# Service difficulty reports: Pratt & Whitney JT3D series

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

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 70 reports

- [SDR IXXA201312040450](https://openairdocs.org/sdr/IXXA201312040450.md): Pressure Switch · malfunctioned · Dec 4, 2013 · N41CX · Doug DC862F · Engine Oil Pressure
  > AFTER TAKEOFF AT 1545Z NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED, PERFORMED APPROPRIATE CHECK LIST, LOW PRESS LIGHT STAYED ON SHUT ENG DOWN. R & R NR 1 LOW OIL PRESS SWITCH IAW 79-32-2, SYS OPERATIONS CHECKED NORMAL IAW DACO DC8 MM 79-32-0 & ATI ERH 70.01GMM 3
- [SDR IXXA110036O](https://openairdocs.org/sdr/IXXA110036O.md): Smoke Detector · defective · Apr 30, 2011 · N71CX · Doug DC862F · Smoke Detection
  > DURING CLIMBOUT, THE NR 2 CARGO SMOKE DETECTOR FLASHED ON MOMENTARLY SEVERAL TIMES WITH ASSOCIATED AUDIBLE WARNING. THE CREW INSPECTED THE CARGO COMPARTMENT FOR SMOKE OR FIRE AND NONE WAS NOTED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX IN
- [SDR IXXA100055O](https://openairdocs.org/sdr/IXXA100055O.md): Control Valve · defective · Nov 23, 2010 · N799AL · Doug DC862F · Cabin Cooling System
  > AFTER TAKEOFF, WHEN THE RT AIR CONDITIONING PACK WAS TURNED ON, THE RT ENVIRONMENTAL CONTROL CIRCUIT BREAKER AND THE RT ACM CONTROL CIRCUIT BREAKER OPENED AND WOULD NOT RESET. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT THE SYS
- [SDR IXXA100056O](https://openairdocs.org/sdr/IXXA100056O.md): Switch · shorted · Nov 23, 2010 · N799AL · Doug DC862F · Cabin Cooling System
  > FIFTEEN MINUTES INTO FLIGHT, BOTH AIR CYCLE MACHINES ON THE RT ENVIRONMENTAL CONTROL CIRCUIT BREAKER AND THE BATTERY DIRECT PACS OVERTEMP TRIPPED. NO CONTROL OF THE LOAD CONTROL VALVE WAS AVAILABLE. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT.
- [SDR IXXA100054O](https://openairdocs.org/sdr/IXXA100054O.md): Duct · disconnected · Oct 28, 2010 · N41CX · Doug DC862F · Pneumatic Distribution System
  > DURING CRUISE, NR 4 ENGINE GENERATOR UNPARALLEL LIGHT FOLLOWED BY GENERATOR DRIVE OIL LIGHT, MANIFOLD PRESSURE LIGHT ILLUMINATED WITH HIGH PRESSURE MANIFOLD AIR PRESSURE OVERTEMP LIGHT CAME ON, LOSS OF EGT INDICATION, ZERO FUEL FLOW AND ZERO EPR. THE CREW SHUT
- [SDR IXXA090072O](https://openairdocs.org/sdr/IXXA090072O.md): Engine · power loss · Dec 14, 2009 · N41CX · Doug DC862F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF FROM WSAP NR 4 ENG FAILED TO PRODUCE TAKEOFF PWR. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PERFORMED POWER RUN AND ACCELERATION CHECK. OPS CHECK GOOD IAW ERH 72.01.1. ACFT WAS RETURNED TO SERVICE.
- [SDR IXXA090068O](https://openairdocs.org/sdr/IXXA090068O.md): Prbc · dry · Nov 29, 2009 · N41CX · Doug DC862F · Turbine Engine Compressor Section
  > DURING CLIMB OUT, THE CREW HEARD A LOUD BANG, F/A REPORTED A FLASH ON LT SIDE. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH NR 1 AND NR 2 ENGINE'S, LUBED THE PRBC'S. OPS CHECK GOOD IAW MM 72-00, ERH 70.01, ERH 75.01, AND MM 12-80-0.
- [SDR IXXA090064O](https://openairdocs.org/sdr/IXXA090064O.md): Wire · burned · Oct 26, 2009 · N799AL · Doug DC862F · Engine Indicating System Wiring
  > DURING CLIMB OUT FROM TAPA NR 4 ENG EPR INOP, NR 4 GENERATOR CAUSED A MOMENTARY LOSS OF ALL POWER THEN LOCKED OUT-SHORTLY AFTER ZOLTS AND FREQUENCY WENT TO ZERO, AND NR 4 ENG BEGAN TO SPARK EVERY 25 SECONDS THE CREW SHUTDOWN NR 4 ENG. THEY RETURNED TO TAPA WI
- [SDR IXXA09SMN089S](https://openairdocs.org/sdr/IXXA09SMN089S.md): Skin · corroded · Aug 11, 2009 · N41CX · Doug DC862F · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSP FOUND RT WING L/E LWR SKIN CORRODED AT STA XFS 566.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION. FABRICATED DOUBLER, AND FILLER. CLEANED, TREATED, AND PRIMED AREA AN
- [SDR IXX2008F00092](https://openairdocs.org/sdr/IXX2008F00092.md): Fan · defective · Sep 3, 2008 · N799AL · Doug DC8* · Air Distribution Fan
  > AFTER LANDING, DURING TAXI IN THE CREW DETECTED AN ODOR OF SMOKE. THE CREW TURNED OFF RT RECIRCULATION FAN THE ODOR WENT AWAY. MAINT DEFERRED RT RECIRCULATION FAN. MAINT REPLACED RT RECIRCULATION FAN, OPS CHECK GOOD IAW MM 21-21-1. AC WAS RETURNED TO SERVICE.
- [SDR IXXA070031O](https://openairdocs.org/sdr/IXXA070031O.md): Clamp · broken · Jun 4, 2007 · N799AL · Doug DC862F · Ice/Rain Protection System
  > DURING CLIMB FROM KTOL NR 1 ENGINE ANTI-ICE LIGHT ILLUMINATED, OIL PRESSURE LIGHT FLICKERED, EGT DROPED TO 270°C, LOW PRESSURE PNEUMATIC CONTROL CIRCUIT BREAKER POPPED, ENGINE GENERATOR FAIL LIGHT ILLUMINATED WHILE VOLTS AND FREQUENIES WERE NORMAL. CLIMB POWER
- [SDR ABXA050307](https://openairdocs.org/sdr/ABXA050307.md): Web · corroded · Nov 9, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > CENTERLINE WEB AT STA 800 - 857, BUTT LINE O CORRODED. FABRICATED WEB AT STA 800 - 857, BUTT LINE 0 IAW REA D853-52543. MATERIAL USED.080 7075-T6, P/O NR 1113384.
- [SDR ABXA050303](https://openairdocs.org/sdr/ABXA050303.md): Web · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > WEB CORRODED AT STA 857, RT BUTT LINE 46. FABRICATED WEB AT STA 857, RT BUTT LINE 46 USING.071 7075-T6, P/O NR 1084025 IAW REA D853-52538.
- [SDR ABXA050304](https://openairdocs.org/sdr/ABXA050304.md): Attach Angle · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > RT PRESSURE PANEL AT STA 857, RT BUTT LINE 40 ATTACH ANGLE CORRODED. FABRICATED ATTACH ANGLE RT PRESSURE PANEL AT STA 857, P/N: 5644678 IAW REA D853-52534.
- [SDR ABXA050301](https://openairdocs.org/sdr/ABXA050301.md): Web · corroded · Nov 7, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > WEB CORRODED AT STA 857, LT BUTT LINE 46. FABRICATED WEB AT STA 857, LT BUTT LINE 46 USING.063 7075-T6, PO NR 1118787 IAW REA D853-52535.
- [SDR ABXA050294](https://openairdocs.org/sdr/ABXA050294.md): Finger Doubler · damaged · Nov 2, 2005 · N826AX · Doug DC863F · Fuselage Miscellaneous Structure
  > INSIDE CENTER TANK, STA 857, LT BUTT LINE 20, AFT FINGER TAB OF DOUBLER BROKEN OFF. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW REA D853-52530.
- [SDR ABXA050295](https://openairdocs.org/sdr/ABXA050295.md): Keelbeam · corroded · Oct 25, 2005 · N826AX · Doug DC863F · Fuselage Main, Keel
  > KEEL BEAM CORRODED AT AFT BULKHEAD OF MID ACCESSORY COMPARTMENT, STA 680, BUTT LINE 0, CORROSION APPEARED TO EXTEND UNDER WING CENTER SECTION. REMOVED CORROSION AT KEEL BEAM STA 620 FWD OF BULKHEAD AND UNDER BULKHEAD AS REQUIRED REF SRM 51-1-8, REF REA D853-
- [SDR ABXA050296](https://openairdocs.org/sdr/ABXA050296.md): Skin · corroded · Oct 20, 2005 · N826AX · Doug DC863F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, STA 1100 TO 1120 AT RT AFT BODY FAIRING, SKIN CORRODED. REMOVED CORROSION AND INSTALLED REPAIRS BETWEEN STA 1100 LONGERON 29 RT TO STA 1120 LONGERON 30 RT IAW REA D853-52518-MR AND SRM 51-1-8, PG 20.
- [SDR ARWA20050803](https://openairdocs.org/sdr/ARWA20050803.md): Link Assy · vibration · Aug 17, 2005 · N441J · Doug DC863F · Nose/Tail Landing Gear
  > AFTER TAKEOFF AND GEAR RETRACTION, EXPERIENCED CONTINUOUS VIBRATION AND NOISE FROM NOSE WHEEL WELL AREA. RETURNED AND LANDED TO INVESTIGATE. REMOVED AND REPLACED RT NOSE DOOR LINK ASSEMBLY IAW MM. PERFORMED ADJUSTMENT TEST SYSTEM IAW M/M. TEST GOOD.
- [SDR IXXA05RNG034S](https://openairdocs.org/sdr/IXXA05RNG034S.md): Support Fitting · cracked · Jul 21, 2005 · N71CX · Doug DC862F · Trailing Edge Flaps
  > DURING ROUTINE "C" CHECK, CRACK 0.5220" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 OUTBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-024 AND EO ATI-071005. FAA FORM 8110-3 WAS ISSUE
- [SDR IXXA05RNG031S](https://openairdocs.org/sdr/IXXA05RNG031S.md): Support Fitting · cracked · Jul 21, 2005 · N71CX · Doug DC862F · Wing, Attach Fittings
  > DURING ROUTINE "0C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF409.664 WAS FOUND CRACKED (LONG 1.570"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-021 & EO ATI-070705. FAA FORM 8110-3 WAS ISSUED APPRO
- [SDR IXXA05RNG038S](https://openairdocs.org/sdr/IXXA05RNG038S.md): Skin · corroded · Jul 19, 2005 · N71CX · Doug DC862F · Wing, Plate/Skin
  > DURING A "C" CHECK INSPECTION, FOUND SKIN CORROSION DAMAGE ON THE RIGHT OUTER WING AT THE INBOARD EXTENDED L/E STA XFS 653.750. RT WING L/E UPPER SKIN WAS REPAIRED IAW EWO ATI 57-030 AND EO ATI-071305. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.
- [SDR COOSDR040042](https://openairdocs.org/sdr/COOSDR040042.md): Longeron · corroded · Oct 11, 2004 · N41CX · Doug DC861F · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT AT Y STA 360.0, LONGERON 28R CORRODED.
- [SDR ABXA040264](https://openairdocs.org/sdr/ABXA040264.md): Longeron · cracked · Jul 12, 2004 · N812AX · Doug DC863 · Fuselage Main, Longeron/Stringer
  > LT MAIN LANDING GEAR WHEEL WELL LONGERON 24 CRACKED ON LOWER FLANGE AT BOTTLE BOLT CAVITY. REPAIRED AREA IAW REA D853-49163MR.
- [SDR ABXA040263](https://openairdocs.org/sdr/ABXA040263.md): Fitting · cracked · Jul 7, 2004 · N812AX · Doug DC863F · Fuselage Main, Attach Fittings
  > FITTING CRACKED AT MOST FORWARD FASTENER HOLES. FABRICATED REPAIR PARTS IAW REA D853-49975MR. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED IAW SRM 51-1-20B.
- [SDR UPS04842868](https://openairdocs.org/sdr/UPS04842868.md): Bracket · gouged · Jul 4, 2004 · N700UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE: C-3, B-PIT DOOR LINK HINGES ARE GOUGED/ WORN PORTION ON AIRFRAME (NOT DOOR). REMOVED 2 EACH EXISTING C2 DOOR LINK HINGE FITTINGS. RECEIVED NEW FITTING 2 EACH PN 4654281. LOCATED AND DRILLED TRANSFER HOLES FOR NEW HINGE FITTINGS IAW SRM 51-1-2
- [SDR UPS04842869](https://openairdocs.org/sdr/UPS04842869.md): Door Frame · cracked · Jul 2, 2004 · N700UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE: C3 B- PIT DOOR FRAME AFT SIDE CRACKED DOT NR Y52Y. MAT ID 2024-0.071 PO 4255761 IAW SRM 52-2-0 AND 52-4-1. RECEIVED MATERIAL USED FOR REPAIR DOUBLER FROM HEAT TREAT. HEAT TREATED FROM 2024-T4 IAW TPS 1003 REV A. FABRICATED REPAIR DOUBLER I
- [SDR COOSDR040009](https://openairdocs.org/sdr/COOSDR040009.md): Panel · corroded · Jun 30, 2004 · N41CX · Doug DC862F · Horizontal Stabilizer, Plate/Skin
  > EMPENNAGE RT STAB LOWER SECTION STRINGER NR 4 WITH CRACK AT XFS 47 AND CORROSION AT XFS 45.
- [SDR ARWA20040603](https://openairdocs.org/sdr/ARWA20040603.md): Amplifier · failed · Jun 21, 2004 · N661AV · Doug DC863F · Attitude and Direction Data System
  > LOG PAGE NR 107128. CAPTAIN'S HEADING FLAG DISPLAYED INTERMITTENTLY; RETURNED TO RAMP. REMOVED AND REPLACED INSTRUMENT AMP IAW M/M 34-21-0; HORIZON SYSTEM OPERATIONAL NORMAL IAW M/M 34-25-0.
- [SDR ARWA20040506](https://openairdocs.org/sdr/ARWA20040506.md): Gyro · faulty · May 21, 2004 · N810BN · Doug DC862 · Directional Gyro and Indicating System
  > CAPTAIN'S COMPASS FAILED IN FLIGHT. REMOVED AND REPLACED CAPTAIN'S PICTORIAL DEVIATION INDICATOR (PDI) AND DIRECTIONAL GYRO (DG) IAW MM 31-10-1 AND MM 34-21-1. SWAPPED INSTRUMENT AMPS IAW 34-00. SYSTEM GROUND TEST NORMAL IAW 34-21-0, 34-52-0 AND 34-28-0.
- [SDR ARWA20040507](https://openairdocs.org/sdr/ARWA20040507.md): Actuator · malfunctioned · May 21, 2004 · N810BN · Doug DC862 · Fuel Dump System
  > UNABLE TO EXTEND FUEL DUMP CHUTES ELECTRICALLY, MOTOR STOPPED APPROXIMATELY 3300 FULL EXTENDED. TRANSFERRED TO DMI NR 18536 CATEGORY (C) IAW MEL 28-9-1. INSTALLED CAT (C) PLACARD; PENDING CLOSING OF DMI. PERFORMED OPERATIONAL CHECK OF FUEL DUMP CHUTE ELECT M
- [SDR IXXA0300070O](https://openairdocs.org/sdr/IXXA0300070O.md): Bearing · lack of lube · Oct 29, 2003 · N728PL · Doug DC862 · Pressure Regulator/Outflow Valve
  > DURING CLIMB FROM FJDG CREW LOST CABIN PRESSURIZATION. CREW RETURNED TO FJDG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED OUTFLOW VALVE. THEY LUBED MECHANICAL ARMS AND BEARINGS. OPERATIONAL CHECK GOOD BOTH IN AUTO AND MANUAL PER ALL APPLICABLE MANUALS. T
- [SDR U2R2004F00001](https://openairdocs.org/sdr/U2R2004F00001.md): Fastener · mismanufactured · Oct 29, 2003 · N921R · Doug DC863F · Fasteners
  > REPAIRED L2 DOOR AT LOWER FORWARD CORNER FS1620 IAW MM.
- [SDR ABXA030392](https://openairdocs.org/sdr/ABXA030392.md): Switch · dirty · Oct 14, 2003 · N819AX · Doug DC863F · Landing Gear Position and Warning
  > DURING DESCENT, LANDING GEAR WAS EXTENDED TO FACILITATE DESCENT. WHEN GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT ILLUMINATED. LANDING GEAR AND DOOR LATCHING "NOT LATCHED" LIGHT ILLUMINATED WITH SELECTOR IN LEFT DOOR POSITION. PERFORMED ABNORMAL PROCEDURE. W
- [SDR ARWA20030603](https://openairdocs.org/sdr/ARWA20030603.md): Engine · failed · Jun 11, 2003 · N8969U · Doug DC862 · Engine (Turbine/Turboprop)
  > PRECAUTIONARY SHUTDOWN NR 2 ENGINE; TIME 0030. OIL PRESSURE -0 OIL TEMP 145. ENGINE WINDMILLED 3 1/2 HOURS, ZERO OIL PRESSURE. ALL ABNORMAL PROCEDURES FOLLOWED. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARDS 72-000-30-02-01, 77-000-00-03-1 & 77-000-02-1; A
- [SDR ARWA20030505](https://openairdocs.org/sdr/ARWA20030505.md): Clip · cracked · May 27, 2003 · N784AL · Doug DC863F · Fuselage Miscellaneous Structure
  > NR 194. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND;FORWARD LOWER CARGO COMPARTMENT STATION 300, BETWEEN L-33R & L-34R FITTING WITH CRACK. REMOVED AND REPLACED FITTING ON FOWARD LOWER CARGO COMPARTMENT STA.300 BETWEEN L-33R & L-34R IAW WITH SRM 51-
- [SDR ARWA20030507](https://openairdocs.org/sdr/ARWA20030507.md): Angle · cracked · May 27, 2003 · N784AL · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT AFT DOOR SUPPORT ANGLE WITH CRACK; STATION 1420. REMOVED ANGLE IAW DPS 3.67-27, FABRICATED NEW ANGLE IAW DPS 3.69-4, PRIMED NEW ANGLE IAW DC8 SRM 51- 1-8 AND INSTALLED ANGLE AIW D
- [SDR ARWA20030508](https://openairdocs.org/sdr/ARWA20030508.md): Fitting · cracked · May 27, 2003 · N784AL · Doug DC863F · Fuselage Main, Longeron/Stringer
  > N/R 421. DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR WHEEL WELL STATION 879, L-24R FITTING WITH CORROSION AND 3 INCH CRACK. REMOVED AND REPLACED FITTING OF R/H MAIN LANDING GEAR WHEEL WELL STA 879, L-24R IAW SRM 51-1-20D AND SR
- [SDR ARWA20030509](https://openairdocs.org/sdr/ARWA20030509.md): Doubler · corroded · May 27, 2003 · N784AL · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT STATION 1620, BETWEEN L-26R AND L-31R INNER SKIN WITH SEVERAL SPOTS OF CORROSION. REPAIRED FUSELAGE INNER DOUBLER AT FS 1620, BETWEEN L-25R AND L-31R IAW MFG ENGINEERING REPAIR O
- [SDR ABXA020369](https://openairdocs.org/sdr/ABXA020369.md): Engine · malfunctioned · Dec 19, 2002 · N848AX · Doug DC861 · Engine (Turbine/Turboprop)
  > DURING CLIMB, LOW OIL PRESSURE LIGHT CAME ON. OIL PRESSURE FLUX AT 35 PSI. OIL QUANTITY DROPPED TO (0), ENGINE SHUTDOWN AT 0405Z, N1 24 PERCENT, N2 33 PERCENT, PRESS 5 PSI, TEMP 125 DEGREES C TOD PRESS 5, TEMP 84, N1 26 PERCENT, N2 36 PERCENT, TIME 0500Z. REMO
- [SDR ARWA20021203](https://openairdocs.org/sdr/ARWA20021203.md): Hose · damaged · Dec 11, 2002 · N802BN · Doug DC862 · Hydraulic System, Main
  > LOST HYDRAULIC QUANTITY TOP OF DESCEND FOLLOWED BY ABNORMAL CHECKLIST AND PROCEDURES. CORRECTIVE ACTION: FOUND HYDRAULIC HOSE FROM PUMP ENGINE NR 2 DAMAGE. REMOVED AND REPLACED HOSE IAW MM, OPERATIONS CHECK OK IAW MM.
- [SDR ABXA020347](https://openairdocs.org/sdr/ABXA020347.md): Control Arm · defective · Dec 6, 2002 · N825AX · Doug DC863 · Landing Gear Position and Warning
  > WITH GEAR HANDLE DOWN, GREEN LIGHTS NOT ON, RED LIGHTS NOT ON EITHER. ACCOMPLISHED ABNORMAL PROCEDURE, STILL NO LIGHTS. OTHER CHECKLIST ITEMS INDICATED ALL GEAR WAS DOWN AND LOCKED. FOUND GEAR WARNING INTERLOCK CIRCUIT BREAKER INTERMITTENT (D-3). REPLACED CIRC
- [SDR ABXA020346](https://openairdocs.org/sdr/ABXA020346.md): Warning Light · illuminated · Dec 4, 2002 · N818AX · Doug DC863 · Landing Gear Position and Warning
  > NOSE GEAR FAILED UPLATCH GEAR UNSAFE LIGHT ON WITH GEAR RETRACTED. FOUND NOSE GEAR PIN INSTALLED WHEN AIRCRAFT TAXIED IN. INSPECTED NOSE GEAR AND CABLES FOR SAFETY OF FLIGHT INSPECTION. NO DEFECTS FOUND. AIRCRAFT OK FOR FLIGHT.
- [SDR ARWA20021108](https://openairdocs.org/sdr/ARWA20021108.md): Cylinder · inoperative · Nov 20, 2002 · N802BN · Doug DC862 · Landing Gear Retraction/Extension System
  > IN FLIGHT, AFTER NORMAL GEAR RETRACTION, RED GEAR LIGHT ON AFTER UP LATCH CHECK. FOLLOWED ABNORMAL CHECKLIST. REMOVED AND REPLACED LEFT GEAR UP LATCH CYLINDER IAW MM, REMOVED AND REPLACED LEFT GEAR ACTUATING CYLINDER IAW MM. PERFORMED CHECK, NO LEAK, GOOD.
- [SDR ARWA20021106](https://openairdocs.org/sdr/ARWA20021106.md): Engine · failed · Nov 14, 2002 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)
  > AT 2130Z, NR 2 OIL QUANTITY RAPIDLY DROPPED TO 1 GALLON, SUBSEQUENTLY OIL PRESSURE DROPPED TO 5 PSI AND OIL PRESSURE LOW LIGHT ILLUMINATED. PERFORMED IN FLIGHT ENGINE SHUTDOWN PROCEDURE IAW ABNORMAL CHECKLIST, WINDMILLING OIL PRESSURE. REMAINED AT 5 PSI. INS
- [SDR ASAA0280479](https://openairdocs.org/sdr/ASAA0280479.md): Lanyard · disconnected · Oct 29, 2002 · N974AS · Doug DC983 · Escape Slide
  > DURING PREFLIGHT CHECK LANYARD BETWEEN GIRT BAR AND SLIDE COVER WAS FOUND DISCONNECTED. REATTACHED LANYARD.
- [SDR ABXA030222](https://openairdocs.org/sdr/ABXA030222.md): Structure · corroded · Aug 6, 2002 · N816AX · Doug DC863F · Leading Edge Devices
  > LT WING LEADING EDGE UPPER SECTION APPROXIMATELY, STA. XFS 126.250, CORROSION AROUND FASTENERS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED IAW REA D857-43958MR.
- [SDR ABXA030219](https://openairdocs.org/sdr/ABXA030219.md): Doubler · cracked · Jul 22, 2002 · N816AX · Doug DC863F · Cargo/Baggage Doors
  > FORWARD LOWER CARGO C1 DOOR, FUSELAGE INNER DOUBLER WAS CRACKED AT FUSELAGE STA. 320, OUTER EDGE AND HAD AN IMPROPER REPAIR. CUT OUT DAMAGED SECTION OF DOUBLER, FABRICATED FILLER, REPAIR DOUBLER SPLICES, AND INSTALLED ALL REPAIRS PARTS IAW DC-8 SRM 51-1-20D, D
- [SDR ABXA030229](https://openairdocs.org/sdr/ABXA030229.md): Longeron · corroded · Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/Stringer
  > REMOVE AND REPLACE LONGERON 32 LEFT INBOARD CHANNEL STA. 190 - 385. REMOVED CORRODED SECTION, FABRICATED LONGERON AND SPLICES. INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-2, AND 51-1-8.
- [SDR ABXA030225](https://openairdocs.org/sdr/ABXA030225.md): Door Frame · corroded · Jul 17, 2002 · N816AX · Doug DC863F · Fuselage Main, Structure
  > AFT CARGO, BS 1220, FUSELAGE FRAME CORRODED JUST INBOARD OF SLIDING DOOR, LOWER AFT CUTOUT. REPLACED DOOR FRAME ZEE FITTING, FABRICATED REPAIR SPLICE ANGLES AND FILLERS. INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-3-0.

Next page: https://openairdocs.org/engine/pratt-whitney-jt3d-series/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 = 'JT3D'
ORDER BY difficulty_date DESC
```

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

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