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 SWAA2020022441638Structure · damagedR/H INBOARD AFT FLAP DAMAGED. / R&R AFT FLAP PER AMM.SDR DALA2020022431369Skin · dented(AIRCRAFT 5649, L/P 1500615) UPON PERFORMING AN IN PROGRESS INSPECTION OF THE RT WING INBD MAIN FLAP, FOUND DENT ON TRAILING EDGE OF FLAP. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON RT WING INBD MAIN FLAP T/E IAW B757-200 SRM 57-53-01-2R FIG.201 DETAISDR FDEA2020022410368Skin · gougedRW INBD FLAP UPPER SURFACE, FWD OTBD CORNER IS GOUGED. COMPLIED WITH EA #:6-5750-T0352296 (P1) TITLE: WING-FLIGHT SURFACES-RH WING INBOARD FLAP UPPER SKIN, EXISTING REPAIR DAMAGED FLAP UPPER SKIN, EXISTING REPAIR DAMAGEDSDR KCSA202002211010Thrust Bearing · corroded#5 FLAP THRUST BEARING BORE CORRODEDSDR SWIA2020033049581Rib · damagedRH INBOARD FLAP VANE LEADING EDGE INBOARD RIB REQUIRES REPLACEMENT (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AND RESTORED FINISH ON RH INBOARD FLAP VANE LEADING EDGE INBOARD RIB. REF: CRJ200 SRM. FOUND TO BE OUT OF LIMITS ON CAMP 20427303 JOB 2736661 OP SDR SWAA2021071382683Skin · debondedLEFT OUTBOARD AFT FLAP; INBOARD TRAILING EDGE LOWER SURFACE HAS DISBOND. / REPAIRED PER SRM 57-53-01-2R-4 AND 51-70-10.SDR SWAA2021071309066Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP INBOARD UPPER SURFACE IS DELAMINATED / UPON INVESTIGATION DAMAGE ON R/H WING O/B AFT FLAP I/B UPPER SURFACE FOUND TO BE BEYOND ALLOWABLE LIMITS PER SRM 57-53-01-1A-4 PARA 4.A.(5). REMOVED DAMAGE AND REPAIRED AREA IAW SRM 51-70-10-2SDR SWIA2020042450317Spring · corrodedRIGHT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED RIGHT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING IAW CRJ200 AMM.SDR SWIA2020042450316Spring · corrodedRIGHT WING #3 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED RIGHT WING #3 O/B FLAP HINGE BOX BUTE COMPRESSION SPRING IAW CRJ200 CMM. TW:STS 3817 DUE: 05 APR 20SDR SWIA2020030348969Cap · chafedADDITIONAL CHAFING FOUND ON LH INBOARD FLAP, INBOARD FLAP VANE CAP (C-CHECK) RO 2/28/2020 REMOVED CHAFFED LH INBOARD FLAP, INBOARD FLAP VANE CAP AND INSTALLED NEW LH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FORSDR AALA2020022419015Flap Track · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD #1 FLAP TRACK RAIL WORN. REPLACED FLAP TRACK RAIL PER AMM 57-54-21-400-801-B.SDR DALA2020022001266Flap · broken(AIRCRAFT 6819, L/P 1496689) DURING SERVICE LANDING GEAR STRUT, WAS BROKEN OUTBD AFT FLAP T.E AT LH WING. CORRECTIVE ACTION: OUTBD AFT FLAP T.E AT LH WING WAS REPAIRED PER B-757-200 S.R.M. 51-70-04-0G. FIG.2 PAR. 5. C.SDR SWIA2020032749500Vane · chafedLH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 95.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON L/H, I/B FLAP VANE L/E AT W/S 95.0 PER CRJ-200 SRM. ORIGINAL MATERIAL THICKNESS IS 050". REMAINING THICKNESS IS .025". MATERIAL LOSS IS .025". AREA FSDR SWIA2020032749499Vane · chafedLH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 55.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ONE L/H, I/B FLAP VANE L/E AT APPROX W/S 55.0. PER CRJ-200 SRM 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING THICKNESS IS .023". MATERIAL LOSSSDR SWIA2020032749498Vane · chafedRH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 95. (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON R/H, I/B FLAP VANE L/E AT APPROX W/S 95.0 PER CRJ-200 SRM. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING THICKNESS IS .025". MATERIAL LOSS IS .025". SDR SWIA2020032749497Vane · chafedRH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 141.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON R/H, I/B FLAP VAN L/E AT APPROX W/S 141.0 PER CRJ-200 SRM-200 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING MATERIAL THICKNESS IS .024". MASDR SWAA2020030542166Flap · delaminatedLEFT HAND WING OUTBOARD AFT FLAP INBOARD CORNER DELAMINATED UPON EVALUATION OF DELAMINATION TO L/H OTBD AFT FLAP FOUND IT BEYOND ALLOWABLE LIMITS OF B737 SRM 57-53-01-1A-4. REPAIRED I.A.W SRM 57-53-01A-2R-4 AND 51-70-10-2R-4 AND 51-70-10-2R-0SDR DALA202002201302Vane · puncturedPD: REF. HGR NRC 308: HOLE IN UNDERSIDE OF VANE OF RT AFT MOVEABLE, RH WING. (MAJOR REPAIR SDR) CA: VANE, REPAIRED PER CMM 27-50-1 REV 27 AND SRM 57-53-01 REPAIR 1 RELEASE #60SDR DALA2020021901249Skin · cracked(AIRCRAFT 6819, L/P 1495423) CRACK ON MAIN INBOARD FLAP UPPER SKIN (32 INCHES FROM INBOARD EDGE) AT RH WING. CORRECTIVE ACTION: REPAIRED PER B-757-200 S.R.M. 51-70-06-0G PAR. 5. ON REFERENCE OF B-757-200 S.R.M. 57-53-01-2R-1, DETAIL I TABLE III.SDR P5CA202002198046Skin · corrodedCORROSION - SKIN, L/H WING INBD AFT FLAP T/E UPPER SURFACE WBL 278.(<P>REMOVE THE DAMAGED MATERIAL AND CLEAN AND MEASURE THE DAMAGED AREA (L = 2.4", W = 0.75", D = 0.012", 8.25" FROM OUTBD EDGE, AT PNL T/E) BOND REPAIR DOUBLER (L = 6.9", W = 2.25", D = 0.025")SDR SWIA2020040349890Skin · dentedRT WING I/B FLAP LOWER SURFACE HAS DENT (C-CHECK) RO 4/2/2020 REPAIRED DAMAGE IAW BOMBA REO REV:-- DATE:2010/01/07SDR DALA2020021700066Cover · missingRIGHT NBR 4 FLAP TRACK FAIRING COVER 533BB MISSING. REPLACED NBR 4 FLAP TRACK FAIRING COVER 533BB. LP 7208153SDR DALA2020021700065Cover · missingFLAP TRACK COVER MISSING FROM RIGHT WING NBR 3 FLAP TRACK FAIRING. REPLACED NBR 3 FLAP TRACK COVER. LP 6901466SDR SWIA2020042450315Bolt · corrodedR/H O/B FLAP #5 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNTS BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACE 4 MOUNT BOLTS AND 4 WASHERS ON R/H OUTBOARD FLAP NUMBER 5 HINGE BOX IAW CRJ200 AMM. TORQUE WRENCH STS 3818 SERIAL NUMBER 0518901775. CAL DUE DATSDR SWIA2020042450314Bolt · corrodedR/H O/B FLAP #4 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED 4 MOUNT BOLTS AND 4 WASHERS ON R/H O/B FLAP # 4 HINGE BOX IAW CRJ200 AMM TORQUE WRENCH: P/N:STS 3818, S/N:0518901775, CAL DUE DATE:05/APR/2020.SDR SWIA2020042450313Bolt · corrodedR/H O/B FLAP #3 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED R/H O/B FLAP #3 HINGE BOX UNDER SPRING (4) FOUR MOUNT BOLTS IAW CRJ-200 AMM. CALIBRATED TOOL: TORQUE WRENCH STS-3818 CAL DUE DATE: 05 APR 2020. SDR SWIA2020042450312Bolt · corrodedL/H O/B FLAP #4 HINGE BOX UNDER SPRING HAS CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED L/H O/B FLAP #4 HINGE BOX UNDER SPRING (04) FOUR MOUNT BOLTS. IAW CRJ200 AMM. CALIBRATED TOOL: TOOL WRENCH STS-3818 S/N 0518901775 CAL DUE DATE: 0SDR SWIA2020042450311Bolt · corrodedL/H O/B FLAP #3 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNT BOLTS (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED L/H O/B FLAP #3 HINGE BOX MOUNTING BOLTS IAW CRJ 200 AMM.SDR SWIA2020042450310Bolt · corrodedL/H O/B FLAP #5 HINGE BOX UNDER SPRING HAS CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REPLACED 4 CORRODED MOUNTING BOLTS ON L/H O/B FLAP #5 HINGE BOX UNDER SPRING IAW CRJ200 AMM.SDR SWIA2020042450309Spring · corrodedLEFT WING #5 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #5 O/B FLAP HINGE BOX BUTE COMPRESSION SPRING IAW CRJ200 AMM.SDR ASAA2020021432623Skin · dentedL/H I/B FLAP IS DENTED ON LOWER SURFACE AT #2 FLAP TRACK. GROUNDED - YES. REPAIRED L/H I/B FLAP DENT ON LOWER SURFACE AT #2 FLAP TRACK IAW A319 SRM 57-52-00-300-015, 51-25-00 & EA #CMPT-57EA-00420 REV:00 REV DATE: 03/20/2020SDR A6WA2020021447181Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED IN TWO PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED TO SMOOTH CONTOUR FLAP STATION 56.50 MATERIAL LOSS .014 FLAP STATION 105.00 MATERIAL LOSS .026 ORIGINAL THICKNESS .050 REMOVED AND REPLACED LEADING EDGESDR SWAA2021062285729Skin · debonded*CUSTOMER REQUEST* LT WING OTBD AFT FLAP DISBOND AT INBD AFT EDGE LOWER SKIN / REPAIRED DISBONDED EDGE ON L/H WING O/B AFT FLAP AT I/B AFT LOWER SKIN IAW 737 SRM 51-70-10-2R-0 AND SRM 57-53-01-2R-14. DISBOND WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-5SDR A6WA202002147178Skin · chafedRIGHT WING IB FLAP VANE SKIN LE CHAFFED IN 3 PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED MID AND INBD AREAS IAW BOMBARDIER REO 601R-57-52-004 REMOVED AND REPLACED LE PANEL AT STA. 141 IAW CRJ200 SRM 51-42-13SDR YENA2020021730175Skin · dentedDURING HEAVY MAINTENANCE, DENT RH INBD FLAP LWR SKIN AT 2.14IN FROM OBD EDGE, 3.95IN FROM LWR EDGE; REF AE NR 2020-20605 W/O 2020-71/1 REPAIRED FLAP AS PER EC A20-109-01 AND EA 57-0077-20 REV 0 PART 1. THIS IS CLASSIFIED A MAJOR REPAIRSDR SWIA2020032749415Skin · dented* LH INBD FLAP LOWER SKIN DENTED MARKED (C-CHECK) RO 3/25/2020 L/H I/B FLAP LOWER SKIN DENT HAS BEEN REPAIRED USING BOMBARDIER REO, ALSO COMPLIED W/SKYWEST TASK CARD AND COMPLETED M337. SEE CONTINUATION SHEET FOR DETAILS.SDR DALA2020021421162Skin · gouged(LOG 1486450) DURING INSPECTION FOUND GOUGE WAS FOUND IN DENT # 32 ON LOWER SKIN OF INBOARD AFT FLAP AT LH WING. LOWER SKIN OF INBOARD AFT FLAP AT LH WING WAS REPAIRED PER B737-800 S.R.M. 51-70-10-2R AND B737-800 S.R.M. 57-53-01-2R-4.SDR DALA2020021421161Skin · cracked(LOG 1486395) DURING INSPECTION FOUND CRACK ON DENTED AREA OF LEFT AFT INBD FLAP LOWER SURFACE 11 FROM OUTBD EDGE AND 5.5 FROM TRAILING EDGE. REPAIR PARTS WERE BONDED ON LEFT AFT INBD FLAP LOWER SURFACE 11 FROM OUTBD EDGE AND 5.5 FROM TRAILING EDGE PER B737-80SDR DALA2020021421160Skin · cracked(LOG 1486388) DURING INSPECTION FOUND CRACK FOUND ON DENT NO 35 WITH 0.600 OF LENGTH ON LOWER SKIN OF INBOARD AFT FLAP AT LH WING. LOWER SKIN OF INBOARD AFT FLAP AT LH WING WAS REPAIRED PER B737-800 S.R.M. 51-70-10-2R AND B737-800 S.R.M. 57-53-01-2R-4.SDR SWIA2020033049545Vane · damagedRIGHT I/B FLAP MIDDLE VANE NEEDS TO BE REPLACED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED RH INBOARD FLAP, MIDDLE VANE CAP PER REFERENCE CRJ 200 SRM SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020033049543Vane · damagedRIGHT I/B FLAP O/B VANE CAP NEEDS TO BE CHANGED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED RH INBOARD FLAP OUTBOARD VANE CAP PER REFERENCE CRJ 200 SRM SEE CONTINUATION CARD FOR DETAILSSDR AALA202002129009Seal · looseAIRCRAFT WAS GROUNDED: DIVERTED TO LAS , VERY LOUD RUMBLING NOISE COMING FROM UNDER WINGS STARTED IN CRUISE AT FL320. NOISE AND RUMBLING CONTINUED TO GET WORSE. F/A'S AN D PAX HEARD IT AND WERE PANICKING. SOMETIME AFTER WE STARTED DES CENT AND POWER WAS REDUCESDR AALA2020032549025Wedge · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD FLAP TRAILING EDGE WEDGE UPPER SURFACE BETWEEN 11 INCHES AND 12 INCHES OUT BOARD OF THE AFT FLAP CUT OUT OUTBOARD EDGE. REPAIRED FLAP WEDGE PER EA 303430.SDR AALA2020032549024Wedge · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD FLAP TRAILING EDGE WEDGE UPPER SURFACE BETWEEN 4 INCHES AND 7 INCHES OUT BOARD OF THE AFT FLAP CUT OUT OUTBOARD EDGE. REPAIRED FLAP WEDGE PER EA 303430.SDR SWAA2021070724300Plate · crackedRH WING LOWER T/E NUT PLATE STRIP (WAFFLE PLATE) JUST OB OF SAIL TAIL IS CRACKED / REMOVED AND REPLACED R/H WING LOWER T/E WIGGLE PLATE IAW BOEING 737 SRM 51-40-02 AND BOEING DWG 115A2001.SDR FDEA2020021080289Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-4SDR FDEA2020021080288Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM SDR FDEA2020021080287Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57SDR EE4Y2020020710629Skin · wornLH WING, OUTBD MID FLAP AT WBL 201 LEADING EDGE SKIN WITH WORN. NOTE: THE OUTBD MID FLAP SKIN WAS REPAIRED AS PER B737-300 SRM AND PER AVIATION PARTNERS INSTRUCTIONS. (REF: JOB: A1H267 ITEM: 5-56).SDR SWIA2020033049541Vane · chafedLEFT HAND INBOARD FLAP VANE €“ LEADING EDGE MIDDLE €“ CHAFED (MARKED) (C CHECK) RO 3/27/2020 REPLACED LEFT HAND INBOARD FLAP VANE - LEADING EDGE MIDDLE CAP REF CRJ 200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.
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