Source: https://www.scribd.com/document/308031860/Beech-b200-Far-23
Timestamp: 2018-10-23 17:20:35
Document Index: 346344500

Matched Legal Cases: ['§21', '§21', '§91', '§21', 'art 21', 'art 36', 'art 36', 'art 36', 'art 36', 'art 23', 'art 23', 'art 21', '§21', '§21', 'art 25', 'art 21', '§21', 'art 21', '§21', '§23', '§23', 'art 23', 'art 33', 'art 21', 'art 23', '§23', 'art 25', 'art 27', 'art 36', 'art 27', 'art 36', 'art 26', '§23', '§23', 'art 91', '§23', '§91', '§23', 'art 26', '§91', '§23', '§23', '§23', '§23', '§23', 'art 91', 'art 125', 'art 91', 'art 125', 'art 91', '§43', '§23', '§23', '§23', '§23', 'art 145', 'art 135', '§23', '§23']

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Proposed Rule: Airworthiness directives: Boeing Model 777-200 series airplanes
130-590031-235_supp_pack
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Airworthiness Directive Bombardier/Canadair 020321
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Airworthiness Directive Bombardier/Canadair 020520
KiwiFlyer Issue 3 Aero Modelling
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TAR 98/18 – Revision 5
BEECH 200/300 KING AIR Series
ADDITIONAL NEW ZEALAND REQUIREMENTS 13 ATTACHMENTS 14 APPENDIX 1 15 Rev. ICAO TYPE CERTIFICATE DETAILS 1 3.43 DATA REQUIREMENTS 6 5.Type Acceptance Report TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. TYPE ACCEPTANCE DETAILS 4 4. INTRODUCTION 1 2. NZCAR §21.5 : 28 May 2015 i TAR 98/18 – Beech Super King Air .
which are now eligible for the issue of an Airworthiness Certificate in the Standard Category in accordance with NZCAR §21.) Additional variants or serial numbers approved under the foreign type certificate can become type accepted after supply of the applicable documentation. serial numbers BB1532-1977 and BL141-151. serial numbers BB1978-2018.000 ft AMSL. FL-424.43(c). BL171. and (b) Identify any special conditions for import applicable to any model(s) covered by the Type Acceptance Certificate.5 : 28 May 2015 1 TAR 98/18 – Beech Super King Air . subject to any outstanding New Zealand operational requirements being met. serial numbers BB2019.535 the aircraft must be fitted with a cabin altitude warning pressure switch which activates at 10. To comply with New Zealand operating rules under §91. FL521-FL523 and FL526-845.Type Acceptance Report Executive Summary New Zealand Type Acceptance has been granted to the Beech Model 200/300 series Super King Air based on validation of FAA Type Certificate number A24CE. FM55 and after) Hawker Beechcraft Corporation (effective 26/03/07. 1. FL137423 and FM9-13. BL152-170. (See Section 5 of this report for a review of compliance of the basic type design with the operating Rules. FL846. Specifically the report aims to: (a) Specify the foreign type certificate and associated airworthiness design standard used for type acceptance of the model(s) in New Zealand. 2. ICAO Type Certificate Details Manufacturer: Beechcraft Corporation (effective 12/4/2013. Introduction This report details the basis on which Type Acceptance Certificate No. BZ1 and BY172. and (c) Identify any additional requirements which must be complied with prior to the issue of a NZ Airworthiness Certificate or for any subsequent operations.177. in accordance with the provisions of NZCAR §21. FM-14-FM54) Raytheon Aircraft Corporation (effective 15/4/96.98/18 was granted in the Standard Category in accordance with NZCAR Part 21 Subpart B. Applicability is currently limited to the Models and/or serial numbers detailed in Appendix 1. FN-2 and up) Beech Aircraft Corporation Type Certificate: A24CE Issued by: Federal Aviation Administration Rev.
500 lb. No. (5670 kg) Max. (5670 kg) Max. of Seats: 15 Noise Standard: FAR Part 36 through amendment 36-10 Engine: Pratt & Whitney Canada PT6A-42 Type Certificate: E-12 Issued by: Transport Canada Propeller: Hartzell HC-B3TN-3G or N/T10178 Series blades Type Certificate: P15EA Issued by: Federal Aviation Administration McCauley 3GFR34C702/100LA-2 Type Certificate: P60GL Issued by: Federal Aviation Administration Hartzell HC-E4N-3G/D9390SK-1R Type Certificate: P10NE Issued by: Federal Aviation Administration McCauley 4HFR34C771/94LA-0 Type Certificate: P3NE Issued by: Federal Aviation Administration TAR 98/18 – Beech Super King Air 2 Rev.500 lb. of Seats: 15 Noise Standard: FAR Part 36 through amendment 36-10 Engine: Pratt & Whitney Canada PT6A-41 Type Certificate: E-12 Issued by: Transport Canada Propeller: Hartzell HC-B3TN-3G or N/T10178 Series blades Type Certificate: P15EA Issued by: Federal Aviation Administration McCauley 3GFR34C702/100LA-2 Type Certificate: P60GL Issued by: Federal Aviation Administration Model(s): B200 and B200C (Super King Air) MCTOW 12. No.Type Acceptance Report Model(s): 200 and 200C (Super King Air) MCTOW 12.5 : 28 May 2015 .
000 lb. of Seats: 15 Noise Standard: FAR Part 36 through amendment 36-20 Engine: Pratt & Whitney Canada PT6A-52 Type Certificate: E-12 Issued by: Transport Canada Propeller: Hartzell HC-E4N-3G/D9390SK-1R Type Certificate: P10NE Issued by: Federal Aviation Administration Note: MT-Propeller MTV27-1-E-C-F-R(P)/CFR225-55f can be fitted under FAA STC SA03209NY Rev.5 : 28 May 2015 3 TAR 98/18 – Beech Super King Air . of Seats: 17 Noise Standard: FAR Part 36 through amendment 36-15 Engine: Pratt & Whitney Canada PT6A-60A Type Certificate: E-12 Issued by: Transport Canada Propeller: Hartzell HC-B4MP-3C/M10476K series blades Type Certificate: P56GL Issued by: Federal Aviation Administration Model(s): B200GT and B200CGT (Super King Air) MCTOW 12.Type Acceptance Report Model(s): B300 and B300C (King Air 350/C) MCTOW 15. (6804 kg) 16.500 lb. (5670 kg) Max. (7484 kg) – 350ER (commercial) variant [aircraft with Drawing 130M000030 or Kit Drawing 130-4014] and B300C aircraft modified by Hawker Beechcraft Drawing 130M000009 Max.500 lb. No. No.
5 psi cabin pressure differential and approval for operation at up to 35. after application by the manufacturer. Specific applicability is limited to the coverage provided by the operating documentation supplied.) The first-of-type was serial number BB-1847 registered ZK-KHP. Type Acceptance Details The application for New Zealand type acceptance of the B200 was from Aeromotive Limited dated 3 June 1998. new aft fuselage and tailcone with a T-tail. new DS compressor turbine blades and a modified exhaust case inner exit ramp. and includes the PT6A-42 engine based on Transport Canada Type Certificate E-12. which can also be certificated in the Restricted category at higher gross weights. (As is now fitted to all the current C90A and B300 models as well.98/18 was granted on 6 July 1998 to the Beech Model B200 based on validation of FAA Type Certificate A24CE.2 as having a type acceptance certificate in force. and increases in MTOW and pressurisation differential up to 6. but all were de-registered prior to 1995 and type acceptance had lapsed. Data on the aircraft was not current and the type was not listed in AC 21-1.5 : 28 May 2015 . The application was from the importer. zero fuel weight. which are fitted with the Collins Pro-Line 21 Electronic Flight Instrument System.0 psi. ZK-KSL and ZK-MGP. The Model 200 Super King Air (originally designated the Model 101) was derived from the A100 by the addition of a new centre wing section with strengthened and extended outer wings. (There have been previous examples of the original Model 300 in New Zealand. while the x200xT is a special version with additional fuel capacity.000 lb. Type acceptance was granted on 19 January 2011. and the first-of-type example was serial no.) These changes improve cruise performance above 15. This report was raised to Revision 1 to include the Models 200 and 200C. 11. There have been three previous examples of the B200 in New Zealand. Type Acceptance Certificate No.000 feet. Type Acceptance was granted on 29 September 2009.000 feet for the B200T and B200CT models. They were later de-registered and placed under military airworthiness control. There are no special requirements for import into New Zealand. double width pedestal. Type acceptance was granted on 1 August 2012. Revision 2 was issued to add the two Models B300 and B300C. 850 shp PT6A-41 engines. The B200 was a development of the Model 200 incorporating the PT6A-42 engine. but are maintained and supported under civil contract.Type Acceptance Report 3.) Revision 3 to this report added the later Model B200 production serial number range. ZK-RGA and ZK-WIL were also operated here but were de-registered in 1987 and 1988 respectively.BL-31 registered ZK-FDR. until replaced by a Beech 300 in 1986.) TAR 98/18 – Beech Super King Air 4 Rev. (Static ratings for the engines are the same but the -42 has new compressor first-stage blades and vanes. (The x200C version has a large cargo door. The first-of-type example was serial number FL-727 registered ZK-MMM. The first example was serial number BB-1054 registered as ZK-KAB. Five aircraft were imported as multi-engine trainers for the RNZAF and initially placed on the Civil Aircraft Register. and maximum flap extension speed increased to 155 knots for the B200/C models. BB-866 was first imported in 1981 as ZK-PBG by James Aviation for corporate use by Watties Industries. Garden City Helicopters Ltd. Other airframe changes include 6.
Rev. use of LED lighting technology. which add such features as RVSM capability. which is the designation of the B200GT with four STCs embodied: SA3366NM (Raisbeck Ram Air Recovery System). The applicant was the aircraft manufacturer and the first-of-type example was serial number BY-57 registered ZK-VMF. and the first-of-type was Model B300 serial number FL-328 registered as ZK-SSH.5 : 28 May 2015 5 TAR 98/18 – Beech Super King Air . MCTOW was further increased to 15. Beechcraft had begun work on the replacement for the 300. Revision 4 to this report added the two B200GT models. which are fitted in place of the wing lockers. This version is sold as the “350ER”. FMS and GPS. with MTOW increased to 14. which includes re-styled seating with integral life vest stowage. Raisbeck dual aft body strakes and wing lockers are also fitted as standard. (The `Super' prefix was dropped from the King Air name in 1996. introduced in 1990 and initially marketed as the Super King Air 350.000 lb (6. The B200GT is the latest variant and evolved from the King Air B200 by the installation of new PT6A-52 engines. The Model 350 is also available in a range of special mission and military variants. and a High Definition Audio Visual display unit.300 kg).750 kg). Because not all countries would then allow an aircraft of this type to be certified at an MCTOW greater than 12. The latter supports use of a range of electronic devices. and included the PT6A-52 engine. the Model 300LW was also developed at the same time. In addition from BY-128 and after Beech is marketing the King Air “250”. This report was raised to Revision 5 to include some additional serial number ranges not covered by the existing report. The PT6A-52 was derived by mating the turbine section of the 1.000 lb (6.050-shp capable PT6A-60A found on the Super King Air 350 with the existing King Air B200 PT6A-42 gearbox. SA02130SE (Hartzell Composite Propeller). The result is an engine that holds its 850-shp flat rating to a much higher altitude. The latest version (marketing name “350i") indicates a new interior upgrade. limited to the lower MCTOW. SA01615SE (Boundary Layer Research [BLR] Winglets). new cabinetry and in particular installation of the Rockwell Collins Cabin Management System (CMS). The fuselage of the 300 was stretched by nearly three feet with two extra cabin windows on each side and winglets added to the wingtips to create the Model B300. The 350C variant features a 132 x 132 cm (52 x 52 in) freight door. Type acceptance was granted on 14 August 2014. and SA02131SE (BLR Ultimate Performance Package).) B300/C aircraft are now fitted with a range of STCs during production. rated at 1050 shp) installed in redesigned nacelles (known as "pitot cowlings" due to the reshaped engine air intakes).500 lb (5. The applicant was Skyline Aviation. improving climb and cruise performance under almost all flight conditions.Type Acceptance Report The Model 300 was a further development of the B200 with some airframe aerodynamic improvements and more powerful engines (PT6A-60A.700 kg). while also controlling the various environmental functions. Another factory option is installation of extended range fuel tanks. By 1988.
1989 – Model B300C approved September 7.A24CE at Revision 110 dated July 9.23. The certification basis of the Beech B300 Series is FAR Part 23. There were three equivalent level of safety findings. plus SFAR 27 effective February 1. Three equivalent safety findings were made. plus Amendment 23-11.Type Acceptance Report 4. 2007 Transport Canada TCDS Number E-12 at Issue 20 dated May 23. 1974. (See the FAA TCDS for full details. effective February 1. 1965. plus some additional FAR 23 paragraphs at later amendment states depending on the aircraft serial number and date of production. 1990 – Model B200C/GT approved November 16. which have been reviewed and accepted by the CAA. plus some Special Conditions. effective February 1. and one exemption. 1973 – Model 200C approved February 21. 3072554 Change A or later (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the Beech 200 Series is FAR Part 23. including Amendments 23-1 through 23-9. TAR 98/18 – Beech Super King Air 6 Rev.000 feet. Later FAR 23 paragraph requirements were also applied for aircraft with Collins Proline 21 Avionics and EFIS installation.43 Data Requirements The type data requirements of NZCAR Part 21B Para §21. There are no non-compliances and no additional special conditions have been prescribed by the Director under §21.5 : 28 May 2015 . 1981 – Model B300 approved December 12. including Amendments 23-1 through 23-34 (Commuter Category). as specified on the TCDS. plus another for EFIS installations. Some paragraphs of FAR Part 25 were applied to aircraft approved for operation up to 35. 1979 – Model B200/C approved February 13.) This is an acceptable certification basis in accordance with NZCAR Part 21B Para §21. 2007 DoT Approved Parts List for the first production engine: – Version PT6A-41 – 21 August 1973 – Version PT6A-42 – 30 August 1979 – Version PT6A-60A – 5 August 1982 – Version PT6A-52 – See EA Dwg. One Special Condition was applied. as FAR 23 is the basic standard for Normal and Commuter Category Airplanes called up under Part 21 Appendix C. 2014 – Model 200 approved December 14.43 have been satisfied by supply of the following documents. plus some additional paragraphs at a later amendment date applicable to particular models. or were already held by the CAA: (1) ICAO Type certificate: FAA Type Certificate Number A24CE FAA Type Certificate Data Sheet no.41 and Advisory Circular 21-1A. 1965. NZCAR §21. including up to Amendment 27-6.
flight performance.621 Radiographic Inspection of Critical Castings – Less than 100% inspection was initially permitted subject to tracking of production examples. minimum operating oil temperatures are specified in the Flight Manual. (iii) Equivalent Level of Safety Findings: Model 200 Series up to S/N BB-1042: FAR §23. Model B300/300C: FAR 23. (ii) Special Conditions: All Models up to the B300: 23-47-CE-5 – At the time of the application for type certification of the Model 200. except A200CT and B200: FAR §23.997(d) Fuel Filter – In lieu of automatic means to maintain fuel flow due to ice clogging of the filter. the Model 200 fuel system includes a fuel-oil heat exchanger downstream of the 20 micron filter. Model 200 Series: 23-ACE-68 – When fitted with EFIS the aircraft must meet some specified Part 23 paragraphs at Amendment 23-41. A range of special conditions in the areas of propulsion. a pressurised turbine-powered aircraft capable of operating up to 33.Type Acceptance Report The certification basis of the Pratt & Whitney Canada PT6A Series is FAR Part 33. because the basic outline shape is the same.1443 Oxygen Mask – P/N 101-384102 mask which has been substantiated to FL340 was approved for operation to FL350 on the basis of a Flight Manual limitation to donn masks and descend immediately when oxygen is required.5 : 28 May 2015 7 TAR 98/18 – Beech Super King Air . and the natural position of the pilot's hand in grasping the knob will result in an equivalent tactile signal. Rev. FAR 23. including Amendments 33-1 to 33-5 inclusive. FAR 23.1321(d) Instrument Arrangement and Visibility – Basic "T" flight instruments. Model B300/300C: 23-ACE-48A – This required protection for systems that perform critical or essential functions from the effects of HIRF and exposure to lightning when an EFIS and autopilot flight director system is incorporated. This is the basic standard for aircraft engines called up under Part 21 Appendix C. An evaluation of each cockpit arrangement and layout was required as part of the B300 certification process. and anti-icing additives are available if those limitations cannot be met due to extremely low OAT.000 feet. and tests to show the aircraft can descend in time. a higher casting factor applied under BS 256.781(b) Cockpit Control Knob Shape – This was granted for the shape of the propeller RPM control lever knob. 23-131-SC – This applies the usual requirements for protection from the effects of HIRF for all systems that perform critical functions. FAA confirmed during these reviews that the ASI and/or altitude instruments were within the angle of 10° above to 15° below a horizontal line through the centre of the attitude indicator.1305(g) Powerplant Instruments – The FAA accepted the use of fuel low pressure warning annunciators would provide the required level of safely in lieu of fuel pressure indicators. the FAA determined the existing FAR Part 23 did not contain adequate safety standards. use of proven design and production principles. All Model 200 Series. stability and controllability were imposed. This Special Condition was originally applied separately to Rockwell Collins for when the Proline-21 EFIS was first fitted under an STC. Further. and satisfactory service experience. Model 200/C/T as noted on TCDS: FAR §23. plus this Special Condition for protection from HIRF for critical systems. fuel outlet. fire detection. which is a full-cylinder shape rather than the segment shown in the applicable requirement.
1305 and 23. and that flight testing would be carried out to ensure that V1 to VR acceleration would still be safe and acceptable. A set of specific criteria was established for defining the stall warning. 5077 FAR 23. including Amendments 36-1 through 36-10. -65B. This would provide considerable benefit to operators by reducing the required takeoff field length under similar conditions. instead of two required by the regulation.807(d)(1)(i) – B300 has only one emergency exit in the cabin.5 : 28 May 2015 . -60A. This was allowed because it had been FAA policy that two exits were not required for SFAR 41 aircraft with 9 or less passenger seats. due to a change in FAA policy. and fuel flow indications. -42A SB13003 – Defining Operating Time Between Overhauls (TBO) and Hot Section Inspection (HSI) Frequency for PT6A-52. It was accepted by the FAA on the grounds the earlier decision point would provide a safety benefit. and was inadvertently not incorporated in Amendment 23-34 which introduced the Commuter Category. (v) Airworthiness Limitations: Airplane Flight Manual Limitations Section – Models 200/200C Airplane Flight Manual Limitations Section – Models B200/C (1981-1984) FAA Approved Airworthiness Limitations Manual – Models B200/C (1985 and on) FAA Approved Airworthiness Limitations Manual – Models B300/C Chapter 4 of B300 Maintenance Manual Supplement 130-590031-67 (FN-1 and up) SB3002 – Defining Rotor Component Service Lives for the PT6A-38/41/42/45 SB3003 – Defining Operating Time Between Overhauls (TBO) and Hot Section Inspection (HSI) Frequency for the PT6A-38. TAR 98/18 – Beech Super King Air 8 Rev. as is permitted under Part 25 for Transport Category aircraft. -42. because of the high angles achieved prior to the stall.1549 – This ELOS provided for the use of digital only oil pressure and temperature. on the basis of satisfactory visibility and location. (Upgraded to Amendment 36-20 for production aircraft 1993 and later. and a set of normal operating procedures detailed during which the stall warning must not activate. 6405 FAR 23. 5599 FAR 23. No. -41. because the accelerate-stop distance would be less. and because trend information is provided by a colour change of the digital display. -60. which can also occur well below the single-engine-failure minimum control speed VMCA. including up to Amendment 27-4. in addition to the passenger entrance door. -61.) The Model B300 Series has been certificated under SFAR Part 27. and FAR Part 36. -65R (3) Aircraft Noise and Engine Emission Standards: (i) Environmental Standard: The Model 200 Series has been certificated under SFAR Part 27. and FAR Part 36. -62. -65AR. including Amendments 36-1 through 36-15. including up to Amendment 27-6. No. With this exemption the aircraft must be limited to a maximum of nine passenger seats.207(c) – Beech petitioned to permit type certification of the Model B300 with a stall warning beginning at airspeeds greater than 10 knots or 15 percent above the stalling speed. Beech contended that there were difficulties in showing compliance with aircraft that have a high power-to-weight ratio.Type Acceptance Report Model B200/B300 with Collins Proline 21 Avionics: ACE-02-16/17 FAR 23.53(c)(1) – Beech requested the use of ground minimum control speed VMCG for determination of takeoff decision speed V1. (iv) Exemptions: Model B300/300C: No.
Noise Certification – Model B200GT – 200E273045 Rev 2 B200GT/B200CGT – FAR 36 thru Amdt 36-28 take-off noise level: 81. 1974 Beech Structural and Flight FAA Substantiation Program for the Model 200 Beech Report 101E415D Rev.9 dB(A) [ICAO Annex 16 Chapter 10 take-off noise level: 76.2 dB(A) – see AFM Section IV B200/C – Flyover noise level: 79.24 dB(A) B200GT/B200CGT with High Flotation Gear (HFG) – FAR 36 thru Amendment 36-28 take-off noise level: 81. 1981 Minutes Final Type Certification Board Meeting B200 series.Type Acceptance Report (ii) Compliance Listing: 200/C – FAR 36 Flyover Noise Level 79.B – Structural Life Summary – Model 200 Beechcraft Type Inspection Report 200-1B – Certification of the Model 200 Includes – Part I – Ground Inspection.5 B300/C – FAR 36 Appendix G take-off noise level: 72. B200C.14 dB(A) (4) Certification Compliance Listing: FAA Airworthiness Requirements Compliance – Super King Air – Model 200 Beech Engineering Structures Report 101E430 SGS – dated January 1. B200C. Jan 29. B200CT and B200T Beech Aircraft Corporation Engineering Report 300E214 – FAA Requirements Compliance Checklist for the Beech King Air 350 Model B300 BAC Engineering Report 300E256 – Compliance Checklist Model B300C Beech Aircraft Corporation Engineering Report 101E3054 – FAA Certification Compliance Collins EFIS-84 Installation – Model B200 Beech Aircraft Corporation Engineering Report 101E3058 – FAA Certification Compliance Collins EFIS-84 Installation – Model B200 (2-Tube) Hawker Beechcraft Report 200E267407 – Engineering Certification Plan – Model B200GT/B200CGT – DOA Project No. B200T. 90-34849A-1 – dated 26 January 1981 Beech Engineering Structures Report 101E1361 S – dated December 22.2 dB(A) [Hartzell] or 75. AT4700WI-A Rev.45 dB(A) Hawker Beechcraft Corporation Engineering Acoustics Report .4 dB(A) [McCauley] Hawker Beechcraft Corporation Engineering Structural Dynamics Report – Takeoff Noise Test Report Model B300 – 300E290 Rev.5 dB(A)] B300/C Heavy Weight Aircraft – FAR 36 Appendix G and ICAO Annex 16 Chapter 10 take-off noise level: 81. 1981 Check Off List for FAA Approval under Delegation Option Procedures Document No. B200CT – dated February 13. Part II – Flight Test Report Beechcraft Type Inspection Report 200-48A – FAA Certification Models B200.5 : 28 May 2015 9 TAR 98/18 – Beech Super King Air . 1980 Structural Justification for Models B200. B200-50 – FAA Project No.
FM-53. 892. 830-853. BB-1843 thru BB-1977. FL 770. 912 and BL-1 thru BL-36) Hawker Beechcraft Super King Air 350. Heavy Weight Aircraft (16. FL-383 thru FL-499. BB-1979 thru BB-1987. Except FL-381. 871-873.5 : 28 May 2015 . 350ERi & 350CER – Pilot's Operating Handbook and FAA Approved AFM – P/N 130-590031-245 – CAA Accepted as AIR 3171 – (applicable to FL-493. FM-36-FM-38. FM-56 and after. 854-870. FM-43.Type Acceptance Report Pratt & Whitney Canada Engineering Report No. 6-733.500 lb) with Extended Range Fuel Tanks) [with Proline 21 Avionics] Beech Super King Air B200 & B200C – Pilot's Operating Handbook and FAA Approved AFM – P/N 101-590010-307 – CAA Accepted as AIR 3224 (applicable to BB-1439. except FL-493. BB-1988 and After. FM-14 and After. and FN-1) Beech Super King Air 350 & 350C – Pilot's Operating Handbook and FAA Approved AFM – P/N 130-590031-71B – CAA Accepted as AIR 3317 (applicable to FL-111 thru FL-382. 794-828. BW-1 thru BW-29) Beech Super King Air B200GT & B200CGT – Pilot's Operating Handbook and FAA Approved AFM – P/N 101-590168-1 – CAA Accepted as AIR 3291 (applicable to BY-1 and BZ-1 and After. Heavy Weight Aircraft With Or Without Extended Range Fuel Tanks) TAR 98/18 – Beech Super King Air 10 Rev. 793. 1440-1443 and BL-37 thru BL-138) Beech Super King Air 200 & 200C – Pilot's Operating Handbook and FAA Approved AFM – P/N 101-590010-127A – CAA Accepted as AIR 3094 (applicable to BB-2. FM-41. FM-12 & FM-13) [with Proline 21 Avionics] Beech Super King Air 350i. FL-938 and after. 894. FM-52. BL-139 thru BL-147. and airplanes with Kit 101-9113) Beech Super King Air B200/B200C – Pilot's Operating Handbook and FAA Approved AFM – P/N 101-590010-425 – CAA Accepted as AIR 3314 (applicable to BB-1834. 829. 350C & 350CER – Pilot's Operating Handbook and FAA Approved AFM – P/N 130-590031-499 – CAA Accepted as AIR 3319 – (applicable to FL-679. 6659 – PT6A-52 Compliance Plan Requirements Documents Summary (5) Flight Manual: Beech Super King Air B200 & B200C – Pilot's Operating Handbook and FAA Approved AFM – P/N 101-590010-147C – CAA Accepted as AIR 2626 (applicable to BB-734. FN-2 and after) [with Proline 21 Avionics] Beech Super King Air 350 & 350C – Pilot's Operating Handbook and FAA Approved AFM – P/N 130-590031-181 – CAA Accepted as AIR 3318 (applicable to FL-381. FM-14 and After)[with Proline 21 Avionics] Hawker Beechcraft Super King Air 350ER. BL-152 and After)[with Proline Avionics] Beech Super King Air 350 & 350C – Pilot's Operating Handbook and FAA Approved AFM – P/N 130-590031-1C – CAA Accepted as AIR 3316 (applicable to FL-1 thru FL-110. 913-1438. FM-9 thru FM-11. 350i & 350C – Pilot's Operating Handbook and FAA Approved AFM – P/N 130-590031-235 – CAA Accepted as AIR 3170 (applicable to FL-493. BB-1444 thru BB-1842. 896-911. BL-148 thru BL-151)[with Proline Avionics] Beech Super King Air B200/B200C – Pilot's Operating Handbook and FAA Approved AFM – P/N 101-590010-479 – CAA Accepted as AIR 3315 (applicable to BB-1978. 893. FM-1 thru FM-8. except BB-1463 and 1834. FL-500 and After. 735-792. 350iER. 874-891. 895. FL-500 and After.
Engine and Propeller: (i) Maintenance Manual: Beech B200/T Wiring Diagram Manual AF101-0010-161 Beech B/200C/T Wiring Diagram Manual AF101-0010-133 Beech Super King Air 200 Series Maintenance Manual AF101-0010-19 Super King Air 350/C Wiring Diagram Manual 130-590031-7 Beech B300/C Avionics Wiring Diagram Manual for Pro Line 21 130-590031-197 Super King Air 350i (B300) Wiring Diagram Manual (Interiors) 130-590031-317 Super King Air 350/C (B300 and B300C) Maintenance Manual 130-590031-11 Super King Air 350ER/CER (for Extended Range Tanks) Maintenance Manual and Wiring Diagram Manual Supplement 130-590031-247 Beech King Air Component Maintenance Manual 101-590097-13 PT6A-38/41/42/42A Maintenance Manual – Part Number 3021442 PT6A-38/41/42/42A Overhaul Manual – Part Number 3021443 PT6A-60A/60AG/61 Maintenance Manual – Part Number 3034342 PT6A-60A/60AG/61 Overhaul Manual – Part Number 3034343 PT6A-52 Maintenance Manual – Part Number 3072862 PT6A-52 Overhaul Manual – Part Number 3072863 (ii) Current service Information: Service Bulletins and Service Letters for Beech Model 200 Series Service Bulletins and Service Letters for Hawker Beechcraft Model B300/C PT6A-41/42/52/60A Service Bulletins (iii) Illustrated Parts Catalogue: Beech B200 IPC AF101-0010-159 Super King Air 350/C IPC 130-590031-9 Super King Air 350i/C IPC 130-590031-315 Super King Air 350ER/CER IPC Supplement 130-590031-247 (7) Agreement from manufacturer to supply updates of data in (5). Letter from Hawker Beechcraft Ref.5 : 28 May 2015 11 TAR 98/18 – Beech Super King Air .com/ (8) Other information: Memorandum Report 101E112 – Electrical Load Analysis – Model 200 Rev.Type Acceptance Report (6) Operating Data for Aircraft. Fax from Hawker Pacific confirming Revision Service ordered. and (6): All Flight Manual amendments currently provided by Raytheon to CAA.beechcraft. 2009 CAA from 2171 from Manager International Certification dated 18 Oct 2010 Access to publications is provided through http://www. 940-2009-05720 dated June 16.
: B300-58 Engineering Report 101E186388 Rev 1 – Electrical Load And Power Source Capacity Report for Model B200 with Proline 21 Phase II Options Hawker Beechcraft Corporation Engineering Report 200E311875 – Electrical Load and Power Source Capacity Report Model B200GT with Aviation Communications and Surveillance Systems TAWS+ Model B200GT – DOA Project No. B200-56 TAR 98/18 – Beech Super King Air 12 Rev.Type Acceptance Report Engineering Report 300E327933 Rev 1 – Electrical Load and Power Source Capacity Report for B300 Interior Upgrade – DOA Project No.5 : 28 May 2015 .
507 91. CAR Part 26 – Subpart B – Additional Airworthiness Requirements Appendix B – All Aircraft PARA: B.2.TSO C126 406 MHz after 22/11/2007 Operating Rule – Compliance to be determined by Operator Oxygen Indicators FAR §23.517 IFR 91.807(b) and §23.2 C.1449 for flight up to 35 000 ft.531(1)(ii).1443 Rev. except as noted: CAR Part 91 – Subpart F – Instrument and Equipment Requirements PARA: 91.Type Acceptance Report 5. Portable PBE 120l §23. This was accepted as meeting the requirements of §91.Pax Oxygen Mask. 15 min PBE See Compliance Table provided by Aeromotive Limited (2) 1 Set of Portable 15 min PBE Standard system designed to meet requirements of FAR (3) Crew Member .000+0/-500 ft cabin altitude with a red warning annunciator and flashing Master Warning annunciator. VFR 91. Oxygen for Pressurised Aircraft (1) Flight Crew Member On-Demand Mask.1 B.505 91.500 feet – this needs Visual/aural warning when cabin to be changed to 10.807(d)(2) FAR §23. It also actuates at 12. Additional New Zealand Requirements Compliance with the retrospective airworthiness requirements of NZCAR Part 26 has been assessed as they are a prerequisite for the grant of an airworthiness certificate.513 91.509 Min.000 feet to comply with §91.807(b) @ 10. (4) Spare Oxygen Masks/PBE (5) Min Quantity Supplement Oxygen FAR §23.1 Emergency Exit Evacuation Equipment – Descent means Emergency Exit Interior Marking – Size/self-illuminating Landing Gear Aural Warning – Automatic Flap Linking FAR §23.807(d)(1)(i) at Amendment 23-11 NOTE: Exemption granted by FAA for Model B300 FAR §23. N/A – Turbine (5) Fuel Contents Fitted as Std – See POH 7-34 (12) Flap Position Fitted as Std – See POH 7-12 (6) Engine RPM Fitted as Std – See POH 7-25 (13) U/c Position Fitted as Std – See POH 7-12 (7) Oil Pressure Fitted as Std – See POH 7-25 (14) Ammeter/Voltmeter Fitted as Std – See POH 7-35 (1)Turn and Slip Fitted as Std – See POH 7-10 (3) Anti-collision Lights Fitted as Std – See POH 7-37 (2) Position Lights Fitted as Std – See POH 7-37 (4) Instrument Lighting Fitted as Std – See POH 7-37 VFR Communication Equipment Operating Rule – Compliance to be determined by Operator (1) Gyroscopic AH Fitted as Std – See POH 7-10 (5) OAT Fitted as Std – See POH 7-10 (2) Gyroscopic DI Fitted as Std – See POH 7-10 (6) Time in hr/min/sec Fitted as Std – See POH 7-12 (3) Gyro Power Supply Suction gauge fitted as Std (7) ASI/Heated Pitot Fitted as Std – See POH 7-55 (4) Sensitive Altimeter Fitted as Std – See POH 7-10 (8) Rate of Climb/Descent Fitted as Std – See POH 7-10 IFR Communication and Navigation Equipment Operating Rule – Compliance to be determined by Operator Emergency Equipment: (a) More Than 9 pax – First Aid Kits per Table 7 To be determined on an individual aircraft basis – Fire Extinguishers per Table 8 To be determined on an individual aircraft basis (b) More than 20 pax – Axe readily accessible to crew Not Applicable – Less than 20 passenger seats (c) More than 61 pax – Portable Megaphones per Table 9 Not Applicable – Less than 61 passenger seats ELT .529 91. pressure altitude exceeds 10 000 The Model B300 has a pressure switch that actuates at 10.See POH 7-25 (3) Altimeter Fitted as Std – See POH 7-10 (10) Manifold Pressure N/A – Turbine (4) Magnetic Compass Fitted as Std – See POH 7-10 (11) Cylinder Head Temp.729(f) – See Flight Manual page 7-13 Compliance with the following additional NZ operating requirements has been reviewed (for the Model B/200/C) and were found to be covered by either the original certification requirements or the basic build standard of the aircraft.531 91.531(1)(ii). safety belts fastened N/A – Direct pilot communication available to passengers (1) ASI Fitted as Std – See POH 7-10 (8) Coolant Temp N/A – Turbine (2) Machmeter N/R (9) Oil Temperature Fitted as Std .93 C.523 91.2.000+500/-0 ft cabin altitude feet AMSL with a white advisory annunciator and cockpit aural warning.2 REQUIREMENT: MEANS OF COMPLIANCE: Marking of Doors and Emergency Exits Crew Protection Requirements – CAM 8 Appdx. B # .807(d)(1) – B200 exits less than 2m from ground To be determined on an individual aircraft basis FAR §23.1 Doors and Exits Additional Emergency Exits – per FAR 23.3.3 C.535 REQUIREMENT: MEANS OF COMPLIANCE: Seating and Restraints – Safety belt/Shoulder Harness Shoulder Harness Fitted as Standard – See POH Section 7 Pax Information Signs – Smoking.449 – Fitted as Standard – See POH Section 7 Volume/Pressure/Delivery NOTE: For Model 200 Series the aural warning is given at 12.5.511 Night 91.35 Placards – See Flight Manual Section II Limitations Not Applicable – Agricultural Aircraft only Appendix C – Air Transport Aeroplanes – More than 9 Pax PARA: REQUIREMENT: MEANS OF COMPLIANCE: C.1441 through FAR §23.5 : 28 May 2015 13 TAR 98/18 – Beech Super King Air .519 91.1 C.2.
Compliance with Part 91/125/135 operating requirements should be checked in each case. Five dual oxygen mask and container units provided.373 125.379 Seating and Restraints Additional Instruments (Powerplant and Propeller) Night Flight Landing light. Beech B300 comes under CAR Part 125 for Air Transport operations because MCTOW over 5700 kg and Payload less than 3410 kg. spare bulbs/fuses Emergency Equipment (Part 91.357 135. Alt.15 (6) Required Supplemental/Therapeutic Oxygen Above FL250 – Quick-Donning Crew On-Demand Mask – Supplemental O2 Masks for all Pax/Crew – Supplemental Mask in Washroom/Toilet Above FL300 – Total Outlets Exceed Pax by 10% – Extra Units Uniformly Distributed – Automatically Presented Above FL140 – Manual Means of Deploying Pax Masks SSR Transponder and Altitude Reporting Equipment Altitude Alerting Device – Turbojet or Turbofan Assigned Altitude Indicator ELT Installation Requirements Crew provided with diluter-demand quick-donning masks.543 91. particularly oxygen system capacity and emergency equipment.377 125.1305 Operating Rule – Compliance to be determined by Operator Operating Rule – Compliance to be determined by Operator Not Applicable – Not SEIFR Operating Rule – Compliance to be determined by Operator Not Applicable – Less than 20 passenger seats Not Applicable – Less than 10 passenger seats Not Applicable – Minimum flight crew is one Not Applicable – Less than 10 passenger seats Not Applicable – Not turbo jet or turbofan powered Operating Rule – Compliance to be determined by Operator Operating Rule – Compliance to be determined by Operator Not Applicable – Not SEIFR Operating Rule – Compliance to be determined by Operator 125. (The 13 seat capacity on the TCDS under Note.11 appears to be only applicable to the B200 with Mod. Pax compartment IFR Operations Speed.7 requires TSO C92 AEDRS Terrain Awareness and Warning System (TAWS) Appendix B.361 125. CAR Part 125 – Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 125. 3.1305 Operating Rule – Compliance to be determined by Operator Operating Rule – Compliance to be determined by Operator Operating Rule – Compliance to be determined by Operator N/A – Only for 2-crew helicopters with more than 10 pax Not Applicable – Less than 10 passenger seats fitted Not Applicable – Not turbo jet or turbofan powered NOTE: When assessing compliance with requirements based on seating configuration. and compliance is achieved by the basic aircraft type design.365 125.) TAR 98/18 – Beech Super King Air 14 Rev. Alt. Basic Operating Weight = 9920 lb.541 91. An FAR reference in the Means of Compliance column indicates the US rule was exactly equivalent to the CAR requirement. spare bulbs/fuses SE IFR Requirements – If Applicable Emergency Equipment (Part 91. 2.381 Operating Rule – Compliance to be determined by Operator NOTES: 1. it was assumed the B/200/C was fitted with 9 passenger seats or less.355 135.) However for compliance with NZCAR §43.10 requires TSO C118/119a or C119b/c FAR §23.523 (a) and (b)) Cockpit Voice Recorder Flight Data Recorder Additional Attitude Indicator FAR §23.367 125.4 requires TSO C124 Additional Attitude Indicator Weather Radar – Appendix B.371 Seating and Restraints – Shoulder harness flight-crew seats Additional Instruments (Powerplant and Propeller) Night Flight Landing light.359 135.369 125.363 125-364 125.3 requires TSO C84/C123 Flight Data Recorder – Appendix B.369 135.785 FAR §23.000 lb.357 125.1447(e) FAR §23.5 : 28 May 2015 .361 135.367 135.361 125.363 135.523 (a) and (b)) Protective Breathing Equipment Public Address and Crew Member Intercom System Cockpit Voice Recorder – App B. (MCTOW = 15. Some means of compliance above are specific to a particular model/configuration. and therefore must be maintained by a Part 145 Maintenance Organisation.545 A.Type Acceptance Report 91.1447(f) Operating Rule – Compliance to be determined by Operator Not Applicable by engine type Operating Rule – Compliance to be determined by Operator To be determined on an individual aircraft basis CAR Part 135 – Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 135.54(a)(1)(ii) the 200/B200/C Series is classified as having a maximum certificated number of passenger seats of more than 10. 101-000015 – High Density Configuration with External Baggage Pod. Pax compartment IFR Operations Speed.371 125.6 requires TSO C63 GPWS – Appendix B.9 requires TSO C151a or b Airborne Collision Avoidance System (ACAS II) Appendix B.359 125.375 125.355 125.785 FAR §23. plus a second manual outlet and a first aid mask in the rear cabin Yes – Ten outlets for nine passengers Yes – In cabin ceiling FAR §23.
........ David Gill Team Leader Airworthiness ……………………………..5 : 28 May 2015 15 TAR 98/18 – Beech Super King Air .Type Acceptance Report Attachments The following documents form attachments to this report: Photographs Beech B200 serial number BB-1087 ZK-KAD (NZ1883) Photographs Hawker Beechcraft B300 “350i” s/n FL-727 ZK-MMM Three-view drawing Beech Model B200 Super King Air Three-view drawing Beech Model B300 King Air 350i Copy of FAA Type Certificate Data Sheet number A24CE Sign off ……………………………………..... Checked – Andrea Wadsworth Airworthiness Engineer Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: B200/C (1981-92) Aeromotive Holdings Limited 98/21B/18 6 July 1998 200/C (1974-81) Garden City Helicopters Limited 9/21B/17 29 September 2009 B300/300C * Hawker Beechcraft Corporation 11/21B/13 19 January 2011 * Aircraft covered by the Flight Manuals P/N 130-590031-235 and -245) B200/C (1992 on) Hawker Pacific NZ Limited 12/21B/20 1 August 2012 B200GT/B200CGT Beechcraft Corporation 15/21B/4 14 August 2014 B300/B300C * Skyline Aviation Limited 15/21B/20 28 May 2015 * All serial numbers up to aircraft covered by POH/AFM P/N 130-590031-235/245/499) Rev...
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