Pratt & Whitney JT8D-219

Service difficulty reports · 1,944

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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 = 'JT8D219'
  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 ASMF200703009Engine · flamed outAIRCRAFT AIR TURNBACK DUE TO A FLAME OUT ON LT ENGINE DURING CLIMB. DURING MAINTENANCE INSPECTION DETECTED THE C1 STUCK AND CONSIDERABLE DAMAGES ON LPT. THE LT ENGINE WAS REPLACED IAW MPCM 71-00-02, TESTED CORRECT IAW 71-00-01. LANDING AIRCRAFT WEIGHT WAS 1Mar 27, 2007 · N755RA · Doug DC987 · Engine (Turbine/Turboprop)SDR ASMF200703006Seal · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN AN UPPER PANEL OF THE LT WING. MAINTENANCE PERSONNEL RELOCATED THE SEAL AND APPLIED SEALANT IAW SRM 51-20-04 AND 51-22-2A, LEAK WAS CORRECTED. AS A PRECAUTIONARY ACTION, DURING OVERNIGHT CHECK THE SEAL WAS REPMar 17, 2007 · N803ML · Doug DC987 · Wing, Plate/SkinSDR ASMF200703005Apu · failedAIRCRAFT RETURNED DUE TO FUEL ODOR IN THE CABIN AT 28,000 FEET. THE UPPER AND LOWER WING PANELS AND APU WERE CHECKED AND NO LEAKS WERE DETECTED. NEVERTHELESS, THE AIR CONDITIONING WATER SEPARATORS AND ENGINES WERE CHECKED BY CONDITION AND LEAKS AND NO ODOR NEIMar 12, 2007 · N169PL · Doug MD88 · APU Core EngineSDR FE5F200700001Engine · surgesB-28025(SN:53602), 0345(UTC) DEPARTING FROM RCTP (TPE TAIWAN), CLIMBING THROUGH 11000 NR,ENCOUNTERING SURGING CONTINUALLY, A/T OFF, LT THROTTLE IDLE AND ADJUST TO EPR 1.4 AND INSTRUMENT SHOWING STABLE, READJUST EPR TO 1.75 ,SURGING HAPPENED AGAIN. REQUESTED APMar 11, 2007 · N28025 · Doug MD83 · Turbine SectionSDR ASMF200703003Skin · dentedDURING TRANSIT CHECK, A DENT WAS DETECTED IN THE RT STATIC PORT AREA. DENT WAS LOCATED AT STATION 389 AND LONGERONS 25 AND 26 RT SIDE AND WAS INSPECTED IAW MM 34-11-01, BEING WITHIN LIMITS.Mar 10, 2007 · N216AM · Doug DC987 · Fuselage Main, Plate/SkinSDR ASMF200703001Line · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE AFT CARGO COMPARTMENT. DURING MAINTENANCE CHECK, THE AFT RT CARGO COMPARTMENT WALLS WERE REMOVED, DETECTING A HYDRAULIC LEAK IN THE HYDRAULIC LINE. THE HYDRAULIC LINE WAS REPLACED IAW MM 20-10-13, TESTMar 1, 2007 · N158PL · Doug MD88 · Hydraulic System, MainSDR ASMF200702008Fuel Control · failedAIRCRAFT RETURNED TO PLATFORM DUE TO RT ENGINE DID NOT ACCELERATE. THE PARAMETERS WERE RT ENGINE N2 54 PERCENT, N1 29 PERCENT AND LT ENGINE N2 56 PERCENT, N1 26 PERCENT, EGT 472 RT AND 462 LT AND FUEL FLOW 87 RT AND 53 LT. AIRCRAFT WAS SENT TO THE HANGAR AND DFeb 27, 2007 · N169PL · Doug MD88 · Fuel Control/Turbine EnginesSDR ASMF200702007Actuator · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE LT SLAT ACTUATOR. THE SLAT ACTUATOR WAS REPLACED IAW MM 27-80-05, TESTED CORRECT.Feb 18, 2007 · N158PL · Doug MD88 · Leading Edge Slat ActuatorSDR AALA20070364Blade · failedDFW INFLIGHT T1511/18FEB - DURING CLIMB, LEFT ENGINE SPOOLED TO IDLE POWER WITH EXCESSIVE VIBRATION AND ENGINE GAS TEMPERATURE AT 800 DEGREES. SHUT DOWN LEFT ENGINE AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT ENGINE DUE TO COMPRESSOR BLADE FAILURE. SYSTFeb 18, 2007 · N562AA · Doug DC983 · Turbine Engine Compressor SectionSDR ASMF200702006Unknown · unknownCAPTAIN REPORTED THAT A GEN LOW AND TAIL COMP TEMP HIGH LIGHTS TURNED ON. DURING MAINTENANCE CHECK, THE TAIL CONE COMPARTMENT WAS DETECTED WITH HIGH TEMPERATURE AND THE FIRE EXTINGUISHER CONTAINER ACTIVATED. AIRCRAFT WAS SENT TO THE HANGAR AND RT FIRE EXTINGUIFeb 15, 2007 · N803ML · Doug DC987 · AC Generation SystemSDR ASMF200702005Proximity Switch · failedCAPTAIN REPORTED THAT 3 RED LANDING GEARS LIGHTS TURNED ON DURING CLIMB AND CRUISE. PROXIMITY SWITCH COMPUTER WAS TESTED, CIRCUIT BREAKER WAS RESEATED, LANDING UP SENSORS AND CONNECTORS WERE CHECKED, ALL CORRECT. DURING TRANSIT CHECK AT GDL, THE PROXIMITY SWITFeb 13, 2007 · N754RA · Doug DC987 · Landing Gear Position and WarningSDR ASMF200702004Fuel Control · failedAIRCRAFT RETURNED TO PLATFORM, LT ENGINE DID NOT STABILIZE IN IDLE, THE PARAMETERS WERE THE FOLLOWING: EPR´S 1.03, N1 20, EGT´S 486 DEGREE C, N2 44, FF 9700 POUND. LT ENGINE WAS TRIMMED IN IDLE WITH EPR´S 1.03, N1 27, EGT´S 460, N2 55, FF 1160 IAW MM 71-00-00Feb 12, 2007 · N169PL · Doug MD88 · Fuel Control/Turbine EnginesSDR AALA20070316Fuel · contaminatedDFW INFLIGHT SAT-ORD, AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKER POPPED. UNABLE TO TRANSFER FUEL FROM CENTER TANK. LANDED DFW WITHOUT INCIDENT. SUMPED THREE GALLONS OF WATER OUT OF CENTER TANK. SYSTEM GROUND CHECKED NORMAL OPERATION.Feb 11, 2007 · N110HM · Doug DC983 · Engine Fuel DistributionSDR ASMF200702003Seal · brokenAIRCRAFT RETURNED, DURING TAKEOFF, THE NOSE LANDING GEAR DID NOT RETRACT, TRANSPONDER DID NOT WORK AND PRESSURIZATION FAILED. ADDITIONALLY, STABILIZER, SPOILERS AND AUTOBRAKES LANDING GEAR ALARMS WERE ACTIVATED, AS WELL AS A STRONG NOISE IN THE NOSE LANDING GEFeb 4, 2007 · N161PL · Doug MD88 · Main Landing Gear Strut/Axle/TruckSDR DLM8K070082Engine · making metalNR TWO ENG LOUD BAND ON TAKEOFF ROLL. METAL FOUND IN TAIL PIPE. FOUND SMALL METAL PARTICLES IN TAIL PIPE. REPLACED NR 2 ENG PER TRANSMITAL CARDS.Feb 4, 2007 · N915DE · Doug MD88 · Engine (Turbine/Turboprop)SDR ASMF200702001Unknown · unknownAIRCRAFT RETURNED, NOSE LANDING GEAR DID NOT RETRACT. LUBRICATION SERVICE TO NOSE LANDING GEAR STRUT WAS ACCOMPLISHED IAW MM 32-21-02. CABLES, PULLEYS AND CONNECTIONS WERE CHECKED AND LUBRICATION WAS ACCOMPLISHED, ALL CORRECT. OVER WEIGHT INSPECTION WAS NOT NEFeb 3, 2007 · N161PL · Doug MD88 · Nose/Tail Landing GearSDR ASMF200702002Skin · damagedDURING OVERNIGHT CHECK AND ACCOMPLISHMENT OF EO 985362, A CRACK OF .1250 LENGTH AT STA Y 198 BETWEEN LONGERONS L20L AND L21L, WAS DETECTED ON THE MAIN STAIRS DOOR. DAMAGED SKIN SECTION WAS REMOVED AND A DOUBLER (PERMANENT REPAIR) WAS INSTALLED IAW SRM 53-05 FIFeb 3, 2007 · N216AM · Doug DC987 · Fuselage Main, Plate/SkinSDR ANCF200600045Engine · malfunctionedON TAKEOFF LT ENGINE PARAMETER DROOPED & EGT RAISED UP TO 610. POWER REDUCED AND EPR 1.61 N1 57 PERCENT N2 62 PERCENT ADVANCING LT THROTTLE THERE WAS NO REACTION AND ENGINE WAS SHUTDOWN. 2 MINUTES BEFORE LANDING, OIL PRESSURE NORMAL, OIL TEMP NORMAL. IAW AMFeb 2, 2007 · N160BS · Doug DC983 · Engine (Turbine/Turboprop)SDR DLM88070067Apu · odorAFTER TAKEOFF EXPERIENCED SMOKE IN CABIN AND COCKPIT OIL SMELL, APU WAS OPERATING. REPLACED APU PER TRANS 9T103. PERFORMED PNEUMATIC DIST CABIN SMOKE ODOR TROUBLESHOOTING PER OPN 5088. PERFORMED DUCT BU OUT PER OPN 5089.Feb 1, 2007 · N965DL · Doug MD88 · APU Core EngineSDR ASMF200701007Blade · nickedDURING TRANSIT CHECK, A BLADE WAS DETECTED DAMAGED DUE TO A FOD IN RT ENGINE. A NICK WAS DETECTED AT 2.5 INCHES BETWEEN PLATFORM AND MIDSPAN SHROUD OF 1 INCH LONG WITH .1250 INCH DEPTH. THE BLADE WAS REWORKED IAW MM 72-33-21 AND BOROSCOPIC INSPECTION WAS PERFOJan 29, 2007 · N216AM · Doug DC987 · Turbine Engine Air Inlet SectionSDR DLM88070053Engine · leakingLEFT ENG OIL QTY DROPPED TO ZERO. THE ENG WAS SHUT DOWN WHEN THE OIL PRESS WAS AT 35 PSI. THE ENG WINDMILLED FOR 10 MINS AT ZERO OIL PRESS. REPLACED ENGINE NR 1 PER TRANSMITTAL 9T102.Jan 24, 2007 · N990DL · Doug MD88 · Turbine Engine Oil SystemSDR ASMF200701006Inlet · obstructedCAPTAIN REPORTED SMOKE ODOR IN THE CABIN. AIR CONDITIONING SYSTEM WAS SHUTDOWN AND APU DOORS WERE CHECKED, DETECTING A PLASTIC IN THE APU INLET. PLASTIC WAS REMOVED AND WATER SEPARATORS WERE REPLACED IAW MM 21-20-2, TESTED CORRECT. DURING BOARDING, CAPTAIN REPJan 23, 2007 · N169PL · Doug MD88 · APU Core EngineSDR ASMF200701005Fairing · damagedAIRCRAFT WAS HIT IN THE RT LOWER WING BY A BAGGAGE CONVEYOR, CAUSING A DAMAGE OF 2 X 2 INCHES WITH .3125 INCH DEPTH IN THE MLG FAIRING. DUE, IT WAS A NON PRESSURIZED AREA, HI-SPEED TAPE WAS INSTALLED IAW MGMYPTA 10-24-1 AND AIRCRAFT WAS DISPATCHED. DURING OVEJan 14, 2007 · N158PL · Doug MD88 · Aerodynamic FairingsSDR ASMF200701003Indicator · failedCAPTAIN REPORTED THAT LT AIRSPEED INDICATOR SHOWED MACH 0.50, SO AIRSPEED INDICATOR WAS REPLACED IAW MM 34-13-01, TESTED CORRECT. AIRCRAFT WAS DISPATCHED BUT REJECTED TAKEOFF AT 80 KNOTS DUE TO LT AIRSPEED INDICATOR FAILED. CADC NR 1 AND 2 WERE TESTED IAW MM Jan 13, 2007 · N158PL · Doug MD88 · Airspeed/Mach IndicatorSDR ASMF200701004Relay · failedCAPTAIN REPORTED AHRS 1, 2 AND 3 BASIC MODE LIGHTS TURNED ON. AHRS 1, 2 AND 3 BREAKERS WERE RESEATED AND AHRS 1 AND 2 WORKED CORRECT BUT AHRS NR 3 FAILED, SO IT WAS DEFERRED IAW MEL 34-38. AIRCRAFT WAS DISPATCHED BUT RETURNED TO PLATFORM DUE TO THE SAME FAILURJan 13, 2007 · N754RA · Doug DC987 · Attitude Gyro and Indicating SystemSDR DLM88070027Duct · contaminatedAIRBORNE RETURN FOR SMOKE/FUMES IN CABIN. FIRST OFFICERS AFT LAV SMOKE DETECTOR ACTIVATED. MTC IN WORK DOING DUCT BURNOUT AND WASHING APU INLET. REMOVED AND REPLACED COALESCER BAGS CLEANED RESIDUAL OIL FROM APU INLET PERFORM FULL DUCT BURNOUT PER OPN 5089. Jan 12, 2007 · N917DL · Doug MD88 · Air Distribution SystemSDR DLM88070025Oil Cap · leakingDURING T/O, STRONG ODOR AND HAZE IN AFT CABIN. FOUND APU OIL CAP LEAKING AND APU INGESTED OIL. FOUND OIL LEAKING PAST OIL FILLER CAP SEAL. REPLACED CAP AND SEAL SERVICED TO FULL. CLEANED AREA LEAK CKS GOOD. REMOVED AND REPLACED COALESCER BAGS AND PERFORMJan 11, 2007 · N917DL · Doug MD88 · APU Oil SystemSDR ASMF200701002Connector · intermittentDURING TRANSIT CHECK, THE ALT LONG TRIM STABILIZER WAS OUT OF SERVICE. CIRCUIT BREAKER WAS RESEATED BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND DURING WIRING CHECK WAS DETECTED THE CONNECTOR P10-41 PIN A WITH INTERMITTENT CONTACT. PIN A WAS REPLJan 8, 2007 · N838AM · Doug DC983 · Flight Control System WiringSDR ASMF200701001Line · leakingDURING PUSH BACK, A WATER LEAK WAS DETECTED ON ELECTRICAL/ELECTRONIC COMPARTMENT AT COMPUTERS AREA. AIRCRAFT WAS SENT TO HANGAR AND DURING MAINTENANCE CHECK, A WATER LINE WAS DETECTED LEAKING ON FORWARD CARGO COMPARTMENT. THE LINE P/N H151-615 WAS REPLACED IAJan 4, 2007 · N161PL · Doug MD88 · Potable Water SystemSDR DLM8K061079Duct · blownDURING CLIMB THROUGH 6,500 MSL, FIRE DETECTOR LOOP OAP APPEARED FOLLOWED BY LEFT FIRE INDICATION. ALL INDICATIONS APPEARED NORMAL AND ENGINE WAS LEFT AT IDLE POWER PER THE QRH. NOTE ENG ANTI-ICE WAS ON. OPENED LT ENG COWL. FOUND DUCT JUST AFT OF ENG COWL ADec 30, 2006 · N911DE · Doug MD88 · Engine Anti-Icing SystemSDR ASMF200612006Line · brokenDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED ON RT HYDRAULIC SYSTEM AT BRAKE LINE. HYDRAULIC LINE WAS REPLACED IAW MM 32-42-00, TESTED CORRECT.Dec 29, 2006 · N168PL · Doug MD88 · Hydraulic System, MainSDR DLM88061076Line · leakingRT HYD QTY WENT TO 1 QT AT CRUISE FL240 QTY RETURNED TO 10 QT AFTER RT ENGINE DRIVEN HYD PUMP SHUTDOWN IAW QRH. LOST RT SYS PRESSURE DURING CONFIG FOR LANDING. USED ALTERNATE GEAR EXTENSION AND STOPPED ON RUNWAY FOUND PRESSURE FLEX LINE FROM NR 2 ENG TO PYLONDec 28, 2006 · N953DL · Doug MD88 · Hydraulic System, MainSDR ASMF200612005Display · failedAIRCRAFT RETURNED TO PLATFORM, ERRONEOUS OIL PRESSURE INDICATION IN THE RT ENGINE, IT SHOWED 60 PSI WITH INTERMITTENT LIGHT. THE PRESSURE RELIEF VALVE WAS ADJUSTED BUT THE DISPLAY SHOWED 8 PSI WITH ENGINES SHUTDOWN. BREAKERS WERE RESEATED, TESTED CORRECT. OILDec 28, 2006 · N160PL · Doug MD88 · Central DisplaySDR ASMF200612004Line · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS OBSERVED IN THE LT WING. DURING MAINTENANCE CHECK, THE LEAK WAS DETECTED IN A HYDRAULIC LINE, LOCATED AT THE EXTERIOR FLAPS ACTUATOR. THE HYDRAULIC LINE WAS REPLACED IAW MM 29-00-00 AND FLAPS WERE TESTED IAW MM 27-50-Dec 20, 2006 · N161PL · Doug MD88 · Hydraulic System, MainSDR DLM88061021Engine · failedNR 1 ENGINE INFLIGHT SHUTDOWN. EXTENSIVE DAMAGE IN TAILPIPE AREA. REMOVED AND REPLACED NR 1 ENG PER TRANS 9T102.Dec 12, 2006 · N925DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DL764061023Engine · odorFLT ATTENDANT REPORTED A SMOKE SMELL IN CABIN CREW SHUTDOWN RECIRC FAN AND SMOKE SEEMED TO START CLEARING, INFO FROM RADIO PATCH LOG. RAN ENGS, NOTICED ODOR WHEN RUNNING RT ENG PERFORMED. CONTAMINATION REMOVAL FOR AIR SYS FROM RT ENG PER MM 21-00-21-102-001 Dec 12, 2006 · N843MH · Boeing 767432ER · Air Distribution SystemSDR ASMF200612003Cadc · failedAIRCRAFT REJECTED TAKEOFF AT 90 KNOTS DUE TO A 15 KTS OF DIFFERENCE BETWEEN SPEED INDICATORS. CADC AND RT AIR SPEED INDICATOR WERE REPLACED IAW MM 34-16-01 AND 34-13-01, TESTED CORRECT.Dec 11, 2006 · N583MD · Doug DC983 · Airspeed/Mach IndicatorSDR DLM88061013O-Ring · cutBOTH AFT SMOKE DETECTORS SOUNDED JUST AFTER TAKEOFF F/A REPORTED SMOKE AND FUME SMELL IN AFT CABIN. FOUND APU OIL CAP O-RING BAD. REPLACED OIL CAP PERFORMED. ALSO OPN 5089 DUCT BURNOUT. REPLACED COALESCER BAGS SYS NOW OK.Dec 9, 2006 · N990DL · Doug MD88 · APU Oil SystemSDR AALA20061194Blades · damagedORD - ON TAKE OFF, AIRCRAFT YAWED TO THE RIGHT. FLIGHT ATTENDANTS REPORTED LOUD PBP BEFORE FLIGHT CREW ABORTED TAKEOFF. BRAKE TEMPERATURES DID NOT EXCEED 150 DEGREES. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. REPLACED NUMBER THREE AND FOUR MAIN LANDINGDec 6, 2006 · N436AA · Doug DC983 · Turbine Engine Compressor SectionSDR ASMF200612001Pump · leakingAIRCRAFT RETURNED DUE TO RT HYDRAULIC SYSTEM LOST. DURING MAINTENANCE CHECK, THE HYDRAULIC CONTAINER WAS EMPTY AND WITH A DRIP IN THE RT AFT CARGO COMPARTMENT. AIRCRAFT WAS SENT TO THE HANGAR AND A BROKEN LINE IN THE RT HYDRAULIC SYSTEM MODULE AND (3) CLAMPS WDec 2, 2006 · N216AM · Doug DC987 · Hydraulic Pump (Electric/Engine), MainSDR ASMF200611010Line · leakingCAPTAIN REPORTED LT REVERSE VERY HARD TO OPERATE. DURING MAINTENANCE CHECK WAS OBSERVED THAT THE LT HYDRAULIC QUANTITY WAS 9 QUARTERS AND THE LT REVERSE CONTROL VALVE HYDRAULIC LINE HAD A LEAK. THE HYDRAULIC LINE WAS REFASTENED BUT LEAK CONTINUED, SO IT WAS RENov 25, 2006 · N160PL · Doug MD88 · Hydraulic System, MainSDR ASMF200611009Skin · corrodedDURING OVERNIGHT CHECK, CORROSION WAS DETECTED IN THE CARGO COMPARTMENT LOWER FUSELAGE SKIN RT SIDE AT STA 1271 AND LONGERON 29. THE NON ROUTINE CARD NR A0103766 WAS ISSUED AND CORROSION WAS REPAIRED IAW MFG MESSAGE NR 1-254115121-2.Nov 24, 2006 · N161PL · Doug MD88 · Fuselage Main, Plate/SkinSDR ASMF200611008Actuator · failedCAPTAIN REPORTED THAT AFTER TAKEOFF AT GDL THE (AUTO SLATS FAIL) LIGHT TURNED ON IN LOW SPEED (150-230 KIAS) AND FLIGHT CONTROLS WITH VIBRATION. THE STALL COMPUTERS WERE TESTED AND SLATS ACTUATORS FAILED IN BOTH COMPUTERS. AIRCRAFT WAS SENT TO THE HANGAR AND Nov 18, 2006 · N583MD · Doug DC983 · Leading Edge Slat ActuatorSDR MWEA060294Coupling · rupturedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. REPLACED COUPLING AND PERFORMED LEAK CHECK GOOD.Nov 13, 2006 · N701ME · Doug MD88 · Air Distribution SystemSDR MWEA060296Angle · damagedDAMAGE ON AFT CARGO DOOR THRESHOLD VERTICAL CHORD AT Y 1184 LONGERON 29 RT, IB SIDE. FABRICATED AND INSTALLED ANGLE.Nov 13, 2006 · N601ME · Doug MD88 · Fuselage Main, Attach FittingsSDR ASMF200611006Transmitter · brokenCAPTAIN REPORTED A BIRD STRIKE IN THE RT SIDE OF FUSELAGE. A BIRD STRIKE INSPECTION WAS PERFORMED IAW MM 05-51-08 DETECTING BROKEN THE RT ANGLE ATTACK TRANSMITTER . RT TRANSMITTER WAS REPLACED IAW MM 34-19-01, TESTED CORRECT.Nov 12, 2006 · N158PL · Doug MD88 · Stall Warning SystemSDR MWEA060292Skin · dentedDENT IN CARGO PIT DOOR SKIN.Nov 10, 2006 · N601ME · Doug MD88 · Cargo/Baggage DoorsSDR MWEA060293Tab · delaminatedLT ELEVATOR CONTROL TAB DELAMINATED TOP SURFACE 36 INCH FROM IB END, 7 INCH FROM TRAILING EDGE.Nov 10, 2006 · N601ME · Doug MD88 · Elevator, Tab StructureSDR MWEA060291Skin · gougedFUSELAGE SKIN IS GOUGED AT Y 698 AT LONGERON 27 LT.Nov 9, 2006 · N601ME · Doug MD88 · Fuselage Main, Plate/SkinSDR ASMF200611005Computer · failedAIRCRAFT RETURNED TO PLATFORM, BOTH FLIGHT DIRECTORS WERE OUT OF SERVICE AND THE (FAST/SLOW) LIGHT TURNED ON IN BOTH PFDS. BOTH DFGC´S WERE RESEATED BUT FAILURE CONTINUED WITH THE FOLLOWING MESSAGES: DFGC NR 1, AIL MECH TORQ SW FLAP NR 1 FAILURE, WINDSHEAR DATNov 9, 2006 · N168PL · Doug MD88 · Autopilot System
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