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 AALA202212023320Strut · corrodedAIRCRAFT IN BASE MAINTENANCE : CORROSION ON LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT. MAINTENANCE REPLACED FLAP INTERCONNECTING STRUT PER TASK CARD 26C57057001.SDR AALA202212029387Strut · corrodedAIRCRAFT IN BASE MAINTENANCE : CORROSION ON RIGHT WING TRAILING EDGE FLAP INTERCONNECTING STRUT. MAINTENANCE REPLACED FLAP INTERCONNECTING STRUT PER TASK CARD 26C67057001.SDR A6WA2023012308442Skin · corrodedCORROSION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498- WS100.009. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SECTION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498 WS100.009. CUTOUT DIMENSIONS L= 29.700X W= 21.250. RESTORED SURFSDR FDEA202211302862Skin · dentedRIGHT WING OUTBOARD AFT FLAP LOWER SURFACE IS DELAMINATED BETWEEN THE INBOARD AND OUTBOARD FLAP TRACKS REMOVED PAINT FINISH ON DENT AREA AND FOUND NO DELAMINATION OR BROKEN FIBERS. REPAIRED DENT IAW B757 SRM 57-53-01-2R FIG. 201 TABLE 2, SRM 51-70-04-0G PARASDR DALA2022120207712Strut · corrodedSHIP 3146 - CORROSION INTERCONNECTING STRUT OB FLAP. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OB FLAP ON RH WING AS PER A320 FAM AMM 27-51-44. (2518460)SDR FDEA202211292992Hinge Fitting · corrodedL/H O/B FLAP I/B FWD HINGE LOWER HINGE MOUNT HAS CORROSION ON THE I/B FACE. REPAIRED L/H O/B FLAP I/B FWD HINGE LOWER HINGE MOUNT I/B FACE IAW CMM 57-44-08 PG603 AND SOPM 20-10-6 PG12 DWG ARC0502.SDR FDEA202211292991Hinge Fitting · corrodedL/H O/B FLAP I/B FWD HINGE LOWER REAR SPAR MOUNT HAS CORROSION ON THE I/B AND O/B SIDE LUG FACES. REPAIRED L/H O/B FLAP I/B FWD HINGE LOWER REAR SPAR MOUNT I/B AND O/B SIDE LUG FACES IAW SPM 20-10-6 PG 17-18 AND DWG ARC0502.SDR FDEA202211292968Hinge Bracket · corrodedR/H O/B FLAP O/B FWD HINGE UPPER REAR SPARE MOUNT HAS CORROSION ON THE MATING SURFACE FACE AND OUTER SURFACE. REPLACED R/H O/B FLAP O/B FWD HINGE UPPER REAR SPARE MOUNT IAW EO 1-5750-7-5002-I-P2SDR A6WA202211298392Skin · dentedLEFT WING INBD FLAP HAS A DENT INBD BOTTOM SIDE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00, REPAIR -3, AND SRM 51-23-00.SDR DALA2023012300473Skin · delaminated(LOG 2515674) DURING INSPECTION FOUND DELAMINATED OB AFTFLAP EXTERNAL SKIN UPPER SURFACE LOCATED AT THE INBOARD EDGE AT RT WING. PERFORMED INTERIM REPAIR ON OB AFT FLAP INBOARD EDGE AT RT WING AS PER B737-900ER SRM 57-53-01-2R REPAIR 16.SDR REXA2022120102654Skin · chafedFLAP PANEL 584JB HAS CHAFE ON L/E CHAFED OUT OF LIMITS REPLACED PANEL 584JB P/N CC670-14178-1 LOCATED HOLES, TRIMMED EDGE. ALODINED, PRIMED, AND PAINTED IAW CRJ900 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-25-06-001-001-A01SDR AALA202211286007Skin · debondedAIRCRAFT WAS GROUNDED: DELAMINATED AREA FOUND ON LEFT OUTBOARD FLAP LEADING EDGE NOSE SKIN. LOCATED AT OTEF STA 44. PERFORMED BONDED REPAIR PER SRM AND EA.SDR IPXA2022112888503Skin · corrodedINSPECTION TYPE:N/ALEFT WING O/B FLAP UPPER SKIN CORRODED UNDER O/B STATIC WICK BASEREPAIRED DAMAGE IAW E.O. A300-5750-85209-BSDR A6WA202211268391Vane · chafedRIGHT WING INBOARD FLAP THE FLAP VANE CHAFING ON THE TOP INBOAD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE RT WING INBOARD FLAP VANE REF REO 601R-57-52-2469 REV-.SDR A6WA202211268388Vane · chafedLEFT WING INBOARD FLAP THE FLAP VANE IS CHAFFED ON THE TOP INBOARD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT WING INBOARD FLAP VANE IAW REO 601R-57-52-2469 REV-.SDR FDEA202211252996Hinge Fitting · damagedLEFT OTBD FLAP INBD AFT HINGE FITTING LOWER INBD LUG HAD A MIGRATED BUSHING. REPAIRED THE FLAP HINGE FITTING IAW EA 1-5750-T0372089 AND CMM 57- 52-04.SDR FDEA202211252995Hinge Fitting · corrodedRIGHT, OTBD FLAP INBD, AFT HINGE FITTING LWR INBD AND OTBD LUGS HAS MIGRATED BUSHING AND I/B LUG I/B FACE WAS CORRODED. REPAIRED THE HINGE IAW CMM 57-52-24 AND EA 1-5750-T0372030 A.SDR FDEA202211252962Hinge Fitting · damagedRH OB FLAP OB, AFT HINGE FITTING LWR IB AND O/B LUG HAS MIGRATED BUSHING REPAIRED R/H O/B FLAP O/B AFT HINGE FITITNG LWR I/B AND O/B LUG IAW MD-11 CMM 57-52-04.SDR FDEA202211252961Hinge Fitting · corrodedRH OB FLAP IB AFT HINGE FITTING OB AND I/B ACTUATOR MOUNT LUG HAS MIGRATED CORROSION BUSHING. REPAIRED R/H O/B FLAP I/B, AFT HINGE FITTING O/B AND I/B ACTUATOR MOUNT LUG IAW MD-11 CMM 57-52-04.SDR FDEA202211252960Hinge Fitting · corrodedR/H O/B FLAP FWD O/B HINGE FITTING HAS CORROSION ON UPPER LUGS. REPAIRED R/H O/B FLAP AFT O/B HINGE FITTING UPPER I/B AND O/B LUGS IAW MD-11 CMM 57-52- 04.SDR DALA2022112807547Strut · corrodedCORROSION INTERCONNECTING STRUT OB FLAP. REPLACED INTERCONNECTING STRUT OB FLAP ON LH WING AS PER A320 FAM AMM 27-51-44. (2510908)SDR SWAA2023010975209Wedge · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING 2022-664065<[01] TOOL USED; CALIPER P/N: 500-464; S/N: B17030933; DUE DATE: 17/OCT/23.;[02] TOOL USED: POSITECTOR P/N: NS2; S/N: 138341; DUE DATE: 07/JUN/2023. HOT BONDER P/N : HCS92SDR FDEA202211232967Vane · corrodedCORROSION ON RH OB FLAP VANE ABOVE FITTING C (CTR MOUNT) REPLACED R/H O/B FLAP O/B FLAP VINE IAW EO 1-5750-7-5002 I P4SDR FDEA202211232833Flap · delaminatedRH WING O/B MAIN FLAP UPPER SURFACE IS DELAMINATED APPROX 40" O/B FROMT THE I/B EDGE REPAIRED RH WING OB MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01 51-70-17. MAJOR REPAIRSDR FDEA202211232832Flap · delaminatedRH WING O/B MAIN FLAP UPPER SKIN IS DELAMINATED APROX 20" OB OF THE IB EDGE REPAIRED RH WING OB MAIN FLAP UPPER SKIN IAW B757 SRM 57-53-01 51-70-17. MAJOR REPAIRSDR FDEA202211232831Flap · delaminatedRH WING OB AFT FLAP UPPER SURFACE IS DELAMINATED BETWEEN THE I/B AND O/B TRACKS REPAIRED RH WING O/B AFT FLAP UPPER SURFACE IAW B757 SRM 57-53-01-2R AND 51-70-17-0G. MAJOR REPAIRSDR SWAA2022121374545Fairing · crackedFLAP TRACK FAIRING 542BB HAS A CRACK ON THE INNER SKIN 47 INCHES AFT OF THE LEADING EDGE, DAMAGE IS OUT OF ALLOWABLE LIMITS IAW SRM 57-53-70-1A-1, FIGURE 101, AND 104, ZONE 1, PARA 4A. TAP TESTED, DEBOND NOTED. REMOVED 1 INCH DIA OF INNER SKIN AND PARTIALSDR SWAA2022112374380Skin · delaminatedRT WING I/B MAIN FLAP DELAMINATED APPROX 11 FOR O/B EDGE. DAMAGE IS APPROX 11.5X5.7. PERFORMED TEMPORARY REPAIR OF RT WING INBD MAIN FLAP PER SRM 57-53-01-1A-1. PERFORMED INTERIM REPAIR OF RH WING INBD MAIN FLAP PER SRM 57-53-01-1A-1.SDR SWAA2022112173157Skin · delaminatedLT WING O/B AFT FLAP; INBOARD LOWER SURFACE IS DELAMINATED LT WING O/B AFT FLAP INBOARD LOWER SURFACE IS DELAMINATED AT OTEF STA 63 / [01] PERFORMED REPAIR IAW SRM 57-53-01-1A-5 STEP 9 ZONE 5.;[02] REVIEWED THE FAULT FOR CORRECT REPAIR REFERENCE SELECTION AND SDR CALA2022112103180Seal · missingPDA 2 LEFT WING OUTBD MAIN FLAP SEAL COMPLETELY MISSING AT INBOARD END ( WHERE INBD. & OUTBD FLAPS MEET ) -- SEE PHOTO PHOTO ADDED SEAL MISSING IS 42 INCHES LONG ... REF IPC 57-53-10-51 ITEM 100 INSTALLED NEW SEAL AT INBOARD END OF OUTBD MAIN FLAP LEFT WING ..SDR SWAA2022123073121Angle · crackedLEFT WING TRAILING EDGE RIB WBL 201.90 HAS WEB AFT EDGE FITTING ANGLE CRACKED. REMOVED AND REPLACED LT WING T/E AT WLB 201.90 WEB AFT EDGE FITTING ANGLE IAW SRM 51-40-02-0G-0.SDR FDEA202211182822Vane · delaminatedL/H O/B FLAP VANE #5 RUBSTRIP DELAM ( POS INTERIOR DELAM) REPAIRED L/H O/B FLAP VANE AT #5 RUBSTRIP AS REQUIRED PER SRM 51-71-00, VOL.II, PARA. #17 PG. 75-80, INADDITION WITH SRM 57-00-01, VOL.I, PG. 11, FIG.#4 REF. JPF STEPS ON BACK 4-11. MAJOR REPAIR. SDR SWIA202266947Skin · damagedREMOVE AND REPLACE LEFTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-51S (C-CHECK) REMOVED AND REPLACED LH INBD FLAP VANE SKIN PANEL P/N 601R14303-51S REF DWG #PL601R14302 REV.E AND CRJ 200 SRM 51-42-13 REV.39 DATED MAR-10-2021. COMPLIED WITH TASK CASDR SWIA202266946Skin · damagedREMOVE AND REPLACE RIGHTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-54S (C-CHECK) REMOVED AND INSTALLED NEW SKIN PANEL P/N: 601R14303-54S AT RIGHTHAND INBOARD FLAP VANE REF CRJ200 SRM 51-42-13 AND DWG# PL601R14302 REV E, COMPLIED WITH TASKCARD 51-SDR SWIA202266945Skin · wornREMOVE AND REPLACE RIGHTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-52S (C-CHECK RO 12/1/2022) REMOVED WORN LEADING EDGE VANE CAP AND INSTALLED NEW R/H MID FLAP VANE SKIN P/N: 601R14303-52. REF: CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV. E. COMPLISDR SWAA2022121371925Wedge · debondedDEBOND INBD MAIN FLAP WEDGE PANEL LOWER SURFACE, RT WING. PERFORMED INTERIM REPAIR IAW SRM 57-53-01-2R-18, REPAIR 18.SDR FDEA202211162828Vane · delaminatedLH OUTBD FLAP VANE #5 RUBSTRIP DELAM ( POS INTERIOR DELAM) REPAIRED PER SRM 57-00-01 FIG.4, SHEET 1SDR DALA2022111707411Bonding Plate · corrodedSHIP 3115 - CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING AS PER ER/A 602909-14 REV. (2499156)SDR SWAA2022112971180Wedge · delaminatedLEFT WING I/B MAIN FLAP T/E WEDGE LOWER SURFACE IS DELAMINATED. (MARKED) / [01] IDENTIFIED PANEL IAW SRM 57-53-02-0I-1 FIGURE 2 SHEET 4 TABLE 2 ITEM 30<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01-1A-1 PAR.4 A(7)(A)2)<BR><BR>DAMAGE IS TO BE RSDR SWAA2022112970927Fairing · cracked#3 FLAP TRACK FAIRING 542BB HAS A CRACK ON THE INNER SKIN 47' AFT OF THE LEADING EDGE AT O/B LOWER RADIUS / [01] IDENTIFIED MATERIAL OF PANEL 542BB IAW SRM 57-53-70-0I-3 FIGURE 1; 2; 4; AND 14; ITEM #1; TABLE 3 AND 12 <BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE SDR SWIA202266942Flap Track · wornLEFT WING FLAP TRACK 1A HAS DEPTH REDUCTION OF 0.052 INCH AT FORWARD END. FLAP TRACK REPLACED IAW AMM 57-54-25.SDR SWIA202266941Flap Track · wornRIGHT WING FLAP TRACK 1A HAS DEPTH REDUCTION OF .0.035 INCH AT FORWARD END. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLAP TRACK IAW AMM 57-54-25.SDR SWIA202266940Flap Track · wornRIGHT WING OTBD FLAP TRACK 2A HAS WIDTH REDUCTION OF .022 INCH ALONG ENTIRE LENGTH. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLAP TRACK IAW AMM 57-54-25.SDR FDEA202211122762Skin · damagedLH WING - OUTBOARD FLAP ASSY LEADING EDGE STRUCTURE IS DAMAGED AT LOCATION ADJACENT TO THE INBOARD SIDE OF THE OUTBOARD FLAP TRACK FAIRING. REPAIRED USING 767 SRM 57-53-01-2R.SDR AALA202211308315Fairing · crackedAIRCRAFT WAS NOT GROUNDED: LEFT INBOARD FLAP TRACK FAIRING HAS MULTIPLE CRACKS PERFORATIONS AND DAMAGE. INSTALLED LEFT INBOARD TAIL CONE FAIRING IAW AMM 27-51-18.SDR AALA202211118315Fairing · crackedAIRCRAFT WAS NOT GROUNDED: LEFT INBOARD FLAP TRACK FAIRING HAS MULTIPLE CRACKS PERFORATIONS AND DAMAGE. (OPEN)SDR DALA2022111007258Bolt · wornSHIP 3310 DURING REMOVAL OF LT #3 LINK FOUND LOWER HOLLOW BOLT WORN BEYOND LIMITS. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. REPLACED HOLLOW BOLT PER AMDS CARD 2754-4003. (2489396)SDR DALA2022111007257Retainer · damagedDURING REMOVAL OF LT #3 LINK FOUND PLATE RETAINER (LOCKING KEY) DAMAGED. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. REPLACED PLATE RETAINER (LOCKING KEY) PER AMDS CARD 2754-4003. (2489395)SDR SWAA2022111768662Bracket · crackedBRACKET FOUND TO BE CRACKED ON PANEL 651FB ( MARKED ) FORWARD SIDE I/B OF PANEL 651DB. / [01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02.;[02] REMOVED AND REPLACED BRACKET PER SRM 51-40-02.<BR>INSPECTION C/W.SDR AALA202212290411Rib · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD FLAP INBOARD RIB 1 LOWER FLANGE WORN / CHAFFED BETWEEN FLAP STRINGERS 2 AND 4. MAINTENANCE REPAIRED RIGHT WING OUTBOARD FLAP INBOARD RIB 1 LOWER FLANGE PER EA 341027.
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