# Service difficulty reports: N254AU, cancelled Jul 16, 2004

A list on [N254AU, cancelled Jul 16, 2004](https://openairdocs.org/deregistered/N254AU-2004-07-16.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 · 58 reports

- [SDR USAASB01301](https://openairdocs.org/sdr/USAASB01301.md): Battery · discharged · Oct 21, 2001 · N254AU · Boeing 737201 · Emergency Lighting
  > BSI - THE EMERGENCY LIGHT ABOVE THE 1R EXIT FLASHES ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)
- [SDR USAASB01289](https://openairdocs.org/sdr/USAASB01289.md): Power Supply · discharged · Oct 10, 2001 · N254AU · Boeing 737201 · Emergency Lighting
  > LGA - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAASB01226](https://openairdocs.org/sdr/USAASB01226.md): Wire · broken · Aug 8, 2001 · N254AU · Boeing 737201 · Light System Wiring
  > BDL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING. OPERATIONAL CHECK NORMAL. (M)
- [SDR USAA010757](https://openairdocs.org/sdr/USAA010757.md): Keelbeam · corroded · Jun 22, 2001 · N254AU · Boeing 737201 · Fuselage Main, Keel
  > CLT - FOUND KEEL BEAM CORRODED 1 INCH DIAMETER BY.020 INCH DEEP, BS 727 PLUS 16, S27L. CORROSION REMOVED, AND REPAIR INSTALLED PER EA 94208, ALONG WITH ACCESS SKIN REPAIR PER SRM 53-30-3. (M)
- [SDR USAA010764](https://openairdocs.org/sdr/USAA010764.md): Keelbeam · corroded · Jun 20, 2001 · N254AU · Boeing 737201 · Fuselage Main, Keel
  > TPA - FOUND LEFT HAND KEEL BEAM CORRODED.75 INCH DIAMETER BY.020 INCH DEEP, BS 727 PLUS 16, LOWER SURFACE. DAMAGE REMOVED, KEEL BEAM REPAIRED PER EA 94208. ACCESS REQUIRES SKIN REPAIR PER SRM 53-30-3, FIG 6. (M)
- [SDR USAA010765](https://openairdocs.org/sdr/USAA010765.md): Stringer · corroded · Jun 19, 2001 · N254AU · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUDN STRINGER CORRODED 10 SQUARE INCHES, BS 967, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3, FIG 1. (M)
- [SDR USAA010748](https://openairdocs.org/sdr/USAA010748.md): Stringer · corroded · Jun 19, 2001 · N254AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > TPA - FOUND STRINGER CORRODED 10 SQUARE INCHES, PREVIOUSLY SPLICED SECTION OF STRINGER 27L AT STATION 967. CORROSION LEVEL 1. SPLICED IN NEW SECTION OF STRINGER USING SPLICES RETAINED FROM PREVIOUS REPAIR PER SRM 53-10-3 FIG 1. (M)
- [SDR USAA010749](https://openairdocs.org/sdr/USAA010749.md): Skin · cracked · Jun 18, 2001 · N254AU · Boeing 737201 · Fuselage Structure (General)
  > TPA - FOUND SKIN CRACKED 1 INCH, AFT OF STATION 907 STRINGER 18L. INSTALLED DOUBLER PER EA 71383 AND SRM 53-00-01 FIG 223. (M)
- [SDR USAA010766](https://openairdocs.org/sdr/USAA010766.md): Skin · cracked · Jun 17, 2001 · N254AU · Boeing 737201 · Fuselage Structure (General)
  > TPA - FOUND SKIN CRACKED 1 INCH, BS 907, STRINGER 18L. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-00-01, AND EA 7183. (M)
- [SDR USAASB01032](https://openairdocs.org/sdr/USAASB01032.md): Compressor · stalled · Feb 1, 2001 · N254AU · Boeing 737201 · Engine (Turbine/Turboprop)
  > CLT - FLT 2676 - EN ROUTE FROM TPA TO LGA, AT FL330, CAPTAIN REPORTED THAT THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. NO ENGINE PARAMETERS WERE EXCEEDED. THROTTLE WAS REDUCED AND THE ENGINE RAN NORMALLY AFTER THE INITIAL STALL. FLIGHT DIVERTED TO CLT A
- [SDR USAASB00133](https://openairdocs.org/sdr/USAASB00133.md): Actuator · failed · May 5, 2000 · N254AU · Boeing 737201 · Leading Edge Slat Actuator
  > IAD - FLT 2755 - ON CLIMB-OUT FROM IAD, THE NR 6 SLAT DID NOT RETRACT WHEN THE FLAPS WERE MOVED TO UP OR ZERO DEGREES. FLIGHT RETURNED TO FIELD AT IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 6
- [SDR USAASB00036](https://openairdocs.org/sdr/USAASB00036.md): Charger · failed · Feb 9, 2000 · N254AU · Boeing 737201 · Emergency Lighting
  > CLE - WHILE ACCOMPLISHING A CHECK, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT AND ASSOCIATED INTERIOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M193 BATTERY PACK (P/N 61-0478-9) AND CHARGER ASSEMBLY. OPERATIONAL CHE
- [SDR USAA000112](https://openairdocs.org/sdr/USAA000112.md): Skin · cracked · Jan 27, 2000 · N254AU · Boeing 737201 · Passenger/Crew Doors
  > CLT - AFTER ENTRY DOOR LOWER FORWARD SKIN HAS A 1.5 INCH CRACK. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 24.. (M)
- [SDR USAA991048](https://openairdocs.org/sdr/USAA991048.md): Skin · cracked · Oct 7, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK IN SKIN AFT ENTRY DOOR LOWER DOOR HINGE CUTOUT. INSTALLED DOUBLER PER TR 53-30-10 REV B AND SRM 53-30-3 FIG 34. (M)
- [SDR USAA991045](https://openairdocs.org/sdr/USAA991045.md): Skin · cracked · Oct 7, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN SKIN AT STATION 727A STRINGER 19R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)
- [SDR USAA990947](https://openairdocs.org/sdr/USAA990947.md): Skin · cracked · Sep 1, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > BOS - DURING RON FOUND 1.125 INCH CRACK IN SKIN AT 767, 1.5 INCH ABOVE STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3, PAGE 2E, FIG 1 SHT 4. (M)
- [SDR USAA990946](https://openairdocs.org/sdr/USAA990946.md): Skin · cracked · Sep 1, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > BOS - DURING RON, FOUND 1.5 INCH CRACK IN SKIN AT STATION 770,.5 INCH BELOW STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3, PAGE 2E, FIG 1 SHT 4. (M)
- [SDR USAASB99144](https://openairdocs.org/sdr/USAASB99144.md): Valve · failed · Jun 14, 1999 · N254AU · Boeing 737201 · APU Bleed Air System
  > BWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE APU FAILED TO START.
- [SDR 99ZZZM393](https://openairdocs.org/sdr/99ZZZM393.md): Oil Cooler · failed · Jun 14, 1999 · N254AU · Boeing 737201 · Engine Oil Cooler
  > BWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE APU FAILED TO START.
- [SDR 99ZZZM392](https://openairdocs.org/sdr/99ZZZM392.md): Csd · failed · Jun 14, 1999 · N254AU · Boeing 737201 · Alternator-Generator Drive
  > BWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE APU FAILED TO START.
- [SDR USAASB99033](https://openairdocs.org/sdr/USAASB99033.md): Pcu · failed · Feb 8, 1999 · N254AU · Boeing 737201 · Elevator Control System
  > BWI - FLT 2605, ON FINAL APPROACH, AFTER LANDING GEAR AND FLAPS WERE EXTENDED, THE 'A' SYSTEM HYDRAULIC QUANTITY DEPLETED TO ZERO WITH THE LOW PRESSURE LIGHT ILLUMINATING. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED CLEAR OF THE RUNWAY. THE AIRCRAFT WAS TOWED
- [SDR USAA980682](https://openairdocs.org/sdr/USAA980682.md): Skin · cracked · Dec 27, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK IN EXTERNAL SKIN STATION 805 STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)
- [SDR USAASB98316](https://openairdocs.org/sdr/USAASB98316.md): Csd · overserviced · Nov 29, 1998 · N254AU · Boeing 737201 · Alternator-Generator Drive
  > PIT - FLT 2691 - AFTER CLIMB-OUT FROM ROC, CAPTAIN REPORTED THAT THE NR 2 ENGINE CSD DISCONNECTED AND THAT HE WAS UNABLE TO START THE APU DUE TO LOW OIL PRESSURE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTEN
- [SDR USAASB98314](https://openairdocs.org/sdr/USAASB98314.md): Engine · fod · Nov 24, 1998 · N254AU · Boeing 737201 · Engine (Turbine/Turboprop)
  > BWI - FL2659 - UPON CLIMB-OUT AT APPROX 3,000 FT, THE NR 2 ENGINE INJESTED A BIRD. A MODERATE VIBRATION WAS NOTICED FROM THE NR 2 ENGINE. CREW SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BWI. THE CABIN WAS PREPPED FOR AN EMERGE
- [SDR USAASB98163](https://openairdocs.org/sdr/USAASB98163.md): Shut Off Valve · failed · Jun 30, 1998 · N254AU · Boeing 737201 · Pneumatic Distribution System
  > PIT - FLT 296 - CREW ADVISED VIA ACARS WERE ENCOUNTERING PROBLEMS WITH THE DUCT PRESSURES. AT CLIMB POWER, THE LEFT DUCT PRESSURE READS 80 PSI WHILE THE RIGHT READS 38 PSI. THE DECISIION WAS MADE TO DIVERT TO PIT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LA
- [SDR USAASB98109](https://openairdocs.org/sdr/USAASB98109.md): Coalescer Bag · dirty · May 9, 1998 · N254AU · Boeing 737201 · Humidity Control System
  > GSO - FLT 1704, EN ROUTE ATL-BWI, BOTH THE FORWARD AND AFT CABIN SMOKE DETECTOR ALARMS WENT OFF DURING FLIGHT. CREW NOTED A BURNING PLASTIC SMELL BUT COULD NOT LOCATE SOURCE. THERE WAS NO INDICATION OF SMOKE OF FIRE. FLIGHT DIVERTED TO GSO AND LANDED WITHOU
- [SDR USAA980099](https://openairdocs.org/sdr/USAA980099.md): Skin · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FUOND CRACK 2 INCHES LONG STATION 727A PLUS 4 INCH STRINGER 18R SKIN. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA980098](https://openairdocs.org/sdr/USAA980098.md): Spar Web · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Wing Spar
  > INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND CRACK.25 INCH LONG LT HORIZONTAL STABILIZER AT STATION 200.5 FRONT SPAR WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 55-10-5. (M)
- [SDR USAA980097](https://openairdocs.org/sdr/USAA980097.md): Skin · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCH LONG STATION 727 A STRINGER 18R SKIN. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA980096](https://openairdocs.org/sdr/USAA980096.md): Stringer · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH AT STATION 747 STRINGER REPAIR, REPAIRED PER 53-10-3. (M)
- [SDR USAA980095](https://openairdocs.org/sdr/USAA980095.md): Bulkhead · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Bulkhead
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK STATION 178 BULKHEAD UNDER RADAR DISH MOUNT, INBOARD SIDE OF RT LOWER HAT SECTION LEG. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11-1, SRM 53-10-11. (M)
- [SDR USAA980094](https://openairdocs.org/sdr/USAA980094.md): Frame · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND,.75 INCH CRACK STATION 616 FRAME INBOARD CHORD, LBL 62.5 WL 202 FRAME. FABRICATED AND INSTALLED REPAIR ANGLE, REPAIRED PER EA 43552. (M)
- [SDR USAA980093](https://openairdocs.org/sdr/USAA980093.md): Frame · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK STATION 616 FRAME INBOARD CHORD RBL 62.5, WL 202 FRAME. FABRICATED AND INSTALLED DOUBLER, REPAIRED PER EA 43551. (M)
- [SDR USAA980092](https://openairdocs.org/sdr/USAA980092.md): Floorbeam · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor Beam
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 3 INCHES STATION 664 BL 0 WL 207.5 TO WL 204 FLOORBEAM WEB. REMOVED DAMAGED AREA INSTALLED WEB REPAIR, REPAIRED PER BOEING DRAWING 65-C34537. (M)
- [SDR USAA980091](https://openairdocs.org/sdr/USAA980091.md): Floorbeam · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor Beam
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK.5 INCH LONG STATION 727 LBL 25 INCH FLOORBEAM LOWER CHORD. REPLACED SECTION OF LOWER CHORD, REPAIRED PER SRM 51-40-4. (M)
- [SDR USAA980090](https://openairdocs.org/sdr/USAA980090.md): Floorbeam · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor Beam
  > INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND SEVERAL.25 INCH CRACK LBL 25 LONGITUDINAL FLOORBEAM LOWER WEB STATION 707 TO STATION 714, WL 203.5. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-2, REPAIRED PER SRM 51-40-2. (M)
- [SDR USAA980089](https://openairdocs.org/sdr/USAA980089.md): Floorbeam · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor Beam
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK.5 INCH LONG STATION 707 TO STATION 714 RBL 25 LONG FLOORBEAM WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-2. (M)
- [SDR USAA980088](https://openairdocs.org/sdr/USAA980088.md): Skin · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.375 INCH CRACK AFT ENTRY GALLEY DOOR UPPER HINGE CUT OUT SKIN EXTERIOR. CUT OUT CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA980087](https://openairdocs.org/sdr/USAA980087.md): Skin · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND.5 INCH CRACK FORWARD ENTRY DOORWAY UPPER HINGE CUTOUT SKIN. CUTOUT CRACK AND INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-10-1, SRM 53-30-3, AND EA 43555. (M)
- [SDR USAA980086](https://openairdocs.org/sdr/USAA980086.md): Frame · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK.5 INCH AT STATION 328 STRINGER 20R FRAME. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-3. (M)
- [SDR USAA980085](https://openairdocs.org/sdr/USAA980085.md): Frame · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1.25 INCH LONG AFT ENTRANCE DOOR FRAME STATION 947 STRINGER 11L WEB (FRAME). INSTALLED DOUBLER ON EXISTING WEB, REPAIRED PR TR 53-30-07. (M)
- [SDR USAA980084](https://openairdocs.org/sdr/USAA980084.md): Blkhd Stiffener · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Bulkhead
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 LBL 5.75 AT WL 183.5 STIFFENER, BULKHEAD. DOUBLER AND STIFFENERS INSTALLED, REPAIRED PER TR 53-10-17. (M)
- [SDR USAA980083](https://openairdocs.org/sdr/USAA980083.md): Bulkhead · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Bulkhead
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK STATION 178 BULKHEAD LBL 5, WL 199. INSTALLED DOUBLER REPAIRED PER SRM 53-10-11. (M)
- [SDR USAA980082](https://openairdocs.org/sdr/USAA980082.md): Keel Beam · worn · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Keel
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND WORN HOLES, HOLES ELONGATED IN CHORD.09375 INCH STATION 695 TO STATION 727 LOWER CHORD (KEEL BEAM). SPOT FACED SCREW HOLES, HFEC INSPECTION INSTALLED STRAP, REPAIRED PER EA 43618 SRM 51-30-6. (M)
- [SDR USAA980081](https://openairdocs.org/sdr/USAA980081.md): Stringer · cracked · Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH CRACK AND.75 INCH CRACK BS 727 LEFT OUTBOARD CHORD STRINGER 18A L/S. CUTOUT AND SPLICED IN NEW SECTION OF STRINGER, REPAIRED EO 5394G068. (M)
- [SDR USAASB97338](https://openairdocs.org/sdr/USAASB97338.md): Garlock Seal · leaking/failed · Dec 10, 1997 · N254AU · Boeing 737201 · Turbine Engine Accessory Drive
  > MEM - FLT 1901 - CAPTAIN REPORTED THE NR 2 ENGINE OIL QUANTITY DROPPED DOWN TO 1 TO 1-1/2 GALLONS DURING FLIGHT. CAPTAIN DECIDED TO DIVERT TO MEM WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. THE NR 2 ENGINE WAS NOT SHUT DOWN IN-FLIGH
- [SDR USAA970321](https://openairdocs.org/sdr/USAA970321.md): Skin · cracked · Nov 6, 1997 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-2 CHECK VISUAL, VERIFIED WITH EDDY CURRENT INSPECTION FOUND 1.5 INCH CRACK IN SKIN STATION 378 WL 148.5. INSTALLED TEMPORARY REPAIR PER E/A 43288, PERMANENT REPAIR TO BE ACCOMPLISHED WITH IN THE NEXT 500 CYCLES OR NEXT Q-CHECK. REPAIRED PER E
- [SDR USAASB97232](https://openairdocs.org/sdr/USAASB97232.md): Wire · broken · Aug 23, 1997 · N254AU · Boeing 737201 · Light System Wiring
  > BWI - EMERGENCY FLOOR LIGHTING STAYS ILLUMINATED ALL THE TIME, ROW 15 TO LAST ROW. REPAIRED BROKEN WIRE AT ROW 16A. SYSTEM OPERATIONALLY CHECKED OK. (M)
- [SDR USAA970016](https://openairdocs.org/sdr/USAA970016.md): Skin · cracked · Jan 15, 1997 · N254AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK AT STATON 332.10 LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED DOUBLER PER EA, GENERATED OM-7 NR 13021 FOR FINAL REPAIR DUE IN 18 MONTHS OR 4500 CYCLES. REPAIRED PER EA 59266 A
- [SDR USAA970015](https://openairdocs.org/sdr/USAA970015.md): Stringer · corrosion · Jan 15, 1997 · N254AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCHES OF STRINGER 27L CORRODED AT STATION 947.5. INSTALLED STRINGER REPAIR PER SRM 53-10-3.(M)

Next page: https://openairdocs.org/deregistered/N254AU-2004-07-16/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 = 'N254AU' AND deregistration_id = 'N254AU-2004-07-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N254AU-2004-07-16/reports

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