TCDS LTC-26

SHINSON DIVISICN CONSCLIDATED VULTEE AIRCRAFT CORPORATION MODEIS: Stirsoved 11/17/47) I-1, I-1A, I-1B, I-1C, L-1D, L-1E, and I-1F SPECHFICATION NUMBER: 1-26-2 (Eligible for Certification in Limited Category only.) (Holder of Limited Type Certificate: Executive Airlines, Inc., Cleveland, OH) Engine Fuel minimum octane aviation gasoline Engine limits Maximum, except take-off (Sea level) 200 rpm (285 hp) Take-off (one minute) 2300 pm (300 hp) Propeller 2820 hub; 62414-6 blades 8 ft. 6 in. Airspeed limits Glide or dive - 160 mph (See NOTE 2) Maximum gross weight I-1-3: 325 1bs. I-1A, I-1B, I-1C, L-1D, L-1E, I-1F-3: 395 1bs. C.G. range 28.5 percent MAC to 36 percent. MAC Catum 76.6 inches forward of L.E. of wing MAC 80 inches L.E. MAC 76.6 inches aft of datum Other operating limitations Army T.O. AN-01-50 DA-1 Certification basis Limited Type Certificate No. 26 (CAR 9 effective 11/21/46) Production basis None may be produced under this approval Export eligibility Not eligible for a Certificate of Airworthiness No equipment other than engines and propellers are specified. However, such as required by Civil Air Regulations Part 43.30 for the particular operation authorized for NC aircraft must be installed. Also, any additional equipment necessary for the proper operation of the aircraft. In addition, the aircraft may incorporate such military equipment (except as was originally incorporated in the type for military or naval Additional equipment may be installed as can re surstantiated on the basis that it presents no obvious hazard to safety. weight and Balance Report including list of equipment included in the certificated empty weight must be surmitted for each aircraft. Navy weight records in current condition may be submitted in lieu of an actual weight. The 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. The equipment list must be prepared by the applicant for the approval of the certificating CAA representative, and in such form that it can be attached to the CAA Operation Limitations. The following placards must be prominenthy displayed in the positions In full view of passengers: ¿This is a military type aircraft and under the Civil Air Regulations shall not re used for the carriage of passengers or cargo for compen- sation or hire." In the cockpit in full view of the pilot: ¿Do not exceed 81 mph with flaps "Maneuvers prohibited: outside loop, snap rolls, inverted spins, inverted flight." The following statement must appear on the Operation Limitations: airplane must be operated at all times within the limitations set forth in the Army Technical Order No. 01-50DA-1, except for limitations specifically called out in Aircraft Specification AI-26 in which case the values given in the Specification must be observed. Army Technical Order 01-50DA-1 and Aircraft Specification AI-26 must be carried during flight. In all cases it will be the responsibility of the applicant to secure copies of the Technical Orders. does not have these documents available for distribution. If any repairs or modifications are made prior to and/or subsequent to NL certification, it is the responsibility of the owner to furnish sufficient evidence to a CAA representative to show that the modified airplane maintains the same degree of airworthiness as the original. The CAA can give no technical assistance on such matters since complete structural data for NI aircraft are not required by Part 9 and therefore available in the CAA. Prior to obtaining certification for "Night Flying" the following modifications to the exterior lighting must be made to comply with CAF, Parts 15.2 and 03.538. Position Lights: Wing Tip - The type A-7 or A-8 light assemblies are not satis- replaced with certificated light assemblies. The type A-9 (AN-3033-10 or AN-3033-5 through -8) light assemblies may be satisfactorily modified by painting the sand-blasted portion of the inner surface of the AN-1042-3 and -4 covers The AN-3033-9 or AN-3033-1 through -4 light assemblies are satisfactory without modification. present lights are not satisfactory and must be replaced with a certificated unit. Position Light Circuit and Control: The fosition light (wing tips ard tail) shall be controlled by one The circuit should be protected by its own fuse or The individual wing tip and tail light switches with dim and bright positions and the dimming resistors presently installed shall be removed. Other Exterior Lights: with the exception of the landing lights, any other exterior lights are not required and may be removed if so desired. No original NL airworthiness certificates may be issued after 8/31/48. list of mandatory changes required prior to original certification may ke obtained from CAA Aircraft Service, Washington, D.C. Attn: A-298.