# TCDS A9WE: Emerald Enterprises Ltd. - Type: Type certificate data sheet - Status: Historical, Abandoned - Holder: Emerald Enterprises Ltd. - Revision: 2 - Revised: January 3, 2023 - Product: Aircraft, Small Airplane - Certification basis: Part 23, CAR 3 - Registered aircraft: 7, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/34/62/34629bddf3a29c8f1fc572057f0dd8b1f91c088f6d8ba27de6d4b968ff82d263 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103820223520250813174312.0001 - Page: https://openairdocs.org/tcds/A9WE ## Models (1) As the data sheet lists them. - D-1 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev. No. 2 1 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A9WE Revision 2 EMERALD (Wing Aircraft) Model D-1 June 3, 1998 TYPE CERTIFICATE DATA SHEET NO. A9WE This data sheet, which is a part of type certificate No. A9WE prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder Record Emerald Enterprises LTD. c/o Hillyer & Irwin 550 West C St., 16th Floor San Diego, CA 92101-3540 I. Wing Aircraft Model D-1 (Normal Category) approved December 20, 1966 Engines 2 Lycoming Model IO-320-B1C or 2 Lycoming Model IO-320-C1A Fuel 100/130 Minimum grade aviation gasoline Engine limits For all operations, 2700 rpm (160 hp) Propeller and 2 Hartzell Model HC-C2YL-2RB/8459-18 propeller limits Diameter: Not over 66 in., not under 64 in. Pitch setting at 30 in. station: Low: 13.5° High: 20.0° Feathered: 77° to 79° Airspeed limits MPH KNOTS (CAS) Vne (Never exceed) 252 219 Vno (Maximum structural cruising) 200 174 Vp ( Design maneuvering) 170 148 Vfe (Max. Flap extended) 135 117 Vle (Max. landing gear extended) 170 148 Vlo (Max. landing gear operating) 170 148 C.G. range Sta. +89.5 to Sta. +93.0 up to 2,400 lbs. (Landing gear extended) Sta. +90.5 to Sta. +93.0 at 3,050 lbs. Straight line variation between points given. Landing gear retraction moment (-165 in.-lbs.) and moves C.G. forward. Empty weight (C.G. range) None Datum Fuselage Station 0 (fuselage nose). Leveling means Partially withdraw two machine screws located at Fus. Sta. 104.75 and Sta. 117.80 at WL 44.680 on the left hand side of the fuselage. These screws are the leveling points. Maximum weight 3,050 lbs. Max. landing weight 2,900 lbs. Type Certificate Holder This Type Certificate (TC) has been designated as Abandoned (See note 3) A9WE 2 Minimum crew One Number of seats Two at Sta. 87.0 Maximum baggage 250 lbs. at Sta. 118.0 Fuel capacity 2 tanks, 265 lbs. each at Sta. 92.0 Oil capacity 2 tanks, 15 lbs. each at Sta. 61.2 Control surface movements Elevator Up 21° + 1° Down 10° + 1° Rudder Right 26 1/2° + 1° Left 26 1/2° + 1° Ailerons Up 30° + 2° Down 10° + 1° Flaps Up 0° + 2° Down 40° + 1 1/2° Stabilizer: (Measured at Leading Edge from Fus. Ref. Line) Leading Edge Angle Electric Sys. Down 3 1/2° + 1/4° Up 1/2° + 1/4° Manual Sys. Down 3 1/2° Up 2° Serial Nos. eligible Serial Numbers 2 and up. Certification basis Civil Air Regulation Part 3 dated May 15, 1956, together with Amendments 3-1 through 3-8, and FAR 23.201, 23.203, 23.205 and 23.207 in lieu of the stall requirement of Amendment 3-7. Production basis None. Prior to original certification of each aircraft an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data, and a check of the flight characteristics. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. Wing Aircraft Report No. RD1-16, Part II, "Equipment List", contains a list of all required equipment that must be installed. NOTE 1. (a) Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter. (b) The airplane must be loaded so that the C.G. is within the specified limits at all times, including the effect of fuel usage. (c) Unusable fuel and undrainable oil must be included in the certificated empty weight and corresponding center of gravity location. NOTE 2. The following placard must be displayed in front of and in clear view of the pilot: "This airplane must be operated as a normal category airplane in compliance with the FAA Approved Airplane Flight Manual." .....END..... NOTE 3. Additional required placards are specified in the Limitations section of FAA Approved Airplane Flight Manual. This Type Certificate (TC) has been designated "ABANDONED". A “Notice of Intent To Designate as Abandoned Certain Type Certificates Issued in the Restricted Category,” was published by the Federal Aviation Administration (FAA) in the Federal Register on January 3, 2023 (68 FR 47379). That Notice listed this TC. The FAA received no comments on the published Notice. The FAA has been unable to contact this TC holder. Hence, the FAA has determined that this TC holder is not complying with its Continued Operational Safety (COS) responsibilities. Therefore, no additional aircraft will be added to this TC and no additional original airworthiness certificates will be issued based on this TC. The effectiveness of this TC is limited to those aircraft that received original airworthiness certification prior to the incorporation of this note (Date of Incorporation, January 3, 2023). Subsequently, if the TC holder is located and assumes their COS responsibilities, the restriction(s) imposed by this note may be lifted. ``` ## ADs (3, in force first) - [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000 - [AD 82-08-05 R1](https://openairdocs.org/ad/82-08-05-R1): Placard - Cabin Heater · Emerald Enterprises D-1. Effective Aug 4, 1982 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 ## Registered aircraft by registry model (OpenAirDocs) - [Wing D-1](https://openairdocs.org/model/wing-d-1): 7 aircraft (registry codes 9690302, 9690303) ## STCs approved under this data sheet (17) - [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd. - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA4316WE](https://openairdocs.org/stc/SA4316WE): Installation of inflatable door seal.. TALCO Aviation Corp. dba RAJAY Turbo Products - [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley - [STC SA4315SW](https://openairdocs.org/stc/SA4315SW): Installation of Brittain B5 flight control system.. Brittain Industries, Inc - [STC SA4553SW](https://openairdocs.org/stc/SA4553SW): Installation of Brittain Model NAV Flite IV Model BI-825 system or B5C Model BI826 system. Brittain Industries, Inc - [STC SA02118CH](https://openairdocs.org/stc/SA02118CH): Installation of C&D Associates Combustion Heater Kit 16 P/N CD11004K16. Hartzell Engine Technologies, LLC - [STC SA1688WE](https://openairdocs.org/stc/SA1688WE): Installation of Brittain Industries Model B-4A flight control system.. Brittain Industries, Inc - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc - [STC SA02168AK](https://openairdocs.org/stc/SA02168AK): Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.. Avalaska Inc - [STC SA4373WP](https://openairdocs.org/stc/SA4373WP): Installation of Astronautics corp of america automatic pilot models P1, P2, P2A, P3, P3A, P3B, EPT, P3A-APT, P3B-APT.. Astronautics Corporation of America - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc - [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.