BOMBARDIER CHALLENGER 350 Model Guide
BOMBARDIER CHALLENGER 350 · Model Guide
Overview
The BOMBARDIER CHALLENGER 350 is a turbofan business jet. It is covered by Airplane Flight Manual BD-100-1A10 (CH 350 and CH 3500) for serial numbers 20501-20999. The manual was first issued Jun 11/2014, and the latest revision supplied is Revision 34 (Jun 14/2022). The supplied documents are mostly limitations and revision history, with no full performance tables.
- Family-level maxima, not this variant's figures: up to 3200 nm range, 458 kt cruise, 45000 ft ceiling, 8 passengers, 18400 kg MTOW.
- Autopilot minimum engage height is 700 ft AGL in climb, en route or descent. Approach minimum use heights are 80, 160 or 200 ft AGL.
- Maximum altitude with the yaw damper off is 31,000 ft.
- Confirm the aircraft's manual is current: the latest supplied is Revision 34 (Jun 14/2022), and it applies to serials 20501-20999.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 48 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Autopilot min engage height (ft) ·
- 700
- Yaw damper off max altitude (ft) ·
- 31,000
- Autopilot min use height visual nonprecision (ft) ·
- 200
Performance
- Family max range (nm) ·
- 3,200
- Family max cruise speed (kt) ·
- 458
- Family max service ceiling (ft) ·
- 45,000
Which serial numbers does the BOMBARDIER CHALLENGER 350 manual cover?
The BOMBARDIER CHALLENGER 350 AFM (BD-100-1A10, CH 350 and CH 3500) covers serial numbers 20501-20999. Some limitations differ by serial, for example the V-speed database split at 20664.
What is the maximum altitude with the yaw damper off on the BOMBARDIER CHALLENGER 350?
The BOMBARDIER CHALLENGER 350 AFM sets a maximum altitude of 31,000 ft with the yaw damper off.
What are the cabin pressure limits on the BOMBARDIER CHALLENGER 350?
For the BOMBARDIER CHALLENGER 350, maximum positive differential pressure is 9.4 psi and maximum negative is -0.5 psi. It must not exceed 0.1 psi on the ground during taxi, or 1.0 psi during landing.
What is the BOMBARDIER CHALLENGER 350 Model Guide?
The BOMBARDIER CHALLENGER 350 Model Guide is a model guide for the BOMBARDIER CHALLENGER 350, dated 2026.
What year was the BOMBARDIER CHALLENGER 350 Model Guide published?
The BOMBARDIER CHALLENGER 350 Model Guide — the BOMBARDIER CHALLENGER 350 model guide on file — is dated 2026.
Common. More common than 97% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the BOMBARDIER CHALLENGER 350.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Pressurization, oxygen and air conditioning limits
Maximum positive differential pressure is 9.4 psi and maximum negative is -0.5 psi. Differential must not exceed 0.1 psi on the ground during taxi, or 1.0 psi during landing. Oxygen masks are not approved above 40,000 feet cabin altitude. Do not select TRIM AIR ONLY on the ground.
FMS and database checks
The FMS is the Rockwell Collins Pro Line 21 Advance system. FMS performance, ETE/ETA and fuel data are advisory only. V-speed database must be 096-5016-001 on 20501-20663 without SB 350-34-012, and 096-5016-002 on 20664 and later. Performance database must be 096-5327-001 on 20578 and later.
Manual revision history
Revision 33 (Mar 29/2022) added the CH 3500 to the effectivity table. Revision 31 (Sep 22/2021) introduced a new landing gear selector lever and Reduced Cabin Altitude. Revision 19 (Sep 5/2018) added a new supplement for steep approaches with glidepaths from 4.5 to 5.5 degrees.
Safety notes
- In ALTS CAP mode the autopilot may not hold airspeed. After an engine failure in climb, airspeed may decay and crew intervention may be required.
- With database 096-5016-001, the FMS cannot calculate actual landing distance on contaminated runways. Use the CAFM or QRH instead.
- At airport pressure altitudes of 8000 ft and above, compare the FMS takeoff field length with the CAFM result. If the CAFM figure is longer, use the CAFM takeoff field length and speeds.
Full document text
BOMBARDIER CHALLENGER 350 Model Guide The BOMBARDIER CHALLENGER 350 is a turbofan business jet. It is covered by Airplane Flight Manual BD-100-1A10 (CH 350 and CH 3500) for serial numbers 20501-20999. The manual was first issued Jun 11/2014, and the latest revision supplied is Revision 34 (Jun 14/2022). The supplied documents are mostly limitations and revision history, with no full performance tables. • Family-level maxima, not this variant's figures: up to 3200 nm range, 458 kt cruise, 45000 ft ceiling, 8 passengers, 18400 kg MTOW. • Autopilot minimum engage height is 700 ft AGL in climb, en route or descent. Approach minimum use heights are 80, 160 or 200 ft AGL. • Maximum altitude with the yaw damper off is 31,000 ft. • Confirm the aircraft's manual is current: the latest supplied is Revision 34 (Jun 14/2022), and it applies to serials 20501-20999. Pressurization, oxygen and air conditioning limits Maximum positive differential pressure is 9.4 psi and maximum negative is -0.5 psi. Differential must not exceed 0.1 psi on the ground during taxi, or 1.0 psi during landing. Oxygen masks are not approved above 40,000 feet cabin altitude. Do not select TRIM AIR ONLY on the ground. FMS and database checks The FMS is the Rockwell Collins Pro Line 21 Advance system. FMS performance, ETE/ETA and fuel data are advisory only. V-speed database must be 096-5016-001 on 20501-20663 without SB 350-34-012, and 096-5016-002 on 20664 and later. Performance database must be 096-5327-001 on 20578 and later. Manual revision history Revision 33 (Mar 29/2022) added the CH 3500 to the effectivity table. Revision 31 (Sep 22/2021) introduced a new landing gear selector lever and Reduced Cabin Altitude. Revision 19 (Sep 5/2018) added a new supplement for steep approaches with glidepaths from 4.5 to 5.5 degrees. Safety notes: • In ALTS CAP mode the autopilot may not hold airspeed. After an engine failure in climb, airspeed may decay and crew intervention may be required. • With database 096-5016-001, the FMS cannot calculate actual landing distance on contaminated runways. Use the CAFM or QRH instead. • At airport pressure altitudes of 8000 ft and above, compare the FMS takeoff field length with the CAFM result. If the CAFM figure is longer, use the CAFM takeoff field length and speeds.