Text in force at CAR3R-8: from CAR3R-7, effective 3 May 1962. OCR text
. . * . . (ce) Category A.* * * (2) For both the flaps retracted and flaps extended conditions, the applicable Hmiting airspeed and positive limit maneuvering load factor shall not be exceeded. For the flaps extended condition, it shall be acceptable to retract the flaps during recovery, provided a placard is installed prohibiting intentional spins with flaps extended. §§ 3.124-1, 3.124-2 [Deletion] 9. By deleting §§ 3.124-1 and 3.124-2. 10. By amending §3.174-1(a) by deleting from the parenthetical expression the words “Secs. 1.654 and 1.655 of ANC— 5a 1949 edition “’ and inserting in lieu thereof “Sections 1.6.5.4 and 1.6.5.5 of MIL-HDBK-5”; and by amending the related footnote to read as follows: +MIL-HDBE-6, “Strength of Aircraft Elements" ts published by the Department of Defense and the Federal Aviation Agency and may be obtained from the Superintendent of Documents, Government Printing Office, Washington 25, D.C. § 3.174-3 [Amendment] 11. By amending § 3.174-3(a) (1) by deleting the expression “ANC-5” and inserting in lieu thereof “MIL-HDBK-5”, §3.174-7 [Amendment] 12. By amending § 3.174-T7(c) by deleting the phrase “in ANC-5 and ANC-— 18” and inserting in lieu thereof “in MIL-HDBK-5, MIL-HDBK-17 Part I, ANC-17 Part Il, ANC-18, MIL-HDBK-23 Part I, and ANC-23 Part II”. § 3.184 [Amendment] 13. By amending § 3.184 by inserting in the first sentence between the words “speeds” and “shall” the words “shall be equivalent air speeds (EAS) and”; and by adding to each of the parenthetical expressions after the word “speed” the abbreviation “, m.p.h.”, §3.216-5 [Amendment] 14, By amending § 3.216-5 by deleting from paragraph (a) the phrase “in § 3.216 (a), (b), and (c)” and inserting in lieu thereof “in § 3.216(c)”; and by deleting from paragraph (b) the phrase “in §3.216(c)” and inserting in lieu thereof “in § 3.216”, § 3.216-6 [Amendment] 15. By amending § 3.216-6 by deleting the equation _TM(W/S) _ (W/S) a ES Cmax and inserting in lieu thereof _TM(W/S) _ (W/S) oe Cras 16 § 3.244 [Amendment] 16. By amending Figure 3-12(b) referred to in § 3.244 as follows: TAIL WHEEL TYPE SEE NOTE 8 BROUND LINE TAN" aK. (SEE NOTE I) at LEVEL LANDING fed LEVEL LANDING WITH INGLINED REACTIONS TaNtK SEE NOTES NOTE] GROUND LINE, TAIL DOWN LANDING FIG. 3- 12 (b) BASIG LANDING CONDITIONS C2 TANT ok n=l LEVEL LANOING WITH NOSE WHEEL JUST CLEAR OF GROUND 17. By amending § 3.301 by deleting the last sentence and inserting in lieu thereof “Values contained in MILHDBK-5, MIL~HDBK-17 Part I, ANC17 Part II, ANC-18, MIL-HDBK-23 Part I, and ANC-23 Part II shall be used unless shown to be inapplicable in a particular case” and by amending the note to read as follows:
section with altitudes from sea level to 8,000 feet and with temperatures at these altitudes from minus 60° F. below standard to plus 40° F, above standard shall be included. § 3.780-2 [Deletion] 60. By deleting § 3.780-1. (Sees. 318(a), 601, 603; 72 Stat. 752, 775, 776; 49 U.S.C, 1354(a), 1421, 1423) Issued in Washington, D.C., on March 27, 1962, N. E. Haasy, Administrator. EPR. Doc. 62-3085; Filed, Apr. 2, 1962; 8:45 a.m.) (As published in the Federal Register Lai FAR. 31607 April 3, 1962) ·