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 DXTA2008120403386Rod End · strippedRT ENGINE QUIT WHEN THROTTLE WAS BROUGHT TO IDLE. REMOVED AND REPLACED RT ENGINE FLOW DIVIDER ROD END AND RIGGED IAW MM 71-01-03. GROUND RUN OPS NORMAL IAW MM 71-01-03 AND MM 76-11-00.Dec 4, 2008 · N398QS · Cessna 560CESSNASDR CA081205004Control Cable · broken(CAN) DURING TAXI, CREW SELECTED SPEEDS HIGH & APPLIED POWER. AS POSITIVE TORQUES WERE CALLED TROUGH ABOUT 1200FT/LBS, A SNAP WAS HEARD & THE LT POWER LEVER ADVANCED FORWARD WITH NO FURTHER ENGINE POWER INCREASE. TAKEOFF ABORTED & CREW SLOWLY REDUCED POWER TNov 26, 2008 · Swrngn SA226TCSDR DXTA200811253373Throttle · out of rigDURING SPEED BRAKE CHECK, WHEN LT THROTTLE WAS BROGHT FWD AND RETURNED TO IDLE, ENGINE ROLLED BACK AND SHUT DOWN. RIGGED THROTTLE LINKAGE AND RAN ACFT STILL SHOT DOWN PERFORMED COMPLETE RIG ON THROTTLE, SAME AS NEW ENGINE INSTALL RAN ACFT TRIED SEVERAL TIMES Nov 25, 2008 · N393QS · Cessna 560CESSNASDR CA081118003Lock Tab · cracked(CAN) FCU FUEL CONDITION LEVER LOCK SPRING TAB THAT IS USED TO PREVENT THE LEVER MOVING TO FUEL CUT-OFF HAS FAILED.Nov 3, 2008 · Airtrc AT502BSDR 2008FA0000755Joint · damagedRT ENGINE POWER CONTROL CABLES FREEZING AT ALTITUDE. INSPECTED CABLE AND FOUND THE STAINLESS STEEL SLEEVE DISCONNECTED AT JOINT TO FLEX SLEEVE. IT APPEARS TO BE A SILVER SOLDERED JOINT, AND SOLDER FAILED ALLOWING MOISTURE TO ENTER THE INTERNAL OF CABLE AND FRESep 30, 2008 · N23RF · Piagio P180SDR CA080918005Spring · broken(CAN) DURING TAKEOFF THE LOW ROTOR HORN SOUNDED. THE PILOT ABORTED THE TAKEOFF, SHUT DOWN THE ENGINE AND CALLED MX. WHEN THE ENGINE COWL WAS OPENED THE FCU THROTTLE RETURN SPRING WAS FOUND IN THE BOTTOM OF THE ENGINE PAN.Sep 14, 2008 · Bell 206BSDR DXTA200809073266Control Lever · obstructedDURING TAXI OUT, CREW PERFORMED TR CHECK. LT THRUST REVERSER DEPLOYED NORMALLY WITH APPROPRIATE ANNUNCIATOR LIGHT SEQUENCE. RT THRUST REVERSER COULD NOT BE VERIFIED TO DEPLOY AND ASSOCIATED LIGHTS ON RT PANEL DID NOT ILLUMINATE. RT THRUST REVERSER PIGGYBACK LESep 7, 2008 · N101QS · Raythn 400ARAYTHEONSDR CA080811006Rod End · worn(CAN) THE FUEL CONTROL WAS BEING REPLACED ON THE RT ENGINE. WHEN THE STARTER GENERATOR WAS REMOVED IT WAS APPARENT THAT THE POWER LEVER, WHERE IT ATTACHES TO THE PROP PITCH CONTROL BY A ROD END, WAS SEVERELY WORN. THE TIME SINCE INSTALL IS NOT KNOWN, HOWEVER TAug 7, 2008 · Swrngn SA226TCSDR CA080722009Throttle Plate · failed(CAN) S61 ENGINEERS WERE REPLACING A EMERGENCY THROTTLE PLATE P/N S6130-62017-3 WITH A PLATE THAT HAD BEEN RECEIVED. ON INSTALLATION WHEN TIGHTENING THE BOLTS, THE PLATE SHATTERED AT THE FWD BOLT HOLE. ALL 10 PLATES RECEIVED IN FROM THIS VENDOR HAVE BEEN ACCOUJul 22, 2008 · Skrsky S61ASDR A6WA200840546Throttle Cable · lack of lubeRT THRUST LEVER DIFFICULT TO MOVE, SHUT OFF THROUGH FULL THROTTLE RANGE. CLEANED AND LUBED RT THROTTLE CABLE CONTROL SYSTEM IAW AWAC SUPP 05-028 AND IAW AMM 76-11-00. PERFORMED FUNCTIONAL TEST OF RT THROTTLE CONTROL GEARBOX ASSEMBLY, OPS CHECK NORMALLY IAW CJul 20, 2008 · N425 · Cndair CL6002B19SDR QRE2008F00000Rod End · bindingTHE PILOT MENTIONED UPON LENDING THE LT ENGINE NG DID NOT GO ALL THE WAY BACK TO IDLE SPEED, BUT STAYED AT 80 PERCENT. UPON EXAMINATION OF THE FUEL CONTROL LINKAGE, IT WAS NOTED THAT THE FUEL CONTROL ARM WAS NOT RESTING ON THE IDLE STOP, BUT WAS UP ABOUT 1 INJul 10, 2008 · N425WD · Cessna 425SDR SWIA200819842Linkage · brokenFLT 6736 - LEFT ENGINE WENT TO IDLE CUTOFF WHILE REDUCING POWER. REPLACED THROTTLE QUADRANT ASSEMBLY AS REQUIRED PER AMM 76-11-01, P/N: FE210-008, S/N OFF: FR-787.Jul 10, 2008 · N908SW · Cndair CL6002B19SDR CA080806010Cable Assy · broken(CAN) WHILE ATTEMPTING TO REDUCE RT ENGINE PWR AFTER TAKEOFF AND CLIMB, FLT CREW REPORTED THAT THE RT ENG WOULD NOT RESPOND TO THROTTLE LEVER INPUTS. THE RT ENGT WAS SHUTDOWN VIA FIRE PUSH SWITCH/LIGHT, ACFT DIVERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT.Jul 5, 2008 · Cndair CL6002B19SDR 08FDEA02396Nut · missingMISSING NUT ON BOLT SECURING NR 3 ENGINE THROTTLE CONTROL ROD INBD OF ENGINE. REMOVED AND REPLACED NUT, BOLT AND LOCK IAW FX B727 76-12-000-5.Jun 24, 2008 · N494FE · Boeing 727227SDR ARWA20080603Throttle · obstructedUPON INITIATION OF TAKEOFF ROLL NR 3 POWER LEVER WOULD NOT ADVANCE BEYOND 128 EPR. RETURNED TO RAMP. OPENED ENGINE FOUND HYD TEMP C/P WIRE AROUND THROTTLE BELL CRANK BEHIND HYD FILTER MODULE. SECURED WIRE IAW M/M 20-30-07. OPS CHECK THROTTLE IAW MM 76-11-0Jun 22, 2008 · N140WE · Doug DC1040FSDR MT9A0000001Screw · missingIN FLIGHT THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO THE LEFT ENGINE. THIS FORCED THEM TO DO AN IN-FLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND SPACER THAT SECURES TJun 19, 2008 · N26932 · Swrngn SA227ACSDR XV62008F00000Control Cable · obstructedR/S POWER LEVER WOULD NOT GO INTO GROUND IDLE AFTER LANDING. FOUND HINGE FROM COCKPIT DOOR INTERFERING WITH CABLES/ PULLEYS TRAVEL AT RT AVIONICS AFT SIDE. REMOVED FOD AS REQUIRED. CABLES/ PULLEYS GROUND RUN SATISFACTORY. A/C APPROVED FOR RTS. (K)Jun 3, 2008 · N331MX · Dorner DO328100SDR SWIA200819725Throttle · bindingLEFT THROTTLE OCCASSIONALLY BINDS AND IS STIFF. (FLT 3801) REPLACED ENGINE THROTTLE CABLE ON LEFT SIDE IAW AMM 76-11-09. ENGINE RUN CHECK GOOD.May 31, 2008 · N439SW · Cndair CL6002B19SDR MT9R00000040Power Lever · brokenENGINE CONTROL QUADRANT POWER LEVER SPRING STOP BROKEN. (K)May 30, 2008 · N1324G · Cessna 208BSDR 2008FA0000366Arm · brokenBOLT CONNECTING CARBURETOR THROTTLE ARM TO THROTTLE CABLE FAILED RESULTING IN THROTTLE STICKING OPEN. PILOT PLACED MIXTURE CONTROL IN IDLE CUTOFF POSITION AND ATTEMPTED TO GLIDE TO RUNWAY AT AIRPORT. AIRCRAFT IMPACTED POWER LINES SHORT OF RUNWAY. BOLT WAS NOT May 24, 2008 · N75528 · Cessna 172NSDR 08FDEA01783Throttle Cable · stuckDURING CRUISE ENG NR 2 THROTTLE WOULD NOT MOVE, STUCK IN HIGH THRUST SETTING.DURING DESCENT SHUTDOWN ENGINE. R&R NR 2 ENG THROTTLE PUSH PULL CABLE IAW AMM 76-11-01-2. INSPECTED AREA PRIOR TO CLOSE UP. CLOSED FAN COWL IAW AMM 71-00-00-2. ENG RUN-UP REQUIRED.May 7, 2008 · N568FE · Doug MD1010FSDR MASA200800382Gearbox · wornFOUND WEAR ON THE ENGINE THROTTLE CONTROL GEARBOX, WEAR GREATER THAT .010 INCH. REMOVED AND REPLACED NR 1 ENGINE THROTTLE CONTROL GEARBOX.May 6, 2008 · N693BR · Cndair CL6002B19SDR A6WA200840400Throttle · out of adjustUPON ENGINE SHUTDOWN, RIGHT ENGINE CONTINUED TO RUN WITH THRUST LEVER IN SHUTOFF POSITION. WORKED THROTTLE LEVER, ENGINE EVENTUALLY SHUTDOWN. ADJUSTED THROTTLE CONTROL RIGHT ENGINE IAW 76-11-17. PERFORMED IDLE SPEED CHECK IAW 70-00-00. OPS CHECK GOOD. (A)May 5, 2008 · N431AW · Cndair CL6002B19SDR SWIA200819506Gearbox · stuckFLT 3921 - LEFT THRUST LEVER WOULD NOT RETURN TO FLIGHT IDLE. REPLACED LEFT ENGINE THROTTLE CONTROL CABLE IAW MM 76-11-09 AND REPLACED LEFT ENGINE THROTTLE GEARBOX IAW 76-11-17. Apr 20, 2008 · N910EV · Cndair CL6002B19SDR VNAA0803011Throttle · out of rigCREW REPORTED THE RIGHT HAND THRUST LEVER AT FULL FORWARD DOES NOT PRODUCE POWER UP TO CLIMB BUGS. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RIGGED THE RIGHT HAND THROTTLE CONTROLS IN ACCORDANCE WITH THE AIRCRAFT MAMar 25, 2008 · N256PS · Cndair CL6002B19SDR UIEA200800093Control Cable · bindingAIR TURN BACK, NR 4 ENGINE THROTTLE ON REDUCED TAKEOFF, THRUST LEVER WAS BINDING AND HAD TO PUSH THROTTLE LEVER 1.5 KNOBS ABOVE THE OTHER THROTTLES TO SET POWER AND STILL COULD NOT REACH CLIMB THRUST. REMOVED AND REPLACED THROTTLE PUSH PULL CABLE AND PLA SENSMar 24, 2008 · N522MC · Boeing 7472D7BSDR DXTA200802962Throttle Cable · frozenLT (NR 1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENGINE RUN AND VERIFIED PROPER RIGGING IAW MM CH 76-11-02.Mar 24, 2008 · N322QS · Cessna 560CESSNASDR DXTA20082962Throttle Cable · frozenLT (NR1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENGINE RUN AND VERIFIED PROPER RIGGING IAW MM CH 76-11-02.Mar 24, 2008 · N322QS · Cessna 560CESSNASDR HALA0800418Rod End · damagedETOPS SIGNIFICANT SYSTEM, ENG THRUST LEVERS MISALIGNED IN NORM MODE IN LEVEL FLT AT FL 390 WITH EPR'S MATCHED AT 1.37 AND N1 AT 86.3, THRUST LEVERS SPLIT ONE FULL KNOB APART, R THRUST LEVER LAGS. CHECKED THRUST LEVERS AND RESOLVER ANGLES ALL OK. FOUND RT INPMar 22, 2008 · N582HA · Boeing 76733ASDR SWIA200819383Cable · out of adjustFLT 3942 - LEFT THRUST LEVER IS VERY STIFF. ADJUSTED AND REPOSITIONED ATR TO GEARBOX CABLE. OPS CHECK GOOD. Mar 18, 2008 · N449SW · Cndair CL6002B19SDR 08FDEA00519Throttle Cable · failedNR 2 THROTTLE STUCK AT HIGH POWER SETTING AT CRUISE ALTITUDE. ALL ATTEMPTS TO THAW LINKAGES WERE UNSUCCESSFUL. NR 2 ENGINE WAS SHUT DOWN ON APPROACH TO KMEM. AFTER LANDING THROTTLE OPERATED NORMALLY. REMOVED AND REPLACE NR 2 ENGINE THROTTLE CABLE AND THROTFeb 20, 2008 · N560FE · Doug DC1030FSDR CA080220001Rod End · bent(CAN) THE PILOT REPORTED A DEFECT NR 2582A: ABOUT 10 MINUTES AFTER TAKEOFF, THE RT ENGINE NR 2 THROTTLE LEVER WAS STUCK. WORKED THE THROTTLE BACK AND FORTH IN CRUISE 3 - 4 TIMES AND FOUND OK. ON FINAL APPROACH INTO ARRIVAL AIRPORT, THE NR 2 THROTTLE WAS DIFFeb 19, 2008 · Dhav DHC6300SDR CA080205008Power Cable · frozen(CAN) DURING A TEST FLIGHT, THE LT POWER LEVER CABLE FROZE AND WOULD NOT RESPOND TO INPUTS. THE OAT AT THE TIME WAS -28 DEG C. THE POWER SETTING WAS AT MAX ITT FOR TEST PURPOSES. SINCE THE PILOT COULD NOT REDUCE POWER, THE ENGINE WAS SHUTDOWN AND THE PROPELLEFeb 4, 2008 · Gulstm 690ASDR C2XA08CL013Control Panel · stuckEWR FLIGHT 2558 THE CREW REPORTED UNABLE TO SELECT CLIMB ON THE THRUST RATING PANEL. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE CLIMB BUTTON TO BE STUCK. REPLACED THE THRUST RATING PANEL AND OPERATIONAL CJan 27, 2008 · N16112 · Emb EMB145XRSDR DXTA200802798Bellcrank · out of adjustNR2 ENGINE WOULD NOT MAINTAIN TAKEOFF TARGET N1 OF 96.9. INITIALLY NR2 N1 INDICATED 96.9 WITH POWER LEVER AT FULL FWD BUT IMMEDIATELY DROPPED TO AND MAINTAINED 94.4. NR1 ENGINE MAINTAINED 96.9 WITH FULL POWER APPLIED. ADJUSTED NR2 ENGINE BELL CRANK ASSY IN REAJan 25, 2008 · N149QS · Beech 400ASDR NWAA080266746Power Lever · malfunctionedDURING THE TAKEOFF ROLL, THE NR 1 ENGINE WOULD NOT REACH TAKEOFF POWER. THE TAKEOFF WAS ABORTED AT 90KTS. DURING TAXI AFTER THE ABORTED TAKEOFF A BRAKE FIRE WAS REPORTED. MULTIPLE TIRES AND BRAKES WERE REPLACED. MAINTENANCE REPLACED THE NR 1 ENGINE POWER LJan 24, 2008 · N646NW · Boeing 747222BSDR CA080205005Ball Joint · worn(CAN) WHEN THROTTLE WAS RETARDED DURING ENGINE START, T4 CONTINUED TO INCREASE. EMERGENCY SHUTOFF PULLED AND ENGINE MOTORED AS T4 REACHED 900C FOR 2 SECONDS. INVESTIGATION FOUND THE THROTTLE LINK DISCONNECTED BUT THE LOCKING PIN WAS PROPERLY ENGAGED AND IN THJan 21, 2008 · Snias AS350B2SDR 2008FA0000057Throttle Cable · inflt separationDURING FLIGHT, THE CREW EXPERIENCED A SEPARATION OF THE THROTTLE CABLE. THE POWER SETTING ALLOWED THEM TO MAINTAIN ALTITUDE PLUS A SLIGHT CLIMB. THE CREW POSITIONED THE AIRCRAFT FOR A LANDING ON A RUNWAY THAT HAD AMPLE LENGTH. AN UNEVENTFUL LANDING WAS MADE. TJan 18, 2008 · N701ER · Piper PA28R201SDR CA080126002Throttle Control · malfunctioned(CAN) CREW REPORTED LT ENG REMAINED AT HIGH POWER SETTING WHEN AC BROUGHT TO IDLE. N1 REMAINED BETWEEN 82 AND 91 PERCENT. IFSD PILOT COMMANDED IN FLIGHT SHUTDOWN: CONFIRMED, AFTER (ABORTED APPROACH) PILOT SHUTDOWN THE LT ENG USING FIRE PUSH DURING (GO AROUND)Jan 17, 2008 · Cndair CL6002B19SDR COMA0860074Throttle Cable · brokenFLIGHT 5175 - LEFT ENGINE WOULD NOT RESPOND WHEN POWER LEVER BROUGHT TO IDLE. ABORTED APPROACH, PERFORMED IFSD, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED "S" CABLE ON LEFT ENGINE. NO FURTHER DEFECTS.Jan 17, 2008 · N954CA · Cndair CL6002B19SDR CA080116009Bellcrank · cracked(CAN) THE RT POWER LEVER BELLCRANK LOCATED IN THE BOTTOM OF THE PEDESTAL WAS REPLACED DUE TO WEAR. AFTER REMOVAL THE PART WAS FOUND TO BE CRACKED. (TC NR 20080116009)Jan 8, 2008 · Beech 1900DSDR CA080108009Link · damaged(CAN) WHILE CONDUCTING AN INSPECTION, IT WAS NOTED THAT THE BEARING LOOKED TO BE SEPERATED FROM THE LINK. THE LINK WAS REMOVED AND INDEED IT WAS. THE LINK AND NEW WASHERS (SB-62) WERE INSTALLED AND NO OTHER ISSUES WERE NOTED. WHILE CONDUCTING RECENT THROTTLE LJan 8, 2008 · Robsin R44RAVENIISDR HALA0800013Throttle · lack of lubeETOPS SIGNIFICANT SYSTEM, BOTH THROTTLES AREA BINDING. LUBE AND CLEANED THROTTLE QUADRANT.Jan 8, 2008 · N596HA · Boeing 767332SDR CA080108007Release Cable · broken(CAN) THE RT POWER CONTROL WAS REPORTED STIFF. AFTER AN INSPECTION ON THIS AREA IT WAS NOTICED THE THE BETA RELEASE CABLE HAD BROKEN AND WAS CAUSING THE POWER CABLE TO BE STIFF. A NEW CABLE WAS PURCHASED AND CABLE WAS CHANGED. (TC NR 20080108007)Jan 3, 2008 · Dhav DHC6300SDR SWIA200819021Gearbox · bindingFLT 4331 - LEFT THRUST LEVER WILL NOT COME OUT OF SHUTOFF POSITION. REPLACED LEFT ENGINE THROTTLE GEAR BOX. OPS CHECK GOOD, PN: 2100140-010, SN OFF: 2297.Jan 2, 2008 · N435SW · Cndair CL6002B19SDR SWIA200819017Flex Drive · bindingFLT 3730 - RIGHT POWER LEVER IS DIFFICULT TO MOVE. REPLACED AND RIGGED FLEX CABLE AND HOUSING, IAW 76-10-02. OPS CHECKS GOOD. Jan 1, 2008 · N561SW · Emb EMB120ERSDR CA080104002Knob · separated(CAN) (2) KNOBS ON EITHER SIDE OF THE POWER LEVER ARE USED TO RAISE A GATE TO ALLOW REVERSE THRUST. THE KNOBS ARE SCREWED TOGETHER. DURING FLIGHT THE KNOBS SEPARATED (UNSCREWED) AND FELL OFF. THIS ALLOWED THE GATE TO PIVOT IF THE POWER LEVER WAS RETARDED ALLOWDec 29, 2007 · Cessna 208BSDR CA071228001Ecu · failed(CAN) POWER LEVER SPLIT AT HIGH POWER SETTINGS. FAULT ISOLATED TO FAULTY LT ENGINE ECU. ECU REPLACED. TESTED SERVICEABLE. (TC NR 20071228001)Dec 24, 2007 · Aerosp ATR42300SDR MAC120701Control Cable · dirtyUPON REACHING FL 210 (RAIN AND ICING TO FL 210) AN ATTEMPT WAS MADE TO ADJUST THE CONDITION LEVERS. AT THIS TIME THE CREW DISCOVERED THE NR 2 ENGINE LEVER COULD NOT BE MOVED FORWARD OR BACKWARD. IT WAS STUCK AT APPROXIMATELY 56 DEGREES. AFTER LANDING AND REDec 15, 2007 · N910FX · Aerosp ATR42300SDR CA071214010Rod End · separated(CAN) ENGINE HAD HIGH IDLE, TRYED TO ADJUST AND WAS UNABLE TO BRING IDLE BELOW 64 PERCENT ENG RPM. INSPECTED THROTTLE LINKAGE AND FOUND ROD END BRG OUTER HOUSING SEPARATED FROM STAKED IN SPHERICAL BEARING. POSSIBLE LOST OF ENGINE CONTROL UNDER QUICK POWER CHANDec 14, 2007 · Robsin R44RAVENII
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