GE CF34-3B1

Service difficulty reports · 5,402

Newest first. General aviation reporting is voluntary.

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 = 'CF343B1'
  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 VNAA0805011Flap System · malfunctionedCREW REPORTED A FLAPS FAIL AT 0 DEGREES DURING FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. SYSTEM OPS CHEMay 8, 2008 · N259PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0805009Flap System · malfunctionedCREW REPORTED A FLAPS FAIL AT 20 DEGREES WARNING MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO LEX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A FUNCTIONAL TEST OF THE FECU BIT TEST SKEW DETECTION. SYSTEM OPS CHECKED GOOD AND MESSAGEMay 6, 2008 · N207PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0805006Fcu · failedCREW REPORTED ON APPROACH A FLAPS FAIL AT ZERO INDICATION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEMay 5, 2008 · N259PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0805005Detection Sys · malfunctionedCREW REPORTED ON APPROACH A FLAPS FAIL AT ZERO INDICATION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE SKEW DETECTION UNIT AND CYCLED THE FLAP CIRCUIT BREAKER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL May 5, 2008 · N259PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA0805007Elbow · failedCREW REPORTED A NR 3 HYDRAULIC LOW PRESSURE IN FLIGHT. CREW ELECTED TO DIVERT TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BULKHEAD ELBOW IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO PROPERLY SERVICED THE May 5, 2008 · N251PS · Cndair CL6002B19 · Hydraulic System, MainSDR VNAA0805002Engine · overtempCREW REPORTED AT 125KTS, RECEIVED AN ITT INDICATION ON THE NR 2 ENGINE. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE MDC AND FOUND THE OVERTEMP TO BE 902 FOR 3.2 SECONDS IN AREA A ON THE RIGHT HANDMay 1, 2008 · N241PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0804023Control Unit · failedCREW REPORTED AN AMBER PITCH TRIM, MACH TRIM AND AUTO PILOT PITCH TRIM CAS MESSAGES ON CLIMB TO CRUISE OUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT WHERE EMERGENCY EQUIPMENT DID RESPOND. MAINTENANCE REMOVED AND REPLACED THE HSTCU INApr 30, 2008 · N223JS · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200819574Engine · malfunctionedFLT 6723 - LEFT ITT CLIMBED TO 903°C AND TAKEOFF WAS ABORTED. REPLACED LEFT ENGINE ASSEMBLY IAW AMM 71-00-00. OPS CHECK AND LEAK CHECK GOOD. Apr 28, 2008 · N924SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0804020Oil System · lowCREW REPORTED AN APU OIL CAUTION MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND VISUALLY CHECKED THE APU OIL LEVEL AND APU OIL SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OIL LEVEL CHECApr 27, 2008 · N254PS · Cndair CL6002B19 · APU System WiringSDR VNAA0804019Warning Light · false activationCREW REPORTED ON CLIMBOUT A LEFT EMERGENCY DOOR MESSAGE. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT HAND EMERGENCY DOOR AND FOUND NO DEFECTS. MAINTENANCE DEFERRED THE DOOR INDICATION ONLY PER MEL 52-70-03. MAIApr 26, 2008 · N237PS · Cndair CL6002B19 · Door Warning SystemSDR VNAA0804018Idg · underservicedCREW REPORTED A NR 1 IDG AND NR 1 GENERATOR INOP CAS MESSAGES ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PROPERLY SERVICED THE NR 1 IDG OIL LEVEL. NO LEAKS NOTED, OPS CHECKS WERE GOOD. AIRApr 26, 2008 · N259PS · Cndair CL6002B19 · AC Generator-AlternatorSDR VNAA0804017Tire · separatedCREW REPORTED ON TAKEOFF ROLL FELT A BUMP. AT DESTINATION, MAINTENANCE INSPECTED AND FOUND THE LEFT INBOARD MAIN TIRE HAD SEPARATED AND CAUSED DAMAGE TO THE UNDERNEATH PORTION OF THE LEFT WING AND LANDING GEAR. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOAApr 24, 2008 · N262PS · Cndair CL6002B19 · TireSDR SWIA200819855Mount · corrodedLT ENGINE MOUNT THRUST FITTING IS CORRODED. (FOUND AT C-CHECK) REPLACED THRUST FITTING ON IAW AMM 71-22-01-400-801. Apr 23, 2008 · N955SW · Cndair CL6002B19 · Engine Mount SectionSDR CHQA200800084Position Sensor · malfunctionedFLIGHT 5612, IAH TO CMH - DURING CLIMB, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WITH THE FLAPS FAILED AT ZERO DEGREES. THE FLIGHT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLAP CONTROL CHANNELS 1 AND 2 AND THE FAULT CLEAApr 21, 2008 · N639BR · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR MASA200800324Scavenge Pump · malfunctionedASH FLT 7140 ORD. RT ENGINE OIL PRESSURE FLUCTUATES AT +/- 6 ABOVE IDLE. CREW DECLARED AN EMERGENCY. REPLACED LUBE SCAVENGE PUMP, OP CHECK GOOD.Apr 19, 2008 · N75995 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200840346Connector · looseGROUND LIFT DUMP AUTO DEPLOY ON ENGINE START. TIGHTENED RADIO ALTIMETER ANTENNA COAX CONNECTOR AND PERFORMED BONDING TEST PER AMM 51-80-00. SPOILER CONTROL SYSTEM OPS CHECK GOOD IAW AMM 27-65-00. RADIO ALTIMETER OPS CHECK GOOD IAW 34-44-01.Apr 17, 2008 · N464AW · Cndair CL6002B19 · Ground Proximity SystemSDR A6WA200840348Snubber · crackedNR 1 T/R ACTUATOR AT 2 O`CLOCK POSITION SNUBBER AND SNUBBER COVER FOUND CRACKED AND BRACKET. (K) REPLACED SNUBBER AND SNUBBER COVER IAW SRM 51-42-06.Apr 14, 2008 · N404AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200840338Engine · bird ingestionLARGE BIRD INGESTED, LEFT ENGINE AT 1000 AGL DURING TAKEOFF FROM PHL, GEAR EXTENDED PERFORMED AIR RETURN TO PHL, LANDED AT 43,700 LBS. C/W BIRDSTRIKE INSP REF AMM 05-51-25 REF W/O 123145 FOR AW WORK FOUND.Apr 14, 2008 · N428AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0804012Steering Sys · malfunctionedCREW REPORTED A LOSS OF DIRECTIONAL CONTROL ON TAKEOFF. THE ACFT PULLED LEFT AND WAS UNCONTROLLABLE WITH THE RUDDER. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE LANDING GEAR AND FOUND NO DEFECTApr 14, 2008 · N246PS · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA200840349Snubber · crackedT/R ACTUATOR AT 1 O`CLOCK POSITION, SNUBBER AND SNUBBER COVER FOUND CRACKED. (K) REPLACED IAW SRM 51-42-06.Apr 13, 2008 · N404AW · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA0804013Fcu · failedCREW REPORTED A FLAPS FAIL CAS MESSAGE DURING APPROACH/LANDING. THE ARFF RESPONDED AND THE ACFT TAXIED TO THE GATE. MAINTENANCE INSPECTED AND DEFERRED THE FECU PER MEL 27-51-01-2. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE ACFT MAINTENApr 11, 2008 · N221PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0804008Winglet · crackedCREW REPORTED A CRACK IN THE RIGHT HAND WINGLET. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND WINGLET TO BE WITHIN LIMITS IN ACCORDANCE WITH THE CRJ200 STRUCTURAL REPAIR MANUAL. MAINTENANCE APPLIED SPEED TAPE. AIRCRAFT WAS RELEASED FOR SERVICE.Apr 10, 2008 · N259PS · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200840347Floor Support · corrodedFLOOR SUPPORT ANGLE BTW FS 319.70 AND FS 349.0 IB OF SERVICE DOOR, BTW RBL 27.00, FOUND CORRODED. (K) FLOOR SUPPORT FABRICATED WITH FORMED ANGLE RAW MATERIAL P/N S6144-14 IAW SRM 51-24-21 AND INSTALL IAW SRM 51-42-06.Apr 8, 2008 · N404AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840293Sill · corrodedCARGO BAY FLOOR SILL BETWEEN FS 574 TO FS 621, ALL NUT PLATE HOLES CORRODED. CORROSION REMOVED IAW SRM 51-21-06 .Apr 7, 2008 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840294Scuff Plate · corrodedCORROSION UNDER SERVICE DOOR SCUFF PLATE. (K) CORROSION REMOVED IAW SRM 51-21-06.Apr 7, 2008 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA080407003Actuator · unserviceableON APPROACH AT 4000 FT SELECTING FLAPS FROM 0 - 8 DEG, FLAP FAIL MSG APPEARED IMMEDIATELY WITH NO MOVEMENT OF FLAPS. AIRSPEED 215 AT THE TIME. A/C WAS AT -57 DEG FOR 1 HR IN CRUISE, GND -4. FECU INTERGRADED AND FOLLOWING FAULT CODES DISPLAYED AS FECU WAS LOApr 6, 2008 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR VNAA0804005Flap · damagedCREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT HAND INBOARD FLAP TRAILING EDGE AND REPAIRED THE DAMAGE UNDER REO 601R-57-52-732 AND THE AIRCRAFT MAIApr 5, 2008 · N216PS · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA0804003Outflow Valve · failedCREW REPORTED A CABIN ALTITUDE CAUTION MESSAGE ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PRESSURIZATION SYSTEM. MAINTENANCE REMOVED AND REPLACED THE PRIMARY OUTFLOW VALVE IApr 4, 2008 · N206PS · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR A6WA200840297Attach Fitting · corrodedCARGO DOOR FITTING ATTACHMENT FS 589 AND FS 605 CORRODED. (K) CORROSION REMOVED ON CARGO DOOR FITTING ATTCHMENT AT FS 589 AND 605 IAW SRM 51-21-06 . (A)Apr 4, 2008 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0804002Connector · looseCREW REPORTED A LEFT ENGINE MISCOMPARE MESSAGE DURING CRUISE. CREW REDUCED THRUST PER THE QRH AND CONTINUED TO STL AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED AND THE EQUIPMENT DID RESPOND. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINES LEFT HAApr 3, 2008 · N220PS · Cndair CL6002B19 · Engine Indicating System WiringSDR A6WA200840296Skin · crackedCRACK FOUND ON RT WING, AFT OF LANDING EDGE AT WS 343, BTWN ACCESS PANEL 603 LZ AND 630 KZ. (K) RT WING L/E ON THE REAR SIDE AT WEB FABRICATED IAW SRM 51-24-16. RT WING L/E ON THE REAR SIDE AT WS 343 WEB INSTALLED IAW SRM 51-42-13. (A)Apr 2, 2008 · N403AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR CA080402007Warning Light · illuminatedAT THE TOP OF DESCENT WHEN PULLING BACK POWER, THE CREW GOT THE "LOW OIL PRES WARNING" ON THE LT ENG, SHORTLY FOLLOWED BY THE LOW OIL PRES INDICATION. ALL OTHER PARAMETERS NORMAL. CREW THEN ACTIONED EMERGENCY PROCEDURES AND SHUT DOWN LT ENG AND LANDED. (TC NApr 2, 2008 · Cndair CL6002B19 · Central WarningSDR CHQA200800069Windshield · crackedFLIGHT 5598, DFW TO CLE, DURING CRUISE, THE FLIGHT CREW REPORTED THAT THE LEFT WINDSHIELD CRACKED. THE FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE.Mar 31, 2008 · N656BR · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200840295Bulkhead · crackedCRACK FOUND ON PRESSURE BULKHEAD FSW 202.75, LBL 23.71, AROUND PARKING BRAKE. (K) REPAIR ON FWD PRESSURE BULKHEAD IAW REO 601R-53-11-563.Mar 31, 2008 · N403AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR CHQA200800068Oil Cooler · cloggedFLIGHT 5756, IAH TO SDF - DURING CRUISE, THE CREW RECEIVED AN APU HIGH OIL TEMPERATURE MESSAGE ON EICAS. THE FLIGHT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND VERIFIED THE OIL WAS SERVICED TO THE CORRECT LEVEL. THE CONNECMar 30, 2008 · N466CA · Cndair CL6002B19 · APU Oil SystemSDR CA080409004Controller · overtempON DESCENT THROUGH 21000 FEET INTO ARRIVAL AIRPORT, CAPTAIN’S LT WINDSCREEN SHATTERED. CREW DONNED OXYGEN MASKS AS A PRECAUTION. CREW DECLARED AN EMERGENCY WITH ATC AND MADE ANNOUNCEMENT TO THE PASSENGERS. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACMar 30, 2008 · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR CHQA200800062Oil Cooler · leakingFLIGHT 5601, IAH TO JAX - DURING CRUISE THE CREW RECEIVED AN APU OIL TEMP MESSAGE ON EICAS. THE PROPER QRH CHECKLISTS WERE FOLLOWED, AND THE FLIGHT DIVERTED TO PNS, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND THAT IT WAS LOW ON Mar 28, 2008 · N466CA · Cndair CL6002B19 · APU Oil SystemSDR VNAA0803012Panel · damagedCREW REPORTED A LIGHTNING STRIKE DURING DESCENT INTO LEX. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT WING PANELS. MAINTENANCE REPAIRED DAMAGE PER REO 601R-57-31-1005. OPERATIONAL CHECMar 28, 2008 · N229PS · Cndair CL6002B19 · Wing, Plate/SkinSDR CHQA200800060Oil System · lowIAH TO ATL - AFTER LEVELING OFF IN CRUISE FLIGHT, THE CREW RECEIVED AN APU HIGH TEMP MESSAGE ON EICAS. AFTER FOLLOWING THE APPROPRIATE QRH CHECKLISTS THE FLIGHT DIVERTED TO MGM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND IT WAS Mar 27, 2008 · N466CA · Cndair CL6002B19 · APU Oil SystemSDR 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 CL6002B19 · Power LeverSDR MASA200800240Engine · malfunctionedASH FLT 7347 ORD-BHM, CAPT REPORTS HEARING A LOUD POPPING NOISE FROM NR 2 ENGINE FOLLOWED BY HIGH ITT (RED-LINE) AND ENGINE VIB. CAPT SHUTDOWN NR 2 ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO SPI. REMOVED AND REPLACED NR 2 ENGINE.Mar 19, 2008 · N27185 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR SWIA200819648Bearing · corrodedLEFT ENGINE YOKE LINK BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED LINK ASSEMBLY PER CRJ200 AMM TASK 71-21-01-420-001 SECTION A. Mar 19, 2008 · N952SW · Cndair CL6002B19 · Engine Mount SectionSDR CA080320002Connector · damagedTASK NR 27-34-05-710-801 WAS BEING PERFORMED ON THE ELEVATOR FLUTTER DAMPERS. IT FAILED THIS TASK FOR LOW FLUID LEVEL TRANSMITTER SWITCHES. THIS TASK WAS CALLED UP DURING THE AIRCRAFT`S PLANNED HEAVY INSPECTION. T HERE WERE NO REPORTED FAILURES WHILE THE AIRMar 18, 2008 · Cndair CL6002B19 · Flight Control System WiringSDR VNAA0803009Door · openCREW REPORTED A NOISE COMING FROM THE NOSE AREA ON TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COMMUNICATION SERVICE DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED AND FOUND NO DEFECTS OR DAMAGE. Mar 16, 2008 · N207PS · Cndair CL6002B19 · Accessory Compartment DoorsSDR CHQA200800052Connector · looseMAF TO IAH - WHILE CLIMBING THROUGH 17,000 FT, THE CREW RECEIVED AT L REV UNLOCKED MESSAGE ON EICAS WITH A REV ICON ON THE N1 GAUGE. THERE WAS NO DEGRADATION OF AIRCRAFT PERFORMANCE NOTED. THE CREW PERFORMED THE APPROPRIATE CHECKLISTS AND RETURNED TO MAF. MMar 15, 2008 · N638BR · Cndair CL6002B19 · Engine Exhaust System WiringSDR VNAA0803007Radome · damagedCREW REPORTED ON APPROACH A LIGHTNING STRIKE TO THE NOSE AREA. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RADOME AND OTHER AREAS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THEMar 15, 2008 · N206PS · Cndair CL6002B19 · Aerodynamic FairingsSDR CA080314002Engine · fire(CAN) AC LANDED, AFTER THE PILOT HAD DECLARED AN EMERGENCY FURTHER TO A FIRE ON ENG NR 2. THE AC FLEW IN CRUISE AT FL 220, WHEN THE PILOT GOT A FIRE ALARM ON ENG 2. THE TEMP (ITT) OF ENGINE SHOWED CLEARLY THAT AN ACTUAL FIRE HAD BROKEN OUT. PILOT DECLARED AN EMar 13, 2008 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CHQA200800049Outflow Valve · malfunctionedIAH TO CMH - AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE AND AN OVERBOARD COOL MESSAGE WAS DISPLAYED ON EICAS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE OVERBOARD EXHAUST SHUTOFF VALVE. THE VALVE WMar 12, 2008 · N639BR · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR VNAA0803005Trim System · malfunctionedCREW REPORTED THE STAB TRIM & MACH TRIM WILL NOT ENGAGE ON CLIMBOUT. CREW ELECTED TO RETURN TO LEX AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED THE HSTCU CIRCUIT BREAKERS, PERFORMED A MEMORY RESET AND PERFORMED AN OPS CHECK IN ACCORDANCE WITH THE AIRCRAFTMar 10, 2008 · N206PS · Cndair CL6002B19 · Stabilizer Control SystemSDR VNAA0803004Adc · failedCREW REPORTED 20 KNOT INDICATED AIRSPEED SPLIT BETWEEN CAPTAINS AND FIRST OFFICERS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE CAPTAINS AND STANDBY TO AGREE BUT THE FIRST OFFICERS TO BE 20 KNOTS SLOW. Mar 7, 2008 · N248PS · Cndair CL6002B19 · Air Data Computer
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