# TCDS A8NM: DMI Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: DMI Aviation Inc. - Revision: 3 - Revised: June 6, 1984 - Product: Aircraft, Large Airplane - Certification basis: Part 21 - Data sheet PDF: https://openairdocs.org/files/sha256/a3/15/a315150d40bf72ba783462d8a1127b3d6413043c006565a001154983cb9cad69 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F22B67F2B8C7741D8525672700601CAB.0001 - Page: https://openairdocs.org/tcds/A8NM ## Models (1) As the data sheet lists them. - C-119F/R4Q2 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 Rev. No. 3 3 3 FEDERAL AVIATION ADMINISTRATION A8NM Revision 3 FAIRCHILD C-119F/R4Q2 June 6, 1984 TYPE CERTIFICATE DATA SHEET NO. A8NM This data sheet which is a part of Type Certificate No. A8NM prescribes the conditions and limitations under which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder DMI Aviation, Inc. 5080 East Nebraska Tucson, Arizona 85706 I - MODEL (FAIRCHILD) C-119F/R4Q2 (RESTRICTED CATEGORY) APPROVED March 31, 1982 Engine 2 Wright R-3350-89, 89A, 89B/95W, 36W, 36WA Fuel 115/145 - Alternate 100/130 Minimum grade aviation gasoline Engine limits 2900 rpm (3420 hp) Takeoff, wet, low blower 2900 rpm (2600 hp) Maximum, dry, low blower 2600 rpm (2555 hp) Meto, low blower 2600 rpm (1710 hp) 10,000 ft. Alt., Meto, high blower 2300 rpm (1520 hp) 10,000 ft. Alt., Cruise, high blower 2100 rpm (1430 hp) 10,000 ft. Alt., Cruise, high blower See NATOPS Flight Manual NAVAIR 01-115CCB-1 Propeller Hamilton Standard P/N 24260-615 (hub); C-2J17AA-3-26R (blades) Airspeed Vne - Never exceed (217 knots) Vc - Structural Cruising (176 knots) Va - Maneuver (162 knots) Flaps or gear extended (140 knots) C.G. range Aft of datum +318.3" to +335.2" at all Wts. Datum Fus. Station 0 (103.8" forward of jig point fitting on front jack pad) Max. gross weight 71,500 lbs. Max. landing weight 69,970 lbs. Max. zero fuel weight 60,500 lbs. (Outer wing tanks to be full before fuel is added to inner wing tanks). Leveling means Eye bolt at ceiling station 310 for plumb bob suspension to cross lined plates under cargo floor between stations 310 and 333. Number of seats Limited to the Flight Crew and number of persons essential to perform the intended function of this operation. Fuel capacity 2798 total - 2 outboard fuel tanks 905 gal. ea. (+354.5) 2 inboard fuel tanks 494 gal. ea. (+354.5) A8NM 2 Oil capacity 120 gal. total - 2 nacelle tanks 60 gal. ea. (+338.4) Cargo capacity See NAVWEPS 01-115CC-9 Control surface movements Aileron Up 24 + 1 Down 12 + 1 (See NAVAIR 01-115CCB-2 Flettner Tab Up 17 + 4 - 2 Down 30 + 6 -2 Sec. II, Fig. 2-11, Trim Tab Up 15 + 1 1/2 Down 12 + 1 1/2 numbers in degrees) Elevator Up 24 1/2 + 1 1/2 Down 20 1/2 + 1 1/2 Spring Tab Up 17 + 0 - 5 Down 24 + 2 - 0 Trim Tab Up 12 + 2 Down 22 + 2 Rudder Right 25 + 2 - 0 Left 20 + 2 - 0 Spring Tab Right 5 + 1 Left 5 + 1 Trim Tab Right 10 1/2 + 1 Left 10 1/2 + 1 Wing Flaps Take-off Down 15 Landing Down 40 Serial Numbers Military Serial Numbers Manufacturers Serial Numbers 131669 10836 131673 10840 131700 10855 131677 10844 Certification basis FAR 21.25(a)(2) dated May 1974 Amendment 21-1 thru 21-53. Restricted Category Type Certificate issued on March 31, 1982. Date of Application: October 19, 1981 Airplane certified for the special purpose of carriage of cargo. Production basis None - prior to original certification of each aircraft, an FAA representative must perform an inspection for airworthiness, workmanship, materials, and conformity with the approved technical data. The FAA representative must verify that the aircraft records are complete, that no major modifications have been accomplished, and that the aircraft was never exported from the United States. Equipment The basic required equipment as prescribed in the applicable Airworthiness Regulations (See Certification Basis), must be installed in the aircraft for certification. In addition, an FAA approved DMI Aviation, Inc. Airplane Flight Manual Supplement is required in addition to the operating limitations specified in Sec. I, Part 4 of NAVAIR 01-115CCB-1. NOTE 1. Current weight and balance report and loading instructions must agree with Sec. I, Part 4 of NAVAIR 01- 115CCB-1. NOTE 2. This approval applies to the basic military C-119F, R4Q2 with no major modifications. In addition, (1) Operation over densely populated areas is prohibited. (2) In addition to the operating limitations in this data sheet, area, economic, passenger and other appropriate operating limitations in accordance with FAR 21.25 shall be shown on placards or listing accessible to the pilot. (3) The following placard must be displayed in front of and in clear view of the pilot: "This airplane must be operated as a restricted category airplane in compliance with the operating limitations stated in the form of placards, markings, and manuals." (4) Red radial line required on airspeed indicator at (217 knots). 3 A8NM (5) The following placard must be displayed adjacent to the APU operating switch: "APU operation prohibited in flight" (6) Carriage of hazardous materials is prohibited unless compliance is shown with the applicable regulations in the Code of Federal Regulation 49, Part 175. NOTE 3. The aircraft must be serviced and maintained in accordance with NAVAIR 01-115CCB-2. .....END..... ``` ## ADs None name its models. ## STCs approved under this data sheet (2) - [STC SA1502NM](https://openairdocs.org/stc/SA1502NM): Installation of Westinghouse J34-WE-36 jet engine on top center line of fuselage.. Hawkins & Powers Avn Inc - [STC SA1632NM](https://openairdocs.org/stc/SA1632NM): ONE-ONLY STC, S/N 10836: Installation of Bulk Liquid Cargo Tank Assembly. Sorm 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.