JASC 5754
Service difficulty reports · 17,340
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 VNAA20250610078Skin · chafedDURING ELECTRICAL RETRACTION OF THE SLATS, FOUND THAT MIDDLE OF SLAT 3 BOTTOM HAS EVIDENCE OF CHAFFING. COMPLIED WITH PSA EA 57-2025-0684 REV-- DATED 2025-05-19. COMPLIED WITH MHIRJ REO 670-57-42-2071, REV--, DATE: 2025-05-08. INSTALLED NEW SERVICEABLE RH FISDR VNAA20250610072Slat Track · corrodedRIGHT SLAT TRACK 3-2 IS CHAFED ON THE LOWER FACE. REPAIRED IAW MHIRJ REO 670-57-42-2007 REV-- DATED 2025-02-25. REFERENCED PSA RII GUIDE REV 00 DATED 29,NOV,24 PN CC670-12081-7SDR DALA2025061104458Structure · damagedAIRCRAFT 9577, AFTER REMOVAL OF RH LEADING EDGE SLAT SEALS, ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS WERE FOUND ON SLAT 1 AND 5. CORRECTIVE ACTION: RH LEADING EDGE SLAT SEALS, ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS WERE FOSDR DALA2025061104457Seal · elongatedAIRCRAFT 9577, AFTER REMOVAL OF LH LEADING EDGE SLAT SEALS, ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS WERE FOUND ON SLAT 1 TO 5. CORRECTIVE ACTION: ELONGATION ON FASTENER HOLES AND MISDRILLS ON COUNTERSINKS ON SLAT 1 TO 5 WERE REPAIRED PER PRISDR DALA2025061304495Slat Track · damagedLH SLAT TRACK #6 PINION TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621359-14 REV 0 AND ERA 621359-14AD REV B SECTION V. MATCHES. (LP# 1014483)SDR DALA2025061304494Slat Track · damagedLH SLAT TRACK #6 RACK TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621359-14 REV 0 AND ERA 621359-14AD REV B SECTION V. MATCHES. (LP# 1014482)SDR DALA2025061304493Slat Track · damagedRH SLAT TRACK #4 RACK TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621242-14 REV 0 AND ERA 621242-14AD REV A SECTION IV. MATCHES. (LP# 1014478)SDR DALA2025061304492Slat Track · damagedRH SLAT TRACK #4 PINION TEETH #1 AND #2 HAS EVIDENCE OF CORROSION WITH NO PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 621242-14 REV 0 AND ERA 621242-14AD REV A SECTION IV. MATCHES. (LP# 1014477)SDR UIEA2025060300723Wedge · damagedLH WING, SLAT# 1, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 1, TRAILING WEDGE, UPPER SURFACE WITH DENTS (9 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG- .201 SHEESDR UIEA2025060300726Wedge · damagedLH WING, SLAT# 4, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 4, TRAILING WEDGE, UPPER SURFACE WITH DENTS (11 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG.201 SHEETSDR UIEA2025060300728Wedge · damagedLH WING, SLAT# 3, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 3, TRAILING WEDGE, UPPER SURFACE WITH DENTS (7 EAS) WERE EVALUATED AND TWO DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG- .201 SHEETSDR SCNA20250626232Flap · crackedCRACKED RH WING INBD KRUEGER FLAP T/E. REMOVED SEAL FOR ACCESS AT RH WING INBD KRUEGER FLAP IAW B737-800 BCF SRM 51-40-02-0G-0. REMOVED DAMAGE AT RH WING INBD KRUEGER FLAP TIE IAW B737-800-BCF SRM 57-43-02-2R-3 REP. 3 PAR 4A FIG 202 REQUEST NDT FOR (HFEC) ANDSDR AALA202506111787Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #11 FORWARD BOLT BETWEEN WS 12277 AND WS 12870. REPLACED BOLT PER TASK CARD 26C61057005.SDR K11A2025061300329Skin · corroded#3 SLAT HAS EVIDENCE OF CORROSION ON UPPER SURFACESDR AALA202506114198Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #3 LOWER AFT BOLT BETWEEN WS 1957 AND WS 2580, BETWEEN RIBS 4 AND 5. REPLACED BOLT PER TASK CARD 26C51057005.SDR AALA202506099861Slat Track · wornAIRCRAFT IN BASE MAINTENANCE: WEAR ON SLAT 1 LOWER SKIN AT LEVEL SLAT TRACK 2 ON LH WING, MEASURES OF DAMAGES ARE L= 3.391INCH W=0.395 INCH D=0.020 INCH. MAINTENANCESDR SWI2025F01514Roller · wornRIGHT SLAT TRACK 3-2 FWD IB, AFT IB, AND AFT OB SIDE ROLLERS WORN OUT OF LIMITS. REMOVED AND REPLACED RH SLAT TRACK 3-2 FWD IB, AFT IB, AND AFT OB SIDE ROLLERS PER CRJ 900 AMM 27-81-44-000-803 CONF A01 AND AMM 27-81-44-400-803 CONF A01.SDR SWIA2025110604Roller · wornRH SLAT TRACK 2-2 AFT IB SIDE ROLLER WORN OUT OF LIMITS (C-CHECK RO 11/06/2025)REMOVED AND REPLACED RH SLAT TRACK 2-2 AFT IB SIDE ROLLER PER CRJ 900 AMM 27-81-44-400-802 (CONFIG A01)SDR CALA2025061905700Slat · damagedBIRD STRIKE RIGHT SIDE OF FUSALAGE. REMOVED RT WING #4 LEADING EDGE SLAT REF AMM 27-81-21-000-801 CORRECTION RH #5 SLAT HAS BEEN REMOVED REF 27-81-21-000-801. NR #4 WAS NOT REMOVED. INSTALLED NEW #5 SLAT IAW AMM 27-81-21-400-801, OPS CHECK REQUIRED AFTER SLATSDR CALA2025061805695Slat · damagedBIRD STRIKE RIGHT SIDE OF FUSALAGE. REMOVED RT WING #4 LEADING EDGE SLAT REF AMM 27-81-21-000-801 CORRECTION RH #5 SLAT HAS BEEN REMOVED REF 27-81-21-000-801. NUMBER #4 WAS NOT REMOVED. INSTALLED NEW #5 SLAT PER AMM 27-81-21-400-801, OPS CHECK REQUIRED AFTER SDR DALA2025061104450Screw · unsecureSHIP 3142 RIGHT WING #3 SLAT T/E DAMAGED BY SCREW STICKING UP. CORRECTIVE ACTION: BLENDED TO WITHIN LIMITS OF SRM 57-40-00-283-004. (6635837)SDR DALA2025060404275Slat Track · corrodedSHIP 3162 LEFT WING N 4 SLAT TRACK N 10 BOTTOM FORWARD AND N 9 TRACK BOTTOM FORWARD/AFT ATTACHMENT BOLT SHANKS HAVE SPOT CORROSION AND PITTING CORROSION. CORRECTIVE ACTION: REPLACED LEFT WING N4 SLAT TRACK N10 BOTTOM. FORWARD AND N9 TRACK BOTTOM FORWARD AFT ATSDR FDEA202506030833Skin · crackedL/T WING # 2 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF O/B MAIN TRACK TRIMMED DAMAGE AREA, LH WING # 2 SLAT O/B MAIN TRACK IAW B757 SRM 57-43-01-2R FIG 201 REP 4, FORMED, TRIMMED, LOCATE, DRILLED AND INSTALLED REPAIR PARTS IAW B757 SRM 57-4SDR FDEA202506030832Skin · crackedLE SLAT NO 9 INTERNAL SKIN WITH CRACK REMOVED L/E SLAT NO 9 INTERNAL SKIN PANEL IAW B757 SRM 51-40-02-0G, FORMED TRIMMED, LOCATED, DRILLED AND INSTALLED NEW SKIN PANEL IAW B757 SRM 51-40-02-0G AND BOEING DWG # 114N4076 REV C.SDR FDEA202506030831Skin · crackedL/T WING # 1 SLAT POSSIBLE CRACK ON SKIN AT BACK SIDE ON LOWER AREA OF I/B MAIN TRACK TRIMMED OUT DAMAGE AREA L/T WING # 1 SLAT ON SKIN AT I/B MAIN TRACK IAW B757 SRM 57-43- 01-2R FIG 201 REP 4, FORMED, TRIMMED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS IAWSDR FDEA202506030830Skin · crackedLE SLAT NO 8 INTERNAL SKIN WITH CRACK REMOVED SKIN PANEL L/E SLAT NO 8 IAW B757 SRM 51-40-02-0G FORMED, TRIMMED, LOCATED DRILLED AND INSTALL NEW SKIN PANEL IAW BOEING DWG # 114N4077 REV D AND B757 SRM 51-40- 02-0G.SDR SWI2025F01513Slat Track · wornLEFT SLAT TRACK 3-2 FWD OB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 3-2 FWD OB SIDE ROLLER PER CRJ900 AMM 27-81-44-400-803-A01SDR SWIA20250602Slat Track · wornLEFT SLAT TRACK 2-2 FWD IB SIDE ROLLER WORN OUT OF LIMITS. REMOVED AND REPLACED LH SLAT TRACK 2-2 FWD IB SIDE ROLLER PER CRJ900 AMM 27-81-44-000-802-A01SDR CALA2025061805694Slat · damagedDURING BIRD STRIKE INSP FOUND DAMAGE TO SLAT #5. DROPPED SLATS, NO DAMAGE NOTED ON AFT STRUCTURE OF SLAT AND NO DAMAGE ON LEADING EDGE OF WING STRUCTURE BEHIND SLAT. L= 8" W =7" DEPTH AT DEEPEST PART IS 2". YOU CAN SEE THE BLEED AIR TUBE IS DAMAGED. ICE BUILSDR AALA202506095042Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT TRACK 5 ON FWD BOLT RH WING CORRODED AREA IS L=0.350 IN W=0.067 IN D= 0.006 IN. MAINTENANCE REPLACED FWD BOLT ON SLAT TRACK 5 PER JOB CARD 26C61057005.SDR AALA202506096931Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 7 ECCENTRIC LOWER BOLT ON RH WING CORRODED AREA IS L=0.256 IN W=0.116 IN D=0.006 IN. MAINTENANCE REPLACED ATTACH BOLT ON SLAT TRACK #7 RH WING IAW JOB CARD 26C61057005.SDR AALA202506062134Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SLAT BOLT AFT POSITION (ECCENTRIC BOLT) TRACK 3 LH WING, CORROSION MEASURES ARE L=0.227 IN; W=0.105 IN; D=0.008 IN. MAINTENANCE REPLACED LOWER SLAT BOLT AFT POSITION LH WING IAW AMM 27-84-63-400-002-A STEP 4. BSDR AALA202505303952Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #12 UPPER AFT BOLT AT RIB 26. REPLACED BOLT PER AMM 27-84-67.SDR SWIA202506020002Slat · damagedTRANSFER FROM EAML 1614417 : CREW REPORTED BIRD STRIKE ON RIGHT WING INBOARD SLAT REVEALED THE FOLLOWING AFTER MECHANIC INSPECTION OF DAMAGE AREA: THE DAMAGE MEASUREMENTS ARE H 3.8 INCHES X W 12.5 INCHES X D 0.445 INCHES (H/D = 8.53) AND IS BEYOND THE MAXIMUM SDR SWIA2025052900008Skin · damagedTRANSFER FROM EAML 1614417 : CREW REPORTED BIRD STRIKE ON RIGHT WING INBOARD SLAT REVEALED THE FOLLOWING AFTER MECHANIC INSPECTION OF DAMAGE AREA: THE DAMAGE MEASUREMENTS ARE H 3.8 INCHES X W 12.5 INCHES X D 0.445 INCHES (H/D = 8.53) AND IS BEYOND THE MAXIMUM SDR SWAA2025061775680Skin · crackedCRACK LOWER SURFACE ACTUATOR AREA LEADING EDGE ON SLAT 4 AT LT WING. FAULT WAS RESOLVED ON ANOTHER FAULT SEE TTG8Q012Y3LU.SDR IPXA2025052891612Skin · dentedGOUGE-SKIN, R/H WING LEADING EDGE #12 SLAT UPPER EDGE AT MIDDLE SUPPORT ADJACENT AREA (AGING A/C NSPECTION) (REPAIR) PERFORMED NDT/ET FOR THE CUTOUT AREA I.A.W. 767 NTM PART6 51-00-19 REV.140 <BR>RESULT:NO CRACK WAS FOUND.SDR UIEA2025041600489Skin · damaged#9 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025041600490Skin · damaged#18 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #18 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025041600491Skin · damaged#19 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #19 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025041600492Skin · damaged#8 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #8 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025041600493Skin · damaged#7 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #7 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025041600494Skin · damaged#6 V/C FLAP LSA LAYER DAMAGED.(<P>PERFORMED REPAIR AT #6 V/C FLAP LSA LAYER DAMAGED AREA PER <SPAN>CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2025050800589Skin · corroded# 23 VC FLAP BULLNOSE FOUND EROSION.(<P>PERFORMED REPAIR AT EROSION AREA IAW SRM 51-70-04 REPAIR 5 REV 45. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025050800590Skin · corroded#4 VC FLAP BULLNOSE FOUND EROSION.(<P>PERFORMED REPAIR AT EROSION AREA IAW <SPAN>SRM 51-70-04 REPAIR 5 REV 45. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR DALA2025052704054Slat Track · crackedLH SLAT TRACK #5 LOWER FWD INBOARD REQUIRES EDDY CURRENT INSPECTION TO BLENDED AREAS, CHECK FOR SIGNS OF CRACKS. LH SLAT TRACK #5 LOWER FWD INBD SURFACE WAS NDT INSPECTED REF A220 ANDTP J-51-01-20. DEFECTS NOTED QC 5257 453307. (LP# 0988435)SDR AALA202506096133Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 2 MID FWD BOLT ON LH WING. L:0.048 IN, W:0.019 IN, D:0.007 IN. MAINTENANCE REPLACED ATTACH BOLT SLAT TRACK #2 ON LH WING IAW JOB CARD 26C51057005.SDR AALA202506052124Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 2 UPPER AFT BOLT ON LH WING. L:0.040 IN, W:0.018 IN, D:0.006 IN. MAINTENANCE REPLACED AFT BOLT LH WING STAT TRACK 2 IAW JOB CARD 26C51057005.SDR SWI2025F01634Skin · damagedRIGHT WING, UNDER PANEL 631BZ HAS TOOLING DAMAGE. (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED TOOL DAMAGE TO RT NR 2 SLAT AFT SKINS BETWEEN SS 261.25, TRACK 2-2, AND BETWEEN SS 315.75, TRACK 2-3 IAW REO 690-57-42-1237, REV-. COMPLIED WITH SKYWEST TASK CSDR SWI2025F01629Skin · damagedRIGHT WING, UNDER PANEL 631CZ HAS TOOLING DAMAGE, (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED TOOL DAMAGE TO RT NR 2 SLAT AFT SKINS BETWEEN SS261.25 - TRACK 2-2, AND BETWEEN SS315.75 - TRACK 2-3 IAW REO 690-57-42-1237 REV- AND SRM 51-12-00-001-001-A01. C
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