JASC 7200

Service difficulty reports · 14,730

Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.

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 jasc_code = '7200'
  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 VNAA0611014Engine · failedCREW REPORTED LOUD BANGS ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AT LOW SPEED AND RETURNED TO GATE. MAINTENANCE INSPECTED AND DETERMINED THE ENGINE NEEDED REPLACED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE. OPERATIONAL CHECKS WERE PERFORMEDNov 10, 2006 · N710PS · Cndair CL6002C10SDR ABXA060304Fitting · crackedNR 2 ENGINE HAD CRACKED FITTING JUST FORWARD OF INBOARD THRUST REVERSER UPPER ATTACH POINT AREA. REMOVED ALL SEALS AND SEAL RETAINERS. REPAIRED FLANGE PER REA B672-55012. REINSTALLED ALL PARTS REMOVED PER SRM 51-40-2.Nov 8, 2006 · N783AX · Boeing 767281SDR NSVA200600198Friction Lock · out of adjustCONFIG LIGHT CAME ON DURING TAKEOFF, ABORTED AT 90 KNOTS INSPECTED, FOUND FRICTION LOCK POSSIBLY AT FAULT. PERFORMED ADJUSTMENT AND TEST PROCEDURES IAW SAAB MM 71-00-00. OPS CHECK NORMAL NO CONFIG LIGHT ILLUM AND CONDITION LEVER FRICTION LOCK WORKS FINE, NO Nov 7, 2006 · N309CE · Saab 340BSDR C2XA06SH126Case · corrodedSHV - DURING C-CHECK THE NUMBER 2 ENGINE FAN CASE FORWARD ATTACHMENT HOLES WERE FOUND TO BE CORRODED. INFORMATION WAS SUBMITTED TO ENGINEERING FOR REPAIR AND DISPOSTION.Nov 6, 2006 · N13978 · Emb EMB145LRSDR C2XA06IA173Engine · shutdownIAH - FLIGHT 2780, THE CREW REPORTED AN UNCOMMANDED ENGINE SHUTDOWN DURING DESCENT INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR Nov 6, 2006 · N11107 · Emb EMB145XRSDR ASMF200611003Blade · fodDURING TRANSIT CHECK, A LEFT ENGINE BLADE WAS DETECTED DAMAGED WITH 1INCH LENGTH, 0.640 INCH WIDTH IN THE MIDSPAN AND 0.359 INCH DEPTH. THE FIRST STAGE BLADES SET WAS REPLACED IAW MM 72-33-21, PAGE 401 AND ENGINE VIBRATION CHECK WAS PERFORMED IAW MM 72-00-00, Nov 6, 2006 · N205AM · Doug DC987SDR C2XA06CL089Bevel Gear · failedPVD FLIGHT NR 2366 THE CREW REPORTED ENGINE NR 2 FAILED IN FLIGHT ON DESCENT INTO PVD. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. DFDR DATA SHOWED NR 2 ENGINE DECREASED FROM 91% TO 0 IN 1 Nov 6, 2006 · N11150 · Emb EMB145XRSDR HALA0600854Engine · vibrationETOPS SIGNIFICANT SYSTEM, IN CRUISE RESONATING VIBRATION CAUSED BY SLIGHT SPLIT IN ENGINE INDICATIONS. FL390 AUTOTHROTTLES ON EPR 1.33L AND R LN,87.8 RN, 88.5 LN2 - 89RN288 FFL4.9 R4.8. INSPECTED NR 1 AND NR 2 ENGINES, NO DEFECTS NOTED ON GRD, ALL PARAMETERSNov 6, 2006 · N588HA · Boeing 767300SDR NSVA200600196Engine · power lossPARTIAL POWER ON NR 2 ENGINE DURING TAKEOFF. TRQ COULD NOT EXCEED 2500 LBS REGARDLESS OF POSITION. TAKEOFF ABORTED. ADJUSTED LOST MOTION LINK REF 76-10-00. RUN UP OPS CHECK NORMAL.Nov 5, 2006 · N172MJ · Beech 1900DSDR CA061113001Engine · malfunctioned(CAN) .5 HRS AFTER A SCHEDULED REPLACEMENT OF THE NR 3 AND NR 4 BEARING ASSY AND THE NR 1 AND NR 2 POWER TURBINE DISC`S DUE TO CYCLE LIFE LIMIT BEING REACHED, THE ENGINE LOST OIL PRESSURE AND WAS SHUTDOWN AND AIRCRAFT RETURNED TO DEPARTURE FIELD WITHOUT FURTHENov 5, 2006 · Beech 1900DSDR HALA0600851Engine · fodETOPS SIGNIFICANT SYSTEM, FOUND ON WALKAROUND PLASTIC BAG STUCK IN NR 2 ENG FAN BLADES NO DAMGE NOTED. INSPECTED NR 2 ENG PER AMM 05-51-00. REMOVED PLASTIC BAG FROM NR 2 ENG. NO DAMAGE NOTED SECURITY CHECK GOOD.Nov 5, 2006 · N589HA · Boeing 767300SDR ARWA20061101Engine · malfunctionedNR 1 ENGINE FAILED TO ACCELERATE PASS 80 PERCENT N1; ABORTED TAKEOFF AT 75 KTS. REMOVED AND REPLACED MAIN FUEL PUMP AND FUEL CONTROL ASSEMBLY IN ACCORDANCE WITH M/M 73-12-01; PERFORMED LEAK CHECK, NO LEAKS NOTED; PERFORMED ENGINE RUN AND TRIM IN ACCORDANCE WINov 3, 2006 · N68041 · Doug DC1010SDR WP07110306Bearing · failedENGINE WAS SENT TO MFG FOR A FLAME OUT INVESTIGATION. AT RECEIPT 2 KEY OBSERVATIONS WERE MADE. FIRST THE FILTER BYPASS INDICATOR WAS EXTENDED AND SECOND THE ROTATING GROUP WOULD NOT ROTATE. ONCE THE NOSE CONE AND DIAPHRAGM WERE REMOVED METAL WAS SEEN SHED THRONov 3, 2006SDR CHQA200600137Engine · malfunctionedFLIGHT 6306 - CMH-BDL - ON TAKEOFF FROM CMH AT ABOUT 500 FEET, LAV SMOKE DISPLAYED ON EICAS AND AT THE SAME TIME, THE FA NOTICED SMOKE IN THE CABIN. COMPLETED MEMORY ITEMS, DECLARED AN EMERGENCY. UNEVENTFUL LANDING. REMOVED AND REPLACED ENGINE 2.Nov 2, 2006 · N841RP · Emb EMB135LRSDR CA061219015Engine · damaged(CAN) ON TAKEOFF, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE. THE FIGHT CONTINUED AND ON DESCENT ENGINE OIL PRESSURE FELL TO ZERO RESULTING IN A PROPELLER AUTOFEATHER. THE ENGINE WAS SHUTDOWN IN FLIGHT. GROUND INSPECTION REVEALED INTERNAL ENGINE DAMAGE. MFGNov 1, 2006 · Emb EMB110*SDR CA061106006Engine · failed(CAN) IN CRUISE THE ENGINE EMITTED A LOUD NOISE AND ENGINE ITT TEMPERATURE WAS SEEN TO INCREASE. POST-FLIGHT INSPECTION FOUND THE PROPELLER COULD NOT BE ROTATED. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Nov 1, 2006 · Aerosp ATR42300SDR HALA0600843Blade · damagedON DEPARTURE NR 2 ENGINE INGESTED A BIRD, ALSO RECEIVED ACARS VIBRATION MESSAGE. FOUND BLADE DAMAGE ON 12 FAN BLADES AND NOSE BULLET. REPAIRS IN WORK.Nov 1, 2006 · N593HA · Boeing 767300SDR UIEA200600281Engine · failedAIR TURN BACK AFTER NR 4 ENGINE FLAMED OUT WHEN CLIMBING OUT, WHEN CLIMBING THROUGH F/L 260 INCH, A COUGH WAS HEARD PRIOR TO FLAME OUT. ENGINE WAS FOUND WITH METAL IN TAIL PIPE, ENGINE WAS REPLACED IAW CF6-50E2 POWERPLANT REMOVAL AND INSTALLATION FORM NR 01-AAOct 30, 2006 · N522MC · Boeing 7472D7BSDR AALA20060961Engine · malfunctionedJFK INFLIGHT T837/30 OCT - AFTER TAKEOFF THE AFT LAVATORY FIRE SMOKE ALARM WENT OFF. FLIGHT ATTENDANT REPORTED SOMETHING BURNING IN AFT LAVATORY. ALSO REPORTED A GRINDING MOTOR SOUND WHEN THE SMOKE DISSIPATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. Oct 30, 2006 · N14065 · Airbus A300B4605RSDR CHQA200600136Engine · malfunctionedAT ACCELERATION ALTITUDE (APPROXIMATELY 500 FEET) "ENG 2 OUT" MESSAGE APPEARED. AT THE SAME TIME, HEARD A LOUD POP. DECLARED AN EMERGENCY. FLIGHT ATTENDANT REPORTED THE SEATBELT SIGNS FLASHING OFF, FOLLOWED BY A SPARK NEAR SEAT 4A PSU. JUST BEFORE ROTATION,Oct 30, 2006 · N269SK · Emb EMB145LRSDR DL757060899Engine · malfunctionedON CLIMB-OUT AT APPROX 8000, LEFT ENG EGT INCREASE INTO RED RADIAL MAX EGT OF 789. LEFT THROTTLE RETARD TO IDLE AFTER APPROX 2 MINUTES EGT WITHIN NORMAL LIMITS. THROTTLE ADVANCE BACK TO CLIMB POWER AND ALL ENGINES INDICATION ARE NORMAL. REPLACED NR 1 ENG PEOct 29, 2006 · N601DL · Boeing 757232SDR ASMF200610012Powerplant · power lossAIRCRAFT REJECTED TAKEOFF AT 40 KNOTS DUE TO THE LT ENGINE DID NOT ACCELERATE MORE THAN 1.2 EPR’S. AT PLATFORM, ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. DURING OVERNIGHT CHECK, ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00 AND 71-00-01, Oct 28, 2006 · N583MD · Doug DC983SDR ANCF200600039Filler · damagedDURING TAKEOFF, ABOUT 400FT, EXPERIENCED RT ENGINE FAILURE WITH BUMPING. RT EGT REACHES 933 DEGREES (C) AFTER THAT THE RT ENGINE WAS SHUTDOWN, EMERGENCY PROCEDURE WAS PERFORMED. THE INSPECTION ON GROUND SHOWED THAT ANNULUS FILLER FROM POS 9 WAS RELEASED CAUSOct 28, 2006 · N506NA · Boeing 757236SDR CA061103016Engine · flamed out(CAN) THE ENGINE FLAMED OUT IN FLIGHT FOLLOWING A COMMANDED REDUCTION IN POWER TO IDLE. PWC WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC# 20061103016)Oct 27, 2006 · Cessna 550SDR 2006FA0001132Engine · failedDURING GROUND RUN FRO A POSSIBLE GENERATOR PROBLEM. WITH THE ENGINE AT FLIGHT IDLE AND SPEED LEVERS FORWARDTHE RT ENGINE HAD A UNCONTAINED ENGINE FAILURE. 2 PIECES OF THE ENGINE PENETRATED THE RT FUSELAGE SKIN ADJACENT TO THE CO PILOT POSITION. (K)Oct 26, 2006 · N93WT · Beech B100SDR AALA20060937Engine · leakingSTL INFLIGHT T2243/25OCT ON ROTATION HEARD LOUD NOISE. OIL QUANTITY AND OIL PRESSURE WENT TO ZERO ON NUMBER ONE ENGINE. SMOKE STARTED TO APPEAR IN CABIN. RETURNED TO STL AND LANDED WITHOUT INCIDENT. LEFT ENGINE WAS SHUT DOWN UPON LANDING. REPLACED NUMBEROct 25, 2006 · N459AA · Doug DC982SDR USAABB06082Engine · failedFLIGHT 818, CLT-BWI: UPON APPLICATION OF TAKEOFF POWER, THE RIGHT ENGINE FAILED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE FOUND SEPARATION OF THE RIGHT NOSE COWL LINER, WHICH CAUSED FOD TO THE RIGHT ENGINE. THE RIGHT ENGINE WAS REPLACED.Oct 25, 2006 · N929UW · Boeing 757225SDR DL777060883Engine · damagedNBR 1 ENGINE REPLACED DUE FAILED BORO INSPECTION DAMAGE TO THE 5 TH STAGE COMPRESSOR. ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.Oct 23, 2006 · N862DA · Boeing 777232SDR 1023200603Warning Light · illuminatedON DEPARTURE (GYD), JUST AFTER V1, NR 1 ENGINE VIBE LIGHT ILLUMINATED, VIBE METER NR 1 OFF SCALE HIGH, INCLUDING VIBRATION AS WELL. ENGINE SHUT DOWN, FUEL DUMP, AND RETURNED TO (GYD).CORRECTIVE ACTIONS, PENDING.Oct 23, 2006 · N361FC · Boeing 747200BSDR CA061219012Engine · unknown(CAN) IN FLIGHT A LOUD NOISE WAS HEARD AND THE WINDSHIELD BECAME COVERED IN OIL. A FORCED LANDING FOLLOWED RESULTING IN AIRFRAME DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.Oct 22, 2006 · Cessna 208BSDR G41A2006001Engine · shutdownON 10/21/2006 ON AN AIR AMBULANCE TRIP, ON THE SECOND LEG, THE AIRCRAFT WAS ON THE GROUND FOR ABOUT 1.5 HRS WHILE TAXIING TO RUNWAY THE LT ENGINE SHUTDOWN FOR UNKNOWN REASON. THE CAPTAIN RESTARTED THE ENGINE AND CONTINUED THE TRIP WITH NO FURTHER PROBLEMS.Oct 21, 2006 · N46MF · Lear 35ASDR USAABB06080Engine · surgesPHL FLT 1707 EN ROUTE FROM DUB TO PHL, CREW REPORTED RIGHT ENGINE SURGES AND LOW CLIMB POWER. RIGHT ENGINE THRUST LEVER IS 3/4 KNOB WIDTH FORWARD OF LEFT AT FL380. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT PHL. MAINTENANCE ACCOMPLISHED FIM POct 21, 2006 · N645US · Boeing 767201SDR SWAA064069Compressor · stalledINFLIGHT SHUTDOWN, AIR TURNBACK, DECLARED EMERGENCY. NR 1 ENGINE COMPRESSOR STALL ON DEPARTURE FROM MDW. F/A REPORTED FIRE ON LT SIDE OF AIRCRAFT, SHUTDOWN NR 1 ENGINE, DISCHARGED FIRE BOTTLE. REMOVED AND REPLACED NR 1 ENGINE PER MT.Oct 21, 2006 · N412WN · Boeing 7377H4SDR VNAA0610034Engine · failedCREW REPORTED SMOKE IN COCKPIT AND CABIN ON TAKEOFF. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND FOUND COKING ON 10TH STAGE DUCTING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAOct 20, 2006 · N253PS · Cndair CL6002B19SDR HALA0600807Engine · faultedDURING TAXI LT ENGINE SYSTEM FAULT. INTERROGATED EEC1 NO FAULTS NOTED. ACCOMPLISHED SYS RETURN TO SERVICE TEST IAW FIM 73-21 TEST PASSED.Oct 20, 2006 · N484HA · Boeing 717200SDR AALA20060891Blade · failedSJC INFLIGHT T1810/19OCT - DURING CLIMB CREW REPORTED LEFT ENGINE ROLLBACK TO TEN PERCENT N1 AT FLIGHT LEVEL 140. PERFORMED ENGINE SHUTDOWN. SINGLE ENGINE TIME TEN MINUTES. LANDED SJC WITHOUT INCIDENT. FOUND COMPRESSOR BLADE FAILURE. REPLACED NUMBER ONE EOct 19, 2006 · N7544A · Doug DC982SDR DXTA200601671Engine · bird ingestionON TAKEOFF ABOUT 20 SECONDS AFTER MAVS SELECTED OPEN (700 MSL) A CHEMICAL ODOR FOLLOWED BY A BURNING OF THE EYES AT 1500 MSL. THE MAV'S WERE SELECTED CLOSED AND THE APU BLEEDS ON. THE CHEMICAL ODOR WENT AWAY SHORTLY AFTER THAT. ISOLATED ODOR TO LEFT ENGINE Oct 19, 2006 · N815QS · Raythn HAWKER800XPSDR 2006UALA02045Tailpipe · fire2 MINUTES AFTER SHUTDOWN OF NR 2 ENG GROUND WORKER CALLED AND INDICATED THAT WE HAD RESIDUAL TAILPIPE FIRE. REPLACED THE NR 5 BEARING SUPPLY & SCAVENGE OIL LINES.Oct 19, 2006 · N840UA · Airbus A319131SDR 2006UALA02021Engine · vibrationDURING ENGINE START NR 2 ENG VIBRATION WAS OBSERVED WITH 2.5 UNITS OF N2 VIBRATION WITH SPARKS OBSERVED FROM ENG INLET, ENGINE WAS SHUTDOWN. ON RESTART ATTEMPT, LOUD NOISE HEARD W ITH START VALVE OPEN, ONLY 4% N2 ROTATION AND NO FAN ROTATION, ENG AGAIN SHUTDOOct 19, 2006 · N836UA · Airbus A319131SDR 101906N133CS1Seal · leakingAFTER TAKEOFF FROM CMH A STRONG BURNING ODOR WAS NOTICED BY THE CREW AND THERE WAS A HAZE FILLING THE CABIN. THE CREW ELECTED TO CALL ATC AND REQUEST A DIVERSION BACK TO CMH. AFTER EXPLAINING PROBLEM AIRCRAFT WAS CLEARED TO LAND. LANDING WAS NORMAL. PROBLEOct 19, 2006 · N133CS · Cessna 525SDR 0602316730Engine · stalledDURING CLIMB NR 2 ENGINE EXPERIENCED AN OVERTEMP WITH AUDIBLE COMPRESSOR STALL. THE ENGINE WAS SHUTDOWN, APPROXIMATELY 120,000 POUNDS OF FUEL WERE DUMPED AND THE FLIGHT RETURNED TO BKK. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SEVER DAMAGE INOct 19, 2006 · N630US · Boeing 7472J9FSDR AT0600038Nose Bullet · failedAT FL 300 IN LIGHT ICING RIGHT ENGINE PRODUCES HIGH VIB N1 (6.8) USED QRH HIGH ENG VIB PROCEDURE TRIED 4 TIMES AND AFTER LEAVING ICING, N1 VIBE DID NOT GO AWAY. F/A INFORMED ME THEY FELT UNUSUAL VIBRATIONS IN GALLEY. SHUT ENGINE DOWN AT 280 AND LANDED IN MEM. Oct 19, 2006 · N990AT · Boeing 717200SDR DXTA200601670Engine · malfunctionedON TAKEOFF ROLL, LEFT ENGINE ITT WENT STRAIGHT TO 780 (DEG)A/ INITIAL POWER UP. NO DELAY IN ABORTING. ABORTED LESS THAN 20 KNOTS AND TEMP WAS ONLY MOMENTARY. PERFORMED ITT INDICATOR SYSTEM CHECK. OPS CHECK GOOD. PERFORMED FIVE POINT RUN CAPPED AND UNCAPPEOct 18, 2006 · N622QS · Cessna 560XLSDR 2006UALA02025Engine · failedNR 1 ENGINE FAILED DURING TAKEOFF RUN. REPLACED NR 1 ENGINE. FOUND FINE METAL SHAVINGS IN TAILPIPE. CAPT REPORTED BURNING ODOR IN CABIN. NO SMOKE. EGT, EPR SPIKED. FADEC MESSAGE, VSV VALVE FAILURE. NOTHING ON PFR. NR 1 ENGINE HAS METAL IN THE AFT FAN Oct 18, 2006 · N472UA · Airbus A320232SDR 2006UALA02003Engine · failedRETURN TO FIELD DUE TO NR 1 ENGINE FAILURE. BORESCOPE AT ORD INDICATES FAILURE OF HPC R3 BLADE. REPLACED ENGINE .Oct 17, 2006 · N834UA · Airbus A319131SDR 1017200602Engine · power lossDURING CLIMB FROM (ELLX) AT AROUND FL 180 FT, NR 1 THROTTLE IS AT FORWARD STOP TO MAINTAIN CLIMB THRUST. IN CRUISE NR 1 THROTTLE IS AT 1.5 UNITS - (4) KNOBS AHEAD OF ENGINES 2, 3, 4. NOTE ALL ENGINE PARAMETERS NORMAL AT LOW ALT, BELOW 189 THROTTLE POSITIONS Oct 17, 2006 · N362FC · Boeing 747200BSDR DXTA200601659Engine · fireUPON STARTING THE RT ENGINE, HAD A HUNG START AND ABORTED PER THE CHECKLIST. AT THAT POINT, GROUND CALLED, STATED FLAMES SHOOTING OUT THE BACK OF THE PLANE. ON THE GROUND, THERE WAS A LARGE PUDDLE OF FUEL AND THE BOTTOM RT SIDE OF THE ELEVATOR WAS BLACKENED Oct 16, 2006 · N226QS · Amd FALCON2000SDR TSAA0672088Nose Bullet · looseNON-ETOPS FLT 281: CLIMBING THRU 16,000 FEET WITH THE ENGINE ANTI-ICE ON, THE CREW HEARD A LOUD BANGING SOUND COMING FROM THE LT SIDE OF THE AIRCRAFT. ENGINE INDICATIONS WERE NORMAL. THE CREW RETARDED THE NR 1 ENGINE THRUST LEVER AND THE BANGING STOPPED. TOct 16, 2006 · N824AL · Boeing 737282SDR NSVA200600179Module · cracked50-100 LBS TQ FLUX ON NR 2 ENG WITH ACCOMP PROP RPM FLEX PROP SYNC ON/OFF. FOUND RT ENG AIRFRAME BLEED LINE CRACKED, REPLACED LINE IAW 71-00-00. FOUND R BRAKE DEICE PNEUMATIC TUBE LOOSE AT FWD FIREWALL, RECONNECTED AND TIGHTENED LINE. INSPECTED PRECOOLER, POct 15, 2006 · N243CJ · Beech 1900DSDR CA061106005Engine · malfunctioned(CAN) DURING GROUND RUNS FOLLOWING EXTENSIVE MAINTENANCE THE POWER SECTION ACCELERATED UNCOMMANDED. POWER WAS REDUCED TO IDE AND THE ENGINE LOW OIL PRESSURE WARNING ACTIVATED. ON SHUT DOWN SMOKE WAS SEEN EMINATING FROM THE EXHAUST. SUBSEQUENT INSPECTION REVOct 15, 2006 · Bell 212
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