STANAG 3105Eed06

STANAG 3105Eed06, STANAGi

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NORTH ATLANTIC TREATY ORGANIZATION
ORGANISATION DU TRAITE DE L’ATLANTIQUE NORD
MILITARY AGENCY FOR STANDARDIZATION (MAS)
BUREAU MILITAIRE DE STANDARDISATION (BMS)
1110 BRUSSELS
Tel : 707.55.89
Fax : 707.57.18
masair@hq.nato.int
AIR BOARD
7 October 1998
MAS(AIR)234-ASSE/3105
See Distribution List Air N° 10
STANAG 3105 ASSE (EDITION 6) - PRESSURE REFUELLING CONNECTIONS
AND DEFUELLING FOR AIRCRAFT
References
:
a.
MAS(AIR)526-ASSE/3105 dated 23 October 1997 (Edition 6)
(Ratification Draft 1)
b.
MAS(AIR)338-ASP/3105 dated 18 September 1995 (Edition 5)
1. The enclosed NATO Standardization Agreement which has been ratified by
nations as reflected in page iii is promulgated herewith.
2. The references listed above are to be destroyed in accordance with local
document destruction procedures.
3.
AAP-4 should be amended to reflect the latest status of the STANAG.
ACTION BY NATIONAL STAFFS
4. National staffs are requested to examine page iii of the STANAG and, if they
have not already done so, advise the Air Board, MAS through their national delegation
as appropriate of their intention regarding its ratification and implementation.
A. GRØNHEIM
Major General, NOAF
Chairman MAS
Enclosure
:
STANAG 3105 (Edition 6)
- 1 -
FB/3105E
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 NATO UNCLASSIFIED
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STANAG No. 3105
(Edition 6)
NORTH ATLANTIC TREATY ORGANIZATION
(NATO)
MILITARY AGENCY FOR STANDARDIZATION
(MAS)
STANDARDIZATION AGREEMENT
(STANAG)
SUBJECT:
PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR
AIRCRAFT
Promulgated on 7 October 1998
A. GRØNHEIM
Major General, NOAF
Chairman, MAS
NATO UNCLASSIFIED
NATO/PfP ONLY
 NATO UNCLASSIFIED
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RECORD OF AMENDMENTS
No.
Reference/date of
amendment
Date
entered
Signature
EXPLANATORY NOTES
AGREEMENT
1. This NATO Standardization Agreement (STANAG) is promulgated by the Chairman
MAS under the authority vested in him by the NATO Military Committee.
2. No departure may be made from the agreement without consultation with the tasking
authority. Nations may propose changes at any time to the tasking authority where they will be
processed in the same manner as the original agreement.
3. Ratifying nations have agreed that national orders, manuals and instructions
implementing this STANAG will include a reference to the STANAG number for purposes of
identification.
DEFINITIONS
4.
Ratification
is "In NATO Standardization, the fulfilment by which a member nation
formally accepts, with or without reservation, the content of a Standardization Agreement"
(AAP-6).
5. Implementation is "In NATO Standardization, the fulfilment by a member nation of its
obligations as specified in a Standardization Agreement" (AAP-6).
6.
Reservation
is "In NATO Standardization, the stated qualification by a member nation
that describes the part of a Standardization Agreement that it will not implement or will
implement only with limitations" (AAP-6).
RATIFICATION, IMPLEMENTATION AND RESERVATIONS
7. Page iii gives the details of ratification and implementation of this agreement. If no
details are shown it signifies that the nation has not yet notified the tasking authority of its
intentions. Page iv (and subsequent) gives details of reservations and proprietary rights that
have been stated.
FEEDBACK
8. Any comments concerning this publication should be directed to NATO/MAS -
Bvd Leopold III - 1110 Brussels - BE.
ii
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 NATO UNCLASSIFIED
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STANAG 3105
Agreed English/French Texts
(Edition 6)
NAVY/ARMY/AIR
NATO STANDARDIZATION AGREEMENT
(STANAG)
PRESSURE REFUELLING CONNECTIONS AND DEFUELLING FOR AIRCRAFT
Related Documents: ISO 45
- AIRCRAFT PRESSURE
REFUELLING CONNECTIONS
STANAG 3632 AE
- AIRCRAFT AND GROUND
SUPPORT EQUIPMENT
ELECTRICAL CONNECTIONS FOR
STATIC GROUNDING
STANAG 3681 ILCEP
- CRITERIA FOR PRESSURE
FUELLING/DEFUELLING OF
AIRCRAFT
STANAG 3682 ILCEP
- ELECTROSTATIC SAFETY
CONNECTION PROCEDURES FOR
AVIATION FUEL HANDLING AND
LIQUID FUEL LOADING/
UNLOADING OPERATIONS
DURING GROUND TRANSFER
AND AIRCRAFT
FUELLING/DEFUELLING
AIM
1. The aim of this agreement is to standardize the aircraft pressure refuelling
connections, to facilitate cross-servicing and to ensure the provision of a selective
aircraft defuelling capability and to establish standard practices which will facilitate
the completion of defuelling operations.
AGREEMENT
2.
Participating nations agree that:
- 1 -
FB/3105E
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 NATO UNCLASSIFIED
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a.
Aircraft Pressure Refuelling Connections
(1)
Pressure refuelling connections, fitted to aircraft, shall conform
to the dimensions specified in ISO 45 and be capable of
accepting not less than 682 Litres (150 Imperial Gallons or 180
US Gallons) of fuel per minute.
(2)
Aircraft shall incorporate an alternative refuelling capability at
least in each main tank for back-up in case the pressure
refuelling adaptor is damaged.
(3)
For those aircraft that require performance of multiple servicing
functions, whilst the aircraft is being refuelled, the pressure
refuelling adaptor shall be located such that the operations can
occur simultaneously. As a design objective, ground support
elevating devices shall not be required to facilitate the
connection of a refuelling nozzle.
(4)
Refuelling controls and quantity gauges, if required, shall be
located adjacent to the pressure refuelling adaptor to facilitate
the operation of the refuelling nozzle and the refuelling controls.
(5)
For those aircraft having the requirement to refuel with engine(s)
operating, the location of the pressure refuelling adaptor and
controls shall be such as to preclude any hazard to
refuelling/maintenance personnel.
b.
Defuelling of Aircraft
(1)
Provision will be made for selective defuelling, through the
aircraft refuelling connection or where it is not possible by
suction through accessible apertures.
(2)
Where practicable, in the case of a wheels-up landing,
defuelling can be accomplished through the connection normally
used for refuelling or by suction through accessible apertures.
(3)
The maximum rate of defuelling can be achieved with the
normal safety precautions required for refuelling.
(4)
It will be possible to defuel each aircraft tank with any single
failure in the aircraft fuel system.
(5)
System design will preclude negative pressures in flexible tanks
that are sufficient to cause collapse of the fuel tanks.
IMPLEMENTATION OF AGREEMENT
- 2 -
FB/3105E
NATO UNCLASSIFIED
NATO/PfP ONLY
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