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 DALA2015091205604Vane · wornWEAR ON REPAIR DOUBLER OF LT OTBD FLAP INBD VANE. LT OTBD FLAP INBD VANE WAS REPAIRED IAW SRM 57-03D, PAR. II.SDR FDEA201509092826Wedge · delaminatedRIGHT OTBD FLAP, TE WEDGE HAS DELAMINATION ON OTBD CORNER. REPAIRED IAW SRM 57-50-80-2R.SDR DALA2015091005543Vane · wornTHE RIGHT WING TE FLAP VANE HAS WEAR ON THE REPAIR DOUBLER. REPAIRED IAW SRM 57-03D, PAR II.SDR SWAA2015091043638Flap · delaminatedLEFT WING OTBD TE AFT FLAP INBD EDGE, LOWER CORNER DELAMINATED. R & R AFT FLAP IAW AMM.SDR DALA2015090805593Support Fitting · corrodedCORROSION ON LT FLAP SUPPORT FITTING HINGE INTERNAL STRUCTURE XW=154. REPAIRED IAW ERA 537789-14, REV O.SDR CALA2015090894282Failsafe · damagedNUMBER 5 FLAP TRACK FAIL SAFE BAR DAMAGED. BUSHING & TOOLING HOLE ELONGATED. SURFACE DAMAGE TO FLAP TRACK, CARRIED FROM 8 18 11. REPAIR ACCOMPLISHED IAW EN-57-0184. PERFORMED DETAILED VISUAL INSPECTION OF THE FAIL SAFE BAR & BUSHING, FOUND SATISFIED IAW ECRSDR HALA201509060187Skin · dentedDURING INSPECTION OF RT FLAP AREA, FOUND DENTED. REPAIRED IAW E105-481209-1N1. OK FOR SERVICE.SDR V0XD20150907181Skin · dentedLEFT INBD FLAP HAS 2 SKIN DENTS. REPAIRED LT INBD FLAP SKIN DENTS BY CUTTING OUT DAMAGE. FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-57-52-323, DATED 5 SEPT 2015.SDR A6WA201543032Skin · dentedRIGHT OTBD FLAP, UPPER SKIN HAS A DENT AT APPROX FLAP STATION 278.00, 2 INCHES AFT OF FRONT SPAR. REPAIRED FLAP UPPER SKIN IAW SRM 57-53-00 REPAIR 2.SDR R61A201509030642Pin · corrodedDURING HEAVY CHECK WAS REPORTED THAT NR 3 FLAP TRACK RT WING FWD HARDWARE IS CORRODED. MX R & R NR 3 FLAP TRACK RT WING FWD HARDWARE IAW AMM LL 57-57-31, STEPS 17-21& 25-26, PN 170-14217-001, PIN.SDR DALA2015090405423Skin · delaminatedACFT HAS A DELAMINATED INBD FLAP OTBD GUIDE VANE LOWER AND UPPER SKIN LT WING. DUE TO SEVERAL DAMAGE INBD FLAP OTBD GUIDE VANE WAS REPLACE WITH REPAIRED INBD FLAP OTBD GUIDE VANE.SDR A6WA201543022Vane · chafedLEFT INBD FLAP VANE LE CHAFFED AT WS 105. REPLACED LE.SDR WVER201509011502Vane · chafedRIGHT INBD FLAP VANE L/E CHAFED APPROXIMATELY 12" L,.250" W,.010" D ABOVE THE INBD ACTUATOR.SDR DALA2015090205398Skin · corrodedACFT HAS CORROSION AND DELAMINATION OTBD FLAP MID GUIDE FLAP VANE LOWER SKIN AT LT WING. DUE TO SEVERAL DAMAGE OTBD FLAP MID GUIDE VANE FLAP AT LT WING WAS REPLACED WITH REPAIRED MID GUIDE VANE AND WILL BE INSTALLED WITH CARD 5730-0631.SDR IPXA2015090293025Skin · damagedINSPECTION TYPE:CR, HW INBD AFT FLAP LOWER MAIN SKIN FOUND DAMAGED D559545. PERFORMED METAL HOT BOND REPAIR IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 3, REV 33.SDR HALA2015082900176Carriage · damagedT/E FLAP DISAGREE EICAS MESSAGE. FOUND RT OTBD FLAP INBD CARRIAGE JOINT 9 INNER PIN PULLED OUT & BENT, INSPECTED AREA & REPLACED INNER & OUTER PINS AT JOINT 9 IAW AMM 27-51-20. ACCOMPLISHED E105-594-INI. VISUALLY INSPECTED LT AND RT WING OTBD FLAP LINKAGE SDR IPXA2015082992862Skin · dentedRIGHT WING INBD AFT FLAP LOWER SKIN DENTED. REPAIRED IAW EO B747-5750-57795-B.SDR DALA2015083105327Stud · corrodedCORROSION WAS FOUND ON THE UPPER STUDS OF RT WING OTBD FLAP HINGE XW 333. THE STUDS WERE REPLACED IAW AMM 57-40-01-201.SDR SWAA2015091743999Tail Cone · crackedNUMBER 6 FLAP TRACK FAIRING TAIL CONE, CRACKED AT AFT UPPER HALF CORNER. REPAIRED TAIL CONE IAW SRM & EA.SDR DALA2015082905281Structure · wornWEAR ON RT FLAP L/E NR 4. REPAIR ON RT FLAP L/E NR 4 WAS REPLACED IAW ER/A 503745-14, REV ORIGINAL.SDR ASOA20150828162Fitting · crackedDURING C-CHECK THE RT OTBD FLAP INBD ROLLER FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5750-01708. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWAA2015092144117Flap · delaminatedRIGHT WING OTBD AFT FLAP TE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2015091844046Flap · delaminatedLEFT WING OTBD AFT FLAP DELAMINATED ON TE AREA. R & R AFT FLAP IAW AMM.SDR SWAA2015091443806Flap · delaminatedLEFT WING TE INBD FLAP DELAMINATED. REPAIRED FLAP IAW SRM.SDR FDEA201508272712Wedge · delaminatedRIGHT OTBD TE FLAP HAS DELAMINATION WITH WATER ACTUALLY DRIPPING FROM AREA AT THE AFT INBD TE CORNER. REPAIRED IAW SRM 57-50-80-212.SDR DALA2015082805266Skin · nickedA NICK WAS FOUND ON THE LOWER SKIN OF THE LT WING OTBD FLAP XFLS 361. REPAIRED IAW SRM 57-03, PAR 9, FIG 8 AND SRM 51-10-3, PAR 14, 21.SDR SWAA2015082843283Flap · delaminatedRIGHT WING OTBD AFT FLAP TE INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.SDR DALA2015082605216Doubler · delaminatedDELAMINATED DOUBLER ON INTRADOSE OF INBD FLAP INBD GUIDE VANE AT RT WING. INBD FLAP, INBD GUIDE VANE AT RT WING WAS REPAIRED IAW SRM 57-03D, PAR 11.SDR DALA2015082605210Skin · nickedSEVERAL NICKS ON INBD FLAP LOWER SKIN ON RT WING. REPAIRED IAW SRM 57-03D FIG 8.SDR FDEA201508242692Fitting · corrodedRIGHT WING OTBD FLAP VANE FITTING F BUSHING BORE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02-2R. REPAIR BUSHING FABRICATED IAW EA 1-5750-T0319728 P 1 STEP 1. BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201508242691Fitting · corrodedRIGHT WING OTBD FLAP VANE FITTING E BUSHING BORE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02-2R. REPAIR BUSHING FABRICATED IAW EA 1-5750-T0319728 P 1 STEP 2. BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR CA150825013Carriage · chafed(CAN) FLAP CARRIAGE ASSY DAMAGED BY REPETITIVELY CONTACTING RIVET TAILS.SDR A6WA201543001Skin · chafedRIGHT INBD FLAP VANE LEADING EDGE CHAFED OUT OF LIMITS AT WS 56.SDR A6WA201543000Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE CHAFED OUT OF LIMITS AT WS 56.SDR AALA201508249010Guide · crackedLEFT INBD TE FLAP, INBD GUIDE RAIL IS CRACKED. REPLACED GUIDE RAIL IAW AMM 57-54-25.SDR DALA2015082405185Guide Vane · damagedNICKS AND WEAR ON REPAIR DOUBLER ON INBD FLAP, GUIDE VANE LT WING. REPAIR DOUBLER WAS REPLACED IAW SRM 57-03D, PAR 11.SDR DALA2015082405179Guide Vane · wornWEAR ON OTBD FLAP, OTBD FLAP VANE UPPER AND LOWER SKIN INBD EDGE AT LT WING. REPAIRED IAW SRM 57-03, PAR II AND OPN 1031.SDR SWAA2015091043602Bracket · crackedRIGHT WING NR 7 MOVABLE FAIRING FLAP TRACK TRANSMISSION BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.SDR DALA2015082205157Guide Vane · wornWEAR ON INBD EDGE UPPER & LWR SIDE OF T/E AT RT WING OTBD FLAP, OTBD GUIDE VANE. REPAIRED IAW SRM 57-03D, PAR 11.SDR FDEA201508212668Fitting · corrodedLEFT WING OTBD FLAP VANE FITTING B BUSHING BORE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02-2R. REPAIR BUSHING FABRICATED IAW EA 1-5750-T0319727 PART 1 STEP 1. BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SWAA2015092144106Skin · delaminatedRIGHT WING INBD FORE FLAP, UPPER SKIN DELAMINATED 13" FROM INBD END. REPAIRED FORE FLAP IAW SRM.SDR SWAA2015082143066Flap · damagedRIGHT WING INBD FORE FLAP DAMAGED ON INBD END. R & R FORE FLAP IAW AMM.SDR FDEA201508202650Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE PIVOT INBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING 1.188", FINAL 1.225" & MAX ALLOWABLE 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-T0319686 PART 1. REPAIR CLASSSDR FDEA201508202649Hinge · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE PIVOT OTBD HOLE BORE CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING 1.218", FINAL 1.225" & MAX ALLOWABLE 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-T0319686 PART 1. REPAIR CLASSSDR AALA20150827005Flap · wornRIGHT INBD MAIN FLAP LE STRUCTURE WORN FROM CONTACT WITH THE FIXED WING STRUCTURE SHELF. ACCOMPLISHED FLUSH DOUBLER REPAIR IAW SRM 57-53-01-2R-2 & EA 253982 DATED 08 24 2015.SDR FDEA201508192617Hinge Bracket · corrodedSNRM N 00363, RIGHT WING OTBD FLAP, INBD FWD HINGE, WING SIDE, LOWER MOUNT HOLE OTBD BORE CORRODED. BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0319687 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201508192644Skin · dentedLEFT WING INBD FLAP, LOWER SURFACE HAS A DENT WS 204. OUND TO BE OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101. REPAIRED IAW SRM 51-70-10-2R PARA 20. PRIMED & TOP COATED IAW SRM 51-70-10-2R PARA 20 & AMM 51-21-10-7.SDR DALA2015082005075Vane · chafedLT WING, CENTER FLAP VANE UPPER SURFACE CHAFED THRU JUST AFT OF INBD FLT SPOILER OTBD END. REPLACE DOUBLER REF SRM 51-70-02 DRD.SDR FDEA201508192639Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD HOLE BORE CORRODED. REPAIRED IAW EA 1-5750-T0319686 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201508192638Hinge · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE CORRODED. REPAIRED IAW EA 1-5750-T0319686 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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