Bushings Rings Shims And Spacers » Shims (38,348 Items)

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Shims | Bushings Rings Shims And Spacers Page 654

4319194CL12 Shim SKU 5365015214874
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
4319194CL19 Shim SKU 5365015214876
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
4319194CL17 Shim SKU 5365015214878
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
4319194CL13 Shim SKU 5365015214881
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
4319194CL20 Shim SKU 5365015214882
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
4319194CL21 Shim SKU 5365015214886
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
BACS40X006D014 Material Aircraft Shim SKU 5365015215047
  • End Application: V-22 tilt rotor aircraft
4319194CL7 Shim SKU 5365015216108
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
5PTC7007A008024 SKU 5365015216113
5HF75412-143 SKU 5365015216274
7379283-1 Pillow Block Shim SKU 5365015216376
  • Hole Diameter: 0.940 inches
  • Overall Length: 5.000 inches
  • Overall Width: 3.250 inches
  • Overall Thickness: 0.120 inches
  • Center To Center Distance Between Bolt Holes Along Width: 1.870 inches
7379286-2 Laminated Aft Door Shim SKU 5365015216461
  • Overall Length: 8.000 inches
  • Overall Width: 3.450 inches
  • Overall Thickness: 0.130 inches
  • End Application: Closure door, acm/hdr seawolf class ssn 21
  • Lamination Quantity: 65
5PTC1001A24C14 SKU 5365015216592
7379272-1 Forward Door Shim SKU 5365015216736
  • Overall Length: 8.880 inches
  • Overall Width: 8.000 inches
  • Overall Thickness: 1.350 inches
  • Construction: One-piece
  • Skewed Angle: 45.0 degrees
7379273-1 Aft Door Shim SKU 5365015216795
  • Overall Length: 8.000 inches
  • Overall Width: 4.790 inches
  • Overall Thickness: 1.350 inches
  • Construction: One-piece
  • Skewed Angle: 45.0 degrees
784653 SKU 5365015217105
784653-4 SKU 5365015217108
4319195CL3 SKU 5365015217229
  • End Application: F119 engine
  • Criticality Code Justification: Feat
71205-85606-102 SKU 5365015217452
4319195CL10 SKU 5365015217559
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL7 SKU 5365015217560
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL4 SKU 5365015217561
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL6 SKU 5365015217562
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL11 SKU 5365015217563
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL8 SKU 5365015217564
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL9 SKU 5365015217565
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL13 SKU 5365015217566
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL12 SKU 5365015217568
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL15 SKU 5365015217570
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL14 SKU 5365015217571
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319195CL16 SKU 5365015217572
  • End Application: F119 engine
  • Criticality Code Justification: Feat
4319194CL3 Shim SKU 5365015217582
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
  • Special Features: Main gearbox helical gearshaft
4319194CL5 Shim SKU 5365015217584
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
  • Special Features: Main gearbox helical gearshaft
4319194CL4 Shim SKU 5365015217585
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
  • Special Features: Main gearbox helical gearshaft
4319194CL15 Shim SKU 5365015217586
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
  • Special Features: Main gearbox helical gearshaft
4319194CL11 Shim SKU 5365015217587
  • End Application: F-119-PW-100 engine on F-22 aircraft
  • Criticality Code Justification: Agav
  • Special Features: Main gearbox helical gearshaft
P103A062-10-3 SKU 5365015217704
4319195CL2 SKU 5365015217794
  • End Application: F119 engine
  • Criticality Code Justification: Feat
71205-22200-110 SKU 5365015217819
71205-22200-113 SKU 5365015217822
71205-22200-114 SKU 5365015217826
71205-22200-115 SKU 5365015217828
71205-22200-116 SKU 5365015217830
71205-22200-117 SKU 5365015217831
71205-22200-118 SKU 5365015217833
LS5909D100-0100 SKU 5365015217868
  • Overall Length: Between 0.968 inches and 1.032 inches
  • Tempurature Rating: 200.0 degrees fahrenheit
  • Overall Thickness: Between 0.091 inches and 0.106 inches
  • End Application: C130-J, aircraft
  • Lamination Quantity: 32
7642202 SKU 5365015217910
LS5909B010-0603 SKU 5365015218190
  • Overall Length: Between 6.156 inches and 6.218 inches
  • Tempurature Rating: 200.0 degrees fahrenheit
  • Overall Width: Between 0.594 inches and 0.656 inches
  • Overall Thickness: Between 0.062 inches and 0.068 inches
  • End Application: C130-J, aircraft
LS5909B010-0802 SKU 5365015218191
  • Overall Length: Between 8.094 inches and 8.156 inches
  • Tempurature Rating: 200.0 degrees fahrenheit
  • Overall Width: Between 0.594 inches and 0.656 inches
  • Overall Thickness: Between 0.062 inches and 0.068 inches
  • End Application: C130-J, aircraft
LS5909B010-1211 SKU 5365015218192
  • Tempurature Rating: 200.0 degrees fahrenheit
  • Overall Width: Between 0.594 inches and 0.656 inches
  • Overall Thickness: 0.062 inches
  • End Application: C130-J, aircraft
  • Lamination Quantity: 21

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