V ,,( J".,, / / ,I ~ ,J =1 ,, ~ I/ , !,( i--
J I,)'-"" ~--y
~ I/ '--'~ - • A --I/ ' i-- ---- / " / ' I f------ I f-~~ / f- - / I?' ,,~ / ,I ,I / .,1\.
.,I I\.
-,/ " I.)" \ / V 11/16/2011 AC 23-8C Appendix 3 Table A3-2 - Tabulated Thrust Horsepower Available and Calculated VMC VC (KCAS) SHAFT HORSEPOWER P THRUST
HORSEPOWER
AVAILABLE AT
SEA LEVEL
CALCULATED VMC C2 = 1394.482 90 1050 .610 640.5 96.3 95 1050 .640 672.0 97.9 100 1050 .665 698.3 99.1 105 1050 .688 722.4 100.2 Figure A3-1 - Thrust Horsepower at Sea Level 85 90 95 100 105 VCAS KNOTS
SEA LEVEL STD. DAY VMC
CALCULATED
VMC VALUES
THRUST HORSEPOWER
AVAILABLE AT SEA LEVEL 620 640 660 680 700 720 740
THRUST HORSEPOWER AT SEA LEVEL A3-3
Primary FAR Support FAR Description Manual Mark Placard Sign 11/16/2011
23.25(a)(2) 23.1557(b) Ib (utility and aerobatic)
23.31(a) 23.31(b) 23.1557(a) Appendix 4 FAR-23 Manuals, Markings, & Placards Checklist
23.373(a)
23.415(€) Maximum weight for tie-down
23.671(b) Identification of controls
23.672(c)(2)
23.677(a)
23.685(d)
23.733(b)
23.777(a)
23.777(h)(1)
23.777(h)(2) in red Indication of tank or function selected for electronic fuel selector. Closed position indicated
23.777(g)(3) Red marking of OFF position of fuel valve selector
23.783(c)(3)-(4) Marking of means of opening external doors
23.785(h) wearing a parachute
23.787(a)(1) Placard for maximum weight capacity of baggage or cargo compartment
23.791 observe other seats
23.807(b)(3) Marking of emergency exit location and operation
23.811(a) External marking of means of opening doors and exits **** * ** *
23.811(b) Internal sign for exits and doors for commuter category airplanes × ×
23.841(b)(7) Warning placard if maximum differential cabin pressure and landing loads exceed limit
23.853(c), (c)(2) Placard or illuminated sign prohibiting smoking if/when applicable
23.853(d)(1) "No cigarette disposal" placard on/near cach disposal receptacle door for commuter category
23.853(d)(2) "No smoking" placards required for lavatories for commuter category
23.903(d) 23.1581(a)(2) Marking or placard for piston engine start techniques and limitations
23.903(e)(1) 23.1581(a)(2) Marking or placard for turbine engine start techniques and limitations
23.903(€)(3) 23.1581(a)(4) Marking or placard for turbine engine in-flight restart techniques and limitations Appendix 4 AC 23-8C
Marking such that pusher propeller disk is conspicuous 11/16/2011
12.1581(a)(2) Turbocharger operating procedures and limitations
23.1555(c)(3) Placard for operating instructions for use of auxiliary fuel tank
23.1557(c) Marking of fuel tank filler Placard for fuel jettisoning means if prohibited in some aerodynamic configurations
23.1557(c) Marking oil filler tank connections
23.1041 Compliance with § 23.1041 must be shown for all flight phases with the procedures established in AFM (turbines)
23.1041 Compliance with §23.1041 must be shown for the climb/descent with the procedures established in AFM (pistons) Marking coolant tank filler connections
23.1555(a) Marking of powerplant controls Labeling of equipment as to its identification, function and/or operating limitations Instrument markings on electronic displays
23.1541(a)(2) Provision of alternate static correction card, if required
23.1547(e) Placard for magnetic indicator deviations of more than 10° Marking of direction of motion of autopilot controls Marking of appropriate units on fuel quantity indicator XXXX Marking of essential circuit breakers and fuses Marking of switches as to operation and circuit controlled
23.1585(a) Recommended procedures for use of ice protection equipment Placard for oxygen flow, duration and warning of hot generator element X
23.1541- Operating limitations and other information necessary for safe operation should be
23.1589 established and furnished to the crew
23.1545-23.1567 Markings and placards specified by §§23.1545-23.1567 Additional information, markings and placards required for safe operation Specifies characteristics of markings and placards Select one category for basis for markings and placards for multi-category airplanes Placards and marking information for all certified categories must be furnished in the AFM Alignment and visibility of instrument markings Marking of speeds on ASI
23.1545(b) Marking of VNE, caution range, flap operating range, OEI en-route climb/descent speed for Appendix 4 AC 23-8C pistons less than 6000 Ib, VMC for pistons less than 6000 Ib.
23.1545(c) Indication of variation of VNE or VNO with altitude
23.1545(đ) Indication of variation of VMO/MMO with altitude or lowest value
23.903(e)(1) 23.903(e)(3) 23.1581(a)(2) 23.1581(a)(4) Marking or placard for turbine engine in-flight restart techniques and limitations Marking or placard for turbine engine start techniques and limitations XX X 1102/91/11
23.905(f) Marking such that pusher propeller disk is conspicuous
23.909(€) 12.1581(a)(2) Turbocharger operating procedures and limitations
23.955(d) (2) 23.1555(c)(3) Placard for operating instructions for use of auxiliary fuel tank
23.973(a) 23.1557(c) Marking of fuel tank filler
23.1001(g) Placard for fuel jettisoning means if prohibited in some aerodynamic configurations
23.1013(c) 23.1557(c) Marking oil filler tank connections
23.1045(a) 23.1041 Compliance with § 23.1041 must be shown for all flight phases with the procedures established in AFM (turbines)
23.1047 23.1041 Compliance with §23.1041 must be shown for the climb/descent with the procedures established in AFM (pistons)
23.1061(c) Marking coolant tank filler connections
23.1141(a) 23.1555(a) Marking of powerplant controls
23.1301(b) Labeling of equipment as to its identification, function and/or operating limitations
23.1311(a)(7) Instrument markings on electronic displays
23.1325(b)(3) 23.1541(a)(2) Provision of alternate static correction card, if required
23.1327(b) 23.1547(€) Placard for magnetic indicator deviations of more than 10°
23.1329(d) Marking of direction of motion of autopilot controls
23.1337(b) Marking of appropriate units on fuel quantity indicator
23.1357(d) Marking of essential circuit breakers and fuses
23.1367(d) Marking of switches as to operation and circuit controlled
23.1419(a) 23.1585(a) Recommended procedures for use of ice protection equipment
23.1450(c) Placard for oxygen flow, duration and warning of hot generator element
23.1501 23.1541- Operating limitations and other information necessary for safe operation should be
23.1589 established and furnished to the crew
23.1541(a)(1) 23.1541(a)(2) 23.1545-23.1567 Markings and placards specified by §§23.1545-23.1567 Additional information, markings and placards required for safe operation XXXXX
23.1541(b) Specifies characteristics of markings and placards
23.1541(c)(1) Select one category for basis for markings and placards for multi-category airplanes
23.1541(c)(2) Placards and marking information for all certified categories must be furnished in the AFM
23.1543 Alignment and visibility of instrument markings
23.1545(a) Marking of speeds on ASI
23.1545(b) Marking of VNE, caution range, flap operating range, OEI en-route climb/descent speed for pistons less than 6000 lb, VMC for pistons less than 6000 1b.
23.1545(c) Indication of variation of VNE or VNO with altitude
23.1545(đ) Indication of variation of VMO/MMO with altitude or lowest value 11/16/2011
23.1547(a) Marking of conditions for, and calibration of, magnetic direction indicator
23.1549(a) Marking of powerplant instruments-red radial line for maximum and minimum operating limits
23.1549(b) Marking of powerplant instruments - green arc for normal range
23.1549(c) Marking of powerplant instruments-yellow arc for caution and take-off range
23.1549(c) Marking of powerplant instruments-red arc for restricted vibration range
23.1551 Marking of oil quantity indicator
23.1553 23.1337(b)(1) Red radial marking at specified zero reading
23.1555(a) Marking of cockpit control as to function and method of operation
23.1555(b) Marking of secondary controls
23.1555(c)(1) Marking of powerplant fuel controls-fuel selector position
23.1555(c)(2) Marking of powerplant fuel controls-fuel tank sequence Placard stating conditions under which maximum usable fuel may be used from restricted
23.1555(c)(3) 23.955(d)(2) usage tank
23.1555(c)(4) Marking of powerplant fuel controls-multi-engine fuel selector position XXXXX
23.1555(d)(1) Marking of usable fuel at indicator, if applicable
23.1555(d)(2) Marking of usable fuel at selector, if applicable
23.1555(e)(1) Marking of landing gear position indicator
23.1555(e)(2) Marking of emergency controls red and of method of operation
23.1557(a) Placard for baggage, cargo and ballast for weight and content
23.1557(b) 23.25(c)(2) Placard for seats not capable of carrying more than 170 lb.
23.1557(c)(1)(i) 23.973(a) Marking of fuel filler openings (piston) XXXX
23.1557(c)(1)(ii) 23.973(a) Marking of fuel filler openings (turbine) and AFM requirement
23.1557(c)(2) Marking of oil filler openings and AFM requirement
23.1557(c)(3) Marking of coolant filler openings
23.1557(d) Placard for emergency exits and controls
23.1557(e) Marking of system voltage of each DC installation
23.1559(a)(1) Placard stating that airplane must be operated in accordance with AFM
23.1559(a)(2) Placard stating the certified category to which placards apply
23.1559(b) For multi-category airplanes, a placard stating that other limitations are contained in the AFM Appendix 4
23.1559(c) 23.1525 Placard specifying the kinds of operation
23.1561(a) Marking of safety equipment as to method of operation
23.1561(b) 11/16/2011
23.1563(a) Placard of VA close to ASI
23.1563(b)
23.1563(c) 23.1525 Ib and turbines
23.1567(a) r normal category airplanes
23.1567(b)(1) gory airplanes es that do not meet the
23.1567(b)(2) aerobatic spin requirements ded entry airspeed; also stating
23.1567(c)
23.1567(đ) om a spin ntain information required by
23.1581(a) 23.1583- 23.1589 ration and information
23.1583- and segregated from
23.1581(b)(1) 23.1589 unapproved information
23.1581(b)(s)(i) 23.1583 shed from other parts of the
23.1581(b)(2)(ii) 23.1589 23.1585- resented in a manner to 6000 1b) acceptable
23.1581 (c) ppropriate instruments and placards
23.1581(d) fied, presented as indicated airspeeds fixed container readily
23.1581 (€) accessible to the pilot tion of revisions and/or
23.1583 23.1581 (f) amendments following: Appêndix 4
23.1583(a)(1) 23.1545 equired in $23.1545
23.1583(a)(2)
VMO/MMO and a statement that this speed must not be deliberately exceeded without 11/16/2011
23.1583(a)(3)(1) authorization (for turbine powered commuters) If an airspeed limitation is based on compressibility effects, a statement to this effect,
23.1583(a)(3)(i) further information and the recommended recovery procedure (for further powered commuters) The airspeed limits must be shown in terms of VMO/MMO for (turbine powered
23.1583(a)(3)(i1) commuters)
23.1583(b)(1),(2) 23.1521 Powerplant limitations required by § 23.1521 and explanations, when appropriate X
23.1549- Information necessary for marking powerplant instruments required in §23.1549 to
23.1583(b)(3)
23.1553 §23.1553
23.1583(c)(1) Maximum weight
23.1583(c)(2) Maximum landing weight (if less than maximum weight)
23.1583(c)(3) 23.63(c)(1) MTOW for each airdrome altitude and temperature selected by the applicant at which the airplane complies with §23.63(c)(1) (not for pistons less than 6000 Ib and commuters) For commuter airplanes, the MTOW for each airdrome altitude and temperature selected by
23.63(d)(1), the applicant at which the airplane complies with the climb requirements of §23.63(d)(1),
23.1583(c)(4) 23.55,23.59(a) the accelerate-stop distance determined in §23.55 is acceptable, the take-off distance
23.59(b) determined in §23.59(a) is acceptable and, optionally, the take-off run determined in §23.59(b) is acceptable For commuter airplanes, the maximum landing weight for each airdrome altitude selected
23.1583(c)(5) 23.63(d)(2), by the applicant at which the airplane complies with the climb requirements of
23.75,23.343 §23.63(d)(2), the landing distance determined in §23.75 is acceptable and the maximum zero wing fuel weight established in §23.343
23.1583(d) The established center of gravity limits
23.1583(€) 23.221(c) Authorized maneuvers, appropriate airspeed limitations, recommended entry speeds, spin recovery procedures and unauthorized maneuvers according to category
23.1583(f) Positive limit load factors and, for aerobatic airplanes, the negative limit load factors
23.1583(g) 23.1523 Number and functions of the minimum flight crew
23.1583(h) 23.1525 Lists of kinds of operation according to §23.1525, installed equipment affecting any operating limitation and identification as to equipment's required operational status
23.1583(I) 23.1527 Maximum operating altitude
23.1583(j) Maximum passenger seating configuration
23.1583(k) 23.1583(1) Maximum allowable lateral fuel loading differential, if less than the maximum possible Maximum allowable load and maximum intensity of loading for baggage and cargo Appêndix 4 compartments or zones
23.1583(m) Any limitations on the use of airplane systems and equipment
23.1583(n) Where appropriate, maximum and minimum ambient temperatures for operation
23.1583(o) Any restrictions on smoking in the airplane 11/16/2011
23.1583(p) 23.1587(a)(5) 23.45(g); Types of surface on which operation may be conducted (see §34.45(g) and §23.1587(a)(5) Information concerning normal, abnormal and emergency procedures and other information
23.1585(a) necessary for safe operation and achievement of scheduled performance, including
23.1585(a)(1) Explanation of significant or unusual flight or ground handling characteristics X
23.1585(a)(2) procedures Maximum demonstrated values of crosswind for take-off and landing and associated
23.1585(a)(3) A recommended speed for flight in rough air
23.1585(a)(4) 23.903(f) Procedures for restarting any engine in flight, including the effects of altitude
23.1585(a)(5) 23.73, 23.75 accordance with §23.73 and §23.75 and transition to the balked landing condition Procedures, speeds and configurations for making a normal approach and landing in
23.1585(b) 23.71 For all single-engine airplanes, procedures, speeds and configurations for a glide following engine failure and the subsequent forced landing
23.1585(c)(1) For all twin-engine airplanes, procedures, speeds and configurations for making an approach and landing with one engine inoperative For all twin-engine airplanes, procedures, speeds and configurations for making a go-
23.1585(c)(2) around with one engine inoperative, the conditions under which it can be performed safely or a warning against attempting a go-around
23.51(a),(b) For all normal, utility and aerobatic airplanes, procedures, speeds and configurations for
23.1585(d)(1) 23.53(a), (b) making a normal take-off (§§23.51(a), (b) 23.53(a), (b)) and subsequent climb (§§23.65,
23.65,23.69(a) 23.69(a))
23.1585(d)(2) For all normal, utility and aerobatic airplanes, procedures for abandoning a take-off For all normal, utility and aerobatic twin-engine airplanes, procedures and speeds for
23.1585(€)(1) continuing a take-off following engine failure, the conditions under which it can be performed safely or a warning against continuing the take-off
23.1585(€)(2) 23.67,23.69(a) For all normal, utility and aerobatic twin-engine airplanes, procedures and speeds for continuing a climb following engine failure after take-off (§23.67) or en-route (§23.69(b))
23.1585(f)(1) For commuter category airplanes, procedures, speeds and configurations for making a normal take-off
23.1585(f)(2) 23.55 For commuter category airplanes, procedures and speeds for carrying out an accelerate-stop
23.57, For commuter category airplanes, procedures and speeds for continuing a take-off following Appêndix 4
23.1585(F)(3) 23.59(a)(1), engine failure (§23.59(a)(1) and for following the flight path (§$23.57, 23.61(a))
23.61(a)
23.1585(g) 23.953 For twin-engine airplanes, information and instructions regarding fuel supply independence
23.1353(g)(2), For cach airplane showing compliance with §23.1353(g)(2) or (g)(3), the procedures for 11/16/2011
23.1585(h)
23.1353(g)(3) disconnecting the battery from its charging source
23.1585(i) Information on the total quantity of usable fuel for each tank and the effect pump failure
23.1585(j) Procedures for the safe operation of the airplane's systems and equipment, in normal use and in the event of malfunction
23.1587 23.45(b) Unless other wise presented, performance information must be provided over the altitude and temperature ranges required by §23.45(b)
23.1587(a)(1) and the effect on these stalling speeds of bank angles up to 60° Stalling speeds Vso and Vsi at maximum weight with landing gear and wing flaps retracted
23.1587(a)(2) Steady rate and gradient of climb with all engines operating The landing distance for each airdrome altitude and standard temperature and the type of
23.1587(a)(3) surface for which it is valid The effect on landing distance of operation on other than smooth hard surfaces, when dry X The effect on landing distance of runway slope, 50% of the headwind component and 150% X of the tailwind component
23.1587(b) 23.77(a) climb/descent For normal, utility and aerobatic piston airplanes of 6000 Ib or less, the steady angle of
23.1587(c)(1) 23.53 which it is valid For normal, utility and aerobatic airplanes, the take-off distance and the type of surface for
23.1587(c)(2) 23.45(g) The effect on take-off distance of operation on other than smooth hard surfaces, when dry
23.1587(c)(3) of the tailwind component The effect on take-off distance of runway slope, 50% of the headwind component and 150%
23.1587(c)(4) 23.66 For twin piston airplanes of more than 6000 Ib MTOW and turbine airplanes, the oneengine inoperative take-off climb/descent gradient
23.1587(c)(5) 23.69(b) For twin-engine airplanes, the en-route rate and gradient of climb/descent with one-engine inoperative
23.1587(c)(6) 23.71 For single-engine airplanes, the glide performance
23.1587(d)(1) 23.55 For commuter airplanes, the accelerate-stop distance
23.1587(d)(2) 23.1587(d)(3) 23.59(a) 23.59(b) For commuter airplanes, the take-off distance For commuter airplanes, the take-off run at the applicant's option Appendix 4 AC 23-8C
23.1587(d)(4) 23.45(g) For commuter airplanes, the effect on accelerate-stop distance, take-off distance and, if determined, take-off run of operation on other than smooth hard surfaces, when dry
For commuter airplanes, the effect on accelerate-stop distance, take-off distance and, if 11/16/2011
23.1587(d)(5) determined, take-off run of runway slope, 50% of the headwind component and 150% of the tailwind component
23.1587(d)(6) 23.61(b) For commuter airplanes, the net take-off path X
23.1587(dy(7) 23.69(b) For commuter airplanes, the en-route gradient of climb/descent with one engine inoperative For commuter airplanes, the effect on the net take-off path and the en-route gradient of
23.1587(d)(8) climb/descent with one engine inoperative, of 50% of the headwind component and 150% of the tailwind component
23.1587(d)(9) 23.63(d)(2), 75 For commuter airplanes, overweight landing performance information (the maximum X weight at which the airplane complies with $23.63(d)(2) and the landing distance in §23.75)
23.1587(d)(10) 23.1323(b).(c) For commuter airplanes, the relationship between IAS and CAS
23.1587(d)(11) 23.1325(€) For commuter airplanes, the altimeter system calibration X
23.1587(d)(7) 23.69(b) For commuter airplanes, the en-route gradient of climb/descent with one engine inoperative
23.1589(a) 23.25 The weight and location of each item of equipment that can be easily removed and was installed when the airplane was weighed
23.1589(b) 23.23, 23.25 Appropriate loading instructions for each permissible loading condition of weight and og App. G23-2,3,4 23.1529 Instructions for continued airworthiness 00 Appendix 4
Appendix 5 Appendix 5 –Guide for Preparing Airplane Flight Manual and Pilots’s Operating Handbook Supplements
1. Introduction. An applicant is responsible for prep aring an Airplane Flight Manual (AFM) supplement when the airplane has been modified in such a manner that limitation, procedures, performance, or loading information have changed. The supplement should be prepared to reflect this supplemental information. If there is no change in one of the sections, it should so state.
a. Pilot's Operating Handbook Supplements. Refer to GAMA Specification No. 1, Revision No. 1.
b. AFM Supplements. Refer to paragraph 2 below and sample AFM.
2. General.
a. Enter name and address of applicant and document number (if used).
b. Enter make and model of the airplane. Multiple models may be used.
c. Enter registration number. Note: If more than one airplane is to be approved under this supplemental type certificate, leave this space blank on the master copy of the supplement so it can be filled in for each airplane as the modification is accomplished.
d. Enter airplane serial number. This number is on the airplane data plate. Note: If more than one airplane is to be approved under this supplemental type certificate, leave this space blank on the master copy of the supplement so it can be filled in for each airplane as the modification is accomplished. If only one airplane is to be approved, add "only" after the serial number.
e. Enter original AFM date or reissue date (if applicable).
f. Enter the type of modification or equipment installed.
g. Enter approval basis such as: Form 337, specification item number, Supplemental type Certificate Number, and so forth.
h. Enter any changed or additional limitations as a result of the modification. Follow the format of the basic AFM. If no change, state "NO CHANGE".
i. Enter any change in or additional procedures as a result of the modification. Follow the format of the basic AFM. This section may be divided into Normal and Emergency Procedures, if necessary. If no change, state "NO CHANGE".
j. Enter any change in performance as a result of the modification. If no change, state "NO CHANGE". In some cases, it is possible to show a statement similar to the following. "The performance of this airplane equipped with the Continental E-225-8 engine and Beech Model 215 propeller is equal to or better than the performance as listed in the original FAA-approved AFM."
k. Enter any change in the loading instructions, if necessitated by the change.
A5-1
___________________________________________________________________________________ Appendix 5
l. Copy this item, as shown on the sample AFM Supplement, leaving a blank space for typing of the ACO Manager's name below the signature line. This item needs to be coordinated with the ACO prior to submitting because in some ACO's the manager does not sign the AFM.
m. Type as shown on sample AFM Supplement, leaving a blank space so date of approval can be added.
n. If the supplement requires more than one page, a cover page should be prepared in accordance with page 3 of this appendix, except that items (h), (u), (j), and (k) should be on page 2 or subsequent. Each page should have: (1) the name and address of applicant and document number; (2) AFM supplement for Make and Model; (3) "FAA-approved" and "date" of approval; and (4) page number as (Page 1 of 3).
o. For those airplanes without flight manuals, and placards are not appropriate, the document should be labeled a Supplemental Airplane Flight Manual and arranged and worded as necessary with reference to the appropriate markings and placards. Identification of the material as Limitations, Procedures, or Performance should be clearly presented.
p. If applicant revises the AFM supplements, pertaining to one airplane model, a log of revisions may be added, as follows: (This revision log also needs a signature block.)
LOG OF REVISIONS Revision No. Pages Affected Description FAA-Approved Date Note: The revision page should immediately follow the cover page.
q. Vertical bars should be placed in the margin of the revised pages to indicate changed material.
A5-2