JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 UIEA2019081535087Rub Strip · brokenBROKEN RUB STRIP NO.1 ENG NOSE COWL AFT BULKHEAD OUTER RING NEAR 8 O'CLOCK POSITION(<P>REMOVE DAMAGED PARTS IAW GEK9250 SPM 70-13-01 REV.108. INSTALL NEW PARTS IAW GEK9250 SPM 70-13-01 REV.108 AND GOODRICH CMM 71-11-16 REV.46. JOB COMPLETED AND CONDITION CHECKSDR UIEA2019081405161Bracket · wornBRACKET WORN, NR 1 PYLON PRV R/H PNEUMATIC DUCT SUPPORT LINK. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G-0 REV 110. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G-0 REV.110 AND DWG 311T2150 SH 5, REV 0.SDR CA191022020Inlet · corroded(CAN) CORROSION FOUND ON THE LH / RH INLET COWL LIP SKINS (TC# 20191022020)SDR FXGA2019081261963Stringer · crackedNR 4 NACELLE STRINGER AND SKIN SPLICE. TO SPLICE NR 4 NACELLE STRINGERS NR 1 AT STATION 436 AND STRINGER 32 AT STATION 432.5. THE NACELLE SKIN WILL BE SPLICED AT STRINGER 2 BETWEEN STATION 400 AND 473. NUMEROUS REPAIRS WERE PREVIOUSLY INSTALLED ON THE UPPERSDR UIEA2019080604956Case · corrodedCORROSION ON OUTER CASE, NR 2 ENG FAN CASE ON 12 O'CLOCK TO 6 O'CLOCK, 8 O'CLOCK TO 12 O'CLOCK POSITION ON NAC STA 163. ACCOMPLISHED FAN CASE CORROSION REPAIR IAW ENG MANUAL GEK92451 ESM 72-23-01-220-572 REV. 88. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR FDEA201908051798Attach Fitting · cracked#1 PYLON INBOARD SIDE PANEL ATTACH STRUCTURE AT PANEL 414CR FORWARD UPPER CORNER IS CRACKED. REMOVED AND REPLACED EXTRUSION AT PANEL 414CR IAW AIRBUS DWG'S A54611629, A54612121 AND A300-600 SRM 51-40-21.SDR SWIA2019082246198Frame · gougedRH AFT PYLON FAIRING FWD FRAME I/B LUG IS GOUGED. (C-CHECK) RO: 08/21/2019 REMOVED AND REPLACED R/H AFT PYLON FAIRING FWD FRAME1 IAW SRM.SDR UIEA2019080204934Torque Box · corrodedNR 1 PYLON UPPER CAVITY TORQUE BOX SKIN CORRODED, FOUND BETWEEN NAC STA 204.5 AND 249.5. REPAIRED IAW RI-54-00-13660 REV. A.SDR IPXA2019081655657Fairing · crackedINSPECTION TYPE:2C#2 PYLON PANEL 457BR SKIN HAS A 6" LONG CRACK.REPAIRED CRACKED #2 PYLON PANEL 457BR SKIN IAW VT-SAA EA 011-5450-01-A7874 REV. IR AND UPS EO MD11-5450-73554-A. (MINOR)SDR UIEA2019080254844Skin · corrodedAFTER REMOVED #1 PYLON FOUND SURFACE CORROSION ON I/B UNDER WING BOTH SIDE.(<P>#1 PYLON OUTBOARD PYLON I/B UNDER WING MID SPAR FTG SURFACE CORROSION SPOT FACE REPAIR AND BUSHING INSTALLED IAW SRM 57-20-90-2R-2 REPAIR 2. THIS REPAIR IS A CATEGORY B REPAIR.</P>)SDR UIEA2019080254845Fitting · corrodedAFTER REMOVED #1 PYLON FOUND SURFACE CORROSION ON O/B UNDER WING BOTH SIDE.(<P>#1 PYLON OUTBOARD PYLON O/B UNDER WING MID SPAR FTG SURFACE CORROSION SPOT FACE REPAIR AND BUSHING INSTALLED IAW SRM 57-20-90-2R-2 REPAIR 2. THIS REPAIR IS A CATEGORY B REPAIR.</P>)SDR IPXA2019082324897Cowling · gougedINSPECTION TYPE:2C, NR 1 ENG. I/B FAN COWL FWD HINGE FITTING IS GOUGED.REPAIRED GOUGED NR 1 ENG. I/B FAN COWL FWD HINGE FITTING IAW VT-SAA EA 011-7110-01-A7870 REV. IR AND UPS EO MD11-7110-73512-A. (MINOR)SDR REXA2019081491241Separator · chafedPANEL 422DB IS CHAFED. REMOVED AND REPLACED FWD AND AFT SEPERATORS ON PANEL 422DB IAW CRJ200 SRM 51-41-06 WVAC EMP STAMP 771SDR REXA2019081491227Separator · chafedPANEL 422DB IS CHAFED. REMOVED AND REPLACED FWD AND AFT SEPERATORS ON PANEL 422DB IAW SRM 51-41-06.SDR ASMF2019100902Acoustic Liner · damagedDURING OVERNIGHT CHECK, IT WAS DETECTED THE LEFT ENGINE ACOUSTIC PANEL DAMAGED. MAINTENANCE PERSONNEL PERFORMED INSPECTION ON THE LEFT ENGINE ACOUSTIC PANEL, DETECTING A CRACK OF 0.500” LENGTH LOCATED AT 01:00 HOUR POSITION AND AT 13.00” FROM REAR EDGE ON INNESDR CA190719011Closeout Panel · damaged(CAN) EAGLE COPTERS IS CURRENTLY INVESTIGATING A CUSTOMER REPORTED MARKING THAT WAS OBSERVED ON THE MAIN ENGINE TO TRANSMISSION DRIVESHAFT (PN 407-340-310-101). IT APPEARS THE DRIVESHAFT BRIEFLY TOUCHED THE 0789-03-132 LOWER CLOSE OUT, PART OF THE AIRCRAFT ENGSDR IPXA2019080214209Rivet · looseINSPECTION TYPE: 4C, NR 2 ENG. INLET COWL L/E LIP HAS NUMEROUS LOOSE RIVETS. REPAIRED THE LOOSE RIVETS IAW EA 011-7110-01-A7844, REV IR, AND EO MD11-7110-73473-A. MINOR.SDR HYIA20190717001Beam · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED IN THE CHANNEL(P/N 5654107-15) THAT ATTACHES THE RT CROSSOVER BEAM(P/N 5654104-12) TO THE RT INBOARD ENGINE BEAM(P/N 5654109-7.) WHEN THIS CHANNEL WAS REMOVED FOR REPLACEMENT, A CRACK IN THE RH INBOARD ENGINE BEAM WAS SDR K11A2019081273205Frame · worn#2 ENGINE PYLON LOWER EDGE HAS WORN FWD CLOSEOUT FRAME @ INLET COWL INTERFACESDR K11A2019081273204Frame · wornNR 1 ENGINE PYLON @ FWD LOWER EDGE HAS WORN FWD CLOSEOUT FRAME @ INLET COWL INTERFACESDR FDEA2019062871420Rib · damagedNR 2 ENG INLET DUCT THRU PANEL 361JL HAS BROKEN PIECE OF RIB REMOVED AND REPLACED BROKEN SECTION OF RIB IAW SRM 54-10-00 VOL 1 AND DWG AJC7173. ADDED NEW REPAIR SPLICE IAW SRM 54-10-00 VOL 1. MAJOR REPAIR.SDR UIEA2019062764597Rod · damagedNR 2 ENGINE OUTBD CORE COWL OPEN HOLD ROD FOUND DAMAGED. REMOVED AND REPLACED OUTBD CORE COWL HOLD OPEN ROD PER AMM 70-11-00.SDR UIEA2019062764598Rod · damagedNR 1 ENGINE INBD CORE COWL OPEN HOLD ROD LOCK DAMAGED. REMOVED AND REPLACED ENGINE INBD CORE COWL OPEN HOLD ROD PER AMM 20-11-00.SDR YENA2019062840354Structure · damagedDURING HEAVY MAINTENANCE, IDENTIFIED HOLE DAMAGE ON THE LH WING PYLON SPIGOT FITTING CENTER HOLE. NOTE AT THE CURRENT CHECK THE SUBJECT AIRCRAFT IS BEING UPGRADED FROM TO WV 017 AND ALL REPAIRS MUST ENSURE WV 17 APPLICABILITY. AIB RESPONDED TO THE DAMAGE EVSDR HKGA20190626038Panel · chafedPANEL CHAFED. REMOVED DAMAGED SEAL RING, MATCH DRILLED NEW PART, INSTALLED NEW SEAL RING (REF. EMB120 SRM 51-40-02 REV 58, EMB120 SRM 51-25-00 REV 58, EMB120 SRM 51-40-02 REV 58). LOCATED AND DRILLED NEW PNL 429AT (PER EMB120 SRM 51-40-04 REV 58).SDR HKGA201906260037Support Channel · crackedSUPPORT CHANNEL CRACKED. MATCH DRILLED NEW HALF FRAME TO COWLING STRUCTURE IAW SRM 51-25-00 REV 58. MATCH DRILLED LATCH PIN GUIDE ASSY'S AND DOOR HOLD OPEN ROD PINS AND INSTALLED ON NEW HALF FRAME IAW AMM 20-10-01-2, REV 43, SRM 51-40-02-PR, AND 51-25-00-PR SDR HKGA201906260024Support · burnedFABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW ETD 2019-120-045306 AND SRM 54-30-02 REV 58.SDR HKGA201906260023Flap · crackedFLAP CRACKED. R & R 18 FASTENERS PER EMB120 SRM 51-40-02 REV 58.SDR CALA2019062201032Skate Angle · crackedSKATE ANGLE CRACKED. CRACK LOCATED AT THE NR 2 PYLON NACELLE I/B COMMON TO LOWER WING SKIN JUST AFT OF I/B HYDRAULIC BAY DOOR. REMOVED, LOACTED, DRILLED, INSTALLED A REPLACEMENT SKATE ANGLE IAW SRM 51-40-02, 51-40-05. PART 4.SDR DALA2020012973593Skate Angle · crackedNR 1 ENGINE PYLON LOWER SKATE ANGLE SUPPORT CRACKED. REMOVED DAMAGED ANGLE ANDINSTALLED NEW ANGLE. REF: B757 SRM 54-51-02.SDR IPXA201906213529Filler · damagedINSPECTION TYPE: C12, BURN DAMAGE ON FILLER AND DOUBLER OF FWD UPR SPAR WEB ON #1 PYLON NEAR NAC STA 228.19.REPAIR IAW SRID : 4-4504150598 AND EO B767-5410-72969-A.SDR REXA2019062080936Doubler · crackedRH ENGINE UPPER CORE COWL 445AT UPPER FWD CORNER IS BENT AND CRACKED. INSTALLED DOUBLER DUE TO CRACKING.SDR IPXA2019061754294Support Plate · crackedINSPECTION TYPE:12YR#2 PYLON, I/B SIDE, BEHIND PANEL 485AL, THE FAIRING SUPPORT PLATE IS CRACKED AT THE FWD END.REMOVED AND REPLACED FAIRING SUPPORT PLATE MEMBER PER A300-600 SRM 51-40-21.SDR REXA2019062070928Panel · damagedPANEL 412DB DIVIDERS ARE KNIFE EDGED. REMOVED AND REPLACED KNIFE EDGED DIVIDERSSDR UIEA2019061074433Door · excess playNR 2 ENG OB CORE COWL PRESSURE RELIEF DOOR HAS PLAY. REMOVED AND REPLACED NR 2 ENG OB CORE COWL PRESSURE RELIEF DOOR HINGE PINS AND RELATED HARDWARE IAW B767 AMM 71-11-09.SDR JJBA2019061105009Yoke · damagedRT PYLON FWD YOKE UPPER FLANGE FASTENER HOLE SHOWS DAMAGE INDICATIONS BY THE HFEC ROTATIVE DRIVE INSPECTION METHOD. COMPLETED INSTALLATION OF FASTENER AT RIGHT PYLON FWD YOKE UPPER FLANGE.SDR HYIA20190606001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE INBOARD LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING, THIS CRACK MEASURES APPROXIMATELY .150 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN MEL-54-02R2 TO SATISFYSDR IPXA2019062874794Support · crackedINSPECTION TYPE:123C, NR 2 PYLON ACCESS PANEL 424CR SUPPORT STRUCTURE, FORWARD UPPER CORNER REENFORCING CLIP WAS CRACKED. REMOVED AND REPLACED THE FISHPLATE PER SRM 51-40-21, AND DWG A54612371.SDR HYIA20190605001Beam · crackedDURING MAINTENANCE TWO CRACKS WERE DISCOVERED ON THE INBOARD FACE OF THE RIGHT HAND INBOARD ENGINE BEAM IN THE AREA OF THE VERTICAL ATTACH CHANNELS FOR THE CROSSOVER BEAM. THESE CRACKS WERE DISCOVERED AFTER CHANGING THE CROSSOVER BEAM VERTICAL ATTACH BRACKET PSDR REXA2019062030912Rub Strip · chafedCOWL 432AT LE SEAL HAS CHAFING DAMAGE. REMOVED/REPLACED RUB STRIP IAW CMM 71-14-01 SRS091SDR REXA201906130824Seal · wornR/H UPPER CORE COWL T/E IS CHAFED, REMOVED OLD AND INSTALLED NEW CLOSURE RING IAW BOMBARDIER CMM 71-12-01.SDR REXA2019061300826Retainer · crackedPYLON ACCESS PANEL 422DB SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETAINER IAW SRM-51-42-06.SDR CA190612001Cowling · delaminated(CAN) DURING FLIGHT CREW FELT STRANGE LOUD VIBRATION AND LEFT HAND ENGINE EXPERIENCED SEVERAL FLAME OUT. FLIGHT WAS COMPLETED AND THE AIRCRAFT LANDED UNEVENTFULLY. DOWNLOAD REVIEWED FROM CAMP SYSTEM, DO NOT SHOW ANY FAULT CODE. FURTHER TROUBLESHOOTING IS GOINGSDR REXA201906030768Retainer · crackedUPON SEAL REMOVAL ,FOUND PANEL 422AT SEAL RETAINER CRACK (REQUIRE NEW RETAINER AND NEW SEAL)
REMOVED/REPLACED DAMAGED SEAL RETAINER IAW CRJ 200 SRM 51-42-06 AAR SM 58SDR REXA201906030757Panel · chafedPYLON PANEL 412DB HAS 2EA. WORN SEPERATOR PANELS. REMOVED AND REPLACED SEPERATORS IAW SRM 51-42-06.SDR REXA2019060300750Panel · chafedPYLON PANEL 422DB HAS 2EA. WORN SEPERATOR PANELS. REMOVED AND REPLACED SEPERATORS ON PANEL 422DB IAW CRJ 200 SRM 51-42-06 AAR SM 58SDR REXA20190603745Rub Strip · chafedLEFT ENGINE COWL PANEL 432AB RUB STRIP KNIFE EDGED. REMOVED AND REPLACED RUB STRIP ON PANEL 432AB IAW CMM 71-14-01.SDR REXA2019060300748Rub Strip · chafedLEFT ENGINE COWL PANEL 432AT RUB STRIP KNIFE EDGED. REMOVED AND REPLACED RUB STRIP ON COWLING 432AT IAW BOMBARDIER CMM 71-14-01 AAR SM 58SDR REXA2019060300747Rub Strip · chafedRIGHT ENGINE COWL PANEL 442AT RUB STRIP KNIFE EDGED. REMOVED AND REPLACED DAMAGED RUB STRIP WITH NEW RUB STRIP IAW BOMBARDIER CMM 71-14-01. AAR SM 58SDR IPXA2019061243152Support Rib · crackedINSPECTION TYPE:12Y, LH #1 ENGINE PYLON L/E, AFT PANEL SUPPORT RIB, FOR SPRING DOORS, 413AL AND 414AR, UPPER INSIDE RADIUS IS CRACKED.REMOVED AND REPLACED RIB ON #1 PYLON IAW AIRBUS DWG A54611461 AND A300 AMM 54-52-61.
Back to JASC 5410