Unification of Military and Civil
Aircraft Certification Procedures
Airworthiness and Type
Certification
‘Airworthiness’ is defined as the demonstrated
capability of an aircraft to satisfactorily fulfill the mission requirements
with acceptable level of safety and reliability. Airworthiness does not
guarantee an ‘absolute safety’
rather an ‘acceptable level’ of
safety which is decided as mutually agreed among designer, manufacturer and
the user on one side and the state or regulator on the other side. The foundation
for this is the acceptability from safety consideration on one hand and the
practicability form the point of technical feasibility and cost of compliance
towards design and manufacture. The ‘Type Certification’ on the other hand is a legal declaration by a
competent authority that the product has been designed, developed, evaluated
and productionised in such a manner that its quality, reliability and integrity
meets or exceeds the specified requirements.
Flight Safety and Risk Threshold
‘Safety’ of any flight would depend
primarily upon, whether we are operating below or above the ‘Risk Threshold’. The basic tenet of flight safety is
to ensure that the chances of achieving the tasks should be optimal while risks
are minimal. The ‘flight safety
directorate’ is to ensure that in peace time high level of risks is avoided.
This is because the accidents have very
deleterious effects on the morale of the flier. During the war time, however,
task achievement is paramount and high degree of risk may have to be taken. Safety
levels are quantified as ‘Casualties per
Ton Kilometer of transportation (CTK)’ for civil aircraft while for
military aircraft; it is ‘Accidents Rate’
per 10,000 hours of flight.
Military and Civil Aircraft
Design Procedures
While, commercial aircraft has a single mission of safe
and comfortable ferrying of passenger and cargo, the military aircraft have to
perform far more varied and different missions with each requiring different
design requirements to be satisfied. Further, commercial aircraft uses only proven technologies, military aircraft
design, to get an edge over the contemporaries, exploits latest but not fully
qualified ‘developments in technologies’.
The new technologies also get certified
along with the military aircraft certification. An aircraft design is a ‘trade off’ amongst diversified
requirements. The ‘trade off criteria’
is different for commercial and military aircraft. For example: while
performance and stealth are high priority for combat fleet, flying qualities and
safety is most desirable for commercial aircraft.
To maintain international safety of air
transportation, ICAO has imposed
that every member country should have a Civil
Aviation Authority (CAA) empowered
by the statutory rules of the country to impose regulations to maintain air
safety. Certification is to be accorded by these CAAs only (for example: FAA (in USA) and EASA (European
countries)) on compliance to the regulations. The military aircraft being ‘state owned’ undergoes government ‘self certification’ as per Mil–Std 516B (USA), JAP-100 (UK), DDPMAS
-2002 (India).
System Safety: Military and Civil
Aircraft
System safety of military aircraft
design is as per Mil-Std-882 while
for civil aircraft FAR 25.1309 and SAE-ARP
4761 are followed. Mil 882 uses improbable (<10-7) and ARP 4761
considers extremely remote (< 10-9) as the limiting values. This
is because military aircraft design accepts a higher risk for mission
accomplishment. However both the designs follow the basic tenet of airworthiness, i.e. there should exist an inverse relation
between the probability of occurrence of an event and the degree of hazard
inherent in its effect.
Inter-Operability
of Civil and Military aircraft in the International/National Air Space
The commercial aircraft need to comply with ICAO
requirements of communication,
navigation and surveillance (CNS) and
Air Traffic Management (ATM). The latest ICAO decision mandated use of GNSS (Global Navigation Satellite
System) and ADS-B (Automatic
Dependence Surveillance Broadcast). With airspace becoming congested, dedicated
airspace for military operation has become an issue. Therefore, optimum
utilization of airspace has become essential. Further, when military aircraft flies
in the national air space, it would share the airspace with national and
international traffic, therefore, the military aircraft also is required to comply with the same
requirement of CNS, ATM and TCAS. Thus for the interoperability of the two
aircraft a common frame of rules are to be formulated. The concept ‘Performance Based certification’ (PBC) has been proposed by Euro
Control for the military systems to meet civil CNS/ATM requirement so as to fly
in common air space.
Civil
Certification of Military Aircraft
Airbus military A400M Transport aircraft has been type
certified by EASA following CS-25 and Initial Operational Clearance accorded on
compliance to the additional military requirement indicated by the French Air
Force. Lockheed martin has notified FAA for type certification of L-382J
Hercules (civil variant of C-130J Super Hercules) to be marketed as LM-100J. In India Advanced Light
Helicopter, Dhruv designed to meet UK MOD Def-Stan-00-970 was type certified by military airworthiness authority CEMILAC, DRDO. The same helicopter was later accorded type certification for
civil use by DGCA, Min of Civil Aviation, Gov. of India, based on the tests earlier
conducted. US military operates FAA certified aircraft as military commercial derivative aircraft (MCDA). FAA has released an
Advisory Circular AC–20-169 and
created a Military Certification Office
to provide certification and continued airworthiness of MCDA. Sweden has also
harmonized civil and military certification procedure considering cost of testing
and certification of the same product more than once to satisfy two different
authorities and applications.
Unified
Procedure – Recommendation
For
criticality of application of military combat aircraft, it is recommended to
continue the military certification of combat aircraft. However, considering
the enormous cost and effort required for certification, it is advisable to
have unified certification for the transport category aircraft for use in civil
and military application. A unified approach is recommended for the
certification of non combat aircraft as follows:
a) Design and Production Organisation approval
(DOA and POA) to be accorded
following international norms as per ICAO Airworthiness Manual. The design
codes to be followed are as per appropriate FAR category.
b) The
basic aircraft (green aircraft) can be certified on compliance to FAR requirements.
The additional military staff requirements are to be marked as ‘Critical Review Item’ (CRI).
c) While
worldwide, the civil certification authorities have wider expertise in aircraft
certification and therefore, are entrusted for military aircraft certification
also. In India, DGCA are not considered to possess requisite manpower and
expertise to take up aircraft certification. Considering the availability of
manpower and other infrastructure, CEMILAC, DRDO is recommended to take up the certification
activity.
d) However,
ICAO recognises only DGCA and not CEMILAC. Thus the type certification for
civil application has to be endorsed by DGCA. Thus it is required to have a
close co-ordination between CEMILAC and DGAQA at all stages of aircraft
certification.
e) It
is recommended to from an apex organisation
(Aerospace Commission) for overseeing these two organisations and provides
directions so that duplication of certification effort is avoided.
f) The
apex organisation will give direction towards acceptance of all CRIs based on
the military compliance and accord operational clearance for service induction
of the aircraft.
g ) To
provide interoperability in the national airspace, performance based
certification and unification of CNS/ATM to be implemented. Conclusion
Certification is a costly and time consuming activity. Besides it is a specialised and a different task compared to design and manufacturing. Safety is a concern for both civil and military authorities. It therefore does not make sense to spend time and effort to certify the same aircraft twice just to satisfy two different regulatory autheirites.
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