# N760SA: 1976 Boeing 747-230B, registration cancelled 2017-10-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 30, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 747-230B](https://openairdocs.org/model/boeing-747-230b) (registry code 1384889)
- 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: 21221
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 29, 1995
- Certificate issued: May 22, 2009
- Last registry action: April 11, 2011
- Mode S code: AA4319
- 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/N760SA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=760SA
- Page: https://openairdocs.org/deregistered/N760SA-2017-10-30

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 747-230B: https://openairdocs.org/model/boeing-747-230b.md

## Service difficulty reports (41)

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

- [SDR Q2SA2012042876002](https://openairdocs.org/sdr/Q2SA2012042876002), Apr 28, 2012: ENGINE. DAMAGED. NUMBER FOUR ENGINE STALLED DURING CLIMB AND FLAP CLEAN UP. AT APPROXIMATELY 3000 FEET THE CREW PULLED THE THRUST LEVER BACK TO BREAK THE ENGINE STALL. THEY THEN
- [SDR TX9Y20111021001](https://openairdocs.org/sdr/TX9Y20111021001), Oct 21, 2011: POST. CRACKED. A CRACK WAS FOUND COMMON TO FWD CARGO SUPPORT POST AT MAIN DECK BS 560 FLOORBEAM DURING INSPECTION. SECTION OF POST ENCOMPASSING THE CRACK WAS TRIMMED AWAY, AND
- [SDR TX9Y20110928005](https://openairdocs.org/sdr/TX9Y20110928005), Sep 28, 2011: SKIN. CRACKED. DURING MAINTENANCE, NR 1 NACELLE SKIN WAS FOUND CRACKED AT LATCH AREA. THE CRACK IS ABOUT 0.8 IN LENGTH. REMOVED THE DAMAGE BY TRIMMING THE SKIN ASSEMBLY PER SR
- [SDR TX9Y20110928004](https://openairdocs.org/sdr/TX9Y20110928004), Sep 28, 2011: STRUT. CRACKED. DURING PERFORMING NR 3 PYLON STRUT CAP SKIN INSPECTION AND MODIFICATION AS PER SB 747-54A2230 R0, CRACK DAMAGE AT NUMEROUS HOLES WERE FOUND IN THE CAP SKIN ASSE
- [SDR TX9Y20110928003](https://openairdocs.org/sdr/TX9Y20110928003), Sep 28, 2011: BULKHEAD. CRACKED. DURING INSPECTION OF THE NR 4 PYLON STA 286 BULKHEAD PER SB 747-54A2202 REV 01, 1EA 0.50 INCHES LONG CRACK WAS FOUND COMMON TO THE FRAME. REPAIRED PER SR 1-1535
- [SDR TX9Y20110928002](https://openairdocs.org/sdr/TX9Y20110928002), Sep 26, 2011: STRUCTURE. CORRODED. LEFT WING I/B T/E AFT FLAP CONER FOUND HEAVY CORROSION. REPLACE THE LT WING I/B T/E AFT FLAP AS PER AMM 27-51-03.
- [SDR TX9Y20110928001](https://openairdocs.org/sdr/TX9Y20110928001), Sep 26, 2011: BEAR STRAP. CORRODED. FWD CARGO BS 550-570, STRINGER 46R BEAR STRAP FOUND CORRODED. BEAR STRAP WAS TRIMMED OUT AND INSTALLED REPAIR DOUBLERS AND FILLER, AND SPLICED A NEW SEGMENT OF 
- [SDR TX9Y20110922005](https://openairdocs.org/sdr/TX9Y20110922005), Sep 20, 2011: DOUBLER. CORRODED. FUSELAGE BS 980-1000 WATER SERVICE PORT AREA DOUBLER FOUND CORROSION. FABRICATE AND INSTALL THE NEW DOUBLER (P/N:65B09637-1) AS PER BOEING DRAWING 65B09637.
- [SDR TX9Y20110922004](https://openairdocs.org/sdr/TX9Y20110922004), Sep 20, 2011: BEAR STRAP. CORRODED. FUSELAGE BS 540-560 FWD LAV SERVICE PANEL CUT OUT SKIN FOUND CORROSION. DURING INSPECTION OF THIS DATUM AIRPLANE, CORROSION WAS FOUND ON THE BEAR STRAP (P/N: 65
- [SDR TX9Y20110922003](https://openairdocs.org/sdr/TX9Y20110922003), Sep 20, 2011: FLOORBEAM. CORRODED. AFT CARGO BS 1800 RBL 58 FLOORBEAM FOUND CORROSION. FABRICATE AND INSTALL THE FLOORBEAM CHORD (P/N:65B04327-71) AS PER BOEING DRAWING 65B04327.
- [SDR TX9Y20110922002](https://openairdocs.org/sdr/TX9Y20110922002), Sep 20, 2011: FRAME. CORRODED. AFT CARGO BS 1920 RT FRAME INNER CHORD FOUND CORROSION. REMOVE THE CORROSION AS PER SRM 51-10-01. CHECK THE ALLOWABLE WITHIN SRM LIMIT AS PER SRM 53-10-01.
- [SDR TX9Y20110922001](https://openairdocs.org/sdr/TX9Y20110922001), Sep 20, 2011: STRINGER. CORRODED. DURING INSPECTION OF THIS DATUM AIRPLANE, THE STRINGER 51R (P/N: 65B04483-13) IS FOUND HEAVILY CORRODED ON THE INBOARD SIDE WEB FLANGE AT STA 1958. THE STRINGER
- [SDR Q2S2010F00034](https://openairdocs.org/sdr/Q2S2010F00034), Mar 4, 2010: FLOOR SUPPORT. CRACKED. WS NR 0978, WC NR 53-520-01-01- FWD CARGO COMPARTMENT AT STA 570, RBL 44 FOUND FLOOR SUPPORT FRAME WEB CRACKED. CRACKED FLOOR SUPPORT WEB REMOVED IAW SRM 51-30-
- [SDR Q2S2010F00042](https://openairdocs.org/sdr/Q2S2010F00042), Mar 3, 2010: SPAR. CORRODED. WS NR 0912, WC NR 57-910-01-01. RT WING L/E FRONT SPAR LOWER CHORD AT OLES 1356 FOUND CORROSION. RT WING LOWER SKIN CORROSION AREA CUT AND REMOVED IAW SRM 57-30
- [SDR Q2S2010F00033](https://openairdocs.org/sdr/Q2S2010F00033), Mar 3, 2010: FRAME. CRACKED. WS NR 0924, WC-SAI EAO NR 4754020R1. NR 4 PLYON INBD REAR EANGINE MOUNT BULKHEAD INBD LOWER CHORD FWD CRACKED. REPAIR CARRIED OUT IAW EN:1014-10, FORM 8100-9, D
- [SDR Q2S2010F00039](https://openairdocs.org/sdr/Q2S2010F00039), Mar 2, 2010: HINGE. CRACKED. WS NR 0896, WC NR 57-940-01-01. RT WING T/E NR 8 SPOILER CTR HINGE AREA FOUND CRACKED BETWEEN FASTENERS. RT WING T/E NR 8 SPOILER REPLACED IAW AMM 27-61-01, REV
- [SDR Q2S2010F00036](https://openairdocs.org/sdr/Q2S2010F00036), Mar 2, 2010: INTERCOSTAL. CRACKED. WS 0907, WC SAI EAO NR 4753028-R2. NLG TORQUE BOX TOP SIDE (PRESSURIZED COMPARTMENT) FOUND INTERCOSTAL CRACKED AT RBL 12, BS 320. CRACKED INTERCOASTAL REMOVED I
- [SDR Q2S2010F00045](https://openairdocs.org/sdr/Q2S2010F00045), Mar 1, 2010: FLOORBEAM. DAMAGED. WS 0784, WC SAI NR 4753119, HFEC OPEN HOLE FOUND 07 HOLES ELONGATED ON UPPER DECK FLOORBEAM AT BS 520, FROM RBL 0 TO RBL 35 FWD CHORD. DAMAGED UPPER CHORD TRIMM
- [SDR Q2S2010F00044](https://openairdocs.org/sdr/Q2S2010F00044), Mar 1, 2010: MOUNT. CRACKED. WS NR 0844, WC SAI NR 4754020R1. NR 1 PYLON AFT ENGINE MOUNT INBD UPPER CHORD FOUND CRACKED. REPAIR CARRIED OUT IAW EN 1013-10. FORM 8100-9, DATED 19 MARCH 2010
- [SDR Q2S2010F00043](https://openairdocs.org/sdr/Q2S2010F00043), Mar 1, 2010: SKIN. CORRODED. WS NR 0827, WC NR 53-176-02-01. LOWER FUSELAGE SKIN AT STA 1504, STRINGER 26L FOUND SKIN CORROSION. REPAIR CARRIED OUT IAW EN NR 1010-10. FORM 8100-9, DATED 22,
- [SDR Q2S2010F00041](https://openairdocs.org/sdr/Q2S2010F00041), Mar 1, 2010: BEAR STRAP. CORRODED. WS NR 0809, WC NR SAI EAO NR 4753028R2. MAIN ENTRY DOOR NR 3 RIGHT CUT OUT AFT TOP SIDE FOUND CORROSION. REPAIR CARRIED OUT IAW EN NR 1019-10. FORM 8100-9, DATE
- [SDR Q2S2010F00029](https://openairdocs.org/sdr/Q2S2010F00029), Mar 1, 2010: FRAME. CORRODED. WORKSHEET NR 0823, WORKCARD NR 53-176-02-01. LOWER FUSELAGE LT BODY FAIRING SUPPORT AT STA 920 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.
- [SDR Q2S2010F00028](https://openairdocs.org/sdr/Q2S2010F00028), Mar 1, 2010: FRAME. CORRODED. WORKSHEET NR 0824, WORKCARD NR 53-176-02-01. LOWER FUSELAGE RT BODY FAIRING SUPPORT AT STA 920 FOUND CORROSION. REPALCED FRAME ASSY IAW SRM 51-30-02, REV 116.
- [SDR Q2S2010F00024](https://openairdocs.org/sdr/Q2S2010F00024), Mar 1, 2010: FRAME. CORRODED. WOKSHEET NR 0821, WORKCARD NR 53-176-02-01, LOWER FUSELAGE RT BODY FAIRING SUPPORT AT STA 880 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.
- [SDR Q2S2010F00023](https://openairdocs.org/sdr/Q2S2010F00023), Mar 1, 2010: PLATE. CRACKED. WORKSHEET NR 0810, WORKCARD NR 4753028R2. MAIN DECK, FWD OF MAIN ENTRY DOOR L1 CUT OUT FOUND DOUBLER PLATE CRACKED AT STA 430, STR 23L. REPLACED NEW STRAP IAW S
- [SDR Q2S2010F00022](https://openairdocs.org/sdr/Q2S2010F00022), Mar 1, 2010: FRAME. CORRODED. WORKSHEET NR 0819, WORKCARD NR 53-176-02-01, LOWER FUSELAGE LT BODY FAIRING SUPPORT AT STA 880 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.
- [SDR Q2S2010F00026](https://openairdocs.org/sdr/Q2S2010F00026), Feb 28, 2010: FLOOR SUPPORT. CRACKED. WORKSHEET NR 0743. WORKCARD NR 53-520-01-01. FWD CARGO COMPARTMENT AT STA 570, LBL 23 FOUND FLOOR SUPPORT FRAME WEB CRACKED. DAMAGED AREA TRIMMED IAW SRM 51-40-
- [SDR Q2S2010F00025](https://openairdocs.org/sdr/Q2S2010F00025), Feb 28, 2010: FLOOR SUPPORT. CRACKED. WORKSHEET NR 0745, WORKCARD REF NR 53-520-01-01. FWD CARGO COMPARTMENT AT STA 570, LBL 44 FOUND FLOOR SUPPORT FRAME WEB CRACKED. CRACKED FLOOR SUPPORT WEB REMOV
- [SDR Q2S2010F00030](https://openairdocs.org/sdr/Q2S2010F00030), Feb 27, 2010: FRAME. CRACKED. WORKSHEET NR 0654, WORKCARD NR 54-410-01-01. PRESSURE BULKHEAD FWD FACE/TOP LT RING FRAME (FACING THE FWD FACE) AT BS 134 FOUND CRACKED AT TOP MOST CORNER. CRCK
- [SDR Q2S2010F00038](https://openairdocs.org/sdr/Q2S2010F00038), Feb 26, 2010: SPAR. CORRODED. WS NR 0630, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD EXTENSION AT APPROX OLES 1361 FOUND CORROSION. REPAIR CARRIED OUT IAW EN 1020-10. FORM 8100-9
- [SDR Q2S2010F00035](https://openairdocs.org/sdr/Q2S2010F00035), Feb 26, 2010: SPAR. CORRODED. WS NR 0631, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD AT APPROX OLES 1305 FOUND EXFOLIATION. REPAIR CARRIED OUT IAW EN NR 1020-10. FORM 8100-9 DATE
- [SDR Q2S2010F00027](https://openairdocs.org/sdr/Q2S2010F00027), Feb 26, 2010: WEB. CRACKED. WORKSHEET NR 0620, WORKCARD NR 53-850-01-01. AFT CARGO COMPARTMENT AT STA 1850, RBL 28 FOUND LATERAL GUIDE SUPPORT WEB CRACKED. CRACKED SUPPORT WEB REMOVED IAW 
- [SDR Q2S2010F00020](https://openairdocs.org/sdr/Q2S2010F00020), Feb 26, 2010: STRAP. CORRODED. WORKSHEET NR 0628, WORKCARD 57-830-01-01. LT WING L/E FRONT SPAR UPPER CHORD STRAP AT APPROX OLES 1481 FOUND CORROSION. CORRODED STRAP REPLACED IAW SRM 51-30-02
- [SDR Q2S2010F00040](https://openairdocs.org/sdr/Q2S2010F00040), Feb 25, 2010: PRESSURE PANEL. CRACKED. WS NR 0437, WC NR 53-842-01-01. LT BODY LANDING GEAR WHEEL WELL AT ABOUT STA 1480 ABOVE ANTI-SKID VALVE MODULE FOUND PRESSURE DECK WEB CRACKED. REPAIR CARRIED O
- [SDR Q2S2010F00021](https://openairdocs.org/sdr/Q2S2010F00021), Feb 25, 2010: MOUNT. CORRODED. WORKSHEET NR 0435, WORKCARD NR 71-012-01-03, ENGINE NR 3 AFT UPPER MOUNT FOUND WITH CORROSION. REPLACED ENGINE NR 3 AFT UPPER MOUNT IAW AMM 71-21-03, REV 142. P
- [SDR Q2S2010F00019](https://openairdocs.org/sdr/Q2S2010F00019), Feb 25, 2010: MOUNT. CORRODED. ENGINE NR 3 AFT LOWER MOUNT FOUND WITH CORROSION. REPLACED ENGINE NR 3 AFT LOWER MOUNT IAW AMM 71-21-04, REV 142. PN ON: 65B94350-5, SN ON: P181R.
- [SDR Q2S2010F00032](https://openairdocs.org/sdr/Q2S2010F00032), Feb 24, 2010: FLOOR SUPPORT. CRACKED. WORKSHEET NR 0292, WORKCARD NR 53-550-02-01. AFT CARGO COMPARTMENT, LT NR 3 PDU SUPPORT WEB AT STATION 1600 TO 1620, LBL 44 FOUND CRACKED. CRACKED FLOOR SUPPORT
- [SDR Q2S2010F00031](https://openairdocs.org/sdr/Q2S2010F00031), Feb 24, 2010: SKIN. DAMAGED. WORKSHEET NR 0127, WORKCARD NR SAI RNR 4753078. FUSELAGE-CURRENTLY 02 EXISTING DOUBLERS FOUND SIDE BY SIDE AT BS 520 TO 550, STRINGER 34R TO 36R. REPAIR CARRIED
- [SDR Q2S2010F00037](https://openairdocs.org/sdr/Q2S2010F00037), Feb 23, 2010: HINGE. CRACKED. WS NR 0066, WC NR 57-530-01-01. LT WING NR 6 GROUND SPOILER LOWER SURFACE FOUND CRACKED AT INBD OF ACTUATOR LUG HINGE ALONG FASTENERS. LT WING NR 6 GROUND SPOIL
- [SDR Q2SA760001](https://openairdocs.org/sdr/Q2SA760001), Oct 30, 2009: FLEX DUCT. CRACKED. ON TAKEOFF CLIMBOUT OF EBLG ENGINE FIRE WARNING CAME ON FOR ENGINE NR 2, CREW ELECTED TO SHUTDOWN ENGINE NR 2, DUMPED 77,000 LBS OF FUEL, RETURNED TO AND LANDED
- [SDR 2007FA0000228](https://openairdocs.org/sdr/2007FA0000228), Mar 6, 2007: SENSOR. MALFUNCTIONED. DURING TAKEOFF, THE LANDING GEAR HANDLE WILL NOT GO TO UP OR RETRACT POSITION. AIRCRAFT RETURNED TO BASE. PERFORMED TROUBLESHOOTING ON THE LANDING GEAR SYSTEM A

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