JASC 5744
Service difficulty reports · 2,731
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 04FDEA00894Hinge · corrodedRIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD UPPER MOUNT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIRSDR 04FDEA00871Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.SDR 04FDEA00870Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.SDR 04FDEA00869Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DRAWING ARC0502, SHT.4, ZONE 40.SDR 04FDEA00868Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648.SDR 04FDEA00843Hinge · corrodedCOMPLY WITH EA 8-5740-75134 WINGS RIGHT INBOARD FLAP, HINGE ASSY ATTACH LUG REWORK. COMPLIED WITH EA 8-5740-75134.SDR 04FDEA00842Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643, TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.SDR 04FDEA00841Hinge · corrodedLT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.SDR 04FDEA00840Hinge · corrodedLEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BORE SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR.SDR 04FDEA00821Bracket · corrodedCOMPLY WITH EA 8-5740-75129 WINGS - OUTBOARD AILERON, BACKUP ACTUATOR BRACKET HOLE REWORK. COMPLIED WITH ENT BY: 484466 RPT BY: 484466.SDR COMA0470030Attach Fitting · crackedTHE RIGHT OUTBOARD MULTI-FUNCTION SPOILER OUTBOARD ATTACH FITTING (WS 216.9) IS CRACKED. REMOVED THE CRACKED ATTACH FITTING AND INSTALLED A NEW ATTACH FITTING P/N CC670-17113-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4790A.SDR 04FDEA00623Bracket · corrodedRIGHT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75298 - WINGS - OUTBOARD TRAILING EDGE FLAPS, INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, - REPAIR.SDR 04FDEA00613Bracket · corrodedLEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.SDR 04FDEA00612Bracket · corrodedLT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.SDR 04FDEA00611Bracket · corrodedLT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B NUT SIDE SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.SDR 04FDEA00610Bracket · corrodedLT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.SDR 04FDEA00608Bracket · corrodedLT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR.SDR 04FDEA00607Bracket · corrodedRIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75297 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIRSDR 04FDEA00606Bracket · corrodedRIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75297 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIRSDR 04FDEA00574Hinge · corrodedREWORK RT OUTBD FLAP OUTBD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION WRITTEN FOR CLARIFICATION JPF. REMOVED BUSHING & CORROSION IAW DC10 CMM 57-44-09, FINAL HOLE SIZE 1.192, FOUND OUT OF LIMITS. FABRICATED BUSHING IAW DC10 CMM 57-44-09 AND EO 8-5SDR 04FDEA00573Hinge · damagedREWORK BARREL NUT HOLE NR 10 IS LARGER THAN CMM LIMIT ON RT WING O/B-I/B FLAP HINGE FITTING. CLARIFICATION OF N01776. N01776 & N02167 REMOVED BUSHING & OPEN BORE TO .748 IAW DC10 MM 57-44-08, HEAT TREATED BUSHING MAT'L IAW DPS 5.00-2 & DPS 1.05.5, ETCHED BSDR 04FDEA00567Bracket · corrodedCOMPLY WITH EA 8-5740-73884 WINGS - LT OUTBOARD FLAP, OUTBOAD HINGE BRACKET CORROSION REPAIR (P/N ARC0503). COMPLIED WITH EA 8-5740-73884 WINGS - LT OUTBOARD FLAP, OUTBOARD HINGE BRACKET CORROSION REPAIR (P/N ARC0503) AT MAE.SDR 04FDEA00566Bracket · corrodedCOMPLY WITH EA 8-5740-73888 WINGS - RIGHT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF ACTUATOR LUG. COMPLIED WITH EA 8-5740-73888 WINGS - RIGHT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF ACTUATOR LUG AT MAE.SDR 04FDEA00553Hinge · corrodedRIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING EO 5750-7-5000, CORROSION WAS FOUND IN THE 2 RIGHT OUTBOARD FLAP HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMETER OF 1SDR 04FDEA00552Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING C-CHECK INSPECTION CORROSION WAS FOUND IN THE INNER BORE OF ARC0538-501 OUTBOARD FLAP FORWARD CLEVIS FITTING. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECSDR 04FDEA00551Hinge Fitting · corrodedRIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING AUCT MOUNT POINT HOLE HAS CORROSION AT BORE 5 A&B. DURING EO 8-5750-7-5000, CORROSION WAS FOUND IN THE 2 RT FLAP OUTBOARD HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMSDR 04FDEA00550Mount · corrodedDURING C-CHECK INSPECTION, CORROSION WAS FOUND IN THE CENTER BORE OF THE ANB7016-6 RT INBOARD FLAP DRIVE BEARING MOUNT BORE. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECT HOLE TO 1.0210 INCH DIA. REMOVED FITTING IAW DC10 SRM 51-31-00 VOL II. RSDR 04FDEA00549Hinge · corrodedLEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REWORK LEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REMOVED BUSHING AND CORROSION IAW CMM 57-44-8. FABRICATESDR 04FDEA00547Hinge · corrodedREWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING, REPAIRED HINGE PER FEDEX EA 8-5710-75067 DATED 01-23-04.SDR 04FDEA00546Hinge · corrodedREWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING AND FOUND BORE TO BE 2.322, OUT OF LIMITS IAW DC10 CMM 57-44-08. HEAT TREATED MATERIAL FOR BUSHING IAWSDR 04FDEA00529Support Bracket · crackedLEFT WING - OUTBOARD TRAILING EDGE FLAP OUTBOARD HINGE NR 3 FRAME FROM AFT FOUND SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AS PER SRM 51-31-01, VOL II AND FABRICATED NEW TEE BRACKET AS PER DRAWING ARC0568. INSTALLED NEW TEE BRACKET AT LT WING OUTBOARDSDR 04FDEA00530Hinge · crackedLT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) NR 3 FRAME AFT FOUND SUPPORT BRACKET CRACKED. FABRICATED NEW TEE AS PER DRAWING NR ARC 0544. LT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) 3 FRAME AFT SUPPORT BRACKET REMOVED AND RSDR 04FDEA00526Hinge · crackedRIGHT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) AT HINGE BRACKET AFT SIDE FOUND TEE CHORD CRACKED. REPAIR CARRIED OUT AS PER EA 1-5750-74329, WINGS - FLAP ASSEMBLIES - TEE CHORD FABRICATION.SDR 04FDEA00498Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARDSDR 04FDEA00499Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBSDR 04FDEA00500Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC502. COMPLIED AS PER EA 1-5470-74323,SDR 04FDEA00501Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHT 4. COMPLIED AS PSDR 04FDEA00502Hinge · corrodedLEFT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUSDR 04FDEA00503Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT SDR 04FDEA00504Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHT 4. COMPLIED ASDR 04FDEA00505Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DWG ARC 0502 SHT 4. COMPLIED AS PER EA 1SDR 04FDEA00506Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA #1-5740-74324, WINGS - LT AND RT OUTSDR 04FDEA00507Hinge · corrodedRIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT ANSDR 04FDEA00508Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 0503, SHT 2. COMPLIEDSDR 04FDEA00509Hinge · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RSDR 04FDEA00510Hinge · corrodedLT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RSDR 04FDEA00511Hinge · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 0503, SHT 2. COMPLIED SDR DL767040154Fitting · corrodedTHE INBOARD SUPPORT BEAM FOR THE INBOARD FLAP ON THE LT WING WAS FOUND WITH CORROSION IN THE FLAP ATTACH HOLES. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLES. ALUMINUM REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IN THE HOLE BORES. THE REPAIR WAS ACCOMSDR 04FDEA00344Hinge · corrodedFOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR.SDR 04FDEA00346Hinge · corrodedFOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE (7) OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR. THE LOWER MOUNT SPOT FACE REMAINING IS WITHIN THE LIMIT
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