# TCDS LTC-26: Executive Airlines Inc. - Type: Type certificate data sheet - Status: Current - Holder: Executive Airlines Inc. - Revision: 2 - Revised: November 17, 1947 - Product: Aircraft, Small Airplane - Certification basis: CAR 9 - Data sheet PDF: https://openairdocs.org/files/sha256/65/38/6538cd8516bea5e6755c11f269174c1483a1db05fbe335ea613909de14791274 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AAD2A9AFABB0FD758525673E0050C2ED.0001 - Page: https://openairdocs.org/tcds/LTC-26 ## Models (7) As the data sheet lists them. - Army L-1 - Army L-1C - Army L-1D - Army L-1E - Army L-1A - Army L-1F - Army L-1B ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text 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. ``` ## ADs None name its models. ## STCs approved under this data sheet (13) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc. - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA6070NM](https://openairdocs.org/stc/SA6070NM): Installation of a 'quick-disconnect drain plug' on the engine rocker sump for the oil drain retrieval system after engine shutdown.. West Coast Air Creations - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey - [STC ST00961LA](https://openairdocs.org/stc/ST00961LA): Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29, 2000, or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1, "Slug Thrower Cartridges Master Drawing List", Revision N/C, dated June 26, 2000, or later FAA approved revisions.. AMETEK AMERON LLC d/b/a MASS Systems - [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC - [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC - [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 SA1351WE](https://openairdocs.org/stc/SA1351WE): Replace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12). Ceconite 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.