Pratt & Whitney JT9D-3A

Service difficulty reports · 20

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = 'JT9D3A'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR BTIA2015F00006Slide · no testDURING 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 PARTIALLYNov 20, 2014 · N706BL · Boeing 747251B · Escape SlideSDR FDEA201008263150Battery Pack · failedEMERGENCY LIGHTS TEST FAILED FROM THE COURIER AREA PUSHBUTTON. R & R EMERGENCY POWER SUPPLY BATTERY, TEST GOOD IAW AMM 33-51-14.Aug 26, 2010 · N417FE · Airbus A310222 · Emergency LightingSDR FDEA201008132992Structure · wornLT 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.Aug 13, 2010 · N417FE · Airbus A310222 · SpoilersSDR FDEA201008042804Manifold · worn(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.Aug 4, 2010 · N417FE · Airbus A310222 · Engine Cooling SystemSDR FDEA201008042805Duct · wornNR 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.Aug 4, 2010 · N417FE · Airbus A310222 · Engine Cooling SystemSDR FDEA201008042806Manifold · damagedNR 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.Aug 4, 2010 · N417FE · Airbus A310222 · Engine Cooling SystemSDR FDEA201008042807Manifold · damagedNR 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.Aug 4, 2010 · N417FE · Airbus A310222 · Engine Bleed Air SystemSDR FDEA201008022772Support Angle · corrodedDORSAL 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.Aug 2, 2010 · N417FE · Airbus A310222 · Vertical Stabilizer Miscellaneous StructureSDR FDEA201008022773Support Angle · corrodedDORSAL 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.Aug 2, 2010 · N417FE · Airbus A310222 · Vertical Stabilizer Miscellaneous StructureSDR FDEA201007302769Housing · corrodedRT WING AILERON D4 HINGE BEARING HOUSING IS CORRODED.Jul 30, 2010 · N417FE · Airbus A310222 · Wing, Control Surface Attach FittingsSDR FDEA201007282695Floorbeam · corrodedAFT 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".Jul 28, 2010 · N417FE · Airbus A310222 · Fuselage Main, Floor BeamSDR FDEA201007212634Support Angle · corrodedDORSAL 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 A31Jul 21, 2010 · N417FE · Airbus A310222 · Vertical StabilizerSDR FDEA201007192589Tee Fitting · crackedLT 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-CJul 19, 2010 · N417FE · Airbus A310222 · Wing Main, Frame StructureSDR FDEA201007132495Fan Blade · crackedNR 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.Jul 13, 2010 · N417FE · Airbus A310222 · Turbine Engine Compressor SectionSDR FDEA201007082416Floor Support · corrodedFUSELAGE 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 Jul 8, 2010 · N417FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR FDEA201007022326Seat Track · corrodedMAIN 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.Jul 2, 2010 · N417FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007022337Frame · dentedFUSELAGE INTERNAL STRUCTURE FRAME IS DENTED AT FRAME 54.2, STRINGER 13L. REPAIRED FRAME AS REQUIRED IAW EA 6-5310-123550.Jul 2, 2010 · N417FE · Airbus A310222 · Fuselage Main, FrameSDR FDEA200911063882Engine · shutdownON 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 INDICATIONov 6, 2009 · N417FE · Airbus A310222 · Turbine Engine Reduction GearSDR TIPR20090020Skin · damagedFUSELAGE SKIN REPAIR DOUBLER/STRAP AT FS 1222 AND S22-24R, REMOVED AND REPLACED REPAIR DOUBLER IAW REO-G12895 REV C, DATED 08/13/09.Aug 27, 2009 · N768VA · Boeing 767222 · Fuselage Main, Plate/SkinSDR EIAA2006044Engine · malfunctionedDURING FLIGHT, OIL PRESSURE LIGHT ILLUMINATED, PRESSURE CONFIRMED AT 0. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. REPLACED NR 3 ENGINE.Apr 5, 2006 · N479EV · Boeing 747132 · Engine (Turbine/Turboprop)
Back to Pratt & Whitney JT9D-3A