N352US, cancelled Sep 6, 2006

Service difficulty reports · 78

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 = 'N352US' AND deregistration_id = 'N352US-2006-09-06'
  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 SB05131Power Supply · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD.Oct 13, 2005 · N352US · Boeing 737301 · Emergency LightingSDR SB05123Battery Pack · dischargedPHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD.Sep 26, 2005 · N352US · Boeing 737301 · Emergency LightingSDR SB05112Outflow Valve · leakingAIRCRAFT WOULD NOT MAINTAIN CABIN PRESSURIZATION. AT FL030, CABIN ALTITUDE CLIMBED 1,200 FEET PER MINUTE WITH OUTFLOW VALVE FULLY CLOSED. CREW DESCENDED BELOW FL020 BEFORE CABIN ALTITUDE WOULD DESCEND BELOW 8,000 FEET. FLIGHT CONTINUED. MX PRESSURIZED AIRCSep 9, 2005 · N352US · Boeing 737301 · Pressure Regulator/Outflow ValveSDR USAA040844Skin · crackedFWD SERVICE DOOR SKIN, .1875 INCH CRACK, UPPER HINGE CUTOUT, LWR RADIUS TO DRAIN HOLE. INSTALLED DOUBLER IAW TYP REP 52-10-13.Nov 12, 2004 · N352US · Boeing 737301 · Service DoorsSDR USAA041040Skin · gougedPIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .75 INCH GOUGE, RT ELEVATOR AT 84.5 AND 4 - 5 INCH IN FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/SkinSDR USAA041039Skin · gougedPIT - Q4 -LOWER SKIN SURFACE, SINGLER LAYER COMPOSITE DAMAGE .50 INCH GOUGE. RT ELEVATOR AT STA 62 AND 15 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA.Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/SkinSDR USAA041038Skin · gougedPIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .50 INCH GOUGE, RT ELEVATOR AT STA 71 AND 10 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/SkinSDR USAA041037Skin · damagedPIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE, 2 GOUGES 1.25 INCHES, COMPOSITE DAMAGE, 2 GOUGES, RT ELEVATOR AT STA 70 AND 8 TO 9 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, SUPPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/SkinSDR USAA041036Skin · damagedPIT - Q4 - LOWER SKIN SURFACE, COMPOSITE DAMAGE, .3750 INCH GOUGE, COMPOSITE DAMAGE - SINGLE LAYER, RT ELEVATOR AT STA 64 + 7 INCH FROM FWD SPAR. REPAIRED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA.Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/SkinSDR USAA041035Skin · damagedPIT - Q4 - LOWER SKIN, COMPOSIT DAMAGE .3750 INCH GOUGING. COMPOSITE DAMAGE - SINGLE LAYER RT ELEVATOR AT STA 68 + 6 INCHES FROM FWD SPAR LOWER SKIN. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA.Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/SkinSDR USAA041034Skin · delaminatedPIT - Q4 - LOWER SKIN SURFACE, 2 INCH SQ DELAMINATION, RT LELVATOR 41 INCH FROM IB END AND 13 INCH AFT OF L/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED SER COR, REPLACEMENT SKIN PANEL IAW SRM, EA.Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/SkinSDR USAA040973Fitting · crackedPIT- Q4 - MLG SUPPORT BEAM AFT FITTING, .0625 INCH CRACK (2) HOLES ON MLG SUPPORT AFT BEAM FITTING, 12 O`CLOCK AND 9 O`CLOCK. REPLACED LT MGL SUPPORT BEAM AFT FITTING IAW EO 5702V054.Nov 11, 2004 · N352US · Boeing 737301 · Fuselage, Landing Gear Attach FittingsSDR USAA040972Spar · crackedPIT - Q4 - LT SPAR UPPER CHORD, .0625 INCH CRACK; NR 2 HOLE VERTICAL LEG OF LT SPAR UPPER CHORD AT MLG SUPPORT. INSTALLED FATIGUE ENHANCEMENT PLATE IAW EA 79286A.Nov 11, 2004 · N352US · Boeing 737301 · Wing SparSDR USAA040971Doubler · crackedPIT - Q4 - DOUBLER, .25 INCH LONG CRACKS (2 EA), RT WING FUEL PANEL REBATE PANEL NR 8817R. INSTALLED EXT DOUBLER .125 THICK IAW EA 79453.Nov 11, 2004 · N352US · Boeing 737301 · Wing, Plate/SkinSDR USAA040875Flange · crackedFUEL PLATE FLANGE, (2 EA) .189 INCH IN LENGTH, CRACK (2) FUEL PANEL NR 881, 17R, 6 O`CLOCK AND 12 O`CLOCK POSITIONS. STOP DRILLED CRACKS, TRIMMED SKIN PANEL, INSTALLED FILLER AND DOUBLER IAW EA 79453.Nov 11, 2004 · N352US · Boeing 737301 · Wing Miscellaneous StructureSDR USAA040874Stiffener · crackedSTIFFENER, .1250 INCH CRACK, LBL 5.7 IB AND OB SIDE 8 INCH IN FROM BOTTOM. STRAPS, ANGLES AND FILLERS INSTALLED ON BOTH SIDES OF VERT CORD IAW EO 5300V155 AND EA 79321.Nov 3, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040856Frame · crackedPIT - Q4 - FRAME, .2500 INCH CRACK. CRACK EMANATING FROM FASTENER, FRAME STA 867 AND STR 9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A.Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040855Frame · crackedPIT - Q4 - FRAME, .1250 INCH CRACK, STA 787 AND STR 9L. INSTALLED DOUBLERS IAE TYP REP 53-10-20A.Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040854Frame · crackedFRAME, .3750 INCH CRACK, STA 540 BETWEEN RT IB SEAT TRACK, RBL 24.75 AND CRT FLOOR SUPPORT BEAM BL 0. DEFECTIVE PART, REPLACED WITH IDENT PN IAW MFG DWG 65-46819.Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040857Frame · crackedPIT - Q4, FRAME, .1250 INCH CRACK, EMANATING FROM FASTENER, FRAME STA 847, STR 9L. INSTALLED DOUBLERS IAW TYPE REP 53-10-20A.Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, StructureSDR USAA040862Angle · wornANGLE, 4, DEEP WEAR MARKS, VERT SUPPORT Z, VERT OB LEG AT AFT LEG GEAR WELL CUTOUT CORNER. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-48690.Oct 28, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040864Skate Angle · chafedSKATE ANGLE, 11 INCHES LONG, EXCESSIVELY DEEP CHAFE MARK, 1104 TO 1121, STR 2 L.Oct 25, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040845Frame · crackedFRAME, .5 INCH CRACK, STR 9 LT AT FRAME, STA 767. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A.Oct 22, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040863Skin · gougedQ4, SKIN, 16 INCHES W BY 22 INCHES L, GOUGES, STA 887 BETWEEN S35R AND S27R. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-00-01.Oct 22, 2004 · N352US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA040853Frame · crackedFRAME .2500 INCH LONG CRACK BS 360 ON FRAME BETWEEN S8L AND S9L. INSTALLED REPAIR ANGLES IAE TYP REP 53-10-20A.Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040851Frame · crackedFRAME, .1250 INCH CRACK, CRACKED AROUND RIVET AT FRAME AT STA 827, STR 9L. REMOVED CRACK AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A.Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040850Stringer · crackedSTRINGER, .5 INCH LONG CRACK, STR 7L AT BS 1010. INSTALLED REPAIR ANGLE IAW 53-00-03.Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040849Frame · crackedFRAME .2500 INCH CRACK, FRAME STA 787 AND STR 9R, CRACK EMANATING FROM FASTENER. INSTALLED REPAIR DOUBLER IAW TR 53-10-20A.Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040861Attach Bracket · damagedPIT - Q4, ATTACH BRACKET, MIGRATING AND MISSING BUSHINGS. RT MLG SUPPORT BEAM, SPOILER ACT ATTACH BRACKET. REPLACED SPOILER ACTUATOR ATTACH BRACKET IAW MFG DWG 63895.Oct 21, 2004 · N352US · Boeing 737301 · SpoilersSDR USAA040860Fitting · wornPIT - Q4, STAB BEAM FITTING, WORN BUSHING. STAB BEAM LUG, RT MLG SUPPORT BEAM. REPLACED STAB BEAM FITTING IAW AMM 57-15-00-434.Oct 21, 2004 · N352US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAA040859Hanger Assy · wornPIT - Q4, WALKING BEAM HANGAR, WORN BUSHINGS. RT MAIN LANDING SUPPORT BEAM. REPLACED WALKING BEAM HANGAR IAW AMM 57-15-00-434.Oct 21, 2004 · N352US · Boeing 737301 · Fuselage, Landing Gear Attach FittingsSDR USAA040952Stringer · crackedPIT - Q4 - STRINGER, .1250 INCH CRACKS, CRACKS IN STRING AROUND FASTENERS, STA 907, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-45772.Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040872Skate Angle · chafedPIT - Q4 - SKATE ANGLE, 10 INCHES, CHAFED, 1006 TO 1016 BETWEEN STR 2L AND 3L. FABRICATED NEW ANGLE IAW MFG ENG DWG 65-548423.Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040873Skate Angle · chafedSKATE ANGLE, 10 INCHES OF CHAFING, 1006 TO 1016 BETWEEN STR 2R AND 3R. FABRICATED NEW ANGLE FROM ENG DWG 65548424.Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040876Stringer · crackedPIT - Q4, STRINGER, .1250 INCH CRACK, STA 907, STR4L, AROUND FASTENERS. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-52988.Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040848Frame · crackedFRAME, .5 INCH CRACK, FRAME STA907,STR9L, CRACK EMANATING FROM FASTENER. CUTOUT CRACKED AREA AND INSTALLED REPAIR ANGLES IAW T.R. 53-10-20A.Oct 19, 2004 · N352US · Boeing 737301 · Fuselage Main, FrameSDR USAA040882Fitting · corrodedPIT - Q4, FITTING, 1 INCH BY .5 INCH AREA, CORROSION; NO LEVEL OR TASK. RT WING AFT SPAR OB BUSHING BORE FTG WALKING BEAM HANGAR LUG AT STA 202. REMOVED AND REPLACED FITTING IAW MFG DWG 6545321 AND SRM 51-20-25.Oct 19, 2004 · N352US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAA040858Bracket · crackedBRACKET, 1 INCH CRACK, LT WING SPAR (AFT) STA 218, MFG NEW BRACKET IAW J020-37-20.Oct 19, 2004 · N352US · Boeing 737301 · Wing Miscellaneous StructureSDR USAA040847Intercostal · crackedINTERCOSTAL, .5 INCH CRACK, STA 947.5, LBL43. REPLACED INTERCOSTAL IAW SRM 51-70-11.Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040883Stringer · corrodedSTRINGER, 6 INCHES FULL WIDTH AND SIDES, CORROSION; LEVEL 1; TASK NR C53-208-01, STR 27 R JUST FWD OF FRAME, STA 1006. CUT STR REPAIR SECTION TO FIT AND INSTALLED REPAIR IAW 53-00-03.Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA040880Fitting · corrodedPIT - Q4, LAV FLOOR ANCHOR FITTING, 2 AREAS, 1 INCH BY 2 INCHES, CORRODED; LEVEL 1; TASK NR C53-107-02, LT AFT LAV STA 986.5. REMOVED AND REPLACED FITTING (2 EA) IAW SRM 51-10-02.Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA040881Anchor Fitting · corrodedPIT - Q4, LAV FLOOR ANCHOR FITTING, 2 INCHES BY 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, RT LAV FLOOR STA 1016.Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA040877Floorbeam · crackedPIT - Q4, BEAM, ABOUT .5 INCH, CRACKED, FLOOR SUPPORT BEAM, STA 540 AND LT OB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-46819-4.Oct 16, 2004 · N352US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA040741Door Frame · crackedPIT, Q4, EDGE FRAME SERVICE DOOR, .5 INCH CRACK, EDGE FRAME CRACKED, FWD SERVICE DOOR AFT EDGE FRAME, MID STOP AREA. INSTALLED DOUBLER IAW TYPE REP 52-10-11.Oct 15, 2004 · N352US · Boeing 737301 · Fuselage Main, StructureSDR USAA040852Door Frame · crackedPIT - Q4 - DOOR EDGE FRAME, .5 INCH CRACK, FWD SERVICE DOOR AFT END FRAME AT MIDSTOP FITTING. ROUTED OUT CRACK, INSTALLED DOUBLER IAW TYP REP 52-10-11.Oct 14, 2004 · N352US · Boeing 737301 · Fuselage Main, StructureSDR USAA040878Attach Bracket · crackedATTACH BRACKET, .5 INCH LONG CRACK, S10L, STA 360. MANUFACTURED ATTACH BRACKET IAW SRM 51-40-03.Oct 14, 2004 · N352US · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA040884Floorbeam · corrodedFLOORBEAM, 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 30.5 BETWEEN STA 947.5 AND 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02.Oct 12, 2004 · N352US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA040885Floor Support · corrodedFLOOR SUPPORT, 4 INCHES BY 1 INCH, CORROSION; LEVEL 1; TASK NR C53-107-02, RBL 17.61, STA 986.5 TO 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02.Oct 12, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040886Support · corrodedSUPPORT, 5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 25 BETWEEN STA 947.5 AND 967.Oct 12, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040846Frame · crackedFRAME, 1.7500 INCH CRACK, BS 787, STR 9L. REPAIRED IAW TYP REP 53-10-20A.Oct 11, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
Back to N352US, cancelled Sep 6, 2006