# N282AU: 1983 Boeing 737-2B7, registration cancelled 2002-09-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 10, 2002
- Exported to: Thailand
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-2B7](https://openairdocs.org/model/boeing-737-2b7) (registry code 138447C)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 23115
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 1983
- Certificate issued: May 2, 2002
- Last registry action: May 2, 2002
- Mode S code: A2D57C
- Owner when cancelled: [Alameda Corp Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORP%20TRUSTEE)
- Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio)
- Owner type: Corporation
- Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N282AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=282AU
- Page: https://openairdocs.org/deregistered/N282AU-2002-09-10

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 737-2B7: https://openairdocs.org/model/boeing-737-2b7.md

## Service difficulty reports (56, newest 50)

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

- [SDR USAASB01322](https://openairdocs.org/sdr/USAASB01322), Nov 22, 2001: BATTERY. DISCHARGED. TPA - THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)
- [SDR USAASB01312](https://openairdocs.org/sdr/USAASB01312), Nov 15, 2001: BATTERY. DISCHARGED. LGA - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONA
- [SDR USAA010780](https://openairdocs.org/sdr/USAA010780), Jul 2, 2001: SPLICE. CORRODED. CLT - FOUND STRINGER SPLICE CORRODED 1 INCH BY 4 INCHES, BS 986.5, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3 FIG 1. (M)
- [SDR USAA010797](https://openairdocs.org/sdr/USAA010797), Jun 12, 2001: SUPPORT FITTING. CORRODED. PIT - FOUND SUPPORT FITTING CORRODED .020 INCH - .010 INCH, NOSE GEAR RIGHT TRUNNION SUPPORT FITTING BORE. REAMED BORE, INSTALLED SLEEVE PER EA 71444. (M)
- [SDR USAASB00296](https://openairdocs.org/sdr/USAASB00296), Oct 18, 2000: DUCT. CRACKED. TPA-LGA - FLT 2676 - AFTER TAKEOFF, THE RIGHT ENGINE START VALVE LIGHT AND THE RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAF
- [SDR USAASB00284](https://openairdocs.org/sdr/USAASB00284), Oct 3, 2000: ACTUATOR. LEAKING. EWR - FLT 2636 - EN ROUTE FROM PBI TO LGA, CAPTAIN NOTICED THAT SYSTEM A HYDRAULIC QUANTITY HAD DECREASED FROM 2.2 GALLONS TO 1.2 GALLONS. ON DESCENT TO LGA, AS
- [SDR USAA001316](https://openairdocs.org/sdr/USAA001316), Aug 24, 2000: STRINGER. CRACKED. CLT - FOUND SHELF CRACKED .5 INCH, STRINGER 18A RIGHT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-02. (M)
- [SDR USAA001318](https://openairdocs.org/sdr/USAA001318), Aug 24, 2000: PRESSURE PANEL. CRACKED. CLT - FOUND PRESSURE DECK WEB CRACKED .5 INCH, STATION 670, RBL 12. INSTALLED FILLER AND DOUBLER PER EA 67747. (M)
- [SDR USAA001317](https://openairdocs.org/sdr/USAA001317), Aug 24, 2000: STRINGER. CRACKED. CLT - FOUND SHELF CRACKED .5 INCH, STRINGER 18A LEFT, BS 727 SHELF. REPLACED WITH NEW SHELF PER SRM 51-10-1. (M)
- [SDR USAA001299](https://openairdocs.org/sdr/USAA001299), Aug 22, 2000: CLEVIS. CORRODED. CLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, AFT SPAR, AFT OUTBOARD CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)
- [SDR USAA001298](https://openairdocs.org/sdr/USAA001298), Aug 22, 2000: CLEVIS. CORRODED. CLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, FWD SPAR, FRONT CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)
- [SDR USAA001297](https://openairdocs.org/sdr/USAA001297), Aug 22, 2000: CLEVIS. CORRODED. CLT - FOUND CLEVIS CORRODED .008 INCH BY .008 INCH, VERT FIN, FWD SPAR, AFT CLEVIS RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)
- [SDR USAA001296](https://openairdocs.org/sdr/USAA001296), Aug 22, 2000: CLEVIS. CORRODED. CLT - FOUND AFT SPAR CLEVIS CORRODED .013 INCH BY .028 INCH, VERT FIN, AFT SAPR, AFT OUTBOARD CLEVIS, RT SIDE. REMOVED AND REPAIRED PER EA 67785. (M)
- [SDR USAA001281](https://openairdocs.org/sdr/USAA001281), Aug 17, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .250 INCH, AFT SERVICE DOOR LOWER HINGE. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-03 AND EA 67849. (M)
- [SDR USAA001254](https://openairdocs.org/sdr/USAA001254), Aug 15, 2000: GUSSET. CRACKED. CLT - FOUND GUSSETT CRACKED .5 INCH, NLG ACTUATOR ATTACH BEAM GUSSETT, STATION 259.5, BL 0. INSTALLED NEW PART PER SRM 51-30-00. (M)
- [SDR USAA001236](https://openairdocs.org/sdr/USAA001236), Aug 14, 2000: TORQUE BOX. CRACKED. CLT - FOUND TORQUE BOX CRACKED .25 INCH, STATION 1112, LEFT SIDE JUST BELOW UPPER TORQUE BOX. INSTALLED DOUBLER AND FILLER PER EA 67773 AND SRM 51-40-3. (M)
- [SDR USAA001237](https://openairdocs.org/sdr/USAA001237), Aug 14, 2000: STRAP. CRACKED. CLT - FOUND STRINGER STRAP CRACKED .75 INCHES LONG, 2 INCHES AFT OF STATION 1138, RT SIDE. INSTALLED REPAIR PER EA 67733, AND SRM 53-00-01 FIG 221. (M)
- [SDR USAA001207](https://openairdocs.org/sdr/USAA001207), Aug 7, 2000: CLIP. CRACKED. CLT - FOUND ATTACH CLIP CRACKED .5 INCH, STATION 380, STRINGER 26L ON BAFFLE ATTACH CLIP. REPLACED PER SRM 51-10-01. (M)
- [SDR USAA001206](https://openairdocs.org/sdr/USAA001206), Aug 7, 2000: SHIM. CRACKED. CLT - FOUND SHIM CRACKED .25 INCH, STATION 440 BETWEEN STRINGER 22R AND STRINGER 23R. REPLACED ATTACH CLIP SHIM PER SRM 51-10-01. (M)
- [SDR USAA001157](https://openairdocs.org/sdr/USAA001157), Aug 4, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 440, STRINGER 22R. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M)
- [SDR USAA001149](https://openairdocs.org/sdr/USAA001149), Aug 4, 2000: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM CRACKED 2 INCHES, BS 663, BL 0. INSTALLED STIFFENER FILLER AND DOUBLER PER EA 67727. (M)
- [SDR USAA001141](https://openairdocs.org/sdr/USAA001141), Aug 2, 2000: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 1 INCH, BS 907, STRINGER 21R FUSELAGE FRAME UPPER LEG. INSTALLED DOUBLER PER SRM 51-40-3. (M)
- [SDR USAA001140](https://openairdocs.org/sdr/USAA001140), Aug 2, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 3 INCHES, BS 328 AFT LOWER CORNER FS 0 CUTOUT. INSTALLED DOUBLER PER TR 53-10-19A. (M)
- [SDR USAA001139](https://openairdocs.org/sdr/USAA001139), Aug 2, 2000: STRINGER CLIP. CRACKED. CLT - FOUND STRINGER TIE CLIP CRACKED .5 INCH, STRINGER 13 STATION 1138. INSTALLED NEW TIE CLIP PER SRM 51-10-01. (M)
- [SDR USAA001112](https://openairdocs.org/sdr/USAA001112), Aug 1, 2000: FRAME. CRACKED. CLT - FOUND 1 INCH CRACK, STATION 951 FRAME WL 254 RT SIDE. FABRICATED REPAIR AND INSTALLED PER TR 53-30-07A. (M)
- [SDR USAA001111](https://openairdocs.org/sdr/USAA001111), Aug 1, 2000: FRAME. CRACKED. CLT - FOUND 1 INCH CRACK, STATION 951 FRAME, WL 254 LT SIDE. FABRICATED AND INSTALLED REPAIR PER TR 53-30-07A. (M)
- [SDR USAA001110](https://openairdocs.org/sdr/USAA001110), Aug 1, 2000: CAP. CORRODED. CLT - FOUND T-CAP CORRODED 2 INCHES, FS 312, RBL 35. CUTOUT DAMAGED FABRICATED REPAIR AND INSTALLED PER 53-10-9 FIG 5. (M)
- [SDR USAA001109](https://openairdocs.org/sdr/USAA001109), Aug 1, 2000: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, STATION 727B, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001108](https://openairdocs.org/sdr/USAA001108), Aug 1, 2000: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, STATION 685, STRINGER 4. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001107](https://openairdocs.org/sdr/USAA001107), Aug 1, 2000: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .250 INCH, STATION 685, STRINGER 3. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001106](https://openairdocs.org/sdr/USAA001106), Aug 1, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, FS 663, STRINGER 10L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001105](https://openairdocs.org/sdr/USAA001105), Aug 1, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616, STRINGER 3R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001104](https://openairdocs.org/sdr/USAA001104), Aug 1, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, FRAME 597 AT STRINGER 8L TIE CLIP. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001066](https://openairdocs.org/sdr/USAA001066), Jul 31, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, FS 727B, STRINGER 5L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001065](https://openairdocs.org/sdr/USAA001065), Jul 31, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001064](https://openairdocs.org/sdr/USAA001064), Jul 31, 2000: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, FS 727A, STRINGER 4L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001063](https://openairdocs.org/sdr/USAA001063), Jul 31, 2000: CLIP. CRACKED. CLT - FOUND CLIP CRACKED .125 INCH, STATION 685, STRINGER 2. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)
- [SDR USAA001062](https://openairdocs.org/sdr/USAA001062), Jul 31, 2000: TIE CLIP. CRACKED. CLT - TIE CLIP CRACKED .125 INCH, STRINGER 9L, AT FRAME 597. INSTALLED STRINGER TIE CLIP PER EO 5393G227. (M)
- [SDR USAA000803](https://openairdocs.org/sdr/USAA000803), Jun 7, 2000: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED .250 INCH BY .250 INCH, BS 312, RBL 11-36. INSTALLED NEW T-CAP PER SRM 53-10-9. INSTALLED NEW T-CAP PER SRM 53-10-9. (M)
- [SDR USAASB99052](https://openairdocs.org/sdr/USAASB99052), Feb 23, 1999: PCU. MALFUNCTIONED. BWI - FLT 2710 - EN ROUTE FROM MCO-BDL, AT FL330 AND .74 MACH, FLIGHT WAS APPROACH SBY ON 'A' AUTOPILOT WHEN THE A/C STARTED PITCHING UP AND ROLLING TO RIGHT 80
- [SDR USAASB98309](https://openairdocs.org/sdr/USAASB98309), Nov 22, 1998: MECHANISM. OUT OF ADJUST. BWI - FLT 2608 - FLIGHT WAS CLEARED FOR APPROACH AT BWI FOR RUNWAY 28. AS CAPTAIN SELECTED FLAPS 1, THE LEADING EDGE TRANSIT LIGHT AND THE NR 4 SLAT TRANSIT LIG
- [SDR USAA980176](https://openairdocs.org/sdr/USAA980176), May 1, 1998: STRINGER. CORROSION. ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 1.333 INCH BY 2.5 INCH CORROSION BS 967 STRINGER 25 LEFT. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. REPA
- [SDR USAASB98055](https://openairdocs.org/sdr/USAASB98055), Mar 9, 1998: LIGHT. FAILED. CLT - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE FORWARD SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (
- [SDR USAASB97332](https://openairdocs.org/sdr/USAASB97332), Dec 6, 1997: BATTERY PACK. DISCHARGED. CLT - MAINTENANCE FOUND THE AFT LEFT AND RIGHT EXTERIOR EMERGENCY ESCAPE SLIDE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (
- [SDR USAASB97073](https://openairdocs.org/sdr/USAASB97073), Mar 7, 1997: GARLOCK SEAL. LEAKING. BWI - FL 8028 - ON CLIMB-OUT OF BWI, AT FL 250, CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO LOW OIL PRESSURE LIGHT ILLUMINATING WHICH WAS VERIFIED BY OIL PRESSURE 
- [SDR USAA960918](https://openairdocs.org/sdr/USAA960918), Sep 18, 1996: BEAM. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACKED BEAM RBL 24.5 BS 674. INSTALLED STIFFENER AND NEW CHANNEL, REPAIRED PER EO 5791G632. (M)
- [SDR USAA960622](https://openairdocs.org/sdr/USAA960622), Sep 18, 1996: FLOOR BEAM. CORROSION. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA OF HEAVY SURFACE CORROSION FLOOR BEAM STATION 360, RBL 12 TO RBL 56. INSTAL
- [SDR USAA960621](https://openairdocs.org/sdr/USAA960621), Sep 18, 1996: WEB. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKED WEBS RBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2, FIG 1. (M)
- [SDR USAA960620](https://openairdocs.org/sdr/USAA960620), Sep 18, 1996: WEB. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKED WEBS LBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 FIG 1. (M)
- [SDR USAA960619](https://openairdocs.org/sdr/USAA960619), Sep 18, 1996: WEB. CRACKED. INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKED WEBS BL 0 BS 707. INSTALLED WEB REPAIR AND FILLERS. REPAIRED PER SRM 51-40-2. (M)

All 56: https://openairdocs.org/deregistered/N282AU-2002-09-10/reports.md

## FAA accident and incident reports (5)

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 20001018016499I](https://openairdocs.org/incident/20001018016499I), Oct 18, 2000: Boeing 7372B7 (N282AU), Tampa, FL. (-23) On October 18, 2000, at 1405 EDT, a B-737-2B7, operated by usaa airlines, on take-off from Tampa International Airport, FL, the number 2 engine start…
- [Incident 19990223016319I](https://openairdocs.org/incident/19990223016319I), Feb 23, 1999: Boeing 7372B7 (N282AU), Baltimore, MD. (-5) Aircraft enroute from mco to hfd experienced uncommanded roll to right at 33,000', mach .74. Followed procedures in qrm to gain control of aircraft and…
- [Incident 19990120011469I](https://openairdocs.org/incident/19990120011469I), Jan 20, 1999: Boeing 7372B7 (N282AU), Rochester, NY. On Wednesday, January 20, 1999, a boeng 737, N282AU, flight 2690, operated by us airways,departed orlando international airport for Rochester,new york. During…
- [Incident 19910831046419I](https://openairdocs.org/incident/19910831046419I), Aug 31, 1991: Boeing 7372B7 (N282AU), Baltimore, MD. Engine kept stalling at different power settings. Landed safely.
- [Incident 19910213006979I](https://openairdocs.org/incident/19910213006979I), Feb 13, 1991: Boeing 7372B7 (N282AU), Dayton, OH, Minor damage. NR1 engine compressor stall. Returned. Nose cone had separated from the gear case and was positioned in nose cowl.

## Other aircraft with N282AU

- [Registered now](https://openairdocs.org/aircraft/N282AU): Cessna T182T, S/N T18208540, built 2006

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