N254AU, cancelled Jul 16, 2004

Service difficulty reports · 58

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAASB01301Battery · dischargedBSI - THE EMERGENCY LIGHT ABOVE THE 1R EXIT FLASHES ON AND OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Oct 21, 2001 · N254AU · Boeing 737201 · Emergency LightingSDR USAASB01289Power Supply · dischargedLGA - THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT POWER SUPPLY. (M)Oct 10, 2001 · N254AU · Boeing 737201 · Emergency LightingSDR USAASB01226Wire · brokenBDL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING. OPERATIONAL CHECK NORMAL. (M)Aug 8, 2001 · N254AU · Boeing 737201 · Light System WiringSDR USAA010757Keelbeam · corrodedCLT - 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)Jun 22, 2001 · N254AU · Boeing 737201 · Fuselage Main, KeelSDR USAA010764Keelbeam · corrodedTPA - 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)Jun 20, 2001 · N254AU · Boeing 737201 · Fuselage Main, KeelSDR USAA010765Stringer · corrodedCLT - FOUDN STRINGER CORRODED 10 SQUARE INCHES, BS 967, STRINGER 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-3, FIG 1. (M)Jun 19, 2001 · N254AU · Boeing 737201 · Fuselage Structure (General)SDR USAA010748Stringer · corrodedTPA - 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)Jun 19, 2001 · N254AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA010749Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, AFT OF STATION 907 STRINGER 18L. INSTALLED DOUBLER PER EA 71383 AND SRM 53-00-01 FIG 223. (M)Jun 18, 2001 · N254AU · Boeing 737201 · Fuselage Structure (General)SDR USAA010766Skin · crackedTPA - FOUND SKIN CRACKED 1 INCH, BS 907, STRINGER 18L. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER SRM 53-00-01, AND EA 7183. (M)Jun 17, 2001 · N254AU · Boeing 737201 · Fuselage Structure (General)SDR USAASB01032Compressor · stalledCLT - 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 AFeb 1, 2001 · N254AU · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAASB00133Actuator · failedIAD - 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 May 5, 2000 · N254AU · Boeing 737201 · Leading Edge Slat ActuatorSDR USAASB00036Charger · failedCLE - 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 CHEFeb 9, 2000 · N254AU · Boeing 737201 · Emergency LightingSDR USAA000112Skin · crackedCLT - AFTER ENTRY DOOR LOWER FORWARD SKIN HAS A 1.5 INCH CRACK. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 24.. (M)Jan 27, 2000 · N254AU · Boeing 737201 · Passenger/Crew DoorsSDR USAA991048Skin · crackedTPA - 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)Oct 7, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA991045Skin · crackedTPA - 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)Oct 7, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990947Skin · crackedBOS - 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)Sep 1, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990946Skin · crackedBOS - 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)Sep 1, 1999 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB99144Valve · failedBWI - 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. Jun 14, 1999 · N254AU · Boeing 737201 · APU Bleed Air SystemSDR 99ZZZM393Oil Cooler · failedBWI - 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. Jun 14, 1999 · N254AU · Boeing 737201 · Engine Oil CoolerSDR 99ZZZM392Csd · failedBWI - 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. Jun 14, 1999 · N254AU · Boeing 737201 · Alternator-Generator DriveSDR USAASB99033Pcu · failedBWI - 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 Feb 8, 1999 · N254AU · Boeing 737201 · Elevator Control SystemSDR USAA980682Skin · crackedTPA - 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)Dec 27, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98316Csd · overservicedPIT - 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. MAINTENNov 29, 1998 · N254AU · Boeing 737201 · Alternator-Generator DriveSDR USAASB98314Engine · fodBWI - 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 EMERGENov 24, 1998 · N254AU · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAASB98163Shut Off Valve · failedPIT - 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 LAJun 30, 1998 · N254AU · Boeing 737201 · Pneumatic Distribution SystemSDR USAASB98109Coalescer Bag · dirtyGSO - 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 WITHOUMay 9, 1998 · N254AU · Boeing 737201 · Humidity Control SystemSDR USAA980099Skin · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980098Spar Web · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Wing SparSDR USAA980097Skin · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980096Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH AT STATION 747 STRINGER REPAIR, REPAIRED PER 53-10-3. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980095Bulkhead · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980094Frame · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980093Frame · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980092Floorbeam · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980091Floorbeam · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980090Floorbeam · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980089Floorbeam · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980088Skin · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980087Skin · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980086Frame · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980085Frame · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980084Blkhd Stiffener · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980083Bulkhead · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980082Keel Beam · wornINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, KeelSDR USAA980081Stringer · crackedINT - 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)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB97338Garlock Seal · leaking/failedMEM - 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-FLIGHDec 10, 1997 · N254AU · Boeing 737201 · Turbine Engine Accessory DriveSDR USAA970321Skin · crackedROA - 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 ENov 6, 1997 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97232Wire · brokenBWI - EMERGENCY FLOOR LIGHTING STAYS ILLUMINATED ALL THE TIME, ROW 15 TO LAST ROW. REPAIRED BROKEN WIRE AT ROW 16A. SYSTEM OPERATIONALLY CHECKED OK. (M)Aug 23, 1997 · N254AU · Boeing 737201 · Light System WiringSDR USAA970016Skin · crackedROA - 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 AJan 15, 1997 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970015Stringer · corrosionROA - 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)Jan 15, 1997 · N254AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
Back to N254AU, cancelled Jul 16, 2004