JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, 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 jasc_code = '5753' 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.
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 jasc_code = '5753' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2013013100059Lever · damagedRT WING OTBD FORE FLAP TRACK NR 12 ATTACH LEVER ASSY DAMAGED. REMOVED DAMAGED LEVER ASSY LOCATED AND INSTALLED NEW LEVER ASSY IAW COMPONENT MM 57-52-51.SDR FDEA201301270196Skin · dentedRIGHT INBD FLAP HAS A DENT ON TOP SIDE, OTBD SIDE ABOVE FAIRING. REPAIRED IAW SRM 57-53-01 AND SRM 51-70-10 REPAIR 4. PERMENANT REPAIR ACCOMPLISHED PER EA F-5750-T0300135. MAJOR REPAIRSDR QXEA2013012700190Flap Track · gougedFLAP TRACK NR 5 ON THE LT SIDE IS GOUGED ON THE INBD AND OTBD SIDES. POLISHED TRACK IAW SRM 57-50-50, TEMP REV 57-010. NO MEASUREABLE MATERIAL REMOVED. EDDY CURRENT NOT REQUIRED AS WEAR IS IN SACRIFICIAL COATING.SDR IPXA13676848Skin · dentedLT WING INBD T/E FLAP LOWER SURFACE DENTED. REPAIRED REF SRM 767 51-70-10-2R.SDR A6WA201302204804Skin · gougedGOUGE ON I/B LOWER SKIN ON RIGHT I/B FLAP. REMOVED & REPLACED SKIN IAW CRJ 200 SRM 57-52-00 REPAIR 3 FIG 202 SHEET 2.SDR 2013FA0000055Rib · corrodedDURING AN ANNUAL INSPECTION, VISUAL INSPECTION UNVEILED THE OTBD RIB ON THE RT FLAP HAD EXCESSIVE CORROSION. AFTER UNRIVETING THE L/E SKIN, IT WAS DISCOVERED THAT ALL THE RIBS WERE CORRODED BEYOND REPAIR AND THE FLAP WAS SCRAPPED FOR A SERVICEABLE UNIT.SDR USAA2013031400015Skin · debonded3S CHECK - DISBONDING ON EXISTING REPAIR ON RIGHT OUTBOARD FLAP ASSEMBLY UPPER SKIN SURFACE BETWEEN WS 8744 TO WS 9235 & BETWEEN RIB 10 TO RIB 11. REPAIRED RIGHT OUTBOARD FLAP ASSEMBLY IAW A320 SRM 57-53-00, PARA 8N, FIG 212.SDR A6WA2013020500667Bracket · brokenLEFT O/B FLAP O/B HINGE ARM HAS BROKEN MOUNT BRACKET FOR PANEL 597BB ON O/B SIDE. REMOVED AND REPLACED MOUNT BRACKET FOR PANEL 597BB.K.SDR IPXA3576820Bracket · crackedINSPECTION TYPE: C13, RT WING OTBD FLAP INBD JACK TRANSMISSION SUPPORT BRACKET CRACKED, OUT OF LIMITS IAW SRM 51-10-02. R & R BRACKET FITTING IAW AMM 27-15-17-424.SDR SWIA201332798Vane · chafedRIGHT INBOARD FLAP VANE IS CHAFED BEYOND LIMITS AND REQUIRES REPLACEMENT. (C-CHECK) REMOVED AND REPLACED RIGHT INBOARD FLAP VANE LEADING EDGE IAW SRM.SDR A6WA20134675Vane · chafedRIGHT I/B FLAP VANE LEADING EDGE I/B, CTR & O/B AREA CHAFED FROM STOPS. REMOVED AND REPLACED I/B LEADING EDGE & BLENDED & TREATED CTR & O/B LEADING EDGE IAW REO 601R-57-52-004.SDR A6WA201302050674Vane · chafedRIGHT INBD FLAP VANE HAS FOUR CHAFE SPOTS. NOT BUMP STOPS. BLENDED CHAFE SPOTS IAW SRM 51-12-00 FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004.SDR SWAA2013012411767Flap · delaminatedLEFT WING TRAILING EDGE OUTBOARD AFT FLAP DELAMINATED AT AFT INBOARD CONNER 3.5" LONG X 1.0" WIDE MOD. PERFORMED INTERIM REPAIR PER SRM REF 57-53-01-1A-4 PARA.5. SEALED DAMAGED AREA WITH SPEED TAPE. MAKE AN INSPECTION OF DELAMINATION AND TAPESDR CA130516010Support Bracket · cracked(CAN) FLAP ACTUATOR BRACKET ASSY FOUND CRACKED AT LIGHTING RELIEF HOLES AND ACROSS DOUBLER, FROM FLANGE TO LIGHTING HOLE DURING PHASE INSPECTION. SERVICE KIT SK208-158 INSTALLED TO RECTIFY PROBLEM.SDR A6WA20134M673Fitting · chafedRIGHT OTBD FLAP ROLLER GUIDE ALIGNMENT FITTING IS CHAFED. BLENDED CHAFE PER CRJ 200 SRM 51-12-00 DEPTH WAS .008 WITHIN LIMITS IAW REO 601R-57-51-143.SDR A6WA20134672Fitting · chafedRIGHT OTBD FLAP ROLLER GUIDE FITTING IS CHAFED. BLENDED CHAFE ON CRJ 200 SRM 51-12-00 DEPTH OF CHAFE WAS .014 WITHIN LIMITS IAW REO 601R-57-53-039.SDR WX0A071493Doubler · chafedLEFT O/B AFT FLAP I/B VANE L/E CHAFED OUT OF LIMITS ON EXISTING DOUBLER. REMOVED DAMAGED DOUBLER, REMOVED DAMAGED SKIN, PERFORMED WATER EVAC. FABRICATED FILLER AND DOUBLER AND BONDED.SDR IPXA3B76799Wedge · damagedRT INBD T/E FLAP WEDGE HAS .5" HOLE. REPAIRED IAE EO B747-5750-48934-B.SDR COEA2013030803913Rib · corrodedHEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION. RIGHT INBOARD FLAP INTERNAL RIB 5 IS CORRODED. REPLACE FLAP PER ATR42 AMM.SDR SWAA2013020712365Skin · puncturedDISCOVERED FOD DAMAGE & SKIN PUNCTURE TO OUTBD FLAP TRAILING SECTION JUST INBD OF CENTER CANOE FAIRING AND OUTBD OF LEFT ENGINE. REMOVED AND REPLACED FLAP PER AMM.SDR SWAA2013012411760Spindle · corrodedNR 8 FLAP SPINDLE IS RUSTED & THERMAL COATING IS MISSING. REMOVED AND REPLACED IAW MT 327-51-08 & MT 327-51-06. P/N OFF:65-46481-145 S/N OFF:B5240R P/N ON:65-46481-155WN S/N ON:B4172RSDR SWAA2013012311719Panel · crackedRT WING INBOARD AFT FLAP OUTBOARD END UPPER FIXED SHELF PANEL IS CRACKED AT SUPPORT BRACKET. REMOVED AND REPLACED PANEL PER AMM.SDR WX0A071490Vane · chafedLEFT WING O/B FLAP I/B VANE L/E CHAFED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED.SDR AALA20130120003Flap · puncturedLEFT INBOARD TRAILING EDGE FLAP HAS PUNCTURE MEASURING 1/4 INCH. ACCOMPLISHED HOT BOND REPAIR PER SRM 57-53-01-2R-4 AND 51-70-10.SDR ASAA2013012093712Wedge · dentedLT WING INBD MIDFLAP T/E WEDGE IS DENIED ON INBD END LWR SURFACE REPAIRED DENT LT WING INBD MIDFLAP T/E WEDGE INBD END LWR SURFACE IAW SRM 51-70-10, REPAIR 4.SDR IPXA3676759Skin · delaminatedTWO AREAS OF DELAMINATED ON T/E WEDGE INNER 3" X 5" BY 1.75 X 3" MUST REPAIR AS 1 DUE TO PROXIMITY OF DAMAGES ONLY 4" APART. REPAIR REF SRM 57-53-01-2R-1, AND SRM 51-70-17.SDR A6WA20134646Fitting · chafedLEFT OUTBOARD FLAP GUIDE ROLLER FITTING IS CHAFED. BLENDED CHAFED AREA ON LEFT O/B FLAP GUIDE ROLLER FITTING IAW REO 601R-57-53-963.SDR A6WA20134645Skin · chafedLEFT INBOARD FLAP INBOARD SIDE SKIN RIB HAS CHAFING DAMAGE. BLENDED CHAFE DAMAGE TO LEFT INBOARD FLAP INBOARD RIB IAW REO 601R-57-52-2007.SDR SWAA2013012811982Flap · delaminatedLEFT OUTBOARD AFT FLAP HS DELAMINATED ON THE INBOARD TRAILING EDGE CORNER. REMOVED DAMAGE CLEANED EVALUATED LEFT O/B AFT FLAP DELAMINATED ON I/B TRAILING EDGE CORNER NO MOISTURE NOTED TAP TEST GOOD REPAIR MATERIALS.SDR WX0A071488Vane · chafedRIGHT WING O/B FLAP I/B VANE L/E STATION XW150 CHAFED OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND BONDED.SDR WX0A071487Vane · chafedLEFT WING O/B FLAP I/B VANE L/E STATION XW150 CHAFED OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED DOUBLER, HOT BOND REPAIRED.SDR ASAA2013011793773Skin · dentedLT WING INBD FOREFLAP UPPER SURFACE IS DENTED. NOTE WAS LISTED ON PLT BUT HAS PROGRESSED IN LENGTH AND DEPTH. ACFT GROUNDED. REPAIRED DENT ON LT WING INBD FOREFLAP UPPER SURFACE IAW SRM 51-70-10, REPAIR 3 AND 4.SDR ASAA2013011793758Skin · chafedLT WING INBD MIDFLAP UPPER SURFACE INBD END IS CHAFED. REPAIRED MIDFLAP SKIN IAW SRM 57-53-01, REP 3, FIG 201.SDR SWAA2013012411796Bushing · corrodedRUSTED ON BUSHING AND BOLT OF SAFETY LINK LOCATED ON O/B MID FLAP CARRIAGE 7. REMOVED AND REPLACED BUSHING AND BOLT OF SAFETY LINK LOCATED ON O/B MIDFLAP CARRIAGE 7 IAW CMM 57-53-22 STEP 1.D.(4)(5),1.B.(5)(B)7).SDR SWAA2013012411785Bearing · looseLOOSE BEARINGS (2E/A) LOCATED AT FWD LOWER POSITION ON O/B MID FLAP CARRIAGE 7. REMOVED AND REPLACED (2E/A) BEARINGS LOCATED AT FWD LOWER POSITION ON O/B MIDFLAP CARRIAGE 7 RIGHT WING IAW CMM 57-53-36.SDR SWAA2013012311724Bushing · corrodedRUSTED ON BUSHING AND BOLT OF SAFETY LINK LOCATED AT OTBD FLAP CARRIAGE NR 2 LT WING. REMOVED AND REPLACED BUSHING AND BOLT IAW CMM 57-53-22 STEP 1.D (4) (5); 1B (5 )(B) 7).SDR SWAA2013012111637Spherical Bearin · looseINBOARD LEFT FLAP INBOARD TRAILING FLT TRACK SPHERICAL BEARING IS LOOSE. REMOVED AND REPLACED BEARING PER AMM.SDR UIEA2013012000015Skin · damagedRT WING INBD AFT T/E FLAP DAMAGED AT WBL 178.46. PREPARED CLEANED AND REPAIRED AREA OF DAMAGE ON RT WING INBD AFT FLAP T/E AT STATION WBL 178.48 IAW SRM 57-51-01-2R1-1. REPAIR 1, FIG 201 SHEET 4 AND 8. IAW 250 DEGREE F; CORE. SRM 51-70-01.SDR SWAA2013011811562Flap · delaminatedRIGHT I/B FOREFLAP HAS DELAM AFT OF PREVIOUS REPAIR. REMOVED AND REPLACED RIGHT I/B FOREFLAP ASSY AND I/B AND O/B TOGGLE ASSYS PER MM. RIG AND OP'S CHECK GOOD. TAG 495044 P/N ON: 65-46430-130 S/N ON: 1909 P/N OFF: S/N OFF: BN813SDR A6WA20134648Vane · crackedRIGHT I/B FLAP VANE CRACKED IN 3 AREAS ON LEADING EDGE. REMOVED UNSERVICEABLE I/B AND CTR LEADING EDGE AND INSTALLED SERVICEABLE I/B AND CTR LEADING EDGE IAW CRJ 200 SRM 51-40-11/51-42-13. BLENDED CHAFE DAMAGE ON O/B LEADING EDGE AND RESTORED FINISH IAW REO SDR FDEA201301160102Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 75.0. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 75.0. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 116.SDR SWAA2013012411806Bearing · damagedMISSING MATERIAL LOCATED ON SPINDLE BEARING AND THRUST BEARING OF OUTBOARD FLAP TRACK CARRIAGE NR 2 LEFT WING. REMOVED AND REPLACED SPINDLE BEARING AND THRUST BEARING AT OUTBOARD FLAP TRACK CARRIAGE NR 2 LEFT WING IAW CMM 57-53-36.SDR SWAA2013021312627Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ON TRACK FAIRING INBOARD SIDE TRAILING EDGE OF LT WING. REPLACED SUPPORT ANGLE LOCATED ON TRACK FAIRING INBOARD SIDE TRAILING EDGE OF LEFT WING IAW B737-300 SRM 51-10-02 ITEM 8, SRM 51-40-02 AND DWG 65C26300SDR USAA2013012900007Skin · cracked2S CHECK - CRACK ON RIGHT INBOARD FLAP TAB BETWEEN RIB 6 TO RIB 8 APPROX 6 INCHES FROM LOWER EDGE. REPAIRED RIGHT INBOARD FLAP TAB LOWER SURFACE IAW A321 SRM 57-52-00.SDR SWAA2013012811974Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ON TRACK FAIRING OUTBOARD SIDE AT WBL 198.60 LEFT WING. REPLACED SUPPORT LOCATED ON TRACK FAIRING OUTBOARD SIDE AT WBL 198.60 LEFT WING IAW SRM B737-300 51-10-02 ITEM 8, SRM B737-300 51-40-02 AND DRAWING 65C26300.SDR SWAA2013012811937Spindle · flakingFLAKED THERMAL COATING ON CARRIAGE SPINDLE NR 8. R & R SPINDLE ASSY NR 8 IAW AMM.SDR SWAA2013012811936Spindle · crackedLT WING OTBD T/E FLAP OTBD SPINDLE CARRIAGE CRACKED. R & R SPINDLE ASSY IAW AMM.SDR SWAA2013021112539Flap · delaminatedDELAMINATION AT 29" FROM INBOARD END OF INBOARD AFT FLAP R/T WING. REPAIRED AT 29" FROM INBOARD END OF INBOARD AFT FLAP R/T WING IAW B737-300 SRM 51-70-10-2R-0.SDR ASAA2013011493789Spar · chafedLT WING INBD MIDFLAP EDGE FWD SPAR ANGLE UNDER THE OTBD ROD ARM IS CHAFED. ACFT GROUNDED. REPAIRED LT INBD MID FLAP T/E WEDGE BEAM IAW ASA EA 400-57EA-09685.SDR ASAA2013011493756Skin · chafedLT WING OTBD FOREFLAP L/E IS CHAFED. REPLACED LT WING OTBD FOREFLAP INBD L/E SECTION IAW SRMS 51-30-01 AND AMM 20-50-11-912-002. FOREFLAP TO MID FLAP GAPS FOUND TO BE ACCEPTABLE AS IS IAW EA 400 27, EA 09690.
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