Pratt & Whitney JT8D-1
Service difficulty reports · 195
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 = 'JT8D1' 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.
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 = 'JT8D1' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ABXA020349Fan · burned outSTRONG ELECTRICAL BURNING ODOR IN COCKPIT. RADIO RACK COOLING FAN FOUND TO BE SOURCE OF BURNING ODOR. REPLACED RADIO RACK COOLING FAN IAW MM. OPS CHECKED GOOD.SDR ABXA020353Link · crackedNR 1 ENGINE UPPER RIGHT LINK THRUST REVERSER CRACKED. REPLACED IAW MM.SDR 0203989955Skin · crackedIN MSP A 2.1 INCH CRACK WAS FOUND ON THE RIGHT SIDE OF FUSELAGE SKIN AT STA 1143 ABOVE L14. REPAIRED IAW EA.SDR 02FDEA00786Bushing · out of adjustMODERATE AIRFRAME FLUTTER ABOVE 280 KNOTS, GOES AWAY WITH SPEED BRAKE HANDLE PULLED TO ABOVE 5 DEGREES WHEN SLOWED DOWN, FLUTTER RETURNS DURING LEFT TURNS. FOUND RIGHT OUTBOARD TRAILING EDGE FLAP, ECCENTRICS REQUIRED ADJUSTMENT. ADJUSTED AFT FLAP ECCENTRIC BSDR ASAA0280448Lanyard · disconnectedDURING PREFLIGHT CHECK LANYARD BETWEEN GIRT BAR AND SLIDE COVER WAS FOUND DISCONNECTED. REATTACHED LANYARD.SDR ASAA0280424Lanyard · disconnectedDURING PREFLIGHT CHECK, LANYARD BETWEEN GIRT BAR AND SLIDE COVER, BECAME DISCONNECTED. REATTACHED LANYARD.SDR C7WA200200035Fitting · crackedDURING CPCP INSPECTION WITH JOB CARD C5322401 FOUND 8 INCH CRACK IN MAIN DECK HORIZONTAL FITTING BETWEEN BS 930 AND BS 950 AT STR 14L. C/A: REMOVED AND REPLACED HORIZONTAL FITTING AT STRINGER 14L. BETWEEN BS 930 AND BS 950 IAW SRM.SDR ASAA0282369Connector · disconnectedDURING PREFLIGHT CHECK SOME EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN WERE FOUND TO BE INOPERATIVE. REATTACHED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY.SDR GTIA020975Light · inoperativeL1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT 1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY.SDR GTIA020973Wire · disconnectedTAIL EMERGENCY AND EVACUATION LIGHTS, INOPERATIVE. FOUND WIRING NOT CONNECTED, RECONNECTED AND SECURED WIRING.SDR GTIA020972Horn · dentedRIGHT SLAT 0 HAS 2 DENTS IN LEADING EDGE. NR 1 15 INCH FROM INBOARD END. NR 2, 18 INCH FROM INBOARD END. SKIN HAS SCRATCHES BETWEEN THE 2 DENTS. REMOVED RIGHT WING SLAT HORN. INSTALLED RIGHT WING SLAT HORN NUMBER ZERO SLAT.SDR GTIA020969Longeron · corrodedMID B/B LONGERON 29L CORRODED AT STA 636, 648 AND 654. REMOVED L29L AT STA 589 TO 664.5 AND SPLICES. FABRICATED LONGERON IAW EA. INSTALLED SPLICES AT STA 589 TO 664.5.SDR GTIA020968Longeron · corrodedCORROSION HEAVY PITTING IN MID CARGO PIT F 674 AND 693 LONG 29L. REMOVED LONG 29L FROM 664.5 TO 740.5 FABRICATED LONGERON 29L AND 2 EACH LONGERON SPLICES , INSTALLED LONGERON AND SPLICES.SDR GTIA020955Door Frame · crackedAFT CARGO DOOR FRAME CLOSE OUT PANEL FS 1212, CRACKED. REMOVED PANEL, FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER.SDR RYN764511Skin · damagedAT C-CHECK, FOUND C-3 UPPER FORWARD DOOR SKIN CREASED AT STATION 1148.SDR GTIA020967Door Frame · corrodedMID PIT LOWER DOOR JAMB CUTOUT HAS CORROSION AT DOUBLER AT STA 522 TO STA 579. REMOVED DOUBLER AND CORRODED STRAP. FABRICATED STRAP. INSTALLED REMOVED DOUBLER AND NEW STRAP.SDR GTIA020970Skin · crackedL1 DOOR SKIN AREA AROUND HOOK CUTOUT CRACKED. REMOVED CRACK AT HOOK CUTOUT AT L1 DOOR. FABRICATED REPAIR, DOUBLER, INSTALLED REPAIRED DOUBLER.SDR GTIA020971Skin · dentedFROM CARRY OVER LIST, 3 DENTS ON NR 2 SLAT R WING, 1ST DENT XOS 204 DEPTH .016, 2ND DENT XOS 235 DEPTH .039, 3RD DENT XOS 264 DEPTH .019. ALL THREE DENTS ARE OUT OF LIMITS, REPAIRED DENTS.SDR RYN764543Seat Track · mismanufacturedAT (C) CHECK, FOUND CABIN SEAT TRACK TWO INCHES SHORTER THEN ORIGINAL CONFIGERATION AT STA 1110 TO 1130, RBL 22.SDR RYN764544Splice · failedAT (C) CHECK, FOUND SEAT TRACK SPLICE NOT REPAIRED IAW THE SRM AT STA 1110, RBL 44.SDR GTIA020286Engine · malfunctionedFLL - FLT 197 - LEFT ENGINE POWER LAGS BEHIND RIGHT ENGINE DURING POWER CHANGES IN CRUISE FLIGHT THROTTLES ARE SPLIT 1-1.25 TO MAINTAIN EVEN POWER SETTINGS. THROTTLES ARE SPLIT 1.5 AT CLIMB POWER. THIS GETS MORE PRONOUNCED AS ALTITUDE INCREASES. AUTO THROTTSDR TX22002F00000Bearing · failedDURING REMOVAL OF THE HORIZONTAL STABILIZER HINGE PINS TO COMPLY WITH THE AD AND SB. FOUND RIGHT HINGE BEARING TO HAVE FAILED WITH PIECES MISSING. LEFT BEARING WAS CRACKED. DURING FURTHER INSPECTION FOUND NUMEROUS BUSHINGS AND ATTACH HARDWARE IN THE HORIZONSDR RRX2001F00000Actuator · leakingLOST (A) SYSTEM HYDRAULIC PRESSURE DURING CLIMB OUT FROM MSY. ACCOMPLISHED EMERGENCY CHECKLIST RELATING TO LOSS OF (A) SYSTEM HYDRAULICS. EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 3 SLAT ACTUATOR ASSEMBLY AND OPERATIONAL CHECK SYSTSDR RYN2002F00004Stringer · corrodedSTRINGER EXFOLIATED BETWEEN BS 1148 TO BS 1166 BETWEEN STRINGER 3L AND 4L IN THE AFT CABIN CROWN AREA. ACCOMPLISHED FUSELAGE STRINGER REPAIR BS 1148 TO 1166 BETWEEN STRINGER 3L AND 4L. DUE TO CORROSION IAW SRM. (MATERIAL USED 301 CRESS .5000 HARD .050 INCH,SDR RYN2002F00001Skin · damagedBULGING/PILLOWING SKIN ALONG STRINGER 4L AT LAP JOINT BS 1130 THRU BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1130 TO BS 1183 STRINGER 4L DUE TO CORROSION IAW SRM. (MATERIAL USED 2024-T3 .050 INCH, 98 INCHES X 9.1250 INCHES)SDR RYN2002F00002Skin · damagedBULGING AND PILLOWING SKIN AT BS 1085 THRU BS 1110 ALONG FASTENER ROWS AT STRINGER 17R THRU 19R ON EXTERNAL FUSELAGE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1085 TO BS 1110 BETWEEN STRINGER 17R AND 19R DUE TO CORROSION IAW MFG ENGINEERING RO. (MATERIAL USSDR RYN2002F00003Skin · corrodedBULGING SKIN/DISHED FASTENER AT BS 1176 THRU BS 1183, STRINGER 20L THRU 21L UNDER AFT LAV SERVICE VALVE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1176 TO BS 1183 STRINGER 20L TO STRINGER 21L DUE TO CORROSION. (MATERIAL USED 2024-T3. 071, 28 INCHES X 30 INSDR AALA20011243Engine · leakingIAH - FLT 1963 - MIA-IAH, ON SHORT FINAL NR 1 ENGINE OIL QUANTITY DECREASED TO ZERO. LANDED IAH WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE. SYSTEM GROUND CHCKED NORMAL OPERATION. (M)SDR AALA20000729Valve · failedDFW - FLT 1044 - AFTER TAKEOFF WHILE PASSING THROUGH 900 AGL, NR 3 ENGINE HAD BANG AND SEVERE VIBRATION. EPR N1 AND N2 DROPPED BUT ROTATION CONTINUED. ENGINE EGT WENT TO 610 AND ENGINE SHUTDOWN. RETURNED TO LAND TO DFW. WHILE ATTEMPTING TO DUMP FUEL, LEFT SDR AALA991676Engine · malfunctionedCCS - FLT 2140 - EN ROUTE CCS/MIA - NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMB. WOULD NOT EXTINGUISH. AIRCRAFT RETURNED TO CCS AND LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF ALL DUCTS AT NR 1 ENGINE PYLON AND LOOP. ACCOMPLISHED ENGINE RSDR TWAA9914603Fuel Pump · failedABORTED TAKEOFF ROLL, DUE TO RT ENG COMPRESSOR STALL. FOUND RT ENG FUEL PUMP OUT PUT SHAFT SHEARED. REPLACED FUEL PUMP ASSY. CC00 7-20-99 STL.SDR 99ZZZX336Chip Collector · failedCHIP COLLECTOR ON RIGHT ENGINE, NR 4 BEARING SCAVENGE LINE, CHIP COLLECTOR MAGNETIC PROBE EJECTED FROM CHIP COLLECTOR BODY. ENGINE OIL DRAINED FROM ENGINE IN-FLIGHT. ANALYSIS DETERMINED THE INTERNAL CHECK VALVE OF CHIP COLLECTOR WAS STUCK IN THE OPEN POSITIOSDR 97ZZZX4281Drive Gear · wornENGINE AUTO ACCEL AT TAKEOFF. WORN SPLINES ON FUEL CONTROL DRIVE GEAR LED TO ZERO SPEED FAIL SAFE FUEL FLOW. DRIVE GEAR AND DRIVESHAFT WERE REPLACED.SDR 97ZZZX3846Case Assy · carbon build upINSPECTION OF COMPRESSOR CASE ASSY FOUND EXCESSIVE CARBON BUILD-UP.SDR 97ZZZX3847Case Assy · carbon build upINSPECTION OF COMPRESSOR CASE ASSY FOUND EXCESSIVE CARBON BUILD-UP.SDR 97ZZZX3848Diffuser Duct · crackedINSPECTION FOUND DIFFUSER DUCT WITH LENGTHY CRACKING ON OUTSIDE DIAMETER ADJACENT TO PORT AREAS.SDR 97ZZZX3849Diffuser Duct · crackedDIFFUSER DUCT INSPECTION FOUND LENGTHY CRACKING ON OUTSIDE DIAMETER ADJACENT TO PORT AREAS.SDR 97ZZZX3850Combustion Chamb · crackedINSPECTION OF COMBUSTION CHAMBER FOUND CRACKS IN FUSION WELD THIRD INNER SEAM. ALL UNITS WERE REJECTED, 7 EACH.SDR 97ZZZX3851Combustion Chamb · crackedINSPECTION OF COMBUSTION CHAMBER FOUND CRACKS IN FUSION WELD THIRD INNER SEAM. ALL UNITS WERE REJECTED, 7 EACH.SDR 97ZZZX3852Combustion Chamb · crackedINSPECTION OF COMBUSTION CHAMBER FOUND CRACKS IN FUSION WELD THIRD INNER SEAM. ALL UNITS WERE REJECTED, 7 EACH.SDR 97ZZZX3853Combustion Chamb · crackedINSPECTION OF COMBUSTION CHAMBER FOUND CRACKS IN FUSION WELD THIRD INNER SEAM. ALL UNITS WERE REJECTED, 7 EACH.SDR 97ZZZX3854Combustion Chamb · crackedINSPECTION OF COMBUSTION CHAMBER FOUND CRACKS IN FUSION WELD THIRD INNER SEAM. ALL UNITS WERE REJECTED, 7 EACH.SDR 97ZZZX3855Combustion Chamb · crackedINSPECTION OF COMBUSTION CHAMBER FOUND CRACKS IN FUSION WELD THIRD INNER SEAM. ALL UNITS WERE REJECTED, 7 EACH.SDR 97ZZZX3856Combustion Chamb · crackedINSPECTION OF COMBUSTION CHAMBER FOUND CRACKS IN FUSION WELD THIRD INNER SEAM. ALL UNITS WERE REJECTED, 7 EACH.SDR 97ZZZX1716C4 Disk · corrodedC4 DISK WAS RETURNED DUE TO CORROSION. DISK WAS RECEIVED WITH 3 BROKEN AND 6 BENT WINDAGE TABS. PER ENGINE MANUAL 481672 SECTION 72-33-35, INSP 01. THIS PART IS SCRAP. PART WAS TAGGED SCRAP AND RETURNED.
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