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 DL72W954438Ribs · crackedRIBS ON I/B AND O/B SIDES OF ACT ATTACH POINT NR 4 SLAT ARE CRACKED FWD OF PREVIOUS REPAIRS. REMOVED OLD DOUBLERS AND DAMAGED AREAS, FABRICATED DOUBLERS PER M/M 57-54-0 FIG 804 AND INSTALLED DOUBLERS PER M/M 57-54-0.SDR DL767954527Skin · delaminatedTHE NR 8 L/E SLAT T/E WEDGE WAS FOUND TO HAVE UPPER SKIN DELAMINATED. REPAIRED PER DL ERA 272443-14AD.SDR DL757960034Te Wedge · wornDURING SHOP INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH TRAILING EDGE WEDGE WORN AND GOUGED. REPAIRED WEDGE PER SRM 51-70-10.SDR UPS805090Skin · crackWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING INBD SLOT PANEL HAS 1 INCH LONG CRACK ON TOP SIDE. REPLACED SLOT PANEL PER MM 27-80-01.SDR UPS805073Chord · crackedWHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E AT THE OTBD END OF THE OTBD SLOT, UPPER TEE CHORD IS CRACKED AT THE OTBD END. THE CRACK IS APPROX 1.8 INCH. STOP DRILLED CRACK IAW SRM 57-2-0. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-2-0 FIG D.SDR DL72S954564Angle · crackedDURING SHOP INSPECTION, THE LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE ACTUATOR RIB. THE CRACK WAS REPAIRED PER THE B-727 M/M 57-54-0 FOR NR 5 L/E SLAT.SDR DL72S954563Skin · crackedDURING SHOP INSPECTION, A CRACK WAS FOUND IN THE EXTERIOR SKIN 37.5 INCHES FROM THE OUTBOARD END AT THE FENCE ATTACH POINT. THE DAMAGE WAS REPAIRED PER THE B-727 M/M 57-54-0, PG 817 FOR NR 5 L/E SLAT.SDR DL72S954562Rib · crackedDURING SHOP INSPECTION, RIB NR 17 WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER B-727 M/M 57-54-0 FOR NR 5 L/E SLAT.SDR DL72S954410Angle · crackedFOUND DURING A-1 LETTER CHECK, 4 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0.SDR 95FDEA01754Flap · corrosionDUE TO EXCESSIVE CORROSION (C57-562-01-2) NR 5 K-FLAP REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 5 K-FLAP IAW FEDEX MM 27-81-1. C/A ADDITION.SDR DL757954538Te Wedge · brokenDURING CRUISE, HAD VIBRATION IN CABIN AT ROWS 23 TO 28. FOUND NR 6 L/E SLAT PANEL TRAILING EDGE WEDGE BROKEN OUT AND VIBRATING. ALSO, A SECTION APPROX 10 BY 20 WITH SURROUNDING HONEY COMB DAMAGED. REPLACED SLAT ASSEMBLY FOR RETURN TO SERVICE.SDR DL72S954364Angle · crackedFOUND ON A2 LETTER CK, .5 INCH VISIBLE CRACK ON COVE SKIN ATTACH ANGLE BELOW THE OUTBOARD STOP PAD NUMBER 5 SLAT. REPAIRED PER MM 57-54-0.SDR CAL951047Skin · crackedIAH - FLT 1879 - INSPECTION FOUND A 3 INCH CRACK IN LOWER SKIN AT OUTBOARD END OF NR 4 LEADING EDGE SLAT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02393. (X)SDR CAL951046Skin · crackedIAH - FLT 1879 - INSPECTION FOUND A 3 INCH CRACK IN LOWER SKIN AT INBOARD END OF NR 5 LEADING EDGE SLAT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02394. (X)SDR DL757960041Te Wedge · damagedUPON ROUTINE INSPECTION, T/E WEDGE WAS FOUND DENTED. REPLACED WEDGE AS PER 57-43-02. ALSO, PERFORMED TERMINATING ACTION OF AD 90-23-06 BY INSTALLING T/E WEDGE 114N3003-34.SDR DL72S960162Rib · crackedNR 5 RIB CRACKED ON FORWARD FLANGE. REPAIRED PER M/M 57-54-0 FIGURE 809. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT.SDR EISA95483Rib · crackedNR 4 SLAT INBOARD AND OUTBOARD NOSE RIB CRACKED AT PREVIOUSLY INSTALLED DOUBLERS WHERE ACTUATOR ROD END ATTACHES. FABRICATED DOUBLERS PER SRM 57-50-03. INSTALLED DOUBLERS PER SRM 57-50-3. (M)SDR EISA95473Bracket · crackedLEFT BRACKET FOUND CRACKED AT OUTBOARD SIDE OF NR 7 SPOILER ACTUATOR CASTING. FABRICATED AND INSTALLED WEB REPAIR IAW SRM 51-40-2. (M)SDR EISA95452Rib · crackedRT WING NR 5 SLAT OUTBOARD NOSE RIB CRACKED WHERE ROD END ATTACHES. REMOVED AND REPLACED RIB IAW SRM 51-10-4. (M)SDR DL757954278Te Wedge · delaminatedDURING SHOP INSPECTION, NR 5 L/E SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED T/E WEDGE PER SRM.SDR DL72L954359Skin · crackedFOUND ON CV2 CHECK, .25 INCH CRACK IN NR 5 SLAT COVE SKIN AT CUTOUT FOR I/B STOP PAD. REPAIRED PER SRM 57-50-3 FIG 23.SDR DL72S954259Angle · crackedDURING F-1 LETTER CHECK, FOUND .375 INCH CRACK AND 1 INCH CRACK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0.SDR CA951116015Hinges · corroded(CAN)DURING ROUTINE INSPECTION THE #2 AND #3 OUTER KRUEGER FLAP HINGES SIGNIFICANTLY CORRODED, EXFOLIATION, AT THE TOP END PIVOT. REPLACED.SDR DL72E954224Angle · crackedFOUND DURING A-2 LETTER CHECK, .25 INCH CRACK IN NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72K954217Angle · crackedFOUND ON A2 LETTER CK, .25 INCH CRACK NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0.SDR DL72W954275Rib · crackedDURING HMV, FOUND NR 8 SLAT, NR 3 L/E REINFORCING RIB CRACKED. REMOVED O/B TRACK FOR ACCESS AND REPAIRED RIB PER M/M 57-54-0 PG 806 AND 807.SDR DL757960032Te Wedge · delaminatedT/E DELAMINATED, REPLACED WEDGE PER SRM 57-43-02. FOUND DURING SHOP INSPECTION FOR NR 7 SLAT.SDR ASAA9580250Fitting · crackedOAK - DURING C-CHECK, CRACK WAS FOUND ON NR 2 L/E SLAT LT OUTBOARD FITTING. REPLACED FITTING IAW DOUGLAS DRAWING 5922534. TAC: 24866.(X)SDR DL72S954123Angle · cracked.25 INCH CRACK, NR 8 SLAT, LWR COVE SKIN ATTACH ANGLE BELOW TAIL DUCT AT PREVIOUS DOUBLER. FOUND AT A-2 LTR CK. REPAIRED PER MM 57-54-0.SDR DL72S954122Angle · cracked.25 INCH CRACK, NR 5 SLAT, LWR COVE SKIN ATTACH ANGLE BELOW O/B STOP PAD. FOUND AT A-2 LTR, CK. REPAIRED PER MM 57-54-0.SDR DL72L954329Angle · crackedDURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH THE LOWER ANGLE CRACKED AT THE I/B SIDE BEHIND UPSTOP. REPAIRED PER MM 57-54-0 FIG 812.SDR DL72L954230Rib · crackedDURING THE SHOP INITIAL INSPECTION, THE INBOARD ACTUATOR RIB WAS FOUND TO HAVE CRACKED AT THE FORWARD LOWER CORNER WHERE THE RIB ATTACHES TO THE SLAT SPAR. THE RIB WAS REPAIRED PER SRM 57-54-0 FIG 804.SDR 96ZZZX2839Bracket · crackedCRACKED DOUBLER INSIDE NR 2 L/E SLAT AT BASE OF INBOARD TRACK OUTBOARD RIB. REMOVED CRACKED BRACKET, STOP DRILLED RIB, FABBED AND INSTALLED NEW L-ANGLE BRACKET PER SRM 5750-3, FIGURE 9.SDR DL757954147Skin · delaminatedA PREVIOUS REPAIR TO THE UPPER SKIN OF THE TRAILING EDGE WEDGE OF THE NR 5 LEADING EDGE SLAT IS DELAMINATED. THE DELAMINATION MEASURES 4 INCHES BY 3.5 INCHES AND IS CENTERED 10 INCHES FROM THE OTBD END AND 6 INCHES FWD OF THE T/E. THE SLAT IS IDENTIFIED AS ASDR DL72S954300Rib · crackedDURING HMV, FOUND NR 7 SLAT, NR 8 RIB CRACKED AND NR 10 RIB MISSING FASTENER AND ONE IS LOOSE. REPAIRED NR 8 PER M/M 57-54-0 PGS 818 AND 819. REPLACED LOOSE AND MISSING FASTENER ON NR 10 RIB.SDR DL72S954299Rib · crackedDURING HMV, FOUND NR 6 SLAT, NR 7 RIB WAS CRACKED. STOP DRILLED CRACK AND REPAIRED RIB PER M/M 57-54-0 FIG 814.SDR DL72S954298Rib · crackedDURING HMV, FOUND NR 6 SLAT, NR 12 RIB WAS CRACKED. STOP DRILLED NR 12 RIB AND REPAIRED CRACK PER M/M 57-54-0 FIG 814.SDR DL72S954297Rib · crackedDURING HMV, FOUND NR 5 SLAT, NR 1 RIB WAS CRACKED. REPAIRED CRACKED RIB PER M/M 57-54-0.SDR DL72S954296Rib · crackedDURING HMV, FOUND NR 4 SLAT, NR 3 RIB WAS CRACKED. MANUFACTURED AND INSTALLED REPAIR PER M/M 57-54-0 PG 818.SDR DL72S954295Rib · crackedDURING HMV, FOUND NR 4 SLAT, NR 2 RIB WAS CRACKED. FABRICATED REPAIR AND INSTALLED PER M/M 57-54-0 PG 818.SDR DL72S954294Rib · crackedDURING HMV, FOUND NR 2 SLAT, RIB NR 6 WAS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-1 PG 818.SDR DL72S954293Rib · crackedDURING HMV, FOUND NR 2 SLAT, RIB NR 7 WAS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-0 PG 818.SDR DL72S954292Rib · crackedDURING HMV, FOUND NR 2 SLAT, RIB NR 8 IS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-0 PG 819.SDR DL72S954290Rib · crackedDURING HMV, FOUND NR 3 SLAT, NR 12 RIB WAS CRACKED. FABRICATED REPAIR DOUBLER AND INSTALLED PER 57-54-0.SDR DL72W954093Angle · crackedFOUND ON A1 LETTER CK, NR 2 SLAT COVE SKIN ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.SDR DL72W954092Angle · crackedFOUND ON A1 LETTER CK, .5 INCH CRACK AT INBD STOP PAD NUMBER 7 SLAT. REPAIRED PER MM 57-54-0.SDR DL72S954291Rib · crackedDURING HMV, FOUND NR 2 FLAT, RIB NR 18 CRACKED AT UPPER SKIN AREA. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER M/M 57-54-00 FIG 809. INSTALLED DOUBLER.SDR DL72S954436Rib · crackedDURING INSPECTION, NR 2 L/E SLAT WAS FOUND WITH L/E SUPPORT RIB NR 3 CRACKED. REPAIRED PER SRM 57-50-3.SDR DL72S954060Angle · crackedNR 6 L/E SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER SRM 57-54-0. FOUND AT LETTER CHECK.SDR 9516716613Flap · damagedAFTER FLIGHT ARRIVAL, MAINTENANCE DISCOVERED THAT A LARGE SECTION OF THE NR 11 LEADING EDGE FLAP WAS MISSING. NO OTHER DAMAGE WAS FOUND. REPLACED FLAP PER MM 27-81-01, PG 401. CHECKED OK. (STA AMS).
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