# N754SA: 1978 Boeing 747-228F, registration cancelled 2014-11-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 18, 2014
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 747-228F](https://openairdocs.org/model/boeing-747-228f) (registry code 1384895)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 21576
- Year built: 1978
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: June 23, 2004
- Certificate issued: January 29, 2009
- Last registry action: January 29, 2009
- Mode S code: AA2A76
- Owner when cancelled: [Air Mobility Inc](https://openairdocs.org/faa-owner/AIR%20MOBILITY%20INC)
- Location: [Norwalk, CT](https://openairdocs.org/faa-place/CT/Norwalk)
- Owner type: Corporation
- Owner's area on the map: 41.1274° N, 73.4453° W: Placed by OpenAirDocs at the center of ZIP code 06850, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N754SA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=754SA
- Page: https://openairdocs.org/deregistered/N754SA-2014-11-18

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 747-228F: https://openairdocs.org/model/boeing-747-228f.md

## Service difficulty reports (13)

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

- [SDR Q2SA754013](https://openairdocs.org/sdr/Q2SA754013), May 14, 2011: FAN. FAULTY. AT 10,000 FEET, ELECTRICAL SMELL AND LIGHT SMOKE ENTERED THE COCKPIT. COMPLETED SMOKE SOURCE IDENTIFICATION PROCEDURE AND ELECTRICAL SYSTEM SMOKE OR FIRE CHECKL
- [SDR Q2SA754012](https://openairdocs.org/sdr/Q2SA754012), Apr 1, 2011: LINE. LOOSE. NR 1 HYDRAULIC SYSTEM QUANTITY LOW. RE-TORQUED HYDRAULIC LINE FROM THE NR 1 SYSTEM, RIGHT BODY GEAR DOOR LINE PER AMM 20-11-05, PG 401. OPERATIONAL AND LEAK CHE
- [SDR Q2SA754011](https://openairdocs.org/sdr/Q2SA754011), Mar 29, 2011: SEQUENCE VALVE. CRACKED. AFTER DEPARTURE FROM JNB, NR 1 ENGINE EDP AND ADP LOW HYDRAULIC PRESSURE LIGHTS ILLUMINATED. HYDRAULIC PRESSURE AND QUANTITY INDICATED "0". PERFORMED QRH PROCED
- [SDR Q2SA754010](https://openairdocs.org/sdr/Q2SA754010), Feb 9, 2011: FAN. VIBRATION. FLIGHT DECK FAN RUMBLES WITH OCCASIONAL BURNED ODOR, SWITCHED OFF AND CIRCUIT BREAKER PULLED. PERFORMED SMOKE INSPECTION REFERENCE AMM 5-51-00, NO DEFECTS NOTED
- [SDR Q2SA754009](https://openairdocs.org/sdr/Q2SA754009), Dec 11, 2010: CONNECTOR. DAMAGED. DURING INITIAL CLIMB, THE FIRE ENGINE WARNING BELL FOR NR1 ENGINE SOUNDED BRIEFLY. AT THAT TIME THE CREW PERFORMED AN INSTRUMENT SCAN AND FOUND THE ENGINE INDIC
- [SDR Q2SA754008](https://openairdocs.org/sdr/Q2SA754008), Nov 28, 2009: CONNECTOR. LOOSE. NR 1 LEFT L1 LOWER LOCK WIRE SMOKES IN FLIGHT EACH TIME HEAT CYCLES TO WINDOW. RE-SECURED L1 WINDOW HEAT CONNECTIONS AND OPS CHECKED IAW B747 AMM 30-40-00. OPS 
- [SDR Q2SA754007](https://openairdocs.org/sdr/Q2SA754007), Nov 27, 2009: UNKNOWN. ODOR. ON DESCENT, EVIDENCE OF STRONG ELECTRICAL ODOR EMITTING FROM FORWARD INSTRUMENT PANEL. ODOR APPEARS TO GO AWAY WHEN STORM LIGHTS ARE TURNED OFF. PERFORMED CONDI
- [SDR Q2SA754006](https://openairdocs.org/sdr/Q2SA754006), Oct 23, 2009: CLAMP. LOOSE. IN CRUISE, ENGINE FIRE WARNING ACTUATED FOR ENGINE NR 2, CREW BROUGHT ENGINE NR 2 TO IDLE POWER AND OPTED TO SHUTDOWN THE ENGINE IN ACCORDANCE WITH QUICK REFERE
- [SDR Q2SA754005](https://openairdocs.org/sdr/Q2SA754005), Sep 15, 2009: SEQUENCE VALVE. FAULTY. ON CLIMBOUT OF WIII, AFTER GEAR RETRACTION, WITH THE GEAR HANDLE IN THE UP POSITION THE NOSE LANDING GEAR HAD AN UNWANTED EXTENSION AND RETRACTION CYCLING. CREW
- [SDR 754004](https://openairdocs.org/sdr/754004), Nov 27, 2007: COMPUTER. NO TEST. AUTOPILOT A WILL NOT ENGAGE AND AUTOPILOT B IS ALREADY DEFERRED. DUMPED FUEL AND DIVERTED INTO RKSI. AUTOPILOT A ROLL COMPUTER DOES NOT PASS SELF TEST. REPLACED
- [SDR 754003](https://openairdocs.org/sdr/754003), Nov 22, 2007: CADC. MALFUNCTIONED. AUTOPILOT B ALTITUDE HOLD WOULD NOT CAPTURE OR HOLD ALTITUDE. VERTICAL SPEED COMMAND UNUSABLE AND MANUAL PITCH WHEEL CONTROL UNUSABLE. AUTOPILOT A PREVIOUSLY DE
- [SDR 754002](https://openairdocs.org/sdr/754002), Nov 12, 2007: CONTROL SYSTEM. UNSTABLE. DURING CLIMB-OUT, THE VERTICAL SPEED WHEEL MOVED TO FULL NOSE UP POSITION WITH "B" AUTOPILOT SELECTED. IN CRUISE AUTO STAB "B" LIGHT ILLUMINATED SEVERAL TIMES. 
- [SDR 754001](https://openairdocs.org/sdr/754001), Oct 28, 2007: FIRE LOOP. INOPERATIVE. DURING CLIMB-OUT, APU FIRE BELL AND LIGHTS ACTIVATED. APU FIRE CHECKLIST PERFORMED BUT DID NOT STOP BELL RINGING OR LIGHTS FLASHING. SELECTED FIRE WARNING SYSTE

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