# N69311: 1985 Boeing 737-3TO, registration cancelled 2010-05-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 18, 2010
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 23362
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 1985
- Certificate issued: October 1, 1985
- Last registry action: June 16, 2009
- Mode S code: A93870
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N69311
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=69311
- Page: https://openairdocs.org/deregistered/N69311-2010-05-18

From the FAA registry file of October 31, 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md

## Service difficulty reports (92, newest 50)

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

- [SDR CALA2009101900634](https://openairdocs.org/sdr/CALA2009101900634), Oct 19, 2009: BATTERY. DISCHARGED. R-1 DOOR OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED BATTERY FOR R-1 DOOR EMERGENCY LIGHTS, OPS GOOD.
- [SDR CALA2009012300054](https://openairdocs.org/sdr/CALA2009012300054), Jan 22, 2009: SKIN. CRACKED. FOUND 1.5 INCH LONG SKIN CRACK AT FUSELAGE OUTER SKIN AT 3 INCHES AFT OF STATION 727E AND S-24R. INSTALLED DOUBLER REPAIR, ALL HOLES WERE ZERO TIMED PER SRM 53-
- [SDR CALA2009012200052](https://openairdocs.org/sdr/CALA2009012200052), Jan 21, 2009: SKIN. CRACKED. AFT LEFT FUSELAGE SKIN CRACKED AT APPROX STATION 747 FOUR STRINGERS BELOW LOWER LAP JOINT, CRACK 1.5 INCH LONG. PERFORMED HF EDDY CURRENT IAW NAT 51-00-00 PART 
- [SDR CALA0700364](https://openairdocs.org/sdr/CALA0700364), Jul 17, 2007: ATTACH FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN H-STRAP ON FUSELAGE STRUCTURE STA 312 L-1 DOOR LOWER HINGE ATTACH FITTING. A REPAIR WAS INSTALLED IAW ECRA 5311-01342.
- [SDR CALA0700361](https://openairdocs.org/sdr/CALA0700361), Jul 16, 2007: SKIN. CORRODED. INSPECTION FOUND SKIN STRAP CORRODED AT STA 1006, S27R, BL 0 TO RBL 8. THE CORRODED SECTION OF SKIN STRAP WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED I
- [SDR CALA0700359](https://openairdocs.org/sdr/CALA0700359), Jul 15, 2007: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT HORSE COLLAR (FITTING). THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0700358](https://openairdocs.org/sdr/CALA0700358), Jul 15, 2007: STRUCTURE. CORRODED. INSPECTION FOUND CHORD CORRODED AT STA 227.8, RBL 9 TO LBL 9. A LOWER O/B CHORD REPAIR WAS INSTALLED IAW ECRA 5311-01340.
- [SDR CALA0700354](https://openairdocs.org/sdr/CALA0700354), Jul 12, 2007: ATTACH FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT AFT END OF ATTACHMENT CLIP, STA 294-309, S10L. THE CLIP WAS REPLACED IAW ECRA 5311-01337.
- [SDR CALA0700353](https://openairdocs.org/sdr/CALA0700353), Jul 12, 2007: STRAP. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN H-STRAP AT THE UPPER L-1 DOOR HINGE ATTACH FITTING, STA 312. THE H-STRAP WAS REPLACED IAW ECRA 5311-01337.
- [SDR CALA0700352](https://openairdocs.org/sdr/CALA0700352), Jul 12, 2007: FRAME. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN STUB FRAME FOR L-2 DOOR UPPER HINGE AREA, STA 947.5, S11L. THE FRAME WAS REPAIRED IAW ECRA 5311-01335.
- [SDR CALA0700351](https://openairdocs.org/sdr/CALA0700351), Jul 12, 2007: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN WEB JUST FORWARD OF L-2 DOOR AT STA 942, S11L. THE CLOSE OUT WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01335.
- [SDR CALA0700350](https://openairdocs.org/sdr/CALA0700350), Jul 12, 2007: ATTACH FITTING. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK AT I/B CORNER OF ATTACHMENT CLIP, STA 360, S10L. THE CLIP WAS REMOVED AND REPLACED IAW ECRA 5311-01339.
- [SDR CALA0700349](https://openairdocs.org/sdr/CALA0700349), Jul 12, 2007: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL WEB AT RIVET LOCATED AT STA 294.5, S12L. THE INTERCOSTAL WEB WAS REMOVED AND REPLACED IAW ECRA 5311-01339.
- [SDR CALA0700347](https://openairdocs.org/sdr/CALA0700347), Jul 11, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED ON FORWARD END BETWEEN STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700343](https://openairdocs.org/sdr/CALA0700343), Jul 10, 2007: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 1006, S27R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW MM 51-40-02.
- [SDR CALA0700348](https://openairdocs.org/sdr/CALA0700348), Jul 7, 2007: FLAP TRACK. CORRODED. INSPECTION FOUND CORROSION INSIDE THE AFT TRANSMISSION MOUNT HOLE OF THE NR 8 FLAP TRACK, RT WING, WS 289-511. THE CORROSION IN THE BORE WAS REAMED, SHOT PEENED
- [SDR CALA0700341](https://openairdocs.org/sdr/CALA0700341), Jul 7, 2007: GUSSET. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN NOSE WHEEL WELL GUSSET AT END OF NLG DRAG BRACE. THE GUSSET WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700339](https://openairdocs.org/sdr/CALA0700339), Jul 6, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 440, S17R TO 24R. THE FRAME WAS REMOVED AND REPLACED IAW 
- [SDR CALA0700338](https://openairdocs.org/sdr/CALA0700338), Jul 6, 2007: PAN. CRACKED. INSPECTION FOUND A .5 INCH CRACK (THREE EACH) IN L-1 DOOR AFT PAN AT NR 5, NR 6, AND NR 7 STOP FITTING ADJUSTMENT ACCESS HOLES. A DOUBLER REPAIR WAS INSTALLED A
- [SDR CALA0700344](https://openairdocs.org/sdr/CALA0700344), Jul 3, 2007: FITTING. CORRODED. INSPECTION FOUND STRINGER 17R END FITTING CORRODED JUST BELOW FLOOR LINE AT STA 1016. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700335](https://openairdocs.org/sdr/CALA0700335), Jul 1, 2007: FITTING. CORRODED. INSPECTION FOUND STRINGER 27R END FITTING CORRODED IN BOLT HOLES AT STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700334](https://openairdocs.org/sdr/CALA0700334), Jul 1, 2007: FITTING. CORRODED. INSPECTION FOUND STRINGER 27L END FITTING CORRODED IN BOLT HOLES, STA 1016. THE END FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-12.
- [SDR CALA0700333](https://openairdocs.org/sdr/CALA0700333), Jul 1, 2007: ANGLE. CORRODED. INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD FACE LOWER CHORD ANGLE CORRODED AT STA 1016 FROM S27L T0 S27R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-0
- [SDR CALA0700331](https://openairdocs.org/sdr/CALA0700331), Jun 30, 2007: DOOR FRAME. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO DOOR CUTOUT FORWARD FRAME AT LOWER STOP FITTING, STA 440. THE FORWARD FRAME WAS REMOVED AND REPLACED IAW SRM 
- [SDR CALA0700330](https://openairdocs.org/sdr/CALA0700330), Jun 29, 2007: PRESSURE PANEL. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN RT WHEEL WELL CEILING PRESSURE DECK ABOVE O/B END OF GROUND SPOILER CONTROL VALVE, STA 664, RBL 40. A REPAIR DOUBLER WAS IN
- [SDR CALA0700329](https://openairdocs.org/sdr/CALA0700329), Jun 28, 2007: WEB. CORRODED. INSPECTION FOUND WEB CORRODED FROM STA 986.5 TO 1006, S21R. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-60-15 AND 51-40-02.
- [SDR CALA0700327](https://openairdocs.org/sdr/CALA0700327), Jun 27, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 986.5, LBL 43. THE CORRODED T-CHORD SECTION OF BEAM WAS REMOVED AND REPLACED IAW SRM 51-40
- [SDR CALA0700326](https://openairdocs.org/sdr/CALA0700326), Jun 27, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND SURFACE CORROSION AROUND SCREW HOLES ON FLOORBEAM AT STA 1016 FROM LBL 30 TO LBL 34, S19L-S21L. THE CORROSION WAS REMOVED AND A REPAIR WAS INST
- [SDR CALA0700324](https://openairdocs.org/sdr/CALA0700324), Jun 26, 2007: FITTING. CRACKED. INSPECTION FOUND A 0.65 INCH CRACK IN CLIP AT STA 616, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0700323](https://openairdocs.org/sdr/CALA0700323), Jun 26, 2007: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN CLIP AT STA 597, S8L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600005](https://openairdocs.org/sdr/CALA0600005), Jan 10, 2006: SPAR. CORRODED. INSPECTION FOUND THE LT HORIZONTAL STABILIZER REAR SPAR UPPER CAP CORRODED FROM STAB STA 196.2 TO 200.3. THE LT HORIZONTAL STABILIZER ASSEMBLY WAS REMOVED AND R
- [SDR CALA0600002](https://openairdocs.org/sdr/CALA0600002), Jan 8, 2006: SKIN. CRACKED. INSPECTION FOUND A 0.35 INCH CRACK IN NR 1 ENGINE UPPER PYLON PANEL (SKIN) 5727L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01
- [SDR CALA0400683](https://openairdocs.org/sdr/CALA0400683), Oct 22, 2004: SKIN. CRACKED. INSPECTION FOUND A 1.8 INCH CRACK IN FUSELAGE SKIN 3 INCHES AFT OF STA 727D AND BELOW S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090.
- [SDR CALA0300525](https://openairdocs.org/sdr/CALA0300525), Sep 11, 2003: KEELBEAM. CORRODED. INSPECTION FOUND LIGHT CORROSION ON O/B FLANGE OF LEFT KEELBEAM FROM BS 663-727. INSTALLED REPAIR IAW ECRA 5311-01167.
- [SDR CALA0300529](https://openairdocs.org/sdr/CALA0300529), Sep 5, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND CORROSION ALONG THE ENTIRE UPPER SECTION OF FLOORBEAM AT STA 967. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT AND A REPAIR SECTION WAS INSTALLED
- [SDR CALA0300514](https://openairdocs.org/sdr/CALA0300514), Sep 5, 2003: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT WING UPPER AFT INBOARD T/E PANEL OUTBOARD SUPPORT FITTING. A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300513](https://openairdocs.org/sdr/CALA0300513), Sep 4, 2003: CARGO TRACK. CORRODED. INSPECTION FOUND LT TIE DOWN RAIL CORRODED AT FASTENERS ON LOWER SURFACE AT STA 947 IN THE AFT CARGO COMPARTMENT. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW
- [SDR CALA0300510](https://openairdocs.org/sdr/CALA0300510), Sep 3, 2003: FRAME. CORRODED. INSPECTION FOUND CORROSION ON FRAME AT STA 793 BETWEEN S26R AND S25R IN AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 51-40-02.
- [SDR CALA0300509](https://openairdocs.org/sdr/CALA0300509), Sep 3, 2003: ANGLE. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN NR 1 ENGINE PYLON ANGLE FOR AFT LOWER O/B ACCESS PANEL. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300507](https://openairdocs.org/sdr/CALA0300507), Aug 30, 2003: BRACKET. CRACKED. INSPECTION FOUND A .2500 INCH CRACK IN VHF RIGHT FORWARD SUPPORT AFT CARGO COMPARTMENT BRACKET AT STA 727D. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-02
- [SDR CALA0300506](https://openairdocs.org/sdr/CALA0300506), Aug 30, 2003: SHEAR TIE. CORRODED. INSPECTION FOUND FORWARD BAGGAGE BIN SKIN SHEAR TIE CORRODED AT STA 460, S28R. THE CORRODED AREA WAS CUT OUT AND A REPAIR DOUBLER AND SHEAR TIE WERE INSTALLED I
- [SDR CALA0300505](https://openairdocs.org/sdr/CALA0300505), Aug 29, 2003: FLOOR PANEL. CRACKED. INSPECTION FOUND A 1 INCH AND .5000 INCH CRACK IN AFT BAGGAGE BIN FLOOR PANEL 1536X AT STA 794.5-807. A DOUBLER WAS INSTALLED AT EACH CRACK LOCATION IAW SRM 53-
- [SDR CALA0300504](https://openairdocs.org/sdr/CALA0300504), Aug 29, 2003: DOOR FRAME. CRACKED. INSPECTION FOUND A 7.5 INCH CRACK IN FORWARD BAGGAGE BIN WEB AT FORWARD LOWER DOOR JAMB, STA 440. A NEW SECTION OF WEB WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0300503](https://openairdocs.org/sdr/CALA0300503), Aug 29, 2003: SUPPORT. CRACKED. INSPECTION FOUND A .5000 INCH CRACK IN RT WING UPPER MOST I/B T/E PANEL SUPPORT. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA0300502](https://openairdocs.org/sdr/CALA0300502), Aug 28, 2003: GALLEY TRACK. CORRODED. INSPECTION FOUND NR 3 GALLEY I/B AFT MOUNT CORRODED. THE GALLEY MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300501](https://openairdocs.org/sdr/CALA0300501), Aug 27, 2003: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616. A DOUBLER ANGLE WAS INSTALLED IAW ECRA 5311-01158.
- [SDR CALA0300500](https://openairdocs.org/sdr/CALA0300500), Aug 27, 2003: STIFFENER. GOUGED. INSPECTION FOUND RT WING NR 6 FLAP TRACK FAIRING I/B STIFFENER GOUGED. THE STIFFENER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300498](https://openairdocs.org/sdr/CALA0300498), Aug 26, 2003: BRACKET. CORRODED. INSPECTION FOUND CORROSION ON CORNER BRACKET O/B OF DOOR CUTOUT RT AFT CORNER FWD ACC COMPT, STA 219. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300497](https://openairdocs.org/sdr/CALA0300497), Aug 26, 2003: FLOOR SUPPORT. CORRODED. INSPECTION FOUND UPPER AND LOWER SURFACE OF FLOOR SUPPORT CORRODED BETWEEN STA 967 AND 986.5. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0300494](https://openairdocs.org/sdr/CALA0300494), Aug 25, 2003: ANGLE. CORRODED. INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT BS 947-986, LBL 48. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.

All 92: https://openairdocs.org/deregistered/N69311-2010-05-18/reports.md

## FAA accident and incident reports (2)

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 19920902038179I](https://openairdocs.org/incident/19920902038179I), Sep 2, 1992: Boeing 7373T0 (N69311), San Francisco, CA. Gear would not retract after takeoff. Returned. Gear handle would not go past off.
- [Incident 19870419018089I](https://openairdocs.org/incident/19870419018089I), Apr 19, 1987: Boeing 7373TO (N69311), Washington, DC. During taxi flight control check, noted b system hydraulic failure. Found a loose cap on system module assembly.

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