# N327AW: 1986 Boeing 737-3Q8, registration cancelled 2007-07-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 31, 2007 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Boeing 737-3Q8](https://openairdocs.org/model/boeing-737-3q8) (registry code 138447V) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Serial number: 23507 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, normal - Airworthiness date: July 18, 1986 - Certificate issued: May 5, 2006 - Last registry action: May 5, 2006 - Mode S code: A38866 - 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/N327AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=327AW - Page: https://openairdocs.org/deregistered/N327AW-2007-07-31 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 737-3Q8: https://openairdocs.org/model/boeing-737-3q8.md ## Service difficulty reports (190, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AWXA200500701](https://openairdocs.org/sdr/AWXA200500701), Jun 14, 2005: INDICATOR. FAILED. PHX - ABORTED TAKEOFF - FLT 792 - DURING TAKEOFF CAPTAINS AIRSPEED INDICATOR WAS FLAGGED AND NO AIRSPEED INDICATION. ABORTED TAKEOFF AT 90 KNOTS, RETURNED TO TH - [SDR AWXA200500193](https://openairdocs.org/sdr/AWXA200500193), Feb 12, 2005: LIGHT. BROKEN. PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE FOUND WIRES PULLED FROM CONNECTOR OF EMERGENCY ES - [SDR AWXA200500134](https://openairdocs.org/sdr/AWXA200500134), Jan 20, 2005: REVEAL. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK, A 3/4 INCH CRACK WAS FOUND IN R-1 DOOR FORWARD UPPER CORNER REVEAL. MAINTENANCE REMOVED CRACKED REVEAL FROM BS 298 TO BS - [SDR AWXA200500115](https://openairdocs.org/sdr/AWXA200500115), Jan 8, 2005: STRINGER CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 5/16 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 867, STR 1. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 86 - [SDR AWXA200500069](https://openairdocs.org/sdr/AWXA200500069), Jan 8, 2005: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT AFT LAVATORY SUBFLOOR PAN TO AFT PRESSURE BULKHEAD CLOSEOUT WEB (INTERCOSTAL FLOOR SEAL) A - [SDR AWXA200500028](https://openairdocs.org/sdr/AWXA200500028), Jan 6, 2005: WEDGE. DELAMINATED. MCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER SURFACE AT INBOARD END BETWEEN SS 131.50 AND SS 132.50. MAINTENANCE - [SDR AWXA200500138](https://openairdocs.org/sdr/AWXA200500138), Jan 3, 2005: FRAME. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER SURFACE, UPPER FLANGE, OF FRAME AT BS 847, RBL 17.50. MAINTENANCE CUTOUT CORRODED - [SDR AWXA200500035](https://openairdocs.org/sdr/AWXA200500035), Jan 3, 2005: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 6 INCHES CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D+17, STR 22 LT. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT BS 72 - [SDR AWXA200500118](https://openairdocs.org/sdr/AWXA200500118), Jan 2, 2005: WEB. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON R-1 DOOR THRESHOLD SHEAR WEB BETWEEN BS 344 AND BS 360, RBL 64 AND RBL 68. MAINTENANCE - [SDR AWXA200500047](https://openairdocs.org/sdr/AWXA200500047), Jan 2, 2005: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D + 17 INCHES, STR 24 RT. MAINTENANCE CUTOUT CRACKED SECTION OF FUSELA - [SDR AWXA200500023](https://openairdocs.org/sdr/AWXA200500023), Jan 2, 2005: SKIN. CRACKED. DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN EXTENDING FROM RIVET HOLE AT BS 727C, STR 15 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE AT BS 727C, - [SDR AWXA200500025](https://openairdocs.org/sdr/AWXA200500025), Dec 29, 2004: STRINGER CLIP. CRACKED. DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT AFT SIDE OF BS 1006, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 1006, - [SDR AWXA200500119](https://openairdocs.org/sdr/AWXA200500119), Dec 28, 2004: ATTACH BRACKET. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON L-1 DOOR AFT GIRT BAR ATTACH BRACKET AT BS 344 LBL 58. MAINTENANCE REMOVED CORRODED L-1 DOOR AFT - [SDR AWXA200500117](https://openairdocs.org/sdr/AWXA200500117), Dec 28, 2004: STIFFENER. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON AFT PRESSURE BULKEAD FORWARD FACE STIFFENER CHANNEL REPAIR ANGLE AT BS 1022, LBL 0.5, WL 195. MAI - [SDR AWXA200500116](https://openairdocs.org/sdr/AWXA200500116), Dec 28, 2004: FLOOR SUPPORT. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 324, RBL 10, WL 208. MAINTENANCE REMOV - [SDR AWXA200500100](https://openairdocs.org/sdr/AWXA200500100), Dec 28, 2004: INTERCOSTAL. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF INTERCOSTAL UPPER LEG AT BS 270, BETWEEN LBL 7 AND RBL 1. MAINTENANC - [SDR AWXA200500099](https://openairdocs.org/sdr/AWXA200500099), Dec 28, 2004: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 328, FROM BL "0" TO RBL 53. MAINTENANCE RE - [SDR AWXA200500070](https://openairdocs.org/sdr/AWXA200500070), Dec 28, 2004: WEB. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON LT AFT OUTBOARD SHEAR WEB, ADJACENT TO WATER LINE FITTING BETWEEN BS 996 AND BS 1005, LBL 3 - [SDR AWXA200500068](https://openairdocs.org/sdr/AWXA200500068), Dec 28, 2004: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 344 BETWEEN LBL 15 AND RBL 10. MAINTENANCE - [SDR AWXA200500060](https://openairdocs.org/sdr/AWXA200500060), Dec 28, 2004: ANGLE. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH CRACKS WERE FOUND IN CABIN FLOOR STIFFENER ANGLE BETWEEN BS 380 AND BS 400, AT BL 0. MAINTENANCE REMOVED CRACKED S - [SDR AWXA200500046](https://openairdocs.org/sdr/AWXA200500046), Dec 28, 2004: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 342, LBL 46, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL FROM BS 328 TO - [SDR AWXA200500045](https://openairdocs.org/sdr/AWXA200500045), Dec 28, 2004: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 326, RBL 34, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 326, RBL - [SDR AWXA200500133](https://openairdocs.org/sdr/AWXA200500133), Dec 27, 2004: CHANNEL. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT BETWEEN BS 353 AND BS 363. MAINTENANCE REMOVED STRINGER TIE CLIP AND C - [SDR AWXA200500132](https://openairdocs.org/sdr/AWXA200500132), Dec 27, 2004: SKIN. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF LOWER SKIN AT BS 358, ON INBOARD AND OUTBOARD SIDE OF STR 27 LT. MAI - [SDR AWXA200500126](https://openairdocs.org/sdr/AWXA200500126), Dec 27, 2004: CHANNEL. CRACKED. MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2" CRACK WAS FOUND IN VERTICAL STABILIZER LOWER ANGLE (CHANNEL) ON AFT SIDE OF RT AFT LUGS BS 1016, STR 2 RT. MAINTEN - [SDR AWXA200500123](https://openairdocs.org/sdr/AWXA200500123), Dec 27, 2004: CHANNEL. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN BS 355 AND BS 363, STR 27 LT. MAINTENANCE REMOVED CORRODED ST - [SDR AWXA200500122](https://openairdocs.org/sdr/AWXA200500122), Dec 27, 2004: ANGLE. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON INTERCOSTAL ATTACH ANGLE AT BS 357, OUTBOARD OF STRINGER 28 LT. MAINTENANCE REMOVED C - [SDR AWXA200500113](https://openairdocs.org/sdr/AWXA200500113), Dec 27, 2004: FRAME. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SIDE OF FRAME AT BS 360, BETWEEN STR 27 LT AND STR 28 LT. MAINTENANCE REMOVED SHEA - [SDR AWXA200500105](https://openairdocs.org/sdr/AWXA200500105), Dec 27, 2004: SHEAR TIE. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BS 1006, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE REMOVED CORRODED S - [SDR AWXA200500156](https://openairdocs.org/sdr/AWXA200500156), Dec 24, 2004: PAN. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT LAVATORY SUB-FLOOR PAN BETWEEN BS 1016 AND BS 1031, LBL - [SDR AWXA200500149](https://openairdocs.org/sdr/AWXA200500149), Dec 24, 2004: SILL. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHEC, EXFOLIATION CORROSION FOUND ON R-1 DOOR SILL INNER CHORD (CREASE BEAM) AT RBL 58, BETWEEN BS 298 AND 360, WL 208 AND WL 2 - [SDR AWXA200500137](https://openairdocs.org/sdr/AWXA200500137), Dec 24, 2004: WEB. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND IN 3 PLACES ON INBOARD SIDE OF WEB BETWEEN BS 847 AND BS 867, RBL 17.50. MAINTENANCE REMOVE - [SDR AWXA200500125](https://openairdocs.org/sdr/AWXA200500125), Dec 24, 2004: PANEL. CHAFED. MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE DORSAL FIN DOUBLER ON TOP OF FUSELAGE CHAFED IN 2 PLACES BETWEEN BS 857 AND BS 907, STR 2 LT AND STR 2 RT. MAIN - [SDR AWXA200500124](https://openairdocs.org/sdr/AWXA200500124), Dec 24, 2004: PAN. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT LAVATORY SUB-FLOOR PAN BETWEEN BS 1017 AND BS 1025, RB - [SDR AWXA200500120](https://openairdocs.org/sdr/AWXA200500120), Dec 24, 2004: STRAP. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CENTER FLOOR STRAP BETWEEN BS 1012 AND BS 1027, LBL 6 AND RBL 6. MAINTENANCE REMOV - [SDR AWXA200500114](https://openairdocs.org/sdr/AWXA200500114), Dec 24, 2004: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN RBL 4 AND RBL 34, WL 208. MA - [SDR AWXA200500110](https://openairdocs.org/sdr/AWXA200500110), Dec 24, 2004: WEB. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT OUTBOARD WEB, BETWEEN BS 995 AND BS 1012, RBL 39 AND - [SDR AWXA200500108](https://openairdocs.org/sdr/AWXA200500108), Dec 24, 2004: FLOOR SUPPORT. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT RBL 38, BETWEEN BS 997 AND BS 1004, WL 208. MAINTENANCE CUTOUT DAMAGE ON - [SDR AWXA200500106](https://openairdocs.org/sdr/AWXA200500106), Dec 24, 2004: FLOOR SUPPORT. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LBL 38, BETWEEN BS 1007 AND BS 1014, WL 208. - [SDR AWXA200500103](https://openairdocs.org/sdr/AWXA200500103), Dec 24, 2004: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN LBL 4 AND LBL 34, WL 208. MA - [SDR AWXA200500059](https://openairdocs.org/sdr/AWXA200500059), Dec 24, 2004: WEB. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT AFT OUTBOARD SHEAR WEB BETWEEN BS 996 AND BS 1005, LBL 39 TO LBL 4 - [SDR AWXA200500030](https://openairdocs.org/sdr/AWXA200500030), Dec 24, 2004: SILL. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON L-1 DOOR SILL INNER CHORD (CREASE BEAM) BETWEEN BS 300 AND BS 349, LBL 60, WL 208. MAINTENANCE REM - [SDR AWXA200500148](https://openairdocs.org/sdr/AWXA200500148), Dec 23, 2004: STRUCTURE. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION FOUND ON L-2 DOOR INNER CHORD (CREASE BEAM) AT LBL 48, BETWEEN BS 940 AND 996, WL 208 AND WL 209. - [SDR AWXA200500112](https://openairdocs.org/sdr/AWXA200500112), Dec 23, 2004: FLOOR SUPPORT. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT RBL 18, BETWEEN BS 969 AND BS 984, WL 208. MA - [SDR AWXA200500111](https://openairdocs.org/sdr/AWXA200500111), Dec 23, 2004: FLOOR SUPPORT. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LBL 18, BETWEEN BS 979 AND BS 983, WL 208. - [SDR AWXA200500109](https://openairdocs.org/sdr/AWXA200500109), Dec 23, 2004: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 986, BETWEEN LBL 45 AND RBL 45, WL 208. MAI - [SDR AWXA200500107](https://openairdocs.org/sdr/AWXA200500107), Dec 23, 2004: FLOORBEAM. CORRODED. DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 967, BETWEEN LBL 50 AND RBL 38, WL 208. MAINTENANCE CUTOUT DAMA - [SDR AWXA200500104](https://openairdocs.org/sdr/AWXA200500104), Dec 23, 2004: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 956, BETWEEN RBL 26 AND RBL 40, WL 208 - [SDR AWXA200500031](https://openairdocs.org/sdr/AWXA200500031), Dec 23, 2004: BOLT. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER LOWER FORWARD ATTACH BOLT BS 1096.428, LBL 35.50. MAINTENANCE RE - [SDR AWXA200500131](https://openairdocs.org/sdr/AWXA200500131), Dec 22, 2004: SKIN. CORRODED. MCN - MAJOR REPAIR - DURING C-17 CHECK, 2 EACH CRACKS WERE FOUND IN FUSELAGE SKIN AT L-1 DOOR LOWER AFT CORNER CUTOUT BS 339, STR 17 LT. MAINTENANCE CUTOUT DAMA All 190: https://openairdocs.org/deregistered/N327AW-2007-07-31/reports.md ## Other aircraft with N327AW - [Cancelled 2019-09-06](https://openairdocs.org/deregistered/N327AW-2019-09-06): Allied Drones AT28, S/N AT28-018-2.2. Registration expired, pending cancellation. Owner: [Unmanned Innovation Inc DBA](https://openairdocs.org/faa-owner/UNMANNED%20INNOVATION%20INC%20DBA), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) --- 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.