# N510AU: Boeing 737-3B7, registration cancelled 2003-06-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 4, 2003
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-3B7](https://openairdocs.org/model/boeing-737-3b7) (registry code 138447F)
- Serial number: 23385
- Type of aircraft: Fixed wing multi engine
- Last registry action: June 4, 2003
- Mode S code: A66182
- Owner when cancelled: [Flight Director Inc](https://openairdocs.org/faa-owner/FLIGHT%20DIRECTOR%20INC)
- Location: [Austin, TX](https://openairdocs.org/faa-place/TX/Austin)
- Owner type: Corporation
- Owner's area on the map: 30.4538° N, 97.6867° W: Placed by OpenAirDocs at the center of ZIP code 78728, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N510AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=510AU
- Page: https://openairdocs.org/deregistered/N510AU-2003-06-04

From the FAA registry file of November 3, 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 737-3B7: https://openairdocs.org/model/boeing-737-3b7.md

## Service difficulty reports (52, newest 50)

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

- [SDR USAASB02154](https://openairdocs.org/sdr/USAASB02154), Aug 16, 2002: PANEL. ILLUMINATED. DURING CRUISE, ENROUTE, THE NR1 ENGINE DRIVEN HYDRAULIC PUMP (A) SYSTEM LOW PRESSURE LIGHT ILLUMINATED. FIVE MINUTES LATER, THE NR 2 ENGINE DRIVEN HYDRAULIC PUM
- [SDR USA2002F00076](https://openairdocs.org/sdr/USA2002F00076), Jul 30, 2002: LIGHT. FAILED. PILOT REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 10ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL.
- [SDR USAASB01315](https://openairdocs.org/sdr/USAASB01315), Nov 19, 2001: BATTERY PACK. DISCHARGED. TPA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHT EXTINGUISHES AFTER A FEW SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPER
- [SDR USAASB01241](https://openairdocs.org/sdr/USAASB01241), Aug 24, 2001: HYDRAULIC LINE. CRACKED. DTW - FLT 1291 - ON CLIMB-OUT FROM DTW, EN ROUTE TO PHL, CAPTAIN REPORTED A FAILURE OF THE 'A' HYDRAULIC SYSTEM ALONG WITH HYDRAULIC QUANTITY LOSS. CAPTAIN DECI
- [SDR USAASB00297](https://openairdocs.org/sdr/USAASB00297), Oct 21, 2000: LIGHT. FAILED. ROA-PIT - FLT 1295 - AFTER LANDING GEAR EXTENSION THE RIGHT MAIN GEAR DOWN LOCK LIGHT DID NOT ILLUMINATE. A VISUAL INSPECTI0N COULD NOT CONFIRM THE LANDING GEAR
- [SDR USAASB00101](https://openairdocs.org/sdr/USAASB00101), Apr 4, 2000: CLAMP. LOOSE. CHS - FLT 1452 - ON CLIMB-OUT FROM RSW, AT FL270, CAPTAIN RECEIVED A RIGHT WING BODY OVERHEAT INDICATION. LIGHT EXTINGUISHED IMMEDIATELY AFTER BLEED SWITCH WAS 
- [SDR USAA000294](https://openairdocs.org/sdr/USAA000294), Mar 2, 2000: KEELBEAM. CRACKED. TPA - FOUND KEEL BEAM CRACKED, RBL 630 KEEL BEAM. INSTALLED DOUBLER PER SRM 53-60-12. (M)
- [SDR USAASB99135](https://openairdocs.org/sdr/USAASB99135), Jun 3, 1999: LIGHT. INOPERATIVE. PHL - PILOT REPORTED THAT THE LOW LEVEL EMERGENCY LIGHTS IN THE AFT SECTION OF THE CABIN, AT ROWS 17-21 ABC, ARE INOPERATIVE. MAINTENANCE FOUND THE SEAT ASSEMBL
- [SDR USAA990548](https://openairdocs.org/sdr/USAA990548), May 29, 1999: KEEL BEAM. CORRODED. CLT - DURING Q4 CHECK, FOUND .5 INCH BY 14 INCH CORRODED AREA AT RT KEEL BEAM AT BS 710 - BS 724, RBL 6.3, WL 148.5. CORROSION LEVEL 1, CORROSION TASK C53-212-0
- [SDR USAA990547](https://openairdocs.org/sdr/USAA990547), May 29, 1999: BRACKET. CRACKED. CLT - DURING Q4 CHECK, FOUND 2 INCH CRACK IN LOWER FLANGE AT ANTENNA SADDLE BRACKET AT STATION 727E - 727D. REPLACED SADDLE BRACKET. (M)
- [SDR USAA990546](https://openairdocs.org/sdr/USAA990546), May 29, 1999: FLOOR. CORRODED. CLT - DURING Q-4 CHECK, FOUND 3 INCH CORROSION AT LT LAV FLOOR PAN. CORROSION LEVEL 1, CORROSION TASK NR C53-107-02. NEW WEB INSTALLED PER SRM 51-10-02. (M)
- [SDR USAA990545](https://openairdocs.org/sdr/USAA990545), May 29, 1999: ANGLE. CORRODED. CLT - DURING Q-4 CHECK, FOUND 40 INCH CORROSION AT Z-ANGLE AT BS 947 TO 986. CORROSION LEVEL 1, CORROSION TASK NR C53-107-02. REPLACED Z-ANGLE PER SRM 51-10-02.
- [SDR USAA990544](https://openairdocs.org/sdr/USAA990544), May 29, 1999: ANGLE. CORRODED. CLT - DURING Q-4 CHECK, FOUND 1 INCH BY 39 INCH CORRODED AREA AT Z-ANGLE AT STATION 947 TO 986. CORROSION LEVEL 1, CORROSION TASK NR C53-107-02. REPLACED Z-ANGL
- [SDR USAA990543](https://openairdocs.org/sdr/USAA990543), May 29, 1999: MOUNT. CORRODED. CLT - DURING Q4 CHECK, FOUND 2 INCH DIAMETER CORRODED AREA AT AFT OUTBOARD LAV MOUNT AT STATION 1012, RBL 37, FLOOR LEVEL. CORROSION LEVEL 1, CORROSION TASK NR 
- [SDR USAA990542](https://openairdocs.org/sdr/USAA990542), May 29, 1999: T-CAP. CORRODED. CLT - DURING Q-4 CHECK, FOUND .5 INCH CORRODED AREA SEVERAL PLACES AT T-CAP AT BS 1016 LBL 28-33. CORROSION LEVEL 1. INSTALLED T-CAP REPAIR PER SRM 53-00-51 FIG
- [SDR USAA990541](https://openairdocs.org/sdr/USAA990541), May 29, 1999: STRAP. CORRODED. CLT - DURING Q-4 CHECK, FOUND 2 INCH BY 14 INCH AREA OF CORROSION AT STRAP AT STATION 1016 TO 1038, WL 3 FLOOR LEVEL. CORROSION LEVEL 2, CORROSION TASK NR C53-1
- [SDR USAA990540](https://openairdocs.org/sdr/USAA990540), May 29, 1999: BEAM. CORRODED. CLT - DURING Q4 CHECK, FOUND PREVIOUS BLEND OUT TOP OF T-CAP ON BEAM AT STATION 328 LBL 49, WL 208. INSTALLED REPAIR DOUBLERS AND SPLICE OT CAP PER SRM 53-10-51
- [SDR USAA990539](https://openairdocs.org/sdr/USAA990539), May 29, 1999: MOUNT. CORRODED. CLT - DURING Q-4 CHECK, FUOND 2 INCH DIAMETER CORRODED AREA IN FORWARD INBOARD LAV MOUNT AT STATION 993 RBL 19 FLOOR LEVEL. CORROSION LEVEL 1. CORROSION TASK NR
- [SDR USAA990538](https://openairdocs.org/sdr/USAA990538), May 29, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK, FOUND SEVERAL 1 INCH DRAIN CORRODED AREAS IN FLOORBEAM AT STATION 986.5 FROM LEFT CREASE BEAM TO RIGHT CREASE BEAM FLOOR LEVEL. CORROSIO
- [SDR USAA990537](https://openairdocs.org/sdr/USAA990537), May 29, 1999: CLIP. CRACKED. CLT - DURING Q4 CHECK, FOUND 1 INCH CRACK IN RADIUS OF VERTICAL FLANGES AT ATTACH CLIP/BRACKETS AT LBL 2 AND RBL 2 AT STATION 727D. DEFECTIVE PART REPLACED WITH
- [SDR USAA990536](https://openairdocs.org/sdr/USAA990536), May 29, 1999: FRAME. CRACKED. CLT - DURING Q-4 CHECK, FOUND .125 INCH CRACK AT FRAME STATION 400 BETWEEN STRINGER 8L - STRINGER 9L (OVERHEAD BIN ATTACH). INSTALLED DOUBLER REPAIR PER SRM 53-
- [SDR USAA990535](https://openairdocs.org/sdr/USAA990535), May 29, 1999: FRAME. CRACKED. CLT - DURIGN Q-4 CHECK, FOUND .12 5INCH CRACK AT FRAME STATION 440 BETWEEN STRINGER 8L - STRINGER 9L (OVERHEAD BIN ATTACH). INSTALLED DOUBLER REPAIR PER SRM 53-
- [SDR USAA990534](https://openairdocs.org/sdr/USAA990534), May 29, 1999: FRAME. CRACKED. CLT - DURING Q-4 CHECK, FOUND FUSELAGE FRAME CRACKED .200 INCH IN LENGTH, THREE (3) HOLES AT CLIP ATTACH ON FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 
- [SDR USAA990533](https://openairdocs.org/sdr/USAA990533), May 29, 1999: CLIP. CRACKED. CLT - DURING Q-4 CHECK, FOUND .125 INCH CRACK IN CLIP AT STATION 380, TOP CENTER CLIP (STRINGER TO FRAME ATTACH CLIP). DEFECTIVE PART REPLACED WITH IDENTICAL PA
- [SDR USAA990532](https://openairdocs.org/sdr/USAA990532), May 29, 1999: BRACKET. CRACKED. CLT - DURING Q-4 CHECK, FOUND .25 INCH CRACK AT ANTENNA BRACKET AT 727 D TO E. INSTALLED NEW PART, IDENTICAL NUMBER PER SRM 51-10-02. (M)
- [SDR USAA990531](https://openairdocs.org/sdr/USAA990531), May 29, 1999: ANGLE. CRACKED. CLT - DURIGN Q-4 CHECK, FOUND 2 INCH CRACK (FASTENER HOLE TO HOLE) AT LOWER END OF BS 618 LEFT FRAME INNER CHORD ANGLE. DEFECTIVE PART REPLACED WITH IDENTICAL P
- [SDR USAA990476](https://openairdocs.org/sdr/USAA990476), May 29, 1999: FLOORBEAM. CORROSION. CLT - DURING Q-4 CHECK, FOUND 1.5 INCH BY .5 INCH CORRODED AREA ON FLOORBEAM AROUND FLOORBOARD HOLE AT BS 412 BL 0. CORROSION LEVEL 1. INSTALLED STRAP ON AFT SI
- [SDR USAA990460](https://openairdocs.org/sdr/USAA990460), May 29, 1999: FRAME. CRACKED. CLT - DURNG Q-4 CHECK, FOUND .125 INCH CRACK IN FRAME AT STATION 400 BETWEEN STRINGER 8R - STRINGER 9R (O/HEAD BIN ATTACH). INSTALLED DOUBLER PER SRM 53-00-07 A
- [SDR 99ZZZM404](https://openairdocs.org/sdr/99ZZZM404), May 29, 1999: BRACKETS. CRACKED. CLT - DURING Q4 CHECK, FOUND 1 INCH CRACK IN RADIUS OF VERTICAL FLANGES AT ATTACH CLIP/BRACKETS AT LBL 2 AND RBL 2 AT STATION 727D. DEFECTIVE PART REPLACED WITH
- [SDR USAASB98269](https://openairdocs.org/sdr/USAASB98269), Oct 13, 1998: SOCKET. FAILED. PIT - MAINTENANCE FOUND THE EMERGENCY FLOOR TRACK LIGHTING AT SEAT ROW 22 INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT ROW 22 FLOOR TRACK LIG
- [SDR USAASB98210](https://openairdocs.org/sdr/USAASB98210), Aug 13, 1998: LIGHT. INOPERATIVE. CLT - PILOT REPORTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 12 IS INOP. MAINTENANCE REMOVED AND REPLACED TWO LAMPHOLDER ASSEMBLIES AT SEAT ROW 12. OP
- [SDR USAASB98123](https://openairdocs.org/sdr/USAASB98123), May 18, 1998: LIGHT. INOPERATIVE. TPA - DURING B-CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT AT THE AFT SERVICE DOOR INOP. MAINTENANCE FOUND THE LIGHT SOCKET WAS BROKEN DUE TO EXCESSIV
- [SDR USAASB97341](https://openairdocs.org/sdr/USAASB97341), Dec 17, 1997: SEAL. FAILED. CLT - FLT 81 - SHORTLY AFTER LEVELING OFF AT FL330, AIRCRAFT EXPERIENCED A RAPID DECOMPRESSION. CREW DECLARED AND EMERGENCY, DESCENDED TO 10,000 FT AND RETURNED
- [SDR USAASB97319](https://openairdocs.org/sdr/USAASB97319), Nov 20, 1997: WIRE HARNESS. FAILED. LAX - FLT 36 - AT DEPARTURE TIME, CREW REPORTED THAT ONE FLOOR LEVEL EMERGENCY LIGHT IN THE FORWARD CABIN WAS INOP. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 
- [SDR USAASB97309](https://openairdocs.org/sdr/USAASB97309), Nov 10, 1997: ADC. FAILED. PIT - FL 152 - SHORTLY AFTER TAKEOFF, THE AUTO-PILOT DISENGAGED, THE FIRST OFFICERS AIRSPEED DECREASED, THE STALL WARNING SOUNDED AND THE STICK SHAKER ACTIVATED
- [SDR USAASB97311](https://openairdocs.org/sdr/USAASB97311), Nov 9, 1997: BATTERY. DISCHARGED. PHL - MAINTENANCE FOUND A STRIP OF EMERGENCY LIGHTS IN THE FORWARD CABIN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND CHARGER ASSEMBLY. OPS CHECK GOOD
- [SDR 97ZZZM1171](https://openairdocs.org/sdr/97ZZZM1171), Nov 9, 1997: CHARGER. INOPERATIVE. PHL - MAINTENANCE FOUND A STRIP OF EMERGENCY LIGHTS IN THE FORWARD CABIN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND CHARGER ASSEMBLY. OPS CHECK GOOD
- [SDR USAASB97282](https://openairdocs.org/sdr/USAASB97282), Oct 12, 1997: WIRE. BROKEN. CLT - FOUND FLOOR TRACK LIGHTING AT ROW 3 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB97278](https://openairdocs.org/sdr/USAASB97278), Oct 7, 1997: WIRE. BROKEN. ORD - FORWARD 4 EMERGENCY FLOOR LIGHTS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB97271](https://openairdocs.org/sdr/USAASB97271), Sep 26, 1997: SOCKET. FAILED. CLT - MAINTENANCE FOUND THE FLOOR TRACK EMERGENCY LIGHTING INOPERABLE AT ROWS 9 AND 18. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET (PN 08169-1) AT ROW 9 
- [SDR USAASB97242](https://openairdocs.org/sdr/USAASB97242), Sep 9, 1997: BATTERY PACK. FAILED. MIA - EMERGENCY EXIT LIGHTS ROW 18 (FLOOR) INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X)
- [SDR USAASB97137](https://openairdocs.org/sdr/USAASB97137), May 24, 1997: O-RING. FAILED. BWI - FLT 2399 - AT FL 210, THE NR 1 ENGINE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. CAPTAIN SHUT DOWN THE NR 1 ENGINE HYDRAULIC PUMP AND MAINTAINED 3
- [SDR USAASB96010](https://openairdocs.org/sdr/USAASB96010), Jan 18, 1996: SENSOR. FAILED. FLT NR 7015 - PIT - AFTER EXTENSION, RED NOSE GEAR LIGHT FAILED TO EXTINGUISH. MAINTENANCE REPLACED THE NOSE GEAR LOCK SENSOR. INDICATIONS NORMAL. (M)
- [SDR USAA950997](https://openairdocs.org/sdr/USAA950997), Aug 29, 1995: FLOOR BEAM. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION BS 947.5 TO BS 967 RBL 45 ON FLOOR BEAM T-CAP. FABRICATED NEW T-CAP 18 INCHES LONG, R
- [SDR USAA950996](https://openairdocs.org/sdr/USAA950996), Aug 29, 1995: ANGLE. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION AT CLIP NUT HOLES, AFT CARGO BIN AFT CENTER BULKHEAD LOWER ATTACH ANGLE. REPLACED ATT
- [SDR USAA950998](https://openairdocs.org/sdr/USAA950998), Aug 28, 1995: STRINGER. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION BS 870 S-21L. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-70-11 FIG 1. CORROSIO
- [SDR USAA950995](https://openairdocs.org/sdr/USAA950995), Aug 25, 1995: SKIN. CHAFED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CROWN SKIN CHAFED UNDER DORSAL FIN CONTACT AREA, S-1 BS 887 TO BS 867. INSTALLED EXT SKIN DOUBLER. REPAIRED PER 
- [SDR USAA950999](https://openairdocs.org/sdr/USAA950999), Aug 24, 1995: DUMP SHOOT BASE. CORROSION. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 6 INCH CORRODED AREA AFT CARGO BS 986.50- BS 1006 DUMP SHOOT BASE. INSTALLED NEW BASE PER DRAWING 65-4
- [SDR USAA950993](https://openairdocs.org/sdr/USAA950993), Aug 24, 1995: STRINGER. CRACKED. INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 500 C PLUS 16, STRINGER 16R. INSTALLED DOUBLER, REPAIRED PER EO 5393X228. (M)
- [SDR USAA950992](https://openairdocs.org/sdr/USAA950992), Aug 24, 1995: STRINGER. CRACKED. INT - DURING Q-3 CHECK VISUAL, FOUND .5 INCH CRACK BS 500 C PLUS 4 STRINGER 16R. INSTALLED DOUBLER, REPAIRED PER EO 539X228. (M)

All 52: https://openairdocs.org/deregistered/N510AU-2003-06-04/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 19901101058709I](https://openairdocs.org/incident/19901101058709I), Nov 1, 1990: Boeing 7373B7 (N510AU), San Francisco, CA, Minor damage. Vibration and fire warning on NR2 engine. Diverted for landing. Complete turbine failure.

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