# N76355: 1987 Boeing 737-3TO, registration cancelled 2011-08-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 11, 2011 - Status when cancelled: First renewal notice - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016) - Serial number: 23593 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 16, 1987 - Certificate issued: June 5, 2009 - Last registry action: June 5, 2009 - Mode S code: AA4FD2 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N76355 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=76355 - Page: https://openairdocs.org/deregistered/N76355-2011-08-11 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 (72, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0800918](https://openairdocs.org/sdr/CALA0800918), Sep 23, 2008: SUPPORT. CRACKED. PARTITION SUPPORT CRACKED AFT OF STA 1016. REMOVED AND REPLACED PARTITION SUPPORT PER 737-300 SRM 51-10-02. - [SDR CALA0800923](https://openairdocs.org/sdr/CALA0800923), Sep 22, 2008: KEELBEAM. CORRODED. KEEL BEAM FOUND WITH CORROSION IN FORWARD CARGO AT BODY STATION 500D+8" TO 500D+12.5" AT LBL 6.5". REPAIRED KEEL BEAM PER B737 SRM 53-60-12, REINSTALLED REMOVED - [SDR CALA0800907](https://openairdocs.org/sdr/CALA0800907), Sep 16, 2008: ANGLE. CORRODED. SURFACE CORROSION ON TRANSITION ANGLE AT STATION 767 STR 24R. REMOVED BAD SECTION OF TRANSITION ANGLE, FABRICATED NEW ANGLE, ALODINED, PRIMED AND INSTALLED NEW - [SDR CALA0800902](https://openairdocs.org/sdr/CALA0800902), Sep 16, 2008: BULKHEAD. DAMAGED. AFT PRESSURE BULKHEAD WEB FROM FLOOR LEVEL TO Y-CORD FROM APPROXIMATELY LBL 6 TO APPROXIMATELY LBL 20 HAS OVERHEAT DAMAGE. REMOVED AFT PRESSURE BULKHEAD WEB FRO - [SDR CALA0800885](https://openairdocs.org/sdr/CALA0800885), Sep 16, 2008: STIFFENER. DAMAGED. STIFFENER ON AFT PRESS BULKHEAD JUST O/B OF APU BLEED DUCT HAS OVERHEAT DAMAGE FROM FLOOR LEVEL DOWN TO Y-CORD. REMOVED STIFFENER FROM AFT PRESSURE BULKHEAD JUS - [SDR CALA0800884](https://openairdocs.org/sdr/CALA0800884), Sep 16, 2008: STIFFENER. DAMAGED. STIFFENER ON AFT PRESS BULKHEAD JUST I/B OF APU BLEED DUCT HAS OVERHEAT DAMAGE FROM FLOOR LEVEL DOWN TO Y-CORD. REMOVED STIFFENER ON AFT PRESSURE BULKHEAD JUST - [SDR CALA0800883](https://openairdocs.org/sdr/CALA0800883), Sep 16, 2008: INTERCOSTAL. OVERHEATED. INTERCOSTAL AT LBL 18.32 FROM 1016 TO AFT PRESS BULKHEAD HAS OVERHEAT DAMAGE. REMOVED INTERCOSTAL IAW B737 SRM 51-40-02. FABRICATED INTERCOSTAL IAW BAC DWG 65C3 - [SDR CALA0800882](https://openairdocs.org/sdr/CALA0800882), Sep 16, 2008: STIFFENER. DAMAGED. Z-ANGLE STIFFENER FROM LBL 3.54 TO LBL 18.32 ADJACENT TO AFT PRESSURE BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED Z-ANGLE STIFFENER IAW SRM 51-A01-02. FABRICA - [SDR CALA0800881](https://openairdocs.org/sdr/CALA0800881), Sep 16, 2008: STIFFENER. OVERHEATED. Z-ANGLE STIFFENER FROM LBL 18.32 TO 27.95 ADJACENT TO AFT PRESSURE BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED Z-ANGLE STIFFENER IAW SRM51-40-02. FABRICATED N - [SDR CALA0800880](https://openairdocs.org/sdr/CALA0800880), Sep 16, 2008: INTERCOSTAL. OVERHEATED. INTERCOSTAL AT LBL 3.54 FROM BS 1016 TO AFT PRESS BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02. FABRICATED NEW INTERCOSTAL IAW DWG - [SDR CALA0800870](https://openairdocs.org/sdr/CALA0800870), Sep 5, 2008: SPAR. CORRODED. VERTICAL STABILIZER HAS CORROSION AT FIN STATION 163.90 - 191.50 LEFT-SIDE AT REAR SPAR. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER EC/RA 5530-01510 - [SDR CALA0800869](https://openairdocs.org/sdr/CALA0800869), Sep 5, 2008: FRAME. CRACKED. BODY STATION 303.9 FRAME WEB P/N 65-17684-107 CRACKED AT S16L. BODY STATION 303.9 FRAME WEB REPLACED PER EC/RA 5310-04826. - [SDR CALA0800868](https://openairdocs.org/sdr/CALA0800868), Sep 5, 2008: FRAME. CRACKED. CRACK ON STIFFENER WHERE LOWER CASTING FOR L-1 DOORSTOP MOUNTS TO FRAME AT BODY STATION 303.9 AFT OF STRINGER 16 AT DOOR CUTOUT. REPAIRED FRAME AT BODY STATION - [SDR CALA0800867](https://openairdocs.org/sdr/CALA0800867), Sep 5, 2008: SKIN. CRACKED. R1 DOOR CUTOUT CRACKED AT LOWER AFT CORNER OF CUTOUT. CUT OUT DAMAGED AREA AND REPAIRED SAME PER SRM 53-10-01 REPAIR 2. - [SDR CALA0800866](https://openairdocs.org/sdr/CALA0800866), Sep 5, 2008: SKIN. CRACKED. FORWARD CARGO DOOR SKIN FOUND CRACKED UNDER DOOR LINER AT EDGE OF LIGHTENING HOLE 21" FROM TOP 21.5" FROM FORWARD EDGE. REMOVED CRACK AND REPAIRED FORWARD CARGO - [SDR CALA0800865](https://openairdocs.org/sdr/CALA0800865), Sep 5, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT INBOARD AFT FLANGE LOCATED AT BODY STATION 303.9 AND S16L. REPLACED INTERCOSTAL AT BODY STATION 303.9 AND S16L PER EC/RA 5310-04826. - [SDR CALA0800863](https://openairdocs.org/sdr/CALA0800863), Sep 5, 2008: ANGLE. CORRODED. CORROSION ON TRANSITION ANGLE AT STATION 727E S-24R. REMOVED BAD TRANSTION ANGLE, FABRICATED NEW SECTION, ALODINED, PRIMED AND INSTALLED ANGLE PER SRM 51-40-02, - [SDR CALA0800859](https://openairdocs.org/sdr/CALA0800859), Sep 4, 2008: INTERCOSTAL. CORRODED. INTERCOSTAL BETWEEN FLOORBEAMS BS 328 AND 344 HAS CORROSION AT BL15R. REMOVED AND REPLACED INTERCOSTAL BETWEEN FLOORBEAMS PER SRM 51-40-02. - [SDR CALA0800850](https://openairdocs.org/sdr/CALA0800850), Sep 4, 2008: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT BODY STATION 270 FROM LBL 10 - RBL 10 LOCATED AT AFT SIDE OF NLG DOWNLOCK VIEWER PANEL. REPAIRED CORRODED FLOORBEAM AT BODYSTATION 270 - [SDR CALA0800849](https://openairdocs.org/sdr/CALA0800849), Sep 4, 2008: FLOOR SUPPORT. CORRODED. G2 GALLEY RIGHT FORWARD FLOOR MOUNT HAS CORROSION. REMOVED MOUNT AND REPLACED THE MOUNT WITH NEW PART IAW SRM 51-40-02. - [SDR CALA0800848](https://openairdocs.org/sdr/CALA0800848), Sep 4, 2008: DOOR FRAME. CRACKED. FORWARD CARGO DOOR FRAME CRACKED. REMOVED CRACKED DOOR FRAME AND REPLACED SAME WITH NEW DOOR FRAME IAW SRM 51-40-02. - [SDR CALA0800800](https://openairdocs.org/sdr/CALA0800800), Aug 21, 2008: ANGLE. CORRODED. Z-ANGLE AT L1 DOOR HAS CORROSION. REMOVED CORRODED Z-ANGLE AT L1 DOOR AND INSTALLED NEW Z-ANGLE IAW B737 SRM 51-40-02. - [SDR CALA0800801](https://openairdocs.org/sdr/CALA0800801), Aug 19, 2008: FRAME. CRACKED. BODYSTATION 380 FRAME CRACK BETWEEN S20R AND 21R. REPAIRED FRAME AT BODYSTATION 380 IAW B737 SRM 51-70-11. - [SDR CALA0800797](https://openairdocs.org/sdr/CALA0800797), Aug 19, 2008: FAILSAFE. CRACKED. FRAME AT BODY STATION 380 BETWEEN S19R AND S20R APPEARS WAVY AT OLD REPAIR. EVALUATE AND REPAIR IF REQUIRED. REMOVED DAMAGED FAILSAFE AND REPAIRED IAW B737 SRM - [SDR CALA0800791](https://openairdocs.org/sdr/CALA0800791), Aug 13, 2008: SKIN. CRACKED. CRACK AT FORWARD CARGO DOOR HANDLE 22.25 INCHES FROM LOWER EDGE AND 17 INCHES FROM AFT EDGE. REMOVED FASTENER, VERIFIED CRACK CONTAINED AT FASTENER HOLE. REPAIR - [SDR CALA0800790](https://openairdocs.org/sdr/CALA0800790), Aug 13, 2008: STRINGER CLIP. CRACKED. STRINGER CLIP AT STATION 727D S23L CRACKED. REMOVED AND REINSTALLED STRINGER CLIP AT STATION 727D S23L PER B737-300 SRM 51-40-02. - [SDR CALA0800789](https://openairdocs.org/sdr/CALA0800789), Aug 13, 2008: SEAT TRACK. CORRODED. RIGHT INBOARD SEAT TRACK HAS CORROSION FROM FS 328-344. REMOVED SEAT TRACK PER B737 SRM 51-40-02, FABRICATED SEAT TRACK SECTION PER B737 SRM 53-00-52, ALODINED - [SDR CALA0800776](https://openairdocs.org/sdr/CALA0800776), Aug 6, 2008: STRUCTURE. DEFORMED. RIGHT WING OUTBOARD MID FLAP DAMAGED ON TRAILING EDGE. REPAIRED DAMAGED AREA RT WING O/B MID FLAP TRAILING EDGE WEDGE REF BOAC 737-300 SRM 51-70-10. - [SDR CALA0800775](https://openairdocs.org/sdr/CALA0800775), Aug 6, 2008: CHANNEL. CORRODED. CORROSION ON SUPPORT CHANNEL FOR NOSE LANDING GEAR VIEWER PANEL. REMOVED AND REPLACED SUPPORT CHANNEL WITH NEW CHANNEL AND REMOVED AND REINSTALLED UPPER VIEW TU - [SDR CALA0800770](https://openairdocs.org/sdr/CALA0800770), Aug 4, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL FOUND CRACKED AT FORWARD END BELOW TRANSITION ANGLE AT BODY STATION BS 500 STR 26L. REMOVED CRACKED ANGLE INTERCOSTAL BS 500 STR 26L. DRILLED NEW AN - [SDR CALA0800779](https://openairdocs.org/sdr/CALA0800779), Jul 28, 2008: SKIN. CRACKED. AFT CARGO DOOR FOUND WITH CRACK APPROX 2.5 INCH ABOVE AFT EDGE OF EXTERNAL HANDLE. REMOVED EXISTING REPAIR DOUBLER PER SRM 51-40-02 FROM AFT CARGO DOOR, FABRICA - [SDR CALA0800778](https://openairdocs.org/sdr/CALA0800778), Jul 28, 2008: ANGLE. CORRODED. R2 DOOR Z-ANGLE CORRODED AND STRAP AFT OF Z=ANGLE IS CORRODED. REMOVED CORRODED R2 Z-ANGLE AND STRAP IAW B737 SRM 51-40-02. CLEANED CORROSION FROM STRAP, FOUND - [SDR CALA0800409](https://openairdocs.org/sdr/CALA0800409), May 4, 2008: INTERCOSTAL. CORRODED. INTERCOSTAL AT STATION 840-855 S-25-R IS CORRODED (LEVEL 2 CORROSION). REPLACED INTERCOSTAL AT STATION 840-855 S-25-R IAW SRM 51-30-01. - [SDR CALA0700692](https://openairdocs.org/sdr/CALA0700692), Nov 19, 2007: SKIN. CRACKED. THE RAMP FOUND A 3.5 INCH CRACK IN AFT CARGO DOOR SKIN ABOVE FORWARD DOOR CUTOUT. DOUBLERS WERE INSTALLED IAW ECRA 5232-01096. A DIP WAS INITIATED TO ACCOMPLISH - [SDR CALA0700380](https://openairdocs.org/sdr/CALA0700380), Jul 8, 2007: SKIN. CORRODED. INSPECTION FOUND LT WING SKIN CORRODED FORWARD OF NR 3 SPOILER, I/B HINGE POINTS, APPROX WS 311.37. REPAIRED IAW ECRA 5720-02022. - [SDR CALA0700379](https://openairdocs.org/sdr/CALA0700379), Jul 8, 2007: SKIN. CORRODED. INSPECTION FOUND LT WING SKIN CORRODED ON TOP SURFACE AT APPROX WS 175 JUST FORWARD OF TRAPEZOIDAL PANEL NEAR CENTER LINE. LOCATED ABOUT 17 FASTENERS I/B OF O/B - [SDR CALA0700217](https://openairdocs.org/sdr/CALA0700217), Apr 25, 2007: WIRE HARNESS. UNKNOWN. FOUND EMERGENCY LIGHT ON SEAT 21C INOP. REPAIRED IAW AMM 33-51-81. - [SDR CALA0700216](https://openairdocs.org/sdr/CALA0700216), Apr 25, 2007: LIGHT. INOPERATIVE. FOUND EMERGENCY LIGHT ON SEAT 12C INOP. REPAIRED IAW AMM 33-51-81. - [SDR CALA0500211](https://openairdocs.org/sdr/CALA0500211), Jul 3, 2005: SKIN. CRACKED. INSPECTION FOUND 1.625 INCH CRACK IN FUSELAGE SKIN AT STA 727E, S22R TO S23R. SKIN REPAIRED IAW ECRA 5330-03459. - [SDR CALA0500177](https://openairdocs.org/sdr/CALA0500177), May 29, 2005: ACTUATOR. INOPERATIVE. THE LT MLG GREEN LIGHT DID NOT ILLUMINATE FOR SEVERAL MINUTES WHEN GEAR WAS EXTENDED ON APPROACH INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. WHEN MAINTENANC - [SDR CALA0400731](https://openairdocs.org/sdr/CALA0400731), Oct 29, 2004: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727D AND 727E AT S22L. REPAIRED IAW ECRA 5330-03388. - [SDR CALA0400697](https://openairdocs.org/sdr/CALA0400697), Oct 29, 2004: SKIN. CRACKED. MAINTENANCE NOTED A 2 INCH CRACK IN THE FUSELAGE SKIN AT STRINGER 22L, BETWEEN STA 727D AND 727E. THE SKIN WAS REPAIRED IAW ECRA 5330-03388. - [SDR CALA0400615](https://openairdocs.org/sdr/CALA0400615), Aug 25, 2004: SKIN. CRACKED. A 2.5 INCH CRACK WAS FOUND IN THE RT FUSELAGE SKIN AT STA 727 UNDER THE EMERGENCY EXIT LIGHT. A SKIN REPAIR WAS INSTALLED IAW ECRA 5330-03090. - [SDR CALA0400582](https://openairdocs.org/sdr/CALA0400582), Jul 21, 2004: SKIN. DAMAGED. INSPECTION FOUND THE LT AILERON DAMAGED ON THE LOWER BONDED SKIN PANEL. THE DAMAGE WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5751-01058. - [SDR CALA0400575](https://openairdocs.org/sdr/CALA0400575), Jul 15, 2004: STIFFENER. CORRODED. INSPECTION FOUND APB VERTICAL STIFFENER CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200. - [SDR CALA0400574](https://openairdocs.org/sdr/CALA0400574), Jul 15, 2004: BULKHEAD. CORRODED. INSPECTION FOUND APB WEB CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200. - [SDR CALA0400573](https://openairdocs.org/sdr/CALA0400573), Jul 14, 2004: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN NR 3 SLAT SKIN LOWER EDGE AT RIVET HOLES ADJACENT TO ACTUATOR. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW S - [SDR CALA0400571](https://openairdocs.org/sdr/CALA0400571), Jul 10, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 910-927. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-00-52. - [SDR CALA0400568](https://openairdocs.org/sdr/CALA0400568), Jul 7, 2004: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED IN E&E COMPARTMENT AT STA 360, LBL 5 BETWEEN S28L AND S29L. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND REPAIRED IAW S - [SDR CALA0400563](https://openairdocs.org/sdr/CALA0400563), Jul 3, 2004: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 907-927. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52 All 72: https://openairdocs.org/deregistered/N76355-2011-08-11/reports.md ## Other aircraft with N76355 - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N76355-undated): Cessna 140, S/N 10772, built 1946. Exported to Canada. Owner: [Personal Airplane Sales Corp](https://openairdocs.org/faa-owner/PERSONAL%20AIRPLANE%20SALES%20CORP) --- 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.