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 MASA20210914407Slat Track · corrodedSLAT TRACK 1-1 OF SLAT #1 ON THE RH WING WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 45, EA 69-2021-148.SDR MASA20210914406Slat Track · corrodedSLAT TRACK 1-3 OF SLAT #1 ON THE RH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 105, EA 69-2021-150.SDR MASA20210914405Slat Track · corrodedSLAT TRACK 2-1 OF SLAT #2 ON THE RH WING WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 15, EA 69-2021-151.SDR MASA20210914404Slat Track · corrodedSLAT TRACK 2-2 OF SLAT #2 ON THE LH AND RH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE LOWER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 85, EA 69-2021-152.SDR DALA2021091305450Skin · scratchedSHIP 1807 MAINTENANCE FOUND L/H NO.4 SLAT TRAINING EDGE LOWER SURFACE SCRATCH AT 53 INCHES TO O/B EDGE. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-10. (LP 1946360)SDR SWAA2021101317030None · crackedCRACK AROUND THE FASTENER AT NR 8 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. FABRICATED REPAIR AND FILLER, APPLIED CHEMICAL CONVERSION COATING IAW SRM 57-42-01-2R-8. APPLIED PRIMER TO REPAIR AND INSTALLED COUNTERSINK REPAIR WASHERS IAW SDR SWAA2021101317029None · crackedCRACK AROUND THE FASTENER AT NO.3 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN. INSTALLED REPAIR IAW SRM 57-42-01-2R-8. STEP 4L. AND 21-157-02763-WIP1. INSTALLED ACCESS PANELS AND FLEX SKIN IAW SRM 51-40-02.SDR DALA2023011900392Wedge · damagedERA 593987-14 ISSUED FOR REPAIR TO SLAT #4 TE WEDGE. SLAT NBR 4 WAS REPLACED FOR SERVICEABLE SLAT PER AMM 27-81-02. AND ER/A 593987-14 REV.ORIGINAL.SDR FDEA202109082251Skin · damagedRW #7 SLAT UPPER INBD T/E SURFACE HAS DAMAGE REPAIRED RIGHT WING #7 SLAT IAW FEDEX EA# F-5750-T0363944-P1 WINGS - FLIGHT SURFACES - #7 SLAT - TRAILING EDGE WEDGE - UPPER SKIN - SRM REPAIR DEVIATIONSDR FDEA202109082250Skin · dentedRW #6 SLAT OTBD UPPER T/E SURFACE HAS A DENT REPAIRED RW #6 SLAT O/B UPPER T/E SURFACE IAW B757-SRM 57-43-02-2R FIG. 201 & 51-70-10- 2R REPAIR 4 & FEDEX EA NO. F-5750-T0363939 P1 WINGS - FLIGHT SURFACES - #6 SLAT - TRAILING EDGE WEDGE - UPPER SKIN - SRM RSDR JR2R202109089088Skin · gougedR/H #2 SLAT DAMAGED ON BACK SIDE OF SLAT DUE TO INTERFERENCE WITH LOOSE SCREWS. REPLACED SKIN ON SLAT.SDR SWAA2021101115438None · crackedCRACKED LOWER SURFACE SLAT 4 NOSE SKIN, LT WING. NO FOUND ALLOWABLE DAMAGE ON SRM. REMOVED NR 4 SLAT SKIN, ACCESS PANEL 522DB, AND FASTENERS IAW SRM 51-40-02. ROTOTEST INSPECTION ACCOMPLISHED IAW NDT MANUAL PART 6 51-00-00, PROCEDURE 16. CRACK INDICATIONS SDR FDEA202109042218Skin · wornRH WING, SLAT NO. 8 TRAILING EDGE WEDGE INNER SKIN WITH COMPOSITE MATERIAL EXPOSED. SLAT #8 TRAILING EDGE WEDGE INNER SKIN AT POSITION OSS 431.1 WAS REPAIRED I.A.W. SRM 57-43-02-2R PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R PAG. 159, 162, 163 FIG. 202 REV. 81SDR DALA2021090705253Wedge · debondedSHIP 5643 HE #3 SLAT T/E WEDGE LWR SURFACE HAS AN AREA THAT HAS AN INDICATION OF DISBOND NOTED. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON #3 SLAT T/E WEDGE IAW BOEING S.B. 757-57-0066, B757-200 SRM. SLAT REMOVED AND INSTALLED ON AMDS W/C. (1933049)SDR MASA20210831387Slat Track · corrodedSLAT TRACK 3-2 OF THE SLAT #3 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 10, ITEM 90, EA 69-2021-131SDR MASA20210831386Slat Track · corrodedSLAT TRACK 2-2 OF THE SLAT #2 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 85, EA 69-2021-132.SDR MASA20210831385Slat Track · corrodedSLAT TRACK 1-2 OF THE SLAT #1 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 85, EA 69-2021-133.SDR FDEA202108292155Skin · debonded#3 SLAT DISBOND INDICATION FOUND: T/E WEDGE LOWER SKIN 1.5" IN DIAMETER, 30" FROM O/B, 2" FROM TOP T/E REPLACED #3 SLAT PER B757 AMM 27-81-02-4SDR DALA2024061106029Wedge · debondedSHIP 649 AD - AA - 17 DISBONDED AREAS WERE FOUND ON TRAILING EDGE WEDGE UPPER SURFACE AT SLAT 3. CORRECTIVE ACTION: ORIG SLAT WAS REPAIRED PER CMM 54-43. REF SRM. SLAT #3 WAS REPLACED FOR SERVICEABLE SLAT #3 WITH AMDS. (1927386)SDR DALA2021082705070Skin · dentedLEFT WING SLAT 4 HAS DENT IN UPPER SURFACE. PREPARED , TREATED AND APPLIED EPOXY PRIMER PER A 321 SRM 57-40-00-300-065 . MEASURED DENTED AREA AND FOUND WITHIN LIMITS PER A 321 SRM 57-40-00-283- 001 DEPTH = .167" / CHORD WISE DIMENTION = 5.01". REPAIRED DENT RSDR SWAA2021092109390Access Panel · elongatedELONGATED HOLE ACCESS PANEL 621NB LEADING EDGE AT RT WING ; 2021-384373 / [24] REPAIRED ACCESS PANEL 621N,NG,NRC,2021-09-16 02:41:39,22Y,N,MX,0,0,,ELONGATED HOLE ACCESS PANEL 621NB LEADING EDGE AT RT WING ; 2021-384373"SDR FDEA202108222189Rub Strip · crackedLH WING: #1 SLAT UPPER SURFACE O/B - T/E RUBSTRIP UNDERSIDE CRACKED. (MRKD) REMOVED AND INSTALLED RUBSTRIP PER E.A 8-5750-T0363959, & REF MD10-30 SRM 51-35-01 VOL II, & REF DAC DWG NRB6224 REF. JPF ITEMS 2,3, AND 4SDR AALA202109025123Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #2 MID FORWARD ATTACH BOLT BETWEEN WS 700 AND WS 1406 BETWEEN RIB 2 AND RIB 3. REPLACED BOLT PER AMM 27-84-63-400-002.SDR AALA202109025778Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #2 UPPER FORWARD ATTACH BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIB 2-3. REPLACED BOLT PER AMM 27-84-63-400-002.SDR AALA202108308295Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #2 UPPER AFT BOLT. REPLACED BOLT PER AMM 27-84-63-400-002-ASDR FDEA202108202046Skin · wornTHREE WEARS ON INNER SIDE OF TRAILING EDGE OF SLAT NO 5 BETWEEN STA 389.71 TO STA 492.95 SLAT NO 5 TRAILING EDGE WEDGE LOWER SKIN AT POSITION OSS 488.7 WAS REPAIRED IAW SRM 57-43-02-2R PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R PAG. 149,152, 163 FIG. 202 REVSDR CALA2021082001386Slat · damagedPDA 1 6"BY 9" PIECE SECTION MISSING FROM #5 SLAT. FOUND ON ARRIVAL. FOLLOWING GMM 02-30-95SDR SWAA2021100508835None · corrodedRT WING SLAT #6 T/E WEDGE TOP SURFACE I/B CORNER HAS CORROSION. ; / [01] REMOVED CORROSION AT R/WING #6 SLAT UPPER SURFACE I/B CORNER AS REFERENCE B737-700 SRM 51-10-02-0G-0; [02] CERTIFIED; [03] VERIFIED CORROSION REMOVAL; [04] PERFORMED UT THICKNESS INSP ON SDR AALA202109283032Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE #1 SLAT, #1 SLAT TRACK MIDDLE FORWARD BOLT. REPLACED BOLT PER AMM 27-84-63-400-002-A.SDR AALA202108244875Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #6 LOWER MID ATTACH BOLT AT WS 6016.4 AND RIB 11. REPLACED BOLT PER AMM 27-84-64-400-002.SDR AALA202108247517Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #8 LOWER AFT ATTACH ECCENTRIC BOLT AT WS 8753.14 AND RIB 16. REPLACED BOLT PER AMM 27-84-65-400-002.SDR FDEA202108132013Skin · wornWEAR IN TRAILING EDGE OF SLAT NO.5 AT 41" FROM INBOARD TO OUTBOARD, LH WING. LH WING TRAILING EDGE OF SLAT NO 5 AT 41" FROM INBOARD TO OUTBOARD WAS REPAIRED I.A.W. SRM 57-43-02-2R PAG. 1 TO 2 FIG. 201 AND SRM 51-70-10-2R PAG. 11,12,53 FIG 202 REV 81 AUGSDR FDEA202108132012Skin · wornWEAR ON LOWER SKIN OF TRAILING EDGE AT SLAT 8 WEAR ON LOWER SKIN OF TRAILING EDGE AT SLAT 8 WAS REPAIRED I.A.W. S.R.M. 57-43-02-2R PAG. 1 TO 2 FIG. 201 AND S.R.M. 51-70-10-2R PAG. 11,12,53 FIG. 202 REV. 81 AUG 15 / 21SDR IPXA2021090973750Fairing · crackedINSPECTION TYPE:3CLH WING SLAT #1 PERFORMANCE FAIRING CRACK AT WEB RIB STA=XIS 150.74.REPAIRED CRACKED LH WING SLAT #1 PERFORMANCE FAIRING WEB RIB AT STA= XIS 150.74 IAW VT-SAA EA 011-5754-01-A9293 REV I/R AND UPS EO MD11-5750-81519-A (MINOR).SDR SWIA2021090360721Roller · deformedLH SLAT TRACK 1-2 4EA SIDE ROLLERS WORN OUT OF LIMITS. (C-CHECK RO 8/31/21) REMOVED AND RE-INSTALLED 4EA NEW SERVICEABLE ROLLERS ON LH SLAT TRACK 1-2 IAW CRJ 700 AMM 27-81-44-000/400-801-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.SDR DALA2021081804806Skin · dentedSHIP 650 DENT #8 ON UPPER TRAILING EDGE WEDGE AT SLAT NBR 10 RH WING. IS OUT OF LIMITS IN REF NRC 00241. CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO. 00976: DENT #8 ON UPPER TRAILING EDGE WEDGE AT SLAT NBR 10 RH WING (REF NRC 00241) WAS REPAIRED PER B-757-2SDR IPXA2021081372710Plate · crackedINSPECTION TYPE:A300LH WING #5 SLAT TRACK HAS BROKEN SHUTTER STOP PLATE.REMOVED AND REPLACED PLATE IAW A300 SRM 51-40-21.SDR DALA2021081604720Wedge · dentedSHIP 650 DENT ON UPPER TRAILING EDGE WEDGE AT SLAT NBR 9 RH WING.DENT #8. CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO. 00975: DENT ON UPPER TRAILING EDGE WEDGE AT SLAT NBR 9 RH WING. DENT #8 (REF. N.R.C. 00239) WAS REPAIRED PER B-757-200 S.R.M. (1908235)SDR DALA2022020400738None · noneSHIP 695 DISBOND NOTED ON #9 SLAT LOWER SURFACE. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON #9 SLAT T/E WEDGE IAW B757-200 SRM 57-43-02-2R-1 FIG.201, BOEING S.B. 757-57-0066 AND B757-200 SRM 51-70-10-2R-4 REP.4. (1904339)SDR DALA2021081104607Wedge · debondedSHIP 6801 DISBOND ON REPAIR AREA OF THE TRAILING EDGE WEDGE (UPPER SIDE) AT SLAT # 10, OSS 786. CORRECTIVE ACTION: SUMMARY OF NRC 00019 : TRAILING EDGE WEDGE (UPPER SIDE) AT SLAT # 10, OSS 786 WAS REPAIRED PER B757-200 SRM. (1903218)SDR DALA2021081004580Skin · debondedSHIP 6801 ONE DISBOND OF 1) 1.125" X 0.875" (LENGHT/WIDTH) ON OSS 490.1 APPROX. UPPER SURFACE AT LE SLAT 8 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF NRC 00077 : LE SLAT 8 TRAILING EDGE WEDGE. WAS REPAIRED PER B-757-200 S.R.M. (1903226)SDR FDEA202108071995Skin · delaminatedDISBOND FOUND 36" INBOARD OF OUTBOARD EDGE, 8" FROM AFT EDGE ON #8 SLAT UPPER SURFACE REMOVED, REPLACED, ADJUSTED AND OPS CHECKED #8 SLAT PER B757 AMM 27-81-02-4SDR FDEA202108071991Skin · delaminatedDISBOND INDICATION FOUND ON #4 SLAT, BOTH UPPER AND LOWER SURFACES 20 INCHES FROM INBOARD EDGE AND 6 INCHES BELOW TRAILING EDGE. REMOVED, REPLACED, ADJUSTED AND OPS CHECKED #4 SLAT IAW B757 AMM 27-81-02-4. OPS CHECK GOOD.SDR P5CA2021080600276Skin · brokenBROKEN - SKIN AND FLEX CORE LH WING #4 SLAT TE WEDGE INBD CORNER(<P>PERFORM PERMANENT REPAIR AT LH WING #4 SLAT TE WEDGE UPPER SKIN. REFER TO JOB CARD ATTACHING #0245471 FOR DETAIL ACTION SUMMARY. CONDITION CHECK IS SATISFACTORY</P>)SDR P5CA2021080600278Skin · brokenBROKEN - SKIN, LH WING #3 SLAT TE WEDGE INBD(<P>PERFORM PERMANENT REPAIR AT LH WING #3 SLAT TE WEDGE UPPER SKIN REFER TO JOB CARD ATTACHING SHEET #0245474 FOR DETAIL ACTION SUMMARY. CONDITION CHECK IS SATISFACTORY</P>)SDR P5CA2021080600279Skin · brokenBROKEN - SKIN AND FLEX CORE, LH WING #5 SLAT TE WEDGE OUTBD CORNER(<P>PERFORM PERMANENT REPAIR AT LH WING #5 SLAT TE WEDGE UPPER SKIN, REFER TO JOB CARD ATTACHING #0245476 DETAIL ACTION SUMMARY. CONDITION CHECK IS SATISFACTORY</P>)SDR SWIA2021090360720Roller · deformedRH SLAT TRACK 1-2 HAS 4EA SIDE ROLLERS WITH FLAT SPOTS OUT OF LIMITS, AND REQUIRE REPLACEMENT. (C-CHECK RO 8/31/21) REMOVED AND REPLACED RH 1-2 4EA SIDE ROLLERS IAW CRJ 700 AMM 27-81-44-000/400-801-A01. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMEDSDR FDEA202108051938Rib · crackedWHILE PERFORMING INTERNAL BORESCOPE INSPECTION (SPECIAL/NON ROUTINE MAINTENANCE FORM NUMBER N00777), LEFT HAND WING NUMBER 8 SLAT INTERNAL RIB FOUND CRACK AT STATION XOS 1141.220. CRACKED RIB REMOVED AS PER SRM 51-31-01-0G AND FABRICATED RIB PER DOUGLAS SDR FDEA202108051937Rib · crackedWHILE PERFORMING INTERNAL BORESCOPE INSPECTION (SPECIAL/NON ROUTINE MAINTENANCE FORM NUMBER N00777), LEFT HAND WING NUMBER 8 SLAT INTERNAL RIB FOUND CRACK AT STATION XOS 1092.115. CRACKED RIB REMOVED AS PER SRM 51-31-01-0G AND FABRICATED RIB PER DOUGLAS SDR FDEA202108051936Rib · crackedWHILE PERFORMING INTERNAL BORESCOPE INSPECTION (SPECIAL/NON ROUTINE MAINTENANCE FORM NUMBER N00777), LEFT HAND WING NUMBER 8 SLAT INTERNAL RIB FOUND CRACK AT STATION XOS 1086.831. CRACKED RIB REMOVED AS PER SRM 51-31-01-0G AND FABRICATED RIB PER DOUGLAS
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