Pratt & Whitney JT8D-217A

Service difficulty reports · 235

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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 = 'JT8D217A'
  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 98ZZZX1875Case · crackedENGINE REMOVED FROM SERVICE DUE TO TURBINE FAILURE. DISASSEMBLY REVEALED HPC AND TURBINE FAILURE DUE TO C-8 SHELF CRACK FAILURE.May 5, 1998 · Turbine SectionSDR TWAA9807002Engine · failedPDX - FLT 350 - LEFT ENGINE OIL FILTER STRAINER CLOGGING LIGHT CAME ON IN-FLIGHT. LIGHT STAYED ON WHEN THROTTLE WAS RETARDED TO IDLE. SHUT DOWN ENGINE AND RETURNED TO PDX. REPLACED ENGINE. (X)May 3, 1998 · Doug DC983 · Engine (Turbine/Turboprop)SDR TWAA9805001Stator Vane · liberatedBNA - FLT 505 - AT FL 270, RT ENGINE PRODUCED TWO LARGE COMPRESSOR STALLS FOLLOWED BY PARTIAL LOSS OF ENGINE POWER. DIVERTED TO BNA. ON APPROACH, EGT STARTED TO RISE AND ENGINE WAS SHUT DOWN. FOUND TURBINE FAILURE. REPLACED ENGINE. S/D: ON ENGINE TEAR DOApr 2, 1998 · N9406W · Doug DC983 · Compressor Bleed ControlSDR TWAA9804303Compressor · stalledRNO - FLT 224 - ABORTED TAKEOFF AT 100 KTS DUE TO COMPRESSOR STALLS ON RT ENGINE. FOUND COMPRESSOR BLADES DAMAGED FROM APPARENT ICE INGESTION. (M)Mar 24, 1998 · N902TW · Doug DC982 · Turbine Engine Compressor SectionSDR CALA9800571Starter · failedTHE A START VALVE LIGHT ILLUMINATED AFTER TAKEOFF FROM CLE. THE LIGHT EXTINGUISHED AFTER ABOUT 30 SECONDS. ENGINE POWER WAS BEING REDUCED, CROSSFEED WAS CLOSED, AND HP BLEED WAS ON HIGH. THE FLIGHT LANDED AT EWR WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND TMar 22, 1998 · N16813 · Doug DC982 · Engine StarterSDR TWAA9802402Bearing · failedMEM - FLT 1226 - DURING FLIGHT, THE LEFT ENGINE, SPOOLED DOWN. MADE UNSCHEDULED LANDING AT MEM. REPLACED ENGINE. ENGINE WAS DISASSEMBLED AND FOUND NR 3 BEARING WAS THE INITIAL FAILURE. IT THEN CAUSED OTHER FAILURES. (M)Feb 16, 1998 · N919TW · Doug DC982 · Turbine Engine Compressor SectionSDR AALA980245Turbine Blade · failedSAN - FLT 1147 - ON APPROACH TO SAN AT 2,000 FEET, CREW HEARD LOUD BANG, NR 2 ENG SHUT DOWN. LANDED WITHOUT INCIDENT. REPLACED NR 2 ENG. SYS GRND CHKED, NORMAL. CONFIRMED 4TH STAGE TURB BLADE FAILED ABOVE ROOT PLATFORM FROM HCF. FRACTURE ORIGIN LOCATED OFeb 1, 1998 · N274AA · Doug DC982 · Turbine SectionSDR TWAA9801702Comp Blades · fracturedSEA - FLT 30 - CLIMBING OUT, LEFT ENGINE HAD COMPRESSOR STALL AT 5000 FT AND ANOTHER AT 7000 FT. EGT JUMPED 40 TO 50 DEGREES HIGHER THAN RT ENGINE. RETURNED TO SEA. FOUND METAL IN TAIL PIPE. CHANGED THE ENGINE. DURING ENGINE TEAR DOWN FOUND SEVEN EACH NINJan 29, 1998 · N9630A · Doug DC983 · Turbine Engine Compressor SectionSDR TWAA9801102Engine · failedAM - FLT 1508 - DURING CRUISE, VIBRATION OCCURED ON THE LEFT ENGINE. ENGINE SHUT DOWN. REPLACED LEFT ENGINE DUE TO FAILURE CAUSED BY BLUE ICE. (M)Jan 19, 1998 · N9409F · Doug DC983 · Engine (Turbine/Turboprop)SDR CALA9800004Support Cover · brokenTHE FLIGHT ATTENDANT REPORTED, LIGHT SMOKE IN THE CABIN WHILE EN ROUTE. WHILE ACCOMPLISHING ABNORMAL PROCEDURES THE RT ENGINE OIL QUANTITY BEGAN TO DECREASE. THE AIRCRAFT WAS DIVERTED TO OMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINJan 4, 1998 · N16804 · Doug DC982 · Engine (Turbine/Turboprop)SDR CALA9900002Duct · rupturedTHE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF. THRUST WAS REDUCED TO IDLE WITH THE FIRE HANDLE AND LOOP LIGHT EXTINGUISHING SHORTLY AFTERWARDS. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RTJan 2, 1998 · N72829 · Doug DC982 · Air Intake Anti/De-Ice SystemSDR CALA9701662Blade · brokenTHE TOWER NOTIFIED CREW THAT SPARKS WERE COMING FROM THE NR 2 ENGINE WHILE ON APPROACH TO BOS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION REVEALED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO A BROKENov 22, 1997 · N83872 · Doug DC982 · Turbine Engine Compressor SectionSDR TWAA9713203Pt2 Line · looseLAS - FLT 501 - DURING CLIMB, THE NR 2 ENGINE, S/N 1405, LOST POWER. THE PT2 LINE WAS FOUND LOOSE, RESECURED LINE. OPERATIONAL CHECKS AND ENGINE RUN NORMAL. (M)Nov 6, 1997 · N9403W · Doug DC983 · Fuel Controlling SystemSDR AALA972023Sensing Line · crackedFLT 751 - AFTER TAKEOFF FLL DURING CLIMB-OUT, AFT COMPT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN POWER LEVERS RETARDED. AIRCRAFT RETURNED TO FLL AND LANDED OVERWEIGHT WITHOUT INCIDENT. PLACARDED RIGHT AUGMENTAOct 27, 1997 · N59523 · Doug DC982 · Engine Anti-Icing SystemSDR 98ZZZX905Blade · failedENGINE REMOVED FOR METAL IN THE TAILPIPE.Oct 20, 1997 · Turbine SectionSDR TWAA9712302Engine · failedSTL - FLT 235 - DURING CRUISE, THE NR 1 ENGINE LOST OIL PRESSURE AND OIL QUANTITY. ENGINE WAS SHUTDOWN INFLIGHT. CHANGED ENGINE. (M)Oct 9, 1997 · N901TW · Doug DC982 · Engine (Turbine/Turboprop)SDR CALA9701400Oil Filter · cloggedTHE RIGHT ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED AFTER TAKEOFF. THE RIGHT ENGINE OIL TEMPERATURE WAS IN THE YELLOW RANGE. THE RIGHT ENGINE WAS REDUCED TO IDLE AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CSep 30, 1997 · N937MC · Doug DC982 · Turbine Engine Oil SystemSDR CALA9701389Oil Pump · failedTHE NR 2 ENGINE LOST OIL PRESSURE WHILE IN FLIGHT AND THE RIGHT OIL PRESSURE LIGHT ILLUMINATED. THE NR 2 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* ANALYSIS REVSep 24, 1997 · N16806 · Doug DC982 · Turbine Engine Oil SystemSDR 97ZZZX4373Stator · damagedENGINE REMOVED FROM SERVICE DUE TO TURBINE FAILURE. DISASSEMBLY OF THE ENGINE REVEALED HEAVY INTERNAL FAILURE OF THE HIGH COMPRESSOR STATOR AND ROTOR BEGINNING WITH 7TH STAGE. FAILURE INVESTIGATION IS IN PROGRESS AT GREENWICH.Sep 17, 1997 · Turbine Engine Compressor SectionSDR CALA9701236Oil Screen Cover · leakingTHE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY OIL PRESSURE DECREASING TO 10 PSI AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PLUG ON MAIN OIL SCREEN COVER LEAKING. A NEW OIL SCREEN COVER ASSEAug 24, 1997 · N809NY · Doug DC982 · Turbine Engine Oil SystemSDR CALA9701237Blade · failedTHE NR 1 ENGINE GAVE OFF A LOUD BANG AND QUIT DURING CLIMBOUT. AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED C-7 BLADE FAILURE.Aug 24, 1997 · N478AC · Doug DC982 · Turbine Engine Compressor SectionSDR TWAA9789002Engine · malfunctionedICT - FLT 1097 - DURING CRUISE AT FL 310, THE NR 2 ENGINE EGT SPIKED AND A LOUD THUD WAS HEARD FOLLOWED BY VIBRATION. SHUT DOWN ENGINE IN-FLIGHT. OP-16 - 2/16/97 - MCI. (X)Aug 5, 1997 · N909TW · Doug DC982 · Engine (Turbine/Turboprop)SDR CALA9700918Stator Suppt · brokenTHE TOWER REPORTED TO FLIGHT CREW THAT THEY SAW SPARKS COMING FROM NR 2 ENGINE AFTER TAKEOFF. ENGINE POWER WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEAJun 17, 1997 · N14831 · Doug DC982 · Compressor Bleed ControlSDR CALA9700821Starter · failedENGINE START WAS ABORTED AFTER PUSHBACK WHEN THE NR 2 ENGINE REACHED 500 DEGREES. THE NR 2 ENGINE COWLING WAS OPENED WHICH REVEALED AN UNCONTAINED STARTER FAILURE. THE STARTER HAD DAMAGED THE SECONDARY FUEL SUPPLY MANIFOLD. THE STARTER AND FUEL MANIFOLD WERJun 4, 1997 · N14880 · Doug DC981 · Engine StarterSDR CALA9700767Stator Suppt · brokenTHE NR 2 ENGINE SURGED WHILE AT CRUISE. THE ENGINE WAS BROUGHT BACK TO IDLE AND THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT ARRIVED WITHOUT FURTHER PROBLEM. THE NR 2 ENGINE WAS REMOVED AND REPLACED. AN ENGINE TRIM AND POWER RUN WAS PERFORMED AND ALL PARAMETERMay 23, 1997 · N93875 · Doug DC982 · Compressor Bleed ControlSDR CALA9700610Oil Presure Tube · crackedCREW NOTICE NR 1 ENGINE OIL PRESSURE DECREASING SHUTDOWN NR 1 ENGINE. INSPECTION FOUND CRACK TUBE TO OIL PRESSURE SWITCH. REPLACED TUBE (P/N 793814-501) LEAKED CHECK AND RETURNED TO SERVICE.Apr 26, 1997 · N72822 · Doug DC982 · Engine Oil PressureSDR TWAA9750004Oil Line · crackedORD - FLT 102 - DURING DESCENT NR 2 ENGINE, S/N 1412, INDICATED LOW OIL QTY. SHUT DOWN ENGINE. REMOVED AND REPLACED CRACKED OIL LINE, MFG P/N 7938314-501. OPERATIONAL CHECK NORMAL. (M)Apr 18, 1997 · N953U · Doug DC982 · Turbine Engine Oil SystemSDR CALA9700478Engine · failedTHE NR 1 ENGINE EPR WENT TO ZERO ACCOMPANIED BY A LOUD BANG AT 5,000 FEET WITH CLIMB POWER LEAVING EWR. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK AND OApr 3, 1997 · N13881 · Doug DC981 · Engine (Turbine/Turboprop)SDR AALA970074Wire Harness · out of positionORD - FLT 358 - AFTER TAKEOFF ORD, LANDING GEAR HANDLE BINDING HALF WAY UP AND UNABLE TO RETRACT LANDING GEAR. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPOSITIONED WIRE BUNDLE FOR FUEL HEAT INDICATION FOUND INTERFERIG WITH LANDING GEAR HANDLE. Jan 8, 1997 · N70401 · Doug DC982 · Engine Fuel System WiringSDR CALA9700008T3 Blade · failedTHE NR 1 ENGINE EXPERIENCED A TURBINE FAILURE AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. TEARDOWN REVEALED PRIMARY CAUSE OF ENGINEJan 3, 1997 · N72824 · Doug DC982 · Turbine SectionSDR CALA9601717Engine · fodTHE NR 1 ENG AUTO SHUTDOWN WHILE CRUISING AT 31,000 FT. THE A/C WAS DIVERTED TO PHX WHERE IT LANDED WITHOUT INCIDENT. INSPECTION FOUND ICE BUILD-UP IN FORWARD LAV PANEL. BLUE ICE WAS SUSPECTED AS CAUSE OF ENGINE FAILURE. THE 6TH, 7TH, 8TH AND 13TH STAGES OF NDec 1, 1996 · N71828 · Doug DC982 · Engine (Turbine/Turboprop)SDR CALA9601563Vane Cluster · failedTHE NR 1 ENGINE GAVE OFF A LOUD POP AND ART FIRED DURING CLIMBOUT AT 1,000 FEET. THE ENGINE EPR WAS AT 1.12 AND VIBRATION WAS STEADY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPNov 7, 1996 · N10834 · Doug DC982 · Engine (Turbine/Turboprop)SDR 97ZZZX106Lpt Shaft · distortedENGINE WAS REMOVED FROM SERVICE DUE TO VIBRATION. DISASSEMBLY OF THE ENGINE REVEALED THAT AN OIL FIRE HAD OCCURRED IN THE N2 COMPRESSOR CENTER TUBE CAUSING THE LPT SHAFT TO DISTORT AND RUB WHICH RESULTED IN ENGINE VIBRATION. THE FAILURE IS STILL UNDER INVESTNov 4, 1996 · Turbine SectionSDR 96ZZZX5733Blade · failedENGINE WAS REMOVED FROM SERVICE DUE TO LOST POWER, LOW SPEED AND TURBINE DAMAGE. THE ENGINE WAS DISASSEMBLED TO DETERMINE CAUSE OF THE TURBINE DAMAGE. ONE T4 BLADE HAD FRACTURED IN HIGH CYCLE FATIGUE CAUSING MASSIVE TURBINE DAMAGE. THE FAILURE IS STILL UNDEOct 11, 1996 · Turbine SectionSDR CALA9601342Oil Line · crackedTHE NR 2 ENGINE OIL QUANTITY BEGAN TO DROP WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LINE TO OIL PRESSURE TRANSMITTER CRACKED. THE LINE WAS REPLACED, THE ENGINE WAS RUN AND LEAK CHECK WAS GOOD.Sep 30, 1996 · N83870 · Doug DC982 · Engine Oil Distribution (Airframe Furnished)SDR 96ZZZM1468Engine · failedGJT - DURING CRUISE NR 1 ENGINE, S/N 1407, SPOOLED DOWN. AIRCRAFT DIVERTED TO GJT, FOR AN ENGINE CHANGE.Sep 27, 1996 · N953U · Doug DC982 · Engine (Turbine/Turboprop)SDR 97ZZZM105Engine · failedFLT 224 - GJT - DURING CRUISE, NR 1 ENGINE SPOOLED DOWN. AIRCRAFT DIVERTED TO GJT FOR AN ENGINE CHANGE. (M)Sep 27, 1996 · N953U · Doug DC982 · Engine (Turbine/Turboprop)SDR CALA9601276T4 Blade · failedTAKEOFF WAS ABORTED AT APPROXIMATELY 50 KNOTS AFTER THE NR 2 ENGINE LOST POWER. THE POWER LOSS WAS ACCOMPANIED BY A LOUD POP. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE FOUND THE NR 2 ENGINE TURBINE HAD FAILED. THE NR 2 ENGINE WAS REMOVED AND REPLASep 9, 1996 · N33817 · Doug DC982 · Turbine SectionSDR CALA9601269Stator Supp · brokenTHE NR 1 ENGINE GAVE A LOUD BANG AND SPOOLED DOWN SHORTLY AFTER TAKEOFF AT 1800 FEET. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED 8TH STAGE STATOR SUPPORT FAILURESep 7, 1996 · N18833 · Doug DC982 · Turbine Engine Compressor SectionSDR CALA9601297Engine · failedTHE TOWER REPORTED FIRE FROM THE NR 2 ENGINE TAILCONE AREA DURING TAXI OUT. THE CAPTAIN DISCHARGED BOTH ENGINE FIRE BOTTLES AND THE FIRE DEPARTMENT WAS SUMMONED. AN EMERGENCY EVACUATION WAS PERFORMED. THE FORWARD SERVICE DOOR AND AFT SERVICE DOOR ESCAPE SLISep 5, 1996 · N14889 · Doug DC982 · Engine (Turbine/Turboprop)SDR CALA9601189T4 Blade · brokenTHE NR 1 ENGINE FAILED WHILE EN ROUTE. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TAKEN OUT OF SERVICE FOR ENGINE REPLACEMENT. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGAug 17, 1996 · N10801 · Doug DC982 · Turbine SectionSDR CALA9601107Stator Suppt · brokenTHE NR 2 ENGINE BEGAN TO VIBRATE ACCOMPANIED BY AN ERRATIC EPR GAGE READING WHILE EN ROUTE. ENGINE POWER WAS REDUCED TO IDLE, ATTEMPTS TO OBTAIN MORE THAN 50 PERCENT POWER CAUSED EXCESSIVE VIBRATION. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT IJul 30, 1996 · N14816 · Doug DC982 · Compressor Bleed ControlSDR CALA9601083Duct · blownTHE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMB-OUT OF MIA. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE ANTI-ICE DUCT FROM NOSE COWL TO SAJul 29, 1996 · N35832 · Doug DC982 · Engine Anti-Icing SystemSDR 96ZZZX4037Vane · failedENGINE WAS REMOVED FROM SERVICE DUE TO A LOUD BANG AND ENGINE EXPERIENCED AN IN-FLIGHT SHUT DOWN. DISASSEMBLY OF THE ENGINE REVEALED A SECOND STAGE VANE CLUSTER WAS MISSING AND THE REMAINDER OF THE N1 TURBINE HAD MASSIVE DAMAGE. THE CAUSE FOR THE FAILURE IS Jul 25, 1996 · Turbine SectionSDR CALA9601051T3 Blade · brokenTHE NR 1 ENGINE FAILED WITH LOSS OF OIL WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO JAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 1 ENGINE TAILPIPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFOJul 23, 1996 · N16883 · Doug DC981 · Turbine SectionSDR CALA9601047Stator Suppt · brokenTHE NR 2 ENGINE COMPRESSOR BEGAN TO STALL AFTER TAKEOFF AT 13,000 FEET. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. INSPECTION BY MAINTENANCE FOUND DAMAGE TO THE NR 2 ENGINE 13TH STAGE COMPRESSOR. THE NR 2 ENGINE WAS REMOVED AND REPLAJul 22, 1996 · N937MC · Doug DC982 · Compressor Bleed ControlSDR 96ZZZM1219Turbine · failedOMA - DURING CRUISE NR 2 ENGINE, S/N 3225, WAS SHUTDOWN DUE TO TURBINE FAILURE. ENGINE TOTAL TIME 34,212, CYCLES 17,878.Jul 6, 1996 · N911TW · Doug DC982 · Turbine SectionSDR 96ZZZX4906Stator · failedOMA - FLT 114 - INVESTIGATION OF NR 2 ENGINE, S/N 3225, SHUTDOWN REVEALED AN 8TH STAGE COMPRESSOR STATOR, MFG P/N 789788, FRACTURED LIBERATING METAL PARTICLES INTO GAS PATH CAUSING MASSIVE HIGH PRESSURE COMPRESSOR AND TURBINE DAMAGE. ENGINE WAS REPAIRED AND RJul 6, 1996 · N911TW · Doug DC982 · Turbine Engine Compressor SectionSDR AALA961020Fuel Control · malfunctionedSFO - FLT 1308 - DURING CLIMB-OUT, RIGHT ENGINE SURGED TO 95 PERCENT N1 FOLLOWED BY FLAME OUT. ACCOMPLISHED ENGINE SHUTDOWN PROCEDURES AND AIRCRAFT DIVERTED TO SFO, LANDING WITHOUT INCIDENT. CHECKED RIGHT ENGINE INLET AND EXHAUST WITH NO DAMAGE OR DEFECTS FJul 6, 1996 · N248AA · Doug DC982 · Fuel Control/Turbine EnginesSDR CALA9600857Stator Vane · failedTHE NR 1 ENGINE COMPRESSOR STALLED AT 37,000 FEET WHEN POWER WAS REDUCED FOR DESCENT. THE STALL WAS ACCOMPANIED BY TWO BANGS AND SUBSEQUENT YAW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PAJun 21, 1996 · N14816 · Doug DC982 · Compressor Bleed Control
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