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 QXEA200501323Nut Plate · damagedPDX: NUT PLATES FOR RT WING PANEL 613DR HAS INSERT MISSING, 2ND NUTPLATE FROM OUTBOARD EDGE. MAINTENANCE DRILLED OFF BROKEN NUT PLATE AND RIVETED IN NEW NUT PLATE IAW Q400 SRM 51-42-05, TASK 51-42-05-330-801.SDR P5CA0501400Fitting · corrodedLEFT WING AT UPPER CHORD OF SPLICE FITTING OF WING REAR SPAR HAS CORROSION BETWEEN WS 553 AND WS 558. CORROSION BLENDED OUT IAW SRM 57-30-01. HFEC & ULTRASONIC INSPECTION OF AREA CONFIRMED REMOVAL OF CORROSION IAW NDT 06-7170 PT 6, 51-00-00 FIG 23, 12. D6-71SDR VTZA200500186Support Angle · crackedLEFT BATTERY RIB SUPPORT ANGLE LWS 48.3 IS CRACKED .25 INCH.SDR VTZA200500182Support Angle · crackedRIGHT BATTERY RIB SUPPORT ANGLE RWS 48.3 IS CRACKED .25 INCH.SDR UPS05845490Fitting · crackedRT WING FUEL TANK NR 4 ALTERNATE STA XW 408 LWR STR NR 58 END FITTING CRACKED 2" LONG. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D.SDR UPS05845489Fitting · crackedLT WING XW 408 STRINGER NR 58 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM51-1-20D AND 51-1-21.SDR UPS05845488Fitting · crackedLT WING XW 408 STRINGER NR 59 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM 51-1-20D AND 51-1-21.SDR USAA051080Support Angle · crackedRT WING T/E SUPPORT ANGLE, JUST INBOARD OF NR 6 SPOILER CRACKED. NEW PART SUPPORT ANGLE INSTALLED PER SRM 57-53-71 & 51-40-02, DEFECT SIZE: 0.050 INCH.SDR MALA050704Tab · chafedWHILE ACCOMPLISHING C1. IG1 INSPECTION FOUND LEFT INBOARD FLAP TAB HAS CHAFING MARKS AT ITS MIDDLE ATTACH POINT.SDR 2005F00097Fitting · crackedCRACK DETECTED IN WING FITTING DURING SIRM INSPECTIONSDR UPS05245437Attach Fitting · crackedINSPECTION TYPE: C, CRACK IN ZEE SECTION ATTACHED TO FRAME AT BS 1050 LBL 21. Z-SECTION REPAIRED IAW SRM 51-40-4 FIG 2.SDR 05FDEA02663Bracket · crackedLT WING BRACKET BROKEN INSIDE ACCESS PANEL 8405. REMOVED AND REPLACED BROKEN BRACKET IAW SRM 51-10-1 AND SRM 51-30-2.SDR UPS05445272Fitting · corrodedLT WING UPPER REAR SPAR SIDE OF BODY SPLICE NR 6 FASTENER HOLE FOUND CORROSION AT UPPER SPLICE FITTING APPROX 0.030" IN LENGTH RUNNING FORWARD O/B, CORROSION BLEND OUT 0.030" IN LENGTH. LEFT NR 6 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032.SDR UPS05445271Fitting · crackedBS 1241 REAR SPAR CRACK INDICATION REVEALED AT UPPER SPLICE FITTING LOWER SURFACE AT NR 6 HOLE. CRACK LENGTH 0.060". RT NR 6 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032.SDR UPS05445270Fitting · crackedRT BS 1241 WING UPPER REAR SPAR SIDE-OF-BODY KICK FITTING AREA FOUND HOLE NR 2 CRACKED AT KICK FITTING APPROX 0.060". RH NR 2 BOLT HOLE BUSHING REPAIRED AS PER EO NR B747-5740-17032.SDR 05FDEA02661Bracket · crackedCOVE PANEL BRACKET IS BROKEN ON LOWER WING PANEL BELOW NR 3 SPOILER. REMOVED AND REPLACED 3 EA BRACKET P/N 65-21658Y29, 65-21658-27, AND 65-21658Y30, AND 1 EA ROD P/N 69-17911-18 IAW SRM 51-30-2.SDR DHL2005748535Channel · brokenNR 1 SLAT ACTUATOR ROD END CHANNEL BRACKET IS BROKEN. REMOVED BROKEN ROD END CHANNEL AND BUSHINGS IAW B727 SRM 51-30-2 LOCATED AND DRILLED NEW CHANNEL P/N 65-17327-7 PO NR 5314113 IAW B727 SRM 51-40-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLESDR DHL2005748534Angle · crackedINNER WEB FWD OF NR 1 SLAT ACTUATOR ROD END IS CRACKED. CUT OUT SECTION OF WEB TO GAIN ACCESS DIM 7.75 BY 1.50 IAW B727 SRM 51-40-2. CUT CRACKED SECTION OF ANGLE IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE PO NR 9081237 .040 2024T3 2" BY 10" IAW B727 SRM 5SDR 05FDEA02577Attach Fitting · corrodedNR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REPLACED NR 7 FLAP TRACK FWD ATTACH FITTING IAW BOEING DWG 65-17357, OHM 20-50-03, MM 28-11-00.SDR ASOA05714Bracket · crackedDURING A C-CHECK IN YUL, FOUR OMEGA BRACKETS ON THE LEFT WING AT THE NR 4 FLAP HINGE, RIB 8 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED FOUR OMEGA BRACKETS ON THE LEFT WING AT THE NR 4 FLAP HINGE, RIB 8 IAW ATR 72 SRM 51-25-01. (SDR 05FDEA02166Attach Fitting · brokenRT I/B FLAP, I/B ACTUATOR AFT ATTACH FITTING BROKEN. REMOVED RT I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-01-2 STEPS A1 THRU ALL. INSTALLED NEW R/H I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-1-2. ENLARGED & REAMED FOUR HOLES IN FITTING PESDR 05FDEA02164Attach Fitting · corrodedCORROSION (27X5710-02) NR 8 FLAP TRACK FWD ATTACH FTG ON WING IS CORRODED ON I/B FACE. REPAIRED FITTING PER EA 7-5750-92237SDR 2005FA0000992Attach Angle · corrodedWING ATTACH ANGLE, CORROSION WITH LINEAR INDICATIONS. (K)SDR IXXA05RNG031SSupport Fitting · crackedDURING ROUTINE "0C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF409.664 WAS FOUND CRACKED (LONG 1.570"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-021 & EO ATI-070705. FAA FORM 8110-3 WAS ISSUED APPROSDR IXXA05RNG030SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 409.664 WAS FOUND CRACKED (LONG: 3.178"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-020 & EO ATI-070605. FAA FORM 8110-3 WAS ISSUED APPRSDR IXXA05RNG029SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 339.723 WAS FOUND CRACKED (0.703"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-019 & EO ATI-070505. FAA FORM 8110-3 WAS ISSUED APPROVING TSDR IXXA05RNG028SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 219.498 WAS FOUND CRACKED (0.177"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-018 & EO ATI-070405. FAA FORM 8110-3 WAS ISSUED APPROVINGSDR IXXA05RNG027SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2035"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-016 & EO ATI-070205. FAA FORM 8110-3 WAS ISSUED APPROVISDR IXXA05RNG026SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF219.498 WAS FOUND CRACKED (1.599"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-017 & EO ATI-070305. FAA FORM 8110-3 WAS ISSUED APPROVINGSDR IXXA05RNG025SSupport Fitting · crackedDURING ROUTINE "0C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2740"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-015 & EO ATI-070105. FAA FORM 8110-3 WAS ISSUED APPROVINSDR AWXA200500958Fitting · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, FORWARD ATTACH FITTING. CORROSION WAS REMOVED IAW BOEING 737-300 SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW BOEING 7 37-300 SRM 57-20-90-1 FIG 102. MAINTENANCE REMOVED THE RT MLG STABILSDR AWXA200500929Fitting · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE LT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE LT MLG STABILIZER BEAM IAW BOEISDR AWXA200500928Fitting · corrodedDURING C18 CHECK DISCOVERED CORROSION ON THE RT MLG STABILIZER BEAM, AFT ATTACH FITTING. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 57-20-30-1. MAINTENANCE REMOVED AND REPLACED THE AFT ATTACH FITTING ON THE RT MLG STABILIZER BEAM IAW BOEISDR DHL2005802524Fitting · crackedLT STUB WING INTERIOR FITTING CRACKED 2.000 (MAJOR REPAIR)STA XOLDO 67.750 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYINGSDR UPS05144964Angle · crackedINSPECTION TYPE: 5YR, LEFT WING INSIDE KRUGER FLAP WELL, CURVED SUPPORT STRUCTURE IS CRACKED IN RADIUS OF 2ND RIB. REMOVED & REPLACED SUPPORT STRUCTURE ANGLE IAW A300-600 SRM 51-40-00.SDR AWXA200500859Attach Angle · crackedDURING C16 CHECK DISCOVERED CRACK, 1.1 INCHES LONG, LOCATED ON ATTACH ANGLE ON BOTTOM OF LT WING, FORWARD SPAR, TERMINAL FITTING. MAINTENANCE STOP DRILLED CRACKS AND FABRICATED REPAIR DOUBLER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5712-05196-DF1. SDR 2005FA0000993Attach Angle · corrodedWING ATTACH ANGLE, CORROSION WITH LINEAR INDICATIONS. (K)SDR 2005FA0000991Attach Angle · crackedWING ATTACH ANGLE, CRACKING BETWEEN ROWS OF FASTENERS. (K)SDR USAA050811Bracket · wornCLT - Q2 - ANGLE BRACKET, 2 INCHES X 3 INCHES, WORN AND CHAFED AREA, LWR WING PANEL OB OF NR 2 FLAP TRACK. FABRICATED AND INSTALLED NEW ANGLE IAW SRM. (K)SDR 2005FA0000953Angle · corrodedUPON COMPLYING WITH EMERGENCY AD 2005-12-51 IT WAS DISCOVERED THE LT OUTER WING LOWER BOLTING ANGLE P/N 54-14030 WAS HEAVILY DAMAGED BY PITTING, FILIFORM & ESPECIALLY EXFOLIATION TYPE CORROSIONS. THIS DAMAGE WAS ONLY FOUND AFTER STRIPPING PAINT & PRIMER AWAY SDR UPS05444864Fitting · crackedINSPECTION TYPE: C, RIGHT WING UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 FASTENER HOLE FOUND CRACK AT INTERNAL SPLICE FITTING (CRACK LENGTH .25 INCH). RIGHT WING INTERNAL SPLICE FITTING BOLT HOLE NR 5 REPAIRED AS PER HX RS R57-18-35333 & UPS EO B747SDR CA051026006Attach Angle · crackedCRACK DETECTION INSPECTION AT WING ATTACHMENT ANGLES ON BOTH WINGS PER AD CF-2005-19. NO CRACK INDICATION WERE DISCOVERED ON THE WING ATTACHMENT ANGLESSDR USAA050785Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED .75 INCH, WING STATION 60.9735. FABRICATED AND INSTALLED A NEW ANGLE IAW BOEING DRAWING 65-50820-362 AND SRM 51-40-02. (M)SDR UPS05444878Fitting · crackedINSPECTION TYPE:C RIGHT WING STA 1241 UPPER REAR SPAR SIDE OF BODY SPLICE FITTING NR 4 HOLE FOUND CRACK & COR AT INTERNAL SPLICE FITTING. RIGHT WING BS 1241 BOLT HOLE NR 4 HOLE REPAIRED AS PER SB B747-5740-17032.SDR AALA20050478Fitting · corrodedAFW - LT WING REPAIR OF OUTBOARD SIDE LOAD FITTING BORE HAS CORROSION BLEND IN AN AREA OF .25 INCH BY 0.4 INCH BY .005 INCH DEEP. REPAIRED PER SRM 57 20 90 FIGURE 202 WITH THE FOLLOWING EXCEPTION. PERFORMED A LOCALIZED BLEND REPAIR.SDR DHL2005784546Bracket · crackedNR 2 LEADING EDGE ACTUATOR UPPER MOUNT IS CRACKED AT LWR INBOARD CORNER, WING STA 224. REMOVED DAMAGED MOUNT ANGLE IAW B727 SRM 51-30-2 AND FABBED NEW FROM 2024T3.063 PO 9002199 DIM 7.375 X 6.5 IAW B727 SRM 57-20-2 FIG 1. TREATED & PRIMED ANGLE IAW B727 SRM SDR DHL2005784501Mount · crackedNR 1 LEADING EDGE FLAP ACTUATOR UPPER MOUNT IS CRACKED AT LWR OUTBOARD CORNER, WING STA 304. REMOVED UPPER ACTUATOR MOUNT AND FABRICATED NEW ANGLE IAW B727 SRM 57-20-2 FIG 1,TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED NEW ANGLE ON NR 1 LEADING EDGE SDR IXXA05Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, RT WING L/E INBOARD STUB WING UPPER SURFACE SCREWS OXIDIZED, XW 257.000. REMOVED OXIDIZED SCREWS IAW DC-8 SRM 51-3-0 PAGE 1. INSTALLED NEW SCREWS ON RT L/E INBOARD STUD WING UPPER SURFACE, XW 257.000 IAW DC-8 SRM 51-3-0 PAGSDR DXTA200500700Attach Bracket · wornYOKE HAS 1-2" DEAD SPOT IN PITCH IN BOTH MANUAL AND AUTO PILOT MODES. FOUND PITCH FEEL ELEVATOR CONTROL BRACKETS ATTACHING HOLE WORN AND ELONGATED, REPLACED BRACKET AND ACCOMPLISHED REPAIR IAW REPAIR DEFINITION S-750-0124/04RD FROM CESSNA DATED APRIL 29, 2005SDR USAA050510Support Fitting · crackedCLT - FOUND SUPPORT FITTING CRACKED .3750 INCH, RT AFT SPAR WBL 142. REPLACED FITTING IAW EO 5702V054. (M)
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