JASC 5744
Service difficulty reports · 2,721
Reports filed under 5744 · Wing, Control Surface Attach Fittings, 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 = '5744' 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 = '5744' 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 IPXA2024080596006Support · cracked**SUPPLEMENTAL SDR**FAULT - CRACK - BRACKET, R/H WING NO.7 SLAT LOWER DOOR. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 89. PERFORMED CHROMIC ACID ANODIZE IAW EGAT WORK SHEET NO. 40586 STEP 7 & SPWPS-AN-004 REV 23 AND SPDS-AN REV 39 (REPLACE) REVIEWED TASK PER GSDR VNAA202409020008Fitting · corrodedAFTER REMOVAL OF LH AILERON BUSHINGS AN BEARINGS, CORROSION AND WEAR WERE FOUND ON LUG BORE OF L 1, L2, L4, LS AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON. LUG BORE OF L1, L2, LS AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON WERE REPAIRED PER PER REO 67SDR VNAA20240724004Lug · corrodedCORROSION ON HOUSING OF LUG 5 AT RH AILERON WAS FOUND. LUG 5 WAS REPAIRED PER REO 670-57-61-237 REV ORIGINALSDR REXA2024062000448Bushing · corroded"THE R/H AILERON HAS CORROSION & PITTING INSIDE OF THE LUG BORE LABELED ""B"". REMOVAL OF DAMAGE IS REQUIRED. COMPLIED WITH STEPS F. #1 - #4 OF BOMBARDIER REO 670-57-61-237 REV - DATED 2017-07-25. STEP F. #3 - FINAL REAMED DIAMETER OF LUG ""B"" IS (0.9538""). SDR REXA2024062000447Lug · corroded"THE L/H AILERON HAS CORROSION & PITTING INSIDE OF THE LUG BORE LABELED ""C"". REMOVAL OF DAMAGE IS REQUIRED. REPAIRED IAW REO 670-57-61-237 REV -- DATED 2017-07-25 REFERENCE HR0043033 FOR INSTALLATION OF FABRICATED BUSHING"SDR SWI2024F00703Hinge Fitting · gougedTHE RH AILERON HINGE FITTING #3 ON THE WING SIDE HAS MULTIPLE GOUGES. (MARKED). REJECTION COMMENTS:SDR MUST BE YES (C-CHECK RO 8/22/2024) BLENDED OUT MULTIPLE GOUDES AT RH AILERON HINGE FITTING # 3 REF-CRJ-700 REO 670-57-51-555 REV -- 2024-07-01. COMPLISDR SWI2024F00702Hinge Fitting · gougedTHE RH AILERON HINGE FITTING #2 ON THE WING SIDE HAS MULTIPLE GOUGES. (MARKED). (C-CHECK RO 8/22/2024) BLENDED OUT MULTIPLE GOUDES AT RH AILERON HINGE FITTING # 2 REF-CRJ-700 REO 670-57-51-555 REV -- 2024-07-01. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR VNAA202407030012Lug · corrodedAFTER BUSHING REMOVAL IN REF CARDTRFKE00BN3Q8:271500-RH-PSA, SCRATCHES ON LUG R5, LUG R6 ON AILERON RH. SCRATCHES ON LUG R5, LUG R6 ON AILERON RH WERE REPAIRED PER REO 670-57-61-237 REV - -SDR VNAA202407030011Lug · corrodedAFTER BUSHING REMOVAL IN REF CARD TRFKE00BN30R:271500-LH-PSA, WEAR ON LUG L2, LUG L5 ON AILERON LH. CORROSION AND WEAR ON LUG L2, LUG L5 ON AILERON LH WERE REPAIRED PER REO 670-57-61-237 REV - - & REO 690-57-61-327 REV. - -SDR SWIA20240823525Lug · damagedINBOARD FLAP, OUTBOARD HINGE ARM, FORWARD LUG HAS IMPACT DAMAGE. (C-CHECK RO 8/22/2024) BLENDED OUTB HINGE ARM REF CRJ-700 SRM 51-12-00-001-001-A01 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-57-52-560 REV -- DATE 2024-07-09 ALL STEPS OF REO COMSDR IXXA2024051108Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED AT MID AUX TRACK.SDR IXXA2024051107Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED. OB OF MID AUX TRACK.SDR DALA2024051305128Trunnion · gougedSHIP 3114 L/H FLAP TRUNNION TORSION SUPPORT ASSY HAS GOUGING DAMAGE. CORRECTIVE ACTION: EVAL & REPAIRED GOUGE ON L/H FLAP TRUNNION TORSION SUPPORT ASSY IAW AD CARD 5751- 01025-01C. (0336225)SDR DALA2024051305127Trunnion · gougedSHIP 3114 R/H FLAP TRUNNION TORSION ASSY HAS GOUGING DAMAGE. CORRECTIVE ACTION: REPAIRED PER AD CARD 5757-01025-07D. (0336221)SDR SWIA2024F00553Attach Fitting · crackedRH WING SLAT TRACK 1-3 CANNISTER ATTACH FITTING, INSIDE FUEL PANEL 651AB, POSSIBLE CRACKS (MARKED) (C-CHECK RO 7/9/2024) CRACK VERIFIED IN R/H SLAT TRACK CANISTER 1-3. REPAIRED PER REO 670-57-42-577 REV -- DATE 2016-12-02, CRJ900SRM 51-42-06-001-001-A0SDR SWIA20240710507Attach Fitting · crackedLH WING SLAT TRACK 1-3 CANNISTER ATTACH FITTING, INSIDE FUEL PANEL 551AB, POSSIBLE CRACKS (MARKED) (C-CHECK RO 7/9/2024) COMPLIED WITH REPAIR OF LH WING SLAT TRACK 1-3 CANNISTER REF REO 670-57-42-577 REV -- DATED 2016-12-02, CRJ900 SRM 51-42-21-001-00SDR VNAA20240619006Lug · corrodedSCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 1, LUG 2 AND LUG 6 AT RH AILERON WAS FOUND WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES FSDR VNAA20240619007Lug · corrodedSCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WAS FOUND. SCRATCH ON HOUSING OF LUG 2 AND LUG 5 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES FSDR VNAA20240619001Hinge · corrodedCORROSION ON HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 2 (OUTBD AND INBD) FITTING 3 (INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - - AND ETI-900-24-004 REV. SDR VNAA20240618012Lug · scratchedHOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD), FITTING 3 (OUTBD AND INBD) & FITTING 4 (OUTBD AND INBD) AT RH WING REAR SPAR WERE REPAIRED PERSDR VNAA20240618011Lug · scratchedHOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WAS FOUND. HOUSING OF HINGE FITTING 1 (OUTBD) FITTING 4 (OUTBD AND INBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-357 REV. - -SDR VNAA20240618003Hinge · corrodedCENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON. CENTER FITTING BORE LUG R1, R2, R5 AND R6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-237 REV--SDR VNAA202406190007Hinge · corrodedCENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON. CENTER FITTING BORE LUG L1, L2, L5 AND L6 AT LH AILERON.SDR VNAA202404170001Fitting · gougedGOUGE DAMAGE TO LH WING TRAILING EDGE MACHINED FITTINGS AT WS199.40, WS202.67 AND WS231.23) CAUSED BY INCORRECT HARDWARE ORIENTATION. DAMAGE CLASSIFIED AND REPAIRED IAW MHIRJ REO 690-57-51-332 REV --.SDR SWIA202405080326Attach Fitting · crackedRH SLAT TRACK 1-3, TRACK CANNISTER ATTACH FITTING CRACKED INSIDE FUEL PANEL 651AB (MARKED) (C-CHECK RO 5/6/2024) COMPLIED WITH REO 670-57-42-577 REV-- DATED: 2016-12-02 AND REPAIRED RH SLAT TRACK 1-3 TRACK CANNISTER ATTACH FITTING. SEE CONTINUATION FOR DESDR JJBA20240322085Support · crackedRH AILERON SUPPORT ACTUATOR ASSY CRACKED. REMOVAL OF CRACKED SUPPORT ASSY IN PROGRESS. RH AILERON SUPPORT ACTUATOR ASSY REMOVED DUE TO CRACK. RH AILERON SUPPORT ACTUATOR ASSY REPLACED.SDR FDEA202403030240Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVESDR FDEA202403030239Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-07. REPAIR EVALUATED AND FOUND SDR FDEA202403030238Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSSDR FDEA202403030237Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATSDR FDEA202403030236Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZED REPAIR BUSHING FABRICATEDSDR FDEA202403030235Bracket · 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 REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSSDR FDEA202403030234Bracket · 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 REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. OVERSIZSDR FDEA202403030233Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZEDSDR FDEA202403030232Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE SURFACE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. REPSDR FDEA202403030231Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED SDR FDEA202403030230Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. REPAIR SDR FDEA202403030229Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED SDR FDEA202403030228Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-52-03. OVERSIZED BSDR IPXA2024022974604Hinge · corrodedREPLACE R/H WING I/B FLAP O/B AFT FLAP HINGE DUE TO HEAVY CORROSION VERIFIED STEP 11 IS C/W AND AUDIT C/W. REMOVE AND REPLACE INBOARD FLAP OUTBOARD HINGE ASSEMBLY P/N ARC2512-504 PER CMM 57-52-03.SDR VNAA202401210014Fitting · corrodedCORROSION ON CENTER HINGE FITTING INNER LUG BORE, LUG L1, L2 AND L6 WAS FOUND. CORROSION ON CENTER HINGE FITTING INNER LUG BORE, LUG L1, L2 AND L6 WERE REPAIRED PER REO 670-57-61-237 REV. --SDR DALA2024010800281Unknown · unknownSHIP 3124 CORROSION ON PLAIN BUSH AILERON HINGE #5 ON L/H AILERON (2 E/A). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #5 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0141640)SDR DALA2024010800280Unknown · unknownSHIP 3124 CORROSION ON PLAIN BUSH AILERON HINGE #4 ON L/H AILERON (2 E/A). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #4 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0141638)SDR DALA2024010800279Unknown · unknownSHIP 3124 CORROSION ON PLAIN BUSH AILERON HINGE #2 ON L/H AILERON (2 E/A). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #2 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0141630)SDR DALA2024010800278Unknown · unknownSHIP 3124 CORROSION ON PLAIN BUSH AT I/B AILERON ACTUATOR BRACKET I/B LUG ON L/H AILERON (1 E/A). CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON I/B AILERON ACTUATOR BRACKET I/B LUG ON LH AILERON AS PER AIRBUS CMM 57-61-21. (0141626)SDR DALA2024010500156Unknown · unknownSHIP 3124 CORROSION ON PLAIN BUSH AT AILERON HINGE 1 I/B LUG ON L/H AILERON. CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) ON HINGE #1 OF L/H AILERON AS PER AIRBUS CMM 57-61-21. (0139854)SDR SWI2024031200226Hinge Fitting · gougedLH AILERON OUTBD #4 HINGE FITTING, ON THE AILERON, HAS A SMALL GOUGE ON THE LOBE (MARKED) (C-CHECK RO 3/9/2024) REPAIRED DAMAGE AT LH AILERON OUTBD #4 HINGE FITTING, ON THE AILERON SIDE, AIL STA 364.016. REF REO 601R-57-61-850 REV--, DATED 2023-12-28. COMSDR SWI2024031200225Hinge Fitting · gougedRH AILERON CENTER HINGE #3, ON THE WING, HAS A SMALL GOUGE ON THE LOBE (MARKED) (C-CHECK RO 3/9/2024) BLENDED OUT GOUGE AT RH AILERON HINGE FITTING NO.3, ON THE WING SIDE . REF. CRJ-200 SRM 51-12-00. RECEIVEDAND COMPLIED WITH ALL STEPS OF REO#601R-57-51-1SDR SWI202403120224Fitting · gougedLH AILERON CENTER FITTING #3, ON THE WING, HAS A GOUGE ON THE LOWER STRUCTURE OUTBD EDGE (MARKED) (C-CHECK RO 3/9/2024) BLENDED OUT CHAFE/GOUGE ON THE LH AILERON CENTER FITTING#3, ON THE WING LOWER STRUCTURE OUTBD EDGE. REF CRJ 200 SRM 51-12-00. RECEIVED ASDR DALA2023110309071Unknown · unknownSHIP 3119 CORROSION ON AILERON HINGE PINS LH WING (4 E/A). CORRECTIVE ACTION: REPLACED AILERON HINGE PINS LH WING (4 E/A) IAW AMDS CARD 5760-1010S-LT. (0046841)
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