# TCDS A5NW: Starbird Inc. - Type: Type certificate data sheet - Status: Current - Holder: Starbird Inc. - Revision: 4 - Revised: June 29, 1981 - Product: Aircraft, Large Airplane - Certification basis: Part 21 - Data sheet PDF: https://openairdocs.org/files/sha256/37/44/3744170a15f32a932d4b787e5395d1f149a8bfa84f86710996828ca911024668 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A7782C983B18D46D852567270060E6F7.0001 - Page: https://openairdocs.org/tcds/A5NW ## Models (1) As the data sheet lists them. - C-119L ## 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. 4 4 4 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A5NW Revision 4 FAIRCHILD C-119L June 29, 1981 TYPE CERTIFICATE DATA SHEET NO. A5NW This data sheet which is a part of Type Certificate No. A5NW prescribes the conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Starbird, Inc. 9333 Stitch Road Lake Stevens, Washington 98258. I - MODEL UNITED STATES AIR FORCE (FAIRCHILD) C-119L (RESTRICTED CATEGORY) APPROVED May 31, 1979 Engine 2 Wright R-3350-89, 89A, 89B/95W Fuel 100/130 Minimum Grade Aviation Gasoline Engine limits 2900 rpm (3500 hp) Takeoff, wet, low blower 2900 rpm (2800 hp) Maximum, dry, low blower 2600 rpm (2600 hp) Meto, low blower 2600 rpm (1760 hp) 10,000 ft. Alt., Meto, high blower 2300 rpm (1560 hp) 10,000 ft. Alt., Cruise, high blower 2100 rpm (1460 hp) 10,000 ft. Alt., Cruise, high blower Propeller Hamilton, Standard 43H60-603 or 605 Hubs with R-A6959B-0 blades. See Note 2. Airspeed limits 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. Sta. 0 (103.8" forward of jig point fitting on front jack pad) Maximum gross wt. 71,500 lbs. Maximum landing weight 69,970 lbs. Maximum zero fuel weight 61,240 lbs. (Outer wing tanks to be full before fuel is added to inner wing tanks). Leveling means Eye bolt at cabin 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 3624 total - 2 outboard fuel tanks 855 Gal. each (+354.5) - 2 inboard fuel tanks 457 Gal. each (+354.5) - 2 auxiliary fuel tanks in fuselage. 500 Gal. each (+338.0). A5NW 2 Oil capacity 120 gal. total - 2 nacelle Applicable Serial No. (AF) tanks 60 gal. each (+338.4) 51-2662 thru 51-8030 51-5098 " 51-8168 51-17365 " 51-17367 52-6000 " 52-6003 53-8069 " 53-8132 Oil capacity (cont'd) 109 gal. total - 2 nacelle 51-8031 thru 51-8097 tanks 54.5 gal. each (+338.4) 52-5840 thru 52-5954 (includes any AF C-119G 52-6004 thru 52-7884 Serial No. except those listed 53-8133 thru 53-8156 above. Cargo capacity See T.O. 1C-119L-1 Section V Control surface movements Aileron Up 24" + 1" Down 12" + 1" (See Sec. VIII T.O. Flettner Tab Up 17" + 4" - 2" Down 30" + 6" -2" 1C-119G-1-1, Trim Tab Up 15" + 1 1/2" Down 12" + 1 1/2" Page 8-4) Elevator Up 24 1/2 + 1 1/2" Down 12" + 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 eligible Air Force Serial Numbers Manufacturers Serial Numbers (See NOTE 2A) 51-2662 thru 51-8168 For aircraft exported and returned to U.S. 51-17365 thru 51-17367 10676-10678 52-6000 " 52-7884 10702-10726 52-5840 " 52-5954 10735-10738 53-3137 " 53-3193 10773-10776 53-3201 " 53-3216 10823-10825 53-7836 " 53-7884 10870-10872 53-8069 " 53-8156 10905-10908 10942-10945 10954-10957 10992-10994 11219 Certification basis FAR 21.25(a)(2) dated May 1974 Amendment 21-1 thru 21-46 Restricted Category Type Certificate issued on May 31, 1979. Date of Application: January 21, 1979. 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 workmanship, materials, and conformity with the approved technical data. 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 Starbird Airplane Flight Manual Supplement is required in addition to the operating limitations specified in Sec. V of T. O. 1C-119L-1. NOTE 1. Current weight and balance report and loading instructions must agree with Sec. V of T.O. 1C-119L-1. 3 A5NW NOTE 2. This approval applies to: A. Basic United States Air Force C-119G airplanes modified to C-119L in accordance with USAF T.O. 1C-119-688 with no other major modification except loading assist device installation per Starbird Drawing SI-1000. B. Airplane certified for special purposes of carriage of cargo. (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 state in the form of placards, markings, and manuals." (4) Red radial line required on airspeed indicator at 217 knots. (5) 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 USAF T.O. 1C-119G-2-1. .....END..... ``` ## ADs None name its models. ## STCs approved under this data sheet (2) - [STC SA2675NM](https://openairdocs.org/stc/SA2675NM): Modify Type Design by the Installation of Buld Liquid Cargo Tank Assembly Installed.. Sorm Inc - [STC SA1549NM](https://openairdocs.org/stc/SA1549NM): Installation of Westinghouse J34-WE-34, J34-WE-36 jet engine on top center line of fuselage.. Hawkins & Powers Avn 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.