N224US

Service difficulty reports not matched to an aircraft · 43

They name N224US, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N224US' AND registry_match IS NULL
  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 USAA000664Skin · crackedTPA - FOUND SKIN CRACKED .25 INCH, AFT ENTRY DOOR UPPER HINGE CUTOUT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 21A. (M)May 4, 2000 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000649Skin · crackedTPA - FOUND SKIN CRACKED 1.24 INCH AND 1.7 INCH, BS 727A PLUS 3 INCHES, STRINGER 18L AND BS 727A PLUS 2 INCHES. INSTALLED DOUBLER PER SRM 53-30-3. (M)May 1, 2000 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA000648Skin · crackedTPA - FOUND SKIN CRACKED 1.25 INCH, STATION 727A PLUS 6 INCHES, STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3. (M)May 1, 2000 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB00103Charger · failedBNA - PILOT REPORTED THAT THE EMERGENCY PATH LIGHTS ILLUMINATED ON 4 ROWS IN THE CABIN. MAINTENANCE CYCLED CIRCUIT BREAKERS FOR TR1, 2 AND 3. OPERATIONAL CHECK GOOD. CLT - PILOT REPORTED THE NEXT DAY (4-5-00) THAT THE FLOOR PROXIMITY EMERGENCY LIGHTS ILLUMIApr 4, 2000 · N224US · Boeing 737201 · Emergency LightingSDR USAASB00100Battery Pack · inoperativePHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT OVER THE FIRST CLASS SECTION IS FLASHING. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY PACK AT SEAT ROW 2. OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM GOOD. (X)Mar 27, 2000 · N224US · Boeing 737201 · Emergency LightingSDR USAA000191Skin · crackedCLT - FOUND SKIN WITH 1 INCH CRACK, BS 755, STRINGER 18R, RT FUSELAGE SKIN. CUTOUT DAMAGE AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 1. (M)Feb 11, 2000 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB99273Power Supply · failedCLT - PILOT REPORTED THAT THE EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY WITH SWITCH IN AUTO POSITION OR OFF POSITION. MAINTENANCE FOUND THE AFT FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH STICKING. REPLACED SAME. OPS CHECK NORMAL. BUF, PILOT REPORTED LATER INNov 18, 1999 · N224US · Boeing 737201 · Emergency LightingSDR USAA990139Skin · crackedCLT - DURING DROP IN VISUAL INSPECTION, FOUND A 2 INCH CRACK IN FUSELAGE SKIN BS 727A PLUS 19 INCHES S18R. INSTALLED DOUBLER PER SRM 53-30-03. (M)Feb 25, 1999 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98276Servo · failedCLT - FLT 357 - DURING CRUISE AT FL330 WITH AUTOTHROTTLE ENGAGED, NR 1 THROTTLE BEGAN MOVING 1 OR 2 INCHES IN EITHER DIRECTIONS. POWER WAS CHANGING WITH THROTTLE MOVEMENT. CAPT DISCONNECTED AUTOTHROTTLE AND NR 1 THRUST LEVER BECAME FROZEN AT CRUISE POWER. NOct 19, 1998 · N224US · Boeing 737201 · Auto Throttle SystemSDR USAA980415Skin · crackedCLT - DURING RON CHECK VISUAL WITH EDDY CURRENT INSPECTION, VERIFIED A 2 INCH CRACK ON SKIN STA 787 BETWEEN STR 22L AND STR 23L. INSTALLED NEW FILLER AND DOUBLER PER SRM 53-30-3. (X)Sep 16, 1998 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980397Skin · crackedPIT - DURING UNSCHEDULED MAINTENANCE, FOUND 3.75 INCH CRACK ON SKIN BETWEEN STATION 771 AND 775 2 INCH ABOVE STRINGER 17L. FOUND 5.5 INCH CRACK ON SKIN BETWEEN STATION 760 AND 766 2 INCH ABOVE STRINGER 17L. VISUALLY DETECTED AND CONFIRMED BY EDDY CURRENT. ISep 5, 1998 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98180Light · inoperativeALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT IN THE COCKPIT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Jul 12, 1998 · N224US · Boeing 737201 · Emergency LightingSDR USAA980173Skin · crackedCLT - DURING PILOTS REPORT A 2.75 INCH CRACK WAS FOUND IN THE SKIN BS 759-761.75 STRINGER 24L. INSTALLED FILLER AND DOUBLER PER REPAIR DOCUMENT SRM 53-30-3 FIG 17. (M)Apr 23, 1998 · N224US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB97329Battery Pack · dischargedPHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTING AT THE AFT ENTRY AND AFT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Nov 26, 1997 · N224US · Boeing 737201 · Emergency LightingSDR USAASB97292Battery Pack · dischargedLGA - AFT SERVICE AND ENTRY DOOR EMERGENCY LIGHT EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY CHARGING UNIT. OPERATIONAL CHECK GOOD. (M)Oct 20, 1997 · N224US · Boeing 737201 · Emergency LightingSDR USAASB97260Battery Pack · dischargedTPA - AFT EXTERIOR ESCAPE LIGHTS AT R2 AND L2 DOORS ARE INOPERATIVE. MAINTENANCE REPLACED THE LEFT REFLECTOR AND BATTERY PACK (61-0478-9). OPERATIONAL CHECK SYSTEM GOOD. (M)Sep 19, 1997 · N224US · Boeing 737201 · Emergency LightingSDR USAASB97259Battery Pack · dischargedTPA - EMERGENCY LIGHTS AFT GALLEY (LOWER INSIDE) INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Sep 19, 1997 · N224US · Boeing 737201 · Emergency LightingSDR USAASB97226Battery Pack · dischargedALB - BOTH INSIDE AFT ESCAPE SLIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPERATIONALLY CHECKED OK. (M)Aug 18, 1997 · N224US · Boeing 737201 · Emergency LightingSDR USAASB97131Battery Pack · dischargedCLT - MAINTENANCE FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATION CHECK GOOD. (M)May 15, 1997 · N224US · Boeing 737201 · Emergency LightingSDR USAA960665Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACKED FRAME .75 INCH LONG STATION 727 JUST BELOW STRINGER 13L. INSTALLED REPAIR DOUBLERS, REPAIRED PER EA 51489. (M)Oct 4, 1996 · N224US · Boeing 737201 · Fuselage Main, FrameSDR USAA960664Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG 1 INCH WIDE BS 1003 TO BS 1014 STRINGER. REMOVED DAMAGE AND FABRICATED REPAIR, REPAIRED PER SRM 53-10-2. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)Oct 4, 1996 · N224US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960663Keel Beam · damageINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND THREE ACCESS PLATE MOUNTING FLANGE HOLES DAMAGED IN KEEL BEAM, RIGHT SIDE KEEL BEAM LOWER CHORD OUTBOARD FLANGE FORWARD OF BS 727. INSTALLED STRAP REPAIR PER EA, REPAIRED PER EA 41514. (M)Oct 4, 1996 · N224US · Boeing 737201 · Fuselage Main, KeelSDR USAA960658Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .75 INCH CRACKS, LBL 25 INCHES LONG FLOOR BEAM WEB STATION 707 TO 712, WL 203.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960657Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKS BL 0 INCH LONG FLOOR BEAM WEB STATION 707 TO STATION 712, WL 203.5. INSTALLED REPAIR WEB, REPAIRED PER SRM 51-40-2. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960656Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK EXTERNAL SKIN DOUBLER FORWARD SERVICE DOOR LOWER HINGE. INSTALLED NEW DOUBLER, REPAIRED PER TR 52-10-01A. (M)Sep 27, 1996 · N224US · Boeing 737201 · Service DoorsSDR USAA960655Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK CORNER OF HINGE CUT OUT FORWARD SERVICE DOOR SKIN. INSTALLED DOUBLER, REPAIRED PER TR 52-40-03A. (M)Sep 27, 1996 · N224US · Boeing 737201 · Service DoorsSDR USAA960654Stub Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 597 STUB BEAM WEB RBL 60 TO RBL 62, WL 207.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960653Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLER, REPAIRED PER DRAWING 65C37732. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA960652Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLERS, REPAIRED PER DRAWING 65C37732. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA960651Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN CIRCUFERENTIAL FRAME STATION 328 3 INCHES BELOW STRINGER STRINGER 20R. FABRICATED 707576 .040 MATERIAL, INSTALLED WEB REPAIR, REPAIRED PER SRM 51-40-2 FIG 1. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, FrameSDR USAA960650Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACKS IN FOUR PLACES, RBL 25 INCHES LONG, FLOOR BEAM WEB STATION 707 TO 712, WL 203.5. INSTALLED WEB REPAIR, REPAIRED PER SRM 51-40-2. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960649Support Channel · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRCK RBL 45 SEAT TRACK SUPPORT CHANNEL ABOVE UPPER INBOARD BOLT. INSTALLED DOUBLERS, REPAIRED PER EA 41455 AND SB 737-53-1120. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960648Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO CRACKS 1 INCH BY 3 INCH CREASE BEAM WEB 2 INCHES AFT OF STATION 639 PLUS 1 INCH FORWARD OF STATION 663 FRAME LBL 67, WL 208. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960647Support Channel · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK LBL BS 520, WL 207.5 SUPPORT CHANNEL. FABRICATED DOUBLER CHANNEL RADIUS FILLERS, INSTALLED CHANNEL AND FILLERS. REPAIRED PER EA 41455 SB 337-53-1120. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960646Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACKS EMITTING FROM FASTENER HOLES (2) STRINGER 15L BS 525. CHANNEL REPAIR INSTALLED ON STRINGER, REPAIRED PER SRM 53-10-3. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960645Stub Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 578 STUB BEAM WEB LBL 61.5 TO LBL 62.5, WL 207.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA960644Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG CRACK STATION 747 STRINGER 19 L CIRCUMFERENTIAL FRAME. INSTALLED DOUBLERS, REPAIRED PER SRM 53-10-4. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, FrameSDR USAA960643Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 1 INCH BY 3 INCH SECTION AROUND RIVETS, BS 363 TO BS 500 PLUS 13 INCHES. REPLACED STRINGER SECTION, REPAIRED PER SRM 53-10-3 FIG 3 SHEET 2 TABLE 1. CORROSION TASK NR C53-107-01, CORROSION Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA960642Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 675 WL 202.5 LONGITUDINAL FLOOR BEAM LOWER CHORD. INSTALLED REINFORCING ANGLE/SPLICE, REPAIRED PER EA 41578. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA960641Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK RBL 45 LONG FLOOR BEAM LOWER CHORD STATION 695 WL 202.5. INSTALLED REPAIR ANGLE, REPAIRED PER EA 41557. (M)Sep 27, 1996 · N224US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAASB96048Engine · failedGSO - FL 8028 - AT APPROXIMATELY 600 FEET AGL AFTER TAKEOFF FROM GSO, THE LEFT ENGINE EXPLODED. TOWER ADVISED CREW THAT ENGINE WAS TRAILING SMOKE AND FIRE. FLIGHT RETURNED TO GSO AND GROUND EMERGENCY CREWS EXTINGUISHED THE ENGINE FIRE. NO FIRE WARNINGS RECEMar 19, 1996 · N224US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAASB96020Gasper Fan · failedCHS - EN ROUTE MCO-IAD - CREW NOTED ELECTRICAL IN SMELL IN CABIN. FLIGHT DIVERTED TO CHS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE GASPER FAN. (M)Jan 26, 1996 · N224US · Boeing 737201 · Air Distribution FanSDR USAA951235Stringer · corrosionROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 30 INCH BY 2 INCH CORROSION AT STRINGER 27 LEFT BS 947 TO 977. REMOVED DAMAGE AND INSTALLED STRINGER SPLICE. (M)Nov 22, 1995 · N224US · Boeing 737201 · Fuselage Main, Longeron/Stringer
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