MODUK - DEF STAN 00-970: PT 7: SEC 2: SUPP 5
Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Supplement 5: Powerplant (Subpart E)
| Organization: | MODUK |
| Publication Date: | 30 January 2015 |
| Status: | inactive |
| Page Count: | 223 |
scope:
INTRODUCTION
This leaflet contains recommendations for the design of facilities for open-orifice, gravity filling of tanks in amplification of Leaflet 701.
Although open-orifice refuelling is principally featured on small rotorcraft with relatively simple fuel systems, gravity-filling can provide a readily available safe back-up refuelling method for rotorcraft equipped with a closed circuit pressure refuelling system.
Access into fuel tanks through standard filler orifices also facilitates defuelling by means of a suction defuelling tube inserted into the tank. This feature of the rotorcraft can prove useful in the case of salvage activity, following a crash landing, when access to the normal suction defuelling connector and tank drains may not be possible.
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