# Hiller 1100

- Type: Aircraft model (FAA registry)
- Registry code: 4361405
- Manufacturer (registry): HILLER
- Model: 1100
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Turbo-shaft
- Seats: 4
- Weight class: Up to 12,499 lb
- Cruise speed: 95 mph
- Certification: Type certificated
- Data sheet: [TCDS H2WE](https://openairdocs.org/tcds/H2WE) (OpenAirDocs)
- Holder: Air Space Design and Manufacturing LLC
- Registered aircraft: 0
- Page: https://openairdocs.org/model/hiller-1100

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 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023
- [AD 79-11-04](https://openairdocs.org/ad/79-11-04): Lower Housing Transmissions · FH1100 Manufacturing 1100 and FH-1100. Effective Jun 4, 1979
- [AD 77-07-08](https://openairdocs.org/ad/77-07-08): Tail Rotor Tension Torsion Bars · FH1100 Manufacturing 1100 and FH-1100. Effective Aug 5, 1977
- [AD 75-03-04](https://openairdocs.org/ad/75-03-04): Tail Fin Spar · FH1100 Manufacturing 1100 and FH-1100. Effective Jul 8, 1975
- [AD 72-13-07](https://openairdocs.org/ad/72-13-07): Drive Shaft Assemblies · FH1100 Manufacturing 1100 and FH-1100. Effective Jun 27, 1972
- [AD 71-24-02](https://openairdocs.org/ad/71-24-02): Failure of Transmission Mount Strut · FH1100 Manufacturing 1100 and FH-1100. Effective Nov 24, 1971
- [AD 71-11-03](https://openairdocs.org/ad/71-11-03): VNE Placard · FH1100 Manufacturing 1100 and FH-1100. Effective May 19, 1971
- [AD 70-18-04](https://openairdocs.org/ad/70-18-04): Transmission Vertical Status · FH1100 Manufacturing 1100. Effective Sep 15, 1970

Historical (superseded or no longer in force):

- [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021

## Information bulletins (advisory) (1)

- [SAIB SW-07-05](https://openairdocs.org/saib/SW-07-05): Inspect the airframe and airframe components. Issued Oct 27, 2006

## Registered aircraft

None registered with this model now.

## STCs approved for it (8)

- [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the
Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [STC SH4173NM](https://openairdocs.org/stc/SH4173NM): Installation of Simplex Model 7600 modular electrical system. (US ARMY OH-13E M74A). Simplex Manufacturing Company
- [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC
- [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC
- [STC SA593CH (3 OF 5)](https://openairdocs.org/stc/SA593CH%20(3%20OF%205)) (historical): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC
- [STC SH3319NM (1 OF 2)](https://openairdocs.org/stc/SH3319NM%20(1%20OF%202)) (historical): Installation of Precise Flight Pulselite Control Unit in the
Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (1)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2012FA0000550](https://openairdocs.org/sdr/2012FA0000550), Aug 7, 2012: FLEX COUPLING. SEPARATED. FLEX COUPLING FAILED AT OUTPUT OF INTERMEDIATE GEARBOX. SUBSTATIAL DAMAGE OCCURED DURING HARD LANDING.

## The same model under other registry codes

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

- [Mini Max 1100](https://openairdocs.org/model/mini-max-1100): 0 registered aircraft, registry code 05902MD
- [Rogerson Hiller 1100](https://openairdocs.org/model/rogerson-hiller-1100): 0 registered aircraft, registry code 4368001

---
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.