JASC 5753
Service difficulty reports · 31,513
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 FMMA2016052700260Rivet · looseREMOVED EIGHT LOOSE RIVETS ON LT FLAP NR 2 RIB AND INSTALLED 8 NEW RIVETS IAW SRM 12-A-51-40-03-00A-041A-A.SDR A6WA201643931Skin · chafedRIGHT INBD FLAP VANE LE IS CHAFED AT THE IN BUMPER STOP, REPLACED.SDR SWAA2016061652945Flap · delaminatedRT WING OTBD FLAP INBD AFT CORNER DELAMINATED. REPAIRED FLAP IAW SRM.SDR SWAA2016061052739Flap Track · corrodedLEFT WING NR 5 FLAP TRACK MOUNT FLANGE CORRODED AT MOUNT HOLES. R & R NR 5 FLAP TRACK IAW AMM & EA.SDR FDEA201605221713Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.313", FINAL HOLE DIA: 1.326" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BSDR FDEA201605221712Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.285" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BSDR FDEA201605221711Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.2834", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABSDR FDEA201605221710Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRSDR HNAA2016052700154Flap Track · crackedRIGHT WING NR 5 FLAPTRACK SHOWS INDICATIONS WHILE PERFORMING EDDY CURRENT INSPECTION AROUND SEVERAL FASTENER HEADS ON OTBD SIDE OF TRACK.SDR HNAA2016052700153Flap Track · crackedRIGHT WING NR 4 FLAP TRACK SHOWS INDICATIONS WHILE PERFORMING EDDY CURRENT INSPECTION AROUND SEVERAL FASTENER HEADS ON OTBD SIDE OF FLAPTRACK.SDR DALA2016052104141Skin · delaminatedLEFT WING OTBD T/E FLAP LOWER SURFACE CTR AREA FOUND DELAMINATION. REPAIRED IAW SRM 51-70-17.SDR DALA2016052104140Skin · delaminatedLEFT WING OTBD T/E FLAP LOWER SURFACE INBD EDGE AREA FOUND DELAMINATION. REPAIRED IAW SRM 57-53-01.SDR DALA2016052104139Fairing · delaminatedRIGHT WING OTBD FLAP LOWER SURFACE AT 10" FROM AFT EDGE 32" FROM OTBD FLAP INBD LINK AFT FAIRING FOUND DELAMINATION. REPAIRED IAW SRM 57-53-01.SDR DALA2016052104138Fairing · delaminatedRIGHT WING OTBD FLAP UPPER SURFACE AT 12" FROM AFT EDGE, 25" FROM OTBD FLAP OTBD LINK AFT FAIRING FOUND DELAMINATION. REPAIRED IAW SRM 57-53-01.SDR SWIA201642205Vane · chafedLEFT INBD FLAP VANE L/E MIDDLE SECTION CHAFED. R & R LT INBD FLAP VANE L/E MIDDLE SECTION AT APPROXIMATELY LT WS 93 - 130 IAW SRM AND EA.SDR SWAA2016060852670Attach Bracket · crackedRIGHT WING NR 6 FLAP TRACK AFT FAIRING ASSEMBLY OTBD UPPER ATTACH BRACKET CRACKED ON AFT END. R & R BRACKET IAW SRM.SDR SWIA201642197Skin · chafedRT INBD FLAP PANEL 684GB IS CHAFED. REPLACED RT INBD FLAP PANEL WITH NEW SERVICEABLE PANEL IAW SRM.SDR FDEA201605201686Lever · excess playHARMONIC VIBRATION LASTED FOR 1 MIN WENT AWAY FOR 10 SECONDS & THEN CAME BACK. VIBRATION WAS WORSE AT HIGHER SPEEDS, LEAST AT 290 KNOTS & BELOW. VIBRATION FREQUENCY WAS MEDIUM & ENTIRE AIRFRAME WAS SHAKING. DID NOT FEEL VIBE IN CONTROL COLUMN, NOR THROTTLESSDR SWAA2016070553396Skin · delaminatedRT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR IPXA2016061504649Skin · delaminatedINSPECTION TYPE: SEG3, RIGHT WING OTBD AFT FLAP LOWER SURFACE OTBD OF INBD TRACK WAS DELAMINATION. REPAIRED IAW SRM 57-53-01 AND 51-70-04.SDR SWAA2016052452039Flap · delaminatedLEFT WING OTBD AFT TE FLAP DELAMINATED. REPAIRED AFT FLAP IAW EA.SDR DALA2016051804116Skin · dentedMAINTENANCE TASK-LEFT WING INBD T/E FLAP FWD LOWER SURFACE FOUND DENT. LEFT WING INBD T/E FLAP LOWER SURFACE FWD AREA REPAIR IAW SRM 51-70-10, REPAIR GENERAL AND SRM 51-70-03.SDR SWAA2016052351991Flap · delaminatedLEFT WING OTBD AFT TE FLAP DELAMINATED ON INBD SIDE. REPAIRED AFT FLAP IAW EA.SDR IPXA2016052003632Skin · delaminatedINSPECTION TYPE: SEG 3, RT WING INBD FLAP LOWER SURFACE HAS DENT BELOW AFT FLAP TRACK FAIRING OTBD ATTACH BRACKET. DOT 135-52, REPAIR IAW SRM 57-53-01-2R AND 51-70-10 350 DEGREE CORE, METAL SKIN, ALUMINUM HONEYCOMB.SDR SWIA201642211Vane · chafedRT INBD FLAP, OTBD FLAP VANE L/E CHAFED. R & R THE RT INBD FLAP, OTBD L/E VANE CAP IAW SRM.SDR SWIA201642210Vane · chafedRT INBD FLAP, INBD FLAP VANE LE CHAFED. R & R THE RT INBD FLAP, INBD L/E VANE CAP IAW SRM.SDR SWIA201642209Vane · chafedLEFT INBD FLAP, OTBD FLAP VANE L/E CHAFED. R & R THE LT INBD FLAP,OTBD L/E VANE CAP IAW SRM.SDR SWIA201642208Vane · chafedLEFT INBD FLAP, CENTER FLAP VANE L/E, WS 104, CHAFED. R & R THE LT INBD FLAP, CENTER L/E VANE CAP IAW SRM.SDR SWIA201642207Vane · chafedLT INBD FLAP, INBOARD FLAP VANE LEADING EDGE CHAFED. R & R THE LT INBD FLAP, INBD FLAP LEADING EDGE VANE CAP, PN 601R14303-53 IAW SRM.SDR SWIA201642204Vane · chafedRIGHT INBD FLAP VANE LE CHAFED INBD SIDE. THE L/E SECTION WAS REMOVED, NEW OTBD MID SECTION, PN: 601R14303-52, WAS INSTALLED IAW SRM.SDR FDEA201605171640Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING B FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.915", WIDTH: 0.621". FINAL SIZE: LENGTH 1.0395", WIDTH: 0.7395", MAXIMUM ALLOWABLE SIZE: LENGTH 0.9SDR FDEA201605171639Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING C FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.918", WIDTH: 0.653". FINAL SIZE: LENGTH 1.019", WIDTH: 0.718", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940SDR FDEA201605171638Fitting · corrodedLEFT WING, OTBD FLAP VANE HORN FITTING D FWD HOLE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02-2R, FIG 201, EXISTING SIZE: LENGTH 0.858", WIDTH: 0.598", FINAL SIZE: LENGTH 0.9495", WIDTH: 0.649", MAXIMUM ALLOWABLE SIZE: LENGTH 0.940SDR FDEA201605171637Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.282", FINAL DIA: 1.315", MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED IAW SDR FDEA201605171636Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIA: 1.283", FINAL DIA: 1.315". MAXIMUM ALLOWABLE DIA: 1.220". REPAIR BUSHING FABRICATED AND INSTALLED ISDR FDEA201605171624Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE OTBD BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.222 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRED BUSHING, FABRICASDR FDEA201605171623Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT HOLE INBD BORE CORROSION. CORROSION AT HOLE INBD BORE REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER 1.2235 INCH, FINAL DIAMETER 1.237 INCH & MAX ALLOWABLE DIAMETER 1.220 INCH. REPAIRSDR DALA2016111108698Panel · corrodedCORROSION ON T/E PANEL STA XA=400 AT LT WING. REPLACED PANEL 5912737-503.SDR SWIA201642214Strap · corrodedEVIDENCE OF CORROSION ON RT SIDE FLOOR STRAP AT APPROXIMATELY BS 559, RBL 36 - 42 IN 3 LOCATIONS. R & R RT FLOOR STRAP IAW SRM.SDR SWIA201642212Vane · chafedRT INBD FLAP, CENTER L/E VANE CAP, WS108 CHAFED. R & R THE RT INBD FLAP, CENTER L/E VANE IAW SRM.SDR SWAA2016060652420Fairing · crackedRIGHT WING NR 6 FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW EA & SRM.SDR FDEA201605161588Skin · dentedFOUND DENT ON THE RT WING CTR FLAP TOP NOSE SKIN, BETWEEN RIB 2 & 3. SPAR WISE 9 INCH, CHORD WISE 3 INCH & DEPTH 0.3 INCH. PERFORMED NOSE SKIN FLUSH REPAIR BETWEEN RIB 2 AND RIB 3 IAW SRM 57-50-00, FIG 208 & EA 6-5750-T0325698, PT1 EA TITLE: WING-FLIGHT
SURSDR AALA201605319005Skin · delaminatedAIRCRAFT IN BASE MX. RT WING OTBD TE FLAP LOWER SURFACE DELAMINATED, 98" FROM INBD EDGE, BETWEEN RIB 13 - 15. REPAIRED RT WING OTBD TE FLAP LOWER SURFACE IAW SRM 57-53-00-201.SDR IPXA2016052603882Vane · chafedINSPECTION TYPE:3C, LEFT INBD FLAP VANE INBD UPPER T/E IS CHAFED. REPAIRED CHAFED LT INBD FLAP VANE IAW SRM 57-50-80, REPAIR 2, PARA 2-A-5 WET LAYUP.SDR AALA20160519002Seal · departedAIRCRAFT WAS NOT GNDED. DURING DEPLANING A PAX INFORMED THE FLIGHT CREW THAT AN OBJECT HAD LIBERATED FROM THE FLAPERON SEAL OF THE RT WING DURING FLIGHT. INSPECTED WING & CONFIRMED THE RT INBD UPPER FLAPERON SEAL WAS MISSING. INSTALLED NEW SEAL IAW AMM 27-1SDR 7C7A2016051400242Flap Track · damagedDAMAGE TO NR 4 FLAP TRACK INBD AFT FACE LOWER PORTION. BLENDED RD8-57-7380.SDR SWIA201642233Vane · wornRIGHT INBD FLAP VANE L/E WORN FROM STOP AT APPROXIMATELY 6" FROM OTBD SIDE. REMOVED AND INSTALLED NEW OTBD VANE CAP FOR RT INBD FLAP, FLAP VANE L/E SKIN IAW SRM.SDR DALA2016051704009Skin · damagedLEFT INBD MAIN FLAP UPPER SURFACE PANEL HAS DAMAGE TO THE HONEYCOMB AT UPPER EDGE. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON LT INBD MAIN FLAP UPPER PANEL IAW SRM.SDR FDEA201605131545Skin · chafedRIGHT OTBD MAIN FLAPS LE, JUST IN FRONT OF NR 11 SPOILER HAS CHAFED MARK. EVALUATED CHAFE MARK, OUT OF LIMITS IAW SRM 57-53-01 FIG 101 DETAIL VI. REPAIRED IAW SRM 57-53-01-2R REPAIR 2 FIG 201 & SRM 51-40-02-0G, REF EA F-5750-T0325268 ISSUED FOR TRACKING. MASDR SWAA2016071153643Flap Track · corrodedRIGHT WING OUTBOARD NR 7 FLAP TRACK ATTACHMENT TO THE WING CORRODED. R & R NR 7 FLAP TRACK ASSY IAW AMM.
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