Attachment_J-08_Aircraft_Specifications.pdf

ATTACHMENT J-08

AIRCRAFT SPECIFICATIONS

HELICOPTER AND MISSION SUMMARY:

a. Registered owner: b. Flag

c. Year built:

d. Tail number (N-number) e. Call letters

f. Aircraft Make/Model/Series: g. Landing Gear Type (Wheel or Skids):

h. Color Scheme:

External Dimensions:

i. Main Rotor diameter: j. Tail Rotor Diameter:

k. Length Overall (Rotors turning): I. Length Overall (Fuselage):

m. Height Overall (Highest Point): n. Width Overall (Airframe):

o. Length Folded or Hangared (If applicable and different from box, l, above):

Internal Dimensions: (Shall exclude cockpit or other non-useable cargo/PAX areas)

q. Cabin Length (Maximum): r. Cabin width (Maximum):

s. Cabin height (Minimum): t. Useable Cargo Capacity (ft3):

u. Offered Internal Cargo Capacity(ft3): v. Offered Medical Litter Capability:

w. Cargo Loading Port Measurements (Width and Height): x. Maximum Passenger Capability:

y. Offered Passenger Capability: z. Maximum Medical Litter Capability:

Weight:

aa. Maximum Gross Weight: ab. Maximum Take-off Weight:

ac. Maximum Internal Cargo Weight: ad. Maximum External Load Weight:

ae. Offered Internal Cargo Weight:

af. Cargo Hook Capacity (Safe Working Load): ag. Cargo Hook Capacity (Maximum):

Propulsion:

ah. Engine Manufacturer: ai. Engine Type:

aj. Number of Engines:

ak. Manufacturer's Mean Time Between Engine Failures:

(Mechanical Failure Statistics):

ATTACHMENT J-08

AIRCRAFT SPECIFICATIONS

Fuel:

Yes No

al. Can Use JP-5:

am. Can Use NATO F-44: Yes No

an. Can Hot Refuel Using Approved Close-Circuit System:

Performance: (At 32 deg OAT; Sea Level; Max Standard Fuel with no reserves, unless otherwise noted; and Aircraft configured and equipped for overwater missions.)

ao. Maximum Range (NM): ap. Maximum Endurance non-VERTREP (minutes):

aq. Maximum Endurance VERTREP (Minutes):

ar. Maximum VERTREP Load (90 minutes fuel): as. Maximum VERTREP Load (10% Fuel):

at. Maximum VERTREP Load (20 minutes mission Fuel):

Aircraft Certification:

au. IFR Certification Date: av. Airworthiness Certificate Date:

Aircraft Physical Particulars/Specification, per Section-C4.0:

Yes No To be Installed Citation in offer

av. External Loads can be visually monitored:

aw. Mechanical Rotor Brake:

ax. Blade Fold System:

ay. Aircraft can be Secured to deck:

az. Working Wheel Brakes:

ba. Flight Time (Hobbs) Meter:

bb. Cockpit Heater:

bc. Window Defogging System:

bd. Windshield Wipers:

be. Transmission Chip Detector:

bf. Fixed ELT:

bg. Transceiver(s) Meeting Section C4.5.15:

bh. GPS With Fixed Antenna:

bi. TACAN System:

bj. VOR/LOC Receiver:

bk. ICS:

bl. Radar Altimeter:

bm. Underwater Acoustic Beacon:

bn. Air Traffic Control Transponder and Altitude Reporting System:

bo. ATC Transponder is Mode IV Capable:

Aircraft Primary Mission Compatibility, per Section C-2.7.2:

Aircraft is offered to provide the following services (Check those that apply):

Yes No Citation in offer bp.Day/Night and VFR/IFR Vertical Replenishment Services:

bq. Visual Search and Rescue:

br. Personnel Recovery System:

br. Internal Cargo

br. Internal Passengers