Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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 = 'JT8D15'
  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 03FDEA00134Control Panel · failedDURING CLIMB OUT AT MEM, COULD NOT PRESSURIZE, AUTO FAIL, STB. MANUAL NOTHING WORKED, PILOTS WINDOW HAD LOUD WIND NOISE BUT AIR FLOW NOT ENOUGH TO AFFECT PRESSURE, RAN EMERGENCY CHECKLIST AND NOTHING HAPPENED, RETURNED TO FIELD. PRESSURIZED AIRCRAFT TO 3 PSIFeb 15, 2003 · N284FE · Boeing 727200 · Cabin Pressure Control SystemSDR AUS20030152Hose · leaking(AUS) NR 2 ENGINE OIL PRESSURE TRANSMITTER SUPPLY LINE HOSE LEAKING.Feb 12, 2003 · Boeing 727277 · Turbine Engine Oil SystemSDR AUS20030271Angle · corroded(AUS) VERTICAL ANGLE LOCATED IN THE AVIONICS COMPARTMENT BILGE AT STA 368 LBL 15 CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030279Strap · corroded(AUS) INTERNAL SKIN REINFORCING STRAP LOCATED ON THE AFT SIDE OF FUSELAGE FRAME AT STA 1090 BETWEEN STRINGERS 26RT AND 27RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, StructureSDR AUS20030280Skin · corroded(AUS) NR 3 CARGO DOOR CUTOUT AFT LOWER CORNER CONTAINED LEVEL 2CORROSION IN THE AREA LOCATED BETWEEN SKIN LAMINATIONS AT STA 1140 TO 1148 AND BETWEEN STRINGER 26 RT AND STRINGER 27 RT. FOUND DURING CPCP INSPECTION IAW C53-111-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Plate/SkinSDR AUS20030281Intercostal · corroded(AUS) INTERCOSTAL LOCATED IN FORWARD CARGO AREA BETWEEN FRAME BS 580 AND FRAME BS 600 AT STRINGER 28 RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030282Frame · corroded(AUS) FUSELAGE FRAME LOWER LEG SHEAR TIES LOCATED AT BS 600 BETWEEN STRINGER 27 RT AND STRINGER 28 RT CONTAINED LEVEL 2 CORROSION.FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030283Frame · corroded(AUS) FUSELAGE FRAME LOWER LEG LOCATED AT ZONE 1 BS 580 BETWEEN STRINGER 27 RT AND STRINGER 28 RT CONTAINED LEVEL 2 CORROSION. FOUND DURINGCPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030284Frame · corroded(AUS) FUSELAGE FRAME FLANGE LOCATED AT BS 720A CONTAINED LEVEL 2 CORROSION IN AREA BETWEEN STRINGER 27R AND 28R. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030285Stringer · corroded(AUS) STRINGER SPLICE ON STRINGER 27L LOCATED AT BS 680 CONTAINED LEVEL2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030286Frame · corroded(AUS) FUSELAGE FRAME LOWER FLANGE CONTAINED LEVEL 2 CORROSION AT BS 660 BETWEEN STRINGER 26R AND STRINGER 27R. FOUND DURING CPCPINSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030287Stringer · corroded(AUS) STRINGER 27R CONTAINED LEVEL 2 EXFOLIATION CORROSION AT BS 480. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030288Frame · corroded(AUS) FUSELAGE FRAME LOCATED AT BS 1050 STRINGER 27R CONTAINED LEVEL 3 CORROSION ON THE TOP FLANGE. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030289Stringer · corroded(AUS) AFT CARGO STRINGER 27L CONTAINED LEVEL 2 CORROSION IN AREALOCATED BETWEEN BS950D AND BS1030. FOUND DURING CPCP INSPECTION IAW C53-013-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030290Stringer · corroded(AUS) STRINGER 30 CONTAINED LEVEL 2 IN AREA LOCATED AT BS1010. FOUNDDURING INSPECTION IAW CPCP C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030291Floorbeam · corroded(AUS) AFT CARGO FLOORBEAM ANGLE CONTAINED LEVEL 2 CORROSION IN AREALOCATED AT BS 1166 ABOVE STRINGER 27L BETWEEN BL16L AND BL23L. FOUND DURING INSPECTION IAW CPCP C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Floor BeamSDR AUS20030292Bracket · corroded(AUS) ANGLE BRACKET LOCATED AT CARGO FLOOR LEVEL BS 720D BL 21L CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030293Frame · corroded(AUS) FRAME FORMER LOCATED AT BS 1090 BETWEEN STRINGER 28R AND STRINGER29R CONTAINED LEVEL 2 CORROSION ON AFT FACE. FOUND DURING CPCPINSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030294Frame · corroded(AUS) FUSELAGE FRAME LOCATED IN BILGE AREA AT BS 970 BETWEEN STRINGER28R AND STRINGER 29R CONTAINED LEVEL 2 CORROSION ON THE LOWER LEG. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030295Frame · corroded(AUS) FUSELAGE FRAME LOCATED AT BS1130 CONTAINED LEVEL 2 CORROSION ON LOWER FLANGE IN AREA BETWEEN STRINGER 28L AND 29L. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030296Bracket · corroded(AUS) CLIP BRACKET JOINING STRINGER 27L TO FRAME AT LOCATION BS 1130 CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INVESTIGATION IAWC53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030297Stringer · corroded(AUS) STRINGER 27L CONTAINED LEVEL 2 CORROSION AT LOCATION BS 1128.FOUND DURING INSPECTION IAW CPCP C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030298Stringer · corroded(AUS) STRINGER 27L CONTAINED LEVEL 2 CORROSION IN AREA LOCATED BETWEEN BS 1070 TO BS 1090. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030299Intercostal · corroded(AUS) INTERCOSTAL IN AFT CARGO AREA CONTAINED LEVEL 2 CORROSION BETWEEN BS1070 TO BS1090 AND STRINGER 30. FOUND DURING CPCP INSPECTIONIAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030300Frame · corroded(AUS) FUSELAGE FRAME LOCATED AT BS 950B BETWEEN STRINGER 27R AND STRINGER 28R CONTAINED LEVEL 2 CORROSION ON THE LOWER FLANGE. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030301Stringer · corroded(AUS) STRINGER 29L CONTAINED LEVEL 2 CORROSION ON THE OUTBOARD LEG ON THE FORWARD AND AFT SIDES OF FRAME 950E. FOUND DURING CPCPINSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030302Frame · corroded(AUS) FUSELAGE FRAME BS 950E CONTAINED LEVEL 2 CORROSION ON LOWER FLANGE IN AREA LOCATED BETWEEN STRINGER 28L AND STRINGER 29L. FOUNDDURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030303Panel · corroded(AUS) AFT CARGO DOOR THRESHOLD PANEL CONTAINED LEVEL 2 CORROSION ANDREQUIRED REPLACEMENT DUE TO BEING WORN BEYOND LIMITS. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Plate/SkinSDR AUS20030153Filter · damaged(AUS) NR 1 ENGINE OIL FILTER THREAD STRIPPED. PERSONNEL/MAINTENANCE ERROR.Feb 11, 2003 · Boeing 727277 · Turbine Engine Oil SystemSDR AUS20030151Relief Valve · faulty(AUS) NR 1 ENGINE OIL PRESSURE RELIEF VALVE FAULTY.Feb 10, 2003 · Boeing 727277 · Turbine Engine Oil SystemSDR AUS20030268Flap Track · corroded(AUS) LT OUTBOARD FLAP OUTBOARD TRACK FORWARD ATTACHMENT FITTINGCONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTION IAW CPCP C57-581-06.Feb 8, 2003 · Boeing 727277 · Trailing Edge FlapsSDR AUS20030269Stringer · corroded(AUS) FUSELAGE STRINGER 18A LOCATED AT STN 930 RT CONTAINED LEVEL 2 CORROSION BETWEEN THE FASTENERS ON THE LOWER LEG OF THE TEE SECTION. FOUND DURING INSPECTION IAW CPCP C53-100-01.Feb 7, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030118Clamp · loose(AUS) NR 3 ENGINE THIRTEENTH STAGE MODULATING VALVE LEAKING FROM REAR DUCT CLAMP.Feb 5, 2003 · Boeing 727277 · Engine Bleed Air SystemSDR 03FDEA00053Duct · blownDURING CLIMBOUT WITH STANDARD TAKEOFF POWER SET, NR 1 ENGINE FIRELIGHT ILLUMINATED WITH HORN ON. SHUT DOWN ENGINE IAW WITH CHECKLIST. REMOVED AND REPLACED MAIN OIL STRAINER DUE TO INFLIGHT SHUT DOWN OF NR 1 ENGINE. ENGINE WINDMILLED FOR APPROXIMATELY 10 MINJan 18, 2003 · N257FE · Boeing 727200 · Pneumatic Distribution SystemSDR CA030123008Module · failed(CAN) DURING CLIMB, IT WAS OBSERVED THAT THE 'A' SYSTEM HYDRAULICS OVERHEAT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. THE 'A' SYSTEM HYDRAULIC MODULE WAS REPLACED AND CHECKED SERVICEABLE IAW WITH MM 29-11-52. 3. NO FURTHER INCIDENT DUJan 14, 2003 · Boeing 727223 · Hydraulic System, MainSDR 03FDEA00006Motor · failedCOMPLETE LOSS OF SYSTEM A HYDRAULIC FLUID JUST PRIOR TO FLAP EXTENSION. SPOILERS HAD BEEN USED JUST PRIOR TO LOSS. REPLACED RIGHT OUTBOARD FLAP MOTOR IAW MM, SERVICED HYDRAULIC SYSTEM TO FULL LEVEL. OPERATED FLAPS UP AND DOWN SEVERAL TIMES, ALL INDICATIONS Jan 8, 2003 · N244FE · Boeing 727200 · Trailing Edge Flap ActuatorSDR AUS20030267Skin · corroded(AUS) WING CENTER SECTION UPPER SKIN CONTAINED LEVEL 2 CORROSION AT SECTION 46 STN 825 RBL 13. FOUND DURING INSPECTION IAW CPCP C53-224-05.Jan 8, 2003 · Boeing 727277 · Wing, Plate/SkinSDR AUS20030270Spar · corroded(AUS) LT WING REAR LOWER SPAR CONTAINED LEVEL 3 CORROSION AT WS 200. FOUND DURING CPCP INSPECTION IAW C57-581-03.Jan 2, 2003 · Boeing 727277 · Wing SparSDR AUS20030304Stiffener · corroded(AUS) FORWARD SPAR LEADING EDGE VERTICAL STIFFENER CONTAINED LEVEL 2CORROSION LOCATED AT STN236. FOUND DURING CPCP INSPECTION IAW C57-562-02.Jan 2, 2003 · Boeing 727277 · Wing Miscellaneous StructureSDR SDR020040Shaft · shearedDURING CLIMB OUT, THROUGH 1000 FT ALT ENGINE NR 1 FLAMED OUT. (FUEL FLOW AND EPR WENT TO ZERO. DURING TAKEOFF ALL ENGINE INDICATIONS WERE NORMAL. C/W AOM PROCEDURES AND RETURNED TO AIRPORT. REMOVED AND REPLACED FUEL CONTROL UNIT AND FUEL PUMP FUEL PUMP UNIDec 24, 2002 · N802MA · Boeing 727225 · Fuel Control/Turbine EnginesSDR FX72003F00000Brake · seizedTHE AIRCRAFT WAS BEING TAXIED FROM BLAST FENCE FOR A DMI ON NR 3 EPR AND NR2 EGT INBOUND ITEM WHEN APPARENTLY THE NR 1 BRAKE SEIZED AND THE GEAR CAUGHT ON FIRE. THE AREA WAS INSPECTED IAW MFG TELEX FAX-MIA-02-00027H 06DEC02 AND SRM 51-10-4. THE GEAR WAS REPLDec 2, 2002 · N64346 · Boeing 727231 · Landing Gear Brake SystemSDR 02FDEA00917Stringer · crackedNR 8R STRINGER CRACKED AT RIB IN VERTICAL STABILIZER TUNNEL.Nov 24, 2002 · N264FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR AWXA200201206Skin · crackedMAJOR REPAIR, DURING C-14 CHECK A .500 INCH CRACK WAS FOUND ON AFT EDGE OF THE LEFT NR 1 DOOR INNER SKIN 12 INCHES ABOVE AFT LOWER LATCH ROLLER. NO NDT NEEDED, CRACK TERMINATES AT THE END OF SKIN. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM.Nov 20, 2002 · N189AW · Boeing 737277 · Passenger/Crew DoorsSDR AUS20021306Panel · separated(AUS) NO2 ENGINE RH FORWARD COWL BLOWOUT PANEL MISSING. PANEL WAS FOUND ON RUNWAY.Nov 14, 2002 · Boeing 727277 · Engine Cowling SystemSDR 02FDEA00831Warning System · malfunctionedON TAKEOFF, GEAR RETRACTED NORMALLY, ALL LIGHTS OUT. WHEN GEAR HANDLE MOVED TO OFF, RED DOORS LIGHT ILLUMINATED, NO INDICATION ON S/O PANEL. LIGHT WENT OUT WHEN HANDLE MOVED TO UP. REPEAT, GAVE SAME INDICATIONS. THIRD ATTEMPT, GEAR HANDLE OFF, ALL LIGHTS ONov 13, 2002 · N490FE · Boeing 727200 · Landing Gear Position and WarningSDR 02FDEA00840Floorbeam · corrodedCORROSION ON FLOORBEAM NUT PLATE HOLES BS 950F, LBL 10, WL 208. REMOVED CORROSION ON FLOORBEAM. FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PARTS IAW SRM.Nov 13, 2002 · N264FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00843Floorbeam · corrodedCORROSION BS 680, LBL 2 TO LBL 24, WL 208 FLOOR SUPPORT TOP AND BOTTOM. BLENDED CORROSION ON FLOORBEAM. FOUND FLOORBEAM TO BE OUT OF LIMITS IAW.Nov 13, 2002 · N264FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00839Floorbeam · corrodedCORROSION AT BS 344, WL 208, LBL 65 UNDERSIDE OF FLOORBEAM UPPER CHORD, AROUND THE NUTCLIP. REMOVED CORROSION ON FLOORBEAM UPPER CHORD. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED CHORD AND SPLICE IAW SRM.Nov 13, 2002 · N264FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00841Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM AROUND FLOORBOARD HOLES AT BS 680, RBL 4 TO RBL 21, WL 208. REMOVED AND REPLACED FLOORBEAM IAW EA AND ER.Nov 13, 2002 · N264FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00848Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE AROUND NUTPLATE HOLES AT BS 950C, RBL45-55, WL 208. REMOVED AND REPLACED FLOORBEAM IAW EA AND SRM.Nov 13, 2002 · N264FE · Boeing 727200 · Fuselage Main, Floor Beam
Back to Pratt & Whitney JT8D-15