Pratt & Whitney JT8D-17

Service difficulty reports · 1,680

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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 = 'JT8D17'
  ORDER BY difficulty_date DESC"

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SDR 2026FA0000477Generator · failedIN V1 IF PRESENT LOSS OF ALL GENERATOR WAS PERFORMED EMERGENCY CHECK LIST WITH UNSATISFACTORY STATE. COME BACK AIRPORT OF BOGOTÁ. ACCOMPLISHED CHECKOUT ANALYSIS OF ELECTRICAL GENERATOR SYSTEM IAW 727 AMM 24-20-00 / 101-113. FOREIGN REGISTRATION: HK-5216Jun 5, 2026 · Boeing 727227 · AC Generator-AlternatorSDR FXGA07312024001Hose · leakingON DESCENT "A" SYSTEM HYDRAULIC QUANTITY FLUID STARTED DECREASING. FOUND LEAK FROM HOSE FITTING ON #2 SPOILER ACTUATOR. REPLACED ORING ON FITTINGJul 27, 2024 · N794AJ · Boeing 727227 · Hydraulic System, MainSDR VGCA20230323001Gearbox · leaking#2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS.Mar 23, 2023 · N215WE · Boeing 7272S2F · Engine Oil PressureSDR FXGA2022121400512Battery · dischargedCREW RECEIVED A LOWER AFT CARGO FIRE WARNING AT FL360 ON ARRIVAL INTO EFD. CREW IMMEDIATELY INITIATED THE EMERGENCY PROCEDURE AND BEGAN AN EMERGENCY DECENT AND DIVERTED TO CWF, WHICH WAS JUST SOUTH OF POSITION. THE FIRE CREW SWEPT AIRCRAFT UPON LANDING AND NO Dec 12, 2022 · N794AJ · Boeing 727227 · Smoke DetectionSDR FXGA20211129001Duct · crackedON CLIMB APPROXIMATELY 1500' #3 ENGINE HAD FIRE WARNING. ACCOMPLISHED CHECKLIST. LIGHT EXTINGUISHED DID NOT FIRE BOTTLE. RETURNED TO KFLL. ON VISUAL INSPECTION OF ENGINE IT WAS FOUND THAT THE BLEED AIR DUCT HAD RUPTURED/CRACKED.Nov 27, 2021 · N794AJ · Boeing 727227 · Engine Bleed Air SystemSDR Y2PA2020102920032Engine · fodDISCREPANCY: CREW REPORTED THAT AFTER DEPARTURE FROM KLRD AND CLIMBING THROUGH 10000 FEET, THE NR 3 ENGINE FAILED WITH ASSOCIATED VIBRATIONS. THEY DECLARED AN EMERGENCY AND PERFORMED THE ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST AND LANDED AT THE DEPOct 28, 2020 · N727US · Boeing 727223 · Engine (Turbine/Turboprop)SDR VGCA20200923001Engine · fodAFTER TAKEOFF DURING CLIMB, NR 3 STARTED VIBRATING EXCESSIVELY. SHUT DOWN ENGINE AND RETURNED TO AIRPORT. UPON INSPECTION OF ENGINE, FOUND EVIDENCE OF FOD DAMAGE TO THE FAN BLADES. REMOVED ENGINE FROM SERVICE.Sep 23, 2020 · N281FL · Boeing 727281 · Engine (Turbine/Turboprop)SDR FXGA201903081925Beam · corrodedCORROSION ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. REMOVE AND REPLACE CORRODED BEAM WITH NEW PER SRM 51-30-2 FASTENER REMOVAL AND INSTALLATION.Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous StructureSDR FXGA201903081924Beam · corrodedCORROSION ON RT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 88.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous StructureSDR FXGA201903081923Beam · corrodedCORROSION ON LT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 82.5 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous StructureSDR FXGA201903081922Beam · corrodedCORROSION ON LT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM. TO REPAIR A CORRODED HORIZONTAL STABILIZER TRAILING EDGE BEAM. CUT DAMAGED BEAM AT STA 78.29 AND SPLICE IN NEW OUTBOARD SECTION PER SRM 55-10-6 FIGURE 1 HORIZONTAL STABILIZER T.E. BEAM REPAIR.Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous StructureSDR Y2PA2018092200029Bearing · failedCREW REPORTED – EXPERIENCED SEVERAL ABNORMAL AIRCRAFT VIBRATIONS. DISCUSSED WITH CREW. DECLARED AN EMERGENCY. LANDED AT NEAREST SUITABLE AIRPORT USING NORMAL PROCEDURES. USA JET MAINTENANCE WAS SENT TO KAFW TO TROUBLESHOOT PROBLEM. UPON INSPECTION OF THE #Sep 22, 2018 · N726US · Boeing 727223 · Turbine Engine Compressor SectionSDR AALA20170109030Engine · smokeAFTER GATE ARRIVAL, MAINTENANCE PULLED FIRE HANDLE DUE TO SMOKE AND FUEL FROM THE LT ENGINE. AIRCRAFT WAS GROUNDED. ACCOMPLISHED VISUAL CHECKS. STARTED AND SHUTDOWN ENGINE TWICE. RESET ENGINE GENERATOR. ALL PARAMETERS NORMAL. OPS CHECKED GOOD.Jan 5, 2017 · N9629H · Doug DC983 · Engine (Turbine/Turboprop)SDR I5PA2016022642501Unknown · malfunctionedSHORTLY AFTER TAKEOFF THE CREW CALLED IN THE COMPANY RADIO THAT THEY WERE NOT GETTING A GREEN LIGHT FOR THE NOSE GEAR & THAT THE RED UNSAFE LIGHT STAYED ILLUMINATED. THEY CYCLED THE GEARS & STILL DID NOT GET THE RED NOSE GEAR LIGHT TO EXTINGUISH & THE GREEN LFeb 26, 2016 · N86425 · Boeing 727200 · Landing Gear Retraction/Extension SystemSDR FXGA20160226001Controller · failedAIRCRAFT DEPRESSURIZED IN THE MIDDLE OF A PARABOLA. DESCENT WAS INITIATED AT FIRST INDICATION OF DEPRESSURIZATION. MAXIMUM ALTITUDE REACHED WAS FLIGHT LEVEL 310. FOUND THAT THE CABIN PRESS CONTROLLER HAD FAILED.Feb 25, 2016 · N794AJ · Boeing 727227 · Cabin Pressure ControllerSDR CA160226003Pressure Switch · shorted(CAN) IN CRUISE, NR 1 ENGINE, START VALVE OPEN, CAUTION LIGHT ILLUMINATE. CREW FOLLOW QRH PROCEDURE AND SHUTDOWN THE AFFECTED ENGINE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE FOUND THAT IT WAS ONLY AN INDICATION PROBLEM. THE STARTER VALVE PFeb 25, 2016 · Boeing 7372S2C · Engine Start Valves/ControlsSDR I5PA2015102631902Line · unknownNUMBER 3 ENG EXPERIENCED OIL LOSS. OIL PRESS AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUBLESHOOTING IN PROGRESS. ENG HAD APPROX 1 GAL IN THE SYS & SERVICED APPROX 3 GAL. FOUND OIL SUPOct 25, 2015 · N319NE · Boeing 727212 · Turbine Engine Oil SystemSDR FXGA20151026001Wire Harness · brokenDURING CRUISE FLIGHT NR 3 ENG FIRE INDICATION. PROCEDURE & CHECKLIST INITIATED. BOTH ENG FIRE BOTTLE DEPLOYED. FIRE INDICATION REMAINED ON. ALL ENG PARAMETERS NORMAL EXCEPT ENG OIL TEMP AT RED LINE. ENG FIRE INDICATION REMAINED ON UP TO SECURING AIRPLANE Oct 22, 2015 · N794AJ · Boeing 727217 · Fire Protection System WiringSDR CA150729007Indicator · failed(CAN) DURING APPROACH THE CREW SELECTED FLAPS 1 POSITION. THE L/E FLAPS LOWERED TO THE EXTEND POSITION, BUT THE TRAILING FLAPS DIDN`T MOVE. THE FLAPS WERE CYCLED SEVERAL TIMES WITH NO MOVEMENT. THE CREW THEN SELECTED ALTERNATE EXTENSION OF THE FLAPS WITH THE SJul 23, 2015 · Boeing 737200 · Trailing Flap Position Indicating SystemSDR PCSA2015072701Warning Light · illuminatedNR 3 ENGINE LOW OIL PRESSURE LIGHT CAME ON & STAYED ON DURING TAKEOFF. REJECTED TAKEOFF AT 100 KNOTS. MODERATE BRAKING. NR 3 ENGINE EGT RUNS HOT AT TAKEOFF POWER, REDUCED POWER A LITTLE BEFORE OIL LIGHT CAME ON. REPLACED THE MAIN OIL FILTER & REPLACED THE Jul 21, 2015 · N199AJ · Boeing 7272F9 · Engine Oil Indicating SystemSDR F7JR2015FA0000417Turbine Wheel · crackedT-3 DISK REMOVED FROM ENGINE. THE T-3 DISK EXPERIENCED A FATIGUE CRACK AND MATERIAL FAILURE. THE CRACK APPEARS TO HAVE ORIGINATED ON THE FRONT OF THE DISK ABOUT HALF WTH WAY UP THE FIR TREE BLADE MOUNT ANEE AT THE ADJACENT BLADE MOUNT. WHEN THE MATERIAL FMar 14, 2015 · Turbine SectionSDR CA150126008Fitting · broken(CAN) DURING INSTALLATION AND RIGGING OF NR 5 SLAT ACTUATOR FAIRING, MAINTENANCE NOTED EXCESSIVE PLAY ON ACTUATOR ATTACHMENT. UPON INSPECTION IT WAS FOUND THAT OUTBOARD ATTACHMENT LUG WAS BROKEN. BUSHINGN P/N NAS72-9E006 WAS NOT FOUND INSTALLED IN THE FITTING Jan 21, 2015 · Boeing 737248C · Trailing Edge FlapsSDR CA140923009Circuit Breaker · failed(CAN) DURING TAXI, THE FLT CREW REPORTED THEY HAD NO HYDRAULIC PRESSURE FROM THE NR 1 HYDRAULIC B PUMP AND RETURNED TO THE RAMP. DURING MAINTENANCE TROUBLESHOOTING, THEY FOUND A SYS 40 AMP CIRCUIT BREAKER TRIPPED WITH SIGNS OF BEING BURNED. THE FAULTY BREAKESep 18, 2014 · Boeing 727281 · Hydraulic Power System WiringSDR CA140619002Hose · failed(CAN) WHILE IN FLIGHT, THE FLIGHT CREW HAD NOTICED THE HYDRAULIC FLUID LEVEL DECREASING. "A" SYSTEM FLUID LEVEL WAS EXHAUSTED, AND THE AIRCRAFT CONTINUED ENROUTE, ON THE "B" SYSTEM IAW THE FLIGHT MANUAL ABNORMAL PROCEDURES. THE LOSS OF "A" SYSTEM AFFECTS THE BJun 16, 2014 · Boeing 7372S2C · Hydraulic System, MainSDR I5PA201405010001Gearbox · unknownAT APPROXIMATELY 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY FOLLOWED BY LOW OIL PRESS, HIGH ENG TEMP AT FL 330. THEY DECLARED AN EMERGENCY AT 0738Z & AIR RETURNED BACK TO HNL STATION SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEAApr 23, 2014 · N86425 · Boeing 727212 · Turbine Engine Accessory DriveSDR I5PA201405010002Gearbox · leakingAT APPROX 0730Z, THE CREW EXPERIENCED NR 3 ENG LOSS OF OIL QTY, FOLLOWED BY LOW OIL PRESS, HIGH ENG EMP AT FL 330. DECLARED AN EMER AT 0738Z & AIR RETURNED BACK SAFELY AT 0908Z. TROUBLESHOOTING IN PROGRESS. R & R NR 3 ENG GEARBOX IAW AMM 72-63-00. INSPECTEApr 23, 2014 · N86425 · Boeing 727212 · Turbine Engine Accessory DriveSDR CA140408002Indicator · failed(CAN) T/E FLAP SYS STALLING AND LOCKOUT TROUBLESHOOTING CARRIED OUT. T/E FLAP ASSEMBLIES INCLUDING TRACKS AND ROLLERS INSPECTED FOR DAMAGE, NO FAULTS FOUND. FLAP POSITION INDICATOR REPLACED AND ACFT RELEASED PENDING SATISFACTORY TEST FLIGHT. TEST FLIGHT CARApr 6, 2014 · Boeing 737242C · Trailing Flap Position Indicating SystemSDR SPUY201403310033Skin · corrodedNR 3 ENGINE, LT UPPER COWLING SKIN SHOWS CORROSION FROM NAC STA. 185.20-194.8.Mar 31, 2014 · N199AJ · Boeing 7272F9 · Nacelle/Pylon, Plate/SkinSDR SPUY201403310037Latch · crackedNR 1 ENGINE, UPPER COWLING FITTING LATCH ATTACHMENT CRACKED ONE INCH.Mar 31, 2014 · N199AJ · Boeing 7272F9 · Nacelle/Pylon, Main FrameSDR SPUY201403310038Former · corrodedNR 1 ENGINE, THRUST REVERSE FWD SIDE EXTERIOR FORMER CORRODED AT STA 96.25 AT 5 O´CLOCK POSITION.Mar 31, 2014 · N199AJ · Boeing 7272F9 · Engine Thrust ReverserSDR CA140311010Heater · shorted(CAN) CAPTAIN`S MAIN WINDSCREEN WINDOW HEAT GOES DIRECTLY TO OVERHEAT WHEN SWITCH SELECTED. DURING TROUBLESHOOTING IT WAS FOUND THAT THE CONTROL BOX HAS AN INTERNAL SHORT CAUSING A VERY LARGE CURRENT DRAW POPPING THE MAIN POWER BREAKER. CONTROLLER REPLACED. MFMar 7, 2014 · Boeing 737248C · Windshield/Door Rain/Ice RemovalSDR CA140225014Proximity Switch · failed(CAN) AFTER TAKEOFF, DURING CLIMB, THE FLAPS HAD BEEN SELECTED UP IAW NORMAL OPERATING PROCEDURE. THE FLAP POSITION INDICATION, INDICATED THAT THE LT INBD FLAP WAS IN TRANSIT AND NOT FULLY RETRACTED. THE ACFT RETURNED TO THE RAMP AFTER EXECUTING A NORMAL LANFeb 24, 2014 · Boeing 7372S2C · Trailing Flap Position Indicating SystemSDR CA140224017Oil System · bypassing(CAN) WITH POWER LEVERS ADVANCED FOR TAKEOFF, AN INDICATION OF AN IMPENDING "OIL FILTER BYPASS" LIGHT ON NR 1 ENGINE HAD OCCURRED. POWER LEVERS RETARDED AND ACFT RETURNED TO THE RAMP. THE NR 1 ENGINE OIL FILTER WAS REMOVED AND INSPECTED. FILTER INSPECTION IFeb 21, 2014 · Boeing 737200 · Turbine Engine Oil SystemSDR CA140130013Hose · failed(CAN) DURING TAKEOFF CREW REPORTED LOSS OF HYDRAULIC SYSTEM "A" AND THE LANDING GEAR WOULD NOT RETRACT. OVERWEIGHT LANDING PERFORMED. ON THE GROUND MAINTENANCE DISCOVERED HYD LEAK FROM RT THRUST REVERSER FLEX LINE. THE HOSE ASSY WAS MFG JAN 1975. HYDRAULICJan 27, 2014 · Boeing 737248C · Hydraulic System, MainSDR CA131017005Tube · fractured(CAN) DURING CLIMB OUT APPROXIMATELY 10 MINUTES THE FLIGHT CREW REPORTED THE NR 2 ENGINE SURGE WITH ASSOCIATED VIBRATION AND HIGH TEMPERATURE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE NR 2 VORTEX DISSIPATOR TUBE FRACTURED AND WAS NOT RECOVEOct 15, 2013 · Boeing 737* · Turbine SectionSDR CA131004006Sliding Window · cracked(CAN) THE CAPTAIN`S SLIDING WINDOW, OUTER PANE CRACKED WHILE IN FLIGHT. PILOTS FOLLOWED THE APPLICABLE AFM PROCEEDURES. TT SINCE O/H 1,219.5 HRS AND 845 CYCLES SINCE O/H. THE WINDOW SHOWED NO SIGNS OF DELAMINATION, OR WATER/MOISTURE INGRESS. ASIDE FROM THE Oct 3, 2013 · Boeing 737* · Flight Compartment WindowsSDR CA131007024Engine · flamed out(CAN) AT TOP OF DECENT, THE NR 2 ENGINE FLAMED OUT. ENGINE FLAMEOUT CHECKLIST WAS COMPLIED WITH AND THE ENGINE WAS RESTARTED. THE NR 2 ENGINE FUEL FILTER WAS INSPECTED, AND REPLACED. THE FUEL S/O VALVE WAS FUNCTION CHECKED WITH NO FAULTS FOUND. ENGINE RUNS Oct 1, 2013 · Boeing 727281 · Engine (Turbine/Turboprop)SDR CA130803010Pressure Switch · malfunctioned(CAN) IN CRUISE, CREW NOTICED THE NR 3 ENGINE, LOW OIL PRESSURE/FILTER BYPASS, LIGHT ILLUMINATE. THE LOW OIL PRESSURE WARNING SYS WAS DEFERRED AND THE ACFT CONTINUED TO FINAL DESTINATION. MAINTENANCE REPLACED THE LOW OIL PRESSURE SWITCH AND THE ACFT RETURNEDJul 30, 2013 · Boeing 727281 · Engine Oil Indicating SystemSDR CA130726007Tire · failed(CAN) ACFT SUSTAINED A MAIN WHEEL TIRE FAILURE NR 1 POSITION. THE TREAD AND CHORD HAD SEPARATED FROM THE TIRE CASING. THE ACFT IS CERTIFIED AND OPERATED FROM GRAVEL RUNWAY SURFACES. THE TIRE IS CONSIDERED AS SCRAP. THE ACFT WAS INSPECTED IAW MM AND RESULTEJul 24, 2013 · Boeing 737* · TireSDR CA130719007Clamp · broken(CAN) SHORTLY AFTER TAKEOFF, THE CREW RECEIVED A START VALVE OPEN CAUTION LIGHT FOR ENGINE NR 1. THE CREW FOLLOWED THEIR SOPS AND SHUTDOWN THE NR 1 ENGINE. THE CREW THEN HELD A CIRCUIT FOR APPROXIMATELY 1 HR TO BURN OFF FUEL SO THEY COULD PERFORM A NON-OVERWJul 17, 2013 · Boeing 737275C · Pneumatic Distribution SystemSDR CA130905014Tube · cracked(CAN) THE CREW REPORTED LOW ENGINE PRESSURE RATIO ON ENGINE NR 2 AND SUBSEQUENTLY REJECTED TAKEOFF, RTO, DUE TO AN EPR FAILURE. MAINTENANCE TROUBLESHOT THE SYS VIA LEAK TESTS ON THE EPR SYSTEM AND, THROUGH THE PROCESS OF ELIMINATION, DETERMINED THE CAUSE WAS Jul 9, 2013 · Boeing 737275C · Engine Pressure Ratio (EPR)SDR CA130702001Power Lever · obstructed(CAN) UNABLE TO REACH TAKEOFF EPR ON NR 2 ENGINE DURING TRIM RUNS AFTER FCU REPLACEMENT DIFFERENT READING WERE OBSERVED WITH COWLING OPEN VERSUS COWLING CLOSED. AFTER TROUBLESHOOTING FCU POWER LEVER FOUND INTERFERING WITH COWLING.Jun 27, 2013 · Boeing 737200 · Power LeverSDR CA130325004Pcu · separated(CAN) DURING ROUTINE MAINTENANCE, WITH "B" PUMPS ON AND HYDRAULIC INTERCONNECT "OPEN" TO LOWER THE FLAPS, WHEN NORMAL OPERATING PRESSURE WAS REACHED IMMEDIATE LOSS OF HYDRAULIC PRESSURE WAS NOTICED ALONG WITH MASSIVE AMOUNTS OF HYDRAULIC FLUID GUSHING OUT OF TMar 22, 2013 · Boeing 737242C · Aileron Control SystemSDR CA130315005Circuit Breaker · burned(CAN) WHILE PERFORMING THE PREFLIGHT INSPECTION THE WINDOW HEAT FAILED. AFTER TROUBLESHOOTING IT WAS FOUND THAT THE CIRCUIT BREAKER FOR THE WINDOW HEAT SUPPLY C239 HAD BURNED. THIS BURNING HAD ALSO CAUSED DAMAGE TO THE CIRCUIT BREAKER IMMEDIATELY ON TOP OF TMar 13, 2013 · Boeing 7372L9 · Ice/Rain Protection System WiringSDR 7AHR20130129011Rib · wornRT ENGINE COWL HAS AREA OF DAMAGE, AREA NR 7 RIB. REMOVED DAMAGE RIB ANGLE IAW SRM 51-40-3. FABRICATED NEW REPAIR ANGLE IAW SRM 51-40-3. INSTALLED NEW REPAIR ANGLE TO NR 7 RIB IAW SRM 51-40-3.Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Main FrameSDR 7AHR20130129012Rib · wornRT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 10 RIB. AREA OF DAMAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGED PARTS (ANGLES). FABRICATED NEW REPAIR ANGLES IAW SRM 51-40-3. INSTALLED REPAIR ANGLES IAW SRM 51-40-3.Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Frame/Spar/RibSDR 7AHR20130129013Rib · wornRT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 11 RIB. AREA OF DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGE AND WORN PARTS (ANGLE) IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW 200 51-40-3.Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Frame/Spar/RibSDR 7AHR20130129014Skin · wornRT ENGINE COWL WORN. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON THE RT ENGINE COWL IAW SRM 51-40-3.Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Plate/SkinSDR R5KB2013031150507Skin · corrodedSKIN CORRODED UNDER EDGE OF DOUBLER AT STA 950E, STR 27R.Dec 12, 2012 · N727NK · Boeing 727212 · Fuselage Main, Plate/SkinSDR CA121113005Pin · failed(CAN) A DEFICIENCY WAS DETECTED ON THE GROUND IN THE NR 7 FLAP UNIVERSAL JOINT, BOLT/PIN, PN 65-76606-01. THE FLAP WOULD NOT FULLY RETRACT PAST THE NR 1 POSITION. THE RETENTION FEATURE OF THE LOCKING NUT WAS LOST AT THE THREAD TO PIN SHANK AREA SHEARED AT THE Nov 9, 2012 · Boeing 7372S2C · Trailing Edge Flap Control System
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