Procurement Summary
Country : USA
Summary : C-17 Pse - Apu - Clamp Meter
Deadline : 19 May 2023
Other Information
Notice Type : Tender
TOT Ref.No.: 82007734
Document Ref. No. : FA852623Q0013
Competition : ICB
Financier : Self Financed
Purchaser Ownership : Public
Tender Value : Refer Document
Purchaser's Detail
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Description
The C-17 program management office has a requirement for a firm-fixed price contract for one (1) each NSN: 6625-01-547-4345, APU-CLAMP METER, P/N 17G245521-1, which includes one first article/production item, one first article test plan, one marking plan, and one first article test report.
The C-17 aircraft contains an auxiliary power unit (APU) that provides electrical power and pneumatic power to the aircraft when the engines are not running. These powers are used for the lighting, avionics, avionics cooling, and starting engines. The APU is a small turbine engine in the forward portion of the right wheel well pod. The APU requires constant air flow to operate. The APU inlet door allows air to flow to the APU. The inlet door needs to remain opened when the APU is running because the APU consumes a large volume of air. The APU inlet door is controlled by a rotary electro-mechanical actuator. When the inlet door is properly rigged, the rotary actuator normally would shut off at fully open or fully closed position. When the inlet door is not properly rigged, the actuator would not be shut off at fully open or fully close position and keep drawing current. In such event, it can cause the actuator to overheat and fail. When the actuator fails, the door could be sucked closed causing very low pressure inside the APU inlet ducting. This would cause an APU implosion event.
A means is required to test the current to the actuator to ensure the actuator is rigged properly at the organizational and depot level of maintenance. This measuring device shall meet the following requirements:
1. Shall be able to measure without opening any electrical connectors.
2. Shall be able to measure dc current from 0 to 1 amp.
3. Shall have accuracy and resolution to show current is less than 0.1a when door is fully closed or fully open.
4. Shall be able to fit around a 0.5” bundle of wiring.
5. Shall be portable and easy to use.
6. Shall be in...
Active Contract Opportunity
Notice ID : FA852623Q0013
Related Notice
Department/Ind. Agency : DEPT OF DEFENSE
Sub-tier : DEPT OF THE AIR FORCE
Major Command : AFMC
Sub Command : AIR FORCE LIFE CYCLE MANAGEMENT CENTER
Sub Command 2 : MOBILITY AIRCRAFT
Office : FA8526 AFLCMC WLMKA
General Information
Contract Opportunity Type: Combined Synopsis/Solicitation (Updated)
All Dates/Times are: (UTC-04:00) EASTERN STANDARD TIME, NEW YORK, USA
Updated Published Date: Apr 21, 2023 01:40 pm EDT
Original Published Date: Mar 22, 2023 03:22 pm EDT
Updated Date Offers Due: May 19, 2023 12:00 pm EDT
Original Date Offers Due: Apr 21, 2023 02:00 pm EDT
Inactive Policy: 15 days after date offers due
Updated Inactive Date: Jun 03, 2023
Original Inactive Date: May 06, 2023
Initiative: None
Classification
Original Set Aside: Total Small Business Set-Aside (FAR 19.5)
Product Service Code: 6625 - ELECTRICAL AND ELECTRONIC PROPERTIES MEASURING AND TESTING INSTRUMENTS
NAICS Code: 334515 - Instrument Manufacturing for Measuring and Testing Electricity and Electrical Signals
Place of Performance:
Documents
Tender Notice
AmendedFA852623Q0013_______0001.pdf
FA852623Q0013_22Mar23.pdf
C-17_PSE_Solicitation_Template-FA8526-XX-Q-XXXX-Rev_B.xlsx
EDL_REV4_18JAN2023.pdf
CDRLA003_IUIDMarkingPlan_17G245521.pdf
CDRLA002_InspectionOnly_17G245521.pdf
CDRLA001_InspectionOnly_17G245521.pdf
FORM_158.pdf
FORM_1653.pdf
MANDATORY_SHIPPING_DOCUMENTS.docx
Use_and_Non-Disclosure_Agreement.docx