JASC 5753
Service difficulty reports · 31,515
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 IPXA1668505Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.SDR IPXA1668504Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1) FIG 5, REV 50.SDR C8GA2011000015Carriage · brokenDURING CLIMB OPERATION, THE OTBD FLAPS FROZE AT 3 DEGREES ON CLIMBOUT, 9 UNITS OF AILERON TRIM WAS REQUIRED FOR LEVEL FLIGHT. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED NOTING THAT BOTH RT OTBD FORE FLAP SESDR IPXA1M68811Skin · dentedINSPECTION TYPE:4C, LT WING INBD FLAP LOWER SURFACE HAS A CREASE 13" INBD OF SPRING CARTRIDGE. REPAIRED LT WING INBD FLAP LOWER SURFACE CREASE, 13" INBD OF SPRING CARTRIDGE REF STA, SA, EA 011-5730-01-A3341 REV I/R AND EO MD11-5750-43966.-ASDR IPXA1168551Bullnose · dentedINSPECTION TYPE:4C, RT WING INBD FLAP BULLNOSE AND 2EA DEFLECTOR PANEL ROLLER STRIPS HAVE DENTS. ACCOMPLISHED REPAIR ON RT WING INBD FLAP BULLNOSE BETWEEN RIB 12 AND RIB 17 IAW SRM 57-50-00, PARA 4H, FIG 208.SDR FDEA201107273002Structure · crackedRT WING INBD MID FLAP T/E CHORD CRACKED AT INBD CABLE CONTROL DRUM CUTOUT. CUT OUT DAMAGE TRAILING EDGE CHORD RIGHTHAND WING INBOARD MID FLAP IAW SRM 51-40-4 FIG 3. FABIRCATED LOCATED AND DRILLED NEW CHORD AND SPLICE IAW 51-40-4 FIG 3 AND 57-50-2. INSTALLESDR UIEA2011072700372Panel · deformedDURING WALK-AROUND INSPECTION, MX REPORTED RT INBD MID FLAP - T/E OF COVE PANEL - DEFORMATION WBL168.55, MEASURING 5.0 IN. LONG X 0.250 IN. DEPTH (UPWARD DEFLECTION) (REF FIG 1).SDR UIEA2011072700373Panel · deformedDURING WALK-AROUND INSP, MX REPORTED RT INBD MID FLAP - T/E OF COVE PANEL - DEFORMATION WBL259.55, MEASURING 10.0 IN. LONG X 0.5 IN. DEPTH UPWARD DEFLECTION REF FIG 2.SDR UIEA2011072700374Panel · deformedDURING WALK-AROUND INSPECTION, MX REPORTED RT INBD MID FLAP - T/E OF COVE PANEL - DEFORMATION (4 PLACES) WBL347.55, MEASURING 4.0 IN. LONG X 0.375 IN. DEPTH (UPWARD DEFLECTION) (REF FIG 3). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED ISDR UIEA2011072700375Panel · deformedDURING WALK-AROUND INSP, MX REPORTED RT INBD MID FLAP -T/E OF COVE PANEL -DEFORMATION WBL435.55, MEASURING 5.0 IN. LONG X 0.250 IN. DEPTH (UPWARD DEFLECTION) (REF FIG 4). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUSDR FDEA201107272989Skin · dentedRT WING OTBD FLAP LOWER SURFACE FOUND LIGHTLY DENTS POSITION NEAR T/E AREA. THE DIMENSION OF THE DAMAGED AREA 4.6"L X 2.5 W X 0.063" MAX DEPTH. THE AREA IS OVER THE LIMITS IAW SRM57-53-12 (TOOL:TS 482). CUT THE DAMAGED AREA AND REPAIRED BY THE DOUBLER AND FASDR FDEA201107262960Skin · dentedRT WING INBD FLAP, INBD SEGMENT UPPER SKIN FOUND SEVERAL DENTS. DENTED AREAS ARE ACCEPTABLE AND WITHIN ALLOWABLE DAMAGED LIMIT OF 0.060" AS PER SRM 51-80-01 REV 47 AT RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SKIN. HFEC INSPECTION CARRIED OUT AS PERSDR FDEA201107262959Skin · dentedLT WING INBD FLAP, INBD SEGMENT UPPER SKIN FOUND SEVERAL DENTS. DENTED AREAS ARE ACCEPTABLE AND WITHIN ALLOWABLE DAMAGED LIMIT OF 0.060" PER SRM 51-80-01 REV 47 AT LEFT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SKIN. HFEC INSPECTION CARRIED OUT AS PER DASDR FDEA201107262958Skin · dentedLT WING INBD FLAP, OTBD SEGMENT UPPER SKIN FOUND SEVERAL DENTS. DENTED AREAS ARE ACCEPTABLE AND WITHIN ALLOWABLE DAMAGED LIMIT OF 0.060" AS PER MD-11 SRM 51-80-01 REV 47 AT LEFT HAND WING INBOARD FLAP OUTBOARD SEGMENT UPPER SKIN. HFEC CARRIED OUT AS PER DACSDR IPXA11B68204Skin · damagedLT IB AFT FLAP T/E UPPER SKIN DAMAGED. REPAIRED IAW EO B747-5750-42879-B.SDR SWAA115416Flap · delaminatedDURING SCHEDULED 26Y CHECK, FOUND LT WING I/B AFT FLAP O/B TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA115364Flap · puncturedDURING SCHEDULED 22Y CHECK, FOUND LT WING O/B TRAILING EDGE FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.SDR FDEA201107262954Hinge · corrodedLT WING OTBD FLAP, OTBD HINGE (WING SIDE) ACTUATOR. OTBD HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 70. ORIGINAL DIAMETER = 1.212", FINAL DIAMETER = 1.250", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR BUSHING FABRICATED ASDR SWAA115312Slide · faultyAIRCRAFT HAS NOTICABLE SHUTTER IN YOKE WHEN TRAILING EDGE FLAPS MOVED FROM POSITION 1 TO 5 AND 5 TO 1. REMOVED AND REPLACED NR 2 SLAP FWD FLAP CARRIAGE SLIDERS AND ADJUSTED RIGHT O/B FLAP UPSTOPS PER MM.SDR FOTR2111712817Skin · debondedLT INBD FOREFLAP UPPER SURFACE HAS 6"DIAMETER DISBOND. REPAIRED ON FASI WO 21117, NR 12817.SDR IPXA11568145Skin · dentedLT OTBD AFT FLAP DENTED UPPER SURFACE. REPAIRED IAW EO B757-5750-43594-A.SDR IPXA11568144Skin · damagedLT OTBD T/E FLAP DENTED WITH DELAMINATED AND CRUSHED CORE. REPAIRED IAW EO B757-5750-43593-A.SDR USAA2011080900015Strut · corroded2S CHECK - CORROSION OF HOUSING INTERNAL AREA OF INTERCONNECTING STRUT AT LEFT WING. REPLACED INTERCONNECTING STRUT IAW A319 AMM 27-51-44.SDR QXEA2011072500589Flap Track · damagedLT WING NR4 FLAP TRACK VERTICAL LEG ON INBD SIDE OF TRACK HAS CHIPPED CARBIDE COATING. BLENDED DAMAGED AREA IAW RD 8/4-57-1238. MINIMUM REMAINING THICKNESS .150" AND CRACK FREE REF RD 8/4-57-1238. BLENDED AREA IS WITHIN LIMITS IAW RD 8/4-57-1238.SDR QXEA2011072500588Flap Track · damagedRT WING NR 4 FLAP TRACK VERTICAL LEG INBD SIDE OF TRACK HAS CHIPPED CARBIDE COATING. BLENDED DAMAGED AREA IAW RD 8/4-57-1238. MINIMUM REMAINING THICKNESS .150" IS WITHIN LIMITS IAW RD 8/4-57-1238. COMPLETED REPAIR IAW RD 8/4-57-1238.SDR USAA2011080900014Strut · corroded2S CHECK - CORROSION OF HOUSING INTERNAL AREA OF INTERCONNECTING STRUT AT RIGHT WING. REPLACED INTERCONNECTING STRUT IAW A319 AMM 27-51-44.SDR QXEA2011072900626Flap Track · chafedLT WING UPPER FLAP TRACK HAS CHAFING ON VERTICAL LEG. BLENDED CHAFING IAW RD 8/4-57-1352. MINIMUM REMAINING THICKNESS IN BLEND AREA .184". CONFIRMED CRACK FREE REF RD 8/4-57-1352. ALODINED, PRIMED AND PAINTED BLEND AREA IAW RD 8/4-57-1611.SDR DXTA2011072204663Circuit Board · inoperativeFLAPS DID NOT EXTEND ON LANDING. R & R HYD PCB IAW WDM DWG PN 6509270. OPS CHECKED GOOD IAW MM 27-51-00.SDR CA110802008Structure · damagedPILOT REPORTED A RUMBLING NOISE DURING CLIMB WITH FLAPS DEPLOYED TO THE CLIMB POSITION. UPON LANDING, THE TRAILING FLAP WAS FOUND DAMAGED ON INBD SECTION. TRAILING FLAP WAS REPAIRED AND REINSTALLED AND TEST FLIGHT WAS COMMENCED. THE SOUND WAS STILL EVIDENT ASDR UALA2011072203739Structure · damagedLEFT INBOARD FORE FLAP DAMAGED ABOVE NR 4 CANOE. THE 'L' SHAPE DAMAGE HAS 20 INCH "V" TRAILING EDGE IS PULLED FROM FORE FLAP AND ON THE SHORT LEG HAS 4.5 INCH TEAR THROUGH UPPER AND LOWER SKINS ABOUT HALF INCH WIDE. ACCOMPLISHED CORE REPLACEMENT T/E WEDGE RESDR UALA2011072103713Structure · puncturedPUNCTURE HOLE IN LOWER SIDE OF RIGHT INBOARD FLAP. SMALL PUNCTURE IN FOIL-TAPE HOLE COVER. HOLE IN QUESTION, 24 INCHES OUTBOARD OF INBOARD EDGE OF RIGHT INBOARD T/E FLAP APPEARS TO BE HOIST POINT. APPLIED METAL TAPE PER MM, TO BE REPAIRED AT NEXT C-CHECK.SDR FDEA201107212887Structure · damagedLT WING OTBD MID FLAP INBD T/E IS CHIPPED. FOUND TO BE UNREPAIRABLE IAW SRM 57-50-1 FIG 3. REMOVED AND REPLACED LT O/B MID FLAP ASSEMBLY IAW AMM 27-51-011-4-0.SDR SWAA115349Skin · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA115348Skin · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA115243Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING O/B T/E AFT FLAP I/B CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR FDEA201107202830Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4 REV 70.0. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REV 70.0 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.SDR IPXA11M68390Skin · puncturedINSPECTION TYPE:3C, RT OTBD FLAP LOWER SKIN PUNCTURED ABOUT 12 INCHES ABOVE T/E APPROX STA XOF632. REPAIRED RT FLAP LOWER SKIN STA XOF632 IAW STASA EA 011-5753-01-A3299 REV IR EO MD11-5750-43701-A.SDR QXEA2011072200580Skin · chafedRT OTBD FLAP UPPER SKIN IS CHAFED BETWEEN STA YW-191.200 & YW-281.019. BLENDED AWAY ALL DAMAGE IAW BOMBARDIER RD 8/4-57-1594. MINIMUM REMAINING THICKNESS .025" REF NTM 51-00-02-250-801 AND DISBOND CRACK FREE REF RD 8/4-57-1594. NOMINAL THICKNESS .032" FOUND SDR SWAA115193Flap · puncturedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B TRAILING EDGE FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP ASSY PER MM.SDR KCSA111166Flap Track · corrodedNR 6 FLAP TRACK HAS RUST UNDER BUSHING PLATE WHERE IT ATTACHES TO REAR SPAR.SDR KCSA111165Flap Track · corrodedNR 3 FLAP TRACK HAS RUST UNDER BUSHING PLATE WHERE IT ATTACHES TO REAR SPAR.SDR KCSA111164Flap Track · corrodedNR 7 FLAP TRACK HAS RUST UNDER BUSHING PLATE WHERE IT ATTACHES TO REAR SPAR.SDR SWAA115155Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR FDEA201107172770Skin · misrepairedREPAIR AT LT WING INBD FLAP LOWER SKIN OTBD SIDE. FOUND NOT ACCOMPLISHED IAW ANY APPROVED DATA. REPAIR AT LT WING INBD FLAP REMOVED IAW SRM 51-35-01, REV 47. NEW REPAIR DOUBLER FABRICATED & INSTALLED IAW SRM 57-50-01, FIG 201, REPAIR 1, REV 47 AND EA 1-573SDR SWAA115107Skin · puncturedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SURFACE SKIN PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA115106Wedge · puncturedDURING SCHEDULED 14Y CHECK, FOUND RT WING I/B MID FLAP LOWER SURFACE PUNCTURED. REPAIRED WEDGE IAW SRM.SDR A6WA201140751Skin · chafedRT INBD (FLAP) VANE WHERE IT CONTACTS RUBBER STOPS. BLENDED CHAFED AREA IAW REO 601R-57-52-004 ALSO NDT.SDR A6WA201140746Vane · chafedLT INBD VANE (FLAP) WHERE IT CONTACTS RUBBER STOPS. BLENDED CHAFED AREA IAW REO 601R-57-52-004, ALSO NDT.SDR FDEA201107162734Skin · misrepairedREPAIR FOUND AT LT WING T/E FLAP LOWER SURFACE OTBD AREA RIB 9 & RIB 10. FOUND PREVIOUSLY NOT REPAIRED IAW ANY APPROVED DATA. NEW REPAIR ACCOMPLISHED IAW SRM 57-52-12 REV 79, FIGURE 205. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR UALA2011072003690Skin · puncturedLT INBD AFT FLAP - 1.5" X 1.5" LOWER SURFACE PUNCTURE. PUNCTURE IS 2 INCHES FROM THE EDGE OF AFT FLAP. 6" FROM THE INBD EDGE OF DAMAGED AFT FLAP. -ACP'D INTERIM RPR PER SRM. APPLIED ALUMINUM FOIL TAPE (SPEED TAPE). INSPECT EVERY AIRPLANE "A" CHECK. REPLACE
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