# Thunder Balloons AX8-105

- Type: Aircraft model (FAA registry)
- Registry code: 8970112
- Manufacturer (registry): THUNDER BALLOONS LIMITED
- Model: AX8-105
- Aircraft type: Balloon
- Category: Balloon
- Engines: None
- Seats: 4
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/thunder-balloons-ax8-105

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2013-03-10](https://openairdocs.org/ad/2013-03-10): Hardware · Aeronaut Instruction Research Skysailor 105, Skysailor 90, 110C and 439 more. Effective Mar 19, 2013
- [AD 2008-04-15](https://openairdocs.org/ad/2008-04-15): Self seal valves · Cameron Balloons AX10-160 (S.1), AX10-160(S.2), AX10-180 (S.1) and 24 more. Effective Mar 25, 2008

## Information bulletins (advisory) (1)

- [SAIB CE-11-44](https://openairdocs.org/saib/CE-11-44): Fuel: Cylinder Strap Installation. Issued Jul 13, 2011

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Head Balloons AX8-105](https://openairdocs.org/model/head-balloons-ax8-105): 58 registered aircraft, registry code 4280300
- [Head Balloons AX8-105](https://openairdocs.org/model/head-balloons-ax8-105): 3 registered aircraft, registry code 4280237
- [Thunder & Colt THUNDER AX8-105](https://openairdocs.org/model/thunder-colt-thunder-ax8-105): 3 registered aircraft, registry code 8970126
- [Thunder & Colt THUNDER AX8-105 S1](https://openairdocs.org/model/thunder-colt-thunder-ax8-105-s1): 2 registered aircraft, registry code 8970124

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.