JASC 7603

Service difficulty reports · 1,582

Reports filed under 7603 · Power Lever, 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 = '7603'
  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 HALA2010060500241Throttle · fluctuatesATB - CLIMBING THROUGH 14,000' ENGINE L SYS FAIL LIGHT CAME ON. WHILE THROTTLE INDICATOR WAS FLUCTUATING ALONG W/THROTTLE. R & R THROTTLE MODULE IAW AMM 76?-01 7010/5295 ENG RUN PEND NR 1 ENGINE RUN ACCOMPLISHED ALL INDICATIONS NORMAL NO FAULTS FOUND, OK FORJun 6, 2010 · N477HA · Boeing 717200SDR HSYA2010060210Cable · looseAFTER ROTATION, CAPTAIN REPORTED AN UNCOMMANDED RT ENGINE AUTO FEATHER. THE ACFT RETURNED TO THE AIRPORT WITHOUT FURTHER INCIDENT ARRIVING BACK IN THE BLOCKS FOR MX TROUBLESHOOTING AND EVALUATION AT 1355Z. MX TROUBLESHOT ACFT AND FOUND BETA VALVE OUT OF ADJUSTJun 2, 2010 · N122GL · Beech 1900CSDR UALA2010052401769Switch · defectiveRT ENG WHEN MOVED TO CUTOFF STAYS AT 1.4 FUEL FLOW FOR 30 SECONDS. POSSIBLE PARTS THAT MAY BE RELATED TO THIS PROBLEM: RELAY K76207, K76204 & CUTOFF SWITCH S76200. REPLACED RT ENG FUEL CUTOFF SWITCH IAW MM. RAN ENGINE TWICE. OPS CK OK.May 21, 2010 · N771UA · Boeing 777222SDR DXTA2010051204093Throttle Cable · failedDURING AN OCF FOR THE RT ENG, THE ENG QUIT AFTER PULLING THE POWER LEVER BACK TO IDLE QUICKLY. ALSO, AFTER LANDING IT QUIT AGAIN AFTER A RAPID POWER LEVER REDUCTION. R & R RT AFT THROTTLE CABLE AND FUSELAGE CABLE IAW MM 76-12-03. OPS CHECK GOOD. AFT CABLE PMay 11, 2010 · N373QS · Cessna 560CESSNASDR 2010FA0000453Control Box · looseDURING MANUAL THROTTLE TRAINING, ON GROUND, IT WAS NOTICED THAT THROTTLES WERE NOT MOVING SYNCHRONOUSLY AND PLA INDICATION DID NOT MOVE WITH PILOT'S THROTTLE. AIRCRAFT WAS SHUTDOWN. AFTER TROUBLESHOOTING IT WAS FOUND THAT THE THROTTLE CONTROL BOX ASSEMBLY DIMay 2, 2010 · N207SM · Agusta A119SDR 2010FA0000427Control Cable · stuck(JX8S) IN CRUISE FLIGHT RT THROTTLE CONTROL BECAME STUCK DURING POWER REDUCTION. THE CONTROL TENSION WAS IMMEDIATELY CHECK /REDUCED BY MOVING FRICTION HANDLE. NO CHANGE NOTED. THE THROTTLE BECAME STUCK AT 24 " MAP NO MOVEMENT IN EITHER DIRECTION OBTAINABLE.Apr 27, 2010 · N157WM · Piper PA44180SDR USAA20100426SB059Push-Pull Cable · bindingCLT - ON DESCENT INTO CLT, CREW REPORTED THE NUMBER 2 THROTTLE WAS BINDING WITH AUTO THROTTLES ON. NUMBER 2 THROTTLE DOES NOT MATCH NUMBER 1 THROTTLE WITH POWER CHANGES; 2 THROTTLE KNOB WIDTHS. SOMETIMES IT "BREAKS" LOOSE AND MATCHES NUMBER 1 WITH A SEVERE JApr 23, 2010 · N454UW · Boeing 7374B7SDR NSVA201076Control Lever · malfunctionedABORTED TAKEOFF DUE TO CONFIGURATION WARNING. CREW RESET CONDITION LEVERS. FLIGHT CONTINUE TO IAD.Apr 19, 2010 · N220MJ · Saab 340BSDR 19MA201004141471Condition Lever · crackedON SHUT DOWN PILOT NOTICED CONDITION LEVER WAS LOOSE. UPON INSPECTION FOUND CONDITION LEVER WORN AND CRACKED MOST OF THE WAY THROUGH. INSPECTION REVEALED POSSIBLE CONSTANT RUBBING CAUSED WORN SPOT LEADING TO THINNING OF THE METAL AND FATIGUE FROM BENDING TO Apr 12, 2010 · N567MA · Beech 1900DSDR N93A03222010Throttle Cable · brokenCREW REPORTED LT THROTTLE IS LOOSE AND INOPERATIVE. MX FOUND LT THROTTLE CABLE BROKEN UNDER FLOOR IN AFT LAV JUST FWD OF WHERE CABLE TURNS UPWARD AT AFT LAV AFT WALL. CABLE APPARENTLY HAD BEEN FRAYING ON STRUCTURE PRIOR TO BREAKING.Mar 22, 2010 · N436QS · Gulstm GIVSDR DATA2010FA0000252Cable · brokenAFTER T/O, LT ENGINE THROTTLE WAS UNRESPONSIVE. ENG WAS SHUTDOWN. ACFT RETURNED BACK TO STATION. POWER CABLE WAS FOUND BROKEN IN FUSELAGE. UNKNOWN THE TRUE AGE OF THE CABLE SINCE IT IS NOT TRACKED.Mar 19, 2010 · N701A · Stbros SD360100SDR FDEA201003160836Cable · failedNR 2 THROTTLE STUCK AT 93 PERCENT AT FL 340 LOWER ALTITUDE AND STARTING APU AIRBORNE DID NOT UNFREEZE THROTTLE. SHUT NR 2 DOWN IAW QRH WINDMILLED FOR 17 MINUTES. RAN NR 2 ENG FOR A MINIMUM OF 3 MINUTES TO OIL/LUBE BRGS, BECAUSE OF WIND MILLING DUE TO INFLMar 16, 2010 · N398FE · Doug MD1010FSDR REXA201000032Solenoid · malfunctionedEN ROUTE FROM KFYM TO KMEM THE FLIGHT CREW RECEIVED A L REV UNLOCKED CAUTION MESSAGE. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. KMEM WAS DETERMINED TO BE THE NEAREST SUITABLE AIRPORT. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMar 2, 2010 · N8883E · Cndair CL6002B19SDR 22AA201000037Clutch · out of adjustNR 1 THROTTLE BINDS CAUSING UNSAFE AUTO THROTTLE OPERATIONS, LUBE NR 1 ENGINE THROTTLE BUT STICKS ON AUTO THROTTLE, ENTERED ON DMI NR 23456, CAT "C" IAW MEL 22-7. ADJUSTED NR 1 AUTO THROTTLE CLUTCH IAW MM 22-31-05, TESTED IAW MM 22-31-05 FOUND NORMAL, THIS CLFeb 15, 2010 · N526MD · Doug DC1030SDR CA100216009Rod · unserviceable(CAN) BOTH THROTTLE ACTUATOR RODS WERE FOUND WITH CHAFING DAMAGE RESULTING FROM CONTACT WITH THE ELEVATOR TORQUE TUBE ASSY PN 600-90410-803. THE CONTACT WAS WHEN THE THROTTLES WERE IN OR BETWEEN IDLE AND CUTOFF. LOCATION DAMAGE ON THE RODS IS AT THE FIRST BEFeb 14, 2010 · Cndair CL604SDR 2011FA0000153Throttle Control · looseTHROTTLE CONTROL ASSEMBLY - ON AFT END OF THE CONTROL, THE PILOT END OF THE PUSH/PULL CONTROL - THE THREADED ALUMINUM ATTACH FITTING IS LOOSE ON THE STEEL SLEEVE, NORMALLY A TIGHT FIT. ON THE FWD END OF THE CONTROL - THE ENGINE ATTACHMENT END , THE SLEEVE ISFeb 10, 2010 · Cessna TU206GSDR CA100127001Throttle Cable · sheared(CAN) ACFT WAS LEAVING AT ABOUT 0330AM. AT THE THRESHOLD, PILOT STARTED TO PUSH THE THROTTLES FWD, WHEN HE NOTICED THAT AT 60 PERCENT N1 THE RT ENGINE WAS ABNORMAL, RETARDED THE THROTTLE AND THE ENGINE SHUTDOWN. PILOT TRIED MULTIPLE RESTARTS, WITH NO SUCCESJan 23, 2010 · Lear 35ASDR AALA20100119SFO01Limit Switch · obstructedSJC - INFLIGHT DFW-SFO. CREW REPORTED LEFT ENGINE THROTTLE STUCK MID-RANGE. EMERGENCY DECLARED DIVERTED SJC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED DEBRIS THEN CLEANED AND LUBED THROTTLE LIMIT SWITCHES. SYSTEM GROUND CHECKED NORMALJan 18, 2010 · N9622A · Doug DC983SDR 2010FA0000046Throttle Cable · frozenON CLIMBOUT, PILOT TRIED TO BRING THROTTLES BACK BUT FOUND THE RT THROTTLE STUCK AT FULL POWER. ENG WAS SHUTDOWN AND ACFT LANDED WITH OUT INCIDENT. UPON INSP BY MX RT THROTTLE CABLE WAS FOUND TO BE CORRODED ON SHAFT WHERE IT EXITS THE PROTECTIVE OUTER HSG AT TJan 13, 2010 · N595ND · Piper PA44180SDR DXTA2010011103942Rod End · out of adjustBOTH THROTTLE LEVERS AT ALTITUDE BECOME EXTREMELY DIFFICULT TO MOVE. THE LT THROTTLE LEVER TAKES 2 HANDS AND EXCESSIVE FORCE TO MAKE ANY TYPE OF POWER CHANGE. AT LOWER ALTITUDES (10,000 AND BELOW) THROTTLE LEVERS SEEM NORMAL. REMOVED BOTH ENGINE THROTTLE CABLJan 9, 2010 · N322QS · Cessna 560CESSNASDR 2010FA0000169Throttle Cable · frayedTHROTTLE CABLE LOCKED IN FLIGHT, EXAMINATION FOUND PARTIAL FAILURE OF INTERNAL CABLE APPROX I5 CM FROM SWAG AT CONTROL KNOB END OF ASSY. BELIEVE FAILURE TO BE CAUSED BY TURNING KNOB WHILE TIGHTENING THROTTLE LOCK OR BY ATTEPTING TO USE A VENIER CONTROL.Jan 8, 2010 · N57651 · Mooney M20JSDR FDEA201001080044Throttle · malfunctionedAFTER TAKEOFF, DURING CLEAN-UP, THROTTLES WOULD CONTINUOUSLY RETARD DUE TO AN UPPER FOOT ON THE PFD LOWERING BELOW PRESENT AIRSPEED. EVEN WITH AUTO THROTTLES OFF, THE THROTTLES WOULD NOT STAY ADVANCED PROBABLY DUE TO THE AIRPLANE TRYING TO PROTECT ITSELF DUE TJan 8, 2010 · N314FE · Doug DC1030FSDR CA100107001Throttle Cable · broken(CAN) UPON ARRIVAL AT THE GATE, LT ENG WOULD NOT SHUTDOWN WITH THRUST LEVER. ENGINE SHUTDOWN ONLY AFTER SELECTING THE LT ENG FIRE SWITCH. INSPECTED LT ENG, FOUND BAD THROTTLE GEAR BOX AND BROKEN THROTTLE CABLE. LT ENG THROTTLE CABLE FROM GEAR BOX TO PYLONDec 22, 2009 · Cndair CL6002B19SDR CA091218003Power Lever · stiff(CAN) CAPTAIN REPORTED THE NR 1 THRUST LEVER WAS STIFF TO OPERATE AND GETTING WORSE AS FLIGHT CONTINUED. A RETURN TO THE FIELD OF DEPARTURE WAS CARRIED OUT. (TC NR 20091218003)Dec 17, 2009 · Cndair CL604SDR CA091223007Rod · binding(CAN) LEFT HAND ENGINE TORQUE DOES NOT DECREASE WHEN POWER LEVER IS RETARDED. LEFT EGINE INSPECTED FOUND AFT FUEL CONROL INTERCONNECT ROD END BIDING AND HOLDING PCU ARM AT A HICH POWER SETTING. AFT ROD END REALIGNED, CLEANED, AND LUBRICATED. AIRCRAFT GROUNDDec 8, 2009 · Beech A100SDR 2010FA0000006Shaft · wornPARTIAL POWER LOSS AT 200 FT AGL. ACFT SUCCESSFULLY LANDED OFF AIRPORT WITHOUT DAMAGE. INSP OF CARBURETOR FOUND FUEL STAINS AROUND THROTTLE SHAFT ON BOTH SIDES- ACCELERATOR PUMP END AND THROTTLE ARM END. UNIT DISASSEMBLED. FOUND SHAFT WEAR EXCESSIVE AND CODec 7, 2009 · N9KA · Cessna 152SDR E81RJT227063Switch · failedINVESTIGATED FLIGHT CREW WRITE-UP OF TAKEOFF WARNING SYS INOPERATIVE. FOUND RT POWER LEVER TAKEOFF WARNING SWITCH ASSY TO HAVE HIGH INTERNAL RESISTANCE. REPLACED SWITCH ASSY AND ADJUSTED AS REQUIRED IAW THE MM 76-11-00. TAKE-OFF WARNING SYS CHECKS OK. RECODec 7, 2009 · N202RL · Cessna 560XLSDR HALA2009120500573Actuator · malfunctionedETOPS SIGNIFICANT SYS - BTB "ENG VALVE" LGT REMAINED ILLUMINATED WITH FUEL CONTROL SWITCH IN RUN POS EICAS MSG: "R ENG FUEL VAL" DISPLAYED. PERFORMED FIM 76-11-00 FIGURE 107A, REPLACED RT ENG CONTROL ACTUATOR IAW AMM 76-11-04, OPS CHECK GOOD.Dec 5, 2009 · N598HA · Boeing 767332SDR 2010FA0000028Throttle Cable · brokenPILOT REPORTED DURING LANDING, THROTTLE WAS NOT GOING FULLY TO IDLE THEN SUDDENLY SOMETHING BROKE AND ENGINE WENT TO FULL POWER. AFTER FURTHER INVESTIGATION FOUND THROTTLE CABLE BROKEN WHERE IT COMES THRU THE FIREWALL. PROBABLE CAUSE UNKNOWN, NO RECOMMENDATIDec 3, 2009 · N861AF · Grob G120ASDR REXA200900129Gearbox · out of rigEN ROUTE FOR KTYS TO KLGA THE LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE ILLUMINATED. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT WAS DIVERTED TO KIAD. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KIAD. MAINTENANCE Dec 3, 2009 · N841AY · Cndair CL6002B19SDR CA091127007Lever · separated(CAN) DURING THE DOWNWIND LEG, PRIOR TO LANDING, THE THROTTLE KNOB UNEXPECTANTLY SEPARATED FROM THE THROTTLE LEVER WHEN THE PILOT SOUGHT TO REDUCE POWER FOR THE DESCENT. THE PILOT WAS ABLE TO CONTINUE THE APPROACH AND LANDING UNEVENTFULLY BY MANIPULATING THE LNov 23, 2009 · Piper PA28140SDR 2009FA0000965Throttle Cable · frozenDURING CRUISE FLIGHT CREW DISCOVERED RT THROTTLE STUCK. ACFT RETURNED TO BASE LANDED WITH OUT INCIDENT. UPON DISASSEMBLE THE THROTTLE CABLE WAS FOUND TO BE FROZEN AT THE ENG SIDE BETWEEN SHAFT AND THE PROTECTIVE SHEATH. THIS HAS HAPPENED ON OTHER ACFT OPERANov 19, 2009 · N595ND · Piper PA44180SDR HALA2009111400527Throttle · lack of lubeETOP SIGNIFICANT SYS - RT ENG THROTTLE STICK/BINDS. CLEANED AND LUBED THRUST LEVER (RT ENG) MECHANISM AT LEVER QUADRANT AND CLUTCH PACK ASSY OPS CKS NORMAL REF AMM 76-11-00, NO DEFECTS NOTED.Nov 14, 2009 · N596HA · Boeing 767332SDR CA091121002Cable · broken(CAN) ON START UP, RPM WENT TO 2300 WITH THROTTLE CONTROL AT IDLE. INSPECTION REVEALED THAT INNER THROTTLE CABLE HAD BROKEN. NEW CABLE INSTALLED. (TC NR 20091121002)Nov 13, 2009 · Diamon DA20C1SDR HALA2009111300525Throttle · misalignedETOPS SIGNIFICANT SYS - FRM 73032501 IN CRUISE FL300 A/C THROTTLES ARE MISALGINED 7/8 OF KNOB DIFFERENCE TO GET ENG PARAMETERS THE SAME WE ADJUSTED LT SIDE IT WAS 7/8 BEHIND R SIDE. INFO NOTED MOC NOTIFIED ACCOMP FIM 73-21-00 FIG 107 BITE PIMU LT AND RT OK INov 13, 2009 · N586HA · Boeing 7673G5SDR HALA2009111300524Throttle · misalignedETOPS SIGNIFICANT SYS - FRM 73032501 IN CRUISE FL300 ACFT THROTTLES ARE MISALGINED 7/8 OF KNOB DIFFERENCE TO GET ENG PARAMETERS THE SAME, ADJUSTED LT SIDE IT WAS 7/8 BEHIND R SIDE. INFO NOTED MOC NOTIFIED ACCOMP FIM 73-21-00 FIG 107 BITE PIMU LT AND RT OK IANov 13, 2009 · N586HA · Boeing 7673G5SDR CA091112004Lever · worn(CAN) THE ALUMINUM INPUT LEVER ARM THAT GOES ONTO THE SHAFT FOR THE ENGINE CONTROL CAMBOX, LOCATED ON THE ENGINE, SLIPPED ON THE SHAFT CAUSING A RE-INDEXING OF THE ENGINE RIGGING, PILOTS WERE UNABLE TO REDUCE THE POWER TO IDLE. THIS IS A VERY POOR DESIGN FROMNov 10, 2009 · Beech 1900CSDR AXSA189WA11709Linkage · frozenFLIGHT 1130 BUF-PBG - WHILE ON DESCENT TO PBG THE PILOT REDUCED POWER TO THE LEFT ENGINE BUT THE ENGINE DID NOT RESPOND. THE PILOT INDICATED THAT POWER COULD BE INCREASED BUT WOULD NOT REDUCE BELOW 1200LBS/TQ AND 92 PERCENT NG. THE PILOT ELECTED TO SHUTDOWN Nov 7, 2009 · N189WA · Beech 99SDR CA091121001Cable · frayed(CAN) DURING GROUND OPERATION IT WAS NOTED THAT THE THROTTLE CABLE MOVEMENT WAS ROUGH AND CATCHES HALF WAY. INSPECTION REVEALED THAT THE INNER PART OF THE CABLE WAS STARTING TO FRAY AND CATCHING IN THE AREA WERE IT PASSES THROUGH THE FIREWALL. NEW CABLE INSTNov 1, 2009 · Diamon DA20C1SDR EVGR20091028Bearing · separatedBEARING FAILED, SB-62 PREVIOUSLY COMPLIED WITH, WHICH INSTALLED LARGE AREA WASHERS. THE WASHERS DID THEIR JOB AND PREVENTED THE BEARING FROM FALLING APART AND CAUSING LOSS OF THROTTLE CONTROL.Oct 26, 2009 · N622 · Robsin R44RAVENIISDR DL75E091626Throttle · malfunctionedAFTER NORMAL ENG START ON LT ENG, NO RESPONSE TO ENG WHEN THROTTLE ADVANCED FOR TAXI. NO EICAS MSG. UPON RESTART AT THE GATE ALL INDICATIONS NORMAL, ENG RUN AT GATE. ALL INDICATIONS NORMAL. THROTTLE ADVANCE NORMAL, ETOPS CATEGORY 'E': PROBLEMS WITH SYS, CROct 10, 2009 · N752AT · Boeing 757212SDR Q2SA749007Control Box · wornIN FLIGHT FROM PANC TO RKSI, CREW HAD NO FORWARD THROTTLE MOVEMENT RESPONSE ON ENGINE NR 3, THE ENGINE RESPONDED NORMALLY DURING RETARDING THROTTLE MOVEMENT. CREW SHUT DOWN ENGINE NR 3 AS PRECAUTION ON TOP OF DESCENT INTO RKSI AND LANDED SAFELY AT RKSI. AFTEOct 10, 2009 · N749SA · Boeing 7473B5SDR 2009FA0001045Throttle · jammedCHECK LEFT THROTTLE OPERATION, PILOT REPORTED LT THROTTLE JAMMED. INSP LT THROTTLE CABLING AT ENG AND AT INSTRUMENT PANEL, NO DEFECTS NOTED. THROTTLE OPERATED SMOOTHLY THROUGH FULL RANGE OF TRAVEL. INSP OF LT THROTTLE, REVEALED THAT THE SMALL CONDUIT HSG THOct 7, 2009 · N2022T · Beech 58SDR REXA200900114Throttle Cable · brokenFLIGHT 4107 MOT/MSP ATC REQUESTED A DESCENT TO BEGIN APPROACH INTO MSP, WHEN THROTTLES RETARDED THE LEFT WAS FOUND TO BE INOPERATIVE, NO ENGINE CHANGE WITH THROTTLE MOVEMENT. QRH FOLLOWED FOR "STUCK THROTTLE" AND ENGINE SHUTDOWN. EMERGENCY DECLARED AND LANDEOct 3, 2009 · N8506C · Cndair CL6002B19SDR CA091021013Throttle Cable · broken(CAN) TWO CONTROL CABLES ARE BOLTED TO A SINGLE THROTTLE CONTROL LEVER IN THE CABIN PEDESTAL. THESE INNER CABLES ARE THEN ROUTED THROUGH THEIR OWN RESPECTIVE OUTER SHEATHS AND CONNECTED TO EACH CARBURRETOR THROTTLE LEVER. THE RIGHT INNER CABLE BROKE AND SEPATSep 23, 2009 · Diamon DA20A1SDR DXTA2009092303796Throttle Cable · brokenWHILE ATTEMPTING TO SET T/O POWER, NR 1 THROTTLE WOULD NOT REMAIN IN T/O DETENT. TAKEOFF ABORTED, NR 2 ENG SHUTDOWN NORMALLY. IN THROTTLE CUTOFF, NR 1 ENG ACCELERATED TO APPROX 72 % N1. WITH EECS SELECTED TO MANUAL, NR 2 ENG NORMAL. PRIOR TO SELECTING EECS MSep 22, 2009 · N661QS · Cessna 560XLSDR SWIA200922730Control Cable · corrodedPOWER LEVER CONTROL CABLES CORRODED. (C-CHECK) REPLACED PER AMM.Sep 14, 2009 · N224SW · Emb EMB120ERSDR CA090911002Control Cable · dislodgedRT THROTTLE STICKING PERIODICALLY AND WILL NOT ALLOW MORE THEN 30-36" OF POWER. CABLE FOUND POPPED OUT OF PULLY GROOVE AT FIREWALL PULLY CLUSTER AND FOUND SITTING IN BETWEEN TWO PULLEYS.Sep 10, 2009 · Gruman FIRECATSDR CA090826011Servo · stickingTHROTTLE PLATE STUCK ON ENG RUN UP RPM WOULD NOT GO BELOW 2000 RPM. WHEN SERVO INJECTOR WAS REMOVED FROM ENG, THROTTLE PLATE WAS MOVING FREELY AGAIN. THROTTLE SHAFT BUSHINGS SHOWED SIGNS OF EXCESSIVE WEAR. THIS PART WAS HIGH TIME.Aug 24, 2009 · Piper PA60600SDR GLBA20090821APower Cable · out of rigAIR RETURN, DUE TO UNAVAILABILITY OF PWR ON THE NR 2 ENG. PILOTS REPORTED THAT AN AIR RETURN OCCURRED DUE TO THE UNAVAILABILITY OF PWR ON NR 2 ENG. MX RIGGED RT ENG PWR CABLE ROD END IAW. OPS CHECK WAS GOOD. RII INSP COMPLIED IAW TASKCARD 4.3.13 AND WAS FOUAug 21, 2009 · N178YV · Beech 1900D
Back to JASC 7603