# Service difficulty reports: Pratt & Whitney JT9D-3A

A list on [Pratt & Whitney JT9D-3A](https://openairdocs.org/engine/pratt-whitney-jt9d-3a.md).

Newest first. General aviation reporting is voluntary.

- [SDR BTIA2015F00006](https://openairdocs.org/sdr/BTIA2015F00006.md): Slide · no test · Nov 20, 2014 · N706BL · Boeing 747251B · Escape Slide
  > DURING CERTICATION EMERGENCY EVACUATION DRILL AT AIRPORT. DOOR 2L SLIDE/RAFT FAILED TO DEPLOY DUE TO THE DOOR NOT OPENING SUFFICIENTLY FOR INFLATION OF THE SLIDERAFT. THE EMERGENCY DOOR OPENING PROCESS WAS TERMINATED BY THE F/A DUE TO THE SLIDE COVER PARTIALLY
- [SDR FDEA201008263150](https://openairdocs.org/sdr/FDEA201008263150.md): Battery Pack · failed · Aug 26, 2010 · N417FE · Airbus A310222 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILED FROM THE COURIER AREA PUSHBUTTON. R & R EMERGENCY POWER SUPPLY BATTERY, TEST GOOD IAW AMM 33-51-14.
- [SDR FDEA201008132992](https://openairdocs.org/sdr/FDEA201008132992.md): Structure · worn · Aug 13, 2010 · N417FE · Airbus A310222 · Spoilers
  > LT WING SPOILER NR 3 T/E SILL IS WORN (KNIFE EDGE). R & R LT WING NR 3 SPOILER T/E RUB STRIP IAW SRM 51-40-21.
- [SDR FDEA201008042804](https://openairdocs.org/sdr/FDEA201008042804.md): Manifold · worn · Aug 4, 2010 · N417FE · Airbus A310222 · Engine Cooling System
  > (1) ENGINE LPT TCC LT BLEED AIR CONNECTOR HAS A LOOSE BOLT. R & R AND REINSTALLED THE NR 1 ENG LT TURBINE CASE COOLING MANIFOLD AND DUCT IAW A310-200 AMM 75-24-09-01. LEAK CHECKED GOOD IAW AMM 71-00-00-5-03.
- [SDR FDEA201008042805](https://openairdocs.org/sdr/FDEA201008042805.md): Duct · worn · Aug 4, 2010 · N417FE · Airbus A310222 · Engine Cooling System
  > NR 2 ENGINE INBD SIDE HAS FASTENERS LOOSE ON BLEED AIR DUCT. REMOVED, REPAIRED AND REINSTALLED NR 2 ENG INBD BLEED AIR DUCT AND MANIFOLD IAW AMM 75-24-10-4. LEAK CHECKED GOOD IAW AMM 71-00-00-5-03.
- [SDR FDEA201008042806](https://openairdocs.org/sdr/FDEA201008042806.md): Manifold · damaged · Aug 4, 2010 · N417FE · Airbus A310222 · Engine Cooling System
  > NR 2 ENGINE OTBD TURBINE CASE COOLING MANIFOLD HAS HAS HOLES WORN IN THE MAIN DUCT CONNECTION. REMOVED, REPAIRED AND REINSTALLED NR 2 ENG OTBD TURBINE CASE COOLING MANIFOLD IAW AMM 75-24-10-4. LEAK CHECK GOOD IAW AMM 71-00-00-5-03.
- [SDR FDEA201008042807](https://openairdocs.org/sdr/FDEA201008042807.md): Manifold · damaged · Aug 4, 2010 · N417FE · Airbus A310222 · Engine Bleed Air System
  > NR 2 ENGINE INBD TURBINE CASE COOLING MANIFOLD HAD ELONGATED BOLT HOLES. REPAIRED AND INSPECTED NR 2 ENG INBD TURBINE CASE COOLING MANIFOLD IAW MM 72-09-76-30, REPAIR NR 9. MANIFOLD REMOVED; REINSTALLED, AND LEAK CHECKED ON N/R N00322.
- [SDR FDEA201008022772](https://openairdocs.org/sdr/FDEA201008022772.md): Support Angle · corroded · Aug 2, 2010 · N417FE · Airbus A310222 · Vertical Stabilizer Miscellaneous Structure
  > DORSAL FIN, RT SIDE SUPPORT SPLICE ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398192920100 IAW SRM 51-74-10, AND 51-40-21, FIG 9, PARA 7, PG 24.
- [SDR FDEA201008022773](https://openairdocs.org/sdr/FDEA201008022773.md): Support Angle · corroded · Aug 2, 2010 · N417FE · Airbus A310222 · Vertical Stabilizer Miscellaneous Structure
  > DORSAL FIN RT SIDE FWD SUPPORT ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398197220100 IAW SRM 51-74-10 AND 51-40-21, FIG 9, PARA 7, PG 24.
- [SDR FDEA201007302769](https://openairdocs.org/sdr/FDEA201007302769.md): Housing · corroded · Jul 30, 2010 · N417FE · Airbus A310222 · Wing, Control Surface Attach Fittings
  > RT WING AILERON D4 HINGE BEARING HOUSING IS CORRODED.
- [SDR FDEA201007282695](https://openairdocs.org/sdr/FDEA201007282695.md): Floorbeam · corroded · Jul 28, 2010 · N417FE · Airbus A310222 · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT, UPPER MAIN CARGO DECK FLOORBEAM AT FRAME 54.3 HAS CORROSION AROUND A FASTENER HOLE, LT SIDE, BL-41L. REPAIRED FLOORBEAM IAW EA 6-5310-136372 "FUSELAGE - CROSSBEAM AT FR 54.3, CORROSION ON LOWER FLANGE".
- [SDR FDEA201007212634](https://openairdocs.org/sdr/FDEA201007212634.md): Support Angle · corroded · Jul 21, 2010 · N417FE · Airbus A310222 · Vertical Stabilizer
  > DORSAL FIN RIGHT SIDE; AFT SUPPORT ANGLE IS CORRODED. REMOVED CORROSION WITH MORE THAT 50% MATERIAL LOSS, OUT OF LIMITS IAW A310-200 SRM 51-74-10. REMOVED AFT SUPPORT ANGLE AND DRILLED UP NEW SUPPORT ANGLE; DEBURRED, INSTALLLED, SEALED AND PAINTED IAW A31
- [SDR FDEA201007192589](https://openairdocs.org/sdr/FDEA201007192589.md): Tee Fitting · cracked · Jul 19, 2010 · N417FE · Airbus A310222 · Wing Main, Frame Structure
  > LT TEE FITTING HOLE "C" SHOWS A CRACK INDICATION WHILE PERFORMING BHEC FOR NDT. CONTACT ENGINEERING. ENGINEER SHALL COORDINATE A REPAIR WITH ACFT MFG THAT IS ACCEPTABLE TO THE FAA OR DGAC. REPAIRED HOLE IAW EA 6-5710-136669, TITLE "WINGS - EO 5710-7-3322-C
- [SDR FDEA201007132495](https://openairdocs.org/sdr/FDEA201007132495.md): Fan Blade · cracked · Jul 13, 2010 · N417FE · Airbus A310222 · Turbine Engine Compressor Section
  > NR 2 ENGINE FAN BLADE NR 9 HAS CRACK IN RADIUS OF MID SPAN SHROUD. R & R NR 2 ENGINE NR 9 FAN BLADE AND NR 29 FAN BLADE IAW FDX A310-200 MM 72-21-02-4. BLADES WERE A MATCHED PAIR. NO FUTHER ACTION REQUIRED IAW FDX A310-200 MM 72-21-02-4 PARA. 3.C.
- [SDR FDEA201007082416](https://openairdocs.org/sdr/FDEA201007082416.md): Floor Support · corroded · Jul 8, 2010 · N417FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > FUSELAGE INTERNAL STRUCTURE,UNDER THE BULK CARGO FLOOR SUPPORT 48R HAS CORROSION FROM FRAME 66 TO FRAME 67. REMOVED CORROSION. TOTAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-17-14, PARA 1, PG 1. REMOVED AND REPLACED FLOOR SUPPORT SECTION AND SPLICE IAW
- [SDR FDEA201007022326](https://openairdocs.org/sdr/FDEA201007022326.md): Seat Track · corroded · Jul 2, 2010 · N417FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE SEAT TRACK HAS EXFOLIATION CORROSION FROM FRAME 18 TO FRAME 19, LBL 28. R & R SEAT TRACK IAW SRM 51-40-21 AND SRM 53-10-16, FIG 208, PARA 6.
- [SDR FDEA201007022337](https://openairdocs.org/sdr/FDEA201007022337.md): Frame · dented · Jul 2, 2010 · N417FE · Airbus A310222 · Fuselage Main, Frame
  > FUSELAGE INTERNAL STRUCTURE FRAME IS DENTED AT FRAME 54.2, STRINGER 13L. REPAIRED FRAME AS REQUIRED IAW EA 6-5310-123550.
- [SDR FDEA200911063882](https://openairdocs.org/sdr/FDEA200911063882.md): Engine · shutdown · Nov 6, 2009 · N417FE · Airbus A310222 · Turbine Engine Reduction Gear
  > ON LANDING ROLL, AT APPROX 80 KTS, NR 1 ENG SHUTDOWN. NR 1 UNLOCK LIGHT REMAINED ON, EGT WAS NOTED AT 670 DEG C AS N1 AND N2 DECRESED TO "0". NO OTHER DAMGE WAS NOTED. FUEL LEVER WAS SELECTED OFF. FIRE HANDLE WAS TESTED TO ENSURE NO MISSING FIRE INDICATIO
- [SDR TIPR20090020](https://openairdocs.org/sdr/TIPR20090020.md): Skin · damaged · Aug 27, 2009 · N768VA · Boeing 767222 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN REPAIR DOUBLER/STRAP AT FS 1222 AND S22-24R, REMOVED AND REPLACED REPAIR DOUBLER IAW REO-G12895 REV C, DATED 08/13/09.
- [SDR EIAA2006044](https://openairdocs.org/sdr/EIAA2006044.md): Engine · malfunctioned · Apr 5, 2006 · N479EV · Boeing 747132 · Engine (Turbine/Turboprop)
  > DURING FLIGHT, OIL PRESSURE LIGHT ILLUMINATED, PRESSURE CONFIRMED AT 0. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. REPLACED NR 3 ENGINE.

## 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 = 'JT9D3A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt9d-3a/reports

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