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Cessna Citation Longitude Model Guide

Cessna Citation Longitude · Model Guide

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Overview

The Cessna Citation Longitude is a twin-jet, super-midsize business aircraft first built in 2019, seating 8 to 12. It has two Honeywell HTF7700L engines and a 45,000 ft certified ceiling. The manufacturer quotes a range of 3,500 nm on a four-passenger mission at Mach 0.80 with NBAA IFR reserves.

  • Max takeoff weight is 39,500 lb. Full fuel (14,500 lb) leaves only 1,600 lb of payload; max payload is 2,400 lb.
  • Typical cruise is 448-483 ktas at FL 350-450. Takeoff distance is 4,810 ft at sea level, ISA, MTOW.
  • Brochures disagree: thrust 7,665 vs 7,600 lb, takeoff 4,810 vs 4,900 ft. The 7,600 lb / 4,900 ft sheet says its data is preliminary.
  • The walk-in baggage compartment is reachable in flight. Specs list 1,115 lb; one sheet says 1,000 lb of storage.

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.

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Document details

Type
·
Model Guide
Year
·
2026
File size
·
48 KB
Copy found at
·
sprinkle.com

Specifications & performance

Extracted from this document.

Specifications

Cabin width (in)
·
77
Cabin height (in)
·
72
Baggage capacity (lb)
·
1,115
Certified ceiling (ft)
·
45,000
Max passengers seats
·
12
Thrust per engine (lb)
·
7,665
Usable fuel capacity (lb)
·
14,500

Performance

Range (nm)
·
3,500
Landing distance (ft)
·
3,170
Takeoff distance (ft)
·
4,810
Max cruise speed (kt)
·
483
Rate of climb one engine (fpm)
·
1,330
Rate of climb two engines (fpm)
·
4,310
Service ceiling one engine (ft)
·
28,420

V-speeds

VLE_KTS
·
230
VLO_KTS
·
230
VMO_KTS
·
325
VFE_FLAPS_1_KTS
·
250
VFE_FLAPS_2_KTS
·
230
VMCA_FLAPS_1_KTS
·
100
VMCA_FLAPS_2_KTS
·
96
VFE_FULL_FLAPS_KTS
·
180

Weight & balance

Max payload (lb)
·
2,400
Max ramp weight (lb)
·
39,700
Max landing weight (lb)
·
33,500
Max takeoff weight (lb)
·
39,500
Max zero fuel weight (lb)
·
26,000
Usable fuel capacity (lb)
·
14,500
Basic operating weight (lb)
·
23,600
Payload with full fuel (lb)
·
1,600
About this document
How many people can the Cessna Citation Longitude carry?

The Cessna Citation Longitude seats up to 12 passengers per the specifications. Library data lists 8 to 12 seats depending on layout. Max payload is 2,400 lb, and only 1,600 lb with full fuel.

What range does the Cessna Citation Longitude have?

The Cessna Citation Longitude is quoted at 3,500 nm. That is for a four-passenger mission at Mach 0.80 with NBAA IFR reserves and zero wind. One sheet states its data is preliminary.

What engines does the Cessna Citation Longitude use?

The Cessna Citation Longitude has two Honeywell HTF7700L engines. The Flight Planning Guide gives 7,665 lb thrust each; an older sheet says 7,600 lb. Overhaul interval is on condition.

What is the Cessna Citation Longitude Model Guide?

The Cessna Citation Longitude Model Guide is a model guide for the Cessna Citation Longitude, dated 2026.

What year was the Cessna Citation Longitude Model Guide published?

The Cessna Citation Longitude Model Guide — the Cessna Citation Longitude model guide on file — is dated 2026.

Documentation completeness
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More Cessna Citation Longitudemanuals & documents

In this document

Cabin and capacity

Cabin is 72 in high, 77 in wide and 25 ft 2 in long, with 755 ft3 of passenger volume and up to 12 seats. Literature describes double-club seating, lay-flat seats and a forward wet galley. Cabin altitude at the 45,000 ft ceiling is 5,950 ft. Baggage volume is 112 ft3.

Performance

Landing distance is 3,170 ft at sea level, ISA, max landing weight. Rate of climb is 4,310 ft/min on two engines and 1,330 ft/min on one. One-engine service ceiling at MTOW is 28,420 ft. Quoted max cruise is 483 ktas, or 476 ktas on an older preliminary sheet.

Avionics and systems

Garmin G5000 avionics with touch-screen control, autothrottles and three 14-inch displays are standard; head-up display and enhanced vision are listed as optional. LinxUs diagnostics, brake-by-wire, fly-by-wire rudders and spoilers, and two independent hydraulic systems are described. Engine overhaul interval is on condition.

Safety notes

  • The Flight Planning Guide does not replace the FAA-approved Aircraft Flight Manual or Electronic Operating Manual. Verify all figures there.
  • MMO is M 0.84 at and above 29,375 ft. VMO is 325 KIAS from 8,000 to 29,375 ft. Gear VLE and VLO are 230 KIAS.
  • One-engine service ceiling at MTOW is 28,420 ft. Check engine-out planning for terrain along your routes.

Full document text

Cessna Citation Longitude Model Guide The Cessna Citation Longitude is a twin-jet, super-midsize business aircraft first built in 2019, seating 8 to 12. It has two Honeywell HTF7700L engines and a 45,000 ft certified ceiling. The manufacturer quotes a range of 3,500 nm on a four-passenger mission at Mach 0.80 with NBAA IFR reserves. • Max takeoff weight is 39,500 lb. Full fuel (14,500 lb) leaves only 1,600 lb of payload; max payload is 2,400 lb. • Typical cruise is 448-483 ktas at FL 350-450. Takeoff distance is 4,810 ft at sea level, ISA, MTOW. • Brochures disagree: thrust 7,665 vs 7,600 lb, takeoff 4,810 vs 4,900 ft. The 7,600 lb / 4,900 ft sheet says its data is preliminary. • The walk-in baggage compartment is reachable in flight. Specs list 1,115 lb; one sheet says 1,000 lb of storage. Cabin and capacity Cabin is 72 in high, 77 in wide and 25 ft 2 in long, with 755 ft3 of passenger volume and up to 12 seats. Literature describes double-club seating, lay-flat seats and a forward wet galley. Cabin altitude at the 45,000 ft ceiling is 5,950 ft. Baggage volume is 112 ft3. Performance Landing distance is 3,170 ft at sea level, ISA, max landing weight. Rate of climb is 4,310 ft/min on two engines and 1,330 ft/min on one. One-engine service ceiling at MTOW is 28,420 ft. Quoted max cruise is 483 ktas, or 476 ktas on an older preliminary sheet. Avionics and systems Garmin G5000 avionics with touch-screen control, autothrottles and three 14-inch displays are standard; head-up display and enhanced vision are listed as optional. LinxUs diagnostics, brake-by-wire, fly-by-wire rudders and spoilers, and two independent hydraulic systems are described. Engine overhaul interval is on condition. Safety notes: • The Flight Planning Guide does not replace the FAA-approved Aircraft Flight Manual or Electronic Operating Manual. Verify all figures there. • MMO is M 0.84 at and above 29,375 ft. VMO is 325 KIAS from 8,000 to 29,375 ft. Gear VLE and VLO are 230 KIAS. • One-engine service ceiling at MTOW is 28,420 ft. Check engine-out planning for terrain along your routes.

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