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 C2XA04SH325Floorbeam · corrodedSHV-DURING C CHECK THE SHELL PLATE ON TOP OF THE CENTER OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Fuselage Main, Floor BeamSDR C2XA04SH327Bracket · corrodedSHV-DURING C CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Passenger/Crew DoorsSDR C2XA04SH328Bracket · corrodedSHV-DURING C CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 27, 2004 · N11565 · Emb EMB145LR · Passenger/Crew DoorsSDR C2XA04IA055Fuel Nozzle · faultyCREW REPORTED THAT THERE WERE FUMES IN THE CABIN AND COCKPIT DURING ANTI-ICE OPERATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. THE ENGINES WERE RUN AND THE ANTI-ICE SYSTEM OPERATED WITH NO FURTHER SMELL NOTED. THE DISCREPANCY WAS THEMay 25, 2004 · N26549 · Emb EMB145LR · Fuel Injector NozzleSDR SIMA200414403Window · failedDURING CRUISE FLIGHT, CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406966)May 23, 2004 · N647AE · Emb EMB145LR · Flight Compartment WindowsSDR SIMA200414601Power Supply · inoperativeTOP AND LOWER LT EXIT LIGHTS ON SERVICE DOOR WILL NOT REMAIN ILLUMINATED. REPLACED NR 2 BATTERY POWER SUPPLY. AC RETURNED TO SERVICE. (SW21200407048)May 23, 2004 · N735TS · Emb EMB135LR · Emergency LightingSDR SIMA200414602Stringer · crackedAIRCRAFT STRUCK BY GPU ON RT SIDE JUST AFT OF RADOME. REPLACED 2 SKIN PANELS, 1 STRINGER, AND 1 FRAME. IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406972)May 23, 2004 · N711PH · Emb EMB135LR · Fuselage Main, Longeron/StringerSDR SIMA200414402Computer · failedIN CRUISE AT FL 290 CAPTAIN MULITFUNCTIONAL DISPLAY AND EICAS FAILED WITH BURNING ODOR. DIVERTED, OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200407047)May 22, 2004 · N707EB · Emb EMB135LR · Central ComputersSDR C2XA04CL057Smoke · detectedSTL FLIGHT NR 2364 THE CREW REPORTED A STRONG ODOR/LIGHT SMOKE IN THE CABIN WITH BOTH APU BLEEDS AND ENGINE BLEEDS ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF BOTH PACKS. NO DEFECTS WERE FOUND.May 21, 2004 · N13992 · Emb EMB145LR · Air Distribution SystemSDR SIMA200414401Drive Unit · inoperativeDURING LANDING, CREW DECLARED AN EMERGENCY DUE TO FLAP FAIL. FLAPS WERE AT 9 DEGREES AND NO INDICATION WAS SEEN IN COCKPIT. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT FOR FLAPS. OPERATIONAL CHECK WAMay 21, 2004 · N845AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR C2XA04BT062Engine · failedCREW REPORTED, NR 1 ENGINE FAILED INFLIGHT. N1 STABILIZED AT ABOUT 14 PERCENT AND 100 DEGREES. FAILURE OCCURRED DURING CLIMBOUT IN SHALLOW LEFT BANK WITH CLIMB THRUST SET. PERFORMED AIR RETURN TO NEWARK. LANDED UNEVENTFULLY. MAINTENANCE FOUND UNACCEPTABLEMay 20, 2004 · N14943 · Emb EMB145ER · Engine (Turbine/Turboprop)SDR SIMA200414202Control Unit · inoperativeMAINTENANCE REPORTED A DUAL PITCH TRIM FAIL ON LANDING AND TWICE ENROUTE PITCH TRIM 1 AND 2 INOPERATIVE. MESSAGE APPEARED FOR 5 SECONDS EACH TIME, THEN WENT OUT. REPLACED HSCU IAW MFG MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406973)May 19, 2004 · N807AE · Emb EMB135KL · Elevator Tab Control SystemSDR C2XA04SH294Skin · dentedDURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2004 · N15973 · Emb EMB145 · Engine Air Intake SystemSDR CHQA000493Engine · odorDURING T/O ROLL PILOT NOTICED FUNNY ODOR IN CABIN SIMILAR TO OIL ODOR. A FEW SECONDS INTO CLIMBOUT, LAV SMOKE DETECTOR SOUNDED. A/C RETURNED TO FIELD AT PHL AND LANDED WITHOUT INCIDENT. MX INSPECTED A/C, PERFORMED GROUND RUNS AT ALL POWER SETTINGS WITH BLEEMay 18, 2004 · N291SK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA000490Engine · smokeFLT 3090 CREW REPORTS, RECEIVED LAV SMOKE WARNING DURING CLIMBOUT OF DCA AND FLT ATTENDANT REPORTED SMOKE IN THE LAV AREA. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FIRE DEPT REPORTS NO VISUAL SIGNS OF SMOKE AND NO SCENT. MX REPORTS, PERFORMED PNEUMATMay 17, 2004 · N291SK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200414201Control Unit · failedON APPROACH, CREW SELECTED FLAPS TO 9 DEGREES AT WHICH POINT THEY RECEIVED FLAPS FAIL MSG AND FLAPS FAILED TO MOVE. DECLARED EMERGENCY AND LANDED SAFELY WITH 0 FLAPS. FPDU OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200406985)May 17, 2004 · N639AE · Emb EMB145LR · Trailing Edge Flap Control SystemSDR RAIA00405011Control Unit · malfunctioned5675-STL- OB BRAKE INOPERATIVE INDICATION. MAINTENANCE RERACKED BRAKE CONTROL UNIT. OPS CHECK GOOD.May 15, 2004 · N818HK · Emb EMB145LR · Landing Gear Brake SystemSDR SIMA200413803Engine · vibrationBOS - FLT 4669 - UNUSUAL ABNORMAL VIBRATION AND NOISE FROM NR 1 ENGINE AT 40 PERCENT N1 AND BELOW, CAN BE FELT THROUGH FLOOR, YOKE AND RUDDER PEDALS. ALSO, IN CABIN AREA. ENGINE INSTRUMENTS READ NORMAL. REPLACED NR 1 ENGINE ASSEMBLY IAW W/C 72-000-00. LEAKMay 14, 2004 · N834AE · Emb EMB135KL · Engine (Turbine/Turboprop)SDR SIMA200413503Charger · inoperativeDISC-EMERGENCY LIGHTS AFT OF EMERGENCY EXIT ROW COME ON AFTER BATTERIES TURNED OFF WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK GOOD, NO FURTHER DEFECTS. (SW21200406974)May 14, 2004 · N810AE · Emb EMB135KL · Emergency LightingSDR UG8AGM0413Yoke · incorrectCONTROL YOKES SHOW 25 DEGREE RT BANK DURING STRAIGHT AND LEVEL. RT AILERON IS UP AND LT ELEVATOR IS UP. PITCH CONTROL FORCE FEELS NORMAL. AMOUNT OF ELEVATOR/AILERON DISPLACEMENT INCREASES WITH SPEED. TROUBLESHOOTING FLIGHT CONTROL SYSTEMS IN PROGRESS. AIRMay 14, 2004 · N5115 · Cessna 750 · Control Column SectionSDR RAIA00405009Control Unit · defective5701-STL- BRAKE DEGRADE MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT.May 12, 2004 · N821HK · Emb EMB145 · Landing Gear Brake SystemSDR SIMA200413201Engine · malfunctionedPWM - FLT 4645 - A/C LEVEL AT 21K FT JUST ABOUT TO SET CRUISE MODE FELT YAW AND HEARD LOUD BANG NOISE. NR 1 ENGINE UNCOMMANDED SHUTDOWN. AIRCRAFT DECLARED EMERGENCY AND LANDED IN PWM. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERMay 9, 2004 · N707EB · Emb EMB135LR · Engine (Turbine/Turboprop)SDR MASA200400253Engine · hot startASH 2767 CLT. CREW REPORTED THE NR 2 ENGINE EXPERIENCED HUNG START WITH EXCESSIVE TAILPIPE FLAME. MX INVESTIGATED AND FOUND ACCORDING TO CMC THAT THE ITT MAXIMUM LIMITS WERE EXCEEDED AT 927 DEGREES C FOR 9 SECONDS AND N1 & N2 WERE OVERSPEED. MX CHANGED NR 2 ENMay 7, 2004 · N830MJ · Emb EMB145LR · Turbine SectionSDR UG8AGM0412Control Unit · inoperativePITCH CONTROL PRESSURE IS EXCESSIVELY HIGH. THE LEFT ELEVATOR (A) SYSTEM PITCH CONTROL UNIT SHUTOFF SOLINOID HAD AN INTERNAL SHORT TO GROUND WHICH CAUSED HYDRAULIC PRESSURE TO BE SHUT OFF TO THE (A) SYSTEM PCU. THE HYDRAULIC DEACTIVATION OF THE (A) PCU, BY DMay 7, 2004 · N5115 · Cessna 750 · Elevator Control SystemSDR C2XA04CL048Engine · malfunctionedCLE FLIGHT NR 2843 THE CREW REPORTED THE NR 1 ENGINE SHUT DOWN IN FLIGHT. THE SHUT DOWN WAS UNCOMMANDED. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.May 5, 2004 · N11127 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR SIMA200412501Control Unit · inoperativePITCH TRIM 1-2 INOPERATIVE ON EICAS AT 520 FT SHORTLY AFTER DISCONNECTING AUTO PILOT. REPLACED HSCU. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406976)May 1, 2004 · N802AE · Emb EMB135KL · Elevator Tab Control SystemSDR SIMA200412107Odor · detectedDURING LANDING, CREW REPORTED SMOKE AND ELECTRICAL ODOR IN COCKPIT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RAN ON GROUND WITH PACKS ON AND NO SMOKE REPORTED. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406986)Apr 29, 2004 · N840AE · Emb EMB135KL · Air Distribution SystemSDR C2XA04TY074Engine · malfunctionedTYS - FLIGHT 2110 PERFORMED AIR RETURN DUE TO ABNORMAL SMELL FROM NR 2 PACK. A/C WAS RELEASED IAW MEL 21-51-00/2 CAT-C CONTROL 041491 TO TYS WHERE MAINT REMOVED AND REPLACED THE NR 2 ENG IAW ROLL ROYCE MM 72-00-00. ALL WORK WAS ACCOMPLISHED WITH LEAK, VIBES Apr 28, 2004 · N18102 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR C2XA04SH253Engine · damagedSHV - FLIGHT 2806 FROM IAH TO MEM CREW REPORTED LOW OIL QUANTITY AND HIGH OIL TEMPERATURE 25 MINUTES AFTER TAKEOFF AT CRUISE ALTITUDE. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT DIVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. Apr 26, 2004 · N18556 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR C2XA04CL042Engine · failedCMH FLIGHT NR 2699 THE CREW REPORTED THE NR 2 ENGINE EXCEEDED 950 DEGREES ON CLIMBOUT. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. THE CREW ALSO REPORTED A SMOKE SMELL. MAINTENANCE REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOODApr 26, 2004 · N41104 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR SIMA200412001Battery Pack · dischargedCREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BY THE FIRST FOUR ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406977)Apr 26, 2004 · N735TS · Emb EMB135LR · Emergency LightingSDR C2XA04CL041Engine · failedCLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.Apr 24, 2004 · N14508 · Emb EMB135ER · Engine (Turbine/Turboprop)SDR C2XA04CL038Engine · failedTHE CREW REPORTED NR 1 ENGINE VIBRATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO DAYTON AND LANDED. AFTER LANDING THE NR 1 ENGINE HAD A SMALL FIRE OUT THE BACK OF THE ENGINE. THE FIRE WAS EXTINGUISHED AND NO OTHER INCIDENT OCCURRED. MAINTENANCE REPLACED THE NApr 19, 2004 · N14991 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200411201Connector · looseDISC - FWD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406984)Apr 19, 2004 · N635AE · Emb EMB145LR · Electrical ConnectorsSDR C2XA04TY070Carbon Seal · leakingAIR RETURN, FERRIED TO TYS FROM EWR, FOR LAV SMOKE ON EICAS, STRONG ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE ZERO CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKED GOOD IAW RR MM 72-25-40, 72-25-25, 72-21-05, 72-21-15, 72-50-00 AND ECApr 15, 2004 · N14514 · Emb EMB135LR · Turbine Engine Oil SystemSDR SIMA200410703Pdu · malfunctionedDURING APPROACH WHEN FLAPS WERE SELECTED FROM 9 DEG TO 22 DEG, EICAS MESSAGE (SPS ADVANCED). FLAP POSITION INDICATOR BOX WENT AMBER WITH AMBER DASH WITH NO FLAP INDICATION, RMU PAGE SHOWING NO FLAP INDICATION BUT AMBER DASHES, EICAS DID NOT PRESENT A FLAP FAIApr 15, 2004 · N835AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR CHQA000477Compressor · damagedFLT 6490 DFW - OKC: JUST AFTER TAKEOFF THROUGH ACCELERATION ALTITUDE WITH ALL ENGINE INDICATIONS NORMAL, NR 2 ENGINE FLAMED-OUT. CREW ADVISED PRIOR TO V1, HEARD A POP. AN EMERGENCY WAS DECLARED AND NR 2 ENGINE WAS SECURED. THE AIRCRAFT RETURNED TO DFW, MADApr 8, 2004 · N841 · Emb EMB135LR · Turbine Engine Compressor SectionSDR CHQA000474Engine · odorAFTER ROTATION OUT OF IND, STARTED TO SMELL FUMES. THERE WAS NO EVIDENCE OF SMOKE IN THE CABIN BUT THE F/A REPORTED THE ODOR WAS STRONGER IN THE FRONT. DECISION WAS MADE TO RETURN TO IND. THE ODOR DID START TO DISSIPATE DURING LANDED. MAINTENANCE CHECKED TApr 4, 2004 · N289 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA000475Transducer · malfunctionedFLT 3099 SDF - DCA: CREW REPORTS ENG 2 OIL PRESS WENT DOWN TO 47 PSI, INTO RED RANGE ON LOW SIDE, THEN WENT TO AMBER DASHES, THEN SPIKED UP INTO TOP OF HIGH SIDE RED RANGE, BUT DID NOT GET EXACT PSI READING. OIL QUANTITY INDICATED 12 QTS AND THERE WERE NO EIApr 3, 2004 · N267 · Emb EMB145LR · Engine Oil Indicating SystemSDR RAIA00403027Engine · overtempRIGHT ENGINE HIGH ITT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE.Mar 27, 2004 · N817HK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR RAIA00403030Engine · malfunctioned5622 - DEN - ATTCS NO MARGIN INDICATION NR 2 ENGINE. MAINTENANCE DEFERRED ATTCS PER MEL 73-22-02. SUBSEQUENTLY CLEARED DMI BY PERFORMING THRUST ASSURANCE RUN WITH NO MESSAGES NOTED.Mar 19, 2004 · N814HK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200406804Control Unit · inoperativeRECEIVED PITCH TRIM, .5 INOPERATIVE MESSAGE. CW ETN EB-27-0022R1 AND REPLACED HSCU OPS CHECKED GOOD. AC RETURNED TO SERVICE. (SW21200404959)Mar 6, 2004 · N811AE · Emb EMB135KL · Elevator Control SystemSDR SIMA200406806Control Unit · inoperativePITCH NR 1 AND NR 2 INOPERATIVE. COMPLIED WITH ETN EB 27-0022R1 AND REPLACED HSCU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (SW21200404960)Mar 6, 2004 · N731BE · Emb EMB135LR · Elevator Control SystemSDR CHQ2004F00000Strut · inoperativeBEARING CAP SHIMS ARE MIGRATING OUT FROM CAP FACES. SOME SHIMS MIGRATE INTO BEARING LANDING, BETWEEN CAP AND BALL JOINT BEARING. THE TORQUE SPECIFICATIONS ARE FOR DRY TORQUE VALUES AND THE BOLTS ARE BEING INSTALLED WITH BOLTS ARE BEING INSTALLED WITH (CA-100Mar 5, 2004 · N262SK · Emb EMB145LR · Nose/Tail Landing GearSDR SIMA200406803Indicator · malfunctionedCREW NOTED AFTER TAKEOFF THAT THE RT FUEL TANK WAS LOOSING ABOUT 300LB PER MINUTE, SO THEY RETURNED FOR MAINTENANCE. INSPECTED RT FUEL SYSTEM AND FOUND NO LEAKS. ALSO CALCULATED FUEL BURN OF LT AND RT ENGINES FOUND TO BE NORMAL. NO DEFECTS NOTED. AC RETURNMar 5, 2004 · N822AE · Emb EMB135KL · Fuel Quantity IndicatorSDR C2XA04SH108Support · corrodedDURING C CHECK THE MAIN DOOR THRESHOLD SILL SUPPORT WAS FOUND TO BE CORRODED AT FRAME 15 TO 18 AND STRINGER 15 LT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL SUPPORT IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04CL015Filter · dirtyCLE FLIGHT 3231 THE CREW REPORTED A ENGINE NR 2 FUEL IMPENDING BYPASS WARNING. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND REPLACED THE FUEL FILTER AND IMPENDING BYPASS INDICATOR. OPERATIFeb 26, 2004 · N27962 · Emb EMB145 · Engine Fuel DistributionSDR MASA200400113Engine · flamed outCREW REPORTED NR 2 ENGINE FLAMED OUT DURING LANDING ROLL-OUT. MX PERFORMED ENGINE RUNS. MX FOUND NO DEFECTS. NO PARTS USED.Feb 26, 2004 · N860MJ · Emb EMB145LR · Engine (Turbine/Turboprop)SDR SIMA200405902Control Unit · inoperativeAFTER LANDING, DURING TAXI, CREW REPORTED THE PITCH TRIM 1 AND 2 INOPERATIVE ILLIMINATED. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNEDFeb 25, 2004 · N731BE · Emb EMB135LR · Elevator Control SystemSDR SIMA200405502Connector · disconnectedEMERGENCY EXIT SIGN ABOVE GALLEY SERVICE DOOR INOPERATIVE AND EMERGENCY EXIT SIGN ON RT FW BULKHEAD IN FRONT OF SEATS 2 B,C INOPERATIVE. FOUND CONNECTOR P8530 OFF, RECONNECTED P8530. AC GOOD IAW MFG AMM. (SW21200406975)Feb 23, 2004 · N639AE · Emb EMB145LR · Emergency Lighting
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