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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)

inactive
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.

Document History

Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Supplement 5: Powerplant (Subpart E)
A description is not available for this item.
DEF STAN 00-970: PT 7: SEC 2: SUPP 5
January 30, 2015
Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Supplement 5: Powerplant (Subpart E)
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...

References

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