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 FDEA2020082652014Bracket · corrodedLT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. RSDR SWAA2021051310648Skin · delaminatedLEFT WING OUTBOARD AFT FLAP. INBOARD LOWER CORNER HAS DELAM / REMOVED & REPLACED L/H O/B AFT FLAP PER AMM 27-51-22 SEC SAM 326 FOR INDIVIDUAL SIGN-OFFS OF WORK PERFORMED (S/N A1200710) POS L/H O/B TAG 111300 PN OFF/ON 113A3700-25 SN OFF 004290 SN ON 004188SDR SWIA202053037Vane · chafedLT INBOARD FLAP VANE LEADING EDGE IS CHAFED INBOARD OF FLAP VANE PANEL 584D/T. C-CHECK RO 10/4/2020. REPAIRED CHAFING ON LT INBOARD FLAP VANE LEADING EDGE INBOARD OF FLAP VANE PANEL 584D/T, REF CRJ200 SRM AND REO PERMANENT REPAIR.SDR SWIA202053036Vane · chafedLT INBOARD FLAP VANE LEADING EDGE IS CHAFED OUTBOARD OF FLAP VANE PANEL 584E/T. C-CHECK RO 10/4/2020. REPAIRED CHAFING ON LT INBOARD FLAP VANE LEADING EDGE OUTBOARD OF FLAP VANE PANEL 584E/T, REF CRJ200 SRM AND REO PERMANENT REPAIR.SDR SWIA202053035Vane · chafedLT INBOARD FLAP VANE LEADING IS CHAFED OUTBOARD OF FLAP VANE PANEL 584FT. C-CHECK RO 10/4/2020. REPAIRED CHAFING ON LT INBOARD FLAP VANE LEADING EDGE OUTBOARD OF FLAP VANE PANEL 584FT, REF CRJ200 SRM AND REO PERMANENT REPAIR.SDR SWIA202053033Vane · chafedRT INBOARD FLAP VANE LEADING EDGE IS CHAFED OUTBOARD OF FLAP VANE PANEL 684E/T. C-CHECK RO 10/4/2020. REPAIRED CHAFING ON RT INBOARD FLAP VANE LEADING EDGE OUTBOARD OF FLAP VANE PANEL 684E/T, REF CRJ200 SRM, REO PERMANENT REPAIR.SDR IPXA2020090869907Beam · crackedINSPECTION TYPE:2C RT WING OUTBOARD FLAP INBOARD FWD HINGE FAIRING OUTBOARD LOWER TEE ANGLE IS CRACKED AT AFT END. REMOVED CRACKED TEE ANGLE BEAM, FABRICATED AND INSTALLED AT RT WING OUTBOARD FLAP INBOARD HINGE IAW SRM 51-31-01. (MINOR)SDR IPXA2020090219768Angle · crackedINSPECTION TYPE:2C LT WING OUTBOARD FLAP INBOARD HINGE Z-ANGLE IS CRACKED. REPAIRED CRACKED ANGLE, FABRICATED AND INSTALLED AT LT OUTBOARD FLAP INBOARD HINGE IAW SRM 51-33-01. (MINOR)SDR IPXA2020090869902Tee Fitting · crackedINSPECTION TYPE: 2CRT WING OUTBOARD FLAP OUTBOARD AFT HINGE FAIRING OUTBOARD CENTER TEE ANGLE IS CRACKED. REMOVED CRACKED TEE, FABRICATED AND INSTALLED ON RT WING OUTBOARD FLAP, OUTBOARD AFT HINGE IAW SRM 51-33-01. (MINOR)SDR SWAA2020082010015Skin · delaminatedRT WING OUTBOARD AFT FLAP DELAMINATED ON UPPER AND LOWER SURFACE AT I/B TRAILING EDGE CORNER.. LOWER SKIN SPANWISE DELAMINATION MEASURES 1' WIDE X 7' LONG; UPPER SKIN DELAMINATION MEASURES 1.4'X .7' WIDE AND LOCATED AT I/B AFT CORNER. REMOVED AND REPLACED R/SDR SWIA202053298Vane · chafedRT WING INBOARD FLAP VANE IS CHAFED BETWEEN WS 97.70 TO WS 104.099. CHAFE IS APPROXIMATELY 1 INCH LONG 0.500 WIDE AND 0.010 DEEP. C-CHECK RO 10/13/2020. FOUND CHAFE ON RT WING INBOARD FLAP VANE BETWEEN WS 97.70 TO WS 104.099 IS OUT OF LIMITS TO BOMBARDIER RSDR SWIA202053297Skin · chafedLT WING INBOARD FLAP VANE SKIN IS CHAFED BETWEEN WS 139.924 TO WS 149.58. CHAFE IS APPROXIMATELY 1 INCH LONG 0.500 WIDE AND 0.010 DEEP. C-CHECK RO 10/13/2020. FOUND CHAFE ON LT WING INBOARD FLAP VANE SKIN BETWEEN WS 139.924 TO WS 149.58 TO BE OUT OF LIMITS.SDR IPXA2020082459450Rib · crackedINSPECTION TYPE:2CL/H WING I/B FLAP ELEPHANT EAR 4TH RIB FROM FWD. END IS CRACKED.REMOVED, FABRICATED AND REPLACED RIB IAW DWG. ARC2784 AND SRM 51-33-01. (MINOR).SDR FDEA202008181916Vane · corrodedLT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING. ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIGSDR FDEA2020090962084Skin · damagedLT WING, OUTBOARD FLAP OUTER SKIN APPROX I/B MIDDLE OF FLAP. PREVIOUS SHEET METAL REPAIR STRIP IS MISSING, MARKED. INSTALLED NEW REPAIR STRIP ON LT WING OUTBOARD FLAP OUTER SKIN APPROX I/B MIDDLE OF FLAP, REF SRM 57-20-00 FIGURE 11 VOL I.SDR FDEA2020082751893Support · corrodedLT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 4 SUPPORT FITTING. ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPSDR FDEA2020082751892Support · corrodedLT WING, OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 2 SUPPORT FITTING. ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPSDR FDEA2020082751890Support · corrodedRT WING, OUTBOARD FLAP VANE NR 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 1 SUPPORT FITTING. ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPSDR FDEA2020082751889Support · corrodedRT WING, OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 2 SUPPORT FITTING. ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPSDR FDEA2020082651891Support Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND WITHIN LIMIT AS PER MD-11 SRMSDR FDEA2020081851893Vane · corrodedLEFT HAND WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONSDR FDEA2020081851892Vane · corrodedLEFT HAND WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONSDR FDEA2020081851891Vane · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONSDR FDEA2020081851890Vane · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONSDR FDEA2020081851889Vane · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONSDR UIEA2020081751776Spar · corrodedRH IB FLAP REQUIRES REPLACEMENT DUE TO CORROSION FINDINGS ON REAR SPAR REMOVED AND REPLACED RH IB MAIN FLAP IAW B767 AMM 27-51-03. PERFORMED SATISFACTORY OPS CHECK IAW B767 AMM 27-51-00SDR FDEA202008141886Hinge Fitting · corrodedRIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE HOLE BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. SDR FDEA202008141885Hinge Fitting · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-52-03. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750SDR FDEA202008141884Hinge Fitting · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-52-03. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-52-03 AND E.A. # 1-5750-SDR FDEA202008141883Hinge Fitting · corrodedRIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHSDR FDEA202008141882Hinge Fitting · corrodedLEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHINSDR U2RA202009200006Skin · gougedWHILE ACCOMPLISHING TASK CARD 57-630-00-02 FOUND LEFT HAND OUTBOARD TRAILING EDGE MID FLAP INTERIOR 1 EA FASTENER HOLE ELONGATED ON SKIN PANEL. REPAIRED PER VT-SAA EA 747-5753-56-A8517 REV I/R.SDR FDEA202008111861Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MDSDR FDEA2020082611859Bracket · corrodedRIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- SDR SWIA202052569Skin · chafedON RT WING INBOARD FLAP, FLAP VANE LEADING EDGE PANEL (684ET) HAS GOUGE/CHAFE. C-CHECK RO 9/20/2020. REMOVED CHAFE ON PANEL 684ET, REF CRJ 700 SRM. EVALUATED BLENDED AREA ORGINAL THICKNESS .050" REMOVED .008" REMAINING .042". FOUND TO BE OUT OF LIMITS DSDR SWAA2020090307581Skin · damagedLT INBOARD AFT FLAP HAS SKIN DAMAGE ON LOWER SURFACE 5.5' FROM OUTBOARD END; 6' FROM T/E. LT INBOARD AFT FLAP SKIN DAMAGE ON LOWER SURFACE 5.5' FROM OUTBOARD END; 6' FROM T/E WAS REPAIRED IAW SRM 51-70-10-2R-2 AND SRM 51-70-10-2R-0.SDR UIEA2020081301649Skin · delaminatedLHW O/B FORE FLAP MOST O/B L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70- PAR.5.A, REV 89.SDR UIEA2020081301650Skin · delaminatedRHW I/B MID FLAP O/B L/E FOUND DELAMINATION. PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR.5.A REV #89.SDR SWAA2020081207009Skin · delaminatedLEFT WING OUTBOARD AFT FLAP INBOARD END; SKIN SEPERATED AT AFT CORNER / REPAIRED AREA OF DELAMINATION OF .50'D X 1.0'L ON LEFT WING AFT I/B EDGE OF AFT FLAP O/B. IAW B737-700 SRM 57-53-01-2R-14; SRM 51-70-10-2R-1; SRM 51-70-10-2R-0SDR U2RA202009200015Spindle · gougedWHILE ACCOMPLISHING TASK CARD 744-27-0003 FOUND RT OUTBOARD NR 8 FWD SPINDLE BEARING HOUSING GOUGED NEAR FAIL-SAFE LINK. REPAIRED PER VT-SAA EA 747-5740-56-A8471 REV A.SDR U2RA202009200014Spindle · gougedWHILE ACCOMPLISHING TASK CARD 744-27-0003 FOUND RT OUTBOARD NR 7 FWD FLAP SPINDLE BEARING HOUSING GOUGED NEAR FAILSAFE LINK. REPAIRED PER VT-SAA EA 747-5740-56-A8471 REV A.SDR SWAA2020092110152Skin · dentedDENTS ON INBOARD MAIN FLAP UPPER SURFACE, DENTED AREA NR 1 IS LOC AT 3' FROM OUTBOARD EDGE AND 3.25' FROM T/E, AND DENTED AREA NR 2 IS LOC AT 17' FROM OUTBOARD EDGE AND 9.25' FROM T/E AT LT WING (REFER TO DEFECT T328194). REPAIRED INBOARD MAIN FLAP UPPER SURFSDR FDEA2020090881827Support · corrodedRT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT RT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT, AS PER MD-11 SRM 57-50-02-2R FIGURE 201 SDR FDEA2020090481824Support Fitting · corrodedLT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 RSDR FDEA2020090481822Support · corrodedLT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. CORROSION AT LT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE. REWORKED BY MACHINING AND FOUND EXCEEDS LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 RSDR FDEA2020081081828Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC HOLE BORE WAS FOUND CORRODED.SDR FDEA2020081081827Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA2020081081824Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR FDEA2020081081822Vane · corrodedLEFT WING, OUTBOARD FLAP VANE NR 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORRODED.SDR SWAA2020082506991Skin · crackedL/H WING INBOARD MAIN T/E FLAP LOWER SURFACE SKIN HAS 0.250' CRACK; 12' FROM THE T/E & 15' FROM THE OUTBOARD EDGE; / CLEANED AND REPAIRED DAMAGE AREA AS MARKED ON L/W I/B MAIN FLAP T/E O/B WEDGE LOWER SURFACE AS PER B737 SRM 51-70-10-2R-4; REPAIR 4 PERMANENT
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