PILATUS PC-24 Model Guide
PILATUS PC-24 · Model Guide
Overview
PILATUS PC-24 is a Pilatus model built in Stans, Switzerland. Registry data for the PC-24 family show up to 10 passengers, up to 1950 nm range, a 45000 ft service ceiling and MTOW up to 8000 kg. The documents supplied are maintenance publications and service bulletins, so this guide focuses on what to check before buying.
- Family-level registry maxima: up to 10 passengers, up to 1950 nm, service ceiling up to 45000 ft, MTOW up to 8000 kg.
- Check the aircraft's MSN against each service bulletin's effectivity range; several apply only to early serial numbers.
- Honeywell APEX DFZ Build 6.0 software (SB 42-026) is mandatory for MSN 101 thru 600; verify it has been loaded.
- Ask for logbook proof of SB 28-002 (fuel pipe clamps) and SB 30-007 (windshield heating relay) on affected MSNs.
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 ·
- 47 KB
- Copy found at ·
- sprinkle.com
Specifications & performance
Extracted from this document.
Performance
- Family max range (nm) ·
- 1,950
- Family max service ceiling (ft) ·
- 45,000
How many passengers can the PILATUS PC-24 carry?
Registry data for the PILATUS PC-24 family show up to 10 passengers. This is a family-level maximum, not a figure for a specific cabin configuration. Check the individual aircraft's documents.
What is the PILATUS PC-24's range and ceiling?
Family-level registry maxima for the PILATUS PC-24 are up to 1950 nm of range and a 45000 ft service ceiling. The supplied documents give no variant-specific performance figures.
Which software update should a PILATUS PC-24 have?
SB 42-026 loads Honeywell Primus APEX DFZ Build 6.0 on PILATUS PC-24 aircraft MSN 101 thru 600. It is mandatory within 13 months of the Nov 03/25 issue. It covers auto flight, communications, indicating and navigation systems.
Do early PILATUS PC-24 aircraft have known fuel system issues?
SB 28-002 covers PILATUS PC-24 MSN 101 thru 150. It replaces saddle clamps and O-rings on the motive-flow fuel pipes to prevent possible leaks. Confirm it is recorded in the logbook.
What is the PILATUS PC-24 Model Guide?
The PILATUS PC-24 Model Guide is a model guide for the PILATUS PC-24, dated 2026.
What year was the PILATUS PC-24 Model Guide published?
The PILATUS PC-24 Model Guide — the PILATUS PC-24 model guide on file — is dated 2026.
Common. More common than 92% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the PILATUS PC-24.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
PILATUS PC-24 for sale now
Free — save the PC-24 to your watchlist and track it in one place.
More PILATUS PC-24manuals & documents
- PC-24 - Service Bulletin - SB 42-026 - Revision 1Service Bulletins
- PC-24 - Service Bulletin - SB 30-007 - Initial IssueService Bulletins
- PC-24 Master Maintenance and Operating Procedures (MMOP)Maintenance Manual
- PC-24 Service Bulletin 25-005Service Bulletins
- PC-24 Service Bulletin Number 28-002Service Bulletins
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In this document
Service bulletins to verify
SB 42-026 (APEX DFZ Build 6.0): MSN 101 thru 600, mandatory within 13 months of the Nov 03/25 issue, 3.75 man-hours. SB 30-007 (LH windshield heating relay): MSN 101-337 with SB 30-004 or 30-006 embodied, and MSN 501-590, within 24 months of May 22/25.
Early-production items (MSN 101-150)
SB 28-002 applies to MSN 101 thru 150: flexible saddle clamps on the motive-flow fuel pipes are replaced with fixed clamps, and four O-rings replaced, because pipe movement could damage O-rings and cause a fuel leak. It was mandatory within 3 months of May 2019 and takes 7.00 man-hours. SB 25-005 (MSN 121-150) replaces the emergency exit upper panel grommets.
Maintenance documentation
The Master Maintenance and Operating Procedures (MMOP), Issue 004 Revision 01 of February 02, 2021, lists tasks by ATA chapter, including air conditioning, auto flight, fuel, landing gear, oxygen and pneumatic systems. Ask for the current revision and the aircraft's compliance records.
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
- SB 28-002: fuel pipe movement can damage O-rings, and a fuel leak is possible on MSN 101-150 if the modification is not done.
- SB 30-007: reverse current in the LH solid state relay can trip the RCCB and make emergency windshield heating ineffective.
- SB 25-005: the original grommets become rigid at low temperatures and make it difficult to remove the emergency exit upper panel.
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
PILATUS PC-24 Model Guide PILATUS PC-24 is a Pilatus model built in Stans, Switzerland. Registry data for the PC-24 family show up to 10 passengers, up to 1950 nm range, a 45000 ft service ceiling and MTOW up to 8000 kg. The documents supplied are maintenance publications and service bulletins, so this guide focuses on what to check before buying. • Family-level registry maxima: up to 10 passengers, up to 1950 nm, service ceiling up to 45000 ft, MTOW up to 8000 kg. • Check the aircraft's MSN against each service bulletin's effectivity range; several apply only to early serial numbers. • Honeywell APEX DFZ Build 6.0 software (SB 42-026) is mandatory for MSN 101 thru 600; verify it has been loaded. • Ask for logbook proof of SB 28-002 (fuel pipe clamps) and SB 30-007 (windshield heating relay) on affected MSNs. Service bulletins to verify SB 42-026 (APEX DFZ Build 6.0): MSN 101 thru 600, mandatory within 13 months of the Nov 03/25 issue, 3.75 man-hours. SB 30-007 (LH windshield heating relay): MSN 101-337 with SB 30-004 or 30-006 embodied, and MSN 501-590, within 24 months of May 22/25. Early-production items (MSN 101-150) SB 28-002 applies to MSN 101 thru 150: flexible saddle clamps on the motive-flow fuel pipes are replaced with fixed clamps, and four O-rings replaced, because pipe movement could damage O-rings and cause a fuel leak. It was mandatory within 3 months of May 2019 and takes 7.00 man-hours. SB 25-005 (MSN 121-150) replaces the emergency exit upper panel grommets. Maintenance documentation The Master Maintenance and Operating Procedures (MMOP), Issue 004 Revision 01 of February 02, 2021, lists tasks by ATA chapter, including air conditioning, auto flight, fuel, landing gear, oxygen and pneumatic systems. Ask for the current revision and the aircraft's compliance records. Safety notes: • SB 28-002: fuel pipe movement can damage O-rings, and a fuel leak is possible on MSN 101-150 if the modification is not done. • SB 30-007: reverse current in the LH solid state relay can trip the RCCB and make emergency windshield heating ineffective. • SB 25-005: the original grommets become rigid at low temperatures and make it difficult to remove the emergency exit upper panel.