# TCDS P9BO: Hoffmann GmbH & Co. KG - Type: Type certificate data sheet - Status: Current - Holder: Hoffmann GmbH & Co. KG - Revision: 1 - Revised: March 12, 2007 - Product: Propeller - Certification basis: Part 21, Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/94/8d/948d713236a72f8115d5ecf8b2497d4cd7e9701952b96e6956c10ab39b1d34c7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C9C1855FD9FA27C78625729F006C3B18.0001 - Page: https://openairdocs.org/tcds/P9BO ## Models (1) As the data sheet lists them. - HO-V 72 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text PAGE 1 2 3 4 REV. 1 1 1 1 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P9BO TCDS NUMBER: P9BO REVISION: 1 HOFFMANN HO-V 72 March 12, 2007 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P9BO) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. TYPE CERTIFICATE HOLDER Hoffmann GmbH & Co.KG Kuepferlingstr. 9 D-83022 Rosenheim Federal Republic of Germany TYPE Constant speed, hydraulic HUB MATERIAL Aluminum alloy BLADE MATERIAL Laminated wood composite structure, epoxy-fibre glass cover with metal tipping NUMBER OF BLADES Two HUB MODEL ELIGIBLE HO-V 72 CERTIFICATION BASIS FAR 21.29, FAR Part 35 of Feb. 1st, 1965, Amdt. 35-1 thru 35-2. Luftfahrt-Bundesamt (LBA) originally type certificated this propeller under its type certificate Number 32.130 / 019. The FAA validated this product under U.S. Type Certificate Number P9BO. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the Federal Republic of Germany. TC (IMPORT) NO: LBA-Data Sheet No. 32.130 / 019, Feb. 4th, 1975 TC APPLICATION DATE: August 1, 1995 TC ISSUED: January 26, 1996 IMPORT REQUIREMENTS: To be considered eligible for installation on U.S. registered aircraft, each propeller to be exported to the United States shall be accompanied by a Certificate of Airworthiness for export endorsed by the LBA on behalf of the European Community which contains the following language: (1) This propeller conforms to its United States type design (Type Certificate Number P9BO) and is in a condition for safe operation. (2) This propeller has been subjected by the manufacturer to a final operational check and is in a proper state of airworthiness. Reference FAR Section 21.500 which provides for the airworthiness acceptance of aircraft engines or propellers manufactured outside the U.S. for which a U.S. type certificate has been issued. Additional guidance is contained in FAA Advisory Circular 21-23, Airworthiness Certification of Civil Aircraft, Engines, Propellers and Related Products, imported into the United States. P9BO 2 OPERATION LIMITS HUB-BLADE-COMBINATION, MEASUREMENTS, WEIGHT HUB (MODEL) HO-V 72 PROPELLER BLADE P at n MD HP kW] [rpm] P at n ST HP [kW] [RPM] DIAMETER LIMITS inches [cm] BLADE TWIST LIMITS IN DEG.* min. max. WEIGHT lbs. [kg] G 170 CK 158 118 2800 158 118 2800 66.9 ± 5.9 170±15 5 45 30 13.6 170 DW 158 118 2800 158 118 2800 66.9 - 3.9 170-10 5 45 30 13.6 L 170 U 158 118 2800 158 118 2800 66.9 ± 5.9 170±15 5 45 30 13.6 170 DW 158 118 2800 158 118 2800 66.9 - 3.9 170-10 5 45 30 13.6 170 CK 158 118 2800 158 118 2800 66.9 - 3.9 170-10 5 45 30 13.6 F 180 CB 158 118 2800 158 118 2800 70.9 - 3.9 180-10 5 45 30 13.6 B 170 DU 116.7 87 2800 116.7 87 2800 66.9 ± 5.9 170±15 5 45 30 13.6 170 DW 116.7 87 2800 116.7 87 2800 66.9 - 3.9 170-10 5 45 30 13.6 170 CK 116.7 87 2800 116.7 87 2800 66.9 - 3.9 170-10 5 45 30 13.6 180 CB 116.7 87 2800 116.7 87 2800 70.9 - 3.9 180-10 5 45 30 13.6 P : Max. take off power ST P : Max. continuous power MD n: RPM r: Propeller radius *) The data of the blade twist lim its is valid for a propeller radius 0.2 through 1.0 r. **) Difference in weight to the basic model: HO-V 72()()-A-(): +1.0 kg (+2.2 lbs) HO-V 72()()-V-(): +2.4 kg (+5.3 lbs) Equipment: Governor, spinner and de-icing system according to manufacturer's list. NOTES NOTE 1. Hub Model Designation HO V 7 2 L () - () -() ___ __ _ _ _ __ __ __ 1 2 3 4 5 6 7 8 1. Hoffman Propeller GmbH & Co. KG 2. Variable pitch propeller 3. Number of model 4. Number of blades 5. Designation of the flange F = ARP 502 Type I B = AS 127D (SAE No. 1) G = SAE No. 2 mod., 6 ea 3/8" - 24 UNF bolts L = SAE No. 2 mod., 6 ea 7/16" - 20 UNF bolts 3 TCDS NO. P9BO 6. Number for hub extension from blade axis to flange, blank = 130 mm (5.1 inches) 1 = 160 mm (6.3 inches) 2 = 179 mm (7.0 inches) 7. Blank = oil pressure to increase pitch F = oil pressu re to increase pitch, with counterweights S = oil pressure to decrease pitch, counterweights to increase pitch until feathering V = oil pressure to decrease pitch, counterweights to increase pitch A = automatic pitch change system, counterweights to increase pitch 8. Minor changes, not affecting interchangeability NOTE 2. Blade Model Designation () 180 CB () - () () ± () __ ___ ___ __ __ __ __ 1 2 3 4 5 6 7 1. Blank = righthand tractor D = righthand pusher L = lefthand tractor LD = lefthand pusher V = changed position of the p itch change pin for oil pressure to decrease pitch 2. Basic diameter in cm 3. Designation of blade drawing 4. Designation of blade twist (small letter) 5. B = electrical de-icing 6. Material of blade blank = compreg - spruce P = compreg 7. Deviation of basic diameter in cm NOTE 3. Pitch Control Eligible with the following governors: Woodward model (X)210-XXX w. 2.5 lb. NOTE 4. (a) Feathering Not applicable (b) Reversing Not applicable NOTE 5. Left-hand Models The left-hand version of an approved model propeller is eligible at the same rating and diameter as listed for the right-hand model. See Notes 1 and 2. NOTE 6: Interchangeability Not applicable NOTE 7: Accessories (a) Propeller anti-icing: Not applicable. (b) Propeller spinners: According to appr oved Hoffman Propeller parts list;, Wt. 4.0 lbs. NOTE 8. Shank Fairings. Not applicable P9BO 4 NOTE 9. Table of Propeller - Engine combinations approved vibrationwise for use on normal category single-reciprocating tractor aircraft. Hub Blade-Type Diameter [inches] [cm] Engine Limitations HO-V72L ()17OU 68.9 175 LYC, O-320 E1A, E1C NONE ()180CB ()180DU 70.9 180 LYC, AEIO-320 D1B NONE HO-V72G ()170CK 66.9 170 LYC, O-320 A1A NONE HO-V72F 170DW 66.9 170 ROTAX 912-F3 NONE NOTE 10. Special Notes. The word "eligible" as used herein does not signify full installation approval. Compliance with the applicable engine and aircraft FAR requirements is necessary before full approval for use on aircraft can be given. NOTE 11: Service Information. Each of the documents listed below must state that it is approved by the European Aviation Safety Agency (EASA) or – for approvals made before September 28, 2003 – by the LBA. Any such documents are accepted by the FAA and are considered FAA approved. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. -END- ``` ## ADs (3, in force first) - [AD 2022-21-13](https://openairdocs.org/ad/2022-21-13): Propeller Hub Section · Hoffmann HO-V 72. Effective Dec 6, 2022 - [AD 2021-23-17](https://openairdocs.org/ad/2021-23-17) (historical): Propeller Hub Section · Hoffmann HO-V 72. Effective Jan 10, 2022 - [AD 2020-25-05](https://openairdocs.org/ad/2020-25-05) (historical): Propeller Hub Section · Hoffmann HO-V 72. Effective Dec 22, 2020 ## STCs approved under this data sheet (1) - [STC SP01222WI](https://openairdocs.org/stc/SP01222WI): Installation of Aircraft Development propeller vortelators.. Aircraft Development Co --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.