Pratt & Whitney JT8D-219

Service difficulty reports · 1,944

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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 = '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 DLM88060931Battery Pack · inoperativeEMERGENCY TRACK LIGHTING INOP AFT OF ROW 30. REMOVED AND REPLACED BATTERY PACK ASSY OPS CHECK NORMALNov 8, 2006 · N957DL · Doug MD88 · Emergency LightingSDR AMF200611004Boot · looseDURING TRANSIT CHECK, CAPTAIN REPORTED A FUEL LEAK AT THE MAIN LANDING GEAR WELL. DURING MAINTENANCE CHECK, A FUEL LEAK WAS DETECTED ON THE RT WING UPPER PANEL (1414C), SO PANEL WAS REMOVED DETECTING THE AUXILIARY TANK DRAIN BOOT LOOSE. BOOT WAS CORRECTLY INSTNov 8, 2006 · N158PL · Doug MD88 · Aircraft Fuel Distribution SystemSDR ASMF200611003Blade · fodDURING TRANSIT CHECK, A LEFT ENGINE BLADE WAS DETECTED DAMAGED WITH 1INCH LENGTH, 0.640 INCH WIDTH IN THE MIDSPAN AND 0.359 INCH DEPTH. THE FIRST STAGE BLADES SET WAS REPLACED IAW MM 72-33-21, PAGE 401 AND ENGINE VIBRATION CHECK WAS PERFORMED IAW MM 72-00-00, Nov 6, 2006 · N205AM · Doug DC987 · Engine (Turbine/Turboprop)SDR ASMF200611002Csd · failedAIRCRAFT RETURNED DUE TO HIGH TEMPERATURE IN THE LT CSD AND APU DID NOT START AT 34,000 FEET. DURING OVERNIGHT CHECK, LT CSD AND HEAT EXCHANGER WERE REPLACED IAW MM 24-10-01 AND 24-10-03, AS WELL AS TRIM AND TEST WERE PERFORMED TO THE APU IAW MM 49-00-00, ALL Nov 2, 2006 · N803ML · Doug DC987 · Alternator-Generator DriveSDR ASMF200610013Panel · leakingDURING TRANSIT CHECK, CAPTAIN REPORTED A FUEL LEAK ON THE RT WING. DURING MAINTENANCE CHECK, A LEAK WAS DETECTED IN THE RT WING UPPER PANEL. TWO NUTS WERE REPLACED IAW SRM 51-30-2 AND PANEL WAS SEALED AGAIN, TESTED CORRECT.Oct 30, 2006 · N205AM · Doug DC987 · Wing, Plate/SkinSDR DLM88060891Wire · burnedDURING ROTATION ON TAKEOFF, HAD A FLASH OF LIGHT IN VINCINITY OF CAPT RUDDER PEDALS AREA. ONCE AIRBORNE FOLLOWING C/B'S POPPED PEDESTAL LIGHTS, FLT RECORDER AND RT ENG IGN. MTC IN PROGRESS, FOUND WIRE BUNDLE THAT RUNS UNDER CAPTS FEET HAS NUMEROUS WIRES BURNOct 28, 2006 · N932DL · Doug MD88 · Electrical Power System WiringSDR ASMF200610012Powerplant · power lossAIRCRAFT REJECTED TAKEOFF AT 40 KNOTS DUE TO THE LT ENGINE DID NOT ACCELERATE MORE THAN 1.2 EPR’S. AT PLATFORM, ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. DURING OVERNIGHT CHECK, ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00 AND 71-00-01, Oct 28, 2006 · N583MD · Doug DC983 · Engine (Turbine/Turboprop)SDR ASMF200610011Transmitter · failedAIRCRAFT REJECTED TAKEOFF AT 60 KNOTS, THE LT ENGINE DID NOT ACCELERATE MORE THAN 1.2 EPR’S, WITH THRUST LEVERS TOTALLY FORWARD, EGT INCREASED TO 570 DEGREE (C) AND N1 AND N2 WERE NORMAL. AIRCRAFT WAS SENT TO THE HANGAR AND ENGINE WAS TESTED IAW MM 71-00-00, EOct 27, 2006 · N216AM · Doug DC987 · Engine Pressure Ratio (EPR)SDR AALA20060937Engine · leakingSTL INFLIGHT T2243/25OCT ON ROTATION HEARD LOUD NOISE. OIL QUANTITY AND OIL PRESSURE WENT TO ZERO ON NUMBER ONE ENGINE. SMOKE STARTED TO APPEAR IN CABIN. RETURNED TO STL AND LANDED WITHOUT INCIDENT. LEFT ENGINE WAS SHUT DOWN UPON LANDING. REPLACED NUMBEROct 25, 2006 · N459AA · Doug DC982 · Engine (Turbine/Turboprop)SDR DLM88060884Tee Fitting · damagedDURING THE CURRENT MTC CHECK EO 09-086680-12 WAS BEING ACCOMPLISHED AND THE REPLACEMENT PRESSURE BULKHEAD TEE CHORD WAS FOUND TO HAVE SHORT EDGE MARGIN ON EXISTING FASTENERS DURING INSTALLATION. DUE TO THIS, A TITANIUM REPAIR STRAP APPROVED BY MFG IS INSTALLEOct 24, 2006 · N935DL · Doug MD88 · Fuselage Main, BulkheadSDR ANCF200600040Pump · failedDURING CLIMB, RT HYDRAULIC PRESSURE DROPPED TO (0) PSI AND QUANTITY GOES UP TO 19 QTY. IAW AMM 29-10-14/201 THE FILTER WERE CHECKED AND BLED AND SYSTEM AND CHECKED HYD LEVEL IAW AMM 12-13-01. THE RT ENGINE DRIVEN HYD PUMP WAS DEFERED TO DMI 849 IAW MEL 29-5 Oct 23, 2006 · N583AN · Doug MD83 · Hydraulic Pump (Electric/Engine), MainSDR DLM88060882Actuator · leakingATL TOWER REPORTS SMOKE COMING FROM LEFT ENGINE ON LANDING. FOUND LEFT ENG THRUST REV ACT LEAKING. FOUND LEFT ENG I/B THRUST REVERSER ACTUATOR LEAKING. REPLACED SAME PER M/M.Oct 22, 2006 · N956DL · Doug MD88 · Engine Thrust ReverserSDR ASMF200610010Wire · brokenAIRCRAFT RETURNED TO PLATFORM, (RUDDER TRAVEL UNRESTRICTED) LIGHT REMAINED OFF. PROXIMITY SWITCH WAS REPLACED AND TESTED, BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND WIRING WAS CHECKED, DETECTING A SENSOR LINE BROKEN. WIRING SENSOR WAS REPAIRED Oct 17, 2006 · N205AM · Doug DC987 · Flight Control System WiringSDR MWEA060240Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT Y 158 TO Y 200 X 7.Oct 15, 2006 · N701ME · Doug MD88 · Fuselage Miscellaneous StructureSDR ASMF200610008Engine · making metalAIRCRAFT RETURNED, DUE TO LOW OIL PRESSURE ON LT ENGINE. CAPTAIN REPORTED THAT DURING DESCENT THE TEMPERATURE REACHED 630 DEGREE (C) AND VIBRATION WAS PRESENT, LT ENGINE WAS SHUTDOWN. DURING MAINTENANCE CHECK, METALLIC CHIPS WERE DETECTED ON ENGINE CHIP DETECTOct 15, 2006 · N861LF · Doug MD83 · Engine (Turbine/Turboprop)SDR ASMF200610007Cadc · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO (F/S FAIL) AND (TRI FAIL) FLAGS WERE SHOWN IN THE LT FLIGHT DIRECTOR. CADC NR 1 WAS RESEATED, BUT FAILURE CONTINUED, THE CADC NR 2 WAS RESEATED, ALL CORRECT. CADC NR 1 WAS REPLACED IAW MM 34-16-01, BUT (MACH) AND (LT ALTIMEOct 13, 2006 · N754RA · Doug DC987 · Air Data ComputerSDR DLM88060847Feeder Cable · damagedDURING THE PREFLT RUN OF SHIP 921, THE APU GENERATOR KICKED Z OFF LINE. FOUND AFTER LOOKING INTO THE PROBLEM, WAS 2 OF THE MAIN GENERATOR FEEDER CABLES AFT OF THE P DOME (AFT) WERE DAMAGED WHERE THEY RUN THROUGH A CLAMP. THIS LOOKS AS IF IT WAS CAUSED BY THEOct 13, 2006 · N921DL · Doug MD88 · Electrical Power System WiringSDR DLM88060836Support Fitting · corrodedTHE LT AND RT MLG RETRACT ACTUATOR SUPPORT FITTING BORE DIAMETERS WERE FOUND CORRODED. THE HOLES WERE OVERSIZED TO REMOVE THE CORROSION AND OVERSIZED BUSHINGS WERE INSTALLED.Oct 10, 2006 · N936DL · Doug MD88 · Wing, Landing Gear Attach FittingsSDR KCSA061404Stiffener · corrodedTOP OF NOSE WHEEL WELL TUNNEL AT STA 300 LBL 6 STIFFENER HAS CORROSION.Oct 9, 2006 · N709CK · Boeing 747132 · Fuselage Miscellaneous StructureSDR ASMF200610005Water Separator · fullAIRCRAFT RETURNED TO PLATFORM DUE TO EXCESSIVE WATER DRIPPED IN THE PASSENGERS CABIN AT ROW 24 NEAR TO THE AFT GALLEY. THE WATER SEPARATORS WERE DRAINED IAW MM 21-70-00 AND BOTH AIR CONDITIONING SYSTEMS WERE OPERATED IN HEAT MODE, ALL CORRECT. DURING OVERNIGHTOct 5, 2006 · N169PL · Doug MD88 · Humidity Control SystemSDR ASMF200610004Indicator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO LT IVSI WAS OUT OF SERVICE. LT IVSI WAS REPLACED IAW MM 34-46-05, TESTED CORRECT. AIRCRAFT WAS REFUELED AND DISPATCHED.Oct 3, 2006 · N838AM · Doug DC983 · Attitude and Direction Data SystemSDR ASMF200610001Relay · failedAIRCRAFT RETURNED TO PLATFORM, LT STATIC PORT HEATER WAS OUT OF SERVICE. CORRESPONDING BREAKERS WERE RESEATED BUT FAILURE CONTINUED. R2-99 RELAY WAS DETECTED DAMAGED, SO IT WAS REPLACED IAW MM 30-30-00, TESTED CORRECT.Oct 1, 2006 · N168PL · Doug MD88 · Pitot/Static Anti-Ice SystemSDR ASMF200610002Dual Valve · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RT HYDRAULIC SYSTEM. DURING MAINTEANCE CHECK, 10 QUARTERS OF HYDRAULIC LIQUID WERE CHARGED AND THE LEAK WAS DETECTED IN THE HOUSING OF THE LT SERVO VALVE. THE LT SERVO VALVE WAS REPLACED IAW MM 32-43-0Oct 1, 2006 · N838AM · Doug DC983 · Hydraulic System, MainSDR AALA20060763O-Ring · leakingSTL - DURING CLIMB, RIGHT HAND ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. RIGHT ENGINE OIL QUANTITY DROPPED TO ZERO. CREW SHUT DOWN RIGHT ENGINE. WINDMILL TIME WITH ZERO OIL PRESSURE 10 MINUTES. LANDED STL WITHOUT INCIDENT. FOUND BLOWN FILTER O-RING IN GEOct 1, 2006 · N9630A · Doug MD83 · Turbine Engine Oil SystemSDR AALA20060765Battery Pack · inoperativeLGA - EMERGENCY LIGHTS AT FORWARD AND AFT CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FORWARD AND AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.Oct 1, 2006 · N966TW · Doug DC983 · Emergency LightingSDR ASMF200609010Cylinder · leakingAIRCRAFT RETURNED, DUE TO NOSE LANDING GEAR DID NOT RETRACT. AT PLATFORM AIRCRAFT WAS JACKED IAW MM 07-11-00 AND 3 EXTENSION AND RETRACTION CYCLES WERE PERFORMED, DETECTING THE NOSE LANDING GEAR STRUT LOW AND WITH LOW AIR LEVEL. NOSE LANDING GEAR STRUT SEALS WSep 24, 2006 · N161PL · Doug MD88 · Main Landing Gear Strut/Axle/TruckSDR DLM8K060764Engine · malfunctionedDURING APPROACH INTO LGA 5000 FT SLOWING TO 170 KTS FLAPS 15THE NR 2 ENGINE RACED TO MAX EGT NEAR 660C, N1 OVER 102 PERCENT ALL PARAMETERS EXCEEDED. SHUTDOWN RT ENGINE. DID NOT PULL FIRE HANDLE. NORMAL SHUTDOWN AND DECLARED EMERGENCY. REPLACED NR 2 ENG IAW RSep 20, 2006 · N909DE · Doug MD88 · Engine (Turbine/Turboprop)SDR DU4R2006639Seat Track · corrodedS/O 291022 NR 29736 CORROSION CABIN LT OB SEAT TRACK FS 769-1032, NICKS, GROOVE MARKS, CHAFE MARKS, TOP CENTER OF TRACK AND FLANGES. CUT OUT CORRODED SECTION OF SEAT TRACK, INSTALLED REPAIR CHANNELS P/N 7452952-7 AND PLUGS P/N 7452952-3 IAW MD-80 SRM 53-05D.Sep 19, 2006 · N921DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DU4R2006621Skin · lightning strikeS/O 291022 NR 29024 LIGHTNING STRIKE LT FUSELAGE STA. 370 - 389 L-28L - L-29L (2 EA.) CUT OUT AREA CONTAINING LIGHTNING STRIKES. FABRICATED AND INSTALLED FUS. SKIN REPAIR 8.5 INCH X 5.2500 INCHES FROM 2024-T3 .050 INCH AND FINGER DOUBLER 10 INCHES X 6.5 INCHESSep 18, 2006 · N921DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DU4R2006617Longeron · gougedS/O 291022 N/R NR 29361 DEEP GOUGE IN LONGERON 3L JUST AFT OF FS 1401. REMOVED GOUGED SECTION OF LONGERON. FABRICATED AND INSTALLED NEW LONGERON SECTION 19.3 INCHES FROM P/N 2777922-4 AND 2 EA. SPLICES 12.2 INCHES X 8.2 INCHES FROM 7637813-3 IAW SRM 53-02 FIGSep 16, 2006 · N921DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DU4R2006620Longeron · crackedS/O 291022 N/R NR 29557 LONGERON 4L AT FS 522 IS CRACKED. FABRICATED AND INSTALLED LONGERON REPAIRS 37-.2500 INCHES FROM 7075-T62P/N S2777922-1, AND LONGERON REPAIR 15 INCHES FROM 7637813-3 IAW SRM 51-10-1, 51-10-3D.Sep 14, 2006 · N921DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR ANCF200600033Compressor · stalledPILOT REPORT: ONE MINUTE AFTER TAKEOFF, LT ENGINE COMPRESSOR STALL WAS PRESENTED AND A STRONG SHAKE ON THE AIRPLANE WAS FELT. LT THROTTLE LEVER WAS REDUCED UNTIL COMPRESSOR STALL STOPPED. ENGINE COMPRESSOR STALL CHECK LIST WAS PERFORMED A NORMAL LANDING WAS PESep 10, 2006 · N836RA · Doug DC983 · Turbine Engine Compressor SectionSDR DLM8K060720Engine · malfunctionedAT TOP OF DESCENT RT ENGINE REMAINED AT FULL THROTTLE POS HAD NO CONTROL WITH THROTTLES. SHUT DOWN RIGHT ENGINE AND LANDED. FLT DATA RECORDER REMOVED AND BOROSCOPE PERFORMED. NO PROBLEMS FOUND ON BOROSCOPE BUT FDR SHOWS EGT, ENG SPEEDSAND TEMPS ALL OUT OF LSep 5, 2006 · N910DE · Doug MD88 · Engine (Turbine/Turboprop)SDR DU4R2006618Skin · lightning strikeS/O 291023 N/R NR21879 LIGHTNING STRIKE BLEND OUT AT FS 730 1.25 INCHES ABOVE L-27R OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR 6 INCHES X 5 INCHES FROM 2024-T3 .032 INCHES IAW SRM 53-04 FIG. 38, 51-10-3D.Sep 2, 2006 · N933DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DU4R2006619Skin · lightning strikeS/O 291023 N/R NR 21880 LIGHTNING STRIKE BLEND OUT AT FS 736 ABOVE L-27R OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR 6.25 INCHES X 6.0 INCHES FROM 2024-T3 .032 INCH IAW SRM 53-04 FIG. 38, 51-10-3D.Sep 2, 2006 · N933DL · Doug MD88 · Fuselage Main, Plate/SkinSDR ASMF200608021Structure · delaminatedDURING TRANSIT CHECK, LT ENGINE NOSE COWLING NOISE SUPPRESSOR WAS DETECTED DELAMINATED IN AN AREA OF 17 INCHES WIDTH X 25 INCHES LENGTH BETWEEN 6 AND 7 HOURS POSITION OUT OF LIMITS IAW MM 72-00-00 PAGE 642. AIRCRAFT WAS SENT TO THE HANGAR. PENDING FINAL ACTIONAug 31, 2006 · N1075T · Doug DC987 · Engine Noise SuppressorSDR ASAA0680912Insert · corrodedCABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL IAW SRM 53 05 AND ASA DWG S4932106.Aug 29, 2006 · N961AS · Doug DC983 · Fuselage Floor PanelSDR AALA20060625Valve · failedDFW - SHUT DOWN LEFT ENGINE INFLIGHT DUE TO FUEL HEAT VALVE REMAINED OPEN. OIL TEMPERATURE IN CAUTION RANGE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FUEL HEAT VALVE AND REPLACED MAIN OIL FILTER. NO CONTAMINATION FOUND. SYSTEM GROUND CHECKED Aug 28, 2006 · N437AA · Doug DC983 · Engine Fuel/Oil CoolerSDR AALA20060623Duct · blownDFW - DURING CLIMB OUT AT CLIMB POWER THE RIGHT ENGINE FIRE WARNING LIGHT ILLUMINATED WITH ORAL WARNING. LANDED DFW WITHOUT INCIDENT. FOUND RIGHT ENGINE ANTI ICE DUCT BLOWN. REPLACED RIGHT ENGINE ANTI ICE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.Aug 27, 2006 · N568AA · Doug DC983 · Engine Anti-Icing SystemSDR ASMF200608016Blade · brokenDURING THE BOROSCOPIC INSPECTION RELATED TO THE EO 987211 R4 PERFORMED DURING OVERNIGHT CHECK, WERE DETECTED SEVERAL BLADES WITH DENTS OUT OF LIMITS AND ONE BLADE BROKEN IN T2 SECTION. LT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-01, ALL CORRECAug 24, 2006 · N754RA · Doug DC987 · Turbine Engine Compressor SectionSDR ASAA0680901Gusset · corrodedAFT CARGO BAY THRESHOLD WEB GUSSET IS CORRODED. REPLACED GUSSET IAW SRM 53 14 3 51 10 2 51 10 3. 51 30 2. AND 51 30 5.Aug 23, 2006 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ANCF200600031Heater · malfunctionedPILOT REPORT: LT FUEL HEAT ON LIGHT CAME ON AFTER TAKE OFF (FUEL TEMPERATURE WENT TO 79 DEGREES, OIL TEMPERATURE COME TO 135 DEGREES)TRANSFERRED TO DMI NR 27 MEL 73-6-2 CATEGORY (C). DISPATCH DEVIATION PROCEDURE GUIDE WAS ACCOMPLISHED. FROM DMI 27: AIR-FUEL Aug 23, 2006 · N593AN · Doug DC983 · Engine Fuel PumpSDR DU4R2006601Skin · dentedS/O 291020, NR 32111 DENT EXT FUSELAGE SKIN AT C-1 DOOR AFT UPPER CORNER. FABRICATED REPAIR DOUBLER 15.5 INCH X 13 INCH X 2.5 INCH X 2.5 INCH FROM 2024-T3 .160 INCH IAW SRM 51-10-3, 51-30-5 AND 51-30-2.Aug 21, 2006 · N924DL · Doug MD88 · Fuselage Main, Plate/SkinSDR ASAA0680900Wire · shortedDURING TAXI AFTER LANDING CABIN FILLED WITH SMOKE. EMERGENCY EVACUATION WAS EXECUTED VIA EMERGENCY SLIDES. SOURCE OF SMOKE WAS ARCING FROM HEATER WIRE DAMAGED BY TA BRACKET WHICH BECAUSE OF VIBRATION EVENTUALLY CUT THROUGH THE WIRE INSULATION. DAMAGED WIRE WASAug 20, 2006 · N944AS · Doug DC831 · Air Conditioning System WiringSDR DU4R2006600Seat Track · corrodedS/O 291020 N/R 32059 RT OB SEAT TRACK AT FS 418-800 RBL 54 CORRODED. REMOVED CORRODED SEAT TRACK, CUT AND INSTALLED 48 FOOT SECTION OF TRACK P/N 5930547U70 IAW SRM 51-10-4 AND 53-05D.Aug 19, 2006 · N924DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DU4R2006605Frame · corrodedS/O 291019 NR 25018 CORROSION IN SEVERAL AREAS AT AFT CARGO LOWER ANGLE FRAME STA. 1322, LONGERON 23L-23R. REMOVED AND REPLACED AFT CARGO LOWER ANGLE FRAME PN 9936664-23 FROM STA. 1322, LONGERON 23L-23R IAW SRM 51-30-2 AND 51-10-03.Aug 18, 2006 · N927DA · Doug MD88 · Fuselage Main, FrameSDR ASMF200608012Control Valve · leakingCAPTAIN REPORTED THAT AFTER LANDING, THE LT HYDRAULIC SYSTEM WAS LOST AND LT REVERSE REMAINED EXTENDED. AIRCRAFT WAS TOWED TO PLATFORM AND RECHARGED OF HYDRAULIC LIQUID, DETECTING A LEAK IN THE LT HYDRAULIC REVERSE VALVE CAP. THE LT HYDRAULIC REVERSE VALVE WASAug 16, 2006 · N1075T · Doug DC987 · Hydraulic System, MainSDR ASMF200608009Tube · leakingAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, THE LT ENGINE (OIL PRESS LOW) LIGHT TURNED ON. CAPTAIN INFORMED THAT DURING CRUISE THE (OIL PRESS LOW) LIGHT TURNED ON, PERFORMED THE EMERGENCY PROCEDURE AND LT ENGINE WAS SHUTDOWN. DURING MAINTENANCE REVIEW, THE OIL Aug 15, 2006 · N1075T · Doug DC987 · Turbine Engine Oil SystemSDR ASMF200608008Generator · failedAIRCRAFT RETURNED TO PLATFORM AFTER ENGINE START, THE LT GENERATOR WAS OUT OF SERVICE, THE CORRESPONDING SWITCH WAS RESEATED AND FREQUENCY AND VOLTAGE WERE WITHOUT INDICATION. LT GCU, CSD AND CHIP DETECTOR WERE CHECKED AND NO FAILURE WAS DETECTED, THEREFORE, GAug 13, 2006 · N881LF · Doug MD83 · Alternator-Generator DriveSDR DU4R2006606Longeron · corrodedS/O 291019 NR 25070, CORROSION AT AFT CARGO LONGERON 28R BETWEEN FS 1287-1309. BLENDED OUT SURFACE CORROSION, MAX DEPTH .018 DEEP. FABRICATED AND INSTALLED U-CHANNEL LONGERON REPAIR 22 INCHES X .75 INCH X 1.5 INCH X 20 INCH FROM 7075-T6 .071 INCH IAW SRM 53-Aug 11, 2006 · N927DA · Doug MD88 · Fuselage Main, Longeron/Stringer
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