# Service difficulty reports: Pratt & Whitney JT8D-17A

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

Newest first. General aviation reporting is voluntary.

Page 1 of 8 · 362 reports

- [SDR MJYA20250613003](https://openairdocs.org/sdr/MJYA20250613003.md): Engine · damaged · Jun 13, 2025 · N467TW · Boeing 737205 · Engine (Turbine/Turboprop)
  > 112000 LBS TAKEOFF, FLAPS 1, V1=144 VR=147 V2=153, RIGHT SEAT TAKEOFF. AFTER NORMAL START AND TAXI OUT FROM WILSON AIR CENTER TO RUNWAY 18L WE PROCEEDED TO TAKE THE RUNWAY AS CLEARED. ROLL OUT WAS NORMAL WITH NORMAL ENGINE SPOOL UP TO STABILIZE ENGINE PARAMETE
- [SDR CA190221011](https://openairdocs.org/sdr/CA190221011.md): Tube · chafed · Feb 21, 2019 · Boeing 737200 · Engine (Turbine/Turboprop)
  > (CAN) ENGINE OIL CONSUMPTION ABNORMAL (CONSUMPTION INCREASING). CAUSE: #6 BEARING PRESSURE TUBE P/N 761392 CHAFFED. RECTIFICATION: #6 BEARING TUBE P/N 761392 REPLACED (TC# 20190221011)
- [SDR MJYA201812076003](https://openairdocs.org/sdr/MJYA201812076003.md): Hose · failed · Dec 4, 2018 · N467TW · Boeing 737205 · Hydraulic System, Main
  > DURING CRUISE FLIGHT PORTION ENROUTE FROM KCKB TO KEWR WE EXPERIENCED AN A SYSTEM HYDRAULIC LOSS. AS SOON AS THE ADVISORY LIGHT ILLUMINATED BOTH THE F.O. AND MYSELF VERIFIED 0 (ZERO) QUANTITY ON HYDRAULIC SYSTEM A. THE LOSS OF SYSTEM A CHECKLIST WAS PERFORME
- [SDR 2017F00024](https://openairdocs.org/sdr/2017F00024.md): Transmitter · faulty · Jan 8, 2017 · N467TW · Boeing 737205 · Trailing Flap Position Indicating System
  > FLAP ASYMMETRY ISSUE AFTER TAKE OFF. DECLARED AN EMERGENCY AND LAND AT ALTERNATE AIRPORT. AFTER TROUBLESHOOTING IT WAS DISCOVERED THAT THE RT FLAP TRANSMITTER AND THE FLAP INDICATOR WERE FAULTY. REPLACED FAULTY UNITS AND THE DISCREPANCY WITH THE FLAP ASYMMET
- [SDR MJYA20170108001](https://openairdocs.org/sdr/MJYA20170108001.md): Transmitter · failed · Jan 8, 2017 · N467TW · Boeing 737205 · Trailing Flap Position Indicating System
  > DURING CLIMB, THE PILOT TRIED TO SELECT FLAP UP WITH NO RESPONSE. THE FLAP INDICATION SHOWED THE RT FLAP AT 1 DEGREE AND THE LT FLAP AT 5 DEGREES. WITH NO RESPONSE TO THE FLAP HANDLE POSITION. DECLARED AN EMERGENCY AND LANDED AT AN ALTERNATE AIRPORT. THE AI
- [SDR CA151218005](https://openairdocs.org/sdr/CA151218005.md): Wire · burned · Dec 16, 2015 · Boeing 737200 · Ice/Rain Protection System Wiring
  > (CAN) FOUND LT WING ANTI-ICE VALVE OPEN WHEN ACFT WAS ON THE GROUND. FAULT WAS FOUND TO BE BURNED WIRING CAUSING THE VALVE TO OPEN AND THE CIRCUIT BREAKER TO OPEN ALONG WITH LT OTBD LANDING LIGHT CIRCUIT BREAKER TO OPEN. DAMAGED WIRING REPLACED AND ALL SYSTEM
- [SDR PCSA2014122201](https://openairdocs.org/sdr/PCSA2014122201.md): Engine · making metal · Dec 20, 2014 · N598AJ · Boeing 727212 · Engine (Turbine/Turboprop)
  > ENGINE NR 3 HAD A COMPRESSOR STALL & A FLAMEOUT AT FL320. METAL FOUND IN TAIL PIPE.
- [SDR CA140908023](https://openairdocs.org/sdr/CA140908023.md): Overheat Loop · open · Sep 7, 2014 · Boeing 737217 · Overheat Detection
  > (CAN) AT THE TOP OF DECENT, OUR ACFT ILLUMINATED AN ENGINE OVERHEAT INDICATION ON NR 1 ENGINE. THE CREW FOLLOWED THEIR NON-NORMAL CHECKLIST WHICH SAID TO RETURN THE ENGINE TO IDLE, WHICH IT ALREADY WAS, CUT FUEL TO THE ENGINE AND FIRE THE BOTTLE. THE OVERHEA
- [SDR CA140806001](https://openairdocs.org/sdr/CA140806001.md): Line · leaking · Aug 1, 2014 · Boeing 737217 · Engine Bleed Air System
  > (CAN) 1 ENGINE OVERHEAT ILLUMINATED. SHUTDOWN NR 1 ENGINE BOTH EXTINGUISHER BOTTLES DISCHARGED. UPON INVESTIGATION MAINTENANCE FOUND NR 1 ENGINE, 13TH STAGE BLEED AIR AND MODULATING VALVE SENSE LINE, PN BACH7D0137DD, BRAIDED HOSE ASSY LEAKING BLEED AIR ONTO
- [SDR 2WAA20140728001](https://openairdocs.org/sdr/2WAA20140728001.md): Engine · power loss · Jul 26, 2014 · N803WA · Doug DC982 · Engine (Turbine/Turboprop)
  > LOST THRUST ON LT ENGINE AFTER TAKEOFF. RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED NORMAL. ACCOMPLISHED NR 1 ENGINE DFGC INTERMIX WIRING IAW MM 71-02-00 PARA (F) PAGE 203. OPS CHECKED NORMAL.
- [SDR CA131213006](https://openairdocs.org/sdr/CA131213006.md): Engine · failed · Dec 11, 2013 · Boeing 7372L9 · Engine (Turbine/Turboprop)
  > (CAN) THE FLIGHT CREW REPORTED HEARING A LOUD BANG FROM THE NR 1 ENGINE AND LOSS OF THRUST. THE ACFT LANDED AND THE ENGINE WAS SHUTDOWN ON THE RUNWAY. MAINTENANCE HAS REPORTED FINDING DAMAGE TO THE POWER TURBINE, THE ENGINE WILL BE REPLACED.
- [SDR CA130905007](https://openairdocs.org/sdr/CA130905007.md): Duct · disconnected · Jul 28, 2013 · Boeing 7372T2 · Engine Bleed Air System
  > (CAN) AIR RETURN DUE TO HIGH, OFF SCALE, ENGINE OIL TEMPERATURE INDICATION. CREW FOLLOWED THE NON-NORMAL CHECKLIST AND ATTEMPTED TO SHUTDOWN THE ENGINE. CREW WAS UNABLE TO SHUTDOWN THE ENGINE USING THE START LEVER. THE CREW THEN PULLED THE FIRE WARNING HAND
- [SDR FDEA201209293509](https://openairdocs.org/sdr/FDEA201209293509.md): Blades · damaged · Sep 29, 2012 · N203FE · Boeing 7272S2F · Turbine Section
  > DURING CRUISE FLIGHT, NR 2 ENGINE THROTTLE LEVER BEGAN VIBRATING WITH ASSOCIATED MILD ACFT VIBRATION FELT. RAN QRH AND REDUCED NR 2 THROTTLE TO IDLE. SHORTLY AFTER REACHING, NR 2 ENGINE EXCELLERATED TO 92 PERCENT N2 AND REMAINED THERE WITH THROTTLE LEVER A
- [SDR SROM2011010](https://openairdocs.org/sdr/SROM2011010.md): Case · cracked · Jul 20, 2011 · N736BP · Boeing 737205 · Turbine Engine Air Inlet Section
  > REPLACED NR 1 ENGINE FAN INLET CASE DUE TO CRACKED FLANGE B WELD WITH OVERHAULED ASSEMBLY; FAN CASE P/N 786269, S/N DX6417, NR 1 BEARING HOUSING P/N 765471, S/N JU7622 AND REAR SUPPORT P/N 5003534-01, S/N LX9712 IN ACCORDANCE WITH PRATT AND WHITNEY MAINTENANCE
- [SDR CA110412006](https://openairdocs.org/sdr/CA110412006.md): Blade · failed · Apr 12, 2011 · Boeing 7372T2 · Engine (Turbine/Turboprop)
  > (CAN) SUSPECT T1 BLADE FAILURE, PRELIMINARY REPORT ONLY, MORE TO COME ONCE ENGINE IS TORN DOWN.
- [SDR TSAA1179002](https://openairdocs.org/sdr/TSAA1179002.md): Oil Filter · separated · Feb 18, 2011 · N841AL · Boeing 7372X6C · Turbine Engine Oil System
  > FLT 40. AFTER ADVANCING THE THROTTLES THE CREW NOTED THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATE FOLLOWED BY A DECREASE IN NR 2 ENGINE OIL QUANTITY. THE CREW ABORTED THE TAKE-OFF AND SHUTDOWN THE NR 2 ENGINE AND RETURNED TO THE CARGO RAMP. MAINTENANCE
- [SDR TSAA1072014](https://openairdocs.org/sdr/TSAA1072014.md): Element · false activation · Sep 9, 2010 · N840AL · Boeing 7372X6C · Fire Detection
  > CREW NOTED THE NR1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND SHUTDOWN THE NR 1 ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE NR1 ENGINE LOWER FIRE DETECTION SENSING ELEMENT IAW AMM 26-11-11, AND OPS CHECK WAS SATISF
- [SDR FDEA201009023245](https://openairdocs.org/sdr/FDEA201009023245.md): A/C Pack · failed · Sep 2, 2010 · N217FE · Boeing 7272S2F · Cabin Cooling System
  > ON TAKEOFF FROM DSM,THE LT PACK TRIPPED AND THE LT DUCT OVERHEAT LIGHT ILLUMINATED. THIS WAS ACCOMPAINED BY THE USUAL ODOR OF A PACK OVERHEATING AND SMOKE IN THE COCKPIT. QRH PROCEDURES ELIMINATED THE SMOKE & REESTABLISHED THE LT PACK. GIVEN THE OUTSIDE A
- [SDR FDEA201008263156](https://openairdocs.org/sdr/FDEA201008263156.md): Unknown · odor · Aug 26, 2010 · N217FE · Boeing 7272S2F · Air Distribution System
  > AIR TURNBACK, SMOKE IN COCKPIT, SMOKE APPEARED TO ORIGINATE FROM THE THROTTLE QUADRANT. VISIBLY CHECKED FWD NOSE COMPARTMENT WIRING, LIGHT BALLAST AND UNDER QUADRANT AREA, FOUND NO EVIDENCE OF FAULT. CHECKED AVIONICS BAY, WIRING, BOXES, FOUND LIGHTS ON EPG
- [SDR EE4Y100180](https://openairdocs.org/sdr/EE4Y100180.md): Angle · corroded · Jun 1, 2010 · N840AL · Boeing 7372X6C · Wing, Attach Fittings
  > ((EE4Y)) LT WING NR 2 SLAT OTBD MAIN TRACK AREA LOWER ANGLE WITH CORROSION. (W/O Y10122, SUB JOB 5, ITEM 18).
- [SDR CA100526002](https://openairdocs.org/sdr/CA100526002.md): Gearbox · leaking · May 25, 2010 · Boeing 737217 · Turbine Engine Accessory Drive
  > ENGINE WAS LEAKING OIL FROM AROUND THE BANJO FITTING, ENGINE APPROX 70HRS SINCE SHOP VISIT - GEARBOX TO BE REPLACED. THIS IS A PRELIMINARY REPORT ONLY
- [SDR FDEA201005071486](https://openairdocs.org/sdr/FDEA201005071486.md): Gearbox · leaking · May 7, 2010 · N211FE · Boeing 7272S2F · Accessory Gearboxes
  > DURING CRUISE NR 3 LOW OIL FILTER BYPASS LITE ILLUMINATED. OIL PRESSURE INDICATED 28PSI QTY WAS 3.5 GALLONS AND TEMP WAS 95 DEG, OPERATED 2 MIN AT IDLE SHUTDOWN IAW RED TABS DID NOT LOOSE OIL QTY. ENGINE CONTINUED TO WINDMILL AFTER SHUTDOWN. R & R THE NR 3
- [SDR FDEA200906182154](https://openairdocs.org/sdr/FDEA200906182154.md): Oil System · low pressure · Jun 18, 2009 · N479FE · Boeing 727227 · Engine Oil Pressure
  > LOW OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE ON S/O'S PANEL INDICATED YELLOW ARC, PREFORMED ENG FAIL/SHUTDOWN CHECKLIST. DURING CHECKLIST OIL QUANITY DROPPED RAPIDLY TO ZERO. OIL PRESSURE IN YELLOW ARE FOR APPROX 130 MIN. DURING DECENT PERFORMED ENG WIN
- [SDR CA100215002](https://openairdocs.org/sdr/CA100215002.md): Gcu · smoke · Apr 22, 2009 · Boeing 737217 · AC Generator-Alternator
  > (CAN) DURING ENGINE START THE GCU STARTED TO SMOKE, THE CREW REMOVED THE GCU, MX INSTALLED A SERVICEABLE GCU. (TC 20100215002)
- [SDR PCSA2008111101](https://openairdocs.org/sdr/PCSA2008111101.md): Transmitter · failed · Nov 11, 2008 · N199AJ · Boeing 7272F9 · Engine Oil Quantity
  > ON DESCENT IN SDQ OIL QUANTITY GAUGE NR 3 BLED SLOWLY DOWN TO ZERO QUANTITY. OIL PRESSURE AND TEMPERATURE NORMAL BUT WERE VERY LIGHT SO A PRECAUTIONARY ENGINE SHUTDOWN WAS DONE. A NORMAL LANDING WAS PERFORMED. AFTER LANDING OIL QUANTITY CHECKED FULL. ENGIN
- [SDR NWAA084589881](https://openairdocs.org/sdr/NWAA084589881.md): Fuse · failed · Oct 10, 2008 · N767MC · Beech C90 · Hydraulic Pump (Electric/Engine), Main
  > AFTER THE ACFT WAS PUSHED BACK FOR DEPARTURE AND FOLLOWING ENGINE START, THE RT HYDRAULIC SYSTEM LOST ALL FLUID. COM PROCEDURES WERE COMPLIED WITH AND THE ACFT RETURNED TO THE GATE. MX FOUND THE RT SIDE LOWER HYDRAULIC FUSE HAD FAILED. A HYDRAULIC SYSTEM RT
- [SDR SROM20080023](https://openairdocs.org/sdr/SROM20080023.md): Engine · bird ingestion · May 23, 2008 · N736BP · Boeing 737205 · Engine (Turbine/Turboprop)
  > INGESTED LARGE BIRD ON APPROACH TO AKU, SHUT-DOWN ENGINE AND COMPLETED MISSED APPROACH. DIVERTED TO SCC AND MADE UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 ENGINE.
- [SDR CA080630001](https://openairdocs.org/sdr/CA080630001.md): Engine · failed · May 22, 2008 · Boeing 737217 · Engine (Turbine/Turboprop)
  > (CAN) - ON DESCENT, A "BUZZING" SOUND WAS HEARD IN THE FLIGHT DECK FOR APPROX 5-10 SEC. THIS WAS FOLLOWED BY 1 OR 2 "POPS" AND THEN A LOUD "BANG" AT WHICH TIME THE NR 2 ENGINE LOST THRUST. NR 2 ENG TEMP CLIMBED BUT THERE WAS NO ENG OVERHEAT OR FIRE WARNING. A
- [SDR SROM2008017](https://openairdocs.org/sdr/SROM2008017.md): Bracket · cracked · Apr 6, 2008 · N733PA · Boeing 737205 · Engine Thrust Reverser
  > LEFT HAND ENGINE TAILPIPE CRACKED AT BRACKET MOUNT (3 O'CLOCK POSITION). REPAIRED LEFT HAND ENGINE TAILPIPE BRACKET MOUNT (3 O'CLOCK POSITION) IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3, 073-1236-08-477 AND ASI SOLUTIONS DRAWING 7830477-1, REV IR, DATED
- [SDR 2008032701](https://openairdocs.org/sdr/2008032701.md): Turbine Blades · failed · Mar 27, 2008 · N495AJ · Boeing 727233 · Turbine Section
  > FLT 433 MIA-BLA - CREW REPORTED, LOSS POWER ON NUMBER NR 3 ENGINE ON TAKEOFF. THE CAPTAIN REJECTED TAKEOFF ROLL AT APPROXIMATELY 10 KNOTS. AIRCRAFT RETURNED BACK TO AMERIJET LINE MAINTENANCE FACILITY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MULTIPLE TURB
- [SDR CA080225014](https://openairdocs.org/sdr/CA080225014.md): Clutch · disengaged · Feb 22, 2008 · Boeing 737200 · Trailing Edge Flap Control System
  > DEPARTING YOW THE AIRCRAFT EXHIBITED AN UNCOMMANDED ROLL TO THE LEFT REQUIRING 2-3 UNITS OF RUDDER TRIM TO CORRECT. THE CREW OBSERVED NO ASSYMMETRY INDICATION IN THE FLIGHT DECK BUT IT WAS VISUALLY CONFIRMED THAT THE RIGHT INBOARD AFT FLAP WAS PARTIALLY EXTEN
- [SDR CA080121003](https://openairdocs.org/sdr/CA080121003.md): Wire · inoperative · Jan 2, 2008 · Boeing 737217 · Navigation System Wiring
  > (CAN) TAIL 523 ON JAN 2ND APPROACH BACK COURSE ON RWY 15 YELLOWKNIFE 1040FT ASL 350FT AGL LEVEL FLIGHT 140K IN THIS CASE THE FLIGHT CREW EXPERIENCED A TAWS GENERATED A PICTORIAL DISPLAYED IMPACT WARNING. THE CREW WAS IN VISUAL CONDITIONS AND SAW NO DANGER OF
- [SDR DHL2007763001](https://openairdocs.org/sdr/DHL2007763001.md): Web · cracked · Nov 10, 2007 · N763AT · Boeing 727264 · Fuselage Miscellaneous Structure
  > A-6 CHECK, DISCREPANCY: AFT AIR STAIRS RT FWD LWR LIGHTING HOLE TORQUE BOX SKIN AREA IS CRACKED. ROUTED OUT CRACK IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER FROM 7075-T6.025 X 2 INCH X 4 INCH IAW SRM 51-40-2 AND 53-10-2, PN 9003505 ALODINED AND PRIMED IAW SRM
- [SDR CA071106012](https://openairdocs.org/sdr/CA071106012.md): Circuit Breaker · failed · Nov 4, 2007 · Boeing 737* · Autopilot System
  > (CAN) ENROUTE AT FL300, THE CREW EXPERIENCED AN AUTO PILOT DISENGAGEMENT AS WELL AS THE LOSS OF THE FOLLOWING, YAW DAMPER, MACH TRIM, CAPTS. PITOT STATIC, NR 1 ENG ANTI ICE, RADAR ALTIMETER, NO 2 EGT AND SEVERAL OTHERS. THE CREW ATTEMPTED A RESET OF THE NR 1
- [SDR 1014200701](https://openairdocs.org/sdr/1014200701.md): Overheat Loop · out of position · Oct 14, 2007 · N495AJ · Boeing 727233 · Overheat Detection
  > AT CRUISE FL 310 AMERIJET FLIGHT 875 NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT WENT OUT AFTER 2 MINUTES AND REMAINED OUT WITH ENGINE AT IDLE ONLY. THE FLIGHT DIVERTED TO KIN. MAINTENANCE DISCOVERED THE STRUT OVERHEAT DETECTOR TOUCHING THE PNEUMATIC D
- [SDR SROM200725](https://openairdocs.org/sdr/SROM200725.md): Wire · burned · Oct 5, 2007 · N736BP · Boeing 737205 · Engine Starting System Wiring
  > DURING CLIMB SPARKS AND SMOKE EMITTED FROM THE AREA OF THE NR 1 START SWITCH. LOW IGNITION CB POPPED AT WHICH TIME THE SPARKS AND SMOKE CEASED. FLIGHT CREW RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL LANDING. REPLACED SWITCH DUE TO ARCING ON CASE AND R
- [SDR DHLA200700045](https://openairdocs.org/sdr/DHLA200700045.md): Engine · power loss · Sep 22, 2007 · N781DH · Boeing 727227 · Engine (Turbine/Turboprop)
  > NUMBER ONE ENGINE DID NOT MAKE TAKEOFF THRUST, TAKEOFF REJECTED. ABNORMAL PROCEDURE COMPLETED N1 INDICATION 86 PERCENT ALL OTHER ENGINE PARAMETERS NORMAL.
- [SDR SROM200700018](https://openairdocs.org/sdr/SROM200700018.md): Skin · nicked · Aug 18, 2007 · N736BP · Boeing 737205 · Fuselage Main, Plate/Skin
  > NICK STA 907 STR 22 LT. NICK AT STA 907, STR 22L REPAIRED IAW SRM 53-30-3, FIG 48. NICK BEYOND LIMITS AND DAMAGE REMOVED. HFEC IAW NDT PART 6, 53-30-00, FIG 4 OF REPAIR AT FUSELAGE SKIN STA 907 STR 22L. NO CRACKS EVIDENT.
- [SDR SROM200700019](https://openairdocs.org/sdr/SROM200700019.md): Skin · nicked · Aug 18, 2007 · N736BP · Boeing 737205 · Fuselage Main, Plate/Skin
  > NICK STA 887 STR 24L-25L LT. DAMAGED AREA OF SKIN REMOVED AND REPAIR PLATES FABRICATED IAW SRM 53-30-3, FIG 48. INSTALLED REPAIR IAW 51-30-2.
- [SDR SROM200700020](https://openairdocs.org/sdr/SROM200700020.md): Skin · nicked · Aug 18, 2007 · N736BP · Boeing 737205 · Fuselage Main, Plate/Skin
  > NICK STA 847 STR 21 LT. NICK AT STA 847 STR 21L FOUND TO BE BEYOND LIMITS. NICK REMOVED AND AREA AT STA 847 STR 21L REPAIRED IAW SRM 53-30-3, FIG 48.
- [SDR SROM200700014](https://openairdocs.org/sdr/SROM200700014.md): Floorbeam · corroded · Aug 10, 2007 · N736BP · Boeing 737205 · Fuselage Main, Floor Beam
  > NR296-CORROSION ON FLOORBEAM UPPER FLANGE AT STA 294 AND RBL 43 TO 53. FLOORBEAM UPPER FLANGE FROM RBL 6 (EXISTING SPLICE) TO RBL 60, STA 294 REMOVED AND REPLACED IAW WITH MFG SRM 53-10-9, FIG 5, SHEET 1-5.
- [SDR SROM200700007](https://openairdocs.org/sdr/SROM200700007.md): Floorbeam · cracked · Aug 7, 2007 · N736BP · Boeing 737205 · Fuselage Main, Floor Beam
  > NR228-CRACK IN FLOORBEAM AND WEB STA 660 BL0. CRACKED FLOORBEAM AND WEB AT STA 660 BL0 REPAIRED IAW MFG SB 737-57-1210, REV 1, DATED AUG 27/07.
- [SDR SROM200700022](https://openairdocs.org/sdr/SROM200700022.md): Frame · corroded · Aug 3, 2007 · N736BP · Boeing 737205 · Fuselage Main, Frame
  > NR145-LIGHT CORROSION ON FRAME AT STA 783 STR 25R. REPAIRED FRAME IAW MFG MESSAGE NR 1-518342007-2, DATED AUG 1, 2007 AND PRODUCTION DRAWINGS FOR PN 65-47959-47 STRAP AND PN 65C31240-1 FRAME DOUBLER.
- [SDR 07FDEA00130](https://openairdocs.org/sdr/07FDEA00130.md): Engine · failed · Jan 18, 2007 · N280FE · Boeing 727200 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED DURING CLIMB-OUT AT APPROX 1500 FT ABOVE GROUND. NOTED HIGH EGT (AROUND 780 C), EPR 0, N1 AND N2 WINDMILLING. OIL QTY 3 GALS ENGINE FAILED WITH A LOUD BANG AND SPARKS REPORTED TRAILING AIRCRAFT BY TOWER. VISUAL INSPECTION OF ENGINE REVEA
- [SDR SROM200600021](https://openairdocs.org/sdr/SROM200600021.md): Landing Gear · contaminated · Dec 21, 2006 · N733PA · Boeing 737205 · Nose/Tail Landing Gear
  > UPON DEPARTURE DURING HEAVY SNOW CONDITIONS WITH GRAVEL SKI EQUIPPED AIRCRAFT THE NOSE GEAR UNLOCK LIGHT REMAINED ON AFTER LANDING GEAR RETRACTION. LANDING GEAR EXTENDED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITH NORMAL LANDING. UPON INSPECTION FOUND GR
- [SDR SROM200600017](https://openairdocs.org/sdr/SROM200600017.md): Accessory Unit · faulty · Nov 9, 2006 · N736BP · Boeing 737205 · Landing Gear Position and Warning
  > DURING DEPARTURE, UPON LANDING GEAR RETRACTION RT MLG INDICATION REMAINED RED. MOVED LANDING GEAR HANDLE TO OFF AND THEN BACK TO UP, RED INDICATOR LIGHT REMAINED ON. SELECTED GEAR DOWN AND GOT 3 GREEN AND NO RED. RETURNED TO ANC WITH NORMAL LANDING. WITH A
- [SDR DHL2006783004](https://openairdocs.org/sdr/DHL2006783004.md): Battery · inoperative · Nov 1, 2006 · N783DH · Boeing 727227 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES. OPS CK NORMAL IAW MM 33-50-71 PN-MISC062.
- [SDR DHL2006770517](https://openairdocs.org/sdr/DHL2006770517.md): Stringer · corroded · Oct 16, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/Stringer
  > BS 950F, STR 29R, OB STR CLIP HAS CORROSION. REMOVED FASTENERS FOR CORROSION REMOVAL IAW SRM 51-30-2. AFTER CORROSION REMOVAL IAW SRM 51-10-6 ON STR CLIP FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED DAMAGED STR CLIP IAW SRM 51-30-2. FAB PART FROM 60-
- [SDR DHL2006770519](https://openairdocs.org/sdr/DHL2006770519.md): Tab · delaminated · Oct 11, 2006 · N770AT · Boeing 7272B7 · Ailerons
  > LT WING, IB AILERON, TAB HAS T/E DAMAGE LWR IB SURFACE. REMOVED TAB IAW MM 27-10-11. CUT OUT DAMAGED AREA ON LWR SURFACE OF AILERON TAB APPOX 4.25 INCH BY 4.25 INCH IAW SRM 51-40-20 AND 51-30-2. FAB FILLER, 4.25 INCH BY 4.25 INCH AND DOUBLER 5.85 INCH BY 6 IN
- [SDR DHL2006513](https://openairdocs.org/sdr/DHL2006513.md): Stringer · gouged · Oct 2, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/Stringer
  > ASTAR NR 111564, DISCREPANCY: BS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPOX SIZE 2 INCH LENGTH IAW SRM 53-10-3 FIG.1. FAB REPAIR FILLER FROM BAC 1498-108, PO NR 6408112, APPOX 1 LONG IAW SRM 53-10-

Next page: https://openairdocs.org/engine/pratt-whitney-jt8d-17a/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 = 'JT8D17A'
ORDER BY difficulty_date DESC
```

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

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