CESSNA 501 Citation 1SP G600 Model Guide
CESSNA 501 Citation 1SP G600 · Model Guide
Overview
CESSNA 501 Citation 1SP G600 is a Cessna jet from the 501 family, which the registry lists as turbofan-powered. Registry data for the whole 501 family shows up to 8 passengers, up to 1320 nm range, up to 41000 ft service ceiling and up to 6000 kg MTOW. These are family maxima, not confirmed figures for this variant. The G600 is a Garmin display system fitted under an STC.
- 501 family data: up to 8 passengers, up to 1320 nm, up to 41000 ft, up to 6000 kg MTOW. These are not variant-specific figures.
- The NZ CAA 501 schedule lists spar cap, brake stator disk and fire extinguisher wiring directives. Check each one in the records.
- The G600 is a Garmin GDU 620 based system installed under an STC. Ask for the installation and calibration records.
- SACAA's 2025 type rating list has a C501/551 entry marked SP HPA. Check what rating your pilots need.
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 does registry data say about the CESSNA 501 Citation 1SP G600's capacity and range?
The CESSNA 501 Citation 1SP G600 has no variant figures in the inputs. The 501 family shows up to 8 passengers, up to 1320 nm range and up to 41000 ft ceiling. Verify the actual figures against the aircraft's flight manual.
What is the G600 on the CESSNA 501 Citation 1SP G600?
On the CESSNA 501 Citation 1SP G600, the G600 is the Garmin display system whose installation manual is in the sources. It uses the GDU 620 display, and the installation must match STC requirements. Ask for the calibration and survey records.
Which inspections matter most when buying a CESSNA 501 Citation 1SP G600?
For a CESSNA 501 Citation 1SP G600, check the spar cap crack inspections, the brake stator disk markings and the fire extinguisher wiring directive. Also confirm all FAA directives have been complied with.
What is the CESSNA 501 Citation 1SP G600 Model Guide?
The CESSNA 501 Citation 1SP G600 Model Guide is a model guide for the CESSNA 501 Citation 1SP G600, dated 2026.
What year was the CESSNA 501 Citation 1SP G600 Model Guide published?
The CESSNA 501 Citation 1SP G600 Model Guide — the CESSNA 501 Citation 1SP G600 model guide on file — is dated 2026.
Common. More common than 85% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 501 Citation 1SP G600.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Airworthiness directives to verify
Spar caps (S/N 0350 through 0520, unless modified): inspect for cracks at wing station 37.0, with repeat intervals of 600 hours. Brakes (S/N 0001 through 0689 with BFGoodrich P/N 2-1528-6 or 2-1530-4): stator disks should be stamped CHG AI or CHG B or higher. Fire extinguisher wiring: Cessna SB500-26-02 identification sleeves.
G600 avionics
The G600 AML STC Installation Manual (Garmin, Rev. B, November 2008) covers the GDU 620 display and its GRS 77, GMU 44, GDC 74A and GTP 59 units. It requires a GPS navigator and standby instruments. A magnetic interference survey is needed after the GMU 44 is mounted. Stormscope and external TAWS functions are noted as not currently supported.
Records and regulatory context
The NZ CAA schedule applies to Cessna model 501 aircraft built under FAA Type Certificate A27CE. It was issued 24 September 2015 and is not maintained, because no NZ-registered aircraft exist. Applicable ADs are those published by the FAA. The schedule also lists FAA ADs on fuel tank vapour, severe icing, thrust reverser and dual flight director, plus an air conditioning motor inspection.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- A spar cap crack of .3 inches or longer requires repair or modification of the wing before further flight.
- Cracked or broken brake stator disks require brake assembly replacement before further flight, to avoid loss of directional control or braking.
- Incorrect fire extinguisher wiring could leave an engine or APU fire unextinguished. Confirm SB500-26-02 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 501 Citation 1SP G600 Model Guide CESSNA 501 Citation 1SP G600 is a Cessna jet from the 501 family, which the registry lists as turbofan-powered. Registry data for the whole 501 family shows up to 8 passengers, up to 1320 nm range, up to 41000 ft service ceiling and up to 6000 kg MTOW. These are family maxima, not confirmed figures for this variant. The G600 is a Garmin display system fitted under an STC. • 501 family data: up to 8 passengers, up to 1320 nm, up to 41000 ft, up to 6000 kg MTOW. These are not variant-specific figures. • The NZ CAA 501 schedule lists spar cap, brake stator disk and fire extinguisher wiring directives. Check each one in the records. • The G600 is a Garmin GDU 620 based system installed under an STC. Ask for the installation and calibration records. • SACAA's 2025 type rating list has a C501/551 entry marked SP HPA. Check what rating your pilots need. Airworthiness directives to verify Spar caps (S/N 0350 through 0520, unless modified): inspect for cracks at wing station 37.0, with repeat intervals of 600 hours. Brakes (S/N 0001 through 0689 with BFGoodrich P/N 2-1528-6 or 2-1530-4): stator disks should be stamped CHG AI or CHG B or higher. Fire extinguisher wiring: Cessna SB500-26-02 identification sleeves. G600 avionics The G600 AML STC Installation Manual (Garmin, Rev. B, November 2008) covers the GDU 620 display and its GRS 77, GMU 44, GDC 74A and GTP 59 units. It requires a GPS navigator and standby instruments. A magnetic interference survey is needed after the GMU 44 is mounted. Stormscope and external TAWS functions are noted as not currently supported. Records and regulatory context The NZ CAA schedule applies to Cessna model 501 aircraft built under FAA Type Certificate A27CE. It was issued 24 September 2015 and is not maintained, because no NZ-registered aircraft exist. Applicable ADs are those published by the FAA. The schedule also lists FAA ADs on fuel tank vapour, severe icing, thrust reverser and dual flight director, plus an air conditioning motor inspection. Safety notes: • A spar cap crack of .3 inches or longer requires repair or modification of the wing before further flight. • Cracked or broken brake stator disks require brake assembly replacement before further flight, to avoid loss of directional control or braking. • Incorrect fire extinguisher wiring could leave an engine or APU fire unextinguished. Confirm SB500-26-02 compliance.