JASC 5740
Service difficulty reports · 3,003
Reports filed under 5740 · Wing, Attach Fittings, 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 = '5740' 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 = '5740' 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 VNAA202601170010Nut Plate · corrodedCORROSION ON NUT STRIPS (2 E/A'S) AT UPPER AREA OF LH/RH WHEEL WELL AREA (APROX. RBL/LBL 49). NUT STRIPS (2 E/A'S) AT UPPER AREA OF LH/RH WHEEL WELL AREA (APROX. RBL/LBL 49) WERE EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACSDR AALA202512051088Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING BEARING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-72-11.SDR IPXA2025111570289Drag Fitting · crackedAFTER ACCOMPLISHING HFEC OPEN-HOLE INSP AT THE NR 2 PYLON WING SKIN FASTENER HOLES PER EO-88069-JIC12, HOLES 2,3,4, AND 9, HAS CORROSION INDICATIONS. ACCOMPLISH REPAIR PER EO-95741-REQ1 AND VT-MAE EA 757-5720-27-A4215, REV. -, PRIOR TO FURTHER FLIGHT.SDR DALA2025110308010Bracket · damagedFOUND DAMAGE ON RT WING #3 FLAP TRACK BRACKET ASSY. REMOVED AND REPLACED BRACKET ASSY REF A319 AMM 57-53-21. (1283709).SDR SWAA2025120430617Nut Plate · crackedCRACK RAIL NUT PLATES, LEADING EDGE INTERNAL CAVITY LOCATED OF SS 499, LT WING. REPLACED RAIL NUT PLATES ON LEADING EDGE INTERNAL CAVITY LOCATED OFSS499, LT WING; IAW 51-40-02, DWG 112A4402, SHEET 13, REV - CRACK LENGTH: 0.449 IN.SDR 2025FA0000736Bracket · corrodedSVO 0145- SUPPORT BRACKETS ON FUSELAGE EXTERIOR FAIRING SUPPORT STRUCTURE AT FS 575 BL 3LH AND RH SIDE WERE FOUND TO BE CORRODED- LEVEL 2 CORROSIONSDR SWAA2025120129794Nut Plate · crackedCRACKED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE, SS 508 RT WING. REPLACED RAIL NUT PLATES IAW SRM 51-10-02, PARAGRAPH 9, AND SRM 51-40-02.SDR SWAA2025120129793Nut Plate · crackedCRACK ON RAIL NUT PLATES LOCATED OFSS 483 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT PLATES AND FASTENERS IAW SRM 51-10-02 AND SRM 51-40-02.SDR IPXA2025111186416Panel · crackedRIGHT WING, L/E, KRUGER FLAP BOX AREA, BY RIB2, PANEL STR HAS A CRACK ON A CORNER. REMOVED OTBD ZEE ANGLE P/N: A5724228220547, INBD ZEE ANGLE P/N: A57242282203, AND THREE STIFFENERS (UPPER, MIDDLE, LOWER) FROM PANEL P/N: A57242282001 TO FOM IAW SRM 51-40-21.SDR HYIA20251027001Fitting · corrodedDURING MAINTENANCE A SMALL AREA OF SURFACE CORROSION WAS VISUALLY IDENTIFIED ON THE TOP FACE OF THE VERTICAL LEG OF THE 0822550-43 WING ATTACH FITTING (LT LOWER AFT). THIS CORROSION MEASURES APPROXIMATELY 1.5 INCHES LONG, BY .125 INCHES WIDE WITH AN APPROXIMATSDR SWAA2025111925722Nut Plate · corrodedCORROSION ON RAIL NUT PLATES LOCATED INTERNAL CAVITY LEADING EDGE OFSS706 AT LT WING. REPLACED RAIL ON NUT PLATES (GANG CHANNEL) LOCATED INTERNAL CAVITY LEADING EDGE OFSS706 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 112A4402 SHEET 14SDR SWAA2025112025597Strap · corrodedCORROSION ON OUTER WING LEADING EDGE LOWER ATTACH STRAP AT OSS 65 RT WING. OBTAINED OK TO INSTALL NUT PLATE ON OUTER WING LEADING EDGE LOWER ATTACH STRAP LOC AT OSS 65 ON RT WING. REPAIRED RH WING - O/B FIXED LEADING EDGE - ATTACH STRAP OUTBOARD - BETWEEN SDR SWAA2025111925572Nut Plate · crackedCRACK ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS569 AT RT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS569 AT RT WING. IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 112A4402 SHEET: 14 REV: - MEASSDR DALA2026031101710Seat Track · corrodedFWD FUSELAGE SEAT TRACK CORROSION LBL 23.0 AT FRAME 22. SSI: 53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-2021/004 00306 ACCOMPLISHED PRI 629312-14 REV 0, REV 1, REV 2, AND ERA 629321-14SDR SWAA2025111223691Nut Plate · corrodedCORROSION ON RAIL NUT PLATES LEADING EDGE LOCATED OFSS449 AT LT WING. REPLACED RAIL NUT PLATES LEADING EDGE LOCATED OFSS449 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SDR SWAA2025111223686Nut Plate · corrodedCORROSION ON RAIL NUTPLATES LOCATED LEADING EDGE OFSS331 AT LT WING. REPLACED RAIL NUTPLATES LOCATED LEADING EDGE OFSS331 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SDR N6WA2025101002Fitting · crackedHINGE FITTING CRACKED AT RH WS 185.11. REMOVED AND REPLACED HINGE FITTINGAT RH WS185.11 IAW CRJ SRM 51-42-21 AND 51-42-06SDR SWAA2025102721977Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.SDR SWAA2025102721978Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.SDR N6WA2025100802Attach Angle · corrodedLH MLG WELL BURST PANEL ATTACH ANGLE IS CORRODED. REMOVED AND REPLACED LH MLG WELL BURST PANEL ATTACH ANGLE IAW CRJ SRM 51-42-21SDR SWAA2025110520293Nut Plate · crackedCRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 573 AT LT WING. REPLACED RAIL NUT PLATE LOCATED OUTBOARD FRONT SPAR OFSS 573 AT LT WING IAW B737-800 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DWG 112A4402 SHEET: 41 REV: A. MEASUREMENT OF CRACK IS L: 0.392 ISDR SWAA2025110520295Nut Plate · crackedCRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 491 AT LT WING. REPLACED RAIL NUT PLATE LOCATED OUTBOARD FRONT SPAR OFSS 491 AT LT WING IAW B737-800 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DWG 112A4402 SHEET: 40 REV: A. MEASUREMENT OF CRACK IS L: 0.254 ISDR SWAA2025110520296Nut Plate · crackedCRACK OTBD FRONT SPAR RAIL NUT PLATE OFSS 333 AT LT WING. REPLACED THE NUT PLATE LOCATED OTBD FRONT SPAR OFSS 333 IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0, ITEM 9, AND DWG 112A4402 SHEET: 40 REV: A. MEASUREMENT OF CRACK L: 0.232.SDR SWAA2025110520292Nut Plate · crackedCRACK ON RAIL NUT PLATE FRONT SPAR OFSS 604 AT LT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHEET 41, REV A.SDR SWAA2025110520294Nut Plate · crackedCRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 506 AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G, & DWG 112A4402, SHEET 40, REV A. MEASUREMENT OF CRACK IS L: 0.168 INCHES.SDR IPXA2025093098082Bracket · crackedDURING ACCOMPLISHING OF T.C T3F18E007GZC1 FOUND 1EA HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED INSIDE ACCESS PANEL 675AB. REMOVED SUPPORT BRACKET IAW SRM 51-40-21. FABRICATED NEW PPORT BRACKET I.A.W A300-600 SRM 57-51-11.INSTALLED NEW BRACKET IAWSDR SWAA2025110419100Nut Plate · crackedCRACK ON RAIL NUT-PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 13, REV -. CRACK MEASUREMENT ISDR SWAA2025110419095Nut Plate · crackedCRACK ON RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET:13 REV-.SDR SWAA2025110319098Nut Plate · crackedCRACK ON RAIL NUT-PLATE, OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02, AND DWG 112A4402, REV -, SHEET 13. MEASUREMENT OF CRACK IS L: 0SDR SWAA2025103117343Nut Plate · crackedCRACK ON RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATEIAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG:112A4402; SHEET:13; REV - .SDR SWAA2025103117349Nut Plate · crackedCRACK ON RAIL NUT PLATE, OFSS 410, INTERNAL CAVITY LEADING EDGE LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02 AND DWG 112A4402 SHEET 13 REV - .SDR SWAA2025103117348Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 330 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 330 INTERNAL<BR>CAVITY LEADING EDGE AT LT WING IAW SRM 51-40, AND DWG 112A4402 SHEET 13 REV-.SDR SWAA2025092215809Bracket · crackedL/H WING UPPER TRAILING EDGE SHELF PANEL BETWEEN #5  SPOILER LOWER CENTER SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED L/H WING TRAILING EDGE SUPPORT WEB BRACKET P/N 115A2982-9 ON UPPER FIXED PANEL PER AMM 20-50-11 AND SRM 51-10-02 PARAGRAPH 9 REPAIRABSDR SWAA2025102115574Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED ORSS 375 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 375 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW B737-800 SRM 51-40-02-0G SRM 51-10-02-0G-0 ITEM 9; DUE TO NOT FOSDR IPXA2025092629651Plate · crackedPANEL 613AB ATTACHMENT PLATE CRACKED AT FWD O/B CORNER. INSTALLED DOUBLER AND SHIM IAW A300 SRM 53-15-63 AND 51-40-21.SDR SWAA2025101413092Nut Plate · corrodedCORROSION RAIL NUT PLATE LOCATED OFSS293 INTERNAL CAVITY LEADING EDGE AT RT WING. EVALUATED RAIL NUT PLATE AND NOT FOUND ALLOWABLE DAMAGE ON SRM IAW B737-700 SRM 57-20-01-1A-1 ALLOWABLE DAMAGE. REPLACED RAIL NUT PLATE LOCATED OFSS293 INTERNAL CAVITY LEADING SDR SWAA2025101413091Nut Plate · corrodedCORROSION ON RAIL NUT PLATE LOCATED OFSS308 INTERNAL CAVITY LEADING EDGE AT RT WING. EVALUATED RAIL NUT PLATE AND NOT FOUND ALLOWABLE DAMAGE ON SRM IAW SRM 57-20-01-1A-1 ALLOWABLE DAMAGE. REPLACED RAIL NUT PLATE LOCATED OF SS308 INTERNAL CAVITY LEADING EDGESDR SWAA2025092912110Attach Angle · crackedRIGHT WING T/E FIXED PANEL MID ATTACH ANGLE CRACKED. R & R RT WING T/E FIXED PANEL MID ATTACH ANGLE IAW SRM 51-40-02, AIPC 57-50-00-25, AND AMM 20-50-11-910-801.SDR SWAA2025092912108Attach Fitting · crackedRIGHT WING T/E FIXED PANEL SUPPORT BEAM, ATTACHMENT FITTING CRACKED, JUST INBD OF DEFLECTION CONTROL RIB. R & R ATTACH FITTING IAW 51-4002-0G-0.SDR SWAA2025100611313Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING IAW IAW SRM 51-40-02 AND DRAWING 112A4402 REV:A.SDR SWAA2025100611321Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 632 INTERNAL CAVITY LEADING EDGE AT LT WING REPLACED RAIL NUT-PLATE LOCATED OFSS 632 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B737-800 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET:40 REV:A.SDR SWAA2025100611323Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 573 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET 40 REV A.SDR SWAA2025100611563Nut Plate · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 491 INTERNAL CAVITY LEADING EDGE RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 491 INTERNAL CAVITY LEADING EDGE AT RT WING AND APPLIED PROTECTIVE TREATMENT ON FASTENERS. IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 8;SDR CALA2025090508503Drag Fitting · crackedRIGHT WING SKIN AND DRAG FITTING. A CRACK INDICATION NOTED AT HOLE NR 2 IN BOTH LAYERS. ACCOMPLISHED A REPAIR IAW ECRA 5720-03563 AND EA 757-572-13-A4083 WITH NO DEVIATIONS.SDR DALA2025090306530Bracket · crackedCRACK BRACKET TELESCOPIC DUCT OB FIXED LEADING EDGE IB SIDE LH WING. REPLACED BRACKET AND FASTENERS ON TELESCOPIC DUCT OB FIXED LEADING EDGE IB SIDE LH WING AS PER A319 SRM 51-72-11 AND A319 SRM51-42-11. (1178540).SDR DALA2025091306745Shim · migratedLEFT WING L/E I/B DRAG FITTING HAS SHIM MIGRATION AT LOCATION (1, A) FIGURE 4. AFT SIDE OF FITTING PER AD CARD #5720-01100-02A. CORRECTIVE ACTION: REPLACED L/W L/E I/B DRAG FITTING SHIM AND OVERSIZED HOLES IAW ERA 628602-14. (LP 1195921)SDR AALA202508298251Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 8 (LOWER MID) ON LH WING L=0.443 INCH, W=0.167 INCH AND D=0.002 INCH. MAINTENANCE REPLACED ATTACHE BOTL AT SLAT TRACK 8 ON LH WING.SDR AALA202508298555Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 8 (LOWER FWD) ON LH WING L=0.445 INCH, W=0.169 INCH AND D=0.001 INCH. MAINTENANCE REPLACED ATTACH BOLT AT SLAT TRACK 8 ON LH WING.SDR AALA202508294542Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 7 (LOWER BOLT) ON LH WING L=0.449 INCH, W=0.170 INCH AND D=0.002 INCH. MAINTENANCE REPLACED ATTACH BOLT AT SLAT TRACK 7 ON LH WING.SDR AALA202508298290Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 3 (LOWER BOLT) ON LH WING L: 0.450 INCH, W: 0.171 INCH, D: 0.001 INCH. MAINTENANCE REPLACED ATTACH BOLT AT SLAT TRACK 3 ON LH WING.
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