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EASA TCDS P.500 Binder Motorenbau GmbH BM Series Propellers 01 11022008

TCDS P.500 · EASA

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Overview

The EASA TCDS P.500 Binder Motorenbau GmbH BM Series Propellers 01 11022008 (TCDS P.500) is a freely reusable EASA document, republished here as a free chaptered HTML edition with a linked table of contents and the official PDF.

Publisher
EASA
Document
TCDS P.500
Pages
5

Key points

  • The BM series propellers are manufactured by Binder Motorenbau GmbH and are certified under Type Certificate Data Sheet P.500.
  • The propeller variant BM-G1 is a 2-blade fixed pitch propeller made of composite materials.
  • The maximum propeller speed is 2400 RPM, with a maximum driving power of 55 KW and a maximum driving torque of 150 Nm.
  • The total service time for the propeller is 400 hours, with a service time between overhauls of 200 hours.
  • The BM-G1 propeller is certified for use exclusively in powered sailplanes.
Frequently asked questions
What is the certification date of the BM series propellers?

The certification date of the BM series propellers is 11 February 2008.

What are the dimensions of the BM-G1 propeller?

The diameter of the BM-G1 propeller ranges from 140 to 160 cm, with a blade pitch of 90 to 130 cm at 75% of the radius.

What materials are used in the construction of the BM-G1 propeller?

The BM-G1 propeller is constructed of composite materials.

What are the recommended overhaul intervals for the BM-G1 propeller?

The total service time is 400 hours, with a service time between overhauls of 200 hours.

In what type of aircraft is the BM-G1 propeller certified for use?

The BM-G1 propeller is certified for use in powered sailplanes only.

Document

European Aviation Safety Agency

EASA

TYPE-CERTIFICATE

DATA SHEET

Number : P.500 Issue : 1 Date : 11 February 2008 Type : Binder Motorenbau GmbH BM series propellers Variants BM-G1 List of effective Pages: Page 1 2 3 4 5 Issue 1 1 1 1 1 TCDS P.500 Binder Motorenbau GmbH 2/5 Issue 1, 11 February 2008 BM series propellers I. General Allgemeines 1. Type / Variants: Muster/Baureihe: BM- G1 2. Type Certificate Holder: Halter der Musterzulassung : Binder Motorenbau GmbH Alter Frickenhäuser Weg 15 97645 Ostheim v.d.Rhön Germany Design Organisation Approval No: EASA.AP 129.

3. Manufacturer: Hersteller : Binder Motorenbau GmbH Alter Frickenhäuser Weg 15 97645 Ostheim v.d.Rhön Germany 4. Date of Application: Antragsdatum: 19 September 2007 5. Certification Date: Datum der Musterzulassung: 11 February 2008 II. Certification Basis Zulassungsbasis 1. Reference Date for determination of the applicable certification specifications: Bezugsdatum für die anwendbaren Bauvorschriften: 19 September 2007 2. Airworthiness Standards: Lufttüchtigkeitsforderungen: CS-22, Subpart J 3. Special Conditions (SC): Sonderforderungen: None keine TCDS P.500 Binder Motorenbau GmbH 3/5 Issue 1, 11 February 2008 BM series propellers 4. Deviations: Abweichungen:: None keine 5. Equivalent Safety Finding (ESF): Nachweise gleichwertiger Sicherheit: None keine III. Technical Characteristics Technische Merkmale 1. Type Design Definition: Musterdefinition: Type Design Definition Propeller BM Issue No. 1 dated October, 2007 (*) (*) = or later approved revisions Musterdefinition Propeller BM Ausgabe Nr.1 vom Oktober 2007 (*) (*)= oder eine spätere anerkannte Revision 2. Description: Beschreibung : 2-blade fixed pitch propeller constructed of composite materials.

2 Blatt Festpropeller, Composite Material.

3. Equipment: Ausrüstung: None keine 4. Dimensions: Abmessungen: according to the particular data in the propeller designation (see chapter 1) - diameter: 140-160 cm - blade-pitch 90-130cm (by 75 % of the radius) entsprechend den Daten der Propellerbeschreibung (siehe Kapitel 1) - Durchmesser: 140-160 cm - Blatteinstellung 90-130 cm bei 75 % vom Radius 5. Weight: Masse : max. 3,00 kg 6. Hub/Blade-Combinations: Nabe/Blatt Kombinationen : not applicable (one-piece propeller) nicht anwendbar ( Propeller einteilig) TCDS P.500 Binder Motorenbau GmbH 4/5 Issue 1, 11 February 2008 BM series propellers 7. Control System: Kontrollsystem: not applicable (fixed pitch propeller) nicht anwendbar (Festpropeller) 8. Adaptation to Engine: Anpassung an den Motor: Hub drilling according to the particular data in the propeller designation (see drawing BM-P001) Nabenbohrung entsprechend den Daten in der Propellerbeschreibung (siehe Zeichnung BM-P001) 9. Sense of Rotation: Drehrichtung: Sense of rotation (viewed in flight direction) corresponding to the particular letter in the propeller designation (clockwise looking at direction of flight) Drehrichtung (gesehen in Flugrichtung) in Übereinstimmung mit dem Abschnitt in der Propellerbeschreibung (in Uhrzeigerrichtung in Flugrichtung gesehen ) IV. Operational Limits Betriebsgrenzen 1. Propeller Speed: Propellerdrehzahl: -1 max. 2400 min 2. Driving Power: Antriebsleistung: max. 55 KW 3. Driving Torque: Antriebsmoment: max. 150 Nm V. Operating and Service Instructions Betriebs-und Instandhaltungsanweisungen Operation- and Maintenance manual for fixed pitch propeller in Glas or Carbon reinforced Plastic type BM, Issue October 21, 2007 (*) = or later approved revision Betriebs- und Wartungshandbuch für Festpropeller in Faserverbundbauweise Propellertyp BM, Ausgabe Oktober 21, 2007 (*) (*)= oder einer später anerkannten Revision.

TCDS P.500 Binder Motorenbau GmbH 5/5 Issue 1, 11 February 2008 BM series propellers VI. Notes Bemerkungen 1. The overhaul intervals recommended by the manufacturer are listed in BM Operation and Maintenance manual Die Überholungsintervalle seitens des Herstellers sind im BM Betriebs- und Wartungshandbuch aufgeführt.

Total service time: 400 hours Service time between overhauls: 200 hours Gesamtbetriebsstunden: 400 h Zwischenüberholzeit: 200 h 2. Propeller designation system Systematik der Propellerbezeichnung BM- G- 160- R- 120- 1- ( ) (1) (2) (3) (4) (5) (6) (7) where: -(1) manufacturer: Binder Motorenbau GmbH -(2) material; G= Glas C= Carbon and variant designation number -(3) propeller diameter (cm).

-(4) sense of rotation R= right L= left -(5) blade pitch at 0,75R (cm) -(6) loadclass -(7) small deviations of hub wobei: -(1) Hersteller Binder Motorenbau GmbH -(2) Werkstoff G= Glasfaser C= Kohlefaser und Nummer der Baureihe -(3) Propellerdurchmesser (cm) -(4) Drehrichtung R= rechts L= links -(5) Steigung bei 0,75 R (cm) -(6) Belastungsklasse -(7) gerigfügige Abweichung vom Nabenkörper bedeuten.

3. The propeller BM, variant G1 is certified for use in powered sailplanes only.

Der Propeller BM, Baureihe G1 ist nur für den Einsatz in Motorseglern zugelassen.

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Document details

Doc number
TCDS P.500
Publisher
EASA
Pages
5
File size
43 KB