What it is
AAEP-02, the Allied Aircraft Electric and Electromagnetic Considerations Publication on static grounding, standardises the electrical connections used to ground aircraft and ground support equipment (GSE) against static electricity. It sets a common connector interface, a marking convention, and a procedure for when and how connections are made, so that static charges are dissipated safely before fuelling, weapons loading and other servicing work. It is covered by STANAG 3632, the NATO agreement through which member nations commit to implement it: AAEP-02 does not bind on its own, and it names STANAG 3632's own custodian as the route for proposing changes to its content (clause 1.3).
The connector interface
Every static grounding point carries a maximum electrical resistance, a distinctive marking, and a mechanical connection point (clause 2.1.1). Two connector types are recognised: a latching-type plug built to the document's own Annex B, mated to a receptacle built to ISO 46, or, where an aircraft carries no receptacle, a heavy-duty electrical clip fitted to a conductive part of the airframe (clause 2.1.3). The receptacle itself is bonded to the airframe and marked under two further NATO publications, and positioned so the fuel nozzle can be bonded to the aircraft during refuelling (clause 2.1.4). The document is direct about why the two connector types both matter: a nation has to keep both available, or suitable adapters, for visiting allied aircraft. That is the interoperability this document exists to deliver, and it is also the first thing a supervisor checking readiness for allied traffic would look for.
The grounding procedure
Chapter 2 sets the sequence and the method. The ground connection is always made before the aircraft connection, and where GSE is involved, the GSE is grounded before the aircraft's own cable is connected (clause 2.2.1). Which of three methods applies depends on the task: single-point grounding (aircraft to earth) for a parked aircraft, maintenance without GSE, or weapons loading; dual-point grounding (aircraft to earth and GSE to earth) where GSE is used but nothing highly flammable or combustible is involved; and three-point grounding (aircraft to earth, GSE to earth, and GSE to aircraft) where the GSE in use involves a flammable or combustible liquid or gas, such as oxygen, alcohol or LOX (clause 2.2.2). That choice, not the hardware, is what a ground crew supervisor actually has to get right on a given day.
What it leaves to other publications
AAEP-02 is explicit about its own boundary: protection against power faults in electrical equipment is not covered here, and sits in STANAG 3682 instead (clause 1.2). Aircraft servicing marking more broadly is STANAG 3109's subject, ground electrical power supplies are STANAG 3457's, and pressure refuelling connections are STANAG 3105's; AAEP-02 names all three as related reading rather than folding them in. Annex A is worth knowing about for a different reason: it shows that while the connector interface is common, how a nation marks its own grounding points is not; one nation marks a concrete block, another does not mark its points at all. Annex B carries the exact plug and receptacle dimensions a manufacturer would build to, which is the level of detail this page does not reproduce.