JASC 7100

Service difficulty reports · 635

Reports filed under 7100 · Powerplant System, newest first.

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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"

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SDR R61A20120058Clamp · corrodedWHILE A/C WAS IN FOR HEAVY CHECK FOUND BRAIDED CONDUIT AND ADEL CLAMPS ON WIRE HARNESS INSIDE INBOARD FLAP WELL HAS SURFACE CORROSION ABOVE AFT PYLON. MX CLEANED BRAIDED CONDUIT AND REPLACED ADEL CLAMP ON BRAIDED HARNESS INSIDE INBOARD FLAP WELL ABOVE AFT PYLJan 20, 2012 · N119HQ · Emb ERJ170200LRSDR REXA201101004Unknown · malfunctionedRIGHT ENGINE WOULD NOT REDUCE TO IDLE AT ALTITUDE (310) FUEL FLOW WITH THRUST LEVERS AT STOPS WERE 550 WHILE THE LEFT ENGINE WAS 350. ALL WAS NORMAL ON APPROACH AND LANDING. PERFORMED ENG ACEL/DECL CHECK ON RT ENGINE IAW AMM 71-00-00. COULD NOT DUPLICATE DIDec 22, 2011 · N8783E · Cndair CL6002B19SDR REXA201100983Fitting · corrodedAFT THRUST FITTING CORRODED. AFT THRUST FITTING REMOVED AND REPLACED IAW PPBM 71-00-03 FIG 39.Dec 18, 2011 · Cndair CL6002B19SDR UALA2011121506890Unknown · unknownON DESCENT GOT STATUS R ENG CONTROL AND R ENG EEC C1. PIMU SHOWS CH A AND CH B B25 TR-CK FAIL. 2.5 BLEED VALVE ACTUATOR CONNECTION CHECKED AND CLEANED, TEST 15 EEC GROUND TEST OF ENGINE CONTROL SYSTEM ACTUATORS CARRIED OUT IAW AMM PAGE 586D AND FIM 71 PIMU MEDec 14, 2011 · N641UA · Boeing 767322SDR CVGA20111202001Unknown · malfunctionedAPPROXIMATELY 38 MINUTES INTO FLIGHT, AT FL410, HEARD A MODERATELY LOUD BOOM NOISE COMING FROM THE BACK LEFT SIDE OF THE AIRCRAFT, FELT A MINOR YAW MOMENT AND OBSERVED THE LEFT ENGINE STACK INCREASE SLIGHTLY THEN RETURN TO NORMAL. FLIGHT CONTINUED WITH NO FURDec 2, 2011 · N95AG · Lear 60LEARSDR HYIA836HC201116Cowling · crackedDURING HEAVY CHECK A CRACK WAS FOUND ON A BEAM IN THE LT LOWER ENGINE COWLING. THE DAMAGE CONSISTS OF A SINGLE CRACK 1.8" LONG THAT RUNS BETWEEN 2 LIGHTNING HOLES IN THE BEAM. THE CRACK WAS REPAIRED IAW STS ENGINEERING SOLUTIONS EA 12-2011-013. REPAIR PERFOROct 27, 2011 · N42836 · Aerosp ATR42320SDR QMLDMG2011Diffuser · crackedWHILE PERFORMING SB SB319722830, VER B CENTRIFUGUAL DIFFUSER VANE BORESCOPE, FOUND A PIECE OF THE DIFFUSER VANE MISSING AND CRACKED. AWAITING MFG TEC TO COME REPLACE THE DIFFUSER.Mar 10, 2011 · N135DU · Urocop EC135T2SDR CA110208010Engine · failed(CAN) IFSD/INABILITY TO MODULATE THRUST DURING TAKE OFF, PILOT HEARD A BUZZING NOISE. PILOT ELECTED TO CONTINUE TO FL180. ONCE AT CRUISE AT FL180, PILOT MODULATED LH ENGINE POWER LEVER AND THE AND ENGINE ROLLED BACK TO FLIGHT IDLE POWER. THE PILOT DECLARED EMEJan 28, 2011 · Raythn 400ARAYTHEONSDR CA101206003Powerplant · failedPOWER LOSS-OPERATOR REPORTED AN IFSD OCCURRED FOLLOWING A LOUD NOISE. NO FURTHER DETAILS ARE AVAILABLE. POST FLIGHT INSP FOUND METALLIC DEBRIS IN THE EXHAUST. THE ENG WILL BE REPLACED.Nov 29, 2010 · Beech 1900DSDR CA101130007Skin · crackedBOTH LOWER FWD ENGINE COWLS ON AIRCRAFT HAD CRACKED DUCT SKINS P/N 101-910020-3.Nov 29, 2010 · Beech B200SDR CA110214010Engine · power lossPOWER LOSS/IFSD ENGINE SHUT ITSELF DOWN WITHOUT ANY NOTICE. AN UNEVENTFUL SINGLE LANDING WAS MADE. POST EVENT INSP FOUND A LARGE TEAR IN THE GAS GENERATOR CASE. THE ENGINE WAS SENT TO MFG FOR INVESTIGATION WHERE THE CAUSE WAS IDENTIFIED A CRACKING FROM FATISep 29, 2010 · Bell 212SDR KGBR2010072300003Rod Bearing · failed(KGBR) AFTER TAKEOFF AND UPON CLIMB TO ALTIUDE, THE NR 2 ENGINE OIL PRESSURE DROPPED RAPIDLY AND THE ENGINE OIL TEMPATURE INCREASED RAPIDLY. THE FLIGHT CREW IMMEDIATELY SHUTDOWN THE ENGINE AND RETURNED TO THE AIRPORT. UPON INVESTIGATION BY THE MX CREW, IT ISJul 22, 2010 · N2871G · Cvac PB4Y2SDR CA100817007Engine · failedDURING REVENUE FLIGHT, THE CREW OBSERVED A LOUD NOISE, FOLLOWED BY VIBRATION AND SMOKE FROM THE EXHAUST. ITT INDICATION DROPPED TO ZERO, THE PROPELLER FEATHERED WITHOUT PILOT INPUT AND THE ENGINE SHUTDOWN WITH OIL STREAMING FROM THE FRONT COWL AREA. NO EMERGJul 16, 2010 · Beech F90SDR CA091207006Latch · worn(CAN) INTAKE COWL LT INSP DOOR LATCH PN 90-015-032-235 HEAVILY WORN AT STRIKER WITH FWD FIREWALL. FWD FIREWALL PN UNK ALSO EXIBITS WEAR.Dec 3, 2009 · Bell 407SDR QXEA2009050800317Unknown · unknownYVR - ON APPROACH TO YVR, NR 1 PPEC, POWERPLANT MESSAGE ON ED, PROP RPM 1060. FEATHERED NR 1 PROPELLER AND DECLARED EMERGENCY. LANDING UNEVENTFUL. INTERROGATED CDS, FOUND FAULT CODES 160/162 ON NR 1 ENG REF FIM 61-20-04-810-814, NO TARGET SCREWS MISSING, DUMay 4, 2009 · N409QX · Bombdr DHC8402SDR HALA2009042800168Unknown · unknownETOPS SIGNIFICANT SYSTEM - L PIMU MSG ON ECS/MSG. TROUBLESHOOT WITH FIM 71-00-00. BITE OF PIMU SHOWED EEC CH A/B XTRN DISAGREE. EPCS PAGE 2 DOESN'T SHOW ANY LABEL BIT INFO FOR OVERSPEED CIRCUITS. ERASED L PIMU PERFORMED BITE AND RAN ENGINE MSG DID NOT RETUApr 28, 2009 · N584HA · Boeing 7673G5SDR 2009FA0000079Duct · crackedDURING REPLACE OF THE RT ENGINE, AFT LOWER COWLING FWD BULKHEAD P/N 101-910038-3, CRACKS WERE DISCOVERED IN THE LT AND RT COWLING AFT DUCTS P/N 101-910049-11 AND 101-910049-12 UPPER MOUNTING FLANGES. THIS AREA IS ONLY ACCESSIBLE BY REMOVING THE PANEL (DOOR) PFeb 3, 2009 · N7232R · Beech 200CBEECHSDR AXS2008F00000Cowling · damagedDEPARTED AND LEVELED OFF AT 9000 FT. DURING DECENT THROUGH 7800 FT THE PILOT NOTED A "LOADING NOISE" AND THE ACFT YAWED FROM THE ASSIGNED HEADING. THE ACFT EXPERIENCED A CONSTANT BUFFETING AND VIBRATION COULD BE FELT THROUGH THE AIRCRAFT. AFTER 5-6 SECONDS THESep 25, 2008 · N197WA · Beech 99ASDR MT92008F00003Screw · misinstalledIN FLIGHT, THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO THE LT ENGINE. THIS FORCED THEM TO DO AN INFLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND SPACER THAT SECURES TJun 19, 2008 · N26932 · Swrngn SA227ACSDR AC2A119271Warning Light · illuminatedNR 2 ENGINE CHIP SUMP LIGHT ILLUMINATED IN FLIGHT. FOLLOWED EMERGENCY CHECKLIST AND LANDED. REMOVED CHIP PLUGS, CLEANED AND PERFORMED PENALTY RUN. FOUND SERVICEABLE.Mar 17, 2008 · N430CT · Bell 430SDR 2007UALA03604Eec · malfunctionedA-T DISCONNECTED FL380 IN CRUISE. CURRENT FAULT SHOWS AUTO DISC EEC L- PRIMARY. REPLACED LEFT EEC. NO FURTHER MAINTENANCE ACTION NEEDED.Sep 7, 2007 · N553UA · Boeing 757222SDR HEEA116985Ecu · inoperativeON LANDING, NR 1 DECU CIRCUIT BREAKER POPPED. ON TURNING ON THE BATTERY, CIRCUIT BREAKER POPPED AGAIN. MAINTENANCE REPLACED THE ELECTRONIC CONTROL UNIT.Aug 22, 2007 · N734P · Skrsky S76CSDR UPS07849776Engine · flamed outINSPECTION TYPE:AS-E AT FLIGHT LEVEL 360 NR 3 ENGINE FLAMED OUT. RAN FLAME OUT CHECKLIST & RESTART IN FLIGHT CHECKLIST WHILE DESCENDING TO FLIGHT LEVEL 240 RESTART SUCCESSFUL OPERATED NORMALLY REMAINDER OF FLIGHT. PERFORMED ENGINE FLAME-OUT T/S REF MM 71-00-May 8, 2007 · N701UP · Doug DC871FSDR YENA2007018Cowling · detachedFLT 830, PBI-JFK, AIR RETURN TO PBI. ENGINE COWL SEPARATED FROM ENGINE NR 1. DAMAGE NOTED ON INBOARD LEADING EDGE ON LEFT WING AND OTHER AREA'S OF ENGINE COWL.Mar 18, 2007 · N635JB · Airbus A320232SDR VNAA0703010Actuator · leakingCREW REPORTED FUEL RUNNING OUT OF RIGHT ENGINE NACELLE. MAINTENANCE INSPECTED AND FOUND THE LEAK OCCURING AT THE VG ACTUATOR WITH THE FUEL PUMP ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 VG MASTER ACTUATOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAMar 15, 2007 · N708PS · Cndair CL6002C10SDR BAQA20070008Thermocouple · erodedDURING NR 2 ENGINE START-UP. NR 2 ECU MAINTENANCE AND TOT CAUTION LIGHT ILLUMINATED AND THE NR 2 ENGINE SHUTDOWN. DOWN LOADED NR 2 ECU AND FOUND FAULT CODE FOR T-4 SIGNAL LOSS. DURING START THE ECU MONITORS T-4 TEMPERATURE. IF SIGNAL IS LOSS THE ECU SHUT THE EFeb 12, 2007 · N109DK · Agusta A109ESDR 2006UALA02340Unknown · unknownRETURN TO FIELD DUE TO NR 1 ENGINE COWLING PROBLEM.Dec 10, 2006 · N831UA · Airbus A319131SDR UPS06647723Engine · shutdownETOP IN-FLIGHT SHUTDOWN, RT ENGINE SHUTDOWN DUE TO HIGH OIL TEMP. (OPEN)Aug 18, 2006 · N309UP · Boeing 76734AFSDR BSYA200600013Flow Divider · low pressureCOMING INTO LCK LEFT ENGINE FLAMED OUT WHEN THROTTLE WAS BROUGHT BACK TO IDLE, LANDED AT LCK NO PROBLEMS. FOUND FLOW DIVIDER LOW PRESSURE, REMOVED AND REPLACED FLOW DIVIDER AND UPDATED N1DEEC ENGINE COMPUTER PER S/B TFE731-76-3076.Mar 22, 2006 · N31WR · Lear 35ASDR 2006FA0000356Duct · crackedLT ENGINE LOWER AFT COWLING, LWR DUCT FOUND CRACKED ABOUT 80 PERCENT ITS ENTIRE WIDTH ALONG FIRST RIVET ROW. REMOVED CRACKED DUCT AND FOUND NOT TO BE ROLLED ENOUGH. THIS PUT STRESS ON RIVET ROW. NEW SPARE PART ORDER FROM MFG WAS ROLLED CORRECTLY AND FIT WITMar 13, 2006 · N326PG · Beech B200SDR MALA060052Engine · power lossDURING T/O ROLL, NOTICED ITT OF 891 ON LEFT ENGINE. DURING CLIMB-OUT, HAD CONSISTENT 100 PLUS SPLIT. THE HIGHEST DT TEMP WE NOTICED WAS 114. WENT THROUGH QRH AND AVOIDED NG RANGE AS BEST AS POSSIBLE. AIR TURNBACK TO MSP COMPLETED 409 #274289. REMOVED PAPER TFeb 7, 2006 · N434XJ · Saab 340BSDR 2006F00002Unknown · unknownDURING TAKEOFF FROM 2W6 LT ENGINE SHUTDOWN, SECURED ENGINE, CIRCLED, RETURNED FOR LANDING. CAUSE YET TO BE DETERMINED. PRELIMINARY INDICATIONS ARE FAILED FUEL PUMP DRIVE/ACCESSORY DRIVE.Jan 12, 2006 · N37676 · Cessna 421BSDR UPS05845646Engine · flamed outNR 4 ENGINE FLAMED OUT IN CRUISE FLIGHT. T/S PER MM 71-00-00-1 FIG 139 SHT 1&2. REPLACED FUEL FILTER ELEMENT, RAN ENG WITH FEED & BOOST PUMP OFF, FUEL PRESS WITHIN LIMITS. ENG OPS NORMAL.Oct 26, 2005 · N706UP · Doug DC871FSDR ASMF200508008Engine · making metalAIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE START, THE RT START VALVE OPEN LIGHT FLASHED AT 40 PERCENT RPM, N2 DECREASED TO 35 PERCENT AND RETURNED TO 50-56 PERCENT, 20 SECONDS AFTER THAT ENGINE STOPPED. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENANAug 17, 2005 · N803ML · Doug DC987SDR VNAA0507023Cowling · damagedAFTER POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT ENGINE LOWER NOSE ACCESS COWL WAS MISSING. THE COWL WAS FOUND ON THE RUNWAY. MAINTENANCE INSTALLED A SERVICEABLE NOSE ACCESS COWL IAW CRJ200 AMM 71-14-01-400-802. THE AIRCRAFT WAS THEN RELEASED FOJul 29, 2005 · N226JS · Cndair CL6002B19SDR CA050722004Oil Filter · out of adjust(CAN) ON TAKEOFF ROLL AT APROX 60 KTS, THE AMBER ICAS (RT ENG OIL PRESS HIGH) POSTED. THE CREW ABORTED THE TAKEOFF. THE RT OIL PRESSURE SWITCH WAS ADJUSTED, OPERATIONAL CHECK AND LEAK TESTS WERE DONE. ACFT RTSJul 10, 2005 · Bombdr BD7001A10SDR DHL2005363002Engine · failedAT VR ENGINE NR 2 FAILED. COMPLETED APPROPRIATE ABNORMAL PROCEDURES. DUMP 18,800 LBS OF FUEL. EGT TEMP EXCEEDED 7 SECONDS AT 940. PERFORM BOROSCOPE INSPECTION ON NR 2 ENG FOR EGT OVERTEMP AND COMPRESSOR STALL ON TAKEOFF. PERFORMED BORO INSP PER MM 72-00-00Apr 27, 2005 · N363DH · Airbus A300B4203SDR TXER100821Baffle · wornWORN BAFFLE.Apr 22, 2005 · N155EW · Urocop EC155BSDR TXER100820Baffle · wornWORN BAFFLE.Apr 22, 2005 · N155EW · Urocop EC155BSDR 2005FA0000383Nose Cowl · corrodedNOSE COWL SENT TO US FOR REPAIR. DURING EVALUATION SEVERE INTERGRANULAR CORROSION WAS DISCOVERED ON THE OUTER SKIN OF THE ACOUSTIC BARREL. SUSPECT IMPROPER HEAT TREATMENT AT MFG. PART IS CONSIDERED BEYOND ECONOMICAL REPAIR AND WILL BE SCRAPPED AT THIS LOCATMar 22, 2005 · Doug DC10*SDR ANCF200400040Engine · failedDURING MAINTENANCE CHECKS WITH ENGINES RUNNING UP THE LT ENGINE HAD A STRONG STALL. THE LT ENGINE WAS IMMEDIATELY SWITCHED OFF. DURING THE PRELIMINARY BOROSCOPE INSPECTION, FOUND C6, C7, C13, COMBUSTION CHAMBER, T1 AND T2 IN GOOD CONDITIONS. THE DAMAGE WASFeb 26, 2005 · Doug MD83SDR P5CA0501299Engine · failedDURING FULL THRUST T/O 650' NR 4 ENGINE FAILED WITH FIRE INDICATION. SHUT DOWN ENGINE AND FIRED BOTTLES. REPLACED NR 4 ENG PER WC 7100-002. RUN UP OK.Dec 30, 2004 · N858FT · Boeing 747123SDR 2004F00358Compressor · stalledON FIRST TAKEOFF OF THE DAY, EXPERIENCED COMPRESSOR STALL. ABORTED TAKEOFF AND HOVERED TO NEAREST PARKING PAD AND REPORTED INCIDENT TO MAINTENANCE AND MANAGEMENT. MAINTENANCE VISUALLY INSPECTED INTAKE AREA FOR HARDWARE AND FROGS, INSPECTED COMPRESSOR BLADES Jul 7, 2004 · N272M · Bell 206L1SDR AMTA200400619Control Unit · failedL ENGINE AND ENGINE LIMITER INOPERATIVE LIGHT ILLUMINATED. EICAS MSG L ENG EEC, L ENG LIMITER DISPLAYED. REMOVED AND REPLACED BOTH DGCU PER AMM 71-00-00-5 TEST NR 3. ALL CONDITIONS NORMAL. OK FOR SERVICE. (M)May 31, 2004 · N522AT · Boeing 75723NSDR AALA20031076Engine · bird ingestionEN ROUTE, AIRCRAFT ENGINE INGESTED BIRD INTO THE NR 2 ENGINE. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT OVERWEIGHT INSPECTION PERFORMED. REPLACED THE NR 2 ENGINE. LEAK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Sep 28, 2003 · N432AA · Doug DC982SDR 2003FA0000804Flywheel · brokenFLYWHEEL ASSEMBLY AFT BELT GROOVE FLANGE BROKEN. FLANGE WEB AREA VERY THIN.Aug 6, 2003 · N577ER · Piper PA44180SDR UIAFAA9204Tscu · malfunctionedDURING T/O AUTOFEATHER NO ARM ,CHK FND TSCU FAULT, IAW PWC 72-01-00 REPLACED TSCU AND IAW AMM 71-00-00 ENG RUNING AUTOFEATHER SYSTEM FUNCTION TEST NORMAL.Jun 20, 2003 · N15225 · Dhav DHC8311SDR CH1A200394006Engine · stalledCOMPRESSOR STALL ENGINE NR 2 AT BEGINNING OF TAKEOFF ROLL EPR APPROX 1.3Mar 27, 2003 · N294AS · Boeing 727290SDR 03010Engine · vibrationDURING T/O ROLL NR 3 ENGINE HAD VIBRATION AND LOUD NOISE. AIRBORNE VISUAL INSPECTION REVEALED DAMAGE TO ENGINE. DUMPED FUEL AND RETURNED TO BASE.Mar 9, 2003 · N713CK · Boeing 7472B4BSDR UPS03440259Compressor · stalledAIR TURNBACK NR 3 ENG COMPRESSOR STALL IN CLIMB AT FL190 PAX REPORTED GLOW IN N1 SECTION. EGT RISING, ENG SHUTDOWN. REMOVED AND REPLACED NR ENGINE S/N OFF P685985CN, INSTALLED S/N P662942 PER TC 5000, 5001, 5016 & MM 71-00-00 OPS & LEAK CHECK GOOD. OK FOR CMar 6, 2003 · N682UP · Boeing 747121
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