# N71314: 1985 Boeing 737-3TO, registration cancelled 2004-02-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 19, 2004 - Exported to: Malaysia - Status when cancelled: Valid registration - 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: 23365 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 24, 1985 - Certificate issued: October 25, 1985 - Last registry action: November 7, 2001 - Mode S code: A989CA - 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/N71314 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=71314 - Page: https://openairdocs.org/deregistered/N71314-2004-02-19 From the FAA registry file of November 5, 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0300047](https://openairdocs.org/sdr/CALA0300047), Feb 14, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN BOTH THE LEFT HAND AND RIGHT HAND PRESSURE DECK AT STA 663.75. BOTH LOCATIONS WERE REPAIRED IAW SRM 53-60-51. - [SDR CALA0101018](https://openairdocs.org/sdr/CALA0101018), Dec 2, 2001: WEB. CORRODED. INSPECTION FOUND AFT CARGO DOOR THRESHOLD SILL WEB CORRODED ON TOP AND UNDER SIDE. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0101012](https://openairdocs.org/sdr/CALA0101012), Nov 25, 2001: FRAME. CORRODED. INSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD FRAME CORRODED AT STA 794.3, STRINGER 25R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. - [SDR CALA0101011](https://openairdocs.org/sdr/CALA0101011), Nov 25, 2001: ANGLE. CORRODED. INSPECTION FOUND FORWARD L-ANGLE SUPPORT FOR SILL WEB CORRODED AT THRESHOLD OF AFT PIT, STA 704, STRINGER 25R. A NEW ANGLE WAS INSTALLED IAW BOEING DRAWING 69-4 - [SDR CALA0101008](https://openairdocs.org/sdr/CALA0101008), Nov 21, 2001: SKIN. CRACKED. INSPECTION FOUND A 2" CRACK IN L/H HORIZONTAL STABILIZER SKIN FORWARD OF I/B BALANCE PANEL. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW - [SDR CALA011007](https://openairdocs.org/sdr/CALA011007), Nov 20, 2001: ANGLE. CORRODED. INSPECTION FOUND AFT L-ANGLE SUPPORT FOR SILL WEB CORRODED AT AFT PIT THRESHOLD, STA 870, LONGERON 25L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00. - [SDR CALA011006](https://openairdocs.org/sdr/CALA011006), Nov 20, 2001: FRAME. CRACKED. INSPECTION FOUND A 1" CRACK IN AFT CARGO DOOR FORWARD FRAME BETWEEN #3 & #4 STOP FITTINGS. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02. - [SDR CALA0101002](https://openairdocs.org/sdr/CALA0101002), Nov 14, 2001: SKIN. GOUGED. INSPECTION FOUND THE R/H O/B FOREFLAP L/E O/B EDGE WITH SEVERAL DEEP GOUGES IN SKIN. A REPAIR WAS INSTALLED IAW SRM 57-53-01. - [SDR CALA0100998](https://openairdocs.org/sdr/CALA0100998), Nov 9, 2001: SKIN. CRACKED. INSPECTION FOUND A 1.3" CRACK IN KEEL BEAM SKIN AT STA 699, RBL 5 AND A 1/2" CRACK WAS FOUND IN KEEL BEAM SKIN AT STA 699, LBL 5. A DOUBLER WAS INSTALLED AT EAC - [SDR CALA0100997](https://openairdocs.org/sdr/CALA0100997), Nov 9, 2001: SKIN. CRACKED. INSPECTION FOUND A 3.5" CRACK IN KEEL BEAM SKIN AT STA 674, RBL 5. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-12, FIGURE 202. - [SDR CALA9901131](https://openairdocs.org/sdr/CALA9901131), Sep 5, 1999: BULKHEAD WEB. CRACKED. INSPECTION FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD WEB CRACKED IN FOUR PLACES AT FASTENER HOLES AT STA 1016, STRINGER 6L-7L. ALSO, SEVERAL ELONGATED HOLES W - [SDR CALA9901097](https://openairdocs.org/sdr/CALA9901097), Aug 27, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND RT AND LT AFT LAV FLOORBEAM CORRODED ON NUT PLATE HOLES AT STA 1016, RBL 0 TO RBL 50 AND LBL 0 TO LBL 40. REPAIRED IAW ECRA 5310-03906. - [SDR CALA9901096](https://openairdocs.org/sdr/CALA9901096), Aug 27, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 985.5 FROM LBL 18 TO R-2 DOOR JAMB. REPAIRED IAW ECRA 5310-03906. - [SDR CALA9901077](https://openairdocs.org/sdr/CALA9901077), Aug 22, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND RT I/B SEAT TRACK CORRODED FROM STA 328-344. REPAIRED IAW SRM 53-00-52, FIGURE 202, SHEET 1. - [SDR CALA9901066](https://openairdocs.org/sdr/CALA9901066), Aug 18, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 14 TO RBL 12. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA9901059](https://openairdocs.org/sdr/CALA9901059), Aug 15, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CORROSION ON FLOORBEAM WITH FASTENERS PULLED THROUGH AT STA 328, LBL 11. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS IN - [SDR CALA9901056](https://openairdocs.org/sdr/CALA9901056), Aug 14, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 312 BETWEEN LBL 10 AND RBL 32. INSTALLED REPAIR IAW SRM 53-10-51, FIGURE 205. - [SDR CALA9800728](https://openairdocs.org/sdr/CALA9800728), Apr 30, 1998: SKIN. WRINKLED. RIGHT WING O/B FOREFLAP HAS WRINKLED SKIN. REPLACED RIGHT WING O/B FOREFLAP PER MM 27-51-37. - [SDR CALA9800007](https://openairdocs.org/sdr/CALA9800007), Jan 8, 1998: SENSOR. OUT OF ADJUST. THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE GEAR HANDLE WOULD NOT GO PAST OFF POSITION. MAINTENANCE FOUND THE MAIN GEAR AIR SAFETY SENSOR OUT - [SDR CALA9600905](https://openairdocs.org/sdr/CALA9600905), Jun 27, 1996: HYD LINE. LEAKING. THE A-HYDRAULIC SYSTEM FLUID WAS LOST ON FINAL APPROACH TO EWR. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOU - [SDR CAL960334](https://openairdocs.org/sdr/CAL960334), Mar 18, 1996: UPLOCK ACT. INOPERATIVE. IAH - FLT 1703 - THE RT MLG GREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. A TOWER FLYBY VERIFIED THE RT GEAR WAS NOT EXTENDED. A M - [SDR CAL960111](https://openairdocs.org/sdr/CAL960111), Feb 9, 1996: FAN. INOPERATIVE. FLT NR 1082 - CLE - A SMOKEY ODOR IN REAR OF CABIN WAS REPORTED TWICE DURING FLIGHT. THE AIR WAS CLEARED BOTH TIMES BY USING HIGH POSITION ON BOTH PACKS. MAINTE - [SDR CAL950868](https://openairdocs.org/sdr/CAL950868), Sep 30, 1995: HYD PUMP. INOPERATIVE. IAH - FLT 1769 - THE B-SYSTEM HYDRAULIC QUANTITY DECREASED TO JUST ABOVE ZERO AND WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 ENGINE B-HYDRAULIC PUMP LOW PRESSU ## FAA accident and incident reports (1) 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 19910908046589I](https://openairdocs.org/incident/19910908046589I), Sep 8, 1991: Boeing 7373T0 (N71314), Newark, NJ. Flight attendant injured by container of cans which fell from overhead bin onto her head. Returned to Newark. ## Other aircraft with N71314 - [Registered now](https://openairdocs.org/aircraft/N71314): Top Dog TD2, S/N 9318, built 2007 - [Cancelled 1969-06-06](https://openairdocs.org/deregistered/N71314-1969-06-06): Cessna 182M, S/N 18259573. Exported to Germany. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - [Cancelled 1951-11-19](https://openairdocs.org/deregistered/N71314-1951-11-19): Luscombe 8A, S/N 2741. Owner: [Ross Donald F](https://openairdocs.org/faa-owner/ROSS%20DONALD%20F), [Ketchikan, AK](https://openairdocs.org/faa-place/AK/Ketchikan) --- 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.