CESSNA 337G Model Guide
CESSNA 337G · Model Guide
Overview
The CESSNA 337G is a six-seat, twin-engine piston Cessna 337 Series (Super Skymaster) with front-tractor and rear-pusher engines. The listed engine is a Continental IO-360-G or -GB rated 210 hp, with a McCauley D2AF34C Series propeller. Maximum takeoff weight is 4630 lb. Buyers should focus on wing spar, flap cable, fuel strainer and trim system records.
- Up to six seats, 4630 lb max takeoff weight, 4465 lb max landing weight and a 365 lb baggage allowance.
- Listed cruise is 165 kt and max speed 198 kt, with 125 gal fuel capacity.
- Wing spar AD inspections apply to 337G serials 33701194 through 33701852; confirm they are logged.
- Flap cables can wear out of sight at the inboard bellcrank; ask when the cables were last removed and inspected.
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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 ·
- 49 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp) ·
- 210
- Max speed (kt) ·
- 198
- Cruise speed (kt) ·
- 165
- Fuel capacity (gal) ·
- 125
- Max takeoff weight (lb) ·
- 4,630
V-speeds
- VFE_KTS ·
- 108
- VNE_KTS ·
- 198
- VNO_KTS ·
- 165
Weight & balance
- Baggage allowance (lb) ·
- 365
- Max landing weight (lb) ·
- 4,465
- Max takeoff weight (lb) ·
- 4,630
What engine does the CESSNA 337G have?
The CESSNA 337G is listed with a Continental IO-360-G or -GB engine rated 210 hp and a McCauley D2AF34C Series propeller. The type acceptance report lists the engine for the 337G as the IO-360-G or -GB.
How many people can the CESSNA 337G carry?
The CESSNA 337G has a maximum of 6 seats and a maximum takeoff weight of 4630 lb. Baggage allowance is 365 lb. Check the actual weight and balance for the individual aircraft.
What mandatory service items affect the CESSNA 337G?
The CESSNA 337G is covered by Service Letter MEL-28-02, a fuel strainer bowl inspection due at the next 100-hour or 12-month inspection. It is also covered by the wing spar inspection AD and the trim system inspection letter ME77-34.
What is the CESSNA 337G Model Guide?
The CESSNA 337G Model Guide is a model guide for the CESSNA 337G, dated 2026.
What year was the CESSNA 337G Model Guide published?
The CESSNA 337G Model Guide — the CESSNA 337G model guide on file — is dated 2026.
Common. More common than 95% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 337G.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
CESSNA 337G for sale now
Free — save the 337 to your watchlist and track it in one place.
More CESSNA 337Gmanuals & documents
See all 15 →- FUEL - FUEL STRAINER INSPECTIONMaintenance Manual
- Type Certificate Data SheetType Certificate
- R1224 REGULATOR INSTALLATION INSTRUCTIONS P/N 12-1001Wiring Diagrams
- Type Acceptance Report - TAR 17/21B/26 - CESSNA F337 SeriesOther Documents
- Airworthiness Directive Schedule Aeroplanes Cessna 337 SeriesService Bulletins
- Type Acceptance Report TAR 18/21B/4 – Cessna 337 SeriesOther Documents
- AD/CESSNA 337/31 Alternate Static Air Source Selector Valve PlacardService Bulletins
- AD/CESSNA 337/30 Pitot Tube InstallationSupplemental Type Certificate
- AIRWORTHINESS DIRECTIVE AD/CESSNA 337/22 Amdt 3Airworthiness Directives
- Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series AirplanesAirworthiness Directives
- AWB 27-3 Issue 1, Cessna 336/337 Flap Cable WearService Bulletins
- Airworthiness Directive AD/CESSNA 337/28 Fuel StrainerService Bulletins
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In this document
What to inspect on a pre-buy
Wing spar: AD/CESSNA 337/22 Amdt 3 requires front and rear spar inspection for cracking, using eddy current on the front spar. Flap cables: wear hides at inboard bellcrank P/N 1462020-27, so the cables must come off for inspection. Fuel strainer: check the 0756008-1 bowl against Service Letter MEL-28-02. Trim: tab actuator mounts and free play are checked every 100 hours.
Records, modifications and paperwork
The NZ AD schedule lists the 337G. Ask for proof that each AD and service letter was done. Aircraft with the Robertson STC SA1627WE conversion get reduced spar inspection thresholds and intervals, and also have a pitot tube rework requirement (Robertson Kit 14-118-100). Check wheel part numbers and manufacture dates against Cleveland SB7064 (date code 03/95 and later). NZ type acceptance covers the 337G with no special import requirements.
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Safety notes
- Failed flap cables have caused asymmetric flap extension and loss of control on landing; inspect cables fully at the 100-hour or annual inspection.
- Cleveland SB7064: defective die-cast wheels can cause loss of directional control or brake effectiveness during taxi.
- Spar cracking is the subject of a repeat inspection AD; do not buy without documented spar inspection compliance.
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
CESSNA 337G Model Guide The CESSNA 337G is a six-seat, twin-engine piston Cessna 337 Series (Super Skymaster) with front-tractor and rear-pusher engines. The listed engine is a Continental IO-360-G or -GB rated 210 hp, with a McCauley D2AF34C Series propeller. Maximum takeoff weight is 4630 lb. Buyers should focus on wing spar, flap cable, fuel strainer and trim system records. • Up to six seats, 4630 lb max takeoff weight, 4465 lb max landing weight and a 365 lb baggage allowance. • Listed cruise is 165 kt and max speed 198 kt, with 125 gal fuel capacity. • Wing spar AD inspections apply to 337G serials 33701194 through 33701852; confirm they are logged. • Flap cables can wear out of sight at the inboard bellcrank; ask when the cables were last removed and inspected. What to inspect on a pre-buy Wing spar: AD/CESSNA 337/22 Amdt 3 requires front and rear spar inspection for cracking, using eddy current on the front spar. Flap cables: wear hides at inboard bellcrank P/N 1462020-27, so the cables must come off for inspection. Fuel strainer: check the 0756008-1 bowl against Service Letter MEL-28-02. Trim: tab actuator mounts and free play are checked every 100 hours. Records, modifications and paperwork The NZ AD schedule lists the 337G. Ask for proof that each AD and service letter was done. Aircraft with the Robertson STC SA1627WE conversion get reduced spar inspection thresholds and intervals, and also have a pitot tube rework requirement (Robertson Kit 14-118-100). Check wheel part numbers and manufacture dates against Cleveland SB7064 (date code 03/95 and later). NZ type acceptance covers the 337G with no special import requirements. Safety notes: • Failed flap cables have caused asymmetric flap extension and loss of control on landing; inspect cables fully at the 100-hour or annual inspection. • Cleveland SB7064: defective die-cast wheels can cause loss of directional control or brake effectiveness during taxi. • Spar cracking is the subject of a repeat inspection AD; do not buy without documented spar inspection compliance.