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 LR7A2016061400811Rib · crackedDURING SCHEDULED C-12 CHECK, UNDER JC HC5712, FOUND THE LT OTBD FLAP BAFFLE HAD MULTIPLE CRACKS, REQUIRING FLAP STATION 0, RIB REPLACEMENT. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH51-60 AND 51-70.SDR FDEA201606141993Fitting · corrodedRIGHT WING OTBD FLAP VANE HORN FITTING-D, FWD HOLE CORROSION. CORROSION FOUND TO EXCEED LIMIT IAW SRM 57-50-02, REPAIR 5, FIGURE 201. EXISTING SLOT: 0.890", LENGTH, 0.625", WIDTH. FINAL SLOT: 0.965", LENGTH, 0.662", WIDTH. MAXIMUM ALLOWABLE: 0.940", LENGTHSDR FDEA201606141991Hinge · corrodedLT WING OTBD FLAP, INBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.162", MAXIMUM ALLOWABLE DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5750SDR FDEA201606131981Hinge · corrodedLEFT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE SURFACE CORROSION. CORROSION FOUND EXCEEDED LIMIT AS CMM 57-52-03, EXISTING THICKNESS: 0.260", MATERIAL REMOVED: 0.074", REMAINING THICKNESS: 0.186", MINIMUM ALLOWABLE THICKNESS: 0.205". STRAP RESDR FDEA201606131978Skin Panel · delaminatedRT WING, INBD T/E MAIN FLAP UPPER INTERSPAR PANEL FOUND DELAMINATION AT MF STA 175, 18" FROM L/E. COMPLIED WITH PART 1 OF EA F-5750-T0327826. SRM REPAIRS ON RT WING INBD MAIN FLAP UPPER BONDED SKIN OUTER AND INNER FACESHEETS, STA 160-180, RSC TRACKING, REPASDR FDEA201606131977Skin Panel · delaminatedRIGHT WING-INBD T/E MAIN FLAP UPPER INTERSPAR PANEL FOUND DELAMINATION AT MF STA 165, 20" FROM L/E. COMPLIED WITH PART 1 OF EA F-5750-T0327826, SRM REPAIRS ON RT WING INBD FLAP UPPER BONDED SKIN, OUTER & INNER FACESHEETS, MF STA 160-180, RSC TRACKING. REPAIRSDR SWAA2016072254138Flap Track · crackedRIGHT WING CENTER MOVABLE NR 8 FLAP TRACK FAIRING CRACKED. REPAIRED FLAP TRACK IAW SRM.SDR SWAA2016072054070Fairing · crackedLEFT WING NR 1 FLAP TRACK CANOE AFT FAIRING CRACKED. REPAIRED THE FAIRING IAW SRM.SDR SWAA2016072054069Fairing · crackedRIGHT WING NR 7 FLAP TRACK FAIRING CRACKED. REPAIRED THE FAIRING IAW SRM.SDR SWAA2016072054068Fairing · crackedRIGHT WING NR 8 FLAP TRACK FAIRING CRACKED. REPAIRED THE FAIRING IAW SRM.SDR SWAA2016062253132Skin · crackedRIGHT WING NR 6 AFT FLAP TRACK FAIRING CRACKED ON INSIDE SKIN APPROXIMATELY 47" AFT OF FORWARD EDGE. REPAIRED FAIRING IAW SRM.SDR FDEA201606101940Skin · chafedRIGHT WING OTBD FLAP L/E BETWEEN NR 5 AND NR 6 TRACKS IS CHAFED. REPAIRED RT WING OTBD FLAP L/E BETWEEN NR 5 AND NR 6 TRACKS IAW SRM 57-50-00. MAJOR REPAIR.SDR FDEA201606101931Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.286", FINAL HOLE DIA 1.290", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783C, PASDR FDEA201606101930Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.253", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71783, CSDR FDEA201606101929Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.375", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PSDR FDEA201606101928Hinge · corrodedLT WING INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORROSION. CORROSION FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA 1.251", FINAL HOLE DIA 1.283", MAXIMUM ALLOWABLE DIA 1.220". REPAIR BUSHING FABRICATED IAW EA 1-5750-71784E, PT5,SDR SWAA2016063053375Fairing · crackedLT WING FLAP TRACK NR 1 FAIRING CRACKED ON INTERNAL AREA. REPAIRED NR 1 FAIRING IAW EA.SDR SWAA2016062753260Fairing · crackedRIGHT WING NR 6 FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW SRM.SDR SWAA2016062753259Fairing · crackedLEFT WING NR 3 FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW SRM.SDR WVER2016061994704Hinge Fitting · gougedLEFT INBD HINGE BOX FITTING ON INBD FLAP IS GOUGED IN MULTIPLE AREAS.SDR GLBA2016060800592Skin · puncturedMAJOR REPAIR DURING A SCHEDULED INSPECTION, MX FOUND A PUNCTURE TO THE LOWER SKIN APPROX 7" TALL BY 2.25" WIDE, 38" OTBD OF INBD EDGE TO 40.25" OTBD OF INBD EDGE, 5" TO 12" FWD OF TE OF LT INBD FLAP.SDR SWAA2016061052738Support Bracket · corrodedLEFT WING OTBD MIDFLAP, INBD CARRIAGE BEARING SUPPORT BRACKET CORRODED. R & R SUPPORT BRACKET IAW MT.SDR SWAA2016060952704Bracket · crackedRIGHT WING FIXED TE PANEL LOWER FORE FLAP BULB SEAL BRACKET CRACKED. R & R BRACKET IAW SRM.SDR SWIA201642280Cap · chafedRIGHT INBD FLAP, MID VANE CAP IS CHAFED. R & R DISCREPANT RT INBD FLAP VANE CAP, PN 601R14303-52 IAW SRM.SDR SWIA201642279Cap · chafedLEFT INBD FLAP, MID VANE CAP CHAFED. R & R DISCREPANT LT INBD FLAP VANE CAP, PN 601R14303-51 IAW SRM.SDR SWAA2016061052737Support Bracket · corrodedLEFT WING OTBD MIDFLAP, OTBD CARRIAGE BEARING SUPPORT BRACKET CORRODED. R & R BRACKET IAW MT.SDR UIEA2016060900408Skin · damagedLEFT OTBD FORE FLAP HAS DAMAGE ON LE LOCATED ON OTBD END 10 - 14 INCHES INBD. REMOVED DAMAGED AREA & REPAIRED SAME IAW SRM 51-70-07 PARA 4 C. PREPARED & APPLIED BMS 8-79 & BMR 5-101 REPAIR PLIES IAW SRM 51-70-7 PARA 4 E. LAYERED UP & VACUUMED BAGGED REPAIR SDR FDEA201606051848Skin · chafedRIGHT WING OTBD TE MAIN FLAP, NOSE SKIN FOUND CHAFE MARK AT 2.5" FROM OTBD EDGE.SDR SWIA201642277Cap · chafedLEFT INBD FLAP, INBD VANE CAP IS CHAFED. R & R LT INBD FLAP, INBD VANE CAP IAW SRM.SDR REXA2016060401022Skin Panel · dentedPERM REPAIR 2 FLAP DENTS RT INBRD LWR SKIN CONTINUATION CARD 8798616 OP 10. REPAIRED 2 DENTS ON RT INBD FLAP LOWER SKIN BY REMOVING DAMAGED SKIN PANEL AND INSTALLING NEW SERVICEABLE SKIN PANEL IAW SRM 51-42-10, 51-42-13, 51-42-14 AND 51-25-01.SDR FDEA201606041812Fitting · corrodedWHILE WORKING THE INBD AFT FLAP RT SIDE, THE OTBD FITTING WAS FOUND WITH PITTING CORROSION. AFTER CORROSION REMOVAL, FOUND OUT OF LIMITS IAW DWG 113N2801 SHT 1 REV. COMPLIED WITH EA F-5750-T0325349 PT 1 DATED 05 27 16. CAT A MAJOR REPAIR FAA FORM 8100-9 ISSSDR SWIA201642278Cap · wornRIGHT INBD FLAP VANE FWD EDGE WORN. R & R RT INBD FLAP VANE OTBD L/E CAP IAW SRM.SDR SWAA2016062153088Channel · crackedLEFT WING OTBD MAIN FLAP CENTER FORE FLAP GUIDE CHANNEL CRACKED. R & R CHANNEL IAW SRM.SDR A6WA201643967Skin · dentedCOMPLY WITH REPAIR TO LT INBD FLAP LOWER SKIN 601R-57-52-2118, 4DMI18552. REPAIRED LT INBD FLAP LOWER SKIN IAW REO 601R-57-52-2118.SDR SWIA201642276Guide Plate · chafedLEFT WING FLAP FAIRING INBD GUIDE PLATE IS CHAFED UNDER PANEL 586BB. R & R LT WING FLAP FAIRING INBD GUIDE PLATE UNDER PANEL 586BB, WITH FACTORY NEW PART, PN: 601R14116-86 IAW SRM.SDR SWAA2016061552888Carriage · corrodedRIGHT WING OTBD MIDFLAP, INBD MIDFLAP, TRACK CARRIAGE, CORRODED, FOUND AT BASE OF CARRIAGE SPINDLE. R & R CARRIAGE IAW MAINTENANCE.SDR SWAA2016061052746Carriage · corrodedLEFT WING NR 2 FLAP TRACK CARRIAGE BASE OF SPINDLE CORRODED. R & R CARRIAGE IAW MT.SDR SWAA2016060352244Skin · delaminatedLEFT WING OTBD TE AFT FLAP LOWER SKIN DELAMINATED. REPAIRED FLAP IAW MM.SDR SWAA2016062153084Skin · delaminatedLEFT WING OTBD AFT FLAP AFT INBD CORNER SKIN DELAMINATED. R & R AFT FLAP IAW AMM.SDR IPXA2016061504663Skin · gougedINSPECTION TYPE: 5YR, LOWER OTBD FLAP L/E GOUGED ON INBD END. REPAIRED IAW SRM 57-50-00, FIGURE 208, SHEET 2, SKIN INSERT FABRICATED FROM 2024-T3 .056 CLAD.SDR FDEA201606011774Rib · crackedLEFT WING CTR FLAP, RIB 26 FOUND CRACKS AT UPPER STRINGER 2.7 & 2.8 LOCATIONS. REPAIRED THE CRACKED RIB IAW EA 6-5750-T0325833, PT1. THIS REPAIR CATEGORY IS "A" MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201606011773Rib · crackedLEFT WING CTR FLAP, RIB 17 FOUND CRACK AT UPPER STRINGER 2.8 LOCATION. REPAIRED THE CRACKED RIB IAW EA 6-5750-T0325833, PT1. THIS REPAIR CATEGORY IS: A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201606011772Rib · crackedLEFT WING CTR FLAP, RIB 18 FOUND CRACK AT UPPER STRINGER 2.8. REPAIRED THE CRACKED RIB IAW EA 6-5750-T0325833 PT1. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.SDR DALA2016062304878Skin · delaminatedDELAMINATION ON LOWER SKIN AT LT WING OTBD FLAP MID GUIDE VANE. CUT NEW WAS DONE AND DAMAGE WAS FOUND ON INTERNAL STRUCTURE THEREFORE IT IS OUT LIMITS IAW SRM 51-70-2D, PAR 6A AND SRM 57-03D, PAR 11. MID VANE WAS REPLACED.SDR SWAA2016060652382Fairing · crackedRIGHT WING NR 8 FLAP TRACK AFT FAIRING CRACKED. REPAIRED FAIRING IAW SRM.SDR SWAA2016060252210Rib · crackedLEFT OTBD TE FLAP, OTBD RIB CRACKED. R & R RIB IAW SRM.SDR DALA2016053104229Structure · damagedLT WING INBD FLAP AFT EDGE NEAREST AFT FLAP SPLITTING APART. ACCOMPLISHED REPAIR OF THE 2 EA DISCREPANT AREAS, DAMAGE SIZES ARE APPROXIMATELY 2" X 10" AT MF BS 223 AND 4" X 10" AT MF BS 232 ON LOWER INBD FLAP AFT EDGE NEAREST AFT FLAP IAW ER/A 546358-14, ORIGSDR DALA2016053104228Wedge · dentedINBD MAIN FLAP T/E WEDGE HAS A LARGE DENT ON LOWER SURFACE. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA, DAMAGE SIZE IS APPROX. 3" X 10" ON RT INBD MAIN FLAP T/E WEDGE IAW ER/A 546359-14 ORIGINAL REVISION.SDR A6WA201643947Skin · chafedRIGHT OTBD FLAP, FLAP VANE OTBD LE CHAFED.SDR VNAA2016052700026Skin · dentedLEFT INBD FLAP HAS A DENT ON TAIL END LOWER SKIN FLS 98.70, APPROXIMATELY 2" IN DIAMETER. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE LT INBD FLAP LOWER EXTERNAL SKIN, PN CC670-14002-7, SN 10143, IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
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