ATTACHMENT_0002_Critical_CharacterIstics.pdf

PDF 11 KB Posted

Attached to
Solicitation for the Overhaul/ Upgrade of the UH-60 Cylinder Assembly Actuator
Solicitation number
W58RGZ-19-R-0047
Issued by

About this file

This document contains a federal solicitation for the overhaul and upgrade of UH-60 aircraft components. The solicitation requests proposals for the inspection, overhaul, and upgrade of Cylinder Assembly Actuators and related parts for UH-60 helicopters. The contractor shall provide all required labor, materials, equipment, and facilities. The procurement is restricted to Sikorsky Aircraft Corporation and is a five-year firm-fixed-price indefinite delivery/indefinite quantity contract for a minimum of 60 units and maximum of 2,100 units annually. Proposals are due by the estimated closing date listed in the solicitation. The contractor must overhaul and upgrade the units in accordance with approved specifications and perform a required Product Verification Audit.

ATTACHMENT 0002 Critical Characteristics.pdf

View the file

Other files

Show all 17

On GovTribe

Work with this file

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file

Text version

09/06/2018

70410-02561-115 1650 01 647 - 4590

Y

Y

N

N

Y

Y

Verification of correct hardware, joining of mating parts, safetying per MS 33540, and torque check per note 19D is a C.C.

Verification of minimum output stroke and maximum input override force per Note 12 is a C.C. Force Requirements: EXTEND Direction, not to exceed 51.2 LBS. RETRACT Direction, not to exceed 51.2 LBS.

Stroke Requirement: EXTEND Direction, 2.400 IN. MIN, RETRACT Direction, 2.400 IN. MIN.

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

ActuatorNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved M&O Sources

09/15/2015CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

11/14/2018

FB765PRID 70410-02561-115Part Number

1650-01-647-4590NSN UH-60System

CYLINDER ASSEMBLY ACTUATORNomenclature

NAdequate DMWR Available?

DMWR ID

DMWR Date

DMWR Chg #

NPre-Award Survey Recommended?

NCorrelation Performance Study Required ? YPVA Recommended?

DMWR 1-1650-385 does not cover the P/N 70140-02561-115 (UH-60M) configuration. This configuration changes the piston from chrome to HVOF, improved the housing mounting feet, replaces the dust boot with an upgraded end cap, redesigns the piston crank and uses different seals throughout the assembly. The instructions in the DMWR are not adequate to overhaul this configuration.

Identify Any Special Processes, Test Procedures, and/or Instructions

YCritical Safety Item?

There are no emerging airworthiness issues, no issues related to ECPs affecting the CSI status, and no concerns over reliability/durability for the UH-60 Cylinder Assembly Actuator at the time of this review.

Special Airworthiness Considerations

AED Notes: AEM Sustainment verified the CSI/NST status through the ARISE data base on 8/1/2018 and the part is CSI and NST. Engineering Testing of fatigue, endurance and interchange are not required for overhaul.JC

Other Requirements / Comments

78286If the item is not a CSI and no adequate DMWR is available, approved sources, if any, are listed by CAGE as follows:

NSpecial Post-Contract Award Requirements?

Special Post-Contract Award Requirements

The Prime or OEM is required to submit a Frozen Plan 30 days after contract award to Engineering Directorate (ED) and Aviation Engineering Directorate (AED). The Frozen Plan will be reviewed and require approval by ED and AED prior to government acceptance of contract deliverable assets.

Other Requirements / Comments (Part II)

No DMWR is available. Recommend contacting UH-60 PM IUID Office, Marty Charlier at (256) 955-9735, for any updates and/or waiver/deviation of IUID Contracting DFAR clauses on the IUID marking of the Cylinder Assembly Actuator.

Other Requirements / Comments (Part III)

AED Notes: AEM Sustainment reconfirmed the CSI/NST status through the ARISE data base on 8/29/2018 and the part is Stil CSI and NST. Engineering Testing of fatigue, endurance and interchange are not required for overhaul. There are no required changes.JC

Other Requirements / Comments (Part IV)

AED Notes: AEM SUSTAINMENT REMOVED MOOG INC. CAGE 94697 AND REPLACED WITH SIKORSKY AIRCRAFT CORP CAGE 78286 ON 11/14/2018. THIS IS A CSI COMPONENT THEREFORE THE SOURCE MUST SUBMIT A SAR, GO THROUGH THE SAR REVIEW PROCESS, AND ONCE ALL REQUIREMENTS ARE MET THEN A SOURCE CAN BE ADDED TO THE ARISE CIM DATABASE. THE ONLY RECOGNIZED M&O SOURCE IN THE ARISE CIM DATABASE IS SIKORSKY

AIRCRAFT CORP CAGE 78286.JC

Other Requirements / Comments (Part V)

YDoes QE-STD-2 Apply?

N

Additional CSI Requirements

CSI Contains CSI Replacement Parts? YEngineering Testing Required?

The solicitation/RFP shall require that all proposals/responses include a special tooling and test equipment section that addresses the contractor's plan to meet all government special tooling and test equipment requirements with either:

1. Physical possession of the required tools, 2. Confirmed requisitions for the required tools, 3. Confirmed arrangements for subcontracting the processes requiring the special tools, or 4. Specific plans describing their technical approach to develop equivalent tools.

RStatus

NTDPL?

09/15/2015Approved Date

M&O AED REQUIREMENTS DATA

Commerciality Determination

Commercial Item? N NBest Commercial Practice Acceptable?

FB765PRID 70410-02561-115Part Number

1650-01-647-4590NSN UH-60System

Not Applicable.

Critical Tools and Test and Inspection Equipment Requiring AED Approval for Substitutes

MEOs Required for Competitive Contract?

RStatus

Correlation Performance Study Requirements

70410-02561-115 1650 01 647 - 4590

Y

Y

N

N

Y

Y

Verification of correct hardware, joining of mating parts, safetying per MS 33540, and torque check per note 19D is a C.C.

Verification of minimum output stroke and maximum input override force per Note 12 is a C.C. Force Requirements: EXTEND Direction, not to exceed 51.2 LBS. RETRACT Direction, not to exceed 51.2 LBS.

Stroke Requirement: EXTEND Direction, 2.400 IN. MIN, RETRACT Direction, 2.400 IN. MIN.

78286 Sikorsky Aircraft Corp

CAGE

Critical CharacteristicsM ID

Part No NSN

ActuatorNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue NEndurance NInterchange

Approved M&O Sources

09/15/2015CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

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