AC 120-45A

TABLE OF FUNCTIONS AND SUBJECTIVE TESTS(Cont'd) LEVEL 2/5/92 1 2 3 4567 Comments situation or condition can be accomplished satisfactorily.

(xiii) Specific flight characteristics.

(xiv) Manual flight control X If appropriate for the reversion. airplane.

(xv) Flight control system failure modes.

(xvi) Other.

(3) Descent.

(i) Normal.

(ii) Maximum rate.

(iii) Manual flight control reversion.

(iv) Flight control system failure modes.

(v) Other.

e. APPROACHES

(1) Nonprecision. Appendix 3 AC 120-45A

(i) All engines operating.

Appendix 3 Comments Level 7 - Applicable only to those highly augmented airplanes in which flight test data verify the absence of motion without pilot input during this maneuver. In the absence of this data for Level 7 and for Levels 6 and 3, this test is accomplished only to verify that the procedures for this situation or condition can be accomplished satisfactorily. Applicable only to those highly augmented air- planes in which flight test data verify the absence of motion without pilot input during this maneuver.

× x x x LEVEL x x TABLE OF FUNCTIONS AND SUBJECTIVE TESTS(Cont'd) (ii) One or more engines (iii) Approach procedures. --NDB --VOR, RNAV TACAN --DME ARC --LOC/BC --LDA, LOC, SDF -- ASR (iv) Missed approach. --All engines operating. --One or more engines inoperative (as applicable).

inoperative.

Par 2

2/5/92 AC 120-45A Appendix 3 Comments As applicable. As applicable. *Auto- coupled approach procedures. Tests accomplished with maximum tailwind and crosswind authorized if less than 10 knots. As applicable.

LEVEL 11 4 X* TABLE OF FUNCTIONS AND SUBJECTIVE TESTS(Cont'd) (i) PAR - Normal. (A) Normal. (B) Category I published: Manually controlled with and without flight director to 100 feet below published decision (C) Category II published: With use of autocoupler, autothrottle, and (D) Category III published: (1) With electrical power, source failure. (2) With 10 knot tailwind. (3) With 10 knot crosswind. (A) Normal. (B) Steep glide slope.

(2) Precision. (ii) ILS. autoland, as applicable. (iii) MIS.

height.

Par 2

TABLE OF FUNCTIONS AND SUBJECTIVE TESTS(Cont'd) LEVEL 1 2 3 4 5/67 Comments

(iv) Effects of crosswind. As applicable. Appendix 3 AC 120-45A

(v) With engine(s) inoperative. Level 7 - Applicable only to those highly augmented airplanes in which flight test data verify the absence of motion without pilot input during this maneuver. In the absence of this data for Level 7 and for Level 6 and below, this test is accomplished only to verify that the procedures for this situation or condition can be accomplished satisfactorily.

(vi) Missed approach.

- (A) Normal. As applicable, (B) With engine(s) Level 7 - Applicable only inoperative. to those highly augmented airplanes in which flight test data verify the absence of motion without pilot input during this maneuver. In the absence of this data for Level 7 and for Level 6 and below, this test is accomplished only to 2/5/92 verify that the procedures for this situation or condition can be accomplished satisfactorily.

TABLE OF FUNCTIONS AND SUBJECTIVE TESTS(Cont'd) LEVEL 2/5/92 1 2 6 Comments (C) From steep glide slope. As applicable.

f. SURFACE OPERATIONS (POST LANDING)

(1) Landing roll.

(i) Spoiler operation. X*_ X* X* *If applicable to installed systems.

(ii) Reverse thrust operation.

(iii) Other.

8. ANY FLIGHT PHASE

(1) Aircraft and powerplant systems If applicable to operation. installed systems.

(i) Air conditioning.

(ii) Antiicing/deicing.

(iii) Auxiliary powerplant.

(iv) Communications.

(v) Electrical.

(vi) Fire detection and suppression.

= Appendix 3 AC 120-45A

TABLE OF FUNCTIONS AND SUBJECTIVE TESTS(Cont'd) LEVEL 2 3 4 5 Comments Appendix 3 AC 120-45A

(vii) Flaps.

(viii) Flight controls (including spoiler/speedbrake).

(ix) Fuel and oil.

(x) Hydraulic.

(xi) Landing gear.

(xii) Oxygen.

(xiii) Pneumatic.

(xiv) Powerplant.

(xv) Pressurization.

(2) Flight management and guidance If applicable to systems. installed systems.

(i) Automatic landing aids.

(ii) Automatic pilot.

(iii) Thrust management/autothrottle.

(iv) Flight data displays.

(v) Flight management computers. 2/5/92

TABLE OF FUNCTIONS AND SUBJECTIVE TESTS(Cont'd) LeVEL 2/5/92 7 Comments ~ (vi) Flight director/system displays.

(A) Head down.

(B) Head up.

(vii) Navigation systems.

(viii) Stall warning/avoidance.

(ix) Stability and control augmentation.

(x) Other.

(3) Airborne procedures If applicable to installed systems.

(i) Holding.

(ii) Other.

(4) Engine shutdown and parking. ¡ X If applicable to installed systems.

(i) Systems operation.

(ii) Parking brake operation.

(5) Other 13 (and 14) Appendix 3 AC 120-45A

Appendix 4 APPENDIX 4. EXAMPLES PAGE NO.

FIGURE 1. APPLICATION LETTER FIGURE 2. ATG COVER PAGE 2 FIGURE 3. INFORMATION PAGE 3 i (and ii)

Appendix 4 APPENDIX 4. EXAMPLES (Cont'd) Name, POI, Airlines

FAA FSDO Address City, state, Zip Dear Mr.

(Operator Name) requests evaluation of our (Type) airplane flight training device for qualification at Level The (Operator Name) flight training device is fully defined on page _ of the accompanying approval test guide (ATG). We have completed tests of the flight training device and certify that it meets all applicable requirements and the guidance of Advisory Circular (AC) 120-45A. Appropriate hardware and software configuration control procedures have been established.

Pilots we have designated as our representatives have assessed the flight training device and we concur with their finding that it conforms to the (Operator Name) _(Type) _ airplane cockpit configuration and that the simulated systems and subsystems function equivalently to those in the airplane. These pilots have also assessed the performance and flying qualities of the flight training device and we concur with their finding that it represents the respective airplane.

(Added comments as desired.)

Sincerely, FIGURE 1. Application Letter

Appendix 4 APPENDIX 4. EXAMPLES (Cont'd) (OPERATOR NAME) (OPERATOR ADDRESS)

FAA APPROVAL TEST GUIDE (AIRPLANE MODEL) (Level of Flight Training Device) (Training Device Identification Including Manufacturer, Serial Number) (Location) FAA Initial Evaluation Date:

(Operator Approval) Date:

Date:

FAA, Manager, National Simulator Program 2 FIGURE 2. Example ATG Cover Page

Appendix 4 APPENDIX 4. EXAMPLES (Cont'd)

OPERATOR OPERATOR DEVICE CODE: MTD-441 #1 AIRPLANE MODEL: MTD-441-B AERODYNAMIC DATA REVISION: MTD-441-B CPX-8D July 1988 ENGINE MODEL AND REVISION: CPX-8D-RPT-1 June 1988 FLIGHT CONTROLS DATA REVISION: MTD-441-B May 1988 ELIGHT MANAGEMENT SYSTEM: Berry XP TRAINING DEVICE MODEL AND MANUFACTURER: MFD-7X Tinker DATE OF MANUFACTURE: 1988 COMPUTER: CIA FIGURE 3. Information Page 3 (and 4)