N234US, cancelled Dec 6, 2004

Service difficulty reports · 41

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 = 'N234US' AND deregistration_id = 'N234US-2004-12-06'
  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 USAA001879Skin · crackedCLT - FOUND SKIN CRACKED 1.6 INCH, RT FUSE STATION 944 AT STRINGER 24R. INSTALLED DOUBLER PER SRM 53-30-03 FIG 6. (M)Nov 7, 2000 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00305Charger · failedTPA - MAINTENANCE FOUND TWO FORWARD CABIN/ENTRY DOOR SECTIONS OF EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY IN THE OVERHEAD BIN NEAR SEAT ROW 1 AND THE POWER SUPPLY (P/N 60-1321-1)Oct 29, 2000 · N234US · Boeing 737201 · Emergency LightingSDR USAASB00130Charger · failedALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN ON THE CEILING IN THE FIRST CLASS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 9008-3-5A) AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Apr 29, 2000 · N234US · Boeing 737201 · Emergency LightingSDR USAA000262Skin · crackedSKIN HAS A 1 INCH CRACK AT 490 STRINGER 24. INSTALLED REPAIR DOUBLER, TRIPLER AND QUADRUPLER PER EA 54235. (M)Feb 24, 2000 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000263Skin · crackedSKIN HAS A 2.5 INCH CRACK AT BS 980, STRINGER 21L. INSTALLED DOUBLER PER SRM 53-303 FIG 1. (M)Feb 24, 2000 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB99243Wire · brokenTPA - MAINTENANCE FOUND THE AISEL EMERGENCY LIGHT AT SEAT ROW 12C INOPERATIVE. MAINTENANCE REPAIRED TWO BROKEN WIRES AT SEAT ROW 12C. OPERATIONAL CHECK GOOD. (M)Oct 2, 1999 · N234US · Boeing 737201 · Light System WiringSDR USAASB98172Battery Pack · dischargedALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY EVACUATION LIGHTS INOP, LEFT OVERWING EXIT HATCH SIDEWALL EXIT LIGHT, THE LEFT OUTSIDE EXIT HATCH WING LIGHT AND THE LEFT GRUOND ILLUMINATION LIGHTS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT Jul 6, 1998 · N234US · Boeing 737201 · Emergency LightingSDR USAASB98143Accessory Unit · failedBUF - FLT 461 - AFTER TAKEOFF FROM BUF, LANDING GEAR FAILED TO RETRACT. FLIGHT RETURNED TO FIELD AT BUF AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPERATIONAL CHECK GOOD. PERFOJun 7, 1998 · N234US · Boeing 737201 · Landing Gear Position and WarningSDR USAASB98132Light · inoperativeALB - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FLIGHT DECK EMERGENCY EVACUATION EXIT LIGHT IN THE CEILING TO BE INOPERABLE WHEN SWITCHED ON FROM THE OVERHEAD PANEL. LIGHT OPERATES NORMALLY WHEN SWITCHED ON AT EXIT LIGHT BATTERY PACK. MAINTENANCE REMOVEDJun 1, 1998 · N234US · Boeing 737201 · Emergency LightingSDR USAA980040Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FLOORBEAM BS 520, RBL 24. INSTALLED DOUBLER AND MOD REPAIRED PER EA 43461. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980039Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 20 INCHES BS 907-927 STRINGER 25L. INSTALLED STRINGER REPAIR SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980038Skin · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 5 INCH SKIN BULGED FUSELAGE SKIN BS 727, STRINGER 27L, STRINGER 27R BELLY. INSTALLED DOUBLER AND FILLERS, REPAIRED PER SRM 53-30-3 FIG 1. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980037Chord · crackedINT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK BS 727 RT STRINGER 18A FORWARD FASTENER HOLE CRACKED FORWARD FLANGE OF OUTBOARD CHORD. INSTALLED CHORD KIT, REPAIRED PER EA 5394GO68 CARD NR 2-21-93834. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980036Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CRACKS, .5 INCH AND 1.5 INCHES LONG AT BS 520 RBL 45 FLOORBEAM. INSTALLED KIT, REPAIRED PER EA 43461. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980035Bulkhead Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 LBL 4.5 AT LOWER LEFT ANT MOUNT BULKHEAD WEB. STOP DRILLED, NDT INSPECTION AND INSTALLED FILLERS AND DOUBLER PER TR 53-10-11. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980034Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK FORWARD DOOR FRAME AT UPPER HINGE CUTOUT. STOP DRILLED CRACK, NDT INSPECTION, INSTALLED REPAIR DOUBLER, REPIRED PER SRM 51-40-3 FIG 1. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980033Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 520, LBL 24 FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER EA 43461. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980032Frame · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 990 WL 208 STRINGER 17R FRAME. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-07, CORROSION LEVEL 2. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, FrameSDR USAA980031Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA BS 344 TO BS 348 STRINGER 25L. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980030Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 7 INCH CRACK, TWO 3.5 INCH CRACKS IN FUSELAGE SKIN AT BS 727 A PLUS 3, TO BS 727B BETWEEN STRINGER 18 AND STRINGER 19 ON LEFT SIDE. INSTALLED DOUBLER, REPAIRED PR SRM 53-30-3. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980029Spar Lug · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVEIS LUG BORE LEFT HORIZONTAL LOWER STABILIZER. INSTALLED OVERSIZED BUSHINGS, REPAIRED PER EA 43494. (M)Jan 23, 1998 · N234US · Boeing 737201 · Horizontal Stabilizer, Spar/RibSDR USAA980028Spar Lug · corrodedINT - DUIRNG Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVIS LUG BORE RT LOWER HORIZONTAL STABILIZER. INSTALLED OVERSIZED BUSHINGS, REPAIRED PER EA 43494. (M)Jan 23, 1998 · N234US · Boeing 737201 · Horizontal Stabilizer, Spar/RibSDR USAA980027Clip · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED AREA E/E BS 345 TO BS 363 STRINGER AND TIE CLIP. INSTALLED STRINGER SPLICE REPAIR AND REPLACED TIE CLIP PER DRAWING 69-46831-1 AND SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980026Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH AFT SERVICE DOOR CUTOUT UPPER HINGE, UPPER FORWARD END SKIN. INSTALLED DOUBLERS, REPAIRED PER EA 43495. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980025Skin · damagedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND PREVIOUS DOUBLER STATION 947 STRINGER 20L TO STRINGER 21L SKIN. INSTALLED EXT SKIN REPAIR, REPAIRED PER EA 43493. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980024Spar · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY .125 INCH CORRODED AREA RT HORIZONTAL STABILIZER UPPER OUTBOARD REAR SPAR TERMINAL LUG. INSTALLED OVERSIZED BUSHING, REPAIRED PER EA 43472. (M)Jan 23, 1998 · N234US · Boeing 737201 · Horizontal Stabilizer, Spar/RibSDR USAA980023Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 1 INCH CORRODED AREA BS 907 - BS 927, S27R STRINGER. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980022Frame · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 2 INCH AREA OF CORROSION LOWER CHORD OF FRAME AT STATION 787 LEFT KEEL BEAM. INSTALLED REPAIR DOUBLER AND ATTACH ANGLES, REPAIRED PER SRM 53-10-4, FIG 9. CORROSION TASK NR C53-208-01, CORROSIONJan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, FrameSDR USAA980021Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION FOUND APPROX 2 INCH BY 2 INCH AREA CORRODED STRINGER 25L AT STATION 968. INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980020Spar · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVIS LUG BORE RT HORIZONTAL UPPER STABILIZER. INSTALLED OVERSIZED BUSHING, REPAIRED PER 43494. (M)Jan 23, 1998 · N234US · Boeing 737201 · Horizontal Stabilizer, Spar/RibSDR USAA980019Spar · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION SPAR CLEVIS LUG LEFT UPPER HORIZONTAL STABILIZER. INSTALLED OVERSIZED BUSHING, REPAIRED PER EA 43494. (M)Jan 23, 1998 · N234US · Boeing 737201 · Horizontal Stabilizer, Spar/RibSDR USAA970276Skin · tornGSO - DURING "UNSCHEDULED MAINTENANCE CHANGE' VISUAL INSPECTION FOUND 1 INCH BY 1 INCH PIECE OF SKIN TORN AWAY, LEFT AFT ENTRY DOOR SKIN ABOVE LOWER HINGE CUTOUT. INSTALLED DOUBLER, REPAIRED PER SRM 52-00-3, FIG 5. (M)Aug 27, 1997 · N234US · Boeing 737201 · Passenger/Crew DoorsSDR USAASB97143Battery Pack · dischargedGSO - MAINTENANCE FOUND THE AFT SERVICE DOOR AND THE AFT ENTRY DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)May 29, 1997 · N234US · Boeing 737201 · Emergency LightingSDR USAASB97020Battery Pack · dischargedROA - MAINTENANCE FOUND THE AFT ENTRY DOOR INTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)Jan 19, 1997 · N234US · Boeing 737201 · Emergency LightingSDR 97ZZZM214Power Supply · inoperativeROA - MAINTENANCE FOUND THE AFT ENTRY DOOR INTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)Jan 19, 1997 · N234US · Boeing 737201 · Emergency LightingSDR USAASB97019Bypass Switch · failedPIT - FL 1261 - ON CLIMB-OUT OF PIT, THE OIL FILTER BYPASS LIGHT FOR THE NR 1 ENGINE ILLUMINATED AT APPROX 11,000 FEET. THE CAPT SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT PIT. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.Jan 17, 1997 · N234US · Boeing 737201 · Engine Oil Indicating SystemSDR USAA960369Stringer · crackedINT - DURING 'DROP-IN' CHECK VISUAL PCI INSPECTION, FOUND 2.2 INCH CRACK, STATION 706 STRINGER 18A RIGHT. INSTALLED REPAIR, REPAIRED PER EA 41018. (M)Mar 22, 1996 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB96018Aux Power Unit · failedFLT NR 1184 - BWI - ON FINAL APPROACH APU FIRE WARNING MOMENTARILY WENT OFF. FIRED FIRE BOTTLE. MAINTENANCE REPLACED THE APU. (M)Jan 22, 1996 · N234US · Boeing 737201 · Airborne Auxiliary Power Unit (APU) SystemSDR USAA960195Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 27L, BS 786.5 TO BS 1016. INSTALLED STRINGER SPLICES, REPAIRED PER SRM 53-10-3. (M)Jan 3, 1996 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB95029Fuel Control · failedFLT NR 8582 - RSW - AFTER SECOND APU START ATTEMPT APU FIRE LIGHT ILLUMINATED APU FIRE SWITCH PULLED AND BOTTLE DISCHARGED. REMOVED AND REPLACED THE APU FCU. ADJUSTED CRACK PRESSURE. CLEANED SHROUD DRAINS. REPLACED IGNITOR LEADS. APU OPS NORMALLY. (M)Dec 16, 1995 · N234US · Boeing 737201 · APU Engine Fuel and ControlSDR USAA950642Actuator · failedBWI - FLT 1120 - UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR ACTUATOR. (W)Jun 18, 1995 · N234US · Boeing 737201 · Landing Gear Actuator
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