• Wishlists
  • 877-477-7823
  • Contact Us
 
 
THE AVIATION SUPERSTORE FOR ALL YOUR AIRCRAFT & PILOT NEEDS | 877-4-SPRUCE

AEROQUIP NIPPLE ASSEMBLY

From $21.50 to $102.75
Description Part Number Price Buy
EATON NIPPLE ASSEMBLY AE21496B AE21496B $29.50
Quantity
EATON NIPPLE ASSEMBLY AE21496E 05-11822 $21.50
Quantity
EATON NIPPLE ASSEMBLY AE21496F 05-11823 $30.50
Quantity
EATON NIPPLE ASSEMBLY AE21496G 05-11824 $30.50
Quantity
EATON NIPPLE ASSEMBLY AE21496H 05-11825 $32.50
Quantity
EATON NIPPLE ASSEMBLY AE21496J 05-11826 $48.95
Quantity
EATON NIPPLE ASSEMBLY AE21496K 05-11827 $59.75
Quantity
EATON NIPPLE ASSEMBLY AE21496M 05-11828 $102.75
Quantity
Subtotal $0.00
Add to Wishlist

Overview

Compression crimp fittings are available in both flared and flareless types to mate with (AS4395) and (AS4375) end connections. In addition, elbow fittings are available in standard 45° and 90° styles. Special elbows, crosses, tees, wyes, adapters, bosses, etc. may be made for customer installations. The unique combination of the “ramped” nipple and the crimping pattern used on the compression crimp fitting results in superior fitting retention under pressure. Burst pressure tests indicate that extreme pressures will result in “free hose” bursts rather than fitting blow-off. The fitting design effectively traps and holds the wire reinforcement of the hose in the area of the ramp on the fitting nipple.

Works with AE21498 Socket, see Accesories tab for part number, (letter size code same as nipple assembly).

Specifications

AEROQUIP THREAD SIZE THREAD MAX DIM A DIM B DIM C MIN I.D. FTG WT (LB)
AE21496B -4 0.4375-20 UNJF-3B 1.12 0.25 0.37 0.132 0.05
AE21496E -3 0.3750-24 UNJF-3B 1.12 0.24 0.34 0.09 0.039
AE21496F -5 0.5000-20 UNJF-3B 1.26 0.31 0.38 0.193 0.065
AE21496G -6 0.5625-18 UNJF-3B 1.37 0.34 0.38 0.256 0.078
AE21496H -8 0.7500-16 UNJF-3B 1.53 0.44 0.43 0.34 0.137
AE21496J -10 0.8750-14 UNJF-3B 1.75 0.56 0.5 0.43 0.191
AE21496K -12 1.0625-12 UMJF-3B 1.96 0.46 0.57 0.548 0.297
AE21496M -16 1.3125-12 UNJF-3B 2.32 0.6 0.6 0.778 0.464

Documents

Reviews

Q&A