Spirit Airlines Memory Items and
Limitations 2024/2025 Exam Q&A 100%
Pass
Non-Sharklet Wingspan - ✔✔111 ft, 10 in
Sharklet Wingspan - ✔✔117 ft, 5 in
A319 Tailstrike Pitch Attitudes - ✔✔Struts compressed: 13.9°
A320 Tailstrike Pitch Attitudes - ✔✔Struts compressed: 11.7°
A321 Tailstrike Pitch Attitudes - ✔✔Struts compressed: 9.7°
A319 Max Landing Weight - ✔✔137,788 lbs
A320 Max Landing Weight - ✔✔145,505 lbs
A320 NEO Max Landing Weight - ✔✔148,591 lbs
A321 Max Landing Weight - ✔✔171,519 lbs
Maximum Certified Altitude - ✔✔FL398
Maximum Allowed Wing Fuel Imbalance In-Flight and at Landing (A319/A320) -
✔✔3,306 lbs
EGT Limit for Starting (A319/320/321) - ✔✔635°C
Page 1 of 11
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT.ALL RIGHTS RESERVED
, Unreliable Speed Indication/ADR Check Procedure - ✔✔If the safe conduct of
the flight is impacted:
• AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
• A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• PITCH/THRUST:
- Below THRUST RED ALT . . . . . . . . . . . . . . . . . . . . . . . .15°/TOGA
- Above THRUST RED ALT and Below FL 100. . . . . . . . .10°/CLB
- Above THRUST RED ALT and Above FL 100. . . . . . . . . . 5°/CLB
• FLAPS (if CONF 0(1)(2)(3)) . . . . . . MAINTAIN CURRENT CONF
• FLAPS (if CONF FULL) . . . . . SELECT CONF 3 AND MAINTAIN
• SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED
• L/G. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
Note: When at or above MSA or circuit altitude, level off for
troubleshooting.
NAV mode may be used in the terminal area, provided: - ✔✔- GPS PRIMARY is
available, or
- HIGH accuracy is displayed, and the appropriate RNP is
checked or entered on the MCDU, or
- FMS navigation is cross-checked with NAVAID raw data.
Page 2 of 11
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT.ALL RIGHTS RESERVED
Limitations 2024/2025 Exam Q&A 100%
Pass
Non-Sharklet Wingspan - ✔✔111 ft, 10 in
Sharklet Wingspan - ✔✔117 ft, 5 in
A319 Tailstrike Pitch Attitudes - ✔✔Struts compressed: 13.9°
A320 Tailstrike Pitch Attitudes - ✔✔Struts compressed: 11.7°
A321 Tailstrike Pitch Attitudes - ✔✔Struts compressed: 9.7°
A319 Max Landing Weight - ✔✔137,788 lbs
A320 Max Landing Weight - ✔✔145,505 lbs
A320 NEO Max Landing Weight - ✔✔148,591 lbs
A321 Max Landing Weight - ✔✔171,519 lbs
Maximum Certified Altitude - ✔✔FL398
Maximum Allowed Wing Fuel Imbalance In-Flight and at Landing (A319/A320) -
✔✔3,306 lbs
EGT Limit for Starting (A319/320/321) - ✔✔635°C
Page 1 of 11
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT.ALL RIGHTS RESERVED
, Unreliable Speed Indication/ADR Check Procedure - ✔✔If the safe conduct of
the flight is impacted:
• AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
• A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• PITCH/THRUST:
- Below THRUST RED ALT . . . . . . . . . . . . . . . . . . . . . . . .15°/TOGA
- Above THRUST RED ALT and Below FL 100. . . . . . . . .10°/CLB
- Above THRUST RED ALT and Above FL 100. . . . . . . . . . 5°/CLB
• FLAPS (if CONF 0(1)(2)(3)) . . . . . . MAINTAIN CURRENT CONF
• FLAPS (if CONF FULL) . . . . . SELECT CONF 3 AND MAINTAIN
• SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED
• L/G. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
Note: When at or above MSA or circuit altitude, level off for
troubleshooting.
NAV mode may be used in the terminal area, provided: - ✔✔- GPS PRIMARY is
available, or
- HIGH accuracy is displayed, and the appropriate RNP is
checked or entered on the MCDU, or
- FMS navigation is cross-checked with NAVAID raw data.
Page 2 of 11
COPYRIGHT©NINJANERD 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER:
619652435. TERMS OF USE. PRIVACY STATEMENT.ALL RIGHTS RESERVED
