AEROPRAKT LTD A-22 LS Model Guide
AEROPRAKT LTD A-22 LS · Model Guide
Overview
The AEROPRAKT LTD A-22 LS is a single-engine piston light aircraft. It has fabric-covered wings with fuel tanks in the wings, wing struts and flaperons. A glider and banner tow release is optional. No registry specs were supplied, and the checklist quotes speeds at a 600 kg MTOW. Check the POH and service bulletins against the serial number you are buying.
- Optional Tost E 85 tow release for glider and banner towing; the towing aircraft's mass may not exceed 500 kg.
- Service bulletin SB A22LS-24 covers landing-gear braking resonance on serials 1-434; check the beam for fatigue cracks.
- Rescue-system bracket SB A22LS-23 is mandatory on listed serials; confirm it was done if a parachute is fitted.
- Pre-purchase run-up at 4,000 rpm: max 300 rpm drop per ignition side, oil pressure 29-73 PSI.
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
What is the maximum weight in the documents for the AEROPRAKT LTD A-22 LS?
The pre-flight checklist for the AEROPRAKT LTD A-22 LS gives speeds at an MTOW of 600 kg. Registry data supplied no weights, so confirm limits in the POH for your serial number.
Can the AEROPRAKT LTD A-22 LS tow gliders?
Yes, with the optional E 85 tow release. The AEROPRAKT LTD A-22 LS may tow a glider up to 700 kg with one pilot aboard, using a 200-300 daN weak link and a 40 to 60 m rope.
What engine check should I see on the AEROPRAKT LTD A-22 LS?
At 4,000 rpm the checklist allows a maximum drop of 300 rpm per ignition side and a 115 rpm difference between sides. Oil pressure should read 29-73 PSI and idle should be at least 1400 rpm.
What is the AEROPRAKT LTD A-22 LS Model Guide?
The AEROPRAKT LTD A-22 LS Model Guide is a model guide for the AEROPRAKT LTD A-22 LS, dated 2026.
What year was the AEROPRAKT LTD A-22 LS Model Guide published?
The AEROPRAKT LTD A-22 LS Model Guide — the AEROPRAKT LTD A-22 LS model guide on file — is dated 2026.
Common. More common than 89% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the AEROPRAKT LTD A-22 LS.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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More AEROPRAKT LTD A-22 LSmanuals & documents
See all 13 →- AEROPRAKT-22LS Pilot Operating HandbookPilot's Operating Handbook
- SERVICE BULLETIN No. SB A22LS-24Service Bulletins
- SERVICE BULLETIN No. SB A22LS-23Service Bulletins
- Aeroprakt Foxbat A22LS - Pre-flight inspection checklistChecklist
- SERVICE BULLETIN No. SB A22LS-15Service Bulletins
- AEROPRAKT-22L2 Airplane Maintenance ManualMaintenance Manual
- SAFETY ALERT - AeropraktService Bulletins
- AEROPRAKT-22LS Airplane Maintenance ManualMaintenance Manual
- AEROPRAKT-22LS Airplane Maintenance ManualMaintenance Manual
- AEROPRAKT-22LS Pilot Operating HandbookPilot's Operating Handbook
- AEROPRAKT-22LS Illustrated Parts CatalogParts Catalog
- AEROPRAKT-22LS (A22L2) Illustrated Parts CatalogParts Catalog
Related documents
- AEROPRAKT-22LS Pilot Operating HandbookAEROPRAKT LTD A-22 LS · Pilot's Operating Handbook
- AEROPRAKT-22LS Pilot Operating HandbookAEROPRAKT LTD A-22 LS · Pilot's Operating Handbook
- AEROPRAKT LTD A-32 Model GuideAEROPRAKT LTD A-32 · Model Guide
- AEROPRAKT-22LS Pilot Operating HandbookAEROPRAKT LTD A-22 LS · Pilot's Operating Handbook
- AEROPRAKT-22L2 Airplane Maintenance ManualAEROPRAKT LTD A-22 LS · Maintenance Manual
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In this document
Glider and banner towing
The optional E 85 tow release fits on the tail fuselage. Glider towing needs one pilot only, and the glider may not exceed 700 kg. The weak link must be 200-300 daN and the rope 40 to 60 m long. Minimum tow speed is 95 km/h and best climb speed is 105 km/h. Takeoff distance to 15 m is under 600 m in the stated conditions. High grass can add up to 25%.
Bulletins to verify on a used aircraft
SB A22LS-24 (landing-gear braking resonance) affects serials 1-434. Its text is built into POH for serials over 434. SB A22LS-23 adds a rescue rocket bracket on listed serials and is mandatory. SB A22LS-15 moved some 50 hour checks to 100 hours for serials 1-282. IB A-22LS-08 moved wing and strut inspection to 500 hours. Propeller hub and spinner are checked every 200 h.
What the pre-flight checklist tells you to inspect
Check engine mount and vibration dampers for cracks, exhaust springs, and fuel, oil and coolant leaks. Inspect nose and main legs and the tyres and brakes. Check wing and strut attachment fittings, fuel tank caps and vents, flaperon hinges, and the baggage container. Verify the recovery system if fitted. Before takeoff, coolant must read at least 60°C and oil at least 50°C.
Safety notes
- Braking: avoid resonant vibration of the main gear legs; hard braking on hard runways may cause fatigue cracks in the gear attachment beam.
- Towing: release the rope or banner before landing and beware of obstacles that may catch it.
- Skipping the rescue-system bracket (SB A22LS-23) will cause incorrect function and injury if the system deploys.
Full document text
AEROPRAKT LTD A-22 LS Model Guide The AEROPRAKT LTD A-22 LS is a single-engine piston light aircraft. It has fabric-covered wings with fuel tanks in the wings, wing struts and flaperons. A glider and banner tow release is optional. No registry specs were supplied, and the checklist quotes speeds at a 600 kg MTOW. Check the POH and service bulletins against the serial number you are buying. • Optional Tost E 85 tow release for glider and banner towing; the towing aircraft's mass may not exceed 500 kg. • Service bulletin SB A22LS-24 covers landing-gear braking resonance on serials 1-434; check the beam for fatigue cracks. • Rescue-system bracket SB A22LS-23 is mandatory on listed serials; confirm it was done if a parachute is fitted. • Pre-purchase run-up at 4,000 rpm: max 300 rpm drop per ignition side, oil pressure 29-73 PSI. Glider and banner towing The optional E 85 tow release fits on the tail fuselage. Glider towing needs one pilot only, and the glider may not exceed 700 kg. The weak link must be 200-300 daN and the rope 40 to 60 m long. Minimum tow speed is 95 km/h and best climb speed is 105 km/h. Takeoff distance to 15 m is under 600 m in the stated conditions. High grass can add up to 25%. Bulletins to verify on a used aircraft SB A22LS-24 (landing-gear braking resonance) affects serials 1-434. Its text is built into POH for serials over 434. SB A22LS-23 adds a rescue rocket bracket on listed serials and is mandatory. SB A22LS-15 moved some 50 hour checks to 100 hours for serials 1-282. IB A-22LS-08 moved wing and strut inspection to 500 hours. Propeller hub and spinner are checked every 200 h. What the pre-flight checklist tells you to inspect Check engine mount and vibration dampers for cracks, exhaust springs, and fuel, oil and coolant leaks. Inspect nose and main legs and the tyres and brakes. Check wing and strut attachment fittings, fuel tank caps and vents, flaperon hinges, and the baggage container. Verify the recovery system if fitted. Before takeoff, coolant must read at least 60°C and oil at least 50°C. Safety notes: • Braking: avoid resonant vibration of the main gear legs; hard braking on hard runways may cause fatigue cracks in the gear attachment beam. • Towing: release the rope or banner before landing and beware of obstacles that may catch it. • Skipping the rescue-system bracket (SB A22LS-23) will cause incorrect function and injury if the system deploys.