HIFR Flashcards
HIFR should be initiated
With sufficient fuel remaining to bingo to a suitable landing site if unsuccessful
Wiggins/NI HIFR Rig
Ships hose - 100ft
HIFR assembly - 10 ft section with female CCR (closed circuit refueling) fittings (wiggins fittings) that connects to hose and male wiggins in helo
Manual emergency disconnect lanyard
NATO - compatible high capacity NHC HIFR rig
2 in lightweight hose Unisex couplings Automatic emergency breakaway Built in 45 psi pressure regulator and on/off control handle Emergency breakaway 450+/-50 lbs
What type of nozzle is required for a NATO ship
If a U.S. Helicopter performs HIFR with a NATO ship, it will be given. Parker nozzle. An adapter to convert the nozzle to a wiggins type connection will be required
Winds for HIFR
Relative winds 10-30 knots, 300-360, minimum pitch and roll
Wiggins/NI fitting can be installed backwards, so
ensure the emergency release t handle is located near the wiggins fitting that attaches to the aircraft fitting.
Aircraft would be forced to shear the hoist to effect an emergency breakaway
A low hover while wind is less than 10 knots may cause
Excessive salt spray which can decrease engine performance and reduce pilot field of view
When using the NHC assembly, the hose shall be
Secured to the deck to ensure proper functionality of breakaway system
Ensure HIFR fitting assembly is —– before connecting the hose to the refueling fitting
Grounded
The PIC shall ensure the _______ is completed prior to commencing approach, HIFR, transfer, etc
Landing checklist
Low fuel flow may be the result of
Low pressure from the ships pump
Aircraft altitude
Contamination in the HIFR filter canister
During HIFR, if the right cell fills faster than the left cell
Monitor fuel quantity gauges closely. If the difference in cell quantities persist, stop refueling before the right cell is full (approximately 1700 lbs) to prevent rupture of fuel cell
Flow of fuel when precheck valve is in precheck position indicates a shutoff system malfunction. If neither precheck switch will secure the fuel flow…
Fueling should be continued only if necessary
The HIFR fuses in the GO/no go canister should be capable of handling approximately _____ lbs. The actual capacity of the fuses depends on ________. The HIFR filter _____ be replaced after each flight involving in flight refueling.
10,000
The quality of fuel received
Should
The go no go canister is sensitive to both
Water and particulate matter