TCDS LTC-30

MODELS: General Dynamics (Consolidated) (Army) C-87A (Approved 1/6/48) SPEC. NUMBER: L-30-2 (Eliqible for Certification in Limited Category only.) (Holder of Limited Type Certificate: William P. Odom, Roslyn, L.I., NY) Engines Pratt & Whitney F-1830-43 or -65 Fuel Engine limits 43.5 in. H9. 2550 Ipm (1100 hp) 2550 Ipm (1100 hp) (6200 ft.) 41.0 in. 48.0 in. Hg.. 2700 rpm (1200 hp) Propellers Hamilton Standard 23E50 hub; 6353A-18 or 6477A-0 (See NOTE 2) Diameter 11'7". Airspeed limits (See NOTE 2) Glide or dive - 355 mph Maximum weight C.G. range 23 percent MAC to 32 percent MAC Datum 311.5 inches forward of center line of main 123.7" L.E. MAC 260 in. aft of datum Other Operating Limitations Technical Order AN-01-bCA-1, 4/25/46 Certification basis Limited Type Certificate No. 30 (CAR ? effective 11/21/46) Production basis None may be produced under this approval Export eligibility Not eligible for a Certificate of Airworthiness for Export No equipment other than engines and propellers are specified. equipment as required by Civil Air Regulations Part 43.30 for the particular operation authorized for NC aircraft must be installed. any additional equipment necessary for the proper speration of the aircraft. In addition, the aircraft may incorporate such military equipment (except armament) as was originally incorporated in the type for military or naval Additional equipment may be installed as on the basis that it presents no obvious hazard to safety. weight and Balance Report including list of equipment included in the certificated empty weiqht must be submitted for each aircraft. or Nary veight records in current condition may be submitted in lieu of an actual weight. The equipment list need include no more than the Required equipment as defined under "Equipment" above. items as may be reasonably removable and are so located or of such weight that their removal or addition could noticeably affect the weight and balance of the aircraft. the aircraft structure need not be listed. The equipment list nust be prepared by the applicant for the approval cating C.A.A. representative, and in such form that it can be attached to the C.A.A. Operation Limitations. The following placards must be prominently displayed in the positions indicated: In full view of passengers: This is a military type aircraft 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 of the pilot: "Do not exceed 155 mph with flaps fully extended or 190 mph with flaps extended 10 degrees. ' "Do not lower landing gear at a speed in excess of 155 mph." "Slow down to 150 mph when flying in extremely turbulent air." "Do not use automatic pilot at a speed less than 155 mph." "With 23850/6353A-18 propellers installed, avoid operation between The following statement must appear on the Operation Limitations: This airplane must be operated at all times within the limitations set forth in Army Technical Order No. AN-01-5CA-1 except for limitations specifically called out in Aircraft Specification AL-30 in which case the values given in the Specification must be observed. A copy of the pertinent Army Technical Order and Aircraft Specification AL-30 must be carried during flight.' In all cases it will be the responsibility of the applicant to secure copies of the Army Technical Orders. does not have these documents available for distribution. NOTE 4. 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 oridence to a C.A.A. representative to shov that the modified airplane maintains the same degree of airvorthiness as the original. The C.A.A. can give no technical assistance on such matters since complete structural data for #I aircraft are not required by Part 9 and ror certification for night flying the folloving must be teplace the ving position lights vith certificated units or modify the lights if pertinent. ving position lights (AN-3033-5 through -8) may be satisfactorily modified by painting the inside frosted portion of the cover black. Type A-9 (AN-3033-1 through -4) are satisfactory without modification. ter te on tors not he die coated or to petition a dear single-pole-single-throw switch should be used to replace the two single-pole-double-throw switches presently installed for ving-tip and tail lights or the switches should be placarded to indicate the "bright condition" should be used. In oither case the tail light and ving-tip lights should operate on one svitch. No original NI airworthiness certificates may be issued after 8/31/48. list of mandatory changes required prior to original certification may be obtained From CAA Aircraft Service, Washington 25, D.C.