Atch 5 - Technical Capability Worksheet DPAA PNG

Attachment 5: Technical Capability Worksheet

Company Name of Offeror:
[Insert Offeror Name Here]
Date of Submission:
[Insert Date]
Solicitation Number:

HTC71126RE147

Project / Program:
DPAA Papua New Guinea Helicopter Support

Instructions to Offerors
Page Limits & Format: The Offeror’s entire Technical Proposal must not exceed a total of thirty (30) pages. Offerors may provide their responses directly below each requirement in this Word document or submit a separate Technical Proposal document that clearly references each section number in numerical order (e.g., “Response to 1.1”). The 30-page limit applies strictly to technical compliance. Do not submit any marketing material, corporate qualifications, or generic company overviews. The Government will not read or evaluate any text that exceeds the stated limits. Diagrams & Flowcharts: If the offeror needs to attach a diagram, workflow, or flowchart showing how the aircraft or operational approach meets requirements, this is authorized. Such attachments must not exceed one (1) page per question, are included in the overall 30-page limit, and must be clearly referenced in the corresponding narrative. Diagrams and flowcharts cannot contain additional narrative text. Evaluation: Each subfactor will be evaluated on an Acceptable/Unacceptable basis in accordance with FAR 52.212-2. To receive an overall Technical rating of “Acceptable,” an offeror must receive an “Acceptable” rating for all subfactors. Failure to clearly demonstrate how you meet the requirements of any single subfactor will result in an overall “Unacceptable” technical rating. Responses that merely restate PWS requirements or use generic language such as “will comply” or “standard techniques will be employed” will be rated as Unacceptable. Exclusions: Do not include pricing, past performance, or business compliance items (such as CARB, AOC, CMMC, or Insurance) in this worksheet. All aircraft specification data must be submitted separately in Attachment 3 (Aircraft Identification Sheet).

Subfactor 1: Aircraft Compliance

1.1 Aircraft Specifications & Performance

PWS Reference: Section 1.3.3 (Aircraft Performance Requirements table only) Requirement: Describe how your proposed aircraft (identified in Attachment 3) are physically suited to meet or exceed the performance parameters specified in the PWS (passenger capacity, service ceiling, internal payload, external sling capacity, and engine type) for all three helicopter types, specifically when operating in Papua New Guinea’s high-altitude and mountainous environments.