TCDS A25WE

Page No. 1 2 3 Rev. No. 3 3 3 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A25WE Revision 5 Grumman TS-2A April 9, 1984 TYPE CERTIFICATE DATA SHEET NO. A25WE This data sheet, which is a part of Type Certificate No. A25WE, prescribes 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 California Division of Forestry Department of Conservation 1416 Ninth Street Sacramento, California 95814 I - Model TS-2A (Restricted Category) Approved August 2, 1974 (See NOTES 2, 4, and 5,) Engine 2 Wright R1820-82 using 100/130 grade fuel; retimed and operated to Wright R1820-80 specifications Fuel Minimum grade as above Oil Esso 100 or equivalent; 3-GP-100, Mil-L-6082 grade 1100 Engine limits (BHP/RPM/MAP/ALT) Takeoff 1475/2800/54.5/S.L. (5 Minutes) 1475/2800/54.0/1700 Normal Rated 1275/2500/46.5/S.L. (Meto) 1275/2500/45.5/3500 Propeller Hamilton Standard Three-bladed Hydromatic Hub Model - 43D51-303, -329, -341, -343, -355 Blade - 6915C-7, 6915E-7, 6985B-7, or 6985C-7 Diameter - 11 ft. 0 in. Airspeed limits Vmo (Maximum operating) 221 KTS - 252 MPH (IAS) Va (Maneuvering) 175 KTS - 201 MPH Vf (Flaps extended) 150 KTS - 172 MPH Vle (Landing gear extended) 150 KTS - 172 MPH Maximum retardant drop speed 130 KTS - 149 MPH C.G. range Fwd. 213.4 in. aft of ref. Datum '0' Landing Gear Aft. 219.63 in. aft of ref. Datum '0' Extended Fwd. 216.05 in. aft of ref. Datum '0' Landing Gear Aft. 220.94 in. aft of ref. Datum '0' Retracted Landing Gear Retraction Moment/1000 = 32.0 in. -lb. (Moves C.G. aft) Datum Reference Datum '0' is located 94.64 forward of jig point forward face of bulkhead at Sta. 96. A25WE Leveling means Exterior skin edge along stringer 12 between Sta. 205 and 255. Maximum weights Takeoff 27,000 lbs. Landing 24,500 lbs. Minimum crew One pilot @ Sta. 111.0 Number of seats 2 at Sta. 110.9 Fuel capacity Two wing tanks, for total of 521 gals. at 227.25 in. Oil capacity One tank each Nacelle, for total of 27 gals. at 192.5 in. Maximum operating altitude 22,000 ft. Control surface movements See Navair 01-85SAA-2 (Handbook of Maintenance Instruction) Serial Numbers eligible The original Navy designation for the following airplanes was the S2F-1 and this designation will appear on the nameplate. Post- delivery modifications were made resulting in S2F-1T for training use. In 1962, a new numbering system was established for all military airplanes and the S2F-1 became the S2A. Consequently, the trainer S2F- 1T version was called the TS-2A. Only those airplanes listed below are eligible for Airworthiness Certification. Airplanes modified for the special purpose of forest and wildlife conservation (fire fighting) in accordance with CDF Drawing List 1277-2000: Grumman S/N Navy S/N 367 136458 423 136514 Airplanes modified for the special purpose of forest and wildlife conservation (fire fighting) in accordance with CDF Drawing List 1277-1000: Grumman S/N Navy S/N Grumman S/N Navy S/N 016 133045 383 136474 017 133046 388 136479 027 133056 399 136490 052 133081 403 136494 061 133090 404 136495 114 133143 410 136501 119 133148 416 136507 128 133157 417 136508 152 133181 419 136582 161 133190 421 136512 170 133199 455 136546 175 133204 476 136567 179 133208 477 136568 195 133224 481 136572 204 133233 492 136583 205 133234 503 136594 208 133237 504 136595 212 133241 522 136613 216 133245 527 136618 217 133246 543 136634 222 133251 549 136640 247 133276 569 136660 249 133278 570 136661 254 133283 572 136663 255 133284 578 136669 3 A25WE 256 133285 585 136676 259 133288 590 136681 266 133295 613 136704 276 133305 624 136715 281 133310 656 136747 293 133322 665 136726 295 133324 666 144705 298 133327 673 144712 308 136399 675 144714 330 136421 684 144723 369 136460 695 147551 Certification basis FAR 21.25(a)(2) effective February 1, 1965. Restricted Type Certificate No. A25WE dated August 2, 1974, issued for the special purpose of forest and wildlife conservation (fire fighting). Application for Restricted Type Certificate dated October 26, 1973. Production 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 must be installed in the aircraft for certification. NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary must be provided for each aircraft at the time of original certification. NOTE 2. The aircraft shall be operated in accordance with the NATOPS Flight Manual 01-85SAA-1, plus the FAA Approved Airplane Flight Manual Supplement dated August 2, 1974, required for the special purpose usage. NOTE 3. Reserved. NOTE 4. Prior to issuance of an airworthiness certificate for each aircraft and at the prescribed intervals, all inspections and modifications must be accomplished per the latest revision of the California Department of Forestry S-2 Airtanker Technical Directive Index. NOTE 5. Upon completion of the conversion to certificated status in the restricted category, the manufacturer's nameplate on the aircraft must be altered to include the TS-2A designation and that it has been modified per T.C. A25WE. In case the original nameplate is not sufficiently large enough to include this additional information, a similar plate should be installed near the original plate. Under no circumstances should the original or any succeeding nameplate be removed from the aircraft. .....END.....