Solicitation_Attachment_0012_-_Critical_Characteristics.pdf

08/25/2016

70410-02561-112 1650 01 375 - 3160

Y

Y

N

N

Y

N

Y

N

Y

N

N

N

N

N

N

N

N

N

Y

Y

Y

Y

Y

Y

Y

Y

Y

Assembly contains CSI (see P/N A10807-3 and A10813-1 for additional CCs)

Embrittlement relief after chrome plate QQ-C-320 (ref drwg A10813, sheet 1, note 5, MOOG Inc)

Proper installation of Bolt and Hardware (items 10, 11, 12, 13, and 14, Fig. 3-2), joining of mating parts, safetying per NASM33540, and torque check (DMWR para 4-1.1.d) Proper installation of Link Bolt and Hardware (items 4, 5, 6, 7, 8, and 9, Fig.3-2), joining of mating parts, safetying per NASM33540, and torque check (DMWR para 4-1.1.e) Proper installation of link bolt (PN A10887-1) and hardware (DWG 70410-02561 note 20) and torque check (note 19) VerificVerification of spring stroke (minimum output, DMWR paragraph 4-3.14.f and g) and spring stroke displacement (DMWR paragraph 4-3.19t) Verification of correct hardware, joining of mating parts, safetying per NASM 33540 and torque check per 19D

Verification of maximum input override force (para 4-3.19)

Verification of minimum output stroke and maximum input override force

29242

52VE4

78286

94697

Texas Aerospace Services Inc

Overhaul Support Services LLC

Sikorsky Aircraft Corp

Moog Inc

CAGE

Critical CharacteristicsM ID

Part No NSN

Actuator Assy, PitchNoun YCritical Safety

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

Approved M&O Sources

06/08/1995CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

A10807-3 1650 01 375 - 3161

Y

Y

Y

N

N

N

N

N

Y

Y

Y

N

Assembly contains CSI see P/N A10813-1

Proper installation and flaring of rivet A10816-1 (DWG 70410-02561 note 20 and DMWR figure 3-3, item 8) per DMWR paragraph 3-15.4.a through m and 3-17.1.av.

Verification of proper installation and swaging of the A10816 rivet per para 6 of EP3250 (ref: Moog Drwg A10807)

94697 Moog Inc

CAGE

Critical CharacteristicsM ID

Part No NSN

Cylinder AssyNoun YCritical Safety

YSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

05/02/2003CSI Date

A10813-1 1650 01 095 - 7615

N

Y

N

N

Y

N

Embrittlement relief after chrome plate (DMWR paragraph 3-15.10.6.f)

Embrittlement relief after chrome plate QQ-C-320 (see dwg A10813, Note 5)

94697 Moog Inc

CAGE

Critical CharacteristicsM ID

Part No NSN

Rod Assy, PistonNoun YCritical Safety

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

Approved Replacement (Spares) Sources

12/17/2007CSI Date

A22785-2 1650 01 375 - 3160

Y

Y

N

N

Y

Y

N

Y

N

N

N

N

N

N

N

N

N

N

N

N

Y

Y

Y

Y

Y

Y

Y

Y

Y

Y

Assembly contains CSI (see P/N A10807-3 and A10813-1 for additional CCs)

Embrittlement relief after chrome plate QQ-C-320 (ref drwg A10813, sheet 1, note 5, MOOG Inc)

Proper installation of Bolt and Hardware (items 10, 11, 12, 13, and 14, Fig. 3-2), joining of mating parts, safetying per NASM33540, and torque check (DMWR paragraph 4-1.1.d) Proper installation of Link Bolt and Hardware (items 4, 5, 6, 7, 8, and 9, Fig.3-2), joining of mating parts, safetying per NASM33540, and torque check (DMWR paragraph 4-1.1.e) Proper installation of link bolt (P/N A10887-1) and hardware (DWG 70410-02561 note 20) and torque check (note 19) Verification of correct hardware, joining of mating parts, safetying per NASM33540 and torque check per 19D

Verification of maximum input override force (DMWR paragraph 4-3.19.o and DMWR paragraph 4-3.19.r)

Verification of minimum output stroke and maximum input override force

Verification of spring stroke (minimum output) and maximum input overide force

Verification of spring stroke (minimum output, DMWR paragraph 4-3.14.f and g) and spring stroke displacement (DMWR paragraph 4-3.19.t)

94697 Moog Inc

CAGE

Critical CharacteristicsM ID

Part No NSN

Actuator Assy, PitchNoun YCritical Safety

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

Approved Replacement (Spares) Sources

06/16/2005CSI Date