JASC 5754
Service difficulty reports · 17,338
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 UIEA2026090300847Support Rib · crackedLEFT WING, NR 3 SLAT, OTBD SUPPORT RIB FOUND CRACKED. RIB CRACK AREA REPAIRED IAW RI-57-42-18506, REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026090300849Slat Track · crackedLEFT WING, NR 3 SLAT, OTBD MAIN TRACK RIB SKIN FASTENER HOLE CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED.SDR FDEA202609101294Slat · gougedNR# 0005: #4 SLAT LWR SURFACE IS GOUGED APPROXIMATELY 36 INCHES FROM INBD EDGE. REPAIRED L/H WING #4 SLAT T/E WEDGE TOP SKIN AT WS 546.2 IN REF. TO 767 SRM 57-43-02-2R AND 767 SRM 51-70-10-2R. THIS IS A MAJOR REPAIR. SEE JPF STEPS FOR OTHER WORK ACCOMPLISHEDSDR SWAA2026100741321Skin · crackedCRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 3, NOSE SKIN AT THE ACTUATOR AROUND FASTENERS LT WING. REPAIRED LOWER SURFACE OF LEADING-EDGE SLAT 3 NOSE SKIN IAW SRM 57-42-01-2R-8.SDR IPXA2026091449035Seal · damagedFAULT - NO.17 V.C FLAP, OUTBOARD MOLDING SEAL DAMAGE. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE ADHESIVE TO REPAIR AREA CURED AT 80°F FOR 10 HOURS.SDR CALA2026091019357Skin · dentedRT WING SLAT NR 6 DENTED OUT OF LIMITS. ACCOMPLISHED REPAIR AT RT WING SLAT #6 PER SRM 57-42-01-2R-1 REPAIR 1 PARAGRAPH 4.0 TABLE 201 FIG. 202.SDR SWAA2026090925419Slat · damagedBIRDSTRIKE ON LEFT LEADING EDGE SLAT. NO ADVERSE FLIGHT CONTROLS NOTED. NO ABNORMAL ENGINE INDICATIONS OR ODORS NOTED. REMOVED NR 1 SLAT IAW AMM 27-81-21.SDR IPXA2026101426713Slat Track · crackedLT SLAT #4 OUTBD TRACK COVER CRACKED. INSTALLED REPLACEMENT COVER AT L/WING #4 SLAT O/B TRACK PER B757-200PF SRM 51-40-05-0G-0 & 51-40-02-0G-0.SDR DALA2026090805037Slat · damagedDAMAGE TO LEFT WING SLAT DUE TO BIRD STRIKE. PERFORMED A BIRD STRIKE INSP PER B717 AMM 05-62 FOUND NO OTHER DAMAGE. REPLACED #3 WING SLAT IAW AMDS JOB CARD 2780-4000-LH-3. A/C OK FOR SERVICE. (9189256) AIRCRAFT WAS GROUNDED.SDR DALA2026091605159Skin · debondedDEBOND (3.0IN X 2.5IN) ON UPPER SURFACE ISS 156, LE SLAT 6 TRAILING EDGE WEDGE, RT WING. RT WING WAS REPAIRED IAW SRM 51-70-10. (1797351)(AIRCRAFT GROUNDED)SDR FDEA202609051264Skin · dentedINBOARD SLAT NR 6 (LEFT) UPPER SURFACE APROX 4' IB MULTIPLE DENTS. REPAIRED THE LT WING NR 6 INBD SLAT AT ISS 204 TOP SKIN SURFACE IAW SRM 57-43-02-2R & SRM 51-70-10-2R. MAJOR REPAIR.SDR DALA2026090805026Roller · wornRIGHT NR 4 SLAT TRACK BOTH INBD ROLLER WORN, EXCEED MAXIMUM DEPTH OF .010" AT .018" PER WC 5742-01028-02B. REPAIRED PER PRI 620677-14AD REV 0 ER/A REV C, AND FINAL ER/A 620677-14AD REV C SEC VI. (LP# 1796021; AIRCRAFT WAS GROUNDED)SDR AALA202609160377Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED BRACKET ANGLE SLAT TRACK OF SLAT8 REAR AREA AT RT WING. REMOVED AND REPLACED BRACKET ANGLE LOC SLAT TRACK AT LEVEL OF ISS 289 OF SLAT 8 REAR AREA AT RT WING IAW SRM 51-40-02-0G AND DWG 114W2510 SHEET 5.SDR FDEA202609011255Skin · delaminatedRIGHT WING, NR 9 SLAT UPPER SURFACE T/E WEDGE DENTED AND DELAMINATED AT INBD EDGE. REPAIRED THE NR 9 SLAT UPPER SURFACE T/E WEDGE INBD EDGE AT STA OSS 531 IAW SRM 57-43-02-2R, FIG 201, REPAIR 1, SHT 1, NOTE B. MAJOR REPAIR.SDR FDEA202609011254Skin · delaminatedRIGHT WING, NR 9 SLAT UPPER SURFACE T/E WEDGE DELAMINATED AT OTBD EDGE. REPAIRED RT WING, NR 9 SLAT, UPPER SURFACE T/E WEDGE, OTBD EDGE AT STA OSS 682 IAW SRM 57-43-02-2R, FIG 201, REPAIR 1, SHT 1, NOTE B. MAJOR REPAIR.SDR UIEA2026073000668Skin · delaminatedRT WING, INBD FORE FLAP FOUND DELAMINATION AT L/E AREA 140" AWAY FROM INBD EDGE. PERFORMED COMPOSITE HOT BOND REPAIR SRM 51-70-07 PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR UIEA2026073000669Skin · delaminatedRT WING, INBD FORE FLAP FOUND DELAMINATION AT L/E AREA 144" AWAY FROM OTBD EDGE. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07 PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR UIEA2026073000670Skin · delaminatedRT WING, INBD FORE FLAP FOUND DELAMINATED AT L/E AREA 8" AWAY FROM OTBD EDGE. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07 PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR UIEA2026073000671Skin · delaminatedRT WING T/E OTBD MID FLAP L/E MID AREA FOUND DELAMINATION. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07 PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR UIEA2026073100672Skin · delaminatedLT WING T/E OTBD FORE FLAP MOST OTBD AREA FOUND DELAMINATION. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07 PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR UIEA2026073100673Skin · wornLEFT WING OTBD T/E FOREFLAP OTBD FIXED T/E FOUND WORN. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07 PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR REXA2026102001951Rib · crackedCRACKED MACHINED RIB, SS 57.16, LT L/E WING. THE RIB WAS REPLACED IAW SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01, & SRM 51-10-06-001-001-A01.SDR VNAA2026083122Slat Track · wornRIGHT SLAT TRACK 1-1 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. REPAIRED RH SLAT TRACK 1-1 IAW MHIRJ REO 670-57-42-2542 REV -.SDR VNAA2026083121Slat Track · wornRIGHT SLAT TRACK 1-2 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. PERFORMED A MAJOR REPAIR TO RH SLAT TRACK 1-2 IAW REO 670-57-42-2532 REV -.SDR VNAA2026083120Slat Track · wornHN00321750 DISCREPANCY: RH SLAT TRACK 1-3 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. CORRECTIVE ACTION: PERFORMED A MAJOR REPAIR TO RH SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-2540 REV.-- DATED 2026-07-07.SDR VNAA2026083119Slat Track · wornLEFT SLAT TRACK 1-1 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES.SDR VNAA2026083118Slat Track · wornLEFT SLAT TRACK 1-2 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. REPAIRED BY BLENDING IAW MHIRJ REO 670-57-42-2531 REV--.SDR VNAA2026083117Slat Track · wornLEFT SLAT TRACK 1-3 WORN IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. REPAIRED IAW IAW REO 670-57-42-2543 REV -.SDR AALA202609090534Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED SLAT 7 ON PLATE OF SLAT TRACK 15 AT LT WING. REMOVED AND REPLACED PLATE OF SLAT 7 TRACK 15 AT LT WING (1 EA) IAW B777-200 SRM 51-40-02-0G AND DWG 114W2510.SDR FDEA202608271239Skin · dentedHAIL DAMAGED ON WEDGE SKIN UPPER SURFACE, SLAT #3. WEDGE SKIN UPPER SURFACE, SLAT #3 WAS REPAIRED IAW B767 SRM 51-70-10-2R FIG.201 REP 4 SHEET 1 REV. 94. DEC 15/2025. AND SRM 57-43-02-2R FIG 201 REP 1 SHEET 1 REV. 94 DEC. 15/2025.SDR UIEA2026082300787Skin · dentedWINGS - OTBD SLAT NR 13, NOSE SKIN DENTED, TIME-LIMITED REPAIR. WINGS OUTBD SLAT NR 13 NOSE SKIN EXISTING TIME-LIMITED REPAIR REMOVED & A NEW PERMANENT CATEGORY A REPAIR CARRIED OUT IAW SRM 57-43-01-2R-2, REPAIR 2, FIGURE 203, REV 53 IAW EA-1957A247, PARTSDR UIEA2026082500796Skin · dentedRIGHT WING NR 14 SLAT L/E NOSE SKIN DENT BTWN OSAS 1454 & 1483 BEYOND SRM REPAIR LIMITS. WINGS OTBD SLAT NR 14, NOSE SKIN DENT AREA TRIMMED OUT AND PERMANENT CATEGORY A REPAIR CARRIED OUT IAW EN 3626, REV 0. NO FURTHER DEFECTS NOTED.SDR IPXA2026092117554Stiffener · crackedRIGHT WING, KRUEGER FLAP MOVABLE VANE, CRACK UNDER TEFLON STOP BASE. INSPECTED AND VERIFIED INSTALLATION OF STIFFENER ON RT WING KRUEGER FLAP MOVABLE VANE IAW SRM 51-40-21.SDR IPXA2026090107073Skin · erodedEROSION SKIN, L/H WING NO. 2 SLAT OUTBD CLOSURE PANEL. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 57-43-01-2R-3 REFER TSDR IPXA2026090107012Skin · erodedEROSION SKIN, L/H WING NO. 2 SLAT INBD CLOSURE PANEL AREA. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. MEASURE THE DAMAGE SIZE AND LOCATION ( L : 1", W : 0.5", 1.2" FROM AFT EDGE, 38.5" FROM INBD EDGE ). BOND THE REPAIR PLIES WITH FILM ADHESIVE SDR SWAA2026091889816Angle · crackedCRACK ANGLE AUXILIARY TRACK SLAT 8 LOC OTBD SIDE OFF SS 660, RT WING. EVALUATED AND REPLACED ANGLE AUXILIARY TRACK SLAT 8 LOC OUTBOARD SIDE OFFSS 660 APROX AT RT WING DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS FOR CRACK IAW SRM 51-10-02, ITEM 9, & SRM 51-40-0SDR IXXA20260822002Former · crackedLE NOSE FORMER AT #5 SLAT TAI DUCT IS CRACKEDSDR JR2R20260821341Guide Track · gougedLEFT OTBD MAIN INBD FLAP ROLLER GUIDE RAIL IS GOUGED. REPAIRED PER ETD.SDR SWAA2026092352715Bullnose · crackedLEFT WING, NR 2 KRUEGER FLAP, BULL NOSE CRACKED AT CENTER RIB. REMOVED AND REPLACED THE LT WING MID BULL NOSE KRUEGER FLAP NR 2 IAW CMM 57-56-44-NG.SDR DALA2026081904729Skin · damagedRIGHT INBD DROOP NOSE DAMAGED. REPAIRED REF: A350 - ASR - A350-A-57-44-63-01001-664A-A - SLAT 1 INBOARD (DROOP NOSE) - DROOP NOSE - NOSE SKIN BETWEEN RIBS - PERMANENT REPAIR (CATEGORY A PERM REPAIR) (1763331) AIRCRAFT WAS GROUNDED.SDR FDEA202608181144Skin · dentedDENT AT R/H WING SLAT #9 UPPER TRAILING EDGE AT OSS 669. REPAIRED DENT ON RH WING SLAT #9 UPPER EDGE AT OSS 669 IAW B757 SRM 51-70-10-2R. MAJOR REPAIRSDR IPXA2026100228085Stiffener · crackedL/H WING, KRUEGER FLAP MOVABLE VANE, CRACK UNDER TEFLON STOP BASE. DOT 73-176. INSTALLED STIFFENER AND REINSTALLED COVER SEAL + FITTING IAW A300 SRM 51-40-21. REVIEWEDSDR SWAA2026092188030Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 385 INTERNAL CAVITY LEADING EDGE OF THE LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A.SDR TAMF20260819058Skin · dentedDURING THE FINAL APPROACH AT VCP AIRPORT, THE AIRCRAFT EXPERIENCED A BIRD STRIKE ON SLAT NO. 6 OF THE LEFT WING LEADING EDGE. IAW AIRBUS SRM 57-40-00-283-019, THE DAMAGE WAS INSPECTED AND FOUND TO BE BEYOND THE ALLOWABLE LIMITS. THEREFORE, REPLACEMENT OF THE SDR DALA2026081704703Slat · crackedAIRCRAFT 8332, UPON INSPECTION OF LT SLAT NR 2, FOUND POSSIBLE CRACK. REQUIRES EDDY CURRENT TO DETERMINE SEVERITY. REPLACED WITH LT NR 2 SLAT IAW W/C 2781-4002-LT. PERFORMED MECHANICAL RIGGING PER W/C 2781-4002-LH. ACCOMPLISHED OPS TEST OF FLAP AND SLAT SYSTSDR IPXA2026100799313Stiffener · crackedLH WING, FIXED LEADING EDGE INTERNAL STRUCTURE, STIFFENER INSIDE FLAP KRUEGER COMPARTMENT HAS A CRACK .INSTALLED NEW STIFFENER AT INSIDE FLAP KRUEGER COMPARTMENT IAW SRM 51-40-21. REVIEWED.SDR CALA2026081718646Skin · crackedLEFT WING LEADING EDGE SLAT NR 2, LOWER SKIN HAS A CRACK, AT 31 INCH. FROM THE INBD EDGE. REMOVED, FABRICATED, AND INSTALLED COVE SKIN ON LT WING L/E SLAT NR 2 IAW SRM 51-40-05-06-0, SRM 51-9 0-02-0G-0, AND DWG 114N4076. REF: 17347.SDR IPXA2026092858039Skin · gougedRT WING, SLAT 1 INNER SKIN HAS A GOUGE BETWEEN SLAT TRACK 3 & FOLDING SLAT. VERIFIED ACCOMPLISHED REPAIR IAW EO-98692 AND STE PNA EA 300-5742-27-A4622, REV-.SDR FDEA202608061090Skin · dented#4 SLAT T/E WEDGE UPPER SURFACE, 22" FROM THE OUTBD END AND 7" FROM THE AFT EDGE HAS SMALL DENT.MWT, REPAIRED DENT ON # 4 SLAT ON UPPER SURFACE 22" FROM OB EDGE AND 7" FROM AFT EDGE. REF B767 SRM 51-70-10-2R REPAIR 2 FIG 201 SHEET (1 OF 5). SEE JPF, THIS ISDR FDEA202608041083Skin · dentedRIGHT WING NR 8 SLAT TOP SIDE APPROX IN THE MIDDLE HAS A DENT. REPAIRED RT WING NR 8 SLAT TRAILING EDGE WEDGE TOP SKIN SURFACE AT WS.465.65 IAW SRM: 57-43-02-2R AND SRM 51-70-10-2R. THIS IS A MAJOR REPAIR, SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.
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