# N563AU: 1987 Boeing 737-301, registration cancelled 2007-08-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 16, 2007
- Exported to: Bermuda
- 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: 23551
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 6, 1987
- Certificate issued: April 24, 2006
- Last registry action: April 24, 2006
- Mode S code: A73222
- 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/N563AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=563AU
- Page: https://openairdocs.org/deregistered/N563AU-2007-08-16

From the FAA registry file of October 31, 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 (53, newest 50)

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

- [SDR COOSDR060032](https://openairdocs.org/sdr/COOSDR060032), Aug 24, 2006: RIB. CRACKED. RT WING AT WBL 114 RIB UPPER CHORD CRACKED NEAR STR-2. (K)
- [SDR SB05062](https://openairdocs.org/sdr/SB05062), May 19, 2005: CHARGER. INOPERATIVE. CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS FOR SEAT ROWS 11 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY. OPERATIONAL CHEC
- [SDR SB05017](https://openairdocs.org/sdr/SB05017), Jan 27, 2005: WIRE. FAULTY. PVD - MAINTENANCE REPORTED THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. MAINTENANCE REPAIRED WIRING AT THE EMERGENCY LIGHT CIRCUIT BREAKER ON THE P-18 PANEL. OPERATI
- [SDR SB04158](https://openairdocs.org/sdr/SB04158), Nov 25, 2004: INDICATOR. FAULTY. DURING APPROACH TO PHL FROM ORD, CREW EXPERIENCED A FLAP DISAGREEMENT WHEN FLAP HANDLE WAS PLACED BEYOND 15 UNITS. A FLAP SPLIT WAS CLEARLY INDICATED. NO ROLL F
- [SDR USAASB04114](https://openairdocs.org/sdr/USAASB04114), Aug 30, 2004: POWER SUPPLY. INOPERATIVE. BOS - PILOT REPORTED THE COCKPIT EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPAIRED EMERGENCY LIGHT IN COCKPIT AND REMOVED AND REPLACED POWER SUPPLY. OPE
- [SDR USA2004F00071](https://openairdocs.org/sdr/USA2004F00071), Jun 8, 2004: WIRE. BROKEN. MAINTNANCE REPORTED THE EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED A BROKEN WIRE. OPERATIONAL CHECK GOOD.
- [SDR USA2004F00080](https://openairdocs.org/sdr/USA2004F00080), Jun 5, 2004: SHUTTLE VALVE. FAULTY. ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON
- [SDR USA2004F00078](https://openairdocs.org/sdr/USA2004F00078), Jun 5, 2004: CONTROL SYSTEM. MALFUNCTIONED. ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON
- [SDR USAA040116](https://openairdocs.org/sdr/USAA040116), Apr 7, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .700 INCH, 3 INCHES AFT OF FS 727D ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAASB03179](https://openairdocs.org/sdr/USAASB03179), Oct 12, 2003: CONTROL COLUMN. STIFF. EN ROUTE FROM CLT TO RDU, CREW REPORTED STIFF FLIGHT CONTROLS, ELEVATOR AND AILERONS. FEELS SOMEWHAT LIKE MANUAL REVERSION. DURING FLARE ON FINAL, THE CONTROL C
- [SDR USAASB03149](https://openairdocs.org/sdr/USAASB03149), Aug 24, 2003: CHARGER. INOPERATIVE. MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 10ABC AND THE LEFT EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND T
- [SDR USAASB03143](https://openairdocs.org/sdr/USAASB03143), Aug 22, 2003: BATTERY PACK. INOPERATIVE. MAINTENANCE REPORTED THE LEFT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03137](https://openairdocs.org/sdr/USAASB03137), Aug 13, 2003: BATTERY PACK. INOPERATIVE. ATL - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY EXIT LIGHTING, AT THE LEFT OVERWING EXIT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT T
- [SDR USAASB03121](https://openairdocs.org/sdr/USAASB03121), Jul 26, 2003: CHARGER. INOPERATIVE. PILOT REPORTED THE RIGHT OVERHEAD EMERGENCY EXIT SIGN, THE LEFT OVERWING EXIT SIGN, THE LEFT SIDEWALL EXIT SIGN AT ROW 10 AISLE EXIT AND THE EMERGENCY LIGHTS AT
- [SDR USAASB02168](https://openairdocs.org/sdr/USAASB02168), Sep 7, 2002: BATTERY PACK. DISCHARGED. GSO - MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT THE LEFT ESCAPE HATCH FLOOR LEVEL, SEAT ROW 10 LEFT SIDE AND THE BULLNOSE LIGHT AT SEAT ROW 15 RIGH
- [SDR USAASB02085](https://openairdocs.org/sdr/USAASB02085), Apr 27, 2002: RELIEF VALVE. FAILED. CLT - FLT 384 - ON CLIMB-OUT FROM TPA, CREW REPORTED AN AUTO FAIL LIGHT AND THE CABIN ALTITUDE CLIMBING AT 4000 FPM. STANDBY MODE HAD NO EFFECT. FLIGHT DESCENDE
- [SDR USAA020113](https://openairdocs.org/sdr/USAA020113), Mar 21, 2002: SKIN. CRACKED. TPA - FOUND SKIN CRACKED 2 FT BY 3 FT DOUBLER INSTALLED, CROWN SKIN DIRECTLY BELOW DORSAL FIN SEAL STATION 1000. INSTALLED NEW DOUBLER PER WORK INSTRUCTIONS OF 
- [SDR USAA020112](https://openairdocs.org/sdr/USAA020112), Mar 21, 2002: SKIN. WORN. TPA - FOUND SKIN WITH WORN AREA, FUSELAGE CROWN STATION 1000, DORSAL FIN CONTACT. INSTALLED DOUBLER AND TRIPLER PER EA 86014A. (M)
- [SDR USAASB01129](https://openairdocs.org/sdr/USAASB01129), May 7, 2001: PROXIMITY SENSOR. FAILED. CLT - FLT 1670 - AFTER TAKEOFF FROM SAV, EN ROUTE TO CLT, CREW ATTEMPTED TO RAISE THE LANDING GEAR HANDLE BUT THE HANDLE WOULD NOT MOVE MORE THAN HALFWAY UP. AF
- [SDR USAASB00251](https://openairdocs.org/sdr/USAASB00251), Sep 11, 2000: ACM. OVERSERVICED. PIT - FLT 9228 - AFTER TAKEOFF, CLIMBING THROUGH 2,000 FEET, CREW NOTICED AN INCREASING OILY SMELL IN THE FLIGHT COMPARTMENT. ODOR SEEMED TO BE MORE OILY THAN E
- [SDR USAASB00242](https://openairdocs.org/sdr/USAASB00242), Sep 2, 2000: SWITCH. FAULTY. PHL - FLT 663 - AFTER TAKEOFF FROM PHL, AT 1,500 FEET, CREW TRIED TO RETRACT FLAPS AND SLAT DISAGREEMENT LIGHTS ON PEDESTAL AND OVERHEAD PANEL ILLUMINATED. CREW
- [SDR USAA000786](https://openairdocs.org/sdr/USAA000786), Jun 5, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .250 INCH, LEFT C/D WINDOW POST. INSTALLED DOUBLER PER EA 67382. (M)
- [SDR USAA000769](https://openairdocs.org/sdr/USAA000769), May 31, 2000: STIFFENER. CORRODED. CLT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH, NOSE W/W STIFFENER BS 235.8, RBL 10. INSTALLED REPAIR ANGLE PER SRM 51-70-12. CORROSION LEVEL 1. (M)
- [SDR USAA000770](https://openairdocs.org/sdr/USAA000770), May 31, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, LBBL 1 PLUS 8. FABRICATED ANGLES AND INSTALLED PER SRM 53-10-51. CORROSION LEVEL 2. (M)
- [SDR USAA000771](https://openairdocs.org/sdr/USAA000771), May 31, 2000: ANGLE. CRACKED. CLT - FOUND Q-3 CHECK, FOUND Z-ANGLE CRACKED 2 INCHES, LEFT AFT ENTRY DOOR THRESHOLD. REPAIRED PER SRM 51-10-2. (M)
- [SDR USAA000772](https://openairdocs.org/sdr/USAA000772), May 31, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES, 328 FLOORBEAM, RBBL 36 TO 38. REPLACED T-CAP PER SRM 53-10-51 FIG 205. CORROSION LEVEL 2. (M)
- [SDR USAA000759](https://openairdocs.org/sdr/USAA000759), May 31, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 199 AND 202 AT RBL 5. INSTALLED REPAIR ANGLE PER TR 53-10-07. (M)
- [SDR USAA000760](https://openairdocs.org/sdr/USAA000760), May 31, 2000: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 291.5 AND STATION 270 BETWEEN STRINGER 11 AND 12R. INSTALLED NEW FABRICATED PART PER SRM 51-30-2. (M)
- [SDR USAA000761](https://openairdocs.org/sdr/USAA000761), May 31, 2000: DOOR FRAME. CRACKED. CLT - FOUND DOOR FRAME CRACKED .25 INCH, STATION 294.5 INBOARD SIDE OF R-1 DOOR FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA000762](https://openairdocs.org/sdr/USAA000762), May 31, 2000: FRAME. CRACKED. CLT - FOUND FORWARD SERVICE DOOR FRAME CRACKED .75 INCH, STATION 294.5, WL 207.5. INSTALLED REPAIR ANGLE PER SRM 53-10-02. (M)
- [SDR USAA000763](https://openairdocs.org/sdr/USAA000763), May 31, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, BS 727C, STRINGER 4L. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000764](https://openairdocs.org/sdr/USAA000764), May 31, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, BS 727D, STRINGER 4L. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000765](https://openairdocs.org/sdr/USAA000765), May 31, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCH, STATION 807, RIGHT BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000766](https://openairdocs.org/sdr/USAA000766), May 31, 2000: TRACK. CRACKED. CLT - FOUND O/H BIN RAIL CRACKED .5 INCH, STATION 827, LEFT O/H BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000767](https://openairdocs.org/sdr/USAA000767), May 31, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, STATION 847, LT O/H BIN RAIL ATTACH STRINGER 8 TO 9. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000768](https://openairdocs.org/sdr/USAA000768), May 31, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .5 INCHES, STATION 908, RIGHT O/H BIN ATTACH RAIL STRINGER 8 TO 9. FABRICATED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000757](https://openairdocs.org/sdr/USAA000757), May 31, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 199 AND 202 AT LBL 5. INSTALLED REPAIR ANGLE PER TR 53-10-07. INSTALLED REPAIR ANGLE PER TR 53-10-07. 
- [SDR USAA000758](https://openairdocs.org/sdr/USAA000758), May 31, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH IN TWO PLACES, BS 178, WL 190, LBL 1 AND RBL 1. INSTALLED REPAIR ANGLE PER TR 53-10-08. (M)
- [SDR USAA000737](https://openairdocs.org/sdr/USAA000737), May 24, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 1 INCH, RBBL 0, 9 AND 12 FLOORBEAM. INSTALLED NEW T-CAP PER SRM 53-10-57. CORROSION LEVEL 2. (M)
- [SDR USAA000732](https://openairdocs.org/sdr/USAA000732), May 23, 2000: FITTING. CRACKED. CLT - FOUND FITTING CRACKED .375 INCH, LEFT MLG SUPPORT FITTING REAR SPAR WALKING BEAM. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000731](https://openairdocs.org/sdr/USAA000731), May 23, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .375 INCH, KEEL BEAM SKIN STATION 661-727, TWO PLACES. INSTALLED FABRICATED DOUBLER PER SRM 53-60-12 FIG 202. (M)
- [SDR USAA000713](https://openairdocs.org/sdr/USAA000713), May 15, 2000: SPLICE. CRACKED. CLT - FOUND SPLICE STRINGER CRACKED.125 INCH, BS 908 STRINGER 4L SPLICE PLATE. INSTALLED NEW SPLICE AND TIE CLIP PER SRM 51-10-2. (M)
- [SDR USAA000526](https://openairdocs.org/sdr/USAA000526), Mar 30, 2000: SUPPORT BRACKET. CRACKED. PIT- FOUND SUPPORT BRACKET CRACKED 2 INCHES, STATION 727D-727E STRINGER NR 1 A/C CENTER LINE NR 3 VHF. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (M)
- [SDR USAASB00058](https://openairdocs.org/sdr/USAASB00058), Mar 3, 2000: BATTERY PACK. INOPERATIVE. CLT - MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK NO
- [SDR USAASB99279](https://openairdocs.org/sdr/USAASB99279), Nov 26, 1999: CONTROLLER. FAILED. PHL - FLT 435 - EN ROUTE FROM BTV TO PHL, AT FL260, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW VERIFIED CABIN ALTITUDE READING AT 10,000 FT. CREW COMPLIED WI
- [SDR USAASB99178](https://openairdocs.org/sdr/USAASB99178), Jul 19, 1999: TR UNIT. MALFUNCTIONED. BWI - FLT 0166 - DURING CRUISE, EN ROUTE PHX/PHL, THE WEATHER RADAR BECAME UNRELIABLE. TEST PAGE SHOWED 'R/T FAULT' FOLLOWED BY 'NO WXR'. SYSTEM WORKED FINE INI
- [SDR USAASB98289](https://openairdocs.org/sdr/USAASB98289), Oct 29, 1998: LOCK ACTUATOR. FAILED. CLT - FLT 984 - AFTER TAKEOFF WITH GEAR LEVER IN THE UP POSITION, THE RED NOSE GEAR WARNING LIGHT ILLUMINATED. GEAR APPEARED TO BE UP. WHEN GEAR LEVER WAS PLACE
- [SDR USAASB98208](https://openairdocs.org/sdr/USAASB98208), Aug 13, 1998: CONTROL VALVE. FAILED. DEN - FLT 136 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT UPON CLIMB-OUT FROM DEN. FLIGHT RETURNED TO FIELD AT DEN AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENC
- [SDR USAASB98135](https://openairdocs.org/sdr/USAASB98135), Jun 2, 1998: TURBOFAN. FAILED. PIT - FLT 1597 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF FROM PIT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS D
- [SDR 98ZZZM533](https://openairdocs.org/sdr/98ZZZM533), Jun 2, 1998: CONTROL VALVE. FAILED. PIT - FLT 1597 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF FROM PIT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS D

All 53: https://openairdocs.org/deregistered/N563AU-2007-08-16/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19950122003829I](https://openairdocs.org/incident/19950122003829I), Jan 22, 1995: Boeing 737301 (N563AU), Indianapolis, IN. Narrative: aircraft departed pit and experienced #1 generator problem. The APU was transferred to the #1 bus and it dropped off the line also. The captain…

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