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 IPXA2020090359694Vane · delaminatedINSPECTION TYPE:2C RT WING I/B FLAP VANE LOWER SKIN IS DELAMINATED. REMOVED AND REPLACED RT WING I/B FLAP VANE IAW AMM 27-50-22-400-801 (MINOR).SDR IPXA2020082159284Vane · puncturedINSPECTION TYPE:2C, LEFT I/B FLAP VANE HAS PUNCTURE DAMAGE ON LOWER SURFACE BETWEEN STA. XIFH 197.6 TO 196.1 & 14" FROM T/EREPAIRED PUNCTURED L/H I/B FLAP VANELOWER SURFACE BETWEEN STA. XIFH 197.6 TO 196.1 AND 14" FROM T/E IAW SRM 51-71-00 REPAIR GENERAL PARASDR SWIA2020091652528Attach Fitting · nickedLT OUTBOARD FLAP WS 220 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 220.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.SDR SWIA2020091652527Attach Fitting · nickedLT OUTBOARD FLAP WS 178 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 178.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD. SDR FDEA2020082741765Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE. REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND UPPER BARREL NUT FACE EXCEEDS LIMIT BASDR FDEA2020080541765Hinge · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION.SDR U2RA202009200004Skin · gougedWHILE ACCOMPLISHING TASK CARD 57-630-00-02 FOUND LEFT HAND TRAILING EDGE MID FLAP INTERIOR, 1 EA PANEL LANDING FASTENER HOLE GOUGED WITH TOOLING MARKS. REPAIRED PER VT-SAA EA 747-5753-56-A8500 REV A.SDR DU4R2020080320053Wedge · damagedDURING SCHEDULED WORK, LT FLAP T/E WEDGE INDICATED PREVIOUS DAMAGE.SDR U2RA202009210001Flap Track · corrodedWHILE ACCOMPLISHING TASK CARD 57-866-01-01 FOUND NR 3 FLAP TRACK FIXED DRIVE LINK OUTBOARD LUG CORRODED. REPAIRED PER VT-SAA EA 747-5740-56-A8470 REV A.SDR U2RA202009200020Rub Strip · gougedWHILE ACCOMPLISHING TASK CARD 57-946-01-01 FOUND RIGHT WING TRAILING EDGE FLAP INBOARD PHENOLIC RUB-STRIP DAMAGED. REPAIRED PER VT-SAA EA 747-5740-56-A8506 REV A.SDR SWIA202052662Skin · chafedLT WING PANEL 584EB IS CHAFED. C-CHECK RO 9/21/2020. REMOVED DAMAGE FROM FLAP PANEL 584EB, REF CRJ 700 SRM. PANEL OUT OF LIMITS. ORDERED AND RECEIVED NEW FLAP PANEL 584EB, SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202052661Skin · chafedFLAP PANEL 684EB CHAFED. C-CHECK RO 9/21/2020. REMOVED DAMAGE FROM FLAP PANEL 684EB, REF CRJ 700 SRM. PANEL OUT OF LIMITS. ORDERED AND RECEIVED NEW FLAP PANEL 684EB, SEE CONTINUATION CARD FOR DETAILS.SDR SWIA202052660Skin · chafedINBOARD FLAP PANEL 684BB CHAFFED INBOARD OUTER SKIN SURFACE. C-CHECK RO 9/21/2020. BLENDED OUT CHAFE ON INBOARD OUT SKIN SURFACE, INBOARD FLAP PANEL 684BB, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.SDR UIEA2020080401701Skin · delaminatedLEFT WING OTBD FLAP, OTBD L/E WAS FOUND DELAMINATED FROM OTBD 12 INCHES. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5.A, REV 88.SDR UIEA2020080401702Skin · delaminatedLEFT WING OTBD FLAP L/E FOUND DELAMINATED FROM OTBD 30 INCHES. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5.A, REV 88.SDR UIEA2020080401703Skin · delaminatedRIGHT WING INBD FORE FLAP T/E EDGE UPPER AND LOWER SURFACES WERE FOUND DELAMINATED FROM INBD 109 INCHES. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5.A, REV 88.SDR UIEA2020080401704Skin · delaminatedLEFT WING INBD FORE FLAP MID AREA OF L/E FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5.A, REV 88.SDR UIEA2020080401707Skin · delaminatedLEFT WING INBD AFT FLAP M/D L/E FAIRING AREA FOUND DELAMINATED. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5.A, REV 88.SDR UIEA2020080401708Skin · delaminatedLEFT WING OTBD FORE FLAP L/E MID AREA FOUND DELAMINATED FROM INBD 126 INCHES. PERFORMED A PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07 PAR 5.A REV 88.SDR UIEA2020080401709Skin · delaminatedLOWER OTBD FORE FLAP L/E MID AREA FOUND DELAMINATED FROM INBD 196 INCHES. PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR 5.A REV 88.SDR SWAA2020080305133Skin · delaminatedRIGHT WING AFT OUTBOARD FLAP UPPER SURFACE DELAMINATED 3' OUTBOARD OF INBOARD EDGE; 3' UP FROM TRAILING EDGE. DAMAGE MEASURES 1.7 X 3' / RIGHT WING AFT OUTBOARD FLAP UPPER SURFACE DELAMINATED 3' OUTBOARD OF INBOARD EDGE; 3' UP FROM TRAILING EDGE. DAMAGE MEASURSDR SWIA2020091652555Vane · chafedTHE LT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 3 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 141.00, REF CRJ200 SRM. OPS CHECKS GOOD.SDR SWIA2020091652554Vane · chafedTHE LT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 2 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 105.02, REF CRJ200 SRM. OPS CHECKS GOOD.SDR SWIA2020091652553Vane · chafedTHE LT INBOARD FLAP VANE IS CHAFED INBOARD OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 56.55, REF CRJ200 SRM. OPS CHECKS GOOD.SDR SWIA2020091652552Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 3 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 141.00 (PN K601R41302-7), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA2020091652551Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 2 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 105.02 (PN K601R41302-7), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA2020091652550Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED INBOARD OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 56.55 (P/N K601R41302-10), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA2020091652503Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED ON TRAILING EDGE UPPER SIDE OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFE ON THE RT INBD FLAP VANE TRAILING EDGE UPPER SIDE OF THE NR 1 ACTUATOR, REF CRJ-200 SRM. NDT COMPLIED WITH (SEE NDT REPORT FOR MSDR KCSA202007301131Attach Fitting · crackedROLLER ATTACH FITTING AT WBL 443.83 IS CRACKED ON RH IB MID FLAPSDR FDEA202007301727Hinge Fitting · corrodedRIGHT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORRODED. WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUND DATA FOR THE PIVOT BORE SHSDR FDEA202007301726Hinge Fitting · corrodedLEFT WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORRODED. 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 BUSHING FABRICATED BY MACHINING AND INSTALLSDR SWAA2021071304746Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP DELAMED AT INBOARD AFT CORNER / REPAIRED RT WING O/B FLAP; I/B AFT CORNER IAW SRM 57-53-01-2R-4 REV. 71; SRM 51-70-10-2R-1 REV. 71; AND SRM 51-70-10-2R-0 REV. 71 FINISHED IAW AMM 51-21-99-300-801 REV 72SDR FDEA202007291703Hinge Bracket · corrodedRT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE). REWORKED AND FOUND EXCEEDS LIMIT, AS PER MD-11 CMM 57- 52-03.SDR FDEA2020090429701Bracket · corrodedLT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (F AND G HOLE). REWORKED AND FOUND EXCEEDS LIMIT AS PER MD-11 CMM 57- 52-03SDR FDEA2020082891704Bracket · corrodedRT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE). REWORKED AND FOUND EXCEEDS LIMIT, AS PER MD-11 CMM 57-52-03.SDR FDEA2020073091704Hinge Fitting · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.SDR FDEA2020073091703Hinge Fitting · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.SDR FDEA202007291702Hinge Fitting · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS. 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. NR 1-575SDR FDEA2020073091701Hinge Fitting · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS.SDR SWIA2020090952359Support Fitting · corrodedRT WING OUTBOARD FLAP, OUTBOARD HINGE BOX FWD SUPPORT LUG FITTING HARDWARE IS CORRODED. C-CHECK RO 9/5/2020. REMOVED & REPLACED FWD AND AFT BOLTS AND NUTS FROM RT OUTBOARD FLAP OUTBOARD HINGE BOX FWD LUG, REF CRJ700 AMM. ALL CHECKS GOOD.SDR SWIA2020090952358Support Fitting · corrodedLT WING OUTBOARD FLAP, OUTBOARD HINGE BOX FWD SUPPORT LUG FITTING HARDWARE IS CORRODED. C-CHECK RO 9/5/2020. REMOVED AND WET INSTALLED 4 EACH NUTS, WASHERS, AND BOLTS AT WS264 HINGEBOX SUPPORT STRUCTURE, REF CRJ 700 AMM. ALL CHECKS GOOD.SDR FDEA202007271674Hinge Fitting · corrodedLT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LT WING, FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED BUSSDR FDEA2020082761660Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08SDR FDEA2020082761659Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08SDR FDEA2020082761658Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATED BYSDR FDEA2020082761657Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-4SDR FDEA202002761656Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09SDR FDEA2020082761655Bracket · corrodedRT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (NR 3 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-SDR IPXA2020072768238Lug · wornINSPECTION TYPE:S/V, RIGHT WING OTBD FLAP INBD AFT HINGE OTBD ACTUATOR LUG BUSHING LOOSE. REPAIRED THE LOOSE BUSHING IAW SOPM 20-20-07 & CMM 57-52-04. (MINOR)SDR IPXA2020072768236Lug · wornINSPECTION TYPE:S/V, RIGHT WING OTBD FLAP OTBD AFT HINGE FITTING OTBD ACTUATOR LUG BUSHING LOOSE. REPAIRED THE LOOSE BUSHING IAW CMM 57-52-04 & SOPM 20-20-7. (MINOR)
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