# Service difficulty reports: Pratt & Whitney PW4152

A list on [Pratt & Whitney PW4152](https://openairdocs.org/engine/pratt-whitney-pw4152.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 145 reports

- [SDR FDEA201512284090](https://openairdocs.org/sdr/FDEA201512284090.md): Engine · power loss · Dec 28, 2015 · N808FD · Airbus A310324 · Engine (Turbine/Turboprop)
  > DURING DESCENT BELOW PROFILE THRUST WAS APPROX 75 - 77% N1. AT PROFILE THROTTLES REDUCED TO IDLE & APPROX 60% N1, A THUMPING SOUND WAS HEARD & FELT. SUSPECT COMPRESSOR STALL. ALTITUDE 30000 FT SPEED 0.8. NO ABNORMAL ENG INDICATIONS. SUSPECT ENG NR 2.
- [SDR FDEA201509172894](https://openairdocs.org/sdr/FDEA201509172894.md): Switch · failed · Sep 17, 2015 · N810FD · Airbus A310324 · Engine Thrust Reverser
  > DURING TAKEOFF ROLL, RECEIVED A MOMENTARY NR 2 THRUST REVERSER UNLOCKED ALERT & INSTRUMENT CLUSTER TOP LIGHT. LIGHT EXTINGUISHED & TAKEOFF WAS CONTINUED. AFTER TAKEOFF & WHEELS UP, THE ALERT CAME BACK ON. NO ADVERSE CONTROL WAS NOTICED. COMPLIED WITH ECAM.
- [SDR FDEA201405211114](https://openairdocs.org/sdr/FDEA201405211114.md): Engine · stalled · May 21, 2014 · N811FD · Airbus A310324 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE HAD A SUSPECTED STALL ON ROLLOUT. TOWER REPORTED LT ENGINE ON FIRE. STOWED THRUST REVERSERS BY 60 KIAS & STOPPED ACFT, SHUTDOWN ENGINE, NO OTHER FIRE INDICATIONS, VISUALLY CONFIRM NO SMOKE. ON SHUTDOWN IN RAMP ADC 1 FAULT OCCURRED & STAYED ON.
- [SDR FDEA201403190525](https://openairdocs.org/sdr/FDEA201403190525.md): Sensor · malfunctioned · Mar 19, 2014 · N803FD · Airbus A310324 · Engine Oil Indicating System
  > DURING CRUISE FLIGHT, NR 2 RT ENGINE OIL TEMP BEGAN TO FLUCTUATE FROM NORMAL CRUISE TEMP OF 116C UP TO 230C. STAYED ABOVE 160C FOR MORE THAN 9 MINUTES BUT CONTINUED TO FLUCTUATE BETWEEN NORMAL & A HIGH OF 230 C. FINALLY TEMP STAYED ABOVE 160 C FOR MORE THA
- [SDR FDEA201305070933](https://openairdocs.org/sdr/FDEA201305070933.md): Wire · damaged · May 7, 2013 · N811FD · Airbus A310324 · Engine Exhaust System Wiring
  > WHEN SETTING TAKEOFF POWER, NR 1 ENGINE REVERSE UNLOCK LIGHT ILLUMINATED. DURING REACTIVATION OF NR 1 THRUST REVERSER, FOUND WIRE CHAFING IN WIRING BUNDLE 21W4082-509 NEXT TO CONNECTOR DS307, FOUND THE WIRE ROUTING TO PIN 4 ON DS307 TO NR 1 THRUST REVERSER
- [SDR FDEA201304090756](https://openairdocs.org/sdr/FDEA201304090756.md): Limit Switch · failed · Apr 9, 2013 · N811FD · Airbus A310324 · Cargo/Baggage Doors
  > CLIMBING THROUGH 5,100 METERS RECEIVED ECAM ALERT. FORWARD CARGO DOOR UNLOCK, PROCEEDED ACCORDING WITH ECAMS SET LANDING ELEVATION AT 10,000 ALERT WENT AWAY AND CAME BACK IN FINAL AGAIN. EXECUTED OVER WEIGHT LANDING IAW QRH. GROUND CHECKED THE FWD CARGO D
- [SDR FDEA201207262710](https://openairdocs.org/sdr/FDEA201207262710.md): Engine · failed · Jul 26, 2012 · N805FD · Airbus A310324 · Engine (Turbine/Turboprop)
  > UPASSING 3000 ON T/O, FELT ABNORMAL VIBRATION WITH UNUSUAL NOISE. NOTICED N1 VIB AT 1.4 AND N2 VIB AT 2.4 ON ENG 1. WHILE TROUBLESHOOTING RECEIVED ENG 1 EPR MODE FAULT AND ATS LEVER KICKED OFF. NOTICED ENG 1 EGT GAUGE INOP AT "0". ENG 1 N1 BEGAN UNCOM
- [SDR FDEA201206272374](https://openairdocs.org/sdr/FDEA201206272374.md): Actuator · faulted · Jun 27, 2012 · N806FD · Airbus A310324 · Fuel Controlling System
  > PRIOR TO THRUST SET FOR TAKEOFF, RECEIVED NR 1 ENGINE FADEC CHANNEL A FAULT AND FADEC CHANNEL B FAULT. REJECTED TAKEOFF AT 45-50 KNOTS. FOLLOWED QRH PROCEDURES. SHUTDOWN AND RESTARTED NR 1 ENGINE, ATTEMPTED TAKEOFF AND RECEIVED SAME FAULTS AT SLIGHTLY HI
- [SDR FDEA201112295456](https://openairdocs.org/sdr/FDEA201112295456.md): Oil System · overtemp · Dec 29, 2011 · N808FD · Airbus A310324 · Turbine Engine Oil System
  > NR 2 ENG, HIGH OIL TEMP - ABOVE 180 DEG - SHUT ENG DOWN. ALL OTHER ENG PARAMETERS OK. INSPECTED NR2 ENG INLET & EXHAUST AREA; NIL ABNORMALTIES NOTED. VISUAL CK OIL QTY; NORMAL. R & R NR 2 ENGINE IAW WC 44T0105-2 AND 44T0708-2. RUN ENG IAW JRH LEAK CHECKED
- [SDR FDEA201110174555](https://openairdocs.org/sdr/FDEA201110174555.md): Engine · failed · Oct 17, 2011 · N804FD · Airbus A310324 · Engine (Turbine/Turboprop)
  > CLIMBING THRU FL300 F/O FELT SLIGHT VIBRATION, BUT NO INDICATIOINS OR ECAM AT FL 355, THERE WAS A YAW AND LOUD BANGING, EPR HAD DROPPED TO BELOW 1, OTHER ENGINE INSTRUMENTS LOOKED NORMAL, BUT THE LOUD BANGING CONTINUED WITH THROTTLE AT IDLE. OIL PRESSURE WAS
- [SDR 2011FA0000222](https://openairdocs.org/sdr/2011FA0000222.md): Jackscrew · out of position · Feb 18, 2011 · N807FD · Airbus A310324 · Stabilizer Control System
  > DURING O/H, MX PERFORMED ON THE SCREW JACK ASSY, FE140 SN 125, IDENTIFICATION OF THE WRONG POSITIONING OF THE RATCHET WHEEL (ITEM 3-620 OF CMM 27-44-13), ASSEMBLED ON THE OPPOSITE POSITION COMPARED TO THE SPEC MENTIONED ON THE CMM 27-44-13. LETTER LT-S9-11-10
- [SDR FDEA201012204727](https://openairdocs.org/sdr/FDEA201012204727.md): Power Supply · failed · Dec 20, 2010 · N803FD · Airbus A310324 · Emergency Lighting
  > EMERGENCY LIGHTS FAIL OPS CHECK FROM COURIER AREA TEST SWITCH. R & R THE POWER SUPPLY UNIT AND BATTERY IAW AMM 33-51-14-04. PERFORMED A SATISFACTORY TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-14-04.
- [SDR FDEA201012164699](https://openairdocs.org/sdr/FDEA201012164699.md): Rib · damaged · Dec 16, 2010 · N803FD · Airbus A310324 · Wing, Rib/Bulkhead
  > LT WING T/E RIB AT WIAX 62.70 HAS EDGE DAMAGE ON THE SPAR ATTACH FLANGE. REMOVED DAMAGE FROM THE SPAR AREA IAW EA 6-5730-136705.
- [SDR FDEA201011194431](https://openairdocs.org/sdr/FDEA201011194431.md): Limiter · failed · Nov 19, 2010 · N801FD · Airbus A310324 · Leading Edge Slat Control System
  > SLATS SYS 1 AND SLATS SYS 2 FLAPS, REPEAT ITEM, NO SLATS LANDING. PERFORMED LGAV, T/S SYS IAW FIM 27-80-02, FIG 101, SHEET 1. FOUND TORQUE LIMITER POPED. R AND R TORQUE LIMITER IAW MM 27-84-12-04. ALSO SERVICED LT WING SLATS, SCREW JACKS AND GEAR BOXES I
- [SDR FDEA201011164400](https://openairdocs.org/sdr/FDEA201011164400.md): Skin · corroded · Nov 16, 2010 · N812FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN EXTERIOR SURFACE FOUND CORROSION UNDER BULK CARGO DOOR SCUFF PLATE (FWD LWR CORNER). REMOVE THE CORROSION IAW SRM 51-74-10. APPLY ALODINE IAW SRM 51-21-10. MEASURE REMAIN THICKNESS OF THE REWORKED AREA IAW NTM51-10-04 (REMAINING THICKNESS WA
- [SDR FDEA201011034244](https://openairdocs.org/sdr/FDEA201011034244.md): Crossbeam · corroded · Nov 3, 2010 · N815FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > FR63 AFT CARGO LBL 10 "T" EXTRUSION EXFOLIATED ON LOWER FWD SIDE INSTALLED SPLICE REPAIR "T EXTRUSION AND L EXTRUSION" AT FR63 AFT CARGO LBL 10 TO RBL 12 ON LOWER FWD SIDE IAW SRM 53-10-15, PAGE 259/260, FIGURE 209, SHEET 1.
- [SDR FDEA201010284181](https://openairdocs.org/sdr/FDEA201010284181.md): Fitting · corroded · Oct 28, 2010 · N815FD · Airbus A310324 · Nacelle/Pylon, Longeron/Stringer
  > NR1 ENG PYLON RIB 18 FWD SIDE CORRODED ABOVE THE BRG REMOVED NR1 PYLON AFT ATTACH FITTING AT RIB 18 IAW AMM 54-51-75-04. REMOVED CORROSION FROM RIB 18 LUG IAW SRM 51-74-10, CHECKED FOR LIMITS FOUND OUT OF LIMITS IAW SRM 54-51-71, PAGE 110. INSTALLED NEW FITT
- [SDR FDEA201010284182](https://openairdocs.org/sdr/FDEA201010284182.md): Panel · cracked · Oct 28, 2010 · N815FD · Airbus A310324 · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON OTBD SIDE AT RIB 8 FWD SCEW HOLE HAS A 0.250 CRACK GOING UPWARDS. TRIMMED OUT CRACK AND REPAIRED PYLON NR 2 SIDE PANEL IAW SRM 54-51-31 FO\IG 201 PAGE 203 TO 207. THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVALS. THE INSP INSTRUCTION REF IS
- [SDR FDEA201010254167](https://openairdocs.org/sdr/FDEA201010254167.md): Fairing · cracked · Oct 25, 2010 · N803FD · Airbus A310324 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON INBD APRON FAIRING SKIN IS CRACKED. INSTALLED REPAIR DOUBLER ON THE NR1 PYLON INBD APRON FAIRING IN REF TO SRM 54-56-10, FIG 201.
- [SDR FDEA201010204122](https://openairdocs.org/sdr/FDEA201010204122.md): Seat Track · corroded · Oct 20, 2010 · N815FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, FWD CABIN SEAT TRACK NR3 LT HAS CORROSION FR 15 TO FR16. REMOVED CORROSION WITH 55 PERCENT MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-10-16, PAGE 108, FIG 101. R & R SEAT TRAC 3L BETWEEN FR15 AND FR16 IAW SRM 53-10-16 PAGE 108, FIG 101 AN
- [SDR FDEA201010204123](https://openairdocs.org/sdr/FDEA201010204123.md): Seat Track · corroded · Oct 20, 2010 · N815FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 3R IS CORRODED BETWEEN FR 18 AND FR 17 APPROX 3 SQ. INCH REMOVED CORROSION WITH 58 PERCENT MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PAGE 108, FIG 101. R & R SEAT TRACK 3R BETWEEN FR 17 AND FR 18 IAW SRM 53-10-16, PAGE 108, FIG 1
- [SDR FDEA201010204124](https://openairdocs.org/sdr/FDEA201010204124.md): Seat Track · corroded · Oct 20, 2010 · N815FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 2R IS CORRODED BETWEEN FR 16 AND FR 15 APPROX 12 INCH LONG REMOVED CORROSION WITH 65 PERCENT MATERIAL LOSS IAW SRM 53-10-16, PAGE 108, FIG 101 R & R SEAT TRACK NR 2R BETWEEN FR16 AND FR 15 IAW SRM 53-10-16, FIG 101 AND SRM 51-40-21.
- [SDR FDEA201010204125](https://openairdocs.org/sdr/FDEA201010204125.md): Seat Track · corroded · Oct 20, 2010 · N815FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 2L IS CORRODED IN 2 EA LOCATIONS BETWEEN FR 19 AND FR14 REMOVED CORROSION AT SEAT TRACK 2L IAW SRM 53-10-16, PAGE 103, FIG 101. AREA FOUND OUT OF LIMIT. R & R SEAT TRACK IAW SRM 53-10-16 AND SRM 51-40-21.
- [SDR FDEA201010194103](https://openairdocs.org/sdr/FDEA201010194103.md): Warning Message · false indication · Oct 19, 2010 · N809FD · Airbus A310324 · Central Warning
  > ON TAKEOFF ROLL APPROX 80 KTS GOT ECAM WARNING FOR PITCH FEEL SYS 1 AND 2 AND RUDDER TRAVEL SYS 1 AND 2 FAULTS. ALL 4 LIGHTS WERE ILLUMINATED ON OVHD PANEL. ABORTED TAKEOFF, COMPLETED APPROPRIATE CHECKLISTS AND RETURNED TO BLOCKS. ACCOMPLISHED AFS/LAND TE
- [SDR FDEA201010134042](https://openairdocs.org/sdr/FDEA201010134042.md): Support · cracked · Oct 13, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > FUSELAGE UNDER THE LT AIR CONDITIONING AFT FAIRING THE AFT INBD EXHAUST SHIELD SUPPORT IS CRACKED. REMOVED SUPPORT BRACKET IAW SRM 51-40-21. RECEIVED NEW SUPPORT BRACKET FROM STORES, PO 693873.1. INSTALLED NEW BRACKET IAW SRM 51-72-10, PAGES 1-3.
- [SDR FDEA201010124021](https://openairdocs.org/sdr/FDEA201010124021.md): Floor Panel · delaminated · Oct 12, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
  > AIR CONDITIONING COMPARTMENT FLOOR PANEL 143 DF HAS A LARGE CORNER THAT IS DELAMINATED AND CONTAMINATED. FABRICATED NEW AIR CONDITIONING COMPARTMENT FLOOR PANEL 143 DF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201010124011](https://openairdocs.org/sdr/FDEA201010124011.md): Seat Track · gouged · Oct 12, 2010 · N815FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 4L BETWEEN FRAME 62 AND FRAME 65 HAS 2 AREAS OF GOUGES AROUND SCALLOPS, APPROX.009" DEEP. REMOVED DAMAGED AREAS BY BLENDING OUT GOUGES ON SCALLOPS OF SEAT TRACK 4L BETWEEN FRAME 62 AND FRAME 65 IAW SRM 51-73-10, PGS 7 THRU 10. CHECKED LIMITS AND
- [SDR FDEA201010073974](https://openairdocs.org/sdr/FDEA201010073974.md): Selector Valve · failed · Oct 7, 2010 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension System
  > LOWERED MLG HANDLE (WITH SYS 2, POSITION DET SELECTED) GOT UNLOCK LIGHTS BUT NO MLG DOWN, SELECTED SYS 1, NO CHANGE, RAISED MLG HANDLE, LIGHTS WENT OUT, LOWERED MLG AGAIN IN SYS 2, AND MLG CAME DOWN NORMALLY. BITE ON PROX BOX, NO FAULT REGISTERED, FOLLOWED TS
- [SDR FDEA201009303818](https://openairdocs.org/sdr/FDEA201009303818.md): Sleeve · cracked · Sep 30, 2010 · N803FD · Airbus A310324 · Engine Thrust Reverser
  > NR 2 ENG RT THRUST REVERSER SLEEVE IS CRACKED AND DAMAGED JUST BELOW THE NR 6 BLOCKER DOOR. REPAIRED NR 2 THRUST REVERSER JUST BELOW THE NR 6 BLOCKED DOOR BY CLEANING EXISTING POTTING AND RE-POTTING DAMAGED AREA AND CURING IAW SRM 54-05- 01, PARA 9.
- [SDR FDEA201009303819](https://openairdocs.org/sdr/FDEA201009303819.md): Filter · leaking · Sep 30, 2010 · N811FD · Airbus A310324 · Hydraulic System, Main
  > DURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QTY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING GEAR. FOUND HYD LEAKAGE CAME FROM THE GREEN SERVO CONTRO FILTER. REMOVED AND REPLACED THE PUMP DELIV
- [SDR FDEA201009303820](https://openairdocs.org/sdr/FDEA201009303820.md): Pickup · malfunctioned · Sep 30, 2010 · N809FD · Airbus A310324 · Trailing Flap Position Indicating System
  > ON FINAL APPROACH, WHEN FLAPS WERE SELECTED TO 40 DEG RECEIVED ECAM. FLAPS STUCK. ALSO RECEIVED SYS 1 AND 2 FAULT LIGHT ON OVERHEAD PANEL. FLAPS STUCK BETWEEN 20 DEG -40 DEG. COMPLIED WITH QRH AND ECAM. REPLACED LT APPU 29CV PER AMM 27-56-11-04. PERFORMED O
- [SDR FDEA201009273747](https://openairdocs.org/sdr/FDEA201009273747.md): Floorboard · cracked · Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD NR 241 YF IS CRACKED AT FRAME 54. FABRICATED NEW FLOORBOARD, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201009273748](https://openairdocs.org/sdr/FDEA201009273748.md): Floor Panel · cracked · Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR261 LF IS CRACKED FROM FRAME 74 - FRAME 75; LBL 12. FABRICATED NEW FLOOR BOARD, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201009273749](https://openairdocs.org/sdr/FDEA201009273749.md): Floor Panel · damaged · Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR251 RG IS CRUSHED FROM APPROX FRAME 60 - FRAME 62; LBL 60. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201009273743](https://openairdocs.org/sdr/FDEA201009273743.md): Floor Panel · cracked · Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 222 CF IS CRACKED ACROSS THE BOTTOM. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201009273750](https://openairdocs.org/sdr/FDEA201009273750.md): Floor Panel · cracked · Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL NR232 RG HAS THE FWD RT EAR CRACKED. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201009263715](https://openairdocs.org/sdr/FDEA201009263715.md): Connector · dirty · Sep 26, 2010 · N804FD · Airbus A310324 · Electrical Power System Wiring
  > CLIMBING THROUGH FL330 GOT RT R1 DOOR NOT CLOSED COMPLIED WITH QRH AND DESCENTED BELOW 10,000. GOING THROUGH FL200 THE WARNING WENT AWAY. ATC WOULD NOT LET US CONTINUE AT 10,000 SO RETURNED TO DEPARTURE. CABIN PRESSURE WAS GOOD. ALL NORMAL, CLEANED THE CON
- [SDR FDEA201009263716](https://openairdocs.org/sdr/FDEA201009263716.md): Computer · malfunctioned · Sep 26, 2010 · N812FD · Airbus A310324 · Fuel Indicating System
  > ON TAKEOFF ROLL, MASTER WARNING REPETITIVE CHIME, AT APPROX 130 KTS RTO. ECAM SHOWED PITCH TRIM 2 YD 2 OFF. PITCH TRIM 2 YD 2 BOTH RESET OK. BRAKE 3 670 DEGREES. WHILE WAITING FOR HOT BRAKES TO COOL, FUEL WENT BELOW RQR FOR FOR TO. SO RETURN TO GATE, O
- [SDR FDEA201009203584](https://openairdocs.org/sdr/FDEA201009203584.md): Actuator · malfunctioned · Sep 20, 2010 · N811FD · Airbus A310324 · Drag Control Actuator
  > ON FINAL TO 15L ICN SELECTING FLAPS 40 HAD AMBER SPOILER 5 FAULT, REPEAT HAPPENED 2 TIMES. DID MISSED APPROACH AND WHILE DOING QRH PROCEDURE ACFT COMMANDED 15 DEG LT TURN WITH CONTROL WHEEL. SELECTED FLIGHT CONTROLS AND NOTED SPOILERS LT 5,6,7 WERE ALL UP
- [SDR FDEA201009173525](https://openairdocs.org/sdr/FDEA201009173525.md): Skin · corroded · Sep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > LT WING TOP SKIN SURFACE IS CORRODED AT THE REAR SPAR AREA FROM RIB 15-RIB 16. REMOVED CORROSION; LT WING TOP SKIN T/E AREA BETWEEN RIBS 15-16 IAW SRM 57-20-12, PG 9. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 9 & 111. TOOL T8285D. FLAP PEENED AREA IA
- [SDR FDEA201009173527](https://openairdocs.org/sdr/FDEA201009173527.md): Skin · corroded · Sep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > LT WING TOP SKIN SURFACE IS CORRODED 2 EA PLACES AT THE REAR SPAR AREA FROM RIB 12 - RIB 13. REMOVED CORROSION IAW SRM 57-00-00, PG 212 AT THE LT WING TOP SKIN UPPER SURFACE T/E BETWEEN RIBS 12-13. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 9 & 111.
- [SDR FDEA201009173528](https://openairdocs.org/sdr/FDEA201009173528.md): Skin · corroded · Sep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > LT WING TOP SKIN SURFACE IS CORRODED AT THE REAR SPAR AREA FROM RIB 4 - RIB 5. REMOVED 2 EA FASTENERS LT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 17 AND RIB 18 IAW SRM 51-40-21. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM
- [SDR FDEA201009173529](https://openairdocs.org/sdr/FDEA201009173529.md): Skin · corroded · Sep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > RT WING TOP SKIN SURFACE FRONT SPAR AREA SKIN IS CORRODED FROM RIB 17 - RIB 18. REMOVED 5 EA FASTENERS RT WING TOP SKIN UPPER SURFACE FRONT SPAR BETWEEN RIB 17 AND RIB 18. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13
- [SDR FDEA201009163502](https://openairdocs.org/sdr/FDEA201009163502.md): Skin · cracked · Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > LT WING BOTTOM SKIN LOWER SURFACE T/E AREA SKIN IS CRACKED FROM RIB 11 TO RIB 12. COMPLIED WITH EA 6-5730-136705.
- [SDR FDEA201009163503](https://openairdocs.org/sdr/FDEA201009163503.md): Skin · corroded · Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > RT WING TOP SKIN UPPER SURFACE, REAR SPAR AREA SKIN IS CORRODED FROM RIB 23 TO RIB 24. REMOVED FASTENER RIGHT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 23 AND RIB 24. BLENDED CORROSION IAW A310-300 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 5
- [SDR FDEA201009163504](https://openairdocs.org/sdr/FDEA201009163504.md): Skin · corroded · Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > RT WING TOP SKIN UPPER SURFACE, REAR SPAR AREA SKIN IS CORRODED FROM RIB 4 TO RIB 5. REMOVED 2 EA FASTENERS RT WING TOP SKIN UPPER SURFACE AT REAR SPAR IAW SRM 51-40-21. BLENDED CORROSION IA SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13 &
- [SDR FDEA201009163505](https://openairdocs.org/sdr/FDEA201009163505.md): Skin · corroded · Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/Skin
  > RT WING TOP SKIN UPPER SURFACE, SKIN IS CORRODED FROM RIB 10 TO RIB 11. REMOVED FASTENER RT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 10 AND RIB 11. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13 & 110. FLAP
- [SDR FDEA201009143386](https://openairdocs.org/sdr/FDEA201009143386.md): Jackscrew · damaged · Sep 14, 2010 · N809FD · Airbus A310324 · Trailing Edge Flap Control System
  > ON FINAL SLATS/FLAPS STUCK 20/17: RECYCLED AND SLAT/FLAP STUCK LIGHT EXTINGUISHED. SELECTED SLAT/FLAP 20/20 TO LAND AND LIGHT REILLUMINATED, THE SECOND TIME. RAN QRH AND LANDED AT SLAT/FLAPS 20/17. ALL HYD'S WERE GOOD. REPLACED NR 3 FLAP JACKSCREW IAW AMM
- [SDR FDEA201009143390](https://openairdocs.org/sdr/FDEA201009143390.md): Floor Panel · punctured · Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > BULK CARGO SLANT PANEL 161 CW IS PUNCTURED AND DENTED IN NUMEROUS PLACES. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND BONDED METAL PLATE IAW DWG SRZ 25-011, REV "C".
- [SDR FDEA201009143391](https://openairdocs.org/sdr/FDEA201009143391.md): Panel · dented · Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > BULK CARGO SLANT PANEL 162 CW HAS DENT DAMAGE. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS REF DWG SRZ 25- 005, REV "H". FABRICATED, TRIMED AND BONDED A METAL PLATE REF DWG SRZ 25-011, REV "C".

Next page: https://openairdocs.org/engine/pratt-whitney-pw4152/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 = 'PW4152'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-pw4152/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.