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CS-25 BOOK 1 EASA Certification Specifications for Large Aeroplanes CS-25 Book 1 Airworthiness code 1-0-1
BOOK 1 CS-25 1-0-2
Page 1 and 2: European Aviation Safety Agency ED
Page 3 and 4: European Aviation Safety Agency Cer
Page 5: CS-25 INTENTIONALLY LEFT BLANK C-2
Page 9 and 10: CS-25 BOOK 1 INTENTIONALLY LEFT BLA
Page 11 and 12: CS-25 BOOK 1 (3) The highest weight
Page 13 and 14: CS-25 BOOK 1 or 2%, whichever is gr
Page 15 and 16: CS-25 BOOK 1 and the corresponding
Page 17 and 18: CS-25 BOOK 1 (ii) 1·5% for three-e
Page 19 and 20: CS-25 BOOK 1 (2) The weight equal t
Page 21 and 22: CS-25 BOOK 1 CONFIGURATION SPEED MA
Page 23 and 24: CS-25 BOOK 1 (c) V MC may not excee
Page 25 and 26: CS-25 BOOK 1 CS 25.171 STABILITY Ge
Page 27 and 28: CS-25 BOOK 1 CS 25.181 Dynamic stab
Page 29 and 30: CS-25 BOOK 1 greater, except that i
Page 31 and 32: CS-25 BOOK 1 INTENTIONALLY LEFT BLA
Page 33 and 34: CS -25 BOOK 1 appropriate to each p
Page 35 and 36: CS -25 BOOK 1 (b) Manoeuvring envel
Page 37 and 38: CS -25 BOOK 1 (1) May not be less t
Page 39 and 40: CS -25 BOOK 1 angular acceleration
Page 41 and 42: CS -25 BOOK 1 (2) At speeds between
Page 43 and 44: CS -25 BOOK 1 flight load condition
Page 45 and 46: CS -25 BOOK 1 the lateral displacem
Page 47 and 48: CS -25 BOOK 1 may be considered. Th
Page 49 and 50: CS -25 BOOK 1 (b) For towing points
Page 51 and 52: CS -25 BOOK 1 CS 25.561 Emergency L
Page 53 and 54: CS -25 BOOK 1 determination must be
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CS-25 BOOK 1 (1) Where applied load
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CS-25 BOOK 1 CS 25.631 (vi) Any sin
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CS-25 BOOK 1 (2) Each fitting, pull
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CS-25 BOOK 1 CS 25.721 LANDING GEAR
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CS-25 BOOK 1 (1) The static ground
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CS-25 BOOK 1 extension or after ret
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CS-25 BOOK 1 inches) in height, is
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CS-25 BOOK 1 (i) If an integral sta
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CS-25 BOOK 1 (b) Signs that notify
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CS-25 BOOK 1 Passenger seating conf
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CS-25 BOOK 1 emergency exit which i
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CS-25 BOOK 1 (1) For aeroplanes tha
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CS-25 BOOK 1 affords a more effecti
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CS-25 BOOK 1 (f) Means to enable th
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CS-25 BOOK 1 (ii) No discharge of t
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CS-25 BOOK 1 For compartments of 14
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CS-25 BOOK 1 CS 25.865 Fire protect
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CS-25 BOOK 1 INTENTIONALLY LEFT BLA
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CS-25 BOOK 1 CS 25.904 Automatic Ta
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CS-25 BOOK 1 CS 25.945 Thrust or po
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CS-25 BOOK 1 structural loads that
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CS-25 BOOK 1 (d) Each fuel filling
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CS-25 BOOK 1 (b) Each drain require
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CS-25 BOOK 1 impaired when the oil
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CS-25 BOOK 1 (i) Under the icing co
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CS-25 BOOK 1 CS 25.1155 Reverse thr
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CS-25 BOOK 1 CS 25.1185 Flammable f
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CS-25 BOOK 1 so that discharge of t
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CS-25 BOOK 1 (8) An augmentation li
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CS-25 BOOK 1 (b) For functions whos
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CS-25 BOOK 1 (d) Each pressure alti
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CS-25 BOOK 1 quantity, in litres, (
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CS-25 BOOK 1 CS 25.1357 Circuit pro
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CS-25 BOOK 1 30º with a vertical l
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CS-25 BOOK 1 Angle above or below t
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CS-25 BOOK 1 (c) Radio and electron
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CS-25 BOOK 1 between which relative
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CS-25 BOOK 1 (2) A common source of
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CS-25 BOOK 1 interphone, public add
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CS-25 BOOK 1 CS 25.1519 Weight, cen
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CS-25 BOOK 1 (d) Each engine or pro
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CS-25 BOOK 1 (e) Kinds of operation
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CS-25 BOOK 1 CS 25A943 Negative acc
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CS-25 BOOK 1 CS 25A1045 Cooling tes
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CS-25 BOOK 1 APU FIRE PROTECTION CS
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CS-25 BOOK 1 (2) Have thermal stabi
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CS-25 BOOK 1 CS 25A1583 AEROPLANE F
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CS-25 BOOK 1 insulated to simulate,
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CS-25 BOOK 1 Appendix A (continued)
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CS-25 BOOK 1 Appendix A (continued)
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CS-25 BOOK 1 FIGURE 1 CONTINUOUS MA
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CS-25 BOOK 1 Appendix C (continued)
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CS-25 BOOK 1 Appendix C (continued)
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CS-25 BOOK 1 Appendix F (continued)
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CS-25 BOOK 1 (a) Summary of Method.
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CS-25 BOOK 1 (c) Diagrams of struct
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CS-25 BOOK 1 (i) Assure an adequate
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CS-25 BOOK 1 Appendix J (continued)
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CS-25 BOOK 2 2-0-2
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CS-25 BOOK 2 order to validate the
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CS-25 BOOK 2 * 2 sec. where a comma
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CS-25 BOOK 2 can be raised from the
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CS-25 BOOK 2 varying performance le
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CS-25 BOOK 2 FIGURE 2. ANTI-SKID SY
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CS-25 BOOK 2 2.1 If the applicant e
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CS-25 BOOK 2 F b ( Tb + αI) = R ty
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CS-25 BOOK 2 The stopping distance
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CS-25 BOOK 2 must not result in add
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CS-25 BOOK 2 AMC 25.119(a) Landing
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CS-25 BOOK 2 AMC 25.143(b)(1) Contr
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CS-25 BOOK 2 3.2 Beyond the buffet
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CS-25 BOOK 2 AMC 25.145(e) Longitud
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CS-25 BOOK 2 The minimum control sp
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CS-25 BOOK 2 sense, and that the fa
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CS-25 BOOK 2 AMC 25.201(b)(1) Stall
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CS-25 BOOK 2 provide a lesser margi
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CS-25 BOOK 2 detent. It is not an a
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CS-25 BOOK 2 exceeded. It is intend
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CS-25 BOOK 2 (1) Encounter with a H
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CS-25 BOOK 2 unique mass and flight
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CS-25 BOOK 2 2.3.4 The limit gust l
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CS-25 BOOK 2 AMC 25.345(a) High Lif
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CS-25 BOOK 2 caused by an increment
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CS-25 BOOK 2 assumed faired relativ
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Dist. Elev. Dist. Elev. Dist. Elev.
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CS-25 BOOK 2 1.1.3 Experience with
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CS-25 BOOK 2 b. 85% of the limit fl
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CS-25 BOOK 2 ii. iii. Locations whe
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CS-25 BOOK 2 3.2.2 Scatter Factor f
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CS-25 BOOK 2 SCATTER FACTOR FLOW CH
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CS-25 BOOK 2 1.2 In addition, where
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CS-25 BOOK 2 2.12 Coupon. A small t
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CS-25 BOOK 2 6.2 Damage Tolerance (
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CS-25 BOOK 2 9.2.1 The nature and e
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CS-25 BOOK 2 AMC No. 2 to CS 25.603
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CS-25 BOOK 2 Identical material (ca
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CS-25 BOOK 2 2-D-12
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CS-25 BOOK 2 AMC 25.607 Fasteners F
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CS-25 BOOK 2 AMC 25.701(d) Flap and
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CS-25 BOOK 2 maintenance at specifi
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CS-25 BOOK 2 (CCR) where appropriat
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CS-25 BOOK 2 d. The value of d used
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CS-25 BOOK 2 CS 25.1315 Negative ac
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CS-25 BOOK 2 (a) Minor Changes. Cha
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CS-25 BOOK 2 the full range of tyre
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CS-25 BOOK 2 stop case and from a 5
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CS-25 BOOK 2 show that no unsafe co
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CS-25 BOOK 2 characteristics of the
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CS-25 BOOK 2 (1) Polycarbonate exhi
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CS-25 BOOK 2 working stress level o
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CS-25 BOOK 2 AMC 25.787(b) Stowage
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CS-25 BOOK 2 EXAMPLE MARKING FOR IN
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CS-25 BOOK 2 AMC 25.851(a)(1) Fire
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CS-25 BOOK 2 5 The installation of
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CS-25 BOOK 2 5.2.2 Isolated conduct
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CS-25 BOOK 2 AMC 25.905(d) Release
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CS-25 BOOK 2 AMC 25.955(a)(4) Fuel
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CS-25 BOOK 2 AMC 25.1041 Tests in h
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CS-25 BOOK 2 2.4.3 Either by separa
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CS-25 BOOK 2 AMC 25.1141(f) Powerpl
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CS-25 BOOK 2 these cases, the provi
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CS-25 BOOK 2 condition to occur, wh
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CS-25 BOOK 2 1.10 A bank angle inde
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CS-25 BOOK 2 reliability demonstrat
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CS-25 BOOK 2 Conditions, resulting
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CS-25 BOOK 2 (2) Remote Failure Con
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CS-25 BOOK 2 Figure 2: Relationship
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CS-25 BOOK 2 Failure Condition is e
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CS-25 BOOK 2 (iii) an advisory, if
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CS-25 BOOK 2 Some of these factors
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CS-25 BOOK 2 (2) Minor Failure Cond
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CS-25 BOOK 2 per flight hour of Fai
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CS-25 BOOK 2 APPENDIX 1. ASSESSMENT
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CS-25 BOOK 2 d. Conduct the analysi
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CS-25 BOOK 2 Figure A2-2: Depth of
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CS-25 BOOK 2 F n ∑ T = T and t -
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CS-25 BOOK 2 Flight Conditions Cond
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CS-25 BOOK 2 CS 25.1303(b)(5) CS 25
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CS-25 BOOK 2 Where the caption or m
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CS-25 BOOK 2 AMC 25.1323(h) Airspee
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CS-25 BOOK 2 1.9 Operating procedur
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CS-25 BOOK 2 basis of a ground and
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CS-25 BOOK 2 5.3.2 Climb, Cruise, D
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CS-25 BOOK 2 FIGURE 1 - DEVIATION P
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CS-25 BOOK 2 2 When ensuring the ad
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CS-25 BOOK 2 e. Difference frequenc
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CS-25 BOOK 2 NOTES: Due account sho
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CS-25 BOOK 2 2.5.4 Ice Accretion on
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CS-25 BOOK 2 AMC 25.1435 Hydraulic
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CS-25 BOOK 2 and turbulence conditi
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CS-25 BOOK 2 AMC 25.1436(b)(3) Pneu
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CS-25 BOOK 2 AMC 25.1447(c)(1) Equi
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CS-25 BOOK 2 AMC 25.1459(b) Flight
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CS-25 BOOK 2 AMC 25.1533(a)(3) Take
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CS-25 BOOK 2 (3) Note. An operating
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CS-25 BOOK 2 e. Aeroplane Flight Ma
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CS-25 BOOK 2 (G) Maximum demonstrat
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CS-25 BOOK 2 (v) (vi) (vii) Operati
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CS-25 BOOK 2 data should cover a pr
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CS-25 BOOK 2 (17) Landing Approach
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CS-25 BOOK 2 (2) Only a single weig
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CS-25 BOOK 2 c. Computerised AFM In
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CS-25 BOOK 2 (4) Although the outpu
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CS-25 BOOK 2 (i) re-assess the soft
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CS-25 BOOK 2 r. References to other
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CS-25 BOOK 2 AMC 25A939(a) Turbine
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CS-25 BOOK 2 3 Method 2 (Interpreta
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CS-25 BOOK 2 Appendix F, Part IV (f
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CS-25 BOOK 2 EASA ED EFIS EHSI EURO
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CS-25 BOOK 2 ED58 Minimum Operation
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CS-25 BOOK 2 (iv) Vertical Speed. D
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CS-25 BOOK 2 (F) Compatibility with
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CS-25 BOOK 2 Selected data, values
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CS-25 BOOK 2 to determine what info
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CS-25 BOOK 2 mode reversions) shoul
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CS-25 BOOK 2 considered the primary
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CS-25 BOOK 2 (iv) Digital present v
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CS-25 BOOK 2 a. Power Bus Transient
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CS-25 BOOK 2 9 MAP MODE CONSIDERATI
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CS-25 BOOK 2 hazardously misleading
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CS-25 BOOK 2 simple methods, such a
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CS-25 BOOK 2 AMC 25-19 Certificatio
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CS-25 BOOK 2 may include, for examp
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CS-25 BOOK 2 9 IDENTIFICATION OF CA
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CS-25 BOOK 2 (1) The term ‘except
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CS-25 BOOK 2 The underlying goal of
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