Pratt & Whitney JT8D-9A
Service difficulty reports · 1,388
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 = 'JT8D9A' 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 = 'JT8D9A' 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 72300021Shear Tie · corroded1.25 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300022Shear Tie · corroded.75 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300023Shear Tie · corroded1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300025Shear Tie · crackedAPPROX 1 INCH CRACK IN SHEAR TIE RADIUS.SDR 72300170Shear Tie · corrodedA .75 X 2 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.SDR 72300176Shear Tie · cracked.5 INCH CRACK IN SHEAR TIE RADIUS.SDR 72300072Frame · corrodedAPPROX 2 INCH BY 3 INCH AREA OF CORROSION ON FRAME.SDR GAIA05003OPIndicator · shortedDURING DESCENT THE RADAR SCREEN FLARED BRIGHTLY, THE RADAR TCAS DISPLAY WENT OUT. SHORTLY AFTERWARD A STRONG ELECTRICAL SMELL WAS NOTICED. THE RADAR AND TCAS WERE TURNED OFF AND ASSOCIATED CIRCUIT BREAKERS WERE PULLED. THE SMELL DISSIPATED WITHIN A FEW MINUSDR 72300016Shear Tie · damagedLOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.SDR CA050128004Engine · failed(CAN) DEPARTING, THE NR2 ENGINE PERAMETERS BECAME ERRATIC ASSOCIATED WITH A LOUD REPORT, BELIEVED TO BE A COMPRESSOR STALL. THE AIRCRAFT LANDED WITHOUT INCIDENT AT POINT OF DEPARTURE. MAINTENANCE FOUND THE NR2 ENGINE TO HAVE SUFFERED SEVERE INTERNAL DAMAGE TOSDR CA050125010Skin · cracked(CAN) AN OUTER FUSELAGE CRACK WAS DISCOVERED AT STRINGER S-18R, STATION 750, APPROXIMATELY 1.125 INCHES LONG. THE CRACK WAS REPAIRED IAW SRM 53-30-3 FIGURE 48, DETAIL IX AND DETAIL XIX.SDR CA050125007Skin · cracked(CAN) AN OUTER FUSELAGE CRACK WAS FOUND DURING A PHASE EIGHT CHECK AT STRINGER 16L, STATION 727+14.5 APPROXIMATELY 1.5 INCHES IN LENGTH. FUSELAGE CRACK REPAIRED IAW REO-L00889 REV 1R TIMES - 59761:05 HOURS AND 54470 CYCLESSDR LCQ49Floor Panel · corrodedMAIN CABIN FLOOR PANEL NR 83 HAS SURFACE CORROSION AND A PUNCTURE. S/O 152051, OPS 29530, ZONE 6C-125SDR LCQ54Panel · elongatedMAIN CABIN PANEL E5-3 HAS ELONGATED HOLES ON THE END OF PANEL. S/O 152051, OPS 29566, ZONE 6C-143SDR LCQ56Channel · crackedMAIN CABIN PANEL NR 75 HAS CHANNELS CRACKED OUT AND SURFACE CORROSION. S/O 152051, OPS 29569, ZONE 6C-146SDR LCQ57Channel · crackedMAIN CABIN PANEL, NR A53 HAS CHANNELS CRACKED. S/O 152051, OPS 29572, ZONE 6C-149SDR LCQ61Floor Panel · brokenMAIN CABIN FLOOR PANEL NR 76 RT CENTER FS 680 - 760 IB HAS HOLES BROKEN OUT ON THE END. S/O 152051, OPS NR 29576, ZONE 6C-153SDR LCQ62Floor Panel · crackedMAIN CABIN FLOOR PANEL NR 81 HAS CRACKS AROUND RIVETS, 2 EACH PUNCTURES AND SURFACE CORROSION. S/O 152051, OPS NR 29583, ZONE 6C-156SDR LCQ30Skin · lightning strikeAIRCRAFT NOSE RT STA 69, APPROX. 15 INCHES ABOVE FLOOR REFERENCE PLANE HAS A LIGHTNING STRIKE. S/O 152051, OPS 29036, ZONE 1A-18SDR LCQ37Door Frame · corrodedSTA. 908.5, AFT CARGO DOOR FRAME WEB HAS CORROSION ON VERTICAL SUPPORT, FOUR CORNERS FWD SIDE. S/O 152051, OPS 29258, ZONE 1E-3SDR CA050204002Mixer Box · separated(CAN) ON DEPARTURE, FORWARD CLOSET SMOKE DETECTOR ACTIVATED AND ACRID SMELL DETECTED IN CABIN. RETURNED WITHOUT FURTHER INCIDENT. FOUND BLEED AIR DUCT AT AIR DISTRIBUTION MANIFOLD LT SIDE A-DRIFT, SECURED DUCT AND LEAK CHECK CARRIED OUT. AS A FURTHER PRECAUTSDR 72300026Stringer · corrodedCORROSION ON STRINGER 27R.SDR 72300039Stringer · corrodedSEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGER.SDR 72300071Angle · corroded1 INCH BY 3 INCH AREA OF CORROSION ON REINFORCEMENT ANGLE.SDR 72300073Frame · corroded1 INCH BY 3 INCH AREA OF CORROSION ON LOWER FRAME ANGLE.SDR 72300076Angle · corroded1 INCH BY 29 INCH AREA OF CORROSION ON ANGLE.SDR GAIA05001STBracket · crackedDURING B-CHECK A CRACK WAS FOUND ON THE NR 3 SPOILER ACTUATOR ATTACH BRACKET AT WING STATION 501. REMOVED AND REPLACED SPOILER ACTUATOR ATTACH BRACKET. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR CA050121003Quick Disconnect · failed(CAN) AC ENCOUNTERED AUTOPILOT, STATIC AIR TEMP INDICATION ANOMALIES. AUTOPILOT PITCH, ROLL COMPUTERS ALONG WITH 3 AIR DATA COMPUTERS (ADC). FOUND PITOT LINE QUICK DISCONNECT TO ADC HAD FAILED. INTERNAL BARREL THAT OPENS PITOT LINE TO ADC HAD FAILED. LINE SESDR 72300040Stringer · corrodedSEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGERSDR 72300068Shear Tie · gouged.1875 INCH DIAMETER GOUGE ON LOWER FLANGE OF SHEAR TIE.SDR 72300017Shear Tie · damagedLOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.SDR 72300024Shear Tie · gougedAPPROX (3) .1875 INCH GOUGES IN SHEAR TIE FLANGE.SDR 72300018Shear Tie · damagedLOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.SDR 72300161Shear Tie · gouged.9375 GOUGE AT SIDE OF FASTENER HOLE ON LOWER FLANGE OF SHEAR TIE.SDR CA050111001Gusset · cracked(CAN) DURING A ROUTINE PHASE 3 CHECK (137.5 HRS.), A 2.75 INCH CRACK WAS FOUND ON THE NOSE LANDING GEAR GUSSET WHILE CARRYING OUT SERVICE DIFFICULTY ALERT AL-2002-03.RETRACT ACTUATOR SUPPORT FITTING GUSSET REPLACED IAW SRM 51-30-2 FIG II. TIMES. 61981.7 CYCLESSDR XNO1218Engine · malfunctionedNR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME.SDR XNOA1218Engine · malfunctionedNR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME.SDR CA041222017Gusset · cracked(CAN) DURING A ROUTINE PHASE 2 CHECK (137.5 HRS.) A 3.5 INCH (THREE AND A HALF INCH) CRACK WAS FOUND ON THE NOSE LANDING GEAR GUSSET WHILE CARRYING OUT SERVICE DIFFICULTY ALERT AL-2002-03. RETRACT ACTUATOR SUPPORT FITTING GUSSET REPLACED IAW SRM 51-30-2 FIGSDR CA041214001Fitting · loose(CAN) AT TRANSITION TO CRUISE FL 350 AFTER DEPARTURE, THE NR 2 ENGINE APPEARED TO SURGE OR COMPRESSOR STALL. AFTER 2 ATTEMPTS TO REDUCE THROTTLE THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE FOUND A LEAK AT THE PS4 FITTINSDR CA041203008Wire · arced(CAN) THE POTABLE WATER INDICATION BECAME INOPERATIVE AND WAS DEFERRED. TROUBLESHOOTING FOUND WIRES IN THE AREA NEAR THE WATER TANK ON A BELLY STRINGER AT STN 960 TO BE BURNED BY ARCING. WIRES AFFECTED WERE POTABLE WATER INDICATION, R2 DOOR WARNING LIGHT AND LSDR GAIA04174AOPSkin · dentedNO FLIGHT: DURING WALK AROUND, A LARGE DENT WAS FOUND ON THE LT SIDE OF THE NOSE OF THE AIRCRAFT BELOW THE L2 WINDOW. THE AIRCRAFT WAS FERRIED FOR REPAIR.SDR CA041129010Skin · cracked(CAN) FUSELAGE CRACK FOUND ON OUTER SKIN AT STN. 955.9 - 959.65 BELOW STR. 21L. FUSELAGE CRACK REPAIRED IAW SRM 53-30-3 FIG 48 DETAIL X. TIMES- 64477:16SDR CA041203006Skin · cracked(CAN) AN OUTER FUSELAGE CRACK WAS FOUND AT STR 16 LT BETWEEN STA 767 & 787 APPROX 2 INCHES LONG. FUSELAGE CRACK REPAIRED IAW SRM 53-30-1 FIG.48 PROCEDURES I, IV & VII. THIS REPAIR IS TIME LIMITED UNTIL 25 FEB. 04. TIMES- 61761:52 CYCLES- 57769.SDR TSAA0472079Engine · failedNON-ETOPS FLT. 241, HNL-LIH: CLIMBING THROUGH 8,000 FEET, HEARD A LOUD BANG AND THE AIRCRAFT YAWED RIGHT. THE NR 2 ENGINE EPR DROPPED FROM 1.82 TO 1.76. REPORTED THAT A PASSENGER OBSERVED FLAMES EXITING THE NR 2 ENGINE EXHAUST. ALL OTHER ENGINE INDICATIONS SDR CA041129008Actuator · malfunctioned(CAN) NOSE WHEEL DISAGREEMENT LIGHT REMAINED ON AFTER GEAR SELECTED UP. RETURNED TO FIELD. NOSE GEAR LOCK ACTUATOR REPLACED, AND GEAR SWINGS C/O. CHECKED SERVICEABLE. TIMES- 59932:32 CYCLES- 55882.SDR CA041125001Bracket · broken(CAN) UPON ARRIVAL, MAINTENANCE PERSONEL NOTED THE NOSE LANDING GEAR DOORS HANGING OPEN. FURTHER INSPECTION FOUND THE BRACKET FOR THE DOOR OPERATION ROD BROKEN. SEE IPC 32-30-00-06 ITEM 89. BRACKET AND HARDWARE REPLACED AND GEAR SWINGS CARRIED OUT, AND A/C SDR 72300200Stiffener · corrodedA 2 X 3 INCH AREA OF CORROSION ON STIFFENER.SDR 72300070Skin · corrodedSEVERAL AREAS OF CORROSION ON LOWER FUSELAGE SKIN.SDR CA041102003Carriage · cracked(CAN) DURING COMPONENT REPLACEMENT AT HEAVY CHECK, A TYPICAL CRACK WAS DETECTED AT THE SPINDLE JOURNAL FORWARD END ON FLAP CARRIAGE NR 7.SDR 72300198Fitting · corrodedA 3 X 1 INCH AREA OF CORROSION ON FITTING.
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