# N376US: 1984 Boeing 737-3B7, registration cancelled 2006-01-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 18, 2006 - Exported to: Indonesia - Status when cancelled: Valid registration - Airframe: [Boeing 737-3B7](https://openairdocs.org/model/boeing-737-3b7) (registry code 138447F) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 22955 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 11, 1984 - Certificate issued: January 3, 2006 - Last registry action: January 3, 2006 - Mode S code: A44BE8 - 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/N376US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=376US - Page: https://openairdocs.org/deregistered/N376US-2006-01-18 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 737-3B7: https://openairdocs.org/model/boeing-737-3b7.md ## Service difficulty reports (71, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA050003](https://openairdocs.org/sdr/USAA050003), Jan 7, 2005: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.750 INCH, STATION 74-2 AT STRINGER 19R. INSTALLED DOUBLER IAW 53-00-01. (M) - [SDR SB04162](https://openairdocs.org/sdr/SB04162), Dec 5, 2004: BATTERY PACK. DISCHARGED. ORD - MAINTENANCE REPORTED A FEW OF THE AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. - [SDR USAASB04117](https://openairdocs.org/sdr/USAASB04117), Sep 2, 2004: INDICATOR. MALFUNCTIONED. BOS - FLT 2022 - ON APPROACH TO BOS, FROM DCA, THE RIGHT FLAP LAGGED BEHIND THE LEFT FLAP TO THE POINT WHERE SELECTING FLAPS TO 25 UNITS, FLAPS ASSYMETRY PROTEC - [SDR USAASB04111](https://openairdocs.org/sdr/USAASB04111), Aug 16, 2004: FUSE. BLOWN. MAINTENANCE REPORTED THE EMERGENCY LIGHT ABOVE THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED THE FUSES AT THE M1132 BATTERY CHARGER ASSEMBLY. OPERA - [SDR USAA040424](https://openairdocs.org/sdr/USAA040424), Aug 11, 2004: FLANGE. CRACKED. PIT - FOUND ATTACH FLANGE CRACKED, 4 INCHES, LEFT RAM AIR INLET DUCT HANGAR ATTACHED TO LOWER SURFACE CETNER TANK. DURING REPLACEMENT, HOLE FOUND DAMAGED, OVERS - [SDR USAA040425](https://openairdocs.org/sdr/USAA040425), Aug 11, 2004: MOUNT. DAMAGED. PIT - FOUND MOUNT HOLE BORE, DAMAGE TO BORE OF MOUNT HOLE, AFT OUTBOARD MOUNT HOLE FOR RAM AIR DUCT LEFT SIDE. OVERSIZED HOLE, INSTALLED FREEZE PLUG PER EA 7884 - [SDR USAA040416](https://openairdocs.org/sdr/USAA040416), Aug 11, 2004: SPAR. CRACKED. PIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, RIGHT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED DOUBLER PER EA 78782. (M) - [SDR USAA040415](https://openairdocs.org/sdr/USAA040415), Aug 11, 2004: SPAR. CRACKED. PIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, AFT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED FREEZE PLUG PER EA 78781. (M) - [SDR USAA040421](https://openairdocs.org/sdr/USAA040421), Aug 9, 2004: BULKHEAD. CRACKED. PIT - FOUND BULKHEAD SKIN CRACKED .5 INCH, BL 0, WL 186, STATION 178 BULKHEAD. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-10-08, FIG 203. (M) - [SDR USAA040419](https://openairdocs.org/sdr/USAA040419), Aug 9, 2004: FITTING. CORRODED. PIT - FOUND BEAM FITTING PITTED AND ELONGED, LEFT L/G SUPPORT BEAM STABILIZER BEAM LUG FITTING, ATTACH BOLT HOLES. REAMED HOLES AND INSTALLED FREEZE PLUGS AND R - [SDR USAA040420](https://openairdocs.org/sdr/USAA040420), Aug 9, 2004: BULKHEAD. CRACKED. PIT - FOUND BULKHEAD SKIN CRACKED .75 INCH, STATION 178 BULKHEAD LBL 5.7 ABOVE WL 184, INBOARD SIDE. REMOVED CRACK AND INSTALLED DOUBLER PER EO 5300V155. (M) - [SDR USAA040423](https://openairdocs.org/sdr/USAA040423), Aug 4, 2004: SUPPORT ANGLE. CRACKED. PIT - FOUND SUPPORT ANGLE CRACKED 1.125 INCH LONG, LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE AT REAR SPAR STAITON 243. REPLACED SUPPORT ANGLE PER BOEING - [SDR USAA040370](https://openairdocs.org/sdr/USAA040370), Aug 3, 2004: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .75 INCH, UNDER DOUBLER PLATE, FS 328 ABOVE STRINGER 17R AT SILL PLATE FASTENERS. REPAIRED PLATES AND FILLERS INSTALLED PER SRM 53-10-0 - [SDR USAA040381](https://openairdocs.org/sdr/USAA040381), Jul 29, 2004: FITTING. CORRODED. PIT - FOUND FITTING CORRODED .25 INCH AREA, RIGHT WING AFT SPAR AND LG BEAM GEAR DOOR HINGE POINT OUTBOARD. REAMED AND COUTNERSINK NEW FITTING PER MM 20-50-11-2 - [SDR USAA040374](https://openairdocs.org/sdr/USAA040374), Jul 29, 2004: FITTING. CRACKED. FOUND AFT SPAR ATTACH FITTING CRACKED .25 INCH, LANDING GEAR BEAM AFT SPAR ATTACH FITTING, RIGHT WING AFT SPAR. MODIFIED PART INSTALLED PER EO 5702V054. (M) - [SDR USAA040378](https://openairdocs.org/sdr/USAA040378), Jul 28, 2004: FITTING. GALLED. PIT - FOUND GALLED FITTING, MLG WALKING BEAM, RIGHT WING REAR SPAR, STATION 200. DEFECTIVE PART REPLACED WITH IDENT PART NR PER BMM 20-50-11-2-912-002 FIG 202. - [SDR USAA040371](https://openairdocs.org/sdr/USAA040371), Jul 28, 2004: PANEL. CRACKED. PIT - FOUND PYLON CRACKED .5 INCH, UPPER PYLON SKIN AT ACCESS PANEL OPENING FOR PANEL 5827R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-0 - [SDR USAA040372](https://openairdocs.org/sdr/USAA040372), Jul 27, 2004: FITTING. CRACKED. PIT - FOUND FITTING CRACKED .75 INCH, RIGHT WING REAR SPAR STATION 224. INSTALLED NEW SUPPORT FITTING PER EA 78781. (M) - [SDR USAA040382](https://openairdocs.org/sdr/USAA040382), Jul 25, 2004: ATTACH FITTING. CORRODED. PIT - FOUND ACTUATOR ATTACH FITTING .25 INCH AREA, RIGHT MLG BEAM NR 6 SPOILER ACTUATOR ATTACH FITTING. INSTALLED NEW FITTING PER BMM 20-50-11-2-912-002 FIG 202 - [SDR USAA040422](https://openairdocs.org/sdr/USAA040422), Jul 23, 2004: SUPPORT BEAM. CORRODED. PIT - FOUND SUPPORT BEAM CORRODED .5 INCH BY .25 INCH, AND .375 INCH BY .25 INCH BY .25 INCH, CORROSION PITTING WITH WEAR, LEFT MLG SUPPORT BEAM, STAB BEAM LUG - [SDR USAA040373](https://openairdocs.org/sdr/USAA040373), Jul 23, 2004: BULKHEAD. CRACKED. PIT - FOUND BULKHEAD WEB CRACKED .5 INCH, FS 178 BULKHEAD WEB, B/L0, WL/L 186. INSTALLED DOUBLER, FILLER PER SRM 53-10-08 FIG 203. (M) - [SDR USAA040383](https://openairdocs.org/sdr/USAA040383), Jul 22, 2004: STIFFENER. GOUGED. PIT - FOUND VERTICAL STIFFENER GOUGED .020 INCH, LT SIDE OF KEELBEAM AT STATION 634, INBOARD. FABRICATED AND REPLACED STIFFENER PER SRM 53-60-12 FIG 1. (M) - [SDR USAA040376](https://openairdocs.org/sdr/USAA040376), Jul 21, 2004: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED .5 INCH, FS 1120, STRINGER 5A, LEFT SIDE. INSTALLED REPAIR ANGLE PE TYPICAL REPAIR 53-80-04. (M) - [SDR USAA040377](https://openairdocs.org/sdr/USAA040377), Jul 21, 2004: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH, BELTFRAME STATION 767 AT STRINGER S14L. INSTALLED DOUBLER AND FILLERS PER SRM 53-00-07 PAGES 202-203. (M) - [SDR USAA040375](https://openairdocs.org/sdr/USAA040375), Jul 21, 2004: BULKHEAD. CRACKED. PIT - FOUND SKIN CRACKED 1.25 INCH, THROUGH FASTENER STATION 1040 BL-0 AFT PRESSURE BULKHEAD, 9 FASTENERS ABOVE CENTER OF BULKHEAD. MANUFACTURED FILLER AND DOUB - [SDR USAA040379](https://openairdocs.org/sdr/USAA040379), Jul 21, 2004: INTERCOSTAL. CORRODED. PIT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH AREA, FS 990, STATION 21, LEFT. FABRICATED NEW INTERCOSTAL PER 51-40-02. CORROSION LEVEL 1, TASK NR C53-202-01 - [SDR USAA040380](https://openairdocs.org/sdr/USAA040380), Jul 21, 2004: FLOORBEAM. CORRODED. PIT - FOUND BEAM CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BEAM, FS 993, RBL 14-44. MANUFACTURED NEW SUPPORT ANGLE PER BOEING DWG 65C19883. CORROSION LEVEL - [SDR USAA040369](https://openairdocs.org/sdr/USAA040369), Jul 19, 2004: BULKHEAD. CRACKED. PIT - FOUND BULKHEAD SKIN CRACKED .25 INCH, AT RIVET OUTBOARD OF RBL 57 AT WL 234 STATION 178 BULKHEAD. INSTALLED DOUBLER PER EO 5300V153. (M) - [SDR USAA040368](https://openairdocs.org/sdr/USAA040368), Jul 13, 2004: SKIN. DELAMINATED. PIT - FOUND TOP SKIN AND CORE MATERIAL DELAMINATED 3 INCH BY 4 INCH AREA, NR 3 SLAT INBOARD T/E CORNER. INSTALLED NEW CORE, INSTALLED FILLER AND UPPER DOUBLER P - [SDR USAA040367](https://openairdocs.org/sdr/USAA040367), Jul 13, 2004: SKIN. CHAFED. PIT - FOUND LOWER SKIN SURFACE CHAFED 2 INCH BY 1 INCH, NR 4 SLAT INBOARD TRAILING EDGE. REMOVED CHAFED AREA, BONDED, SEALED EDGE AND REFINISHED PER BOEING SRM - [SDR USAA040437](https://openairdocs.org/sdr/USAA040437), Jul 8, 2004: SKIN. CORRODED. PIT - FOUND SKIN CORRODED .25 INCH BY .5 INCH SPOT, AFT PRESS BULKHEAD, AFT SIDE, STATION 1016 BL 0 . CLEANED LIGHT CORROSION PER SRM 51-21-31. (M) - [SDR USAA040341](https://openairdocs.org/sdr/USAA040341), Jul 7, 2004: WEB. CRACKED. PIT FOUND WEB CRACKED 2 INCHES, STATION 1040, BL 0, 9 RIVETS UP FROM CENTER OF AFT PRESSURE DOME. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER - [SDR USA2004F00052](https://openairdocs.org/sdr/USA2004F00052), May 8, 2004: SHUTOFF VALVE. FAILED. RT PACK TRIP OFF LIGHT ILLUMINATED, WOULD NOT RESET. LT PACK TRIP OFF LIGHT ILLUMINATED DURING TEMP ADJMT. IMMEDIATE DESCENT WAS INITIATED TO 10,000 FT BUT CABI - [SDR USAASB04049](https://openairdocs.org/sdr/USAASB04049), May 3, 2004: WIRE HARNESS. FAULTY. PIT - FLT 991 - EN ROUTE FROM PHL TO DFW, SOUTH OF PIT, CREW REPORTED THE NR 2 ENGINE EGT SPIKED TO 1,000 DEGREES WITH THE RED OVERHEAT LIGHT ILLUMINATING. ALL - [SDR USAA040187](https://openairdocs.org/sdr/USAA040187), Apr 29, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.35 INCHES, STATION 760 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) - [SDR USAA030192](https://openairdocs.org/sdr/USAA030192), Sep 13, 2003: SKIN. CRACKED. FOUND SKIN CRACKED .5 INCH, AFT ENTRY DOOR LOWER HINGE CUTOUT AT STATION 947.5, S-14L. DOUBLERS INSTALLED PER EA 76982 AND SRM 53-60-01, FIG 1, FIG 207. (M) - [SDR USAASB02093](https://openairdocs.org/sdr/USAASB02093), May 13, 2002: BATTERY PACK. DISCHARGED. EWR - MAINTENANCE FOUND THE FORWARD TO MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB02056](https://openairdocs.org/sdr/USAASB02056), Mar 18, 2002: BATTERY PACK. CRACKED. PHL - MAINTENANCE REPORTED AN OVERHEAD EMERGENCY LIGHT BATTERY PACK, FOR LOW LEVEL LIGHTING, WAS LEAKING FROM CEILING INTO OVERHEAD COMPARTMENT ABOVE SEAT ROW 1 - [SDR USAASB02055](https://openairdocs.org/sdr/USAASB02055), Mar 18, 2002: LIGHT. FAILED. IND - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 6ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET ASSEMBLY AT SEAT ROW 6 ABC. OPERA - [SDR USAASB01251](https://openairdocs.org/sdr/USAASB01251), Sep 11, 2001: BATTERY PACK. DISCHARGED. ORD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MID LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL C - [SDR USAASB00325](https://openairdocs.org/sdr/USAASB00325), Nov 22, 2000: ACM. OVERSERVICED. PIT - FLT 9550 - AIRCRAFT WAS ON A TEST HOP AFTER A MAINTENANCE CHECK, WHEN JUST AFTER TAKEOFF, A SMALL AMOUNT OF SMOKE WAS NOTED IN THE COCKPIT. FLIGHT RETURNE - [SDR USAA001979](https://openairdocs.org/sdr/USAA001979), Nov 22, 2000: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .25 INCH, FS 663.75 AT CUTOUT FOR NR 1 STRINGER. INSTALLED REPAIR PER SRM 53-00-07 FIG 207 SHT 6. (M) - [SDR USAA001947](https://openairdocs.org/sdr/USAA001947), Nov 18, 2000: SKIN. DELAMINATED. PIT - FOUND RUDDER DELAMINATED IN 7 AREAS, LEFT AND RIGHT RUDDER SKIN DELAMINATE 1ST LAYER. 200-230 DEGREE CURE. WET LAY UP REPAIR USING 51-70-17 THEN BALANCED - [SDR USAA002107](https://openairdocs.org/sdr/USAA002107), Nov 3, 2000: BRACKET. CRACKED. PIT - FOUND ANGLE BRACKET CRACKED .25 INCH, STATION 440 BETWEEN STRINGER 8 AND 9 RT OVERHEAD PIN ATT PT. INSTALLED .045 INCH ANGLE COUPLER PER US AIRWAYS TYPICA - [SDR USAA002108](https://openairdocs.org/sdr/USAA002108), Oct 25, 2000: FITTING. CORRODED. PIT - FOUND FITTINGS CORRODED .75 INCH BY 1 INCH, STRINGER FITTINGS STATION 1016 STRINGER 23L, 24L, 25L. CORROSION LEVEL 1 TASK NR C53-701-01. CLEANED CORROSION - [SDR USAA002110](https://openairdocs.org/sdr/USAA002110), Oct 25, 2000: RING. CORRODED. PIT - FOUND DOME SUPPORT RING CORRODED .5 INCH BY 1.5 INCH, STATION 1016 DOME SUPPORT RING 23R-21R AND 18R-8R. CLEANED CORROSION, TREATED AND PRIMED PER 51-20-0 - [SDR USAA002109](https://openairdocs.org/sdr/USAA002109), Oct 3, 2000: BRACKET. CRACKED. PIT - FOUND ANGLE BRACKET CRACKED .25 INCH, STATION 380 BETWEEN STRINGER 8 AND 9 RT OVERHEAD BIN ATTACH PT. INSTALLED .045 INCH ANGLE DOUBLER PER US AIRWAYS TYP - [SDR USAA002111](https://openairdocs.org/sdr/USAA002111), Oct 3, 2000: WEB. CRACKED. PIT - FOUND WEB CRACKED 1.5 INCH, WL 207, RBL 28 AFT STATION 178 LIGHTENING HOLE. REMOVED, FABRICATED NEW WEB FROM .071 2024-T3 AND INSTALLED. (M) - [SDR USAA001726](https://openairdocs.org/sdr/USAA001726), Oct 3, 2000: SKIN. CRACKED. PIT - SKIN CRACKED .25 INCH, STA 440 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED .045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X) - [SDR USAA001725](https://openairdocs.org/sdr/USAA001725), Oct 3, 2000: SKIN. CRACKED. PIT - SKIN CRACKED .25 INCH, STA 380 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED .045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X) All 71: https://openairdocs.org/deregistered/N376US-2006-01-18/reports.md ## Other aircraft with N376US - [Registered now](https://openairdocs.org/aircraft/N376US): Costruzioni Aeronautiche Tecna P2010 TDI, S/N 376/US --- 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.