GE CF34-3B1

Service difficulty reports · 5,402

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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 = '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 SWIA2019072346083Engine · failedLEFT ENGINE FAILURE IN FLIGHT. LOUD NOISE FROM LEFT ENGINE. LEFT ENGINE OIL PRESS WARNING MESSAGE. COMPLIED WITH QRH. RTF. (FLT#5108) FO: 07/23/2019 CLOSED REMOVED AND REPLACED LT ENGINE ASSY IAW AMM. OPS AND LEAK CHECKS GOOD.Jul 21, 2019 · N986SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA191004002Engine · damaged(CAN) LEFT ENGINE FAILURE IN FLIGHT. LOUD NOISE FROM LEFT ENGINE. LEFT ENGINE OIL PRESS WARNING MESSAGE. COMPLIED WITH QRH. CORRECTIVE ACTION: REMOVED AND REPLACED L/H ENGINE ASSEMBLY IN REF TO THE AMM 71-00-00. (TC# 20191004002)Jul 21, 2019 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA190723001Rudder · malfunctioned(CAN) WE WERE CLEARED FOR T/O. FINISHED ALL CHECKS IN ACCORDANCE WITH SOPS. ONCE THE AIRCRAFT WAS LINED UP WITH CENTRE LINE I GAVE CONTROL OVER TO THE F/O, MY HANDS AND FEET WERE OFF ALL CONTROLS. THE F/O APPLIED POWER UP TO 50% N1 AND KEPT ADDING RIGHT RUDDERJul 19, 2019 · Cndair CL6002B19 · Rudder Control SystemSDR CA190625025Sensing Element · faulty(CAN) AFTER TAKE-OFF, CREW RECEIVED THE RH 14TH STAGE DUCT WARNING LIGHT. AIRCRAFT RETURNED TO DEPARTURE POINT. MAINTENANCE RECTIFICATION INCLUDED THE BLEED AIR LEAK CONTROL BEING REPLACED IAW AMM TASK 36-21-10-400-801 AND THE ISOLATION SHUTOFF VALVE ALSO REJun 20, 2019 · Cndair CL6002B19 · Pneumatic Indicating SystemSDR CA190621001Anchor Fitting · cracked(CAN) DURING SCHEDULED MAINTENANCE THE AFT PASSENGER DOOR ANCHOR FITTING,WAS OBSERVED TO BE CRACKED. THE FITTING WAS REPLACED IAW THE APPLICABLE AMM REFERENCE. AC HOURS: CYCLES 27737, HOURS: 34622. (TC# 20190621001)Jun 17, 2019 · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019061145967Engine · failedDURING CLIMB OUT, LOUD BANG FOLLOWED BY SPIKE IN ITT AND CONSTANT N2 VIB MESSAGE. (FLT#4330) REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW AMM. OPS AND LEAK CHECK GOOD.Jun 7, 2019 · N429SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA190531004Wire Harness · damaged(CAN) AFTER TAKE-OFF FLAPS WERE SELECTED TO 0*. FLAPS BEGAN TO TRANSIT FOLLOWED BY FLAPS FAIL MESSAGE. BOTH LEFT AND RIGHT FLAPS INDICATED 5. FOUND R/H O/B HARNESS WITH HIGH RESISTANCE. (TC# 20190531004)May 29, 2019 · Cndair CL6002B19 · Flight Control System WiringSDR CA190521004Smoke Detector · failed(CAN) INITIALLY AFTER PAX DOOR CLOSED. THE ASU (AIR START UNIT) AND BOTH PACKS WERE PUT ON, `SMOKE AFT LAV` (W) MSG WAS LIT, AND OFFENSIVE ODOR REPORTED BY FA. (SMELL LIKE PLASTIC). ANOTHER ASU CONNECTED AND PERFORMED SMOKE DETECTOR TEST AND A/C WAS RTS, AFTERMay 12, 2019 · Cndair CL6002C10 · Smoke DetectionSDR CA190718005Engine · failed(CAN) SHORTLY AFTER TAKEOFF THE RH ENGINE EXPERIENCED A SUDDEN LOSS OF POWER ALONG WITH A VIBRATION. THE ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER ISSUES. A QUICK INSPECTION THROUGH THE EXHAUST DETERMINED THMay 9, 2019 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA201904295789Switch · failedR/H ENG T/R UNLOCK IN FLIGHT PERFORMED QRH DID NOT CLEAR. (FLT#5228) RE-RIGGED THROTTLE LOCKOUT SWITCH IAW AMM. OPS CHECK GOOD, NO DEFECTS NOTED.Apr 29, 2019 · N908SW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA190501003Engine · damaged(CAN) RIGHT ENG N2 VIB ICON WHEN BRINGING THRUST LEVERS UP NEAR 73% N2, ABORTED TAKEOFF LOW SPEED NO EXCEEDANCES. FELT SHUDDER THROUGH AIRFRAME DURING THROTTLE INCREASE. CORRECTIVE ACTION: REF AMM 05-51-27 NO HIGH ENERGY STOP/RTO INSPECTION REQUIRED BTMS OPS Apr 22, 2019 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA190425028Skin · damaged(CAN) FOUND THE RIGHT ENGINE UPPER CORE COWL HAD A HOLE IN IT. WHEN THEY OPENED THE COWL THEY FOUND THE IGNITOR STILL ATTACHED TO THE LEAD BUT NOT INSTALLED INTO THE COMBUSTION CHAMBER. THERE IS ALSO EVIDENCE OF HEAT DAMAGE ALONG THE COWL. WE DID NOT HAVE ANYApr 21, 2019 · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR SWIA201904125761Pump · failedON TAKEOFF AT 1000 FEET. THE LEFT ENGINE HAD A FLAMEOUT. CREW HEARD A BANG AND THE ENGINE ROLLED BACK. ITT SPIKED TO 973 FOR 11 SECONDS. NO RELIGHT WAS ATTEMPTED. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. LANDED WITHOUT INCIDENT. (FLT#5313) REMOVEApr 11, 2019 · N907EV · Cndair CL6002B19 · Engine Fuel PumpSDR CA190402011Warning Message · illuminated(CAN) L WSHLD HEAT CAUTION MESSAGE, OPS CHECK OF TEMP CONTROLLERS GOOD.Apr 1, 2019 · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR SWIA20190405666Engine · smokeRETURNED TO FIELD AFTER DEPARTURE DUE TO FA REPORTS OF THICK SMOKE WITH A STRONG ODOR IN THE CABIN. FA REPORTED SMOKE SEEMED TO BE COMING FROM THE AREA NEAR THE WINGS AND LAV SEEMED CLEAR. SMOKE APPEARED TO BE AT ITS WORST AT HIGH POWER SETTINGS AND SEEMED TO Mar 25, 2019 · N912SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2019040545663Line · leakingENGINE TWO LOW OIL PRESSURE IN FLIGHT. ENGINE SHUT DOWN IN FLIGHT ACCOMPLISHED. (FLT#5223) REMOVED AND REPLACED OIL SUPPLY LINE IAW AMM. NO LEAKS NOTED AFTER ENGINE RUNS.Mar 23, 2019 · N863AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REXA2019040800350Rub Strip · gouged#2 UPPER FAN COWL GOUGED ON AFT LIP. REMOVED ADN REPLACED RUB STRIP IAW CRJ 200 71-14-01-350-075-A01 AAR SM 58Mar 18, 2019 · N8683B · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR CA190316001Acm · seized(CAN) AFTER LANDING A THICK HAZE WITH STRONG ODOR. GROUND CREW REPORTED HOT TEMPERATURE IN THE CARGO HOLD. AIRCRAFT WAS ALREADY OPERATING UNDER MEL FOR THE RIGHT PACK. UPON TROUBLESHOOTING FOUND LEFT PACK ACM SEIZED AND THE OVER TEMPERATURE SWITCH U/S. DEFECTMar 14, 2019 · Cndair CL6002B19 · Cabin Cooling SystemSDR CA190314001Shutoff Valve · leaking(CAN) ON THE GROUND, A RUNNING FUEL LEAK WAS NOTED, ORIGINATING FROM THE RIGHT HAND MAIN LANDING GEAR WHEEL WELL AREA. INVESTIGATION FOUND THE FUEL WAS ESCAPING THROUGH A WIRE CONDUIT THAT TERMINATES IN THE RIGHT HAND WHEEL WELL. THE CONDUIT CARRIES WIRES FOR Mar 11, 2019 · Cndair CL6002B19 · Fuel Boost PumpSDR CA190311001Rod End · detached(CAN) THE MAIN CABIN DOOR COULD NOT BE OPENED FROM INSIDE OR OUTSIDE THE AIRCRAFT. SUBSEQUENT INVESTIGATION FOUND THAT A ROD END HAD BECOME DETACHED ON THE DEPRESSURIZATION PANEL PUSHROD ASSEMBLY.Mar 10, 2019 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA190304013Control Unit · inoperative(CAN) DURING TAXI, A FLAPS FAIL MESSAGE APPEARED WITH THE FLAPS AT ZERO DEGREES. DURING A SUBSEQUENT TEST OF THE FLAP ELECTRONIC CONTROL UNIT (FECU), THE FECU WAS FOUND INOPERATIVE. THE FECU WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Mar 2, 2019 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA190301006Sensor · false activation(CAN) ON APPROACH, AFTER SELECTING FLAPS 45 DEGREES, A FLAPS FAIL MESSAGE APPEARED AND THE FLAPS STOPPED AT 41 DEGREES. THE AIRCRAFT LANDED WITH THE FLAPS AT 41 DEGREES. SUBSEQUENT TROUBLESHOOTING WAS CARRIED OUT PER FIM 27-50-00 FIGURES 101 AND 102 (REF AD CFMar 1, 2019 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA190311025Windshield · cracked(CAN) CAPTAIN`S WINDSHIELD CRACKED DURING LINE UP FOR T.O. RIGHT AFTER WINDSHIELD HEAT CAUTION MESSAGE ILLUMINATED. WINDSHIELD CRACK TOP LEFT & TOP RIGHT CORNERS (TC# 20190311025)Feb 27, 2019 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2019022211101Check Valve · failedDURING THE DECENT, THE CREW RECEIVED A RIGHT HAND OIL PRESSURE WARNING MESSAGE. THE CREW STOPPED THE DECENT AND RAN THE QRH. THE CREW DECIDED TO DIVERTED. THE CREW PULLED BACK THE ENGINE TO IDLE AND LANDED AS NORMAL. THE CREW WAS ABLE TO TAXI TO THE GATE.Feb 22, 2019 · N206PS · Cndair CL6002B19 · Engine Oil Indicating SystemSDR SWIA201904035727Bonding Strap · corrodedRIGHT ENGINE PYLON TRAILING EDGE. TWO UPPER AND TWO LOWER BONDING STRAPS CORRODED. (C-CHECK) RO: 04/01/2019 REPLACED BONDING STRAPS ON RH ENGINE PYLON TRAILING EDGE IAW RIL.Feb 18, 2019 · N449SW · Cndair CL6002B19 · Turbine Engine System WiringSDR SWIA2019021945530Regulator Valve · smokeAFTER DEPARTURE WE RECEIVED SMOKE TOILET CAUTION MESSAGE. WITH A SLIGHT HAZE AND A MUSTY SMELL IN THE CABIN. WE RETURNED TO THE FIELD. SMOKE TOILET CAUTION MESSAGE WENT AWAY, BEFORE WE LANDED. (FLT#5074) FO: 02/18/2019 CLOSED REMOVED AND REPLACED LH ENGINE PREFeb 16, 2019 · N975SW · Cndair CL6002B19 · Compressor Bleed ControlSDR VNAA2019020411101Engine · power lossON APPROACH, THE CREW REPORTED A LOSS OF POWER FROM THE L ENGINE. THEY REPORTED A L ENGINE FUEL LOW PRESS MSG AND AC BUS 1 WAS AUTO TRANSFERRED. THE N2 DROPPED TP 42% AND THE ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. AFTER LANDING THE ENGINE ITT SPIKED INJan 31, 2019 · N241PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2019102131101Wire Harness · damagedON APPROACH TO PHL, THE CREW REPORTED A LOSS OF POWER FROM THE L ENGINE. THEY REPORTED A L ENGINE FUEL LOW PRESS MSG AND AC BUS 1 WAS AUTO TRANSFERRED. THE N2 DROPPED TP 42% AND THE ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. AFTER LANDING THE ENGINE ITT SPJan 31, 2019 · N241PS · Cndair CL6002B19 · Turbine Engine System WiringSDR SWIA2018110945257Warning Message · illuminatedLEFT ENGINE OIL PRESSURE WARNING INFLIGHT. RAN QRH - FLIGHT CREW SHUTDOWN THE ENGINE. DIVERTED. (FLT#5073) FO: 11/09/2018 CLOSED REMOVED AND REPLACED LH ENGINE IAW AMM. OPS, RIG AND LEAK CHECK GOOD AT THIS TIME.Nov 8, 2018 · N937SW · Cndair CL6002B19 · Engine Oil PressureSDR REXA2018110301079Torque Box · cracked#1 ENGINE T/R TORQUE BOX CRACKED ARE HI- LITE FASTNER ON AFT FLANGE @ 6 O'CLOCK POSITION. REPAIRED CRACK IAW ENDEAVOR EA CRJ 254-07814 REV IR AAR SM-35Nov 3, 2018 · N800AY · Cndair CL6002B19 · Engine Thrust ReverserSDR CA180907010Bpsu · failed(CAN) DURING CRUISE THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE. THE FLIGHT WAS DIVERTED TO A MAINTENANCE BASE AND LANDED WITHOUT ISSUE. NO EMERGENCY DECLARED. A SYSTEM RESET WAS ATTEMPTED WITHOUT SUCCESS AND MAINTENANCE TROUBLESHOOTING DISCOVERED THE LT Sep 6, 2018 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR REXA2018090400768Not Reported · malfunctionedDURING ENGINE START OF THE NUMBER 2 ENGINE THERE WAS NO LIGHT OFF. SHORTLY THERE AFTER THE GROUND CREW INFORMED US SMOKE AND A LITTLE BIT OF FLAMES WERE COMING OUT OF THE ENGINE. REMOVED FUEL CONTROL UNIT IAW AMM 73-21-01. BREAKERS PULLED + COLLARED CBP-1 M2, Aug 28, 2018 · N981EV · Cndair CL6002B19 · Fuel Controlling SystemSDR CA180822005Splice · corroded(CAN) DURING THE 48M-72M INSPECTION CHECK, CORROSION DAMAGE WAS FOUND. (TC# 20180822005)Aug 19, 2018 · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWIA2018082144957Engine · seizedDURING DESCENT, LEFT ENGINE SEIZED IN FLIGHT, AURAL WARNING, ENGINE SHUT DOWN. R & R THE LT ENGINE IAW AMM. OPS AND LEAK CHECKED GOOD.Aug 2, 2018 · N418SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2018073044896Carbon Seal · failedLT ENG LOW OIL PRESS MSG DURING FLIGHT. COMPLIED WITH QRH. (FLT#5504) FO: 07/24/2018 CLOSED REMOVED AND REPLACED HYDRAULIC PUMP, IDG, AND STARTER CARBON SEALS IAW ENGINE MANUAL. ALSO REMOVED AND REPLACED C-SUMP COMPONENTS . EXHAUST FRAME AND NR 7 CARBON SEAL IJul 23, 2018 · N971SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA2018062544808Engine · failedLEFT ENGINE FAILURE ON CLIMB OUT. FOLLOWED THE QRH FOR IN-FLIGHT ENGINE SHUT DOWN. NO VISIBLE DAMAGE TO THE EXTERNAL PORTION OF THE ENGINE. DECLARED AN EMERGENCY SHORTLY AFTER THE ENGINE FAILURE, RETURNED TO FIELD. NO ABNORMAL MESSAGES ON EICAS OTHER THAN L ENJun 23, 2018 · N980SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2018061544781Engine · failedLOST RIGHT ENGINE RESPONSE JUST OUTSIDE OF THE FINAL APPROACH FIX WHEN RIGHT THRUST LEVER WAS ADVANCED. RIGHT ENGINE SPOOLED DOWN AND ITT WENT RED. ACCOMPLISHED ENGINE SHUTDOWN IN FLIGHT. (FLT 7423) 06/15/2018 CLOSED REMOVED AND REPLACED RT ENGINE. OPS AND LEAJun 15, 2018 · N457SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA180618005Fitting · corroded(CAN) UPON INSPECTION, CORROSION FOUND ON THE PAX DOOR LONGERON LOWER SILL. (TC# 20180618005)Jun 14, 2018 · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REXA2018051700455Stiffener · crackedLEFT ENGINE EXHAUST FAIRING, CIRCUMFERENTIAL STIFFNER WAS CHAFED AND CRACKED AT THE FIVE O`CLOCK POSITION. REPAIRED THE STIFFNER IAW CMM 78-11-00-306-810-A01.May 17, 2018 · N8970D · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR SWIA2018051744638Engine · flamed outCAPTAIN REPORTED THAT DURING APPROACH, RECEIVED A RT MAIN EJECTOR AND RT SCAVENGE EJECTOR CAUTION MESSAGES AND RIGHT AFTER TOUCH DOWN THE RT ENGINE FLAMED OUT. ENGINE SHUT DOWN AFTER THRUST REVERSER ACTIVATION. REMOVED AND REPLACED THE RT ENGINE ASSY IAW AMMay 6, 2018 · N913SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA201804304598Engine · contaminatedSMOKE IN THE AFT CABIN. RETURNED TO THE FIELD. PERFORMED AN ENGINE RUN DRY OUT PROCEDURE IAW AMM ON THE RT ENGINE DUE TO COMPRESSOR WASH ON PREVIOUS NIGHT. NO DEFECTS OR SMOKE ODOR IN THE AIRCRAFT WAS NOTED. OPS CHECKED GOOD.Apr 30, 2018 · N472CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2018040244460Engine · vibrationDURING CLIMBOUT, CREW FELT A COUPLE OF ABRUPT VIBRATIONS, THEN NOTICED THE ITT WAS ABOUT 910. CREW DECREASED ENGINE POWER AND FELT MORE VIBRATIONS, LEVELED OUT 13000 FT. FA REPORTED VIBRATIONS ON THE LT SIDE OF THE ACFT, RETURNED TO FIELD. EMERGENCY DECLAMar 30, 2018 · N926EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2018032944438Oil System · fluctuatesLEFT ENGINE OIL PRESSURE FLUCTUATED INFLIGHT BETWEEN 25-45 PSI. OIL PRESSURE WARNING. ENGINE SHUTDOWN ON APPROACH. OPENMar 27, 2018 · N699BR · Cndair CL6002B19 · Engine Oil Indicating SystemSDR A6WA2018032845720Landing · crackedPANEL 446BL LANDING IS CRACKED. REPLACED LANDING IAW CMM 20-42-06.Mar 20, 2018 · N430AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR VNAA2018031611102Boss · faultyIN FLIGHT, THE LEFT ENGINE N1 AND N2 FLUCTUATED. THE LEFT ENGING WAS JUST BROUGHT DOWN TO IDLE AND STILL PRODUCING THRUST. AN EMERGENCY WAS DECLARED. LANDED SAFETLY AND WAS ABLE TO TAXI TO A GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE LEFT GEAR BOSS ONMar 16, 2018 · N248PS · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA180313019Detector Loop · damaged(CAN) BLEED LEAK DETECTION LOOP MISSING BONDING PROTECTION, AFFECTED AIRCRAFT ARE CRJ700/900/1000 (APPROX. 45 AIRCRAFT). BONDING PROTECTION HAS BEEN OMITTED ON MULTIPLE BLEED LEAK DETECTION LOOP CONNECTIONS. UNABLE TO ESTIMATE THE POTENTIAL DEGRADATION IN LEMar 12, 2018 · Cndair CL6002C10 · Fire Protection SystemSDR SWIA2018030144334Inlet · dentedLH ENG. - NOSE INLET-COWL - L/E DENTED. (C-CHECK) RO: 02/28/2017 REMOVED AND REPLACED L/H ENGINE NOSE INLET COWL IAW AMM. OPS CHECKS SATISFACTORY.Jan 28, 2018 · N709BR · Cndair CL6002B19 · Engine Air Intake SystemSDR BLUA20180111001Tube · chafedTUBE WAS CHAFED AT TWO LOCATIONS UNDER ADEL CLAMPS USED FOR ROUTING THE STAINLESS STEEL TUBE. WEAR WAS NOT TO THE POINT OF CAUSING ANY LEAKAGE IN THIS 3000 PSI PRESSURE LINE. THESE WERE BOTH LOCATIONS REQUIRED FOR INSPECTION WHEN PERFORMING SB 605-29-008. CJan 11, 2018 · N138DM · Cndair CL6002B16 · Hydraulic System, MainSDR CA180103004Light · overheated(CAN) DURING BOARDING, A PASSENGER IN SEAT 1F NOTICED AN UNUSUAL ODOR. THE PASSENGER BROUGHT THIS TO THE CREW`S ATTENTION. THE CREW DECIDED TO DE-PLANE THE PASSENGERS VIA THE MAIN CABIN DOOR. SUBSEQUENT INVESTIGATION FOUND THE SIDEWALL LIGHT ASSEMBLY IN THEJan 2, 2018 · Cndair CL6002B19 · Passenger Compartment LightingSDR SWIA201744173Thrust Reverser · chafedENGINE THRUST REVERSER CHAFED. R & R THE THRUST REVERSER IAW AMM.Dec 8, 2017 · N925EV · Cndair CL6002B19 · Engine Thrust Reverser
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