# Service difficulty reports: N267AU, cancelled Aug 24, 2004

A list on [N267AU, cancelled Aug 24, 2004](https://openairdocs.org/deregistered/N267AU-2004-08-24.md).

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

Page 1 of 2 · 56 reports

- [SDR USAA010452](https://openairdocs.org/sdr/USAA010452.md): Doubler · cracked · Apr 25, 2001 · N267AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN DOUBLER CRACKED.09375, BS 178, 12 OCLOCK POSITION, STRINGER 1L. ROUTED OUT DAMAGE (TIME LIMITED REPAIR) PER EA 69533. (M)
- [SDR USAA010451](https://openairdocs.org/sdr/USAA010451.md): Frame · cracked · Apr 25, 2001 · N267AU · Boeing 7372B7 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED.5 INCH, BS 178 WL 207 LEFT SIDE. REMOVED DAMAGED SECTION, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)
- [SDR USAA010450](https://openairdocs.org/sdr/USAA010450.md): Frame · cracked · Apr 25, 2001 · N267AU · Boeing 7372B7 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED, BS 178 WL 207 RIGHT SIDE CHORD. DAMAGED SECTION CUTOUT, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)
- [SDR USAASB00355](https://openairdocs.org/sdr/USAASB00355.md): Battery Pack · discharged · Dec 24, 2000 · N267AU · Boeing 7372B7 · Emergency Lighting
  > BWI - DURING THE OVERNIGHT CHECK, MAINTENANCE FOUND THE FORWARD EMERGENCY EXIT SIGN, AT SEAT ROW 2, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB00285](https://openairdocs.org/sdr/USAASB00285.md): Windshield · cracked · Oct 4, 2000 · N267AU · Boeing 7372B7 · Flight Compartment Windows
  > BDL - FLT 2612 - EN ROUTE FROM MHT TO BWI, THE FIRST OFFICERS WINDSHIELD CRACKED IN FLIGHT. COCKPIT VISION WAS AFFECTED. CREW DECLARED AN EMERGENCY AND DIVERTED TO BDL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFI
- [SDR USAASB00171](https://openairdocs.org/sdr/USAASB00171.md): Duct · ruptured · Jun 18, 2000 · N267AU · Boeing 7372B7 · Engine Bleed Air System
  > TPA - FLT 2704 - ON CLIMB-OUT FROM TPA, AT 6,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. WHEN THROTTLE WAS REDUCED, LIGHT EXTINGUISHED. WHEN THROTTLE WAS ADVANCED, LIGHT ILLUMINATED AGAIN. FLI
- [SDR USAASB99246](https://openairdocs.org/sdr/USAASB99246.md): Csd · failed · Oct 10, 1999 · N267AU · Boeing 7372B7 · Alternator-Generator Drive
  > MCO - FLT 2646 - FLIGHT DEPARTED MIA WITH THE NR 1 GENERATOR ON MEL. DURING CRUISE, THE NR 2 GENERATOR LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE NR 2 CSD AND DIVERTED TO MCO WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS
- [SDR USAASB99235](https://openairdocs.org/sdr/USAASB99235.md): Valve · failed · Sep 22, 1999 · N267AU · Boeing 7372B7 · Brake Anti-Skid Section
  > ORD - FLT 2704 - AFTER TAKEOFF FROM BWI, THE INBOARD ANTI-SKID LIGHT ILLUMINATED AND DID NOT EXTINGUISH AFTER GEAR RETRACTION. FLIGHT DIVERTED TO ORD FOR MAINTENANCE AND LONGER RUNWAYS. LIGHT REMAINED ON WHEN LANDING GEAR WAS DOWN AS WELL. FLIGHT LANDED WIT
- [SDR USAASB99226](https://openairdocs.org/sdr/USAASB99226.md): Power Supply · inoperative · Sep 4, 1999 · N267AU · Boeing 7372B7 · Emergency Lighting
  > BOS - MAINTENANCE FOUND THE AFT EMERGENCY LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB99161](https://openairdocs.org/sdr/USAASB99161.md): Light · inoperable · Jul 3, 1999 · N267AU · Boeing 7372B7 · Emergency Lighting
  > BWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE DOORS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT ASSEMBLY AND THE BATT
- [SDR 99ZZZX2823](https://openairdocs.org/sdr/99ZZZX2823.md): Battery Pack · discharged · Jul 3, 1999 · N267AU · Boeing 7372B7 · Emergency Lighting
  > BWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE DOORS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT ASSEMBLY AND THE BATT
- [SDR USAASB99114](https://openairdocs.org/sdr/USAASB99114.md): Connector · loose · Apr 28, 1999 · N267AU · Boeing 7372B7 · Engine Anti-Icing System
  > BWI - FLT 2681 - DURING CLIMB-OUT FROM BWI, THE NR 2 ENGINE FUEL HEAT LIGHT ILLUMINATED. THE NR 2 ENGIN OIL TEMP BEGAN TO EXCEED LIMITS. CREW TRIED DIFFERENT POWER LEVELS, BUT THE OIL TEMPERATURE REMAINED IN THE YELLOW TO RED BAND. CREW DECIDED TO RETURN TO
- [SDR USAA990423](https://openairdocs.org/sdr/USAA990423.md): Stringer · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT TERMINAL END STRINGER 26R AT STATION 540. INSTALLED NEW END FITTING PER SRM 51-10-01. (M)
- [SDR USAA990391](https://openairdocs.org/sdr/USAA990391.md): Web · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND A 2 INCH CRACK AT STATION 259 BL 0 CEILING ON NWW VERT STIFFENER WEB. REPAIRED PER SRM 51-10-01 PAGE 5. (M)
- [SDR USAA990390](https://openairdocs.org/sdr/USAA990390.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 12 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRAPS PER TR 53-10-13. (M)
- [SDR USAA990382](https://openairdocs.org/sdr/USAA990382.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING A Q-2 CHECK, VISUAL INSPECTION FOUND A 1 INCH AREA OF CORROSION AT STATION 312 LBL 1 FLOORBEAM. INSTALLED NEW 'T' CAP WITH SPLICES AND REPAIR STRAPS PER TR 53-10-13. (M)
- [SDR USAA990364](https://openairdocs.org/sdr/USAA990364.md): Frame · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Frame
  > CLT - DURING A Q-C CHECK, VISUAL INSPECTION, FOUND A.125 INCH CRACK AT BS 727 LEFT STRINGER 18A OUTER CHORD FRAME. INSTALLED NEW CHORD PER EO 5394G068 AND EO 5394G076. (M)
- [SDR USAA990363](https://openairdocs.org/sdr/USAA990363.md): Angle · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH CRACKS AT BS 727 BETWEEN STRINGER 24R AND 25R CHORD ANGLE. REPAIRED PER EA 64377, 64403 AND EO 5394G068. (M)
- [SDR USAA990353](https://openairdocs.org/sdr/USAA990353.md): Stringer · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2.5 INCH CORRODED AREA AT STRINGER 20L AND STATION 911 AFT CARGO. INSTALLED J ANGLE, U CHANNEL, SHIMS AND CLIP PER SRM 53-10-3 AND SRM 51-20-1. (M)
- [SDR USAA990314](https://openairdocs.org/sdr/USAA990314.md): Skin · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Service Doors
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR LOWER AFT CORNER SKIN. INSTALLED EXTERNAL DOUBLER PER T/R 53-10-19 REV A AND EA 64244 AND 64167. (M)
- [SDR USAA990313](https://openairdocs.org/sdr/USAA990313.md): Skin · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > CLT - DURING Q-2 CHECK HFEC INSPECTION, FOUND A.09375 INCH CRACK IN FORWARD ENTRY DOOR LOWER HINGE CUTOUT FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3 FIG 31. (M)
- [SDR USAA990312](https://openairdocs.org/sdr/USAA990312.md): Angle · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK IN FLOORBEAM TO FUSELAGE ATTACH ANGLE AT BS 597, RBL 70.85 AND WL 204-208. INSTALLED ANGLE REPAIR PER EA 64287. (M)
- [SDR USAA990309](https://openairdocs.org/sdr/USAA990309.md): Creasebeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING VISUAL CHECK INSPECTION, FOUND SEVERAL AREAS OF CORROSION AT BS 270 TO BS 360 STRINGER 17L CREASEBEAM INNER CHORD ANGLE. REPAIRED PER BOEING DRAWING 65-17688 AND SRM 51-30-3. (M)
- [SDR USAA990303](https://openairdocs.org/sdr/USAA990303.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 947 RBL 6 FLOORBEAM. INSTALLED REPAIR ANGLES AND FILLERS PER SRM 53-10-09 PAGE 26 THROUGH PAGE 30. (M)
- [SDR USAA990302](https://openairdocs.org/sdr/USAA990302.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 986.5. SPLICED IN NEW SECTION OF FLOORBEAM 'T' CAP PER TR 53-60-01 AND EA 64288. (M)
- [SDR USAA990301](https://openairdocs.org/sdr/USAA990301.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND CORROSION ALONG TOP SURFACE OF FLOORBEAM AT STATION 967, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP AND DOUBLER PER SRM 53-10-9 FIG 2 AND EA 64204. (M)
- [SDR USAA990300](https://openairdocs.org/sdr/USAA990300.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 328 LBL 12 AND RBL 1. INSTALLED NEW 'T' CAP REPAIR ANGLES AND STRAPS PER TR 53-10-13. (M)
- [SDR USAA990299](https://openairdocs.org/sdr/USAA990299.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 294.5 BL 0. SPLICED IN NEW 'T' CAP PER TR 53-10-04B. (M)
- [SDR USAA990298](https://openairdocs.org/sdr/USAA990298.md): Cap · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION AT BS 344 LBL 6 AND LBL 10 FLOOR 'T' CAP, CORROSION TASK NR C53-107-01. INSTALLED NEW 'T' CAP REPAIR ANGLES AND CAPS PER TR 53-10-13. (M)
- [SDR USAA990297](https://openairdocs.org/sdr/USAA990297.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING A Q-2 CHECK, VISUAL INSPECTION, FOUND SEVERAL 1 INCH AREAS OF CORROSION AT STATION 967 BETWEEN LBL 10 AND RBL 50 FLOORBEAM. SPLICED IN NEW 'T' CAP PER SRM 53-10-09 AND EA 64202. (M)
- [SDR USAA990296](https://openairdocs.org/sdr/USAA990296.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON SURFACE TOP OF FLOORBEAM STATION 1006, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER SRM 53-10-09 AND EA 64206, R 53-10-13. (M)
- [SDR USAA990291](https://openairdocs.org/sdr/USAA990291.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY.5 INCH AREA OF CORROSION AT STATION 947 RBL 6 ON FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLED ANGLE PER SRM 53-10-9. (M)
- [SDR USAA990290](https://openairdocs.org/sdr/USAA990290.md): Angle · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY 20 INCH AREA OF CORROSION AT STATION 947 TO STATION 1016 LBL 53 INNER CHORD ANGLE, CORROSION TASK NR C53-107-02. REPAIRED PER SRM 51-10-1. (M)
- [SDR USAA990289](https://openairdocs.org/sdr/USAA990289.md): Floorbeam · corroded · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Main, Floor Beam
  > CLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION ON FLOORBEAM AT STATION 328 LBL 12 AND RBL 1, CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER TR 53-10-13. (M)
- [SDR USAA990259](https://openairdocs.org/sdr/USAA990259.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 767 STRINGER 16R TIE CLIP. REPAIRED PER SRM 51-10-01. (M)
- [SDR USAA990220](https://openairdocs.org/sdr/USAA990220.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 847 STRINGER 1 TIE CLIP. INSTALLED NEW TIE CLIP PER EO NR 5393G227. (M)
- [SDR USAA990214](https://openairdocs.org/sdr/USAA990214.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 767 STRINGER 10R TIE CLIP. REPLACED PART. (M)
- [SDR USAA990213](https://openairdocs.org/sdr/USAA990213.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRCK BS 787 STRINGER 10L TIE CLIP. REPLACED PART. (M)
- [SDR USAA990212](https://openairdocs.org/sdr/USAA990212.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 727 STRINGER 8L TIE CLIP. REPLACED PART. (M)
- [SDR USAA990211](https://openairdocs.org/sdr/USAA990211.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK BS 727A STRINGER 1 TIE CLIP. REPLACED PART. (M)
- [SDR USAA990210](https://openairdocs.org/sdr/USAA990210.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 727B STRINGER 8R TIE CIP. REPLACED PART. (M)
- [SDR USAA990209](https://openairdocs.org/sdr/USAA990209.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 727B STRINGER 15R TIE CLIP. REMOVED ORIGINAL CLIP AND HFEC PART AND STRINGER, NO CRACK FOUND. REINSTALLED ORIGINAL PART PER SRM 51-30-02. (M)
- [SDR USAA990208](https://openairdocs.org/sdr/USAA990208.md): Tie Clip · cracked · Apr 23, 1999 · N267AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 727B STRINGER 5R TIE CLIP. REPLACED PART. (M)
- [SDR USAASB99047](https://openairdocs.org/sdr/USAASB99047.md): Power Supply · inoperative · Feb 20, 1999 · N267AU · Boeing 7372B7 · Emergency Lighting
  > CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVICE DOOR EMERGENCY EX
- [SDR 99ZZZM195](https://openairdocs.org/sdr/99ZZZM195.md): Battery · discharged · Feb 20, 1999 · N267AU · Boeing 7372B7 · Emergency Lighting
  > CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVICE DOOR EMERGENCY EX
- [SDR 99ZZZM194](https://openairdocs.org/sdr/99ZZZM194.md): Battery Pack · discharged · Feb 20, 1999 · N267AU · Boeing 7372B7 · Emergency Lighting
  > CLT - PILOT REPORTED VARIOUS CABIN AND FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT CABIN POWER SUPPLIES AND BATTERY PACKS. OPERATIONAL CHECK GOOD. ALSO, REPLACED FORWARD ENTRY AND SERVICE DOOR EMERGENCY EX
- [SDR USAA970090](https://openairdocs.org/sdr/USAA970090.md): Skin · cracked · Mar 12, 1997 · N267AU · Boeing 7372B7 · Service Doors
  > GSO - DURING TRANSIT CHECK VISUAL, VERIFIED BY EDDY CURRENT INSPECTION, FOUND TWO.25 INCH CRACKS LEFT FORWARD SERVICE DOOR, SKIN AT AFT CORNERS OF LOWER HINGE CUT OUT. INSTALLED DOUBLER, REPAIRED PER TYPICAL REPAIR 52-40-03A. (M)
- [SDR USAA970089](https://openairdocs.org/sdr/USAA970089.md): Skin · cracked · Mar 12, 1997 · N267AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
  > GSO - DURING TRANSIT CHECK VISUAL, VERIFIED WITH EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN SKIN FUSELAGE RIGHT SIDE, STATION 764, STRINGER 19R. INSTALLED DOUBLER, REPAIRED PER TYPICAL REPAIR 53-30-3 FIG 6. (M)
- [SDR USAA960784](https://openairdocs.org/sdr/USAA960784.md): Stringer · corrosion · Dec 7, 1996 · N267AU · Boeing 7372B7 · Fuselage Main, Longeron/Stringer
  > ROA - DURING CX-4 CHECK, VISUAL INSPECTION FOUND 2 INCH BY 12 INCH CORROSION, STR 27L, BS 967. REMOVED CORROSION AND INSTALLED DOUBLER AND SPLICED, REPAIRED PER SRM 53-10-3, FIG 1. (X)
- [SDR USAASB96197](https://openairdocs.org/sdr/USAASB96197.md): Fuel Heat Vlv · stuck open · Sep 19, 1996 · N267AU · Boeing 7372B7 · Engine Anti-Icing System
  > CMH - FL 1183 - DURING CLIMB AT FL 280, CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO HIGH OIL TEMPERATURE. THE OIL TEMPERATURE WAS IN THE YELLOW BAND FOR APPROX 15 MINS PRIOR TO SHUTDOWN. CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH WHERE THE FLIGHT LANDED WIT

Next page: https://openairdocs.org/deregistered/N267AU-2004-08-24/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N267AU' AND deregistration_id = 'N267AU-2004-08-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N267AU-2004-08-24/reports

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