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 DXTA200802854Brake Assy · weakCO PILOTS RT BRAKE PEDAL SOFT, PRESSURE DROPS DURING BRAKING. PERFORMED ANTI-SKID BRAKE SYS BLEED PROCEDURE. BRAKES CHECK GOOD AT THIS TIME. NO PRESSURE DROP NOTED, IAW MM 32-42-00.Feb 8, 2008 · N386QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200802851Master Cylinder · leakingLT BRAKE PEDAL ON FO'S SIDE SPONGY, SQK 2. REMOVED AND REPLACED CHECK VALVE FOR CABIN PRESSURE TO BRAKE RESERVOIR. REMOVED AND REPLACED PRESSURE RELIEF VALVE FOR BRAKE RESERVOIR. ALL WORK DONE IAW MM 20-10-01 REMOVED AND REPLACED MASTER CYLINDER IN-LINE FILFeb 7, 2008 · N394QS · Cessna 560CESSNA · Master Cylinder/Brake ValveSDR DJFA2008015Coalescer Bag · odorDURING CRUISE, CREW REPORTED BURNING ODOR WITH HEAT IN AUTO OR MANUAL. AIRCRAFT LANDED SAFELY AT INTENDED DESTINATION. MAINTENANCE RAN THE ENGINES AND NOTED A MOLDY SMELL BUT NOT A BURNING SMELL. THE COALESCER BAG WAS REPLACED AND ALL SMELLS WENT AWAY.Feb 5, 2008 · N441LX · Beech 400A · Humidity Control SystemSDR DXTA200802835Indicator · inoperativeON TAKEOFF LT OIL TEMP WENT TO 0, ABORTED TAKEOFF. SWAPPED GAUGES FROM RT TO LT, STARTED ENGINES, DID FIND OIL TEMP NEEDLE DID NOT RISE TAPPED ON GAUGE AND IT CAME UP. SWAPPED GAUGES TO THE ORIGINAL POSITION, RAN ENGINES AGAIN PROBLEM STILL FOLLOWED. REPLACEDFeb 4, 2008 · N131QS · Beech 400A · Engine Oil TemperatureSDR DXTA200802836Line · wornON FO SIDE, RT BRAKE FEELS SLUGGISH COMPARED TO THE LT BRAKE. REMOVED AND REPLACED CO-PILOTS LT AND RT BRAKE MASTER CYLINDER PRESSURE AND RETURN LINES (4EA) AND BLED HYD SYS ALL WORK PERFORMED IAW MM, CH 32-42-02 AND 32-42-00.Feb 4, 2008 · N394QS · Cessna 560CESSNA · Hydraulic System, MainSDR DXTA200802837Pcu · malfunctionedROLL CONTROL FEELS ABNORMAL. CONTROLS ARE BINDING, THEN RELEASING. ESPECIALLY NOTICEABLE DURING SLOW FLIGHT. REMOVED AND REPLACED LT AND RT AILERON PCU'S IAW MM 27-11-05. OPS AND RIGGING CHECK GOOD.Feb 4, 2008 · N936QS · Cessna 750 · Aileron Control SystemSDR DXTA200802829Connector · brokenWHILE AT CRUISE ALT 32000 WITH 28 MIN INTO THE FLIGHT, ACFT FAIL LIGHT CAME ON WITH MASTER WARNING. ACFT FAIL LIGHT STAYED ON UNTIL WE RESET MASTER WARNING AFTER 5 MIN. DURING THIS TIME VOLTS SHOWED 28 AND GENS SHOW 50 AMPS EACH AND WERE STEADY. INVERTERS SHOWFeb 2, 2008 · N390QS · Cessna 560CESSNA · Electrical Power System WiringSDR DXTA200802830Switch · damagedMAIN ENTRY DOOR UNLOCK LIGHT ILLUMINATED AFTER DEPARTURE AT ABOUT 200FT AGL. FOUND DOOR LOCK SWITCH PLUNGER NOT TO HAVE ENOUGH TRAVEL. ADJUSTED PLUNGER TRAVEL IAW MM 52-10-02. OPS CHECK GOOD.Feb 2, 2008 · N379QS · Cessna 560CESSNA · Door Warning SystemSDR DXTA200802831Oxygen Mask · malfunctionedBOTH PILOT AND COPILOT OXYGEN MASK HAVE REDUCED OXYGEN FLOW, AS IF AN OBSTRUCTION OF VALVE FAILURE OCCURED. RESEATED OXYGEN MASKS OPS CHECKED SATISFACTORY IAW MM 35-00-00.Feb 1, 2008 · N324QS · Cessna 560CESSNA · Crew Oxygen SystemSDR DJFA2008013Ring · crackedDURING INSP, MAINT FOUND THE RT ENGINE INLET RING CRACKED BETWEEN THE 1200 AND 0100 O CLOCK POSITION. MAINTENANCE REPLACED THE INLET RING.Feb 1, 2008 · N408CW · Beech 400A · Air Intake Anti/De-Ice SystemSDR DXTA20082907Unknown · unknownAFTER DEPARTING, A CONTAMINATING RUNWAY GEAR UNLOCKED LIGHT, ILLUMINATED. CLEANED GEAR AND FLAP WELLS, INSPECTED, AND OPERATED SYSTEMS NUMEROUS TIMES WITH NO DEFECTS NOTED.Feb 1, 2008 · N315QS · Cessna 560CESSNA · Landing Gear SystemSDR DXTA200802815Connector · looseDURING T/O POWER APPLICATION HYD PRESS LIGHT CAME ON AT APPX 80 PERCENT N1. ABORTED T/O. GAINED ACCESS TO SPEED BRAKE SWITCHES. FOUND CONNECTOR FOR SWITCH WIRING IN LT SPEED BRAKE COVE NOT FULLY SEATED. C/W SPEEDBRAKE SWITCH RIG. SECURED CONNECTORS. C/W SJan 31, 2008 · N393QS · Cessna 560CESSNA · Flight Control System WiringSDR DJFA2008012Rib · 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. OPENJan 29, 2008 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200802805Hose · leakingF/O'S BRAKE PEDALS ARE SOFT. INSPECTED SYS AND FOUND UPPER (SUPPLY) HOSE OF CO-PILOTS RT MASTER CYLINDER BRAIDING BROKEN AND FRAYED. ALSO FOUND SWIVEL FITTING FOR BRAKES ON TOP OF LT MLG LEAKING. CLEANED AND TIGHTENED FITTING AND REPLACED FRAYED LINE. BLEEDJan 28, 2008 · N386QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DJFA2008011Hmu · malfunctionedDURING CRUISE, CREW NOTED LT ENGINE ROLL BACK FROM 95.7 TO 91.0 WITH SIMULTANEOUS FUEL FLOW AND ITT FLUX. AC WAS AT FL 380 WITH AN OAT OF -33 C IN CLEAR AIR. ENGINE ANTI-ICE WAS OFF. MAINTENANCE FOUND THE LEFT HMU FAILED. IT WAS REPLACEDJan 26, 2008 · N482LX · Beech 400A · Fuel Controlling SystemSDR 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 400A · Power LeverSDR DJFA2008008Unknown · odorIN FLIGHT, CREW REPORTED BURNING RUBBER SMELL WHEN AIR IS HOT. MAINT RAN BOTH ENGINES AND BLEED AIR SYSTEM WITH CABIN TEMP TO FULL HOT BUT COULD NOT DUPLICATE THE DISCREPANCY.Jan 24, 2008 · N464LX · Beech 400A · Air Distribution SystemSDR DJFA2008007Sensor · inoperativeDURING CRUISE CREW REPORTED BURNING ODOR NEAR THE LAV AREA. CREW CONTINUED TO DESTINATION. MAINTENANCE FOUND THE CABIN TEMP SENSOR FAILED. THE TEMP SENSOR WAS REPLACED.Jan 24, 2008 · N454LX · Beech 400A · Cabin Temperature SensorSDR DXTA200802786Switch · out of adjustINITIAL SELECTION OF FLAPS 10DEG AT 200KIAS FLAP ASYM CAUTION LIGHT CAME ON. TROUBLESHOT, ADJUSTED LT AND RT FLAP FOLLOW UP SWITCHES, AND LT FLAP POSITION TRANSMITTER, ALSO ADJUSTED RT FLAP FOLLOW UP SWITCH LINK AREA AND CHECKED FLAP TRAVEL ANGLES. ALL CHECKEJan 22, 2008 · N131QS · Beech 400A · Trailing Edge Flap Control SystemSDR DJFA2008005Bumper Block · out of adjustON TAKEOFF, AFTER RAISING THE GEAR, THE RED LIGHT IN THE GEAR HANDLE STAYED ILLUMINATED. CREW RECYCLED THE GEAR AND SAME INDICATIONS RETURNED. FLY-BY OF TOWER CONFIRMED GEAR WAS UP AND MAIN GEAR DOORS WERE DEPLOYED. CREW RETURNED TO FTY WHERE MAINT FOUND THE Jan 21, 2008 · N447LX · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2008006Hmu · out of adjustDURING TAXI, PRIOR TO FLIGHT, WHILE PERFORMING THE EFC AUTHORITY CHECK THE NR1 ENGINE SHUTDOWN. MAINT FOUND THE NR1 HMU OUT OF ADJUSTMENT. THE HMU WAS ADJUSTED IAW THE MM AND THE ENGINE OPERATIONAL CHECK WAS SUCCESSFUL.Jan 21, 2008 · N712TA · Beech 400A · Fuel Control/Turbine EnginesSDR E0X2008F00000Engine · bird ingestionAFTER FULLY CONFIGURING AC FOR LANDING, ON APPROACH, AT APPROX 1500 FT, AGL AND 5 MILES FROM RUNWAY, AC SUFFERED A BIRD INGESTION AND CATASTROPHIC RT ENGINE FAILURE. THIS WAS FOLLOWED BY A SUCCESSFUL EMERGENCY LANDING WITH NO INJURIES TO PASSENGERS OR CREW. Jan 18, 2008 · N52AW · Beech 400A · Engine (Turbine/Turboprop)SDR DXTA200802772Squat Switch · inoperativeIMMEDIATELY AFTER T/O GEAR HANDLE WOULD NOT RELEASE TO RETRACT GEAR. FOUND LEFT SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED LT SQUAT SWITCH. SYSTEM OPERATION CHECKS GOOD. WORK PERFORMED IAW CH. 32-61-00 OF THE 560 CES. M.M.Jan 16, 2008 · N319QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200802765Wire Harness · shortedAT APPROXIMATELY 70 KNOTS THE ANTI-SKID INOP LIGHT CAME ON. ABORTED THE TAKEOFF. REMOVED THE LT ANTI-SKID TRANSDUCER WIRE BUNDLE FROM LEFT GEN TO WHEEL WELL CONNECTOR DUE TO OPEN. INSTALLED NEW WIRE BUNDLE IAW CE5650 M/M CH 32-42-00. OPS CHECKED GOOD.Jan 13, 2008 · N314QS · Cessna 560CESSNA · Landing Gear System WiringSDR DXTA200802753Wire · damagedON INITIAL CLIMB OUT LANDING GEAR HANDLE WOULD NOT MOVE. REPLACED 5 EA WIRE SPLICES AT LT MAIN GEAR SQUAT SWITCH, REPACKED LT MAIN GEAR STRUT, SERVICED STRUT, IAW 560 MM 32-11-02, 32-61-00, 32-42-01, 12-14-01 PERFORMED GEAR SWING, OPS CHECKED GOOD, IAW 560 MJan 8, 2008 · N374QS · Cessna 560CESSNA · Landing Gear System WiringSDR DXTA200802748Brake Assy · malfunctionedUPON LANDING WITH NORMAL BRAKING ON DRY RUNWAY THE BRAKES PULSED HEAVILY CAUSING THE A/C TO SKID CONTINUALLY. INSPECTED WHEELS, TIRES, BRAKES, PERFORMED HUB CAP INSPECTION, CHECKED BRAKE ACCUMULATOR. TAXIED AIRCRAFT, NO DEFECTS FOUND, WORK DONE IAW MM 32-00-Jan 5, 2008 · N151QS · Beech 400A · Landing Gear Brake SystemSDR EOX2008F00001Sealant · smokeAC EXPERIENCED SMOKE IN THE CABIN AT FL 22 ENROUTE, FLIGHT CREW FOLLOWED PROCEDURE WITH CAPTAIN DAWNING O2 MASK AND 2ND OFFICER INSPECTING CABIN. NO DISCREPANCIES WERE NOTED OTHER THAN SMOKE IN CABIN, WHICH WAS DISSIPATING. FLIGHT CREW FELT THAT THE ISSUE WAJan 5, 2008 · N527XP · Beech 400A · Airfoil Anti/De-ice SystemSDR DJFA2008001Uplock Switch · erraticDURING CLIMB-OUT CREW REPORTED RED LIGHTS IN GEAR SELECT HANDLE ILLUMINATED FOLLOWED BY SLIGHT DECELERATION AND A THUMP. CREW SUSPECTS THE GEAR EXTENDED AND RETRACTED UNCOMMANDED. MAINTENANCE FOUND THE LT MLG UPLOCK SWITCH ERRATIC IN COLD TEMPERATURES. THE Jan 2, 2008 · N709TA · Beech 400A · Landing Gear Position and WarningSDR DXTA200802740Control Unit · malfunctionedRED HSTAB FAIL WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. REPLACED 170 AND 180 KNOT AIRSPEED SWITCHES WITH NEW IAW HAWKER 400XP WIRING MANUAL CH 30-12-01. REPLACED OAT BIAS BOX WITH NEW IAW HAWKER 400XP MM CH 32-12-00. H-STAB DEICE SYSTEM OPS CHECK GOODJan 1, 2008 · N125QS · Beech 400A · Central WarningSDR DJFA2007153Downlock Switch · inoperativeON APPROACH CREW REPORTED THE LT MAIN GEAR DOWN AND LOCKED LIGHT WOULD NOT ILLUMINATE. GEAR WAS CYCLED 6 TIMES AND ON THE 6TH ATTEMPT THE DOWN AND LOCKED LIGHT FINALLY ILLUMINTATED. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE LTDec 31, 2007 · N463LX · Beech 400A · Landing Gear Position and WarningSDR DXTA200702723Unknown · unknownACFT DID NOT PRESSURIZE ON DEPARTURE. GROUND RAN AIRCRAFT CK LEFT AND RIGHT ENGINE SEPARATELY FOR PRESSURIZATION. OPS CK GOOD. CHECK PRE PRESS. OP'S CK GOOD. INSPECTED AND OP'S CK WOW SWITCH OP'S CK GOOD. NO DEFECTS NOTED ON GROUND IAW CESSNA 560 MM CH 21-31-Dec 30, 2007 · N335QS · Cessna 560CESSNA · Cabin Pressure Control SystemSDR DJFA2007152Terminal · looseON CLIMB OUT CREW REPORTED A BURNING ODOR FROM THE PILOT'S CIRCUIT BREAKER PANEL. MAINTENANCE FOUND A LOOSE TERMIAL ON A CIRCUIT BREAKER ON THE NON-ESSENTIAL BUSS. THE TERMIAL APPEARED TO BE OVERHEATED AND WAS REPLACED.Dec 29, 2007 · N783TA · Beech 400A · Electrical Power System WiringSDR DXTA200702725Unknown · malfunctionedAFTER ESTABLISHING A POSITIVE RATE FOR TAKEOFF, ATTEMPTED TO RETRACT MLG. MLG HANDLE WOULD NOT RETRACT. NOTICED ALL LIGHTS EXTINGUISHED AND CB BREAKER POPPED. MLG CB WOULD NOT RESET, MANUALLY EXTENDED MLG AS A PRECATIONARY MEASURE AND LANDED SAFELY. RESET CIDec 28, 2007 · N340QS · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA200702728Line · contaminatedEMERGENCY DECLARED, LOST PRESSURIZATION WHILE IN CRUISE AT FL390. HEARD AUDIBLE "POP" FOLLOWED BY AIR "HISSING" AND CABIN CLIMBING AT >4000 FPM. CABIN ALT REACHED 10000 FEET. DEPLOYED MASKS MANUALLY FOR ELDERLY PAX. PERFORMED EMER DESCENT CABIN REMAINED NEADec 28, 2007 · N335QS · Cessna 560CESSNA · Passenger/Crew DoorsSDR DJFA2007150Unknown · odorIN CRUISE, CREW NOTED BURNING ODOR FROM HEAT DUCTS. MAINTENANCE TESTED THE ENVIRONMENTAL SYSTEM BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY.Dec 26, 2007 · N783TA · Beech 400A · Air Distribution SystemSDR CA080116011Fuel Control · inoperative(CAN) DURING APPROACH, THE ENGINE DID NOT RESPOND TO THRUST LEVER INPUTS AND REMAINED AT IDLE. AFTER LANDING GROUND TESTS INDICATED THAT THE ENGINE WOULD NOT ACCELERATE ABOVE 46 PERCENT, N2. THE FUEL CONTROL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NDec 26, 2007 · Cessna 560CESSNA · Fuel Controlling SystemSDR DJFA2007149Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION 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 COMMUNIQUDec 24, 2007 · N793TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007148Fan · overheatedON LANDING CREW REPORTED BURNING ODOR IN THE CABIN. MAINTENANCE FOUND THE CABIN TEMP SENSOR FAN OVERHEATING. THE FAN WAS REPLACED.Dec 22, 2007 · N439LX · Beech 400A · Air Distribution FanSDR DXTA200702706Gyro · inoperativeNR 1 HEADING INDICATOR FAILED. 1 PFD, STANDBY HEADING INDICATOR AND MFD HEADING INDICATOR FAILED. REMOVED & REPLACED NR 1 DG IAW CE560 MM CHAPTER 34-21-05. OPS CHECKS GOODDec 22, 2007 · N322QS · Cessna 560CESSNA · Directional Gyro and Indicating SystemSDR DXTA200702708Control Box · inoperativeON LANDING AND AFTER APPLYING THE BRAKES, THE BRAKES SEEMED TO GRAB AND WE BEGAN TO SKID. THE RT MAIN TIRE BLEW. AIRCRAFT VEERED TO THE RT SKIDDING OFF THE RWY. NO OTHER DAMAGE TO AIRCRAFT OBSERVED ON POST FLIGHT. REMOVED AND REPLACED ELECTRONIC CONTROL BOX IDec 22, 2007 · N319QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200702712Computer · inoperativeRUDDER BOOST FAIL LIGHT CAME ON AND YAW DAMPNER/AUTOPLOT KICKED OFF AT F230 LEVEL FLIGHT AT THE SAME TIME. REPLACED #1 FGC-4007 WITH OVH. UNIT IAW ROCKEWELL COLLINS MANUAL 523-0225807-0411A REV 9 OCT. 2005. GROUND OPS CHECK GOOD.Dec 21, 2007 · N117QS · Beech 400A · Autopilot SystemSDR DXTA200702697Controller · inoperativeWINDSHIELD OVERHEAT ANNUNCIATOR ILLUMINATED WITH WINDSHIELD HEAT SELECTED ON IN THE LOW POSITION. RAN CHECKLIST AND SELECTED OFF. CONDITION OCCURED ABOUT 30 TO 60 SECONDS AFTER SELECTING ON. HOT BURNING ODOR WAS PRESENT.KSPI-KLAL. TROUBLESHOT PROBLEM DOWN TO ADec 20, 2007 · N335QS · Cessna 560CESSNA · Windshield/Door Rain/Ice RemovalSDR DXTA200702700Bulb · burned outLT MAIN GEAR DOWN AND LOCK INDICATION INOPERATIVE. REPLACED LT MAIN LANDING GEAR DOWN INDICATION BULB. OPS CHECK GOOD IAW HAWKER 400XP MM CH 32-60-00.Dec 20, 2007 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200702692Bracket · crackedPILOT SIDE BRAKES ARE VERY SOFT AND MORE THAN NORMAL TRAVEL FOR BRAKES TO GRAB. FOUND PILOT'S RUDDER PEDAL SUPPORT BRACKET ASSY CRACKED. REMOVED AND REPLACED BRACKET ASSY WITH NEW I/A/W CE560 S/R/M 51-30-03. PERFORMED BLEEDING PROCEDURE OF ANTI-SKID SYSTEM. PDec 19, 2007 · N351QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR CA071220004Hose · cracked(CAN) ALL GEARS DOWN AND LOCK WITH (3) GREEN LIGHTS. WHEN PILOT SELECTED FLAPS DOWN, LT HYD FLOW LIGHT COMES ON AND FOLLOW THE RT SIDE. FINALLY, HYD FLUID LEVEL LIGHT COMES ON. AC LANDED SAFELY WITH NO HYD SYS AVAILABLE. FOUND LT ENG HYD PRESSURE HOSE CRACKEDec 15, 2007 · Cessna 560CESSNA · Hydraulic System, MainSDR DXTA200702678Warning System · false activationRED LIGHTS IN GEAR HANDLE REMAINED ILLUMINATED AFTER GEAR RETRACTION. UPON EXTENTION THE RED LIGHTS WENT OUT AND (3) GREENS ILLUMINATED. JACKED AC VISUALLY INSPECTED LANDING GEAR UPLOCK AND DOWN LOCK SWITCHES. VISUALLY INSPECTED MLG DOOR SWITCHES. NO DEFECTS Dec 14, 2007 · N154QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200702680Grommet · wornFL410 AT CRUISE, SOUND OF SIGNIFICATE AMOUNT OF AIR PASSING THRU MAIN CABIN DOOR.CABIN PRESSURE MAINTAINED. ADJUSTED DOOR FRAME SOCKETS AS REQUIRED DUE TO DOOR SEAL CLEARANCE GAPS AND REPLACED DOOR SEAL GRUMMET WITH NEW GROMMET DUE TO WEAR IAW THE 560 MM CHAPDec 14, 2007 · N332QS · Cessna 560CESSNA · Passenger/Crew DoorsSDR DJFA2007142Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUDec 13, 2007 · N741TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007143Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, THE RIGHT INBOARD RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINEDDec 13, 2007 · N743TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200702675Uplock Switch · out of adjustAFTER RETRACTING THE GEAR, THE HYD PRESS ON LIGHT AS WELL AS THE GEAR UNLOCKED LIGHTS WERE ON. WE RAN THE CHECKLISTS BROUGHT THE GEAR DOWN AND USED THE BLOW DOWN AS A PRECAUTION. INSPECTED AND ADJUSTED UP-LOCK SWITCH. OPS CHECKED GOOD IAW CESSNA 560 MM 32-31Dec 13, 2007 · N330QS · Cessna 560CESSNA · Landing Gear Position and Warning
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