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 CALA9800605Ribs · crackedINSPECTION FOUND A 1 INCH CRACK IN THREE RIBS OF NR 1 LT SLAT. THE CRACKED RIBS WERE REMOVED. NEW RIBS WERE FABRICATED AND INSTALLED IAW SRM 57-55-01 FIGURE 2 51-20-00 AND 51-31-01.SDR SWAA980421Skin · crackedDURING SCHEDULED C4 CHECK, FOUND NR 1 KRUEGER DEFLECTOR DOOR CUTOUT CRACKED .25 AT RADIUS. REPAIRED PER SWA RA 1-357-0540.SDR 98FDEA00218Rib · corrodedLEFT WING NR 2 LEADING EDGE SLAT, INBOARD CLOSURE RIB IS BADLY CORRODED ON THE INSIDE, EXFOILATED. *S/D* COMPLIED WITH EA 8-5750-38493.SDR DL76S980655Wedge · delaminatedWINGS NR 1 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 1 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 4 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364345-14AD.SDR DL76S980654Wedge · delaminatedWINGS NR 2 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 2 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 7 BY 4.5 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364346-14AD.SDR DL76S980653Wedge · delaminatedWINGS NR 8 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 5 BY 9 AREA OF DELAMINATION ON THE UPPER SKIN. THE DELAMINATION WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364347-14AD.SDR DL76S980652Skin · delaminatedWINGS LEADING EDGE SLAT NR 11, TRAILING EDGE WEDGE, SKIN DELAMINATION REPAIR. THE UPPER SKIN OF THE NR 11 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 6 AREA OF DELAMINATION. THE DAMAGE WAS TRIMMED OUT AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER SDR VJ9800058Fitting · gougedATTACH FITTING RT WING, NR 1 SLAT MAIN TRACK (CENTER), GOUGED. BLENDED AREA IAW DC9 SRM 53-01, FIG 1. BLEND DEPTHS WITHIN LIMITS PER RES 1 1668, TREATED AREA IAW SRM 51-10-3 AND AERO EO 98-822, COMPLETED FORM 8110-3. (M)SDR UPS98226214Rib · crackedINSPECTION TYPE-C, NR 4 LE SLAT CRACK ON RIB (THIRD FROM OUTBOARD). REPAIR CARRIED OUT IAW SRM 51-40-3 FIGURE 1.SDR UPS98226212Rib · crackedINSPECTION TYPE-C, NR 4 LE SLAT CRACK ON RIB (THIRD FROM OUTBD). DAMAGED AREA BLENDOUT IAW SRM 51-40-01.SDR SWAA980369Skin · crackedDURING SCHEDULED C2 CHECK, FOUND CRACK ON L/E SKIN AT KRUEGER FLAP SEAL DOOR CUTOUT. REPAIRED PER SWA RA 1-357-0538.SDR EIAA980152Skin · damagedHKG - DURING 'B' CHECK INSPECTION, NR 18 L/E FLAP BULLNOSE INBOARD END SKIN DAMAGED. REPAIRED IAW SRM 57-50-03 FIG 8. (M)SDR DL72S980622Web · crackedNR 8 SLAT ACT I/B AND O/B ATTACH ANGLE CRACKED AT WEB. REPAIRED PER MM 57-20-21.SDR DL72S980621Angle · crackedFOUND ON A1 LETTER CK, NR 8 SLAT LOWER ATTACH ANGLE CRACKED AT THE INBD STOP PAD. REPAIRED PER MM 57-54-0.SDR CALA9800576Skin · debondingINSPECTION FOUND RT WING NR 6 KRUEGER FLAP DEBONDING. A REPAIR WAS ACCOMPLISHED IAW ECRA 5720-01064.SDR CALA9800555Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 LEADING EDGE SLAT FIRST RIB INBOARD OF ACTUATOR AT WS 629. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-0.SDR DL76S980618Wedge · delaminatedTHE RT NR 8 SLAT WAS FOUND WITH A 2.5 DIAMETER AREA OF DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. THE DAMAGE WAS TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364264-14AD.SDR DL76L980582Wedge · gougedTHE LT WING NR 7 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 1INCH LONG GOUGE THROUGH THE LOWER SKIN. THE DAMAGE WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364249-14AD.SDR DL767980581Wedge · dentedTHE RT WING NR 7 SLAT WAS FOUND WITH A 5 X 2.5 X .025 DENT ON THE LOWER SURFACE THE TRAILING EDGE WEDGE. THE DENT WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A364235-14AD.SDR CALA9800440Skin · dentedINSPECTION FOUND A DENT 19.5 INCHES FROM OUTBOARD END IN LT WING NR 2 LEADING EDGE SLAT UPPER SKIN. A REPAIR WAS INSTALLED IAW SRM 57-50-3.SDR CALA9800436Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 1 SLAT LOWER LEADING EDGE SKIN TO INBOARD TRACK ATTACH BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1.SDR 98FDEA00161Panel · missingNR 7 LEADING EDGE SLAT ACTUATOR DOOR MISSING. * S/D* REPLACED AND ADJUSTED NR 7 SLAT ACTUATOR DOOR PER MAINTENANCE MANUAL 27-81-32, OPERATIONAL CHECK NORMAL.SDR DL767980499Wedge · delaminatedTHE LT WING NR 4 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF SKIN DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364149-14AD.SDR CALA9800359Vane · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP VANE AT STA XW 280. THE FLAP VANE WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 27-50-01.SDR DHL9872631CChord · crackedAT D CHECK, NR 3 SLAT HAS CRACKS IN CHORD BELOW TAI DUCT INSIDE SLAT. STOP DRILLED CRACK. NDT CRACK, INSTALLED REPAIR PER SRM 51-40-4. N/R 1294.SDR CALA9800358Vane · disbondedINSPECTION FOUND LT WING INBOARD FLAP VANE DISBONDED ON UPPER SURFACE. THE FLAP VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 57-54-00.SDR DL72S980489Rib · crackedFOUND DURING D-1 LETTER CHECK, NR 6 L/E SLAT ACTUATOR ATTACH RIB CRACKED AT PREVIOUS REPAIR. REPAIRED PER M/M 57-54-0 AND ERA 364139-14.SDR DL72S980480Angle · crackedFOUND DURING B-2 LETTER CHECK, NR 2 SLAT COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.SDR CALA9800338Rib · crackedINSPECTION FOUND A 4 CRACK IN FLANGE OF LT NR 1 SLAT OUTBOARD END RIB. THE WEB AND RIB WERE REMOVED IAW SRM 51-31-10. A NEW RIB WAS INSTALLED IAW 51-31-10 AND 51-21-01. SKIN WAS INSTALLED IAW SRM 51-01-10.SDR 98FDEA00149Skin · crackedRT WING NR 8 L/E SLAT, LOWER SKIN TANG BELOW INBD TRACK ATTACH CRACKED AND RIVETS PULLED. ACCOMPLISHED REPAIR ON RT WING NR 8 L/E SLAT FOR CRACKED LWR SKIN TANG BELOW INBOARD TRACK PER AA 7-5750-29381 AND AA SRM 57-50-1 PGS 7A AND 7B.SDR DL76S980466Skin · delaminatedTHE NR 2 LEADING EDGE SLAT WAS FOUND WITH A 5 DIA DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. THE NR 4 SLAT WAS FOUND WITH A 7 DIA DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. BOTH DELAMINATIONS WERE REPAIRED PER THE B767 SRM 57-SDR DL72W980459Bracket · crackedFOUND AT B2 LETTER CHECK, NR 2 LE FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER EDGE. REPAIRED PER M/M 57-20-21.SDR 98ZZZX1275Slat · damagedAFTER ARRIVAL, INSPECTION FOUND DAMAGES TO SLAT NR 9 LEADING EDGE. AIRCRAFT WAS GROUNDED DUE TO UNAIRWORTHY CONDITION. INCIDENT UNDER INVESTIGATION.SDR UPS98225856Rib · crackedINSPECTION TYPE-SI, WHILE WORKING CARD NR 465869 FOUND L/W NR 3 SLAT O/B TRACK O/B TRACK RIB CRACKED. INSTALLED NEW RIB AT O/B TRACK STATION PER 727 SRM 51-30-2.SDR DL767980419Wedge · delaminationTHE UPPER SKIN OF THE LT WING NR 4 SLAT TRAILING EDGE WEDGE WAS FOUND WITH 2 AREAS 2 INCH DIAMETER DELAMINATIONS. THE THE DAMAGE WAS REPAIRED PER THE B767 SRM AND DOCUMENTED PER ER/A 364074-14AD.SDR DL72K980425Bracket · crackedNR 8 SLAT I/B AND O/B ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-20-21 P 812.SDR DL72S980406Rib · crackedNR 6 SLAT RIB CRACKED. REPAIRED PER M/M 57-54-0.SDR P5CA9800320Flap · crackedLT WING NR 3 L/E FLAP INBD ACTUATING ARM NOSE AREA L/E NOSE BEAM RIB CHORD FLANGE AT LOWER END FOUND CRACK. NOSE BEAM RIB CHORD REPAIRED PER SRM 57-20-03.SDR DL767980421Wedge · delaminatedTHE UPPER SKIN OF THE RT WING NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 4 X 2.5 AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364048-14AD.SDR DL767980420Wedge · delaminationTHE UPPER SKIN OF THE LT WING NR 5 SLAT WAS FOUND WITH A 1 INCH DIAMETER AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364049-14AD.SDR AALA980372Structure · corrodedTUL - CORROSION INSIDE MAIN SECTION OF KRUEGER FLAP. REPLACED MAIN KRUEGER FLAP WITH NEW SERVICEABLE FLAP. TST: 25,415.42 HOURS. CYCLES: 9,488. (X)SDR TWAA9804009Skin · delaminatedLAX - DURING C-CHECK MAINTENANCE, NR 6 LE SLAT INBAORD TOP SIDE WAS DELAMINATED AT TOP CENTER, 9 INCH BY 2 INCH, 36 INCH FROM INBOARD END. REPAIRED DELAMINATED AREA PER 51-70-10 AND SEALED EDGES. (M)SDR MZZA98104Rib · crackedKUL - NR 6 SLAT HAS CRACKING IN THE FOLLOWING PLACES UPPER SKIN AT OUTBOARD HOOK AFT FASTENER HOLE (2 CRACKS), EYE END ATTACH INBOARD RIB AT UPPER FWD CORNER AND LOWER AFT CORNER. REPAIR CARRIED OUT TO THE UPPER SKIN OF OUTBOARD HOOK AS PER SRM 57-50-3. REPLSDR UPS98225861Bullnose · corrodedINSPECTION TYPE-SI, L/W NR 2 K-FLAP BULLNOSE I/B MOUNT LUG CORRODED AROUND I/B FASTENER. REMOVED CORRODED BULLNOSE, CORROSION OUT OF LIMITS, INSTALLED SERVICABLE BULLNOSE IAW MM 27-81-01.SDR MWEA98159Panel · corrodedLEFT HAND WING SLAT ACCESS PANEL NR 1136A FOUND PITTING CORROSION ON THE OUTER SURFACE. REPAIRED IAW SRM 57-01 FIG 3.SDR P5CA9800429Panel · corrodedLEVEL 1 CORROSION ON NUMBER 13 LEADING EDGE FLAP INBOARD CORNER INTERNAL PANEL. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.SDR CALA9800260Rivets · shearedINSPECTION FOUND A ROW OF SHEARED RIVETS AND A BROKEN BRACKET ON LT WING NR 1 LEADING EDGE SLAT LOWER EDGE INBOARD SKIN SURFACE. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.SDR CALA9800223Slat · damagedA CATERING TRUCK STRUCK THE RT OUTBOARD NR 6 SLAT. A REPAIR WAS COMPLETED IAW SRM 57-43-01.SDR P5CA9800430Skin · dentedDENT ON NUMBER 11 LEADING EDGE FLAP BULL NOSE SKIN. REPAIRED PER BAC SRM 51-40-01 AND TREATED PER SRM 51-10-02.SDR CALA9800231Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN LT WING NR 2 SLAT CHORD ANGLE BELOW WHERE INBOARD STOP PAD MOUNTS. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-01.
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