# Service difficulty reports: Pratt & Whitney JT8D-15

A list on [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 55 · 2,710 reports

- [SDR K11A2020091600012](https://openairdocs.org/sdr/K11A2020091600012.md): Engine · stalled · Sep 16, 2020 · N729CK · Boeing 727264 · Engine (Turbine/Turboprop)
  > PROBLEM DESCRIPTION: ON CLIMBOUT BETWEEN 9000’ - 10000’ EXPERIENCED A COMPRESSOR STALL EPR INDICATED 1.9 ON NR 2 AND NR 3 AND 1.8 ON NR 1. AT 11000’ EXPERIENCED A SECOND COMPRESSOR STALL AND SUBSEQUENT ENGINE ROLLBACK ON NR 1 ENGINE. CORRECTIVE ACTION & OTH
- [SDR K11A2020081400008](https://openairdocs.org/sdr/K11A2020081400008.md): Fcu · fluctuates · Aug 14, 2020 · N726CK · Boeing 7272M7 · Fuel Control/Turbine Engines
  > AFTER TAKEOFF AND AT 70 % THE NUMBER 3 ENGINE SURGED WITH THE FUEL FLOW AND EGT INDICATIONS ALL FLUCTUATING. REMOVED AND REPLACED FUEL CONTROL IAW JT8 MAINTENANCE MANUAL 73-21-01, PERFORMED LEAK CHECK, TRIM CHECK AND ACCEL / DECAL CHECKS IAW B727 AMM 72-00-00
- [SDR K11A2018060702001](https://openairdocs.org/sdr/K11A2018060702001.md): Compressor · stalled · Jun 6, 2018 · N720CK · Boeing 7272B6 · Engine (Turbine/Turboprop)
  > ON THROTTLE UP FOR TAKEOFF, THE NR 1 ENGINE HAD A COMPRESSOR STALL, RETURNED TO BLOCKS. OPEN
- [SDR PCSA2017120801](https://openairdocs.org/sdr/PCSA2017120801.md): Warning Light · illuminated · Dec 8, 2017 · N395AJ · Boeing 727233 · Engine Oil Pressure
  > #1 ENGINE SHUTDOWN (BY CREW)DUE TO OIL PRESSURE LIGHT ILLUMINATED.
- [SDR K11A2017090772501](https://openairdocs.org/sdr/K11A2017090772501.md): Engine · fluctuates · Sep 7, 2017 · N725CK · Boeing 727224 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE AT TAKEOFF AND CLIMB OUT, EPR, N1, N2, FUEL FLOW, AND EGT SURGED WITH BLEED PRESSURE FLUXING 20-40 PSI.
- [SDR K11A2016122372001](https://openairdocs.org/sdr/K11A2016122372001.md): Warning Light · illuminated · Dec 23, 2016 · N720CK · Boeing 7272B6 · Pneumatic Indicating System
  > NR 3 BLEED TRIP LIGHT CAME ON DURING CRUISE.
- [SDR K11A2016122272000](https://openairdocs.org/sdr/K11A2016122272000.md): Valve · stuck · Dec 21, 2016 · N720CK · Boeing 7272B6 · Fuel Transfer Valve
  > DURING CLIMB OUT, NR 3 FUEL CROSS FEED VALVE WAS STUCK CLOSED.
- [SDR CA160119025](https://openairdocs.org/sdr/CA160119025.md): Blades · failed · Jan 13, 2016 · Boeing 727225 · Turbine Section
  > (CAN) ENGINE FAILURE ON TAKEOFF. AFTER LETTING THE ENGINES STABILIZE AT 70 PERCENT N1 FOR 15 SECONDS FOLLOWING DE-ICING, WITH NO ABNORMAL INDICATIONS, WHEN THE BRAKES WERE RELEASED AND TAKEOFF THRUST WAS APPLIED THERE WAS A LOUD BANG AND ENGINE NR 2 WAS OBSERV
- [SDR K11A2015122172001](https://openairdocs.org/sdr/K11A2015122172001.md): O-Ring · leaking · Dec 21, 2015 · N720CK · Boeing 7272B6 · Engine Fuel Pump
  > FUEL LEAKING FROM NR 3 ENGINE FUEL PUMP, INSPECTED AND FOUND O-RING WAS BAD, REPLACED O-RING WITH NEW, LEAK AND OP'S CHECK GOOD. NO OTHER DEFECTS NOTED.
- [SDR CA151209014](https://openairdocs.org/sdr/CA151209014.md): Line · cracked · Dec 8, 2015 · Boeing 727225 · Turbine Engine Oil System
  > (CAN) UPON DECENT THE CREW NOTICED NR 2 ENGINE OIL PRESSURE WAS BELOW THE RED LINE AND DECREASING. OIL QTY SHOWED "0". CREW SHUTDOWN THE ENGINE AND COMPLETED CHECKLIST. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LINE AT FUEL/OIL HEATER CONNECTION CRACK
- [SDR CA151007024](https://openairdocs.org/sdr/CA151007024.md): Hose · leaking · Oct 5, 2015 · Boeing 737200 · Hydraulic System, Main
  > (CAN) AIRCRAFT TOOK OFF AND HAD TO RETURN WHEN THEY DECLARED HAVING A HYDRAULIC PROBLEM IN CLIMB. UPON RETURN, HYDRAULIC LINE ON THE AILERON PCU HYDRAULIC B SYS IN THE LT WHEEL WELLWAS FOUND LEAKING UNDER THE ATTACH FITTING. UNABLE TO SEE DAMAGE OR LEAK BY G
- [SDR K11A2015052172401](https://openairdocs.org/sdr/K11A2015052172401.md): Warning Light · illuminated · May 21, 2015 · N724CK · Boeing 727225 · Turbine Engine Oil System
  > NR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. PERFORMED PRECAUTIONARY SHUTDOWN IAW ABNORMAL PROCEDURES AND RETURNED TO DEPARTURE.
- [SDR CA150506005](https://openairdocs.org/sdr/CA150506005.md): Roller Cam · sheared · May 5, 2015 · Boeing 727260 · Passenger/Crew Doors
  > (CAN) DURING DAILY MAINTENANCE, THE AFT LOWER ROLLER CAM ON THE MAIN ENTRANCE DOOR WAS FOUND SHEARED OFF. THE ROLLER CAM WAS REPLACED IAW THE AMM AND FUNCTION CHECKED SERVICEABLE. THE ACFT WAS RETURNED TO SERVICE.
- [SDR CA150429010](https://openairdocs.org/sdr/CA150429010.md): Hose · leaking · Apr 28, 2015 · Boeing 7372K2C · Hydraulic System, Main
  > (CAN) AFTER REPLACEMENT OF ANOTHER NLG HYDRAULIC LINE WHO NEEDED TO BE REPLACED DUE TO SEEPING, WE PROCEEDED TO CARRY OUT A GEAR SWING FOR PROPER OPERATION AND LEAK CHECK. AFTER SELECTING GEAR UP AND HOLD FOR 5 MINUTES AT 3000 PSI, HYDRAULIC FLUID STARTED COM
- [SDR CA150505007](https://openairdocs.org/sdr/CA150505007.md): Cable · broken · Apr 22, 2015 · Boeing 727223 · Trailing Edge Flap Control System
  > (CAN) BOTH MID FLAP EXTENSION CABLES,, WERE FOUND BROKEN DURING A DAILY INSPECTION WHEN THE FLAPS WOULD NOT RETRACT. BOTH CABLES WERE REPLACED AND FLAPS WERE CYCLED REPEATEDLY WITH NO FURTHER PROBLEM. ACFT WAS RETURNED TO SERVICE.
- [SDR CA150505008](https://openairdocs.org/sdr/CA150505008.md): Roller Cam · sheared · Apr 21, 2015 · Boeing 727260 · Passenger/Crew Doors
  > (CAN) WHILE CLOSING MAIN ENTRANCE DOOR, THE UPPER AFT CRANK ROLLER CAM SHAFT SHEARED. THE SHEARED CRANK ROLLER CAM WAS REPLACED AND CHECKED IAW THE AMM. THE ACFT WAS RETURNED TO SERVICE.
- [SDR R34R2015040220150](https://openairdocs.org/sdr/R34R2015040220150.md): Garlock Seal · leaking · Mar 26, 2015 · N289MT · Boeing 727223 · Turbine Engine Oil System
  > THE ACFT WAS BEING FLOWN ON A POST-MAINTENACE ACCEPTANCE CHECK FLIGHT. SHORTLY AFTER TAKEOFF, THE FLIGHT ENGINEER NOTED A NOTICABLE DROP IN THE OIL QUANITY ON THE NR1 ENGINE. THE OIL QUANITY WAS BELOW 2 QUARTS. 15 MINUTES AFTER LEVEL OFF OIL QUANITY DROPPED T
- [SDR CA150224030](https://openairdocs.org/sdr/CA150224030.md): Mount · misaligned · Feb 23, 2015 · Boeing 727260 · Engine Mount Section
  > (CAN) DURING ROUTINE MAINTENANCE INSPECTION THE NR 2 ENGINE RT FORWARD ISOLATOR MOUNT ALIGNMENT MARKS WERE FOUND MISALIGNED AND BONDING STRAP SHEARED.
- [SDR CA150114008](https://openairdocs.org/sdr/CA150114008.md): Duct · ruptured · Jan 13, 2015 · Boeing 727223 · Pneumatic Distribution System
  > (CAN) DURING CLIMB OUT NR 3 ENGINE FIRE INDICATION APPEARED, AFTER FOLLOWING CHECKLIST PROCEDURE NR 3 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO EWR AIRPORT. FIRE INDICATION WENT AWAY AS THROTTLE WAS RETARDED TO IDLE AS PART OF ENGINE SHUT-DOWN PROCEDURE. M
- [SDR CA141111006](https://openairdocs.org/sdr/CA141111006.md): Lock Actuator · inoperative · Sep 23, 2014 · Boeing 727225 · Landing Gear Retraction/Extension System
  > (CAN) AFTER TAKE-OFF, RT MAIN GEAR WOULD NOT RETRACT. GEAR CYCLED, RETRACTION WAS UNSUCCESSFUL. AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. RT MAIN GEAR LOCK ACTUATOR REPLACED.
- [SDR CA140627004](https://openairdocs.org/sdr/CA140627004.md): Line · burst · Jun 24, 2014 · Boeing 727223 · Hydraulic System, Main
  > (CAN) CREW REPORTED UPON GEAR RETRACTION AFTER TAKEOFF THEY HAD A SYSTEM A HYDRAULIC FAILURE. MAINTENANCE FOUND THE RT MAIN GEAR ACTUATOR "UP" LINE BURST APPROXIMATELY 1" FROM B-NUT FITTING. LINE REPLACED.
- [SDR CA140225024](https://openairdocs.org/sdr/CA140225024.md): Rod · sheared · Feb 6, 2014 · Boeing 727223 · Nose/Tail Landing Gear
  > (CAN) NLG SAFETY SWITCH PUSH/PULL TUBE FOUND SHEARED WHILE PREPARING ACFT FOR DEPARTURE. ROD ASSY REPLACED AND SAFETY SWITCH TESTED IAW 32-09-22.
- [SDR PCSA2014012001](https://openairdocs.org/sdr/PCSA2014012001.md): Unknown · vibration · Jan 18, 2014 · N495AJ · Boeing 727233 · Engine (Turbine/Turboprop)
  > VIBRATION FELT IN NR 1 POWER & FUEL LEVERS. VIBRATION REDUCED WHEN POWER REDUCED, ENG SHUT DOWN. WIND MILLED FOR 45 MINUTES WITH 30-35 PSI OIL PRESS.
- [SDR CA140113003](https://openairdocs.org/sdr/CA140113003.md): Coupling · failed · Jan 6, 2014 · Boeing 727223 · Pneumatic Distribution System
  > (CAN) AFTER TAKEOFF, ON CLIMB-OUT, THE FLIGHT CREW RECEIVED A NR 1 STRUT OVERHEAT INDICATION. THE ACFT RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL, UNSCHEDULED LANDING. UPON INSPECTION BY MAINTENANCE, A DUCT LEAK WAS FOUND AT THE NR 1 ENGINE STRUT HEA
- [SDR K11A2013070825002](https://openairdocs.org/sdr/K11A2013070825002.md): Window Frame · corroded · Jun 8, 2013 · N725CK · Boeing 727224 · Fuselage Main, Structure
  > MAIN DECK WINDOW FRAME CORRODED, BS 1080.
- [SDR K11A2013070825006](https://openairdocs.org/sdr/K11A2013070825006.md): Shear Tie · corroded · Jun 8, 2013 · N725CK · Boeing 727224 · Fuselage Internal Mounting Structure
  > FUSELAGE FRAME SHEAR TIE CORROSION BS 990, STR 28L.
- [SDR PCSA2013051001](https://openairdocs.org/sdr/PCSA2013051001.md): Fuel Control · faulty · May 6, 2013 · N598AJ · Boeing 727212 · Fuel Control/Turbine Engines
  > ENGINER 2 FLAMEOUT AT CRUISE. ALL PARAMETERS NORMAL. ENG WINDMILL FOR ABOUT 15 MIN. 20 PSI OIL PRESS. THE NR 2 ENGINE OIL FILTER WAS CHECKED, FOUND NORMAL, THE NR 2 FUEL PUMP AND FUEL CONTROL UNIT REPLACED AND TESTED PER THE B727 AMM AND THE AIRCRAFT RETURN
- [SDR CA130411007](https://openairdocs.org/sdr/CA130411007.md): Brake Assy · overheated · Apr 8, 2013 · Boeing 727225 · Landing Gear Brake System
  > (CAN) ON TAKE-OFF ROLL CREW NOTICED ACFT PULLING TO THE LT. T/O REJECTED AT 60KTS. UPON TAXING BACK TO GATE MAINTENANCE INFORMED CREW OF NR 2 BRAKE ON FIRE. APU FIRE EXTINGUISHER DISCHARGED. FIRE SERVICES CALLED, FIRE EXTINGUISED. FIRE WAS CONTAINED WITHIN
- [SDR FAA20140307000145](https://openairdocs.org/sdr/FAA20140307000145.md): Wheel · separated · Mar 19, 2013 · N45NA · Doug DC933F · Wheel/Ski/Float
  > ON LANDING, THE NLG, NR 2 WHEEL ASSY, INNER WHEEL RIM-BEAD SEPARATED FROM THE RIM ASSY. THE NR 2 NLG TIRE MAINTAINED AIR PRESSURE AND THE ACFT TAXIED FROM THE LANDING RUNWAY TO PARKING UNDER ITS OWN POWER. AFTER PARKING THE CREW DISCOVERED A DENT IN THE LT W
- [SDR CA130322008](https://openairdocs.org/sdr/CA130322008.md): Tube · broken · Mar 19, 2013 · Boeing 727225 · Landing Gear Retraction/Extension System
  > (CAN) DURING NORMAL TAXI IN TO RAMP NOSE GEAR DOORS OPENED WITH NORMAL HYD PRESSURE. LOUD BANG HEARD IN COCKPIT. MAINTENANCE FOUND THE NOSE GEAR DOOR SYNCHRONIZING ROD BROKEN. CRACK STARTED FROM GREASE FITTING HOLE. ROD REPLACED.
- [SDR PCSA2013020801](https://openairdocs.org/sdr/PCSA2013020801.md): Shutoff Valve · malfunctioned · Feb 5, 2013 · N495AJ · Boeing 727233 · Engine Fuel Distribution
  > AFTER START, ENGINE NR 2 SHUTDOWN. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL SHUTOFF VALVE PER THE B727 AMM.
- [SDR CA121210006](https://openairdocs.org/sdr/CA121210006.md): Housing · separated · Dec 7, 2012 · Boeing 727225 · Elevator Control System
  > (CAN) DISPATCH WAS NOTIFIED BY CREW THAT DURING TAXI FOR TAKEOFF, THE, A-SYSTEM HYDRAULIC PRESSURE WAS DROPPING AND THE QTY HAD DROPPED TO ZERO. THE CREW REQUESTED A TOW TO RETURN THE ACFT TO THE RAMP, NO NOSE WHEEL STEERING AVAILABLE. MAINTENANCE TOWED THE
- [SDR CA121207008](https://openairdocs.org/sdr/CA121207008.md): Fuel Cap · missing · Dec 5, 2012 · Boeing 727225 · Fuel Storage
  > (CAN) CREW ADVISED DISPATCH ON RADIO, 30 MINUTES AFTER DEPARTURE WITH MESSAGE THAT THEY WOULD RETURN BACK. NEXT CALL FLIGHT CREW NOTIFIED THAT THEY HAVE FUEL LEAK ON NR 3 ENGINE AND TANK IMBALANCE OF 5000 LBS. AFTER LANDING, MAINTENANCE ARRIVED AIRPLANE AND
- [SDR FDEA201209203363](https://openairdocs.org/sdr/FDEA201209203363.md): Packing · leaking · Sep 20, 2012 · N223FE · Boeing 727233 · Turbine Engine Oil System
  > LOST OIL QUANTITY ON THE NR 1 ENGINE DURING INITIAL CLIMB. QRH PROCEDURE WAS FOLLOWED. THE OIL QUANTITY DECREASED TO ZERO.THE OIL PRESSURE DECREASED BELOW 40PSI AND THE NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED. THE NR 1 ENGINE WAS SECURED FOLLOWING QRH PRO
- [SDR FDEA201209153330](https://openairdocs.org/sdr/FDEA201209153330.md): Transmitter · failed · Sep 15, 2012 · N494FE · Boeing 727227 · Engine Pressure Ratio (EPR)
  > REJECTED TAKEOFF AT 60 KNOTS NR 1 EPR ERROR AT 70 KNOTS. REMOVED AND REPLACED THE EPR TRANSMITTER.
- [SDR C8GA20120921011](https://openairdocs.org/sdr/C8GA20120921011.md): Accessory Unit · failed · Sep 15, 2012 · N801EA · Boeing 727225 · Landing Gear Retraction/Extension System
  > ON DEPARTURE, RECEIVED THREE RED GEAR LIGHTS WITH WARNING HORN, FOLLOWED ABNORMAL CHECKLIST, UNABLE TO RESOLVE. R & R LANDING GEAR ACCESSORY UNIT, OPS CHECKED GOOD, MX EVALUATION FLIGHT SUCCESSFUL.
- [SDR C8GA20120913010](https://openairdocs.org/sdr/C8GA20120913010.md): Switch · damaged · Sep 13, 2012 · N801EA · Boeing 727225 · Drag Control System
  > TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL ALL PARAMETERS NORMAL. ABORTED TAKEOFF. DURING TROUBLESHOOTING FOUND SPEED BRAKE TAKEOFF WARNING SWITCH S867 TERMINAL RINGS LOOSE AND NR 2 PIN RING TERMINAL BROKEN. SECURED RING TERMINALS AND REPAIRED NR 2 PIN RI
- [SDR CA120918024](https://openairdocs.org/sdr/CA120918024.md): Actuator · bent · Sep 13, 2012 · Boeing 727225 · Landing Gear Actuator
  > (CAN) DURING SHORT FINAL, THERE WAS NO POSITIVE INDICATION OF THE NOSE GEAR EXTENSION. THE FLIGHT CREW PERFORMED AN OVERSHOOT AND ENTERED INTO A HOLDING PATTERN. THE LANDING GEAR WAS RECYCLED WHICH DID NOT PROVIDE POSITIVE NLG EXTENSION. MANUAL GEAR EXTENSIO
- [SDR FDEA201209063246](https://openairdocs.org/sdr/FDEA201209063246.md): Slide · dislodged · Sep 6, 2012 · N467FE · Boeing 727225 · Escape Slide
  > ESCAPE SLIDE FELL OUT OF DOOR CONTAINER DURING FLIGHT/LANDING. R & R ESCAPE SLIDE AND HARDCASE IAW MM 25-60-015-2.
- [SDR FDEA201209053228](https://openairdocs.org/sdr/FDEA201209053228.md): Light · inoperative · Sep 5, 2012 · N487FE · Boeing 727227 · Emergency Lighting
  > FOUND COCKPIT EMERGENCY LIGHTS WILL NOT TEST FROM P5 OVERHEAD SWITCH. REPLACED COCKPIT EMERGENCY EXIT LIGHT IAW MM.
- [SDR FDEA201209053230](https://openairdocs.org/sdr/FDEA201209053230.md): Slide · dislodged · Sep 5, 2012 · N487FE · Boeing 727227 · Escape Slide
  > ON DESCENT, HEARD THUMP & DISCOVERED ESCAPE RAFT HAD FALLEN OUT OF COMPARTMENT. INSTALLED ESCAPE SLIDE INTO DOOR IAW MM CH 25-60-015-2.
- [SDR FDEA201208313201](https://openairdocs.org/sdr/FDEA201208313201.md): Slide · damaged · Aug 31, 2012 · N288FE · Boeing 7272D4 · Escape Slide
  > INDIVIDUAL EXPULTED THE EVACUATION SLIDE. R & R L1 DOOR ESCAPE SLIDE IAW MM 25-60-015-2.
- [SDR FDEA201208293193](https://openairdocs.org/sdr/FDEA201208293193.md): Slide · dislodged · Aug 29, 2012 · N467FE · Boeing 727225 · Escape Slide
  > MAIN DOOR SLIDE FELL OUT OF HOUSING UNIT. REINSTALLED L1 ESCAPE SLIDE IN AMM 25-60-015-2. ACFT OK FOR SERVICE.
- [SDR FDEA201208243149](https://openairdocs.org/sdr/FDEA201208243149.md): Oxygen Bottle · low · Aug 24, 2012 · N265FE · Boeing 727233 · Portable Oxygen System
  > PERFORMED TRANSIT CHECK. PORTABLE CREW OXYGEN BOTTLE LOW. REQUIRES REPLACEMENT. R & R FLIGHT CREW PORTABLE OXYGEN BOTTLE OPS NORMAL IAW MM35-30-000-0-0. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. R & R FLIGHT CREW PORTABLE OXYGEN BOTTLE OPS NORMAL IAW
- [SDR FDEA201208163040](https://openairdocs.org/sdr/FDEA201208163040.md): Slide · dislodged · Aug 16, 2012 · N467FE · Boeing 727225 · Escape Slide
  > WHEN ENTRY DOOR OPENED, GIRT BAR CAUGHT DOOR FRAME AND PULLED OUT EMERGENCY EXIT SLIDE PACK OUT OF UNIT. REMOVE DOOR SLIDE AND INSPECTED AND REINSTALLED PACK AMM 25-60-015-2. NO DEFECTS NOTED.
- [SDR CA120817008](https://openairdocs.org/sdr/CA120817008.md): Sliding Window · cracked · Aug 14, 2012 · Boeing 727231 · Flight Compartment Windows
  > (CAN) IN CRUISE NOTICED ARCHING ON R2 WINDOW AND DISCOVERED OUTER PANE WAS CRACKED. WINDOW REPLACED.
- [SDR FDEA201208042838](https://openairdocs.org/sdr/FDEA201208042838.md): Light · inoperative · Aug 4, 2012 · N494FE · Boeing 727227 · Emergency Lighting
  > DURING PRE-DEPARTURE CHECK, FOUND FWD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. PERFORMED TEST OF EMERGENCY ESCAPE SLIDE LIGHT IAW MM 33-50-041-2. OPS TESTS OK FOR SERVICE.
- [SDR FDEA201208032828](https://openairdocs.org/sdr/FDEA201208032828.md): Light · failed · Aug 3, 2012 · N469FE · Boeing 727225 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE, TOP FWD ENTRY DOOR. R & R EMERGENCY LIGHT IAW AMM 33-50-101-2.
- [SDR CA120817009](https://openairdocs.org/sdr/CA120817009.md): Sliding Window · cracked · Jul 31, 2012 · Boeing 727260 · Flight Compartment Windows
  > (CAN) R2 WINDOW OUTER PANE FAILED IN CRUISE, ACFT LANDED WITHOUT INCIDENT MAINTENANCE REPLACED WINDOW ASSY.
- [SDR PCSA2012072101](https://openairdocs.org/sdr/PCSA2012072101.md): Connector · damaged · Jul 19, 2012 · N598AJ · Boeing 727212 · Fire Protection System Wiring
  > ENGINE NR 2 FIRE WARNING BELL AND LIGHT ACTUATED IN FLIGHT.

Next page: https://openairdocs.org/engine/pratt-whitney-jt8d-15/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 = 'JT8D15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt8d-15/reports

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