JASC 7712

Service difficulty reports · 1,239

Reports filed under 7712 · Engine BMEP/Torque Indicating, 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 = '7712'
  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.

SDR QR9R2026031300001Torque Box · malfunctionedENGINE PARAMETER MALFUNCTION DURING START RUN-UP. REMOVED AND REPLACED TORQUE ADJUSTMENT BOX IAW AMM 77-12-00, 4-2. T/F MOC COMPLETED; CHECKS GOOD.Mar 13, 2026 · Bolkms BK117C2SDR COEA2025072404711Gauge · erraticFLT 8735, ENROUTE ANC-ENA AIR TURNBACK. DURING CLIMB OUT, THE PILOT NOTICED ERRATIC FLUCTUATIONS OF THE TORQUE GAUGE. RETURNED TO ANC. NO EMERGENCY WAS DECLARED. LANDED WITHOUT FURTHER INCIDENT. REPLACED THE TORQUE GAUGE. OPS CHECK GOOD.Jul 23, 2025 · N711FX · Cessna 208BSDR ABXA2023050882Tach Generator · intermittentN1'S FLUCTUATING AT IDLE BOTH ENGINES 23.3-26.5 ACCOMPANIED BY INTERMITTENT VIBRATION IN COCKPIT THAT DOES NOT APPEAR ON VIBRATION GAUGES. ALL OTHER EICAS GAUGES WITHIN LIMITS. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACEMay 2, 2023 · N651GT · Boeing 767231SDR YENA2023032700290Wire Harness · failedFLT#523, JFK-LAX. (ETOPS) ENG 2 FADEC SYS FAULT; R & R WIRE HARNESS WO4 4088K REF L/P 3569608 (FOUND OPEN WIRE 3" BACK FROM CONNECTOR P63 ON #2 ENGINE N2 (4065KS). R & R HARNESS W04 ON #2 ENGINE PER MM 73-21-64.). IDLE CHK PASS. FAULT CLEAR ENG #2. [ REF L/P Mar 26, 2023 · N2142J · Airbus A321271NSDR ABXA2023021524Unknown · unknownAFTER ENGINE START RT ENGINE SHOWED N1 EXCEEDANCE 124.3 OUR START WAS NORMAL WITH NO EXCEEDANCE NOTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK ON N1 INDICATION IAW B767 AMM 77-12-01. NO FAULTS NOTED. INDICATION CLEARFeb 13, 2023 · N774AX · Boeing 767281SDR QR9R20210928001Torque Box · splitON HOVER, ENG SPLIT AND ENG PA DIS CAUTION ON CAD RESULTING IN A MISSION ABORT. A T/F EVALUATION REVEALED SYSTEM 1 AND 2 ENG PA DIS DISPLAYED ON CAD WITH BOTH NUMBER 1 AND 2 TQ INDICATIONS IN YELLOW WHEN PICKING THE ACFT UP TO A HOVER. ENGINE SPLIT DISPLAYED ISep 28, 2021 · Bolkms BK117C2SDR UIEA2021080201669Engine · malfunctionedON CLIMBOUT NAI ON, LEFT ENG N1 2% LOWER THAN R ENG. LEFT N1 SHOWED 103.1, R ENG SHOWED 105.5. AFTER NAI SWITCH OFF, BOTH ENG SHOWED SAME N1(<P>PERFORMED FIM TASK 77-12 FT 825, NO DISCREPANCIES FOUND. RUN ENGINES 1 AND 2 ABOVE IDLE AND NAI ON. IAW B767 AMM 77-Aug 1, 2021 · N1361A · Boeing 76731BSDR UIEA2021020100169Sensor · failedRIGHT ENGINE SPEED CARD STS MSG. R & R RT ENGINE N2 SPEED CARD OFF PN 285T0458-303, SN D04761. OPS CHECK NORMAL IAW AMM 73-21-54. MSG CLEARED. 28JAN21 LOG PG 1271503 ITM 5 MIA; R & R RIGHT ENGINE N2 SPEED SENSOR. OPS CHECK NORMAL IAW AMM 77-12-02. PERFORMJan 28, 2021 · N1229A · Boeing 767306SDR UIEA2020052641121Warning Message · false activationRIGHT ENGINE ANALOG N2 STATUS MSG. PERFORMED FIM 77-12- FT 809. NO DEFECTS NOTED. MESSAGE CLEARED.May 24, 2020 · N1997A · Boeing 76733ASDR UIEA2020043000922Sensor · faultyR ENG ANALOG N2 STATUS(<P>REPLACED N2 SPEED SENSOR AND PERFORMED POWER PLANT TEST 4 . CHKS GOOD PER AMM 71-00-00-795-034-M03.</P>)Apr 30, 2020 · N1997A · Boeing 76733ASDR COEA2019112601797Indicator · erraticFLIGHT 8775 ROUTE: PHX-FLG DISCREPANCY: DURING TAKEOFF, THE TORQUE GAUGE BEGAN TO GIVE ERRATIC READINGS. PILOT ELECTED TO DECLARE AN EMERGENCY AND RETURN TO PHX. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE TORQUE INDICATOR. ALNov 26, 2019 · N797FE · Cessna 208BSDR UIEA2019093005608Status Message · false activationSTATUS MESSAGES: L ENG ANALOG N2 & R ENG ANALOG N2. (<P>ACCOMPLISHED FIM 77-12 FT 806 AND FIM 71-01 FT 804, NO FAULTS OR DISCREPANCIES NOTED. RESET SYSTEM, OPS CHECK NORMAL. </P>)Sep 28, 2019 · N662GT · Boeing 76731ASDR UIEA2019090505445Status Message · false activationR ENG ANALOG STATUS MESSAGE. L ENG ANALOG STATUS MESSAGE. ACCOMPLISHED FIM 77-12 FT 805, NO DISCREPANCIES NOTED. RESET EICAS MESSAGES.Sep 4, 2019 · N662GT · Boeing 76731ASDR CA190725007Indicator · shorted(CAN) TORQUE GAUGE FAILED AND POPPED CIRCUIT BREAKER. (TC# 20190725007)Jul 19, 2019 · Bell 212SDR UIEA2019070104635Unknown · malfunctionedDURING #1 ENGINE START, N1 DISPLAY WENT BLANK.(<P>ACCOMPLISHED FIM TASK 77-12 FT 803. RESET SYSTEM, OPS CHECK NORMAL (EEC/PIMU). </P><P>NOTE: ENGINE RUN ACCOMPLISHED BY CREW, ALL NORMAL. </P>)Jun 30, 2019 · N662GT · Boeing 76731ASDR UIEA2019061324469Status Message · false activationSTATUS MESSAGE, LEFT ENGINE SPEED CARD. PERFORMED OPS CHECK IAW PER B767 AMM 77-12-00. OPS CHECKED GOOD, NO STATUS MESSAGE DISPLAYED.Jun 12, 2019 · N1409A · Boeing 767306SDR CA190614003Engine · reads high(CAN) THE AIRCRAFT TOOK OFF AND AT ABOUT 1,000 FT. ABOVE GROUND LEVEL, PILOT GLANCED DOWN AT THE EIS (ENGINE INDICATING SYSTEM). AT THIS TIME HE NOTED TORQUE WAS INDICATING ABOVE 60 PSI AND THE RED WARNING ANNUNCIATOR WAS FLASHING. HOWEVER, THE PILOT ALSO NOTEJun 1, 2019 · Pilats PC1245SDR UIEA2019031103516Warning System · false activationDURING ENG START MOMENTARY OVERSPEED WARNING MSG(<DIV>PERFORMED FIM TASK 71-01-00 PIMU BITE CHECK NO FAULT FOUND AT THIS TIME. STARTED ENGINE MULTIPLE TIMES IAW 71-00-00, ALL ENGINE STARTS NORMAL AT THIS TIME. </DIV>)Mar 9, 2019 · N1409A · Boeing 767306SDR QXEA2019082700331Indication Sys · false indicationABORT TAKEOFF DUE TO NR 2 ENGINE TORQUE BUG TORQUE INDICATED 92% FOR ABOUT 1.5 SECONDS. ABORTED TAKE OFF. REMOVED FROM SERVICE. NO ENGINE PARAMETER EXCEEDANCES RECORDED. NO FURTHER ACTIONS REQUIRED. NO FURTHER DEFECTS. REF AMM 05-11-00-992-802 REF MCN 6050080-Aug 27, 2018 · N432QX · Bombdr DHC8402SDR 2018FA0000200Transducer · failedTORQUE PRESSURE TRANSDUCER FAILEDJul 2, 2018 · N812SS · Dhav DHC6*SDR UIEA2018040300522Sensor · intermittentDURING CRUISE FLIGHT, N1 INDICATION FLUCTUATED INTERMITTENTLY, FOR THE NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENG N1 FAN SPEED SENSOR IAW AMM 77-12-01. OPS CHECKED NORMAL IAW AMM 71-00-00.Mar 28, 2018 · N1709A · Boeing 767375SDR UIEA2017060500939Sensor · erraticLEFT ENGINE N2 INDICATION FOUND ERRATIC ON EICAS DISPLAY DURING ENGINE RUN. THE LT ENGINE N2 SENSOR WAS REMOVED AND REPLACED IAW AMM 77-12-02, REV 121.Jun 7, 2017 · N1321A · Boeing 767306SDR PNSA2017040201Torque Sensor · faultedRIGHT ENGINE POWER INDICATION FLUCTUATED PLUS OR MINUS G & PU'S RT ENGING MAINT AND APU STARTED AUTOMATICALLY. REMOVED AND REPLACED FAULTY TORQUE SENSOR.Apr 2, 2017 · Saab 2000SAABSDR UIEA2017030900312Sensor · failedENGINE VIBRATION BITE MAINTENANCE MESSAGE, PERFORMED FIM 77-31, FT 808, 77-31, FT 812. LEAD TO RT ENGINE N1 SENSOR SIGNAL CUT OUT. REMOVED AND REPLACED THE RT ENGINE N1 SENSOR IAW 77-12-01. OPS CHECKED GOOD.Mar 9, 2017 · N1049A · Boeing 76736NSDR UIEA2017022200230Indication Sys · malfunctionedAT RT ENGINE START, THE N1 INDICATION WAS ZERO UNTIL FUEL CONTROL WAS IN RUN, FAN ROTATION VERIFIED BY GROUND CREW WHEN N1 SHOWED ZERO. PERFORMED PIMU BITE, NO FAULTS NOTED IAW FIM 71-01-00/101. PERFORMED OPS TEST IAW AMM 77-12-00. NO FAULTS NOTED, OPS NORFeb 22, 2017 · N1049A · Boeing 76736NSDR 2016F00236Torquemeter · blockedPILOT EXPERIENCED HIGH TORQUE INDICATION ON INSTRUMENT. TROUBLESHOOTING WAS PERFORMED AND FOUND TO BE INTERNAL TO THE ENGINE GEARBOX TORQUEMETER. UPON REMOVAL OF ENGINE, DELIVERY TO OVERHAUL FACILITY, AND DISASSEMBLY OF GEARBOX AND TORQUEMETER, PLASTIC MEDIA WNov 12, 2016 · N30HF · Bell 407SDR UIEA2016110700831Sensor · malfunctionedLEFT N2 ERRATIC BELOW 20% AT START. REMOVED AND REPLACED THE NR 1 ENGINE N2 SPEED SENSOR IAW AMM 77-12-02. OPS CHECKED NORMAL.Oct 7, 2016 · N1997A · Boeing 76733ASDR JJBA20160929002Indication Sys · fluctuatesNR 1 TORQUE FLUCTUATING +/-20 % ABOVE 60% TORQUE. PERFORMED ENG PERFORMANCE TEST NO FLUCTUATION/SURGED NOTED.Sep 29, 2016 · N362PH · Dhav DHC8202SDR JJBA20160712003Tscu · inoperativeNR 2 ENGINE FEATHERED UNCOMMANDED. POWER UPTRIM ILLUMINATED. WHEN THE POWER WAS RETARDED THE PROP UNFEATHERED. WITH THE SYS DESELECTED, OFF AND POWER APPLIED THE ENGINE/PROP OPERATE NORMALLY. DEFERRED IAW MEL. R&R TSCU. OPS CHECK SAT. MEL CLOSED.Jul 12, 2016 · N358PH · Dhav DHC8202SDR HNAA2016061700186Tscu · malfunctionedDURING TAKEOFF ROLL AT 85 PERCENT TORQUE AUTO FX FAILED TO ARM, REJECTED T/O. LIGHT ILLUMINATED UPON REDUCED POWER. R & R NR 2 ENGINE TSCU IN REF TO 77-10-00 C/W CARDS 72-01-10X & 72-00-10Q. RAN ACFT, OPS CHECK GOOD.Jun 16, 2016 · N938HA · Dhav DHC8102SDR JJBA20160614007Tscu · inoperativeNR 2 ENGINE TORQUE AT 150+ FOR 7-10 SECONDS. R & R NR 2 PROP ASSEMBLY AND R & R NR 2 TSCU. CREW SHUTDOWN THE ENGINE AND RETURNED TO FIELD. PROP ASSEMBLY, PN:806700-1, SN: 970610, TSN: 31647.45, CSN: 42798.Jun 14, 2016 · N375PH · Dhav DHC8202SDR JJBA20160210002Tscu · failedON CLIMB OUT AT 400 - 500 FEET, THE NR 1 ENG FEATHERED UNCOMMANDED. LOST ALL TORQUE. THE CREW RAN THE CHECKLIST & SHUTDOWN THE ENG. INSPECTED THE NR 1 ENG WIRE HARNESS, PLA CLA MICRO SWITCHES. R & R NR 2 TSCU.Feb 10, 2016 · N367PH · Dhav DHC8202SDR JIKA2016012001Signal Cond Unit · intermittentAFTER TAKEOFF, THE RT ENG AUTO FEATHERED. THE RT ENG TORQUE READOUT WAS ZERO. ALL OTHER ENG PARAMETERS SHOWED NORMAL ENG OPERATING CONDITIONS. THE PILOT RETURNED & LANDED WITHOUT INCIDENT. INSPECTED THE RT ENG TORQUE SYS & FOUND THE RT ENG TORQUE SIGNAL COJan 17, 2016 · N258AS · Emb EMB120ERSDR 6CBA20160106147Indication Sys · reads lowCREW REPORTED LOW TORQUE INDICATION, APPROX 5.2-5.3 PSI.Jan 6, 2016 · N978AF · Pilats PC1247ESDR CA160106014Limiter · stripped(CAN) PILOT HAD TO CARRY OUT A PRECAUTIONARY IN-FLIGHT SHUTDOWN OF NR 1 ENGINE DUE TO TORQUE FLUCTUATION AND OIL PRESSURE DROPPING. ACFT LANDED SAFELY WITHOUT FURTHER INCIDENT. NR 1 ENGINE TORQUE LIMITER HAD COME AWAY FROM THE REDUCTION GEAR BOX THREADED BOJan 4, 2016 · Beech 200BEECHSDR CA151204013Control Unit · malfunctioned(CAN) ON TAKE OFF FROM CLIMBING THROUGH 800FT NR 2 ENGINE EXPERIENCED AN UNSCHEDULED AUTOFEATHER. ENGINE WERE SET AT TAKE OFF POWER WHEN NR 2 ENGINE TORQUE WENT TO APPROXIMATELY 136% AND PROP RPM DROPPED TO 500 RPM. ALL ENGINE PARAMETERS WERE NORMAL UNTIL UNSCDec 1, 2015 · Dhav DHC8311SDR CA160301007Indicator · malfunctioned(CAN) DURING CLIMB OUT, THE NR 1 ENGINE TORQUE INDICATION WENT TO 165%. THE POWER WAS REDUCED BUT THE TORQUE INDICATION REMAINED THE SAME. ALL OTHER ENGINE PARAMETERS APPEARED TO BE NORMAL AND NO AIRCRAFT YAW WAS NOTICED. THE FLIGHT CREW FOLLOWED THEIR QUICK RNov 20, 2015 · Dhav DHC8102SDR CA151120001Tscu · malfunctioned(CAN) DURING CLIMB OUT, NR 1 ENGINE TORQUE INDICATION WENT TO 165 PERCENT. POWER WAS REDUCED BUT TORQUE INDICATION REMAINED THE SAME, ALL OTHER ENGINE PARAMETERS APPEARED TO BE NORMAL AND NO ACFT YAW WAS NOTICED. FLIGHT CREW FOLLOWED THEIR QRH AND PERFORMED Nov 20, 2015 · Dhav DHC8102SDR JJBA20151119005Unknown · malfunctionedON LANDING ROLLOUT WITH NR 2 ENG POWER LEVER AT DISK, THE TORQUE & RPM ADVANCED TO TAKEOFF POWER UN-COMMANDED. PERFORMED BETA BACKUP, OVERSPEED GOVERNOR, MINIMUM GOVERNOR & MAXIMUM GOVERNOR SPEED TEST, RUNS WERE SATISFACTORY WITH NO SIGNS OF TORQUE OR RPM SURNov 19, 2015 · N360PH · Dhav DHC8202SDR S9BA201510170014Transducer · malfunctionedLT ENGINE ONLY PRODUCING 40 LBS TORQUE ON TAKEOFF. TAKEOFF WAS ABORTED. TORQUE TRANSDUCER WAS REPLACED IAW AMM 79-31.Oct 12, 2015 · Dhav DHC6300SDR AALA20150915004Circuit Card · faultyAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RECEIVED A TAT PROBE EICAS MSG, NO AUTO THROTTLE/LNAV/VNAV/NO ICE PROTECTION, ACCOMPANIED BY THE RT EEC INOPERATIVE LIGHT ILLUMINATING. ACCOMPLISHED FIM 30-33-00-815 802, FOUND Sep 15, 2015 · N176AA · Boeing 757223SDR CA150410019Indicator · false indication(CAN) NR 1 ENGINE TORQUE INDICATION BOTH ANALOGUE AND DIGITAL WENT TO TO ZERO AND NR 1 ECU WENT TO MANUAL MODE IN CLIMB. THE ANALOGUE TORQUE INDICATION WENT TO ZERO AND THE DIGITAL PORTION WENT TO DASHES. CLIMB POWER WAS SET TQ WAS 90 PERCENT BEFORE GUAGE WENApr 9, 2015 · Dhav DHC8301SDR JJBA20150302001Control Unit · malfunctionedNUMBER 2 ENG SHUTDOWN AT 500 FEET. AFTER NR 2 ENG SHUTDOWN PILOT HEARD PROP FEATHER ON ITS OWN. AUTO FEATHER WAS ARMED & UP TRIM LIGHT ILLUMINATED. NO FIRE INDICATIONS, CAUTION LIGHTS CAME ON AS NORMAL WHEN NR 2 ENG SHUT OFF. TORQUE WAS AT 97 JUST BEFORE PMar 2, 2015 · N360PH · Dhav DHC8202SDR HDNA201501230002Torque Sensor · unknownUPON APPROACH TO DESTINATION HELIPAD & AS POWER REDUCED BELOW 80% N1, NR 2 ENG WAS NOTED TO DROP TO 0% TORQUE WITH ASSOCIATED, ENG SPLIT, CAUTION. ATTEMPTS TO REJOIN FLI NEEDLES WITH COLLECTIVE N2 TRIM SWITCH MET WITH NEGATIVE RESULTS. OEI FLIGHT CONDITIONS Jan 23, 2015 · N131LF · Urocop BK117C1EUROSDR HNAA2015010700007Indicator · inaccurateWHEN APPLYING POWER ON TAKEOFF ROLL, NR 1 WENT TO 80 PERCENT. NR 2 WOULD NOT GO ABOVE 28 PERCENT. R & R NR 2 TORQUE INDICATOR IAW MM 77-10-00. ENGINE RUN IAW RUN UP MANUAL. OPS CHECKED GOOD.Jan 7, 2015 · N942HA · Dhav DHC8102SDR AALA20141210015Transmitter · failedDURING TAKEOFF CREW REPORTED RT ENGINE N3 INDICATION WAS ERRATIC. DURING CLIMB RT ENG BLEED VALVE WAS CYCLING OFF & ON, ACFT DID NOT PRESSURIZE. CREW TURNED OFF RT ENG BLEED & ACFT BEGAN TO PRESSURIZE. RETURNED TO DEPARTURE & EMERGENCY DECLARED. LANDING UNDec 10, 2014 · N690AA · Boeing 757223SDR AALA20141209016Transmitter · defectiveAIR INTERRUPT, RETURNED & EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB THE LT ENG BLEED OFF & LT PACK OFF INDICATORS ILLUMINATED. AT THE SAME TIME, THE RT CTR FUEL PUMP LOW PRESS LIGHT FLICKERED ON & OFF. R & R ENG SPEED CARD MDec 9, 2014 · N690AA · Boeing 757223SDR JJBA20141206002Tscu · malfunctionedNUMBER 1 ENG FAILED AFTER ACCELERATION. R & R NR 1 TSCU.Dec 6, 2014 · N375PH · Dhav DHC8202SDR CA141008003Indicator · malfunctioned(CAN) DURING LAST OPERATIONS BEFORE LANDING THE PILOT REPORTED THAT NR 1 ENGINE TORQUE INDICATION WAS DECREASING WHILE NR 2 ENGINE TORQUE WAS INCREASING. ITT THEN SUDDENLY DASHED OUT. THE PILOT ELECTED TO ABORT LANDING AND RETURNED TO POINT OF ORIGIN. ITT CSep 9, 2014 · Agusta AW139SDR CA141031001Warning Light · illuminated(CAN) CHIP LIGHT ILLUMINATED AND BOTH CHIP DETECTORS HAD MORE THAN PERMISSIBLE AMOUNT AND DIMENSIONS OF CHIPS. ENGINE SENT, INFORMATION RECEIVED SAYS TORQUEMETER BEARING FAILURE.Aug 25, 2014 · Bell 407
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