Pratt & Whitney JT15D-5

Service difficulty reports · 953

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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"

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SDR DXTA200803014Unknown · odorELECTRICAL BURNING ODOR COMING FROM VANITY LIGHT AREA OF THE LAVATORY. PASSENGERS CAME UP TO THE COCKPIT TO COMPLAIN ABOUT THE ODOR. WE COULD DETECT IT FROM THE COCKPIT. TROUBLESHOT AND PERFORMED A DETAIL INSPECTION OF THE WHOLE LAV. AREA, INCLUDING SIDEWALL, Apr 23, 2008 · N151QS · Beech 400A · Air Distribution SystemSDR 2008FA0000300Bulkhead · crackedWHILE PERFORMING AN (A-B) INSPECTION FOUND RT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKETS PULLED FROM AFT FUSELAGE BULKHEAD RESULTING IN CRACKS IN THE BULKHEADS AT FRAME STA 329.92. RECOMMEND INSPECTING AREA THOROUGHLY AT EACH INSPECTION. RECOMMEND CONTACTINApr 22, 2008 · N400SF · Beech 400A · Fuselage Main, BulkheadSDR A8OA200800001Engine · seizedUPON VR DEPARTING, RT ENGINE FAILED. DETECTED BY THE FLIGHT CREW AFTER HEARING (2) LOUD POPS FOLLOWED BY INCREASE OF ITT AND FUEL FLOW. ENGINE WAS SHUTDOWN AND AC RETURNED TO DEPARTURE UNEVENTFULLY. ENGINE REMOVED AND CURRENTLY IN TEARDOWN. A SUPPLEMENT WIApr 22, 2008 · N913MC · Beech 400BEECH · Engine (Turbine/Turboprop)SDR DXTA200803003Flow Divider · out of adjustDURING SPEED BRAKE TEST, LT ENGINE SHUTDOWN AND RT ENGINE SHUTDOWN. ADJUSTED TENSION ON BALL PLUNGER ON THE FUEL FLOW DIVIDER, PERFORMED OPS CHECK WITH NO DEFECTS NOTED REF ENGINE MM 71-01-03Apr 18, 2008 · N302QS · Cessna 560CESSNA · Fuel Controlling SystemSDR DXTA200802996Pump · inoperativeCREW REPORTED LIGHT ILLUMINATED AS SOON AS SQUAT SWITCH MADE ON LANDING, THEY ONLY GOT 2 GOOD APPLICATIONS BEFORE PREX DEPLETED. AFTER LANDING "POWER BRAKE LOW PRESS" LIGHT CAME ON. NOISE CAME FROM NOSE LIKE ACCUMULATOR IS TRYING TO CHARGE. AFTER SHUTDOWN, BApr 14, 2008 · N353QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200802994Brake Assy · weakBOTH COPILOTS BRAKE PEDALS GO ALMOST TO THE FLOOR. VERIFIED NO LEAKAGE UNDER PEDALS IN COCKPIT. BLED BRAKES PER CESSNA MODEL 560 MM 32-42-00. OPERATIONAL CHECKED GOOD.Apr 13, 2008 · N396QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DJFA041208001Circuit Breaker · arcedCREW EXPERIENCED A STRONG ELECTRICAL SMELL IN THE COCKPIT DURING FLIGHT. MAINT FOUND THE 15 AMP STANDBY POWER CIRCUIT BREAKER ARCING. THE CIRCUIT BREAKER WAS REPLACED. FUNCTIONAL CHECKS WERE GOOD AND THE AC WAS RETURNED TO SERVICE.Apr 12, 2008 · N790TA · Beech 400A · Electrical Power System WiringSDR DJFA2008042Circuit Breaker · arcedCREW EXPERIENCED A STRONG ELECTRICAL SMELL IN THE COCKPIT DURING FLIGHT. MAINT FOUND THE 15 AMP STANDBY POWER CIRCUIT BREAKER ARCING. THE CIRCUIT BREAKER WAS REPLACED. FUNCTIONAL CHECKS WERE GOOD AND THE AC WAS RETURNED TO SERVICE.Apr 12, 2008 · N790TA · Beech 400A · AC Power Distribution SystemSDR DXTA20082982Engine · bird ingestionDURING CLIMB OUT AT 500 FEET, EXPERIENCED BIRD STRIKE TO LT ENGINE. CREW REPORTED A VERY LOUD BANG, FOLLOWED BY A COUPLE OF MINUTES OF SMOKE/ODOR IN CABIN.Apr 6, 2008 · N343QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200802982Engine · bird ingestionDURING CLIMB OUT AT APPROX 500 FEET, EXPERIENCED BIRD STRIKE TO LT ENGINE. CREW REPORTED A VERY LOUD BANG, FOLLOWED BY A COUPLE OF MINUTES OF SMOKE/ODOR IN CABIN. REMOVED AND REPLACED LT ENGINE IAW MM 71-01-02. LEAK AND OPS CHECK GOOD.Apr 6, 2008 · N343QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DJFA2008038Unknown · odorAC DIVERTED ON REPOSITION LEG FOR OILY ODOR IN CABIN WHEN TEMPERATURE WAS TURNED TO HOT. WITH TEMPERATURE TURNED DOWN, THE ODOR DISAPPEARED. MAINT RAN THE AC WITH TEMPERATURE IN FULL HOT AND FULL COLD. NO OILY ODOR WAS NOTICED. CABIN AIR OUTLETS WERE CHECKApr 5, 2008 · N755TA · Beech 400A · Air Distribution SystemSDR DXTA200802978Indicator · failedABOVE 40 KTS, LT AIRSPEED FAILED WITH RED X ACCOMPANIED BY GPWS WINDSHEAR FAIL ANNUNCIATOR. INSPECTED GPWS SYSTEM PERFORMED GPWS SELF TEST NO FAULTS FOUND CHECKE IAC FAULTS NONE FOUND PERFORMED OPS CHECK OPS CK GOOD IAW MM 34-41-04.Apr 2, 2008 · N352QS · Cessna 560CESSNA · Airspeed/Mach IndicatorSDR DXTA20082972Wheel · vibrationVIOLENT NOSEWHEEL SHIMMY ON TAKEOFF BETWEEN 20-30 KNOTS (ABORTED TAKEOFF).Mar 30, 2008 · N398QS · Cessna 560CESSNA · TireSDR DXTA20082974Brake Assy · failedCO-PILOT'S BRAKES FEEL MUSHY AND SOFT WITH MORE THEN USUAL TRAVEL DURING LANDING. BLED ANTI SKID BRAKE SYSTEM. OPS CHECKED GOOD. LEAK CHECKED GOOD. WORK DONE IAW 560 M.M. CHAPTER 32-42-00.Mar 30, 2008 · N399QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200802974Brake · weakCO-PILOT'S BRAKES FEEL MUSHY AND SOFT WITH MORE THEN USUAL TRAVEL DURING LANDING. BLED ANTISKID BRAKE SYS. OPS CHECKED GOOD. LEAK CHECKED GOOD. WORK DONE IAW MM, CHAPTER 32-42-00.Mar 30, 2008 · N399QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200802972Actuator · vibrationVIOLENT NOSEWHEEL SHIMMY ON TAKEOFF BETWEEN 20-30 KNOTS (ABORTED TAKEOFF). REMOVED AND REPLACED NOSE GEAR ACTUATOR IAW THE CHAP 32-21-03. LEAK AND OPERATIONAL CHECK NORMAL. R7R SHIMMY DAMPER IAW THE MM CHAPTER 32-21-02. LEAK AND OPS CHECK NORMAL. REMOVED Mar 30, 2008 · N398QS · Cessna 560CESSNA · Landing Gear ActuatorSDR DJFA2008035Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN CMar 29, 2008 · N792TA · Beech 400A · Horizontal Stabilizer Miscellaneous StructureSDR DJFA2008034Unknown · smokeREPORTED EXTREME HEAT COMING INTO AIRCRAFT ACCOMPANIED BY A BLUE HAZY TYPE SMOKE AND BURNING ODOR IN CABIN. AIR CONDITIONING SYSTEM WAS PREVIOUSLY MEL'D. MAINT FOUND THE AIR CYCLE MACHINE CIRCUIT BREAKER PULLED AND COLLARED. THE CIRCUIT BREAKER WAS RESET. TMar 28, 2008 · N755TA · Beech 400A · Air Distribution SystemSDR DXTA20082961Autopilot Sys · inoperativeAT FL430 ACCIDENTLY HIT TURN KNOB, AUTO PILOT WOULD NOT WORK CORRECTLY. IN HEADING MODE IT WOULD ALWAYS STOP 10 DEG SHORT OF THE HEADING BUG. NO FAULT CODES REPORTED. DISCREPANCY RELATED TO INVERTER FAULT. INVERTER SELECT SWITCH REPLACED. OPERATIONAL CHECMar 24, 2008 · N391QS · Cessna 560CESSNA · Autopilot SystemSDR 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 560CESSNA · Power LeverSDR DXTA200802961Switch · inoperativeAT FL430 ACCIDENTALLY HIT TURN KNOB, AUTO PILOT WOULD NOT WORK CORRECTLY. IN HEADING MODE IT WOULD ALWAYS STOP 10 DEG SHORT OF THE HEADING BUG. NO FAULT CODES REPORTED. DISCREPANCY RELATED TO INVERTER FAULT. INVERTER SELECT SWITCH REPLACED. OPERATIONAL CHEMar 24, 2008 · N391QS · Cessna 560CESSNA · Autopilot SystemSDR 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 560CESSNA · Power LeverSDR DXTA20082960Sprocket · obstructedJAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED, CLEANED AND LUBED TRIM COMPONENTS, OPS CHECK AND TRAVEL CHECKS GOOD AT THIS TIME. REF. CE560 M/M 27-31-00.Mar 23, 2008 · N374QS · Cessna 560CESSNA · Control Column SectionSDR VQMA032308001Hose · rupturedMAIN BRAKES FAILED ON LANDING, EMERGENCY BRAKES HAD TO BE USED, FLUID FOUND ON BOTTOM OF WING AND RT FLAP. SIGHT GAGE INDICATES FLUID LEVEL EMPTY.Mar 23, 2008 · N56GA · Cessna 560CESSNA · Hydraulic System, MainSDR DXTA200802960Trim Tab · obstructedJAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED, CLEANED AND LUBED TRIM COMPONENTS, OPS CHECK AND TRAVEL CHECKS GOOD AT THIS TIME. REF MM 27-31-00.Mar 23, 2008 · N374QS · Cessna 560CESSNA · Elevator, Tab StructureSDR DJFA2008030Hmu · failedON TAXI FOR TAKE-OFF, WHILE PERFORMING THE EFC TEST, THE NR 2 ENGINE SHUT DOWN UNCOMMANDED. MAINTENANCE CHECKED RIGGING AND PERFORMED SEVERAL OPERATIONAL CHECKS. MAINTENANCE DETERMINED THAT THE HMU REQUIRED REPLACEMENT. THE HMU AND FLOW DIVIDER WERE REPLAMar 21, 2008 · N708TA · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA2008029Inlet · crackedDURING A SCHEDULED INSP, MAINT DISCOVERED THE NR 2 ENGINE HEATED INLET CRACKED AT THE 4 O'CLOCK POSITION. MAINT REMOVED AND REPLACED THE INLET.Mar 19, 2008 · N745TA · Beech 400A · Air Intake Anti/De-Ice SystemSDR DXTA20082948Brake · weakRT PILOT BRAKES ARE SOFT (NOTE APPROX 75 PERCENT TRAVEL BEFORE BRAKING IS FELT. PERFORMED THE ANTI-SKID BRAKE SYSTEM BLEEDING PROCEDURE IAW THE CESSNA MM CHAPTER 32-42-00. OPERATIONAL CHECK OF AIRCRAFT BRAKING SYSTEM SATISFACTORY.Mar 18, 2008 · N391QS · Cessna 560CESSNA · Brake Anti-Skid SectionSDR DJFA2008028Inlet · crackedDURING A SCHEDULED INSPECTION, MAINT DISCOVERED THE NR 2 ENGINE HEATED INLET CRACKED. MAINTENANCE REPLACED THE INLET.Mar 18, 2008 · N438LX · Beech 400A · Air Intake Anti/De-Ice SystemSDR DJFA2008027Connector · dirtyON TAXI TO TAKEOFF, DURING EFC TEST, CREW EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 2 ENGINE. MAINTENANCE CLEANED THE EFC CONNECTOR AND PERFORMED SEVERAL GROUND RUNS, EFC TESTS, AND A T/R CHECK WITHOUT FAILURE.Mar 17, 2008 · N708TA · Beech 400A · Engine Fuel System WiringSDR DXTA20082938Sensor · failedHORIZONTAL STAB FAILED IN FLIGHT. TROUBLESHOT IAW MM 30-12-00 FOUND LEFT STAB TEMP SENSOR TO HAVE SPLIT READINGS FROM P473 AT THE CONTROLLER, AT 238.3 OHMS AND ONE AT 203.2 OHMS. CLEANED TERMINAL STRIP 061. RECHECKED RESISTANCE FOUND GOOD AT 202 EACH. PERFORMMar 14, 2008 · N119QS · Beech 400A · Stabilizer Control SystemSDR DJFA2008026Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70.Mar 13, 2008 · N493CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA20082935Uplock Sensor · malfunctionedUPON GEAR RETRACTION, OUT OF DEPARTURE, RT GEAR WOULD NOT RETRACT. REMOVED AND REPLACED RT UPLOCK SWITCH WITH NEW. C/W FULL GEAR FUNCTIONAL CHECK. ALL OPS CHECK GOOD AT THIS TIME. IAW MM 32-61-00.Mar 12, 2008 · N382QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DJFA2008025Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. MAMar 10, 2008 · N790TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR ZESA030808001Hinge · crackedPOST FLIGHT, PILOTS COULD NOT CLOSE AND LATCH MAIN CABIN DOOR. FOUND CABIN DOOR HINGE CRACKED THROUGH ON LOWER ARM.Mar 8, 2008 · N400LX · Cessna 560CESSNA · Fuselage, Door HingeSDR DJFA2008022Support Bracket · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70.Mar 2, 2008 · N751TA · Beech 400A · Horizontal Stabilizer StructureSDR DJFA2008023Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT AND RT IB RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70.Mar 2, 2008 · N479LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2008021Support Bracket · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 7Mar 1, 2008 · N449LX · Beech 400A · Horizontal Stabilizer StructureSDR DXTA20082906Relay · inoperativeCABIN CLIMBED AT MAX RATE, 10,000 FT, CABIN PRESSURE LIGHT CAME ON. THE PNUEMATIC RELAY WAS REMOVED AND REPLACED S/N OFF 15-2131. WORK PERFORMED IAW MM 21-31. SYSTEM OP'S AND LEAK CHECKED GOOD. ALSO REMOVED AND REPLACED FAULTY LT MLG SQUAT SWITCH IAW MM 32-61Feb 29, 2008 · N312QS · Cessna 560CESSNA · Cabin Pressure Control SystemSDR F2P2008F00000Hose · looseDURING TAKEOFF ROLL, NR 2 ENGINE LOST POWER AND ROLLED BACK TO LOW IDLE, TAKEOFF WAS ABORTED WITH NO FURTHER INCIDENT. CAUSE OF TROUBLE WAS FOUND TO BE THAT THE P2/T2 SENSOR LINE, PN 2525499 FROM PT/T2 SENSOR TO FUEL CONTROL UNIT(FCU) CAME LOOSE AND SEPARATEFeb 28, 2008 · N716SX · Cessna 560CESSNA · Fuel Controlling SystemSDR DJFA2008018Connector · damagedCREW REPORTED AFTER TAKEOFF UPON GEAR RETRACTION THE RED UNSAFE LANDING GEAR LIGHT REMAINED ILLUMINATED. EMERGENCY GEAR EXTENSION WAS PERFORMED WITH NORMAL INDICATION AFTERWARD. THE AC DIVERTED, MAINT FOUND PIN M OF THE RT DOOR UPLOCK SWITCH PUSHED BACK. THFeb 27, 2008 · N429LX · Beech 400A · Landing Gear System WiringSDR DXTA20082896Brake Assy · weakRT BRAKE PEDAL ON RT SEAT SIDE GOES TO THE FLOOR WHEN BRAKES ARE PRESSED. COMPLIED WITH BRAKE BLEED IAW MM 32-42-00.Feb 24, 2008 · N337QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA20082891Brake Assy · malfunctionedCOPILOTS SIDE BRAKES REQUIRE MORE THAN NORMAL PRESSURE TO GET ANY BRAKING. RAN AC WITH ANTI-SKID ON AND OFF CONDUCTING HIGH SPEED STOPS AND MANY MANUVERING TURNS WITH NO DISCREPANCIES NOTED FROM EITHER PILOT OR COPILOT SIDE. ANTI-SKID BIT INDICATORS WERE CHEFeb 20, 2008 · N352QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA20082880Landing Gear · malfunctionedMANUAL GEAR EXTENSION WITH BLOW DOWN DUE TO NOSE GEAR NOT EXTENDED DURING LANDING. RESET BLOWDOWN BOTTLE AND SERVICED SWING GEAR MULTIPLE TIMES. UNABLE TO DUPLICATE PROBLEM. REF: MM SEC 32-30-00Feb 17, 2008 · N382QS · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA20082885Master Cylinder · bypassingCO PILOTS LT BRAKE DEPRESSES ALL THE WAY TO THE FLOOR. PUMPING PEDAL TEMPORARILY RESTORES EFFECTIVNESS FOR A FEW SECONDS ONLY. REMOVED COMPLETE LT WHEEL BRAKE MASTER CYL PN 95367-17 SN 0921. INSTALLED OVERHAULED CO-PILOT LT WHEEL BRAKE MASTER CYL PN 95367-17Feb 16, 2008 · N312QS · Cessna 560CESSNA · Master Cylinder/Brake ValveSDR 2008FA0000155Rib · crackedFOUND SEVERAL CRACKS (25) IN RIB TO LOWER SKIN ATTACH FLANGES, AT RIVET HOLES , IN 3 LT , AND 4 RT HORIZONTAL STABILIZER INNER SPAR RIBS. RIBS NR 234 ON LT SIDE, AND NR 2345 ON RT SIDE AFFECTED.Feb 15, 2008 · N907JE · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA20082875Starter Gen · vibrationBUFFETING/GRINDING NOISE INTERMITTENT AT ALL ALTITUDES AND SPEEDS. FOUND STARTER/GENERATOR ON LT ENGINE VIBRATING EXCESSIVELY. REMOVED AND REPLACED GENERATOR IAW ULTRA MM 80-11-01. GROUND RUN OPERATIONAL CHECKS SATISFACTORY. EXTERIOR INSPECTION OF AC REVEALED Feb 14, 2008 · N373QS · Cessna 560CESSNA · Starter-GeneratorSDR DXTA20082877Unknown · warning lightAFTER GEAR RETRACTION WAS SELECTED RED INTRANSIT LIGHT REMAINED ON. JACKED AC, INSPECTED W/W AND WIRING CK'D SWITCHES IAW WDM 32-30-01-02 AND 32-60-01-04 ALL NORM. HOOKS APPEAR NORMAL. NO ABNORMAL INDICATION AT THIS TIME.Feb 14, 2008 · N367QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA20082871Brake Assy · malfunctionedCO-PILOT'S LT BRAKE DEPRESSES TO FLOOR WITH NO RESULT. COMPLETED BRAKE BLEED PROCEDURE. BRAKES OPS CHK GOOD. AMM 32-42-00.Feb 13, 2008 · N312QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA20082873Brake · weakBOTH LT BRAKES REQUIRE MORE PRESSURE THAN THE RT. REMOVED AND REPLACED LT AND RT BRAKE ASSY'S IAW MM CH. 32-42-00. BLED BRAKES IAW MM CH 32-42-00. TAXI CHECK GOOD. LEAK CHECK GOOD.Feb 13, 2008 · N322QS · Cessna 560CESSNA · Landing Gear Brake System
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