Pratt & Whitney JT8D series

Service difficulty reports · 1,122

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 = 'JT8D'
  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 C8GA2010000029Bulkhead · corrodedWHILE IN HEAVY MX PERFORMING INSP, THE INTERNAL CABIN AFT PRESSURE BULKHEAD RT STATION 1183 LOWER LOBE WEB WAS CORRODED. FABRICATED LOWER LOBE WEB FROM 2024 T3 .040" R & R LOWER LOBE, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Aug 24, 2010 · N755DH · Boeing 727225 · Fuselage Main, BulkheadSDR DALA1020529759Battery Pack · inoperativeDURING LINE CHECK, MX FOUND EMERGENCY TRACK LIGHTS AFT CABIN INOPERATIVE. MX REPLACED BATTERIES IN AFT POWER SUPPLY. OPERATION OF LIGHTS ARE NORMAL ACFT OK FOR SERVICE.Aug 24, 2010 · N759NW · Doug DC941 · Emergency LightingSDR DALA1020020909Skin · chafedVERTICAL STAB REMOVABLE L/E LOWER FASTENERS LOOSE, SKIN WASHERS DIGGING INTO VERT SKIN.Aug 20, 2010 · N909DL · Doug MD88 · Vertical Stabilizer, Plate/SkinSDR DALA1020350928Door Frame · corrodedFOUND DURING OPN 57422 INSP OF CARGO DOOR JAMBS, CORROSION AT C-3 DOOR JAMB LOWER CUT-OUT, STA 1154 TO 1211. FABRICATED NEW STRAP IAW SRM 53-05, FIG 103. INSTALLED NEW STRAP IAW SRM 53-05, FIG 123.Aug 20, 2010 · N928DL · Doug MD88 · Fuselage Main, StructureSDR DALA1019430977Oil System · leakingON CLIMB OUT, F/A REPORTED SMOKE IN THE CABIN WITH AFT LAVATORY SMOKE DETECTORS SOUNDING. MX ACCOMPLISHED OPS, 5088 SMOKE IN CABIN TROUBLESHOOTING. FOUND APU LEAKING OIL, CORRECTED OIL LEAK AND ACCOMPLISHED SEVERAL DUCT BURN OUTS IAW OPS 5089. REPLACED H2O Aug 13, 2010 · N977DL · Doug MD88 · APU Oil SystemSDR DALA1019470986Light · inoperativeMX FOUND THE ESCAPE PATH LIGHT AT SEAT 2C TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.Aug 13, 2010 · N986DL · Doug MD88 · Emergency LightingSDR DALA1019629001Pan · crackedDURING HMV3, FOUND MID CARGO DOOR AFT END BETWEEN NR 2 AND NR 3 BEAMS. BEAM PAN HAS APPROX 2" CRACK ABOVE END FITTING. STOP DRILLED CRACK IAW SRM 51-01, HFEC INSP VERIFIED CRACK CONTAINMENT IAW NDT SPM 06-10-01 LOCATED DRILLED AND INSTALLED NEW REPAIR DOUBLERAug 11, 2010 · N901DE · Doug MD88 · Fuselage Main, StructureSDR DALA1019279001Skin · crackedLT WING L/E SKIN/LOWER SURFACE XOS 243 CRACKED. INSTALLED PERMANENT REPAIR IAW ERA 380953-14MA AND ERA 482367-14.Aug 9, 2010 · N901DE · Doug MD88 · Wing, Plate/SkinSDR DALA1017460983Connector · damagedTHE EMERGENCY FLOOR LIGHTS AT SEAT 10D WERE FOUND TO BE INOPERATIVE. MX RE-TERMINATED THE LIGHT CONNECTORS. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.Jul 25, 2010 · N983DL · Doug MD88 · Light System WiringSDR DALA1017450974Light · inoperativeMX FOUND THE EMERGENCY PATH LIGHT AT SEAT 30D TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.Jul 24, 2010 · N974DL · Doug MD88 · Emergency LightingSDR FDEA201007212633Valve · failedON CLIMBOUT NOTICED NR 1 OIL TEMP IN YELLOW RANGE. RAN THE QRH AND AFTER 15 MINUTES WE SHUT DOWN THE NR 1 ENGINE PER THE QRH. OPERATED NR 1 ENG FUEL HEAT SWITCH VALVE NO INDICATION NOTED.VISUALLY CHECKED FUEL HEAT VALVE, FOUND OPEN.REMOVED AND REPL ACED VJul 21, 2010 · N284FE · Boeing 727233 · Engine Oil Indicating SystemSDR DALA1016530962Oil Cap · misinstalledDURING CLIMB PASSING THROUGH 8000 FT, THE CABIN CREW REPORTED A BURNING OIL SMELL FOLLOWED BY THE AFT LAVATORY SMOKE DETECTORS SOUNDING. SMELL DISSIPATED AND FLIGHT CONTINUED TO ATL. UPON ARRIVAL MAINTENANCE FOUND THE APU OIL CAP IMPROPERLY INSTALLED. REPLAJul 14, 2010 · N962DL · Doug MD88 · APU Oil SystemSDR FDEA201007142561Skin · gougedSURROUND INNER SKIN GOUGES STA 640 STR 16L COMPLIED WITH EA 7-5330-135570 FUSELAGE AD 98-11-03 R1, SURROUND STRUCTURE, INNER SKIN GOUGE REPAIR BY BLENDING GOUGES IAW SRM 727 51-10-01 AND EA 7-5330-135570 AND FOUND WITHIN LIMITS EA 7-5330-135570.Jul 14, 2010 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR DALA1018939005Spar Cap · crackedREF EA 09-471576-12, REV ORIG ME05 HIDDEN DAMAGE: CRACK OF APROX 3.312 INCH ON THE RT WING LOWER SPAR CAP AT STA XRS=108 REF NRC T0178869 AND T0179341. SLOT CUT CRACK IAW AMR 0907304 REV 3, FAB NEW SPLICES IAW AMR0957304, REV 3 REPAIR INSTRUCTIONS 23 AND 24. TJul 14, 2010 · N905DE · Doug MD88 · Wing SparSDR FDEA201007092440Skin · gougedSURROUND INNER SKIN GOUGED STA 620, STR 5L. REMOVED INNER SKIN 600 TO 640 UPPER AFT IAW SRM 51-30-2. FABRICATED INNER SKIN FROM 2024T3 .125 DIM 48" X 79" IAW DRAWING 53FX2022. INSTALLED NEW INNER SKIN IAW SRM 51-30-2.Jul 9, 2010 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201007092441Skin · gougedMCD SURROUND INNER SKIN GOUGED STA 460 STR 5L. REMOVED INNER SKIN BS 460-510 UPPER FWD IAW SRM 51-30-2. FABRICATED INNER SKIN FROM 2024 T3 .125" PO 90010048 DIM: 48" X 79" IAW DRAWING 53FX2022 REV C. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED FWD UPPER INJul 9, 2010 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR KNNA20100037Web · crackedDURING C-CHECK, ACCOMPLISHMENT OF AD 2005-05-29A NDT INSP REVEALED A CRACK AT THE FWD PRESSURE BULKHEAD STA 178, WL218-219, BL 1R.Jul 7, 2010 · N252TR · Boeing 737228 · Fuselage Main, BulkheadSDR DALA1018919005Spar Cap · damagedREF EA 09-471576-12, REV ORIGINAL ME05 OPN NR0 502 REPAIR (5) CRACKS OF 812, .0.750, 0.125, 1.00 LENGTH ON THE WING REAR SPAR LOWER CAP AFT VERTICAL LEG AT INBD ATTACH POINT_OF THE RT WING FLAP HINGE FITTING XRS=164. GAINED ACCESS IAW AMR 0957304 REV 2 AND DWGJul 4, 2010 · N905DE · Doug MD88 · Wing SparSDR DALA1018869005Support Fitting · damagedSCRATCHES ON RT MLG SUPPORT FITTING BEARING BORE. DAMAGE BLENDED OUT IAW EA 09-093855-03AD REV B, ME02 OPN 0203AND FOUND WITHIN LIMITS. BEARING BORE TREATED IAW SRM 51-10-3.Jun 29, 2010 · N905DE · Doug MD88 · Wing, Landing Gear Attach FittingsSDR DALA1018879005Support Fitting · corrodedPITTING CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE AT WALL AND AFT FACE. CORROSION BLENDED OUT IAW EA 09-093855-03, AD REV B, ME01, OPN 0103 AND FOUND WITHIN LIMITS IAW DWG 5935812. BUSHING BORE TREATED IAW SRM 51-10-3.Jun 29, 2010 · N905DE · Doug MD88 · Wing, Landing Gear Attach FittingsSDR DALA1018859005Door Frame · corrodedEXFOLIATION CORROSION ON LOWER DOORJAMB PAN OF C1. DOORJAMB WAS REPLACED IAW SRM'S 51-10-3 PAR 26, 53-05D FIG 804D, AND ERA 483910.Jun 22, 2010 · N905DE · Doug MD88 · Fuselage Main, StructureSDR DALA1014210995Longeron · crackedDURING HMV, MAIN CABIN LT AFT LAV STA 1338 L-7-L END FITTING IS CRACKED. REMOVED END FITTING, RECEIVED NEW FITTING PN 4913329-501, INSTALLED IAW SRM 51-30-5, 51-10-3 (DLM88101571)Jun 21, 2010 · N995DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR YYFA201000019Engine · overtempON TAKEOFF, LT ENGINE DID NOT REACH TO POWER, EGT REACHED 630 DEGRESS AT APPROX 94 PERCENT N1. REQUIRED N1 AT 1,000 FT AND 26 DEGRESS IS 97.1 PERCENT. BOTH PILOT'S SAW EXCESSIVE EGT AND ABORTED TAKEOFF AT APPROX 30-40 KTS.Jun 18, 2010 · N836RA · Doug MD83 · Engine (Turbine/Turboprop)SDR TSAA1026012Circuit Breaker · failedDURING CLIMB, THE CREW NOTED THE NR 2 TRANSFER BUS CIRCUIT BREAKER POPPED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX R & R THE NR 2 TRANSFER BUS CIRCUIT BREAKER (C821) AND OPERATIONALLY CHECKED SATISFACTJun 15, 2010 · N826AL · Boeing 737282C · DC Power Distribution SystemSDR FDEA201006101937Web · crackedAFT AIRSTAIRS RT LOWER TORQUE BOX WEB AT BS 1243 HAS UPPER LIGHTNING HOLE CRACKED. CUTOUT DAMAGED AREA APPROX DIM: 5/8" X 3/8", FABRICATED REPAIR DOUBLER FROM 7075T6 .032 APPROX DIM: 4" X 1 1/4" & INSTALLED REPAIR DOUBLER AT BS 1243 RH LOWER TORQUE WEB IJun 10, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006091917Skin · corrodedCORROSION IN SKIN BS 600, STR 28L. CUTOUT DAMAGED AREA APPROX DIM: 2.5" X 1" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .100 APPROX DIM: 8 3/4" X 12 5/8". INSTALLED REPAIR DOUBLE AT BS 600 STR 28L IAW SRM 53-30-3 FIG 1, SRM 51-30-2, SRM 51-10-2, & SRM 51-10-6Jun 9, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR DALA1013310922Structure · damagedVERT STAB REMOVABLE L/E UPPER EDGE HOLES DAMAGED, REPAIRED IAW ERA 483240-14.Jun 9, 2010 · N922DL · Doug MD88 · Vertical StabilizerSDR XSK2010F00000Line · weakON A FLIGHT, 06/05/2010, WE EXPERIENCED A LT HYD SYS FAILURE AND SOON AFTER, APRATIAL RT HYD SYS FAILURE. WERE IN A CLIMB TO FL260 AND PASSING ABOUT 16,000 FT WHEN THE INITIAL INDICATION OF A LT HYD SYS PRESSURE LOW WAS ANNUCIATED. THE LT HYD PRESSURE GAGE VJun 5, 2010 · N287KB · Doug DC987 · Hydraulic System, MainSDR FDEA201006031809Structure · crackedNR 7 SLAT T/E CHORD CRACKED AT INBD UP STOP. REMOVED NR 7 SLAT LOWER CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD USING BAC1514-1559, 2024-T3511, 113.7500", IAW SRM 57-50-2 FIG 2 AND 51-30-5. INSTALLED LOWER CHORD IAW SRM 51-30-2.Jun 3, 2010 · N267FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006031810Angle · crackedRT WING INBD MID FLAP LOWER T/E CHORD ANGLE IS CRACKED, 2 PLACES, WBL 100. R & R DUE TO DELAMINATION ON SNRM NR N00544, WO NR00048343.Jun 3, 2010 · N267FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA201006031812Stringer · corrodedCORROSION ON STRINGER 29L, FROM BS 950B TO 950C. REMOVED FASTENERS IAW SRM 51-30-2. REMOVED CORROSION FROM STR 29L IAW SRM 51-10-6. UT INSPECTED AREA IAW NDTM 51-00-00, FIG 3 PART 4, ORIGINAL .150", REMAINING .136". FOUND MATERIAL LOSS OF .014" TO BE WITHJun 3, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006022027Fitting · damagedTAIL STAND FITTING AFT SIDE OF 1183 BULKHEAD, LBL19 HAS A DRILL START REPAIRED TAIL STAND FITTING AFT SIDE OF BS 1183 BULKHEAD, LBL19 IAW EA 7-5310- 135541 ( FUSELAGE AD 98-11-03 R1, BS1183 AFT PRESSURE BULKHEAD VERTICAL BEAM WITH INSUFFICIENT FASTENER SPACINJun 2, 2010 · N268FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201006011758Stringer · crackedCRACK AFT END OF STRINGER 27L AT BS 740, AC DISTRIBUTION COMPARTMENT. CUT OUT DAMAGED SECTION OF STR 27L AT BS 740, 11.5" LONG IAW SRM, REV 103, 53-10-3 FIG 1. FABRICATED STRINGER USING BAC 1498-146, 7075-T6, 11.5" LONG AND SPLICE USING BAC1498-131, 7075-T6,Jun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006011764Fitting · corrodedCORROSION BS 740 FITTING EXTERIOR FUSELAGE KEELBEAM AREA LBL 10. REMOVED KEEL BEAM FITTING AT BS 740 LBL 10 IAW SRM 51-30-2 REV 103 AND FABRICATED FITTING FROM 70750 .190 DIM: 190" X 10 1/4' X 7" IAW DWG 69-43695 OF AND HEAT TREATED TO T6 CONDITION IAW FAS EJun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR FDEA201005311747Angle · crackedCRACKED ANGLE CHORD FALSE SPAR AT NR 8 SPOILER ACTUATOR ATTACH FITTING. CUT OUT DAMAGED SECTION OF WEB, 9.5" IAW DWG SR27-57-038, REV C. FABRICATED NEW DOUBLER USING 20245-T3, .050" X 12" X 9.7500" IAW DWG SR27-57-038, REV C. INSTALLED DOUBLER IAW DWG SR27May 31, 2010 · N267FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA201005281704Connector · defectiveCREW PERFORMED AN AIR TURN BACK TO MEM FOR AN UNSAFE INDICATION ON THE NR 3 L/E SLAT. WHEN CREW WENT FROM FLAPS 5 TO 2 THEY HAD AN UNSAFE INDICATION ON NR 3 L/E SLAT. WHEN CREW RETURNED TO FLAPS 5 THE UNSAFE INDICATION WENT AWAY. NR 3 LED UNSAFE WHEN RAISINMay 28, 2010 · N283FE · Boeing 727233 · Flight Control System WiringSDR FDEA201005281703Intercostal · crackedNR 1 CARGO DOORWAY FRAMES, BS 560, BETWEEN STR 23R AND 24R, CRACKED INTERCOSTAL. REMOVED INTERCOSTAL NR 1 CARGO DOOR WAY BS 560 STR 23R - 24R IAW SRM 51-30-2. FABRICATED NEW INTERCOSTAL USING 7075 O .063" PO 9009533 DIM 19.7500" X 6.2500" IAW MM 51-20-1 May 28, 2010 · N268FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR DALA1013420999Tab · damagedRT ELVATOR CONTROL TAB LIGHTENING STRIKE REPAIR ACCOMPLISHED IAW SRM 55-04 PAR 3A.May 25, 2010 · N999DN · Doug MD88 · Elevator, Tab StructureSDR FDEA201005221733Rib · crackedRIB CRACKED AT OTBD TRACK OF NR 6 SLAT REMOVED RIB IAW SRM 51-30-2. FABRICATED NEW RIB FROM 2024-0 .050" DIM 15" X 6" IAW SRM 51-20-1 AND 57-50-2. HEAT TREATED PART FROM 2024-0 TO 2024T4 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A INSTALLED RIB IAW SRM 51May 22, 2010 · N268FE · Boeing 727233 · Wing, Rib/BulkheadSDR FDEA201005201594Angle · crackedNR 8 SLAT LOWER T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED NR 8 SLAT LOWER T/E ANGLE IAW SRM REV 102, 51-30-2. FABRICATED NEW ANGLE USING BAC1514-1559, 2024 T3511 86 1/4" LONG IAW SRM 51-30-5 AND 57-50-2 FIG 2. INSTALLED NEW ANGLE IAW 51-30-2.May 20, 2010 · N268FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201005201595Angle · crackedNR 6 SLAT LOWER AFT T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED ACCESS PANELS NR 6 SLAT IAW SRM 51-30-2, FABRICATED NEW T/E ANGLE. MATERIAL USED BAC1514-1559 2024T3511 PO 20035137 DIM 9' 6" LONG IAW SRM 57-50-2 FIG 2, 51-30-5 TREATED AND PRIMED IAWMay 20, 2010 · N268FE · Boeing 727233 · Leading Edge DevicesSDR DALA1013440999Bushing · corrodedPITTING CORROSION ON LT GEAR SUPPORT FITTING BUSHING. LT MLG SUPPORT FITTING BUSHING BORE WAS MACHINED TO REMOVE CORROSION IAW EA 09-093855-03 AD 0109.May 19, 2010 · N999DN · Doug MD88 · Wing, Landing Gear Attach FittingsSDR DLM88101255Splice · wornREMOVABLE L/E OF VERTICAL SCREW ATTACH HOLES AND COUNTERSINKS WORN UPPER SPLICE REPAIRED ON ERA 482407-14, NR 128.May 19, 2010 · N936DL · Doug MD88 · Vertical StabilizerSDR DLM88101269Wire · brokenESCAPE PATH LIGHT INOP AT 31D. FOUND WIRE BROKEN AT PLUG ON LIGHT ASSY. REPLACED LIGHT ASSY.May 19, 2010 · N954DL · Doug MD88 · Light System WiringSDR DLM88101279Light · inoperativeMX FOUND THE ESCAPE PATH LIGHT AT SEAT 31D TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.May 19, 2010 · N954DL · Doug MD88 · Emergency LightingSDR FDEA201005171748Doubler · gougedGOUGES ON INNER DOUBLER BS 620, STR 16L. TRIMMED OUT DAMAGED AREA DIM. 1.75" X 1" IAW EA 7-5330-135544. FABRICATED FILLER FROM 2024T3 .125" DIM. 1.75" X 1" AND DOUBLER FROM 2024T3 .125" DIM. 4.75" X 3.75" IAW EA 7-5330-135544. INSTALLED REPAIR PARTS IAW SRM May 17, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR DALA1013450999Tab · damagedDAMAGED METALLIZED COAT ON RUDDER CONTROL TAB. METALLIZED COAT ON RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1AD PARA 23. (DLM88101533)May 17, 2010 · N999DN · Doug MD88 · Rudder, Tab StructureSDR DLM88101243Unknown · odorSTRONG BURNING RUBBER ODOR AT ALTITUDE (FL330) AT EMERGENCY EXIT ROWS OVER WINGS. RETURNED TO DEPARTURE, MX IN PROGRESS TROUBLESHOOTING ODOR IN CABIN.May 17, 2010 · N908DE · Doug MD88 · Air Distribution SystemSDR DLM88101248Indicator · stuckFLIGHT CREW ABORTED TAKE-OFF AT 60 KNOTS DUE TO NR 1. ENGINE EPR INDICATION STUCK. CREW TAXIED CLEAR OF RUNWAY, PLACED NR 1 EPR SYS ON MCO AND FLIGHT DEPARTED. MX LATER R & R THE EPR TRANSMITTER AND SNUBBER. THE MCO WAS REMOVED.May 17, 2010 · N946DL · Doug MD88 · Engine Pressure Ratio (EPR)SDR DLM88101272Ballast · failedRETURNED TO DEPARTURE DUE TO STRONG BURNING RUBBER ODOR AROUND EMERGENCY EXIT ROWS. ACFT WAS AT FL330, ODOR DISSIPATED ON DESCENT AND WAS GONE BY TOUCHDOWN. PERFORMED OPERATION 5088 (SIC TROUBLESHOOTING) ITEM 3 FOUND LIGHT BALLAST B6-53 BAD. R & R SAME. RMay 17, 2010 · N908DE · Doug MD88 · Passenger Compartment Lighting
Back to Pratt & Whitney JT8D series