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 AALA2020022519006Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #3 LOWER BOLT. REPLACED BOLT PER AMM 27-84-63-400-002-A.SDR IPXA2020012745344Wedge · delaminatedINSPECTION TYPE: SEG4, DELMINATED DENT ON THE NR 2 SLAT T E WEDGE UPPER SURFACE. REPAIRED THE NR 2 TE SLAT WEDGE IAW SRM 57-43-02-2R-1, AND SRM 51-70-10-2R-4.SDR DALA2020012730606Skin · debondedTHE NR 9 SLAT T/E WEDGE UPPER SURFACE OTBD SIDE HAD AN INDICATION OF SKIN TO CORE DEBONDING. REMOVED THE DEBONDED SKIN. ACCOMPLISHED A PERMANENT METAL BOND REPAIR. NDT ACCOMPLISHED POST REPAIR, INSPECTED IAW SB 757-57-0066 WITH NO INDICATIONS OF DEFECTS NSDR DALA2020012720604Skin · debondedDEBOND OF 0.875" X 0.875" AT DENTED AREA ON THE LT WING LE SLAT NR 4 TRAILING EDGE WEDGE UPPER SKIN. REPAIRED IAW SRM 57-43-02-2R-1, AND SRM 51-70-10-2R PROCEDURE. REPAIR GENERAL.SDR AALA202001239023Slat Track · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING LEADING EDGE SLAT TRACK #6 OUTBOARD SIDE HAS WIDTH REDUCTION / WEAR AT WS 8979 AND RIB 18. REPLACED SLAT TRACK PER AMM 57-47-00-400-801.SDR DALA2020012300520Skin · damagedNR 7 SLAT T/E WEDGE INBD EDGE AFT, HAD BENT SKIN AND SEPARATED FORM COMPOSITE. REPAIRED IAW SRM 51-70-10.SDR SWAA2020012340717Skin · delaminatedNR 6 SLAT LOWER TRAILING EDGE WEDGE OUTBOARD END HAS REPAIR DELAMINATED. NR 6 SLAT LOWER TRAILING EDGE WEDGE OUTBOARD END DELAMINATION WAS REPAIRED IAW SRM 51-70-10-2R-0.SDR SWAA2020012340716Skin · delaminatedNR 6 SLAT LOWER TRAILING EDGE WEDGE INBOARD END HAS REPAIR DELAMINATED. NR 6 SLAT LOWER TRAILING EDGE WEDGE OUTBOARD END DELAMINATION WAS REPAIRED IAW SRM 51-70-10-2R-0SDR DALA2020012000406Skin · crackedLT WING NR 4 SLAT SURFACE SKIN FOUND CRACK FROM LOWER EDGE 10.5", O/B EDGE 41". C/A LT WING NR 4 SLAT SURFACE SKIN FROM EDGE 10.5", O/B EDGE 41" CRACK AREA REPAIRED AS PER SRM 57-43-01-2R-2 RELEASE.SDR SWAA2021082201238Skin · deformedCUSTOMER WALK; #3 SLAT HAS SKIN DEFORMED ON THE TOP SURFACE INBOARD OF EXITING REPAIR. / REMOVED AND REPLACED SLAT #3 AS PER B737 AMM 27-81-71-400-801 PERFORMED SLAT #3 ADJUSTMENT CHECK FOUND NORMAL PER B737 AMM 27-81-00-820-803.SDR DALA2020012390529Skin · debondedDEBONDS, 4" X 1.750" WAS FOUND ON SLAT WEDGE NR 1 UPPER SKIN OSS 806, LT WING. REPAIRED IAW SRM 57-43-02-2R-1, AND SRM 51-70-10-2R-4.SDR DALA2020012390528Skin · debondedDEBONDS, 3.00" X 1.500" ON THE UPPER AND LOWER SKINS OF THE LT WING SLAT NR 3 TRAILING EDGE WEDGE AT STA SS=438.1. REPAIRED IAW SRM 57-43-02-2R-1, AND SRM 51-70-10-2R, PROCEDURE. REPAIR GENERAL.SDR IPXA2020020311639Skin · crackedINSPECTION TYPE:C12CRACK ON #10 SLAT L/E SKIN (P/N : 114T4103-4) NEAR OSS 724REPAIR I.A.W 767-300F SRM 57-43-01-2R-1 REV.76.01SDR SWIA2020012347982Angle · crackedLH OUTBOARD SLAT CONDUIT CLIP IS CRACKED. (C-CHECK) RO:1/22/2020REMOVED AND REPLACED THE L/H SLAT #4 O/B BACKWALL-TEMP SENSOR BONDING TAB IN REFERENCE TO ERJ 175 AMM.SDR DALA2020012218510Wedge · dentedTWO DENTS ON THE LT WING NR 5 SLAT WEDGE, UPPER SURFACE. FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED IAW SRM.SDR DALA2020012400586Wedge · delaminatedPD: T/E WEDGE DELAMINATED ON UPPER SURFACE I/B. REPAIRED REF. 767-300 SRM 51-70-10, REF. 57-43-02-2R-1.SDR SWIA2020012347977Tab · brokenR/H SLAT #4 O/B BACKWALL-TEMP SENSOR BONDING TAB BROKEN. (C-CHECK) RO:1/22/2020 / REMVOED AND REPLACED THE R/H SLAT #4 O/B BACKWALL-TEMP SENSOR BONDING TAB IN REFERENCE TO ERJ 175 AMM.SDR SWIA2020012347976Tab · brokenR/H SLAT #2 O/B BACKWALL-TEMP SENSOR BONDING TAB BROKEN. (C-CHECK) RO:1/22/2020 / REMVOED AND REPLACED THE R/H SLAT #2 O/B BACKWALL-TEMP SENSOR BONDING TAB IN REFERENCE TO ERJ 175 AMM.SDR SWAA2020021214198Skin · crackedL/H WING #4 SLAT NOSE SKIN ACTUATOR RIBS CRACKED AROUND THE FASTENER.. / REPAIRED SKIN IAW SRM.SDR DALA2020012150434Skin · debondedONE DISBOND OF 4 X 3 AT UPPER SKIN OF LE SLAT 9 TRAILING EDGE WEDGE OSS-679 RT WING. REPAIRED IAW SRM 51-70-10-2R-4, AND SRM 57-43-02-2R-1.SDR DALA2020012150432Skin · debondedTHREE DEBONDS FOUND ON THE UPPER SKIN OF THE LE SLAT NR 7 TRAILING EDGE WEDGE, RT WING. REPAIRED IAW SRM 51-70-10-2R-0G, PAR. 3, 7, 8, 14, 20, AND 22, AND SRM 57-43-02-2R-1.SDR DALA2020012150431Skin · debondedTWO DISBONDS AT UPPER SKIN OF LE SLAT 8 TRAILING EDGE WEDGE, RH WING. REPAIRED IAW SRM 51-70-10-2R-4 AND SRM 57-43-02-2R-1.SDR CALA2020011900164Skin · dented(SUPPORT TASK) L-23 NO DOT. LEFT WING NUMBER 2 SLAT HAS A DENT APPROX 8" O/B OF TRACK 5 AND 1" FWD OF STRINGER. NONROUTINE 9825786 ACCOMPLISHED REPAIR OF LEFT WING NUMBER 2 SLAT DENT APPROXIMATEL Y 8" O/B OF TRACK 5 AND 1" FWD OF STRINGER IAW SRM 57-40-00 -300SDR DALA2020011700361Skin · delaminatedNR 1 SLAT TRAILING EDGE WEDGE UPPER SURFACE HAS (3) SEPERATE INDICATIONS OF DELAMINATIONS OF SKIN CORE DISBONDS. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-10-2R REP 4 ON THE NR 1 SLAT TRAILING EDGE WEDGE UPPER SURFACE.SDR DALA2020011700359Skin · dentedDENTED AREA ON LT WING SLAT 3 TRAILING EDGE WEDGE AT STA SS=523.8 UPPER SKIN. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-10-2R-0G PAR 7, 8, 14, 15, 18 AND 20 ON REFERENCE OF SRM 57-43-02-2R-1.SDR DALA2020011500289Wedge · dentedDENT ON LT WING NR 4 SLAT WEDGE UPPER SURFACE OUT OF LIIMITS IN ACCORDANCE WITH SRM 57-43-02-1A-1 FIG 101 DETAIL III. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-01-2R-1 ON REFERENCE OF SRM 57-43-02-1A-1 FIG 101 NOTE J.SDR DALA2020011500288Wedge · dentedDENT ON LT WING SLAT NR 2 SLAT WEDGE UPPER SURFACE OUT OF LIIMITS IN ACCORDANCE WITH SRM 57-43-02-1A-1 FIG 101 DETAIL III. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-01-2R-1 ON REFERENCE OF SRM 57-43-02-1A-1 FIG 101 NOTE J.SDR DALA2020011500287Wedge · dentedDENT ON RT WING NR 9 SLAT WEDGE UPPER SURFACE OUT OF LIIMITS IN ACCORDANCE WITH SRM 57-43-02-1A-1 FIG 101 DETAIL III. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-01-2R-1 ON REFERENCE OF SRM 57-43-02-1A-1 FIG 101 NOTE J.SDR DALA2020011400263Wedge · dentedDENTS (2EA) ON RT WING NR 7 SLAT WEDGE UPPER SURFACE OUT OF LIIMITS IN ACCORDANCE WITH SRM 57-43-02-1A-1 FIG 101 DETAIL III. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-01-2R-1 ON REFERENCE OF SRM 57-43-02-1A-1 FIG 101 NOTE J.SDR DALA2020011400262Wedge · dentedDENTS (2EA) ON RT WING NR10 SLAT WEDGE UPPER SURFACE OUT OF LIIMITS IN ACCORDANCE WITH SRM 57-43-02-1A-1 FIG 101 DETAIL III. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-01-2R-1 ON REFERENCE OF SRM 57-43-02-1A-1 FIG 101 NOTE J.SDR DALA2020011400261Wedge · dentedDENTS (2EA) ON RT WING NR 6 SLAT WEDGE UPPER SURFACE OUT OF LIIMITS IN ACCORDANCE WITH SRM 57-43-02-1A-1 FIG 101 DETAIL III. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-01-2R-1 ON REFERENCE OF SRM 57-43-02-1A-1 FIG 101 NOTE J.SDR DALA2020060402448Skin · debondedONE DISBOND OF 1.00" OF LENGTH X 0.500" OF WIDTH ON UPPER SKIN AT LE SLAT 2 TRAILING EDGE WEDGE, STA: OSS 705 LT WING. SUMMARY NRC 00104:DISBOND WAS REPAIRED PER SRM.SDR ASAA2020030232312Skin Panel · gougedLEFT WING INBOARD LEADING EDGE AT SLAT #1 ON THE INBOARD SIDE OF THE FIXED LEADING EDGE IS GOUGED WITH BARE METAL. "MARKED IN RED" GROUNDED - YES. REMOVED AND REPLACED L/H I/B FIXED L/E SKIN PANEL P/N D5745004820639 REF AIRBUS DWG D57450033 AND A320 SRM 51-42-SDR FDEA2020010970033Rib · crackedLEFT WING - NUMBER 1 LEADING EDGE SLAT CRUISE PERFORMANCE FILLET RIB FOUND CRACK AT STATION XIS 150.74 LEFT WING - NO 1 LEADING EDGE SLAT CRUISE PERFORMANCE FILLET CRACKED RIB AT STATION XIS 150.74 CARRIED OUT REPAIR AS PER SRM 57-40-71-2R FIGURE 201 REPAISDR FDEA2020010970032Rib · crackedRIGHT WING - NUMBER 1 LEADING EDGE SLAT CRUISE PERFORMANCE FILLET RIB FOUND CRACK AT STATION XIS 150.74 RIGHT WING - NO 1 LEADING EDGE SLAT CRUISE PERFORMANCE FILLET CRACKED RIB AT STATION XIS 150.74 CARRIED OUT REPAIR AS PER SRM 57-40-71-2R FIGURE 201 REPSDR R61A2020012870095Slat Track · crackedDURING HEAVY CHECK...LH WING LEADING EDGE SLAT 2 BOTH TRACK CUTOUTS CRACKED. REPAIRED IAW SRM 57-49-01 REPAIR 6. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR DALA2020010900143Slat · debonded(AIRCRAFT 5641, L/P 1435427) L/H WING SLAT #4 INBD UPPER CORNER DISBONDED. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR IAW B757-200 SRM 57-43-02-2R1, SRM 51-70.SDR DALA2020010900162Panel · worn# 6 SLAT SPRING LOADED PANEL AT OUTBOARD END OF SLAT WORN THRU ON LEADING EDGE REPAIRED PANEL PER SRM 57-10-17 (LP 1434234)SDR DALA2020010900160Skin · debonded#11 SLAT UPPER SURFACE, OUTBOARD EDGE HAS A DISBONDED PREVIOUS REPAIR. REPAIRED PER SRM 57-43-02. (LP 1434040)SDR DALA2020010900159Skin · debonded#12 SLAT UPPER SURFACE INBOARD EDGE HAS A DISBONDED PREVIOUS REPAIR. C/W SRM 57-43-02 (LP 1434031)SDR DALA2020010900158Wedge · dentedR/H WING #7 SLAT T/E WEDGE UPPER SURFACE HAS DENTED AREA 41 INSCHES FROM I/B END OF SLAT. REPAIRED PER SRM 57-43-02 (LP 1434018)SDR SWAA2021082201396Skin · damagedLEFT WING # 4 SLAT HAS PULLED IN FASTENERS AT SLAT- ACTUATOR NOSE SKIN. / REMOVED; REPLACED; REDJUSTED AND FUNCTIONAL TESTED #4 SLAT IAW MM 27-81-21-000-801 AND MM 27-81-21-400-801 ADJUSTMENT / TEST CHECK GOOD (POS: 4; TAG NO.: 655594; P/N OFF: 114A5040-3; S/NSDR IPXA2020020765878Skin · crackedINSPECTION TYPE:3CR/H WING #2 SLAT UPPER O/B SKIN IS CRACKED AT EXISTING REPAIR DOUBLER STA. XIS=328.106.REPAIRED R/H WING #2 SLAT UPPER SKIN AT STA. XIS= 328.106 IAW VT-SAA EA 011-5754-01-A8005 REV. I/R AND UPS EO MD11-5750-75285-A. (MAJOR)SDR SWAA2021072629388Skin · delaminatedRIGHT HAND WING #8 SLAT UPPER SURFACE IS DELAMINATED AT 39' O/B AND 1.5' T/E / RIGHT HAND WING #8 SLAT UPPER SURFACE DELAMINATED AT 39' O/B AND 1.5' T/E REPAIRED IAW SRM 57-42-01-2R-4 AND IAW SRM 51-70-10-2R-2. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-42-01-1SDR SWAA2020011340409Skin · delaminatedR/H WING #8 SLAT UPPER SURFACE DELAMINATED AT 39" OUTBOARD AND 1.5" TRAILING EDGE. / REPAIRED SLAT IAW SRM.SDR DALA2020010600061Wedge · delaminatedRH WING NO.11 SLAT I/B T/E WEDGE CORNER FOUND DELAMINATED C/A REPAIRED RH WING NO.11 SLAT I/B T/E WEDGE CORNER DELAMINATED AS PER B767-400 SRM57-43-02-2R-1 AND SRM51-70-10,RELEASE 59.00 DATE :19DEC19. (1430544)SDR DALA2020010200007Wedge · wornR/H #8 SLAT TRAILING EDGE FOUND WORN AT LES 455 C/A ENTR 00861558 W R/H #8 SLAT TRAILING EDGE WEDGE AT LES 455 REPAIRED AS PER B767- 400 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4, RELEASE 59.00 (1426833)SDR DALA2020010200005Wedge · wornR/H #10 SLAT TRAILING EDGE WEDGE FOUND WORN AT LES 708. C/A R/H #10 SLAT TRAILING EDGE WEDGE AT LES 708 REPAIRED AS PER B767 -400 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4, RELEASE 59.00 (1426836)SDR ABXR2020010131350Support Beam · corrodedLEFT WING NR 2 FLAP SUPPORT 1-2-3 BEAM HAD CORROSION IN 5 CODE C FASTENER HOLES.SDR ABXR2020010130351Skin · crackedNR 9 SLAT SKIN LOWER TRAILING EDGE HAD A MISSING FILLER.
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