Technical Data Sheet B-00371-1
MAULE M-5-180C · Parts Catalog
Overview
This document is a parts catalog for the Maule M-5-180C aircraft, detailing the specifications and eligibility of a 14V single engine alternator control. It includes technical data, operational notes, and a list of compatible aircraft models.
- The alternator control is factory set to 14.0V.
- Maximum load current is 5A.
- Over-voltage trip point is set at 16.0V.
- The unit weighs a maximum of 0.3 lb.
- Dimensions are 3.5"L x 3.125"W x 1.75"H.
- Includes over-voltage protection that latches off the regulator output.
- Self-protected against damage from shorted output circuits.
- Compatible with various aircraft models including the Maule M-5-180C.
Document
Source
Originally published by cdn-website.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Parts Catalog
- File size ·
- 25 KB
- Publisher ·
- cdn-website.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Weight (lb) ·
- 0.3
- Dimensions (in) ·
- 3.5L x 3.125W x 1.75H
What is the Technical Data Sheet B-00371-1?
The Technical Data Sheet B-00371-1 is a parts catalog for the MAULE M-5-180C.
Where does the Technical Data Sheet B-00371-1 come from?
This copy of the Technical Data Sheet B-00371-1 was originally published by cdn-website.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the MAULE M-5-180C.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Technical Data
Details specifications such as voltage, load current, over-voltage trip point, and dimensions of the alternator control.
Operation Notes
Cautions regarding the use of the alternator control, including warnings against bypassing the bus to field.
Part Number and Aircraft Eligibility
Lists the part number B-00371-1 and various aircraft models compatible with the alternator control.
Safety notes
- Do not bypass bus to field when checking the alternator.
- Over-voltage protection latches off regulator output after an event.
- A shorted output will latch off until reset.
- Restoration of output requires momentary turn off of supply voltage.
Full document text
NOTE: Installer must cross-check eligibility with applicable technical data. Data Sheet B-00371-1.A Technical Data Sheet B-00371-1 14V SINGLE ENGINE ALTERNATOR CONTROL Duty Voltage Factory Set To Load Current Over-Voltage Trip Point Over-Voltage Trip Time Weight Dimensions Continuous PWM 14.0V 5A Max. 16.0V 0.5V Above Trip Point = 0.50 seconds; 3.0V Above Trip Point = 0.15 seconds 0.3lb Max. 31/2”L x 31/8”W x 13/4”H PINOUT FUNCTION Red Black Blue Supply, 14V Nominal from alternator switch/field circuit breaker Ground Output, Field terminal of alternator OPERATION NOTES DESCRIPTION Note 1: Note 2: Note 3: Note 4: Operating Caution: When used with an operating alternator, do not bypass bus to field as a means of checking the alternator or the over-voltage protection action. Over-voltage protection is incorporated which latches off regulator output after an over-voltage event. This unit is self protected against damage due to output (field) circuit being shorted to ground. A short will latch output off until reset. Rest of latch off caused by either over-voltage or shorted output is accomplished by momentary turn off of supply voltage. PART NUMBER AIRCRAFT ELIGIBILITY B-00371-1 557-337 B-00371-2 B-00371-4 B-00371-5 B-00371-7 B-00371-8 B-00371-9 B-00371-10 B-00371-11 B-00371-12 B-00371-13 B-00371-14 B-00371-15 B-00371-16 Piper 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-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, Zenair CH2000, Robinson R22, R22 Alpha, R22 Beta, R22 Mariner, Taylorcraft 2000 BC, BCS, BC-65, BCS-65, BC12-65 (Army L-2H), BCS12-65, BC12-D, BCS12-D, BC12-D1, BCS12-D1, BC12D- 85, BCS12D-85, BC12D-4-85, BCS12D-4-85, 19, F19, F21, F21A, F21B, F22, F22A, F22B, F22C, Socata TB 9, TB 10, TB 20, TB 21,TB 200, TBM 700, Apex Aircraft(Avions Pierre Robin – France/Canada) R3000/160, (Avions Mudry) CAP10B, Alpha Aviation Concept(Avions Pierre Robin – France/Canada) R2160, Maule M-4, M-4C, M-4S, M-4T, M-4-180C, M-4-180S, M-4-180T, M-4-210, M-4-210C, M-4-210S, M-4-210T, M-4-220, M-4-220C, M-4-220S, M-4-220T, M-5-180C, M-5-200, M-5-210C, M-5-210TC, M-5- 220C, M-5-235C, M-6-180, M-6-235, M-7-235, M-7-235A, M-7-235B, M-7-235C, M-7-260, M-7-260C, M-7- 420A, M-7-420AC, M-8-235, MT-7-235, MT-7-260, MT-7-420, MX-7-160, MX-7-160C, MX-7-180, MX-7- 180A, MX-7-180AC, MX-7-180B, MX7-180C, MX-7-235, MX-7-420, MXT-7-160, MXT-7-180, MXT-7-180A, Enstrom F-28, F28A, F-28C, F-28C-2, F-29C-2R, F-28F, F-28F-R, 280, 280C, 280F, 280FX, 480, 380B, TH-28, Slingsby Aviation T67M260, T67M260-T3A, FFA AS 202/15 “Bravo”, AS 202/18A “Bravo”, AS 202/18A4 “Bravo”, Vulcanair S.p.A.(Partenavia) P68, P68B, P68C, P68C-TC, P68 ”Observer”, AP68TP300 ”Spartacus”, P68TC ”Observer”, AP68TP 600 “Viator”, P68 “Observer 2”, American Champion 11AC, S11AC, 11BC, S11BC,7AC, 7ACA, S7AC, 7BCM, 7CCM, S7CCM, 7DC, S7DC, 7EC, S7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7HC, 7JC, 7KC, 7KCAB, 8KCAB, 8GCBC, Brantly (YHO 3BR) B-2, B-2A, B-2B, 305