# TCDS LTC-12: Cameron Leland H. - Type: Type certificate data sheet - Status: Current - Holder: Cameron Leland H. - Revision: 0 - Revised: April 14, 1947 - Product: Aircraft, Small Airplane - Certification basis: CAR 9 - Data sheet PDF: https://openairdocs.org/files/sha256/de/1c/de1c4a51ed3b9f417bcbbc0df228c05c16d64810b8f7dc72f170b4e0d6e29096 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33F3078ADCED98788525672E0064AAA5.0001 - Page: https://openairdocs.org/tcds/LTC-12 ## Models (4) As the data sheet lists them. - Army AT-10GF - Army AT-10 - Army AT-10BH - Army AT-10GL ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text BEECH_AIRCRAFT CORPORATION MODELS: Beech, Army AT-10, AI-10BH, AI-10GL, AI-10GF I.C. NUMBER: LTC-12 (Approved 4/14/47) Eligible for Certification in limited Category only. (Holder of Limited Type Certificate, Leland H. Cameron, Chicago, IL.) Engines 2 Lycomings R-680-9 or -13 Fuel 87 minimum octane aviation gasoline Engine limits Maximum. except take-off (Sea 2200 Ipm Propellers Hamilton Standard 2B20 hub: 1012 (285 hp) ; take-off (one min.) 2300 rpm (300 hp) 6135A-9 blades Diameter - 8ft. 3 in. Gor. Airspeed limits (See NOTE 2) glide or dive 230 mph Maximum weight 6600 1bs. C.G. range 18.1 percent to 26.2 MAC (gear down) Datum 41.16 in. forward of jig point at front face of pilot's compartment which is 95 in. forward CL of spar at fuselage MAC 90 in. L. E. MAC +72.4 1n. Other Operating Army T.O. No. AN-01-90KB-1, 9/25/44 Certification basis Limitations Limited Type Certificate No. 12 (CAR 9 effective 11/21/46) Export eligibility Production basis None may be produced under this approval Nor eligible for Export Certificate EQUIPMENT: No eguipment other than engine and propellers are specified. However, such equipment as required CAR 43.30 for the particular operation authorized for NC aircraft must be installed. additional equipment necessary for the proper operation of the aircraft. In addition, the aircraft may incorporate such military equipment (except armament) as was originally incorporated in the type for military or Additional equipment may be installed as can be substantiated on the basis that it presents no obvicus hazard to safety. Weight and Balance Report required. Army or Navy weight records in current condition may be submitted in lieu of an actual weight. equipment list need include no more than the following: Required equipment as defined under "Equipment" above. Additional items as may be reasonably considered removable and are so located or of such weight that their removal or addition could noticeably affect the weight and balance of the aircraft. built into the aircraft structure need not be listed. list must be prepared by the applicant for the approval of the CAA agent and in such form that it can be attached to the CAA Operations Limitations. NOTE 2- The following placards must be prominently displayed in the positions indicated: In full view of passengers: 'This is a military type aircraft and under the Civil Air Regulations shall not be used for the carriage of passengers or cargo for compensation or hire." In the cockpit in full view or the pilot: "Do not lower landing gear above 125 mph." extended.i "Do not retract flaps under 100 mph if extended." "Do not exceed 125 mph with cockpit enclosure open." Do not operate landing lights above 110 mph any longer than necessary." "All acrobatics prohibited." The following statement must appear on the Operation Limitations, "This airplane must be operated at all times within the limitations set forth in Army T.O. No. AN-01-90KB-1 except for limitations specifically called out in Aircraft Spec. AL-12 in which given in the specification must be observed. A copy of the pertinent Army I.O. and Aircraft Spec. AL-12 must be carried during flight. all cases it will be the responsibility of the applicant to secure copies of the Army Technical and Navy Service Change orders. have these documents available for distribution. If any repairs or modifications are made prior to and/or subsequent to NI certification, it is the responsibility of the owner to furnish sufficient evidence to CAA representative to show that airplane maintains the same degree of airworthiness as the original. The CAA can give no technical assistance on such matters since structural data for NL aircraft are not required by Part 9 and therefore are not available in the CAA. For certification for night flying the folloving must be Replace the wing position lights with certificated units or satisfactorily modify the lights if pertinent. wing position lights (AN-3033-5 through -8) may be satisfactorily modified by painting the inside frosted portion of the cover black. through -4) are satisfactory without Replace the tail light with a certicated unit. 'Bright and Dimi conditions are provided for the positich lights, the resistors should be disconnected from the circuits and a single-pole-single-throw switch should be used to replace the two single-pole-double-throw switches presently installed for tail lights, or the switches should be placarded to indicate that only the "bright condition" should be used. case the tail light and wing-tip lights should operate on one No original NL airworthiness certificate may be issued after 9/31/'?. The mandatory changes required prior to original certification may be obtained from CAA Aircraft Service, Washington, D.C. Attn: A-208. ``` ## ADs None name its models. ## STCs approved under this data sheet (1) - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc --- 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.