JASC 5743
Service difficulty reports · 3,097
Reports filed under 5743 · Wing, Landing Gear 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 = '5743' 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 = '5743' 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 DLL10951795Fitting · corrosionLT MLG AFT TRUNNION FITTING A HAS CORROSION ON AFT FACE OF FWD LUG. BURNISHED FACE TO REMOVE LIGHT CORROSION.SDR DLL10951914Fitting · corrodedLT GEAR FITTING FWD TRUNNION AFT BORE HAS CORROSION ON FWD FACE AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.229 TO REMOVE CORROSION. BLENDED AREAS TO REMOVE MINOR CORROSION. TREATED/PAINTED PER SRM 57-14-00.SDR DLL10951808Trunnion Fitting · corrosionLEFT GEAR FITTING AFT TRUNNION AFT BORE HAS CORROSION FWD FACE. CORR SPOT FACED .004 DEEP AND LOCALLY BLENDED AREA, REMOVED CORROSION PER SRM 57-14-00. ALL REMAINING REWORK COMPLIED WITH ON RC'S 1453/1454.SDR DLL10951791Fitting · corrodedLT GEAR FITTING AFT TRUNNION FWD BORE PITTED IN BORE. BORED LUG TO 4.7095 INCHES TO REMOVE CORROSION.SDR DLL10951790Fitting · corrosionLT GEAR FITTING FWD TRUNNION FWD BORE HAS CORROSION ON FWD/AFT SIDES AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.218 0 TO REMOVE CORROSION. BURNISHED FACES TO REMOVE PITS PER SRM 57-14-00.SDR DLL10951911Fitting · corrodedLT MLG RETRACT FITTING, CORRODED HOLES 1 THROUGH 6 TO .750 TO REMOVE CORROSION. SPOT FACED NR 2 HOLE TO .060 DEEP. HOLE ID'S ARE WITHIN LIMITS PER SRM 57-14-00. CORROSION REMOVAL IN HOLES IS OK. FUTHER REPAIR COMPLETED ON JPC 032169 TRK NR MRL465. COMPLETSDR DLL10951910Fitting · corrodedAT HMV, MLG FITTING, CORRODED HOLES 17 THROUGH 20 COMMON TO WING AT THE RETRACT FITTING ATTACH AREA ARE CORRODED. CONTINUED ON N/R 2125. REAMED HOLES 17 TO 20 TO .625 TO REMOVE CORROSION. CORROSION REMOVAL OK PER SRM 57-14-00, HFEC PER SRM 57-14-00 CK OK. SDR DLL10951752Fitting · corrodedLT MLG FITTING CORRODED ON UPPER SURFACE OF LWR RETRACT ACT ATTACHMENT. REMOVED CORROSION BY LOCAL BLEND, .020 DEEP. REMOVED CORROSION PER SRM 57-14-00, HFEC PER SRM 54-14-00 PG 809. ROTO PEENED PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED ANDSDR DLL10951751Fitting · corrosionLT MLG FITTING HOLES 1 THROUGH 6 COMMON TO WING AT RETRACT FITTING ATTACH AREA ARE CORRODED. REMOVED HOLES 1 THROUGH 6 TO .750 TO REMOVE CORROSION. CORROSION REMOVED PER 54-14-00 HFEC PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED.SDR DLL10951747Fitting · corrosionMLG FITTING, CORROSION HOLES 17 THROUGH 20 COMMON TO WING AT THE RETRACT FITTING ATTACH AREA ARE CORRODED. REAMED HOLES 17 THROUGH 20 TO .625 TO REMOVE CORROSION. CORROSION REMOVED PER SRM 51-14-00 HFEC. ROTO PEENED PER SRM 57-14-00 PG 809. CAD PLATE PER PSDR DLL10951749Fitting · corrodedLT MLG FITTING TRUNION FITTING HAS CORROSION ON FACE AT FWD ATTACH POINTS. REMOVED CORROSION PER SRM 51-21-02 MAX MATERIAL REMOVED .005 ROTO PEENED PER 51-21-00 CAD PLATE PER PS 900-3-9 PRIMED AND PAINTED.SDR DL72W951480Fitting · corrosionLMG SUPPORT BEAM OB FITTING AT REAR SPAR HAS CORROSION IN BORE OF FWD SUPPORT FITTING. REPAIRED PER SRM 57-40-00 FIG 1. FOUND AT HMV.SDR DL72W951551Attach Fitting · elongated holesDURING HMV, FOUND HOLES ELONGATED LMLG SUPPORT BEAM ATTACH FITTING. REPAIRED PER SRM 57-40 PG. 3.SDR 9505999162Fitting · corrodedDURING LINE CHECK, FOUND CORROSION AND PREVIOUS REWORK ON THE LEFT MAIN LANDING GEAR SIDE BRACE ATTACH LUG FACES. REWORKED PER EA 91-64916, SEC 1.SDR DALR950001Fitting · corrodedATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 AND AD 93-17-10 DURING THE REPLACEMENT OF THE INBOARD LEFT AND RIGHT REAR SPAR WEB AND REWORK OF THE UPPER 1.1250 INCH (2 TOTAL) AND INBOARD .6250 INCH (4 TOTAL) HOLES AT THE MLG BACKUP FITTING IWSSDR DLAR950007Fitting · corrodedATL - DURING LETTER CHECK AT DALR, THE LEFT MLG UPPER ACTUATOR ATTACH FITTING LUGS WERE FOUND CORRODED ON THE INSIDE DIAMETER. THE LUG HOLES WERE BORED OUT TO CLEAN UP CORROSION PER DL ERA 270493-14. TT, 38155 HRS. CYCLES, 18905. (X)SDR DALR950007Fitting · corrodedATL - DURING LETTER CHECK AT DALR, THE LEFT HAND MAIN LANDING GEAR UPPER ACTUATOR ATTACH FITTING LUGS WERE FOUND CORRODED ON THE INSIDE DIAMETER. THE LUG HOLES WERE BORED OUT TO CLEAN UP CORROSION PER DL ERA 270493-14. (W)SDR DLL17951469Hole · corrodedAT HMV, FOUND HOLE CORRODED/PITTED. FITTING FOR RT MLG ACT. REAMED HOLE TO .690, TURNED BUSHING TO SIZE AND CAD PLATED PER PS 900-3-9, PRIMED HOLE PER PS 900-3-6, INSTALLED BUSHING PER SRM 57-14-00.SDR DLL17951348Fitting · damagedDURING HMV, FOUND FITTING ON LT MLG DAMAGED AT LOWER HOLES 17 TO 20. REAMED HOLES TO .625 TO REMOVE DAMAGE. DID HFEC CHECK, PRIMED HOLES AND INSTALLED BUSHINGS AS PER SRM 57-11-00.SDR DLL17951294Fitting · corrodedAT HMV, FOUND FITTING CORRODED, LEFT MLG UPPER HOLES AT NR 1 TO 6 ATTACH POINT FOR RETRACT ACT FITTING. REAMED HOLES TO REMOVE CORROSION. INSTALLED BUSHING, PER SRM 57-14-00.SDR DALR950015Fittings · corrodedATL - DURING LETTER CHECK AT DALR, LEFT MLG TRUNNION ATTACH FITTINGS (FWD AND AFT) WERE FOUND WITH WEAR DAMAGE AND CORROSION ON THE FACE AND IN THE BORE OF THE FWD AND AFT LUGS. REPAIRED PER SRM 57-14-00, PAGE 803. AIRFRAME TT 38,155 HRS. CYCLES, 18905. (SDR DALR950014Fitting · corrodedATL - DURING LETTER CHECK AT DALR. THE LEFT MLG FORWARD AND AFT TRUNNION ATTACH LUGS, BOTH THE FORWARD AND AFT LUGS WERE FOUND WORN AND WITH SURFACE CORROSION ON THE FACE AND INSIDE THE BORE. REPAIRED PER SRM 57-1400, PAGES 802-803. AIRFRAME TT 38,155 HRS. SDR 95ZZZW666Support Mlg · crackedDURING C-CHECK, FOUND RT MLG SUPPORT FITTING CRACKED. REPAIRED FITTING PER DOUGLAS S/B 53-61. TOTAL CYCLES 25,289.SDR UPS202595Fwd Trunnion · corrodedWHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON RT MLG RT FWD TRUNNION FITTING INNER FACES AROUND BUSHING BORES. REPLACED PER SRM 51-30-2.SDR DLL10950854Trunnion Fitting · corrodedPAINT PEELING AND RUST ON O/B SURFACE OF MLG TRUNNION FITTING. CLEAN CORROSION PER SRM 57-14-00 FIG 804 DAMAGE FOUND AT LETTER CHECK.SDR DL757951708Skin · delaminatedAT SHOP INSPECTION, L/E SLAT PANEL WAS FOUND WITH THE TRAILING EDGE WEDGE DELAMINATED. REPLACED WEDGE PER SRM 57-43-02.SDR CKSA95008Trunnion · crackedOSC - DURING D-CHECK, FOUND APPROX 2.75 INCH LONG CRACK, LEFT MLG SUPPORT ATTACHED FITTING. REF DOUG SB 57-94, FIG 1, VIEW FF LOCATION E. REMOVED AND REPLACED LEFT MLG FITTING IAW AD 89-10-04 AND SB 57-94 AND FAA LETTER DATED 11-4-94. (W)SDR DLL16950927Act Fitting · damagedAT HMV, FOUND HOLES DAMAGED IN LMLG ACTUATOR FITTING. DRILLED HOLES 17 THROUGH 20 TO .628 TO REMOVE DAMAGE. CORROSION REMOVED. ALL REMAINING WORK DONE ON JPC 031255.SDR DLL16950926Act Fitting · corrodedAT HMV, FOUND HOLES CORRODED HOLES 1, 2, 4, 6, IN LMLG ACTUATOR FITTING CORRODED. REF TASK C-32-730-01. REAMED HOLES 1, 2, 4, 5 AND 6 TP .688. REMOVED DAMAGE AND TO FACILATATE MAINT ON HOLE NR 5, REAMED NR 3 .719 TO REMOVE DAMAGE. CORROSION REMOVED, ALL RESDR UPS202407Fitting · crackedDURING 'C' CHECK, MAINTENANCE REPORTED FORWARD SUPPORT ATTACH FITTING (WING ATTACH) IS CRACKED. REPLACED FITTING PER SRM 51-10-1, 51-30-2.SDR UPS202406Fitting · crackedDURING 'C' CHECK, MAINTENANCE REPORTED FORWARD SUPPORT ATTACH FITTING (WING ATTACH) CRACKED AND CORRODED, LEFT AND RIGHT MLG. REPLACED FITTING PER SRM 51-30-2, 51-10-1.SDR CAL950167Bracket · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN RT WING, NR 5 LEADING EDGE SLAT ACTUATOR ATTACH BOLT BRACKET. A REPAIR WAS PERFORMED IAW SRM 51-30-2 AND BOEING DRAWING 65-17276. (X)SDR DL72S954267Flap Track · corrosionTHE LEFT SIDE INBOARD TRACK FOR THE INBOARD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE, FORWARD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBOARD AND OUTBOARD SIDES OF THE TRACK. THE HOLES WERE BOTH OVERSIZED TO SDR 9502322284Beam · corrodedDURING PERIODIC CHECK, MAINTENANCE FOUND LEFT MAIN LANDING GEAR BEAM BORE CORRODED. REPAIRED PER NWA EA 22-093796.SDR 9502372284Att Fitting · corrodedDURING PERIODIC CHECK, FOUND RIGHT MAIN LANGING GEAR BEAM OUTBOARD END REAR SPAR ATTACH FITTINGS CORRODED. REPAIRED PER NWA EA 22-093797.SDR HAL95015Spar Cap Fitting · crackedHNL - DURING ACCOMPLISHMENT OF AD 84-26-01, AMENDMENT 39-4971 (VISUAL INSP MLG ATTACH FITTING) A CRACK WAS FOUND IN AN ADJACENT UPPER AUXILIARY SPAR CAP FITTING, ATTACHED TO THE RT MLG ATTACH FITTING. REPLACED RT AUXILIARY SPAR CAP FITTING. (W)SDR 9502099863Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LEFT MAIN LANDING GEAR SIDE BRACE ATTACH FITTING LUG. REPAIRED PER EA 98-094923.SDR 9501589947Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LEFT AND RIGHT MAIN LANDING GEAR ATTACH FITTINGS AT THE FIXED STRUT. REPAIRED BOTH PER EA 99-095679.SDR HAC000001Support Fitting · crackedTRUNNION SUPPORT FITTING REMOVED DUE TO CORROSION ON RIGHT WING LOWER REAR SPAR. DURING INSPECTION, A CRACK WAS FOUND IN BOLT HOLE. THE CRACK WAS 1 INCH LONG AND .3750 INCH DEEP. THE CRACK COULD HAVE BEEN CAUSED BY HARD LANDING OR FLAW IN CASTING. (X)SDR DLL16950275Fitting · rustyAT HMV, THE RIGHT MAIN GEAR FITTING AT UPPER LATERAL BRACE LUG WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 57-14-00 FIG 804.SDR DLL16950273Trunion Fitting · rustyAT HMV, THE RIGHT MAIN LANDING GEAR FWD TRUNNION ATTACH FITTING WAS FOUND CORRODED AT THE FWD TRUNNION LUG AND IN AREA OF AFT LUG. REPAIRED PER SRM 57-14-00 FIG 804.SDR DLL16950266Trunnion Fitting · rustyHMV, THE RIGHT MAIN LANDING GEAR TRUNNION FITTING WAS FOUND CORRORDED BETWEEN FWD TRUNNION LUGS. REMOVED CORROSION PER SRM 57-14-00 FIG 804.SDR DLL16950265Trunnion Fitting · rustyAT HMV, THE RIGHT MAIN LANDING GEAR TRUNION FITTING BETWEEN LATERAL BRACE LUGS ARE RUSTY. REPAIRED PER SRM 57-14-00 FIG 804.SDR DL757950671Wedge · delaminatedDURING OVERHAUL, DELAMINATION WAS DISCOVERED ON THE NR 9 SLAT WEDGE THE WEDGE WAS REPLACED PER SRM 57-43-02.SDR DL733950160Attach Fitting · crackedDURING ROUTINE INSPECTION AT HMV, THE RT WING O/B AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. THE CRACKED FITTING WILL REMAIN IN SERVICE PER S/B 737-57-1216 AND WILL BE REPAIRED PER S/B REQUIREMENTS.SDR DLL16950263Fitting · corrodedAT HMV, FOUND LMLG RETRACT ACT FITTING ATTACH STRUCTURE CORRODED IN UPPER MATING SURFACE AROUND BOLT HOLES. LOCAL BLENDED SURFACES TO REMOVE CORROSION, HFEC INSPECTED ALL SURFACES AND FOUND OK. REPAIRED PER SRM 57-14-00 PG 809.SDR IXXA9537Trunnion · crackedDURING ROUTINE C-CHECK INSPECTION, THE LT MLG TRUNNION FITTING WAS FOUND CRACKED. INSPECTION WAS ACCOMPLISHED IAW SB 57-94. THE CRACK WAS LOCATED, 8 INCHES, IN THE FORWARD LANDING GEAR ATTACH LUG. THE FITTING WAS REMOVED AND REPLACED IAW DOUGLAS INSTALLATIO
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