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 SWAA982361Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND CRACKED EXTENDING FROM FASTENER HOLES ON NR 3 SLAT LOWER SKIN. REMOVED AND REPLACED PER BOEING DRAWING 65C30133.SDR MZZA98260Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .625 INCH LONG CRACK WAS FOUND ON NR 6 SLAT INTERIOR FORWARD WEB AT SS 156. THE CRACK END WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. (M)SDR MZZA98254Skin · disbondedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DISBONDED WAS FOUND ON RT WING T/E INBOARD FORE FLAP UPPER SKIN EXISTING FIBERGLASS REPAIR DOUBLER. THE DAMAGED SKIN 13 INCHES BY 1.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR MZZA98239Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP UPPER SKIN AT WBL 72. THE DAMAGED SKIN 7.125 INCH BY 5.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR MZZA98238Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E OUTBOARD FORE FLAP T/E LOWER SKIN AT WBL 485. THE DAMAGED SKIN 2.5 INCH BY 2.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR DL72W981971Spar · crackedSPAR CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.SDR CALA9801830Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 5 SLAT INBOARD AND OUTBOARD RIBS AT ACTUATOR ROD END ATTACH POINT. BOTH THE INBOARD AND OUTBOARD RIBS WERE REMOVED AND REPLACED IAW SRM 51-30-2.SDR TWAA9815002Skin · delaminatedDURING CHECK-C MAINT, FOUND RT WING NR 11 LE SLAT REPAIR LOOSE IN CENTER AREA, 1.5 IN BY 2.5 IN. REMOVED OLD REPAIR. REMOVED 1 IN BY 3 IN DELAMINATION ON O/B END OF OLD REPAIR TO SKIN, AND REMOVED DAMAGED CORE. INSTALLED SKIN AND CORE REPLACEMENT WITH HOT BSDR DL72S982077Rib · crackedAT HMV, FOUND RIB NR 5 AND RIB NR 15 CRACKED. ROUTED FRAME 5. REPAIRED DOUBLER AND FILLER AS PER M/M 57-54-0 FIG 814. OK TO INST REPAIR NR 5 RIB. INSTALLED REPAIR ON NR 5 RIB PER M/M 57-54-0 FIG 814. BEGAN MAKING DOUBLER. FINISHED ROUTING RIB NR 15. REPSDR CALA9801738Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN NR 2 SLAT PANEL ATTACH ANGLE BY ANTI-ICE DUCT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, FIGURE 4.SDR CALA9801737Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN NR 3 SLAT LOWER ATTACH ANGLE FOR PANELS AT ACTUATOR ATTACH AREA. THE CRACK WAS ROUTED OUT. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-4, FIGURE 3.SDR CALA9801734Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 8 SLAT INNER SKIN AT OUTBOARD STRIKER PLATE AREA. THE OUTBOARD STRIKER SKIN PLATE WAS REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR DL72S981896Rib · crackedFOUND ON L/O CK, NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED AT FWD END. REPAIRED PER MM 57-54-0.SDR CALA9801718Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN BOTH INBOARD AND OUTBOARD RIBS OF NR 4 SLAT AT ACTUATOR ROD END ATTACH POINT. THE ACCESS PANEL ON NR 4 SLAT WAS REMOVED IAW SRM 51-30-2. THE CRACKED RIBS WERE REMOVED IAW SRM 51-30-2. NEW RIBS WERE INSTALLED IAW SRM 51-30SDR DL72W982210Guide · wornAT HMV, FOUND GUIDE ON NR 5 SLAT TRAILING EDGE O/B OF ACTUATOR WORN. WEAR LIMITS OK, REPAIRED PER M/M 27-81-11.SDR DL72W982209Angle · crackedAT HMV, FOUND NR 5 SLAT ANGLES - ACTUATOR ATTACH POINT BOTH I/B AND O/B ANGLES CRACKED. STOP DRILLED CRACK PER M/M, FABD REPAIR DOUBLERS, INSTALLED PER MM 57-54-00 FIG 809.SDR CALA9801639Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 8 SLAT INNER SKIN AFT OF ACTUATOR CUTOUT. THE SLAT PANEL WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2.SDR 98ZZZX3541Swivel · shearedDISCOVERED DURING KRUEGER FLAP REMOVAL FOR ACCESS DURING AIRCRAFT D-CHECK. THE INBOARD OF THE TWO KEUGER FLAP ATTACHMENT BOLTS WAS FOUND TO HAVE SHEARED AT THE WASHER ABUTEMENT FLANGE. SUBMITTER SUSPECTED THE WRONG THICKNESS OF WASHER FITTED (A300 IPC 27-81-SDR DHL9870830CSlat · crackedAT C-CHECK, LEFT WING NR 4 L/E SLAT HAS SMALL CRACK AT VERTICAL SUPPORT STRAP NEXT TO ACTUATOR LOWER END AND I/B SIDE. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 X 1 X 9.5. N/R 1694SDR DL73E981814Hinge · failedRT I/B LEADING EDGE FLAP SKIN BENT/CRACKED AT UPPER I/B EDGE DUE TO FAILURE OF I/B HINGE.SDR UPS98227721Rib · crackedINSPECTION TYPE:D CRACK AT NR 6 SLAT I/B TRACK O/B RIB. REPAIRED RIB IAW SRM 51-40-2.SDR 98FDEA00541Fairing · departed98-214 - LT WING NR 1 SLAT WING TO BODY FAIRING DEPARTED A/C ON ROTATION OUT OF MEM.SDR AU981222Slat · delaminated(AUS) NR 1 AND NR 3 LEADING EDGE SLAT TRAILING EDGES DELAMINATING.SDR CALA9801581Track Guide · gougedINSPECTION FOUND THE OUTBOARD TRACK GUIDE FOR NR 3 SLAT INBOARD TRACK GOUGED. THE TRACK GUIDE WAS REMOVED AND A NEW GUIDE WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801577Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT ACTUATOR INBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9801539Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 SLAT AT OUTBOARD HOOK. A REPAIR WAS ACCOMPLISHED IAW SRM 57-50-3, FIGURE 10.SDR DL757981759Wedge · dentedTHE NR 3 SLAT TRAILING EDGE WEDGE WAS FOUND DENTED FROM A BIRD STRIKE. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 (AS REFERENCED IN SRM 57-43-02). SINCE THE SLAT WEDGES ARE THE SUBJECT OF AD T91-22-51, THE REPAIR WAS DOCUMENTED PER ER/A 365517-14AD.SDR DL72W981735Angle · crackedFOUND ON B2 LETTER CK, .5 INCH CRACK COVE SKIN ATTACH ANGLE I/B SIDE OF I/B UPSTOP NR 4 SLAT. REPAIRED PER MM 57-54-0.SDR CALA9801500Skin · crackedINSPECTION FOUND TWO 2.5 INCH CRACKS AT RIVET HEADS FORWARD OF OUTBOARD SEQUENCE CARRIAGE ATTACH POINT OF RT INBOARD FOREFLAP. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30.SDR MWEA98941Skin · chafedLEFT FLAP INBOARD LEADING EDGE EXTERIOR SKIN IS GOUGED AND CHAFED. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.SDR CALA9801452Angle · crackedINSPECTION FOUND APPROXIMATELY A 2 CRACK IN LT WING LEADING EDGE SLAT NR 2 INBOARD SLAT TRACK OUTBOARD SIDE L ANGLE. THE ANGLE WAS REPLACED IAW SRM 57-30-4, 51-20-12, AND 51-30-2.SDR 9810436730Web · crackedDURING M-CHECK, FOUND CRACK ON CENTER WEB TO FITTING ON RIGHT WING, NR 15 KRUEGER FLAP. REPAIRED PER EA 67-162311.SDR 9810186730Web · crackedDURING M-CHECK, FOUND CRACKS IN THE CLOSURE PANEL/WEB OF THE NR 12 KRUEGER FLAP. REPAIRED PER EA 67-158217.SDR DL72W981887Heat Shield · crackedCRACKS IN HEAT SHIELD, NR 6 LE SLAT, ONE IS JUST OUTBOARD OF ACTUATOR ATTACH RIB, THE OTHER IS JUST OUTBOARD OF OUTBOARD TRACK. MANUFACTURED AND INSTALLED DOUBLERS ON HEAT SHIELD SKIN PER MM 57-54-0 FIG 803A. MANUFACTURED AND INSTALLED DOUBLER ON HEAT SHIELDSDR AU981152Slat · delaminated(AUS) NR 2 LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED IN FOUR AREAS. FOUND DURING INSPECTION IAW AD/B767/73.SDR CALA9801414Skin · crackedINSPECTION FOUND A .15625 AND .09375 CRACK IN LT WING NR 4 SLAT LOWER TRAILING EDGE SKIN AT RADIUS OUTBOARD OF INBOARD TRACK, 36.5 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, 51-10-2, AND 51-40SDR DHL98708002Casting · brokenNR 2 LEADING EDGE FLAP HAS BROKEN CASTING AT ACTUATOR MOUNT ON FLAP. REPLACED FLAP PER MM 27-81-1.SDR 98ZZZX3341Slat · separatedON POST-FLIGHT INSPECTION, LT INBD SLAT WAS DISCOVERED MISSING (38) RIVETS ON THE UNDERSIDE AND BOTH INBD RIBS CRACKED AND BROKEN, HOLES VERY ELONGATED. ALSO, WING LEADING EDGE SKIN IMMEDIATELY AFT, MISSING (5) RIVETS, RIBS CRACKED (OLD CRACKS). 1ST STAGE COSDR SWAA981604Bracket · crackedDURING SCHEDULED C2 CHECK, FOUND K-FLAP MOST I/B SEAL BRACKET CRACKED. REPAIRED PER BOEING SRM.SDR UPS98227494Skin · crackedINSPECTION TYPE:D, CRACKS AT NR 8 SLAT UPPER SIDE AT AFT I/B HOOK ATTACH HOLE. REPAIR CARRIED OUT IAW SRM 57-50-3.SDR UPS98227491Rib · crackedINSPECTION TYPE:D, NR 2 LE SLAT RIB CRACKED ADJACENT TO ANTI-ICE DUCT (TELESCOPIC). NR 2 SLAT RIB REPAIRED IAW SRM 51-40-2.SDR DL72S981579Rib · crackedNR 7 SLAT O/B ACTUATOR ATTACH RIB HAS BEEN STOP DRILLED TWICE INDICATING THAT CRACK HAS CONTINUED TO GROW. REMOVED ACCESS PANELS TO RIB. FABRICATED DOUBLER. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER MM 57-54-0 FIG 804. REPAIR OK PER M/M. OK TO CLOSE SSDR DL72S981578Angle · crackedNR 5 SLAT ANGLE CRACKED AT O/B SIDE OF ACTUATOR ATTACH RIB. REMOVED PANELS 6501, 6573 AND 6502 FOR ACCESS. REPAIRED PER MM 57-54-0, FIG 804. INSTALLED PANELS 6501, 6573 AND 6502.SDR AALA981438Skin · corrodedTUL - FOUND CORROSION BEHIND DATA PLATE ON NR 1 AND NR 6 L/E FLAPS. REMOVED DATA PLATE. REMOVED CORROSION AND INSTALLED DOUBLERS PER SRM 57-50-3. (M)SDR CALA9801345Skin · dentedINSPECTION FOUND LT LEADING EDGE SLAT NR 1 SKIN DENTED AT STA XIS 136 AND XIS 132. REPAIRED IAW SRM 57-09, FIGURE 10 AND 10A.SDR SWAA981511Angle · crackedDURING SCHEDULED BC1 CHECK, FOUND NR 6 LE SLAT ACTUATOR DOOR FWD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED PER BOEING MM.SDR DL72S981669Rib · crackedAT HMV FOUND, RIBS CRACKED I/B AND O/B OF GUIDE TRACK NR 6 SLAT I/B GUIDE TRACK. REMOVED ARM, FABRICATED DOUBLER MM 57-54-00 PG 813A, INSTALLED DOUBLER PER SAME.SDR DL72S981537Rib · crackedFOUND ON C-1 LETTER CHECK, 1.5 INCH CRACK IN I/B SLAT ACTUATOR ATTACH NOSE RIB ON NR 1 SLAT. INSTALLED DOUBLER PER M/M 57-54-0 NR 4.SDR TWAA9812126Skin · dentedDURING OP 16 MAINT CHECK, FOUND DENT ON NR 1 L/E SLAT, LT WING, EXCEEDING ALLOWABLE LIMITS PER SRM 57-03, PG 20A. DENT IS 2.5 BY 17 IN BY .150 DEEP. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR PER SRM 57-09, FIG 10F.SDR CALA9801278Rib · crackedINSPECTION FOUND A .375 INCH CRACK AT O/B RIB WHERE LT WING NR 4 SLAT ACTUATOR FORWARD ROD END ATTACHES INSIDE SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.
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