JASC 7100
Service difficulty reports · 635
Reports filed under 7100 · Powerplant System, 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 = '7100' 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 = '7100' 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 SWIA202161800None · vibratesHIGH LEFT ENGINE VIB ON TAKEOFF ROLL. REACHED 2.5 IN YELLOW ARC. LEVELED AND RAN QRH HAD POWER BACK TO UNDER 50% N1 TO GET OUT OF YELLOW ARC AND EVEN AT FLIGHT IDLE WE WERE AT 1.6 VIB. ANY USE OF POWER BROUGHT THE VIBRATION LEVEL INTO THE YELLOW ARC. (FLIGHSDR VGCA20211023001Not Reported · not reportedENGINE FLAMEOUT / LOSS OF POWER DURING CRUISE. ACCESSOPRY DRIVE HOUSING GEARBOX IS NOT ROATATINGSDR IPXA2021102475274Engine · noneINSPECTION TYPE:N/A**SUPPLEMENTAL SDR **REQUEST DMI TO COMPLY WITH EO 7100-53507 BETWEEN 10-20 FLIGHT CYCLES FOR RH ENGINE AFTER INSTALLATION.COMPLIED WITH EO-M-7100-53507COMPLIED WITH EO M-7100-53507 APPX A. NO LEAKS NOTED. THIS CLEARS M760587SDR IPXA2021102475273Engine · noneINSPECTION TYPE:N/A**SUPPLEMENTAL SDR**REQUEST DMI TO COMPLY WIT EO M-7100-53507 BETWENN 10 AND 20 FLIGHT CYCLES FOR LH ENG AFTER INSTALL. COMPLIED WITH EO M7100-53507 REF D760586COMPLIED WITH EO M-7100-53507 APPX A. NO LEAKS NOTED. THIS CLEARS M760586SDR CALA2021102501959Engine · noneREFERENCE LOG PAGE 7284669: AFTER ENGINE 1 HYD LOW PRESS INDICATION IN CRUISE, ENGINE 1 OIL FILTER BYPASS SHOWED ON THE ENGINE DISPLAY. ENGINE WAS SHUT DOWN AS PRECAUTIONARY PER QRH PROCEDURE. OIL PSI AT SHUT DOWN WAS 70. WINDMILL TIME WAS 33 MINUTES. NO OIL QSDR 9WGA2021102125801None · noneAIR RETURN FOR COMPRESSOR STALL #3 ENGINE. RAN ENGINE LIMITER SURGE OR STALL CHECK, ENGINE CONTINUED TO RUN AT REDUCED THRUST AND WOULD NOT RESPOND TO THRUST LEVER MOVEMENT.SDR SWIA202162821None · chafedRT LOWER TRANSCOWL, LATCH DOOR SPIGOT HOLE ELONGATED AND AREA CHAFFED AND COAMING BENT ON AFT EDGE (C-CHECK RO 11-24-21) REPAIRED RT LOWER TRANSCOWL LATCH DOOR SPIGOT ELONGATED HOLE REF REO 670-54-21-1207 REV A 2015-08-27 C/W SKY CARD 51-900-1002-SKYSDR SWIA202162820None · wornRT LOWER TRANSCOWL BOTH TRIGGER LATCH BEARING PADS WORN. (C-CHECK RO 11-24-21) REPAIRED RT LOWER TRANSCOWL TRIGGOR LATCH BEARING PADS REF MHIRJ REO 670-54-21-1480 REV -- 2021-11-08. COMPLIED WITH SKYCARD 51-900-1002.SDR SWIA202162819None · wornLH UPPER TRANSCOWL, BOTH LATCH DOOR TRIGGER LATCH BEARING PADS WORN. (C-CHECK RO 11-24-21) REMOVED AND REPLACED AFT LATCH BEARING PAD AND REPAIRED AFT C-CHANNEL REF. REO 670-54-21-1481 REV. --, 2021-11-08 AND COMPLIED WITH SKY CARD 51-900-1002-SKY. REMOVESDR ASAA2021100836237Unknown · unknown#1 ENGINE SHUT OFF LEVER IS STUCK IN AN ABNORMAL POSITION - ENGINE IS OFF, BUT LEVER IS OUT OF POSITION. GROUNDED - YES. CYCLED #1 ENGINE CUTOFF/SHUT OFF LEVER MULTIPLE TIMES, OPS CHECK NORMAL. OK FOR SERVICE.SDR CALA2021100601778Engine · none3 POSSBL COMPSSR STALLS 1AT V1 OTHR 2 INFLT L ENG THRUST LITE IL L REFERENCE L/P 7163041 & EGC ENGINE R/R ENGINE 1 POWER PLANT REMOVAL I.A.W. A.M.M. 71-00-02-000-801-G00. ACCOMPLISHED TASKS LETTER STEP H PREPARE FOR REMOVAL UP TO AND INCLUDING STEP 18 FAN COWLSDR FDEA202110022486Skin · damagedNUMBER ONE R/H SLAT HAS SKIN DAMAGED FORWARD SIDE. REPAIRED DAMAGE IN REFERENCE TO MD-10-30 SRM 57-10-00 FIG 43 VOL 1SDR 2021FA0000276Crankcase · crackedA PERSISTENT ENGINE OIL LEAK WAS TRACED TO THE RIGHT HAND SIDE OF THE ENGINE CRANKCASE IN FRONT AND BELOW THE VALVE ROCKER BOX COVER AN DRAIN FITTING.SDR IPXA2021092974386Start Valve · inoperativeINSPECTION TYPE:N/A**SUPPLEMENTAL SDR** #1 ENGINE WOULD NOT START. NO ROTATION ON A OR B IGNITOR PACKS DISENGAGED BUT STILL NO ROTATION. DEFERRED #1 ENG START VALVE IAW MEL 80-13-01-1. DMP C/W.REPLACED #1 STARTER SHUTOFF VALVE PER AMM 80-13-02-0401. OPS CHECK SDR CALA2021092801720Drain Mast · cracked#1 ENG DRAIN MAST HARD LINE CRACKED ( ACOC) APROX 180 DEGREES AROUND LINE WHERE BRAZED INTO MAST. UPDATED TO SDR. REMOVED AND REPLACED #1 ENGINE DRAINS MAST I.A.W. A319 AMM 71-71-42.SDR SWIA202162746None · cracked*RH UPPER TRANSCOWL MOST INBD €ŒA€? FITTING IS CRACKED (C-CHECK RO 11-20-2021) REMOVED DAMAGED R/H UPPER TRANSCOWL INBD "A" FITTING, AND INSTALLED 1 EA NEW "A" FITTING P/N CN624-2082-201 REF REO 670-54-21-971 REV (A) 2017-05-11 STEPS 1-3.SDR SWIA202162745None · cracked*LH UPPER TRANSCOWL MOST INBD €ŒA€? FITTING IS CRACKED (C-CHECK RO 11-20-2021) REMOVED AND REPLACED INBD STAND OFF ANGLE ( A-FITTING ) P/N CN624-2082-201 ON LH UPPER TRANSCOWL IAW ALL STEPS OF REO 670-54-21-971 REV -A, DATED 2017-05-11. WEIGHT REMOVED = SDR SWIA202162719None · worn*LH UPPER TRANSCOWL LATCH DOOR COAMING HAS WEAR. AREA MARKED. (C-CHECK RO 11-20-2021) REPAIRED WEAR DAMAGE ON LH UPPER TRANSCOWL LATCH DOOR COAMING IAW ALL STEPS OF REO 670-54-21-1028 REV -NC, DATED 2009-06-15. COMPLIED WITH SKY CARD 51-900-1002-SKY. FUNCTSDR SWIA202162850None · seizedRH CORE COWL OB ATTACHMENT LINK FITTING BOLT IS SEIZED. (C-CHECK RO 11-24-21) REMOVED RH CORE COWL OB ATTACHMENT LINK FITTING BOLT REF CRJ 700 SRM 51-41-02-001-001-A01.SDR P5CA2021092100355Harness · noneENG #1 CONDUIT OF ALTERNATE GEN DAMAGED(<P><SPAN>REPAIRED HARNESS CONDUIT 31 ENG PER SWPM 20-10-13 REV 77; EEC GEN ALT T1519 CONNECTORES</SPAN></P> / <P><SPAN>ENG #1 RUN UP TEST OK AMM 71-00-00/501 REV 133</SPAN></P>)SDR IPXA2021092474255Bracket · damagedINSPECTION TYPE:A300ENG 2 FAN COWL I/B FITTING SUPPORT BRACKET DAMAGED.REMOVE AND REPLACE IAW SRM 51-40-21.SDR EVCA091821None · crackedENGINE EXHAUST COLLECTOR AFT FACE HAS 2EA 0.3" CRACKS POSITIONED AT 2 & 10 O'CLOCK.SDR SWIA202162124None · chafedRH LWR TRANSCOWL ALIGNMENT HOLE FOR LATCH DOOR CHAFED. (C-CHECK RO 10/30/2021) REPLACED RH LWR TRANSCOWL LATCH COAMING P/N CN624-2060-209 IAW ALL STEPS OF REO 670-54-21-1207 REV -A, DATED 2015-08-27. OPS CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR 2LCF20210916001Engine · fracturedDURING CLIMB FROM FL310 TO FL330, THERE IS A SUDDEN LOSS OF N1 AND STRONG VIBRATION ON THE RIGHT ENGINE. THEREFORE, THE CREW CONSIDERS SEVERE DAMAGE; THE CREW SHUTS DOWN THE ENGINE, DECLARES AN EMERGENCY (MAYDAY) AND OPTS TO LAND IN KINGSTON. (JAMAICA). THE LASDR UIEA2021091602028Engine · warning messageUPON SHUTTING DOWN LEFT ENGINE L AC BUS MESSAGE DISPLAYED REMAINED ILLUMINATED UNTIL EXT POWER SELECTED.(<P>PERFORMED FIM TASK 24-32 FT803 BLOCKS 1 AND 2 FOLLOWED BY ENGINE RUN IAW AMM 71-00-00. OPS NORMAL AT THIS TIME. NO FURTHER DEFECTS NOTED. NUSSIANCE FAULSDR SWIA202161904None · chafedCOMPLY WITH REO 690-54-22-027 REV.-- DATED 2021-09-06 FOR BLENDED CHAFE DAMAGE TO LH LOWER TRANSCOWL HINGE BEAM. (C-CHECK RO 10/22/2021) COMPLIED WITH REO 690-54-22-027 REV.-- DATED 2021-09-06 ALL STEPS COMPLETED FOR BLENDED CHAFE DAMAGE TO THE LH LOWERSDR MASA20210914418Skin · wornRH ENGINE CORE COWL WAS FOUND TO HAVE EDGE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-13-01, FIGURE 54-13-01-991-801, ITEM 1, EA 72-2021-151.SDR SWIA202161903None · damagedCOMPLY WITH REO 690-54-24-007 REV. -- DATED 2021-09-06 FOR BLENDED CHAFE DAMAGE TO LH TRANSCOWL FLOATING TIE BAR. (C-CHECK RO 10/22/2021) COMPLIED WITH REO 690-54-24-007 REV --, DATED 2021-09-06 FOR BLENDED CHAFE DAMAGE TO L/H TRANSCOWL FLOATING TIE BARSDR DALA2021091305441Skin · perforatedSHIP 3327 PERFORATION ON INTERNAL SKIN OUTBOARD FAN COWL LOC. FWD LOWER POSITION ON ENGINE 2. CORRECTIVE ACTION: REPAIRED INTERNAL SKIN OUTBOARD FAN COWL LOC. FWD LOWER POSITION ON ENGINE 2, AS PER ER/A 593877-14 PRI REV 0. AND ROHR SRM54-20-00 REPAIR 3. (1943SDR SWIA202162486None · gougedL/H ENGINE C-DUCT HINGE BEAM HAS MULTIPLE GOUGES (C-CHECK RO 11/10/2021) BLENDED GOUGES TO A SMOOTH TRANSITION, REF CRJ700 SRM 51-12-00-001-001-A01 REV 38 JUL25/2020. FOUND TO BE WITHIN ALLOWABLE LIMITS PER REO 670-78-34-1021 REV-- 2021-09-03. COMPLIED WISDR IPXA2021092474253Bracket · damagedINSPECTION TYPE:A300ENG 2 FAN COWL O/B FITTING SUPPORT BRACKET DAMAGED.REMOVE AND REPLACE IAW SRM 51-40-21.SDR SWIA202161895None · chafedLH LOWER TRANSCOWL OUTBOARD LEADING EDGE CHAFED ON INNER SURFACE (C-CHECK RO 10/22/2021) LH LOWER TRANSCOWL OUTBOARD LEADING EDGE BLENDED AND FINISH RESTORED AND REPLACED COAMING REF REO 670-54-21-1207 REV. A DATED 2015-08-27, REO 690-54-21-394 REV.-- SDR SWAA2021100515038None · looseLOOSE FASTENER LIP INLET COWL ON RT ENGINE ; 2021-392678 / [01] REMOVED FASTENERS LOC. LIP INLET COWL ON RT ENGINE BETWEEN NINE OCLOCK TO TWELVE OCLOCK IAW B737-700 SRM 51-40-02 FOR GAIN ACCES AND PERFORMED VISUAL INSPECTION AND NO FOUND MORE DAMEGE.; [02] STESDR UIEA2021071501550Skin · scratchedNO.3 ENG NOSE COWL LIP SKIN 5:30 O'CLOCK AREA FOUND SCRATCH MARK.(<P>THE NOSE COWL SUBJECT AREA BLEND OUT REPAIR CARRIED OUT AS PER SRM 54-10-01-1A-1 REV 34 DATE 20 JUL 2021.</P>)SDR CALA2021042200526Unknown · odorSTRONG SMELL OF OILFUMES INFLIGHT... ESPECIALLY AT LOWER ALTITUD ES.ONLY IN COCKPIT. ASED ON FLIGHT CREW SMOKE/ODOR IN THE PLANE (NOTABLY FLIGHT DECK) WORKING TSM TASK 71-00-00-810-801-A , # 1 ENGINE FOR EVIDENCE OF OIL LEAK. LOCKING FOR SIGNOFF CONCURRENCE WISDR SWIA202157515Pan · blockedLH ENGINE INLET PANDOWN IS INSTALLED PER SB CF34-NAC-71-039 AND NDT TASK 54-430-602 CAN NOT BE PERFORMED. (C-CHECK RO 4/12/2021) REMOVED AND INSTALLED LH ENGINE INLET PANDOWN TO PERFORM NDT TASK 54-430-602 IAW MHIRJ REO 601R-54-11-3752 REV -- DATED 20SDR 2022F00165Governor · out of adjustNUMBER 2 GOVERNOR STAY OVER 102 RPM AND DO NOT KEEP STEADY CONTINUOSLY.SDR P5CA2021022300050None · noneBIRD STRIKE ON NR 1 ENGINE RT INLET SIDE(CLEANED AND INSPECTED BIRD STRIKE ON RT SIDE OF NR 1 ENGINE INLET IAW AMM 05-51-18. NO DEFECTS NOTED.SDR IPXA2020120763174Structure · crackedINSPECTION TYPE: SV NR 2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION IS CRACKED. REPAIRED CRACKED NR 2 ENGINE INLET LOWER VERTICAL STABILIZER REAR SPAR FIRE SEAL ZEE EXTRUSION, IAW VT-SAA EA 011-5530-01-A8753 REV. I/R AND UPS EO MSDR 2022F00145Bearing Seal · leakingPRECAUTIONARY SHUTDOWN PERFORMED FOR RH ENGINE PER QRH EAC 72.32 AND QRH EAC 72.26 DUE TO IN-FLIGHT OIL STRAINER CLOGGING LIGHT CAME ON AND AN INCREASE IN OIL TEMPERATURE WAS OBSERVED.SDR IKBR2020072100002Seal · leakingPILOT REPORTED OIL ON COWLING. ON INVESTIGATION, FOUND THE PROP SHAFT SEAL LEAKING. INSTALLED A NEW SEAL IAW MANUFACTURE INSTRUCTION 1324.SDR VNAA2020032011101Engine · contaminatedAFTER TAKEOFF THE AIRCRAFT HAD SMOKE IN THE CABIN DUE TO RESIDUE BURNING OFF FROM AN OVERNIGHT ENGINE WASH. THE CREW RAN QRH AND RETURNED TO FIELD FOR MAINTENANCE. THEY DECLARED AN EMERGENCY. MX PERFORMED HIGH POWER DRYOUT RUN TO CLEAR COMPRESSOR WASH FLUID FRSDR DALA2020031201798Unknown · malfunctionedSHIP 3147 - ATO - LESS THAN 20KTS DUE TO FLIGHT CREW REPORT OF RIGHT ENGINE SLOW TO ADVANCE. CORRECTIVE ACTION: PERFORMED NO-GO ODI PREVENTION ATA 7185 PROCEDURE. C/W TSM 71-00-00-810-807-A AND A319 AMM 71-00-00-710-010-A. ENGINE ACCELS WITHIN LIMITS. REVIEWEDSDR EVCA202003061Line · separatedDURING FLIGHT, THE AIRCRAFT EXPERIENCED POWER LOSS RESULTING IN A HARD LANDING. UPON INSPECTION OF THE AIRCRAFT, THE PC LINE PN: 23065814 FROM THE COMPRESSOR SCROLL TO PC FILTER HAD CRACKED AND SEPARATED AT A WELD POINT.SDR AC2A2020050113919Filter · crackedIBF MAINTENANCE INDICATOR FOUND CRACKED. *SUPPLEMENTAL INFORMATION* PART NUMBER ENTERED ON ORIGINAL SDR IN SECTION 5 WAS IN ERROR. PART NUMBER WAS SUBMITTED AS 104440-201 AND SHOULD HAVE BEEN 104441-201. *SUPPLEMENTAL INFORMATION* THE UNIQUE CONTROL CODE WAS ASDR DALA2020012300545Master Switch · faultedINFLIGHT SHUTDOWN, DIVERTED DUE TO MULTIPLE ECAM MESSAGES AND RIGHT ENGINE INFLIGHT SHUTDOWN. FOUND FAULT ON NR 2 ENGINE MASTER SWITCH. REPLACED INTEGRATED CONTROL PANEL. LP 6695790SDR UIEA2019111505913None · noneBIRD STRIKE RIGHT ENGINE(<P>PERFORMED #2 ENGINE BOROSCOPE INSPECTION PER B767 AMM 72-00-00/601. NO DAMAGE OR DEFECTS NOTED. C/W FIM 71-05 FT 822 AND AMM 05-51-18.</P><P>LP 1110215 - M2: INSTALLED BOROSCOPE MOTERIM COVER PAD AND SEAL, REFSDR ASAA2019072430190Bearing · worn#1 ENGINE START DUCT LINK AFT CONNECTION TO FAN FRAME BRACKET HAS WORN BEARING. GROUNDED - YES. REPLACED #1 ENG. START DUCT LINK AFT IN REF TO PPBM 71-00-02.SDR CA190711016Button · failed(CAN) AFTER PREVIOUS RTO, PAX WERE REMOVED FROM AIRCRAFT. PAX WERE RE BOARDED WHEN MTC DEEMED AIRCRAFT AS SERVICEABLE. ON RUNWAY 27R, FLIGHT DID ANOTHER REJECTED TAKE OFF AT 60KTS WITH SAME DEFECTS REAPPEARING AS IN REJECT NUMBER 1 AND 2. AIRCRAFT TAXIED BACK SDR 2019FA0000194Engine · making metalENGINE CHIP LIGHT ILLUMINATED WHEN ENGINE WAS BROUGHT TO FLIGHT IDLE AFTER ENGINE START UP. MAINTENANCE FOUND 2 FLAKES WITHIN LIMITS ON THE UPPER CHIP PLUG.A 30 MINUTE GROUND RUN WAS PERFORMED, THE PLUGS WERE INSPECTED AGAIN AND FOUND CLEAN. AIRCRAFT RETURNED
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