JASC 5744
Service difficulty reports · 2,730
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 FDEA200902020413Hinge Bracket · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127439, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200902020412Hinge Bracket · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127439, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902020411Hinge · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORRODED. REPAIRED AS PER EA 1-5750-127440, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200902020410Hinge Bracket · corrodedRIGHT WING, AIRCRAFT SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REPAIR 1-1. NEW BUSHING FABRICATED AND INSTALLED ON INBOARD ACTUATOR HOLE AS PER EA 1-5750-127440, THIS REPAIR SDR GUUA91255013109AHinge Bracket · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR CENTER HINGE BRACKET HAS SURFACE CORROSION. REPLACED RT ELEVATOR CENTER HINGE BRACKET.SDR GUUA95455012909AHinge · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED LT ELEVATOR CENTER HINGE CORRODED AT BONDING JUMPER ATTACH POINT. REPLACED LT ELEVATOR CENTER HINGE.SDR FDEA200901210298Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT INBOARD, BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127894, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100SDR FDEA200901210296Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT OUTBOARD, SPOT FACE INBOARD AND OUTBOARD SIDE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127894, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100SDR FDEA200901210295Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED) LOWER ATTACHMENT INBOARD, SPOT FACE INBOARD AND OUTBOARD SIDE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127894, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR FDEA200901210284Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), UPPER ATTACHMENT OUTBOARD BORE FOUND CORROSION AT CHAMFER AREA. COMPLIED WITH E.A. 1-5750-127891, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR FDEA200901210283Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), ACTUATOR ATTACHMENT LUG INBOARD BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127890. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR FDEA200901210282Hinge · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), LOWER ATTACHMENT OUTBOARD BORE, BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127890, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR FDEA200901210281Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), LOWER ATTACHMENT INBOARD BORE, BORE FOUND CORROSION. COMPLIED WITH E.A. 1-5750-127890, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR FDEA200901110145Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AT RT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE AS PER E.A. 1-5750SDR FDEA200901110144Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT BORE FOUND WITH CORROSION. OUTBOARD PIVOT BORE HOLE AT LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AT LTSDR FDEA200901070050Mount · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR MOUNT OUTBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127715. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200901070049Mount · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR MOUNT INBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127715. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR C2XA09TY004Bushing · migratedRT GROUND SPOILER MOST INBD ATTACHMENT LUG (ON WING) HAS MIGRATED HAT BUSHING. INSTALLED HAT BUSHING IAW EC5740-01152. ACFT CURRENTLY IN C-CHECK.SDR FDEA200901040018Mount · corrodedRIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER MOUNT OUTBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127716. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200901040017Mount · corrodedRIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER MOUNT INBOARD BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127716. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR FDEA200901040016Mount · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT NUT SIDE FACE FOUND CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200901040015Mount · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE INBOARD ACTUATOR MOUNT BORE FOUND WITH CORROSION. COMPLIED WITH E.A 1-5750-127714. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR FDEA200901040014Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER MOUNT OUTBOARD BORE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-127870, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200812265308Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FORWARD AND AFT SURFACE FOUND WITH CORROSION. REWORKED AS PER EA 1-5750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200812265307Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FOUND WITH CORROSION. REWORKED AS PER EA 1-5750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200812265306Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH OUTBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200812265305Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH INBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR CA081126004Support Bracket · cracked(CAN) SUPPORT BRACKET FOR RT AILERON INPUT QUADRANT FOUND CRACKED AND CONFIRMED BY NDT RT WING ACCESS PANELS 625AT, 632ET AND 625BB REMOVED. RT AILERON WING CABLES LOOSE. RT WING AILERON INPUT QUADRANT REMOVED FOR SHEET METAL REPAIR. REMOVED AND REPLACED NESDR 08FDEA04895Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNT SURFACE FOUND CORROSION. CORROSIONS REMOVED ON SIDE LOAD MOUNT AT LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER EA 1-5750-122634, REPAIR CLASSIFIED AS MINOR RESDR 08FDEA04894Hinge Bracket · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNTING SURFACE FOUND CORRODED. CORROSION REMOVED ON SIDE LOAD MOUNTING SURFACE AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER CMM 57-44-08. EXISTING THICKNESSDR 08FDEA04494Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH OUTBOARD HOLE FORWARD MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04493Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE AFT MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR USAA920081892Spindle · crackedPIT FPBH MAJOR REPAIR LOG NR 4352180 AND 03T30757001 OTBD LT SPINDLE SHOWS CRACK 60% AT 35 THRU GATE VERTICALLY TO 40% AT 50 HORIZONTALLY. REPLACED SPINDLE IAW B737 MM 27-51-44-404-006.SDR 08FDEA04336Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER ATTACHMENT OUTBOARD HOLE AFT SPOTFACE FOUND SURFACE CORROSION. SURFACE CORROSION REPAIRED AS PER E.A. 1-5750-122592, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04334Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER OUTBOARD BORE HOLE FOUND WITH CORROSION. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER OUTBOARD BORE HOLE CORROSION REPAIRED AS PER E.A. 1-5750-122590, THIS REPAIR CLASSIFIED AS MAJOR PER GMMSDR 08FDEA04333Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER INBOARD BORE HOLE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-122590, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04332Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) LOWER ATTACHMENT OUTBOARD HOLE FORWARD SPOTFACE FOUND SURFACE CORROSION. SPOTFACE CORROSION REPAIRED AS PER E.A. 1-5750-122592, SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-08. REPAIR CLASSIFIED AS MAJOR SDR 08FDEA04323Hinge Fitting · corrodedLEFT HAND WING: OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR HOLE OUTBOARD BORE HOLE FOUND WITH CORROSION. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-122591, THIS REPAIR CLASSIFIED AS MAJOR PERSDR 08FDEA04320Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR HOLE INBOARD BORE HOLE FOUND WITH CORROSION. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-122591, THIS REPAIR IS CLASSIFIED AS MAJOR PSDR CA080603006Hinge Bracket · worn(CAN) REAR SPAR, RT LOWER WING AILERON, HINGE BRACKET INNER OUTER SHELL BECOMING LOOSE IN BEARING (REPLACED WITH NEW) (TC NR 20080603006)SDR SWAA082717Mount · brokenDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD MOUNT LUG BROKEN. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.SDR 08FDEA01831Hinge · corrodedRIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 INBD BORE IS CORRODED. REMOVED THE CORROSION FROM THE INBD BORE IAW CMM 57-44-01. MACHINED NEW BUSHINGS FOR THE INBD BORE IAW CMM 57-44-09. CAD PLATED BUSHING IAW QQP-416-7Y2- CL2. INSTALLED THE NEW BUSHISDR 08FDEA01830Hinge · corrodedRIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 OUTBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUND AND REMOVED FROM THE LUG FACE TO .405. LUG FOUND TO BE OUT OF LIMITS IAW BAC CMM 57-44-01. ETCSDR 08FDEA00980Hinge · damagedFRAGMENTS ARE MISSING FROM THE INBD PIANO HINGE ON PANEL 551 CB LT WING T/E LOWER SURFACE. REMOVED PANEL IAW SRM 51-31-01; VOL II. REMOVED HINGED PANEL IAW SRM 51-33-01 VOL II. LOCATED & DRILLED HOLES IAW SRM 51-33-01 VOL II. ALODINED & PRIMED IAW SRSDR F3LA200800066Attach Fitting · damagedDURING C3/S1 C CHECK, INSPECTION REPORTED THE RIGHT, OUTBOARD NUMBER 3 FLAP DRIVE LEVER EXTENSION ARM FITTING WAS FOUND GOUGED WHERE IT CONNECTS TO BOTTOM OF THE DRIVE ARM. MAINTENANCE BLENDED THE DAMAGED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 5SDR 1218363041408Hinge · brokenLEADING EDGE 511 HINGE BROKEN. REMOVED AND REPLACED HINGE IAW SRM.SDR USAA920070923Attach Fitting · crackedMCN - MAJOR REPAIR - C-18 CHECK - NR 5976581, RIGHT AILERON INBOARD ATTACH FITTING CRACKED, WS 517.75. REPLACED RIGHT AILERON INBOARD ATTACH FITTING, WS 517.75 IAW B737-300 SRM 51-40-02.SDR UPS07M51205Hinge Fitting · corrodedINSPECTION TYPE:C RHW O/B FLAP I/B HINGE (WING SIDE) LWR MOUNT I/B BORE SPOT FACE FOUND CORRODED. RT FWD OB FLP I/B HINGE LWR MOUNT I/B HOLE SPOTFACE CORROSION REMOVED FOUND EXCEED LMT PER CMM 57-44-08 PG 602-607 R.58. FPI C/O IAW DAC NDT SPM R.13 PART 8 AND SDR UPS07M50600Hinge · corrodedINSPECTION TYPE:C LEFT WING O/B FLAP I/B HINGE (WING MOUNTED), O/B LOWER ATTACHMENT SPOT FACES 02 EA FOUND CORROSION AS MARKED. AFFECTED AREA O/B HOLE SPOTFACE CORR REMOVD & FOUND EXCEED LIMIT CMM57- 44-08 PG 602-607 R58. ORG THK 0.482" REMN THK 0.462" MIN ASDR UPS07M50599Hinge · corrodedINSPECTION TYPE:C LEFT WING O/B FLAP I/B HINGE (WING MOUNTED), I/B LOWER ATTACHMENT SPOT FACES 02 EA FOUND CORROSION AS MARKED. AFFECTED AREA CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG 602- 607 R58. ORG THK 0.530" REMN THK 0.523" MAT'L RMVD 0.
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