JASC 5754
Service difficulty reports · 17,344
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 DHL2003873589Skin · damagedLT OUTR WING CTR L/E SLOT LWR OUTR PLATING ELONG HOLES AROUND STA XFS.526.000. PERFORMED MJR REPAIR IAW EODHL-030613, ED-3456. REMOVED FASTNR IAW SRM 51-1-21 PG 1. BLENDED OUT ELONG HOLES SKIN AREA IAW EODHL-030613, ED-346. PERFORMED NDT INSP IAW NDT SPM PART SDR DHL2003873546Skin · corrodedLT INBD WING L/E SLOT SKIN CORRODED, XS.220.000 - XS.250.089. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT CORRODED ARESDR 2003F00545Skin · delaminatedMSY-BNA - DURING POST REPOSITIONING FLIGHT INSPECTION, FLIGHT CREW OBSERVED UPPER SKIN DELAMINATION OF THE TRAILING EDGE NR 2 L/E SLAT, P/N 65-46422-267. A FOUR INCH SECTION OF THE UPPER SKIN HAD DELAMINATED THE ENTIRE LENGTH OF THE LE SLAT AND DEPARTED THE ASDR 03FDEA01023Fitting · corrodedLEFT WING (FLAP SIDE) - INBOARD T/E FLAP, OUTBOARD AFT HINGE FITTING FOUND PIVOT BEARING MOUNT HOLE OUTBOARD SIDE CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-69357 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT INBOARD FLAP HINGE BRACKET REPAISDR 03FDEA01022Hinge · chippedRIGHT WING INBOARD FLAP OUTBOARD FWD HINGE PIVOT LUG BORE AT INBOARD LOWER SIDE FOUND CHIPPED OFF. RIGHT WING INBOARD FLAP OUTBOARD FWD HINGE PIVOT LUG BORE AT INBOARD LOWER SIDE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-69363 - WINGS - TRAILING EDGE & TRAISDR 03FDEA01016Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE FOUND CORROSION. RIGHT WING OUTBOARD FLAP INBOARD FWD HINGE ACTUATOR LUG BORE OUTBOARD SIDE CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5750-69354 - WINGS - TRAILING EDGE & TRAILING EDSDR DLM88030592Skin · damagedNR 1 SLAT OUTER SKIN ASSEMBLY, XFS 155 TO XFS 168 REPAIR OF DAMAGE TO OUTER SKIN. REPAIRED PER ER/A 418073-14.SDR GTIA030500Rib · crackedFTW - RIGHT WING OUTBOARD SLAT EDGE SEAL TORN, FOUND CRACKED CASTING. REMOVED CASTING. LOCATED AND DRILLED NEW RIB. INSTALLED NEW RIB. (M)SDR 03FDEA01015Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE INBOARD FOUND CORROSION. RIGHT WING OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR LUG BORE INBOARD CORROSION REPAIR CARRIED-OUT IAW FEDEX EA 1-5740-71734 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE SDR DHL2003604591Panel · crackedRT OUTBOARD SLOT UPPER CENTER DOOR WITH 0.500 CRACK IN IT. REMOVED AND REPLACED RT OUTBOARD SLOT UPPER CENTER DOOR IAW MM 27-80-2 PG 201-204. REFER TO NR 0531 FOR OPS CHECK.SDR 03FDEA00979Slat Track · crackedSUSPECT HAIRLINE CRACK ON LT WING NR 16 SLAT TRACK INBOARD FITTING. REMOVED AND REPLACED RIB AT LT WING LEADING EDGE INBOARD SLAT TRACK NR 16 SUPPORT IAW SRM 51-31-01 VOL. II AND DRAWING NR ARC2850.SDR CA030624002Bearing · failed(CAN) AT H 02 CHECK ,FOUND RT SLAT TORQUE TUBE STEADY BEARING FIN 6081CM WITH NO BALL BEARINGS LEFT IN BEARING ASSEMBLY THIS STEADY BEARING IS LOCATED INBOARD OF RIB 13 INBOARD SIDE OF TELESCOPING PNEUMATIC DUCT BRACKET ON RT WING LEADING EDGE REMOVE AND REPLSDR C8GA20030018Bearing · seizedFLT 231 FROM MIA TO PTY. AFTER TAKEOFF, NR 2 SLAT DID NOT RETRACT. CYCLED SYSTEM TWICE STILLS NO RETRACTION. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NR 2 LEADING EDGE SLAT ACTUATOR WAS REPLACED. PESDR 03FDEA00919Hinge · corrodedRIGHT WING- O/B FLAP O/B HINGE I/B ACTUATOR BORE FOUND CORROSION. SNRM N0588 - RIGHT WING- O/B FLAP O/B HINGE I/B ACTUATOR BORE REPAIRED AS PER FEDEX EA 1-5750-69373, TITLE: WINGS- TRAILING EDGE FLAP- OUTBOARD TRAILING EDGE FLAP- SUPPORT BRACKETS- CORROSISDR 2003UALA00516Skin · delaminatedNR 5 SLAT T/E WEDGE LOWER SKIN DELAMINATED. REPLACED 100 PERCENT OF UPPER & LOWER SKIN OF THE T/E WEDGE.SDR UPS03840892Skin · damagedINSPECTION TYPE: C3, RIGHT WING LEADING EDGE INBOARD END OF OUTBBOARD. SLOT HAS SCREWS PULLING THRU SKIN AT XFS XOLDI 6.225. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM. 57-2-0 FIG. 2ASDR UPS03840872Skin · crackedINSPECTION TYPE: C3, RIGHT WING CENTER LE LOWER SKIN IS CRACKED JUST AFT OF IB END OF SLOT DOOR AT 225. STOPDRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW E.O. DC8-5720-4087.SDR UPS03840878Doubler · crackedINSPECTION TYPE: C3, RIGHT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335 REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG.5769589,AND SRM. 51-1-20D,51-1-21SDR UPS03840856Rib · crackedINSPECTION TYPE: C3, LT WING LE LOWER RIB IS CRACKED AT XFS 385, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLERS I.A.W. SRM. 57-2-0 FIG.2SDR SWAA031327Skin · crackedNR 4 L/E FLAP SKIN CRACKED AT WEB STIFFENER. REMOVED AND REPLACED NR 4 L/E FLAP PER MM.SDR 03FDEA00902Rib · crackedRIGHT WING L/E NR 16 SLAT TRACK I/B RIB FOUND CRACKED. SNRM N0066 - NEW RIB FABRICATED AS PER DRAWING NR ARB2850. CRACKED RIB ON RIGHT WING L/E NR 16 SLAT TRACK I/B AREA REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.SDR CALA0300307Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 6 SLAT PANEL SKIN AT LOWER RIVET LOCATED JUST O/B OF I/B AUX TRACK, RIGHT SLAT STA 300. A REPAIR WAS INSTALLED IAW SRM 57-43-01.SDR COMA0360262Panel · crackedRIGHT WING LEADING EDGE PANEL ASSEMBLY 630JL HAS A 3.0 INCH VERTICAL CRACK AT WS 190.0. REMOVED RIGHT WING LEADING EDGE PANEL 630JL, FITTED AND INSTALLED NEW SERVICEABLE RIGHT WING LEADING EDGE ASSEMBLY IAW CRJ AMM 57-41-01-400-804.SDR SWAA031273Slat · crackedDURING SCHEDULED 1/2D CHECK, FOUND NR 3 L/E SLAT CRACKED AT OUTBD AUX TRACK CUTOUT. REPAIRED NR 3 L/E SLAT PER SRM.SDR CALA0300296Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT PANEL AT I/B AUX TRACK. REPAIRED SLAT SKIN IAW SRM 57-43-01, FIGURE 206, SHEETS 1-4.SDR UPS03M40954Rib · crackedINSPECTION TYPE: C, LT NR 08 SLAT FOUND NR 16 SLAT AT X0S98 WITH I/B RIB CRACK AS MARKED. CRACKED SUPPORT LT NR 8 SLAT XOS98 REMOVED IAW SRM 51-35-01V2.R33. INSTALLED NEW SUPPORT RIB PER SRM 51-35-01 & 51-33-01V.2.R33.SDR UPS03M40953Rib · crackedINSPECTION TYPE:C, RT NR 08 SLAT FOUND NR 16 SLAT TRACK AT X0598.0 WITH I/B SUPPORT RIB CRACKED AS MARKED. CRACKED SUPPORT RIB RT NR 08 SLAT XOS98.0 REMOVED IAW SRM 51-35-01V2.R 33. INSTALLED NEW SUPPORT RIB PER SRM 51-35-01 & 51-33-01 V2.R33.SDR SWAA031254Slat · out of rigNR 4 L/E SLAT VISUALLY NOT ALIGNED WITH OTHER SLATS. REMOVED AND REPLACED NR 4 L/E SLAT AND OUTBD GUIDE STOP.SDR SWAA031217Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT INBD FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LT INBD FOREFLAP PER MM.SDR QXEA200300698Panel · chafedCKB - RIGHT HAND WING SLAT PANEL 1 CHAFED ON OUTBOARD EDGE AFT SIDE. REPAIRED IAW CRJ 700 SRM 51-25-01.SDR DHL2003604643Skin · damagedRT INBOARD SLOT VANE OUTER PLATING SHOWS ELONGATED HOLES AT STA XS 247.000. PERFORMED MAJOR REPAIR. REMOVED FASTERNERS FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR EXTERNAL DOUBLER AN INTERNAL DOUBLER ANDSDR DHL2003604604Vane · damagedRT WING EXTENDED LE OB VANE HAS SEVERAL ELONGATED HOLES AND INTERIM REPAIR AT STA XOLDO 67. REMOVED FASTENERS. REMOVED THE EXISTING INTERIM REPAIR IAW EO DHL 030558, ED-3351. CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL REPAIR DOUBSDR DHL2003604599Vane · damagedLT WING EXTENDED L/E INBD VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030563, ED-3312. REMOVED FASTENERS AND THE EXSISTING DOUBLER IAW SRM 51-1-21 PG 1. TRIMMED OUT THE ELONGATED HOLES SKIN AREA. CLEANED, SDR 03FDEA00802Skin · crackedNR S 17 COMPLY WITH E.A.8-5710-70392.WINGS-RT-FIXED LEADING EDGE BEADED DOUBLER REPAIR ACB 1242. CLOSING ACTION ON 05/23/03. COMPLIED WITH E.A.8-5710-70392.SDR 2003UALA00505Wedge · delaminatedT/E WEDGE DELAMINATED, SLAT NR 5. MAJOR REPAIR ACCOMPLISHED. REMOVED, REPAIRED AND REINSTALLED T/E WEDGE.SDR DHL2003604606Doubler · crackedRT OUTER WING CTR EXTENDED L/E SLOT INNER DOUBLER CRACKED 0.630 AT STA XFS 526.000. PERFORMED MAJOR REPAIR IAW EODHL-030532, ED-3350. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED THE CRACK END 0.250 DIA IAW EODHL-030532, ED-3350. CLEANED, TREATED ASDR UPS03240752Angle · crackedINSPECTION TYPE: C, NR 6 SLAT, O/B TRACK TO SLAT ATTACH ANGLE IS CRACKED. ANGLE FABRICATED IAW SRM 51-20-01. ANGLE INSTALLED IAW SRM 51-20-02.SDR DLM88031034Attach Fitting · crackedNR 3 SLAT MIDDLE ATTACH FITTING CRACKED BETWEEN ATTACH POINT AND EDGE OF FITTING 100 PERCENT. REPLACED SAME.SDR UPS03240746Bracket · crackedINSPECTION TYPE: C, NR 3 SLAT, STRUCTURE SUPPORT ANGLE IS CRACKED JUST I/B OF WHERE ACTUATOR EYE END ATTACHES TO SLAT. BRACKET REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. BRACKET INSTALLED IAW SRM 57-50-03 & SRM 51-30-02.SDR AWXA200300667Skin · crackedDURING C-17 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT FASTENER HOLES ON NR 2 SLAT LOWER LEADING EDGE. MAINTENANCE CUTOUT DAMAGED AREA NR 2 SLAT LOWER LEADING EDGE; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 PG 216-219 FIGSDR ASAA0310453Skin · corrodedDURING C-CHECK, FOUND LEFT WING FORE FLAP LEADING EDGE SKIN AT WING STATION 417 CORRODED. REMOVED CORROSION AND REPAIRED PER SRM. (M)SDR EVAS092013Doubler · crackedDURING PERFORM E/O V02102, FOUND CRACK ON RIGHT AND LEFT WING FIXED LEADING EDGE STRINGER DOUBLER AT STATION XOS 906. INSTALLATION OF INTERNAL DOUBLERS MADE FROM TI-6AI-4V 0032 (THICK AT STATION XOS 906).SDR DHL2003747509Support · crackedDURING C CHECK, UPON REMOVAL OF NR 7 SLAT ACTUATOR SUPPORT STRUCTURE FOUND O/B MOUNT CRACKED AND I/B MOUNT CHAFED. REMOVED FUEL TANK ACCESS PANEL 7615 AND 7618 IAW B-727 M.M. 28-11-21. REMOVED DAMAGED ANGLES AND INSTALLED NEW FABBED FROM BAC1503-100145 P.O.SDR AWXA200300633Skin · delaminatedDURING C-15 CHECK THE NR 3 SLAT INBOARD END UPPER SKIN WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 3 SLAT IAW AWA T/C R3M27002.SDR AWXA200300632Slat · delaminatedDURING C-15 CHECK THE NR 5 SLAT OUTBOARD TRAILING EDGE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT IAW AWA T/C R3M27008.SDR DHL2003747510Stiffener · crackedDURING "C" CHECK N/R 53650 LT WING LE CAVITY LE STA. 1307 VERTICAL STIFFENER IS CRACKED AT BOTTOM END (FRONT SPAR WBL 92.8. REMOVED L/H WING ACCESS PANEL 6303 TO FACILITATE SM WORK IAW B-727 M.M. 57-30-0. REMOVED LT WING FUEL TANK ACCESS 7340 TO FACILITATE SSDR SWAA031083Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED ON LOWER SKIN AROUND ACTUATOR CUTOUT. REPAIRED SKIN PER SRM.SDR QXEA200300582Slat · chafedPDX - SLAT CHAFING AGAINST LEADING EDGE ON LEFT HAND WING. REPAIRED IAW HORIZON AIR EA R-57-32.SDR SWAA031078Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SKIN PER SWA EA.SDR DHL2003747501Structure · chafedDURING C-CHECK DISCREPANCY AS FOLLOWS, DEEP CHAFE MARK ON DOUBLER OUTBOARD LEADING EDGE OF INBOARD FOREFLAP LT. REMOVED OLD DOUBLER AND FABBED NEW DOUBLER IAW B-727 SRM 57-50-4 FIG 1 FROM 2024-T3 .050 PO 9912495 2. DOUBLER DIMENSIONS 4 INCH X 4 INCH. ALODIN
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