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 ASAA2014072308800Skin · chafedRIGHT INBD MID FLAP IS CHAFED AT THE VERY INBD TOP SIDE, JUST AFT OF INBD SIDE SEAL. ACFT GROUNDED. CHAFE ON RT INBD MID FLAP UPPER SKIN WAS ON A EXISTING REPAIR. REPAIRED UPPER SKIN IAW SRM 57-53-01-2R-3.SDR FDEA201407221918Fastener · looseRIGHT WING OTBD TE MAIN FLAP OTBD CARRIAGE FWD MOUNT SUPPORT, FOUND ONE LOCK FASTENER BROKEN & TWO LOCK FASTENERS LOOSE. REPAIRED IAW EA F-5750-T0312509. REPAIR CLASSIFIED AS MINOR.SDR SWAA2014080730676Skin Panel · damagedRIGHT WING OTBD FORE FLAP EXTERNAL UPPER SKIN PANEL DAMAGED AT WBL 213. REPAIRED SKIN IAW EO & EA.SDR SWIA201438875Skin · chafedRT INBD FLAP PANEL 684AB CHAFED. R & R FLAP PANEL IAW SRM.SDR USAA2014072100028Flap · delaminatedRON VISIT DELAMINATION ON RT WING OTBD FLAP TE APPROX BETWEEN WS 5512 TO WS 1166418 & RIB-10 TO RIB 22. REPAIRED RT WING OTBD FLAP TE EA 208083 & DWG D57571108.SDR FDEA201407201876Repair · damagedEXSITING REPAIR FOUND AT RIGHT WING INBOARD FLAP OUTBOARD WEB AT APPROXIMATELY XIFH 133.9. EXISTING REPAIR EVALUATED AND FOUND DAMAGED. REPAIR REMOVED AND REPLACED AS PER DRAWING NR ARC2305 REVISION C AND SRM 51-35-01 REVISION 56. EO 1-5100-7-5001 B4 PART 1SDR SWAA2014072930441Stiffener · crackedRIGHT WING NR 6 FLAP TRACK FAIRING TE UPPER STIFFENER CRACKED AT WBL 188.40. R & R STIFFENER IAW SRM & DWG.SDR SWAA2014072830406Stiffener · crackedLEFT WING NR 3 FLAP TRACK FAIRING TE INTERNAL STRUCTURE INBD SIDE LOWER STIFFENER CRACKED AT WBL 188.40. R & R STIFFENER IAW SRM & DWG.SDR SWAA2014080130530Fairing · delaminatedLEFT WING INBOUND FLAP TRACK CANOE FAIRING DELAMINATED. REPAIRED FAIRING IAW EA.SDR CALA2014072191487Skin · wornRIGHT WING INBD MAIN FLAP UPPER OTBD EDGE WORN IAW ECRA 5753-01414. THE RT INBD FLAP UPPER SKIN REPAIR RECEIVED FIRST STAGE APPROVAL. A NEW FAA 8100-9 APPROVAL SHOWING COMPLIANCE WITH 14 CFR 26.43 D & 25.571 IS REQUIRED ON OR BEFORE 20 OCT 2014 FOR THE ACFT SDR R61A201407170927Bolt · corrodedDURING HEAVY CHECK, FOUND LT FLAP POSITION SENSOR MOUNT BOLTS ARE CORRODED. MAINTENANCE R & R LT FLAP POSITION SENSOR MOUNT BOLTS IAW AMM 27-53-04.SDR SWAA2014072330268Flap Track · corrodedRIGHT WING NR 5 FLAP TRACK INBD CORRODED. REPAIRED FLAP TRACK IAW CMM.SDR FDEA201407171842Flap · chafedRIGHT WING INBD TE FLAP LE ABOVE FLAP FAIRING FWD END HAVE DEEP CHAFED MARK. REPAIRED RT WING INBD TE FLAP LE IAW SRM 57-10-00 FIG 86. TRACKED ON EA 8-5710-T0309738. MAJOR REPAIR.SDR DALA2014071804159Skin · gougedFOUND TWO GOUGES ON RT WING INBD FLAP LOWER SKIN. REPAIRED GOUGES IAW SRM 57-01, FIG 1 AND 57-03D, FIG 8.SDR IPXA2014080183821Skin · chafedRT OTBD FLAP INBD BULLNOSE SKIN CHAFED. REPAIRED R/T OTBD FLAP INBD BULLNOSE SKIN IAW SRM 57-50-00, FIG 208, REV 25.SDR REXA2014071600721Skin · dentedTASK CARD 900-57-680-302 RT WING INBD FLAP LOWER SURFACE HAS 2 DENTS. REPAIRED RT WING INBD FLAP LOWER SURFACE DENT AT FLS 46.5 IAW SRM 57-52-01-201-001-A01. TYPE IV & EOR57184
DENT AT FLS 34, 1.1 INCHES FROM RIB, 11.2 INCHES FROM TE MEASURING 1.12 INCHES X SDR SWAA2014072230197Stiffener · crackedRIGHT WING NR 6 FLAP TRACK FAIRING INTERNAL AREA STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.SDR SWIA201438936Skin · chafedLT INBD FLAP VANE L/E SKIN CHAFED AT INBD END. C-CHECK, COMPLIED WITH REPAIR OF CHAFE ON LT INBD FLAP VANE SKIN L/E AT INBD END IAW REO.SDR SWIA201438935Skin · chafedLEFT INBD FLAP VANE L/E SKIN CHAFED AT OTBD END. C-CHECK, COMPLIED WITH REPAIR OF CHAFE ON LT INBD FLAP VANE SKIN L/E AT OTBD END IAW REO.SDR FDEA201407141776Skin · gougedRIGHT INBD FLAP UPPER SKIN GOUGED AT NUMEROUS LOCATIONS, XIFH 250 - 295. BLENDED UPPER SKIN DAMAGE AREA DIM L=.100", W=.050", D=.002". L=.100", W=.050", D=.002". L=.150", W=.100", D=.003". L=.100", W=.080", D=.002". L=.100", W=.080", D=.002". FOUND TO BSDR SWIA201438888Vane · chafedRIGHT INBD FLAP VANE L/E CAP CHAFED. C-CHECK, R & R FLAP VANE L/E IAW SRM.SDR USAA2014072900006Wedge · delaminatedC1 CHECK DELAMINATION ON LT WING INBD FLAP TE WEDGE AT APPROX 64.5 INCHES FROM OTBD END & 5.875 INCHES FWD OF TE. REPAIRED LT WING INBD FLAP TE IAW SRM 57-53-01-2R-1 & 51-70-10.SDR SWIA201438892Vane · chafedLEFT INBD FLAP VANE HAS CHAFING AT INBD VANE ACTUATOR. C-CHECK, REPAIRED LT INBD FLAP VANE AT INBD ACTUATOR, IAW REO.SDR SWIA201438891Vane · chafedLEFT INBD FLAP VANE CHAFED AT CENTER VANE ACTUATOR. C-CHECK, REPAIRED LT INBD FLAP VANE CAP AT CENTER ACTUATOR, IAW REO.SDR SWIA201438890Vane · chafedLEFT INBD FLAP VANE CHAFED AT OTBD VANE ACTUATOR. C-CHECK, REPAIRED IAW REO.SDR SWIA201438889Vane · chafedRT INBD FLAP VANE CHAFED ON INBD SIDE OF L/E. REPLACED RT INBD FLAP VANE IAW SRM AND REO.SDR SWIA201438887Vane · chafedRIGHT INBD FLAP VANE CHAFED ON OTBD SIDE OF L/E. BLENDED RT INBD FLAP VANE IAW REO.SDR A6WA201441787Skin · chafedRIGHT INBD FLAP VANE CHAFED INBD LE.SDR SWAA2014071429954Flap · delaminatedRIGHT WING INBD AFT FLAP ASSEMBLY DELAMINATED. R & R AFT FLAP ASSEMBLY IAW AMM.SDR A6WA201441756Attach Fitting · gougedRT WING INBD FLAP, INBD HINGE BOX, AFT ATTACHMENT FITTING IS GOUGED.SDR A6WA201441758Support · crackedRIGHT INBD FLAP INBD HINGE ARM FAIRING GUIDE PLATE SUPPORT STRUCTURE ON FWD SIDE OF HINGE ARM IS CRACKED.SDR SWAA2014072830380Skin · delaminatedRIGHT WING OTBD AFT FLAP OTBD END LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2014072530315Skin · delaminatedLEFT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2014072530314Skin · delaminatedRIGHT WING OTBD AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2014072430279Angle · crackedLEFT WING INBD SIDE OF THE MOST INBD FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.SDR A6WA201441755Plate · crackedLEFT OTBD FLAP CTR HINGE ARM SHROUD PLATE IS CRACKED.SDR SWAA2014080630634Splice Plate · crackedRIGHT WING FORE FLAP OTBD SLICE PLATE CRACKED. REPAIRED FORE FLAP IAW EO & EA.SDR SWAA2014071129886Flap · looseLEFT WING OTBD AFT FLAP TRACK 3 ATTACH POINT LOOSE. R & R AFT FLAP IAW AMM.SDR DALA2014071004017Panel · delaminatedDELAMINATED TRAILING EDGE METALIC HONEYCOMB PANEL FROM XRS 500 - 838, LT WING. REPAIRED IAW ERA 526957-14 & ETI-88-14-095 REV 2SDR DALA2014071004015Bar · corrodedCORROSION ON FLEX JOINT LOWER BAR FOUR LT FLAPS. REPAIRED IAW ERA 526968-14 REV ORIGINAL.SDR FDEA201407081953Skin · gougedLEFT WING INNER FLAP SKIN UPPER SURFACE HAS GOUGE. BLENDED AREA IAW SRM 51-73-10, L=3.0 INCHES, W=1.3 INCHES & D=.020 INCHES, FOUND OUT OF LIMITS IAW SRM 57-50-00 FIG 101. PERFORMED SKIN PATCH REPAIR BY FABRICATED REPAIR DOUBLER FROM MATERIAL 2024T3-056C BATSDR SWAA2014071429935Flap · delaminatedLEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MT.SDR SWIA201438840Vane · chafedLEFT INBD FLAP VANE, INBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.SDR SWIA201438839Vane · chafedLEFT INBD FLAP VANE OTBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.SDR SWIA201438838Vane · chafedRT INBD FLAP VANE INBD L/E CHAFED. BLENDED CHAFE IAW REO & SRM.SDR SWAA2014072530351Flap · delaminatedRIGHT WING AFT FLAP OTBD EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2014071830081Flap · delaminatedLEFT WING OTBD AFT FLAP INBD LOWER CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR DALA2014070703900Spar · corrodedDURING INSPECTION, FOUND CORROSION ON EXTERNAL SURFACE OF THE FRONT SPAR ON OTBD FLAP INTERNAL DOUBLER BETWEEN RIBS 5 - 6 LT WING MEASURE APPROXIMATELY L= 1.000", W=0.500", D=0.005", SSI 575309. REPLACED FRONT SPAR, TRACK 3 ON OTBD FLAP INTERNAL DOUBLER BETWSDR SWIA201438856Skin · chafedLEFT INBD FLAP PANEL NR 584 EB IS CHAFED, C-CHECK, BLENDED PANEL IAW SRM.SDR HALA2014070600104Flap Track · damagedLOWER INBD L/E BEHIND FLAP TRACK DAMAGED. SLAT ANTI ICE COVER LT INBD BENT AT AFT INBD CORNER. COLD WORKED IAW SEM 51-10-02/OGO1.
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