JASC 5753
Service difficulty reports · 31,521
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 04FDEA03358Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03357Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03356Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03355Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03354Hinge · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR AWXA200401464Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 1 INCH CRACK WAS FOUND IN RT WING OUTBOARD MID FLAP SKIN AT LEADING EDGE, NR 8 FLAP CARRIAGE CUTOUT WBL 363.60. MAINTENANCE CUTOUT DAMAGE IN RT WING OUTBOARD MID FLAP SKIN AT WBL 363.60; FABRICATED A FILLER AND DOUBLER; SDR USAA041029Skin · chafedPIT - RON - L/E SKIN, .5 INCH X 4 INCH CHAFE MARK, LT OB MID FLAP L/E APPROX WBL 204 LT. INSTALLED REPAIR DOUBLER IAW SRM.SDR 04FDEA03353Hinge · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03352Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03351Hinge · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03349Skin · damagedCOMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. RT WING REPAIR RT INBD FLAP LWR SURFACE. REPAIRED IAW EA 6-5750-81812SDR 04FDEA03348Skin · damagedREPAIR RT OUTBOARD TE FLAP LOWER SURFACE OUTBOARD OF NR 2 CANOE FAIRING. REPAIRED IAW EA 6-2750-50362, DATED JUNE/16/2000.SDR 04FDEA03347Skin · activatedCOMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. REPAIR RT INBD FLAP UPPER SURFACESDR SWAA043526Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT INBOARD T/E AFT FLAP PER MM.SDR 04FDEA03336Support · corrodedWING D-LT OUTBD FLAP-FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-55416.SDR DHL2004873546Skin · wornLT WING OUTBOARD FLAP L/E UPPER PART SKIN WORN BETWEEN XF 200.000 AND XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R03 REV: TR DATE 11/08/04 FAA FORM 8110-3 DATED 11-30-04. TRIMMED OUT PLATING SEGMENT (DAMAGED) IAW DWG W90-R03. PERFORMED NDSDR GTIA040866Wedge · dentedFTW - FOUND RIGHT WING INBOARD FLAP OUTBOARD WEDGE BOTTOM SIDE HAS DENT WITH FILLER COMPOUND. STRIPPED FILLER COMPOUND DENT OUT OF LIMITS, CUT OUT DAMAGE 1.5 INCH BY 2.5 INCH, FABRICATED FILLER AND DOUBLER, DRILLED HOLES. OK TO TREAT AND PRIME AND INSTALLED SDR SWAA043490Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E AFT FLAP PER MM.SDR 04FDEA03317Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03316Hinge · corrodedRIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03312Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4.SDR 04FDEA03305Fitting · corrodedLEFT HAND INBOARD FLAP OUTBOARD FITTING OUTBOARD STRAP PIVOT HOLE SURROUNDING AREA OF HOLE SURFACES FOUND PITTING CORROSION OUT OF LIMIT. LEFT HAND INBOARD FLAP OUTBOARD FITTING OUTBOARD STRAP REPLACED BY NEW STRAP AS PER SRM 51-33-01 VOL II.SDR SWAA043486Structure · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E MID FLAP, CRACKED. REPAIRED RT WING MID FLAP PER SRM.SDR SWAA043480Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM.SDR SWAA043479Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM.SDR 04FDEA03289Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03288Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03287Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03286Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03285Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03284Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03283Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03282Hinge · corrodedLEFT HAND WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03281Hinge · corrodedLT HAND WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03280Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03279Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03278Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03277Hinge · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03276Hinge · contaminatedLEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03275Hinge · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 04FDEA03274Hinge · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.SDR 2005FA0000367Flap Track · wornWHILE FLAPS WERE BEING RETRACTED, THE LT IB FLAP ATTACH BRACKET CAUGHT ON THE WING COVE PANEL SUPPORT. THIS CAUSED SUBSTANTIAL DAMAGE TO THE COVE PANEL SUPPORT AS WELL AS THE ATTACH BRACKET. CAUSE WAS DETERMINED TO BE WORN FLAP TRACKS. THE FLAP TRACKS AND RSDR DHL2004873530Skin · damagedRIGHT WING OUTBOARD FLAP LWR FWD SKIN DAMAGED (BROKEN 1.000) AT XF 203.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG 1 PG 3/4, 5/6. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-5 FIG 1 PG 5-6. FABRICATED PLATING SEGMENT (AL2024-T3 0.032) SPLICE (ALSDR QXEA200400857Structure · chafedYYC - LEFT HAND INBOARD FLAP HAS CHAFE DAMAGE FROM CONTACT WITH WING UPPER TRAILING EDGE ALONG THE ENTIRE FLAP LENGTH. REPAIRED IAW SRM 57-51-30-320-001.SDR QXEA200400854Structure · chafedYYC - RIGHT HAND INBOARD FLAP HAS CHAFING DAMAGE FROM CONTACT WITH WING UPPER TRAILING EDGE ALONG THE ENTIRE FLAP LENGTH. REPAIRED IAW SRM 57-51-30-992-001.SDR AWXA200401360Structure · delaminatedMCN - MAJOR REPAIR - DURING C-15 CHECK, THE LOWER RT INBOARD FORE FLAP WAS FOUND DISBONDED JUST OUTBOARD OF THE CENTER MID FLAP TRACK BETWEEN WBL 120.5 AND WBL 121.5. MAINTENANCE CUTOUT DAMAGE IN LOWER RT INBOARD FORE FLAP OUTBOARD OF CENTER MID FLAP TRACK; FSDR 04FDEA03248Hinge · corrodedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING OUTBD HINGE SECTION OF OUTBD FLAP STA XW 638 RUST NEAR HOLES FOR STUDBOLTS. ACCOMPLISH CORROSION REWORK OF ATTACH HOLES (NR 3) FWD/OUTB HINGE OUTBD FLAP IAW CMM 57-44-09 AT HOLES MARKED 7. ACCOMPLISH COSDR 04FDEA03246Hinge · corrodedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT OUTBOARD FLAP, FWD HINGE SECTION, STA XW 486 WITH CORROSION IN THE BORE OF BUSHINGS ACTUATOR ATTACH POINTS. ACCOMPLISH CORROSION REWORK AT RT OUTBOARD FLAP INBOARD FWD HINGE HOLES BORES (5A), (5B) IAW CMM 57-SDR 04FDEA03245Hinge · corrodedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT OUTBOARD FLAP FWD HINGE SECTION STA XW 638 WITH CORROSION IN THE BORE OF BUSHINGS ACTUATOR ATTACH POINTS. ACCOMPLISH CORROSION REWORK AT RT OUTBD FLAP OUTBD FWD HINGE HOLE BORES (5A), (5B) IAW CMM 57-44-09 RESDR 04FDEA03242Hinge · corrodedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING FWD INSIDE HINGE SECTION OF OUTBOARD FLAP STA XW 486 FOUND RUST NEAR HOLES FOR STUD BOLT AND IN THE HOLES OF THE LATERAL BRACE. ACCOMPLISH CORROSION REWORK OF RT FWD INBOARD HINGE OF RT OUTBOARD FLAP IAW
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