Pratt & Whitney JT8D-9A

Service difficulty reports · 1,388

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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.

SDR 72300021Shear Tie · corroded1.25 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.Feb 1, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300022Shear Tie · corroded.75 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE.Feb 1, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300023Shear Tie · corroded1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.Feb 1, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300025Shear Tie · crackedAPPROX 1 INCH CRACK IN SHEAR TIE RADIUS.Feb 1, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300170Shear Tie · corrodedA .75 X 2 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.Feb 1, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300176Shear Tie · cracked.5 INCH CRACK IN SHEAR TIE RADIUS.Feb 1, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300072Frame · corrodedAPPROX 2 INCH BY 3 INCH AREA OF CORROSION ON FRAME.Jan 31, 2005 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 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 MINUJan 28, 2005 · N856AA · Boeing 727223 · Weather Radar SystemSDR 72300016Shear Tie · damagedLOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.Jan 25, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 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 TOJan 24, 2005 · Boeing 737210C · Turbine Engine Compressor SectionSDR 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.Jan 22, 2005 · Boeing 7372Q9 · Fuselage Main, Plate/SkinSDR 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 CYCLESJan 21, 2005 · Boeing 737296 · Fuselage Main, Plate/SkinSDR LCQ49Floor Panel · corrodedMAIN CABIN FLOOR PANEL NR 83 HAS SURFACE CORROSION AND A PUNCTURE. S/O 152051, OPS 29530, ZONE 6C-125Jan 20, 2005 · N867AT · Doug DC932 · Fuselage Floor PanelSDR LCQ54Panel · elongatedMAIN CABIN PANEL E5-3 HAS ELONGATED HOLES ON THE END OF PANEL. S/O 152051, OPS 29566, ZONE 6C-143Jan 20, 2005 · N867AT · Doug DC932 · Fuselage Miscellaneous StructureSDR LCQ56Channel · crackedMAIN CABIN PANEL NR 75 HAS CHANNELS CRACKED OUT AND SURFACE CORROSION. S/O 152051, OPS 29569, ZONE 6C-146Jan 20, 2005 · N867AT · Doug DC932 · Fuselage Miscellaneous StructureSDR LCQ57Channel · crackedMAIN CABIN PANEL, NR A53 HAS CHANNELS CRACKED. S/O 152051, OPS 29572, ZONE 6C-149Jan 20, 2005 · N867AT · Doug DC932 · Fuselage Miscellaneous StructureSDR 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-153Jan 20, 2005 · N867AT · Doug DC932 · Fuselage Floor PanelSDR 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-156Jan 20, 2005 · N867AT · Doug DC932 · Fuselage Floor PanelSDR 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-18Jan 19, 2005 · N867AT · Doug DC932 · Fuselage Main, Plate/SkinSDR 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-3Jan 19, 2005 · N867AT · Doug DC932 · Fuselage Main, StructureSDR 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 PRECAUTJan 17, 2005 · Boeing 737210C · Engine Bleed Air SystemSDR 72300026Stringer · corrodedCORROSION ON STRINGER 27R.Jan 17, 2005 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300039Stringer · corrodedSEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGER.Jan 17, 2005 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300071Angle · corroded1 INCH BY 3 INCH AREA OF CORROSION ON REINFORCEMENT ANGLE.Jan 17, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300073Frame · corroded1 INCH BY 3 INCH AREA OF CORROSION ON LOWER FRAME ANGLE.Jan 17, 2005 · N723CK · Boeing 7272H3 · Fuselage Main, FrameSDR 72300076Angle · corroded1 INCH BY 29 INCH AREA OF CORROSION ON ANGLE.Jan 17, 2005 · N723CK · Boeing 7272H3 · Fuselage Miscellaneous StructureSDR 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)Jan 14, 2005 · N69739 · Boeing 727224 · SpoilersSDR 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 SEJan 14, 2005 · Boeing 737242C · Pitot/Static SystemSDR 72300040Stringer · corrodedSEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGERJan 14, 2005 · N723CK · Boeing 7272H3 · Fuselage Main, Longeron/StringerSDR 72300068Shear Tie · gouged.1875 INCH DIAMETER GOUGE ON LOWER FLANGE OF SHEAR TIE.Jan 14, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300017Shear Tie · damagedLOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.Jan 14, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300024Shear Tie · gougedAPPROX (3) .1875 INCH GOUGES IN SHEAR TIE FLANGE.Jan 14, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300018Shear Tie · damagedLOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.Jan 14, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 72300161Shear Tie · gouged.9375 GOUGE AT SIDE OF FASTENER HOLE ON LOWER FLANGE OF SHEAR TIE.Jan 14, 2005 · N723CK · Boeing 7272H3 · Fuselage Internal Mounting StructureSDR 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 CYCLESJan 5, 2005 · Boeing 7372Q9 · Nose/Tail Landing Gear Attach SectionSDR 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.Dec 21, 2004 · N79754 · Boeing 727200 · Engine (Turbine/Turboprop)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.Dec 21, 2004 · N79754 · Boeing 727200 · Engine (Turbine/Turboprop)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 FIGDec 20, 2004 · Boeing 737201 · Nose/Tail Landing Gear Attach SectionSDR 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 FITTINDec 12, 2004 · Boeing 737210C · Compressor Bleed ValveSDR 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 LDec 1, 2004 · Boeing 7372H4 · Water/Waste System WiringSDR 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.Nov 29, 2004 · N856AA · Boeing 727223 · Fuselage Main, Plate/SkinSDR 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- 64477:16Nov 28, 2004 · Boeing 737201 · Fuselage Main, Plate/SkinSDR 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.Nov 28, 2004 · Boeing 7372Q9 · Fuselage Main, Plate/SkinSDR 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 Nov 27, 2004 · N819AL · Boeing 73725A · Engine (Turbine/Turboprop)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.Nov 26, 2004 · Boeing 737201 · Landing Gear ActuatorSDR 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 Nov 22, 2004 · Boeing 727225 · Landing Gear DoorsSDR 72300200Stiffener · corrodedA 2 X 3 INCH AREA OF CORROSION ON STIFFENER.Nov 22, 2004 · N723CK · Boeing 7272H3 · Fuselage Miscellaneous StructureSDR 72300070Skin · corrodedSEVERAL AREAS OF CORROSION ON LOWER FUSELAGE SKIN.Nov 19, 2004 · N723CK · Boeing 7272H3 · Fuselage Main, Plate/SkinSDR 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.Nov 18, 2004 · Boeing 737248C · Trailing Edge FlapsSDR 72300198Fitting · corrodedA 3 X 1 INCH AREA OF CORROSION ON FITTING.Nov 18, 2004 · N723CK · Boeing 7272H3 · Fuselage Miscellaneous Structure
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