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 AALA202206069342Strap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING LEADING EDGE LOWER ATTACH STRAP LOCATED BETWEEN OUTBOARD SLAT STATIONS (OSS) 60 AND 79. REPAIRED PER EA 336267 AND SRM 57-20-01-2R.SDR DALA2022041902717None · noneSHIP 3259 CORROSION HINGE ARM 3 AILERON BUSHING ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING PER A320 SRM 51-72-12. (2196191)SDR DALA2022041902716None · noneSHIP 3259 CORROSION HINGE ARM 1 AILERON BUSHING ON LH WING. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-72-12. (2196189)SDR CALA2022040600895None · missingPDA 3 LEFT WING #2 SLAT HAS ONE FASTENER HEAD BROKEN OFF/MISSING AND ANOTHER LOOSE AT ACTUATOR ATTACH POINT -- SEE PHOTO PHOTO ADDED PHOTO ADDED PHOTO ADDED UPDATE -- ONE FASTENER MISSING AND 3 FASTENERS LOOSE -- SEE PHOTO INSTALLED MISSING HI LOCK AND TIGHTENSDR VNAA20220326994Skin · dentedR/H INBOARD FLAP UPPER SKIN DENTED.SDR DALA2022032301921None · noneSHIP 3270 CORROSION BUSHING OB SERVO CONTROL ACTUATOR AILERON INBOARD LUG ON LH WING. CORRECTIVE ACTION: REPLACED BUSHING (1E/A) ON I/B LUG O/B SERVO CONTROL ACTUATOR AILERON LH WING AS PER A320 SRM 51-72-12. OK FOR SERVICE. (2163950)SDR CALA2022011000106Skin · missingPDA 3 LEFT WING #1 SLAT SKIN TAB AT OUTBOARD AUX TRACK FOUND MISSING. PLACED ON CDL PER LP 7782538.SDR LR7A2021121303037Flap Track · crackedDURING SCHEDULED C-9 CHECK UNDER JOB CARD HC5711, FOUND LH WING FLAP WELL TRACK ASSY FITTING CRACKED THOUGH FASTENER HOLE AT OWS241L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0339. / PSE# 57-50-16, AD 2012-06-09SDR JJBA2021090885005Attach Fitting · corrodedLEFT WING AILERON ATTACHMENT LUGS "4" EACH HAVE LIGHT SURFACE CORROSION EXPOSED AND BARE METAL. BLENDED CORROSION 4 EACH LUGS.SDR SWIA2021091360957Attach Fitting · gougedRH WING FLAP HINGEBOX ATTACH FITTING AT WS54.55 IS GOUGED NEAR AFT INBOARD BOLT. (MARKED) (C-CHECK RO 9/8/2021) REMOVED DAMAGE FROM RH WING FLAP HINEBOX ATTACH FITTING AT WS54.55. REF CRJ900 SRM 51-12-00-001-001-A01. RECEIVED AND COMPLIED WITH ALL STEPSSDR JJBA20210729004Attach Fitting · corrodedRIGHT WING AILERON ATTACHMENT LUGS "4" EACH HAVE LIGHT SURFACE CORROSION EXPOSED AND BARE METAL. BLENDED CORROSION 4 EACH AREAS ON RIGHT AILERON LUGS UPPER SURFACE.SDR MASA20210728312Hinge Arm · gougedGOUGE ON LH INBOARD FLAP HINGE ARM FITTING AT WS54.55 REPAIRED ON BOMBARDIER REO 690-57-52-384
DEFECT LOCATION: LH IB HINGE ARM AT WS54.55SDR SWIA2021091360955Attach Bracket · crackedRH SLAT TRACK CANNISTER 1-3 ATTACH BRACKET INSIDE FUEL PANEL 651AB IS CRACKED (MARKED) (C-CHECK RO 9/8/2021) PERFORMED PERMANENT REPAIR ON R/H SLAT TRACK CANISTER 1-3 ATTACH BRACKET. REF. MHIRJ REO 670-57-42-577 REV. €“ DATED: 2016-12-02. SEE CONTINUATSDR MASA20210726302Hinge Box · damagedLEFT FLAP HINGE BOX ASSY AT WS 178 DAMAGED | REPAIRED IAW MHI RJ REO 690-57-54-031SDR SWIA202158696Attach Bracket · crackedL/H WING INBD FLAP OUTBD FAIRING ATTACH BRACKET CRACKED. (C-CHECK RO 6/04/2021) REMOVED AND REPLACED L/H WING INBD FLAP OUTBD FAIRING ATTACH BRACKET WITH NEW BRACKET P/N CC670-14188-3 REF. CRJ 700 SRM 51-42-06-001-001-A01.SDR SWAA2021052476030Mount · looseR/H FLAP DEFLECTION RIB UPPER SHELF PANEL ATTACHMENT MOUNT LOOSE AND WORN / REPAIRED IAW SRM 57-51-02-2R-1 REPAIR 1 AND SRM 57-51-02-2R-4 REPAIR 4; REF EA# 20-157-00906.SDR SWIA202158339Bolt · corroded* RIGHT HAND WING OUTBOARD FLAP , OUTBOARD FLAP ACTUATOR MOUNT BOLT AND WASHER CORRODED. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED RH OUTBOARD FLAP, OUTBOARD FLAP ACTUATOR MOUNT BOLT AND WASHER. REF: CRJ200 57-21-35-000-801 AND CRJ200 AMM 57-21-35-40SDR DALA2021030801325Attach Fitting · crackedDURING INSPECTION MAINTENANCE FOUND CRACK OF 0.093" ON BOX SUPPORT ASSY OF THE AILERON TRIM ACTUATOR ATTACHMENT LUG AT LH MLG WHEEL WELL. BOX SUPPORT ASSEMBLY OF THE AILERON TRIM ACTUATOR ATTACHMENT LUG AT LH MLG WHEEL WELL WAS REPAIRED ERA 590462-14. (LP 1748SDR SWAA2021032650144Angle · crackedLT WING TRAILING EDGE RIB WBL 201.90 HAS WEB AFT EDGE FITTING ANGLE CRACKED. / REMOVED AND REPLACED LT WING TRAILING EDGE RIB WBL 201.90 AFT EDGE FITTING ANGLE PER REF B737-700 SRM 51-40-02-0G-0.SDR SWAA2021032649661Support · crackedDEFLECTOR BEAM PANEL RH T/E BETWEEN SPOILER #7 AND #8 ;BOTTOM BRACKET SUPPORT IS CRACKED. / REMOVED AND INSTALLED NEW BRACKET SUPPORT AT DEFLECTOR BEAM PANEL R/H T/E BETWEEN SPOILER #7 AND #8 BOTTOM IAW B737-700 SRM # 51-40-02-0G-0.SDR SWAA2021032648937Support · crackedLH TRAILING EDGE DEFLECTOR BEAM PANEL BETWEEN SPOILER #5 AND #6 HAS BRACKET SUPPORT BOTTOM I/B POSITION CRACKED. / REMOVED AND REPLACED BRACKET SUPPORT AT L/H; T/E; DEFLECTOR BEAM PANEL; BETWEEN SPOILERS #5 AND #6 IAW B737-700 SRM 51-40-02-0G-0SDR DALA2020111703762Strut · corrodedCORROSION INBOARD FLAP INTERCONNECT STRUTS ON LT WING (1 EA). CORRECTIVE ACTION: REPLACED INBOARD FLAP INTERCONNECT STRUTS ON LT WING (1 EA) (1657048).SDR SWIA202054003Attach Fitting · corrodedWS 264.00 LT OUTBOARD FLAP, OUTBOARD FWD HINGE BOX ATTACH FITTING ON THE WING, ATTACH HARDWARE CORRODED, MARKED. C-CHECK RO 11/11/2020. REMOVED AND REPLACED THE 1 INBOARD FORWARD BOLT AND HARDWARE AT LEFT WS 264.00 HINGE BOX FITTING AND REPLACED WITH 1 NEW BSDR SWIA202054262Hinge Arm · gougedLT OUTBOARD FLAP CENTER HINGE ARM HAS GOUGE AT CONNECTION OF HINGE BOX, AS MARKED. C-CHECK RO 11/21/2020. REPAIRED GOUGES AND COMPLIED WITH REO.SDR DALA2022030201338None · noneSHIP 686 DISBOND OF 6.900" X 0.650" ON OSS 327 ON REPAIR DOUBLER UPPER SURFACE TRAILING EDGE WEDGE SLAT # 7 RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00133:UPPER SURFACE TRAILING EDGE WEDGE SLAT # 7 RH WING WAS REPAIRED PER B757-200 SRM 57-43-02-2R-1 REPAIR 1SDR SWIA202053955Attach Fitting · chafed*WS54.55, LT INBOARD FLAP INBD AFT HINGE BOX ATTACH FITTING ON THE WING, INNER SET OF LUGS, THE OUTER LUG IS CHAFED ON THE AFT EDGE, MARKED. C-CHECK RO 11/11/2020. BLENDED OUT CHAFFING ON LT INBOARD FLAP INBOARD HINGE BOX INNER SET OF LUGS ON THE OUTER LUG TSDR IPXA2020092560613Hinge Bracket · corrodedINSPECTION TYPE: 2C RT WING TRAILING EDGE INBOARD FLAP OUTBOARD HINGE BRACKET ASSY HAS CORROSION. REPAIRED RT WING TRAILING EDGE INBOARD FLAP OUTBOARD HINGE BRACKET ASSY, IAW VT-SAA EA NR 011-5700-01-A8557 I/R AND UPS EO NR MD11-5740-77940-A. (MINOR)SDR SWIA202053947Nut · corrodedLT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACED NUT P/N MS17825-7 ON LT HINGE BOX AT WS 220.00 OUTBOARD SIDE, IAW CRJ 200 AMM. REMOVED AND REPLACED NUT P/N MS17828-7 ON LT HINGE BOX AT SDR SWIA202053946Nut · corrodedRT FLAP HINGE BOX AT WS 220.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET AND FWD BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED RT HINGE BOX AT WS 220.00, THE NUTS ON INBOARD AND OUTBOARD SIDE OF BRACKET AND THE FWD BRACKET, IAW CRJ 200 SDR SWIA202053945Nut · corrodedLT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD AND OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVED AND REPLACED LT HINGE BOX INBOARD & OUTBOARD NUTS (P/N MS17825-7) AT WS 264.00, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SESDR SWIA202053944Nut · corrodedRT FLAP HINGE BOX AT WS 264.00 NUT CORRODED ON AFT INBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE NUT ON RT FLAP HINGE BOX AT WS 264.00 ON AFT INBOARD SIDE OF BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPT 21.SDR SWIA202053943Bracket · corrodedRT FLAP HINGE BOX AT WS 178.00 NUT CORRODED ON AFT OUTBOARD SIDE OF BRACKET. C-CHECK RO 11/11/2020. REMOVE AND REPLACE RT FLAP HINGE BOX AT WS 178.00 THE NUT ON THE AFT OUTBOARD SIDE OF THE BRACKET, IAW CRJ 200 AMM. TORQUE WRENCH WVACT 10147, CAL DUE 30 SEPSDR SWIA202053751Lug · chafedRIGHT INBOARD FLAP, INBOARD FLAP HINGE LUG PLATES ARE CHAFED ON BOTH LOWER POSITIONS (2 EA), MARKED. C-CHECK RO 10/29/2020. COMPLIED WITH PERMANENT REPAIR RT INBOARD FLAP, INBOARD FLAP HINGE LUG, REF REO. VERIFIED ALL STEPS COMPLIED WITH.SDR SWIA202053758Lug · chafedLT WING INBOARD FLAP HINGE LUG PLATES HAS CHAFING DAMAGE, AS MARKED. C-CHECK RO 10/29/2020. BLENDED, NO DEFECTS NOTED, EVALUATED REPAIR, FOUND OUT OF LIMITS. RECEIVED ENGINEERING REQUESTED SUPPORT REO, COMPLIED WITH ALL STEPS OF REO PART IN LIMITS. ROTO PESDR SWIA202053602Attach Fitting · gougedLEFT OUTBOARD FLAP INBOARD HINGE BOX AFT ATTACH FITTING ON WING INBOARD ATTACH POINT OUTBOARD LUG GOUGED. C-CHECK RO 10/20/2020. BLENDED OUT GOUGE ON LEFT OUTBOARD FLAP INBOARD HINGE BOX AFT ATTACH FITTING ON WING INBOARD ATTACH POINT OUTBOARD LUG, IAW CRJ20SDR SWIA2020090252188Mount · corrodedLEFT WING INBOARD AND OUTBOARD GROUND SPOILER PCU MOUNTING HARDWARE CORRODED. C-CHECK RO 8/29/2020. INSTALLED SERVICEABLE MOUNTING AND ATTACHING HARDWARE TO LT WING INBOARD AND OUTBOARD GROUND SPOILERS PCU IAW CRJ 200 AMM. OPERATIONAL TEST CHECKS GOOD IAW CSDR SWIA2020090252187Nut · corrodedLEFT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU MOUNTING HARDWARE (NUTS) ARE CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CORRODED NUTS IAW CRJ-200-AMM.SDR SWIA2020090252181Bolt · corrodedRIGHT WING INBOARD AND OUTBOARD GROUND SPOILER PCU MOUNTING HARDWARE CORRODED. REPLACED THE RT INBOARD AND OUTBOARD GROUND SPOILER ACTUATOR MOUNTING HARDWARE WITH NEW SERVICABLE HARDWARE IAW CRJ 200 AMM. OPERATIONAL TEST CHECKS GOOD IAW CRJ 200 AMM.SDR SWIA202052180Nut · corrodedRIGHT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU MOUNTING HARDWARE (NUTS) ARE CORRODED. C-CHECK RO 8/29/2020. REPLACED CORRODED NUTS ON THE RT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU TO WING ATTACHMENT POINT WITH NEW SERVICSDR FDEA2020070641445Hinge · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACES FOUND WITH CORROSION. LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07, REPAIR EVALUATED ANSDR FDEA2020070641444Hinge · corrodedRIGHT HAND WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACES FOUND WITH CORROSION. RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE SURFACE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07, REPAIR EVALUATEDSDR FDEA2020062541325Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09 AND FOUND EXCEED LIMIT BASEDSDR IPXA2020062256796Hinge · excess playINSPECTION TYPE:SV RT O/B FLAP O/B HINGE BEARING HAS AXIAL PLAY. REPAIRED R/T O/B FLAP O/B HINGE BEARING LUG BORE IAW CMM 57-44-09. (MINOR)SDR IPXA2020062256798Bearing · migratedINSPECTION TYPE:SV RT O/B FLAP I/B HINGE BEARING IS MIGRATED. REPAIRED RT O/B FLAP I/B HINGE BEARING LUG BORE IAW CMM 57-44-08. (MINOR)SDR FDEA202006161246Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT SURFACE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-SDR FDEA2020063041216Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE FORWARD (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED SDR FDEA2020061641235Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD FORWARD MOUNT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD FORWARD MOUNT HOLE BORE (6 HOLE) REWORKED AND FOUND EXCEED LIMIT ASSDR FDEA2020061641234Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD FORWARD MOUNT HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD FORWARD MOUNT HOLE BORE (6 HOLE) REWORKED AND FOUND EXCEED LIMIT SDR FDEA2020061641233Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) INBOARD LOWER MOUNT HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM SDR FDEA2020061641232Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD LOWER MOUNT HOLE CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE FORWARD (WING SIDE) OUTBOARD LOWER MOUNT HOLE BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CM
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