B-00368-2 LAMAR ALT CONTROL
Part #: B-00368-2
B003682
$643.10
Overview
| The Lamar MC10 is a master electrical control unit developed for 14V and 24V single engine experimental aircraft. It is designed to mount on the firewall or fuselage. It houses all the major electrical components except for the battery, starter, and alternator. The MC10 provides a greater degree of protection against moisture, dust and accidental electrical shorts along with the convenience of all the primary electrical components in one location. Features low installation cost, ease of installation and simplified troubleshooting and repair with several new performance and safety features.
* All astricked items are available through OEM only. |
Alternate Part Numbers
Part number B-00368-2 has 1 known alternate, superseded or replacement part number. Search any of them, or call, text or WhatsApp +1 (954) 493-5088 for availability.
| Part Number | Manufacturer | Relationship | Notes |
|---|---|---|---|
| 584-290 | Piper | Replaces OEM Part | FAA-PMA eligibility: Piper Aircraft, Inc. PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28-201T, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-20 … (see FAA record); basis: identicality; 2 current supplements |
Alternate and superseded part numbers are listed for reference from FAA PMA data, manufacturer cross-references and illustrated parts catalogs. Always confirm eligibility for your aircraft, engine and serial number before installation.
| Weight | .458 lbs |
|---|---|
| Dimensions | 6.63 × 4 × 2.375 in |
| Brands |
Specifications
Piper PA28-240, PA28-150, PA28-151, PA-28-160, PA-28-161, PA-28-180, PA28-181, PA-28-201T, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-28S-160, PA-28S-180, PA-32-260, PA-32-300, PA-32-301, PA-32-301FT, PA-32-301T, PA-32-301XTC, PA-32R-300, PA-32R-301(HP), PA-32R-301(SP), PA-32R-301T, PA-32RT-300, PA-32RT-300T, PA-32S-300, PA-38-112
Functions
- Master (battery) (solenoid) control closing the master switch on pilot’s panel connects the battery to the primary bus
- 3 aircraft bus outputs, protected via resetable circuit breakers
- Alternator Control; voltage regulation, overvoltage protection, field output over-load protection, alternator feeder fault protection
- Starter control (solenoid)
- Low voltage warning.(L model also includes overvoltage, over-current and reverse-current annunciation)
- Battery charge/ discharge ammeter drive (current shunt)
- Clock output (always-on) pro-tected with easily accesible external mounted fuse
- Ground power receptacle & control (solenoid) with reverse polarity protection
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