Humidity-temperature Probes - Page 2 of 8
186 part numbers
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pacer special end application
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feat criticality code justification
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hardness critical item special features
M26
NSN 6685-01-268-6638
Cross Reference:
2D62066PK
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3.624 inches overall length
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missile mx peacekeeper end application
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f100/f200 engines end application
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f100 engine end application
B-18453-11
NSN 6685-01-291-1041
Cross Reference:
C-18453-11
709B504G02
NSN 6685-01-299-9118
Cross Reference:
688J400PC36
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zzzy criticality code justification
230N-120
NSN 6685-01-299-9842
Cross Reference:
688J400PC75
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ready for back transfer; j6r; 4-28-2008. special features
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6530-00-890-1976 end application
123SCEC5165-5
NSN 6685-01-317-4639
Cross Reference:
EEWB517A, JOHN BEAN#3.5
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13.940 inches overall length
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aircraft model e-2c end application
5875W47G802
NSN 6685-01-324-3910
Cross Reference:
10173029
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6.640 inches overall length
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engine model f-404 end application
23031050
NSN 6685-01-326-2418
Cross Reference:
153BK2
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engine model t-56 end application
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mtg flange with two (2) holes special features
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zzzy criticality code justification
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zzzy criticality code justification
5875W47G801
NSN 6685-01-327-3627
Cross Reference:
10173030
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6.640 inches overall length
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engine model f-404 end application
22197
NSN 6685-01-328-7691
Cross Reference:
5001-113, M2
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35 thrust stand end application
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66.56 max lg; special features
2979A
NSN 6685-01-334-1164
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engine, aircraft -f108 (cfm-56), (kc-135r) end application
G1C-200-WRSS
NSN 6685-01-335-4449
Cross Reference:
27255, RCT9500
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between 1.835 inches and 1.875 inches overall length
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-65.0/+500.0 degrees fahrenheit operating tempurature range
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et f112-wr-100 e end application
2977A
NSN 6685-01-335-7827
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engine, aircraft -f108 (cfm-56), (kc-135r) end application
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6640-01-084-7374 end application
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for use on incubator; model 351820 special features
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6640-01-084-7374 end application
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for use on incubator; model 351820 special features