Allison AE-3007A

Service difficulty reports · 3,309

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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 = 'AE3007A'
  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 CHQA200800082Fan · faultyFLIGHT 7795, IAD TO YYZ - AFTER TAKEOFF, UPON GEAR RETRACTION, FLT CREW NOTICED A SLIGHT HAZE IN COCKPIT. FLT CREW PERFORMED CHECKLISTS AND RECIRCULATION FAN TURNED OFF, AFTER WHICH THE SMOKE DISAPPEARED. FLT ATTENDANT VERIFIED SLIGHT HAZE IN CABIN AS WELL.Apr 20, 2008 · N977RP · Emb EMB145LR · Air Distribution FanSDR CHQA200800080Pump · overheatedFLIGHT 5901, CLE TO MSY - WHILE CRUISING AT FL360 THE FLIGHT CREW RECEIVED A MASTER CAUTION AND EICAS MESSAGE FOR HYD SYS 1 OVHT. THE CREW RAN THROUGH THE APPROPRIATE QRH CHECKLISTS AND SHUT OFF THE SYSTEM. AFTER WAITING THE QRH RECOMMENDED TIME, THE NR 1 HYApr 19, 2008 · N287SK · Emb EMB145LR · Hydraulic Pump (Electric/Engine), MainSDR CHQA200800081Wire Harness · faultyFLIGHT 7844, IAD TO CMH - DURING CLIMB WHEN THE CREW ATTEMPTED TO RAISE THE GEAR THEY RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS AND THE LANDING GEAR WOULD NOT RETRACT. THE CREW PERFORMED THE APPROPRIATE CHECK LISTS AND LANDED WITHOUT INCIDENT. MAINTENANCE Apr 19, 2008 · N292SK · Emb EMB145LR · Landing Gear System WiringSDR CHQA200800079Gasket · missingFLIGHT 6239, BOS TO SAV, DURING CRUISE, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW OF A FLUID LEAK COMING FROM THE LEFT WING. THE FLIGHT CREW VERIFIED THE FLUID LEAK AND DIVERTED TO IAD. THE FLIGHT LANDED WITHOUT INCIDENT IN IAD. MAINTENANCE INSPECTED THApr 14, 2008 · N566RP · Emb EMB145LR · Fuel StorageSDR CHQA200800078Switch · faultyFLIGHT 6360, CVG TO STL - DURING CLIMB IN ICING CONDITIONS, CREW RECEIVED AN E1 BLEED VALVE FAIL MESSAGE, WITH THE ASSOCIATED BLEED VALVE CLOSED AND WING ANTI-ICE FAIL MASTER WARNING. THE CREW RAN THE APPROPRIATE QRH CHECKLISTS AND RETURNED TO CVG. THE AIRCRApr 13, 2008 · N568RP · Emb EMB145LR · Pneumatic SystemSDR FDKA200804157Engine · malfunctionedFDM FLT 9962 BWI-JFK (0650 PHX LCL). LAV SMOKE WARNING IN FLIGHT WITH SMOKE IN THE CABIN AND FLIGHT DECK. MX REMOVED AND REPLACED NR 2 ENG, OPS GOOD.Apr 13, 2008 · N844MJ · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA200800077Fan · inoperativeFLIGHT 3019, GSO TO CLT, DURING INITIAL CLIMB AT APPROXIMATELY 2,000 FT THE FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN THE CABIN EMANATING FROM THE GASPER VENTS. THE FLIGHT CREW CONTACTED DEPARTURE TO RETURN TO FIELD AND FOLLOWED APPROPRIATE QRH CHECKLISTS. Apr 12, 2008 · N259JQ · Emb EMB145LR · Air Distribution FanSDR CHQA200800074Windshield · crackedFLIGHT 5801, BDL TO CLE - IN CRUISE AT FL240, WITH WINDSHIELD HEAT ON, THE CREW HEARD A LOUD POP AND NOTICED THAT THE CAPTAIN'S WINDSHIELD HAD SHATTERED (SPIDER WEBBED). THE FLIGHT DIVERTED TO SYR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIApr 10, 2008 · N285SK · Emb EMB145LR · Flight Compartment WindowsSDR CHQA200800075Electronic Unit · faultyFLIGHT 7827, IAD TO CMH - AFTER TAKEOFF, CREW ATTEMPTED TO RAISE THE LANDING GEAR AND RECEIVED A "LG AIR/GND FAIL" MESSAGE AND THE GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE LGEUApr 10, 2008 · N292SK · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA200800076Hydraulic System · malfunctionedFLT 5284, AFTER LANDING, THE AIRCRAFT ENCOUNTERED A HYDRAULIC FAILURE AFFECTING BRAKING AND STEERING. APPROXIMATELY 3 SECONDS INTO ROLL-OUT THE AIRCRAFT BEGAN TO VEER TO THE LEFT AND A RUDDER SYS 1-2 INOP MESSAGE APPEARED ON EICAS. NORMAL BRAKING THEN BECAMApr 10, 2008 · N374SK · Emb EMB135KL · Hydraulic System, MainSDR CHQA200800073Engine · leakingFLIGHT 5940. CREW RETURNED TO FIELD FOR A LAV SMOKE INDICATION ON EICAS. MAINT FOUND THE LAVATORY SMOKE DETECTOR FULL OF DUST. AFTER CLEANING THE SMOKE DETECTOR THE SYS WAS OPS CHECKED GOOD. LATER THAT DAY THE MESSAGE RETURNED WHILE ON APPROACH AND CLEAREDApr 9, 2008 · N291SK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA200800072Pressure Switch · inoperativeFLIGHT 5284, STL TO BDL, DURING CRUISE AT FL340, THE CREW RECEIVED A RUDDER SYS 1-2 INOP EICAS MESSAGE, FOLLOWED BY AUTOPILOT AND YAW DAMPER FAIL. THE QRH WAS FOLLOWED AND THE RUDDER 2 BUTTON WAS RELEASED WHICH THEN RESTORED POWER TO THE RUDDER 1 SYSTEM. THEApr 4, 2008 · N380SK · Emb EMB135KL · Rudder Control SystemSDR CHQA200800070Holder · chafedFLIGHT 6217, CAK TO CVG. WHILE CRUISING AT FL200, THE FLIGHT CREW NOTICED THE COCKPIT BEGAN TO FILL WITH SMOKE. THE PROPER QRH CHECKLISTS WERE FOLLOWED AND THE FIRST OFFICER NOTICED THE SMOKE WAS COMING FROM HIS CHART HOLDER. AFTER TURNING OFF THE CHART HOLApr 1, 2008 · N843RP · Emb EMB135LR · Flight Compartment LightingSDR CHQA200800071Engine · making metalFLIGHT 6221, CHA TO CVG - JUST OUTSIDE THE OUTER MARKER THE FLIGHT CREW SMELLED SMOKE AND BEGAN RUNNING THROUGH THE QRH CHECKLISTS. ONCE CLEARED TO LAND A LAV SMOKE EICAS MESSAGE WAS DISPLAYED. AT THE SAME TIME THE NUMBER 1 ENGINE WAS TEMPING OUT. THE THRUSApr 1, 2008 · N566RP · Emb EMB145LR · Engine (Turbine/Turboprop)SDR DXTA200802976Acm · frozenCANNOT CONTROL TEMP ON CABIN PAC. CABIN FILLED WITH SMOKE. REMOVED & REPLACED FORWARD ACM IAW MM 21-51-00. OPS & LEAK CHECKS ARE GOOD.Apr 1, 2008 · N932QS · Cessna 750 · Cabin Temperature Control SystemSDR CHQA200800067Noise Attenuator · meltedFLIGHT 6380, STL TO CVG - AFTER LEVELING OFF AT FL230, THE FLIGHT CREW NOTICED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK. THE AIRCRAFT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. DURING ENGINE RUNS, MAINTENANCE WAS ABLE TO DUPLICATE THE SMELL AND INSPECMar 30, 2008 · N575RP · Emb EMB145LR · Cabin Cooling SystemSDR SIMA200809303Carbon Seal · leakingON FLIGHT 3861, CREW REPORTED STRONG OIL BURNING SMELL IN CABIN DURING TAKEOFF WITH APU ON. ALSO GOT STRONGER OIL BURNING SMELL ON DESCENT WITH APU OFF. AIRCRAFT REMOVED FROM SERVICE. C/A-REMOVED AND REPLACED LEFT ENGINE ZERO CARBON SEAL. OPERATIONAL CHECK GMar 30, 2008 · N815AE · Emb EMB135KL · Turbine Engine Oil SystemSDR DJFA2008036Display · smokeIN FLIGHT CREW REPORTED EICAS FAIL ACCOMPANIED WITH SMOKE IN THE COCKPIT. THE EICAS DISPLAY CIRCUIT BREAKER TRIPPED AND THE SMOKE DISSIPATED. MAINTENANCE FOUND THE NR 3 EICAS DISPLAY INOPERATIVE. AN INSPECTION OF ALL ASSOCIATED WIRING WAS COMPLIED WITH. NO Mar 29, 2008 · N904LX · Emb EMB135BJ · Central WarningSDR CHQA200800066Engine · leakingFLIGHT 7820, CMH-IAD, AFTER TAKEOFF AT 400 FEET, THE CREW RECEIVED A LAV SMOKE MESSAGE. THE FLIGHT ATTENDANT REPORTED THAT THERE WAS NO SMOKE PRESENT IN THE LAVATORY OR CABIN. THE FLIGHT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE ENGINMar 29, 2008 · N294SK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA200800063Proximity Sensor · faultyFLIGHT 7847, IAD TO YYZ - AFTER TAKEOFF, WHEN THE CREW ATTEMPTED TO RAISE THE LANDING GEAR THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS AND THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. THE FLIGHT RETURNED TO IAD AND LANDED WITHOUT INCIDMar 28, 2008 · N292SK · Emb EMB145LR · Landing Gear Position and WarningSDR CHQA200800064Warning System · malfunctionedFLIGHT 5953 - PHL TO CLE - THE CREW RECEIVED A BLEED 1 LEAK MESSAGE DURING CLIMB, RAN THE APPROPRIATE QRH CHECKLISTS AND LANDED BACK AT PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 BLEED SYSTEM AND COULD FIND NO LEAKS. MAINTENANCE RAN THE ENGINES ANDMar 28, 2008 · N267SK · Emb EMB145LR · Pneumatic Indicating SystemSDR CHQA200800065O-Ring · blownFLIGHT 5984 -JAX TO CLE - DURING CLIMB, THE FLIGHT CREW RECEIVED A BLEED 1 LEAK MESSAGE AND RETURNED TO JAX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SEVERAL PANELS IN THE CARGO COMPARTMENT THAT WERE ABNORMALLY WARM, AND THE SOURCE WAS FOUND TO BE THE O-Mar 28, 2008 · N267SK · Emb EMB145LR · Pneumatic Distribution SystemSDR C2XA08CL039Engine · malfunctionedCLE FLIGHT 2890 - THE CREW REPORTED ENGINE NR 2 CAUSING SMOKE SMELL IN THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT TO FOLLOW.Mar 26, 2008 · N22971 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA200800058O-Ring · leakingCVG TO GSP - DURING CLIMB, THE CREW RECEIVED A BLEED 2 LEAK MESSAGE ON EICAS. THE AIRCRAFT THEN RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE BLEEDS AND INSPECTED FOR LEAKS. A LEAK WAS FOUND AT JOINT 4 AND AFTER REPLACING THE O-RINGS ATMar 25, 2008 · N573RP · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA200800059Spoiler Sys · malfunctionedCVG TO STL - ON APPROACH TO STL, THE CREW RECEIVED A SPOILER FAIL MESSAGE. THE CREW EXECUTED A GO AROUND AND FOLLOWED THE APPROPRIATE QRH CHECKLISTS AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE AIRCRAFT POWER AND OPERATED THE SPOILER SYSTEM WITHOUT DEFMar 25, 2008 · N579RP · Emb EMB145LR · Drag Control SystemSDR CHQA200800057Filter Element · dirtyCLE TO RDU - WHILE CLIMBING THROUGH 7,000 FT, THE CREW RECEIVED A BLEED 1 OVERTEMP MESSAGE. THE PROPER CHECK LISTS WERE FOLLOWED IN THE QRH AND IT WAS DECIDED TO DIVERT TO CMH. THE FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT IN CMH. MAINTENANCE TROUBLESHOT Mar 24, 2008 · N275SK · Emb EMB145LR · Pneumatic Distribution SystemSDR C2XA08IA089Engine · leakingIAH - FLIGHT 2725, THE CREW REPORTED SMOKE IN THE LAV AND CARGO COMPARTMENT ON LANDING. THE CREW DISCHARGED BOTH FIRE BOTTLES, AND THE AIRCRAFT WAS EVACUATED. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CMar 24, 2008 · N17524 · Emb EMB135LR · Engine (Turbine/Turboprop)SDR DXTA200802963Apu · defectiveSTRONG ODOR COMMING FROM AIR CONDITION AND IN CABIN OF AC. REMOVED DEFECTIVE APU AND INSTALLED A REPAIRED APU. PERFORMED AN OPERATIONAL AND LEAK CHECK. ALL CHECKS PASSED. ALL WORK ACCOMPLISHED IAW MM CHAPTER 49-10-00.Mar 24, 2008 · N923QS · Cessna 750 · Airborne Auxiliary Power Unit (APU) SystemSDR CHQA200800056Warning System · malfunctionedORF TO IAD - UPON DEPARTURE FROM ORF, THE LANDING GEAR WAS SELECTED UP, BUT WOULD NOT RETRACT. THIS WAS ACCOMPANIED BY AN LG AIR/GRD FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL THE WEIGHT ON WMar 23, 2008 · N292SK · Emb EMB145LR · Landing Gear Position and WarningSDR SIMA200808402Carbon Seal · wornON FLIGHT 3900 - CREW REPORTED NUMBER 1 ENGINE OIL QUANTITY WENT FROM 11 TO 4 QTS IN LESS THAN 15 MINUTES. PERFORMED PRECAUTIONARY SHUTDOWN. OVERWEIGHT LANDING PERFORMED 43700 LBS TOUCHDOWN OF LESS THAN 100 FPM. AIRCRAFT LANDED UNEVENTFULLY. AIRCRAFT REMOVMar 22, 2008 · N833AE · Emb EMB135KL · Turbine Engine Oil SystemSDR C2XA08ON107Engine · malfunctionedFLT 0224 - SMF - FLIGHT CREW REPORTED SMOKE IN THE COCKPIT WHILE CLIMBING; AIRCRAFT RETURNED TO BLOCK; FLIGHT CREW DID NOT DECLARED EMERGENCY; AIRCRAFT LANDED SAFELY. MX PERSONNEL REMOVED AND REPLACED NR 1 ENGINE OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT Mar 21, 2008 · N13202 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR SIMA200808118Carbon Seal · faultyON FLIGHT 3799, CREW REPORTED SMOKE IN CABIN AND COCKPIT WHEN POWER WAS APPLIED FOR TAKEOFF. ABORTED TAKEOFF AND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO GATE UNEVENTFULLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY IAW WOMar 20, 2008 · N696AE · Emb EMB145LR · Turbine Engine Oil SystemSDR CHQA200800055Power Supply · inoperativeDURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE NON FUNCTIONAL. THE NR 4 EMERGENCY LIGHT POWER SUPPLY WAS REPLACED AND THE OVERWING EMERGENCY LIGHT SYSTEM OPERATED NORMALLY.Mar 18, 2008 · N567RP · Emb EMB145LR · Emergency LightingSDR CHQA200800054Controller · malfunctionedCLE TO ATL - DURING FLIGHT, THE AIRCRAFT CABIN WOULD NOT PRESSURIZE FULLY. THE CREW DROPPED BELOW 10,000 FT AND USED THE PRESSURE DUMP TO RELEASE REMAINING PRESSURE AND RETURNED TO CLE. MAINTENANCE TROUBLESHOT THE PRESSURIZATION SYSTEM AND FOUND THE DIGITAL Mar 17, 2008 · N260SK · Emb EMB145LR · Cabin Pressure ControllerSDR CHQA200800053Control Unit · malfunctionedCVG TO GSP - DURING CLIMB-OUT, THE CREW RECEIVED AN AMBER EICAS SPOILER FAIL MESSAGE. THE APPROPRIATE CHECKLISTS WERE FOLLOWED IN THE QRH AND THE AIRCRAFT RETURNED TO CVG WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE SPOILER ELECTRONIC CONTROL UMar 17, 2008 · N567RP · Emb EMB145LR · Drag Control SystemSDR CHQA200800051Controller · faultyMSN TO CVG - WHILE CLIMBING THROUGH 13,000 FT, THE CREW RECEIVED A CABIN ALTITUDE RED MESSAGE CABIN ALTITUDE 10,000 ALONG WITH A WARNING MESSAGE. THE CREW LEVELED OFF AT 15,000 FT THEN STARTED TO DESCEND. WHILE DESCENDING THE CABIN PRESSURE BECAME AMBER THENMar 15, 2008 · N579RP · Emb EMB145LR · Cabin Pressure ControllerSDR CHQA200800050Printed Ckt Board · burnedRIC TO CVG - ON APPROACH TO CVG, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW THAT THERE WAS SMOKE COMING FROM THE OVERHEAD AROUND ROW 8 ACCOMPANIED BY THE SMELL OF BURNING ELECTRONICS. THE FLIGHT CREW HAD NO INDICATIONS ON EICAS AND THE AIRCRAFT CONTINUED AMar 14, 2008 · N579RP · Emb EMB145LR · Passenger Compartment EquipmentSDR CA080314007Engine · leakingOIL IMPENDING BYPASS INDICATION ILLUMINATED ALONG WITH OIL TEMPERATURE RISING TO 141 DEGREES. THE PILOT COMMANDED THE SHUT DOWN OF THE ENGINE DUE TO OIL TEMPERATURE AND QUANTITY INDICATING THREE QUARTS. AIRCRAFT RETURNED TO CMH WITHOUT INCIDENT. MAGNETIC INMar 12, 2008 · Emb EMB135ER · Turbine Engine Oil SystemSDR C2XA08IA079Engine · leakingIAH - FLIGHT 2156 - AFTER TAKEOFF THE LAVATORY SMOKE INDICATOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. UPON INSPECTION THE NR 2 ENGINE WAS FOUND TO BE THE SOURCE OF THE SMOKE. MAINTENANCE REMOVED AND REPLACED THEMar 10, 2008 · N13978 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CA080314009Bearing · failedENGINE REMOVED FOR ITT EXCEEDANCE, AUTO IFSD, SMOKE IN COCKPIT/CABIN, OIL DEBRIS ON ALL CHIP DETECTORS. TEARDOWN OF ENGINE REVEAL NR 4 BEARING FAILURE AND ALSO NR 3 BEARING FAILURE. EXCESSIVE DAMAGE IN COMPRESSOR AREA DUE TO BOTH SUPPORTING BEARING FAILURE. Mar 10, 2008 · Emb EMB145LR · Turbine Engine Compressor SectionSDR CHQA200800048Actuator · out of adjustCMH TO CMH - DURING CLIMB-OUT FROM CMH, THE CREW RECEIVED AN E1 REVERSER DISAGREE MESSAGE ON EICAS. THE CREW LEVELED OFF, FOLLOWED THE APPROPRIATE QRH CHECKLISTS, AND E1 WAS SHUTDOWN. THE AIRCRAFT THEN LANDED AT CMH WITHOUT INCIDENT. MAINTENANCE TROUBLESHOTMar 9, 2008 · N272SK · Emb EMB145LR · Engine Thrust ReverserSDR CHQA200800047Engine · leakingCMH TO BOS - WHILE CLIMBING THROUGH FL190, THE CREW RECEIVED AN E1 IMPENDING OIL BYPASS MESSAGE. THE FIRST OFFICER PERFORMED THE QRH CHECKLISTS, WHILE THE CAPTAIN CHECKED THE ENGINE STATUS ON THE MFD. THE CAPTAIN NOTICED THAT THE OIL QUANTITY WAS DOWN TO 3 QMar 6, 2008 · N575RP · Emb EMB145LR · Turbine Engine Oil SystemSDR SIMA200806504Carbon Seal · wornON FLIGHT 9811, CREW REPORTED CABIN ODOR DURING TAKEOFF IN COCKPIT. ODOR DISAPPEARED DURING CLIMB. ODOR RE-EXPERIENCED ON APPROACH BELOW 7000 MSL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE ZERO CARBON SEAL IAW EMB 145 AMM 72-25-25. AMar 4, 2008 · N699AE · Emb EMB145LR · Turbine Engine Oil SystemSDR CHQA200800046Filter Element · dirtySBN TO CVG - DURING CLIMB-OUT, CREW RECEIVED A BLEED 1 OVERTEMP MESSAGE AT AROUND 4,000 FEET. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT AT SBN. MAINTENANCE TROUBLESHOT THE BLEED SYSTEM PER THE FIM, REMOVED THE FAN AIR VALVE FILTER AND CLEANED Mar 3, 2008 · N573RP · Emb EMB145LR · Pneumatic Indicating SystemSDR CHQA200800045Warning Message · false activationIAD TO BUF - AFTER ROTATION THE CREW RECEIVED A BRAKE OVERHEAT MESSAGE ON EICAS. THE LEFT OUTBOARD BRAKE WAS INDICATING FULL HOT. THE GEAR WAS NOT RETRACTED AND THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT AT WHICH TIME THE TEMPERATURE INDICATIONFeb 28, 2008 · N271SK · Emb EMB145LR · Central WarningSDR CHQA200800044B-Nut · looseLGA TO GSP - AFTER TAKEOFF WHILE CLIMBING IN ICING CONDITIONS, THE CREW RECEIVED AN ENGINE NR 1 BLEED OVERHEAT AND ENGINE ANTI-ICE FAIL MESSAGE ON EICAS. THE CREW EXITED THE ICING CONDITIONS AND RETURNED TO LGA. MAINTENANCE OPENED THE AIRCRAFT AND INSPECTED Feb 26, 2008 · N257JQ · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA200800043Duct · crackedIAH TO STL - THE CREW RECEIVED A BLEED 1 LEAK MESSAGE DURING CLIMB AND RETURNED TO FIELD AT IAH. MAINTENANCE SECURED THE BLEED 1 SYSTEM CLOSED AND DEFERRED THE NR 1 BLEED SYSTEM. ON THE 26TH MAINTENANCE TROUBLESHOT THE BLEED SYSTEM AND FOUND A LEAK COMING FRFeb 25, 2008 · N288SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA200800042O-Ring · leakingIAH TO STL. DURING CLIMB THE CREW RECEIVED A BLEED 1 LEAK MESSAGE AT 4,000FT. THE MESSAGE DISAPPEARED AND THEN RETURNED AT 8,000 FT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED 1 SYSTEM FOR LEAKS AND REPAIREDFeb 25, 2008 · N288SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA200800041Clamp · missingCVG TO GSP - DURING CLIMB-OUT THE CREW RECEIVED AN E1 EXCEEDANCE MESSAGE ON EICAS. THE ITT REACHED 901 FOR 25 SECONDS. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. EMINENCE PERFORMED A GVI OF THE ENGINE AND FOUND THE CUSTOMER MANIFOLD DUCTINGFeb 25, 2008 · N571RP · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA200800040Electrical Sys · malfunctionedCVG TO STL. DURING CLIMB, WHILE PASSING THROUGH 10,000FT THE CABIN EMERGENCY LIGHTS FLASHED ON, OFF, ON AND THE CREW RECEIVED AN EMERGENCY LIGHTS NOT ARMED MESSAGE. ALL OTHER INDICATIONS WERE NORMAL AND ALL INDICATIONS ON THE ELECTRICAL PAGE OF THE MFD WERE Feb 23, 2008 · N562RP · Emb EMB145LR · Electrical Power System
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