org/sdr/NACA20010038), Nov 10, 2001: SMOKE DETECTOR. MALFUNCTIONED. MECHANICAL INTERRUPTION IN ANCHORAGE AT 1522Z DUE TO LOWER CARGO FIRE WARNING HORN WENT OFF 3 TIMES. OPENED BOTH BELLY DOORS IMMEDIATELY UPON AIRCRAFT RETURN. F
- [SDR NACA2001018](https://openairdocs.org/sdr/NACA2001018), Apr 30, 2001: DISK. VIBRATION. MI AT ANC AT 2102Z, ENGINE SHUTDOWN DUE TO SEVERE VIBRATION. REMOVED AND REPLACED NR 1 ENGINE.
- [SDR NACA20010005](https://openairdocs.org/sdr/NACA20010005), Jan 23, 2001: CONTROL UNIT. MALFUNCTIONED. WITH ANTI SKID ON BRAKES RELEASED ON ROLLOUT. REPLACED ANTI SKID CONTROL MODULE.
- [SDR NACA20010004](https://openairdocs.org/sdr/NACA20010004), Jan 20, 2001: SWITCH. DIRTY. ON LANDING AT ANCHORAGE LOSS OF BRAKE, LOSS OF LEFT PACK, LOSS OF APU, GPWS, AND STICK SHAKER CAME ON. CLEANED NOSE GEAR SAFETY WARNING SWITCH.
- [SDR NACA200000018](https://openairdocs.org/sdr/NACA200000018), Aug 16, 2000: BRAKE. OVERHEATED. ON DOWN WIND AT AKN, WHEEL WELL WARNING LIGHT AND BELL SOUNDED. AS SOON AS THE GEAR WENT OUT AS PER PROCEDURES THE BELL AND LIGHT WENT OUT, VISUAL VERIFICATION 
- [SDR 98ZZZM502](https://openairdocs.org/sdr/98ZZZM502), Jun 1, 1998: LONGERON. WORN. DURING C-CHECK INSPECTION DISCOVERED WEAR MARKS ON THE LEFT AND RIGHT KEEL BEAM LONGERONS AT THE MAIN LANDING GEAR DOOR HINGES, STATION 947 LEFT AND STATION 910
- [SDR 98ZZZM501](https://openairdocs.org/sdr/98ZZZM501), Jun 1, 1998: SKIN. CRACKED. DURING C-CHECK INSPECTION DISCOVERED A CRACK IN THE FIXED LEADING EDGE SKIN AT RIGHT WING LEADING EDGE STATION 155. REPAIRED BY TRIMMING OUT THE CRACK, HFEC NDT
- [SDR 98ZZZM500](https://openairdocs.org/sdr/98ZZZM500), Jun 1, 1998: BULKHEAD FITTING. CORRODED. DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT BULKHEAD TERMINAL FITTING AT STATION 870. REPAIRED BY BLENDING AWAY THE CORROSION, HFEC NDT INSPECT
- [SDR 97ZZZX3523](https://openairdocs.org/sdr/97ZZZX3523), Jul 12, 1997: ACTUATOR. INACCURATE. ANC - FLT 74 - RETURNED TO ANC AT 0235Z DUE TO NR 7 LEADING EDGE SLAT INDICATING IN-TRANSIT. MAINTENANCE REPLACED NR 7 LEADING EDGE SLAT ACTUATOR DUE TO FAULTY 
- [SDR 97ZZZX3517](https://openairdocs.org/sdr/97ZZZX3517), Jun 8, 1997: SLAT ACTUATOR. LEAKING. ON TAKEOFF ROLL, A-SYSTEM LOW LEVEL LIGHT CAME ON, TAXIED OFF AT BRAVO TO COMPANY RAMP. MAINTENANCE REPLACED NR 5 LEADING EDGE SLAT ACTUATOR AND RETURNED AIRCRA
- [SDR 96ZZZX1465](https://openairdocs.org/sdr/96ZZZX1465), Jan 10, 1996: WINDSHIELD. CRACKED. ANC - FLT 105 - RETURNED TO ANC DUE TO FAILURE OF CAPTAIN'S WINDSHIELD OUTER PANEL. MAINTENANCE REPLACED L1 WINDOW. REPLACED WINDSHIELD HEAT CONTROLLER AS A PRE

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19980319007919I](https://openairdocs.org/incident/19980319007919I), Mar 19, 1998: Boeing 72723 (N930FT). Narrative: ptrs-AL039812348. Aircraft lost "a" system hydraulic pressure in cruise flight. A/b interconnect left closed. Manual gear extension was made. A/c…
- [Accident 19900131064399A](https://openairdocs.org/incident/19900131064399A), Jan 31, 1990: Boeing 72723 (N930FT), Indianapolis, IN, Minor damage, 1 fatal. Tug rolled forward and pinned driver between aircraft and tug while operator was attaching tow hook.
- [Incident 19870401016499I](https://openairdocs.org/incident/19870401016499I), Apr 1, 1987: Boeing 72723 (N930FT), St Louis, MO. Low oil pressure light during climb with pressure drop. Returned with engine shutdown. Oil pump drive had failed.

## Other aircraft with N930FT

- [Registered now](https://openairdocs.org/aircraft/N930FT): Bombardier BD-700-1A10, S/N 60209, built 2025

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