Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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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 = 'JT8D15'
  ORDER BY difficulty_date DESC"

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SDR CA090611007Windshield · failed(CAN) ACFT ENROUTE, IN CRUISE AT FL 380 CAPTAIN`S FRONT WINDSHIELD SHATTERED. ACFT DIVERTED, LANDED WITHOUT INCIDENT. MX DETERMINED OUTER PANE FAILED, WINDOW REPLACED.Jun 3, 2009 · Boeing 727225 · Flight Compartment WindowsSDR CA090601004Duct · ruptured(CAN) ACFT RETURNED TO YOW AFTER APPROX 30 MINUTES INTO FLIGHT DUE TO FIRE ALARM ON NR 2 ENGINE. ALARM WOULD NOT GO OFF AFTER NORMAL PROCEDURE SO ENGINE SHUTDOWN AND FIRE BOTTLE DISCHARGED. MX FOUND A 4 INCH HOLE IN THE 13TH STAGE BLEED AIR DUCT TO THE NOSE ANMay 30, 2009 · Boeing 727200 · Compressor Bleed ValveSDR C8GA20090075Pump · faultyFLT 720 FROM TOL TO ATL, DURING CLIMB-OUT THE NR 2 ENGINE FUEL FLOW BECAME ERRATIC, THE N1 AND N2 STARTED WINDING DOWN FOLLOWED BY COMPRESSOR STALL. THE NR 2 ENGINE WAS SHUT DOWN, EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT IMay 13, 2009 · N815EA · Boeing 727225 · Engine Fuel PumpSDR C8GA20090064Fan · bentFLT 706 FROM ILN TO MSP, DURING TAKEOFF ROLL THE NR 3 ENGINE HAD A COMPRESSOR STALL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 ENGINE HAD INGESTED A GOOSE. THE C1 AND C2 FMay 1, 2009 · N713AA · Boeing 727200 · Turbine Engine Compressor SectionSDR CA090224001Windshield · failed(CAN) THE ACFT SUFFERED AN OUTER PANE FAILURE ON RT WINDSHIELD AT THE TOP OF THE CLIMB. THE ACFT DIVERTED AND LANDED WITHOUT FURTHER PROBLEM. MX REPLACED THE WINDSHIELD AND THE ACFT WAS RETURNED TO SERVICE.Feb 22, 2009 · Boeing 727233 · Flight Compartment WindowsSDR CA090119014Drum · frozenON APPROACH INTO YYZ WHEN FLAPS 30 WAS SELECTED NEEDLES REMAINED IN FLAPS 25 POSITION BAND. "TO LOW FLAPS" AURAL WARNING SOUNDED. MISSED APPROACH WAS EXECUTED. RECTIFICATION TROUBLESHOOTING CARRIED OUT AS PER MM 27-51-000-5. UNABLE TO FAULT. SUSPECT FROZEN DJan 16, 2009 · Boeing 727225 · Trailing Edge Flap Control SystemSDR CA090116003Switch · worn(CAN) ESSENTIAL POWER WAS LOST AT ROTATION DURING TAKE-OFF. SECOND OFFICER WAS UNABLE TO ESTABLISH ESSENTIAL POWER WHEN CYCLED FROM GENERATOR 3, TO GEN 1, TO GEN 2. STANDBY POWER WAS SELECTED. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT OFJan 15, 2009 · Boeing 727225 · AC Power Distribution SystemSDR CA090113005Cabin Pressure · unknown(CAN) ENROUTE YOW FROM YVO, THE CREW OBSERVED THE CABIN ALTITUDE CLIMBING BEYOND THE PRESET VALUE. THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER PROBLEM. (TC NR 20090113005)Jan 11, 2009 · Boeing 727233 · Cabin Pressure Control SystemSDR C8GA20080073Oil System · reads highFLT 706 FROM TOL TO MSP. DURING CRUISE OPERATION THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED. APPROPRIATE CHECKLIST WAS FOLLOWED AND THE ENGINE WAS SHUT DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT IN MSP. POST FLIGHT INSPECTION WAS PERFORMED, FOUND NR 2 ENGIDec 19, 2008 · N713AA · Boeing 727223 · Engine Oil Indicating SystemSDR CA081222003Hose · failed(CAN) ON DEPARTURE FROM YVR, WHEN GEAR SELECTED UP, HYDRAULIC `A` SYSTEM FAILED. HYDRAULIC QUANTITY INDICATION 0, HYDRAULIC PRESSURE INDICATION 0. CREW EXTENDED GEAR IN ACCORDANCE WITH FLIGHT MANUAL PROCEDURES. THE AIRCRAFT RETURNED TO YVR, STOPPED ON THE RDec 19, 2008 · Boeing 727225 · Hydraulic System, MainSDR CA081205006Stator · broken(CAN) DURING PUSHBACK ON C-FCJF EXCESSIVE FORCE WAS REQUIRED TO MOVE ACFT AND DETERMINED NR2 MAIN WHEEL WAS DEFLATED. ACFT PULLED BACK TO GATE FOR INVESTIGATION. MAINT WAS UNABLE TO REMOVE NR2 WHEEL. AFTER SEVERAL EFFORTS WITHOUT SUCCESS IT WAS DECIDED THE TIDec 2, 2008 · Boeing 727223 · Landing Gear Brake SystemSDR C8GA20080084Structure · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER CHORD RUNNING ALONG STR 27R BY THE C2 DOOR IS CORRODED AND CRACKED AT BOTH ENDS, STA 950E-1010. CUT OUT DAMAGED AREA, PERFORMED HFEC INSPECTION AND FABRICATED REPAIR ANGLE FROM 7075Nov 1, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20080083Frame · corrodedWHILE IN HEAVY PERFORMING INSPECTIONS IT WAS NOTED THAT THE FRAME WAS DENTED AT BS 1110 JUST ABOVE STR 26R CUT OUT DAMAGED FRAME AND FABRICATED NEW FRAME FROM 7075-O .063 INCH 23 INCH BY 4.5 INCH. HEAT TREATED FRAME TO T6. INSTALLED REPAIR IAW SRM 53-10-2 ANOct 29, 2008 · N715AA · Boeing 727223 · Fuselage Main, FrameSDR C8GA20080083AIntercostal · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS SURFACE CORROSION WAS NOTED ON INTERCOSTAL BS 695 STR 27R. DAMAGED INTERCOSTAL WAS REMOVED, A NEW INTERCOSTAL WAS FABRICATED. INSTALLED REPAIR IAW SRM 53-10-2 AND 51-10-3. NO OTHER DEFECTS NOTED. AIRCRAFT WOct 29, 2008 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR CA081009007Switch · failed(CAN) JUST AFTER DEPARTURE FROM YYZ, THE PILOTS NOTICED WHEN SELECTING FLAPS 5 TO FLAPS 2, THE LEADING EDGE FLAP INDICATOR ON THE FORWARD PANEL WENT MOMENTARILY GREEN THEN BACK TO AMBER. THE LEADING EDGE INDICATOR ON THE REAR PANEL INDICATED THE NR 1 LEADING Oct 9, 2008 · Boeing 727247 · Leading Edge Slat Position Indicating SystemSDR CA081016004Hose · leaking(CAN) DURING DEPARTURE OF THE ACFT PRIOR TO ENGINE START, FUEL WAS NOTICED LEAKING FROM NR 3 ENGINE. MX REQUESTED NORMAL ENGINE START TO VERIFY FUEL LEAK. ENGINE WAS SHUT DOWN, AND ACFT TOWED BACK TO GATE FOR FURTHER INVESTIGATION. THE FUEL HOSE ASSEMBLY WAOct 8, 2008 · Boeing 727225 · Engine Fuel DistributionSDR SPA2008F00001Battery Pack · inoperativeLOWER EMERGENCY LIGHTS AT DOORS L2 AND R2 WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-21-27. FUNCTIONAL CHECK SATISFACTORY. (K)Sep 17, 2008 · N712S · Boeing 7372Y5 · Emergency LightingSDR SPA2008F00002Battery Pack · inoperativeLOWER EMERGENCY EXIT LIGHT AT R1 AND L1 DOOR POSITIONS WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MANUAL 33-21-27. FUNCTIONAL CHECK SATISFACTORY. (K)Sep 17, 2008 · N712S · Boeing 7372Y5 · Emergency LightingSDR SPA2008F00003Power Supply · failedLOWER EMERGENCY EXIT LIGHTS AT DOORS L2 AND R2 WILL NOT ILLUMINATE. REPLACED POWER SUPPLY IAW MM 33-21-27. FUNCTIONAL CHECK SATISFACTORY. (K)Sep 17, 2008 · N712S · Boeing 7372Y5 · Emergency LightingSDR CA080911005O-Ring · leaking(CAN) WHILE CLIMBING OUT, NOTICED ENG NR 1 OIL QUANTITY INDICATOR SLOWLY DECREASING, QUANTITY WAS 1 GALLON AT TOP OF CLIMB. AT MID POINT, QUANTITY DECREASED TOWARD ZERO. ENGINE SHUTDOWN DRILL AND CHECK LIST COMPLETED. ENGINE WINDMILLING SUPPLEMENT COMPLETEDSep 11, 2008 · Boeing 727247 · Engine Oil Distribution (Airframe Furnished)SDR C8G2008F00018Turbine · damagedON TAKEOFF, JUST AFTER V2 THE NR 2 ENGINE FAILED. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED TURBINE DAMAGE. THE NR 2 ENGINE WAS REMOVED AND REPLACED. OPS CHECK GOOD. NO OTHER DEFECTS WERE Sep 10, 2008 · N808EA · Boeing 727225 · Turbine SectionSDR SPA2008F00000Battery Pack · failedMID CABIN CEILING EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK AND POWER SUPPLY IAW MM 33-51-81. FUNCTIONAL CHECK SATISFACTORY. (K)Sep 1, 2008 · N712S · Boeing 7372Y5 · Emergency LightingSDR PCS2008F00000Compressor · failedDURING CLIMB BETWEEN 180 TO 210 FLIGHT LEVEL NR 1 ENG COMPRESSOR STALL FOLLOWED BY OIL TEMP RISE. AFTER SECOND COMPRESSOR STALL NR 1 ENG OIL PRESS LIGHT ILLUMINATED. ENG WAS SHUT DOWN PER AOM. NR 1 ENG OPERATED APPROX 9 MINUTES OIL PRESS ABOUT 20 PSI. POSTAug 26, 2008 · N794AJ · Boeing 727227 · Turbine Engine Compressor SectionSDR C8GA20080053Mount · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 7 SLAT ACTUATOR IB MOUNTING BRACKET HAD A 1" CRACK. REMOVED CRACKED SUPPORT. FABRICATED NEW DOUBLER FROM 301 1/2 HD .100" (7.5 X 3) AND NEW STIFFNER FROM BAC 1503-100145 (9" X 4"). INSTAAug 23, 2008 · N713AA · Boeing 727223 · Leading Edge DevicesSDR DHLA200800088Engine · malfunctionedREJECTED TAKEOFF, ENG NR 3 WAS 1.88 EPR WITH BUG OF 2.05. GROSS WEIGHT 173.4, AIR SPEED 70 KTS, PRESS ALTITUDE 2360FT, AIR TEMP 39C. TRIMMED ENG TO CORRECT PP AND IDLE PARAMETERS PER MM CH 71-00-87. PP STOP REMOVED AND SAFTIED. TO EPR 2.07. ACFT WAS GROUNAug 15, 2008 · N749DH · Boeing 7272J0 · Engine (Turbine/Turboprop)SDR CA080730002Smoke Detector · failed(CAN) ON CLIMB THROUGH FL290 CARGO SMOKE 6TH POSITION LIGHT ILLUMINATED AND FIRE WARNING BELL SOUNDED. ACFT RETURNED. ON ARRIVAL, NO SMOKE DETECTION LIGHTS WERE ILLUMINATED ON FE PANEL. CARGO AREA INSPECTED FOR SMOKE. NONE FOUND. SUSPECTED FAILURE OF NR 6 SMOKJul 30, 2008 · Boeing 727225 · Smoke DetectionSDR CA080801003Engine · power loss(CAN) WHILE AIRCRAFT WAS IN CRUISE ENROUTE, THE ACFT EXPERIENCED AN UNCOMMANDED POWER LOSS, DECELERATING TO FLIGHT IDLE. THE CREW SELECTED NR 2 THRUST TO IDLE AND THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. THE ACFT FERRIED FOR Jul 28, 2008 · Boeing 727233 · Engine (Turbine/Turboprop)SDR PID2008F00001Bypass Switch · inoperativeOIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN RT ENGINE IAW QRH. DIVERTED FLT. INSPECTED NR 2 MAIN ENGINE OIL FILTER AND CLEANED BYPASS CONNECTOR SWITCH. RAN NR 2 ENGINE, BYPASS CONNECTOR SWITCH. RAN NR 2 ENGINE, BYPASS LIGHT DID NOT ILLUMINATE. Jul 13, 2008 · N250TR · Boeing 7372K5 · Engine Oil Indicating SystemSDR PID2008F00003Sensor · failedGEAR WOULD NOT RETRACT. OVER RIDE TRIGGER USED TO RETRACT GEAR. AC RETURNED TO FIELD. PERFORMED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-291. AC IS SAFE FOR INTENDED FERRY FLIGHT.. 7/11/2008: FOUND AIR SAFETY SENSOR BAD. REPLACED AIR SAFELY SENSOR AND OJul 10, 2008 · N251TR · Boeing 737228 · Landing Gear Position and WarningSDR NWAA083069941Engine · flamed outDURING TOP OF DESCENT AS THRUST WAS REDUCED, ENGINE NR 2 FLAMED OUT. FLIGHT CREW DIVERTED TO ABE PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLACED ENGINE NR 2. (A)Jul 10, 2008 · N3324L · Doug DC932 · Engine (Turbine/Turboprop)SDR PID2008F00005Battery Pack · inoperativeAFT EMERGENCY EXIT LIGHTS NOT WORKING. REMOVED AND REPLACED AFT BATTERY PACK IAW MM 33-51-57. LIGHTS WORKING NORMAL. (K)Jul 1, 2008 · N251TR · Boeing 737228 · Emergency LightingSDR 08FDEA02452Bolt · damagedNR 3 ENGINE STARTER CONTROL ROD INBD OF ENGINE, NUT HAS NO THREADS SHOWING AND SPRING CLIP NOT BENT OVER BOLT HEAD. PROPERLY INSTALLED NR 3 ENG START CONTROL ROD (UPPER) BOLT AND ATTACHING HARDWARE IAW FX MM 76-11-021-2.Jun 25, 2008 · N494FE · Boeing 727227 · Fuel Control/Turbine EnginesSDR CA080624003Indicator · malfunctioned(CAN) ON TAKE-OFF/CLIMB OUT, THE NR 3 ENGINE EGT WAS 60 DEGREES HIGHER THAN ENGINES 1 AND 2. THROUGH 1000 FEET AGL THE NR 3 OIL TEMP WENT INTO THE RED BAND. A REDUCTION IN POWER FOR QUITE THRUST BROUGHT THE OIL TEMP BACK TO THE YELLOW BAND. A RESUMPTION IN POWJun 24, 2008 · Boeing 727225 · Engine Oil TemperatureSDR C8G2008F00003Fitting · looseDURING CLIMB OPERATION, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENG WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AC LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 2 ENGINE OIL FILTER BYPASS SWJun 11, 2008 · N708AA · Boeing 727223 · Turbine Engine Oil SystemSDR C8G2008F00013Indicator · faultyDURING TAKEOFF ROLL THE NR 2 ENGINE EGT INDICATOR WENT TO ZERO INDICATION. THE TAKEOFF WAS ABORTED, WHERE THE AC RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED NR 2 ENGINE EGT INDICATOR AT FAULT. THE NR 2 ENGINE EGT INDICATOR WAS REMOVED Jun 11, 2008 · N801EA · Boeing 727225 · Engine EGT/TIT Indicating SystemSDR PID2008F00004Battery Pack · inoperativeMID CABIN CEILING - EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS AT MID CABIN CEILING. OPS CHECK, EMERGENCY EXIT LIGHTS GOOD, IAW MM33-51-81. (K)Jun 6, 2008 · N249TR · Boeing 7372K5 · Emergency LightingSDR CA080418002Fire Detector · false indication(CAN) AFTER TAKEOFF, AT APPROX 1,000 FEET AGL, THERE WAS A FIRE WARNING ON THE NR 1 ENGINE. THRUST LEVER RETARDED, LIGHT REMAINED ON. EMERGENCY DRILL COMPLETED AND LIGHT EXTINGUISHED AFTER FIRE BOTTLE DISCHARGED. AC RETURNED AND LANDED WITHOUT FURTHER INCIDENApr 17, 2008 · Boeing 727247 · Fire DetectionSDR CA080411004Line · leakingAFTER TAKEOFF WHEN GEAR SELECTED UP, HYDRAULIC SYSTEM "A" LOW LEVEL LIGHT ILLUMINATED AND HYDRAULIC QUANTITY DROPPED TO 2.0 GAL. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED FOR APPROACH. PER FLIGHT CREW CHECKLIST GEAR WAS MANUALLY LOWERED HOWEVER FLIGHT CApr 8, 2008 · Boeing 727223 · Hydraulic System, MainSDR C8GA20080012Helicoil · damagedFLT 708 FROM MCI TO PHX - DURING CRUISE OPERATION THE CAPTAIN WAS NOTIFIED THAT THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE NR 1 ENGINE WAS SHUT DOWN AND EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO ABQ WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT Mar 25, 2008 · N899AA · Boeing 727223 · Turbine Engine Accessory DriveSDR CA080124002Swivel · leaking(CAN) AC WAS DISPATCHED AND DURING CRUISE FLIGHT, THE FLIGHT ENGINEER NOTICED THAT THE (A) SYS HYDRAULICS INDICATED .1250 OF A TANK REMAINING. THE CREW DECIDED TO DECLARE AN EMERGENCY AND THE LANDING GEAR NEEDED TO BE CRANKED DOWN. THE AC LANDED SAFELY AND WASJan 24, 2008 · Boeing 727247 · Hydraulic System, MainSDR DU4R2008191Skin · corrodedS/O 304002 N/R NR26444 CORROSION FWD CARGO BILGE AREA BS 660 S-28L - S-28R. REPAIRED BY CUTTING OUT CORRODED AREA BS 661 TO BS 664.5, NDT VERIFIED NO CRACKS IAW NPTM PT. 6 51-00-00 FIG. 23. FABRICATED AND INSTALLED REPAIR DOUBLER 11.6 INCH X 16.25 INCH FROM 2Jan 19, 2008 · N289MT · Boeing 727223 · Fuselage Main, Plate/SkinSDR CA080121007Volt Regulator · odor(CAN) DURING FLIGHT CREW SHUTDOWN CHECKLIST, ON APU POWER, SMOKE ALARM SOUNDED IN THE AC LAVATORY. LAVATORY INSP REVEALED SOME SMOKE. ALARM SILENCED WHILE INSPECTING THE LAVATORY AREA. AFTER APPROXIMATELY 30 SECONDS, THE ALARM SOUNDED AGAIN, AND THE AC POWEJan 16, 2008 · Boeing 727225 · DC RegulatorSDR CA080115007Pcu · frozen(CAN) THE AC ARRIVED AT DESTINATION AND WAS ON A TURN-AROUND WHEN THE CREW NOTICED ON TAXI OUT, THAT THE AILERONS HAD FROZEN UP. THE AC RETURNED TO THE RAMP WHERE MAINT INSPECTED THE SYS. IT WAS DETERMINED THAT THE AILERON POWER CONTROL UNIT HAD FROZEN UP. HEJan 15, 2008 · Boeing 727247 · Aileron Control SystemSDR CA080109004Uplock Switch · faulted(CAN) FLIGHT WAS DEPARTING AND THEN DURING THE TAKEOFF ROLL, THE CREW SELECTED THE LANDING GEAR UP. WHEN THE GEAR HAD CYCLED UP THERE REMAINED A RED NOSE GEAR UNSAFE LIGHT. THE CREW CYCLED THE LANDING GEAR 3 TIMES BEFORE THE UNSAFE LIGHT EVENTUALLY WENT OUT. TJan 8, 2008 · Boeing 727247 · Landing Gear Position and WarningSDR KNNA200700068Skin · damagedWHILE PERFORMING AN A-7 CHECK, A LIGHTNING STRIKE WAS FOUND ON THE LT ELEVATOR AT THE OUTBOARD TRAILING EDGE LOWER SIDE, UNDER I/B STATIC WICK, SPECIAL INSPECTION WAS PERFORMED IAW SKY KING GMM SECTION 4.03 AND AMM 05-51-151-201 WITH NO OTHER DAMAGE NOTED. ELDec 10, 2007 · N326DL · Boeing 737232 · Elevator, Plate/SkinSDR CA071204004Accessory Unit · unserviceable(CAN) SHORTLY AFTER TAKEOFF WHEN GEAR WAS BEING RETRACTED, CREW NOTICED THAT THE RT MAIN GEAR RED LIGHT WAS STILL ILLUMINATED. CREW CYCLED THE LANDING GEAR (3) TIMES WITH THE SAME RESULTS. THE CREW ADVISED THAT AIR NOISE COULD BE HEARD. GEAR WAS SELECTED DOWN Dec 4, 2007 · Boeing 727247 · Landing Gear Retraction/Extension SystemSDR C8GA20070012Helicoil · damagedFLT 708 FROM TOL TO MCI - DURING CRUISE OPERATION AT FLT LEVEL 320, THE NR 3 ENGINE LOW OIL PSI LIGHT ILLUMINATED. OIL QUANTITY WAS OBSERVED TO BE DECREASING FOLLOWED BY A DECREASE IN OIL PSI. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO STL WHNov 20, 2007 · N713AA · Boeing 727223 · Turbine Engine Accessory DriveSDR KNNA200700061Slat Track · jammedAFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILINov 13, 2007 · N326DL · Boeing 737232 · Leading Edge DevicesSDR KNNA200700043Slat Track · jammedAFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILINov 13, 2007 · N326DL · Boeing 737232 · Leading Edge DevicesSDR CA071122006Accessory Unit · inoperative(CAN) THE CREW DISCOVERED THAT THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE (OFF) POSITION WITHOUT THE USE OF THE OVERRIDE TRIGGER. AT THE TERMINATING STATION, MAINTENANCE REPLACED THE LANDING GEAR ACCY UNIT AND RETURNED THE AIRCRAFT TO SERVICE. (TC NR 2007Nov 9, 2007 · Boeing 727223 · Landing Gear Retraction/Extension System
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