Model: AMS-QQ-A-250/5

Metal Sheet

Properties:

Fabrication Method
Rolled
Width
48.000 inches
Length
12.000 feet
Cross-sectional Thickness
0.0800 inches
Basic Shape Style
Solid
Cladding Thickness
0.0020 inches both sides
Weight Per Unit Measure
1.150 pounds per square foot
Min. Tensile Strength (psi)
61000 pounds per square inch
Minimum Yield Strength
40000 pounds per square inch
Heat Treatment
T-3 solution heat treated
Material
Aluminum alloy ams-qq-a-250/5, alloy 2024, alclad
Material
Aluminum alloy ams-qq-a-250/5, alloy 2024, alclad
Nondefinitive Specification/std Data
T3 temper
NSN
9535-00-232-0398
Part Number
AMS-QQ-A-250/5
Description
Sheet,metal
CAGE
81343

Part AMS-QQ-A-250/5 NSN 9535-00-232-0398

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
37015
FIIG:
A13100
Concept No.:
App. Key:
AN
Cond. Code:
2
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
57.3000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
Z
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
030740
UFC:
14990
LTL:
60.0
LCL:
--
WCC:
576
TCC:
Z
SHC:
9
ACC:
Construction Materials

End Items End applications NSN 9535-00-232-0398 is a component of

  • Iroquois Uh-1 Helicopter
  • Phantom F-4 Aircraft
  • Stratofortress B-52 Aircraft
  • Hc-130) Ec-130e Mc-130h Sof ( Ac-130h Aircraft
  • Airlifter C-17a Aircraft
  • Sof / Hh-53j/m Pave Low Helicopter
  • Joint Stars Target Radar System
  • T1a Aircraft
  • Oh-58d Helicopter Observation (ahip)
  • Aircraft Mh-47e Special Operations Aircraft
  • 010883669
  • Cargo-transport Helicopter
  • 006202517
  • Cowling

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