JASC 7321

Service difficulty reports · 2,878

Reports filed under 7321 · Fuel Control/Turbine Engines, 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 = '7321'
  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 CA120717003Fuel Control · fluctuates(CAN) DURING REPOSITIONING FLIGHT, WHILE IN CRUISE, CREW NOTICED NR 2 ENGINE TORQUE FLUCTUATION. JUST PRIOR TO DESCENT, NR 2 PARAMETER DROPPED TO IDLE. THE POWER SECTION FLAMED OUT AS THE PILOT CLOSED THROTTLE TO IDLE. ACFT DIVERTED AND LANDED WITHOUT INCIDEJul 10, 2012SDR UALA2012071103734Actuator · faultyENG CONTROL L STATUS MSG. ACCOMPLISHED FIM 75-31 TASK 811 ENG CHECK 4 VARIABLE STATOR VANE SYS 71-08 816. ALL CORRESPONDING VALUES ON EPCS PAGE NORMAL. PERFORMED ENG RUN, ALL OKAY NO STS MSG. REPLACED SVA. ALL CHECKED OKAY. NO LEAKS EVIDENT.Jul 8, 2012 · N218UA · Boeing 777222SDR UALA2012071103729Sensor · faultedSTATUS MESSAGE "L ENG EEC C1" DISPLAYS ALONG A-T DISCONNECT. REPLACED N1 SPEED SENSOR 514020 SERIAL NR VP3758 PER AMM. RAN ENGINE AT IDLE NO LEAKS. PERFORMED AUTOTHROTTLES CAT 3 TEST MM TEST 30, ALL TESTS PASSED.Jul 7, 2012 · N660UA · Boeing 767322SDR UALA2012071103732O-Ring · leakingNR 1 ENGINE FMU LEAKING PROFUSELY AT BLUE END CAP. NOTED PACKING PROTRUDING. ORDERED NEW PACKING. RAN 5 MIN IDLE NO LEAKS NOTED. REPLACED LEAKING O-RING FUEL CONTROL WITH NEW.Jul 7, 2012 · N589UA · Boeing 757222SDR ASAA2012070692503Hmu · faultyWHILE ACCOMPLISHING T/C 78273000, FOUND FAULT 75-20581, TBV DEMAND AND POSITION SIGNAL DISAGREE. FAULT CAUSES ENG CONTROL LIGHT. NO GO FAULT NR 1 ENGINE. ACCOMPLISHED FIM 75-23, TASK 801, NO FAULTS FOUND, ALL VALUES WITHIN LIMITS DUE TO HISTORY OF TBV AND LJul 6, 2012 · N508AS · Boeing 737890SDR USAA2012070600006Eec · surgesPRIOR TO 1,000 AGL ENGINE 1 SHUT DOWN - ECAM ACTIONS COMPLETED DURING DOWN WIND - POPPING SOUND COMPRESSOR STALL. COMPLIED WITH TROUBLESHOOTING AND ENGINEERING REQUEST. REMOVED AND REPLACED FMU, FUEL PUMP, AND EEC. COMPLIED WITH FUNCTIONAL CHECK OF BLEED VAJul 4, 2012 · N820AW · Airbus A319132SDR CA120702011Fuel Control · unknown(CAN) IN FLIGHT RECEIVED L/T FADEC FAULTY ICAS MSG AND EICAS COMPARITOR FAIL WITH YELLOW DASH LINES IN THE ITT. ABOUT 5 MIN LATER WE FELT A LIGHT SHUTTER ASSOCIATED WITH THE ENGINE ROLLING BACK AND FAILED. AFTER ABOUT 30 SEC THE ENGINE AUTO LIGHTED. NO ABNOJun 28, 2012 · Propjt 200ASDR KCSA20120625007Fcu · malfunctionedNR 2 ENGINE SHUTDOWN DUE EGT EXCESSIVE AND PARAMETERS UNCONTROLLABLE IN CLIMB. WINDMILL PROCEDURES COMPLIED WITH. PERFORMED EVBC TRIM IAW B747 AMM 71-00-00 TEST 8, NO DEFECT NOTED. TROUBLESHOT NR 2 ENGINE IAW FIM 71-01-00 REMOVED AND REPLACED NR 2 ENGINE FUJun 25, 2012 · N794CK · Boeing 747222BSDR FDEA201206232320Fuel Control · malfunctionedFLEX PWR SET FOR 50 PERCENT, THROTTLES ADVANCED SMOOTHLY WHEN AUTOFLT SELECTED TO THE APPROPRIATE REDUCED PWR CHEVRON INDICATED SETTINGS ON THEN 1 GUAGE. THROTTLES CLAMPED NORMALLY PRIOR TO 80KTS. AFTER 80 KTS THE NR 3 ENGINE BEGAN NOTICEABLY SURGING WITH NJun 23, 2012 · N370FE · Doug MD1010FSDR SWAA2012062105143Mec · malfunctionedUPON DESCENT BOTH ENGINES ROLLED BACK. REMOVED AND REPLACED CIT SENSOR, VBV GEAR MOTOR, MEC AND FUEL PUMP PER MM.Jun 18, 2012 · N615SW · Boeing 7373H4SDR CA120629001Fuel Control · failed(CAN) BOTH ENGINES HAVE FAILED TO START. ABORTED CURRENT RT ENGINE START, ATTEMPTED ANOTHER START AND IT FAILED AGAIN, RESET THE BREAKERS AND CLEARED THE PROBLEM. CAIMS SHOWED RT FMU, HP SOV FOR BOTH CHANNELS A & B. SIMILAR ISSUE OCCURRED ON LT ENGINE. USE OJun 14, 2012 · Bombdr BD7001A10SDR 2012FA0000513Fuel Control · failedPILOT REPORTED THAT THE ENGINE DID NOT RESPOND TO POWER LEVER MOVEMENTS AND WAS UNABLE TO CONTROL ENGINE POWER. ENGINE WAS OVER TEMPING AND OVER TORQUING. HE THEN FLEW TO A NEAR BY AIRPORT AND USED EMERGENCY SHUTDOWN CONTROL TO SHUTDOWN THE ENGINE. LANDING Jun 10, 2012 · N70WY · Swrngn S2RG6SDR CA120702001Fuel Control · malfunctioned(CAN) DURING CRUISE AT FL190, THE ENGINE POWER INCREASED UNCOMMANDED FOR 3 SECONDS AND THEN RETURNED TO NORMAL. THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL UNTIL SHORT FINAL WHEN THE POWER LEVER WAS REDUCED TO FLIGHT IDLE, THE TORQUE WAS STILL READING 12 PSI IJun 7, 2012 · Pilats PC1245SDR QMLA2012060112092Fcu · out of tolerancePERFORMED ENGINE ZONE 8 INSPECTION, RUN UP AND LEAK CHECKED, AND STARTED POWER CHECK PROCEDURE. N1, N2 AND TORQUE FLUCTUATING, 1-2 PERCENT ON N1, 2-3 PERCENT ON THE TORQUE. INSPECTED P2 LINE, PERFORMED LEAK CHECKS, AS DIRECTED BY THE TECH REP AND RAN UP AGAJun 1, 2012 · N587MH · Bolkms BK117C2SDR CA120604017Fuel Control · malfunctioned(CAN) ON CLIMBOUT, THE PILOTS REPORTED THAT THROUGH 18,000 FT THE POWER LEVERS WOULD DEVELOPED A 3 KNOB SPLIT AND THE RT ENGINE WOULD HAVE A ITT, TEMPERTURE INCREASE OF 35 DEGREES. ONCE THE ACFT REACHED DESIRED ALTITUDE, THE POWER LEVERS WOULD MATCH UP OVER TMay 30, 2012 · Beech B200SDR CA120605005Line · broken(CAN) DURING APPROACH, AN ENGINE POWER LOSS OCCURRED. THE ACFT LANDED SAFELY AND POST FLIGHT INSPECTION FOUND A BROKEN P3 AIR SENSING TUBE AT THE FUEL CONTROL. THE TUBE WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE.May 23, 2012SDR AALA20120518006Fuel Control · defectiveDFW - CREW REPORTED LEFT ENGINE PARAMETERS FLUCTUATING. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE FUEL CONTROL. SYSTEM GROUND CHECK NORMAL OPERATION.May 18, 2012 · N7538A · Doug DC982SDR QMLA2012051812083Fcu · unserviceableFUEL LEAKING FROM OVERBOARD DRAIN DETECTED AFTER ENGINE SHUTDOWN FROM GROUND RUN LEAK CHECK FOR PERFORMED MX NOT ASSOCIATED WITH THIS FAILURE. TROUBLESHOOTING IAW MM REVEALED THAT THE FCU HAD FAILED, LEAKING FUEL AT A RATE WELL ABOVE THAT ALLOTED BY MFG. CONFEMay 18, 2012 · N854UH · Bolkms BK117C2SDR USAA2012051700016Hmu · malfunctionedON TAKEOFF ROLL, LEFT ENGINE NEVER REACHED TAKEOFF POWER. ABORTED TAKEOFF AT 85 KTS. MAINTENANCE REMOVED AND REPLACED LEFT HYDROMECHANICAL UNIT IAW AIRBUS MAINTENANCE MANUAL 73-21-10.May 16, 2012 · N191UW · Airbus A321211SDR QMLA2012051412081Fcu · leakingCREW MEMBER SMELLED FUEL. COULD SEE LIQUID ON THE RT REAR CLAM SHELL GLASS WINDOW. CONTINUED FLIGHT AND LANDED WITHOUT INCIDENT. AFTER LANDING, FOUND THE FUEL CAP SECURE, BUT FUEL ON NR 1 ENGINE DECK AND ON THE ACFT SKIN BELOW AND AFT OF THE ENGINE DECK. May 14, 2012 · N101VU · Bolkms BK117C2SDR CA120524005Fuel Control · malfunctioned(CAN) AFTER T/O, THE ENGINE POWER COULD NOT BE REDUCED. THE FLIGHT WAS DIVERTED AND THE ENGINE WAS NOT SHUTDOWN BY PRECAUTION. THROTTLE CONTROL WAS EVENTUALLY RE-GAINED AND THE ACFT LANDED SAFELY. POST FLIGHT INSPECTION FOUND NO ISSUES WITH THE THROTTLE CONTMay 11, 2012SDR CA120524003Fuel Control · malfunctioned(CAN) DURING FLIGHT, 40 SECONDS AFTER RETURNING THE FUEL CROSS FEED VALVE OF BOTH ENGINES FROM AFT TO NORMAL, THE ENGINE SHUT ITSELF DOWN. A RE-START WAS ATTEMPTED AND WAS SUCCESSFUL. THE ACFT LANDED SAFELY, AFTER WHICH TROUBLESHOOTING LED TO THE REPLACEMENT OMay 10, 2012 · Dhav DHC6300SDR 2012FA0000296Fcu · inoperativeWHILE IN FLIGHT, ACFT RPM`S AND N2 CLIMBED QUICKLY. RAISED COLLECTIVE AND ROLLED THROTTLE DOWN UNTIL THE RPM`S STABILIZED. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. TROUBLESHOT SYS, FOUND THE FUEL CONTROL WAS NOT FUNCTIONING PROPERLY. A REPLAMay 10, 2012 · N315SH · Hughes 369DSDR USAA2012050700013Eec · faultyON LANDING ROLL OUT ENGINE 1 THRUST REVERSER SHOWED AMBER AND NO REVERSE THRUST WAS FELT ON ENGINE. NO ECAM WARNINGS OR FAULTS. ENGINE 1 THRUST REVERSER DEACTIVATED AND PLACED ON MEL. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ELECTRONIC ENGINE CONTROL (EMay 5, 2012 · N553UW · Airbus A321231SDR UALA2012050302613Fmu · faultedNR 1 ENGINE HAD AN OVERSPEED FAULT. MAINTENANCE INTERROGATED CFDS LAST LEG AND LAST LEG ECAM REPORTS SHOW 7 3-22-52, FADEC 1A AND 1B CELLS 07 AND 08 HAVE MULTIPLE HITS OF FAULT CODE, OSFFMU, ALSO ACCOMPLISHED ENG 1 FADEC BOTH CHANNELS GROUND SCAN AND SELF TESMay 2, 2012 · N809UA · Airbus A319131SDR ASAA12511478Fuel Control · malfunctionedWHILE PERFORMING TC 78273000, FOUND FUEL CONTROL 73-10321, HMU FMV CONTROL CURRENT IS OUT OF RANGE. SHORT TIME FAULT NR 1 ENG. ACFT GROUNDED. REPLACED NR 1 ENG EEC IAW AMM 73-21-60-000-801 F00 AND 73-21-60-400-801 F00. PERFORMED TESTS LISTED IN THE POWER PApr 27, 2012 · N584AS · Boeing 737890SDR 9JLA2012071600799Fuel Control · leakingCREW REPORTED THE NR 2 ENGINE FUEL CONTROL IS LEAKING WITH THE APU RUNNING. THE LEAKING FUEL CONTROL WAS REMOVED AND A O/H FUEL CONTROL WAS INSTALLED ONTO ENGINE. FUNCTIONAL CHECKS SATISFACTORY.Apr 23, 2012 · N904HD · Lear 45LEARSDR CA120507003Fuel Control · malfunctioned(CAN) DURING T/O, BEFORE V1 SPEED, THE PILOT OBSERVED A REDUCTION OF ALL PARAMETERS OF ENGINE NR 1 A TORQUE DROP TO 0. THE T/O WAS ABORTED AND THE ACFT WAS RETURNED TO THE RAMP. POST EVENT INSPECTION FOUND A FRACTURED P3 AIR TUBE. THIS IS THE SECOND SIMILARApr 18, 2012SDR G1IAN20120427001Fuel Control · erraticSUPPLEMENTAL RECORD - THE LEFT FUEL CONTROL UNIT WAS REPLACED WITH A OVERHAULED UNIT. OPS CHECK NORMAL AND FLIGHT CHECK NORMAL.Apr 17, 2012 · N81MR · Lear 35ASDR UALA2012041702297Wire Harness · defectiveNR 2 ENG OVERTEMP, RTFL. PERFORMED BOROSCOPE INSP AS PER MM 72-00-97. CHECKED COMPESSOR BLADES, NO DEFECTS, TURBINE BLADES, COMBUSTER BORE. REPLACED NR 2 ENGINE 14 STAGE CONVERTER VALVE PER MM. ACCOMPLISHED IDT INSPECTION OF NR 2 ENGINE 14 STAGE CONVERTERApr 16, 2012 · N532UA · Boeing 757222SDR DALA1221130660Fcu · inoperativeNR 1 ENGINE HAD LOSS OF THRUST PRIOR TO TOP OF DESCENT. UNRESPONSIVE TO THROTTLE INPUT. FOLLOWED COM ENGINE FAILURE CHECKLIST, AND SHUT ENGINE DOWN. LANDED AT DESTINATION UNEVENTFULLY. REPLACED ENGINE DRIVEN FUEL PUMP, FCU, EEC, MAIN OIL FILTER, INSPECTED Apr 7, 2012 · N660DL · Boeing 757232SDR CA120405004Fuel Control · malfunctioned(CAN) DURING DESCENT, BOTH THRUST LEVERS WERE RETARDED TO IDLE. THE RT ENGINE FLAMEDOUT. THE CREW ELECTED TO CONTINUE WITH THE APPROACH SINGLE ENGINE. THE CUSTOMER IS REQUESTING TROUBLESHOOTING GUIDE LINES. ACFT WAS 5.5 HRS INTO FLIGHT LEG, STARTING DESCENTApr 4, 2012 · Cndair CL6013ASDR USAA2012040600008Fmu · cokedON TAKEOFF, AS THRUST WAS INCREASED, NR 1 ENGINE EPR STAGNATED AT APPROXIMATELY HALFWAY POINT AND THEN ENGINE FAILED ECAM APPEARED. TAKEOFF ABORTED, NR 1 ENGINE WAS SHUTDOWN. ENGINE CONTINUED TO SMOKE. REMOVED AND REPLACED ENGINE 1. VENDOR (IAE) TEARDOWN RApr 1, 2012 · N836AW · Airbus A319132SDR CA120402004Fuel Control · malfunctioned(CAN) ACFT ABORTED TAKEOFF BECAUSE ENGINE POWER WAS UNMATCHED. CONDUCTED RUN-UP AND FOUND NO PROBLEMS, STATIC RUN ON GROUND ABLE TO ACHIEVE 95 PERCENT TORQUE AS WELL. STATIC POWER CHECK CONDUCTED AGAIN JUST BEFORE TAKEOFF WITH NO PROBLEMS. AT 2000 FT AGL THEMar 31, 2012 · Beech B300SDR UALA2012032301858Fuel Control · leakingNR 1 ENGINE HAS FUEL LEAK. FUEL LEAKING FROM TOP COVER ON FUEL CONTROL. RMV'D FUEL CONTROL PER AMM. REPLACED FUEL CONTROL.Mar 23, 2012 · N571UA · Boeing 757222SDR UALA2012031301659Fmu · faultyREPLACE FUEL PUMP AND METERING UNIT FMU AS FOLLOW UP TO TAILPIPE FIRE REMOVED NR 1 ENGINE FMU REF MM. MR73205-57 OFF PER EG6769-1. REPLACED NR 1 ENG FUEL METERING UNIT PER MM, REFERENCE EG6769-1.Mar 12, 2012 · N791UA · Boeing 777222SDR UALA2012030501376Eec · faultyENG 2 FADEC B FAULT, RTFL. WITH FADEC2 GRD POWER SWITCH ON, NO RESPONSE WHEN FADEC 2A AND 2B LINE SELECT KEYS PRESSED ON MCDU FOR CFDS TEST. EIU-2 GROUND SCAN SHOWED NO FAILURE. EEC PCN 482-9585, EIU PCN 482-9526. REPLACED NR 2 ENG EEC PER MM. OPS CHECK GMar 5, 2012 · N498UA · Airbus A320232SDR UALA2012030701507Fmu · faultyNR 1 ENG WOULD NOT SHUT DOWN AFTER TWO ATTEMPTS. FUEL VALVE L ENG STATUS. MAINT MSG 73-60211. STATUS MSG WAS ALSO DISPLAYED WHEN ACFT WAS PICKED UP FROM GATE. ACCOMPLISHED CALLOUT EG6740 (PTT SEQ 7032006), NO FAULTS, NO MESSAGES. NR 1 ENG REQUIRES START AMar 4, 2012 · N791UA · Boeing 777222SDR UALA2012030101276Eec · faultyNO REVERSE ABOVE IDLE REVERSE BOTH ENGINES. ON EPCS SHOWED P & S 2.5 BLEED-EEC, P351-25, S351-25, P350-22. CHECK WIRES FROM 2.5 BLEED TO EEC NO FAULTS FOUND. REPLACED EEC AND TESTED ON ENGINE RUN. BOTH ENGINES REVERSED AND INTERLOCK RELEASED ALLOWING REVERMar 1, 2012 · N550UA · Boeing 757222SDR UALA2012030101286Fmu · defectiveENG 3 OSCILLATING AT FL390 EVERY 2 SECONDS. EPR FROM 1.27 TO 1.35NI FROM 89 TO 90. REPLACED FMU PER MM.Feb 29, 2012 · N104UA · Boeing 747422SDR CA120312003Fuel Control · malfunctioned(CAN) DURING TAXI-OUT, 1 ENGINE ROLLED BACK TO SUB-IDLE AND SEEMED TO HUNG. THE ENGINE WAS SHUTDOWN AND LARGE AMOUNT OF SMOKE APPEARED IN THE BACK. STREAM OF FUEL POOLED UNDER THE ENGINE. ACFT WAS TOWED BACK TO ORIGIN. GROUND TECH CONFIRMED FUEL LEAKING FRFeb 27, 2012 · Beech 400ASDR UALA2012022701193Eec · malfunctionedENG EXPERIENCED A 'SILENT SURGE'. PLEASE REPLACE THE EEC MR73412 PCN 480-9191. REF MM 73-21-04 P4XX. PUT EG ALERT TAG ON REMOVED EEC. WRITE RMVL REASON AS "ROUTE TO HS FOR PB SENSORS RPLMNT. REF HS SB EEC131-73-62 DUE SURGE". REPLACED LT ENG EEC PER MM, Feb 26, 2012 · N643UA · Boeing 767322SDR CA120217008Fcu · malfunctioned(CAN) THE PILOT REPORTED DIFFICULTIES RELATING TO HUNG OR HOT STARTS, IN ADDITION TO ROTOR SPEED PROBLEMS. DURING AN INSPECTION AT THE END OF THE DAY, AIR WAS FOUND IN THE AIRFRAME FUEL FILTER SIGHT GLASS. MAINTENANCE TROUBLESHOOTING WAS SYSTEMATICALLY CARRIFeb 13, 2012 · Snias AS350BSDR HNAA2012020300554Hmu · failedPROGRESSIVE POWER LEVER SPLIT AFTER TAKEOFF APPROX 3 KNOB SPLIT, NR 1 POWER LEVER MAX TORQUE AT 70 PERCENT CHECKED RIGGING IAW 76-00-10Q, NO FIX. SWAPPED PROP GAUGES, NO FIX. SWAPPED GAUGES BACK TO ORIGINAL POSITION. R & R PCU IAW 61-10-10RQ, NO FIX. PROP GOFeb 3, 2012 · N938HA · Dhav DHC8102SDR 2012FA0000081Fuel Control · failedDURING RUNUP, PROP FEATHER CHECK CONDUCTED NORMALLY. WHEN ADVANCING POWER LEVER TO DO A PROP OVERSPEED TEST, COULD NOT REACH 1900 RPM WITH POWER LEVER FORWARD. HIGHEST RPM ACHIEVED WAS 1700. SHUTDOWN AND RESTART. DURING THE START, AT LOW IDLE, FLAMES SHOTJan 31, 2012 · N701QD · Socata TBM700SDR CA120131010Actuator · failed(CAN) LINEAR ACTUATOR FAILED, UNABLE TO TRIM ENGINE. DURING TROUBLESHOOTING TEST FLIGHT. ACFT SAFELY RETURNED TO BASE. ACTUATOR WAS REMOVED.Jan 30, 2012 · Bolkms BK117B2SDR QMLA2012012712014Fuel Control · leakingAFTER TAKEOFF, NOTICED FLUID ON THE HELIPAD WHERE THE HELICOPTER WAS SITTING. WHILE SETTING UP FOR FINAL APPROACH BACK TO BASE, RECEIVED COMMUNICATION THAT FLUID WAS IDENTIFIED AS JET FUEL. AFTER LANDING, NOTED FLUID COMING OUT OF NR 2 ENGINE DRAIN PORT. Jan 27, 2012 · N587M · Bolkms BK117C2SDR WOWY2012012601Fuel Control · unserviceableDISCOVERED OCCURRENCE WHEN A UNIT WAS RETURNED FOR AN N1 OVERSPEED EVENT. UNIT WAS RETURNED THOUGH THE REPAIR STATION AND INVESTIGATED AT MFG. HOWEVER, WE RECENTLY DISCOVERED THAT THE EVENT HAD OCCURRED ON THE 21ST OF MAY 2011. THE UNIT WAS FOUND TO HAVE A FJan 26, 2012 · Boeing 757*SDR CA120126002Actuator · failed(CAN) WHILE CARRYING OUT THROTTLE RIGGING ON NR 3 ENGINE FOUND FUEL CONDITION CONTROL MOTOR ACTUATOR WITH ONE OF THE 3 ATTACH LUGS BROKEN. NO SYMPTOMS DURING AIRCRAFT OPERATION (GRD ENGINE RUNS OR FLIGHTS). CHECKED AND FOUND ONE SB TARGETTING THAT SPECIFIC SIJan 25, 2012 · Boeing 747SPJ6SDR USAA2012012300034Servo Valve · failedPHL FLT 723 EN ROUTE DUB TO PHL. R ENG LOW OIL PRESS ON LANDING ROLL OUT; PRECEDED BY R GEN OFF INTERMITTENT INDICATIONS ON FINAL APPROACH. RIGHT ENGINE SHUTDOWN AT 1937Z. RIGHT OIL PRESSURE LESS THAN 10. REMOVED AND REPLACED ENGINE MEC ASSY. GRD RUN UP Jan 20, 2012 · N256AY · Boeing 7672B7ER
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