Type Certificates and Maintenance Data

2-32 United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate _____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. _____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) Page 1 of 1 This certificate may be transferred in accordance with FAR 21.47.

Number SA7855SW This Certificate issued to certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part 23 of the Federal Aviation Regulations. Original Product Type Certificate Number : Description of Type Design Change: Installation of McCauley B3D32C419/82NHA-5 Propeller on Commander Model 114 airplane in accordance with Commander Aircraft Co., Installation Instructions dated July 13, 1990, Revision A dated August 22, 1990, or later FAA approved revision. Limitations and Conditions: FAA approved Commander Aircraft Co. Flight Manual Supplement dated August 23, 1990, must accompany this modification. The installer must determine whether this design change is compatible with previously approved modifications.

If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Commander Premier Aircraft Corporation 20 Stanford Drive Farmington, CT 06032 A12SO Make : Commander Model : 114 Date reissued :March 03, 2006 Date amended :Amd. 1, September 10, 1990 By direction of the Administrator _______________________________________________________ ( Signature) Michele M. Owsley, Manager Airplane Certification Office, Southwest Region _______________________________________________________ ( Title) Date of application :February 09, 1990 Date of issuance :August 23, 1990 SAMPLE 2-33 After 1978, the POHs generally took on both roles.

• Maintenance Manuals—These manuals are often referred to as Aircraft Maintenance Manual (AMM) or Component Maintenance Manual (CMM). The AMM is focused on the entire aircraft and provides the “big picture” for the maintenance technician. It provides information concerning the maintenance, including troubleshooting and repair, of the aircraft and systems on the aircraft. The CMM, on the other hand, is focused on a specific item or component, such as hydraulic pump, generator, or thrust reverser. It provides the bench mechanic with detail troubleshooting information and usually serves as an overhaul manual giving details for disassembly, cleaning, inspection, repair as necessary, reassembly, and testing in accordance with approved standards and technical data accepted by the Administrator. Refer to 14 CFR part 43 section 43.2(a).

When maintenance is done according to the CMM, the technician must always include the appropriate references in the maintenance record entry required by 14 CFR part 43, section 43.9 or 43.11. Service Bulletins (SB) Throughout the life of a product (whether TC’d or not), manufacturing defects, changes in service, or design improvements often occur. When that happens, the OEM frequently uses an SB to distribute the information to the operator of the aircraft. SBs are good information and should be strongly considered by the owner for implementation to the aircraft. However, SBs are not required unless they are referred to in an AD note or if compliance is required as a part of the authorized inspection program. Refer to section 14 CFR part 39, 39.27.

Structural Repair Manual (SRM) As the name implies, this manual carries detail information for the technician concerning an aircraft’s primary and secondary structure, criteria for evaluating the severity of the detected damage, determining the feasibility of a repair, and alignment/inspection information. This manual is usually a separate manual for large aircraft. On small aircraft, this information is often included in the AMM.

Forms

Airworthiness Certificates In addition to the registration certificate that indicates the ownership of an aircraft, an airworthiness certificate indicates the airworthiness of the aircraft. AC 21-12, Application for U.S. Airworthiness Certificate, FAA Form 8130-6, is a comprehensive guide for the completion of the application form for this certificate. There are two certificates: standard • Recommended overhaul periods • Details for an inspection program that identifies both the frequency and the extent of the inspections necessary to provide for continued airworthiness • Troubleshooting information • The order and method for proper removal and replacement of parts • Procedures for system testing during ground operations • Diagrams for structural access plates • Details for application of special inspection techniques • Information concerning the application of protective treatments after inspection • Information relative to the structural fasteners • List of any special tools needed Airworthiness Limitations The ICA must contain a separate and clearly distinguishable section titled “Airworthiness Limitations.” Within this section are mandatory replacement times, structural inspection interval, and related inspection procedures.

All of this is included in the initial release of documents when the aircraft is delivered. However, over the course of the life of an aircraft, various modifications can and often do occur. Whether these are as simple as a new cabin to galley sliding door, or as complex as a navigation related STC, any major alteration requires that this type of maintenance data be provided to the owner, so that subsequent maintenance, inspection, and repair can be properly accomplished. As aircraft and their systems become more and more complex, and society continues its preoccupation with litigation for every incident, it is imperative that the technician have the right information, that it is current, and that they have the proper tools, including those required for any special inspection, and correct replacement parts. If any one of these items is required, and the technician does not have it accessible, they are in violation of 14 CFR sections 65.81(b), 43.13(a), and 43.16 if they attempt to return the aircraft to service.

Manufacturers may provide this required information in a variety of different manuals: • Operating Instructions—The Airplane Flight Manual (AFM) or the Pilot’s Operating Handbook (POH) provides the pilot with the necessary information to properly operate the aircraft. These manuals are usually listed in the aircraft TCDS, and therefore are a required item for the aircraft to be considered airworthy. Note that the AFM is generally serial number specific, whereas the POH is model specific. 2-34 CodeBranch AC ASW-150 Description Ft. Worth Airplane Certification Office AK ACE-115N Anchorage Aircraft Certification Office AT ACE-115A Atlanta Aircraft Certification Office BA ANM-100B Boeing Aviation Safety Oversight Office (BASOO) BO ANE-150 Boston Aircraft Certification Office CE ACE-112 Small Airplane Directorate CH ACE-115C Chicago Aircraft Certification Office DE ANM-100D Denver Aircraft Certification Office EN ANE-140 Engine Certification Office GU ACE-100G Gulfstream Aviation Safety Oversight Office (GASOO) IB ANM-116 Transport Airplane Directorate International Branch LA ANM-100L Los Angeles Aircraft Certification Office MC ACE-100M Military Certification Office NY ANE-170 New York Aircraft Certification Office RC ASW-170 Ft. Worth Rotorcraft Certification Office SC ASW-190 Ft. Worth Special Certification Office SE ANM-100S Seattle Aircraft Certification Office Code Description A Small Airplane B Balloon E Engine G Glider P Propeller R Rotorcraft S Airship T Transport Airplane I Experimental Q Other, or not product ST New Supplemental Type Certificate (STC) AT Amended Type Certificate SA Amended Supplemental Type Certificate SP Special Project (e.g. approval under section 21.305 project) Table 3–Product Type Designators Code Description EPD Engine-Propeller RCD Rotorcraft SAD Small Airplane TAD Transport Airplane Table 4–Directorate Designators Code Description BOS-AEG Boston AEG FTW-AEG Fort Worth AEG MKC-AEG Kansas City AEG LGB-AEG Long Beach AEG Table 5–Aircraft Evaluation Group Designators WI ACE-115W Wichita Aircraft Certification Office SEA-AEG Seattle AEG As an example, TC00125AT-A would be a TC project assigned by the Atlanta ACO on a small airplane with the assigned number 00125.

FAA Project Numbering and Designators Table 1–Project Type Designators Code Description TC New Type Certif icate (TC) PM Parts Manufacturer Approval (PMA) Table 2–Aircraft Certification Office (ACO) Designators FAA Project Numbers will use the following format: AAnnnnnYY-X Where: • AA is the two-letter designator for Project Type – see table 1 below • nnnnn is the integer sequential number for the specified ACO; e.g., 00146 • YY is the two-letter designator for the Aircraft Certification Office (ACO) – see Table 2 below • X is the one-letter designator for the Product Type – see Table 3 below As an example, TC00125AT-A would be a TC project assigned by the Atlanta ACO on a small airplane with the assigned number 00125.

and special. FAA Form 8100-2, Standard Airworthiness Certificate, may be issued to allow operation of a type- certificated aircraft in one or more of the following categories: [Figure 2-20] • Normal • Utility • Acrobatic • Commuter • Transport • Manned free balloon • Special classes FAA Form 8130-7, Special Airworthiness Certificate, may be issued to authorize the operation of an aircraft in the following categories: [Figure 2-21] • Primary • Restricted • Multiple • Limited • Light-sport 2-35 SAMPLE 2-36 Page No 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 Rev. No. 111 101 104 97 82 97 82 99 97 101 111 104 96 101 101 110 Page No 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 Rev. No. 111 101 82 95 91 108 111 101 101 101 101 101 100 78 101 110 Page No 33 34 35 36 37 38 39 40 41 42 43 Rev. No. 104 111 110 110 111 108 111 96 100 101 101 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A24CE Revision 111 Beechcraft 200 A100-1 (U-21J) 200C A200 (C-12A) 200CT A200 (C-12C) 200T A200C (UC-12B) B200 A200CT (C-12D) B200C A200CT (FWC-12D) B200CT A200CT (C-12F) B200T A200CT (RC-12D) 300 A200CT (RC-12G) 300LW A200CT (RC-12H) B300 A200CT (RC-12K) B300C A200CT (RC-12P) B300C (MC-12W) A200CT (RC-12Q) B300C (UC-12W) B200C (C-12F) 1900 B200C (UC-12M) 1900C B200C (C-12R) 1900C (C-12J) B200C (UC-12F) 1900D B200GT B200CGT July 21, 2015 TYPE CERTIFICATE DATA SHEET NO. A24CE This data sheet which is part of Type Certificate No. A24CE prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.

Type Certificate Holder: Beechcraft Corporation 10511 E. Central Wichita, Kansas 67206 Type Certificate Holder Record: Beech Aircraft Corporation transferred to Raytheon Aircraft Company on April 15, 1996 Raytheon Aircraft Company transferred to Hawker Beechcraft Corporation on March 26, 2007 Hawker Beechcraft Corporation transferred to Beechcraft Corporation on April 12, 2013 I. Model 200, Super King Air (Normal Category), Approved December 14, 1973 (See NOTES 10 and 11) Model A200C (UC-12B), Super King Air (Normal Category), Approved February 21, 1979 (See NOTE 11) Model 200C, Super King Air (Normal Category), Approved February 21, 1979 (See NOTE 11) Model B200, Super King Air (Normal Category), Approved February 13, 1981 (See NOTES 10 and 11) Model B200C, Super King Air (Normal Category), Approved February 13, 1981 (See NOTES 10 and 11) Model B200C (C-12F), (UC-12F), (UC-12M) and (C-12R), Super King Air (Normal Category), Approved February 13, 1981, (See NOTES 10, 11, and 12) For Notes, refer to Data Pertinent to All Model 200 Series Engine Two United Aircraft of Canada, Ltd., or Pratt & Whitney PT6A-41 (turboprop) per Beech Specification BS 22096 (200, 200C, A200C)