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Atlas / Aircraft / ELOS findings

ELOS TC4948NY-T-A-25

Current · Issued 04/18/2013 · FAA DRS

Emergency Landing Conditions PDF ↗

14 CFR sections Project Other ELOS Special conditions Same CFR sections

14 CFR sections deviation applies to

§ 25.721
§ 25.963

Project

Finding #: TC4948NY-T-A-25
Applicant: Bombardier Aerospace
Make: Bombardier Aerospace | Bombardier Aerospace
Model: BD-500-1A10 | BD-500-1A11
Office: AIR-770: West Certification Branch LA

Other ELOS on this aircraft

ELOS TC4948NY-T-CS-10INFORMATION: Equivalent Level of Safety (ELOS) Finding for Symbolic Exit Signs on Model BD-500-1A10 / -1A11, FAA Project # TC4948NY-T
ELOS TC4948NY-T-P-06INFORMATION: Equivalent Level of Safety (ELOS) Finding for Automatic Takeoff Thrust Control System (ATTCS) Appendix I Thrust Setting, Lack of On/Off Switch and Indication Requirements on BD-500-1A10 and 1A11, FAA Project TC4948NY-T
ELOS TC4948NY-T-ES-20Oxygen Quantity Indication
ELOS TC4948NY-T-ES-19NFORMATION: Equivalent Level of Safety (ELOS) Finding for Penetrations in Fire Barrier of Cargo Compartment and WTBF on Model BD-500-1A10 / -1A11, FAA Project #TC4948NY-T
ELOS TC4948NY-T-S-13INFORMATION: Equivalent Level of Safety Finding (ELOS) for use of ARAC Recommendation Revision to 25.1301 and 25.1309 on Bombardier Aerospace Model BD-500-1A10/-1A11
ELOS TC4948NY-T-P-16Engine and APU Fire Protection on the BD-500-1A10 and 1A11, FAA Project TC4948NY-T

Special conditions on this aircraft

SC 25-731-SCSpecial Conditions: Bombardier Model BD-500-1A10 and BD-500-1A11 Airplanes, Installation of Inflatable Lap Belts on Seats
SC 25-597-SCSpecial Conditions: Bombardier Aerospace Inc. Model BD-500-1A10 and BD-500-1A11 Airplanes; Flight-Envelope Protection, High Incidence Protection Function
SC 25-591-SCSpecial Conditions: Bombardier Aerospace, Models BD-500-1A10 and BD-500-1A11 Series Airplanes; Installed Rechargeable Lithium Batteries and Battery Systems
SC 25-576-SCSpecial Conditions: Bombardier Aerospace Incorporated, Models BD- 500-1A10 and BD-500-1A11 Series Airplanes; Electronic Flight-Control System (EFCS): Pitch-and Roll-Limiting Functions
SC 25-584-SCSpecial Conditions: Bombardier Aerospace, Models BD-500-1A10 and BD-500-1A11; Electronic Flight Control System: Lateral-Directional and Longitudinal Stability and Low-Energy Awareness

Same CFR sections

ELOS TC-01-2010-0024-A-5Structural Integrity of Fuel Tanks for Emergency Landing Conditions and Landing Gear
ELOS TC0717IB-T-A-6INFORMATION: Equivalent Level of Safety (ELOS) Finding for Crash Protection of Fuel Tanks and Systems on Embraer Model EMB-550 and EMB-545 airplanes, FAA Project # TC0717IB-T and AT10256IB-T
ELOS AT7180NY-T-GA-A-04Finding for GA-A-04 on a Model BD-700-2A12 & BD-700-2A13 airplane, FAA Project # AT7180NY-T & AT7285NY-T
ELOS TC0717IB-T-A-6INFORMATION: Equivalent Level of Safety (ELOS) Finding for Crash Protection of Fuel Tanks and Systems on a Model EMB-550 airplane, FAA Project # TC0717IB-T
ELOS AT0329IB-T-A-10R1Belly-mounted fuel tanks

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