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3.  STATUS AND IMPLEMENTATION OF JAA WORK

3.1   Certification

JAA are committed to the joint certification of new aircraft, engines, propellers, and equipment. They have established a joint system for the approval, using a multinational Team or local Authority according to the complexity, of these products, Auxiliary Power Units (APUs) and equipment coming under the Joint Technical Standards Order (JTSO) system.

At present JAA have adopted, amongst others, codes for the certification of large aeroplanes (JAR-25), small aeroplanes including commuters (JAR- 23), sailplanes and powered sailplanes (JAR-22), very light aeroplanes (JAR-VLA), helicopters (JAR-27 and -29), engines (JAR-E), auxiliary power units (JAR-APU), propellers (JAR-P) and equipment (JAR-TSO).

Joint Type Certifications have already been completed on the following large aeroplanes:

 

Airbus A340-200/-300

Airbus A320-232

McDonnell Douglas MD-11

Airbus A320-214

Jetstream 4100

Airbus A321

Canadair CL600-2B19 Regional Jet

Airbus A319

Dornier 328 - 100/300

Airbus A320

CASA CN-235-100

Airbus A330-200

Saab 2000

Airbus A330-321/-322

Boeing 777-200/-200IGW/-300

Airbus A330-341/-342

IPTN CN 235-110

Airbus A340-212/-312

EMB145/135

Falcon 2000

Boeing 737-700/-800/-600

Learjet 45

MD 90-30

deHavilland DHC-8-400

B 767-400 ER

Boeing 717-200

Boeing 757-300

Citation X

Global Express

 

In addition the following joint aeroplane certification programmes are in progress:

 

Boeing 737/-700C/-900

IPTN-N250

Gulfstream V

B767-400 ER

Tupolev 204-200

Raytheon 4000

Canadair CL-600-2C10

A340-500,-600

Boeing 777-200LR/300ER

Airbus A3XX-100

Dornier 728/528/928

Embraer 140

Airbus A318

Embraer 170/190

Cessna - model 680 (sovereign)

BD-100-1A10

CL- 600-2D24

 

The JAA and FAA have agreed to perform mutually validation, using the agreed FAA/JAA Validation Principles documents. This process is being applied, to the extent practicable, on current validation projects and are applied to all new validation projects unless the Applicant elects to use the "Co-operative and Concurrent Certification" procedure as was applied to the Boeing 717.

On the engine side Joint Type Certification/Validation have been completed on:

 

Williams International FJ44-1A

(for Citation Jet)

Pratt & Whitney Canada PWC 119B/119C

(for Dornier DO328)

Allison AE 2100A

(for Saab 2000)

General Electric CF6-80E1A1/A2/A4

(for Airbus A330)

Rolls-Royce RB211 Trent 700 series

(for Airbus A330)

Pratt & Whitney PW 4164/4168/4168A

(for Airbus A330)

CFE Company CFE 738-1-1B

(for Falcon 2000)

Several Rolls-Royce RB211 Trent 800 series variants

(for Boeing B777)

Several Pratt & Whitney PW 4084 series variants

(for Boeing B777)

General Electric GE 90 series

(for Boeing B777)

Turbomeca ARRIEL 2S1/2B/2C/2C1

(for Sikorsky76C+, (AS350 B3 and SA365N helicopter)

Pratt & Whitney Canada PWC 206A/B/C/E

(for MD900, EC135, AgustaA109 and MD900A helicopter)

Pratt & Whitney Canada PW 545A

(for Citation Exel)

Allied Signal TFE 731-20/-20R/40/40R/-60

(for Learjet 45, Falcon 50EX, ASTRA SPX and Falcon 900EX)

Turbomeca ARRIUS 2B/2B1/2B1A

(for EC-135/EC135A helicopter)

Pratt & Whitney Canada PWC530A

(for Citation Bravo)

BR 700-710 A1-10 and 710 A2-20

(for Gulfstream V and - Canadair Global Express)

BR700-715A1/B1/C1-30

(for Boeing B717)

Allison AE3007A/3007C

(Embraer 145 and Citation X)

Allison 250-C47B/-C47M

(for Bell 407 and MDH/MD600N Helicopter)

Pratt & Whitney Canada PW306A & PW306B

(for IAI Galaxy and Dornier 328 jet)

Pratt & Whitney Canada PW150A

(for Dash 8-400)

Pratt & Whitney Canada PW 535A

(for Citation Ultra Encore)

GE CF34-8C1

(for Regional Jet CL600-2C10)

 

Additional 27 Joint Engine programmes are in progress.

One of them comprises four new Diesel Piston Engines and is handled under the Joint Local Procedure with DGAC-F as PCA.

Another Piston Engine programme (Rotax 936) has been initiated under the Joint Local Procedure with ACG as candidate PCA.

A further Diesel Piston Engine to be certified under JAR-22 subpart H is handled under JLP with LBA as candidate PCA.

On the propeller side one Joint Type Certification (Dowty Aerospace R408 for PWC150A/Dash 8-400) has been completed under the JAA Local Procedures with CAA-UK as PCA.

On the helicopter side, one JAA type certification to JAR-27 has been completed: Eurocopter EC 120B. EC 130B with DGAC-F as PCA is in the process of Joint Certification.

A new application for Joint Local Certification Procedures has been received: the Agusta A119 with ENAC Italy as PCA.

Further one validation of the FAA primary certification has been completed:

MD HS MD 900 Explorer and variants (category A, IFR, Gross Weight increase).

Several validations of the FAA/TCA primary certificates are in progress:

United Technologies Sikorsky S92 (JAR-29):  FAA
Bell 427:  TCA
Bell-Agusta D609 Tilt Rotor:  FAA

On the small aeroplane side, the joint type certifications/validations are in process for the following programs:

JAR 23:
SJ30-2 (Validation, FAA)
Euro-ENAER Eaglet (Certification, RLD as PCA)
Raytheon 390 (Validation, FAA)
CAP Aviation CAP 222 (Certification, DGCA-France as PCA)
SOCATA TB 360 (Certification, DGCA-France as PCA)
Diamond DA.40. (Certification, Austro-Control as PCA)

JAR VLA:
Europa ISA 235 (Certification, CAA UK as PCA)
Speed Arrow TL 750 (Certification, ENAC as PCA)

Joint Type Certifications have already been completed on the following VLA:
Zenair CH 2000 (Validation TCA)
Issoire Aviation Lionceau (Certification, DGCA-France as PCA)

JAR-21, "Certification Procedures for Aircraft and Related Products and Parts", was adopted in November 1993 and became effective on 1 January 1995. JAR-21 covers the policy and arrangements between JAA and European industry applicants for product certification and design and manufacturing approvals, and will be jointly implemented by JAA on the basis of an agreed schedule in a progressive manner.

JAR-21 regulations covering products imported from non-JAA countries have been adopted in March 1996 with an effectivity date of 1 June 1999. Currently JAR-21 is applicable to new European products and voluntary to new imported products as well. There is a need for products previously certificated nationally by one or more JAA Member States to be caught-up. This catch-up process is a special process to define a standard for existing aircraft accepted by the JAA Member States which allows free movement of existing aircraft in the "JAA space" without constraints.

The first list of caught-up products has been adopted by the JAAC in May 1999 together with the regulatory changes in JAR-21. Procedural material will be ready for publication in the near future. Jointly type certificated large aeroplanes and other products will be caught-up additionally. JAAC has adopted in June 2000 the list of jointly type certificated European and imported Large aeroplanes.

In addition JAA publish Joint Implementation Procedures for certification/validation. These define the arrangements between the JAA Members to achieve the mutual recognition of the joint certification/validation; they were developed in discussions between JAA and industry. The following procedures are adopted by the JAAC:

Joint Multinational and Joint Local Certification
Design Organisation Approval
Production Organisation Approval
Joint Technical Standard Order Authorisation
JAA STC Procedures
JAA Validation Procedures based on Validation Item Concept (JVPVIC)

Furthermore additional procedures should become available to enable the progressive implementation of JAR-21 (eg JPA, Repairs....).

3.2   Maintenance

JAR-145 is a requirement to approve/accept maintenance organisations to maintain any aircraft used for commercial air transport. Originally published in 1991, there are some 3100 organisations approved/accepted throughout the world of which 1970 are in Europe, 1220 in North America and 240 in the rest of the world.

The current status of JAR-145 is at change 2 which includes NPAs 145-1 to 145-6. NPA 145-7 concerning the interface with JAR-66 was adopted in August 1999. NPA 145-8 addresses a stronger quality system, qualification of NDT personnel and design of repairs to complement NPAs 21-8 & 21-17. NPA 145-8 will be published end 2000.

JAR-OPS Parts 1 & 3, Subpart M : "Maintenance"

This is a section of JAR-OPS and covers the operator's responsibility for maintenance management and includes the aircraft maintenance programme and flight technical log. There are about 50 operators maintenance arrangements accepted at this time. NPA-OPS-11 covering a number of minor improvements to JAR-OPS 1 (3) Subpart M was adopted in August 1999.

JAR-66:  "Certifying Staff"

JAR-66 is a requirement about qualifying maintenance personnel to issue certificates of release to service for JAR-145 organisations. JAR-66 specifically covers the issue of an aircraft maintenance basic licence but must be read in conjunction with NPA 145-7 regarding the JAR-145 certification authorisation issued to certifying staff. JAR-66 was published on 3 April 1998 with mandatory compliance by 1 June 2001. Each JAA member Authority must successfully meet with a JAR-66 Review Board. So far, the experience with the JAR-66 Review Board has been positive.

The first JAR-66 licences have been issued as from mid 1999.

JAR-147  Approved Maintenance Training

JAR-147 is a requirement for approved maintenance training to satisfy part of the JAR-66 requirements including in particular the conduct of basic and type examinations to be accepted by the JAA-NAA as a basis for issue of the proposed JAR-66 Licence.

JAR-147 was published on 3 April 1998 with mandatory compliance by 1 June 2001 for those organisations that wish to claim reduced time to qualify for JAR-66 licence.

JAR-Maintenance

JAR-M is a new proposed requirement covering the maintenance of all aircraft not used for commercial air transport. It specifically includes requirements on accountability, standards, fitness for flight, maintenance test flights, maintenance personnel, control of parts and human factors.

The current status of JAR-M is that the 4th draft was on limited consultation during the 2nd half of 1999. JAR-Maintenance is put on hold, awaiting the outcome of JAR-OPS 2 and 4 Subpart M.

Maintenance Review Boards (MRB)

The MRB process is a logic method used by aircraft manufacturers in conjunction with operators to develop a maintenance programme for each new large aircraft type.

The MRB procedure was first published in July 1993 as chapter 16 of JAA administrative and guidance material and has been used ever since as the basis for all new large aircraft.

Maintenance Standardisation

The JAA concept for the approval of maintenance is that this is the responsibility of the national authorities; however, an important foundation for the mutual acceptance of maintenance is the use of Maintenance Standardisation Teams (MAST). Three such teams are operating and visits continue since 1993 to be carried out to all "full" JAA members about every 15 months.

The National Authorities and organisations located in the USA/Canada which have been accepted in accordance with JAR-145 by JAA are subject to sample audits carried out by Maintenance International Standardisation Teams (MIST) operating in a similar manner to MAST teams. Canada and all FAA regions of the USA continue to be audited every 12 months in the case of the USA and 18 months for Canada.

Maintenance Bilaterals

The JAA has been working for some time with both the FAA for the USA and Transport Canada to agree a bilateral covering maintenance. The Maintenance Implementation Procedures (MIP) dated May 97 was accepted by the JAA Committee and the FAA in June 97 to form the basis of agreements to be signed by the FAA and each JAA-NAA. Germany, Ireland and France signed the MIP and implementation of the bilateral agreement is expected to start shortly after. Other JAA-NAAs are expected to sign aswell. An agreement was signed in July 1996 between Canada and all JAA countries. These agreements should make our work a little easier as it will be possible to place greater reliance on the American and Canadian systems.

3.3   Operations

JAR-OPS Parts 1 and 3 (covering Commercial Air Transportation by aeroplanes and helicopters respectively) were adopted by the JAA Committee at the end of March 1995, the first issue being published on 22 May. At that time it was decided that JAR-OPS should, initially, be implemented under national legislation no later than 1 April 1998 with JAR-OPS 1 being subject to "phased implementation" such that the operators of large aeroplanes (those over 10 tonnes MTOM or with 20 or more passenger seats) and mixed fleets of large and small aeroplanes would be affected first, followed 1 year later (1 April 1999) by those AOC Holders operating small aeroplanes only. It was intended that JAR-OPS 3 should be implemented in toto on 1 April 1998.

As the Authorities and the industry have been working towards these implementation dates, the workload on both the Authorities and the operating industry, and the fact that some impending amendments were being processed, necessitated a delay in implementation.

The proposed Subparts of JAR-OPS Parts 1 & 3 on Flight and Duty Time Limitations and Rest Requirements (Subpart Q) have been the subject of particularly careful consideration, the JAR-OPS 1 material being sent out for consultation on three occasions to date. For a variety of reasons, these important elements of JAR-OPS have not yet been adopted. The current situation in this area is that the European Commission has resolved to try and adopt a 'new approach' with a view to progressing the issue. There has been considerable general discussion on the subject in the EU forum and the European Commission is now preparing draft proposals drawing upon these discussions. As a result of this activity, the JAA Committee has decided to await developments before considering the matter further.

Since the adoption and publication of JAR-OPS 1 and 3, the Operations Joint Implementation Procedures have been completed and published. These procedures must be followed by the authorities when implementing JAR-OPS in all JAA Member States. Included in this material is the mechanism under which Operations Standardisation Teams (OPST) (similar in function to the MAST system for maintenance) will operate. Unfortunately, for different reasons, the work of the OPSTs has not been started yet. In advance of the commencement of this standardisation activity, JAR-OPS training is being provided by the JAA Headquarters Operations Division for both Authorities and industry personnel. JAR-OPS Training commenced at the end of October 1995.

A 'package' of proposed amendments to JAR-OPS 1 (NPA-OPS-7) was sent out for consultation in the first quarter of 1997. The changes proposed vary between those necessitated by amendments to ICAO Annex 6 (upon which JAR-OPS 1 is based) and other proposals that could not be included in the first issue of JAR-OPS 1. The processing of comments arising from this NPA started at the beginning of May and was completed at the end of 1997. The amendments have been incorporated in a new edition of JAR-OPS 1 identified as Change 1, dated 1 March 1998. A corresponding 'package' of amendments for JAR-OPS 3 was sent out for consultation early in 1998. The results were processed and published in an updated version, JAR-OPS 3, change 1, dated 1 February 1999.

Operational requirements covering General Aviation (including Aerial Work) activity by aeroplanes and helicopters will be contained in Parts 2 and 4 respectively. Work has started on JAR-OPS 2 and 4 with the Aerial Work and General Aviation Sub-Committee (AWGAS), concentrating on Corporate Transport and the Helicopter Sub-Committee (HSC) primarily concerned with Commercial Aerial Work. The intention remains that both sub-committees will produce draft material - AWGAS for aeroplanes and the HSC for helicopters. In addition a concept paper is to be developed by the end of this year which will discuss and recommendd to the JAAC those areas of general aviation activity which should be regulated in JAR-OPS Parts 2 & 4.

In addition to the above-mentioned operational regulations, requirements have also been developed for Flight Simulators and Flight Navigation and Procedures Trainers. All of the requirements concerning the evaluation and qualification of the various types of Synthetic Training Devices used for training flight crew are covered by a set of requirements, to be known as JAR-STD (Synthetic Training Devices), which will be divided into separate Parts. The suffixes 'A' and 'H' are used to denote the applicability of the various Parts of JAR-STD to Aeroplanes or Helicopters respectively. The first of these (JAR-STD Part 1A) addresses Flight Simulators (Aeroplanes) and was published on 30 April 1997. The implementation date of JAR-STD Part 1A coincided with that of JAR-OPS 1 implementation in April 1998. JAR-STD 3A which governs Flight and Navigation Procedures Trainers was published on 9 January 1998 and has an implementation date coincident with that of JAR-FCL in July 1999. JAR-STD 2A addressing Flight Training Devices (FTD) of aeroplanes having been developed and undergone the NPA process, was adopted in March 1999 by the JAAC. Additional Parts of JAR-STD will be developed to cover Helicopter Synthetic Training Devices. Draft JAR-STD 1H (Flight Simulators Helicopters) is out for comment under NPA-STD-5 and work is in process for JAR-STD 3H (Helicopter FNPT). If deemed necessary, certain other types of synthetic training devices will be addressed. The intention behind JAR-STD is that there should be a single evaluation of a Synthetic Training Device, the findings of which should be acceptable to all JAA Member Authorities. Such processes should result in considerable savings in that repetitious evaluations by individual authorities will no longer be required.

In a manner similar to that followed for JAR-OPS, Joint Implementation Procedures for JAR-STD have now been completed and published. As with the procedures relating to JAR-OPS, the procedures for JAR-STD must be followed by the Authorities when evaluating and qualifying Synthetic Training Devices in accordance with JAR-STD. STD Standardisation Teams, modelled on the principles established for OPSTs and MAST, have commenced their activity in 1998, co-ordinated by the JAA Headquarters Operations Division. For the time being 7 JAA Authorities enjoy mutual recognition of Flight Simulator Evaluations and qualifications.

3.4   Licensing

Licensing involves all matters relating to personnel training, testing, authorisation and medical certificates. Arrangements applicable to flight crews have been adopted with a distinction being made between regulatory licensing requirements (known as JAR-FCL) and their accompanying implementation procedures, referred to as the Joint Implementation Procedures (JIP).

JAR-FCL 1 (Aeroplane), 2 (Helicopter), 3 (Medical) and 4 (Flight Engineers) contain licensing and medical requirements for flight crews and include acceptable means of compliance and interpretative material for training, testing and licensing of Airline Transport Pilots, Commercial Pilots, Flight Engineers and Private Pilots for aeroplanes and helicopters. The medical requirements are set out in JAR-FCL 3 which further comprises the Aviation Medical Manual, providing guidance for Authorised Medical Examiners and Aeromedical Sections of the National Authorities.

After adoption of JAR-FCL 1 and 3 by the JAAC in 1996 and JAR-FCL 2 in 1997, several NPAs have been issued to further improve the documents. Implementation of JAR-FCL 1 and 3 commenced from 1 July 1999 and all States are busy with their implementation plans. Implementation of JAR-FCL 2 will follow starting January 2000. JAR-FCL 1 has been re-issued as "Amendment 1" and incorporates the contents of 3 NPAs. JAR-FCL 2 and 3 will be re-issued later in 2000, incorporating the results of the NPA process aswell.

The responsibility to issue JAR-FCL licences, certificates, ratings and authorisations rests with the National Authorities. By adopting and implementing a common set of requirements, the overall aim is to achieve mutual recognition of licences between all JAA Member States. Licensing and Medical Standardisation Teams took up their work in May 1999 and the results of their visits are evaluated in the Licensing Division. Recommendation for mutual recognition of licences is issued to the JAA Committee when compliance with JAR-FCL and JIP has been demonstrated.

Future work on JAR-FCL requirements may also include the development of JAR-FCL 5 (Gliders and Balloons).

Training courses on the JAA structure, JAR-FCL and JIP continue to be made available to Authorities' staff, Industry and Organisations, in order to familiarise personnel with the new requirements in the field of Flight Crew Licensing.