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 DL72S981085Rib · crackedFOUND ON A-1 LETTER CHECK, NR 6 SLAT NOSE RIB CRACKED I/B SIDE OF ACTUATOR .75 INCH. REPAIRED PER M/M 57-54-0.SDR DL76S981053Skin · delaminatedNR 1 L/E SLAT T/E WEDGE WAS FOUND TO HAVE THE UPPERR SKIN DAMAGED AT A LOCATIONS WHICH IS APPROX 24 INCHES FROM THE OUTBD EDGE AND RUNS APPROX 2 INCHES FWD FROM THE AFT EDGE. REPAIRED PER ERA 364811-14AD.SDR DL72S981068Skin · crackedNR 5 L/E FLAP CRACKED AT I/B GATE HINGE CUTOUT O/B SIDE. REPAIRED PER M/M 57-53-0.SDR UPS98226830Rib · crackedINSPECTION TYPE:C, CRACK GROWING PAST STOP DRILL HOLD IN NR 4 SLAT I/B END RIB. REMOVED CRACKED RIB AND REPLACED WITH NEW ITEM PER SRM 51-30-2 AND SRM 20-50-01.SDR 98UAL900292Bracket · brokenFOUND (P/N 114W2512-18) SKIRT EXTENSION BRACKET, FOR THE MAIN RIBS INBOARD NR 8 SLAT, BROKEN IN HALF AND CRACKED AT THE FASTENER AREA AT END. *S/D* DAMAGED PART REPLACED AT LHR.SDR EIAA980203Slat · bentSIT - ON POST FLIGHT WALKAROUND, FOUND LEFT WING SLAT ASSEMBLY BENT WITH SLIP JOINT BETWEEN SEGMENT NR 1 AND NR 2 BENT AND BUCKLED. (M)SDR DL72L981042Angle · crackedFOUND ON E1 LETTER CK, 1 INCH CRACK INBD ATTACH CASTING NR 5 L/E SLAT ACTUATOR. REPLACED ANGLE.SDR DL72L981041Angle · crackedFOUND ON E1 LETTER CK, 1.25 INCH CRACK INBD ATTACH CASTING FOR NR 4 L/E EDGE SLAT ACTUATOR. REPLACED ANGLE.SDR DHL9870629CRib · crackedAT C-CHECK, NR 1 SLAT INBD TRACK OUTBD RIB IS CRACKED AT FWD END. STOP DRILLED, HFEC, INSTALLED DOUBLER PER SRM 57-50-3, 1 X 4. N/R 1668.SDR DHL9870628CRib · crackedAT C-CHECK, NR 4 SLAT INBD TRACK OUTBD RIB IS CRACKED PAST STOP DRILL. STOP DRILLED END OF CRACK, HFEC, FABRICATED RIB REPAIR PER SRM 57-50-3, 4 X 5. N/R 1667.SDR UPS98226735Flap · corrodedINSPECTION TYPE:C, NR 5 K-FLAP NOSE FLAP TO K-FLAP BONDING JUMPER BOLTS HOLES ARE CORRODED. REMOVED AND REPLACED K-FLAP ASSEMBLY DUE TO NO FLAP NOSE ASSEMBLY AVAILABLE PER MM 27-81-01.SDR DHL9870626CAngle · crackedAT C-CHECK, LEFT WING L/E, NR 2 SLAT OUTBD TRACK, INBD SUPPORT RIB AFT VERTICAL DOUBLER HAS A VERTICAL CRACK AT BOTTOM. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 57-10-1, 16 LONG. N/R 1615.SDR DL72W981026Rib · crackedFOUND ON C1 LETTER CK, L/E NOSE RIB CRACKED 1.25 INCH PAST, STOP DRILL, NR 5 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PER MM 57-54-0.SDR DHL9870633CAngle · crackedAT C-CHECK, TR WING NR 5 KRUEGER FLAP ACTUATOR INBD VERTICAL SUPPORT ANGLE CRACKED IN RADIUS FWD UPPER END. REMOVED AND REPLACED VERTICAL SUPPORT ANGLE, 7 X 5. N/R 2020.SDR DHL9870612CSkin · crackedAT C-CHECK, RIGHT WING LEADING EDGE NR 6 SLAT INBD TRACK CUTOUT HAS 1 INCH CRACK AT TOP END. STOP DRILLED, HFEC OF STOP DRILL, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 3 X 3. N/R 2042.SDR TWAA9807911Skin · delaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND NR 7 LE SLAT WITH 4 INCH BY 3 INCH BULGE ON AFT SIDE OF SLAT, WITH 5/16 IN HEIGHT, APPROX 5.5 FEET FROM INBOARD END AND 2 INCHES ABOVE SEAL. REMOVED DELAMINATED AREA, FOUND NO EVIDENCE OF WATER. INSTALLED CORE AND DOUBSDR TSAA9807911Skin · delaminatedLAX - DURING CHECK-C., MAINTENANCE FOUND NR 7 LE SLAT WITH 4 INCH BY 3 INCH BULGE ON AFT SIDE OF SLAT WITH .3125 INCH IN HEIGHT, APPROX 5.50 FEET FROM INBD END AND 2 INCHES ABOVE SEAL. REMOVED DELAMINATED AREA, FOUND NO EVIDENCE OF WATER. INSTALLED CORE AND SDR SWAA980829Skin · crackedDURING SCHEDULED BC4 CHECK, FOUND NR 4 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD MAIN TRACK. REPAIRED PER BOEING DRM NR 65C30133.SDR SWAA980815Seal · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND NR 1 KRUGER FLAP SEAL CRACKED OUT/BD TOP. REMOVED AND REPLACED PER BOEING SRM.SDR DL72S980968Skin · crackedA 1.5 INCH CRACK AT NR 3 L/E FLAP I/B LIP HINGE CUTOUT. REPAIRED PER M/M 57-53-0 AND ERA 364735-14.SDR UPS98226588Skin · crackedINSPECTION TYPE-SI, NR 2 SLAT LOWER SKIN FASTENERS SHEARED AND CRACK EMITTING FROM FASTENER HOLE JUST BELOW UPSTOP (I/B). REMOVED AND REPLACED NR 2 SLAT IAW MM 27-81-11.SDR CALA9800774Rib · crackedFOUND CRACK (2) IN SLAT NUMBER 1 RT. CRACKED RIB REMOVED, INSTALLED NEW RIB ARB1566-502 AS ORIGINAL PER SRM 51-31-01.SDR P5CA9800937Skin · damagedRT WING NR 16 KRUEGER FLAP CAVITY FWD CUTOUT FOUND CRACK AT ILES 542. REPAIRED IAW SRM 51-40-03 FIG 1.SDR DL76L980893Wedge · delaminatedWING, NR1 LEADING EDGE SLAT, TRAILING EDGE WEDGE. DELAMINATION REPAIR A 1.5 BY 1.2 AREA OF DELAMINATION WAS FOUND ON THE UPPER SURFACE OF THE TRAILING EDGE WEDGE ON THE NR 1 SLAT. THE DELAMINATION WAS REPAIRED PER THE B676 SRM 57-43-02 AND DOCUMENTED PERSDR DL72S980879Rib · crackedFOUND ON E2 LETTER CK, 2 CRACKS IN NR 7 SLAT NOSE RIB AT THE OUTBD SIDE OF THE ACTUATOR. REPAIRED PER MM 57-54-0.SDR ARWA980499Skin · damagedDURING D-CHECK, FOUND REMOVED TEMPORARY REPAIR LEFT WING LEADING EDGE SLOT AT STA XFS 526. PERFORMED REPAIR OF LEFT HAND WING LEADING EDGE SLOT AT XFS=526 AS APER EO 98012105 AND ARROW AIR RED BORDER NR 8071.SDR TWAA9807007Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND ANGLE BRACE CRACKED AND DOUBLER BELOW ALSO CRACKED, JUST INBD OF NR 2 LE SLAT INBD TRACK. MANUFACTURED ANGLE BRACE AND DOUBLER AND INSTALLED PER SRM 51-01, PAGE 1 ITEM C, AND STANDARD PRACTICES. (X)SDR G60A022Skin · dentedDURING WALK-AROUND, GROUND MAINTENANCE FOUND A DENT IN THE RIGHT HAND NR 1 LEADING EDGE SLAT. THE DENT WAS 6 INCHES LONG BY 4 INCHES WIDE AND .125 INCHES DEEP. GROUND MAINTENANCE REWORKED THE AREA TO ALMOST SMOOTH SURFACE AND APPLIED FILLER MATERIAL IAW SRM SDR DL757980870Te Wedge · dentedWING RT, NR 8 SLAT, TRAILING EDGE WEDGE REPAIRED FOR DENT. THE TRAILING EDGE WEDGE ON THE RT WING NR 8 SLAT WAS FOUND WITH A 4 BY .875 BY .040 DEEP DENT. THE DAMAGED AREA WAS REPAIRED PER B757 SRM 57-43-02, FIG. 201. BECAUSE THE SLAT WEDGES ARE THE SUBJECT SDR DL72E980871Bracket · crackedFOUND ON F1 LETTER CHK, NR 1 SLAT ACT IB MOUNT BRACKET CRACKED AT WEB. REPAIR PER M/M 57-20-21.SDR DHL9870745CAngle · crackedAT C-CHECK, 36 SLAT ACTUATOR ACCESS PANEL ATTACH ANGLES ARE CRACKED. REPLACED ANGLES PER SRM 51-40-4, N/R 2814.SDR DHL9870706CAngle · crackedAT C-CHECK, NR 5 SLAT THE INBD SLAT TO TRACK ATTACH ANGLES ARE CRACKED. REPLACED ATTACH ANGLES PER SRM 51-40-4, 4.25. N/R 2808SDR F3LA98033Skin · crackedPAE - DURING C-CHECK, INSPECTION REPORTED NR 1 SLAT SKIN CRACKED AROUND FASTENER HEADS. MAINTENANCE REMOVED DAMAGED AREA (18 INCH BY 4.5 INCH). FABRICATED REPLACEMENT PARTS PER BOEING DRAWING 65C 30133, SHEET 3, AND REPAIRED PER SRM 51-40-02. (M)SDR DL72S980959Bracket · crackedACTUATOR ATTACH BRACKET CRACKED FWD LOWER INBD CORNER OF NR 5 KRUEGER FLAP. REPAIRED PER M/M 57-20-21 FIG 807.SDR MWEA98495Skin · tornRT NR 4 SLAT HAS TORN METAL SKIN AT FASTENER HOLES ON THE OUTBOARD EDGE. MTC REPAIRED SKIN USING APPROVED DATA.SDR DL72K981029Bracket · crackedNR 8 SLAT ACT ATTACH BRACKET CRACKED AT WEB. REPAIRED PER MM 57-20-21 P 812.SDR DL72S980835Rib · crackedFOUND ON A1 LTR CHECK, NR 4 SLAT NOSE RIB CRACKED 1.5 INCH O/B SIDE OF ACTUATOR ROD END. REPAIRED PER M/M 57-54-0.SDR DL72S980832Stiffener · crackedFOUND ON A1 LETTER CK, 2 SPAR STIFFENERS CRACKED AT NR 7 SLAT INBD AND OUTBD STIFFENERS AT THE OUTBD TRACK. REPLACED STIFFENERS PER MM 57-20-21.SDR SWA980613Skin · crackedDURING SCHEDULED D CHECK, FOUND CRACKED NR 5 SLAT LOWER SKIN AT FS 172, AFT ROW. REMOVED AND REPLACED PER DRAWING 65C30133 BOEING SRM.SDR SWA980612Skin · crackedDURING SCHEDULED D CHECK, FOUND CRACKED NR 5 SLAT LOWER SKIN AT WBL 167.5, AFT ROW. REMOVED AND REPLACED PER DRAWING 65C30133 BOEING SRM.SDR DL76S980782Wedge · delaminatedDELAMINATION WAS FOUND ON THE NR 1 L/E SLAT TRAILING EDGE WEDGE NEAR THE INB'D END. DELAM WAS APPROX 3 BY 6. REPAIRED PER ERA 364501-14AD.SDR EISA98077Skin · crackedWHILE ACCOMPLISHING 'B' CHECK WORK CARD, A .20 INCH LONG CRACK WAS NOTED AT OUTBOARD END OF NR 1 SLAT. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 57-02. (M)SDR F3LA98015Skin · delaminatedPAE - DURING C-CHECK, MAINTENANCE REPORTED DISBONDING ON NR 4 SLAT TRAILING EDGE WEDGE OUTBOARD UPPER END. MAINTENANCE REMOVED 52.0 INCHE OF DELAMINATED SKIN FROM OUTBOARD LOWER SURFACE, 13 INCHES OF DELAMINATED SKIN FROM OUTBOARD UPPER SURFACE AND 15 INCHES SDR DL72W980767Rib · crackedFOUND ON E1 LETTER CK, 1 INCH CRACK AT NR 7 SLAT ACTUATOR ATTACH RIB I/B SIDE. REPAIRED PER MM 57-54-0.SDR TSAA9827199Guides · wornFLT 272 - HNL-OGG - DURING APPROACH PHASE WITH FLAPS 5 SET, THE NR 3 SLAT TRANSIT LIGHT REMAINED ILLUMINATED AND PILOTS VISUALLY CONFIRMED THE SLAT PARTIALLY EXTENDED. DECLARED EMERGENCY AND LANDED WITHOUT NO INCIDENT. REPLACED NR 3 SLAT OUTBOARD TRACK GUIDESDR CALA9800619Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 4 SLAT INBOARD END RIB. THE CRACKED AREA WAS REMOVED IAW SRM 51-30-2. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-40-2, AND 51-10-2.SDR DL757980713Wedge · delaminatedNR 5 L/E SLAT T/E WEDGE IS DELAMINATED AT I/B END APPROX 4 BY 6. REMOVED AND REPLACED SLAT.SDR DL72E980710Stiffener · crackedA 2 INCH CRACK WING L/E VERT STIFFENER AFT OF NR 3 SLAT I/B TRACK. REPAIRED PER MM 57-20-21 PG 813.SDR CALA9800607Skin · puncturedINSPECTION FOUND A 1 INCH DIAMETER HOLE IN NR 4 LEADING EDGE SLAT JUST OUTBOARD OF CENTER TRACK. THE DAMAGED AREA WAS CUT OUT, FILLER, DOUBLER, BAFFLE AND SPLICE PLATE WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, PAGE 27 AND ECRA 5752-01022.SDR CALA9800606Skin · dentedINSPECTION FOUND A DENT IN LT WING LEADING EDGE NR 1 SLAT. THE DENTED AREA WAS REMOVED. THE AREA WAS REINFORCED WITH A NEW DOUBLER WHICH WAS FABRICATED AND INSTALLED IAW SRM 57-10-00 FIGURE 18A 51-20-00 AND 51-31-01.
Back to JASC 5754