JASC 5742
Service difficulty reports · 258
Reports filed under 5742 · Wing, Nacelle/Pylon 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 = '5742' 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 = '5742' 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 LR7A06176Fitting · damagedDURING SCHEDULED B 1 CHECK PER JOB CARD HSP5785, FOUND NR 4 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP INBOARD FITTING BOLT HOLES OVERSIZED AT RT OWS162.8. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-086.SDR LR7A06175Fitting · crackedDURING SCHEDULED B 1 CHECK PER JOB CARD HSP57131, FOUND NR 3 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP OUTBOARD FITTING CRACKED AT CWS178.8. REPLACED FITTING IAW LOCKHEED DWG 371232 AND LAC MEA 382-57-06-087. NR 1105SDR LR7A06174Fitting · damagedDURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE OUTBOARD TRUSS MOUNT UPPER RIB CAP OUTBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS197.2. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-086.SDR LR7A06173Fitting · damagedDURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE OUTBOARD TRUSS MOUNT UPPER RIB CAP INBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS197.2. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-086.SDR LR7A06172Fitting · damagedDURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP OUTBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS162.8. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-042. NR 1101.SDR LR7A06171Fitting · damagedDURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP INBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS162.8. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-042.SDR DL76S060583Fitting · misalignedTHE NR 1 PYLON INBOARD PITCH LOAD FITTING UPPER LINK BUSHING HAS MIGRATED 0.004 INCH. THE MIGRATED BUSHING WAS REPLACED. AD 2004-16-12, B767-57-0053.SDR LR7A06038Attach Fitting · damagedDURING SCHEDULED C6 CHECK FOUND NR 4 I/B LWR TRUSS MOUNT ATTACH FITTING TO HAVE OVERSIZED HOLE AT FS 517, RT OWS 162, WL 260. REPAIRED FITTING IAW LAC MEA 382-57-06-022.SDR LR7A06030Attach Fitting · damagedDURING SCHEDULED C6 CHECK, FOUND NR 1 INBD TOP TRUSS MOUNT ATTACH FITTING TO HAVE OVERSIZED HOLE AT FS 517, LT OWS 162, WL 280. REPLACED FITTING IAW LOCKHEED DWG 3308216.SDR LR7A06029Fitting · oversizedDURING SCHEDULED C6 CHECK, FOUND NR 4 OB TOP TRUSS MOUNT ATTACH FITTING TO HAVE OVERSIZED HOLE AT FS 517, RT OWS 197, WL 280. REPLACED FITTING IAW LOCKHEED DWG 3308216.SDR QXEA200601176Attach Angle · chafedPDX: WING TO NACELLE ATTACHED ANGLE CHAFED AT FWD LOWER EDGE JUST BELOW DEICING TUBE AND 4.5 INCHES FWD OF FRONT SPAR AND APPROX YW191.200. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00, SRM 51-21-10 AND SRM 51-25-10.SDR LR7A06005Mount · crackedDURING 'B-1' CHECK PER HN7101, FOUND NR 1 ENGINE OUTBOARD TRUSS MOUNT CRACKED AT FS 598, WL 280-284, OWS197.2. REPLACED TRUSS MOUNT IAW SMP583 54-30-05 AND 54-30-06 AND SB 382-71-13, N/R 0009.SDR 05FDEA02136Fitting · corrodedFOUND THE NR 1 ENG PYLON, INBD MOUNT OUTBD SHACKLE HAS PITTING CORROSION IN THE FACE SIDE OF THE SHACKLE.SDR 05FDEA02131Sleeve · corrodedNR 1 PYLON TO WING ATTACH FITTING SLEEVE (OUTBD LUG/LWR) HAS GOUGED MARK AND HAS CORROSION ON THE HEAD END INNER COLLAR.SDR 05FDEA02130Fitting · corrodedNR 1 PYLON TO WING ATTACHMENT FITTING SHACKLE OUTBD/INBD LOWER BUSHING HAS CORROSION CHROME PLATING WORN.SDR CALA0500107Fitting · crackedRIGHT PYLON FRAME CRACKED INBOARD AT AFT ACCESS PANEL. INSTALLED NEW FITTING PER SRM 51-40-02.SDR GTIA040489Attach Angle · crackedCRACK ON RT LOWER ATTACH ANGLE FOR PYLON ON AFT END. TRIMMED CRACKED AREA. FABRICATED REPAIR ANGLE. FABRICATED FILLER. INSTALLED REPAIR DOUBLER AND FILLER.SDR DL757030731Fitting · gougedGOUGE REPAIR THE INBD SURFACE OF THE INBD SIDE LOAD FITTING ON THE RT WING NACELLE ATTACH STRUCTURE WAS GOUGED DURING ACCOMPLISHMENT OF THE STRUT INPROVEMENT MODIFICATION IAW AD 2000-20-09. THE GOUGE WAS BLENDED SMOOTH AND ROTO PEENED AND THE ADJACENT FASTENESDR DL757030557Fitting · mismanufacturedLEFT WING, PYLON BACKUP FITTING, NR 2 HOLE THE FACTORY HOLE ON THE FITTING DID NOT LINE UP WITH THE EXISTING HOLE IN THE WING. OPENED UP HOLE TO INSTALL BUSHING TO ALLOW INSTALLATION OF THE NEW FITTING. REINSTALLED THE ORIGINAL FASTENER TYPE. ER/A 385153-14SDR DL757030263Fitting · damagedWHILE ACCOMPLISHING THE ENGINE PYLON AND WING MODIFICATIONS REQUIRED BY AD 2000-20-09, 2 ATTACH HOLES FOR THE INBOARD SIDE LOAD FITTING WERE DAMAGED. THE HOLES WERE OVERSIZED TO CLEAN AND ROUND CONDITION AND INSPECTED FOR CRACKS. OVERSIZE BOLTS WERE INSTALLESDR DL76G011677Fitting · mismanufacturedDURING ACCOMPLISHMENT OF REWORK TO THE LT STRUT AS DETAILED IN THE STRUT IMPROVEMENT PROGRAM THE INBOARD AFT PITCH LOAD FITTING WAS INCORRECTLY MACHINED. REPAIR ER/A 398045-14AD.SDR ERKR200100162Fitting · damagedLT TRAPEZOIDAL FITTING ELONGATED HOLE.SDR AU010322Mount · cracked(AUS) LH WING FITTING OUTBOARD LUG CRACKED DIAGONALLY ACROSS THE UPPERFLANGE FACE THROUGH THE LUG FILLET RADIUS. THE CRACK WAS FOUNDVISUALLY AND CONFIRMED USING NDI. FOUND DURING INSPECTION IAW ERB76-57-40-19.SDR AU010323Fitting · cracked(AUS) RT WING FITTING OUTBOARD LUG CRACKED AROUND THE INBOARD AFT CORNER OF THE LUG APPROXIMATELY 10MM (0.393IN) FORWARDAND 5MM (0.196IN) OUTBOARD. CRACK CONFIRMED USING NDI. FOUND DURING INSPECTION IAW ER B76-57-40-18.SDR AU010298Fitting · cracked(AUS) LT WING PYLON ATTACHMENT FITTING OUTBOARD LUG CRACKED. FOUND DURING VISUAL INSPECTION IAW ER B76-57-40-19.SDR AU010297Fitting · cracked(AUS) RT WING PYLON ATTACHMENT FITTING OUTBOARD LUG CRACKED. CRACK PENETRATES THE FULL THICKNESS OF THE LUG AND EXTENDSAPPROXIMATELY 25.4MM (1IN) ALONG THE INBOARD FACE AND APPROXIMATELY 12.7MM (0.5IN) ALONG THE OUTBOARD FACE. FOUND USING EDDY CURRENT INSPECTISDR RRXA003799Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT.WW BATHTUB FITTING AT STA. 960 AND L24L FWD SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DSDR RRXA10808Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SKIN AT O/B AFT END OF R/H W/W BELOW FIRE BOTTLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE,TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC8- SDR AWXA0001098Fitting · gougedLEFT PYLON IB AFT FRAME TOP SURFACE AT PANEL 5735L NICKED AND GOUGED BEYOND LIMITS AT IB FASTENER HOLE; FABED SHIM AND FLAP PEENED DAMAGED AREA AND SHIM IAW ENG SUPPORT/REPAIR SOPM 20-10-03 ER 0357540033-DL1; HFEC INSPECTED AREA NO CRACKS NOTED PER NDT; TREAT SDR RRXA003801Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT. WW LONGERON 24 AT STA. 902-920, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DOUGLAS REPLACEMENSDR RRXA003804Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA. 920 AMD L24 AND LT WW, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SDR DL767001797Fitting · tool damageTOOLING DAMAGE OCCURRED IN THE LT AND RT WING O/B PITCH LOAD FITTINGS. THE DAMAGE WAS LOCATED ON THE THIRD FROM BOTTOM HOLE ON THE VERTICAL LEGS OF THE BACK-UP FITTINGS. REWORK CONSISTED OF OS AND RE-COLD WORKING HOLES. ER/A 334916-14.SDR UPS00833959Fitting · crackedINSPECTION TYPE:C123, NR 1 PYLON FWD OF FWD V-BLOCK SUPPORT FTG FOR PYLON PLANK PNL IS CRACKED P/N 5756790-1. REMOVED CRACKED V-FITTING IAW DC8 SRM 51-1-20D & 51-3-0. INSTALLED FWD V-BLOCK IAW DC8 SRM 51-1-20D & 51-3-0. LEAK CHECK OF FWD V-BLOCK TO BE PERFOSDR DL767001615Fitting · misalignedTHE LT AND RT SIDE LINK FITTINGS HAVE SHORT E/D HOLES IN ADDITION TO ONE OVERSIZED HOLE AND ONE SPOTFACE AREA. ER/A 334808-14.SDR AU000543Rivet · misaligned(AUS) LEFT OUTBOARD ENGINE NACELLE COWL RIVET MISALIGNED TO SPAR CAP RIVETS BY APPROXIMATELY 3.175 MM (0.125 INCH). FOUND DURING INSPECTION IAW AD/P68/46. (X)SDR 2000UALA00279Bolt · crackedNR 2 PYLON O/B SIDELOAD FITTING I/B BOLT FOUND CRACK INDICAITON. *S/D* BOLT MATERIAL IS H11 STEEL AND CRACK IS THE RESULT OF STRESS CORROSION, A CHARACTERISTIC OF H11 MATERIAL. INCONEL 718 BOLTS WERE INSTALLED PER PROCEDURES OUTLINED IN BOEING SERVICE BULLESDR 2000UALA00259Bolt · crackedDURING C-CHECK, NR 16 THE NR 2 PYLON OUTBOARD WING STRUT SUPPORT INBOARD AND OUTBOARD BOLT (BACB30MT12K32) WAS FOUND SHEARED. ALSO, THERE WAS SLIGHT CORROSION AND GOUGING IN THE BORE. ON THE INBOARD WING STRUT SUPPORT FITTING THE OUTBOARD BOLT WAS FOUND CRACSDR EIAA2000103Fitting · damagedHAECO-HKG - C6/D-CHECK - NR 4 PYLON OUTBOARD UPPER LINK FITTING FASTENER HOLE HAD SHORT EDGE MARGIN. HOLE INSPECTED AND FASTENER INSTALLED PER SB. THREAD TRIMMED PER HAECO REPAIR SCHEME R-57-04-34318 AND BOEING MESSAGE EVG-HKG-00-00024H/-00027F/-00027F/-0003SDR AU000313Fitting · corroded(AUS) LEFT INBOARD NACELLE TO FORWARD SPAR ATTACHMENT CASTING UPPER LUG CORRODED IN THE AREA AROUND HI-LOC FASTENER.SDR 20000802SH026Rib · crackedRIB FOUND CRACKED AT INBOARD RIGHT WING AT INBOARD ENGINE MOUNT SUPPORT. ADDED A DOUBLER SUPPORT AND STOP DRILLED CRACK. THIS IS THE THIRD AIRCRAFT OF THIS TYPE WITH THIS PROBLEM FOUND DURING AN ANNUAL INSPECTION, ONE AIRCRAFT WAS FOUND WITH BOTH ENGINES'' SDR RRXA98027Bolt · missingDURING A MAINTENANCE VISIT, FOUND NR 2 PLYON SKATE ANGLE MISSING BOLT AT XW=253, 20 INCHES AFT OF FRONT SPAR. REPLACED BOLT BY INSTALLING FASTENER (NAS4205) BY MATERAIL SUBSTITUTION IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04195.SDR CA971028006Bracket · cracked(CAN) THE FOLLOWING BRACKETS AND CHANNELS WHICH ARE PART OF THE ENGINE MOUNT PYLON WERE FOUND TO CONTAIN CRACKS: BRACKET P/N 1213433-20, 1213433-21, CHANNELS 1213433-19, 1213433-14 AND 1213433-15.SDR DL72L971899Fitting · pittedLT PORK CHOP FITTING PITTED. BORED HOLES OVERSIZE WITHIN M/M 57-42-0 PG 806 814 LIMITS. HFEC SHOWS NO CRACKS. ROTO AND SHOT PEENED PER M/M 57-42-0. CAP PLATED AND PAINTED PER M/M.SDR DL72L971898Fitting · pittedRT PORK CHOP FITTING PITTED. BORED HOLES OVERSIZE WITHIN M/M 57-42-0 PG 806 814 LIMITS. HFEC FOUND NO CRACKS. CAP PLATED AND PAINTED PER M/M 57-42-0.SDR P5CA9701539Fitting · crackedNR 1 PYLON UNDERWING DIAGONAL BRACE FITTING CRACKED AT OUTBOARD SIDE AFT RADIUS POSITION. FITTING REPLACED PER SB 57-2288.SDR ABXA9701461Fitting · crackedDURING C-CHECK, FOUND ATTACH FITTING AT AFT INBD END OF RT HAND UPPER BONDED PNL CRACKED. REPLACED FITTING IAW DC-9 SRM 51-31-1.SDR CA961220002Fitting · cracked(CAN) THE FITTING IDENTIFIED IS MOUNTED AND COVERED PREVENTING IT FROM BEING CLEANED AND INSPECTED OR TREATED FOR CORROSION. THE FITTING WAS FOUND TO BE CRACKED DURING WINTER MAINTENANCE INSPECTION. ALL AIRCRAFT WILL BE NDT CHECKED USING ULTRASONIC AND EDDY CUSDR DLL10961540Fitting · crackedLT WING PYLON BACKUP FITTING BULKHEAD BETWEEN IWS 503 AND IWS 529 FOUND WITH A 6 INCH CRACK ORIGINATING AT THE I/B RAD OF THE SKIN ATTACH TAB, TRAVELING THROUGH THE INTEGRAL FLANGE AND PROCEEDED ACROSS THE WEB TOWARD THE CENTER RING INNER CAP AT45 DEG. THE FISDR CA960508006Bracket · cracked(CAN)VIBRATION FELT ON CLIMB OUT. INSPECTION REVEALED RH FAIRING (CONE) P/N 1417836-201 LOOSE. ATTACHMENT BRACKET (P/N 14157629-30 AND 32) WERE FOUND CRACKED, WITH LOOSE AND WORKING RIVETS. UPON REMOVAL O F THE BRACKETS ELONGATED HOLES, CHAFED AND CRACKED SKISDR UPS96805681Fitting · damagedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT. REWORKED NR 2 AND NR 3 PYLON FOOTSTOOL FITTING IAW UPS EO DC8-57-0641.
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