# TCDS H6NE: Eurocopter Canada Limited - Type: Type certificate data sheet - Status: Historical - Holder: Eurocopter Canada Limited - Revision: 4 - Revised: January 25, 2010 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheet PDF: https://openairdocs.org/files/sha256/f1/16/f1168f2c267a7b1fff84b66d46d7d651f41a8b228b46d4eb2a0e58987948e729 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AFAB7B46AB67081A862576DA00567520.0001 - Page: https://openairdocs.org/tcds/H6NE ## Models (1) As the data sheet lists them. - BO 105 LS A-3 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text This Type Certificate Data Sheet (TCDS) is canceled effective January 25, 2010. Superseded by TCDS H3EU, dated November 24, 2009. Page No. 1 2 3 4 Rev. No. 4 4 4 4 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION H6NE Eurocopter Canada Ltd. BO 105 LS A-3 January 25, 2010 Revision 4 TYPE CERTIFICATE DATA SHEET NO. H6NE This data sheet which is a part of Type Certificate No. H6NE prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal Air Regulations. Type Certificate Holder. Eurocopter Canada Limited 1100 Gilmore Road P.O. Box 250 Fort Erie, Ontario Canada L2A 5M9 Model BO 105 LS A-3 (Normal Category) Helicopter, approved October 1, 1986 (see Note 9) Engines 2 Allison Model 250-C28C Fuel MIL-T-5624 Grade JP-4 and JP-5 ASTM-D-1655A ASTM-D-1655A-1 ASTM-D-1655B (see NOTES 4 and 5) Installed Engine Limits Allison Model 250-C28C (See NOTE 7) Output Shaft Gas Generator Output Shaft Measured Torque Speed - N1 Speed - N2 Gas Temp. % (FT-LBS) % (RPM) % (RPM) C° (°F) Normal Operation - Take-off Power ( min.) 75 (363) 104 (52980) 102 (6136) 791 (1455) - Maximum Continuous 72 (344) 104 (52980) 102 (6136) 741 (1365) One Engine Inoperative - Power (2.5 min.) 100 (481) 104 (52980) 102 (6136) 810 (1490) - Maximum Continuous 90 (432) 104 (52980) 102 (6136) 791 (1455) See FLM for other limitations including speed and temperature transients. Rotor Limits Power off Maximum 442 rpm (Triple tach. reading 104%) Minimum 361 rpm (Triple tach. reading 85%) Power on Maximum 433 rpm (Triple tach reading 102%) Minimum 424 rpm (Triple tach reading 100%) above 8000 ft. Minimum 416 rpm (Triple tach reading 98%) below 8000 ft. See FLM for transient limits. H6NE This Type Certificate Data Sheet (TCDS) is canceled effective January 25, 2010. Superseded by TCDS H3EU, dated November 24, 2009. 2 Airspeed Limits Never Exceed Speed Vne (CAS) - 145 Knots (167 m.p.h.) Decrease Vne with altit ude in accordance with FLM Vne for steady autorotation is limited to 90 Knots (104 m.p.h.) or less (See FLM) C.G. Range Longitudinal C.G. Limits: Max. forward up to 1800 kg: (3968 lbs.): 3081 mm aft of RB Max. forward up to 2000 kg: (5732 lbs.): 3140 mm aft of RB Max. rearward up to 2600 kg: (5732 lbs.): 3245 mm aft of RB Max. rearward up to 2000 kg: (4409 lbs.): 3395 mm aft of RB Straight Line varia tion between points given. Lateral CG Limits: 100 mm/3.9 in, left or right of longitudina l plane of symmetry of the helicopter for weights up to 5291 lbs. (2400 kg) 80 mm/3.15 in for weights greater than 5291 lbs. (2400 kg). Empty Weight C.G. Range None Maximum Mass 2600 kg/5732 lbs. Minimum Crew 1 at 1481 mm to 1681 mm/58.3 to 66.2 in. Passengers 1 at 1735 mm to 1935 aft RD/68.3 in. to 76.2 in. 3 at 2690 mm aft RD or 4 at 2550 mm aft RD if the optional equipment "Back to Back 4 Seat Bench" (MBB 105-826601) is installed. Maximum Baggage Small compartment: 20 kg at 4250 mm aft RD/44.0 lbs. at 167.3 in. aft RD. Cargo compartment: Maximum cargo floor loading is 600/kg/m 2/120 p.s.f. Maximum cargo load is limited by weight and balance considerations. Fuel Capacity 579 l/153 gal total (570 l/150.5 gal, usable); 477 l/126 gal in main tank at 3221 mm/126.8 in. aft RD and 93 l/24.5 gal in supply tank at 2276 mm/89.6 in. aft RD. Oil Capacity Engine Oil: 10.0 l/2.64 gal. total (5.0 l/1.32 gal. at 3294 mm/129.7 in. aft RD for each engine) (See Note 1 for undrainable oil data) Transmission Oil: 13.25 l/3.5 gal. total at 3294 mm/129.7 in aft RD (See Note 1 for undrainable oil data) Maximum Operating Altitude 20,000 ft. when operating on MIL-T-5624 Grade JP5 or ASTM-D-1655 Jet A, Jet A-1, or MIL-T-5624 Grade JP4 or ASTM-D-1655 Jet B, or alternate fuel (AVGAS Mixture). Rotor Blade and For rigging information refer to the Model BO 105 LS A-3 Maintenance Manual Control Movements Datum 118.1 in., forward of bulkhead No. 7. Leveling Means Leveling point on bulkhead No. 7. Serial Nos. Eligible A Transport Canada Certificate of Airworthiness endorsed as noted below under "Import Requirements" must be submitted for each i ndividual Rotorcraft for which application for FAA Certification is made (See NOTES 8, 9, 10, 11, and 12). 3 H6NE This Type Certificate Data Sheet (TCDS) is canceled effective January 25, 2010. Superseded by TCDS H3EU, dated November 24, 2009. Certification Basis FAR 21.29 and FAR 27 effective 1 February 1965 plus Amendments 27-1 through 27-3 plus Special Conditions No. 27. 31-EU-6 issued November 8, 1970. For the Model BO 105 LS A-3: The following amendments have been inco rporated in the certification basis: 27-5 ( 27.1195), 27-11 ( 27.939), 27-12 ( 27.923 and 27.927) and 27-14 ( 27.67 and 27.75) Equivalent Safety Findings in Note 6. Effective February 25, 1991 the type desi gn approval is transferred from FAA Type Certificate Data Sheet No. H3EU to Type Certificate Data Sheet No. H6NE. Reference letter dated January 24, 1991 from Trans port Canada to the Federal Aviation Administration. Import Requirements U.S. Sta ndard Airworthiness Certificate may be issued on the basis of Transport Canada Certificate of Airworthiness for Export signe d by an authorized representative of the Minister of Transport, Transport Canada containing the following statement: "The rotorcraft covered by this certificate has b een examined, tested and found to comply with the type design approved under Type Certifi cate H6NE and to be in condition for safe operation". Equipment The minimum equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in th e helicopter for certification. In addition the following items of equipment are required: (a) Engine-out Warning System (light) (b) Outside Air Temperature Indicator (c) Transport Canada-approved Flight Manual Service Information MBB Service Bulletins (Technical In formation), published for the U.S. Type Design that carry a statement "Approved by Minister of Transport, Transport Canada," may be interpreted as FAA-approved. Available documents for M BB BO 105 LS A-3 Flight Manual: Subsequent to the release of the Transport Canada-approved Flight Manual - third issue, revisions to the earlier issues of the BO 105 Flight Manual have been discontinued. Maintenance and Overhaul Manual, Ch apter 11, "AIRWORTHINESS LIMITATIONS;" dated October 13, 1970. Available documents for MBB BO 105 LS A-3. 1) Model BO 105 LS A-3 Flight Manual: Approved MBB BO 105 LS A-3 Flight manual dated February 25, 1991, or later, Transport Canada approved issue. Maintenance Manual BO 105 LS, "CHAPTER 101-9 AIRWORTHINESS LIMITATIONS" dated June 30, 1986. NOTES NOTE 1. Current weight and balance report including list of required equipment and list of equipment included in certificated empty weight and loading instructions when necessary, must be provided for each helicopter at the time of original certification. The certificated empty weight and corresponding center of gravity location must include unusable fuel of 17.6 lbs., at 120 in. aft RD and undrainable engine and transmission oil of zero (0) lb. H6NE This Type Certificate Data Sheet (TCDS) is canceled effective January 25, 2010. Superseded by TCDS H3EU, dated November 24, 2009. 4 NOTE 2. The following placard must be di splayed in clear view of the pilot: "This helicopter must be operated in compliance with the operating limitations specified in the Transport Canada-approved Rotorcraft Flight Manual. The "INSPECTIONS and AIRWORTHINESS LIMITATIONS" section of the Mainte nance Manual must be complied with. In addition, all placards required in the Transport Canada approved Rotorcraft Flight Manual must be installed in the appropriate locations. NOTE 3. Refer to the Messerschmitt-Bolkow-Blohm He licopter, Canada Limited, Model BO 105 LS A-3 Maintenance Manual Chapter 101 "Inspection and Airwor thiness Limitation" dated June 30, 1986, or later approved issue, for the retirement life limitations of the helicopter parts which are critical from a fatigue standpoint. These values of retirement or serv ice life cannot be increased without FAA approval. Additional information essential for proper maintenance of the helicopter is contained in the Messerschmitt- Bolkow-Blohm Helicopter, Canada Limited, Model BO 105 LS A-3 Maintenance Manual, dated June 20, 1986. NOTE 4. For operation below 40 °F ambient temperature, all fuel used must contain Phillips PFA-55MB (MIL-I- 27686) anti-icing additive in concentrations of not le ss than 0.035% nor more than 0.15% by volume. Blending this additive into the fuel and checking its concentration must be conducted in the manner prescribed by the Rotorcraft Flight Manua l. Eligible with or without glycerine. NOTE 5. For emergency use, an alternate fuel mixture cons isting of 1/3 by volume of 80/87 aviation gasoline and 2/3 by volume of ASTM D 1655 Jet A or A1 aviation turbine fuel may be used at outside air temperatures of 40 °F (4°C) or below. NOTE 6. Equivalent Safety Findings for the Model BO 105 LS A-3: FAR 27.175 (b) and (c), and FAR 27.927 (b) (2). NOTE 7. The limits shown ar e installed limits. For computation purposes 100 percent engine output shaft (N2) speed is 6016 r.p.m. and 100 percent gas generator speed is 50,942 r.p.m. NOTE 8. The Model BO 105 LS A-3 is limited to serial number 2001 and up. NOTE 9. Model LS A-3, serial numbers 2001-2016 were manuf actured by Messerschmitt-Bolkow-Blohm GmbH Ltd. Helicopter and Transport Division, D-8000 Munchen 80, under Luftfahrt Bundesamt Type Certificate 3025, and approved under FAR Part 21.29 by the Federal Aviation Administration (FAA), Type Certificate Data Sheet No. H3EU. NOTE 10. Model LS A-3, serial numbe rs 2017-2032 were manufactured by MBB Helicopter Canada Limited, Fort Erie, Ontario, under Transport Canada Type Approval H-79. NOTE 11. Model LS A-3 serial number 2033 and subsequent will be manufactured by MBB Helicopter Canada Limited, Fort Erie, Ontario, under Transport Canada Type Approval H-94. NOTE 12. Effective February 25, 1991, design responsibility for all BO 105 LS A3 helicopters is transferred from Messerschmitt-Bolkow-Blohm GmbH Helicopter and Tr ansport Division D-8000 Munchen 80, and Luftfahrt Bundesamt to MBB Helicopter Canada Lim ited and Transport Canada Aviation Group. NOTE 13. Helicopter serial numbers 2014, 2015, 2016, 2017, and 2018 which have sandfilter system installations (modification number 10-22), part number 105-853181, FAA Flight Manual Supplement No. 10-22, approved December 5, 1988, are acceptable with th is Type Certificate Data Sheet No. H6NE ...END... ``` ## ADs None name its models. ## STCs approved under this data sheet (33) - [STC SR02232LA](https://openairdocs.org/stc/SR02232LA): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc. - [STC SR02160LA](https://openairdocs.org/stc/SR02160LA): Removal of two (2) Rolls-Royce engine models 250-C28C and installing two (2) Rolls-Royce engine models 250-C30P in accordance with CALSTAR Master Drawing List CAL201, Revision B, dated May 16, 2008, or later FAA-approved revision. The following CALSTAR continued airworthiness supplement is applicable to aircraft modified in accordance with this STC: Installation of (2) Rolls-Royce Engines 250-C30P Engines, Eurocopter Canada Limited BO 105 LS-A-3, Calstar 203-ICA The CALSTAR FAA-approved Rotorcraft Flight Manual Supplement, CAL204, Revision I/R, dated July 30, 2008, or later FAA-approved revision is required with this installation. CALSTAR FAA-approved Installation Instructions Rolls-Royce 250-C30P Engine, CAL205, Revision A, dated May 16, 2008, or later FAA-approved revision is required with this installation. Certification Basis for this modification: See TCDS H6NE. It was determined that there is no acoustical change in accordance with 21.93(b) as a result of this modification.. California Shock/Truma Air Rescue (CALSTAR) - [STC SR02189NY](https://openairdocs.org/stc/SR02189NY): Iinstallation of SkyTrac ISAT-100 Airborne Position/Data Communicator System.. SkyTrac Systems Ltd. - [STC SH8681SW](https://openairdocs.org/stc/SH8681SW): Installation of a pilot/copilot seat back shroud with area for flight manual on the Eurocopter Canada MBB Model BO-105LS A-3 helicopters in accordance with Era Aviation, Inc., drawing list 10525-1000, Rev. B, dated 8/5/93, or later FAA approved revision.. Apical Industries Inc - [STC SH1315GL](https://openairdocs.org/stc/SH1315GL): Installation of a Shadin Co. engine trend monitoring system.. Shadin Avionics - [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models.. Technisonic Industries Limited - [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System.. Atlantic Avionics Inc. - [STC SH1260EA-D](https://openairdocs.org/stc/SH1260EA-D): Installation of Pulsed Chip Detector System.. American Eurocopter Corporation - [STC SH8173SW-D](https://openairdocs.org/stc/SH8173SW-D): Installation of nose mounted six-16 searchlight system.. American Eurocopter Corporation - [STC SH8174SW-D](https://openairdocs.org/stc/SH8174SW-D): Installation of an Emergency Medical Service Interior.. American Eurocopter Corporation - [STC SH8175SW-D](https://openairdocs.org/stc/SH8175SW-D): Installation of cross tube mounted external loud hailer speakers.. American Eurocopter Corporation - [STC SH880NE-D](https://openairdocs.org/stc/SH880NE-D): Installation of No. 1 Navigation System 105-A0002.. American Eurocopter Corporation - [STC SH881NE-D](https://openairdocs.org/stc/SH881NE-D): Installation of No. 2 navigation system 105-A0003.. American Eurocopter Corporation - [STC SH882NE-D](https://openairdocs.org/stc/SH882NE-D): Installation of Automatic Direction Finder 105-A0004.. American Eurocopter Corporation - [STC SH883NE-D](https://openairdocs.org/stc/SH883NE-D): Installation of Radio Master 105-A0010.. American Eurocopter Corporation - [STC SH884NE-D](https://openairdocs.org/stc/SH884NE-D): Installation of radar Altimeter 105-A0006.. American Eurocopter Corporation - [STC SH885NE-D](https://openairdocs.org/stc/SH885NE-D): Installation of Automatic Terminal Copntrol 105-A0007.. American Eurocopter Corporation - [STC SH886NE-D](https://openairdocs.org/stc/SH886NE-D): Installation of Communication Control 105-A0008.. American Eurocopter Corporation - [STC SH887NE-D](https://openairdocs.org/stc/SH887NE-D): Installation of Radio Magnetic Indicator 105-A0009.. American Eurocopter Corporation - [STC SH889NE-D](https://openairdocs.org/stc/SH889NE-D): Installation of AFT Equipment Provision 105-E0050.. American Eurocopter Corporation - [STC SH890NE-D](https://openairdocs.org/stc/SH890NE-D): Installation of Forward Equipment Provision.. American Eurocopter Corporation - [STC SH891NE-D](https://openairdocs.org/stc/SH891NE-D): Installation of Center Console 105-E0052.. American Eurocopter Corporation - [STC SH892NE-D](https://openairdocs.org/stc/SH892NE-D): Installation of Instrument Panel 105-E0053.. American Eurocopter Corporation - [STC SH893NE-D](https://openairdocs.org/stc/SH893NE-D): Installation of Communications 105-A0001 per MBB Installation Drawing List Document No. 105-A- RPT-1, Rev C, dated 8/29/1991.. American Eurocopter Corporation - [STC SH894NE-D](https://openairdocs.org/stc/SH894NE-D): Installation of Second Airspeed Indicator 105-A0015.. American Eurocopter Corporation - [STC SR00611AT](https://openairdocs.org/stc/SR00611AT): Installation of an air conditioning system in accordance with Aero Aire Corporation Master Drawing List 1054RO10,Revision. 2, dated November 3, 1994, or later FAA approved revision.. Enviro Systems Inc. - [STC SR01265NY](https://openairdocs.org/stc/SR01265NY): Bearpaw installation.. Dart Aerospace Limited - [STC SH589NE](https://openairdocs.org/stc/SH589NE): Installation of wire strike protection system. (BO-105C VARIANTS CB-2 CB-2) (BO-105S VARIANTS CBS-2 CBS-4). Eurocopter Canada Limited - [STC SH888NE](https://openairdocs.org/stc/SH888NE): Installation of radio master 105-A0010.. American Eurocopter Corporation - [STC SH888NE-D](https://openairdocs.org/stc/SH888NE-D): Installation of radio master 105-A0010.. American Eurocopter Corporation - [STC SH3568SW](https://openairdocs.org/stc/SH3568SW): Installation of under fuselage recognition lights.. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SH1065EA](https://openairdocs.org/stc/SH1065EA): Installation of Devore tail rotor floodlight on upper surfaces of horizontal stabilizer.. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SH588NE](https://openairdocs.org/stc/SH588NE): Installation of High Skid Landing Gear.. MBB Helicopter Canada Ltd --- 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.