# Fairchild 22 C7A

- Type: Aircraft model (FAA registry)
- Registry code: 3370104
- Manufacturer (registry): FAIRCHILD
- Model: 22 C7A
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 2
- Weight class: Up to 12,499 lb
- Cruise speed: 90 mph
- Certification: Type certificated
- Data sheet: [TCDS ATC 438](https://openairdocs.org/tcds/ATC%20438) (OpenAirDocs)
- Holder: Fairchild Industries Inc.
- Registered aircraft: 4
- Page: https://openairdocs.org/model/fairchild-22-c7a

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 46-40-02](https://openairdocs.org/ad/46-40-02): Oleo Tube Reinforcement · Fairchild Industries 22 C7, 22 C7A, 22 C7AM and 23 more

## Registered aircraft (4)

- [N12611](https://openairdocs.org/aircraft/N12611): [Hodgdon Theodore E III](https://openairdocs.org/faa-owner/HODGDON%20THEODORE%20E%20III), [Danbury, CT](https://openairdocs.org/faa-place/CT/Danbury), built 1931, S/N 1013
- [N12674](https://openairdocs.org/aircraft/N12674): [Petro Jerry R](https://openairdocs.org/faa-owner/PETRO%20JERRY%20R), [Williamsburg, VA](https://openairdocs.org/faa-place/VA/Williamsburg), built 1932, S/N 1033
- [N2816](https://openairdocs.org/aircraft/N2816): [Western Antique Aeroplane & Automobile Museum](https://openairdocs.org/faa-owner/WESTERN%20ANTIQUE%20AEROPLANE%20%26%20AUTOMOBILE%20MUSEUM), [Hood River, OR](https://openairdocs.org/faa-place/OR/Hood%20River), built 1933, S/N 1053
- [N2871](https://openairdocs.org/aircraft/N2871): [Petro Jerry R](https://openairdocs.org/faa-owner/PETRO%20JERRY%20R), [Williamsburg, VA](https://openairdocs.org/faa-place/VA/Williamsburg), built 1933, S/N 1055

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (7)

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

- [SDR CA070827009](https://openairdocs.org/sdr/CA070827009), Aug 8, 2007: ACTUATOR. STIFF. (CAN) PILOT COMPLAINED ABOUT AILERON STIFF TO MOVE AND WOULD OCCASIONALLY STICK IN THE FULL RT POSITION. UPON MAINTENANCE TROUBLESHOOTING IT WAS NOTICED THAT TH
- [SDR LNX2005F00002](https://openairdocs.org/sdr/LNX2005F00002), Nov 15, 2005: LINE. LOOSE. DURING INTIAL DEPARTURE CLIMB THE CREW OBSERVED A FIRE WARNING LIGHT ILLUMINATION ON THE LT ENGINE FIRE WARNING PANEL. EMERGENCY CHECKLIST COMPLETED TO INCLUDE 
- [SDR O05R200466978](https://openairdocs.org/sdr/O05R200466978), Jan 27, 2004: BLADE. DAMAGED. BLADE REJECTED IAW MFG CONCESSION 102556/C/P.
- [SDR O05R200423591](https://openairdocs.org/sdr/O05R200423591), Jan 27, 2004: BLADE. UNSERVICEABLE. BLADE REJECTED IAW MFG CONCESSION 102566/C/P.
- [SDR O05R200411256](https://openairdocs.org/sdr/O05R200411256), Jan 27, 2004: BLADE. DAMAGED. BLADE REJECTED IAW MFG CONCESSION 102566/C/P.
- [SDR 2001FA0000522](https://openairdocs.org/sdr/2001FA0000522), Oct 30, 2001: DRAG BRACE. FAILED. DRAG BRACE FAILURE.
- [SDR 20000829SH001](https://openairdocs.org/sdr/20000829SH001), Jul 19, 2000: DRIVE GEAR. FRACTURED. LOSS OF OIL PRESSURE (ENGINE) IN FLIGHT. FOUND MAIN OIL PUMP, PN 33019, DRIVESHAFT SHEARED JUST BELOW THE SCAVENGE VANES. THE CAUSE APPEARS TO BE A FATIGUE FRAC

## STCs that may be installed (OpenAirDocs) (4)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA01406NY](https://openairdocs.org/stc/SA01406NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and rotary wing. Airwolf Filter Corporation
- [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts. Andrew D. Humphrey
- [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. M-20 Oil Separators LLC

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