# N326AW: 1985 Boeing 737-301, registration cancelled 2007-05-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 29, 2007 - Exported to: Belgium - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23258 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 25, 1985 - Certificate issued: June 28, 2001 - Last registry action: July 18, 2006 - Mode S code: A384AF - 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/N326AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=326AW - Page: https://openairdocs.org/deregistered/N326AW-2007-05-29 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 737-301: https://openairdocs.org/model/boeing-737-301.md ## Service difficulty reports (168, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AWXA200601127](https://openairdocs.org/sdr/AWXA200601127), Jul 5, 2006: BATTERY PACK. INOPERATIVE. PHX - EEL - FLT 33 - LG 4104284 - LEFT EMERGENCY OVERWING EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-51-2. OPERATIONAL CHECKS GOOD. - [SDR AWXA200600855](https://openairdocs.org/sdr/AWXA200600855), May 24, 2006: COALESCER BAG. ODOR. LAS - BURNING SMELL - F/A`S REPORTED A BURNING SMELL OF RUBBER COMING FROM THE AFT GALLEY AREA AT CRUISE ABOUT 25 MINS PRIOR TO LANDING IN LAS WITH NO IND OF SM - [SDR AWXA200600767](https://openairdocs.org/sdr/AWXA200600767), May 2, 2006: UNKNOWN. LOW PRESSURE. EN ROUTE, CREW REPORTED THAT AT FL 340 AUTO STANDBY DID NOT HOLD ALTITUDE. CREW DESCENDED TO FL 100. MASKS DID NOT DEPLOY DUE TO GRADUAL LOSS OF PRESSURIZATION. - [SDR AWXA200501105](https://openairdocs.org/sdr/AWXA200501105), Sep 25, 2005: CIRCUIT BREAKER. DAMAGED. CREW REPORTED "ON CLIMB OUT LEFT GENERATOR CAME OFF LINE FOLLOWED BY RIGHT GENERATOR. AC POWER LOST MOMENTARY. CYCLED BOTH GENERATORS. BOTH CAME BACK ON." CREW - [SDR AWXA200500900](https://openairdocs.org/sdr/AWXA200500900), Jul 29, 2005: WARNING SYSTEM. FALSE ACTIVATION. SJC - ABORTED TAKEOFF - FLT 165 - ABORTED TAKEOFF FOR UNSPECIFIED WARNING. CLEARED RUNWAY THEN RE-ATTEMPTED T/O. TAKEOFF WAS UNEVENTFUL. - [SDR AWXA200500831](https://openairdocs.org/sdr/AWXA200500831), Jul 19, 2005: LIGHT. INOPERATIVE. DEN - EEL - DURING 4 DAY CHECK DISCOVERED THE EMERGENCY EXIT LIGHT AT ROW 19C IS INOPERATIVE. MAINTENANCE PLACED ON MEL. REQUIRES NEW LIGHT ASSEMBLY. - [SDR AWXA200500614](https://openairdocs.org/sdr/AWXA200500614), May 26, 2005: ALTIMETER. FAULTY. AT CRUSE ALTITUDE OF 360FL CABIN ALTITUDE HORN CAME ON & CABIN PRESSURE UNCONTROLLABLE. A BLEED TRIP OCCURRED ON NR 1 PACK ALONG WITH 2 DUCT OVERHEATS IN 3 MIN - [SDR AWXA200500297](https://openairdocs.org/sdr/AWXA200500297), Feb 19, 2005: CHANNEL. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND AFT CARGO DOOR SILL LOWER CHANNEL AT BS 837, STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR S - [SDR AWXA200500307](https://openairdocs.org/sdr/AWXA200500307), Feb 17, 2005: FRAME. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FRAME AT FORWARD SIDE OF BS 847 JUST INBOARD OF STR 25 RT. MAINTENANCE REMOVED DAMAGED SECTION OF - [SDR AWXA200500298](https://openairdocs.org/sdr/AWXA200500298), Feb 15, 2005: CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FRAME ATTACH CLIP AT BS 807, STR 25 RT. MAINTENANCE REMOVED CRACKED A - [SDR AWXA200500309](https://openairdocs.org/sdr/AWXA200500309), Feb 13, 2005: BEAR STRAP. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND INTERNAL SURFACE OF AFT CARGO DOOR CUTOUT LOWER FORWARD BEAR STRAP BS 807, STR 25 RT. MAINTENANCE CUT - [SDR AWXA200500334](https://openairdocs.org/sdr/AWXA200500334), Feb 12, 2005: WEB. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL WEB BETWEEN BS 794 AND BS 799, AT STR 25 RT. MAINTENANCE REMOVED CORRODED AFT - [SDR AWXA200500332](https://openairdocs.org/sdr/AWXA200500332), Feb 12, 2005: ANGLE. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL ATTACH ANGLE AT BS 847, BETWEEN STR 24 RT AND STR 25 RT. MAINTENANCE REMOVED C - [SDR AWXA200500315](https://openairdocs.org/sdr/AWXA200500315), Feb 12, 2005: FRAME. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR FORWARD TORQUE BOX FRAME AT BS 794.3, STR 25 RT. MAINTENANCE REMOVED CORRODED SECTI - [SDR AWXA200500314](https://openairdocs.org/sdr/AWXA200500314), Feb 12, 2005: STRAP. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL UPPER STRAP BETWEEN BS 794 AND BS 847 AT STR 25 RT. MAINTENANCE RE - [SDR AWXA200500303](https://openairdocs.org/sdr/AWXA200500303), Feb 10, 2005: FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK 3 EACH .25 INCH CRACKS WERE FOUND IN FUSELAGE FRAME AT BS 663.75, BETWEEN STR 2 RT & STR 3 LT. MAINTENANCE CUT OUT CRACKS - [SDR AWXA200500293](https://openairdocs.org/sdr/AWXA200500293), Feb 10, 2005: FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .1875 INCH CRACKS WERE FOUND IN R-2 DOOR LOWER FORWARD FRAME SECTION BS 957, STR 16 RT. MAINTENANCE CUT OUT DAMAGE - [SDR AWXA200500235](https://openairdocs.org/sdr/AWXA200500235), Feb 8, 2005: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM STIFFENER ANGLE ON AFT SIDE FLOORBEAM AT BS 328, BETWEEN RBL 43 AND RBL 60. - [SDR AWXA200500310](https://openairdocs.org/sdr/AWXA200500310), Feb 7, 2005: REVEAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-2 DOOR LOWER FORWARD REVEAL AT 957, STR 17 RT. MAINTENANCE REMOVED AND REPLACED R-2 DOOR LO - [SDR AWXA200500232](https://openairdocs.org/sdr/AWXA200500232), Feb 7, 2005: CREASE BEAM. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN WEB UNDER CREASE BEAM INNER CHORD AT BS 986.5, LBL 43. MAINTENANCE REMOVED DAMAGED WEB FROM - [SDR AWXA200500292](https://openairdocs.org/sdr/AWXA200500292), Feb 3, 2005: SKIN. WORN. MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND FUSELAGE SKIN WORN IN SEVERAL AREAS AT LT AND RT DORSAL FIN SEALS BETWEEN BS 860 AND BS 907.5. MAINTENANCE CUT OUT - [SDR AWXA200500326](https://openairdocs.org/sdr/AWXA200500326), Jan 31, 2005: SUPPORT. CORRODED. MCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL OUTER SUPPORT WBL 185.0. MAINTENANCE REMOVED AND RE - [SDR AWXA200500325](https://openairdocs.org/sdr/AWXA200500325), Jan 31, 2005: GIMBAL JOINT. CORRODED. MCN - FLIGHT CONTROL - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBAL INDEX PLATE WBL 185.0. MAINTENANCE REMOVED AND REPL - [SDR AWXA200500324](https://openairdocs.org/sdr/AWXA200500324), Jan 31, 2005: SUPPORT. CORRODED. MCN - FLIGHT CONTROL - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBAL OUTER SUPPORT WBL 71.24. MAINTENANCE REMOVED AN - [SDR AWXA200500226](https://openairdocs.org/sdr/AWXA200500226), Jan 31, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE SKIN OF THE NR 2 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD END, SLAT STA 251. MAINTENANCE CUT OUT DAMA - [SDR AWXA200500191](https://openairdocs.org/sdr/AWXA200500191), Jan 31, 2005: GIMBAL JOINT. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL INDEX PLATE AT WBL 184. MAINTENANCE REMOVED AND R - [SDR AWXA200500190](https://openairdocs.org/sdr/AWXA200500190), Jan 31, 2005: GIMBAL JOINT. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP OUTBOARD GIMBAL OUTER SUPPORT AT WBL 184. MAINTENANCE REMOVED AND - [SDR AWXA200500329](https://openairdocs.org/sdr/AWXA200500329), Jan 28, 2005: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD LOWER CUTOUT OF R-2 DOOR BS 947. MAIN - [SDR AWXA200500296](https://openairdocs.org/sdr/AWXA200500296), Jan 28, 2005: STRAP. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN LOWER FORWARD INBOARD EDGE OF FRAME STRAP AT BS 349, STR 16 LT. MAINTENANCE REMOVED DAMAG - [SDR AWXA200500248](https://openairdocs.org/sdr/AWXA200500248), Jan 28, 2005: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN L-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 317, STR 14 LT. MAINTENANCE CUT OUT CRACK - [SDR AWXA200500294](https://openairdocs.org/sdr/AWXA200500294), Jan 27, 2005: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .0625 INCH CRACKS WERE FOUND IN L-1 DOOR FORWARD FRAME INTERCOSTAL WEB BS 294.5, STR 7 LT. MAINTENANCE REMOVED DAM - [SDR AWXA200500287](https://openairdocs.org/sdr/AWXA200500287), Jan 27, 2005: CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .0265 INCH CRACK WAS FOUND IN RADIUS OF ANGLE CLIP AT AFT SIDE OF STRINGER SPLICE CHANNEL BS 348.2, STR 16 LT. MAINTENA - [SDR AWXA200500286](https://openairdocs.org/sdr/AWXA200500286), Jan 27, 2005: STRINGER CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN INBOARD FORWARD LOWER EDGE OF STRINGER SPLICE CHANNEL CLIP & FRAME STRAP AT BS 349, STR 1 - [SDR AWXA200500282](https://openairdocs.org/sdr/AWXA200500282), Jan 27, 2005: WEB. CHAFED. MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND L-1 DOOR UPPER HINGE CUTOUT UPPER WEB CHAFED ON LOWER SIDE BETWEEN BS 294.5 AND BS 303.9, STR 13 LT. MAINTENANCE RE - [SDR AWXA200500261](https://openairdocs.org/sdr/AWXA200500261), Jan 27, 2005: CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK, A 3" CRACK WAS FOUND IN AFT SIDE L-1 DOOR FRAME INTERCOSTAL ATTACH CLIP AT BS 348.2, STR 17 LT. MAINTENANCE REMOVED CRAC - [SDR AWXA200500302](https://openairdocs.org/sdr/AWXA200500302), Jan 26, 2005: LIGHT. INOPERATIVE. MCN - EEL - DURING C-18 CHECK FOUND THE L-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED L-2 DOOR EMERGENCY EXIT SIGN, OPERATIONAL CHE - [SDR AWXA200500328](https://openairdocs.org/sdr/AWXA200500328), Jan 25, 2005: PLATE. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND IN CLOSE PANEL BETWEEN FORWARD END OF R-2 DOOR CUTOUT AND BS 947. MAINTENANCE REMOVED CRACKED - [SDR AWXA200500327](https://openairdocs.org/sdr/AWXA200500327), Jan 25, 2005: REVEAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN R-1 DOOR UPPER AFT REVEAL. MAINTENANCE REMOVED CRACKED R-1 DOOR UPPER AFT REVEAL FROM BS 320 - [SDR AWXA200500301](https://openairdocs.org/sdr/AWXA200500301), Jan 25, 2005: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN EMANATING FASTENER HOLE AT LOWER HINGE CUTOUT BS 328, STR 15-16 RT - [SDR AWXA200500300](https://openairdocs.org/sdr/AWXA200500300), Jan 25, 2005: FLASHLIGHT. INOPERATIVE. MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT AFT LAVATORY WALL EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT LAVAT - [SDR AWXA200500299](https://openairdocs.org/sdr/AWXA200500299), Jan 25, 2005: FLASHLIGHT. INOPERATIVE. MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE LT FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY F - [SDR AWXA200500285](https://openairdocs.org/sdr/AWXA200500285), Jan 25, 2005: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT FORWARD UPPER CORNER CUTOUT OF R-1 DOOR. MAI - [SDR AWXA200500331](https://openairdocs.org/sdr/AWXA200500331), Jan 24, 2005: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 986, LBL 44, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 986 - [SDR AWXA200500290](https://openairdocs.org/sdr/AWXA200500290), Jan 24, 2005: SILL. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL INNER CHORD BETWEEN BS 950 AND BS 994, LBL 50. MAINTENANCE REMOVED CORRODED L-2 DOOR - [SDR AWXA200500262](https://openairdocs.org/sdr/AWXA200500262), Jan 24, 2005: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK, A 0.8125 INCH CRACK WAS FOUND IN UPPER AFT CORNER OF INTERCOSTAL AT BS 293, LBL 33, WL 208. MAINTENANCE CUTOUT DAMAGE IN - [SDR AWXA200500249](https://openairdocs.org/sdr/AWXA200500249), Jan 24, 2005: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN UPPER RADIUS OF INTERCOSTAL AT BS 306, LBL 27. MAINTENANCE CUT OUT DAMAGE IN UPPER RADIUS - [SDR AWXA200500333](https://openairdocs.org/sdr/AWXA200500333), Jan 23, 2005: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOORBEAM T-CAP AT BS 1016, RBL 5, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM T-CAP AT BS 101 - [SDR AWXA200500295](https://openairdocs.org/sdr/AWXA200500295), Jan 23, 2005: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND LOWER SURFACE OF TRANVERSE FLOORBEAM T-CAP AT BS 986, BETWEEN RBL 40 AND RBL 44, WL 208. MAINTENANCE - [SDR AWXA200500229](https://openairdocs.org/sdr/AWXA200500229), Jan 23, 2005: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT BS 445, BL 0. MAINTENANCE REMOVED EXISTING - [SDR AWXA200500185](https://openairdocs.org/sdr/AWXA200500185), Jan 23, 2005: WEB. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF SHEAR WEB BETWEEN BS 1009 AND BS 1015, LBL 41 AND LBL 45, WL 207.5. M All 168: https://openairdocs.org/deregistered/N326AW-2007-05-29/reports.md ## Other aircraft with N326AW - [Registered now](https://openairdocs.org/aircraft/N326AW): Pilatus PC-12/47G, S/N 3131 --- 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.