BRM AERO Bristell NG-5 Model Guide
BRM AERO Bristell NG-5 · Model Guide
Overview
The BRM AERO Bristell NG-5 is a single-engine, all-metal, low-wing, two-seat piston aircraft. It is built for recreational and cross-country flying, basic training and non-aerobatic use. The standard engine is a Rotax 912 ULS of 100 hp. It flies from a 600 kg (1320 lb) maximum takeoff weight. The manuals describe it as a light sport design.
- Two side-by-side seats, Rotax 912 ULS 100 hp, maximum takeoff weight 1320 lb (600 kg).
- The 2018 manual lists 102 KCAS cruise at 75% power and 570 NM range with no reserve.
- Wing is 8.13 m short or 9.13 m long. The 2024 manual shows different performance figures, so check which wing the aircraft has.
- Weight and balance data was corrected by a safety directive. Confirm the aircraft's manual pages are current.
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
- Height (ft) ·
- 7.48
- Length (ft) ·
- 21.1
- Wing span (ft) ·
- 26.65
- Engine power (hp) ·
- 100
- Usable fuel (gal) ·
- 31.4
- Cockpit width (in) ·
- 51.17
- Empty weight (lb) ·
- 715
- Fuel capacity (gal) ·
- 31.7
Performance
- Range (nm) ·
- 570
- Top speed (kt) ·
- 113
- Rate of climb (fpm) ·
- 920
- Cruise speed 65pct (kt) ·
- 97
- Cruise speed 75pct (kt) ·
- 102
V-speeds
- VA_KTS ·
- 96
- VX_KTS ·
- 60
- VY_KTS ·
- 72
- VFE_KTS ·
- 75
- VNE_KTS ·
- 157
- VNO_KTS ·
- 129
- VS0_KTS ·
- 38
- VS1_KTS ·
- 45
Weight & balance
- Cg aft limit (in) ·
- 34.9
- Max baggage (lb) ·
- 33
- Empty weight (lb) ·
- 715
- Cg front limit (in) ·
- 29.5
- Max wing locker (lb) ·
- 44
- Min crew weight (lb) ·
- 121
- Max front locker (lb) ·
- 22
- Max takeoff weight (lb) ·
- 1,320
What engine does the BRM AERO Bristell NG-5 use?
The manuals for the BRM AERO Bristell NG-5 list a Rotax 912 ULS of 100 hp at 5800 rpm for a maximum of 5 minutes. Maximum continuous power is 5500 rpm. It is paired with a three-blade ground-adjustable propeller.
How far can the BRM AERO Bristell NG-5 fly?
The 2018 manual for the BRM AERO Bristell NG-5 gives 570 NM at 75% power at 4000 ft with no fuel reserve. The 2024 manual shows 630 NM. Plan with your own reserves.
Can the BRM AERO Bristell NG-5 fly at night or in IMC?
The BRM AERO Bristell NG-5 may fly day VFR. Night VFR and IFR under VMC are allowed if it is properly equipped and the pilot is rated. IFR in IMC and icing are prohibited.
What is the BRM AERO Bristell NG-5 Model Guide?
The BRM AERO Bristell NG-5 Model Guide is a model guide for the BRM AERO Bristell NG-5, dated 2026.
What year was the BRM AERO Bristell NG-5 Model Guide published?
The BRM AERO Bristell NG-5 Model Guide — the BRM AERO Bristell NG-5 model guide on file — is dated 2026.
Common. More common than 91% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the BRM AERO Bristell NG-5.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
BRM AERO Bristell NG-5 for sale now
Free — save the NG-5 to your watchlist and track it in one place.
More BRM AERO Bristell NG-5manuals & documents
Related documents
- Bristell Aircraft Operating InstructionsBRM AERO Bristell NG-5 · Pilot's Operating Handbook
- DynAero MCR ULC Model GuideDynAero MCR ULC · Model Guide
- DynAero MCR-01 Sportster Model GuideDynAero MCR-01 Sportster · Model Guide
- AEROPRAKT LTD A-22 LS Model GuideAEROPRAKT LTD A-22 LS · Model Guide
- Betriebshandbuch D-MDMPBRM AERO Bristell NG-5 · Pilot's Operating Handbook
If you fly the BRM AERO Bristell NG-5, you may also be researching these.
In this document
What it carries
Two seats, a minimum pilot weight of 121 lb, and 1320 lb maximum takeoff weight. Standard empty weight is 715 lb. Baggage behind the seats is limited to 33 lb. Optional wing lockers take 44 lb each and the front locker 22 lb. Total fuel is 31.7 US gal, of which 31.4 is usable.
How it performs
The 2018 manual gives 113 KCAS top speed at sea level, 102 KCAS at 75% power and a Vy climb of 920 fpm. The 2024 manual (long-wing aircraft) gives 123 KCAS top speed, 108 KCAS cruise, 630 NM range and 860 fpm at Vy. Stall speed is 45 KCAS clean and 38 KCAS with full flaps (2018).
What to check
Confirm the wing length, the engine variant, and the current weight and balance pages. A safety directive revised the pilot arm and moved the datum to the firewall. Fuel can be mogas (EN 228 super) or AVGAS 100LL; follow the engine service instruction for fuel selection. Ask for the actual weighing report.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- IFR flight in IMC and flight in icing are prohibited. Aerobatics and intentional spins are prohibited.
- Safety directive ALL-SA-0-0-0-0001-2020 corrected the pilot arm and moved the datum to the firewall. Use the revised W&B data.
- Do not exceed maximum takeoff weight of 1320 lb (600 kg). Maximum limit load factors are +4 g and -2 g.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
BRM AERO Bristell NG-5 Model Guide The BRM AERO Bristell NG-5 is a single-engine, all-metal, low-wing, two-seat piston aircraft. It is built for recreational and cross-country flying, basic training and non-aerobatic use. The standard engine is a Rotax 912 ULS of 100 hp. It flies from a 600 kg (1320 lb) maximum takeoff weight. The manuals describe it as a light sport design. • Two side-by-side seats, Rotax 912 ULS 100 hp, maximum takeoff weight 1320 lb (600 kg). • The 2018 manual lists 102 KCAS cruise at 75% power and 570 NM range with no reserve. • Wing is 8.13 m short or 9.13 m long. The 2024 manual shows different performance figures, so check which wing the aircraft has. • Weight and balance data was corrected by a safety directive. Confirm the aircraft's manual pages are current. What it carries Two seats, a minimum pilot weight of 121 lb, and 1320 lb maximum takeoff weight. Standard empty weight is 715 lb. Baggage behind the seats is limited to 33 lb. Optional wing lockers take 44 lb each and the front locker 22 lb. Total fuel is 31.7 US gal, of which 31.4 is usable. How it performs The 2018 manual gives 113 KCAS top speed at sea level, 102 KCAS at 75% power and a Vy climb of 920 fpm. The 2024 manual (long-wing aircraft) gives 123 KCAS top speed, 108 KCAS cruise, 630 NM range and 860 fpm at Vy. Stall speed is 45 KCAS clean and 38 KCAS with full flaps (2018). What to check Confirm the wing length, the engine variant, and the current weight and balance pages. A safety directive revised the pilot arm and moved the datum to the firewall. Fuel can be mogas (EN 228 super) or AVGAS 100LL; follow the engine service instruction for fuel selection. Ask for the actual weighing report. Safety notes: • IFR flight in IMC and flight in icing are prohibited. Aerobatics and intentional spins are prohibited. • Safety directive ALL-SA-0-0-0-0001-2020 corrected the pilot arm and moved the datum to the firewall. Use the revised W&B data. • Do not exceed maximum takeoff weight of 1320 lb (600 kg). Maximum limit load factors are +4 g and -2 g.