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Airman Knowledge Testing Supplement for Airline Transport Pilot and Aircraft Dispatcher

Front Matter
Appendix 1
Legends 1–20
Legends 21–40
Legends 41–60
Legends 61–72
Appendix 2
Figures 1–20
Figures 21–40
Figures 41–65
Figures 66–118
Figures 118A–146
Figures 147–170A
Figures 170B–198
Figures 198A–228
Figures 229–248
Figures 249–264
Figures 265–285
Figures 286–305
Figures 306–326
Figures 327–347
Figures 348–366
Figures 367–386
Figures 387–406
Figures 407–426
Figures 427–448
Figures 449–470
Figures 473–492
1. Figure 473 Q400—Maximum Permissible Takeoff Weight (WAT Limit)—Takeoff Flap 5°
2. Figure 474 Q400—First Segment Takeoff Gross Climb Gradient One Engine Inoperative—Flap 5°
3. Figure 475 Q400—Second Segment Takeoff Gross Climb Gradient One Engine Inoperative—Flap 5°
4. Figure 476 Q400—Takeoff Distance Required—Zero Wind, Zero Runway Slope—Flap 10°
5. Figure 477 Q400—Takeoff Run and Takeoff Distance Required Wind and Runway Slope Correction—Flap 5°
6. Figure 478 Q400—Accelerate—Stop Distance Required—Zero Wind, Zero Runway Slope Flap 5°
7. Figure 479 Q400—Accelerate-Stop Distance Required Wind and Runway Slope Correction— Flap 5°
8. Figure 480 Q400—Flap Retraction Initiation Speed—Flap 5° and Flap 10°
9. Figure 481 Q400—Net Takeoff Flight Path—Radius of Steady 15° Banked Turn
10. Figure 482 Q400—Enroute Climb Ceiling—One Engine Inoperative (Based on Zero Net Climb Gradient)
11. Figure 483 Q400—Approach, Go-Around, and VREF Speeds
12. Figure 484 Q400—Maximum Permissible Landing Weight (WAT LImit) Landing Flap 10°, Approach Flap 5°
13. Figure 485 Q400—Unfactored Landing Distance—Flap 10°
14. Figure 486 Q400—Expected Touch Down Speeds—Abnormal Flap Landing (Flap 0°)
15. Figure 487 Q400—Minimum Turn-Around Time
16. Figure 488 14 CFR part 117 Tables A, B, and C
17. Figure 489 S-92—Personnel and Baggage Centroids
18. Figure 490 S-92—Cockpit and Cabin Weight and Moment Table
19. Figure 491 S-92—Cockpit and Cabin Weight and Moment Table
20. Figure 492 S-92—Usable Fuel Weight and Moment Table
Figures 493–503

Airman Knowledge Testing Supplement for Airline Transport Pilot and Aircraft DispatcherFAA-CT-8080-7D

Appendix 2

Figures 473–492

20 FiguresPDF Pages 470–489

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Figure 473 Q400—Maximum Permissible Takeoff Weight (WAT Limit)—Takeoff Flap 5°

FAA-CT-8080-7D, Figure 473. Q400—Maximum Permissible Takeoff Weight (WAT Limit)—Takeoff Flap 5° (printed page image, PDF page 470)

Figure 474 Q400—First Segment Takeoff Gross Climb Gradient One Engine Inoperative—Flap 5°

FAA-CT-8080-7D, Figure 474. Q400—First Segment Takeoff Gross Climb Gradient One Engine Inoperative—Flap 5° (printed page image, PDF page 471)

Figure 475 Q400—Second Segment Takeoff Gross Climb Gradient One Engine Inoperative—Flap 5°

FAA-CT-8080-7D, Figure 475. Q400—Second Segment Takeoff Gross Climb Gradient One Engine Inoperative—Flap 5° (printed page image, PDF page 472)

Figure 476 Q400—Takeoff Distance Required—Zero Wind, Zero Runway Slope—Flap 10°

FAA-CT-8080-7D, Figure 476. Q400—Takeoff Distance Required—Zero Wind, Zero Runway Slope—Flap 10° (printed page image, PDF page 473)

Figure 477 Q400—Takeoff Run and Takeoff Distance Required Wind and Runway Slope Correction—Flap 5°

FAA-CT-8080-7D, Figure 477. Q400—Takeoff Run and Takeoff Distance Required Wind and Runway Slope Correction—Flap 5° (printed page image, PDF page 474)

Figure 478 Q400—Accelerate—Stop Distance Required—Zero Wind, Zero Runway Slope Flap 5°

FAA-CT-8080-7D, Figure 478. Q400—Accelerate—Stop Distance Required—Zero Wind, Zero Runway Slope Flap 5° (printed page image, PDF page 475)

Figure 479 Q400—Accelerate-Stop Distance Required Wind and Runway Slope Correction— Flap 5°

FAA-CT-8080-7D, Figure 479. Q400—Accelerate-Stop Distance Required Wind and Runway Slope Correction— Flap 5° (printed page image, PDF page 476)

Figure 480 Q400—Flap Retraction Initiation Speed—Flap 5° and Flap 10°

FAA-CT-8080-7D, Figure 480. Q400—Flap Retraction Initiation Speed—Flap 5° and Flap 10° (printed page image, PDF page 477)

Figure 481 Q400—Net Takeoff Flight Path—Radius of Steady 15° Banked Turn

FAA-CT-8080-7D, Figure 481. Q400—Net Takeoff Flight Path—Radius of Steady 15° Banked Turn (printed page image, PDF page 478)

Figure 482 Q400—Enroute Climb Ceiling—One Engine Inoperative (Based on Zero Net Climb Gradient)

FAA-CT-8080-7D, Figure 482. Q400—Enroute Climb Ceiling—One Engine Inoperative (Based on Zero Net Climb Gradient) (printed page image, PDF page 479)

Figure 483 Q400—Approach, Go-Around, and VREF Speeds

FAA-CT-8080-7D, Figure 483. Q400—Approach, Go-Around, and VREF Speeds (printed page image, PDF page 480)

Figure 484 Q400—Maximum Permissible Landing Weight (WAT LImit) Landing Flap 10°, Approach Flap 5°

FAA-CT-8080-7D, Figure 484. Q400—Maximum Permissible Landing Weight (WAT LImit) Landing Flap 10°, Approach Flap 5° (printed page image, PDF page 481)

Figure 485 Q400—Unfactored Landing Distance—Flap 10°

FAA-CT-8080-7D, Figure 485. Q400—Unfactored Landing Distance—Flap 10° (printed page image, PDF page 482)

Figure 486 Q400—Expected Touch Down Speeds—Abnormal Flap Landing (Flap 0°)

FAA-CT-8080-7D, Figure 486. Q400—Expected Touch Down Speeds—Abnormal Flap Landing (Flap 0°) (printed page image, PDF page 483)

Figure 487 Q400—Minimum Turn-Around Time

FAA-CT-8080-7D, Figure 487. Q400—Minimum Turn-Around Time (printed page image, PDF page 484)

Figure 488 14 CFR part 117 Tables A, B, and C

FAA-CT-8080-7D, Figure 488. 14 CFR part 117 Tables A, B, and C (printed page image, PDF page 485)

Figure 489 S-92—Personnel and Baggage Centroids

FAA-CT-8080-7D, Figure 489. S-92—Personnel and Baggage Centroids (printed page image, PDF page 486)

Figure 490 S-92—Cockpit and Cabin Weight and Moment Table

FAA-CT-8080-7D, Figure 490. S-92—Cockpit and Cabin Weight and Moment Table (printed page image, PDF page 487)

Figure 491 S-92—Cockpit and Cabin Weight and Moment Table

FAA-CT-8080-7D, Figure 491. S-92—Cockpit and Cabin Weight and Moment Table (printed page image, PDF page 488)

Figure 492 S-92—Usable Fuel Weight and Moment Table

FAA-CT-8080-7D, Figure 492. S-92—Usable Fuel Weight and Moment Table (printed page image, PDF page 489)

Previous GroupFigures 449–470 Next Group Figures 493–503

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Figure 473 Q400—Maximum Permissible Takeoff Weight (WAT Limit)—Takeoff Flap 5°

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