Pratt & Whitney JT8D-7B

Service difficulty reports · 753

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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 = 'JT8D7B'
  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 06FDEA0103Shear Tie · corrodedAFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BETWEEN STR. 28 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR 06FDEA0104Shear Tie · unknownAFT CARGO COMPARTMENT ON SHEAR TIE BETWEEN STR 30 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting StructureSDR ABXA060014Shear Tie · crackedSHEAR TIE DOUBLER CRACKED AT STA. 1019 BETWEEN LONGERON 13-14. REMOVED AND REPLACED DOUBLER IAW ABX DWG K05159.Dec 23, 2005 · N932AX · Doug DC933F · Fuselage Internal Mounting StructureSDR 05FDEA04402Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 25 LT AND 27 LT BS 990, ON IB FLANGE. REPAIRED FRAME PER SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04403Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 26 RT AND 23 RT BS, 1148 IN IB FLANGE. AFT CARGO COMPARTMENT FRAME AT BS 1148 BETWEEN STR 23R, AND 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04404Frame · dentedN00987 AFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 26 LT AND 27 LT BS 1148 ON IB FLANGE ** SD ** COMING.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04405Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 24 LT AND 27 LT BS 1010 ON IB FLANGE. REPAIRED PER 51-40-03 & 53-10-1.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04406Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR. 24 LT AND 27 LT BS 1030 ON IB FLANGE. REPAIRED IAW SRM 51-40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR 05FDEA04407Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BETWEEN STR 25 LT AND 27 LT BS 1050 ON IB FLANGE. REPAIRED DENTED FRAME BETWEEN STR 25LT AND 27LT, BS 1050 ON I/B FLANGE IAW SRM 51- 40-3.Dec 22, 2005 · N191FE · Boeing 727100 · Fuselage Main, FrameSDR ABXA060012Strap · crackedPYLON UPPER REAR SPAR STRAP BROKEN APART AT NR 2 PYLON. REMOVED AND REPLACED SPAR STRAP IAW SRM 51-30-1 AND 51-30-5.Dec 21, 2005 · N932AX · Doug DC933F · Nacelle/Pylon, Main FrameSDR ABXA060011Shelf · crackedCRACKED FLANGE ON RT AFT PYLON BULKHEAD GUSSET SHELF AT STA. 1038, LONGERON 15 RT. REMOVED AND REPLACED GUSSETT SHELF IAW SRM 51-30-2.Dec 20, 2005 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA050380Landing Gear · out of adjustAFTER TAKE-OFF WITH GEAR HANDLE UP, RT GEAR UNSAFE LIGHT ILLUMINATED ALONG WITH GEAR DOOR OPEN LIGHT. COMPLETED GEAR UPLATCH CHECK AND STILL HAD THE SAME INDICATIONS AS STATED ABOVE. RIGGED LT AND RT UPLATCHES, MAIN LANDING GEAR SEQUENCE PUSH PULL CABLES AND PDec 19, 2005 · N943AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA050318Battery Pack · dischargedDURING PREDEPARTURE CHECK FOUND COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. DEFERRED NR 47327 REMOVED AND REPLACED BATTERIES IN PACK IAW AMM.OPS CHECKED GOOD. DEFERRED IAW GMM. ITEM 2 A12 FOR BATTERY PACK REPLACEMENT WITHIN 3 FLIGHT DAYS. PLACARD INSTALLED, Dec 6, 2005 · N909AX · Doug DC932F · Emergency LightingSDR ABXA050291Battery · weakEMERGENCY COCKPIT LIGHTING WAS INOPERATIVE. REPLACED EMERGENCY COCKPIT LIGHTING BATTERIES IAW AMM 33.53.00.8. OPS CHECKED GOOD.Nov 29, 2005 · N937AX · Doug DC931 · Emergency LightingSDR 0501649997Seal · leakingON DESCENT, WITH ENGINES BROUGHT TO FLIGHT IDLE, THE CABIN WOULD CLIMB. ALTERING ENGINE THRUST WOULD NOT CORRECT CABIN CLIMB. CREW DECLARED AN EMERGENCY AND BEGAN AN IMMEDIATE DESCENT TO 10,000 FEET. NO MENTION OF COM PROCEDURES BUT CABIN PRESSURE CONTROL WAS Nov 26, 2005 · N8933E · Doug DC931 · Fixed Inner DoorsSDR 05FDEA03489Intercostal · crackedN01148 CRACK BS 660 STR 2L UPPER INTERCOSTAL EXTENSION. [OPEN]Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 05FDEA03490Floorbeam · corrodedBS 480 FLOORBEAM UPPER CHORD CORRODED AT RBL 48, WL 208. [OPEN]Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 05FDEA03491Skin · crackedCRACK IN FUSELAGE OUTER SKIN STA 591 STR 15R FWD UPPER CORNER OF WING L/E ILLUMINATION LIGHT CUT OUT. REPAIRED PER FED EX EA 7-5330-95384.Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR ABXA050259Roller · out of adjustON TAKEOFF, RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR HANDLE PLACED IN UP POSITION. GREEN SAFE LIGHT WAS NOT ILLUMINATED. AC FELT LIKE GEAR WAS UP. RECYCLED GEAR DOWN (SHOWED NORMAL INDICATION) THEN BACK UP AND GEAR UNSAFE LIGHT WENT OUT. DEFERREDOct 25, 2005 · N928AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA050244Engine · defectiveNR 1 ENGINE HIGH OIL TEMP. LEFT ENGINE SHUTDOWN AT FLT LEVEL 310 DUE TO OIL TEMP IN THE RED ZONE. INITIALLY TEMP WAS AT TOP OF YELLOW BAND, THEN WENT TO RED, THEN PEGGED ON SHUTDOWN. REMOVED AND REPLACED LEFT ENGINE IAW ABX JOB CARD 90900010.Oct 3, 2005 · N986AX · Doug DC932 · Turbine Engine Oil SystemSDR NACA20050023Wire · damagedENGINE NR 1, NR 2 & 3 FUEL FLOW INDICATORS READ ZERO AT TAKEOFF. REMOVED CONNECTOR FROM PREVIOUSLY DEFERRED NR 3 ENGINE FUEL FLOW TRANSMITTER AND NR 1 & NR 2 ENGINE FUEL INDICATIONS OP CHECKED GOOD ON GROUND RUN. THE FUEL FLOW POWER SUPPLY WAS REPLACED WITH Oct 3, 2005 · N792A · Boeing 72722C · Engine Fuel System WiringSDR GAIA05024OPSkin · crackedNO FLIGHT; DURING INSPECTION A SMALL CRACK WAS FOUND ON THE L1 DOOR UPPER AFT BEARING WHICH CAUSED THE DOOR FRAME TO CRACK. REMOVED AND REPLACED L1 DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (K)Sep 12, 2005 · N180AX · Boeing 727222 · Passenger/Crew DoorsSDR VGC2005F00002Engine · flamed outCREW REPORTED NR3 ENG WHILE IN FLIGHT AT FL320, SUSPECTED FUEL ICING (FUEL ICE LIGHT FLICKERING). PERFORMED PROCEDURES AS REQUIRED. AFTER TURNING FUEL HEAT ON 10 SECONDS LATER, NR3 ENGINE FLAMED OUT. CREW PERFORMED ABNORMAL CHECKLIST, RE-STARTED ENGINE. ALSep 1, 2005 · N261FL · Boeing 72725C · Engine (Turbine/Turboprop)SDR ABXA050182Panel · debondedLT WING OB UPPER TRAILING EDGE PANEL HAD SKIN DAMAGE AT STA. XRS 516. SKIN DEBONDED AND ROLLED BACK FROM THE LEADING EDGE PANEL. DAMAGED AREA MEASURED 6 INCHES LONG BY 18 INCHES WIDE. DEFERRED: NR 45199. TEMP REPAIRED IAW REA D957-52280. CLEARED: DI NR 45199.Aug 3, 2005 · N933AX · Doug DC933F · Wing, Plate/SkinSDR NACA20050018Indication Sys · inoperativeNR 2 ENGINE FUEL FLOW INDICATION INOPERATIVE. ENGINE SLOW TO ACCELERATE. FUEL FLOW INDICATION DEFERRED IAW MEL 73-7. PERFORMED ACCELERATION CHECK, FOUND TO BE WITHIN LIMITATIONS.Aug 2, 2005 · N792A · Boeing 72722C · Fuel Flow IndicatingSDR 05FDEA02087Compressor · stalledDURING T/O THROTTLE UP THE NR 3 ENG HAD A COMPRESSOR S TALL . RAN NR 3 ENG UP INDIVIDUALY AND AT A VERY LOW EPR NR 3 EXPERIENCED ANOTHER COMPRESSOR STALL. WINDS CALM. INSP INLET & EXH AREA. ALL NORMAL CKED FOR BLEED VALVE OPERATION, NORMAL, HEARD ALL 3 CJul 25, 2005 · N194FE · Boeing 727100 · Turbine Engine Compressor SectionSDR XNA01244Tube · crackedENGINE FIRE WARNING NR 2 ENGINE PERFORMED ALL REQUESTED CHECKLIST RETURN TO AIRPORT AS REQUEST. REMOVED AND REPLACED FUEL DE-ICING CRACKED TUBE ASSY IAW MM 73-14-00. OPS CK OK IAW MM 73-10-00. (ORIG/CLOSED)Jul 6, 2005 · N793A · Boeing 727227 · Engine Fuel PumpSDR CA050602001Ring · leaking(CAN) AFTER DEPARTING YOW FOR YFB THE CREW OBSERVED AN 'A' HYD. SYSTEM FLUID LOSS CONDITION WITH 2.5 GAL.INDICATED CLIMBING THROUGH FL190. THE AIRCRAFT WAS REROUTED TO POINT OF DEPARTURE AND FUEL WAS DUMPEDPRIOR TO THE LANDING AT YOW. POST ARRIVAL INVESTIGATIOJun 1, 2005 · Boeing 72744C · Trailing Edge Flap ActuatorSDR NACA20050012Linkage · looseNR 2 ENGINE WENT TO FULL POWER UPON TAXI-OUT. SECURED ENGINE AND RETURNED TO RAMP. FOUND THRUST REVERSER LINKAGE LOOSE, (NUT MISSING AT AFT END), AT CROSSOVER TUBE ON RIGHT SIDE OF ENGINE. SECURED LEVER ROD END WITH NEW HARDWARE (NO RIGGING CHANGE). CHECKEApr 23, 2005 · N792A · Boeing 72722C · Engine Thrust ReverserSDR NACA20050010Pump · leakingLOSS OF "A" SYS HYDRAULIC QUANTITY UPON GEAR RETRACTION AT TAKEOFF. REPLACED NR 2 A-SYSTEM HYDRAULIC PUMP. LEAK AND OP CHECK GOOD.Apr 11, 2005 · N792A · Boeing 72722C · Hydraulic Pump (Electric/Engine), MainSDR GAIA05014STSkin · delaminatedDURING A-CHECK, NO FLIGHT, FWA: FOUND LT IB MID-FLAP OB T/E MISSING 6 INCHES OF SKIN. REMOVED AND REPLACED LT IB MID-FLAP AND AFT FLAPS ASSY. OPS CHECKED NORMAL IAW MM 27-51. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200506017) (K)Mar 19, 2005 · N1269Y · Boeing 727243 · Trailing Edge FlapsSDR ABXA050030Tube · brokenNR 1 ENGINE FLAME-OUT DURING CLIMB AT 7,000 FT. OIL PRESSURE STAYED ABOVE 10 PSI FOR APPROXIMATELY 20 MINUTES DURING WINDMILLING AFTER FLAME-OUT. AIR TURNBACK TO ILN. ACCOMPLISHED TROUBLESHOOTING PER P&W MM FOR FLAME-OUT, INSPECTED INLET AND EXHAUST AREAS. Feb 17, 2005 · N937AX · Doug DC931 · Turbine Engine Oil SystemSDR C7WA200400074Engine · damagedNR 3 THROTTLE VIBRATION FELT INFLIGHT ALL OTHER ENGINE INSTRUMENT AND INDICATIONS NORMAL, REF LOGPAGE NR 21307. C1, C2, AND C3 DAMAGE FOUND, NR 3 ENGINE REPLACED, S/N OF INSTALLED ENGINE IS 654920. (M)Jan 11, 2005 · N511PE · Boeing 727232 · Engine (Turbine/Turboprop)SDR GAIA04176OPGcu · malfunctionedDURING APPROACH, LOST ALL (REMAINING, NR 2 AND NR 3) GENERATORS IN FLIGHT DURING APPROACH. RESET NR 2 GEN. NO VOLTAGE OR FREQS. ON NR 3, UNABLE TO RESET. FAULT PANEL INDICATED NR 3 SYSTEM UNDER VOLTAGE. LANDING WAS MADE WITHOUT INCIDENT. SWAPPED NR 3 GCU Dec 7, 2004 · N252US · Boeing 727251 · AC RegulatorSDR C7WA200400068Pressure Switch · inoperativeNR 3 ENGINE START VALVE LIGHT CAME ON DURING FLIGHT. FOUND NR 3 ENGINE START VALVE PRESSURE SWITCH INOPERATIVE. REMOVED AND REPLACED PRESSURE SWITCH IAW MM.Nov 11, 2004 · N7638U · Boeing 727222 · Engine Start Valves/ControlsSDR ABXA040368Pump · defectiveRIGHT ENGINE FLAMED OUT ON SHORT FINAL TO ILN, SPEED 135 KT, ALT 2100. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP IAW DC-9 MM 73-10-01-2. REMOVED AND REPLACED NR 2 ENGINE FCU IAW DC-9 MM 73-20-01-2.Nov 2, 2004 · N923AX · Doug DC931 · Engine Fuel PumpSDR 04FDEA02959Engine · overtempPDIS 192 79-10 0009533 20OCT04 MEM OPEN U LOGPAGES: 00949069 ENG NR 2 AND NR 3 OIL TEMPS BOTH IN THE YELLOW BAND AND OCCASSIONALLY SPIKING INTO THE RED DURING CLIMBOUT BOTH ENGINE HAD TO BE KEPT ABOVE IDLE TO MAINTAIN LOWER TEMPS.Oct 20, 2004 · N192FE · Boeing 727100 · Engine (Turbine/Turboprop)SDR C7WA200400052Skin · crackedNR 3 RT COCKPIT WINDOW UPPER SKIN (EXTERIOR) HAS AN APPROXIMATELY 1 INCH CRACK. INSTALLED EXTERNAL SKIN REPAIR ON RT NR 3 WINDOW UPPER SKIN. REMOVED DAMAGED SKIN PORTION. SKIN TRIM OUT 4.00 X 5.00. FABRICATED AND INSTALLED REPAIR FILLER PLATE FROM 2024-T3 Oct 11, 2004 · N7635U · Boeing 727222 · Fuselage Main, Plate/SkinSDR C7WA200400053Floorbeam · corrodedFLOORBEAM AT BS 660 RBL 45.50 HAS LIGHT CORROSION. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 660, RBL 45.50. REMOVED DAMAGED CHORD PORTION, FINAL TRIM OUT WAS 2.00 INCH. FABRICATED REPAIR SECTION FROM ALUM 7075-0 X 0.090 INCH X 16 INCHES. HEAT TREATED TO TOct 11, 2004 · N7635U · Boeing 727222 · Fuselage Main, Floor BeamSDR C7WA200400054Beam · corrodedBULKHEAD STA 1183 HAS A 6 INCH CRACK IN THE VERTICAL BEAM AT LBL 24.5, WL 250. INSTALLED INTERNAL REPAIR ON DAMAGED VERTICAL BEAM AT BS 1183 AT LBL 24.50, WL 250. DRILLED STOP HOLE .250. REPAIR CHANNEL 65C33556-45 AND SHIMS INSTALLED IAW SB. REPAIR PARTS AOct 11, 2004 · N7635U · Boeing 727222 · Fuselage Main, BulkheadSDR C7WA200400055Shear Tie · crackedSHEAR TIE CRACKED AT FRAME STA 930 BETWEEN STRINGER 13 RT AND STRINGER 14 RT. INSTALLED INTERNAL REPAIR ON SHEAR TIE AT BS 930 BETWEEN STRINGER 13 RT AND 14 RT. DAMAGED SHEAR TIE REMOVED. REPAIR PART FABRICATED FROM 7075-T6, X .063. REPAIR PARTS AND BARE EOct 11, 2004 · N7635U · Boeing 727222 · Fuselage Main, StructureSDR C7WA200400056Floorbeam · corrodedTRAVERSE FLOORBEAM STA 720 HAS CORROSION BETWEEN BL0 AND LBL 24.5. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 720A, BETWEEN BL0.0 AND LBL 24.5. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DIMENSION WAS 6.00 INCH X 2.00 INCH. REPAIR SECTION FABROct 11, 2004 · N7635U · Boeing 727222 · Fuselage Main, Floor BeamSDR C7WA200400057Floorbeam · corrodedFLOOR TRAVERSE BEAM AT STA 600 HAS LIGHT CORROSION BETWEEN BL0 AND RBL 24.5 AND BETWEEN LBL 45.5 AND LBL50. INSTALLED INTERNAL FLOORBEAM REPAIR ON DAMAGE LOCATED AT BS 600 BETWEEN BL0 AND LBL 24.50. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DIOct 11, 2004 · N7635U · Boeing 727222 · Fuselage Main, Floor BeamSDR C7WA200400059Structure · damagedRT HORIZONTAL STABILIZER BALANCE PANELS NR 2, NR 3, AND NR 4 CAVITIES T/E LOWER BEAM RUB BLOCKS ADJUSTMENT SCREW SAFETY WIRE HOLES CRACKED. INSTALLED SPLICE REPAIR ON RT HORIZONTAL STABILIZER T/E BEAM BALANCE PANELS CAVITIES NR 2, NR 3, AND NR 4. DAMAGED CHOOct 11, 2004 · N7635U · Boeing 727222 · Horizontal Stabilizer, Spar/RibSDR C7WA200400060Keelbeam · corrodedAFT CARGO COMPARTMENT, STA 1007 RT KEELBEAM CHORD HAS CORROSION. INSTALLED INTERNAL SPLICE REPAIR ON RT HEELBEAM CHORD SECTION BETWEEN BS 980 AND BS 1007. DAMAGED KEELBEAM CHORD SECTION REMOVED. NEW KEELBEAM CHORD SECTION FABRICATED IAW SAMPLE AND MFG DWG 6Oct 11, 2004 · N7635U · Boeing 727222 · Fuselage Main, KeelSDR C7WA200400061Flap Track · corrodedRT WING IB FLAP OB TRACK AFT MOUNT PAD HAS CORROSION. RT WING IB FLAP OB. TRACK NR 6 PN 65192493, CORROSION ON AFT MOUNT PAD REMOVED. MATERIAL REMOVED WAS 0.020. REPAIR ACOMPLISHED IAW EO.Oct 11, 2004 · N7635U · Boeing 727222 · Trailing Edge FlapsSDR C7WA200400040Duct · brokenAIR RETURN, INTERMITTENT FIRE WARNING LIGHT ON NR 2 ENGINE AFTER TAKEOFF. FOUND NR 2 ENGINE Y-DUCT BROKEN. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE DUCT.Oct 7, 2004 · N902PG · Boeing 727200 · Engine Anti-Icing SystemSDR Y2PA04023Ground Wire · brokenNO GEAR INDICATION ON LT MAIN GEAR, EITHER RED OR GREEN. CREW DECLARED AN EMERGENCY AND DIVERTED. CREW FOLLOWED COM PROCEDURES WITH NO HELP. LT GEAR INDICATION DOES NOT TEST (RED AND GREEN LIGHTS INOPERATIVE). AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC SESep 23, 2004 · N194US · Doug DC915F · Landing Gear System WiringSDR NACA20040039Switch · out of adjustMAIN CARGO DOOR UNLOCKED LIGHT CAME ON IN FLIGHT. VERIFIED MAIN CARGO DOOR CLOSED AND LOCKED. DEFERRED LIGHT ASSEMBLY. REPLACED LATCH PIN ROD ACTUATOR CHECK VALVE, INSPECTED ALL WARNING SWITCHES AND WIRING WITH NO DEFECTS FOUND. TESTED PER FED-EX MM 52-70Sep 21, 2004 · N992AJ · Boeing 72723 · Door Warning SystemSDR ABXA040337Fitting · crackedEND FITTING ANGLES ON AFT SIDE OF STA. 604, BUTT LINE 0, ARE CRACKED AND CORRODED. REMOVED AND REPLACED END FITTING ANGLES ON AFT SIDE OF STA. 604, BUTT LINE 0 IAW SRM 51-30-5. PN: 3924029-2N AND 3924029-1N.Sep 21, 2004 · N902AX · Doug DC932 · Fuselage Main, Attach Fittings
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