# N300AU: 1985 Boeing 737-301, registration cancelled 2008-09-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 5, 2008
- Status when cancelled: Valid registration
- 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: 23228
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 19, 1985
- Certificate issued: March 13, 2007
- Last registry action: March 13, 2007
- Mode S code: A31F65
- 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/N300AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=300AU
- Page: https://openairdocs.org/deregistered/N300AU-2008-09-05

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 737-301: https://openairdocs.org/model/boeing-737-301.md

## Service difficulty reports (82, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR USAA051413](https://openairdocs.org/sdr/USAA051413), Nov 22, 2005: SKIN. DEBONDED. NR 2 SLAT T/E WEDGE SS 246.4 - 241.9 DEBONDED. INSTALLED DOUBLER IAW EA 97124. DEFECT SIZE: 5 INCH X 4 INCH.
- [SDR USAA051199](https://openairdocs.org/sdr/USAA051199), Oct 12, 2005: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD CRACKED. REPAIRED AS REQUIRED, DOUBLER INSTALLED EA 96994, DEFECT SIZE 1 INCH.
- [SDR USAA200509002](https://openairdocs.org/sdr/USAA200509002), Sep 15, 2005: SKIN. CRACKED. 2 INCH CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT STA 727E - 747 STRINGER 23L. REMOVED REPAIR DOUBLER, FABRICATED NEW DOUBLER AND FILLERS AND INSTALLED REP
- [SDR SB05108](https://openairdocs.org/sdr/SB05108), Sep 3, 2005: PUMP. LEAKING. PHL - FLT803 - ON CLIMB-OUT FROM PHL, CREW REPORTED THE NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON GEAR RETRACTION. SYSTEM "A" HYDRAULIC QUANT
- [SDR USAA041111](https://openairdocs.org/sdr/USAA041111), Dec 28, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1.5 INCH, S-23R AT STATION 727D. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR USAA041110](https://openairdocs.org/sdr/USAA041110), Dec 28, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 3 INCHES, S-19R AT STATION 767. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR USA2004F00036](https://openairdocs.org/sdr/USA2004F00036), May 13, 2004: CHARGER. FAILED. MAINTENANCE REPORTED THE AFT SIX ROWS OF THE AISLE SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER ASSY
- [SDR USA2004F00037](https://openairdocs.org/sdr/USA2004F00037), May 8, 2004: BATTERY PACK. DISCHARGED. MAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD BATTERY PACKS. OPERATIONAL CHECK GOOD.
- [SDR USAA040191](https://openairdocs.org/sdr/USAA040191), May 7, 2004: SKIN. CRACKED. PIT - FOUND SKIN CRACKED 4 INCHES, FORWARD SERVICE DOOR LOWER AFT CORNER STATION 328, APPROX STRINGER 16R. INSTALLED DOUBLER, TRIPLER AND FILLERS PER EA 78356. 
- [SDR USAA040055](https://openairdocs.org/sdr/USAA040055), Mar 8, 2004: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED 1.25 INCH, AT STRINGER 23L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVAL PER SRM 53-00-01 DETAIL XI FIG 229. 
- [SDR USAA040054](https://openairdocs.org/sdr/USAA040054), Mar 8, 2004: STRINGER. CRACKED. FOUND STRINGER CRACKED TWO PLACES 1.5 INCH AND 1.25 INCH, STRINGER 24L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVED PER SRM 53-00-01 FIG 
- [SDR USAASB03170](https://openairdocs.org/sdr/USAASB03170), Sep 18, 2003: BATTERY PACK. MALFUNCTIONED. MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EMERGENCY LIGHT EXTINGUISHES AFTER APPROXIMATELY FIVE SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE B
- [SDR USAA030171](https://openairdocs.org/sdr/USAA030171), Aug 21, 2003: SKIN. CRACKED. FOUND SKIN CRACKED 1 INCH, AFT OF FS 727D BELOW S23R. INSTALLED DOUBLER PER EA 94615. (M)
- [SDR USAA030012](https://openairdocs.org/sdr/USAA030012), Jan 16, 2003: SKIN. CORRODED. PIT - FOUND SKIN CORRODED 2 INCHES BY 4 INCHES, BELOW CABIN FLOOR STATION 1016 AT BL 0 AFT PRESSURE BULKHEAD, CORROSION LEVEL 2, TASK NR C53-107-02. REMOVED COR
- [SDR USAASB02210](https://openairdocs.org/sdr/USAASB02210), Nov 24, 2002: DOOR. OUT OF RIG. IND - FLT 338 - ON CLIMB-OUT FROM IND, EN ROUTE TO CLT, THE FORWARD MAIN ENTRY DOOR WARNING LIGHT ILLUMINATED. CREW REPORTED THE HANDLE COMES UP IN FLIGHT WHEN 
- [SDR USAA020417](https://openairdocs.org/sdr/USAA020417), Nov 7, 2002: ELEVATOR. DELAMINATED. PIT - FOUND LEFT ELEVATOR SPLINTERING AND DELAMINATED, STATION 95, 81, 100 INBOARD SIDE. ACCOMPLISHED SKIN AND CORE REPAIRS PER SRM 55-20-01, 51-70-17 AND EA 75
- [SDR USAA020418](https://openairdocs.org/sdr/USAA020418), Nov 4, 2002: STRINGER. CRACKED. PIT - FOUND SHELF CRACKED 1 INCH LONG, AFT END OF RIGHT 18A SHELF, FED OF STATION 727. REMOVED AND REPLACED SHELF PER SRM 51-10-02. (M)
- [SDR USAA020419](https://openairdocs.org/sdr/USAA020419), Nov 4, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH DIAMETER, S27L AND STATION 336 IN FRAME OF EYE OPENING. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020421](https://openairdocs.org/sdr/USAA020421), Nov 4, 2002: INTERCOSTAL. CRACKED. PIT - FOUND INTERCOSTAL CRACKED .75 INCH LONG, STATION 357 AND STRINGER 16L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020422](https://openairdocs.org/sdr/USAA020422), Nov 4, 2002: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED .375 INCH LONG, STRINGER 17R BETWEEN STATION 616-639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020423](https://openairdocs.org/sdr/USAA020423), Nov 4, 2002: SHEAR TIE. CRACKED. PIT - FOUND SHEAR TIE CRACKED .5 INCH LONG, SHEAR TIE S2L AT STATION 639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020424](https://openairdocs.org/sdr/USAA020424), Nov 4, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .375 INCH, STATION 663 AND STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND STRINGER SPLICES PER EA 74814. (M)
- [SDR USAA020425](https://openairdocs.org/sdr/USAA020425), Nov 4, 2002: CLIP. CRACKED. PIT - FOUND CLIP CRACKED .5 INCH LONG, STATION 663 STRINGER 10L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020426](https://openairdocs.org/sdr/USAA020426), Nov 4, 2002: BRACKET. CRACKED. PIT - FOUND BRACKET CRACKED .5 INCH LONG, STATION 663 STRINGER 8L AND 9L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
- [SDR USAA020427](https://openairdocs.org/sdr/USAA020427), Nov 4, 2002: STRINGER. CRACKED. PIT - FOUND STRINGER CRACKED .5 INCH LONG, FS 663 STRINGER 4L. REMOVED TIE CLIP, HFEC INSPECTION OF STRINGER AND CLIP PER SRM 51-40-02 AND NDT 0-4-53-10. (M)
- [SDR USAA020428](https://openairdocs.org/sdr/USAA020428), Nov 4, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH LONG, FS 480 STRINGER 8L AND 9L. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)
- [SDR USAA020429](https://openairdocs.org/sdr/USAA020429), Nov 4, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .125 INCH, STATION 480 STRINGER 8R AND 9R. REMOVED DAMAGED AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)
- [SDR USAA020432](https://openairdocs.org/sdr/USAA020432), Nov 4, 2002: STRINGER. CRACKED. PIT - FOUND SHELF WITH 1 INCH LONG CRACK, AFT END OF LEFT 18A SHELF, FORWARD OF STATION 727. REMOVED AND REPLACED 18A SHELF PER SRM 51-10-02. (M)
- [SDR USAA020415](https://openairdocs.org/sdr/USAA020415), Nov 4, 2002: SKIN. CRACKED. PIT - FOUND LEADING EDGE REMOVABLE SKIN WITH CRACKS, 1 INCH BY 1 INCH AREA BEYOND 25 PERCENT MAXIMUM LIMITS, 14 EACH BLENDED AREAS, LEFT HORIZ STABILIZER LEADIN
- [SDR USAA020420](https://openairdocs.org/sdr/USAA020420), Nov 4, 2002: INTERCOSTAL. CRACKED. PIT - FOUND INTERCOSTAL CRACKED .5 INCH BY 7 INCH AREA, STATION 303 AND 310 AT STRINGER 4L. FABRICATED WEB, STRAP AND T-FITTING PER SRM 53-02-04. (M)
- [SDR USAA020416](https://openairdocs.org/sdr/USAA020416), Oct 2, 2002: SUPPORT. CORRODED. PIT - FOUND SUPPORT CORRODED SEVERAL AREAS, BS 960 Z-ANGLE SUPPORT, AFT ENTRY THRESHOLD DOOR JAM. CORROSION, LEVEL 2, TASK NR C53-107-01. REPLACED Z-ANGLE PER B
- [SDR USAA020369](https://openairdocs.org/sdr/USAA020369), Sep 27, 2002: STRUCTURE. CHAFED. PIT - FOUND TRAILING EDGE HAS CHAFE, 59 INCHES INBOARD FROM INBOARD END. BURNISHED/BLENDED AND INSTALLED WEAR PAD PER TYPICAL REPAIR 57-50-17. (M)
- [SDR USAA020371](https://openairdocs.org/sdr/USAA020371), Sep 25, 2002: MOUNT. WORN. PIT - FOUND ENGINE MOUNT CROSSBEAM WORN LUG, LUG BORE ON ENGINE MOUNT. MACHINE INSIDE DIAMETER OF LUG BORE TO OVERSIZE BEARING PER TYPICAL REPAIR 550-19 REV B. 
- [SDR USAA020414](https://openairdocs.org/sdr/USAA020414), Sep 20, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH LONG, STATION 616 RIGHT SIDE FRAME LOWER INBOARD END. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74856. (M)
- [SDR USAA020365](https://openairdocs.org/sdr/USAA020365), Sep 20, 2002: FRAME. CRACKED. PIT - FOUND FRAME CRACKED 1 INCH, STATION 616 RIGHT SIDE, FRAME LOWER INBOARD END CABIN FLOOR. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74256.
- [SDR USAA020364](https://openairdocs.org/sdr/USAA020364), Sep 19, 2002: SKIN. DELAMINATED. PIT - FOUND RUDDER DELAMINATED, LEFT SIDE, BOTTOM EDGE 19 INCHES AFT OF LEADING EDGE. RESIN AND OVERLAYED WITH TWO PLIES OF GRAPHITE FABRIC PER EA 74841, SRM 55
- [SDR USAA020367](https://openairdocs.org/sdr/USAA020367), Sep 17, 2002: SKIN. CRACKED. RIGHT AILERON, CRACKED 2 LOCATIONS. LOWER SKIN FLANGE AT NR 3 HINGE AND NR 2 HINGE. REMOVED ALL DAMAGE PLUS COMPLETED WET LAYUP REPAIR IAW SRM AND EA.
- [SDR USAA020282](https://openairdocs.org/sdr/USAA020282), Jul 23, 2002: MOUNT. WORN. PIT - FOUND ENGINE MOUNT STRUT WORN BEYOND LIMITS, ENGINE MOUNT MAIN SLEEVE REPAIR. REAMED, CHAMFERED, BLENDED AND ROTOPEENED THE FITTING BORE PER TYPICAL 54-50
- [SDR USA2002F00053](https://openairdocs.org/sdr/USA2002F00053), Jun 2, 2002: SENSOR. FAILED. AFTER TAKEOFF, CREW WAS UNABLE TO MOVE THE LANDING GEAR SELECTOR HANDLE PAST THE OFF POSITION TO RETRACT THE GEAR. CREW ALSO TRIED THE GEAR OVER RIDE WITH NO HE
- [SDR USAA020184](https://openairdocs.org/sdr/USAA020184), Apr 30, 2002: RIB. CORRODED. PIT - FOUND RUDDER CORRODED 3 INCHES BY 12 INCH AREA, COVER FACE OF RIB BEHIND BALANCE WEIGHTS ON BEAM. REPLACED RIB PER SRM 51-10-02, 51-20-01, 51-20-00 AND 51
- [SDR USAASB01349](https://openairdocs.org/sdr/USAASB01349), Dec 23, 2001: WIRE. DISCONNECTED. BWI - PILOT REPORTED THE WIRING FOR THE EMERGENCY EXIT LIGHTS UNDER SEAT 21C IS DISCONNECTED AND THE LIGHTS ARE INOPERATIVE. MAINTENANCE RECONNECTED AND SECURED
- [SDR USAA011393](https://openairdocs.org/sdr/USAA011393), Dec 17, 2001: STRUCTURE. DAMAGED. PIT - FOUND RUDDER DAMAGED, NR 7 HINGE AREA RSTA 225-235 LEADING EDGE. PER SRM 51-70-17 2 EXTRA PLIES WITH HALF OVERLAP PER EA 73066. (M)
- [SDR USAA011394](https://openairdocs.org/sdr/USAA011394), Dec 17, 2001: STRUCTURE. DAMAGED. PIT - FOUND RUDDER 8 INCH BY .750 INCH GOUGED, CLOSE TO T/E WEDGE BETWEEN R STA 121164 AND 174.12. REPAIRED PER SRM 51-70-17 WITH 2 EXTRA PILES WITH .5 OVERLAP 
- [SDR USAA011395](https://openairdocs.org/sdr/USAA011395), Dec 17, 2001: SKIN. DAMAGED. PIT - FOUND RUDDER SCREW PULLED THROUGH SKIN, LEFT SKIN PANEL AT R STATION 225 APPROXIMATELY. TWO EXTRA REPAIR PLIES WITH .5 INCH PER PLY OVERLAP PER EA 73064. 
- [SDR USAASB01083](https://openairdocs.org/sdr/USAASB01083), Mar 20, 2001: DOOR. NOT CLOSED. BWI - FLT 1568 - ON CLIMB-OUT FROM DCA, AT APPROXIMATELY 4,500 FEET, THE FLIGHT ATTENDANT ADVISED CREW OF A LOUD AIR NOISE COMING FROM THE FORWARD ENTRY DOOR. S
- [SDR USAASB01009](https://openairdocs.org/sdr/USAASB01009), Jan 18, 2001: WIRE HARNESS. OUT OF POSITION. LGA - MAINTENANCE FOUND THE EMERGENCY EXIT PATH LIGHTING AT SEAT 16C INOPERATIVE. MAINTENANCE REPOSITIONED WIRING HARNESS FOR SEAT ROW 16ABC EMERGENCY EXIT PATH
- [SDR USAASB00223](https://openairdocs.org/sdr/USAASB00223), Aug 19, 2000: CHARGER. FAILED. CLT - PILOT REPOTED THAT THE EMERGENCY EXIT PATH LIGHTS FROM SEAT ROWS 5 TO 11 ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSY AND THE BATTER
- [SDR USAASB00089](https://openairdocs.org/sdr/USAASB00089), Mar 28, 2000: POWER SUPPLY. FAILED. TPA - DURING ANNUAL OPERATIONAL CHECK OF THE AFT LEFT SERVICE DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO IL
- [SDR USAA991435](https://openairdocs.org/sdr/USAA991435), Dec 9, 1999: SKIN. CRACKED. PIT - DURING RON VISIT, FOUND 1.0625 INCH LONG CRACK ON FUSELAGE SKIN AT RT SIDE, STATION 767 STRINGER 22 TO 23 RT. REMOVED CRACK WITH CUTOUT. INSTALLING EXTERN
- [SDR USAASB99290](https://openairdocs.org/sdr/USAASB99290), Dec 8, 1999: CABIN PRESSURE. FAILED. PIT - FLT 2380 - DURING CLIMB-OUT FROM PIT, THE AUTO PRESSURIZATION SYSTEM FAILED TO STANDBY. CREW WAS UNABLE TO CONTROL CABIN IN STANDBY OR MANUAL MODE. CABIN 

All 82: https://openairdocs.org/deregistered/N300AU-2008-09-05/reports.md

## Other aircraft with N300AU

- [Registered now](https://openairdocs.org/aircraft/N300AU): Schweizer HUGHES 269C, S/N S1168

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