Pratt & Whitney JT9D-7J

Service difficulty reports · 257

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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 = 'JT9D7J'
  ORDER BY difficulty_date DESC"

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SDR EIA2005262Csd · failedPERFORMED INFLIGHT ENGINE SHUTDOWN DUE TO FAILURE OF NR 1 CSD TO DISCONNECT. FL 290, TAT -17, SAT -47, 312 KTS, .81 MACH, 11:08Z OIL PRESS 20 PSI, OIL TEMP 78 DEG C, DURATION 2:08. PMG VOLTS 52, N1 30 PERCENT, CSD RPM 520, N2 27 PERCENT. DFRL DMI 572 PER MEDec 18, 2005 · N482EV · Boeing 747212B · Alternator-Generator DriveSDR EIA2005259Engine · failedDURING CLIMB-OUT AT 5,000 FT AGL, NR 3 ENG EMITTED A BIG BANG AND STALLED. CAUSE OF DAMAGE UNDETERMINED. REMOVED AND REPLACED ENGINE PER WORK CARD F7201-7204 AND 7207.Dec 11, 2005 · N485EV · Boeing 747212B · Engine (Turbine/Turboprop)SDR WRNA20050028Fuse · blownTAKEOFF WARNING WENT OFF AT 140 KTS. ABORTED TAKEOFF. NR1,3,5,6, AND 7 MLG WHEEL ASSY'S THERMAL FUSE PLUG DISCHARGED AFTER RETURNING TO GATE. FREIGHT REMOVED FROM AIRCRAFT. PERFORMED TAKEOFF WARNING SYSTEM CHECK IAW 31-26-00 PGS 101 AND 501. SYSTEM OPS NORMALDec 1, 2005 · N524UP · Boeing 747200 · Wheel/Ski/FloatSDR WRNA200050026Cowling · missingUPON LANDING AT SKBO, POST FLIGHT REVEALED THAT NR 1 ENGINE REVERSER COWLING MISSING.Nov 5, 2005 · N524UP · Boeing 747200 · Engine Thrust ReverserSDR EIA2005152Controller · malfunctionedNR 3 ENGINE ON DESCENT FL 350 WOULD NOT RESPOND TO PUSH-UP. RESTART REQUIRED ALL PAREMETERS WERE NORMAL RESTART OK. NR 3 EVC REPLACED AND TRIMMED PER MMS 71-00-00 AND 75-31-01 RESPONCE NORMAL.Aug 23, 2005 · N486EV · Boeing 747212B · Compressor Bleed ControlSDR EIA2005132Engine · failedFL 340 IN CRUISE, NO TURBULENCE LOUD BANG WITH YAW TO RIGHT ENG NR 4 N1, N2 EGT PARAMETERS INDICATION EXCEEDENCES (RED) ENGINE FLAMED OUT. SECURED ENG. NO FIRE WARNING. METAL IN TAILPIPE REMOVED AND REPLACED NR 4 ENGINE IAW F7201/9724001.Jun 30, 2005 · N471EV · Boeing 747273C · Engine (Turbine/Turboprop)SDR 05039Wire · damagedDURING DESCENT B-LOOP ON NR 3 NACELLE WENT FIRE INDICATION WITH A-INOP. PRECAUTIONARY SHUTDOWN NR 3 ENG. REPAIRED DAMAGED WIRE ON UPPER LOOP BELOW PYLON CLOSE TO CANNON PLUG AND SECURED LOOSE LOOP ASSY AT UPPER I/B BRACKET IAW B747 MM 26-11-02 AND OPS CHECKEMay 7, 2005 · N713CK · Boeing 7472B4B · Fire Protection System WiringSDR WRNA200500001Cap · looseON CLIMB-OUT FROM MIA, NR 1 OIL QTY STARTED TO DECREASE RAPIDLY. DID A PRECAUTIONARY ENG SHUTDOWN OF NR 1 ENGINE FOR OIL QTY LOSS. RETURNED TO AIRFIELD, LANDING NORMAL. MAINTENANCE INSPECTED NR 1 ENG AND FOUND OIL TANK CAP NOT IN CLOSE POSITION. SERVICED EFeb 20, 2005 · N524UP · Boeing 747200 · Turbine Engine Oil SystemSDR 05010Duct · looseAT FL 34.0, NR 2 ENG START VALVE LIGHT ILLUMINATED; FOLLOWED CHECKLIST. NR 2 THROTTLE SEIZED; RAN SEVERE DAMAGE CHECKLIST. ALL ENGINE INDICATIONS NORMAL. PERFORMED VISUAL INSPECTION TO ENGINE. FOUND 8TH STAGE BLEED DUCTS LOOSE AND START VALVE DAMAGED. INSFeb 4, 2005 · N713CK · Boeing 7472B4B · Pneumatic SystemSDR 05007Compressor · stalledNR 2 ENGINE COMPRESSOR STALL AT 31,500 FT AND AGAIN AT FL350. ENGINE SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE. PERFORMED TEST NUMBERS 3, 6, 8, 9, 11, 12, AND 16. TRIM RUNS PERFORMED. OPS AND LEAK CHECK GOOD AND FINAL PARAMETERS RECORDED. ALL WORK PERFOJan 24, 2005 · N710CK · Boeing 7472B4B · Turbine Engine Compressor SectionSDR 05003Gearbox · damagedNR 4 ENG SLOW/STEADY OIL LEAK FROM 5.6 GALS DOWN TO 0.6 GALS. OIL TEMP CONSTANT AT 75 TO 79C AND OIL PRESS STEADY AT 47 TO 49 PSI. ACCOMPLISHED PRECAUTIONARY ENG SHUTDOWN IAW AOM VOL I, LOW OIL QTY PG 3-109, IN FLT ENG SHUTDOWN PG 3-97 AND WINDMILLING ENG PRJan 7, 2005 · N710CK · Boeing 7472B4B · Turbine Engine Reduction GearSDR EIA2004136Engine · failedEN ROUTE FRA/HKG, CRUISE CONFIGURATION AT FLT LEVEL 37K, CREW NOTICED MOMENTARY VIBRATION/RUMBLE, AND OBSERVED LOSS OF NR 2 ENGINE POWER (ROLL BACK). ENGINE INSTRUMENTS AT IDLE VALUES WITH N1 RPM ZERO. REPEATED THROTTLE CYCLING PRODUCED NO ENGINE RESPONSE. PNov 5, 2004 · N482EV · Boeing 747212B · Engine (Turbine/Turboprop)SDR EIA2004132Strap · corrodedUPPER DECK FLOORBEAM STRAP HAS EXFOLIATION CORROSION, STA 420R, 3 INCHES IB FUSELAGE SKIN. REPLACED STRAP IAW SRM 51-30-02, PGS 8-9, 51-30-05, FIG 4, AND 51-30-02, PGS 8-9Oct 16, 2004 · N470EV · Boeing 747273C · Fuselage Main, Floor BeamSDR EIA2004135Web · cracked1.1 INCH CRACK ON NOSE WHEEL WELL BOX WEB, STA. 340, RBL 15, WL 150. REMOVED DAMAGED WEB, FABBED AND INSTALLED REPLACEMENT PARTS IAW ECRA 470-53-207-2Oct 7, 2004 · N470EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR 0401436718Engine · fireDURING TAXI IN, THE NR 2 ENGINE FIRE WARNING ANNUNCIATED. THE CREW SHUT DOWN THE ENGINE AND DISCHARGED THE LT FIRE BOTTLE FOR NR 2 ENGINE. THE FIRE WARNING CEASED. NO OTHER ABNORMAL ENGINE INDICATIONS WERE OBSERVED. MAINTENANCE INSPECTION FOUND EVIDENCE OF A Aug 24, 2004 · N618US · Boeing 747251F · Engine (Turbine/Turboprop)SDR EIA2004092Splice · crackedSTA 520, STR 12R, STRINGER SPLICE FOUND CRACKED ON REMOVAL. REMOVED CRACKED SPLICE, LOCATED, DRILLED AND INSTALLED NEW SPLICE IAW SRM 51-30-02, PGS 2-3 AND 8-9.Jul 15, 2004 · N470EV · Boeing 747273C · Fuselage Miscellaneous StructureSDR EIA20041130Pressure Panel · delaminatedMAIN CABIN STA 1380, RBL 75.9, PRESSURE DECK WEB SHOWS EVIDENCE OF DELAMINATION. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR IAW SRM 51-10-07, FIG 251-30-05 PGS 6-9, AND 51-30-02.Jun 16, 2004 · N470EV · Boeing 747273C · Fuselage Main, BulkheadSDR EIA2004014Engine · flamed outCLIMBING THROUGH 38500 FT NR 4 ENGINE FLAMED OUT. INFLIGHT RESTART NORMAL. INSPECTED INTAKE AND EXHAUST NO DEFECTS NOTED INSPECTED BLEED SCREENS NO FOREIGN OBJECTS NO DEFECTS. REPLACED MAIN FUEL FILTERS, SUMPED NR 4 FUEL DRAIN NO WATER FOUND. FUEL PUMP PRESSMar 28, 2004 · N482EV · Boeing 747212B · Engine (Turbine/Turboprop)SDR P5CA0300982Connector · dirtyON PUSHBACK NR 3 ENG FUEL FLOW RESPONDED ERRATICALLY. CLEANED CONNECTOR ON FUEL FLOW TRANSMITTER, OPS NORMAL ON RELIABILITY CHECK PER MM 73-00-00.Nov 7, 2003 · N524UP · Boeing 747200 · Fuel Flow SensorSDR EIA2003147Hose · failedNR 1 ENGINE OIL QUANTITY DECREASED RAPIDLY ON CLIMB OUT FROM EROS. REDUCED NR 1 ENGINE TO IDLE AND DECREASED LESSEND , PERFORMED FUEL JETTISON AND RETURNED TO EROS. CORRECTIVE ACTION SECURED CLAMP MID POSITION NR 4 BEARING SCAVENGE LINE RETORQUED MID (B) NUT Oct 26, 2003 · N482EV · Boeing 747212B · Engine Oil QuantitySDR P5CA0300969Engine · stalledNR 4 ENGINE STALLED AT FL 310, GOING TO 340. INSPECTED INLET/EXHAUST GAS PATH IAW 72-00-00. NO DEFECTS NOTED. REPLACED ENGINE M7100-002.Oct 26, 2003 · N524UP · Boeing 747200 · Engine (Turbine/Turboprop)SDR EIA2003108Engine · vibrationAT 200 MILES FROM ZURICH FL 400 AT 1/2 THROTTLE NOTICED SHUDDER AND STALL. FUEL OFF THEN ON EGT DROP BUT NO RELIGHT SHUTDOWN CHECKLIST C/W. RAN INFLIGHT ENG START CHECK LIST RELIGHT BUT ENG SHAKING INCREASED TOWARD IDLE. SHUT ENG DOWN AND INFLIGHT SECURING Aug 9, 2003 · N485EV · Boeing 747212B · Engine (Turbine/Turboprop)SDR EIA2003093Engine · stalledAT CRUISE ALTITUDE FL 320 NOTICED NR 1 ENG EPR DROP TO .25 LOWER THAN THE OTHERS. ALL OTHER READINGS AND INDICATIONS WERE NORMAL. WHEN ADJUSTING THRUST LEVER, ENGINE COMPRESSOR STALLED MULTIPLE TIMES, SHUT DOWN ENGINE. AFTER SHUTDOWN OIL PRESS 29 PSI, N1 29Jul 10, 2003 · N486EV · Boeing 747212B · Engine (Turbine/Turboprop)SDR P5CA0300899Engine · malfunctionedAT FL 39.0 NR 4 ENGINE WOULD NOT MAINTAIN POWER AND SLOW RESPOND. ENGINE REPLACED FOR COMPANY CONVENIENCEJul 9, 2003 · N524UP · Boeing 747200 · Engine (Turbine/Turboprop)SDR EIA2003090Line · brokenENGINE NR 1 FIRE LIGHT ILLUMINATED DISCHARGED BOTH FIRE BOTTLES. EGT RED BALL AND NACELLE INDICATES IN RED ZONE SHUT DOWN ENG DUMPED FUEL LANDED JFK. NTSB NOTIFIED. INVESTIGATION IN PROGRESS. NR 4 BEARING OIL PRESSURE LINE BROKE EARLY INDICATION OF CAUSE.Jun 25, 2003 · N471EV · Boeing 747273C · Turbine Engine Oil SystemSDR P5CA0300877Line · leakingDURING CRUISE NR 1 ENG OIL QTY SLOWLY PROGRESSED TOWARD ZERO, LOW OIL PRESS LIGHT ILLUM. FOUND OIL LEAKING FROM NR 1 ENG GEN TRANSFER TUBE PER MM 24-11-00 GEN & CSD REMOVED FOR FLT P/N 2MIT60B00010 KIT INSTALLED PERFORMED ENG RUN - NO LEAKS NOTICED. OIL LEAKIMay 14, 2003 · N524UP · Boeing 747237B · Engine Oil Distribution (Airframe Furnished)SDR EIA2003075Engine · malfunctionedNR 4 ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE, AFTER SHUTDOWN ENGINE WINDMILLED FOR 20 MINUTES. REMOVED AND REPLACED NR 4 ENGINE PER WORKCARD F7201, F7202, F7203 AND F7207, OPS CHECK GOOD.May 14, 2003 · N486EV · Boeing 747212B · Turbine Engine Oil SystemSDR P5CA0300874Compressor · stalledAT FL 330 NR 3 ENG COMPRESSOR STALLED. EPR WENT FROM 1.45 - 1.56 WITH 120 DEGREES RISE IN TEMP. INSP INLET AND EXHAUST (2) PERFORMED CHIP DETECTOR INSP (3) PERFORMED BORESCOPE INSPECTION. NO DEFECTS NOTED (4) REPLACED TT2 SENSOR PRECAUTIONARY. AMM 73-21-04Apr 30, 2003 · N524UP · Boeing 747200 · Turbine Engine Compressor SectionSDR 03010Engine · vibrationDURING T/O ROLL NR 3 ENGINE HAD VIBRATION AND LOUD NOISE. AIRBORNE VISUAL INSPECTION REVEALED DAMAGE TO ENGINE. DUMPED FUEL AND RETURNED TO BASE.Mar 9, 2003 · N713CK · Boeing 7472B4B · Powerplant SystemSDR P5CA0300772Compressor · stalledAT FLT LEVEL 19.0 WHEN THRUST LEVER WAS RETARDED NR 3 ENG COMPRESSOR STALLED. REMOVED AND REPLACED FLOW DIVIDER AND SECURE PT 2 LINE. OPERATIONAL CHECK OK ON ENGINE RUN UP. APPARENT FAILURE OF ENG BLEED SYSTEM ON DESCENT WHEN THROTTLE WAS RETARDED.Mar 4, 2003 · N524UP · Boeing 747200 · Compressor Bleed ValveSDR P5CA0200701Garlock Seal · leakingUSED 2 GALLONS OF ENG OIL ON NR 2 ENG IN 3.7 HOURS OF FLT. QTY LOSS TO 0.1 GALLONS INDICATED. NR 2 ENG OIL SYSTEM STATIC LEAK CHECKED IN HKG. TEST NR 6 CARRIED IAW AMM 71-00-00. FOUND GENERATOR DRIVE CARBON GARLOCK SEAL LEAKING. SEAL CHANGED IAW AMM 72-61Oct 6, 2002 · N524UP · Boeing 747200 · Turbine Engine Oil SystemSDR P5CA0200700Oil System · malfunctionedPRECAUTIONARY ENGINE SHUTDOWN OCCURRED AT 2250 DUE TO NR 2 OIL QTY DECREASED TO 0.1 GAL. INDICATED, FOLLOWED BY SLOW DECREASE IN OIL PRESSURE ALT PROCEDURES 6-15-9 & 6-15-11 C/W & ENGINE SECURED IAW 5-04-9. FL 390 FUEL APPROX 78.0. DISPATCH NOTIFIED, PROCEOct 5, 2002 · N524UP · Boeing 747200 · Turbine Engine Oil SystemSDR 0202406717Engine · malfunctionedWHILE CLIMBING THROUGH FL280, THE NR 4 ENGINE FLAMED OUT FOLLOWED BY THE FIRE WARNING ACTIVATING FOR THE NR 4 ENGINE. COM PROCEDURES WERE FOLLOWED TO SECURE THE ENGINE AND BOTH FIRE BOTTLES WERE DISCHARGED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNEDJul 24, 2002 · N617US · Boeing 747251F · Engine (Turbine/Turboprop)SDR EIAA2002088Engine · stalledFLT 481 - PANC - WHILE CRUISING AT FL35.0, NR 1 ENGINE COMPRESSOR STALLED, N1 RPM DECREASED AND EGT INCREASED RETARDED THROTTLE NO RESPONSE, SHUTDOWN NR 1 ENGINE. DURING WINDMILLING ATTEMPTED RESTART, EGT OUT OF LIMITS, RETURN TO ANC. (M)Jul 23, 2002 · N481EV · Boeing 747132 · Engine (Turbine/Turboprop)SDR EIA2002088Fuel Control · malfunctionedWHILE CRUISING AT FL 35.0, NR 1 ENGINE COMPRESSOR STALLED, N1 RPM DECREASED AND EGT INCREASED RETARDED THROTTLE. NO RESPONSE, SHUTDOWN NR 1 ENGINE. DURING WINDMILLING ATTEMPTED RESTART. EGT OUT OF LIMITS, RETURN TO ANC. REMOVED AND REPLACED NR 1 ENGINE MAIJul 23, 2002 · N481EV · Boeing 747132 · Fuel Control/Turbine EnginesSDR EIA2002035Actuator · failedCBBI - AFTER NR 4 THRUST LEVER WAS RETARDED TO IDLE ON DESCENT THE NR 4 ENGINE HAD AN UNRECOVERABLE COMPRESSOR STALL. ENGINE SHUTDOWN ACCOMPLISHED. RESTART UNSUCCESSFUL. INSPECTED ENGINE. REPLACED NR 4 ENGINE EVC UNIT (P/N 7479555) AND STATOR VANE CONTROL Apr 12, 2002 · N482EV · Boeing 747212B · Turbine Engine Compressor SectionSDR 200200182Nozzle · crackedNR 4 ENGINE EXHAUST NOZZLE AT THE 2:00 POSITION, 4 INCHES FROM THE TRAILING EDGE HAS A 10 INCH CRACK IN THE OUTER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER 747 SRM 54-30-03.Mar 13, 2002 · N471EV · Boeing 747273C · Engine Collector/Tailpipe/NozzleSDR EIA2001240Line · failedSUU - WHEN CLIMBING THROUGH FL300 TO FL380 NR 1 ENGINE HAD AN UNRECOVERABLE COMPRESSOR STALL, EPR WAS APPROX 1.49, WHEN STALL OCCURRED N1 AND N2 DECREASED EGT INCREASED THEN DECREASED PEAKING AT 850 DEGREE SHUTDOWN, RESTARTED ENGINE. PARAMETERS NORMAL AFTER RAug 21, 2001 · N479EV · Boeing 747132 · Fuel Controlling SystemSDR 0101666612Check Valve · failedAFTER BEGINNING DESCENT FROM FL300, THE NR 4 ENGINE FLAMED OUT. THE CREW TRIED TO RESTART THE ENGINE PER COM PROCEDURES WITHOUT SUCCESS. THE REMAINDER OF THE DESCENT AND LANDING WERE MADE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE 8THMay 4, 2001 · N612US · Boeing 747251B · Pneumatic Distribution SystemSDR 0100916613Engine · stalledDURING LANDING ROLLOUT (NKT) WHILE COMING OUT OF REVERSE THRUST, THE NR 4 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 1291C AND THE CONTROL TOWER REPORTED FLAMES FROM THE ENGINE. THE CREW FOLLOWED ENGINE FIRE PROCEDURES AND DISCHARGED ONE FIRE BOTTLE. MAINTEMar 1, 2001 · N613US · Boeing 747251B · Turbine Engine Compressor SectionSDR 20010406SG001Garlock Seal · damagedRJCC - NR 2 ENGINE INDICATED OIL QTY LEAK OF APPROX 1 HAL/HR DIVERTED TO RJCC. OIL QTY DROPPED BELOW ZERO, IFSD NR 2 ENGINE. PERFORMED WINDMILL INSPECTION, NO DEFECTS. FOUND NR 2 CSD FILTER HOUSING CRACKED AND HEAT DAMAGED. REPLACED CSD AND GARLOCK SEAL. Feb 22, 2001 · N470EV · Boeing 747273C · Turbine Engine Oil SystemSDR 0100566729Clamp · failedDURING INITIAL CLIMB AT 300 FEET, THE NR 1 ENGINE FIRE WARNING ACTIVATED. THE NACELLE TEMPERATURE INDICATION WAS PEGGED IN THE WARNING RANGE AND THE POWER LEVER WAS STUCK IN MID RANGE. THE ENGINE WAS SHUT DOWN PER COM AND ONE FIRE BOTTLE WAS DISCHARGED. AFTFeb 14, 2001 · N629US · Boeing 747251F · Pneumatic Distribution SystemSDR 2000UALA00682Light · inoperativeEMERGENCY EXIT SIGN ABOVE DOOR 5 LEFT IS INOP.Nov 7, 2000 · N164UA · Boeing 747238B · Emergency LightingSDR 2000UALA00579Wire · brokenAFT EEL LIGHTING STAYING ON CAN NOT TURN OFF. *S/D* A BROKEN WIRE WAS FOUND (REF MRR 200UALA00578. NEW WIRE WAS SPLICED IN AND SYSTEM CHECKED OK PER MM 33-51-21.Oct 4, 2000 · N165UA · Boeing 747238B · Light System WiringSDR 2000UALA00578Wire · brokenD ZONE EMERGENCY EXIT LIGHTS ARE ILLUMINATED WHEN SELECTED OFF. *S/D* CLEANED CONNECTOR , CK''D OK. A BROKEN WIRE WAS FOUND (REF MRR 200UALA00579). NEW WIRE WAS SPLICED IN AND SYSTEM CHECKED OK PER MM 33-51-21.Oct 2, 2000 · N165UA · Boeing 747238B · Light System WiringSDR 2000UALA00531Battery Pack · dischargedEEL LIGHT CAME ON DURING TAXI AT SEAT 20-23C. *S/D* REPLACED POWER SUPPLY (P/N: 65B54476-1) AT MAIN ENTRY DOOR 3L OVERHEAD PANEL PER MM33-51-02, CHECKS OK.Sep 4, 2000 · N160UA · Boeing 747238B · Emergency LightingSDR EIA2000027Engine · leakingJFK - AFTER TAKEOFF, NR 4 ENGINE LOST OIL QTY AND PRESSURE. ACCOMPLISHED IN FLT SHUTDOWN. ENGINE SHUTDOWN WITH APPROX 1 GAL OIL AND 20 PSI PRESSURE 20 SECONDS AFTER PRESS DROP, WINDMILL 8 MIN. RAN NR 4 ENGINE AT IDLE COULD NOT FIND OIL LEAK. DRIVE SEAL CHEJul 16, 2000 · N482EV · Boeing 747212B · Engine (Turbine/Turboprop)SDR 2000UALA00471Switch · failedSTRONG ELECTRICAL SMELL AND SMOKE IN FORWARD CABIN WHILE ON TAXI OUT. AIRCRAFT RETURNED TO GATE. *S/D* THE LAVATORY FLUSH MOTOR WAS CONTINUOUSLY RUNNING AND OVERHEATED, CAUSED BY A STICKING LAVATORY FLUSH SWITCH. THE FLUSH MOTOR AND TIMER WERE REPLACED. AJun 14, 2000 · N163UA · Boeing 747238B · Waste Disposal SystemSDR 2000UALA00297Unknown · odorELECTRICAL BURNING SMELL WAS NOTICED BY PASSENGER IN D ZONE ON RIGHT SIDE PULLED CIRCUIT BREAKERS FOR READING LIGHTS AND SIDE-WALL LIGHTS. *S/D* RESET CIRCUIT BREAKERS FOR READING AND SIDEWALL LIGHTS. TURNED READING LIGHTS ON FOR TWO HOURS, NO ELECTRICAL ODJun 2, 2000 · N165UA · Boeing 747238B · Air Distribution SystemSDR EIA2000024Blade · bird strikeJFK - ON TAKEOFF ROLL, NR 2 ENGINE INGESTED SEVERAL BIRDS. EGT TO 1232 FOR 76 SECONDS, CAT D O/H EXCEEDANCE. POST FLIGHT INSPECTION INDICATED DAMAGE TO NR 2 CANOE, LEFT OUTBOARD FORE FLAP, LEFT MID FLAP, BENT FAN BLADES. (M)Jun 1, 2000 · N470EV · Boeing 747273C · Turbine Engine Compressor Section
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