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 IPXA2021100674654Doubler · gougedINSPECTION TYPE:3CR/H WING FIXED L/E UPPER EXTERNAL REPAIR DOUBLER IS GOUGED AT STA. XIS= 247.028.REMOVED, FABRICATED AND REPLACED R/H WING FIXED L/E UPPER EXTERNAL REPAIR DOUBLER AT STA. XIS= 247.028 IAW SRM 57-40-02 REPAIR 8 FIG. 201. (MAJOR)SDR SWAA2021092219693Support Fitting · corrodedLT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD (#4);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14SDR SWAA2021092219694Fitting · corrodedLT MLG FWD TRUNNION SUPPORT FITTING; LOWER OTBD (#3);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14SDR SWAA2021092220592Fitting · corrodedLT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD (#4);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14SDR SWAA2021092220593Fitting · corrodedLT MLG FWD TRUNNION SUPPORT FITTING; LOWER OTBD (#3);INNER FACE HAS EVIDENCE OF CORROSION. ; / [01] REPAIRED PER. EA 1-A57-3246 REV. 14SDR DALA2021091005341Fitting · crackedSHIP 5642 WHILE WORKING AA27-01030-01,FOUND CRACK ON LOWER FITTING OF ATTACHMENT LUG ON AILERON TRIM ACTUATOR BOX SUPPORT ASSY. CRACK RUNS FWD AND AFT AND IS THROUGH ENTIRE THICKNESS OF MATERIAL FOR LOWER BUSHING. CORRECTIVE ACTION: REMOVED/REPLACED SUPPORT BOSDR SWIA2021091561082Bolt · wornRH AILERON CONTROL SYSTEM INBOARD PCU FAILED BACKLASH FUNCTIONAL TEST. (C-CHECK RO 9/14/21) / REMOVED AND REPLACED RH IB PCU TOGGLE LINK TO AILERON SURFACE BOLT, BUSHING, AND WASHERS, AND RE-CHECKED RH AILERON IB PCU BACKLASH. BACKLASH IS WITHIN SPECS. ASSETSDR V0XD20210903002Bracket · crackedRH SLAT TRACK 1-3 HOUSING AFT BRACKET IS CRACKED. PERFORMED REMOVAL OF OLD BRACKET AND COMPLETED REPAIR IAW BOMBARDIER REO 670-57-42-577 REV -- DATED 2016-12-02.SDR IPXA2021090473550Bracket · corrodedINSPECTION TYPE:3CRT WING O/B FLAP I/B HINGE BRACKET ASSY. HOLE #7 IS CORRODED.REPAIRED CORRODED RT WING O/B FLAP I/B HINGE BRACKET ASSY. XW 486.403 HOLE #7 IAW VT-SAA EA 011-5740-01-A9326 REV. IR AND UPS EO MD11-5740-81500-A. (MINOR)SDR SIMA20210822005Spar · crackedRH WINGLET FWD SPAR IS CRACKED.-C/A-COMPLETE:SEE CORRECTIVE ACTION OF RH WINGLET FWD SPAR CRACK ON ENVOY EO-EJ-5700-004 WING TIP INBOARD SPAR I WITH REINFORCED SPAR SECTIONSDR HYIA20210817001Attach Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND UPPER FORWARD WING ATTACH FITTING. IT IS LOCATED ON THE BOTTOM FACE OF THE UPPER HORIZONTAL LEG OF THE FITTING AND MEASURES APPROXIMATELY .555 INCHES LONG, .300 INCHES WIDE, AND .0SDR IPXA2021081472731Bracket · crackedINSPECTION TYPE:A300RH WING SUPPORT BRACKET INSIDE OF PANEL 612DB BROKENREMOVED AND REPLACED BRACKET IAW A300 SRM 51-40-21SDR FDEA202108011910Fitting · crackedJUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 LH SIDE FRAME LOCATION O/B ROW FWD FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 LH SIDE FRAME LOCATION O/B ROW FWD CRACKED FASTENSDR IPXA2021080272291Fitting · crackedINSPECTION TYPE:A300LH WING UPPER FUSELAGE FR46.5 BRACKET SUPPORT CRACKED.REMOVED AND REPLACED BRACKET FITTING IAW A300 SRM 51-40-21. A300-5310-18290.SDR U2RA2021101100062Bushing · gougedUPON REMOVAL OF THE #5 T/E FLAP TRACK, FOUND FWD. MOUNT FITTING BOLT HOLE INNER BUSHINGS GOUGED.
ACCOMPLISHED MAJOR REPAIR OF THE R/H WING #5 FLAP TRACK SUPPORT FITTING P/N 65B 11592-24 GOUGE AT WSTA 487.0 IAW VT-SAA EA 747-5751-56-A9245 REV. I/R. 8110-3 APPSDR IPXA2021072371996Bracket · crackedINSPECTION TYPE:A300LT WING KRUEGER FLAP BOX PANEL SUPPORT STRUCTURE HAS 2EA CRACKED BRACKETSREMOVED AND REPLACED 2EA BRACKETS IAW SRM 51-26-10 AND 53-15-63 FIG 1 ITEM 255SDR FDEA202107121752Attach Angle · crackedR/W L/E STRUCTURE FSS 560 ATTACH ANGLE IS CRACKED REMOVED AND REPLACED ANGLE PER DWG #114N2034 REV CSDR SWIA2021090760793Nut · corrodedCORRODED HARDWARE ON R/H FLIGHT SPOILER, INBD HINGE NUT (1) AND KEEEPER PLATE BOLTS (2), CENTER HINGES INBD AND OTBD NUTS (2), AND OTBD HINGE NUT (1 (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON R/H FLIGHT SPOILER, INBD HINGE NUT (1) AND KSDR SWIA2021090760792Nut · corrodedCORRODED HARDWARE ON R/H SPOILERON, INBD HINGE NUT (1) AND KEEPER PLATE BOLTS (4), CENTER HINGES INBD AND OTBD NUTS ONLY (2), AND OTBD HINGE NUT (1) AND KEEPER PLATE BOLTS (4) (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON R/H SPOILERON, SDR IPXA2021072872207Bracket · crackedINSPECTION TYPE:SEGLH WING RIB 16 INTERCOSTAL BRACKET BETWEEN SPOILER 4 AND 5 IS CRACKED.REMOVED CRACKED INTERCOSTAL AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-21SDR SWIA2021090760791Bolt · corrodedCORRODED HARDWARE ON L/H INBD GROUND SPOILER, CENTER HINGE LINK ASSEMBLY LOWER ATTACH BOLT AND NUT. (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON L/H INBD GROUND SPOILER, CENTER HINGE LINK ASSEMBLY LOWER ATTACH BOLT AND NUTIAW CRJ-200 AMM SDR SWIA2021090760790Nut · corrodedCORRODED HARDWARE ON L/H OTBD GROUND SPOILER OTBD HINGE NUT(1), CENTER HINGE NUT (1), AND INBD HINGE NUT (1). (C-CHECK RO 9/3/21) REMOVED AND REPLCED HARDWARE IAW CRJ 200 AMM 27-65-01-400-801, ALL CHECKS PASS. REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202160789Bolt · corrodedCORRODED HARDWARE ON L/H FLIGHT SPOILER OTBD HINGE NUT (1), OTBD CENTER HINGE NUT(1), AND INBD HINGE NUT(1) AND STOPPER BRACKET BOLTS (2) . (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON L/H FLIGHT SPOILER OTBD HINGE NUT (1), OTBD CENTER HISDR SWIA2021090760788Bolt · corrodedCORRODED HARDWARE ON L/H SPOILERON OTBD HINGE NUT, AND STOPPER BRACKET BOLTS(4), CENTER HINGES INBD AND OTBD NUTS (2), AND INBD HINGE NUT AND STOPPER BRACKET BOLTS (4). (C-CHECK RO 9/3/21) REMOVED AND REPLACED CORRODED HARDWARE ON L/H SPOILERON OTBD HINGSDR SWAA2021080990339Fitting · crackedR/W FIXED T/E DEFLECTION CONTROL RIB PANEL VERTICAL SEAL FITTING CRACKED O/B SIDE UPPER MKD DOT ; / [01] REMOVED AND REPLACED RIGHT WING FIXED T/E DEFLECTION CONTROL RIB PANEL VERTICAL SEAL FITTING O/B UPPER SIDE IAW B 737-7 SRM 51-40-02-0G-0; [02] VERIFIED STSDR IPXA2021070971464Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E LOWER STRINGER EXISTING REPAIR DOUBLER IS CRACKED AT STA. XOS. 906.5607.REMOVED AND REPLACED CRACKED R/H WING FIXED L/E LOWER STRINGER REPAIR DOUBLER AT STA. XOS. 906.5607 IAW SRM 57-40-03 REPAIR 1 FIG. 201. (MAJOR)SDR SWAA2021071989205Attach Bracket · crackedL/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANE LOWER WEB O/B ATTACHED RACKET CRACKED AT FASTENER TAIL MKD DOT ; / [01] REMOVED AND REPLACED CLIP AT L/W REAR SPAR B737-700 SRM 51-40-02-0G -0; [02] CERTIFIED REPLACED CLIP INSTALLATION; [03] VERIFIED INSTALLSDR SWIA2021090760780Bolt · corrodedR/H ELEVATOR POSITION TRANSMITTER LINK HARDWARE IS CORRODED. (ALL LOCATIONS) (C-CHECK RO 9/3/21) REMOVED AND REPLACED RIGHT ELEVATOR POSITION TRANSMITTER LINK HARDWARES IAW CRJ 200 AMM TASK 27-34-01-000/400-801. OP TEST OF RH POSITION TRANSMITTER GOOD. SDR SWIA2021090760779Nut · corrodedR/H ELEVATOR FLUTTER DAMPER ATTACHING HARDWARE (NUTS) AT ELEVATOR ARE CORRODED. (C-CHECK RO 9/3/21) DUPLICATE WRITE UP, REF CAMP 22978663 FOR CORRECTIVE ACTIONSDR IPXA2021070971463Stringer · crackedINSPECTION TYPE:2CR/H WING FIXED L/E UPPER STRINGER IS CRACKED AT STA. XOS. 908.REPAIRED CRACKED R/H WING FIXED L/E UPPER STRINGER BETWEEN STA. XOS. 901.5 TO 912.0 IAW SRM 57-40-03 REPAIR 2 FIG. 202. (MAJOR)SDR FDEA202106251590Attach Fitting · crackedCHECK FOUND RH WING OUTBOARD DRAG FITTING NO. 4# FASTENER HOLE CRACKED REPLACED THE RH WING OUTBOARD DRAG FITTING PER EA:F-5740-T0361981 P1, EA TITLE: WINGS - ATTACH FITTINGS - CRACK FINDING IN RH WING DRAG FITTING NO.4# FASTENER HOLE, THIS IS CAT B REPAISDR V0XD20210701003Bracket · crackedL/H SLAT TRACK BOX BRACKET IS CRACKED AT WELD #3. CORRECTIVE ACTION: REPAIRED L/H SLAT TRACK BOX BRACKET BY CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING A NEW BRACKET IAW BOMBARDIER REO 670-57-42-577 REV. -- DATED 2016-12-02 (PNS- 670-57-42-577-1,-3,-5,-7 SDR IPXA2021070971465Skin · gougedINSPECTION TYPE:2CL/H WING FIXED L/E UPPER SKIN IS GOUGED BETWEEN STA. XOS. 1187 TO 1191.REPAIRED GOUGED L/H WING FIXED L/E UPPER SKIN BETWEEN STA. XOS. 1187 TO 1191 IAW SRM 57-40-01 REPAIR 16. (MAJOR)SDR SWIA2021090760805Bolt · corrodedALL MOUNTING HARDWARE ON RH FLIGHT SPOILER IS CORRODED (C-CHECK RO 8/29/2021) DUPLICATE WRITE UP, REF CAMP 23100770 FOR CORRECTIVE ACTION.SDR SWIA2021090760802Bolt · corrodedALL MOUNTING HARDWARE ON RH O/B GROUND SPOILER IS CORRODED (C-CHECK RO 8/29/2021) REMOVED AND REPLACED MOUNTING HARDWARE ON RH O/B GROUND SPOILER IAW CRJ-200 AMM 27-65-01-000/400-801SDR SWIA2021090760800Nut · corrodedALL MOUNTING HARDWARE ON LH SPOILERON IS CORRODED (C-CHECK RO 8/29/2021) REMOVED AND REPLACED HARDWARE ON L/H SPOILERON IAW CRJ-200 AMM 27-64-01-000/400-801SDR SWIA2021090760782Bolt · corrodedLH FLIGHT SPOILER PCUS LOWER ATTACHING HARDWARE IS CORRODED (C-CHECK RO 8/29/2021) REMOVED AND REPLACED LH FLIGHT SPOILER PCUS LOWER ATTACHING HARDWARE IAW CRJ-200 AMM 27-62-01-000/400-801SDR SWIA2021090760781Bolt · corrodedLH SPOILERON I/B AND O/B PCUS LOWER ATTACHING HARDWARE IS CORRODED (C-CHECK RO 8/29/2021) REMOVED AND REPLACED HARDWARE IAW CRJ 200 AMM 27-62-01-400-801, ALL REQUIRED CHECKS PASS, REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA2021090760778Bolt · corrodedRH SPOILERON I/B PCU LOWER ATTACHING HARDWARE IS CORRODED (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH SPOILERON I/B PCU LOWER ATTACHING HARDWARE IAW CRJ-200 AMM 27-62-01-000/400-801SDR SWIA2021090760777Nut · corrodedRH O/B GROUND SPOILER ACTUATOR ATTACHING HARDWARE IS CORRODED (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH O/B GROUND SPOILER ACTUATOR ATTACHING HARDWARE IAW CRJ-200 AMM 27-63-01-000/400-801SDR SWIA2021090760775Bolt · corrodedRH I/B GROUND SPOILER ACTUATOR LINK LOWER ATTACHING HARDWARE IS CORRODED (C-CHECK RO 8/29/2021) REMOVED AND REPLACED RH I/B GROUND SPOILER ACTUATOR LINK LOWER ATTACHING HARDWARE IAW CRJ-200 AMM 27-63-01-000/400-801SDR AALA202106238458Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORRODED AREA AT STA 10729 TO 11198 AND RIB 20 TO RIB 21 ON BOLT. REMOVED AND REPLACED BOLT REF A319 AMM 27-84-66-400-002.SDR V0XD20210609001Bracket · crackedL/H #3 SLAT #1 SLAT BOX SUPPORT CRACKED INSIDE FUEL TANK. CORRECTIVE ACTION: REMOVED CRACKED BRACKET, FABRICATED AND INSTALLED A NEW BRACKET(CC670-12992) IAW BOMBARDIER DRAWING # CC670-12992, 51-21-11, 51-25-06 AND CRJ 900 SRM 51-42-02SDR SWIA2021073059849Attach Fitting · corroded* LH FLIGHT SPOILER OTBD PCU ATTACH HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH FLIGHT SPOILER OTBD PCU ATTACH HARDWARE IAW CRJ-200 AMM 27-62-01-000-801 AND 27-62-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR SDR SWAA2021061577003Attach Angle · crackedDOT 45-005; PANEL 651FB OUTBOARD ATTACH ANGLE; FORWARD ATTACH POINT; ATTACH BRACKET COMMON TO WING IS CRACKED IN HALF. ; / REMOVED AND REPLACED PANEL 651FB OUTBOARD ATTACH ANGLE COMMON TO WING WITH P/N 115A5552-2 A52333 IAW SRM 51-40-02-0G-0; VERIFIED ITEM 1.<SDR SWAA2021061576678Attach Angle · crackedDOT 45-002; RH RIB DEFLECTOR; INBOARD ATTACH ANGLE IS CRACKED AT LOWER FASTENER HOLE COMMON TO RIB DEFLECTOR. ; / REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0 FIGURE 8. VERIFIED NEW CLIP P/N115A6260-2 TAG# 52109 IAW DWG 115A6200 REV .B VERIFIED STEP 2 IS COMPLESDR CALA2021052400710Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. N/ R 6205887. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL.15.04 IAW B737-700. SRM. 51-60.02 AND SWG 111A2000. DATA WAS TRANSCRIB ED FROM N/R 6205887, WORK ACCOMPLISHED BY MECHANIC V901SDR SWIA2021082060609Bolt · corrodedLEFT WING, OUTBOARD FLAP HINGE WS. 178.00 SUPPORT FITTING ( FWD ) HAS BOLTS CORRODED. (C-CHECK RO 8/19/2021) REMOVED AND REPLACED L/H WING O/B FLAP HINGE BOX FWD FITTING FWD BOLT'S AT WING STATION 178.00 REF. CRJ 700 AMM 57-54-02 AND ACCOMPLISHED LEASDR IPXA2021060970347Bracket · crackedINSPECTION TYPE:A300RH WING INBD FIXED LE HAS A CRACKED STRUCTURAL ANGLE BRACKET LOCATED AT OUTB EDGE OF KRUGER FLAP BOX CUTOUT AREA AT LWR CORNER OF RIBREMOVE AND REPLACED IAW SRM 51-40-21SDR SWAA2021052670946Attach Angle · crackedLEFT WING T/E I/B OF DEFLECTION CONTROL RIB LOWER WEB ATTACH ANGLE CRACKED. REMOVED AND REPLACED LT WING T/E I/B OF DEFLECTION RIB LOWER WEB ATTACH ANGLE P/N 115A2953-1 IAW SRM 51-40-02 AND AIPC 57-50-00-25.
Back to JASC 5740