AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
Part Number NX12290PC2 described as Lever Remote Control with NSN 2990-00-363-8093 with FSC 2990 Miscellaneous Engine Accessories Nonaircraft by Manufacture General Motors Corp is available in stock. We provide comprehensive database of aerospace and aviation components, sub-assemblies, and completed assemblies allows us to respond to your RFQ within 15 minutes.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2990-00-363-8093 Item Description: LEVER,REMOTE CONTROL | 2990 | 003638093 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 5151519 | 5 | 1 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | OVERALL WIDTH | 0.875 INCHES NOMINAL" |
| ABRR | KEYWAY WIDTH | 0.095 INCHES MINIMUM AND 0.105 INCHES MAXIMUM" |
| ABXV | BORE DIAMETER | 0.500 INCHES MINIMUM AND 0.503 INCHES MAXIMUM" |
| ADGE | BORE LENGTH | 0.500 INCHES NOMINAL" |
| AFYS | KEYWAY LENGTH | 0.094 INCHES NOMINAL" |
| AGAV | END ITEM IDENTIFICATION | GRUMMAN AIRCRAFT,MODEL A10 AND GENERAL MOTORS CORP,LIGHT ARMORED VEHICLE MODEL LAV-25; GOVERNOR, DIESEL ENGINE" |
| ASBP | BORE TYPE | PLAIN STRAIGHT" |
| BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.250 INCHES NOMINAL" |
| BFGX | SHAFT END THICKNESS | 0.344 INCHES NOMINAL" |
| BFGY | LINK END THICKNESS | 0.319 INCHES MINIMUM AND 0.320 INCHES MAXIMUM" |
| BFHA | LINK END HOLE DIAMETER | 0.311 INCHES MINIMUM AND 0.314 INCHES MAXIMUM" |
| CBBL | FEATURES PROVIDED | KEYWAY" |
| CZLP | SHAFT SECURING METHOD | KEYWAY" |
| FEAT | SPECIAL FEATURES | OFFSET HEIGHT: 0.375 IN. NOMINAL" |
| MATT | III MATERIAL | STEEL" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | SAE 1117 ASSN STD 1ST MATERIAL RESPONSE OR SAE 1118 ASSN STD 2ND MATERIAL RESPONSE" |
| ABMK | OVERALL WIDTH | 0.875 INCHES NOMINAL" |
| ABRR | KEYWAY WIDTH | 0.095 INCHES MINIMUM AND 0.105 INCHES MAXIMUM" |
| ABXV | BORE DIAMETER | 0.500 INCHES MINIMUM AND 0.503 INCHES MAXIMUM" |
| ADGE | BORE LENGTH | 0.500 INCHES NOMINAL" |
| AFYS | KEYWAY LENGTH | 0.094 INCHES NOMINAL" |
| AGAV | END ITEM IDENTIFICATION | GRUMMAN AIRCRAFT,MODEL A10 AND GENERAL MOTORS CORP,LIGHT ARMORED VEHICLE MODEL LAV-25; GOVERNOR, DIESEL ENGINE" |
| ASBP | BORE TYPE | PLAIN STRAIGHT" |
| BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.250 INCHES NOMINAL" |
| BFGX | SHAFT END THICKNESS | 0.344 INCHES NOMINAL" |
| BFGY | LINK END THICKNESS | 0.319 INCHES MINIMUM AND 0.320 INCHES MAXIMUM" |
| BFHA | LINK END HOLE DIAMETER | 0.311 INCHES MINIMUM AND 0.314 INCHES MAXIMUM" |
| CBBL | FEATURES PROVIDED | KEYWAY" |
| CZLP | SHAFT SECURING METHOD | KEYWAY" |
| FEAT | SPECIAL FEATURES | OFFSET HEIGHT: 0.375 IN. NOMINAL" |
| MATT | III MATERIAL | STEEL" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | SAE 1117 ASSN STD 1ST MATERIAL RESPONSE OR SAE 1118 ASSN STD 2ND MATERIAL RESPONSE" |
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