# N767TW: 1972 Boeing 737-230C, registration cancelled 2009-10-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 13, 2009 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-230C](https://openairdocs.org/model/boeing-737-230c) (registry code 13844BW) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 20258 - Year built: 1972 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 17, 2000 - Certificate issued: July 13, 2000 - Last registry action: September 15, 2009 - Mode S code: AA5D47 - Owner when cancelled: [Sierra American Corp](https://openairdocs.org/faa-owner/SIERRA%20AMERICAN%20CORP) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7376° N, 75.6671° W: Placed by OpenAirDocs at the center of ZIP code 19808, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N767TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=767TW - Page: https://openairdocs.org/deregistered/N767TW-2009-10-13 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 737-230C: https://openairdocs.org/model/boeing-737-230c.md ## Service difficulty reports (98, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0711002](https://openairdocs.org/sdr/0711002), Nov 9, 2007: POSITION SENSOR. MALFUNCTIONED. FLAP ASYMMETRY LOCKOUT AT 1 UNIT. DIVERTED FROM KLZU TO KATL (RUNWAY TOO SHORT FOR FLAPS 1 LANDING). - [SDR 0701001](https://openairdocs.org/sdr/0701001), Jan 17, 2007: LAMP. LOOSE. R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. - [SDR 0601027](https://openairdocs.org/sdr/0601027), Jan 6, 2006: SKIN. CANNING. FUSELAGE SKIN SECTION REPAIRED DUE TO OIL CANNING. - [SDR 0601012](https://openairdocs.org/sdr/0601012), Jan 6, 2006: FRAME. DENTED. FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR 0601011](https://openairdocs.org/sdr/0601011), Jan 6, 2006: FRAME. DENTED. FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR 0601010](https://openairdocs.org/sdr/0601010), Jan 6, 2006: FRAME. DENTED. FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR 0601026](https://openairdocs.org/sdr/0601026), Jan 6, 2006: STRINGER. CRACKED. FUSELAGE STRINGER REPAIRED DUE TO CRACK. - [SDR 0601025](https://openairdocs.org/sdr/0601025), Jan 6, 2006: STRINGER. CORRODED. FUSELAGE STRINGER REPAIRED DUE TO CORROSION. - [SDR 0601024](https://openairdocs.org/sdr/0601024), Jan 6, 2006: SHEAR TIE. CORRODED. FUSELAGE FRAME SHEAR TIE REPAIRED DUE TO CORROSION. - [SDR 0601009](https://openairdocs.org/sdr/0601009), Jan 6, 2006: FRAME. DENTED. FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR 0601023](https://openairdocs.org/sdr/0601023), Jan 6, 2006: SKIN. DENTED. FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR 0601022](https://openairdocs.org/sdr/0601022), Jan 6, 2006: SKIN. DENTED. FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR MJYA0601021](https://openairdocs.org/sdr/MJYA0601021), Jan 6, 2006: SKIN. DENTED. FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR MJYA0601005](https://openairdocs.org/sdr/MJYA0601005), Jan 6, 2006: FRAME. DENTED. FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR MJYA0601015](https://openairdocs.org/sdr/MJYA0601015), Jan 6, 2006: SKIN. OUT OF LIMITS. LOWER FUSELAGE E/E COMPARTMENT CUTOUT SKIN REPAIRED DUE TO SKIN HOLE EDGE DISTANCE OUT OF LIMITS. - [SDR MJYA0601020](https://openairdocs.org/sdr/MJYA0601020), Jan 6, 2006: SKIN. DENTED. FUSELAGE FORWARD CARGO COMPARTMENT DOOR EXTERNAL SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR MJYA0601008](https://openairdocs.org/sdr/MJYA0601008), Jan 6, 2006: FRAME. DENTED. FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR MJYA0601004](https://openairdocs.org/sdr/MJYA0601004), Jan 6, 2006: SPAR. CORRODED. WING CENTER SECTION REAR SPAR LOWER CHORD WAS REPAIRED DUE TO CORROSION. - [SDR MJYA0601019](https://openairdocs.org/sdr/MJYA0601019), Jan 6, 2006: FLOORBEAM. CRACKED. FUSELAGE AFT CARGO COMPARTMENT DOOR LOWER BEAM REPAIRED DUE TO CRACK. - [SDR MJYA0601017](https://openairdocs.org/sdr/MJYA0601017), Jan 6, 2006: SKIN. DENTED. FUSELAGE SKIN SECTION REPAIRED DUE TO DENTS OUT OF LIMITS. - [SDR MJYA0601016](https://openairdocs.org/sdr/MJYA0601016), Jan 6, 2006: SKIN. DENTED. FUSELAGE SKIN SECTION REPAIRED DUE TO DENTS OUT OF LIMITS. - [SDR MJYA0601013](https://openairdocs.org/sdr/MJYA0601013), Jan 6, 2006: SHEAR BEAM. CRACKED. RIGHT WHEEL WELL SHEAR BEAM REPAIRED DUE TO CRACK. - [SDR MJYA0601007](https://openairdocs.org/sdr/MJYA0601007), Jan 6, 2006: FRAME. DENTED. FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR MJYA0601018](https://openairdocs.org/sdr/MJYA0601018), Jan 6, 2006: FAIRING. CRACKED. FUSELAGE WING TO BODY FAIRING FORMER REPAIRED DUE TO CRACK. - [SDR MJYA0601014](https://openairdocs.org/sdr/MJYA0601014), Jan 6, 2006: SKIN. CORRODED. FUSELAGE SKIN SECTION REPAIRED DUE TO CORROSION. - [SDR 0601030](https://openairdocs.org/sdr/0601030), Jan 6, 2006: SKIN. CRACKED. REPAIRED FUSELAGE SKIN SECTION DUE TO CRACK. - [SDR MJYA0601041](https://openairdocs.org/sdr/MJYA0601041), Jan 6, 2006: FLOORBEAM. CORRODED. REPAIRED MAIN CARGO CABIN FLOORBEAM UPPER CHORD DUE TO CORROSION. - [SDR 0601040](https://openairdocs.org/sdr/0601040), Jan 6, 2006: FLOOR SUPPORT. CORRODED. REPAIRED MAIN CARGO CABIN FLOOR SUPPORT CHANNEL DUE TO CORROSION. - [SDR 0601038](https://openairdocs.org/sdr/0601038), Jan 6, 2006: FITTING. DAMAGED. REPAIRED FUSELAGE MAIN CARGO CABIN FITTING UNDERNEATH LONGITUDINAL FLOOR BEAM DUE TO MISSING MATERIAL. - [SDR 0601034](https://openairdocs.org/sdr/0601034), Jan 6, 2006: WEB. CORRODED. REPAIRED FUSELAGE MAIN CARGO CABIN LOWER JAMB FLOOR WEB DUE TO CORROSION. - [SDR 0601033](https://openairdocs.org/sdr/0601033), Jan 6, 2006: FLOORBEAM. CORRODED. REPAIRED FUSELAGE MAIN CARGO CABIN FLOOR BEAM UPPER CHORD DUE TO CORROSION. - [SDR 0601035](https://openairdocs.org/sdr/0601035), Jan 6, 2006: SKIN. DENTED. REPAIRED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS. - [SDR 0601032](https://openairdocs.org/sdr/0601032), Jan 6, 2006: FLOORBEAM. CORRODED. REPAIRED FUSELAGE MAIN CARGO CABIN FLOORBEAM UPPER CHORD DUE TO CORROSION. - [SDR 0601048](https://openairdocs.org/sdr/0601048), Jan 6, 2006: SKIN. ELONGATED. REPLACED RT WING TO NR 2 ENGINE AFT FAIRING IB SKIN PANEL DUE TO ELONGATED HOLES. - [SDR 0601047](https://openairdocs.org/sdr/0601047), Jan 6, 2006: SKIN. DENTED. REPAIRED APU DOOR NONPRESSURIZED OUTER SKIN AT 2 LOCATIONS, FROM B/S 1098.5 TO 1108, AND FROM B/S 1113.5 TO B/S 1129.5 AT CENTER SECTION, DUE TO DENTS OUT OF LI - [SDR 0601043](https://openairdocs.org/sdr/0601043), Jan 6, 2006: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN DUE TO SCRIBE LINES DAMAGE. - [SDR 0601039](https://openairdocs.org/sdr/0601039), Jan 6, 2006: WINDOW FRAME. CORRODED. REPAIRED FUSELAGE WINDOW FRAME AT TWO LOCATIONS, FROM B/S 688 TO 703.25, AND FROM B/S 727+3 TO 727+18.25, DUE TO CORROSION. - [SDR 0601046](https://openairdocs.org/sdr/0601046), Jan 6, 2006: SKIN. DENTED. REPAIRED NONPRESSURIZED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS. - [SDR 0601042](https://openairdocs.org/sdr/0601042), Jan 6, 2006: FLOORBEAM. CORRODED. REPAIRED MAIN CARGO CABIN TRANSVERSAL BEAM DUE TO CORROSION. - [SDR 0601044](https://openairdocs.org/sdr/0601044), Jan 6, 2006: SKIN. DAMAGED. REPAIRED FUSELAGE SKIN DUE TO SCRIBE LINES DAMAGE. - [SDR 0601049](https://openairdocs.org/sdr/0601049), Jan 6, 2006: SKIN. DAMAGED. REPAIRED RIGHT WING OUTBOARD MID FLAP TRAILING EDGE LOWER SKIN DUE TO SHARP EDGE. - [SDR 0601050](https://openairdocs.org/sdr/0601050), Jan 6, 2006: SKIN PANEL. DELAMINATED. REPAIRED RIGHT WING TRAILING EDGE LOWER FIXED PANEL DUE TO DELAMINATION. - [SDR 0601045](https://openairdocs.org/sdr/0601045), Jan 6, 2006: FLOORBEAM. CORRODED. REPAIRED FUSELAGE MAIN CARGO CABIN FLOORBEAM WEB AND REPLACED PRODUCTION DOUBLER DUE TO CORROSION. - [SDR 0601031](https://openairdocs.org/sdr/0601031), Jan 6, 2006: DOOR FRAME. CRACKED. REPAIRED FUSELAGE FORWARD GALLEY DOOR, UPPER AFT FRAME, DUE TO CRACK. - [SDR 0601006](https://openairdocs.org/sdr/0601006), Jan 6, 2006: FRAME. DENTED. FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS. - [SDR 0601036](https://openairdocs.org/sdr/0601036), Jan 6, 2006: SKIN. DENTED. REPAIRED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS. - [SDR 0601029](https://openairdocs.org/sdr/0601029), Jan 6, 2006: FITTING. CORRODED. REPLACED FUSELAGE BULKHEAD LEFT FITTING DUE TO CORROSION. ALSO REPAIRED FUSELAGE SKIN AND DOUBLER DUE TO CRACK. - [SDR 0601028](https://openairdocs.org/sdr/0601028), Jan 6, 2006: STIFFENER. CORRODED. REPAIRED -579 STIFFENER AND PERFORMED BLEND OUT IN THE AFT PRESSURE BULKHEAD "Y" CHORD DUE TO CORROSION. REPAIRED AFT PRESSURE BULKHEAD WEB AND RADIAL STIFFENER - [SDR 0601051](https://openairdocs.org/sdr/0601051), Jan 6, 2006: SPOILER. DELAMINATED. REPAIRED LEFT WING SPOILER #3 DUE TO DELAMINATION. - [SDR 0601037](https://openairdocs.org/sdr/0601037), Jan 6, 2006: BULKHEAD. CRACKED. REPAIRED FUSELAGE AFT PRESSURE BULKHEAD WEB DUE TO CRACK. All 98: https://openairdocs.org/deregistered/N767TW-2009-10-13/reports.md --- 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.