STATEMENT OF WORK FOR THE RE-CERTIFICATION / OVERHAUL OF EUROHAWK (EH) ENGINE BEFORE USE ON NATO AGS - LIFE CYCLE MANAGEMENT DIRECTORATE AIRBORNE ...
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LIFE CYCLE MANAGEMENT DIRECTORATE
AIRBORNE SURVEILLANCE SYSTEMS PROGRAMME OFFICE
AGS SYSTEM MANAGEMENT GROUP
STATEMENT OF WORK
FOR THE RE-CERTIFICATION / OVERHAUL
OF EUROHAWK (EH) ENGINE BEFORE USE
ON NATO AGS
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AMENDMENT RECORD
Version / Revision Pages(s) As Of / Date Remarks
1.1 Version All 11 Mar 2021
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TABLE OF CONTENTS
1. Background .............................................................................................................................4
2. Purpose ...................................................................................................................................4
3. Scope ......................................................................................................................................4
4. Applicable Documentation ....................................................................................................... 4
5. Control ....................................................................................................................................5
6. Contractor Services Requirement ............................................................................................ 5
7. Packaging, Handling, Storage and Transportation (PHST) ...................................................... 6
8. Reporting Requirements.......................................................................................................... 7
9. Meetings / Progress Reviews .................................................................................................. 7
10. Contract Deliverables Requirement List (CDRL)...................................................................... 7
Definition of acronyms ........................................................................................................... 8
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1. Background
1.1. NATO Support and Procurement Agency (NSPA) purchased from German Ministry of
Defence (MoD), among other stuff, an EuroHawk (EH) Aircraft Engine (Model/Type
AE3007H) with the intention to use it on the North Atlantic Treaty Organization
(NATO) Alliance Ground Surveillance (AGS) Unmanned Aerial Vehicle (UAV). This
engine has been identified as of direct use to NATO AGS UAV based on
Model/type, Part Number (P/N) and Nato Stock Number (NSN) commonality.
1.2. The above engine has been purchased from the German MoD as spare engine for
the EH aircraft in new/unused condition and within the original shipment packaging
of the Original Equipment Manufacturer (OEM). The engine received by the German
MoD in Airworthiness (AW) condition for use on the EH UAV and since the receipt
was stored for a long period (at least 6 years, in average) in controlled warehousing
environment (e.g.: temperature, humidity, EMI/EMC protection, etc…) however,
without any kind of inspection / test performed in the meanwhile.
1.3. Although this engine is identified being the same configuration (Model/type, P/N,
MFC, NSN) of the NATO AGS UAV, it is operating under Computer Software
control, which may has undergone updates/revisions. In addition, due to long
storage time there is a possibility that the OEM has issued improvements, which
have to be considered before releasing it to service for the NATO AGS UAV.
1.4. Therefore, the engine above has to run the process of recertification / Overhaul
(O/H), by the System Design Responsible (SDR) or the OEM, in order to be declared
serviceable and approved / released for use on NATO AGS UAV configuration.
2. Purpose
2.1. This Statement of Work (SOW) provides for recertification / O/H requirements for
the EH engine purchased by NSPA for use on NATO AGS UAV and the
implementation of it, as required.
3. Scope
3.1. This SOW applies to the EH engine identified as follows:Model/type AE3007H;
P/N 23065502, MFC 63005;
S/N CAE380066;
NSN 2840-01-507-6569
4. Applicable Documentation
4.1. AER(EP).P-145 (Annex 1 and 2)
4.2. AER(EP).P-2005 (EN)
4.3. AQAP 2070 V3, Aug 2015
4.4. STANAG 4281 Edition 3, 4 Oct 2016
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5. Control
5.1. Service validation
5.1.1. NSPA shall validate that all contract requirements have been met, through
analysis of Contractor reports, customer feedback, NSPA audits (if and as
needed) and observations.
5.1.2. Specifically regarding the acceptance of a certified part, this shall be considered
completed, based on the approval by NSPA of the relevant part certification
documentation.
5.1.3. NSPA reserves the right to request approval by DAAA of the relevant part
certification documentation.
5.1.4. In the event of contractual disagreement between the Contractor and NSPA
(or other Contractors), both NSPA and the Contractor shall document the nature
and details of the disagreement and both parties shall endeavour to implement
remedial action (if appropriate) as soon as possible. Should the matter not be
resolved in this manner, it shall be referred to the CO as a Contract(s) issue for
resolution according to the Terms and Conditions of the Contract.
6. Contractor Services Requirement
6.1. The Contractor shall prepare and submit a project plan, which shall include the
following (as a minimum):
6.1.1. The procedures / method to be implemented for the recertification of the
engine identified in para. 3 of the SOW, considering the provisions of para. 1.3 and
1.4, with references to the applicable technical documentation.
6.1.2. The individual recertification tasks (if any) to be performed on items
assembled with the engine, thus being one part with it, considering the item
category, configuration status, and functionality.
6.1.3. A time scheduled plan, including the certification process steps for the engine
(e.g.: induction for certification date, required maintenance actions, expected
certification completion date).
6.1.4. The template of the certification document (Certificate of Conformity - CoC),
which shall be issued and signed by the Contractor for the engine, after the
completion of the required work. This template shall match the structure of the
CoC template of the AQAP 2070 V3, Aug 2015,
6.1.5. The Contractor personnel assigned to that project (roles and responsibilities)
as well as data for communication.
6.2. The Contractor shall re-certify the engine according to the agreed Project Plan and
issue a CoC or EASA Form one, or FAA 8130-3 form, which declares for the engine
serviceable and approved / released for use on NATO AGS UAV. The CoC shall be
signed by the NATO AGS SDR or by the OEM for that engine, but in case the EASA
Form or FAA form is provided it shall be properly completed and signed. The
certification process may also include an O/H, if required to complete the certification
process. In such a case, the O/H requirement shall be properly justified and
documented by the Contractor prior to implementation. The SDR and the OEM are
specified as follows:
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6.2.1. SDR
CAGE Code 78022
Name NORTHROP GRUMMAN SYSTEMS CORPORATION
Address 17066 GOLDENTOP RDSAN DIEGO, CAL, UNITED STATES
6.2.2. OEM
CAGE Code 63005
Name ROLLS-ROYCE CORPORATION
Address 450 S MERIDIAN ST, INDIANAPOLIS, IN, UNITED STATES
6.3. The Contractor shall implement all pending Service Bulletins in accordance with the
Technical Documentation issued by the OEM.
6.4. The Contractor shall document all the activities performed in the Engine Log Book that
will be accompanying the Engine.
6.5. When the Contractor identifies cases where the engine cannot be either processed at
all for certification, or it fails / cannot complete the certification process, the Contractor
shall report (properly justified) that to NSPA for getting further evaluation and advice.
6.6. In case NSPA, after having received Contractor's justification, decides for the engine's
disposal, the Contractor shall be notified to ship the engine back to NSPA for disposal
action.
6.7. Disposal in Contractor’s premises might be mutually agreed, subject to a supplemental
agreement. In this case, a certificate of disposal shall be issued by the Contractor.
7. Packaging, Handling, Storage and Transportation (PHST)
7.1. NSPA shall deliver the engine identified in para. 2 of the SOW to the Contractor
premises, with the original packaging as they have been received from the German
MoD.
7.2. The Contractor shall acknowledge the receipt of the engine to NSPA, within one (1)
week, after it reaches Contractor's premises stating any discrepancies / Non-
conformities found out.
7.3. The Contractor shall crate/pack the engine after certification is completed using its
original packaging (as received by him) if possible, otherwise he shall pack it in a way
to assure the engine safe storage and condition during shipment and transportation
with the provided means, to the final destination as foreseen in OEM's publications for
storage and shipment.
7.4. The Contractor shall enclose in engine's packing a copy of the required certification
documents (see para. 6.2) and send the originals by mail to NSPA’s TO.
7.5. The Contractor shall notify NSPA well in advance (but not less than 2 weeks) for the
forthcoming shipment of the engine to NSPA, in order to allow for transportation
arrangements.
7.6. The Contractor shall identify the relevant applicable classification, and identify specific
special transportation requirement.
7.7. Labelling of the engine after certification shall comply with the provisions of STANAG
4281.
7.8. Transportation to the Contractor
7.8.1. NSPA shall inform the Contractor about the forthcoming arrival of the engine
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and his freight forwarder details.
7.8.2. NSPA Freight Forwarder shall perform all required customs formalities for
temporary import, in accordance with the contract terms and conditions.
7.9. Transportation from the Contractor
7.9.1. NSPA will provide its freight forwarder details with shipping instructions
(information copy to the Contractor), upon receipt of Contractor’s notification that
the engine is ready for dispatch.
7.9.2. The NSPA freight forwarder shall pick up the engine at the Contractor’s point of
dispatch set forth in the Contract Schedule and will forward the consignment to
the final destination.
7.9.3. The NSPA freight forwarder shall perform all customs formalities iaw the
contract terms and conditions.
8. Reporting Requirements
8.1. Non-Certifiable part report:
8.1.1. The Contractor shall report to NSPA in case of non-certifiable engine, within
one (1) week after the engine is inducted for certification.
8.1.2. The report shall justify the reasons for which the Contractor cannot proceed in
engine's certification and proposal for further use on the engine.
9. Meetings / Progress Reviews
N/A
10. Contract Deliverables Requirement List (CDRL)
The following tables shows the list of contractual deliverables associated with this SOW.
T0 stands for the date of issuance of the Purchase Order.
SOW Acceptance Delivery time or
ID Deliverable Ref. Reqd. Milestone Frequency Comments
CDRL#1 Project plan 6.1 No T0 With the proposal
Certification of Following the certification
CDRL#2 6.2 Yes T0+6M
Conformity (CoC) of the engine
Non-Certifiable 6.5,
CDRL#3 Yes T0+1M If required
part report 8.1
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Definition of acronyms
Acronyms
AW Airworthiness Alliance Ground
AGS Surveillance
CO NSPA Contracting Officer
CoC Certificate of Conformity
DAAA Directorate for Aeronautical Armaments and Airworthiness
EH EuroHawk
LCH Local Civilian Hires
MoD Ministry of Defence
MTC Military Type Certificate
NATO North Atlantic Treaty Organization
NSN NATO Stock Number
NSPA NATO Support and Procurement Agency
OEM Original Equipment Manufacturer
O/H Overhaul
PHST Packaging, Handling, Storage and Transportation
P/N Part Number
QA Quality Assurance
SDR System Design Responsible
SOW Statement of Work
TAA Technical Airworthiness AuthorityNSPA
TO Technical Officer
UAV Unmanned Aerial Vehicle
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