# N758SA: 1984 Boeing 747-281F, registration cancelled 2015-12-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 23, 2015 - Status when cancelled: Third renewal notice - Airframe: [Boeing 747-281F](https://openairdocs.org/model/boeing-747-281f) (registry code 13848AB) - Engine: [GE CF6-50E2](https://openairdocs.org/engine/ge-cf6-50e2) (registry code 30089) - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 23138 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 20, 2006 - Certificate issued: January 23, 2009 - Last registry action: January 23, 2009 - Mode S code: AA3952 - 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/N758SA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=758SA - Page: https://openairdocs.org/deregistered/N758SA-2015-12-23 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 747-281F: https://openairdocs.org/model/boeing-747-281f.md ## Service difficulty reports (28) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR Q2SA2012072875813](https://openairdocs.org/sdr/Q2SA2012072875813), Jul 28, 2012: SKIN. FAILED. DURING POST-FLIGHT, FOUND A HOLE AND CRACK DAMGE AT SECTION 48 LH SIDE BETWEEN STATION 2638 AND 2658 AND S-11L AND S-13L. STRINGER (P/N 65B 02976-1) CHORD (P/N - [SDR TX9Y20111214011](https://openairdocs.org/sdr/TX9Y20111214011), Dec 11, 2011: CARGO TRACK. CRACKED. FORWARD CARGO TRACK FORWARD RIGHT CORNER WAS FOUND CRACKED. REPAIRED AS PER SRM 53-10-05 FIG 5 REV 120. - [SDR TX9Y20111208008](https://openairdocs.org/sdr/TX9Y20111208008), Dec 7, 2011: STRUCTURE. CORRODED. LT WING T/E INBOARD MID FLAP T/E LOWER CHORD WAS FOUND CORROSION. THREE CORROSION AREAS WERE FOUND ON LEFT T/E INBOARD MID FLAP (P/N:65B02025-35) T/E LOWER CHOR - [SDR TX9Y20111208009](https://openairdocs.org/sdr/TX9Y20111208009), Dec 7, 2011: MOUNT. CORRODED. NR 4 ENG AFTER UPPER ENG MOUNT UPPER SURFACE WAS FOUND RUSTED HEAVILY. NR 4 ENGINE AFTER ENGINE MOUNT WAS REPLACED AS PER AMM 71-21-03 REV 86. - [SDR TX9Y20111208010](https://openairdocs.org/sdr/TX9Y20111208010), Dec 7, 2011: SKIN. CRACKED. DURING REMOVING TWO ADDITIONAL DOUBLERS, THREE HOLE CRACK ON THE LEFT DOUBLER FUSELAGE SKIN AND TWO HOLE CRACK ON THE RIGHT DOUBLER FUSELAGE SKIN WERE FOUND. FO - [SDR TX9Y20111207007](https://openairdocs.org/sdr/TX9Y20111207007), Dec 5, 2011: LONGERON. CRACKED. DURING INSPECTION OF NR 3 ENGINE RT SIDE COWL, ONE CRACK AND ONE DEEP CHAFING DAMAGE WERE FOUND AT LOWER LONGERON (P/N:65B94280-199). THE REPAIR WAS PERFORMED A - [SDR TX9Y20111206004](https://openairdocs.org/sdr/TX9Y20111206004), Dec 4, 2011: SKIN. DENTED. FUSELAGE SKIN (STA2200-STA2400,STR27-STR28) WAS FOUND ONE ORIGINAL REPAIR RIVET AND DENT. FUSELAGE SKIN DOUBLER WAS REPAIRED AS PER SRM 53-30-03 FIG 4 REV 120. - [SDR TX9Y20111205003](https://openairdocs.org/sdr/TX9Y20111205003), Dec 3, 2011: FAILSAFE. CORRODED. DURING DATUM AIRCRAFT INPUT,A CORROSION (SIZE ABOUT:3.3"*0.8") WAS FOUND ON BULK CARGO FRAME LOWER LOBE FAIL SAFE CHORD (P/N:65B04347-149,STA2200) HORIZONTAL FL - [SDR TX9Y20111202001](https://openairdocs.org/sdr/TX9Y20111202001), Dec 1, 2011: SKIN. DENTED. BULK CARGO DOOR SKIN FORWARD LOWER CORNER WAS FOUND A DENT. THE SKIN SMOOTHED OUT WAS FOUND OUT LIMITS. BULK CARGO DOOR SKIN DENT AREA WAS REPAIRED AS PER SRM 5 - [SDR TX9Y20111202002](https://openairdocs.org/sdr/TX9Y20111202002), Dec 1, 2011: DOUBLER. CRACKED. NR 9 SPOILER HINGE DOUBLER AND NR 11 SPOILER HINGE DOUBLER WERE FOUND CRACKED. NR 9 SPOILER AND NR 11 SPOILER WERE REPLACED AS PER AMM 27-61-02 REV 86. - [SDR Q2SA758012](https://openairdocs.org/sdr/Q2SA758012), Sep 24, 2010: ENGINE. FAILED. FLIGHT MAS6145, WHILE PREPARING FOR TAKEOFF, EXPERIENCED AN UNCONTAINED ENGINE FAILURE. - [SDR Q2SA795002A](https://openairdocs.org/sdr/Q2SA795002A), Aug 24, 2010: ACTUATOR. MISSING. ACFT 795 DEPARTED AS FLT SOO113, BOTH TAXI & TAKEOFF OPS WERE NORMAL. MLG HANDLE SELECTED TO "UP" POSITION AFTER LIFTOFF. BOTH RED "DOOR OPEN" & "RED "GEAR" LIG - [SDR Q2SA758011](https://openairdocs.org/sdr/Q2SA758011), Jul 22, 2010: ENGINE. LEAKING. DURING THE TAKEOFF ROLL IN OMDB NR 1 EGT GAUGE BRIEFLY WENT TO 0, THEN RETURNED TO NORMAL. DURING THE CLIMB TO FL 300 IT WAS NOTICED, NR 1 EGT WAS RUNNING SIGNI - [SDR 2010FA0000346](https://openairdocs.org/sdr/2010FA0000346), Apr 15, 2010: HINGE FITTING. CRACKED. HORIZ STABILIZER LT 2 PLACES 0.9 INCH AND 0.8 INCH & RT 2 PLACES 1.1 INCH AND 0.85 INCH, HINGE FITTING CRACKED. - [SDR 2010FA0000345](https://openairdocs.org/sdr/2010FA0000345), Apr 15, 2010: STIFFENER. CRACKED. PYLON NR 2 INBD NR 3 STIFFENER CRACK 0.67 INCH BETWEEN NAC STA 248 AND NAC STA 259 ON THE RT SIDE. - [SDR 2010FA0000344](https://openairdocs.org/sdr/2010FA0000344), Apr 15, 2010: SKIN. CORRODED. FWD CARGO LOWER FUSELAGE SKIN AT STA 1000 WAS CORRODED LEVEL 2. - [SDR 2010FA0000343](https://openairdocs.org/sdr/2010FA0000343), Apr 15, 2010: DOUBLER. CRACKED. MAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK, 0.35 INCH AT UPPER HINGE DOOR. - [SDR 2010FA0000342](https://openairdocs.org/sdr/2010FA0000342), Apr 15, 2010: STIFFENER. CRACKED. PYLON NR 1, INBD NR 3, STIFFENER CRACK. - [SDR Q2SA758010](https://openairdocs.org/sdr/Q2SA758010), Apr 12, 2010: DOUBLER. CRACKED. MAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK AT UPPER HINGE DOOR. - [SDR Q2SA758009](https://openairdocs.org/sdr/Q2SA758009), Apr 12, 2010: STIFFENER. CRACKED. PYLON NR 1 INBOARD NR 3 STIFFENER CRACK. - [SDR Q2SA758008](https://openairdocs.org/sdr/Q2SA758008), Nov 13, 2009: A/C PACK. VIBRATION. DEPARTURE FROM VAKK TO VMCC: AFTER TAKEOFF NR 1 AIR CONDITIONING PACK STARTED SEVERE RUMBLING NOISE AND EMITTED AN ODOR. AIRCRAFT QUICK HANDBOOK PROCEDURE ACCOM - [SDR Q2SA758007](https://openairdocs.org/sdr/Q2SA758007), Oct 24, 2009: FUEL FILTER. FAILED. ON TAKEOFF CLIMBOUT OF KJFK, ENGINE NR 1 AND ENGINE NR 4 FUEL FILTER BYPASS INDICATION LIGHTS CAME ON AND STAYED ON, CREW ELECTED TO TERMINATE FLIGHT, DUMPED 15 - [SDR Q2SA758006](https://openairdocs.org/sdr/Q2SA758006), Apr 20, 2009: SLIDE. UNWANTED DEPLOY. PRIOR TO DEPARTURE FROM KJFK, LEFT UPPER DECK EMERGENCY EXIT SLIDE INADVERTENTLY DEPLOYED. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DEFERRE - [SDR Q2SA758005](https://openairdocs.org/sdr/Q2SA758005), Mar 17, 2009: PMS. INACTIVE. CLIMB-OUT OF EBLG, PERFORMANCE MANAGEMENT SYSTEM (PMS) LIGHT ILLUMINATED IN FLIGHT AND AUTOPILOTS "A" AND "B" WOULD NOT FOLLOW FLIGHT MANAGEMENT SYSTEM (FMS) CO - [SDR Q2SA758004](https://openairdocs.org/sdr/Q2SA758004), Dec 21, 2008: THRUST REVERSER. DEPLOYED. ON CLIMB-OUT FROM ADDIS ABABA, ETHIOPIA (HAAB), AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO INDICATION OF NR 4 ENGINE THRUST REVERSER TRYING TO DEPLOY IN FLIGHT. - [SDR Q2SA758003](https://openairdocs.org/sdr/Q2SA758003), Oct 9, 2008: ENGINE. DAMAGED. DURING TAKEOFF AFTER V1 FROM HAAB, BIRD INGESTION INTO NR 3 ENGINE. AIR TURNBACK TO HAAB. FUEL DUMP OF 50,000 LBS. INSPECTION AFTER LANDING CONFIRMED DAMAGE TO - [SDR Q2SA758002](https://openairdocs.org/sdr/Q2SA758002), May 15, 2008: ACCESS PANEL. CRACKED. POST FLIGHT WALK-AROUND, FOUND HYDRAULIC ACCESS PANEL ON NR 1 ENGINE SAIL BOAT FAIRING OPEN. FOUND CRACK AT NR 1 ENGINE INBOARD SAIL BOAT DOOR, AT THE FORWARD H - [SDR 758001](https://openairdocs.org/sdr/758001), Feb 14, 2007: TRIM SYSTEM. FAILED. ASTU WAS ON DEFERRAL. REMOVED AND REPLACED ASTU PRIOR TO DEPARTURE OUT OF PANC IAW AMM 22-14-01. AFFECTED BOTH AUTOPILOT A AND B SYSTEMS AND COULD NOT ENGAGE BO ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ENG10RA054](https://openairdocs.org/ntsb/ENG10RA054), Sep 23, 2010: Boeing 747 (N758SA), Frankfurt, Germany, incident, minor damage ## Other aircraft with N758SA - [Cancelled 2026-02-14](https://openairdocs.org/deregistered/N758SA-2026-02-14): DJI AGRAS T50, S/N 63YBM6J0020053. Assigned, pending cancellation --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.