# N323AW: 1987 Boeing 737-300, registration cancelled 2006-06-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 23, 2006 - Exported to: Australia - Status when cancelled: Valid registration - Airframe: [Boeing 737-300](https://openairdocs.org/model/boeing-737-300) (registry code 138447P) - 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: 23684 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 16, 1995 - Certificate issued: March 29, 1999 - Last registry action: July 29, 2003 - Mode S code: A3798A - 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/N323AW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=323AW - Page: https://openairdocs.org/deregistered/N323AW-2006-06-23 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 737-300: https://openairdocs.org/model/boeing-737-300.md ## Service difficulty reports (153, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AWXA200600229](https://openairdocs.org/sdr/AWXA200600229), Jan 31, 2006: BATTERY. INOPERATIVE. MCN - EEL - DURING C16 CHECK DISCOVERED 2 EMERGENCY FLASHLIGHTS ON THE FORWARD WALL OF AFT LT LAV INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FLASHLIGHT - [SDR AWXA200600195](https://openairdocs.org/sdr/AWXA200600195), Jan 18, 2006: SUPPORT FITTING. CRACKED. MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED RT MLG SUPPORT BEAM OUTBOARD AFT SUPPORT FITTING CRACKED 2.75 INCHES IN LENGTH. MAINTENANCE REMOVED AND REPLACE - [SDR AWXA200600085](https://openairdocs.org/sdr/AWXA200600085), Dec 30, 2005: STRINGER CLIP. CRACKED. MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED, .50 INCHES, AT STR 10L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 10L AND B - [SDR AWXA200600084](https://openairdocs.org/sdr/AWXA200600084), Dec 30, 2005: STRINGER CLIP. CRACKED. MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED, .75 INCHES, AT STR 5L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 5L AND BS - [SDR AWXA200600015](https://openairdocs.org/sdr/AWXA200600015), Dec 28, 2005: REGULATOR. STUCK. EMERGENCY EQUIPMENT, DURING C 16 CHECK DISCOVERED CAPTAIN'S OXYGEN MASK DEMAND REGULATOR STUCK IN EMERGENCY POSITION. MAINTENANCE REMOVED AND REPLACED THE O2 MA - [SDR AWXA200600087](https://openairdocs.org/sdr/AWXA200600087), Dec 21, 2005: ANGLE. CRACKED. MCN - DURING C16 CHECK DISCOVERED REINFORCEMENT ANGLE CRACKED AT BS 294.5, WL 208 AND FROM BL 40R TO BL 55R. MAINTENANCE REMOVED AND INSTALLED FABRICATED REINFO - [SDR AWXA200600197](https://openairdocs.org/sdr/AWXA200600197), Dec 18, 2005: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED LEVEL TWO CORROSION ON FLOORBEAM LOCATED AT BS 294.5, WL 207 AND BL 44R. RE-WORK WAS FOUND TO BE OUT OF LIMITS - [SDR AWXA200600108](https://openairdocs.org/sdr/AWXA200600108), Dec 18, 2005: STRUCTURE. CORRODED. MCN - DURING C19 CHECK DISCOVERED CORROSION ON RT CHORD FROM BS 288 TO BS 292, WL 208 AND BL 52R. REMOVED CORROSION AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IA - [SDR AWXA200600083](https://openairdocs.org/sdr/AWXA200600083), Dec 16, 2005: STRINGER CLIP. CRACKED. MCN - DURING C16 CHECK DISCOVERED STRINGER CLIP CRACKED, .25 INCHES, AT STR 8L AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT STR 8L AND BS - [SDR AWXA200600082](https://openairdocs.org/sdr/AWXA200600082), Dec 16, 2005: STRINGER CLIP. CRACKED. MCN - DURING C16 CHECK DISCOVERED STRINGER TIE CRACKED, .25 INCHES, AT STR 7L. AND BS 1006. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE AT STR 7L AND BS - [SDR AWXA200600092](https://openairdocs.org/sdr/AWXA200600092), Dec 15, 2005: SKIN. DEBONDED. MCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DISBONDED 3" FROM THE INBOARD EDGE FROM WS 230.68L TO WS 232.68L. MAINTENANCE REMOVED DISBONDED SKIN IAW - [SDR AWXA200600081](https://openairdocs.org/sdr/AWXA200600081), Dec 14, 2005: STRINGER. DAMAGED. MCN - DURING C16 CHECK DISCOVERED STRINGER 9R, BS 907 TO BS 947, HAS 1/4" HOLE IN IT. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER AT STRINGER 9R, BS 907 TO B - [SDR AWXA200600196](https://openairdocs.org/sdr/AWXA200600196), Dec 13, 2005: WIRE HARNESS. DAMAGED. MCN - EEL - DURING C16 CHECK DISCOVERED EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED FROM BS 360 TO BS947, WL 208 AND BL 26L. MAINTENANCE REPAIRED SPLICES AND CO - [SDR AWXA200600095](https://openairdocs.org/sdr/AWXA200600095), Dec 9, 2005: SKIN. CRACKED. MCN - DURING C16 CHECK DISCOVERED, THE R1 DOOR LOWER HINGE CUTOUT, LOWER RADIUS, CRACKED, .25 INCHES AT BS 294 AND STRINGER 13R. MAINTENANCE CUTOUT DAMAGED AREA - [SDR AWXA200600094](https://openairdocs.org/sdr/AWXA200600094), Dec 9, 2005: FRAME. CRACKED. MCN - DURING C16 CHECK DISCOVERED THE L2 DOOR FRAME CRACKED, .125 INCHES, AT BS 957 JUST BELOW STR 8L. MAINTENANCE REMOVED CRACKED L2 DOOR FRAME FROM BS 957, ST - [SDR AWXA200600080](https://openairdocs.org/sdr/AWXA200600080), Dec 9, 2005: CHANNEL. CRACKED. MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, 1.1 INCHES, AT BS 907 AND STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL AT BS 907 AND STR 4R IAW BOEI - [SDR AWXA200600079](https://openairdocs.org/sdr/AWXA200600079), Dec 9, 2005: CHANNEL. CRACKED. MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, 1.2 INCHES, AT BS 907 AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL AT BS 907 AND STR 4L IAW BOEI - [SDR AWXA200600097](https://openairdocs.org/sdr/AWXA200600097), Dec 7, 2005: SKIN. CRACKED. MCN - DURING C16 CHECK DISCOVERED 5 CRACKS, .80 INCHES EACH, ON THE BOTTOM OF THE NR 6 SLAT SKIN, FROM SS 320R TO SS 325R. MAINTENANCE CUT OUT DAMAGED SKIN IAW - [SDR AWXA200600096](https://openairdocs.org/sdr/AWXA200600096), Dec 7, 2005: SKIN. CRACKED. MCN - DURING C16 CHECK DISCOVERED 4 CRACKS, .500 INCHES EACH, ON THE BOTTOM OF THE NR 4 SLAT SKIN, FROM SS 57R TO SS 61R. MAINTENANCE CUT OUT DAMAGED SKIN IAW B - [SDR AWXA200600089](https://openairdocs.org/sdr/AWXA200600089), Dec 7, 2005: SUPPORT. CORRODED. MCN - DURING C16 CHECK DISCOVERED CORROSION AROUND 4 FASTENER HOLES ON LOWER SURFACE OF THE RT MLG AFT SUPPORT BEAM. MAINTENANCE REMOVED CORROSION ON LOWER SURF - [SDR AWXA200600093](https://openairdocs.org/sdr/AWXA200600093), Dec 6, 2005: SKIN. DEBONDED. MCN - DURING C16 CHECK DISCOVERED TWO SPOTS OF DISBOND ON THE NR 6 SPOILER, LOWER SURFACE, FROM WBL 228.53R TO WBL 330.53R. MAINTENANCE REMOVED DISBONDED SKIN A - [SDR AWXA200600086](https://openairdocs.org/sdr/AWXA200600086), Dec 6, 2005: SHEAR TIE. CORRODED. MCN - DURING C16 CHECK DISCOVERED CORROSION ON INTERCOSTAL SHEAR TIE BETWEEN STATIONS 727A AND 727B AT BL 17L IN THE AFT PIT. MAINTENANCE FOUND CORROSION TO BE - [SDR AWXA200600078](https://openairdocs.org/sdr/AWXA200600078), Dec 6, 2005: CHANNEL. CRACKED. MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, .75 INCHES, AT BS 540, WL 206 AND BL 1L. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL ASSY AT BS 540, WL 206 - [SDR AWXA200600077](https://openairdocs.org/sdr/AWXA200600077), Dec 6, 2005: CHANNEL. CRACKED. MCN - DURING C16 CHECK DISCOVERED CHANNEL CRACKED, .7 INCHES, AT BS 540, WL 206 AND BL 1R. MAINTENANCE REMOVED AND INSTALLED NEW CHANNEL ASSY AT BS 540, WL 206 - [SDR AWXA200600099](https://openairdocs.org/sdr/AWXA200600099), Dec 5, 2005: SKIN. CRACKED. MCN - DURING C16 CHECK DISCOVERED 1 CRACK, .375 INCHES, ON THE BOTTOM OF THE NR 3 SLAT SKIN, AT SS 92L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM - [SDR AWXA200600098](https://openairdocs.org/sdr/AWXA200600098), Dec 5, 2005: SKIN. CRACKED. MCN - DURING C16 CHECK DISCOVERED 2 CRACKS ON THE BOTTOM OF THE NR 3 SLAT SKIN, FROM SS 67L TO SS 69L. MAINTENANCE CUT OUT DAMAGED SKIN IAW BOEING 737-300 SRM 5 - [SDR AWXA200600090](https://openairdocs.org/sdr/AWXA200600090), Dec 5, 2005: SKIN. DELAMINATED. MCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WS 230.68L TO WS 234.68L. MAINTENANCE REMOVED DISBONDED SKI - [SDR AWXA200600088](https://openairdocs.org/sdr/AWXA200600088), Dec 4, 2005: INTERCOSTAL. CRACKED. MCN - DURING C16 CHECK DISCOVERED INTERCOSTAL CRACKED, 1.5 INCHES, AT BS 347 ABOVE THE E-2 SHELF, BL 11.1 AND WL 207. MAINTENANCE REMOVED AND INSTALLED FABRICAT - [SDR AWXA200600091](https://openairdocs.org/sdr/AWXA200600091), Dec 3, 2005: SKIN. DELAMINATED. MCN - DURING C16 CHECK DISCOVERED RT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD TRAILING EDGE FROM WBL 289R TO WBL 309R. MAINTENANCE REMOVED DISBONDED SKIN AN - [SDR AWXA200501130](https://openairdocs.org/sdr/AWXA200501130), Sep 28, 2005: WIRE HARNESS. INOPERATIVE. PHX - EEL - DURING 8 DAY CHECK, DISCOVERED ROW 16, EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY WIRE HARNESS AT ROW 16. OPER - [SDR AWXA200500990](https://openairdocs.org/sdr/AWXA200500990), Aug 22, 2005: WIRE. INOPERATIVE. PHX - EEL - DURING 8 DAY CHECK, DISCOVERED EMERGENCY ESCAPE PATH LIGHTING FOR SEAT 11 TO 15 ON THE LT SIDE INOPERATIVE. MAINTENANCE REPAIRED A WIRE AT SEAT 15 I - [SDR AWXA200500913](https://openairdocs.org/sdr/AWXA200500913), Aug 7, 2005: WIRE HARNESS. DAMAGED. DEN - EEL - DURING 4 DAY CHECK DISCOVERED ROW 22L, SEAT MOUNTED, EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHTING - [SDR AWXA200500850](https://openairdocs.org/sdr/AWXA200500850), Jul 25, 2005: WIRE. FAILED. PHX - SMOKE - FLT 0075 - PILOT REPORTED ON GROUND THAT THE A1 CB POPPING AND WONT RESET. MAINTENANCE REMOVED AND REPLACED THE PITOT STATIC WINDOW HEAT MODULE ON - [SDR AWXA200500768](https://openairdocs.org/sdr/AWXA200500768), Jun 29, 2005: GIRT BAR. LOOSE. DURING GROUND HANDLING CREW REPORTED DOOR L1 SLIDE/GIRT BAR LOOSE. MAINTENANCE REPACKED L1 DOOR SLIDE GIRT BAR AND SLIDE IAW AMERICA WEST AIRLINES TASKCARD R1C2 - [SDR AWXA200500737](https://openairdocs.org/sdr/AWXA200500737), Jun 22, 2005: WIRE. BROKEN. FOUND EMERGENCY EXIT LIGHTS AT ROWS 11 THROUGH ROW 15 ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. SEATS OPERATIONAL CHECKS GOOD. - [SDR AWXA200500562](https://openairdocs.org/sdr/AWXA200500562), May 13, 2005: CSD. FAILED. EN ROUTE NR 1 CONSTANT SPEED DRIVE (CSD) LOW OIL PRESSURE LIGHT ILLUMINATED & NR 1 GENERATOR DROPPED OFF LINE, APU ALREADY ON MEL, DIVERTED INTO RNO FOR REPAIR. - [SDR AWXA200500537](https://openairdocs.org/sdr/AWXA200500537), May 4, 2005: INDICATOR. FAULTY. ON APPROACH, T/E FLAPS WOULD NOT EXTEND PAST 8 DEGREES, L/E FLAP INTRANSIT LIGHT REMAINED ILLUMINATED. MX R & R THE T/E FLAP POSITION INDICATOR IAW 27-58-41. DU - [SDR AWXA200500304](https://openairdocs.org/sdr/AWXA200500304), Mar 3, 2005: MODULE. FAULTY. AFTER DEPARTURE AT APPROXIMATELY 1,000 FT A-SYSTEM HYDRAULICS AND FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, FLIGHT CONTROLS FELT STIFF BUT FUNCTI - [SDR AWXA200500101](https://openairdocs.org/sdr/AWXA200500101), Jan 31, 2005: WIRE HARNESS. BROKEN. PHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRE HARNESS TO EMERGENC - [SDR AWXA200401317](https://openairdocs.org/sdr/AWXA200401317), Nov 12, 2004: ATTACH ANGLE. CORRODED. MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN UPPER ATTACH ANGLE OF FLOOR INTERCOSTAL BETWEEN BS 380 AND BS 400, BL 0. MAINTENANCE REMOVED - [SDR AWXA200401352](https://openairdocs.org/sdr/AWXA200401352), Nov 11, 2004: DOUBLER. CRACKED. MCN - MAJOR REPAIR - DURING C-15 CHECK A 3/8 INCH CRACK WAS FOUND IN TCAS EXTERNAL DOUBLER SKIN LOCATED BETWEEN BS 380 AND BS 390, STR 1 RT AND STR 2 RT. MAINTE - [SDR AWXA200401348](https://openairdocs.org/sdr/AWXA200401348), Nov 4, 2004: PANEL. CRACKED. MCN - FLIGHT CONTROL - DURING C-15 CHECK A .50 CRACK WAS FOUND ON NR 4 SPOILER CENTER OUTBOARD HINGE. MAINTENANCE REMOVED AND REPLACED NR 4 SPOILER PANEL ASSEMB - [SDR AWXA200401284](https://openairdocs.org/sdr/AWXA200401284), Nov 4, 2004: SLIDE. FRAYED. MCN - EES - DURING C-15 CHECK THE R-2 DOOR EMERGENCY ESCAPE SLIDE WEBBING WAS FOUND FRAYED. MAINTENANCE REPLACED THE R-2 DOOR EMERGENCY ESCAPE SLIDE WEBBING IAW - [SDR AWXA200401351](https://openairdocs.org/sdr/AWXA200401351), Nov 3, 2004: SHEAR TIE. CORRODED. MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AND BEAR STRAP IN AFT BILGE AREA BS 967, BL "0". MAINTENANCE REMOVED SHEAR T - [SDR AWXA200401347](https://openairdocs.org/sdr/AWXA200401347), Nov 3, 2004: ANGLE. CORRODED. DURING C-15 CHECK, CORROSION WAS FOUND ON ATTACH ANGLE AT BOTTOM OF L-2 CREASE BEAM INNER CHORD BETWEEN BS 969 AND BS 979, LBL 49. MAINTENANCE BLENDED OUT CORRO - [SDR AWXA200401244](https://openairdocs.org/sdr/AWXA200401244), Nov 3, 2004: SKIN. DEBONDED. DURING C-15 CHECK, AN AREA OF DISBOND WAS FOUND ON LT WING NR 3 SLAT INBOARD TRAILING EDGE TIP BETWEEN SLAT STA 12.25 AND 15.25 LT. MAINTENANCE REMOVED DISBONED - [SDR AWXA200401303](https://openairdocs.org/sdr/AWXA200401303), Nov 2, 2004: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .125 INCH CRACKS WERE FOUND IN NR 6 SLAT LOWER SKIN AT AFT ROW RIVET HOLES INBOARD OF ACTUATOR ATTACH FITTINGS SLA - [SDR AWXA200401245](https://openairdocs.org/sdr/AWXA200401245), Nov 2, 2004: TAB. DEBONDED. DURING C-15 CHECK AN AREA OF DISBOND WAS FOUND ON RT AILERON TAB AT OUTBOARD AFT CORNER BETWEEN WBL 479.75 AND WBL 480 RT. MAINTENANCE PERFORMED BOND REPAIR IAW - [SDR AWXA200401290](https://openairdocs.org/sdr/AWXA200401290), Nov 1, 2004: DOOR FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 4TH DOOR STOP FROM BOTTOM BS 312, STR 12 RT. MAINTENANCE TRIMMED O - [SDR AWXA200401289](https://openairdocs.org/sdr/AWXA200401289), Nov 1, 2004: DOOR FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 3RD DOOR STOP FROM BOTTOM BS 312, STR 13 RT. MAINTENANCE STOP DRIL All 153: https://openairdocs.org/deregistered/N323AW-2006-06-23/reports.md ## Other aircraft with N323AW - [Cancelled 2019-09-06](https://openairdocs.org/deregistered/N323AW-2019-09-06): Allied Drones AT28, S/N AT28-030-2.2. 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.