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bushed    
a. 被草丛笼罩的,疲倦的

被草丛笼罩的,疲倦的

bushed
adj 1: very tired; "was all in at the end of the day"; "so beat
I could flop down and go to sleep anywhere"; "bushed
after all that exercise"; "I'm dead after that long trip"
[synonym: {all in(p)}, {beat(p)}, {bushed(p)}, {dead(p)}]

bushed \bushed\ (b[.u]sht), pred. adj.
very tired from exertion.

Syn: all in(predicate), beat(predicate), dead(predicate),
dead tired(predicate), knocked out(predicate).
[WordNet 1.5]


Bush \Bush\, v. t. [imp. & p. p. {Bushed} (b[.u]sht); p. pr. &
vb. n. {Bushing}.]
1. To set bushes for; to support with bushes; as, to bush
peas.
[1913 Webster]

2. To use a bush harrow on (land), for covering seeds sown;
to harrow with a bush; as, to bush a piece of land; to
bush seeds into the ground.
[1913 Webster]


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英文字典中文字典相关资料:


  • PART 23—AIRWORTHINESS STANDARDS: NORMAL CATEGORY AIRPLANES
    View the PDF for 14 CFR Part 23; These links go to the official, published CFR, which is updated annually As a result, it may not include the most recent changes applied to the CFR Learn more
  • Federal Aviation Regulation Sec. 23. 25 - Weight limits. - RisingUp. com
    Sec 23 25 — Weight limits (a) Maximum weight The maximum weight is the highest weight at which compliance with each applicable requirement of this part (other than those complied with at the design landing weight) is shown
  • Quick Reference for Part 23 and Associated Advisory Circulars
    Latest Revisions of ACs are available at rgl faa gov Part 23 Rules Applicable Advisory Circulars, latest revision AC Titles Subpart A, General 23 1, Applicability 1AC 23-21, 2AC 23-8, Weight limits AC 23-8 23 29, Empty weight and corresponding center of gravity AC 23-8 23 31, Removable ballast AC 23-8 23 33Propeller speed and pitch limits
  • § 23. 25 - Weight limits. , General, Subpart B - Flight, Part 23 . . .
    § 23 25 Weight limits (a) Maximum weight The maximum weight is the highest weight at which compliance with each applicable requirement of this part (other than those complied with at the design landing weight) is shown The maximum weight must be established so that it is - (ii) The required minimum crew, and fuel and oil to full tank capacity
  • 14 CFR § 23. 25 - Weight limits. - GovInfo
    Chapter I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION Subchapter C - AIRCRAFT Part 23 - AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES Subpart B - Flight Subjgrp - General Section § 23 25 - Weight limits
  • 14 CFR §23 Airworthiness Standards: Normal Category Airplanes - Code of . . .
    PART 23 - AIRWORTHINESS STANDARDS: NORMAL CATEGORY AIRPLANES Authority: 49 U S C 106(f), 106(g), 40113, 44701-44702, 44704, Pub L 113-53, 127 Stat 584 (49 U S C 44704) note Source: Doc No FAA-2015-1621, Amdt 23-64, 81 FR 96689, Dec 30, 2016, unless otherwise noted
  • AC 120-27F - Aircraft Weight and Balance Control
    This advisory circular (AC) provides operators with guidance on how to develop and receive approval for a Weight and Balance (W B) control program for aircraft operated under Title 14 of the Code of Federal Regulations (14 CFR) part 91 subpart K (part 91K), and parts 121, 125, and 135
  • 14 CFR § 23. 2100 - Weight and center of gravity.
    § 23 2100 Weight and center of gravity (a) The applicant must determine limits for weights and centers of gravity that provide for the safe operation of the airplane
  • 14 CFR 23. 2005 -- Certification of normal category airplanes.
    § 23 2005 Certification of normal category airplanes ( a ) Certification in the normal category applies to airplanes with a passenger-seating configuration of 19 or less and a maximum certificated takeoff weight of 19,000 pounds or less
  • Federal Aviation Regulations
    Sec 23 25 - Weight limits (a) Maximum weight The maximum weight is the highest weight at which compliance with each applicable requirement of this part (other than those complied with at the design landing weight) is shown





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