# Service difficulty reports: Pratt & Whitney JT8D-17

A list on [Pratt & Whitney JT8D-17](https://openairdocs.org/engine/pratt-whitney-jt8d-17.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 34 · 1,680 reports

- [SDR 2026FA0000477](https://openairdocs.org/sdr/2026FA0000477.md): Generator · failed · Jun 5, 2026 · Boeing 727227 · AC Generator-Alternator
  > IN 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-5216
- [SDR FXGA07312024001](https://openairdocs.org/sdr/FXGA07312024001.md): Hose · leaking · Jul 27, 2024 · N794AJ · Boeing 727227 · Hydraulic System, Main
  > ON DESCENT "A" SYSTEM HYDRAULIC QUANTITY FLUID STARTED DECREASING. FOUND LEAK FROM HOSE FITTING ON #2 SPOILER ACTUATOR. REPLACED ORING ON FITTING
- [SDR VGCA20230323001](https://openairdocs.org/sdr/VGCA20230323001.md): Gearbox · leaking · Mar 23, 2023 · N215WE · Boeing 7272S2F · Engine Oil Pressure
  > #2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS.
- [SDR FXGA2022121400512](https://openairdocs.org/sdr/FXGA2022121400512.md): Battery · discharged · Dec 12, 2022 · N794AJ · Boeing 727227 · Smoke Detection
  > CREW 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
- [SDR FXGA20211129001](https://openairdocs.org/sdr/FXGA20211129001.md): Duct · cracked · Nov 27, 2021 · N794AJ · Boeing 727227 · Engine Bleed Air System
  > ON 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.
- [SDR Y2PA2020102920032](https://openairdocs.org/sdr/Y2PA2020102920032.md): Engine · fod · Oct 28, 2020 · N727US · Boeing 727223 · Engine (Turbine/Turboprop)
  > DISCREPANCY: 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 DEP
- [SDR VGCA20200923001](https://openairdocs.org/sdr/VGCA20200923001.md): Engine · fod · Sep 23, 2020 · N281FL · Boeing 727281 · Engine (Turbine/Turboprop)
  > AFTER 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.
- [SDR FXGA201903081925](https://openairdocs.org/sdr/FXGA201903081925.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION 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.
- [SDR FXGA201903081924](https://openairdocs.org/sdr/FXGA201903081924.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION 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.
- [SDR FXGA201903081923](https://openairdocs.org/sdr/FXGA201903081923.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION 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.
- [SDR FXGA201903081922](https://openairdocs.org/sdr/FXGA201903081922.md): Beam · corroded · Mar 8, 2019 · N794AJ · Boeing 727227 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION 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.
- [SDR Y2PA2018092200029](https://openairdocs.org/sdr/Y2PA2018092200029.md): Bearing · failed · Sep 22, 2018 · N726US · Boeing 727223 · Turbine Engine Compressor Section
  > CREW 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 #
- [SDR AALA20170109030](https://openairdocs.org/sdr/AALA20170109030.md): Engine · smoke · Jan 5, 2017 · N9629H · Doug DC983 · Engine (Turbine/Turboprop)
  > AFTER 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.
- [SDR I5PA2016022642501](https://openairdocs.org/sdr/I5PA2016022642501.md): Unknown · malfunctioned · Feb 26, 2016 · N86425 · Boeing 727200 · Landing Gear Retraction/Extension System
  > SHORTLY 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 L
- [SDR FXGA20160226001](https://openairdocs.org/sdr/FXGA20160226001.md): Controller · failed · Feb 25, 2016 · N794AJ · Boeing 727227 · Cabin Pressure Controller
  > AIRCRAFT 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.
- [SDR CA160226003](https://openairdocs.org/sdr/CA160226003.md): Pressure Switch · shorted · Feb 25, 2016 · Boeing 7372S2C · Engine Start Valves/Controls
  > (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 P
- [SDR I5PA2015102631902](https://openairdocs.org/sdr/I5PA2015102631902.md): Line · unknown · Oct 25, 2015 · N319NE · Boeing 727212 · Turbine Engine Oil System
  > NUMBER 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 SUP
- [SDR FXGA20151026001](https://openairdocs.org/sdr/FXGA20151026001.md): Wire Harness · broken · Oct 22, 2015 · N794AJ · Boeing 727217 · Fire Protection System Wiring
  > DURING 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
- [SDR CA150729007](https://openairdocs.org/sdr/CA150729007.md): Indicator · failed · Jul 23, 2015 · Boeing 737200 · Trailing Flap Position Indicating System
  > (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 S
- [SDR PCSA2015072701](https://openairdocs.org/sdr/PCSA2015072701.md): Warning Light · illuminated · Jul 21, 2015 · N199AJ · Boeing 7272F9 · Engine Oil Indicating System
  > NR 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
- [SDR F7JR2015FA0000417](https://openairdocs.org/sdr/F7JR2015FA0000417.md): Turbine Wheel · cracked · Mar 14, 2015 · Turbine Section
  > T-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 F
- [SDR CA150126008](https://openairdocs.org/sdr/CA150126008.md): Fitting · broken · Jan 21, 2015 · Boeing 737248C · Trailing Edge Flaps
  > (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
- [SDR CA140923009](https://openairdocs.org/sdr/CA140923009.md): Circuit Breaker · failed · Sep 18, 2014 · Boeing 727281 · Hydraulic Power System Wiring
  > (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 BREAKE
- [SDR CA140619002](https://openairdocs.org/sdr/CA140619002.md): Hose · failed · Jun 16, 2014 · Boeing 7372S2C · Hydraulic System, Main
  > (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 B
- [SDR I5PA201405010001](https://openairdocs.org/sdr/I5PA201405010001.md): Gearbox · unknown · Apr 23, 2014 · N86425 · Boeing 727212 · Turbine Engine Accessory Drive
  > AT 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 GEA
- [SDR I5PA201405010002](https://openairdocs.org/sdr/I5PA201405010002.md): Gearbox · leaking · Apr 23, 2014 · N86425 · Boeing 727212 · Turbine Engine Accessory Drive
  > AT 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. INSPECTE
- [SDR CA140408002](https://openairdocs.org/sdr/CA140408002.md): Indicator · failed · Apr 6, 2014 · Boeing 737242C · Trailing Flap Position Indicating System
  > (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 CAR
- [SDR SPUY201403310033](https://openairdocs.org/sdr/SPUY201403310033.md): Skin · corroded · Mar 31, 2014 · N199AJ · Boeing 7272F9 · Nacelle/Pylon, Plate/Skin
  > NR 3 ENGINE, LT UPPER COWLING SKIN SHOWS CORROSION FROM NAC STA. 185.20-194.8.
- [SDR SPUY201403310037](https://openairdocs.org/sdr/SPUY201403310037.md): Latch · cracked · Mar 31, 2014 · N199AJ · Boeing 7272F9 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE, UPPER COWLING FITTING LATCH ATTACHMENT CRACKED ONE INCH.
- [SDR SPUY201403310038](https://openairdocs.org/sdr/SPUY201403310038.md): Former · corroded · Mar 31, 2014 · N199AJ · Boeing 7272F9 · Engine Thrust Reverser
  > NR 1 ENGINE, THRUST REVERSE FWD SIDE EXTERIOR FORMER CORRODED AT STA 96.25 AT 5 O´CLOCK POSITION.
- [SDR CA140311010](https://openairdocs.org/sdr/CA140311010.md): Heater · shorted · Mar 7, 2014 · Boeing 737248C · Windshield/Door Rain/Ice Removal
  > (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. MF
- [SDR CA140225014](https://openairdocs.org/sdr/CA140225014.md): Proximity Switch · failed · Feb 24, 2014 · Boeing 7372S2C · Trailing Flap Position Indicating System
  > (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 LAN
- [SDR CA140224017](https://openairdocs.org/sdr/CA140224017.md): Oil System · bypassing · Feb 21, 2014 · Boeing 737200 · Turbine Engine Oil System
  > (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 I
- [SDR CA140130013](https://openairdocs.org/sdr/CA140130013.md): Hose · failed · Jan 27, 2014 · Boeing 737248C · Hydraulic System, Main
  > (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. HYDRAULIC
- [SDR CA131017005](https://openairdocs.org/sdr/CA131017005.md): Tube · fractured · Oct 15, 2013 · Boeing 737* · Turbine Section
  > (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 RECOVE
- [SDR CA131004006](https://openairdocs.org/sdr/CA131004006.md): Sliding Window · cracked · Oct 3, 2013 · Boeing 737* · Flight Compartment Windows
  > (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
- [SDR CA131007024](https://openairdocs.org/sdr/CA131007024.md): Engine · flamed out · Oct 1, 2013 · Boeing 727281 · Engine (Turbine/Turboprop)
  > (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
- [SDR CA130803010](https://openairdocs.org/sdr/CA130803010.md): Pressure Switch · malfunctioned · Jul 30, 2013 · Boeing 727281 · Engine Oil Indicating System
  > (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 RETURNED
- [SDR CA130726007](https://openairdocs.org/sdr/CA130726007.md): Tire · failed · Jul 24, 2013 · Boeing 737* · Tire
  > (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 RESULTE
- [SDR CA130719007](https://openairdocs.org/sdr/CA130719007.md): Clamp · broken · Jul 17, 2013 · Boeing 737275C · Pneumatic Distribution System
  > (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-OVERW
- [SDR CA130905014](https://openairdocs.org/sdr/CA130905014.md): Tube · cracked · Jul 9, 2013 · Boeing 737275C · Engine Pressure Ratio (EPR)
  > (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
- [SDR CA130702001](https://openairdocs.org/sdr/CA130702001.md): Power Lever · obstructed · Jun 27, 2013 · Boeing 737200 · Power Lever
  > (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.
- [SDR CA130325004](https://openairdocs.org/sdr/CA130325004.md): Pcu · separated · Mar 22, 2013 · Boeing 737242C · Aileron Control System
  > (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 T
- [SDR CA130315005](https://openairdocs.org/sdr/CA130315005.md): Circuit Breaker · burned · Mar 13, 2013 · Boeing 7372L9 · Ice/Rain Protection System Wiring
  > (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 T
- [SDR 7AHR20130129011](https://openairdocs.org/sdr/7AHR20130129011.md): Rib · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Main Frame
  > RT 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.
- [SDR 7AHR20130129012](https://openairdocs.org/sdr/7AHR20130129012.md): Rib · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Frame/Spar/Rib
  > RT 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.
- [SDR 7AHR20130129013](https://openairdocs.org/sdr/7AHR20130129013.md): Rib · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Frame/Spar/Rib
  > RT 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.
- [SDR 7AHR20130129014](https://openairdocs.org/sdr/7AHR20130129014.md): Skin · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Plate/Skin
  > RT 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.
- [SDR R5KB2013031150507](https://openairdocs.org/sdr/R5KB2013031150507.md): Skin · corroded · Dec 12, 2012 · N727NK · Boeing 727212 · Fuselage Main, Plate/Skin
  > SKIN CORRODED UNDER EDGE OF DOUBLER AT STA 950E, STR 27R.
- [SDR CA121113005](https://openairdocs.org/sdr/CA121113005.md): Pin · failed · Nov 9, 2012 · Boeing 7372S2C · Trailing Edge Flap Control System
  > (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

Next page: https://openairdocs.org/engine/pratt-whitney-jt8d-17/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt8d-17/reports

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