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 SWIA2026071377494Slat Track · corrodedREMOVE AND REPLACE LT SLAT TRACK 2-2. REMOVED AND INSTALLED A NEW LT SLAT TRACK 2-2 IAW AMM 27-81-41-400-802-A01.SDR SWIA2026071377436Slat Track · not reportedREMOVE AND REPLACE LH SLAT TRACK 3-3. REMOVED AND INSTALLED THE LH SLAT TRACK 3-3 AT LT WING, IAW AMM27-81-41-000-803-A01 AND AMM27-81-41-400-803-A01SDR SWIA2026071277504Slat Track · corrodedREMOVED AND REPLACED LH SLAT TRACK 1-2. REMOVED AND INSTALLED NEW SLAT TRACK 1-2 IAW AMM 27-81-41-400-802-A01.SDR SWIA2026071277498Slat Track · corrodedREMOVE AND REPLACE RIGHT HAND SLAT TRACK 1-3 . REMOVED AND INSTALLED SERVICEABLE, PN , RH SLAT TRACK 1-3 USING NEW COTTER PINS IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01.SDR SWIA2026071277497Slat Track · corrodedREMOVE AND REPLACE RIGHT HAND SLAT TRACK 1-1. REMOVED AND INSTALLED A NEW, , RT WING SLAT TRACK 1-1 IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01.SDR SWIA2026071277492Slat Track · corrodedREMOVE AND REPLACE LT SLAT TRACK 1-3. INSTALLED A NEW LT SLAT TRACK 1-3 IAW AMM 27-81-41-400-801-A01.SDR IPXA2026091726026Skin · crackedMAJOR REPAIR, NR 1 SLAT, INNER SURFACE ON THE OUTBD SIDE, IS CRACKED. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98297-REQ1 AND STE PNA EA 300-5742-27-A4593, REV -.SDR FDEA202607100889Skin · unknownNEED TO REPAIR DAMAGE ON #4 SLAT, OTBD CLOSURE PANEL (MPN: 114T4151-7) AT OSS 641. REPAIRED #4 SLAT OTBD CLOSE OUT PANEL AT OSS 641 MPN# 114T4104-407G SN# 000359 IN REF TO B767 SRM 57-43-01-2R FIG 201 SHT. 3, REPAIR 2 AND B767 SRM 51-70-07-0G PAR. 5.G. SEE JSDR FDEA202607100888Skin · delaminatedNEED TO REPAIR DAMAGE ON #4 SLAT, INBD CLOSURE PANEL (MPN: 114T4151-5) AT OSS 572. REPAIRED #4 SLAT INBD CLOSE OUT PANEL AT OSS 572 MPN# 114T4104-407G SN# 000359 IN REF TO B767 SRM 57-43-01-2R FIG 201 SH 3 REPAIR 2 AND B767 SRM 51-70-07-0G PAR. 5.G. SEE JPF SDR SWAA2026080540700Skin · crackedCRACK LOWER SURFACE OF RT WING LEADING EDGE SLAT 7 NOSE SKIN AT ACTUATOR LOCATION AROUND THE FASTENER. PERFORMED A REPAIR ON LOWER SURFACE OF LEADING EDGE SLAT 7 NOSE SKIN IAW SRM 57-42-01-2R, REPAIR 8, & DWG 114A5020, REV A, SHEET 38.SDR SWAA2026080580743Skin · crackedCRACKED LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN AT THE ACTUATOR LOCATION. AROUND FASTENER. PERFORMED A REPAIR ON THE LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN IAW SRM 51-40-02, AND SRM 57-42-01-2R-8, REPAIR 8, AND DWG 114A5030, REV A, SHEET 2.SDR IPXA2026073173712Hinge · brokenFOUND RT WING NR 24 V.C FLAP INBD SIDE FOLDING NOSE HINGE BROKEN. OK TO INSTALL, CONDITION CHECK SATISFIED. IAW AMM 27-81-02-404-010 REV.117 ASSEMBLY RT WING NR 24 V.C FLAP INBD SIDE FOLDING NOSE & INBD SIDE HINGE. CONDITION CHECK NORMAL.SDR SCNA20260730333Beam · crackedDURING THE HFEC FASTENER HOLE PERFORMED AT RT WING SLAT NR 7 PER NRI 6-6, FOUND CRACK IN THE NOSE BEAM AT OPEN HOLE ADJACENT TO THE ACTUACTOR RIB. PERFORMED REPAIR RT WING SLAT NR 7 NOSE BEAM SECTION FROM SS290.250" TO SS343.750" DUE TO CRACK IAW BCF SRM 57-SDR CALA2026071017648Skin · dentedSLAT NR 2 UPPER SKIN HAS A DENT. REPAIRED THE NR 2 SLAT UPPER SKIN IAW SRM 51-70-10-2R-0.SDR DALA2026070904031Skin · crackedCRACK INNER SKIN OF SLAT NR 2 NEAR SLAT TRACK NR 5 STA XOS= 240 AT LEFT WING. REPAIRED INNER SKIN IAW SRM 57-00-00-2R. (1689281) (AIRCRAFT GROUNDED).SDR DALA2026070904026Repair · delaminatedFOUND LT WING NR 4 SLAT UPPER SKIN OTBD TRAILING EDGE CORNER, REPAIR DOUBLER DELAMINATED. REPAIRED THE LT WING NR 4 SLAT UPPER SKIN OTBD TRAILING EDGE CORNER IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0. (LP 1687855 - AIRCRAFT WAS GROUNDSDR IPXA2026071539478Stringer · damagedFOUND LT WING NR 5 VC FLAP UPPER SIDE STRINGER DAMAGE. INSTALL NEW STRINGER IAW SRM 51-40-02-0G REV.107 AND DWG 65B15168, SH2, REV G.SDR SWAA2026072797693Slat · crackedPERFORMED OPEN HOLE INSP IAW B737 NDTM P6, 51-00-00 PROC 16. FOUND 1 EA FASTENER CRACKED IN FITTING ON NR 3 LE SLAT. REMOVED AND REPLACED NR 3 L/E SLAT ASSY IAW AMM27-81-21. ADJUSMENT & OPS TESTS GOOD,SDR SWAA2026072742218Slat · crackedPERFORMED OPEN HOLE INSP IAW NDTM P6, 51-00-00 PROC 16. FOUND 1EA FASTENER CRACKED IN FITTING ON NR 5 LE SLAT. REMOVED AND REPLACED NR 5 L/E SLAT ASSY IAW AMM 27-81-21. ADJUSMENT & OPS TESTS GOOD VERIFIED REMOVED AND REPLACED #5 L/E SLAT ASSY IAW AMM27-81-21.SDR VNAA202608210005Skin · crackedIAW TRFKE00F6TG7: 2800FH PERM REPAIR - TEMPORARY DISPOSITION FOR REWORKED DENT TO LHS SLAT#1 OUTER SKIN AND LOWER ANGLE AT WS58.75. ENGINEERING COMMENTS: ANGLE PN CC670-12648-1 MUST BE REPLACED. TRFKE00F6TG7 DISPLAYED THAT THE ENTIRE SLAT PN CC670-12600-3 IS SDR IPXA2026080475424Skin · gougedMAJOR REPAIR, RT WING SLAT NR 1 HAS A GOUGE AND CRACK DAMAGE AT LOWER SKIN, OTBD SIDE. ACCOMPLISHED REPAIR IAW EO-98059-REQ1 AND VT-MAE EA 300-5742-27-A4556, REV -.SDR R61A2026072200210Slat Track · crackedDURING HEAVY CHECK RT FIXED LEADING EDGE WING SLAT #2 INBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW EMB ETD 2026-170-012050SDR R61A2026072200209Slat Track · crackedDURING HEAVY CHECK L/H FIXED LEADING EDGE WING SLAT #2 OUTBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW EMB ETD 2026-170-012049SDR R61A2026072200208Slat Track · crackedDURING HEAVY CHECK LT FIXED LEADING EDGE WING SLAT #2 INBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW ETD 2026-170-012048SDR IPXA2026070724623Seal · brokenBROKEN MOLDING SEAL, LT WING NR 11 KRUEGER FLAP INBD SIDE MOLDING. CHECKED OK.SDR IPXA2026070724617Seal · brokenBROKEN MOLDING SEAL, LT WING NR 6 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIRSDR IPXA2026070624604Seal · brokenBROKEN MOLDING SEAL, LT WING NR 3 VC FLAP INBD SIDE, IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR.SDR SWIA2026062977532Slat Track · chafedRH SLAT TRACK 2-2 IS CHAFED C-CHECK RO 10062026EVALUATED DAMAGE PER CRJ700 SRM 51-12-00-001-001-A01 DAMAGE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN REPAIRED SLAT TRACK 2-2 IAW MHIRJ REO 670-57-42-2557 REV --DATED 2026-07-09SDR IPXA2026070697892Seal · brokenBROKEN MOLDING SEAL, L/H WING NR 4 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12 REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED.APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.SDR IPXA2026070697902Seal · brokenBROKEN MOLDING SEAL, LT WING NR 5 VC FLAP INBD SIDE. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12, REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED, APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.SDR IPXA2026070395238Former · crackedCRACKED FORMER, RT WING NR 8 SLAT OTBD TRACK, OSS 499. INSTALL A NEW FORMER IAW SRM 51-40-02-0G, REV 95, AND SREO-50900-REQ001, REV.2 AND DWG 114T2511, SH 1, REV D.SDR UIEA2026061700513Skin · tornRT WING L/E #19 VC FLAP LSA LAYER FOUND TORN. PERFORMED REPAIR AS PER CMM 57-55-42-81205-601 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2026061700518Skin · dentedLT WING L/E #12 K FLAP EXTERNAL SURFACE FOUND 1EA DENT. PERFORMED REPAIR AS PER SRM 51-70-05 REPAIR 1. NO FURTHER DEFECTS NOTED.SDR UIEA2026062400536Bearing · looseNR 16 K FLAP PNL LWR SPAR O/B BULL NOSE MOUNTING BEARING FOUND LOOSE. NR 16 KL FLAP PANEL LWR SPAR O/B BULLNOSE MOUNTING BEARING BUSHING REPAIRED (TEMPORARY REPAIR) AS PER RI-27-81-18369 REV.B. NO FURTHER DEFECTS NOTED.SDR IPXA2026070371137Closeout Panel · crackedCRACKED PANEL, LT WING L/E NR 1 SLAT LOWER SURFACE INBD CLOSURE PANEL. REMOVED THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE IAW SRM 57-43-01-2R-3 REFER TO SRM 51-70-07-0G-0 REV. 95.SDR IPXA2026070371125Closeout Panel · crackedCRACKED PANEL, LT WING L/E NR 1 SLAT OTBD CLOSURE PANEL. REMOVED THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-43-01-2R-3, REFER TO SRM 51-70-07-0G-0 REV. 95.SDR IPXA2026070271137Panel · crackedCRACKED PANEL, LT WING L/E NO.1 SLAT LOWER SURFACE INBD CLOSURE PNL. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.144 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. RESULT: NO DEFECT FOUND.SDR DALA2026062903830Wedge · debondedDEBOND OF 1.5IN X 1.5IN AT OSS 389 UPPER SURFACE OF LE SLAT 4, TRAILING EDGE WEDGE. LT WING. OSS 389 UPPER SURFACE OF LE SLAT 4, TRAILING EDGE WEDGE LT WING WAS REPAIRED PER SRM 51-70-10-2R PROCEDURE REPAIR GENERAL WITH REFERENCE TO SRM 57-43-02-2R, PROCEDURESDR DALA2026062403763Wedge · debondedDISBOND OF 1.2IN X 1.2IN ON PREVIOUS REPAIR AT UPPER SURFACE ISS114 LE SLAT 6, TRAILING EDGE WEDGE. AREA ON UPPER SURFACE ISS114 LE SLAT 6, TRAILING EDGE WEDGE WAS REPAIRED IAW SRM 51-70-10-2R PROCEDURE REPAIR GENERAL IAW SRM 57-43-02- 2R PROCEDURE 1 REPAIR SDR AALA202607159479Skin · crackedAIRCRAFT IN BASE MAINTENANCE: NR 1 SLAT LOWER LE SKIN CRACKED BELOW ACTUATOR. CASTING. MAINTENANCE REPLACED THE NR 1 SLAT IAW AMM 27-81-21 AND INSTALLED ON TASK CARD: 08L00027002_01.SDR IPXA2026071686426Bracket · crackedSLAT #3 I/B ND O/B SLAT DRIVE ARM GAP PANELS ARE LOOSE. . REMOVED 2EA GAP PANEL AND 2EA BRACKETS FROM #3 SLAT I/B AND O/B IAW B757-200PF SRM 51-40-02-0G-0. DURING REMOVAL WAS FOUND 1EA BRACKET CRACKED, NEED TO BE REPLACED. INSTALLED BOTH I/B AND O/B BRACKETS ASDR IPXA2026071586789Cover Plate · crackedSLAT NR 9, OUTBD TRACK GAP PANEL COVER IS CRACKED. REMOVED COVER SLAT #9, OUTBD TRACK GAP IAW SRM 51-40-02-0G. VERIFIED INSTALLED SKIRT EXTENSION PANEL ON #9 SLAT IAW B757-200 SRM 51-40-02.SDR IPXA2026071586820Cover Plate · crackedSLAT NR 8, INBD TRACK GAP PANEL COVER IS CRACKED. REMOVED COVER ON SLAT NR 8, INBD TRACK GAP I.A.W B757-200 SRM 51-40-02-0G. INSTALLED IAW SRM 51-40-02. VERIFIED INSTALLED SKIRT EXTENSION PANEL ON #8 SLAT IAW SRM 51-40-02.SDR IPXA2026092068403Skin · dentedDENT FOUND IN LEADING EDGE FLAP NR 16 IN APPROX CENTER OF FLAP. ALL STEP OF EO-97822-REQ4 COMPLETED. FLAP OK TO INSTALL.SDR IPXA2026062957241Seal · damagedNR 26 V.C FLAP, OUTBOARD MOLDING SEAL DAMAGE. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.107 & CMM IPL 71-13-24 REV.50.SDR DALA2026062203698Doubler · debondedDEBONDED ON PRODUCTION DOUBLER OF 2.5IN X 1.5IN AT LOWER SURFACE OSS305.5 LE SLAT 7 TRAILING EDGE WEDGE. LOWER SURFACE OSS305.5 LE SLAT 7 TRAILING EDGE WEDGE WAS REPAIRED IAW SRM-51-70-10-2R IAW SRM-57-43-02-2R-1. (1657512) AIRCRAFT WAS GROUNDED.SDR FDEA202606190782Wedge · gougedLEFT WING OTBD L/E SLAT # 4 I/B LOWER SURFACE REAR EDGE HAS (2) GOUGES APPLIED PERMANENT REPAIR AT L/WING O/B L/E SLAT # 4 I/B LOWER SKIN IAW SRM 57-43-02- 2R, REP 1, TABLE 201, FIG 201, SHEET 6 AND SRM 51-70-10-2R, REP 4SDR FDEA202606180778Skin · dentedDENT ON UPPER SKIN WEDGE OF SLAT NR 8 OSS 457 SLAT NR 8 OSS 457 WAS REPAIRED IAW SRM 57-43-02-2R FIG 201 SHEET 1 AND SRM 51-70-10-2R PAR G FIG 209, SHEET 1, REV 94. DEC 15 /2025SDR VNAA202607280013Canister · crackedCRACKS IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LT MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV --SDR DALA2026061903677Skin · scratchedSCRATCH ON LOWER SKIN OF AFT MOVABLE VANE (3 INCHES FROM T.E. AND 6 INCHES FROM INBRD EDGE APPROX) AT RT WING. LOWER SKIN OF AFT MOVABLE VANE WERE REPAIRED IAW SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND IAW SRM 51-70-02-0G PROCEDURE GENERAL. (LP 1651992 - AIRC
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