
The Lockheed WP-3D Orion (P-3) is a highly instrumented aircraft made to sustain large amounts of damage and fly through adverse conditions. The Aircraft Operations Center has two P-3’s. The primary goal of the P-3 during hurricane season is to penetrate into the eye while dropping dropwindsondes in order to get data to Hurricane Research Division. An average hurricane reconnaissance mission lasts about 9-10 hours.
Since the P-3’s are equipped to take atmospheric measurements
they participate in a number of projects, from hurricane reconnaissance
to ocean wind experiments and bow echo research, the P-3 is made to do
just about any kind of weather research all over the world.
A few past projects that the P-3 participated in are explained below:
- BAMEX: Bow Echo and Mesoscale Convective Vortices Experiment in 2003.
BAMEX, which was conducted in the Midwest, was dedicated to bow echo
evolution experimentation.
- SALLJEX: South American Low-Level Jet Experiment in late 2002 through
2003. SALLJEX was conducted over northern Argentina and western
Paraguay. The primary goal was to improve short and long term
forecasting.
- WSR: Winter Storm Reconnaissance Program in 2008. The P-3
took over for the GIV in 2008 during the annual NCEP winter storm
missions.
- Ocean Winds: The P-3’s work with NESDIS to verify their satellites
accuracy.
-TEXAQS: Texas Air Quality Study in 2006.
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Type Engines: |
4 Allison T56-14 Turbo Prop Engines |
|
Crew: |
2 Pilots, Flight Engineer, Navigator, 1 Flight Director (flight meteorologist), 1 ASPEN Director (flight meteorologist), 2 or 3 Engineering/Electronic specialists, Radio/Avionics specialist, and a up to 12 Scientist or Media personnel. |
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Max. Takeoff Weight: |
135,000 lbs. |
|
Ceiling: |
27,000' |
|
Rate of Climb: |
Up to 3000 FPM depending on aircraft gross weight and density altitude |
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Operational Airspeeds: |
170 - 250 KIAS |
|
Electrical: |
4 Generators (3 are engine driven, 1 Auxiliary Power
Unit) |
|
Max. Gross Weight: |
135,000 lbs max takeoff weight |
|
Empty Weight: |
Approximately 73,000 lbs depending on scientific gear installed |
|
Maximum zero Fuel weight: |
Approximately 77,000 lbs. |
|
Useful Load: |
Approximately 62,000 lbs |
|
Fuel Load: |
58,000 lbs. |
|
Type Fuel: |
JP4, JP5, JP8, JET A, JET A-1, JET B |
|
Standard Fuel Burn: |
4500 - 6000 lbs/hr depending on altitude and airspeed |
|
Maximum Range and Duration: |
LOW ALTITUDE - 2500 NM OR 9.5 HRS |
|
Dimensions (external): |
Wingspan = 99 ' 8" |
|
Additional Standard Equipment (Cockpit): |
Skywatch Collision Avoidance System (TCAS) |
|
Skywatch Collision Avoidance System (TCAS): |
An airborne traffic advisory system that assists the flight crew in visual acquisition of aircraft that may pose a collision threat. |
|
Altitude Alert System: |
System that provides flight crew with visual and audio warnings about a variety of flight conditions regarding the altitude of the aircraft. |
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Radars: |
Rockwell Collins C-band nose radar |
|
Cloud Physics: |
PMS 2-dimensional and 1-dimensional precipitation and
cloud particle probes |
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Radiation: |
Sea surface temperature radiometer |
|
Expendables: |
GPS dropwindsonde atmospheric profiling system |
|
Miscellaneous: |
C-band and Ku-band scatterometers |

Nose art from the WP-3Ds, N43RF and N42RF
© The Jim Henson Company