GE CF6-50C2

Service difficulty reports · 719

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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 = 'CF650C2'
  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 2004000004Gasket · leakingNR 3 ENGINE OIL LOSS, APPROXIMATELY 2 QTS. PER HOUR. MX ADVISED CREW TO RETURN TO BWI FOR REPAIRS. REPLACED GASKET ON OIL VENT LINE FOR B-SUMP AND OIL TANK. RAN ENGINE AT POWER. NO FURTHER LEAKING NOTED.May 1, 2004 · N49082 · Doug DC1030 · Turbine Engine Oil SystemSDR WRLA200414Cowl Door · missingAIRCRAFT N14075 DEPT. FROM LIRN TO KNGU AT 2100Z WHILE AIRCRAFT CRUISING AFTER 5 HOURS AND 40 MIN.APPROX. 0240Z (ACCORDING TO THE CAPTAIN REPORT) THE ACFT. SHUDDERED AND BOUNCED FOR APPROX. 1/2 SECOND, THEN RETURNED TO STABLE FLIGHT, ACFT. CONTINUE TO KNGU ANApr 11, 2004 · N14075 · Doug DC1030 · Engine Cowling SystemSDR WRNA200400003Engine · failedDURING TAKEOFF ROLL AT 110KTS, LOUD BANG AND FLASH, COMPRESSOR STALL, NR 1 ENGINE. ABOURTED TAKEOFF AND PERFORMED ENGINE SHUTDOWN. EGT HAD EXCEEDED MAXIUM LIMIT, 935 DEGREES. BOROSCOPE OF HOT SECTION ENTAILED, REVIELED NO DAMAGE. ENGINE R & R IAW ENGING CHANGEMar 19, 2004 · N502TA · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR G6OA022404Air Duct · blownON TAKEOFF CREW REPORTED A LOSS OF POWER ON NR 3 ENGINE THEY ABORTED TAKEOFF AT THIS TIME. A VISUAL INSPECTION IDENTIFIED THE 14 STAGE DUCT HAD BLOWN.Feb 24, 2004 · N612GC · Doug DC1030F · Engine Bleed Air SystemSDR WRLA200409Turbine Blades · failedNR 1 ENGINE COMPRESSOR STALLED / FAILED AT A/C ROTATION COMPLETED EMERGENCY & ABNORMAL CHECK LISTS. REMOVED AND REPLACED ENGINE ASSY.Feb 6, 2004 · N352WL · Doug DC1030 · Turbine SectionSDR XNOA1173Igniter · malfunctionedNR 1 ENG B-SYSTEM IGNITION FAIL WITH IGNITION B-CIRCUIT BREAKER POPPED & NR 1 ENG IGNITION EXCITER POWER TRANSFER FAILED. RETIGHTENED B-IGNITER BOX PER A-300 AMM 74-21-00, OPS CHECK GOOD. DUE TO POWER TRANSFER FAIL, A-SYS INOP, POWER TRANSFER NOT REQUIRED UTJan 22, 2004 · N13974 · Airbus A300B4203 · Spark Plug/IgniterSDR G6OA03073Terminal Block · shortedMOMENTARY FLASH OF MASTER WARNING 3 SEPERATE TIMES 3RD TIME POSSIBLY ACCOMPANIED BY CARGO FIRE LIGHT ON PILOTS PANEL.Dec 30, 2003 · N612 · Bell 206B3 · Instrument System WiringSDR WRNA200300014Check Valve · faultyNR 2 ENGINE HAD SEVERE VIBRATION ON DESCENT FROM 29,000 FT. ENGINE PARAMETERS WERE ALL OK EXCEPT N1 NR1 85 PERCENT, NR 2 60 PERCENT VIBRATION STOPPED WHEN THROTTLE BOUGHT BACK BELOW 53.5 PERCENT. FUEL DUMPED. NORMAL LANDING. TROUBLESHOT TO FAULTY IP CHECK VDec 10, 2003 · N502TA · Airbus A300B4203 · Pneumatic Distribution SystemSDR 03FDEA01762Engine · failedAPPROX 1710Z FL330 CRUISE, RECEIVED A NR 1 ENG OIL LOW LIGHT, WITH L/O PSI & 0 OIL QUANTITY. ENG WAS SHUT DOWN IAW RED TABS. WINDMILL RPM REMAINED THROUGH OUT FLT. PER FLIGHT CREW EMP 447288 THE NR 1 ENG WAS RUN AT IDLE FOR A MINIMUM OF 2 MIN PER MM REF 7Oct 16, 2003 · N309FE · Doug DC1030 · Turbine Engine Oil SystemSDR WRNA200300013Clamp · looseNR 1 ENG NACELLE TEMP READ 300+ ON CLIMB OUT. TEMP. REACTED TO THROTTLE MOVEMENT. DUMPED APPROX. 30K LBS. RETURNED TO FIELD, LANDING NORMAL. MAINTENANCE FOUND IP CHECK VALVE CLAMP OFF DUCT. REINSTALLED CLAMP IAW PROCESS MATERIAL SPEC. MANUAL 01-05-42. ENGINE Oct 1, 2003 · N501TR · Airbus A300B4203 · Pneumatic Distribution SystemSDR XNOA01156Element · malfunctionedDURING CLIMB NR 1 ENG (B LOOP) LT ILLUM WITH LOOPS LT ILLUM ON MWP. CHECKLIST CARRIED OUT AND ENG FIRE WARNING REMAINED ON AFTER POSITIVE TEST OF (LOOP A). ENG FIRE CHECKLIST CARRIED OUT AND FIRE IND CEASED AFTER LEFT FIRE BOTTLE DISCHARGED. INSP NR 1 ENG NO LSep 22, 2003 · N371PC · Airbus A300B4203 · Fire DetectionSDR XNOA01155Starter · failedNR 1 ENGINE NO N-2 DURING START, NO ENG ROTATION, START VALVE OPEN. REMOVED AND REPLACED NR 1 ENG STARTER, GROUND CHECK OK IAW A300 AMM 80-13-01. STATUS: (SUPP/CLOSED)Sep 20, 2003 · N371PC · Airbus A300B4203 · Engine StarterSDR XNOA01154Warning Light · illuminatedDURING CLIMB AT FL 170 NR 1 ENG (B) LOOP LT ILLUM WITH LOOPS LT ON MWP. CHECKLIST CARRIED OUT AND ENG FIRE WARN REMAINED ON AFTER POSITIVE TEST OF LOOP (A). INFLIGHT ENG FIRE PROC CARRIED OUT AND A/C RETURNED TO HONG KONG. NOTE: FIRE WARNING CEASED WITH FUELSep 18, 2003 · N371PC · Airbus A300B4203 · Fire DetectionSDR XNOA01145Indicator · inoperativeNR 1 EGT GAUGE INOPERATIVE. RED FLAG. NO INDICATION ON DIGITAL OR ANALOG DURING START. ACTION TAKEN: REMOVE AND REPLACE EGT INDICATOR. OPS CHECK GOOD IAW A300 MM 77-21-11.Aug 19, 2003 · N474AS · Airbus A300B4203 · Engine EGT/TIT Indicating SystemSDR XNOA01120Engine · out of rigNO THROTTLE RESPONSE ON NR 1 ENGINE. RIG VSV AND VBV IAW ENGINE MANUAL 72-00-00. POWER RUN CHECK GOOD.May 27, 2003 · N373PC · Airbus A300B4203 · Fuel Controlling SystemSDR 03FDEA00448Manifold · dentedNR 1 ENGINE SIDE LONGITUDINAL CDP AIR 14TH STAGE MANIFOLD FWD END 90 DEG ELBOW PART HAS 2 EA ADJACENT DENTS. CLOSING ACTION ON 04/14/03. ON N/R 00425. REMOVED AND REPLACED CDP AIR TUBE MANIFOLD AT 14TH STAGE IAW M/M 75-00-04-4.Apr 15, 2003 · N320FE · Doug DC1030 · Engine Cooling SystemSDR 03FDEA00431Bracket · crackedNR 2 ENGINE FAN CASE ANTI-ICE HOT DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT HAS CRACK. CLOSING ACTION ON 04/10/03. REMOVED AND REPLACED NR 2 ENGINE FAN CASE ANTI-ICE HOT AIR DUCT HOLDING BRACKET AT 12 O`CLOCK NEAR LT FWD ENGINE MOUNT IAW M/Apr 11, 2003 · N320FE · Doug DC1030 · Nacelle/Pylon Miscellaneous StructureSDR XNOA01110Engine · malfunctionedENGINE 1 N1 114 EGT 410 DEGREE C N2 47 PERCENT FF 2300. ACTED LIKE A HUNG START AT 50 SEC. WE REJECTED TAKE OFF. PERFORMED ENG RUN. ALL PARAMETERS NORMAL IAW A300 MM 72-00. INSPECTED NR 1 ENG. NO DEFECTS NOTED.Mar 26, 2003 · N473AS · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR DHL2003367502Flange · crackedItem Ref. N/R 0029640:T/R fwd. skin attach cracked on #2 O/B T/R. Corrective action:Cut out damaged area,fabricated repair IAW Timco REO-GO9089. Alodined an primed IAW A300 SRM 51-40-10 an installed IAW A300 SRM 51-30-30.Mar 3, 2003 · N367DH · Airbus A300B4203 · Engine Thrust ReverserSDR DHL2003367501Flange · crackedItem Ref.N/R:36725:#2 O/B rev. upper side has internal metal structure broken. Corrective action:Cut out damaged area,fabricated repair IAW Timco REO-GO9095. Alodined an primed IAW A300 SRM 51-30-30.Feb 25, 2003 · N367DH · Airbus A300B4203 · Engine Thrust ReverserSDR DHL2003367511Doubler · worn#1 eng. L/H core cowl aft ctr. inside doubler has depth wear on doubler. Corrective action:Removed worn doubler fabricatednew doubler IAW A300 SRM 54-00-00 primed new doubler IAW A300 SRM 51-40-12,installed new doubler IAW A300SRM 51-40-21. Removed an replacedFeb 22, 2003 · N367DH · Airbus A300B4203 · Engine Cowling SystemSDR XNOA01106Connector · dirtyON TAKEOFF NR 1 ENGINE N1 ERRATIC BETWEEN 93 PERCENT TO 124 PERCENT. CLEANED AND RESEATED CONNECTOR P1 GOOD AT NR 1 PYLON. PERFORMED ENG RUN. OPS CHECKS GOOD. NO DEFECTS NOTED IAW A300 MM 71-00-00.Feb 21, 2003 · N13974 · Airbus A300B4203 · Engine Indicating System WiringSDR XNOA01102Engine · malfunctionedON TAKEOFF, POWER APPLICATION NR 2 ENG N2 INDICATED LOW. TAKEOFF REJECTED (NO HIGH ENERGY STOP). AS PER MAINTENANCE CONTROL INLET & EXHAUST INSPECTED. NO DEFECT NOTED. ACCOMPLISHED POWER RUN TO 70 PERCENT. FOUND FUEL FLOW N2 & EGT IN PARAMETERS. DEFERREJan 31, 2003 · N473AS · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR DHL2003362006Fuel Filter1) ENGINE #1 FUEL CLOG LIGHT ILLUMINATED AFTER T/O AT T/O THRUST SETTING. LIGHT EXTINGUISHED AFTER INITIAL POWER REDUCTION. DURING CRUISE LIGHT ILLUMINATED AGAIN RAN ABNORMAL PROCEDURES.2) REMOVED AND REPLACED #1 ENGINE FUEL FILTER. GROUND RAN ENGINE OPS CHJan 24, 2003 · N362DH · Airbus A300B4203 · Engine Fuel DistributionSDR WRNA200300001Engine · overtempDuring climb out of flt level 75, time 0540Z, heard an expolosion from #1 engine, confirmed #1 engine failure, #1 engine EGT went to max indication, followed emergency and abnormal procedure, fuel dump procedure was followed down to max landing weight. A/C retJan 17, 2003 · N820SC · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR XNOA10196Engine · stalledDURING DESCENT 12,000 FT NR 2 ENG BEGAN TO COMPRESSOR STALL. FUEL FLOW NORMAL. EGT ENG STABLE AT IDLE POSITION. INSPECTED NR 2 ENG MAIN FUEL FILTER, NO DEFECTS NOTED. INSPECTED NR 2 ENG FUEL PUMP STRAINER, NORMAL AND NO DEFECTS NOTED. INSPECTED NR 2 ENG VDec 21, 2002 · N224KW · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR XNOA01096Compressor · stalledDURING DESCENT 12,000 FT NR 2 ENG BEGAN TO COMPRESSOR STALL. FUEL FLOW NORMAL. EGT ENG STABLE AT IDLE POSITION. INSPECTED 2 ENG MAIN FUEL FILTER, NO DEFECTS NOTED. INSPECTED NR 2 ENG FUEL PUMP STRAINER, NORMAL. NO DEFECTS NOTED. INSPECTED NR 2 ENG VSVS, Dec 21, 2002 · N224KW · Airbus A300B4203 · Turbine Engine Compressor SectionSDR 02FDEA00813Compressor · damagedON TAKEOFF AND JUST 5 AFTER ROTATION HEARD LOUD NOISE AND ENGINE NR 3 ROLLED BACK TO APPROXIMATELY 35 PERCENT N1. ENGINE OVER TEMP LIGHT CAME ON MOMENTARILY. ENGINE CONTINUED TO WINDMILL. DUE TO NOISE AND VIBRATION PULLED ENGINE FIRE HANDLE AND BLEW NR 1 BONov 8, 2002 · N318FE · Doug DC1030 · Turbine Engine Compressor SectionSDR 02FDEA00811Chip Detector · contaminatedENGINE NR 2 OIL FILTER LEVEL 2 ALERT, CAME ON AT TOP OF CLIMB. THROTTLE WAS RETARDED TO IDLE BUT ALERT STAYED ON. ENGINE NR 2 WAS SHUT DOWN IAW THE CHECKLIST. ENGINE FAN COWLS WERE OPENED AND THE MASTER CHIP DETECTOR WAS PULLED, FERROUS METAL STRANDS WERE CNov 7, 2002 · N303FE · Doug DC1030F · Turbine Engine Accessory DriveSDR WRLA200224Blade · failedNR 3 ENGINE SUSPECTED COMPRESSOR STALL ON TAKE OFF, CLIMB OUT. EGT OFF SCALE, NR 1 DROPPED, VIBRATION NOTED, SHUT DOWN ENGINE IAW INFLIGHT SHUTDOWN PROCEDURES. COMPLIED WITH DC10 MM CHECK LIST TWO ENGINE FERRY FLIGHT. ACCOMPLISH BORESCOPE NR 1 AND NR 2 ENGIOct 6, 2002 · N526MD · Doug DC1030 · Turbine Engine Compressor SectionSDR XNOA01076Ignition Lead · looseNR 2 ENGINE B IGNITION INOPERATIVE. CLEANED & RESECURED B IGNITION LEAD. OPS CHECK GOOD ON GROUND RUN.Sep 29, 2002 · N371PC · Airbus A300B4203 · Ignition Harness (Distribution)SDR XNOA01075Connector · looseUNABLE TO START NR 2 ENGINE WITH "B" IGNITION. RESEATED CONNECTOR PLUG ON "B" IGNITION EXCITER BOX. OPS CHECK NORMAL IAW MM 74-11-01.Sep 26, 2002 · N371PC · Airbus A300B4203 · Ignition Harness (Distribution)SDR WRNA200200005Line · broken#1 engine oil qty dropped to zero (0) after flt level 27.0 #1 eng oil press flux between 40-30 psi then 30-20 psi then steady no psi. Aircraft made unscheduled landing @ MSY. No fuel was dumped. Aircraft landed normally.Corrective Action: Found "D" sump scavenSep 26, 2002 · N502TA · Airbus A300B4203 · Engine Oil PressureSDR XNOA01072Lead · failedUNABLE TO START NR 2 ENGINE WITH 'B' IGNITION. SWAPPED IGNITER LEADS IN ACCORDANCE WITH A300MM 74-11-00. OPS CHECK GOOD ON GROUND.Sep 24, 2002 · N371PC · Airbus A300B4203 · Ignition Harness (Distribution)SDR XNOA01066Case · damagedNR 2 ENGINE FIRE WARNING AFTER TAKEOFF. AFTER PULLING THROTTLE TO IDLE, INDICATION WENT OUT. ELECTED TO RETURN FOR OVERWEIGHT LANDING. T/S AND FOUND NR 12 LP FUEL NOZZLE FLANGE BURN HOLE IN ENG CASE. REPLACE NR 2 ENG ASSY PER ENA AMM A300-71-00-00 PERFORMEAug 27, 2002 · N371PC · Airbus A300B4203 · Turbine Engine Combustion SectionSDR DHL2002367008Engine · malfunctionedAS THROTTLES WERE ADVANCED FOR TAKEOFF WITH THROTTLE POSITION EQUAL, ENGINE NR 1 N1 HUNG BACK AT 20 PERCENT WITH ENG NR 2 AT 70 PERCENT. UNABLE TO MAINTAIN RUNWAY CENTER LINE. REJECTED TAKEOFF AT LESS THAN 10 KTS. PERFORMED MAX POWER ASSURANCE RUN PER JRH Aug 21, 2002 · N367DH · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR WRNA200200002Fuel Control · out of adjustDURING CLIMB NR 2 ENGINE BLEED VALVE REG FAULT LIGHT CAME ON. TEMP INCREASE TO 230 DEGREES AND TEMP HI LIGHT CAME ON FOLLOWED BY A/C PACK FAULT LIGHT. UNABLE TO CONTROL PRESSURIZATION DUE TO NR 1 BLEED VALVE CURRENTLY ON MEL (LOCKED OUT) NR 2 HP BLEED FAULT Jul 25, 2002 · N821SC · Airbus A300B4203 · Fuel Control/Turbine EnginesSDR XNOA01060Connector · damagedNR 1 ENGINE OIL PRESSURE GAUGE READS ZERO WITH ENGINE RUNNING-ALL OTHER PARAMETERS NORMAL. CLEANED & RESET CONNECTOR AT OIL PRESS TRANSMITTER. OPS CHECK NORMAL IAW MM 79-00-00.Jul 11, 2002 · N13974 · Airbus A300B4203 · Engine Oil Indicating SystemSDR CNMA200200004Engine · malfunctionedNR 2 ENGINE OR ACFT SHUTTERED, MADE A POP, THEN WENT QUIET. NR 2 ENGINE'S EGT WENT TO 945. REDUCED THROTTLE TO 740 N1 AND N2. CLIMBING TO 2100 FT EGT STABILIZED AROUND 915 - 925 AND OIL FILTER CLOG LIGHT CAME ON NR 2 ENGINE. SHUT DOWN NR 2 ENGINE. RETURNEJul 8, 2002 · N540AX · Doug DC1030 · Engine (Turbine/Turboprop)SDR WRLA200217Sensor · erraticENGINE FAIL CAUTION LIGHT ILLUMINATED DURING TAKE OFF DUE TO NR 1 ENGINE N1 TACH GIVING ERRATIC INDICATIONS. (REJECTED TAKE OFF AT 70 KNOTS.) REMOVED AND REPLACED NR 1 ENGINE FAN SPEED SENSOR , RAN ENGINE NR 1 UP TO 85 PERCENT NR 2, FOUND NO ERRATIC FLUCTUAJul 7, 2002 · N304WL · Doug DC1030F · Engine RPM Indicating SystemSDR UIE2002F00003Clamp · looseAFTER TAKEOFF NR 3 ENGINE FIRE WARNING LIGHT CAME ON AND NACELLE HEAT FOR NR 3 ENGINE READ 8 ON BOTH SIDES. AFRTER LEVELING OFF AND REDUCING POWER, THE LIGHT WENT OUT. ENGINE SHUT DOWN PERFHB AIRCRAFT RETURNED TO AIRPORT. C/A: FOUND 14TH STAGE DUCT CLAMPS Jun 22, 2002 · N506MC · Boeing 7472D3B · Compressor Bleed ControlSDR XNOA01053Relay · looseDURING NR 2 ENGINE START ALL ENGINE PARAMETERS EXCEEDED NORMAL AND IDLE VALVES. FOUND GROUND SAFETY RELAY 91GB LOOSE. REINSTALLED GROUND SAFETY RELAY AND SECURED IAW SP. OPS CHECK NORMAL.Jun 21, 2002 · N370PC · Airbus A300B4203 · Compressor Bleed ValveSDR CA020607005Valve · inoperative(CAN) REACHING FL290 ABNORMAL CABIN RATE. DOING THE CHECK LIST, UNABLE CONTROL CABIN ALTITUDE. INITIATING EMERGENCY DESCENT AND TURNING BACK TO DEPARTING AIRPORT.May 29, 2002 · Airbus A300B4203 · Cabin Pressure Control SystemSDR 02FDEA00327Engine · damagedAT 31,000 FT ALT, JUST BEFORE DESCENT NR 3 ENGINE RUMBLED TWICE AND N1 STARTED TO DECREASE. RETARDED THROTTLE TO IDLE AND N1 WAS 38 PERCENT. ADVANCE THROTTLE NO MOVEMENT ON ENGINE WHEN PASSED THROUGH 10,000 FT. ENGINE RUMBLED AND CAME BACK TO NORM. REINSTAMay 11, 2002 · N307FE · Doug DC1030 · Engine (Turbine/Turboprop)SDR 0201461244Engine · making metalDURING CLIMB AT 10,000 FEET, NR 3 ENGINE COMPRESSOR STALLED AND FLAMED OUT. FLIGHT CREW DID NOT ATTEMPT ENGINE RESTART. APPROXIMATELY 65,000 LBS OF FUEL WAS DUMPED. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE May 6, 2002 · N244NW · Doug DC1030 · Engine (Turbine/Turboprop)SDR 0201471242Engine · flamed outDURING CRUISE FLIGHT AT 36,000 FEET THE NR 3 ENGINE ROLLED BACK APPROXIMATELY 20 PERCENT. THRUST LEVER INPUT HAD NO EFFECT ON ENGINE RPM AND 30 SECONDS AFTER INITIAL ROLLBACK THE NR 3 ENGINE FLAMED OUT. FLIGHT CREW WAS UNABLE TO RESTART THE NR 3 ENGINE. FLIApr 29, 2002 · N242NW · Doug DC1030 · Engine (Turbine/Turboprop)SDR 02FDEA00249Mec · out of rigON TAKEOFF NR 3 ENG W/N ATTAIN MAX PWR. ADJUSTED NR 3 ENG MEC 1/2 TURN UPTRIM, RAN ALL ENG PER JRH CHAPTER 5 AND ACCOMPLISHED MAX. ALL ENGINES OPERATING OKAY.Apr 12, 2002 · N319FE · Doug DC1030F · Fuel Control/Turbine EnginesSDR CNMA200200003Cowling · missingNR 2 ENGINE FAN COWL FOUND MISSING UPON WALK-AROUND AFTER LANDING. REPLACED LEFT ENGINE SIDE COWL AND ASSOCIATED HARDWARE, NO OTHER DAMAGE NOTED.Mar 30, 2002 · N630AX · Doug DC1030 · Engine Cowling SystemSDR XNOA01042Engine · out of rigNR 1 ENGINE IS SLOW TO SPOOL. LAGS BEHIND NR 2 ENGINE BY 35 PERCENT N1. PERFORMED STATIC RIG CHECK VSV. NO FAULT FOUND. BOROSCOPED 1,5,6,13,14 COMPRESSOR, HPT-1 LPT-2. NO FAULTS FOUND ALL IAW A300 MM 71-00-00.Mar 29, 2002 · N472AS · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR XNOA01040Engine · out of trimNR 1 ENGINE IS SLOW TO SPOOL & WILL NOT OBTAIN MAX POWER. TRIMMED NR 1 ENGINE MEC IAW A300 MM 71-00-00. OPS & LEAK CHECK GOOD.Mar 26, 2002 · N472AS · Airbus A300B4203 · Engine (Turbine/Turboprop)
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