# Service difficulty reports: Pratt & Whitney JT3D-3

A list on [Pratt & Whitney JT3D-3](https://openairdocs.org/engine/pratt-whitney-jt3d-3.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 55 reports

- [SDR U2RA485FLP5226](https://openairdocs.org/sdr/U2RA485FLP5226.md): Inu · inoperative · Dec 14, 2010 · N155CA · Doug DC873F · Inertial Guidance System
  > NR1, IMMEDIATELY AFTER ROTATION, NR 1 INU FAILED, CAPT INSTRUMENTS FLAGGED FAIL. NR 2, IMMEDIATELY AFTER ROTATION GPWS WENT INOP. NR 3, IMMEDIATELY AFTER ROTATION YAW DAMPER KICKED OFF AND A/P OR YAW DAMPER WOULD NOT ENGAGE FROM EITHER PILOTS A/P TRANSFER SW
- [SDR IXXA10SMN069S](https://openairdocs.org/sdr/IXXA10SMN069S.md): Longeron · corroded · Jun 19, 2010 · N71CX · Doug DC862F · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON L-23 RT INTERIOR CORRODED AT STA 1380-1400. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABERCATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW
- [SDR IXXA10SMN070S](https://openairdocs.org/sdr/IXXA10SMN070S.md): Skin · corroded · Jun 19, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING OTBD L/E OUTER SECTION LOWER SKIN CORRODED AT STA XFS 710.000 - 760.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP. NO DISCREPAN
- [SDR IXXA10SMN071S](https://openairdocs.org/sdr/IXXA10SMN071S.md): Skin · dented · Jun 19, 2010 · N71CX · Doug DC862F · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSP FOUND THE LT WING OTBD FLAP UPPER SKIN DENTED AT STA XF 238.000 - 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW F
- [SDR IXXA10SMN072S](https://openairdocs.org/sdr/IXXA10SMN072S.md): Skin · cracked · Jun 19, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING NR 4 STUB WING LOWER SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLERS AND INTERNAL DOUBLERS. PERF
- [SDR IXXA10SMN067S](https://openairdocs.org/sdr/IXXA10SMN067S.md): Cargo Track · corroded · Jun 18, 2010 · N71CX · Doug DC862F · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 6 TRACK CORRODED AT STA 372.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW TRACK SEGMENT AND RE
- [SDR IXXA10SMN063S](https://openairdocs.org/sdr/IXXA10SMN063S.md): Skin · corroded · Jun 17, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER, AND FILLERS.
- [SDR IXXA10SMN065S](https://openairdocs.org/sdr/IXXA10SMN065S.md): Angle · corroded · Jun 17, 2010 · N71CX · Doug DC862F · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE VERTICAL STABILIZER TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE, FILLER AND TAPERED SHIMS. PERFORMED HEAT TREATMENT. CLEANED,
- [SDR IXXA10SMN066S](https://openairdocs.org/sdr/IXXA10SMN066S.md): Skin · corroded · Jun 17, 2010 · N71CX · Doug DC862F · Elevator, Plate/Skin
  > DURING ROUTINE C-CHECK INSP, FOUND LT HORIZ STABILIZER ELEVATOR LOWER SKIN CORRODED AT STA XE 195.313, 149.000, AND 132.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, FINGE
- [SDR IXXA10SMN064S](https://openairdocs.org/sdr/IXXA10SMN064S.md): Fitting · corroded · Jun 16, 2010 · N71CX · Doug DC862F · Fuselage Main, Attach Fittings
  > DURING ROUTINE C-CHECK, INSP FOUND LT MLG WHEEL WELL FRAME FITTING CORRODED AT FS 879.000 LONGERON 24. REMOVED CORRODED FITTING. FABRICATED NEW FITTING, SPLICES AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PAR
- [SDR IXXA10SMN061S](https://openairdocs.org/sdr/IXXA10SMN061S.md): Skin · corroded · Jun 16, 2010 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND LT WING UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 STR 14. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN AND
- [SDR IXXA100036O](https://openairdocs.org/sdr/IXXA100036O.md): Controller · defective · Jun 4, 2010 · N71CX · Doug DC862F · Cabin Pressure Controller
  > DURING CRUISE, CABIN RATE OF CLIMB RAISED QUICKLY TO 10,000 FT, FLIGHT ENGINEER RAN PNEUMATIC TO HIGH AND OPERATED THE PRESSURE CONTROL VALVE. THE CREW WAS PERMITTED PARTIAL CONTROL OF CABIN PRESSURE UNTIL ACFT DESCENDED BLOW FL200. THEY RETURNED TO DEPARTURE
- [SDR IXXA100029S](https://openairdocs.org/sdr/IXXA100029S.md): Skin · cracked · May 1, 2010 · N71CX · Doug DC862F · Vertical Stabilizer, Plate/Skin
  > DURING PREFLIGHT, FOUND VERTICAL STABILIZER L/E CRACKED AT STA ZFS 292 CTR LINE. REPLACED CRACKED L/E WITH INTERIM REPAIR IAW FVCI DWG NR 55-10165-1.
- [SDR IXXA090065O](https://openairdocs.org/sdr/IXXA090065O.md): Regulator · defective · Nov 5, 2009 · N71CX · Doug DC862F · Compressor Bleed Valve
  > DURING CLIMB OUT FROM NR 2 ENG COMPRESSOR STALLED WITH GEAR UP, EPR 1.86 AND ANTI-ICE VALVE ON. THE CREW RETURNED TO WITHOUT FURTHER INCIDENT. MX REPLACED BOTH ANTI-ICE VALVE REGULATOR'S. OPS CHECK GOOD IAW MX MM 75-10-2. ACFT WAS RETURNED TO SERVICE.
- [SDR IXXA090038O](https://openairdocs.org/sdr/IXXA090038O.md): Antenna · defective · Aug 5, 2009 · N71CX · Doug DC862F · Weather Radar System
  > DURING CRUISE, WEATHER RADAR WILL NOT PAINT AND STABILIZATION INOP. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER AND RADAR ANTENNA. OPS CHECK GOOD IAW MM 34-41-1. ACFT WAS RETURNED TO SERVICE.
- [SDR IXX2008F00093](https://openairdocs.org/sdr/IXX2008F00093.md): Line · loose · Sep 7, 2008 · N71CX · Doug DC862F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL, NR (1) ENGINE WOULD NOT ACCELERATE PAST 78 PERCENT. NR 2 WITH CORRESPONDING LOW N1, FUEL FLOW AND EGT. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINT INSPECTED AND FOUND LOOSE PT2 LINE ON PRBC VALVE. MAINT RECONNECTED LINE. OPER
- [SDR UPS08852685](https://openairdocs.org/sdr/UPS08852685.md): Structure · dented · Jul 8, 2008 · N868UP · Doug DC873F · Passenger/Crew Doors
  > DENT IN MAIN ENTRY DOOR AROUND AFT FRAME.
- [SDR UPS08852664](https://openairdocs.org/sdr/UPS08852664.md): Frame · corroded · Jun 12, 2008 · N700UP · Doug DC871F · Fuselage Main, Frame
  > INSPECTION TYPE-C1, AREA OF CORROSION EXFOLIATON ON AFT SIDE OF STA 70 FRAME, A PIT, BETWEEN L29L AND L30L. REMOVED DAMAGE AND FABRICATED DOUBLER IAW SRM 53-02-05 FIG 008C.
- [SDR UPS07850577](https://openairdocs.org/sdr/UPS07850577.md): Starter · leaking · Sep 1, 2007 · N750UP · Doug DC871F · Engine Cranking
  > INSPECTION TYPE:N/A IFSD - NR 1 ENG SHUTDOWN IN CLIMB PASSING 25000 DUE TO OIL QTY GOING TO ZERO. OIL PRESSURE WAS 12 PSI. SERVICED OIL, RAN ENGINE, FOUND OIL LEAKING FROM STARTER. REMOVED AND REPLACED NR 1 ENGINE STARTER IAW MM 80-10-01-2. OPS CHECK REQUI
- [SDR IXXA060453O](https://openairdocs.org/sdr/IXXA060453O.md): Engine · leaking · Jun 21, 2006 · N799AL · Doug DC862 · Turbine Engine Oil System
  > APPROXIMATELY FIVE HOURS AFTER TAKEOFF FROM TAPA THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 20 PSI. THE ENGINE WAS SHUTDOWN AND CHECKLIST WAS COMPLIED WITH THE CREW RETURNED TO TAPA AND LANDED. MAINTENANCE FOUND THE OIL E
- [SDR ARWA20051005](https://openairdocs.org/sdr/ARWA20051005.md): Brake Assy · damaged · Oct 20, 2005 · N661AV · Doug DC863F · Brake
  > LOG PAGE NR 117327. NR 2 MAIN WHEEL TIRE BLOWN; NR 2 BRAKE DAMAGED. REMOVED AND REPLACED NR 2 MAIN WHEEL IAW M/M 32-40-1; REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY IAW MM 32-42-1, NO LEAKS NOTICE.
- [SDR ABXA050090](https://openairdocs.org/sdr/ABXA050090.md): Indicator · defective · Apr 11, 2005 · N847AX · Doug DC861 · Engine Oil Pressure
  > ON TAKEOFF AND CLIMB, NR 3 ENGINE OIL PRESSURE CLIMBED TO 75 - 80 PSI. TOOK THROTTLE TO IDLE, PRESSURE WENT TO 60 PSI. SECURED NR 3 ENGINE. AIR TURN BACK. AFTER SECURING THE ENGINE, THE PRESSURE READ 14 PSI STATIC ON TAXI. REPLACED NR 3 ENGINE OIL PRESSUR
- [SDR IXXA0400113O](https://openairdocs.org/sdr/IXXA0400113O.md): Warning Light · false activation · Oct 19, 2004 · N71CX · Doug DC862F · Fire Detection
  > DURING CRUISE AT FL 370 LOWER CARGO COMPARTMENT FIRE WARNING ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. CREW RETURNED AND LANDED WITHOUT INCIDENT. UPON LANDING MAINTENANCE INSPECTED ALL LOWER CARGO COMPARTMENTS AND FOUND NO EVIDENCE OF FIRE. REF DMI NR
- [SDR IXXA0400102O](https://openairdocs.org/sdr/IXXA0400102O.md): Engine · failed · Aug 7, 2004 · N71CX · Doug DC862F · Engine Oil Quantity
  > DURING CRUISE FROM KSUU TO PHIK, NR 4 ENGINE LOSS OF ALL OIL QUANTITY AND OIL PRESSURE OF 12PSI. ENGINE NR 4 OIL LIGHT CAME ON. CREW SHUT DOWN NR 4 ENGINE AND AFTER SHUT DOWN NR 4 ENGINE WINDMILLING OIL PRESSURE AT 5PSI. AIRCRAFT ARRIVED IN PHIK AND LANDED
- [SDR UPS04842886](https://openairdocs.org/sdr/UPS04842886.md): Fitting · gouged · Jul 22, 2004 · N700UP · Doug DC871F · Cargo/Baggage Doors
  > INSPECTION TYPE: C3, C-1 DOOR AFT LOWER GUIDE PIN FITTING WORN GOUGED. REMOVED DAMAGED FITTING IAW UPS SRM 51-3-0. DAC DWG NR 5754075. FOUND TO BE OUT OF LIMITS IAW UPS SRM 53-2-0. RECEIVED NEW FITTINGS P/N NR SP 003923. LOCATED AND DRILLED AND DEBURRED FIT
- [SDR ARWA20040704](https://openairdocs.org/sdr/ARWA20040704.md): Skin Panel · cracked · Jul 19, 2004 · N661AV · Doug DC863F · Wing, Plate/Skin
  > DURING C-CHECK INSPECTION, RT WING BETWEEN XRS.428 AND XRS.463 AT STRINGER S-64 LOWER SKIN PANEL WITH CRACK, LENGTH 5.25 INCHES.
- [SDR UPS04842885](https://openairdocs.org/sdr/UPS04842885.md): Seat Track · cracked · Jul 16, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C3 STA 65-75 RBL 36 SEAT TRACK LOBES OBLONGED. REMOVED FLOOR PANELS FS 70-170 FOM. REMOVED SEAT TRACK,DAMAGED OUT OF LIMITS IAW SRM 53-2-3. DRILLED NEW SEAT TRACK AND TRACK SPLICE TO FIT. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED FLOOR
- [SDR UPS04842874](https://openairdocs.org/sdr/UPS04842874.md): Seat Track · worn · Jul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C3, STA 595-600 RBL 36 SEAT TRACK LOBES ELONGATED/OBLONGED. DAMAGE FOUND OUT OF LIMITS IAW SRM 53-2-3. REMOVED SEAT TRACK SECTION IAW SRM 51-3-0, DRILLED NEW SEAT TRACK SECTION TO FIT IAW SRM 51-1-24. INSTALLED IAW SRM 51-3-0 AND 51-3-1.
- [SDR UPS04842876](https://openairdocs.org/sdr/UPS04842876.md): Floorboard · corroded · Jul 2, 2004 · N700UP · Doug DC871F · Fuselage Floor Panel
  > INSPECTION TYPE: C3, STA 280 RBL 1 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION SECTION OF FLOORBOARD FAB SPLICE PLATES. ALODINED AND PRIMED. INSTALLED SPLICE PLATES AND SECTION OF FLOORBOARD IAW SRM 51-3-0, 51-3-1, 5
- [SDR UPS04842877](https://openairdocs.org/sdr/UPS04842877.md): Floorboard · corroded · Jul 2, 2004 · N700UP · Doug DC871F · Fuselage Floor Panel
  > INSPECTION TYPE: C3, STA 235 RBL 8 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBOARD. LOCATED NEW FLOORBOARD AND SPLICE PLATES. ALODINED AND PRIMED. INSTALLED FLOORBOARDS. ALL IAW SRM 51-3-0, 51-3-1, 51-1-8, AND 5
- [SDR UPS04842878](https://openairdocs.org/sdr/UPS04842878.md): Seat Track · gouged · Jul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C3, STA 1580 RBL 18 SEAT TRACK LOBES GOUGED AND OBLONGED. BLENDED OUT DAMAGED LOBES AND FOUND OUT OF LIMITS. REMOVED 4 HOLES SEAT TRACK PLUG P/N DC8-53B-007-002 PO NR SP0906208 AND INSTALLED IAW EO NR 5340-7779-B. ALL IAW SRM 53-2-0, 53-2-3, A
- [SDR UPS04842879](https://openairdocs.org/sdr/UPS04842879.md): Seat Track · worn · Jul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C3, SEAT TRACK (D) HAS WORN SCALLOPS AND LUGS BETWEEN FS 1560-1580 DOT NR D 973. BLENDED SEAT TRACK LUGS AND SCALLOPS, FOUND OUT OF LIMITS. OPEN FLOORBOARDS FROM FS 1495 TO 1690 LBL 16 TO LBL 32 IAW DC8 SRM 51-3-0 TO FOM, REMOVED SEAT TRACK
- [SDR UPS04842880](https://openairdocs.org/sdr/UPS04842880.md): Seat Track · worn · Jul 2, 2004 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C3 SEAT TRACK E HAS WORN SCALLOPS AND LUGS BETWEEN FS 1400 AND 1410. BLEND AREA IAW UPS SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3, CUT OUT DAMAGE ON SEAT TRACK IAW EO 5340-7779B. ALODINED AND PRIMED CUT AREA, MAT ID PLUG SEAT T
- [SDR UPS04842881](https://openairdocs.org/sdr/UPS04842881.md): Longeron · cracked · Jul 1, 2004 · N700UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C3, FUSELAGE INTERIOR L 17 RT CRACKED FROM FS 1770 TO FS 1774. REMOVED L17R AT STA 1766 IAW SRM 51-1-20D. RECIEVED NEW LONGERON PN 5 649327-43. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED LONGERON IAW SRM 51-1-21 AND 51-1-20D.
- [SDR UPS04842882](https://openairdocs.org/sdr/UPS04842882.md): Frame · corroded · Jun 30, 2004 · N700UP · Doug DC871F · Fuselage Main, Frame
  > INSPECTION TYPE: C3, FLC BILGE FRAME HAS CORROSION AT FS 600 RBL 12. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT PART OF FRAME WITH CORROSION FAB NEW FRAME SECTION IAW DWG 5750886. SECTION HEAT TREATED TO 17075+6 FAB SPLICES AND STAPS. SPLICES HEAT TRE
- [SDR UPS04842883](https://openairdocs.org/sdr/UPS04842883.md): Web · corroded · Jun 30, 2004 · N700UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C3, AFT PIT WEB CORRODED BETWEEN FS 1200 L35R. REMOVED WEB FROM STA 1160 TO 1220, MAT ID FOR WEB AND SPLICES 7075T6.125 PO NR 424554.3 IAW DWG NR 3753772, FAB WEB AND SPLICES. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED WEB FROM STA 1160
- [SDR ARWA20040602](https://openairdocs.org/sdr/ARWA20040602.md): Indicator · erratic · Jun 19, 2004 · N906R · Doug DC863F · Engine Pressure Ratio (EPR)
  > LOG PAGE NR 107344, AFTER ALL ENGINES SPOOLED AND TAKEOFF STARTED NR 1 EPR (ENGINE PRESSURE RATIO) ERRATIC; DISCONTINUED TAKEOFF AND TAXIED BACK TO RAMP. TRANSFERRED TO DMI NR 18568 IAW MM. AIRCRAFT RELEASED IAW MEL NR 77-1-2 CAT (A). REMOVED AND REPLACED NR
- [SDR ARWA20040601](https://openairdocs.org/sdr/ARWA20040601.md): Amplifier · malfunctioned · Jun 9, 2004 · N906R · Doug DC863F · Fire Detection
  > DURING TAXI, NR 2 ENGINE FIRE WARNING INTERMITENTLY ILLUMINATED FIRE WARNING TEST INOPERATIVE, SHUT DOWN ENGINE; RETURNED TO RAMP. NO FIRE NOTED. CHECK FIRE WARNING SYSTEM AT RUNUP CONDITION. CHECK WIRING FOR CONDITION, ELEMENTS FOR CONDITION AT NR 2 ENGIN
- [SDR 0375](https://openairdocs.org/sdr/0375.md): Frame · corroded · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Frame
  > DURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT CIRCUMFERENTIAL FRAME LOWER LEG CORRODED AT FS 80 BETWEEN LONGERON 36R AND 35R AND IDENTIFIED AS LEVEL 2 CORROSION.
- [SDR 0378](https://openairdocs.org/sdr/0378.md): Frame · cracked · Feb 17, 2004 · N865F · Doug DC863F · Fuselage Main, Frame
  > DURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT FORWARD FRAME FITTING CRACKED AT FS299 BETWEEN LONGERON 32R AND 33R.
- [SDR U2R2004F00000](https://openairdocs.org/sdr/U2R2004F00000.md): Spar Cap · cracked · Oct 29, 2003 · N921R · Doug DC863F · Wing Spar
  > DURING REPETIVE COMPLIANCE WITH AD AND SB, DETECTED 2 CRACKS AT RT WING FRONT SPAR LOWER CAP, REPAIRED IAW SB. REMAINING HOLES STRESS COINED TO CONDITION 1, OPTION 2.
- [SDR IXXA0300059O](https://openairdocs.org/sdr/IXXA0300059O.md): Valve · malfunctioned · Sep 17, 2003 · N728PL · Doug DC862 · Turbine Engine Oil System
  > DURING CLIMB NR 4 ENG QTY DROPPED & OIL PRESS ROSE TO 60 PSI, TEMP INCREASED. POWER WAS REDUCED PARAMETERS REDUCED OIL PRESS, OIL TEMP REDUCED 20 DEGREES & OIL QTY INCREASED. OIL PRESS LIGHT NEVER ILLUM & OIL PRESS NEVER DROPPED BELOW 40 PSI. MX REMOVED & I
- [SDR ARWA20030606](https://openairdocs.org/sdr/ARWA20030606.md): Pin · damaged · Jun 25, 2003 · N661AV · Doug DC863F · Landing Gear Retraction/Extension System
  > ON WALK-AROUND FOUND LT MAIN LANDING GEAR EYEBOLT ACTUATOR WITH EXCESSIVE GAP AT PIN BOSS ATTACHMENT. REMOVED LT MAIN LANDING GEAR ROUTED TO SHOP FOR ACTUATOR PIN REPLACEMENT, REINSTALLED SERVICIABLE MAIN LANDING GEAR IAW MM 32-11-0, OPERATIONAL LEAK CHECK OK
- [SDR UPS03840930](https://openairdocs.org/sdr/UPS03840930.md): Longeron · cracked · Jun 16, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C LONGERON 17L AND FWD END FITTING CRACKED AT BS 1768 REMOVED LONGERON 17L AND END FITTING. LOCATED, DRILLED LONGERON AND END FITTING IAW SRM 51-1-24. REMOVED AND REINSTALLED HYDRAULIC CASE AND LINES AT STA 1768 IAW MM 20-12-00. INS
- [SDR UPS03840931](https://openairdocs.org/sdr/UPS03840931.md): Door Frame · mislocated · Jun 16, 2003 · N851UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C, MAIN CABIN AT STA 1660-R2 DOOR JAMB WEB HAS DOUBLE DRILLED HOLES. REM FASTENERS FROM DOOR JAMB WEB. REM AIR GRILL AND R2 DOOR DRAIN PAN. TRIMMED OUT DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 DWG DC8-53A-01 0 AND UPS EO DC8-5310-11728-A
- [SDR UPS03840908](https://openairdocs.org/sdr/UPS03840908.md): Longeron · cracked · Jun 6, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C3 AFT PIT FS 1350, LONGERON 35L IS CRACKED. REMOVED CRACKED LONG 35L FS 1270 TO 1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 3 5L FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0.
- [SDR UPS03840907](https://openairdocs.org/sdr/UPS03840907.md): Skin · cracked · Jun 5, 2003 · N851UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 LOWER FUSELAGE CENTER SECTION AT FS 1350 LONGERON 34L FUSELAGE SKIN IS CRACKED. REMOVED 2 EA EXISTING REPAIR DOUBLERS, TRIMMED OUT CRACK FS 1350 LONG 34L FABBED REPAIR DOUBLER COMBINING 2 EA EXISTING REPAIR DOUBLERS, FABBED SKIN FILLERS AN
- [SDR UPS03840906](https://openairdocs.org/sdr/UPS03840906.md): Longeron · cracked · Jun 4, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 MAIN CABIN AT FS 1660, LONGERON 11R IS CRACKED. REMOVED OLD LONG 11RT TO FOM, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONG 11RT IAW DC8 SRM 51-1-21.
- [SDR UPS03840932](https://openairdocs.org/sdr/UPS03840932.md): Angle · cracked · Jun 3, 2003 · N851UP · Doug DC873F · Fuselage Main, Keel
  > INSPECTION TYPE: C, R/W/W KEEL BEAM INSIDE ACCESS DOVER STA 935, BEAM IS CRACKED REM MLG LT AND RT DOOR ACTUATORS, LT AND RT W/W WEBS TO FOM. LOC DRI LLED AND INSTALLED NEW SPLICE ANGLE IAW DAC DWG 5750371 P/N 5750042- 1N. FAB -51, -53, -55, -57 AND -59 R
- [SDR ABXA020364](https://openairdocs.org/sdr/ABXA020364.md): Link · broken · Dec 18, 2002 · N842AX · Doug DC861 · Drag Control System
  > RT WING INBOARD SPOILER WOULD NOT DEPLOY. REMOVED AND REPLACED BROKEN ACTUATOR CRANK LINKS IN THE INBOARD AND OUTBOARD POSITIONS FOR THE RT INBOARD SPOILER PANEL IAW MM. OPS CHECKED GOOD.

Next page: https://openairdocs.org/engine/pratt-whitney-jt3d-3/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 = 'JT3D3'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-jt3d-3/reports

---
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.