CAR 521.57(2)(a) and AWM 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d). The following table lists exemptions that have been issued by the Aircraft Certification Standards in Headquarters or that affect aircraft certification activities in Headquarters. To permit the removal of the engine inlet deflector system on the Viking DHC-6 “Twin Otter” Models 100, 200 and 300 aeroplanes and reissue the corresponding supplemental type certificate (STC) to KBA. The purpose of this exemption is to permit Airbus to obtain an amended type certificate to include Airbus “Cabin-Flex” option aeroplane models A321-271NX and A321-272NX (A321neo ACF models), which contain design features that do not comply with the applicable standards of airworthiness of the AWM [Change 525-23] specifying the maximum number of passenger seats permitted for all Type III exits. Transport Canada is closely monitoring the COVID-19 situation. The purpose of this exemption is to permit the issuance of the corresponding Supplemental Type Certificate (STC) to NEDL for the installation of a loading ramp, which facilitates the loading of medical stretchers on the Bombardier model CL600-2B16 aeroplane without fully complying with the original design requirements for emergency exits. CAR 521.158(1) and AWM 525.841(a)(2)(i) and (3), Airbus A321-271N and A321-272N (A321neo), and models A321-271NX and A321-272NX (A321neo ACF). Found inside â Page 283TAS TATP Tb TBD TBP TBT TBV Tc TC TC TCLo TCA TCAP TCC TCDD TCDF TC/DOT TCDS TCE TCF TCIM TCLP TCM TCMD TCP TCP TCP ... Transport Canada lowest published toxic concentration Truckload Carriers Association tricyclic acetone peroxide, ... The installation of side-facing divan(s), permitting that divan(s) be occupied during taxi, take-off and landing. You may experience longer than usual wait times or partial service interruptions. CAR 521.158(1) and AWM 525.841(a)(2)(i) AND (3), A321-271N and A321-272N (A321neo), and models A321-271NX and A321-272NX (A321neo ACF). x��\�n�8� ��_iPӼ_�� ���Lf�ƻ�E1?4��h����"����o1�в�Td�ZT6-�Z���Ṓ����eu^��uu�qvA>������ӻ������/�z�\��n�����Yu1[��yu8!��߳�:����:G����9e��f�{��@�{]ǽ���_s���r�9����VK�#��0�͙%W7�{�\�+�\����PLˑ.&�g�-ȯ�.�xM_������{G��/%��(& �JP�RP�'�(L/+��̎�2�ǑȈQ�$��(�� Reference Date for determining the applicable airworthiness requirements: 27 March 1998 (PT6C-67C) 02 November 2009 (PT6C-67E) 12 September 2014 (PT6C-67A) 3. Replaced by 01 Sep. 2000 revision. Please check if any of these measures apply to you. Refer to Advisory Circular 21-1 Appendix 2 for the New Zealand type acceptance status of any engines and propellers listed above. 2 0 obj C-GCFG. First Name . endobj Found inside â Page 9TCDS ( Type Certificate Data Air Traffic Control Handbook Replaces Data Communications Sheets and Specifications ) ... S / N 050-07-00922-4 authorized by the FAA , Department Basic book : $ 35 of the Navy , and Transport Canada ; ⢠Vols . Transport Canada is closely monitoring the COVID-19 situation. CAR 521.158(1) with respect to 525.1301 and 525.1309 of the AWM, BD-700-1A10 (Global Express) and BD-700-1A11 (Global 5000). E21 for P&WC PT6A Series at Issue 15 dated September 20, 2007 FAA Type Certificate Data Sheet E26NE at Revision 13 dated 19 November 2007 Transport Canada TCDS No. refer to the following modifications which are approved in Canada. CAR 513.07 and AWM 513.07(1)(b) & FAR Sec. 1, Ground loads and landing gear requirements. For many years now, the AV developing community have been mentioning in qualitative terms how TCDs can support AV deployment. If you cannot get through, please contact us by email. Type Certificate Holder: Bombardier Inc. 800 Boul. ]{M� N�8�uV� �6�ɂv�\����@p�(�^-�z�9]1�^.������-@؊h�F�f %PDF-1.7 To grant approval only to permit certification of all a/c, DA20-C1 VLA, at a Maximum Approved Takeoff Mass (Weight) of not more than 800 kg (1764 lbs). Certifying Authority: Transport Canada Civil Aviation Aircraft Certification Branch (AARD) 159 Cleopatra Drive Nepean, Ontario K2G 5X4 Canada 5. To provide additional time to install an ELT where the a/c is a multi-engined turbo-jet aeroplane of more that 5,700 kg MCTOW that is being operated in IFR flight within controlled airspace over land, and south of latitude 66o30o N. Installation of mid-cabin door on any BD700-1A10 a/c. The purpose of this exemption is to permit CSALP to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the CSALP model BD-500-1A10 (Marketing designation “A220-100”, formerly the CS300). Transport Canada has released Issue 9 of Type Certificate Data Sheet Number A-24, dated 02 October 2014. Interior Doors Revised Dec. 00. This Type Certificate Data Sheet, which is part of Type Certificate Number A-24, prescribes the conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of Transport . H3EU, Rev 19 The purpose of this exemption is to permit Bombardier to obtain an amended type certificate for the Bombardier CSeries aeroplane model BD-500-1A10 (CS100), where the amended type design to be approved includes a Flight Management System (FMS) with embedded software whose demonstrated design assurance processes do not permit a complete showing of compliance to 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) of the AWM. This exemption does not permit a non-compliance with AWM 525.841(a) for any other system and structural failure events not shown to be extremely improbable. Helicopter Amendment to Type Certificate Acceptance Revision status of M/s Bell Helicopter Model 412 EP (S. No. The purpose of this exemption is to permit Conair Group Inc. to obtain a supplemental type certificate (STC) for the Bombardier aeroplane model DHC-8-402, where the change to the type design to be approved contains design features that do not comply with the applicable standards of airworthiness for the protection from serious injury during emergency landing conditions for occupants of berths intended for a non-ambulant persons. Found insideAviation Safety Agency, EASA Type-Certificate Data Sheet, TCDS No. ... See Canadian Union of Public Employees v. ... between the Government of Canada and the Government of the Hellenic Republic on Air Transport, 20 August 1984, ... endobj In particular, this exemption is intended to provide relief from the requirement from paragraph 525.809(a) to provide a means of viewing the likely areas of evacuee ground contact prior to opening the over-wing emergency exits. This exemption would permit the dispensing units providing the required oxygen flow to be automatically presented to the occupants before the cabin pressure altitude exceeds 17,000 feet. Please check if any of these measures apply to you. The purpose of this exemption is to allow the installation of an incubator unit without demonstrating restraint of its plastic cover, where the applicable standards of airworthiness of 14 CFR 25.561(c) would not be met. EASA Certification Basis 3.1. Comply with TCCA environmental requirements 3.2.2(a)(1) 2. The approved change to the type design includes a Flight Management System (FMS) with embedded software whose demonstrated design does not permit a complete showing of compliance to paragraphs 525.1301(a)(1) and (a)(4), 525.1309(a) and (b) of the AWM as well as paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness (SCA) 2013-03. CAR 3.606. Type acceptance of the Diamond Aircraft model DA 62 for Transport Canada TCDS A-273 Issue 03 dated 12.05.2020. CAR 513.07 and AWM 513.07(1)(b), U.S. This is an illustrated technical guide to the Boeing 737 aircraft. The purpose of the major design change is to introduce a new Flight Management System (FMS) Build 8A2 to replace Build 8A1. Email Address * Let us guide you. The purpose of this exemption is to permit Airbus to obtain an amended type certificate to include new A321neo ACF aeroplane models (including any models designated as A321-2**NX), which have design features that do not fully comply with the applicable standards of airworthiness for “Emergency Exit Arrangement” in accordance with paragraph 525.809(a) of the AWM [Change 525-23]. To approve the installation of a door in a partition between passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. To permit the installtion of a door in a partition between passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. Transport Canada TCDS. EASA Certification Application Date: November 12, 2008 6. For information on these exemptions refer to the Civil Aviation Exemptions Search page at http://wwwapps2.tc.gc.ca/saf-sec-sur/2/exemptions/e_s.aspx?lang=eng. Save money and time with our professional advice +61 497 700 135. Transport Canada is responsible for transportation policies and programs. Written by globally renowned experts in the field, both clinicians and researchers will find this book invaluable to update their knowledge. This volume is divided into two sections, one covering the brain, the other the spinal cord. h¿ÏÍí£ÜH5ÖÍÁ¡7´âÉÍ"íæq֪ܥ¸O'^èÃE¤òÕ´èãà±+6ÿÊ Outlining the state-of-the-art in aircraft sustainment, this book covers the use of quantitative fractography to determine the in-service crack length versus flight hours curve, the effect of intergranular cracking on structural integrity ... 36087 thru 36999) TC No. To permit Bombardier Inc. to install side-facing divan(s). The Federal Aviation Administration (FAA) has published the Private Pilot - Airplane Airman Certification Standards (ACS) document to communicate the aeronautical knowledge, risk management, and flight proficiency standards for the private ... 6 0 obj For information on COVID-19 updates, please visit Canada.ca/coronavirus. CAR 521.33 and AWM 525.177(d), 525.251(d), 525.671(c)(1), 525.735(b)(1), 525.735(c)(1), 525.783(h)(4), 525.810(a)(2), 525.810(c), 525.856(b), 525.903(e), 525.981(a), 525.1301(a)(1), 525.1302(c)(1), 525.1309(a), 525.1309(b), 525.1309(c) 525.1309(d), 525.1459(a)(2) and 525.1523; as well as SCA 2013-03. Permit the installation of emergency exit signs with non-English lettering and/or markings that do not comply for the purpose of facilitating delivery of the affected a/c to a foreign customer. ÿØÿà JFIF À À ÿÛ C 197, dated June 30, 2021 or later issue. 18-1 Item 1810-01: Added relief for Vibration Monitoring System. AWM 513.07(1)(b), CAR 513.07 & FAR 25.813(e). A treatment of automatic flight control systems (AFCS) for fixed wing and rotary wing aircraft. The text covers in detail the subject of stability and control theory. The purpose of this exemption is to permit Viking to obtain a design change approval for the DHC-6 “Twin Otter” Series 400, as well as Series 1, 100, 110, 200, 210, 300, 310 and 320 aeroplane models incorporating type design changes recorded in Viking Report AEROC 6.1.G.11 DHC-6 Certified Airplane – Basic Definition, where the design change to be approved contains design features that do not comply with the applicable standards of airworthiness for “Takeoff speeds” and “Operating limitations – Takeoff weight limitations” in accordance with SFAR 23-1. Save money and time with our professional advice +61 497 700 135. Found inside â Page 595Une lignée cellulaire immortalisée du tube contourné distal de souris ( TCDS ) a été largement utilisée pour examiner les mécanismes cellulaires du transport du magnésium dans ce segment du néphron . Les hormones peptidiques , telles ... National Authority Type Certificate Date: June 24, 2010 Transport Canada Type Certificate A-82, Transport Canada Safety and Security. Featuring a case study on the continuous safety assessment process of the civil airborne electrical power system, this book addresses problems, issues and troubleshooting techniques such as single event effects (SEE), the failure effects of ... Quickly modify the flight crew compartment doors to delay or deter unauthorized entry. EASA Certification Basis 3.1. Last Name . Transport Canada Web sites do not automatically gather any specific personal information from you, such as your name, phone number or email address. The purpose of this exemption is to permit Field Aviation to obtain a supplemental type certificate for the Bombardier model CL600-2C10 (CRJ-700) aeroplane, serial number 10343, in respect of a modified cargo door installation, where a full showing of compliance to 14 CFR 25.783 has not fully been completed. AWM 513.07(1)(b), CAR 513.07 & FAR 25.813(e), AWM 513.07(1)(b), CAR 513.07 & FAR 25.815, British Aerospace (BAe) Jetstream Series 3112. A321neo ACF aeroplane models (including any models designated as A321-2**NX). 2. The most current aviation maintenance technician general textbook available. Bombardier CL-600-2C10 (CRJ-700) aeroplane, serial number 10343. 2. Please check if any of these measures apply to you. René-Lévesque Ouest Montreal, QC, Canada H3B 1Y8 6. In response, we have issued some transportation-related measures and guidance. Refer to Transport Canada TCDS A-177 EASA Certification Basis: CS-25 for Large Aeroplanes, Amendment 1, 12 December 2005 CS-AWO for All Weather Operations, Initial Issue, 17 October 2003 Special Conditions: CRI F-12-GVFD HIRF Protection CRI F-23-GVFD LCD Head-Up Display CRI F-27-GVFD Data Link Single European Sky <> The purpose of the major design change is to introduce a new Flight Management System (FMS) Build 8A2 to replace Build 8A1. Transport Canada Type Certificate Number A-131 Transport Canada TCDS Number A-131 at Issue 60 dated November 22, 2019 ‒Model CL-600-2B16 (604 Variant) approved September 20, 1995 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the -600-2B16 (604 Variant) is CLFAR Part 25 dated To permit the configuration of a passenger compartment that includes a side-facing divan, which would be intended for occupant use during all phases of flight and issue the corresponding supplemental type certificate. For further information, please contact the Manager, Domestic Regulations, Aircraft Certification Standards at 613-941-8382 or email aartc-d@tc.gc.ca. This exemption supersedes Exemption No. Preface -- Definition and acronyms -- Acknowledgements -- Introduction -- The composition and regulation of international commercial aviation -- Metamorphosis of the airline industry from 1992 to 2013 -- Competition and the evolving value ... Aircraft Certification Standards - Exemptions, http://wwwapps2.tc.gc.ca/saf-sec-sur/2/exemptions/e_s.aspx?lang=eng, transportation-related measures and guidance. Transport Canada is closely monitoring the COVID-19 situation. Refer to Advisory Circular 21-1 Appendix 2 for the New Zealand type acceptance status of any engines and propellers listed above. The approved type design includes a Flight Management System (FMS) with embedded software whose demonstrated design assurance processes do not permit a complete showing of compliance to paragraphs 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) of the AWM. In particular, and in consideration of the possibility of this aeroplane model to conduct high-altitude airport operations into airports constructed at elevations greater than 13,800 feet above sea level, this exemption is intended to provide relief from the application of the subject provision in order to prevent nuisance presentation of the oxygen dispensing units when operating at high-altitude airports. To obtain an Appliance Tye Certificate without complying with the donning time test as required by the HPTSS Standard. EASA Certification Basis 3.1. To permit Bombardier Inc. to install a door in a partition betweeen passenger compartments for the purpose of private operator passenger transportation pursuant to CAR 604 or on-demand air transport service pursuant to CAR 704. <> To carry external loads on their float equipped a/c without an authorization in the TC or STC . Transport Canada TCDS. To obtain a design approval for a cabin design that does not comply with the minimum cabin aisle width requirements of the applicable standards of airworthiness. EUROCOPTER CANADA LIMITED Ontario, Canada (formerly Messerschmitt-Bolkow-Blohm) BO 105 LS A-3. TYPE-CERTIFICATE DATA SHEET CHALLENGER 300 CHALLENGER 350 Manufacturer: BOMBARDIER INC. 800 Boul. endobj Airworthiness Standards Beretter om de Havilland flyfabrikationen i Canada og flytyperne herfra In response, we have issued some transportation-related measures and guidance. (c) in the case of an overwing passenger exit, it is not required for a person to be able to view the likely areas of evacuee ground contact while in a position to open the exit. Transport Canada Publication (TP) 6327, Safety Criteria for Approval of Extended Range Twin-Engine Operations (ETOPS) dated June 2007; TCCA Type Certificate Data Sheet A-146, Issue No. Please check if any of these measures apply to you. (a) in the case of the flight crew emergency overhead exit (hatch), where due to fuselage curvature the path from the exit to the ground contact point is not a straight line, a viewing means with the exit closed is not required to be capable to permit viewing of the likely areas of evacuee ground contact during all lighting conditions with the landing gear extended, as well as in all conditions of landing gear collapse; (b) in the case of a non-overwing passenger exit, a viewing means with the exit closed in not required to permit viewing of the likely areas of evacuee ground contact during all lighting conditions with the landing gear in all conditions of collapse; and. <> Airworthiness Standards JAR E Change 9 dated 21 October 1994 (PT6C-67C) CS-E Amendment 1, dated 03 December 2007 (PT6C-67E) 21-1 Item 2140-01: Changed par 1) thru 3) relief from C to D (correction). Side Facing Divans. The purpose of this exemption is to permit Viking to obtain a design change approval in respect of an aeroplane flight manual supplement containing Reduced Ground Roll – 20 Degree Flap Take-Off procedures and performance data for the DHC-6 “Twin Otter” Series 400, as well as Series 1, 100, 110, 200, 210, 300, 310 and 320 aeroplane models incorporating type design changes recorded in Viking Report AEROC 6.1.G.11 DHC-6 Certified Airplane – Basic Definition to comply with SFAR 23-1, without fully complying with the applicable standards of airworthiness for “Takeoff speeds” and “Operating limitations – Takeoff weight limitations” in accordance with SFAR 23-1. all users of Helicopter External Transport System (HETS) conducting or permitting a take-off in a helicopter that does not meet Part I, Paragraph (B) of Airworthiness Directive (AD) CF-2014-26. René-Lévesque Ouest Montreal, QC, Canada H3B 1Y8 6. CAR 521.158(1) and AWM 525.1301(a)(1) and (a)(4), 525.1309(a), 525.1309(a) and (b), and paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness 2013-03, BD-500-1A11 (Marketing designation “A220-300”, formerly the CS300). Paragraph 525.1322(a)(2) specifies that flight crew alerts must be readily and easily detectable and intelligible by the flight crew under all foreseeable operating conditions, including conditions where multiple alerts are provided. Provide to TCCA for review: Send through ACO, unless prior approval . Maximum certificated take-off weight restricted category. The purpose of this exemption is to permit ACLP to obtain an approval for a major change to the type design that results in a re-issuance of the type certificate data sheet (TCDS) for the ACLP model BD-500-1A11 (Marketing designation “A220-300”, formerly the CS300). In particular, the proposed design exceeds the standard limit of 70 passenger seats permitted for all Type III exits, and therefore does not meet the standard. To permit the configuration of a passenger compartment that includes a side-facing divan, which would be intended for occupant use during all phases of flight and issue the corresponding supplemental type certificate to Innotech Aviation. Found inside â Page 203Transit - sensitive land use design can be developed through the designation of transit corridor districts ( TCDs ) ... at the Sixth National Conference on Light Rail Transit , held in Calgary , Alberta , Canada , May 24-27 , 1992 ) . You will not receive a reply. We are a federal institution, leading the Transport Canada portfolio and working with our partners. 10, dated October 9, 2018 or later issue. E12 for P&WC PT6A Series at Issue 20 dated May 23, 2007 FAA Type Certificate Data Sheet E4EA at Revision 24 dated 21 June 2007 Transport Canada TCDS No. To allow the Bombardier CL-600-2E25 to be certificated without a complete showing of compliance with AWM 525.981(a)(3) at the time of certification. 23, AS AMENDED BY SFAR 23-1, DHC-6 “Twin Otter” Series 400, as well as Series 1, 100, 110, 200, 210, 300, 310 and 320 aeroplane models. Found inside â Page 985... tcd's time certificates of deposit (TCDs) TCDU Transport Command Development Unit tce ton-coal equivalent; ... Carrier Group tch travel counselor's handbook Tch (TCH) Tacoma (container symbol) TCH Trans-Canada Highway tchg teaching ... 3 0 obj If you cannot get through, please contact us by email. The purpose of this exemption is to permit Bombardier to obtain an amended type certificate to include a new aeroplane model BD-700-2A12 (Global 7000), which contains design features that do not fully comply with the applicable standards of airworthiness for “Emergency Exit Arrangement” in accordance with paragraph 525.809(a) of the AWM [Change 525-22]. Permit Bombardier Inc. to install side-facing divan(s). <>/ExtGState<>/XObject<>/ProcSet[/PDF/Text/ImageB/ImageC/ImageI] >>/MediaBox[ 0 0 595.32 841.92] /Contents 4 0 R/Group<>/Tabs/S/StructParents 0>> CL600-2A12 S/N 3022 Reg. The product detailed below will be accepted for compliance with the applicable Lloyd's Register Rules and Regulations with regards to the International Convention for the Safety of Life at Sea, (SOLAS), 1974, as endobj CAR 521.158 and SCA 2010-02 part of Para 3.2(a)(1), To permit certification of the GIV-X aeroplane for maximum operating altitude above 41000 feet up to 45000 feet without meeting one of the requirements of SCA 2010-02, Canadian air operators, Part V, Subpart 21. Refer to Transport Canada TCDS A-177 EASA Certification Basis: CS-25 for Large Aeroplanes, Amendment 1, 12 December 2005 CS-AWO for All Weather Operations, Initial Issue, 17 October 2003 Special Conditions: CRI F-12-GVFD HIRF Protection CRI F-23-GVFD LCD Head-Up Display CRI F-27-GVFD Data Link Single European Sky 7 0 obj see Transport Canada TCDS E-32 2. The purpose of this exemption is to permit Bombardier to obtain an amended type certificate to include the Bombardier aeroplane model BD-700-2A12 (marketing designation “Global 7000”), where the type design to be approved contains design features that do not comply with the applicable standards of airworthiness for flight crew alerting. Transport Canada Certification Basis details see Transport Canada TCDS E-19 3. BD-500-1A10 (Marketing designation “A220-100”, formerly the CS100). The approved type design includes a Flight Management System (FMS) with embedded software whose demonstrated design assurance processes do not permit a complete showing of compliance to paragraphs 525.1301(a)(1), 525.1309(a), 525.1309(b), and 525.1309(d) of the AWM. Certifying Authority: Transport Canada Civil Aviation Aircraft Certification Branch (AARD) 159 Cleopatra Drive Nepean, Ontario K2G 5X4 Canada 5. Appendix 1 - Difference legends The Bell 429 is manufactured in Canada and Transport Canada Civil Aviation (TCCA) is the Regulatory body for Canada. This exemption provides relief from the requirements of paragraphs AWM 525.841(a)(2)(i) and (3) [Change 525-22] for uncontained engine rotor failure (UERF) scenarios. To permit the installation of a loading ramp which facilitates the loading of the medical stretchers on this a/c, operated by the Gouvernement du Québec, Service aérien gouvernemental. Transport Canada Certification Basis: See Transport Canada TCDS E-28 2. Email Address * Let us guide you. A-131) that includes the CL-600-2E25 (CRJ 1000) model aeroplane, without a complete showing of compliance to 525.981(a)(3) of the AWM, where the structural aspects of the fuel tank system have not yet been demonstrated to have two independent means of lightning protection. The approved change to the type design includes a Flight Management System (FMS) with embedded software whose demonstrated design does not permit a complete showing of compliance to paragraphs 525.1301(a)(1) and (a)(4), 525.1309(a) and (b) of the AWM as well as paragraphs 4(a) and (c)(2) of Special Conditions-Airworthiness (SCA) 2013-03.
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