# Service difficulty reports: Pratt & Whitney JT9D-7R4E1

A list on [Pratt & Whitney JT9D-7R4E1](https://openairdocs.org/engine/pratt-whitney-jt9d-7r4e1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 127 reports

- [SDR FDEA201208092925](https://openairdocs.org/sdr/FDEA201208092925.md): Hinge Fitting · gouged · Aug 9, 2012 · N454FE · Airbus A310222 · Fuselage, Landing Gear Attach Fittings
  > RIGHT 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.
- [SDR FDEA201203100867](https://openairdocs.org/sdr/FDEA201203100867.md): Transmitter · cracked · Mar 10, 2012 · N419FE · Airbus A310222 · Engine RPM Indicating System
  > ON 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 77-11-01-04
- [SDR FDEA201202170603](https://openairdocs.org/sdr/FDEA201202170603.md): Line · loose · Feb 17, 2012 · N447FE · Airbus A310222 · Fuel Controlling System
  > AT 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, NO
- [SDR FDEA201202080513](https://openairdocs.org/sdr/FDEA201202080513.md): Signal Cond Unit · malfunctioned · Feb 8, 2012 · N450FE · Airbus A310222 · Engine Oil Quantity
  > ON 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 T58
- [SDR FDEA201112085220](https://openairdocs.org/sdr/FDEA201112085220.md): Oil System · low pressure · Dec 8, 2011 · N455FE · Airbus A310222 · Engine Oil Pressure
  > YELLOW 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 OVERNIG
- [SDR FDEA201110064343](https://openairdocs.org/sdr/FDEA201110064343.md): Hmu · failed · Oct 6, 2011 · N455FE · Airbus A310222 · Fuel Control/Turbine Engines
  > ON 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.
- [SDR FDEA201109274156](https://openairdocs.org/sdr/FDEA201109274156.md): Wire Harness · damaged · Sep 27, 2011 · N455FE · Airbus A310222 · Turbine Engine System Wiring
  > REJECTED 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
- [SDR FDEA201012294774](https://openairdocs.org/sdr/FDEA201012294774.md): Power Unit · malfunctioned · Dec 29, 2010 · N419FE · Airbus A310222 · Trailing Edge Flap Control System
  > FLAP 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 DOW
- [SDR FDEA201012174712](https://openairdocs.org/sdr/FDEA201012174712.md): Door Frame · gouged · Dec 17, 2010 · N455FE · Airbus A310222 · Fuselage Main, Structure
  > LT 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 IAW
- [SDR FDEA201012164698](https://openairdocs.org/sdr/FDEA201012164698.md): Engine · malfunctioned · Dec 16, 2010 · N450FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > AFTER 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
- [SDR FDEA201012094623](https://openairdocs.org/sdr/FDEA201012094623.md): Bracket · cracked · Dec 9, 2010 · N455FE · Airbus A310222 · Cargo/Baggage Doors
  > BULK 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 51-23
- [SDR FDEA201011304517](https://openairdocs.org/sdr/FDEA201011304517.md): Angle · cracked · Nov 30, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous Structure
  > NR1 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 DRI
- [SDR FDEA201011294512](https://openairdocs.org/sdr/FDEA201011294512.md): Stop Fitting · cracked · Nov 29, 2010 · N455FE · Airbus A310222 · Fuselage Main, Structure
  > RT 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.
- [SDR FDEA201011164395](https://openairdocs.org/sdr/FDEA201011164395.md): Skin · damaged · Nov 16, 2010 · N456FE · Airbus A310222 · Trailing Edge Flaps
  > LT WING - INBD FLAP - T/E SKIN FOUND DAMAGED. DUE TO NON APPROVED EXISTING REPAIRS THE T/E HAD TO BE REPLACED.
- [SDR FDEA201011154371](https://openairdocs.org/sdr/FDEA201011154371.md): Profile · misrepaired · Nov 15, 2010 · N456FE · Airbus A310222 · Wing Miscellaneous Structure
  > PREVIOUS 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.
- [SDR FDEA201011154372](https://openairdocs.org/sdr/FDEA201011154372.md): Profile · misrepaired · Nov 15, 2010 · N456FE · Airbus A310222 · Wing Miscellaneous Structure
  > PREVIOUS 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.
- [SDR FDEA201011154373](https://openairdocs.org/sdr/FDEA201011154373.md): Profile · misrepaired · Nov 15, 2010 · N456FE · Airbus A310222 · Wing Miscellaneous Structure
  > PREVIOUS 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.
- [SDR FDEA201011154367](https://openairdocs.org/sdr/FDEA201011154367.md): Floor Support · cracked · Nov 15, 2010 · N455FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > FWD 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.
- [SDR FDEA201011124320](https://openairdocs.org/sdr/FDEA201011124320.md): Skin · corroded · Nov 12, 2010 · N456FE · Airbus A310222 · Cargo/Baggage Doors
  > FWD CARGO COMPARTMENT DOOR - LOWER INTERNAL SKIN FOUND CORRODED. PANEL SKIN WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA201011124326](https://openairdocs.org/sdr/FDEA201011124326.md): Skin · damaged · Nov 12, 2010 · N456FE · Airbus A310222 · Trailing Edge Flaps
  > PREVIOUS 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.
- [SDR FDEA201011124324](https://openairdocs.org/sdr/FDEA201011124324.md): Pressure Panel · corroded · Nov 12, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > FWD 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
- [SDR FDEA201011104311](https://openairdocs.org/sdr/FDEA201011104311.md): Skin · cracked · Nov 10, 2010 · N456FE · Airbus A310222 · Cargo/Baggage Doors
  > FWD CARGO DOOR - CRACK FOUND AT INNER PLATE AT LOWER AFT CORNER. INNER SKIN REPAIRED IAW 6-5230-144190.
- [SDR FDEA201011104305](https://openairdocs.org/sdr/FDEA201011104305.md): Fitting · corroded · Nov 10, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous Structure
  > NR 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".
- [SDR FDEA201011104306](https://openairdocs.org/sdr/FDEA201011104306.md): Fitting · corroded · Nov 10, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous Structure
  > NR1 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".
- [SDR FDEA201011084286](https://openairdocs.org/sdr/FDEA201011084286.md): Transmitter · failed · Nov 8, 2010 · N419FE · Airbus A310222 · Engine Oil Pressure
  > REJECTED 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 FO
- [SDR FDEA201011084277](https://openairdocs.org/sdr/FDEA201011084277.md): Floor Panel · dented · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > BULK 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".
- [SDR FDEA201011084278](https://openairdocs.org/sdr/FDEA201011084278.md): Floorboard · torn · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOORBOARD 132 QF IS TORN AND PUNCTURED. FABRICATED NEW FLOORBOARD 132 QF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084279](https://openairdocs.org/sdr/FDEA201011084279.md): Floorboard · damaged · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > AFT CARGO FLOORBOARD 151 FF HAS A BROKEN CORNER. FABRICATED NEW FLOORBOARD 151 FF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084280](https://openairdocs.org/sdr/FDEA201011084280.md): Floorboard · damaged · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN 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".
- [SDR FDEA201011084281](https://openairdocs.org/sdr/FDEA201011084281.md): Floorboard · damaged · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN 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".
- [SDR FDEA201011054263](https://openairdocs.org/sdr/FDEA201011054263.md): Attach Fitting · corroded · Nov 5, 2010 · N455FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > LT 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.
- [SDR FDEA201011044252](https://openairdocs.org/sdr/FDEA201011044252.md): Skin · corroded · Nov 4, 2010 · N455FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FUSELAGE 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.
- [SDR FDEA201011044253](https://openairdocs.org/sdr/FDEA201011044253.md): Support · cracked · Nov 4, 2010 · N803FD · Airbus A310222 · Wing Miscellaneous Structure
  > RT 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 PANEL
- [SDR FDEA201011024210](https://openairdocs.org/sdr/FDEA201011024210.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 232 SF IS CRACKED. FABRICATED NEW FLOOR PANEL 232 SF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024211](https://openairdocs.org/sdr/FDEA201011024211.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231 AH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 AH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024212](https://openairdocs.org/sdr/FDEA201011024212.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231 BH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 BH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024213](https://openairdocs.org/sdr/FDEA201011024213.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242 QJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 QJ IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024214](https://openairdocs.org/sdr/FDEA201011024214.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242 UJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 UJ IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024217](https://openairdocs.org/sdr/FDEA201011024217.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 GF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 GF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024218](https://openairdocs.org/sdr/FDEA201011024218.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 UH IS CRACKED. FABRICATED NEW FLOOR PANEL 252 UH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024219](https://openairdocs.org/sdr/FDEA201011024219.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 BF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 BF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024220](https://openairdocs.org/sdr/FDEA201011024220.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 232 YH IS CRACKED. FABRICATED NEW FLOOR PANEL 232 YH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201010254161](https://openairdocs.org/sdr/FDEA201010254161.md): Crossbeam · damaged · Oct 25, 2010 · N456FE · Airbus A310222 · Fuselage Main, Structure
  > FWD CARGO COMPARTMENT - CROSSBEAM UPPER FLANGE AT FR25 DAMAGED BTW Y480 & Y- 480. CROSSBEAM WAS REPAIRED IAW SRM 53-10-15 FIG 207.
- [SDR FDEA201010254162](https://openairdocs.org/sdr/FDEA201010254162.md): Crossbeam · damaged · Oct 25, 2010 · N456FE · Airbus A310222 · Fuselage Main, Structure
  > FWD CARGO COMPARTMENT - CROOSBEAM UPPER FLANGE AT FR36 DAMAGED BTW Y480 & Y- 480. CROSSBEAM WAS REPAIRED IAW SRM 53-10-15 FIGURE207.
- [SDR FDEA201010254163](https://openairdocs.org/sdr/FDEA201010254163.md): Fitting · corroded · Oct 25, 2010 · N456FE · Airbus A310222 · Passenger/Crew Doors
  > FITTING LOCATED AT L1 DOOR FOUND CORRODED. REPLACED BY A NEW ONE.
- [SDR FDEA201010214132](https://openairdocs.org/sdr/FDEA201010214132.md): Frame · misrepaired · Oct 21, 2010 · N456FE · Airbus A310222 · Fuselage Main, Frame
  > FWD CARGO COMPARTEMENT - PREVIOUS REPAIR FOUND AT FR20A NOT IAW FAA APPROVED DATA. NEW REPAIR TO THE FR20A PERFORMED IAW EA 6-5310-144063.
- [SDR FDEA201010144062](https://openairdocs.org/sdr/FDEA201010144062.md): Seat Track · corroded · Oct 14, 2010 · N456FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK Y954 FOUND CORRODED BTW FR18 & FR19. SEAT TRACK REPLACED BY A NEW ONE.
- [SDR FDEA201010144063](https://openairdocs.org/sdr/FDEA201010144063.md): Skin · dented · Oct 14, 2010 · N456FE · Airbus A310222 · Leading Edge Devices
  > RT 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.
- [SDR FDEA201009303805](https://openairdocs.org/sdr/FDEA201009303805.md): Skin · misrepaired · Sep 30, 2010 · N456FE · Airbus A310222 · Cargo/Baggage Doors
  > BULK 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.
- [SDR FDEA201009303806](https://openairdocs.org/sdr/FDEA201009303806.md): Skin · corroded · Sep 30, 2010 · N456FE · Airbus A310222 · Horizontal Stabilizer, Plate/Skin
  > RIGHT 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.

Next page: https://openairdocs.org/engine/pratt-whitney-jt9d-7r4e1/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt9d-7r4e1/reports

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