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Part Information
Continuity test of the impact sensor assembly is required to impact sensor test; a pre-power static manually measure the impact sensor loop and the ordnance alarm loop circuit continuity. The impact sensor loop continuity resistance is not to exceed 2.0 ohms. The ordnance alarm loop continuity resistance is not to exceed 1.0 ohm.Afm-124
| Part Number | RNVC | RNAAC | DAC | CAGE |
|---|---|---|---|---|
| 40A91490-1 | 2 | ZZ | 2 | 98748 |
| Code | Definition |
|---|---|
| FN | Factory New. Parts manufactured by then OEM and includes manufacturer certification. |
| NE | New. Parts manufactured by the OEM. May include manufacturer certification or company certification. |
| NS | New Surplus. New material item purchased from excess inventory. |
| OH | Overhauled. Product has been rebuilt and tested in accordance with the manufacturer's specifications by a repair shop (MRO). |
| SV | Serviceable product. |
| AR | As Removed. Product removed from aircraft or platform with no guarentee on the functionality of the part. |
| RP | Repairable. Product can be repaired by a MRO and be given a FAA 8130 or EASA Form 1 certification. |