TCDS LTC-28

SUPERIOR AIRCRAFT COMPANY MODELS: Superior Culver Army PQ-14A, PQ-14B, YPQ-14A, YPQ-14B (Navy) ID2C1 (Approved 12/16/47) SPECIFICATICN NUMBER: I-28-2 (Eligible for Certification in Limited Category only.) (Holder of Limited Type Certificate: N.A. Kalt, Dallas, IX) Engine Franklin 0-300-11 Fuel Grade 100/130 Engine limits Maximum, except take-off (Full throttle) (17,000 ft.) 3200 rpm (90 hp) (Full throttle) (7,500 ft.) 3200 rpm (130 hp) (22.3 in.Hg.) (Sea level) 3200 rpm (130 họ) 2930 rpm (155 hp) Take-off (one minute) 3.3 in. Hg.) 3200 rpm (130 h Propeller fixed pitch wood, Model 66CA63. Diameter 66 inches. Airspeed limits (See NOTE 2) Glide or dive - 234 mph Maximum gross weight C.G. range 26.07 inches (19.8 percent MAC) to 27.23 inches (22.4 percent MAC) Datum Forward face of firewall bulkhead MAC 44.75 inches I.E. MAC 17.2 inches other operating limitations сту T.0. 09-5FC-1 (1/31/40 Certification basis imited Type Certificate No. 28 (CAR 9 effectiv 11/21/46) Production basis None may be produced under this approval Export eligibility for a Certificate of Airworthiness No equipment other than engines and propellers are specified. such 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 operation of the aircraft. In addition, the aircraft may incorporate such military armament) as was originally incorporated in the type for military or naval Additional equipment may re installed as can be substantiated on the rasis that it presents no obvious hazard to safety. Weight and Balance Report including list of equipment included in the certificated empty weight must be submitted for each aircraft. or Navy weight records in current condition may be surmitted in lieu of an actual weight. The equipment list need include no more than the Required equipment as defined under "Equipment" above. so located or of such weight that their remova! or arditioritems noticeably affect the weight and balance of the aircraft. Additional items as may be reasonably considered removable and are built into the aircraft structure need not be listed. list must be prepared by the applicant for the approval of the 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 In full view of passengers: 'This is a military type aircraft and under the Civil Air Regulations shall not be used for the carriage passengers or cargo for compensation or hire. ' In the cockpit in full view of the pilot: Wing Flaps - Do not lower above 117 Landing Gear - Do not lower above 117 mph. All acrobatics except stalls prohibited. The following statement must appear on the Operation Limitations: 'This airplane must be operated at all times within the limitations set torth in the Army Technical Order No, 09-5FC-1, 1/31/46, except for limitations specifically called out in Aircraft Specification AI-28 in which case the values given in the Specification must be observed. A copy of Army Technical Order 09-5FC-1 and Aircraft Specification AL-28 must be carried during flight." In all cases it will be the responsibility do have the secret ailable Technical Orders. The C.A.A. 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 C.A.A. representative to show that the modified airplane maintains the same degree of airworthiness as the original. C.A.A. can give no technical assistance on such matters since complete structural data for NL aircraft are not required by Part are not available in the C.A.A. For certification for night flying the following must re accomplished: factorily modify the lights if vin certificated upe satis Type A-9 wing positior. lights (AN-3033-5 through -8) may be satisfactorily modified by painting the inside frosted portior of the cover black. through -4) are satisfactory without modification. Replace the tail light with a certificated unit. (c) If "Bright and Dim" conditions are provided for the position lights, either 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 wing-tip and tail lights, or the switches should be placarded to indicate that only the "bright condition" should be used. In either case the tail light and wing-tip lights should operate on one switch. No original NI airworthiness certificates may be issued after 8/31/48. The list of mandatory changes required prior to original certification may be obtained from CAA Aircraft Service, Washington, D.C. Attn: A~298_