Pratt & Whitney PW2040

Service difficulty reports · 2,201

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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 = 'PW2040'
  ORDER BY difficulty_date DESC"

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SDR UPS07550357Skin · gougedINSPECTION TYPE: C VERT STAB. UPPER MOST AFT PANEL SKIN GOUGED AS SEEN THRU PANEL 324EL. ACCOMPLISHED REPAIR AT VERT. STAB IAW EA NR 757-5530-27-A1720 AND UPS EO NR 57-55-20030.Jul 22, 2007 · N401UP · Boeing 75724APF · Vertical Stabilizer, Plate/SkinSDR UPS07550356Skin · bulgedINSPECTION TYPE: C LWR EXT FUSELAGE SKIN BULGING APPROX BSTA 563 BETWEEN S24L S25L. REMOVED FAST AT AFFECTED AREA COMMON TO REPAIR IAW SRM 51-40-02 AND CUT OUT DAMAGED SECTION L 2.8 INCH X W 2.4 INCH IAW SRM 53-00-01-2R3. HFEC INSPECTED CUTOUT IAW NTM 51-00-0Jul 19, 2007 · N401UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR UPS07550352Structure · damagedN/A NR 2 LEADING EDGE SLAT HAS VARIOUS DENTS FROM HAIL DAMAGE. NR 2 SLAT HAS 98 DENTS FROM HAIL DAMAGE. DENTS GREATER THAN .010 INCH ARE DOCUMENTED IN FIG 1 EO B757-5750-27018-A. 10-8-07 ACCOMPLISHED REMOVAL OF NR 1 L/E SLAT UP THROUGH STEP D14 OF MM 27-Jul 3, 2007 · N421UP · Boeing 75724APF · Leading Edge DevicesSDR UPS07549642Engine · bird strikeINSPECTION TYPE:N/A ENGINE PNEUMATICS PRODUCING A BURNT SMELL IN COCKPIT. WHEN TAI IS ACTIVATED SMELL GETS STRONGER. ODOR IS UNUSUAL APU PNEUMATICS DOES NOT PRODUCE THE ODOR. FOUND EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. PERFORMED BIRD STRIKE INSPECTION PEApr 19, 2007 · N413UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR XXUA200701037Oven · inoperativeOVEN NR 2 AFT INOPERATIVE (CB PULLED AND COLLARED AFTER SEVERE SMOKE) SPILLAGE NOTED. REPLACED OVEN IAW MM 25-31-00, OPS CHECKS NORMAL.Feb 21, 2007 · N401JS · Boeing 7572Q8 · Buffet/GalleysSDR ASMF200701008Blade · bentDURING TRANSIT CHECK, A BLADE WAS DETECTED DAMAGED DUE TO A FOD IN RT ENGINE. 3 BENDS WERE DETECTED AT 2 INCHES FROM BLADE LEADING EDGE TO MIDSPAN SHROUD, ONE OF 1.2500 INCH, OTHER OF 1.1250 INCH AND THE LAST ONE OF .8750 INCH. (2) BLADES SETS OF FAN STAGE WJan 31, 2007 · N703AM · Boeing 757200 · Engine (Turbine/Turboprop)SDR UPS06548247Skin Panel · damagedINSPECTION TYPE: DROP AFT FUSELAGE LWR SKIN DENTS BETWEEN STA 1589 AND 1614 REQUIRE REPAIR EA 757-5361-27-A14566. REPAIRS ACCOMPLISHED EA NR 757-5361-27-A14566 AND UPS EO NR B757-5330-25350-A, WITH NO DEVIATIONS.Oct 12, 2006 · N435UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR UPS06548246Skin Panel · damagedINSPECTION TYPE: DROP FUSELAGE DAMAGED AT BS 1500 TO 1540, S25R - 26R DUE TO CONTACT WITH GROUND EQUIPMENT. FUSELAGE REPAIR ACCOMPLISHED IAW EA NR 757-5361-27-A1558, AND UPS EO NR B757-5330-253479-A, WITH NO DEVIATIONS.Oct 7, 2006 · N435UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR XXUA200609030Indicator · inoperativeCAPT AIRSPEED INDICATOR SPEED POINTER SHOWED ZERO AT 80 KNOTS. ACCOMPLISHED HIGH SPEED ENERGY STOP IAW MM CHAP. 5-51-14 WITH NO FINDINGS AND ISSUED A DEFERRAL IAW MEL 34-13-1 AND DEPARTED. REPLACED CAPT AIRSPEED INDICATOR IAW 34-13-02, OPS CHECKS NORMAL. MEL Sep 19, 2006 · N401JS · Boeing 7572Q8 · Airspeed/Mach IndicatorSDR UPS06547988Frame · dentedINSPECTION TYPE-C DENT IN AFT CARGO FUSELAGE FRAME STA. 1580, BET S25L TO S26L REPAIR ACCOMPLISHED IAW EA 757-5367-27-A1525 AND UPS E.O. NR B757-5310-2 5093-A. NO DEVIATIONS NOTED.Aug 29, 2006 · N423UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547449Frame · dentedINSPECTION TYPE: C FRAME STA 1681 RT UPPER FRAME DENTED, (2) SHEAR CLIPS (15R AND 16R) DAMAGED. REPAIRED DAMAGED FRAME IAW EA 757-5362-27-A1499 NR UPS EO B757 5310-24769-A. ACCOMPLISHMENT FOR REPAIRS HAS BEEN DOCUMENTED ON ECA NR 115492.Jul 3, 2006 · N429UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS06547173Nose Bullet · contaminatedINSPECTION TYPE:N/A STRONG BAD ODOR FROM PACKS SUSPECT LT PACK. INSPECTED AND CLEANED BUGS OFF LT AND RT ENGINE SPINNERS. RAN ENGINES AND PACKS. ALL CHECKS NORMAL OK FOR CONTINUED SERVICE PER 21-00-01-2.Jun 22, 2006 · N409UP · Boeing 75724APF · Turbine Engine Air Inlet SectionSDR UPS06547440Frame · gougedNR 1 ENGINE FAN AFT FRAME HAS SEVERAL GOUGES 10:00 AND 12:00 O'CLOCK POSITION. ACCOMPLISHED EA 757-7231-27-A1493 IAW UPS EO 2040-7200-24717-A.Jun 20, 2006 · N429UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR UPS06546487Engine · damagedRUBBER SMELL IN COCKPIT ON LANDING FROM RIGHT PACK. POSSIBLE FOD INGESTION. A/C IS OOS ENGINE CHANGE IS RECOMMENDED. R/R RT ENG PER AMM 71-00-02-4 & TC 5001. ACP ENG TEST PER TC 5002. OPS CK GOOD. S/N ON 727122.Mar 21, 2006 · N405UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR DU4R0508184Floorbeam · damagedFLOORBEAM AT BS 480 HAS SEVERAL ELONGATED HOLES FORM OB SEAT TRACK TO CREASEBEAM.Aug 24, 2005 · N672DL · Boeing 757232 · Fuselage Main, Floor BeamSDR 0401735801Line · chafedTHE FUEL SUPPLY TUBE IN THE RT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED IAW EO 2822-01068-01. OPERATIONAL CHESep 27, 2004 · N581NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR 0401765814Fuel Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONASep 26, 2004 · N594NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR 0401755810Fuel Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONASep 25, 2004 · N590NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR 0401745813Line · chafedTHE FUEL SUPPLY TUBE IN THE RT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED IAW EO 2822-01068-01. OPERATIONAL CHESep 25, 2004 · N593NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR 0401615807Fuel Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200472. OPERATIONAL CHESep 20, 2004 · N587NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR 0401625804Fuel Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200233. OPERATIONAL CHSep 20, 2004 · N584NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR 0401635806Fuel Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-199805. OPERATIONAL CHSep 20, 2004 · N586NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR 0401565816Fuel Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200234. OPERATIONAL CHSep 19, 2004 · N596NW · Boeing 757351 · Aircraft Fuel Distribution SystemSDR UPS04543126Hinge · brokenMCD HINGE FWD AND AFT WORN FIFTH FROM FWD HINGE HAS THREE BROKEN HINGES. ACCOMPLISHED EO B757-5230-17511-B, APPENDIX A, REQUIRES DEFERRAL D287700 WAITING FOR NRC 431008. VISUALLY CHECKED ALL MCD PIANO HINGES ALL OTHER PIANO HINGES ARE IN SERVICEABLE CONDITSep 14, 2004 · N425UP · Boeing 75724APF · Cargo/Baggage DoorsSDR UPS04543127Door · inoperativeMAIN CARGO DOOR WILL NOT CLOSE. COMPLY WITH DMP 52-32-1, REPLACED ARM SWICH IN P 81 PANEL IAW MM 52-32-13-4. OPS CHECK GOOD.Sep 14, 2004 · N422UP · Boeing 75724APF · Cargo/Baggage DoorsSDR 0401325803Line · crackedIN CRUISE AT FL 37,000 FT RECEIVED R HYD SYS PRESS AND R HYD SYS QTY MESSAGES. QUANTITY SHOWED ZERO IN RT SYSTEM. DECISION WAS MADE TO DIVERT TO DTW. LANDING UNEVENTFUL, MAINTENANCE FOUND THE RETURN LINE FROM THE RT (ALTERNATING CURRENT MOTOR PUMP (ACMP) CRACKAug 12, 2004 · N583NW · Boeing 757351 · Hydraulic System, MainSDR UPS04542786Tailpipe · fireDURING LT ENG START MX EXPERIENCED TAIL PIPE FIRE. REPLACED NR 1 FUEL CONTROL PER AMM 73-21-01. REPAIRED OUTBOARD FLAP TRACK FAIRING PER SRM 51-70-05. REPLACED NR 5 SPOILER, WIRE BUNDLES W3315 & W3319. REPAIRED AND REPLACED LT WING T/E PANELS, FLAPS, FLAP Jul 27, 2004 · N405UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR UPS04542419Oil System · overservicedINSPECTION TYPE:N/A ATB - APU FAILED IN FLT W/RT ENG GEN ON MEL. FOUND OIL OVER SERVICED. NO FAULTS FOUND ON APU CONTROLLER GROUND. RAN APU A/C OK FOR SERVICE.May 23, 2004 · N414UP · Boeing 75724APF · APU Oil SystemSDR UPS04541697Fire Warning · false indicationAT 3000 FEET ON APP INTO SAT WE RECEIVED A MASTER WARNING AND CARGO FIRE BELL WITH ICAS MESSAGE. IT WENT OUT ABOUT A SECOND LATER, T/S IAW FIM 26-16-00 SHEETS 1-9 SYS. OPS CKS OK, OK FOR SERVICE.Jan 8, 2004 · N411UP · Boeing 75724APF · Fire DetectionSDR UPS03540407Compressor · stalledLOUD BANG AND HARD YAW TO LT ON TO AT 700 FT AGL. RETURNED TO DFW. BOROSCOPED N2 HIGH COMPRESSOR, NO DEFECTS NOTED. C/W CHECK 4 SVA INSP, NO DEFECTS NOTED. C/W ENG CK 6 14TH STG BLEED SYS. A/C OKAY FOR SERVICE.Apr 3, 2003 · N418UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR UPS03540312Compressor · stalledAT FIRST POWER REDUCTION AFTER TAKEOFF LEFT ENGINE COMPRESS OR STALL OBSERVED. GROUND OBSERVERS NOTED FLAME SMOKE FOR 1 SECOND DURING HOLDING PATTERN, WITH EPR AT 1.25, LEFT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 125 & 165 PSI AND VIB. COMPLIED WITH FIM 71-0Mar 19, 2003 · N418UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR 2002UALA01852Floorbeam · corrodedSTATION 1640, RBL 57 FLOORBEAM UPPER CAP CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED.Dec 13, 2002 · N552UA · Boeing 757222 · Fuselage Main, Floor BeamSDR UPS02539824Engine · overtempRT ENGINE TEMP CLIMBED TO 944 +. ENGINE WAS SHUT DOWN AND ONE FIRE BOTTLE WAS BLOWN. T/S PER FIM 71-05-00 FIG 110- REPLACED W-31 EGT HARNESS - PERFORMED EGT CABLE & THERMOCOUPLE TEST, CHECKED OK PER MM77-21-03-5.SEI 6 LOW COMPARED TO EICAS. W31 HARNESS. ENOct 30, 2002 · Boeing 75724APF · Powerplant SystemSDR UPS02537808Actuator · leakingINSPECTION TYPE:N/A UPON LANDING AT OMA CABIN SMOKE WHEN REVERSE INITIATED (NOTE: ONLY RT PACK ON DURING LANDING). INSPECTED A/C FOR LEAKS. FOUND UPPER I/B TR ACT LEAKING REPLACED RT UPPER I/B ACTUATOR. RAN PACK, OPS CHECKS NORMAL.Mar 9, 2002 · N416UP · Boeing 75724APF · Engine Thrust ReverserSDR UPS01536933Compressor · stalledLT ENGINE SHUTDOWN DUE TO COMPRESSOR STALLS, A/C DIVERTED TO BIL. R AND R NR 1 ENGINE PER TASK CARD 5001 PW OK FOR SERVICESep 28, 2001 · N432UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR UPS00533567Engine · stalledINSPECTION TYPE:N/A, RIGHT ENGINE SURGED DURING CONSTANT POWER AT 27,000 ENG SHUTDOWN. RPM WAS NORMAL. ENG CONTINUED TO COMPRESSOR STALL AT IDLE RPM. EGT CONTINUED TO RISE. EMERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT AT RFD. *S/D* PULLED OIL SCREAug 15, 2000 · N420UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR UPS00533242Selector Valve · inoperativeAFTER RIGHT ENGINE START, GOT STATUS MESSAGE SHOWING RT ENG SEC CONTROL. MECHANIC DIRECTED TOGGLING FROM NEUTRAL TO SEC TO AUTO ON CHANNEL SELECTOR. ON DOING THIS THE ENGINE QUIT. THE MECHANIC REPORTED THE ENGINE WAS ON FIRE. SELECTED CUTOFF ON FUEL CONTROL AJul 7, 2000 · N422UP · Boeing 75724APF · Fuel Controlling SystemSDR UPS00532149Engine · malfunctionedATB TO MEM, ON CLIMBOUT, LT ENGINE OVERHEAT MASTER CAUTION ILLUMINATED, FOLLOWED QRH PROCEDURE AND SHUT DOWN LT ENGINE. RETURNED TO MEM. PERFORMED BITE CHECK IAW FIM 26-11-00 TO BLK 113 PG 109. PERFORMED LOOP DETECTOR RESISTANCE CK IAW FIM 26-11-00 PMar 31, 2000 · N432UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR UPS00531688Switch · failedHAD L OIL FILTER STATUS MSG. SHUT ENG DOWN. SYSTEM CHECKED IAW FIM 79-21-00, FIG 104, CHECKED CHIP DETECTORS. REPLACED OIL FILTER, REPLACED DIFF PRESSURE SWITCH IAW MM 79-35-01, CHECKED CIRCUIT BETWEEN SWITCH AND EICAS COMPUTER CONNECTOR. RUN ENGINE TEST 3Feb 16, 2000 · N420UP · Boeing 75724APF · Engine Oil PressureSDR UPS00531257Engine · leakingRUBBER SMELL FROM LT PACK ON TAKEOFF AFTER GEAR WAS RETRACTED AND LEFT PACK SELECTED OFF SMELL WENT AWAY. TAKEOFF PWR REQUIRED FOR SMELL. NO SMELL NOTICED ON TAXI. REPLACED LEFT ENGINE PER TC 5001 (RR), 5002 (RR) OPS CHECKS NORMAL.Jan 4, 2000 · N443UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR UPS00531252Valve · inoperativeAFTER T/O A RUMBLE NOISE IN THE RIGHT PACK. SWITHCHED TO LEFT PACK. LATER IN FLIGHT RESELECTED RIGHT PACK AND WENT UNCONTROLLABLE (TEMP) AND SMELLED SMOKE IN COCKPIT. REPLACED FLOW CONTROL VALVE PER MM 21-51-01. OPS, LEAK AND BITE TEST NORMAL. CLEARED M18Jan 3, 2000 · N429UP · Boeing 75724APF · Cabin Cooling SystemSDR 99ZZZX4009Carbon Seal · failedTEAR DOWN INSPECTION REVEALED NR 2 CARBON SEAL FRACTURED APPROXIMATELY .250 INCH WIDE BY 2.300 INCHES LONG AND FAILED SECTION ADHERED TO SEAL PLATE FACE. LOCKING TABS OF 6TH DISK TIE RODS LIBERATED, POSSIBLE FRACTURE CAUSE. P & W ENGINEERING E.H., IS CONDUCTOct 7, 1999 · N426UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR 99ZZZX2066Shaft · crackedSUBJECT ENGINE RECEIVED FOR MAINTENANCE DUE TO PERFORMANCE DETERIORATION. INSPECTION OF SHAFT THREADS BY ULTRASONIC MEANS IAW SB 72-510 REVEALED CRACK INDICATIONS. CRACK CONFIRMED BY P&W AS BEING INTERMITTENT 2 INCH CRACK TYPICAL OF THE TYPE ADDRESSED BY THEApr 13, 1999 · Turbine Engine Compressor SectionSDR UPS98525378Elect Eng Cntrl · failedINSPECTION TYPE-N/A ON SHORT FINAL, RT ENG FAILED. EPR REMAINED AT 1.0. N1 AND N2 WERE FROZEN, EGT 450C, AT ALL THRUST LEVER SETTINGS. ENG WAS NOT SHUT DOWN. ENG WENT TO FAIL-SAFE FLT IDLE POSITON. ENG RUN ON PRI AND SEC CHANNEL IN LGB WAS NORMAL. EEC WAJan 5, 1998 · N418UP · Boeing 75724APF · Fuel Control/Turbine EnginesSDR UPS97523974Computer · malfunctionedINSPECTION TYPE-N/A, LT ENG IFSD DUE TO OIL PRESS LOW. *S/D* REMOVED AND REPLACED LEFT EICAS COMPUTER PER MM 31-41-02 (P/N 622-6540-111) (S/N 1350) OFF, (S/N 3342) ON. OPS CHECK GOOD, BITE CHECKS GOOD.Jul 29, 1997 · N423UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR UPS97522371Engine · failedINSPECTION TYPE-N/A, AIR TURNBACK DUE TO SMOKE IN COCKPIT AND MAIN CARGO FIRE WARNING. LEFT ENGINE LOST 8 QTS IN 16 MIN OF FLIGHT AND 45 MIN OF BLOCK TIME. CLIMBING THROUGH 12,000 FT MAIN CARGO FIRE WARNING CAME ON AND SMOKE ENTERED COCKPIT. ACCOMPLISHED CHMar 13, 1997 · N406UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR 97ZZZX1059Stator Vane · failedENGINE WAS IN-FLIGHT, SHUT DOWN. DISASSEMBLY INSPECTION REVEALED ONE LIBERATED 10TH STAGE STATOR VANE AT THE CONVEX END OF ONE QUADRANT AT 9:00. THREE ADDITIONAL VANES IN THE SAME CLUSTER OF FIVE ARE FRACTURED THROUGH AT THE OUTSIDE DIAMETER SHROUD VANE BRAZFeb 18, 1997 · Boeing 757* · Turbine Engine Compressor SectionSDR UPS96521199Engine · high oil consmptACID SMELL IN COCKPIT IN-FLIGHT. SAME INTENSITY NOTICED WITH EITHER ACM OPERATING. ENG ANTI-ICE WAS USED FOR SHORT DURATION. DID NOT NOTICE SMELL ON GROUND WITH ACM'S RUNNING WITH BLEED SOURCE. BURNS EYES AND THROATS. NR 2 ENG REQUIRES CHANGING DUE TO HIGSep 30, 1996 · N428UP · Boeing 75724APF · Turbine Engine Oil SystemSDR UPS505225Engine · flame-outCREW REPORTED, RT ENGINE FLAMED-OUT ON APPROACH. REMOVED AND REPLACED RT ENGINE.Jan 18, 1996 · N434UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR 96ZZZX653Stator Vanes · crackedMDW - LEFT ENGINE SURGE DURING DECELERATION. ENGINE PARAMETERS NORMAL AFTER SURGE. REMOVED AND REPLACED LEFT ENGINE. FOUND CRACKED STATOR VANES.Oct 14, 1995 · N756AT · Boeing 7572Q8 · Compressor Bleed Control
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