N274US, cancelled Sep 25, 2003

Service difficulty reports · 46

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 = 'N274US' AND deregistration_id = 'N274US-2003-09-25'
  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 USAA990826Skin · crackedTPA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK ABOVE RIVET .125 INCH CRACK BELOW RIVET STRINGER 17R, WL STATION 344 SKIN. INSTALLED REPAIR DOUBLER PER SB 737-53-1083 FIG 3C. (M)Aug 7, 1999 · N274US · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99014Coalescer · dirtyFWA - FLT 1177 - EN ROUTE FROM BWI TO ORD AT FL310, ONE OF THE FLIGHT ATTENDANTS ADVISED THE COCKPIT CREW THAT THERE WERE FUMES IN THE CABIN AND THE FUMES WERE IRRITATING THE PASSENGERS. AN EMERGENCY DECLARED AND FLT DIVERT TO FWA. THE FUMES DISSIPATED ON DEJan 15, 1999 · N274US · Boeing 7372B7 · Humidity Control SystemSDR USAA980523Skin · crackedPIT - FOUND RON, FOUND 3 INCH CRACK IN SKIN AT STATION 767 .5 INCH ABOVE STRINGER NR 20. INSTALLED DOUBLER PER SRM 53-30-03. (M)Oct 15, 1998 · N274US · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980339Skin · crackedTPA - DURING CX-5 CHECK EDDY CURRENT, FOUND A .125 INCH CRACK IN OUTER SKIN AT LOWER CORNER OF AFT ENTRY DOOR, LOWER HINGE CUTOUT STATION 950.5 2.5 INCHES BELOW STRINGER 14L. ROUTED OUT CRACK AND REFINISHED AREA PER SRM 53-00-1 PAGE 102. (M)Aug 7, 1998 · N274US · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980338Skin · crackedTPA - DURING CX-5 CHECK EDDY CURRENT INSPECTION, FOUND A .5 INCH CRACK IN OUTER SKIN OF AFT ENTRY DOOR, LOWER AFT CORNER OF UPPER HINGE CUTOUT. ROUTED DAMAGE AND INSTALLED DOUBLER OF .071,2024-T3 PER SRM 52-10-01, 51-30-8 AND EA 62192. (M)Aug 7, 1998 · N274US · Boeing 7372B7 · Passenger/Crew DoorsSDR USAA980337Angle · crackedTPA - DURING CX-5 VISUAL INSPECTION, FOUND A 1 INCH CRACK IN ANGLE AT STATION 727 COMPRESSION CHORD RBL 25. INSTALLED DOUBLER PER TYPICAL REPAIR NR 53-10-03A PART 3. (M)Aug 7, 1998 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAASB98200Light · inoperativePHL - WHILE TESTING EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 9A WITHOUT A LENSE AND SMOKING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 9A. OPERATIONAL CHECK GOOD. (M)Jul 28, 1998 · N274US · Boeing 7372B7 · Emergency LightingSDR USAASB98111Battery Pack · dischargedALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT THE CENTER AISLE CEILING BETWEEN THE EXIT HATCHES INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)May 11, 1998 · N274US · Boeing 7372B7 · Emergency LightingSDR USAA960757Skin · crackedROA - DURING CX-3 CHECK, EDDY CURRENT INSPECTION FOUND .25 INCH CRACK IN A/C SKIN AT LOWER HINGE CUT OUT FORWARD ENTRY DOOR. BODY STA 302 - JUST ABOVE STR 13L. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-30-11. (X)Nov 27, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB96214Fuel Control · malfunctionedEVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW Oct 21, 1996 · N274US · Boeing 7372B7 · Fuel Control/Turbine EnginesSDR 96ZZZM1487Fuel Pump · malfunctionedEVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW Oct 21, 1996 · N274US · Boeing 7372B7 · Engine Fuel PumpSDR USAASB96039Filter Bypass Sw · intermittentFLT NR 797 - MCO - FIVE MINUTES AFTER TAKEOFF, 'OIL FILTER BYPASS' LIGHT FOR NR 1 ENGINE CAME ON. RETARDED THROTTLES, NO HELP. SHUT DOWN ENGINE AND RETURNED TO MCO. MAINTENANCE REPLACED THE FILTER BYPASS SWITCH. (M)Mar 2, 1996 · N274US · Boeing 7372B7 · Engine Oil Indicating SystemSDR USAA960240Fitting · crackedINT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A RIGHT. INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 POUND. REPAIRED PER EA 40644. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960239Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 4 INCH CORRODED WEB AFT ENTRY DOOR Z-ANGLE THRESHOLD WEB. FABRICATED NEW WEB, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-52878. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960238Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION Z-ANGLE AFT ENTRY DOOR. REPLACED WITH IDENTICAL PART NR 65-52878-533, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960237Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED NUT PLATE HOLES 3 FLOOR BEAM, STATION 986.5 RBL 36, LBL 5, RBL 5. INSTALLED DOUBLERS, REPAIR PER SRM 53-10-9 FIG 7. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960236Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE AT STATIO N967 TO 947 RBL 20. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65-46812. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960235Floor Beam · gougedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGE APPROXIMATELY 22 INCHES FLOOR BEAM BS 312, LBL 12 INCHES TO RBL 10 INCHES. CUT OUT DAMAGED AREA AND INSTALLED NEW SECTION WITH REPAIR ANGLES. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROFeb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960234Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORRODED AREA ON SIDE OF STRINGER BS 351.2 - BS 380, STRINGER 28L. REPLACED STRINGER SECTION REPAIRED PER SRM 51-10-1, PAGE 5, STEP 4. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA960233Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM UPPER T-CAP BS 1016 LBL 3 INCHES. INSTALLED T-CAP, REPAIR PLUS 2.6 LB WT CHANGE, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960232Seat Track · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR SEAT TRACK BETWEEN STATION 1016 AND STATION 986.5. INSTALLED NEW SEAT TRACK SECTION, REPAIRED PER SRM 51-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA960231Floor Support · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION 8 INCH FLOOR SUPPORT INTERCOSTAL STATION 986.5 LNL 15 INCHES. REPLACED WITH IDENTICAL PART NR 65-46812-191, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960230Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR BEAM STATION 1006, LBL 11 INCHES. SPLICED IN NEW SECTION OF FLOOR BEAM, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960229Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION INTERCOSTAL STATION 1006 - 986.5 '0' BL. REPLACED WITH INDENTICAL PART NR 65-46812-170, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960228Intercostal · corrosionINT - DURING Q-6 CHCK VISUAL INSPECTION, FOUND TWO CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH, INTERCOSTAL LBL 10 INCHES BETWEEN BS 328 AND BS 344. REPLACED WITH IDENTICAL PART NR 65-45834-259, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROFeb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960227Intercostal · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA INTERCOSTAL LBL 11 INCHES BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PART NR 65-45834-260, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960226Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREAS, APPROXIMATELY 1 INCH BY 1 INCH AT INTERCOSTAL, RBL 10 INCH BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PART NR 1137215, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROFeb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960225Floor Beam · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM 'T' CAP CABIN BS 294.5 LBL 10 INCHES, RBL 20. CUT AND REPLACED T-CAP, LESS THAN 1 LB WEIGHT CHANGE, REPAIRED PER TR 53-10-04B. CORROSION TASK NR C53-107-02, CORROSION LFeb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960224Intercostal · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CORRODED AREAS APPROXIMATELY 2 INCHES BY 2 INCHES INTERCOSTAL, BS 297 AND BS 303 LBL 12. INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960223Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA 4 PLACES INTERCOSTAL, BS 344 TO BS 360 RBL 11. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960222Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA AT INTERCOSTAL BS 292 LBL 12 INCHES. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960221Intercostal · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH ON INTERCOSTAL, RBL 10 INCHES BETWEEN BS 294.5 AND BS 312. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45834. CORROSION TASK NR C53-107-0Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960220Angle · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES 'Z' ANGLE BS 294.5 TO BS 344 RBL 56. REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45875. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960219Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 CORRODED AREAS AT CLIP NUT HOLES APPROXIMATELY 1 INCH BY 1 INCH BS 306 TO BS 345 LBL 48 'A' ANGLE LEFT ENTRANCE DOOR. REMOVED AND INSTALLED NEW PART, REPAIRED PER SRM 51-10-1 PAGE 5. CORROSION TASK NR C53-107Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960218Intercostal · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES BS 312 TO BS 328 RBL 11 INTERCOSTAL. REMOVED AND INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1 PAGE 5. CORROSION TASK NR C53-107-02, CORROSION LEVEL Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960217Blkhd Fitting · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 727 BULKHEAD STIFFENER FITTING AT BL 0 WL 202.5. REMOVED CRACKED FITTING, INSTALLED NEW ONE, REPAIRED PER EO 5394G176. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, BulkheadSDR USAA960216Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TOP FLANGE OF FRAME STATION 807 LEFT BETWEEN STRINGER 24 AND STRINGER 25. CUT OUT CRACK, FABRICATED FILLER AND REPAIRED DOUBLER PER SRM 51-40-3. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, FrameSDR USAA960213Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED FLOOR SUPPORT ANGLE STATION 986.5 TO 967 LBL 12. REPLACED ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR 53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960212Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH FLOOR SUPPORT ANGLE CORROSION STATION 967 TO 947 RBL 6. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65C10592-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960211Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCH CORROSION FLOOR BEAM STATION 967 BL 0 TO LBL 45. INSTALLED ONE DUOBLER AT LBL 42, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960210Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 11 INCH BY 40 INCH CORROSION FLOOR SUPPORT ANGLE AT STATION 957 RBL 6 TO RBL 45. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65-C10592-5 OR 6. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960209Angle · crackedINT - DURING Q-6 CHECK VISUAL EDDY CURRENT INSPECTION, FOUND 1 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A LEFT. INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 LB, REPAIRED PER EA 40644. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960208Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 2 INCH CORRODED FLOOR BEAM AREA AND AT ALL CLIPNUT HOLES BS 328 RBL 6 TO RBL 56. INSTALLED NEW T-CAP AND DOUBLERS, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA960207Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE, STATION 967 TO STATION 947 RBL 45, REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65C10592-4. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960206Angle · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION AT FLOOR BEAM SUPPORT ANGLE STATION 967 TO 947 LBL 12. REPLACED WITH IDENTICAL PART NR 65-46812-170 AND ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVELFeb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA960205Floor Beam · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCHES CORROSION STATION 967 BL 0 TO RBL 45 FLOOR BEAM. CUTOFF TOP CAP, FABRICATED AND REPAIRED SPLICE AND INSTALLED PER SRM 53-10-9 FIG 2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Feb 7, 1996 · N274US · Boeing 7372B7 · Fuselage Main, Floor Beam
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