PWCPT6A-41UC-12Engine12-2019_20200110183348.063_X.pdf

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Attached to
Pratt & Whitney Canada PT6A-41 Engine w/ Core Exchange Federal contract opportunity
Solicitation number
80LARC719623Q
Issued by
National Aeronautics and Space Administration Langley Research Center

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Other files attached to Pratt & Whitney Canada PT6A-41 Engine w/ Core Exchange, newest first.
File Type Posted
PWCPT6A-41UC-12Engine20200131.pdf PDF
UC-12 PT6A41 Core to Exchange Specs.pdf PDF
FedBizOpps PWCPT6A-41_Instructions.pdf PDF
80LARC719623Q Q&A.docx DOCX document
80LARC719623Q Q&A.docx DOCX document
80LARC719623Q Q&A.docx DOCX document
80LARC719623Q Q&A.docx DOCX document
UC-12 PT6A41 Core to Exchange Specs.pdf PDF
FedBizOpps PWCPT6A-41_Instructions.docx DOCX document

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Text version

Pratt & Whitney Canada PT6A-41 with Core Exchange

Type of Request: Best Value

Item to be purchased: Pratt & Whitney Canada PT6A-41

Engine Condition: Overhauled, Repaired, or Used

Deliverables Prior to Award:

Engine Records, to include but not limited to:

1. Maintenance Records

2. Pratt & Whitney Canada Service Bulletin Compliance

3. Pratt & Whitney Canada`s Recommended Time Between Overhaul Interval

4. Last Overhaul Date (Month & Year)

5. Engine Hours & Cycles:

a. Total Flight Hours Since New

b. Total Flight Hours Since Overhaul

c. Total Cycles Since New

d. Total Cycles Since Overhaul

6. Rotating Component Part Numbers & Total Cycles Since New for;

a. Hub, Compressor (1st Stage)

b. Rotor, Compressor

c. Disk, Compressor (2nd Stage)

d. Disk, Compressor (3rd Stage)

e. Impeller, Centrifugal

f. Disk, Compressor Turbine

g. Disk, Power Turbine (1st Stage)

h. Disk, Power Turbine (2nd Stage)

7. Accessory Part Numbers & Total Time Since Engine Overhaul for;

a. Fuel Control Unit (FCU)

b. Fuel Heater

c. Propeller Governor

d. Compressor Bleed Valve

e. Flow Divider / Starting Control Installation

f. Fuel Pump

g. Ignition Exciter

h. Torque Limiter

File details come from the government source that posted it. Updated .