RFQPWCPT6A-42Engines8-2019(002)_20190815130351.654_X.pdf
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- Attached to
- Pratt & Whitney Canada PT6A-42 Engine(s)
- Solicitation number
- 80LARC708399Q
About this file
Specifications.
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Other files
| File | Type | Posted |
|---|---|---|
| Q&A-20190930.pdf | ||
| N529NA_Engine_Data.pdf | ||
| RFQInstrctns-Rev1-PWCPT6A-42.docx | DOCX document | |
| RFQInstrctns-PWCPT6A-42.pdf |
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Text version
1 V2.0 9-22
SECTION 1
STATEMENT OF WORK/BID SCHEDULE
This is a Brand Name requirement for a Pratt & Whitney Canada PT6A-42
Engine(s), Exchange with current NASA Langley engine core(s).
Type of Request: Best Value Item to be purchased: One Pratt & Whitney Canada PT6A-42 Engine
Condition: Overhauled
Option for purchase: One Pratt & Whitney Canada PT6A-42 Engine (this option is for a second engine for a total purchase, with option, of 2 engines)
Condition for Option: Overhauled
Deliverables Prior to Award: Engine Record 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
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