Pratt & Whitney JT15D-5

Service difficulty reports · 953

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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 engine_model_key = 'JT15D5'
  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 2009FA0000778Indicator · reads lowAT TAKEOFF BOTH AIRSPEED INDICATORS SHOWED A YELLOW "IAS". THE CO-PILOT AIRSPEED SHOWED 40KTS SLOWER THAN THE LT SIDE AIRSPEED INDICATOR.Sep 8, 2009 · N309QS · Cessna 560CESSNA · Airspeed/Mach IndicatorSDR 2009FA0000722Bracket · crackedDURING SCHEDULED A, B, AND C INSP FOUND ROLLER BRACKETS CRACKED ON LT AND RT INBD FWD HORIZ STAB RIBS. REPLACED INBD RIB COMPONENTS WITH IMPROVED PN COMPONENTS IAW MFG COMMUNIQUE 83. RECOMMEND MFG ISSUE A RECOMMENDED SB OR KIT TO REPLACE THE ORIGINAL PN COMPAug 17, 2009 · N68JV · Beech 400A · Horizontal Stabilizer Miscellaneous StructureSDR DJFA2009033Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STAB ROLLER INSP OF THE HORIZ STAB INBD RIB AND BRACKET ASSEMBLIES, BOTH INBD RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. THE LT AND RT RIB Aug 11, 2009 · N745TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA2009072003732Bushing · wornLT ENGINE SHUTDOWN ON CONTROLS AND SPEED BRAKE TEST. FOUND BUSHING IN RT ENGINE BELLCRANK WORN. REPLACED BUSHING. C/W RIGGING CHECK OF LT FCU, FLOW DIVIDER AND AIRFRAME TO ENGINE CABLE. RE-RIGGED FCU TO FUEL FLOW DIVIDER. ADJUSTED GROUND IDLE. ENGINE RUNJul 19, 2009 · N319QS · Cessna 560CESSNA · Power LeverSDR DXTA2009062503699Throttle Cable · out of adjustDURING SPEED BRAKE TEST, RT ENGINE SHUTDOWN. NORMAL FORCE USED DURING TEST. (REPEAT WRITE UP). REMOVED RT LWR COWLING ADJUSTED THROTTLE CABLE FRICTION BLOCKS. CHECKED FRICTION IN COCKPIT-FRICTION IS GOOD ON RT THROTTLE LEVER- RAN ACFT AND CHECKED FOR ENGINE Jun 23, 2009 · N373QS · Cessna 560CESSNA · Power LeverSDR BUEA634C61809Fuel Control · power loss"RT ENG EFC OFF" ANNUNCIATOR ILLUMINATED DURING FLIGHT. RT ENGINE ROLLED BACK 35-40 PERCENT N1.Jun 18, 2009 · N660CC · Beech 400A · Fuel Controlling SystemSDR DXTA2009051503653Engine · odorFOUL ODOR COMING FROM OVERHEAD VENTS ESPECIALLY DURING DECENT. IT HAD A FAINT ODOR OF OIL. REMOVED RIGHT ENGINE ASSEMBLY. INSTALLED SERVICEABLE ENGINE ASSEMBLY IN ACCORDANCE WITH MM 71-01-02. ALL OPERATIONAL AND LEAK CHECKS GOOD.May 14, 2009 · N309QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA2009051403649Throttle · out of rigDURING SPEED BRAKE TEST WITH ENGINES RUNNING, RT THROTTLE WAS MOVED FWD AND THEN BACK TO IDLE. AT THE IDLE STOP, RT ENGINE SHUTDOWN. INSPECTED NR 2 ENGINE S/N PCE-JC0408 THROTTLE RIGGING. FOUND THROTTLE RIGGING TO BE OUT OF MM LIMITS. RE-RIGGED THE NR 2 ENGINMay 12, 2009 · N336QS · Cessna 560CESSNA · Power LeverSDR DXTA2009050103627Bulb · inoperativeLEFT MLG INDICATOR LIGHT DID NOT ILLUMINATE WHEN GEAR WAS PUT DOWN. ROTARY TEST: LIGHT OUT, UNLOCK LIGHT EXTINGUISHED. WITH FLAPS DOWN, THROTTLES IDLE, SPEED BELOW 150KTS: NO HORN. GEAR BLOWN WITH EMERGENCY SYSTEM USING CHECKLIST PROCEDURES. RELAMPED LT MLG Apr 30, 2009 · N314QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR 2009F00030Inlet · damagedDURING SCHEDULED INSP, IT WAS DISCOVERED THAT 1 INLET RIVET HEAD WAS MISSING FROM THE NR 2 ENGINE INLET INNER SKIN (BARREL). THE INLET WAS INSTALLED 288.1 HOURS 206 CYCLES AFTER REPAIR DUE TO SAME CONDITION OF SEVERAL MISSING AND CRACKED RIVETS ON THE INNER SKApr 22, 2009 · N425CT · Beech 400A · Engine Air Intake SystemSDR 2009FA0000296Packing · missingNOTED OIL LEAKAGE AROUND LOWER N2 SPEED SENSOR DURING SCHEDULED INITIAL AIRFRAME/ENGINE INSPECTION. FOUND O-RING SEAL MISSING FROM SPEED SENSOR (REF. JT15D-5/-5R IPC 73-20-05 FIG. 1, ITEM 30). ENGINE RECORDS NOT AVAILABLE, CANNOT VERIFY WHETHER SENSOR REMOVED Apr 16, 2009 · N449TM · Beech 400A · Engine RPM Indicating SystemSDR 2009FA0000322Rod End · bindingON TAKEOFF, PILOT COULD NOT SELECT LANDING GEAR UP. ACFT RETURNED AND COMPLETED A NORMAL LANDING. TROUBLESHOOTING REVEALED A BINDING ROD END BEARING ON THE LT SQUAT SWITCH CAUSED SWITCH TO INTERMITTENTLY NO ACTUATE. REPLACED ROD END BEARING AND RIGGED IAW MApr 15, 2009 · N103BG · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA2009040703584Engine · shutdownDURING THE SPEED BRAKE TEST, WHEN THROTTLE WAS BROUGHT BACK TO IDLE, LT ENGINE SHUTDOWN. RESTARTED AND PERFORMED SPEED BRAKE TEST AGAIN WITH SAME RESULT OF LT ENGINE SHUTTING DOWN.Apr 6, 2009 · N394QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA2009040703585Friction Block · damagedDURING THE SPEED BRAKE TEST, WHEN THROTTLE WAS BROUGHT BACK TO IDLE, LT ENG SHUTDOWN. RESTARTED AND PERFORMED SPEED BRAKE TEST AGAIN WITH SAME RESULT OF LT ENGINE SHUTTING DOWN. REMOVED AND INSTALLED NEW FRICTION BLOCK. OPS CHECKS GOOD AT THIS TIME. ALL WOApr 6, 2009 · N394QS · Cessna 560CESSNA · Drag Control SystemSDR DXTA2009040703586Friction Block · damagedDURING THE SPEED BRAKE TEST, WHEN THROTTLE WAS BROUGHT BACK TO IDLE, LT ENG SHUTDOWN. RESTARTED AND PERFORMED SPEED BRAKE TEST AGAIN WITH SAME RESULT OF LT ENGINE SHUTTING DOWN. REMOVED AND INSTALLED NEW FRICTION BLOCK. OPS CHECKS GOOD AT THIS TIME. ALL WOApr 6, 2009 · N394QS · Cessna 560CESSNA · Drag Control SystemSDR CA090325011Window · cracked(CAN) AT FLIGHT LEVEL 370, THE COCKPIT LT SIDE WINDOW OUTER PANE CRACKED. THE CRACK WAS A 7 INCH CRACK ON THE FWD LWR CORNER. THE ACFT THEN RETURNED TO BASE WITH NO FURTHER INCIDENT. UPON REMOVAL OF THE LT SIDE WINDOW IT WAS FOUND THAT SEVERAL OF THE FASTENERSMar 24, 2009 · Cessna 560CESSNA · Flight Compartment WindowsSDR 2009FA0000206Motor · failedTHE BLOWER MOTOR FAILED INTERNALLY SENDING SMOKE INTO THE CABIN. AC WAS AT ALTITUDE WHEN SMOKE CAME OUT OF THE GASPER SYS. ACFT DESCENDED TO A LOWER ALTITUDE AND THE CABIN CLEARED. (K)Feb 18, 2009 · N17PL · Cessna 560CESSNA · Air Distribution FanSDR 2009FA0000173Motor · burned outWHILE ENROUTE AT 41000 FT HEAVY ACRID BLACK SMOKE THE INUNDATED CABIN. OXYGEN MASKS WERE DEPLOYED AND AN EMERGENCY DESCENT WAS INITIATED. ACFT WAS LANDED AT THE NEAREST SUITABLE AIRPORT WITHOUT INCIDENT. ON FEB 21ST, MX IDENTIFIED THE MALFUCTION AS A OVERHEAFeb 17, 2009 · N17PL · Cessna 560CESSNA · Air Distribution FanSDR 2009F00010Fuel Control · malfunctionedCREW REPORTED LT ENGINE WOULD NOT ACHIEVE CALCULATED TAKEOFF POWER N1. VERIFIED COMPLAINT, ENGINE COULD NOT ACHIEVE MORE THAN 94 PERCENT, N1 AND NOTED NO RPM DROP DURING EFC AUTHORITY CHECKS. ALSO NOTED FLUCTUATING ENGINE VIBRATION INDICATION. EFC AUTHORITY ADFeb 6, 2009 · N465TM · Beech 400A · Fuel Control/Turbine EnginesSDR K452009F00000Manifold · leakingMECHANIC EXPERIENCED A SLOW/COLD START ON LT ENGINE. ENGINE IDLED SLOWER THAN NORMAL. ALL OTHER PARAMETERS WERE NORMAL. UPON SHUTDOWN, FLUID (FUEL) WAS PUDDLED IN BYPASS DUCT AND DRIPPING FROM AFT ENGINE CORE. INVESTIGATION REVEALED PRIMARY AND SECONDARY CROSFeb 5, 2009 · N103BG · Cessna 560CESSNA · Engine Fuel DistributionSDR DJFA2009004Turbine Blades · missingON TAKEOFF ROLL LT ENG EFC DROPPED OFF-LINE AND A SHUDDER WAS FELT BY THE CREW. TAKEOFF WAS ABORTED BELOW 80 KTS. AFTER SHUTDOWN, CREW NOTED 1 AFT TURBINE BLADE MISSING. ENGINE IS BEING REPLACED.Jan 22, 2009 · N485FL · Beech 400A · Turbine SectionSDR CA090130010Turbine Blades · damagedDURING TAKEOFF ROLL, THE ENGINE ELECTRONIC CONTROL WENT OFF LINE AND THE CREW ABORTED THE TAKEOFF AFTER RETURNING TO THE RAMP, INSPECTION OF THE ENGINE SHOWED POWER TURBINE BLADE DAMAGE. THE ENGINE WILL BE REMOVED AND FORWARDED FOR INVESTIGATION AND REPAIR. Jan 22, 2009 · Raythn 400ARAYTHEON · Turbine SectionSDR DXTA2008121803406Engine · shutdownAFTER NORMAL ENGINE START LEFT ENGINE SHUT DOWN DURING THE SPEED BRAKE TEST.Dec 17, 2008 · N345QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA2008121703406Engine · malfunctionedNORMAL ENGINE START, LT ENGINE SHUTDOWN DURING THE SPEED BRAKE TEST. REMOVED LOWER COWLING ON LT ENGINE AND INVESTIGATED. NO DISCREPANCIES NOTED. STARTED BOTH ENGINES, RT FIRST THEN THE LT SIDE. LT ENGINE STARTED FINE. ATTEMPTED SEVERAL THINGS TO TRY ADec 17, 2008 · N345QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200811123352Flow Divider · misriggedRT ENGINE QUIT ON LANDING ROLL OUT. ENGINE QUIT WHEN RT THROTTLE WAS BROUGHT TO IDLE. RT THROTTLE SEEMS TO HAVE AN EXCESSIVE AMOUNT OF SLOP WHEN BROUGHT BACK TO IDLE THRUST. VERIFIED DISCREPANCY, FOUND RT ENGINE CONTROLS AT FCU AND FUEL FLOW DIVIDER IMPROPERNov 12, 2008 · N302QS · Cessna 560CESSNA · Fuel Controlling SystemSDR CA081125006Engine · flamed out(CAN) DURING SHORT FINAL, UPON REDUCING THE POWER TO IDLE, THE ENGINE FLAMED OUT. THE EVENT OCCURRED AT AN ALTITUDE OF APPROX. 100 FEET AND THE CREW LANDED THE ACFT SINGLE ENGINE. NOV. 12 2008: ENGINE FLAME-OUT EVENT OCCURRED WHILE DEPLOYING THE THRUST REVERNov 11, 2008 · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200811113349Engine · unknownRT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES IDLE. REMOVED LT/RT ENG LWR COWLS FOR ACCESS. RE-RIGGED RT FDV TO FUEL CONTROL RD. ADJUSTED RT THROTTLE CABLE. INSPECTED LT FDV TO FUEL CONTROL RIGGING AND THROTTLE RIGGING AT FCU NO DEFECTS NOTED. RANov 11, 2008 · N302QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA2008102703321Engine · unknownLT & RT ENGINE FAILED TO DEVELOP TAKEOFF THRUST. PERFORMED MULTIPLE ENGINE RUNS. ADJUSTED EFC AUTHORITY ON LT ENGINE AND CHECKED ALL RIGGING AND PARAMETERS. AT OAT 10 DEGREE C DESIRED THRUST OF 98-0 BOTH ENGINES PRODUCED 99-0. IAW MM AND MFG REF, BOTH ENGINEOct 26, 2008 · N161QS · Beech 400A · Engine (Turbine/Turboprop)SDR 2008FA0000900Actuator · bypassingHYD LOW LEVEL LIGHT CAME ON AFTER TAKEOFF AND REMAINED ON UNTIL FLAPS AND GEAR WERE SELECTED UP AND LOCKED. REPLACED NOSE GEAR ACTUATOR DUE TO INTERNALLY BYPASSING INTO THE EMERGENCY SIDE FOR GEAR EXTENSION. SENT NOSE GEAR ACTUATOR OUT FOR OVERHAUL AND INSTAOct 9, 2008 · N3FA · Cessna 560CESSNA · Landing Gear ActuatorSDR DJF2008F00014Engine · making metalREPORTED LOW OIL PRESSURE IN FLIGHT. THE AFFECTED ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED. MAINTENANCE FOUND METAL IN THE OIL SYSTEM. THE ENGINE WAS REMOVED FOR OEM EVALUATION. AIRCRAFT RETURNED TO SERVICE. (K)Sep 9, 2008 · N465LX · Beech 400A · Engine (Turbine/Turboprop)SDR CA080917016Engine · malfunctioned(CAN) DURING A RE-POSITIONING FLIGHT, THE PILOT NOTED LOW AND FLUCTUATING OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND SECURED AND A SINGLE ENGINE LANDING WAS PERFORMED. GROUND INSPECTION FOUND CONTAMINATION IN THE OIL FILTER AND FILTER BOWL. THE ENGINE WILL Sep 8, 2008 · Beech 400A · Engine (Turbine/Turboprop)SDR CA080912002Hmu · malfunctioned(CAN) ACFT EXPERIENCED LOSS OF POWER TO FLIGHT IDLE (FI) ON LT ENGINE DURING FLIGHT WHICH LEAD TO A COMMANDED ENGINE IN-FLIGHT SHUTDOWN + RESTART WITH INABILITY TO GO ABOVE FI. FLIGHT WAS DIVERTED WHERE THE A/C LANDED WITH THE LT ENGINE AT FI POWER. EXTENSIVE Aug 26, 2008 · Beech 400A · Fuel Controlling SystemSDR DXTA200807183181Starter Gen · faultyLT FUEL FLOW FLUCTUATION DURING CLIMB AND CRUISE FOLLOWED BY LT GEN FAILURE, FOLLOWED BY LT ENGINE VIBRATION SUB: FOUND LT START GEN EXHAUST DUCT HAS LARGE AMOUNT OF SOOT. REMOVED AND REPLACED LT START GEN. C/W SATISFACTORY, OPS CHECK AND PARALLEL IAW MM 24-Jul 18, 2008 · N325QS · Cessna 560CESSNA · Starter-GeneratorSDR DXTA200803181Fuel Sys · fluctuatesLT FUEL FLOW FLUCTUATION DURING CLIMB AND CRUISE FOLLOWED BY LT ENG FAILURE, FOLLOWED BY LT ENGINE VIBRATION.Jul 17, 2008 · N325QS · Cessna 560CESSNA · Engine Fuel DistributionSDR CIE2008F00001Ignition Lead · out of positionDURING TAKEOFF, THE PILOT REPORTS THAT THE RT ENG POWER LEVER IS BINDING. MAX POWER ON TAKEOFF ROLL 83 PERCENT. ABORTED TAKEOFF AT 30 KNOTS. ONCE THE AC RETURNED TO MAINT FACILITY; THE RT ENG COWLING WAS REMOVED AND FOUND THE RT ENG OB IGNITER LEAD ELBOW POJul 14, 2008 · N594M · Cessna 560CESSNA · Ignition Harness (Distribution)SDR 2008FA0000500Wire · chafedON CLIMB OUT, AFTER DEPARTURE, THE LT THRUST REVERSER DEPLOY LIGHT ILLUMINATED. NO ABNORMAL FLIGHT CHARACTERISTICS WERE FELT IN THE AC. AFM PROCEDURES WERE FOLLOWED AND A SAFE LANDING BACK AT DEPARTURE AIRPORT WAS MADE. AFTER LANDING, THE PILOT CYCLED THE LJul 13, 2008 · N67SF · Cessna 550 · Engine Exhaust System WiringSDR 2008FA0000545Bellows · rupturedTHE BELLOWS INSIDE THE BRADED CONNECTION CRACKED OUT LEAVING A HOLE ABOUT .75 IN IN DIA AT THE UP STREAM SIDE OF THE FLEXIBLE CONNECTOR. THE PROBLEM WAS DISCOVERED ON A MAINT RUN UP AT WHICH TIME THE FIRE DETECTION SYS WAS ACTIVATED FROM AN OVERHEAT SITUATIONJul 12, 2008 · N17PL · Cessna 560CESSNA · Pneumatic Distribution SystemSDR 2008FA0000454Bracket · crackedHORIZ STAB IB RIBS LT AND RT ROLLER BRACKETS FOUND CRACKED. REPLACED PN 45A21085-003 LT FWD BRACKET. PN 45A21086-003 LT AFT BRACKET, PN 45A21085-004 RT FWD. BRACKET PN 45A21086-004 RT AFT BRACKET WITH IMPROVED PN 128-620021-0001 (LT) AND PN 128-620021-0002 (Jun 30, 2008 · N184AR · Beech 400A · Horizontal Stabilizer StructureSDR DJF2008F00000Skin · crackedDURING A ROUTINE SERVICE CHECK IT WAS NOTED THAT THE LT ENGINE INLET INNER SKIN WAS CRACKED AT THE 9 O’CLOCK POSITION. THE SDR WILL BE UPDATED UPON COMPLETION OF THE C/A. (K)Jun 19, 2008 · N439LX · Beech 400A · Engine Air Intake SystemSDR DXTA200803132Fuel Control · malfunctionedLT ENGINE SHUT DOWN IN FLIGHT WHEN THROTTLE WAS BROUGHT BACK TO IDLE FIRMLY. ADJUSTED FCU, IAW MM 71-00-00 CHECK GOOD. C/W ENGINE RUN CHECKS IAW MM 71-00-00. OP'S CHECK GOOD.Jun 18, 2008 · N361QS · Cessna 560CESSNA · Fuel Control/Turbine EnginesSDR E0X2008F00006Switch · faultyON DEPARTURE, ON A MAINT/ REPOSITION FLIGHT, FLIGHT CREW NOTED NR 2 T/R STOW LIGHT ON. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE. CREW NOTED ON SELECTING GEAR DOWN THAT THE NR 1 GEAR DOWN LIGHT WAS NOT ILLUMINATED. CREW ELECTED TO DO A FLY BY TO VISUALLY VJun 13, 2008 · N311GL · Beech 400A · Landing Gear Position and WarningSDR DJF2008F00001Skin · crackedDURING ROUTINE MAINTENANCE THE LT INLET SKIN AT THE INLET TEMP PROBE WAS FOUND CRACKED. THE SDR WILL BE UPDATED UPON COMPLETION OF THE C/A. (K)Jun 4, 2008 · N482LX · Beech 400A · Nacelle/Pylon StructureSDR DXTA200803078Actuator · malfunctionedAFTER TAKE-OFF, LANDING GEAR WOULD NOT RETRACT.May 26, 2008 · N313QS · Cessna 680CE · Landing Gear ActuatorSDR DXTA200803064Brake Sys · malfunctionedON TAXI OUT BOTH PILOT AND CO-PILOT BRAKES WERE VERY HARD DURING APPLICATION, WHEN BRAKES WERE APPLIED (CO-PILOT OR PILOT), AIRCRAFT WOULD NOT SLOW UNTIL A GREAT DEAL OF PRESSURE WAS APPLIED. SUSPECTED AIR IN SYSTEM, BLED LEFT & RIGHT BRAKES SEVERAL TIMES & PMay 17, 2008 · N302QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200803065Actuator · malfunctionedUPON LOWERING LANDING GEAR, BOTH MAIN GEAR LIGHTS WERE GREEN, BUT THE NOSE GEAR LIGHT DID NOT ILLUMINATE. REPLACED NLG ACTUATOR WITH REPAIRED UNIT PERFORMED PROPER FUNCTION CHECKS. FUNCTION CHECK SATISFACTORY AT THIS TIME CE560 M/M 32-31-03.May 17, 2008 · N371QS · Cessna 560CESSNA · Landing Gear ActuatorSDR CIEA200800003Control Valve · malfunctionedAIRCRAFT WAS COMPLYING WITH FAA CHECK RIDE, AFTER TAKEOFF, THE LANDING GEAR APPEARED TO ONLY PARTIALLY RETRACT. FLIGHT CREW FOLLOWED APPROPRIATE CHECK LIST AND RETURN TO DEPARTURE AFTER GEAR EXTENDED NORMALLY. EMERGENCY GEAR EXTENSION WAS NOT REQUIRED. AIRCRAFMay 5, 2008 · N566VR · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA200803035Brake · weakRT SEAT BRAKES ARE SPONGY. PERFORMED BRAKE BLEED ON BOTH BRAKES, NO LEAKS NOTED & BRAKES ARE GOOD REF CE560E 32-42-00.Apr 30, 2008 · N314QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200803026Computer · inoperative1 HOUR INTO FLIGHT, AT FL380, THE RUDDER BOOST FAIL LIGHT CAME ON. REMOVED AND REPLACED WITH OVERHAULED FGC COMPUTER. RUDDER BOOST OPS CHECKED GOOD IAW MM 27-21.Apr 27, 2008 · N132QS · Beech 400A · Flight Management Computing Hardware SystemSDR DXTA200803025Relay · inoperativeDURING TAXI OUT, IT REQUIRED COMPLETE RUDDER PEDAL COMPRESSION TO ENGAGE THE BRAKES. TROUBLESHOT, REMOVED AND REPLACED POWER BRAKE VALVE. PERFORMED BRAKE SYSTEM FUNCTIONAL TESTING, NO DISCREPANCIES NOTED AT THIS TIME. SERVICES HYDRAULIC RESERVOIR. PERFORMEApr 26, 2008 · N161QS · Beech 400A · Landing Gear Brake SystemSDR DXTA200803022Brake Sys · malfunctionedCOPILOT'S LT BRAKE PEDAL REQUIRES SIGNIFICANTLY MORE TILT TO ENGAGE BRAKE THAN RT PEDAL, NO VISIBLE FLUID OR LEAKS. BLED BRAKES IAW MM 32-42-00. OPS CHECK GOOD.Apr 24, 2008 · N318QS · Cessna 560CESSNA · Landing Gear Brake System
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