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 AALA201710119021Strut · damagedLEFT FLAP INTERCONNECT STRUT ROCK END, EXTENDED OUT TO FAR CAN'T SEE THREADS THROUGH CHECK HOLE. REPLACED LEFT FLAP INTERCONNETING STRUT IAW 27-51-44.SDR SWIA2017102743929Skin · dentedRIGHT WING, INBD FLAP LOWER SKIN DENTED. REPAIRED IAW SRM.SDR SWIA201743903Vane · wornRIGHT INBD FLAP VANE HAS MULTIPLE WEAR SPOTS ON LEADING EDGE. REMOVED AND REPLACED THE THE FLAP VANE IAW SRM AND REO.SDR SWIA201743902Vane · wornLEFT INBD FLAP VANE HAS MULTIPLE WEAR SPOTS ON LEADING EDGE. REMOVED AND REPLACED THE FLAP VANE IAW SRM AND REO.SDR DALA2017100807363Skin · puncturedPUNCTURE IN THE LOWER SKIN ON THE AFT MOVABLE VANE OF THE RT WING TE FLAP. THE SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1, PAR 4.SDR AALA201710069005Skin · delaminatedDELAMINATION FOUND ON THE LOWER SKIN LEFT OTBD FLAP TE BETWEEN RIBS 4 AND 5, AT FLAP TRACK NR 3. REPAIRED THE SKIN IAW EA 273948. AIRCRAFT WAS GROUNDEDSDR A6WA2017101145338Skin · damagedLEFT WING INBD FLAP LOWER SKIN HAS DAMAGE IN LINE WITH MLG TIRES.SDR AALA201710279006Strut · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON INBOARD FLAP INTERCONNECTING STRUT RIGHT WING AT RIB 9. REMOVED AND REPLACED INTERCONNECTING STRUT PER AMM 27-51-44.SDR AALA201710279004Strut · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON INBOARD FLAP INTERCONNECTING STRUT LEFT WING AT RIB 9. REMOVED AND REPLACED INTERCONNECTING STRUT PER AMM 27-51-44.SDR SWAA2017100616919Flap · delaminatedRT WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED. R&R AFT FLAP PER AMM.SDR 2017FA0000508Flap · corrodedLEFT INBOARD FLAP CORRODED.SDR 2017FA0000507Flap · corrodedLEFT INBOARD FLAP CORRODED.SDR DALA2017100207188Vane · dentedDISBOND WAS FOUND ON DENTS AT AFT MOVABLE FLAP VANE LOWER SURFACE, ON THE LT WING. REPAIRED IAW SRM 57-53-01-2R-1.SDR DALA2017100207187Vane · debondedDISBONDING WAS FOUND ON DENTS AT THE INBD FIXED FLAP VANE LOWER SKIN XRS=137 OF THE RT WING. REPAIRED IAW SRM 57-53-01-2R-1.SDR DALA2017100207186Vane · debondedTHREE DISBONDS WERE FOUND AT OTBD FLAP FIXED VANE UPPER SURFACE OF THE LT WING. REPAIRED IAW SRM 57-53-01-2R-1, AND JIC 5552700.SDR FDEA201709303046Skin · crackedLEFT OTBD FLAP UPPER SKIN HAS A .75 INCH CRACK AT XOF 572. 5 INCHES FWD OF TRAILING EDGE. REPAIRED IAW SRM 57-00-01, FIG 4, SHT 2.SDR FDEA201709303045Skin · crackedLEFT OTBD FLAP UPPER SKIN HAS A 2.875 INCH CRACK AND A .4 INCH CRACK AT XOF 569. 8 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.SDR FDEA201709303044Skin · crackedLEFT OTBD FLAP UPPER SKIN HAS A 2.0 IN. CRACK AT XOF 563. 12 INCHES FWD OF TRAILING EDGE. REPAIR IAW SRM 57-00-01, FIG 4, SHT 2.SDR SWIA2017102743923Skin · dentedLEFT WING INBOARD FLAP LOWER SKIN DENTED. REPAIRED THE SKIN IAW SRM.SDR AALA201710319015Repair · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP UPPER SURFACE EXISTING REPAIR IS DISBONDED AT RIB 10. REPAIRED OUTBOARD TRAILING EDGE FLAP UPPER SURFACE PER EA 274090.SDR FDEA201709282777Tee Fitting · corrodedLT WING O/B FLAP VANE T FITTING 'B' FWD HOLE CORROSION. REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2R FIG 201.EXISTING SLOT HOLE:L=0.858Ï¿½ X W=0.558Ï¿½, FINAL SLOT HOLE:L=0.957Ï¿½ X W=0.657Ï¿½, MAXIMIMUM ALLOWABLE SLOT HOLE; LSDR FDEA201709282776Tee Fitting · corrodedRT WING O/B FLAP VANE 'T' FITTING 'F' FWD HOLE CORROSION. REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIG 201.EXISTING SLOT HOLE:L=0.864Ï¿½X W=0.608Ï¿½, FINAL HOLE:L=0.950Ï¿½ X W=0.650Ï¿½, MAXIMIMUM ALLOWABLE SLOT HOLE; L=0.9SDR FDEA201709282775Tee Fitting · corrodedRT WING O/B FLAP VANE 'T' FITTING 'E' FWD HOLE CORROSION. REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIG 201.EXISTING SLOT HOLE:L=0.889Ï¿½X W=0.638Ï¿½, FINAL SLOT HOLE:L=0.9745Ï¿½ X W=0.680Ï¿½, MAXIMIUM ALLOWABLE SLOT HOLE; SDR FDEA201709282774Hinge · corrodedRT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B LUG SURFACE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE LUG SURFACE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING THICKNESS 0.447", MATERIAL REMOVSDR FDEA201709282773Hinge · corrodedRT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING HOLE 1.195", FINAL HOLE 1.200", MAXIMUM ALLOWABLE HSDR A6WA2017100245316Vane · gougedLEFT INBD FLAP VANE CTR LEADING EDGE IS GOUGED.SDR SWAA2017092816705Flap · delaminatedLT WING OUTBOARD TRAILING EDGE AFT FLAP INBOARD CORNER DELAMINATED. R&R AFT FLAP ASSEMBLY PER MM.SDR FDEA201709252708Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE (FLAP SIDE) PIVOT INBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533C-PT5, STEP 2B, AND 2A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201709252707Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OTBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533E-PT6, STEP 2B, AND 2A. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GSDR FDEA201709252706Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE (FLAP SIDE) PIVOT INBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533E-PT6, STEP 2B, AND 2A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1SDR UIEA2017092501839Skin · damagedCHAFED, CREASE TYPE DENT ON UPPER LEADING EDGE SURFACE OF THE LT WING, INBD T/E FLAP. REMOVED AND REPLACED THE LT WING TE FLAP SKIN IAW SRM 51-40-04-0G-0.SDR UIEA2017092501838Skin · chafedRIGHT INBD SIDE OF AFT FLAP HAS CHAFE DAMAGE FROM FWD FLAP SEAL RETAINER. REMOVED AND REPLACED THE RT WING FLAP SKIN IAW SRM 51-40-04-0G-0.SDR IPXA2017092822122Skin · delaminatedINSPECTION TYPE: 3C, RT INBD FLAP DELAMINATED AT AT OTBD TRAILING EDGE. REPAIRED IAW SRM 57-50-02, REPAIR 2.SDR LR7A2017091901188Stiffener · crackedDURING SCHEDULED B1 CHECK UNDER JOB CARD HB2703, FOUND THE RT OUTBOARD WING REAR SPAR OWS173R FLAP TRACK SUPPORT VERTICAL STIFFENER WITH 3" CRACK, FS598 WL260. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.SDR LR7A2017091901187Angle · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND THE RT OUTBOARD WING OWS173R FLAP TRACK SUPPORT BRACKET ANGLE CRACKED, FS598 WL260. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70.SDR SCNA20170918191Rub Strip · damagedLT WING, OUTBOARD FLAP, INBD TRAILING EDGE RUB STRIP DAMAGED. REPLACED DAMAGE PORTION OF RUB STRIP ON LT WING OUTBOARD FLAP.SDR SCNA20170918184Mount · wornNR 6 FWD FLAP TRACK FAIRING FWD MOUNT IS WORN. REMOVED & REPLACED NR 6 FWD FLAP TRACK FWD FAIRING MOUNT.SDR SWAA2022020133581Flap · delaminatedL/H WING O/B AFT FLAP I/B LOWER SKIN DELAMINATED. DELAMINATION IS 10' X 7' DELAMINATION STARTS 1' FROM T/E AND 1 1/4' FROM I/B END / COMPLETED REPAIR PER REPAIR-57EA-04257 REINSPECT-ECTC 04259.SDR DALA2017092507133Stud · corrodedCORROSION ON RT FLAP HINGE FITTING AROUND OF OUTBD LOWER STUD XW 251. RT CENTER FLAP HINGE FITTING, WING FLAP HINGE MOUNTING STUD WERE REPLACED IAW AMM 57-55-25 AND HYDRAULIC LINES AND ACTUATOR CYLINDER WERE REMOVED AND INSTALLED IAW AMM 27-55-03 AND LEAK ANSDR SWAA2017091816402Skin · delaminatedLT WING OUTBOARD AFT FLAP INBOARD LOWER SKIN DELAMINATED. REPAIRED AFT FLAP PER EA.SDR DALA2017091706928Fitting · crackedCRACKED FITTING ON THE LT FLAP INTERNAL STRUCTURE XCW 65. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, SRM 51-41-05-0G, AMM 20-00-02, AND AMM 20-50-01.SDR DALA2017091606914Vane · corrodedCORROSION ON FITTING AT THE RT WING OTBD FLAP CENTER GUIDE VANE. THE FLAP CENTER GUIDE VANE WAS REPLACED IAW AMDS 2710-4628, AND 2710-4629.SDR CALA2017091503161Skin · puncturedRIGHT WING AFT FLAP HAS A .50 INCH ROUND HOLE 24 INCHES INBD AND 12 INCHES UP FROM THE LOWER EDGE ON OTBD END OF FLAP. REMOVED AND REPLACED THE RT OTBD AFT FLAP IAW AMM 27-51-22, 27-5 1-23, AND 27-51-31. RIG AND OPS CHECKED GOODSDR FDEA201709142565Skin · wornLEFT WING, OTBD MAIN FLAP, INBD UPPER LEADING EDGE GOUGED. INSTALLED A REPAIR DOUBLER IAW SRM 57-53-01-2R REPAIR 5, SRM 51-70-10-2R, AND EA F-5750-T0335592 P1. MAJOR REPAIR.,SDR DALA2017091506901Intercostal · crackedCRACKED INTERCOSTAL ON LT FLAP, XCW 65. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-05-0G, SRM 51-41-02-0G, AND DWG 9958001, REV U.SDR SWAA2017100616923Skin · delaminatedLT WING OUTBOARD TRAILING EDGE LOWER SKIN FLAP DELAMINATED. R&R AFT FLAP IAW AMM.SDR AALA201709269026Strut · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING INBOARD FLAP INTERCONNECTING STRUT BETWEEN RIBS 9 AND 10. REPLACED INTERCONNECTING STRUT PER AMM 27-51-44.SDR AALA201709269025Strut · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING INBOARD FLAP INTERCONNECTING STRUT BETWEEN RIBS 8 AND 9. REPLACED INTERCONNECTING STRUT PER AMM 27-51-44.SDR FDEA2017091922504Hinge Bracket · corrodedTHE BORE WAS REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-08. EXISTING HOLE DIA: 0.873", FINAL HOLE DIA: 0.983", MAXIMUM ALLOWABLE HOLE DIA: 0.983". RIGHT WING OUTBD FLAP INBD FWD HINGE REMOVED AND REPLACED AS PER AMM 57-53-01-4. REPAIR CLASSIFIESDR SWAA2017091316331Flap · delaminatedRT WING OUTBOARD MAIN FLAP DELAMINATED. REPAIRED MAIN FLAP PER EA.
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