Atch 3 - Aircraft Identification Sheet

HTC71126RE147 DPAA PAPUA NEW GUINEA

Attachment 3: Aircraft Identification Sheet

Instructions:
The aircraft identified in this attachment are the only aircraft approved for contract performance. In Part 1, provide the specifications for each primary and alternate aircraft you propose. In Part 2, certify that each proposed primary aircraft meets or exceeds the minimum requirements detailed in the Performance Work Statement (PWS). Part 1: Proposed Aircraft Data
This section is for data entry only. Offerors will certify compliance in Part 2. The offeror shall insert the proposed aircraft in the table below that will be utilized in performance of the Defense POW/MIA Accounting Agency (DPAA) Helicopter Support Services in Papua New Guinea per the Performance Work Statement (PWS). Aircraft Specification
Helo 1 (Primary)
Helo 2 (Primary)
Helo 3 (Primary)
Alternate 1
Alternate 2
Aircraft Type/Model

Aircraft Tail No.

Owned/Controlled By(Offeror or Subcontractor Name)

Number of Pax Seats

Service Ceiling (Feet)

Internal Payload (lbs)

External Sling Load (lbs)

Engine Type (Single/Twin)

Aircraft Range (NM)

Cruise Speed (Knots)

Fuel Burn Rate (GPH)

Part 2: PWS Compliance Certification Checklist
By checking the boxes below, the Offeror certifies that the proposed primary aircraft listed in Part 1 meet or exceed the corresponding PWS requirements. Verify
PWS Reference
Requirement Description
Aircraft Performance Requirements
[ ]
PWS 1.3.3
The proposed “Helo 1” meets or exceeds all minimums: 5 Pax, 9,000 ft Service Ceiling, 500 lbs Internal Payload, 2,000 lbs External Sling, Single Engine. [ ]
PWS 1.3.3
The proposed “Helo 2” meets or exceeds all minimums: 9 Pax, 15,000 ft Service Ceiling, 1,000 lbs Internal Payload, 3,300 lbs External Sling, Twin Engine.

[ ]
PWS 1.3.3
The proposed “Helo 3” meets or exceeds all minimums: 12 Pax, 15,000 ft Service Ceiling, 1,300 lbs Internal Payload, 4,400 lbs External Sling, Twin Engine. Aircraft Communication & Safety Equipment
[ ]
PWS 1.3.3.2
All proposed aircraft are equipped with a VHF/AM radio (118.000–136.975 MHz). [ ]
PWS 1.3.3.2
All proposed aircraft are equipped with a VHF/FM ground comms radio (138–174 MHz). [ ]
PWS 1.3.3.2
All proposed aircraft are equipped with an HF/SSB radio (2–30 MHz). [ ]
PWS 1.3.3.2
All proposed aircraft are equipped with a dual-frequency ELT (121.5 MHz and 406 MHz). [ ]
PWS 1.3.3.2
All proposed aircraft are equipped with a functioning Automatic Direction Finder (ADF).