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 SWI2023F00456Unknown · corrodedAFTER REMOVAL OF PANEL 542AZ FOUND THE FWD ATTACH ANGLE TO BE CORRODED (C-CHECK RO 11/4/2023) REMOVED CORROSION ON PANEL 542AZ - FWD ATTACH ANGLE AND FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 57-22-32-101-001-A01. REPLACED WITH NEW SUPPORT ANGLE PN CC670-1SDR SWAA2023101397002Nut Plate · corrodedCORROSION OUTBOARD FRONT SPAR LOWER ATTACH RAIL NUTPLATE LOCATED AT OFSS 449 AT LT WING 2023-550126<[01] REPLACED OUTBOARD FRONT SPAR LOWER ATTACH RAIL NUTPLATE LOCATED AT OFSS 449 AT LT WING IAW B737-800 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9.;[02] RESDR YENA2023090101028Unknown · unknownDURING HEAVY MAINTENANCE: CRACK ON RH WING FIXED LEADING EDGE BTW RIB 19 AND RB20. SLAT TRACK # 5 CUTOUT; REF TOMX WO 2313 NR # 00024 RH WING FIXED LEADING EDGE BTW RIB 19 AND RB20. SLAT TRACK # 5 CUTOUT WAS REPAIRED PER EMB-190 SRM 57-49-01 REPAIR 5.SDR YENA2023090101019Unknown · unknownDURING HEAVY MAINTENANCE: WEAR AND BARE SKIN FOUND ON LH WING FIXED LEADING EDGE BTW RIBS 10 AND 11; WEAR AND BARE SKIN ON LH WING L/E FIXED BTW RIB 10 AND 11 WAS REPAIRED PER ETD 2023-190-019820 REV B. AND EC# E23-737-01 REFERENCE TOMX NRC# 00291 FOR ALL WORKSDR YENA2023090101013Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / LH WING / BIRD STRIKE STRUCTURE ASSY / SKIN / RIB 10 TO RIB 11 / WEAR DAMAGE – PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR SWAA2023082994111Attach Bracket · crackedRH WING TRAILING EDGE PANEL 661AB UPPER SUPPORT ROD ATTACH BRACKET IS CRACKED AT LOWER RADIUS.<[01] REPAIRED PER EA 23-157-02632SDR SWAA2023082994114Attach Bracket · crackedRH WING T/E PANEL 661AB AFT ATTACH CHANNEL SERRATED ATTACH BRACKET JUST OUTBOARD OF 120 DEGREE GEARBOX IS CRACKED IN HALF.<[01] REMOVED AND REPLACED RH WING T/E PANEL 661AB AFT ATTACH CHANNEL SERRATED ATTACH BRACKET IAW SRM 51-40-02SDR HNAA2023091800324Unknown · unknownE992717 RH WING UPPER WING TIP ATTACHMENT FLANGE HAS AN ELONGATED NUTPLATE HOLE. : RAR R/H WING UPPER WING TIP RIB IAW EMB 145 SRM 51-40-02.SDR SWAA2023090790526Attach Angle · crackedRT WING DEFLECTION CONTROL RIB TO UPPER T/E PANEL SUPPORT ANGLE ATTACH CLIP IS CRACKED.<[01] REMOVED DAMAGED CLIP FOR REPLACEMENT; LOCATED; AND DRILLED PER SRM 51-40-02 AND SRM 51-40-05.;[02] REMOVED AND REPLACED RT WING DEFLECTION CONTROL RIB TO UPPER T/E PANSDR V0XD20230818001Fitting · gougedGOUGE IN RH MFS MACHINED FITTING AT WS231.23. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR IAW OLIVER WYMAN CAVOK EA 23-C7-57-0976 REV. B PART III. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE RETURN TO SERVICE DATE FOR THE SECTION III REPAIR IAW AC 120-SDR DALA2023081506657Unknown · unknownSHIP 0667 MIGRATED SHIM ON INBD WING ATTACH FITTING-STRUT AT WSTA 280 RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00470: PERMANENT REPAIR WAS PERFORMED ON MIGRATED SHIM ON INBD WING ATTACH FITTING-STRUT AT WSTA 280 RH WING PER ER/A 610262-14. (2914883)SDR DALA2023081406610Unknown · unknownSHIP 0667 RH WING / ATTACH FITTINGS / NACELLE SUPPORT / INBOARD SIDE-LOAD FITTING / OUTBOARD HALF, WSTA 280 AT FRONT SPAR / MIGRATED SHIM. CORRECTIVE ACTION: REF ERA 610262-14. (2911033)SDR NACA2023080900003Unknown · unknownLH WING #2 SLAT DEICING DUCT SUPPORT BRACKET CORRODED AT FSS419. REPLACED DAMAGED PARTS AT LH WING #2 SLAT FSS 419 PN# 652627C5U89 IAW B737 SRM 51-40-02SDR DALA2023081006524Unknown · unknownSHIP 690 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE # 3 SCRATCHES ON SKIN AND FITTING ALL AROUND; HOLE # 7 CORROSION ON FITTING BTW 6 AND 7 O CLOCK POSITION. ; HOLE # 8 SCRATCHES ON SKIN AND FITTING ALLSDR SWI2023F00397Unknown · scratched*TOOL MARKS NOTED ON L/H WING MOUNTING LUG ON INBD SIDE FOR CENTER OTBD FLAP HINGE BOX @WS220 (MARKED), MX#26956366 (C-CHECK RO 10/4/2023) REPAIRED L/H WING MOUNTING LUG ON INBD SIDE FOR CENTER OTBD FLAP HINGE BOX @WS220 REF-CRJ-700 REO 670-57-21-953 REV -SDR SWAA2023073183469Attach Bracket · crackedLEFT WING UPPER AFT I/B ACCESS PANEL SUPPORT BEAM FWD ATTACH BRACKET CRACKED. (Z BRACKET)<[01] R&R LEFT WING UPPER AFT I/B ACCESS PANEL SUPPORT BEAM FWD ATTACH BRACKET IN REF TO SOPM 20-50-18.SDR SWAA2023073183470Attach Bracket · crackedRIGHT WING UPPER AFT I/B ACCESS PANEL SUPPORT BEAM FWD ATTACH BRACKET CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RIGHT WING UPPER AFT I/B ACCESS PANEL SUPPORT BEAM FWD ATTACH BRACKET PER SRM 51-40-02.SDR AALA202307269720Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR DALA2023072506008Unknown · unknownSHIP 3355 CORROSION ON NUT ON ANCHORAGE BEARING MLG LH. CORRECTIVE ACTION: REF ER/A 610135-14. (2877871)SDR DALA2023071705753Unknown · unknownSHIP 3277 RIGHT MAIN LANDING GEAR - RETRACT ACTUATOR ANCHORAGE FITTING HAS PITTING CORROSION AT BEARING MATING SURFACE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-26-13. (2866453)SDR DALA2023071705754Unknown · unknownSHIP 3277 LEFT MAIN LANDING GEAR - RETRACT ACTUATOR ANCHORAGE FITTING HAS PITTING CORROSION AT BEARING MATING SURFACE. CORRECTIVE ACTION: COMPLIED WITH A320 SRM 57-26-13. (2866445)SDR DALA2023070705490Unknown · unknownSHIP 3248 A320/WINGS/LH ANCHORAGE FTG/LUG CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 605165-14AD REV A. (2852490)SDR SWAA2023072073668Angle · crackedL/H WING FWD BOOST POMP AREA UPPER ANGLE CRACK<[01] REMOVED AND REPLACED DAMAGE ANGLE UPPER OF BOOST POMP ;PER REF. SRM 51-40-02-0G-0 AND DRAWING # 112A2004;[02] VERIFIED REMOVAL AND REPLACEMENT OF UPPER ANGLE OF BOOST PUMPSDR FDEA202306261109Attach Angle · corrodedL.WING L/E #3 SLAT IS CORRODED ON THE LOWER ATTACH ANGLE FOR COVE SKIN.. REMOVED AND REPLACE #3 SLAT ASSY ON FEDEX N/R N00374 AND HAECO N/R 22374. PER B757 AMM 27-81-02-4.SDR SWAA2023081459829Bracket · crackedR/W REAR SPAR T/E DEFLECTOR CONTROL RIB PANEL LOWER HORIZONTAL BULB SEAL RETAINER O/B END SUPPORT BRACKET CRACKED @ FASTENER'S TAIL MKD DOT<[01] REMOVED AS REPLACED CLIP PN 115A6260-2 AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR DALA2023111609473Unknown · unknownSHIP 6705 B757 / WINGS / UPPER SURFACE / LH FWD DRAG FITTING, HOLE LOCATION #2 / CRACK REPAIR. CORRECTIVE ACTION: REF ERA 577692-14AD. (2806894)SDR KCSA202305301061Fitting · damagedLH WING OB AILERON #5 WS 1548 HINGE TUB FITTING DAMAGEDSDR SWAA2023061353378Bracket · brokenLT WING I/B OF NACELLE STRUT - FRONT SPAR AT IFSS 192 PNEUMATIC BLEED SUPPLY DUCT SUPPORT BRACKET AND CLAMP IS BROKEN.<[01] INSTALLED PNEUMATIC BLEED SUPPLY DUCT SUPPORT BRACKET AND CLAMP FROM LT WING I/B OF NACELLE STRUT - FRONT SPAR AT IFSS 192 PER AMM 36-13SDR SWAA2023062051105Bracket · elongatedELONGATED HOLE LEADING EDGE BRACKET LOC. IFSS 83 AT LT WING 2023-334518<[01] REPLACED BRACKET LOCATED ON LEADING EDGE IFSS 83 AT LT WING IAW B737-700 51-40-02; 5-10-02 ITEM 9 AND 212A1901 SHEET: 3; REV.: ?;[02] CORRECTED STEP 1 <BR>REPLACED BRACKET LOCATED ON SDR KCSA202305221053Attach Fitting · damagedLH WING OB AILERON #3 ATTACH FITTING AT WS 1423 HAS DAMAGED TUB FITTINGSDR KCSA202305221051Attach Fitting · damagedLH WING OB AILERON #3 ATTACH FITTING AT WS 1423 HAS DAMAGED UPPER CHORDSDR SWAA2023061248560Web · corrodedCORROSION WEB INDICATOR FUEL LOCATED LEADING EDGE INTERNAL CAVITY ACCESS PANEL 621GB AT RT WING 2023-311341<[01] REPLACED REFUEL STATION PANEL IAW B737-700 AMM 28-41-61. TEST OK. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP: REPLACED WEB REFUEL STATION PASDR YENA2023051800535Unknown · unknownDURING HEAVY MAINTENANCE: R/H WING LEADING EDGE SKIN AT RIB 17 HAS WEAR AND A CRACK; THIS HAS BEEN ACCOMPLISHED BY EC E-23-368-01. A/C IS OK FOR SVC.SDR YENA2023051600521Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / RH WING / LEADING EDGE SKIN AT RIB 17 / WEAR AND CRACK - PERMANENT REPAIR. ( CONSIDERED AS A MAJOR REPAIR)SDR SWAA2023061447827Bracket · elongatedELONGATED HOLE INTERNAL CAVITY SUPPORT BRACKET INBOARD LEADING EDGE AT RT WING 2023-310566<[01] REPLACED BRACKET INBOARD LEADING-EDGE AT RT WING I.A.W. B737-700 SRM 51-40-02-0G-0;[02] TASK COMPLETEDSDR HALA2023051100175Unknown · unknownSHIP 393 DURING CCK AT SIAEC (SIN), THE LHW RIB 6 FITTING FWD AND AFT BORES WERE FOUND CORRODED. NEW BUSHES WERE MANUFACTURED AND INSTALLED. THIS WAS COMPLETED IAW REFERENCE REPAIR INSTRUCTIONS (R575-58471 ISSUE E)SDR HALA2023051100174Unknown · unknownDURING C CK, THE RHW RIB 6 FITTING FWD LUG WAS FOUND CORRODED. RH WING MLG RIB 6 FWD LUG, FWD SPT FACE FOUND CORROSION BEYOND WORK CARD, TO CARRY OUT CORROSION REMOVAL. CORRECTIVE ACTION: NEW OVERSIZE BUSHES WERE MANUFACTURED AND INSTALLED IN ACCORDANCE WITH RSDR SWAA2023061547148Angle · crackedCRACK ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WING 2023-310499<[01] REPLACED ANGLE LOCATE ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT LT WIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWSDR SWAA2023051946012Attach Angle · crackedCRACK FOUND ON ATTACH ANGLE STA 663 AT LBL 8 (WL 167)<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTQ8QOOKVEM5 FOR REPAIR;[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2023051946004Angle · crackedDOT A24-22 LH WING I/B L/E STRUCTURE / SUPPORT RIB ANGLE FOR PANEL 195AL IS CRACKED. MARKED<[01] STARTED REMOVAL OF SUPPORT RIB ANGLE FOR PANEL 195AL I.A.W. SRM 51-40-02-0G-0;[02] C/W;[03] C/W;[04] AUDIT CWSDR IPXA2023050493120Fitting · crackedINSPECTION TYPE:1C*MAJOR REPAIR* AFT CARGO FITTING AT FR54, -Y1959 CRACKED.REMOVED AND REPLACED FITTING IAW SRM 51-40-21SDR AALA202307178543Anchor Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR ANCHORAGE FITTING LOWER AND UPPER AREA OF BUSHING BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND 3. REPAIRED ANCHORAGE FITING PER EA 344928SDR YENA2023042000417Unknown · unknownDURING HEAVY MAINTENANCE: WEAR ON LH WING LEADING EDGE AT WING ROOT UPPER AREA; REF AEROMAN NRC 2023-170674 WO# 2023-3/1 PERFORMED PERMANENT REPAIR IAW 57-0116-23 AND EC A23-288-01 CAT A REPAIR.SDR SWAA2023042028554Angle · cracked(A-204 DOT 02); RH WING L/E ATTACH ANGLE CRACKED AT FASTENER HOLE; STA 500D; STR. 19R; 6' OUTBOARD OF FUSELAGE SKIN.<[01] VERIFIED ITEM 1 OF STEPS 1 - 3;[02] OK TO APPLY TOP COAT;[03] APPLIED TOP COAT FINISH TO ATTACH ANGLE I.A.W MM 51-21-99-300-901;[04] VERIFSDR ASAA2023041143034Skin · crackedLH WING L/E SKIN 116A4410 HAS 17 EA HI-LOKS PULLING THROUGH THE SKIN AT THE OB CORNER OF THESKIN DIRECTLY IB OF #1 PYLON ON THE UPPER SURFACE. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS REPAIRED IAW B737-900 SRM 57-41-01-2R-3.SDR DALA2023040302540Unknown · unknownSHIP 3354 CORROSION FWD PINTLE PIN THREAD NUT ON RH MAIN LANDING GEAR. CORRECTIVE ACTION: COMPLETED WITH ER/A 606743-14 REV ORIGINAL MATCHES WITH ALL STEPS ON PRI REV 0. IT HAS BEEN VALIDATED TO PERFORMED PERMANENT REPAIR INSTRUCTIONS ON FWD PINTLE PIN THREAD SDR SWAA2023050521715Fairing · crackedCRACK FLAP SUPPORT FAIRING 644BB AT RT WING 2023-212746<[01] TOOL USED CALIPER P/N: 500-197-30 S/N: B20189526 DUE DATE: 20 DEC 23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 23/JAN/24;[03] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18185SDR UIEA2023032700283Unknown · unknownLH WING, SLAT #1 SURFACE INNER, UPPER WITH EVIDENCE OF CORROSION.(<P>SLAT #1 SURFACE INNER, UPPER WAS REPAIRED IAW SRM 57-43-02-2R-1 REPAIR 1 FIG 201 SHEET 2-3 PAGE 1-3 AND SRM 51-70-10-2R-4 REP 4. REV 121 DEC15/2022 </P>)SDR SWAA2023041716206Strap · corrodedCORROSION LEADING EDGE LOWER STRAP LOCATED OFSS 410 AT RT WING 2023-185369<[01] TOOL USED; CALIPER; PN: 700-113-10; SN: 0033170; DUE DATE: 24-OCT-23.;[02] TOOL USED; CALIPER; PN: 700-113-10; SN: 0033170; DUE DATE: 24-OCT-23.;[03] TOOL USED: EDDY CURRENT FLAW DSDR YENA2023031400237None · noneDURING HEAVY MAINTENANCE: CRACK ON FIXED LEADING EDGE BTW RIB 19/20 AT RH WING; REF TOMX WO#2162 NR 00013 FOR WORK PERFORMED FIXED LE BTW RIB 19/20 AT RH WING WAS REPAIRED PER EMB190 SRM 57-49-01 REPAIR 51P SDR REQUIRED.
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