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 CA130226005Rod End · seized(CAN) DURING INSPECTION THE THROTTLE WAS FOUND TO BE VERY STIFF. AFTER INSPECTION OF THE CONTROLS IT WAS FOUND THAT THE ROD END ATTACHMENT AT THE THROTTLE BODY WAS SEIZED AND WAS MAKING THE THROTTLE VERY HARD TO MOVE. THE ROD END WAS REPLACED. A SIMILAR PROJan 11, 2013 · Diamon DA20C1SDR REXA2012122701828Gearbox · malfunctionedON FLIGHT 4320 FROM DTW TO PVD THE CREW RECEIVED LEFT TR UNLOCK MESSAGE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MDT. REPLACED LT ENGINE THROTTLE CONTROL GEAR BOX. TEST OKAY.Dec 27, 2012 · N8797A · Cndair CL6002B19SDR CA121210007Throttle Cable · binding(CAN) IN CRUISE FLIGHT THE CREW NOTICED THAT THE LT THROTTLE WAS JAMMED. THEY WERE ABLE TO LOOSEN THE THROTTLE SOMEWHAT DURING THE DESCENT BUT IT WAS STILL VERY STIFF TO MOVE. ONCE ON THE GROUND THE THROTTLE SEEMED TO WORK NORMALLY. THE LT THROTTLE GEARBOX Dec 7, 2012 · Cndair CL6002B19SDR 9JLA2013010803563Throttle · out of adjustTHE CREW REPORTED THE RT ENGINE SHUTDOWN DURING TAXI, WHEN THE THROTTLE WAS ADVANCED, RETURNED BACK TO IDLE. THE MX TEAM RIGGED THROTTLE ADJUSTMENT IAW THE MM 76-11-00, PAR E AND FIG 502. POST MX ENGINE RUNS AND FUNTIONAL CHECKS SATISFACTORY.Dec 5, 2012 · N523KW · Cessna 560XLSDR CA121203012Control Cable · binding(CAN) THROTTLE CONTROL STIFF TO OPERATE.Nov 30, 2012 · Piper PA31350SDR CA121203010Throttle · binding(CAN) THROTTLE CONTROL STIFF AND GRINDING NOISE.Nov 16, 2012 · Piper PA31350SDR CA121114013Power Lever · fouled(CAN) PRODUCTION NOTED THAT DURING RIGGING OF THE LT POWER LEVER THE STOP BOLT WAS CONTACTING THE ADJACENT STRUCTURE WHEN THE BOUNCE GAP OF 0.80, 0.120. REQUIRED BY DWG C6EC1007 WAS ACHIEVED. MFG ENGINEERING IS INVESTIGATING FURTHER.Nov 9, 2012 · Dhav DHC6SDR DALA12012479006Lever · disconnectedDIVERTED DUE TO LT ENGINE OVERSPEED CONDITION. CREW COULD NOT CONTROL ENGINE. THROTTLE LOCKED IN FORWARD POSITION. CREW SHUTDOWN ENGINE. MX FOUND NR 1 ENGINE THRUST LEVER DISCONNECTED AND FUEL SHUTOFF BOLT BACKED OUT. INSTALLED NEW HARDWARE. R & R OIL FILTNov 8, 2012 · N906DE · Doug MD88SDR 2012FA0000741Gear · obstructedON APPROACH, PILOT UNABLE TO RETARD THE RT THROTTLE COMPLETELY. A SUCCESSFUL LANDING WAS ACCOMPLISHED. INSPECTION REVEALED ONE OF THE DUST COVER SEGMENTS FOR THAT THROTTLE WAS NOT MOVING IN SEQUENCE WITH THROTTLE MOVEMENT. ON FURTHER INVESTIGATION, IT WAS FNov 1, 2012 · N648DX · Emb EMB500SDR GTIA20121026499Control Unit · failedNR 2 THRUST LEVER DISAGREE POSITION. R & R THROTTLE CONTROL UNIT IAW AMM 76-11-19-000-041A. OPS CHECKED IAW AMM 76-11-00-710-040-A. OPS CHECKED OK.Oct 26, 2012 · N534NK · Airbus A319132SDR CALA2012102500686Throttle · bindingBOTH THROTTLE LEVERS BINDING & RATCHETING. PERFORMED FIM TEST, FAILED. 76-11-00-815-802 PERFORMED FIM TASK 76-11-00-815-802-R-00, NO FAULTS NOTED.Oct 25, 2012 · N75851 · Boeing 757324SDR CA121019008Support Bracket · cracked(CAN) RIGHT ENGINE CONTROL CABLE SUPPORT BRACKET CRACKED AT FWD ATTACHMENT INBD.Oct 19, 2012 · Saab 340BSDR SWIA201231956Control Cable · failedDURING CLIMB THRUST SETTING, LEFT THRUST LEVER HAD MOVEMENT BUT NO N1 THRUST REDUCTION. AFTER CYCLING THRUST, N1 STOPPED AT 93% AND WOULD NOT FURTHER TO THROTTLE MOVEMENT. INITIALLY STARTED QRH SINGLE ENGINE PROCEDURE, BUT THRUST LEVER WOULD NOT SHUT OFF. UOct 14, 2012 · N984CA · Cndair CL6002B19SDR USAA2012101100001Control Quadrant · erraticFLIGHT 970, PHL-BOS - ON TAKEOFF ROLL, ENGINE NR 2 WENT TO RSV POWER. AFTER TOGA POWER WAS ENGAGED THE NR 2 N1 SHOT PAST THE SELECTED POWER SETTING, NR 1 N1 LAGGED BEHIND QUITE A BIT, WHEN BOTH N1 GAUGES FINALLY MET AT POWER SETTING, IT THEN WENT INTO TO-2 RSOct 10, 2012 · N944UW · Emb ERJ190100IGWSDR 2012FA0000692Control Cable · wornNR 2 ENGINE POWER LEVER FROZE DURING CRUISE AT 43,000 FT. ISA -10. CONTROL CABLE WORN.Oct 8, 2012 · N111SW · Amd FALCON900EXSDR QXEA2012100601184Switch · dirtyON LANDING THE GROUND SPOILERS FAILED TO DEPLOY. FLIGHT/TAXI SWITCH WILL NOT REMAIN IN THE TAXI POSITION. CLEANED NR 1 & NR 2 POWER LEVER 12 DEGREE SWITCHES IN POWER LEVER MODULE IAW CMM 76-10-01 PG 401 & 402. PERFORMED FUNCTIONAL TEST OF THE GROUND SPOILEROct 6, 2012 · N430QX · Bombdr DHC8402SDR UALA2012100505641Control Unit · faultyNR 2 ENGINE TLA FAULT. DUE TO CHRONIC NR 2 ENGINE TLA FAULT "ENGINE 2 ONE TLA FAULT" HITTING SINCE 8-8-12 ACP TSM 76-00-00-810-802-B. THIS FAULT IS INTERMITTENT SO HARNESS MAY BE SUSPECT. POS PART TCU PCN 565-0099, EEC PCN 482-9588 (MR73908). REPLACED NR 2Oct 5, 2012 · N441UA · Airbus A320232SDR UALA2012092705474Throttle · dirtyLEFT THROTTLE MECHANICALLY STOPS SHORT ABOUT 2 INCHES OF FULL THROTTLE TRAVEL. FOUND UNDER SIDE OF THROTTLE VERY DIRTY. CLEANED AND OPS CHECKED NORMAL.Sep 25, 2012 · N506UA · Boeing 757222SDR CA120914001Cable · lack of lube(CAN) ON DESCENT, NR 2 ENGINE UNABLE TO RETARD THRUST BELOW 51 PERCENT N1. ACFT WAS DIVERTED, LANDED WITHOUT INCIDENT, NR 2 ENGINE SHUTDOWN USING LP FUEL COCK. RT ENGINE CONTROL TELEFLEX INSPECTION, CHECK AND LUBRICATION CARRIED OUT IAW AMM. ENGINES GROUND RSep 13, 2012 · Raythn HAWKER850XPSDR 2012FA0000629Module · faultedON CLIMBOUT, FADEC FAULT INDICATED, AT 15000 FT ALTITUDE ENGINE NR 1 (LT) ROLLED BACK TO IDOL WITH FADEC FAIL INDICATION. PILOTS WERE UNABLE TO GET CONTROL OF ENGINE. DECLARED AN EMERGENCY AND LANDED WITH LT ENGINE AT IDLE. CONTROL OF RT ENGINE WAS NORMAL. Aug 31, 2012 · N402SE · Hawbee 4000SDR V2JA078L111183012Throttle · malfunctionedON TAKEOFF ROLL, THE CREW ABORTED DUE TO THE RT ENGINE AFX DID NOT ARM, RETURNED BACK TO DEPARTURE. REPLACED THE THROTTLE QUADRANT AND PERFORMED POWER CONTROL CAM SWITCH OPS CHECK IAW MM 76-11-00. ALL OPS CHECKS WERE SATISFACTORY.Aug 29, 2012 · N150SL · Piagio P180SDR REXA2012081801274Gearbox · malfunctionedRIGHT THRUST LEVER BINDS AT HIGH THRUST SETTING, WOULDN'T ALLOW CLIMB THRUST TO BE SET AT HIGHEST N1 SETTING. CARAT INDICATED 95.0 SHOULD BE SET AND COULD ONLY SET 94.2. REMOVED AND REPLACED RIGHT THROTTLE GEARBOX IAW AMM 76-11-17. CHECKED RIGGING ON POWER Aug 18, 2012 · N8696C · Cndair CL6002B19SDR REXA2012081601266Gearbox · restrictedRIGHT THRUST LEVER QUADRANT HAS LOT OF FRICTION IN HIGHER TRUST SETTINGS. HARD TO SET TRUST AT HIGHER LEVELS. REMOVED AND REPLACED RIGHT ENGINE THROTTLE CONTROL GEARBOX PER AMM 76-11-17. RIQ CHECKS, FRICTION TEST, AND FUNCTIONAL CHECKS ARE GOOD PER AMM 76-11Aug 16, 2012 · N8696C · Cndair CL6002B19SDR A6WA201240769Lever · looseFUEL SHUTOFF LEVER ON LT THRUST LEVER IS VERY LOOSE. R & R THROTTLE QUADRANT IAW 76-11-01.Aug 13, 2012 · N446AW · Cndair CL6002B19SDR VNAA2012080800003Throttle Cable · brokenAT 7,000 FEET ON CLIMBOUT, CREW REPORTED LEFT ENGINE DID NOT RESPOND TO THRUST LEVER COMMANDS. CREW FOLLOWED QRH AND SHUT DOWN NUMBER ONE ENGINE. BRINGING THRUST LEVER TO SHUT OFF DID SHUT DOWN ENGINE SUCCESSFULLY. CREW RETURNED TO FIELD AND LANDED WITHOUT Aug 8, 2012 · N237PS · Cndair CL6002B19SDR 7EMA20120806429Linkage · dirtyON DESCENT, THE RT ENGINE FAILED TO RESPOND TO POWER-LEVER MOVEMENT, TORQUE REMAINED AT 2000 LBS. AFTER TRYING SEVERAL TIMES TO GET RT ENGINE TO RESPOND BY MOVING POWER LEVER FORWARD AND AFT, ENGINE WAS SECURED, DECLARED EMERGENCY AND MADE SAFE LANDING. MX CAug 6, 2012 · N429EM · Beech 200BEECHSDR REXA2012080101214Lever · out of adjustTHRUST LEVERS DON'T MOVE EASILY, TRIED TO ADJUST KNOB AT BASE OF THRUST LEVER QUADRANT WITH NO SUCCESS. ADJUSTED FRICTION CONTROL KNOB WITH NO DIFFICULTY. OPS CHECKED THRUST LEVERS IAW AMM 76-10-00. LEVERS MOVED FREELY, NO DEFECTS FOUND.Aug 1, 2012 · N8808H · Cndair CL6002B19SDR A6WA201240734Control Cable · failedON DESCENT, LT THRUST LEVER STUCK AT AROUND 82 PERCENT, N1. COMPLIED WITH QRH, SHUTDOWN NR 1 ENGINE IN FLIGHT, ALL ENGINE PARAMETERS NORMAL. R & R LT ENGINE THROTTLE CONTROL CABLE IAW AMM 76, OPS CHECKED GOOD.Jul 29, 2012 · N449AW · Cndair CL6002B19SDR CA120727006Linkage · binding(CAN) UPON SHUTDOWN, THE PILOT REPORTED THAT HE COULD NOT PULL THE CONDITION LEVER INTO THE FUEL CUTOFF POSITION. THEY USED THE FIREWALL SHUTOFF TO SHUTDOWN THE RT ENGINE. UPON INSPECTION BY MAINTENANCE, IT WAS FOUND THAT THE LINKAGE BETWEEN THE POWER LEVER Jul 26, 2012 · Beech 200BEECHSDR CA120727001Control Cable · damaged(CAN) THE ACFT WAS BEGINNING A DESCENT. THE PILOT HAS REDUCED THE THRUST LEVERS OF BOTH ENGINES. THE RT ENGINE HAS PRODUCED REDUCTION N1 AND N2 RPM NORMALLY. BUT THE LEFT ENGINE HAS CHANGED THE N1 AND N2 RPM ONLY A LITTLE AND COULD NOT BE REDUCED MORE WITH THEJul 21, 2012 · Cndair CL6002B19SDR SWIA201231286Switching Unit · failedMULTIPLE GEAR INDICATION MESSAGES. (FLT 5492) REPLACED THROTTLE QUADRANT ADJUSTABLE CAM SWITCHING UNIT. PN: FE210-302, SN OFF: FR1008.Jul 17, 2012 · N405SW · Cndair CL6002B19SDR CA120708001Condition Lever · broken(CAN) WHILE TAXING, PILOT ATTEMPTED TO REDUCE CONDITION LEVER TO "GROUND IDLE" NOTICED SOMETHING DID NOT FEEL RT WITH THE MOVEMENT. PILOT THEN MOVED CONDITION LEVER BACK TO "FLIGHT IDLE" WHERE THE LEVER BROKE. THE PILOT THEN TAXIED THE ACFT BACK TO THE COMPAJul 7, 2012 · Cessna 208BSDR ASAA2012071292547Relay · failedON NORMAL ENGINE SHUTDOWN AT GATE AFTER GROUND. POWER SWITCHED, ENG FAILED WARNING CAME ON OVER EGT GAUGE. ACFT GROUNDED. CREW STATED LIGHT CAME ON WHEN NR 1 ENGINE WAS SHUTDOWN. ACCOMPLISHED FIM 73-05-00-810-805, NO FAULTS FOUND. REPLACED NR 1 ENGINE STJul 1, 2012 · N579AS · Boeing 737890SDR FDEA201206292423Throttle · malfunctionedAFTER PUSHBACK AND DURING CONFIGURATION BEFORE TAXI, THROTTLE WENT FULL FORWARD TO TAKEOFF POWER WHILE BRAKES WERE SET, HANDS WERE NOT ON THROTTLES, HAD TO FORCEABLY PULL THROTTLES BACK TO IDLE AND FINALLY HAD TO DISCONNECT AUTOTHROTTLES, RETURNED TO THE GATEJun 29, 2012 · N885FD · Boeing 777FS2SDR SWIA201231134Throttle · out of rigWITH THRUST LEVER AT COMPLETE AFT STOP THE LEFT ENGINE WOULD NOT SHUT DOWN. RAMP PERSONNEL REPORTED SMOKE. (FLT 6398) RE-RIGGED LEFT ENGINE THROTTLE.Jun 25, 2012 · N924SW · Cndair CL6002B19SDR REXA2012062501016Power Lever · dirtyRIGHT THRUST LEVEL HAS SIGNIFICANT RESISTANCE WHEN APPLYING POWER OR REDUCING IT. CLEANED DUST FROM THROTTLE QUADRANT AND OPS CHECKED GOOD IAW AMM 76-10-00. AIRCRAFT OK FOR SERVICE.Jun 25, 2012 · N8577D · Cndair CL6002B19SDR REXA2012062401019Cable · out of rigTHRUST REVERSER WILL NOT DEPLOY. RIGGED THROTTLE GEAR BOX IAW AMM 76-11-17. OP`S CHECKED GOOD AT THIS TIME RIGGED ATR CABLE IAW AMM 78-35-01. OP`S CHECK GOOD.Jun 24, 2012 · N824AY · Cndair CL6002B19SDR REXA2012062301007Power Lever · bindingLEFT ENGINE THRUST LEVER BUCKLES. DOES NOT GO FULL/MAX POWER AT ALTITUDE. VERY UNEVEN THRUST ADVANCE AND RESEND BETWEEN LEVERS. COULD NOT DUPLICATE PROBLEM AT THIS TIME. OK FOR SERVICE, CREW NOTIFIED AND OK WITH IT.Jun 23, 2012 · N8506C · Cndair CL6002B19SDR CA120911001Throttle Cable · disconnected(CAN) AFTER LANDING, THE ENGINE WOULD NOT RETURN TO IDLE. IT WAS SHUTDOWN USING THE FUEL VALVE. FOUND THAT THE CONTROL ASSY, THROTTLE CABLE, HAD DISCONNECTED INTERNALLY.Jun 17, 2012 · Bell 407SDR 2012FA0000426Throttle Cable · brokenPILOT REPORTED RT THROTTLE CABLE BROKE ON LANDING ROLL OUT, SHUTDOWN LT TO BETTER CONTROL ACFT THEN SHUTDOWN RT AS ACFT WAS UNDER CONTROL AND ROLLED TO STOP. INSP FOUND RT CABLE BROKEN AT THROTTLE HANDLE END WHERE IT ENTERS INTO THE CABLE HSG. HOUSING APPEARJun 11, 2012 · N407T · Beech 95C55SDR REXA2012060500818Throttle · failedRT THRUST REVERSER HANDLE WILL NOT COME OUT OF IDLE DETENT. REMOVED AND REPLACED THROTTLE QUADRANT IAW AMM 76-11-01. RT THRUST REVERSER OPS CHECKED GOOD.Jun 5, 2012 · N824AY · Cndair CL6002B19SDR CA120512001Throttle Cable · not reported(CAN) AC WAS ENROUTE. CREW ADVISED DISPATCH THAT THE RT ENGINE WAS UNRESPONSIVE. THE CREW ELECTED TO DIVERT TO ANOTHER AIRPORT DUE TO LONGER RUNWAY AT THAT LOCATION. WHEN RETARDING POWER DURING DESCENT, THE RT ENGINE REMAINED AT 94 PERCENT. THERE WAS NO RESPOMay 11, 2012 · Cndair CL6002B19SDR ASOA201201627Push-Pull Cable · bindingRIGHT THRUST LEVER CAUSED NO CHANGE IN ENGINE POWER SETTING (94 PERCENT). ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. FOLLOWED QRH FOR JAMMED THROTTLE. SHUTDOWN ENGINE IN FLT. DIVERTED, EMERGENCY DECLARED. R & R RT PYLON PUSH-PULL THROTTLE CABLE IAW IAWMay 11, 2012 · N930EV · Cndair CL6002B19SDR CA120523004Power Lever · malfunctioned(CAN) DURING TAXI , THE PILOT NOTICED THE ACFT WAS VEERING LT WITH THE ENGINE NOT RESPONDING TO THROTTLE INPUT. DURING SUBSEQUENT TROUBLESHOOTING, WHEN THE POWER LEVER WAS ADVANCED, THE ENGINE POWERED UP NORMALLY BUT WHEN IT WAS RETARDED, THE ENGINE FLAMED OUMay 4, 2012SDR REXA2012042500566Friction Lock · stuckTHRUST LEVER FRICTION ADJUSTMENT KNOB IS STUCK WILL NOT MOVE EITHER DIRECTION. RELEASED THRUST LEVER FRICTION LOCK FROM BEING OVER TIGHTENED. OPS CHECK NORMAL IAW AMM 76-10-00.Apr 25, 2012 · N8492C · Cndair CL6002B19SDR REXA2012042200556Gearbox · failedLEFT THRUST REVERSER INOPERATIVE. REPLACED THROTTLE GEAR BOX . Apr 22, 2012 · N801AY · Cndair CL6002B19SDR CA120423012Cable · corroded(CAN) OCCURRENCE ON AIRCRAFT, ENGINE POWER CONTROL CABLE TORN OFF. THE FLIGHT CREW WAS ON THE APRON PERFORMING THE LT SIDE ENGINE START. NH SHOULD BE STABILIZED AT 78.5 PERCENT, BUT SUDDENLY THIS PARAMETER INCREASED UP TO A VALUE OF 107 PERCENT AND SUBSEQUENTApr 19, 2012 · Cndair CL2156B11215SDR QMLA2012041212059Throttle · roughPILOT WAS PERFORMING PRE-START CHECKLIST FOR 2ND FLIGHT OF THE DAY. WHILE OPERATING NR 2 TWIST GRIP FROM "0" TO "F" NOTICED EXTREME FRICTION FROM BETWEEN "30" AND "F". MADE SEVERAL ATTEMPTS TO GO TO "F" BUT WAS CONCERNED THAT SOMETHING MAY BREAK. ACFT REMOVApr 12, 2012 · N854UH · Bolkms BK117C2SDR NSVA20120411514Power Lever · out of adjustABORTED TAKEOFF AT 70KT DUE TO LT CTOT/APR NOT ENGAGING. MAINTENANCE ADJUSTED LT POWER LEVER. PERFORMED OP'S CHECKS. ALL CHECKED GOOD.Apr 11, 2012 · N220MJ · Saab 340BSDR ECPR201204130001Throttle Cable · detachedON CLIMBOUT, 600-700FT AGL, INSTRUCTOR PILOT (IP) REDUCED RT THROTTLE TO IDLE TO SIMULATE ENGINE FAILURE. STUDENT PILOT (SP) SIMULATED FEATHERING RT PROPELLER AND WHEN ATTEMPTING TO SET ZERO THRUST, IP DISCOVERED THAT THERE WAS NO THRUST AVAILABLE. RT ENGINE Apr 10, 2012 · N7720Y · Piper PA44180
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