Pratt & Whitney JT8D-17

Service difficulty reports · 1,680

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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 = 'JT8D17'
  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 DHL2003741009Screw · looseCOCKPIT DOOR IS DIFFICULT TO OPEN AND CLOSE. TIGHTENED SCREWS ON DOOR FRAME AND DOOR. OPS CHECKED GOOD IAW 20-80-1 AND 52-50-1.Oct 2, 2003 · N741DH · Boeing 7272Q9 · Fixed Inner DoorsSDR CA030929006Actuator · malfunctioned(CAN) ON CLIMB OUT THE AIRCRAFT EXPERIENCED A TOTAL LOSS OF HYDRAULIC SYSTEM A FLUID. AIRCRAFT TURNED BACK TO YUL AND LANDED WITHOUT INCIDENT. THE NR 3 SPOILER ACTUATOR WAS FOUND TO BE THE CAUSE OF THE FLUID LEAK.ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERSep 28, 2003 · Boeing 737217 · Drag Control ActuatorSDR C1HA200394018Switch · malfunctionedON DEPARTURE RETRACTED THE GEAR AND HAD THREE RED GEAR LIGHTS ILLUMINATED AT REMAINED ILLUMINATED. CLEANED GEAR HANDLE POSITION POSITION SWITCH S92 IAW B727MM32-60-0 OPS CK GOOD IAW B727MM32-60-0.Sep 26, 2003 · N294AS · Boeing 727290 · Landing Gear SelectorSDR DHL2003782011Warning Light · false activationIN FLIGHT, RED LT GEAR ANNUNCIATOR ILLUMINATED. HYDRAULIC SYSTEM (A) NORMAL AND NO INDICATION ON S/O'S ANNUNCIATOR PANEL. AFTER 5 MINUTES THE RED LEFT GEAR ANNUNCIATOR LIGHT EXTINGUISHED. ALL INDICATIONS NORMAL. PERFORMED OPERATIONAL CHECK OF LANDING GEARSep 25, 2003 · N769AT · Boeing 727227 · Landing Gear Position and WarningSDR C1HA200395069Uplock · wornDURING TAKEOFF ROLL RED DOORS LIGHT ON FORWARD PANEL ILLUMINATED, LT GEAR DOOR LIGHT (AMBER) ON ENGINEERS PANEL ILLUMINATED TAKE OFF WAS ABORTED AT 80 KTS. VERY LIGHT BRAKING WAS USED WITH 9000 FEET OF RUNWAY REMAINING FOUND LT MLG UPLOCK ASSY HAD 2 BOLTS WITHSep 19, 2003 · N295AS · Boeing 727290 · Landing Gear Position and WarningSDR CA030918008Bolt · improper part(CAN) NOSE LANDING GEAR LOCK ACTUATOR LOWER ATTACH BOLT SHEARED, ALLOWING ACTUATOR TO FAIL. BOLT IDENTIFIED AS AN UNAPPROVED PART. THIS BOLT WAS NOT INSTALLED BY THIS OPERATOR.Sep 11, 2003 · Boeing 737* · Nose/Tail Landing GearSDR C1HA200382009Engine · malfunctionedNR 2 ENG WAS FLUC EPR+- 4 N1, N2 EGT AND FUEL FLOW ALL WERE FLUCT. PRIOR TO SHUTDOWN NR 2 ENG FUEL HEAT ICING LIGHT STROBING EVEN WITH FUEL HEAT ON. ENG SHUT DOWN DURING FINAL CLIMB TO 37000 WHEN ENG SHUT DOWN ENG OIL CLIMBED TO 140 C ENG WINDMILLED FOR 37 MINSep 6, 2003 · N682CA · Boeing 7272S7 · Engine (Turbine/Turboprop)SDR 03FDEA01395Engine · leakingAT FL 330 NR 1 OIL QTY WENT RAPIDLY TO ZERO. OIL PRESS DROPPED TO 30 PSI. ENGINE SHUTDOWN IAW RED TABS. REMOVED AND REPLACED NR 1 ENG ASSY AS PER WORK CARD 70T0001-01, A/C OK FOR SERVICE.Aug 27, 2003 · N481FE · Boeing 727200 · Turbine Engine Oil SystemSDR CA030902002Circuit Board · failed(CAN) AIRCRAFT REPORTS SHORTLY AFTER TAKE OFF ROTATION, NUMEROUS THREE PHASE CIRCUIT BREAKERS (2 AND 3 THRUST REVERSER, GASPER FAN AND PANEL INSTRUMENT INDICATOR NR 1 DC) POPPED CAUSING LOSS OF SEVERAL SYSTEMS AND ANNUNCIATIONS. NR 2Aug 25, 2003 · Boeing 737281 · AC Generator-AlternatorSDR C1HA200392004Fuel Control · malfunctionedON TAKEOFF ROLL, NR 2 ENGINE EGT PEAKED AT 650 DEG, THEN HEATED TO 670 FOR 5 SECONDS. ABORTED TAKEOFF, FULL POWER USED FOR T/O. REMOVED AND REPLACED NR 2 ENGINE FUEL CONTROL IAW P&W MM 73-21-01.Aug 4, 2003 · N292AS · Boeing 727212 · Fuel Control/Turbine EnginesSDR CA030805001Landing Light · fire(CAN) DURING TROUBLESHOOTING OF AN OUTBOARD (LT HAND) LANDING LIGHT SNAG MAINTENANCENOTICED SMOKE ODOR IN THE COCKPIT AND THEN SEVERAL C/BS POPPED. MAINTENANCE SHUT ALL AIRCRAFT POWER DOWN. SMOKE WAS NOTICED BY MAINTENANCE COMING FROM THE LT PYLON AREA FWD. PAug 2, 2003 · Boeing 737217 · Exterior LightingSDR DHL2003782006Smoke Detector · false indicationNR 6 MAIN CARGO SMOKE DETECTOR ILLUMINATED AT FL 310. PERFORMED EMERGENCY CHECKLIST. LANDED AT MDT. REMOVED AND REPLACED NR 6 MAIN CARGO COMPARTMENT SMOKE DETECTOR. OPS CHECKED GOOD IAW AMM 26-17-0.Jul 22, 2003 · N769AT · Boeing 727227 · Smoke DetectionSDR DHL2003741005Smoke Warning · false activationCARGO SMOKE LIGHT ILLUMINATED ON FINAL APPROACH. PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE OK FOR SERVICE. CARGO LIGHT IS NOT ILLUMINATED.Jul 18, 2003 · N741DH · Boeing 7272Q9 · Smoke DetectionSDR C1HA200381015Scavenge Pump · failedDURING TAXI OUT TOWER ADVISED NR 2 ENGINE SMOKING EXCESSIVLY ALSO NOTED NR 2 OIL QTY DECREASING BELOW 1 GAL-FOUND NR 6 SCAVAGE PUMP BAD. REMOVED AND REPLACED ENGINE.Jul 10, 2003 · N681CA · Boeing 7272S7 · Turbine Engine Oil SystemSDR SROM200300034Seat Track · gougedDURING D CHECK INSPECTION FOUND NUMEROUS GOUGES IN CENTER AND TOP OF SEAT TRACK BETWEEN BS 540 - 727, LBL 24. REMOVED AND REPLACED SEAT TRACK BETWEEN BS 540 TO 727 IAW SRM 51-30-2, 51-10-2 AND MM 51-21-0.Jul 2, 2003 · N736BP · Boeing 737205 · Fuselage, Seat/Cargo Attach FittingsSDR 0301219860Fuel Control · malfunctionedDURING TAKEOFF ROLL, FLIGHT CREW OBSERVED A FLOCK OF BIRDS PASS CLOSE TO THE AIRCRAFT AND THEN HEARD A POSSIBLE ENGINE COMPRESSOR STALL. FLIGHT CREW ABORTED TKAEOFF AT 118 KNOTS. MAINTENANCE INSPECTED BOTH ENGINES FOR EVIDENCE OF A BIRD STRIKE, NONE FOUND. Jun 29, 2003 · N769NC · Doug DC951 · Turbine Engine Compressor SectionSDR C1HA200394012Bleed Valve · failedNR 2 ENGINE COMPRESSOR STALL ON FINAL AS POWER ADDED. ON GROUND COMPRESSOR STALL WHILE TAXIING.Jun 28, 2003 · N294AS · Boeing 727290 · Compressor Bleed ControlSDR C1HA200381014Bleed Valve · malfunctionedON APPROACH INTO PVR ADVANCED THRUST LEVERS FROM IDLE TO APPROX 1.4 EPR NOTICED A COMPRESSOR STALL. THIS HAPPENED TWICE ON APPROACH. SUSPECT NR 2 ENGINE BECAUSE THE EPR'S JUMPED ERRATICALLY. ALL OTHER INDICATIONS WERE NORMAL.Jun 23, 2003 · N681CA · Boeing 7272S7 · Compressor Bleed ControlSDR C1HA200385004Fuel Control · malfunctionedNR 1 ENGINE NOT MAKING TAKE-OFF POWER. NR 1 2.07 EPR NR 2 AND NR 3 AT 2.15 EPR ALL OTHER INDICATIONS REFLECT SAME POWER DIFFERENCE. NR 1 SLIGHTLY LOWER N1, N2, EGT. ABORTED TAKEOFF IAW AOM -SMAC PROCEDURES 4.51.28Jun 20, 2003 · N685CA · Boeing 7272S7 · Fuel Controlling SystemSDR C1HA200392002Compressor · stalledON POWER UP 1.4 EPR CHECK NR 3 ENGINE COMPRESSOR STALL FOLLOWED BY EPR FLUCTUATION APPROX .2 TO .3. ALL OTHER ENGINE INDICATIONS NORMAL.Jun 16, 2003 · N292AS · Boeing 727212 · Turbine Engine Compressor SectionSDR CA030611002Pcu · broken(CAN) DURING LANDING THROUGH APPROXIMATELY 60 KNOTS, AIRCRAFT EXPERIENCED A COMPLETE LOSS OF 'A' SYSTEM HYDRAULICS. (NOTE: 'A' PUMPS ON WITH LOW PRESSURE LIGHTS ILLUMINATED - MAX 1.5 MINUTES) MAINTENANCE INSPECTION REVEALED POSITION NR 1 LOWER AILERON PCU FILTJun 9, 2003 · Boeing 737281 · Aileron Control SystemSDR AUS20030568Skin · separated(AUS) LT INBOARD FOREFLAP UPPER SKIN DISBONDED AND SEPARATED. SIZE OF DISBONDED PIECE APPROXIMATELY 355.6MM BY 177.8MM (14IN BY 7IN). SUSPECT CAUSED BY FOREIGN OBJECT LODGED BETWEEN FOREFLAP AND WING UPPER SURFACE. FOD.Jun 3, 2003 · Boeing 727281 · Trailing Edge FlapsSDR CA030528003Selector Valve · faulty(CAN) ON APPROACH THE CREW REPORTED THE NOSE GEAR DID NOT UNLOCK OR EXTEND ON THE INITIAL EXTENSION ATTEMPT. THE GEAR HANDLE WAS RECYCLED AND THE NOSE GEAR CAME DOWN NORMALLY. IT WAS DECIDED TO OPERATE THE AIRCRAFT UNDER A FLIGHT PERMIT (FERRY PERMIT) FOR TRMay 25, 2003 · Boeing 7372T2 · Landing Gear SelectorSDR DHL2003781003Engine · malfunctionedRTO: 158,500 LBS, 80 KTS, 26 DEGREE C, 570 FT PA, BRAKE ENERGY ZONE NORMAL. ENGINE NR 3 WOULD NOT MAKE T/O THRUST 2.04 ACTUAL EPR 2.16 TARGET 93 PERCENT N, ACTUAL, 100 DEG TARGET, EGT 645 DEG (FF 10,000). ENGINE NR 1 AND NR 2 NORMAL 216, 218, 100 PERCENT. EMay 15, 2003 · N768AT · Boeing 727227 · Engine (Turbine/Turboprop)SDR C8GA20030013Fuel Control · out of adjustFLIGHT 717 FROM ELP TO STL. THE NR 2 ENGINE WOULD NOT ACHIEVE TAKE-OFF POWER. TAKE-OFF WAS STOPPED, AIRSPEED HAD NOT COME OFF "PEG" AT THE TIME TAKE-OFF WAS STOPPED AND ONLY MINIMAL BRAKES WERE USED. AIRCRAFT RETURNED TO BLOCKS WITHOUT INCIDENT. PERFORMED ENGIMay 13, 2003 · N89427 · Boeing 727227 · Fuel Control/Turbine EnginesSDR CA030505003Window · cracked(CAN) F/O,S NR 1 WINDOW OUTER (POSS MIDDLE) PANE CRACKED AT 31000 WINDOW SLOWLY DELAMINATED AND AFTER WE TURNED HEAT OFF WINDOW CRACKED. WINDOW REPALCED AS PER AMM.May 3, 2003 · Boeing 7372T7 · Flight Compartment WindowsSDR CA030417011Pcu · inoperative(CAN) AFTER PUSHBACK AND START, FLAP 2 SELECTED AND HYDRAULIC SYSTEM A LOW PRESSURE ILLUMINATED AND HYD QTY GUAGE DECREASED TO ZERO. MAINTENANCE FOUND THE A SYSTEM AILERON POWER CONTROL UNIT (PCU) FILTER BOWL HAD FRACTURED RESULTING IN LOSS OF HYD PRESS/FLUID.Apr 15, 2003 · Boeing 7372T5 · Aileron Control SystemSDR CH1A200393008Compressor · stalledFL310 NR 2 ENGINE COMPRESSOR STALLED DUE TO MOMENTARY FUEL STARVATION. THRUST LEVER IDLE, FUEL FLOW RESTORED TO NORMAL ALL OTHER INDICATIONS NORMAL RETURNED TO CRUISEApr 13, 2003 · N293AS · Boeing 727212 · Turbine Engine Compressor SectionSDR CH1A200392001Compressor · stalledON TAKEOFF, AN ENGINE EXPERIENCED COMPRESSOR STALL AT 1.2 EPR WINDS 300 AT 5. NO OTHER INDICATIONSApr 11, 2003 · N292AS · Boeing 727212 · Turbine Engine Compressor SectionSDR SROM200300022Indicator · failedDURING CLIMB THE NR 2 MACH/AIRSPEED INDICATOR FAILED WITH FLAG PRESENT. RETURNED TO DEPARTURE AIRPORT. DURING APPROACH, JUST PRIOR TO TOUCH DOWN FLAG WENT AWAY AND INDICATOR BEGAN WORKING PROPERLY. REPLACED AIRSPEED/MACH INDICATOR. GROUND FUNCTION CHECKED OApr 7, 2003 · N733PA · Boeing 737205 · Airspeed/Mach IndicatorSDR CH1A200381011Receiver · inoperativeDURING FLIGHT WEATHER, RADAR WOULD TEST BUT NOT PAINT WEATHER. DIVERTED INTO MCO TO REPAIR WEATHER RADAR.Apr 5, 2003 · N681CA · Boeing 7272S7 · Weather Radar SystemSDR CH1A200381010Engine · stalledON TAKEOFF ROLL NR 2 ENGINE COMPRESSOR STALLED NR 2 EPR DROPPED TO 1.2 AUTO PACK TRIP SYSTEM ACTIVATEDMar 27, 2003 · N681CA · Boeing 7272S7 · Engine (Turbine/Turboprop)SDR CH1A200394006Engine · stalledCOMPRESSOR STALL ENGINE NR 2 AT BEGINNING OF TAKEOFF ROLL EPR APPROX 1.3Mar 27, 2003 · N294AS · Boeing 727290 · Powerplant SystemSDR DHL2003741519Floorbeam · crackedDURING (C) CHECK, FUSELAGE INTERIOR FLOORBEAMS BS 640 AND BS 660 SPLICE PLATE TO MCD LWR. BEAMS ARE CRACKED 2 EACH NDT CONFIRMED.CA: 1) REMOVED FWD. PIT LT UPPER SIDEWALL GILLINER SUPPORTS FROM BS 580 TO 680. REMOVED LWR JAMB WEB ANGLE LWR EDGE FOR WEB REMMar 25, 2003 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR CH1A200395008Engine · malfunctionedTAKE OFF ROLL, ENGINES WERE SPOOLED TO 1.4 EPR BRAKES WERE RELEASED AND EPR POWER WAS ABOUT 1.8 WHEN A DIFINITE LOUD VIBRATION WAS HEARD AND FELT. NR 2 N2, N1, AND EPR JUMPED ABRUPTLY AND AUTO PACK TRIP OCCURED. TAKE OFF ABORTED AND RETURNED TO GATE SPEED =Mar 24, 2003 · N295AS · Boeing 727290 · Engine (Turbine/Turboprop)SDR CH1A200382005Compressor · stalledON APPROACH TO LAS AT 500FT, NR 2 ENGINE COMPRESSOR STALLED. DID NOT USE NR 2 REVERSER. FLT ATTND REPORTED COMP STALL ON ROLL OUTMar 24, 2003 · N682CA · Boeing 7272S7 · Turbine Engine Compressor SectionSDR 2003F00264Dome · damagedNR 2 ENGINE WENT INTO A CONTINUOUS COMPRESSOR STALL SHORTLY AFTER LANDING GEAR RETRACTIONON TAKEOFF AT MSP. EGT CLIMBED INTO AND STABILIZED IN THE RED ARC FOR 1 MINUTE, RETARDED ENGINE THROTTLE TO IDEL POSITION AND ENGINE STABILIZED, ALL OTHER SYSTEMS NORMAL.Mar 21, 2003 · N919PG · Boeing 727200 · Turbine Engine Compressor SectionSDR 2003F00330Engine · stalledNR 2 ENGINE WENT INTO A CONTINUOUS COMPRESSOR STALL SHORTLY AFTER LANDING GEAR RETRACTION ON TAKEOFF AT MSP. EGT CLIMBED INTO AND STABILIZED IN THE RED ARC FOR 1 MINUTE, RETARDED ENGINE THROTTLE TO IDLE POSITION AND ENGINE STABILIZED, ALL OTHER SYSTEMS NORMALMar 21, 2003 · N919PG · Boeing 727200 · Engine (Turbine/Turboprop)SDR DHL2003741517Skin · damagedDURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS PILLOWING BETWEEN BS 294 AND 312 AT STR. 24 R. REMOVED RT FLOOR PANEL IN DOG HOUSE FOR ACCESS STA. 294 TO 330 RBL 30 IAW B-727 SRM 51-30-3. 2) CUT-OUT 2 EACH DAMAGE AREA 5 INCHES X 1.7500 INCH OF 8 INMar 20, 2003 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2003741518Skin · dentedDURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS DENTS AT BS 1090 STR'S 18, 19, AND 20 L. C/A: 1) REMOVED PAINT I.A.W. B-727 M.M. 51-20-01. 2) EVALUATE 5 EACH DENTS, 2 EACH OUT OF LIMITS, 3 EACH IN LIMITS WITH A/Y RATIOS OF 1/.013 =76, .6/.009 = 66Mar 20, 2003 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR CH1A200383006Bleed ValveEngine #3 had a compressor stall on approach at 1.2 EPR at 4000 ft and 180 KTSMar 16, 2003 · N683CA · Boeing 7272S7 · Compressor Bleed GovernorSDR CA030318018Actuator · leaking(CAN) DURING CRUISE THE AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC FLUID. THE AIRCRAFT WAS DIVERTED TO WHERE EMERGENCY VEHICLES MET THE AIRCRAFT ON LANDING.THE LOSS OF FLUID WAS ATTRIBUTED TO THE NR 2 FLIGHT SPOILER ACTUATOR. THE ACTUATOR IS BEING TESTED AND ASSMar 15, 2003 · Boeing 737217 · Drag Control ActuatorSDR CA030327003Bearing · failed(CAN) DURING CLIMB IN MANUAL FLIGHT , BEOND 5 DEG. LT WHEEL DEFLECTION AILERONS FELT VERY HEAVY 9 AS IF IN MANUAL REVERSION ) AT THIS POINT IN TIME RUDDER TRIM 0 UNITS AND ADI BALL CENTERED. AILERON TRIM 1/2 UNIT LT IN STABLE CRUISE. AILERON TOWER SHAFT UPPER Mar 12, 2003 · Boeing 7372T7 · Aileron Control SystemSDR CA030313007Engine · failed(CAN) FLIGHT 41, NR 1 ENG FAILURE ON CLIMBOUT SHORTLY AFTER TAKEOFF THROUGH 3200 FT ASL, CREW HEARD A BANG FROM NR 1 ENG AFTER CLIMB THRUST WAS SET & FLAPS HAD RETRACTED. CREW IDENTIFIED PROBLEM AS NR 1 ENG NOT PRODUCING THRUST & THE 'EGT' WAS PEGGED HIGH OFFMar 11, 2003 · Boeing 737281 · Turbine SectionSDR GTIA030115Sign · inoperativeTAILCONE INTERIOR LUMINESCENT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED TAILCONE INTERION LUMINESCENT EXIT SIGN. OPS CHECK GOOD.Mar 2, 2003 · N130NK · Doug DC941 · Emergency LightingSDR GTIA030116Flashlight · inoperativeFORWARD F/A HANDHELD EMERGENCY LIGHT, INOPERATIVE. REMOVED AND REPLACED FWD HANDHELD EMERGENCY LIGHT. OPS CHECK GOOD.Mar 2, 2003 · N130NK · Doug DC941 · Emergency EquipmentSDR BJNA030219Skin · corrodedDURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED ON NR 2 ENGINE INBOARD COWLING. CORROSION WAS LOCATED UNDERNEATH THE FIRE SEAL AREA THROUGHOUT THE FORWARD AND AFT SECTION. REMOVED FIRE SEAL FOR ACCESS TO THE CORRODED SECTION OF SKIN. REMOVEFeb 27, 2003 · N789TM · Boeing 737282 · Nacelle/Pylon, Plate/SkinSDR BJNA030218Stringer · corrodedDURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON STRINGER 26 RIGHT, LOCATED AT BS 980. REMOVED THE CORRODED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR SECTION AND STRINGER SPLICE IAW WITH SRM.Feb 27, 2003 · N789TM · Boeing 737282 · Fuselage Main, Longeron/StringerSDR BJNA303217Frame · corrodedDURING A SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS DISCOVERED IN THE AFT CARGO PIT ON A FRAME MEMBER LOCATED AT BS787 BETWEEN STRINGERS 22 AND 24 LEFT.Feb 27, 2003 · N789TM · Boeing 737282 · Fuselage Main, FrameSDR AUS20030312Drive Shaft · failed(AUS) NR 1 ENGINE TOWER DRIVE SHAFT FAILED.Feb 27, 2003 · Boeing 7272J4 · Turbine Engine Accessory Drive
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