Pratt & Whitney JT9D-7R4E1

Service difficulty reports · 127

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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 = 'JT9D7R4E1'
  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 FDEA201208092925Hinge Fitting · gougedRIGHT NLG AFT DOOR UPPER FWD HINGE FITTING HAS .2500" X .5" GOUGE FROM CONTACT WITH DOOR CONTROL ROD (ON AFT FACE OF HINGE FITTING) R & R RT NLG AFT DOOR UPPER FWD HINGE FITTING IAW SRM 51-72-10. REMOVED AND REINSTALLED FLOOR PANEL 122 PF IAW AMM 53-10-27-04.Aug 9, 2012 · N454FE · Airbus A310222 · Fuselage, Landing Gear Attach FittingsSDR FDEA201203100867Transmitter · crackedON TAKEOFF ROLL, NR 1 ENGING OVERLIMIT ON ECAM TOLD TO REDUCE POWER TO CLR WARNING LOW SPEED ABORT 85 KTS. OPENED RT FAN COWL IAW MM CH 71-13-00 AND FOUND N1 TACHOMETER TRANSMITTER CRACKED. REPLACED NR 1 ENGINE N1 TACHOMETER TRANSMITTER, REF MM 77-11-01-04Mar 10, 2012 · N419FE · Airbus A310222 · Engine RPM Indicating SystemSDR FDEA201202170603Line · looseAT FL 390, NR 2 ENGINE QUIT RESPONDING TO THROTTLE MOVEMENT. PARAMETERS WERE NORMAL BUT CLOSE TO IDLE POWER. DESCENDED TO FL 290, NORMAL OPERATION RETURNED PASSING FL 320. FLEW REST OF FLIGHT AT FL 300. TEMP AT FL 390 WAS -55C. SUMPED ALL FUEL TANKS, NOFeb 17, 2012 · N447FE · Airbus A310222 · Fuel Controlling SystemSDR FDEA201202080513Signal Cond Unit · malfunctionedON CLIMBOUT LOSS OF OIL PRESSURE NR 1 ENGINE ONLY OTHER ABNORMAL INDICATION WAS INCREASE IN NR 1 OIL QUANTITY TO FULL SCALE HIGH. FOLLOWED PROCEDURES SHUT ENGINE- DOWN AND RETURNED TO AIRPORT. TROUBLESHOT IAW ASM 79-30-00 SUSPECT OIL PRESSURE TRANSMITTER T58Feb 8, 2012 · N450FE · Airbus A310222 · Engine Oil QuantitySDR FDEA201112085220Oil System · low pressureYELLOW OIL PRESSURE LIGHT ILLUMINATED DURING TAKE OFF ROLL AT 110 KTS. ABORTED TAKE OFF, COMPLIED WITH QRH. RAN ENGINES AT POWER, OIL PRESSURE STAYED AT 52 PSI IN THE NORMAL RANGE IAW JRH. SUSPECTED COLD ENGINE OIL ON COLD SOAKED ENGINE THAT LAYED OVERNIGDec 8, 2011 · N455FE · Airbus A310222 · Engine Oil PressureSDR FDEA201110064343Hmu · failedON TAKEOFF, NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. R & R NR 2 ENGINE HMU IAW AMM 73-21-01-04. CHECKED GOOD. PERFORMED IDLE LEAK CHECK AND POWER TRIM RUN IAW MM 71-00-00-05 LEAK CHECKS GOOD AND POWER RUNUP CHECKS GOOD.Oct 6, 2011 · N455FE · Airbus A310222 · Fuel Control/Turbine EnginesSDR FDEA201109274156Wire Harness · damagedREJECTED T/O, SET BOTH ENGINES TO 40 PERCENT N1, TOGA'D AND ENGINE NR1 IMMEDIATELY POWERED UP AND ENGINE 2 STOPPED ACCELERATING AT 50 PERCENT N1. MADE 2ND ATTEMPT BUT REJECTED DUE TO ENGINE 2 WOULD NOT ACCELERATE ABOVE 50 PERCENT N1 EVEN WITH PILOT ATTEMPTED Sep 27, 2011 · N455FE · Airbus A310222 · Turbine Engine System WiringSDR FDEA201012294774Power Unit · malfunctionedFLAP SYSTEM 1&2 FAULTED AT FLAPS 0. CHECKED SFCC'S BOTH SHOW ASYMMETRY FAULTS. REMOVED FPPU AND NULLED R & R IAW MM 27-56-00-05. RESET FAULTS ON BOTH SFCC'S AND PERFORMED BITE TEST IAW MM 27-51-00-05-0, NO FAULTS OCCURED. RAN FLAPS FULL TRAVEL UP AND DOWDec 29, 2010 · N419FE · Airbus A310222 · Trailing Edge Flap Control SystemSDR FDEA201012174712Door Frame · gougedLT MLG DOOR TOP AFT INNER MATING SURFACE IS GOUGED. REMOVED GOUGE AND FOUND TO BE OUT OF LIMITS. MATERIAL LOSS 0.022 FROM 0.078., 0.056 MATERIAL REMAINING. FABBED DOUBLER IAW EA 6-5280-136728, " DOORS - LT MLG MAIN DOOR UPPER FRAME". ALODINED AND PRIMED IAWDec 17, 2010 · N455FE · Airbus A310222 · Fuselage Main, StructureSDR FDEA201012164698Engine · malfunctionedAFTER TOUCHDOWN, HAD A HARD TIME PULLING REVERSER LEVERS INTO REVERSE, GOT THEM INTO REVERSE. SPOILERS INITIALLY DEPLOYED, THEN GOT ECAM ALERT FOR GROUND SPOILERS NOT DEPLOYED. THEN WE HEARD A LOUD BANG AND A FLASH ON THE RT SIDE AND THE NR 2 ENG QUIT AS WE Dec 16, 2010 · N450FE · Airbus A310222 · Engine (Turbine/Turboprop)SDR FDEA201012094623Bracket · crackedBULK CARGO DOOR STAY BRACKET IS CRACKED AT FRAME 68, BEAM 3. ACQUIRED MATERIAL ID FOR NEW STAY BRACKET IAW SRM 52-34-00, PO 680480.1. FORMED NEW STAY IAW SRM 51-26-00. ALODINED NEW STAY IAW SRM 51-21-10, PARA 4, PG 6. PRIMED & PAINTED NEW STAY IAW SRM 51-23Dec 9, 2010 · N455FE · Airbus A310222 · Cargo/Baggage DoorsSDR FDEA201011304517Angle · crackedNR1 PYLON ACCESS PANEL 475 AL (STRINGER), RT SIDE, CTR SECTION OF PANEL "T" ANGLE IS CRACKED. REMOVED CRACKED FRAME AND FABBED NEW FRAME FROM 0.063, 2024-0, PO NR673099.1 IAW SRM 54-55-51, FIG 3. HEAT TREATED TO 2024-T3 IAW AMS 2770, REV "H". FIT AND DRINov 30, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201011294512Stop Fitting · crackedRT AFT PAX / CREW DOOR STOP FITTING IS CRACKED AT THE INBD LOWER FASTENER; LOWER AFT DOOR FRAME STOP FITTING IN THE DOOR CUTOUT. REPLACED RT AFT PAX DOOR STOP FITTING IAW SRM 51-72-10 AND SRM 51-40-21, PG 5-7.Nov 29, 2010 · N455FE · Airbus A310222 · Fuselage Main, StructureSDR FDEA201011164395Skin · damagedLT WING - INBD FLAP - T/E SKIN FOUND DAMAGED. DUE TO NON APPROVED EXISTING REPAIRS THE T/E HAD TO BE REPLACED.Nov 16, 2010 · N456FE · Airbus A310222 · Trailing Edge FlapsSDR FDEA201011154371Profile · misrepairedPREVIOUS REPAIR FOUND AT T/E PROFILE BETWEEN RIB13/15 NOT TO CONFORM WITH FAA APPROVED DATA. T/E WAS REPLACED IAW EA 6-5750-144066 INSTRUCTIONS.Nov 15, 2010 · N456FE · Airbus A310222 · Wing Miscellaneous StructureSDR FDEA201011154372Profile · misrepairedPREVIOUS REPAIR FOUND AT T/E PROFILE BTW RIB4/5 NOT TO CONFORM WITH FAA APPROVED DATA. T/E WAS REPLACED IAW EA 6-5750-144066 INSTRUCTIONS.Nov 15, 2010 · N456FE · Airbus A310222 · Wing Miscellaneous StructureSDR FDEA201011154373Profile · misrepairedPREVIOUS REPAIR FOUND AT T/E PROFILE BTW RIB11/15 NOT TO CONFORM WITH FAA APPROVED DATA. T/E WAS REPLACED IAW EA 6-5750-144066 INSTRUCTIONS.Nov 15, 2010 · N456FE · Airbus A310222 · Wing Miscellaneous StructureSDR FDEA201011154367Floor Support · crackedFWD PIT, AFT FLOOR SUPPORT, RT SIDE IS CRACKED BETWEEN FRAME 38.2 AND FRAME 39. REMOVED AND REPLACED AFT FLOOR SUPPORT, R/H SIDE AT FRAME 38.2 IAW SRM 51-40-21, PARA 5 AND 6.Nov 15, 2010 · N455FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR FDEA201011124320Skin · corrodedFWD CARGO COMPARTMENT DOOR - LOWER INTERNAL SKIN FOUND CORRODED. PANEL SKIN WAS REPLACED AS PER SRM 51-72-10.Nov 12, 2010 · N456FE · Airbus A310222 · Cargo/Baggage DoorsSDR FDEA201011124326Skin · damagedPREVIOUS REPAIR FOUND AT LT INBD FLAP LOWER SKIN BTW STGR 13 & REAR SPAR AND RIBS 12/14. NEW REPAIR PERFORMED IAW EA 6-5750-144069. REPAIR NR2.Nov 12, 2010 · N456FE · Airbus A310222 · Trailing Edge FlapsSDR FDEA201011124324Pressure Panel · corrodedFWD CARGO COMPARTMENT HORIZ PRESSURE DECK UPPER SURFACE AT FRAME 40/41 IS CORRODED AT THE SPLICE. REPAIRED PER FEDEX EA 6-5310-136722, TITLE " FUSELAGE - PRESSURIZED FLOOR BETWEEN FR 39 AND FR 40 AT Y-95.3". REMOVED AND RE-INSTALLED 1 EA. SUPPORT BRACKET Nov 12, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011104311Skin · crackedFWD CARGO DOOR - CRACK FOUND AT INNER PLATE AT LOWER AFT CORNER. INNER SKIN REPAIRED IAW 6-5230-144190.Nov 10, 2010 · N456FE · Airbus A310222 · Cargo/Baggage DoorsSDR FDEA201011104305Fitting · corrodedNR 2 ENG PYLON SPIGOT RECEPTICAL FITTING BALL JOINT FLANGE IS PITTED AT THE UPPER AND LOWER FLANGE PLATES INCLUDING THE BEARING BORE. COMPLIED WITH EA 6-5450-136723; " NACELLES / PYLON - SB A310-54-2020 - NR1 AND NR2 PYLON SPIGOT FITTING BORE CORROSION".Nov 10, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201011104306Fitting · corrodedNR1 ENGINE PYLON SPIGOT RECEPTICAL FITTING BALL JOINT FLANGE IS PITTED AT THE UPPER AND LOWER PLATES INCLUDING THE BEARING BORE. COMPLIED WITH EA 6-5450-136723; " NACELLES / PYLON - SB A310-54-2020 - NR 1 AND NR2 PYLON SPIGOT FITTING BORE CORROSION".Nov 10, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201011084286Transmitter · failedREJECTED TAKEOFF FOR ENGINE NR 2 HIGH OIL PRESSURE REPEAT WRITE UP REJECT APPROX 85KTS. REPLACED NR 2 ENG. OIL PRESSURE TRANSMITTER IAW MM 79-33-11-04. LEAK AND OPS CKS GOOD. RAN ENG IAW JRH AND OIL PSI WAS 56PSI AT IDLE. RAN AT 75%N2 AND PSI WAS 58PSI. OK FONov 8, 2010 · N419FE · Airbus A310222 · Engine Oil PressureSDR FDEA201011084277Floor Panel · dentedBULK CARGO COMPARTMENT FLOOR PANEL 162 HF TOP SURFACE IS DENTED AND CRUSHED. FABRICATED NEW FLOOR PANEL 162 HF IAW DWG 25-005, REV "H" AND DWG 25-011, REV "C".Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011084278Floorboard · tornFWD CARGO COMPARTMENT FLOORBOARD 132 QF IS TORN AND PUNCTURED. FABRICATED NEW FLOORBOARD 132 QF IAW DWG 25-005, REV "H".Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011084279Floorboard · damagedAFT CARGO FLOORBOARD 151 FF HAS A BROKEN CORNER. FABRICATED NEW FLOORBOARD 151 FF IAW DWG 25-005, REV "H".Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011084280Floorboard · damagedMAIN DECK FLOORBOARD BETWEEN FRAME 53 AND FRAME 54, LBL 78 AND LBL 98 IS BROKEN OFF AT THE AFT END. FABRICATED NEW FLOOR PANEL IAW DWG 25-005, REV "H".Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011084281Floorboard · damagedMAIN CABIN FLOORBOARD UPPER SKIN IS CRUSHED AND BROKEN FROM FRAME 60 TO FRAME 62, RBL 57 TO RBL 77. FABRICATED NEW FLOORBOARD 252 UF IAW DWG 25-005, REV "H".Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011054263Attach Fitting · corrodedLT MLG DOOR ACTUATOR ATTACH FITTING IS CORRODED. REMOVED WORN JACK FITTING REF SRM 51-40-21, PAPR 7. INSTALLED NEW JACK FITTING REF SRM 51-40-21, PAPR 7. ALODINED AND PRIMED TOP SKIN REF SRM 51-21-10. APPLIED TOP COAT REF SRM 51-21-11.Nov 5, 2010 · N455FE · Airbus A310222 · Fuselage Main, Attach FittingsSDR FDEA201011044252Skin · corrodedFUSELAGE INTERNAL STRUCTURE FWD CARGO COMPARTMENT AFT DOOR CUTOUT AT THE LOWER CORNER, THE SKIN IS CORRODED FROM FRAME 26 TO FRAME 27, STR 25R TO STR 26R.Nov 4, 2010 · N455FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR FDEA201011044253Support · crackedRT WING ALL SPEED AILERON ACTUATOR UPPER PANEL SUPPORT IS CRACKED ON THE OTBD SIDE. PARTIALLY REMOVED OTBD UPPER AILERON PANEL AND REMOVED CRACKED LANDING. INSTALLED NEW PANEL LANDING PN A5724275920300, PO 691739.5 AND RE-INSTALLED OTBD UPPER AILERON PANELNov 4, 2010 · N803FD · Airbus A310222 · Wing Miscellaneous StructureSDR FDEA201011024210Floor Panel · crackedMAIN CABIN FLOOR PANEL 232 SF IS CRACKED. FABRICATED NEW FLOOR PANEL 232 SF IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024211Floor Panel · crackedMAIN CABIN FLOOR PANEL 231 AH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 AH IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024212Floor Panel · crackedMAIN CABIN FLOOR PANEL 231 BH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 BH IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024213Floor Panel · crackedMAIN CABIN FLOOR PANEL 242 QJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 QJ IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024214Floor Panel · crackedMAIN CABIN FLOOR PANEL 242 UJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 UJ IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024217Floor Panel · crackedMAIN CABIN FLOOR PANEL 252 GF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 GF IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024218Floor Panel · crackedMAIN CABIN FLOOR PANEL 252 UH IS CRACKED. FABRICATED NEW FLOOR PANEL 252 UH IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024219Floor Panel · crackedMAIN CABIN FLOOR PANEL 252 BF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 BF IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201011024220Floor Panel · crackedMAIN CABIN FLOOR PANEL 232 YH IS CRACKED. FABRICATED NEW FLOOR PANEL 232 YH IAW DWG SRZ 25-005, REV "H".Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201010254161Crossbeam · damagedFWD CARGO COMPARTMENT - CROSSBEAM UPPER FLANGE AT FR25 DAMAGED BTW Y480 & Y- 480. CROSSBEAM WAS REPAIRED IAW SRM 53-10-15 FIG 207.Oct 25, 2010 · N456FE · Airbus A310222 · Fuselage Main, StructureSDR FDEA201010254162Crossbeam · damagedFWD CARGO COMPARTMENT - CROOSBEAM UPPER FLANGE AT FR36 DAMAGED BTW Y480 & Y- 480. CROSSBEAM WAS REPAIRED IAW SRM 53-10-15 FIGURE207.Oct 25, 2010 · N456FE · Airbus A310222 · Fuselage Main, StructureSDR FDEA201010254163Fitting · corrodedFITTING LOCATED AT L1 DOOR FOUND CORRODED. REPLACED BY A NEW ONE.Oct 25, 2010 · N456FE · Airbus A310222 · Passenger/Crew DoorsSDR FDEA201010214132Frame · misrepairedFWD CARGO COMPARTEMENT - PREVIOUS REPAIR FOUND AT FR20A NOT IAW FAA APPROVED DATA. NEW REPAIR TO THE FR20A PERFORMED IAW EA 6-5310-144063.Oct 21, 2010 · N456FE · Airbus A310222 · Fuselage Main, FrameSDR FDEA201010144062Seat Track · corrodedSEAT TRACK Y954 FOUND CORRODED BTW FR18 & FR19. SEAT TRACK REPLACED BY A NEW ONE.Oct 14, 2010 · N456FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010144063Skin · dentedRT WING - SLAT NR1 L/E - PREVIOUS DENT FOUND AT RIB 4. EVALUATED AND FOUND TO BE CONFORM WITH EA 6-5710-50155. DENT WAS FILLED USING THE GUIDELINES OF SRM 51-73-10.Oct 14, 2010 · N456FE · Airbus A310222 · Leading Edge DevicesSDR FDEA201009303805Skin · misrepairedBULK CARGO DOOR - PREVIOUS REPAIR FOUND AT INTERNAL SKIN, LOCATED BTW FR67 & FR69 AND BTW BEAM1 & BEAM4, NOT CONFORM WITH SRM. NEW REPAIR WAS PERFORMED IAW SRM 52-30-00, FIG 206.Sep 30, 2010 · N456FE · Airbus A310222 · Cargo/Baggage DoorsSDR FDEA201009303806Skin · corrodedRIGHT THS TOP SKIN - CONNECTION PART AT THE INTERIOR OF THE SPAR BOX AT S11 FOUND CORRODED BTW RIB 3 & RIB 4. CONNECTION WAS REPLACED IAW 51-72-10 AFTER FABRICATION.Sep 30, 2010 · N456FE · Airbus A310222 · Horizontal Stabilizer, Plate/Skin
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