N228US, cancelled Jan 31, 2001

Service difficulty reports · 36

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 = 'N228US' AND deregistration_id = 'N228US-2001-01-31'
  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 USAA001205Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, LEFT FUSE EXT SKIN STATION 766, STRINGER 18L. INSTALLED DOUBLER PER EA 67770. (M)Aug 7, 2000 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000833Skin · crackedTPA - FOUND DOOR EXT SKIN CRACKED 1.75 INCH, AFT ENTRY DOOR FWD LOWER CORNER. INSTALLED DOUBLER PER SRM 52-10-1. (M)Jun 13, 2000 · N228US · Boeing 737201 · Passenger/Crew DoorsSDR USAASB00144Connector · dirtyCLT - WHILE A/C WAS ON THE GROUND, PILOT REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED MOMENTARILY AND EXTINGUISHED ON THEIR OWN. HOWEVER, DURING FLT, THE EMERGENCY EXIT LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH UNLESS LIGHT SWITCH WAS TURNED OFF. MX CYCLMay 17, 2000 · N228US · Boeing 737201 · Emergency LightingSDR USAA000309Skin · crackedCLT - FOUND TWO CRACKS, 3.5 INCH AND 1 INCH, LT FUSE EXT STATION 759-763 AND STATION 780-781 STRINGER 17L. REPAIRED PER EA 66792. (M)Mar 6, 2000 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00007Bulb · faultyPHL - FLT 1223 - DURING DESCENT INTO PHL, BOTH MASTER CAUTION FIRE WARNING LIGHTS ILLUMINATED FOR APPROXIMATELY FIVE SECONDS. NO OTHER LIGHTS OR BELLS WERE NOTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS IN THJan 8, 2000 · N228US · Boeing 737201 · Fire DetectionSDR USAA991383Skin · crackedTPA - DURING CX-3 CHECK, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727A PLUS 8 AT STRINGER 18R. INSTALLED REPAIR DOUBLER PER SRM, DOUBLE MADE FROM 2024-T3 .071 PER SRM 53-30-3 FIG 6. (M)Nov 24, 1999 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB99110Power Supply · inoperativeCLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FOUND THE INTERIOR LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD.Apr 26, 1999 · N228US · Boeing 737201 · Emergency LightingSDR 99ZZZM358Battery Pack · dischargedCLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FOUND THE INTERIOR LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD.Apr 26, 1999 · N228US · Boeing 737201 · Emergency LightingSDR USAA980625Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 1.1 INCH CRACK IN EXTERNAL SKIN .5 INCH ABOVE STRINGER 18R AT STATION 754 SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Dec 2, 1998 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980404Skin · crackedCLT - DURING RON CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK OUT OF FORWARD EDGE OF EQUIPMENT COOLING DUCT CUT OUT STA 368 ON SKIN. INSTALLED DOUBLER PER TR 53-30-04 DRAWING 65C33930. (X)Sep 12, 1998 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980403Skin · crackedCLT - DURING RON CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND APPROXIMATELY .75 INCH CRACK FUSELAGE SKIN STA 727A JUST ABOVE STR 16R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (X)Sep 12, 1998 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98001Battery · failedALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE AFT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPS CHECK GOOD. (M)Jan 2, 1998 · N228US · Boeing 737201 · Emergency LightingSDR USAA970364Floorbeam · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 947 LBL 41 TO LBL 48. INSTALLED BEAM SPLICE, REPAIRED EPR TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M)Dec 7, 1997 · N228US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA970363Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN CREASE BEAM WEB BS 637 LBL 71, WL 208. INSTALLED NEW WEB PER SRM 51-10-1. (M)Dec 7, 1997 · N228US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA970362Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 360 2 INCH ABOVE STRINGER 20R FRAME. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-2 AND SRM 51-40-3. (M)Dec 7, 1997 · N228US · Boeing 737201 · Fuselage Main, FrameSDR USAA970361Stringer · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 370 STRINGER 27R ON SIDE OF STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3 FIG 1. CORROSION TASK NR C53-202-01, CORRSION LEVEL 1. (M)Dec 7, 1997 · N228US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA970360Skin · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND BULGE IN 2 PLACES LOWER FUSELAGE SKIN BS 727 PLUS 16 INCHES, 6 INCHES LBL AND 6 INCHES RBL. INSTALLED DOUBLER, REPAIRED PER SRM53-30-3 FIG 6. (M)Dec 7, 1997 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970359Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 328 FRAME 2 INCH BELOW STRINGER 20R. INSTALLED DOUBLER AND FILLER, REPAIRED PER SRM 51-40-2. (M)Dec 7, 1997 · N228US · Boeing 737201 · Fuselage Main, FrameSDR USAA970358Floorbeam · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 22 INCH BY 1 INCH STATION 259, LBL 11 TO RBL 11 FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER TR 53-10-16. (M)Dec 7, 1997 · N228US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA970245Skin · crackedROA - DURING CX-6 CHECK VISUAL INSPECTION, FUOND 1.75 INCH CRACK BS 792 STRINGER 18L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)Jul 31, 1997 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970244Skin · crackedROA - DURING CX-6 VISUAL/EDDY CURRENT INSPECTION, FOUND 1.25 INCH CRACK BS 747 STRINGER 18L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Jul 31, 1997 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA970243Skin · crackedROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK AND .25 INCH CRACK BS 727A PLUS 8 INCHES STRINGER 18L FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Jul 31, 1997 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97017Heat Manifold · failedTPA - FL 232, FLIGHT WAS CLIMBING THRU 12,000 FT WHEN THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPT RETARDED THROTTLE AND THE LGIHT WENT OUT. ADVANCED THROTTLE AND THE LIGHT ILLUMINATED AGAIN. CAPT DECIDED TO RETURN TO FIELD AT TPA. NO EMERGENCY WAS DECLJan 15, 1997 · N228US · Boeing 737201 · Engine Anti-Icing SystemSDR 97ZZZM223Anti-Ice Tube · failedTPA - FL 232, FLIGHT WAS CLIMBING THRU 12,000 FT WHEN THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPT RETARDED THROTTLE AND THE LGIHT WENT OUT. ADVANCED THROTTLE AND THE LIGHT ILLUMINATED AGAIN. CAPT DECIDED TO RETURN TO FIELD AT TPA. NO EMERGENCY WAS DECLJan 15, 1997 · N228US · Boeing 737201 · Engine Anti-Icing SystemSDR USAASB96225Connector · looseRSW - FL 1429 - ON APPROACH TO RSW, CREW RECEIVED THE FIRE WARNING FOR THE NR 2 ENGINE. CREW SHUT DOWN ENGINE AND FIRED BOTH BOTTLES. FLIGHT LANDED AT RSW WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO EVIDENCE OF FIRE. THE D1096 CNov 8, 1996 · N228US · Boeing 737201 · Fire DetectionSDR USAA960688Skin · crackedROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 1.375 INCH CRACK AFT GALLEY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17 R BS 857) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 24, EA 58949. (M)Oct 21, 1996 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960687Skin · crackedROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2 CRACKS 3.1875 INCH AND .5 INCH FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17R BS 328) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 26. (M)Oct 21, 1996 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960468Stringer · corrosionROA - DURING 'BX TRANSIT' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION STRINGER 27L BS 986.5. INSTALLED DOUBLER AND STRINGER, REPAIRED PER SRM 53-10-3. (M)Jun 1, 1996 · N228US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960467Skin · crackedROA - DURING 'TRANSIT CHECK' VISUAL INSPECTION VERIFIED WITH HFEC, FOUND TWO .75 INCH CRACK IN FUSELAGE SKIN JUST ABOVE STRINGER 18L, FORWARD OF BS 787. INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 53-30-3 FIG 6. (M)Jun 1, 1996 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA960014Shear Beam · crackedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM WEB AT BS 706. INSTALLED DOUBLER. REPAIRED PER EO 5393G259 REV 'A' 11/01/95. (M)Jan 4, 1996 · N228US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960013Shear Beam · crackedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND ONE .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM AT BS 727. INSTALLED DOUBLER. REPAIRED PER EO 5393G256 REV 'A' 11/01/95. (M)Jan 4, 1996 · N228US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA951334Skin · delaminationINT - DURING 'TRANSIT CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 RHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M)Dec 15, 1995 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951333Skin · delaminationINT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M)Dec 15, 1995 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA951332Skin · delaminationINT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 360-540 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M)Dec 15, 1995 · N228US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA950614Strap · looseEWR - FLT 371 - LOUD BANGING NOISE ON CLIMB-OUT. WARNING STRAP CAUGHT IN FORWARD GALLEY SERVICE DOOR. FLIGHT RETURNED TO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED STRAP FROM FORWARD GALLEY SERVICE DOOR. INSPECTED DOOR AND FUSELAGEJun 19, 1995 · N228US · Boeing 737201 · Galley DoorsSDR USAA950596R/T Unit · failedCLT - FLT 97 - FLIGHT EN ROUTE PIT TO MIA WHEN RADAR QUIT WORKING. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED R/T UNIT. RADAR WORKED NORMAL. (M)Jun 4, 1995 · N228US · Boeing 737201 · Weather Radar System
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