JASC 5754
Service difficulty reports · 17,348
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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 = '5754' 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 DL72S972245Angle · crackedTHE LOWER AFT CHORD ANGLE WAS FOUND CRACKED DURING SHOP INSPECTION AT HMV VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY STOP DRILLING CRACK AND INSTALLING A DOUBLER.SDR ASAA9780254Skin · dentedFAI - AFTER ARRIVAL OF FLT 191; CREW REPORTED BIRD STRIKE DURING APPROACH. ACCOMPLISHED BIRD STRIKE INSPECTION AND FOUND RT WING NR 1 L/E SLAT DENTED. FERRIED AIRCRAFT TO SEA, REPAIRED AND INSTALLED DOUBLER IAW ASA EA 5750-01258. TT: 37,613 HOURS. TC: 25SDR DL72S972124Hinge · crackedFOUND ON D2 LETTER CHECK, .5 INCH CRACK AT NR 3 L/E FLAP OUTBD HINGE. REPAIRED PER ERA 363018-14 CODE 4-57-54.SDR P5CA9701803Skin · delaminatedDELAMINATED, L/WING NR 10 LED AFT END. REPAIRED PER SRM 51-40-09.SDR 97FDEA00761Wedge · delaminatedRT WING O/B MIDFLAP T/E WEDGE IS DELAMINATED 24 FROM I/B END AND AT THE NR 2 AFT FLAP TRACK, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.SDR 97FDEA00760Wedge · delaminatedLT WING I/B MIDFLAP T/E WEDGE IS DELAMINATED AT 20 FROM I/B END, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.SDR UPS97224726Fitting · corrodedINSPECTION TYPE-SI, NR 2 K-FLAP CENTER HINGE FITTING (WING SIDE) IS CORRODED. REMOVED AND REPLACED NR 2 K-FLAP CENTER HINGE FITTING IAW SRM 51-30-5, 51-30-2 MISMATCH VERIFICATION TO BE ACCOMPLISHED ON NRC 644506.SDR 97FDEA00755Bonding Jumper · corrodedNR 2 K-FLAP BULLNOSE CORRODED ON O/B BONDING JUMPER. *S/D* REMOVED CORROSION AND REPAIRED NR 2 K-FLAP O/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT IAW FED-EX SRM 57-50-3.SDR DL72L972076Rib · crackedA .25 INCH CRACK IN NR 4 SLAT I/B ACTUATOR ATTACH NOSE RIB. REPAIRED PER MM 57-40-0.SDR P5CA9701752Bracket · crackedCRACKED BRACKET GROUP 1 LEADING EDGE DE-VICE LEFT WING. REPAIRED PER SRM 51-40-03.SDR 98ZZZM139Angle · corrodedRT WING L/E SLAT NR 7 INTERIOR, LOWER ANGLE SHOWS LEVEL 2 CORROSION NEAR WS 586. REMOVED AND REPLACED DOUBLER AT AFFECTED AREA AS PER SRM 51-14-4. (M)SDR 98ZZZM138Angle · corrodedRT WING LE SLAT NR 6 INTERIOR LOWER ANGLE SHOWS LEVEL 2 CORROSION NEAR WS 615.0. BLENDED OUT AFFECTED ITEM, WITHIN PERMISSIBLE LIMITS AS PER SRM 51-8-1. (M)SDR 98ZZZM137Rib · corrodedRT WING NR 7 RT SLAT INTERIOR, RIBS SHOW LEVEL 2 CORROSION. REPAIRED RIBS AS PER SRM 57-4-5.SDR 98ZZZM135Rib · corrodedRT WING NR 6 SLAT WELL RIBS SHOW LEVEL 2 CORROSION. REPAIRED RIBS AS PER SRM 57-4-2.SDR DL72S971984Flap · crackedA .75 INCH CRACK IN NR 4 L/E FLAP AT OUTBOARD LIP HINGE CUTOUT. REPAIRED PER ERA NR 362925-14 AND M/M 57-53-0.SDR DL72S971982Fitting · crackedFOUND DURING A1 LETTER CHECK, 1 INCH CRACK NR 8 SLAT ACT INBD ATTACH FITTING OUTBD SIDE. REPAIRED PER M/M 57-20-21.SDR DL72S971980Rib · crackedFOUND ON A1 LETTER CK, 2 IN VISIBLE CRACK NR 1 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PER MM 57-20-21.SDR ASAA9780239Skin · crackedBFM - DURING 30K CHECK, CRACKS AND BROKEN RIVETS WERE FOUND IN LEFT WING NR 2 L/E SLAT LOWER SKIN. SPLICED SKIN IAW DC9 SRM 57-09, FIG 10. (M)SDR DL72S972094Rib · crackedRIB CRACKED, THE NR 4 L/E SLAT ACTUATOR SUPPORT RIB IS CRACKED AND MARKED WITH TEMPORARY REPAIR. REMOVED TEMP REPAIR AND BEGAN FABRICATION OF PERMANENT REPAIR PER M/M 57-54-0 FIG 804. INSTALLED REPAIR.SDR DL72S972071Rib · crackedNR 4 L/E SLAT ATTACH RIBS ARE CRACKED I/B AND O/B SIDE OF ACTUATOR ATTACH POINT. REMOVED TEMP REPAIR ON OTBD RIB OF ACTUATOR ATTACH POINT AND BEGAN FABRICATION OF RIB DOUBLERS PER M/M 57-54-0 FIG 804. OK TO INSTALL INBD REPAIR. OK TO INSTALL OUTBD REPAIR. SDR DL72S972067Rib · crackedRIB CRACKED NR 6 SLAT, RIB NR 18 IS CRACKED. FABRICATED REPAIR DOUBLER PER M/M 57-54-0 FIG 814. OK TO INSTALL. REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72S972066Rib · crackedRIB CRACKED NR 6 SLAT, RIB NR 12 IS CRACKED. FABRICATED REPAIR DOUBLER PER M/M 57-54-0 FIG 814. OK TO INSTALL. REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72S972026Rib · crackedNUMBER 3 AND 7 RIB CRACKED. REPAIRED PER SRM 57-54-0.SDR DL72S972015Rib · crackedRIB CRACKED NR 17 ON L/E NR 3 SLAT. REPAIRED PER MM 57-54-0.SDR DL72S972000Rib · crackedNUMBERS 5, 8 AND 12 RIB CRACKED ON NR 3 SLAT. REPAIRED PER MM57-54-0.SDR CALA971402Chord · crackedINSPECTION FOUND A 3 CRACK IN LOWER T-CHORD AT NR 5 SLAT. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA9701540Skin · dentedINSPECTION FOUND LEADING EDGE OF NR 6 SLAT DENTED. THE DENTED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 1.SDR DL72S971976Rib · crackedPREVIOUS NOSE RIB O/B CRACKED 1 INCH AT NR 6 L/E SLAT PANEL. REPAIRED PER MM 57-54-0 FIG 804.SDR ABXA9701869Vane · corrodedCORROSION FOUND INBOARD SLOT VANE, OUTBOARD ATTACH UPPER SURFACE, RIGHT WING. REPAIRED IAW ABX REA D857-20509MR AND SRM 51-1-8.SDR TWAA9711702Rib · crackedMCI - REPAIRED CRACK AT NR 6 LEADING EDGE SLAT 1ST RIB OUTBOARD OF OUTBOARD TRACK AT LOWER END. (M)SDR P5CA9701601Support · brokenBROKEN LEFT WING LEADING EDGE SUPPORT ROD AFT OF NR 6 LEADING EDGE FLAP. REPLACED SUPPORT ROD PER BAC MM 57-21-00.SDR DL72K971895Skin · crackedA 2 INCH CRACK NR 7 SLAT COVE SKIN ATTACH ANGLE AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72S971857Rib · crackedFOUND DURING E 1 LETTER CHECK .0625 INCH CRACK PAST STOP DRILL AT NR 4 SLAT O/B ACTUATOR MOUNT RIB. REPAIR PER MM 57-54-0.SDR UPS97224518Skin · crackedINSPECTION TYPE:W/E, 3 CRACKS FOUND ON NR 2 K-FLAP ANTI-ICE SKIN. COMPLIED WITH UPS EO 9650. D 137034.SDR UPS97824663Skin · crackedINSPECTION TYPE-C, RT O/B SLOT VANE I/B L/E SKIN HAS HEAVY CORROSION UNDER SURFACE AND 3 CRACKS. REPAIRED IAW SRM 57-2-0.SDR UPS97224477Rib · corrodedINSPECTION TYPE-C, CORROSION AT THE O/B LOWER BONDING JUMPER ON THE NR 3 K-FLAP RIB. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER EO 5740-3980. REPAIRED PER SRM 57-50-03.SDR UPS97224476Rib · corrodedINSPECTION TYPE-C, CORROSION AT THE I/B LOWER BONDING JUMPER ON NR 3 K-FLAP RIB. REMOVED CORROSION PER EO B727-5740-3980, FOUND TO BE OUT OF LIMITS PER EO B727-5740-3980. REPAIRED PER SRM 57-50-3.SDR DL72E971855Rib · crackedRIB IS CRACKED AT ACTUATOR ATTACH HOLE I/B RIB. PLATE AT ATTACH HOLE IS WORN ON SAME RIB. SMALL LEG ON RIB IS MISSING THAT ATTACHES CHORD ANGLE. REPAIRED PER MM 57-54-00 PG 805 ITEM 2, REPLACED PLATE PER SRM 51-00.SDR DL72E971854Rib · crackedRIB IS CRACKED AT NUT PLATE O/B RIB AT ACTUATOR ATTACH HOLE ON NR 4 SLAT. REPAIR DOUBLER IS CRACKED ON SAME RIB. REPAIRED PER MM 57-54-0 PG 805.SDR CALA9701478Skin · crackedAPPROX 3 CRACK AT RIGHT WING OUTBOARD FORE FLAP LEADING EDGE ABOVE NR 8 TRACK AREA. HOT BOND DOUBLER REPAIR ACCOMPLISHED PER SRM 51-40-6SDR CALA9701472Skin · cracked.25 PREVIOUSLY STOP DRILLED CRACK AT INBOARD LEADING EDGE OF RIGHT WING NR 6 SLAT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3.SDR CALA9701471Skin · crackedTWO SMALL CRACKS AT RIGHT WING NR 6 SLAT AT UPPER TRAILING EDGE SKIN FROM AFT SCREW HOLE WHER INBOARD HOOK MOUNTS. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3.SDR USAA970282Carriage · shearedCLT - DURING VISUAL INSPECTION, FOUND THE RIGHT OUTBOARD FLAP INBOARD CARRIAGE SHEARED 1.25 INCHES FROM THE SHOULDER. PART REPLACED PER CMM 57-53-32. (X)SDR DL757971879Wedge · dentedTHE NR 6 L/E SLAT WAS PUNCTURED ON ITS UPPER SURFACE, 16 OB FROM THE IB EDGE, AND 3 FWD OF THE TE. THE TE WEDGE IS MF FROM ALUMINUM HONEYCOMB WITH ALUMINUM FACESHEETS. THE TE WEDGE IS THE SUBJECT OF TWO AD'S, THEREFORE THIS ER/A WILL AUTHORIZE REPAIR.SDR DL72S971818Web · crackedDURING MV-2 VISIT INSPECTION FOUND CRACKED WEB IN NR 5 SLAT AT INBD SIDE OF ACTUATOR ROD END ATTACH WEB. REPAIRED PER M/M 57-54-0 FIG 804.SDR DL72S971806Web · crackedAT MV2, FOUND WEB CRACKED .5 ON NR 3 AT INBD STOP CUTOUT. STOP DRILLED CRACK AND MADE DOUBLER PER MM 57-54-0 FIG 810. INSTALLED DOUBLER PER MM 57-54-0 FIG 810.SDR DL72S971805Web · crackedAT MV2, FOUND WEB CRACKED 1/2 PAST STOP DRILL IN NR 4 SLAT AT INBD ROD END ATTACH WEB. REMOVED ACCESS PANEL AND DYE CHECKED RIB. STOP DRILLED CRACK PER M/M 57-54-0 FIG 811. FABRICATED AND DRILLED REPAIR PARTS IAW M/M 57-54-0 FIG 804. INSTALLED DOUBLER IAW SDR DL72S971782Angle · crackedANGLE AT NR 8 SLAT O/B UPSTOP IS CRACKED. REPAIRED PER M/M 57-54-0 PG 816.SDR DL72S971781Rib · crackedNOSE RIB AT NR 7 SLAT IS CRACKED. REPAIRED PER M/M 57-54-0 PG 819. REPAIRED UPPER CRACK PER M/M 57-54-00 PG 809.SDR SCNA97325Flap · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND CORROSION BEYOND LIMITS ON NUMBER 4 KRUEGER FLAP OUTBOARD RIB. REMOVED AND REPLACED NUMBER 4 KRUEGER FLAP PER MM 27-81-1.
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