PILATUS PC-12/47 Model Guide
PILATUS PC-12/47 · Model Guide
Overview
PILATUS PC-12/47 is a turboprop in the Pilatus PC-12 family (PC-12, PC-12/45, PC-12/47, PC-12/47E, PC-12/47G). No variant-specific specifications were supplied, so confirm figures against the aircraft's own handbook. This guide gives family-level maxima and the service bulletin and modification points in the supplied documents.
- Family-level maxima, not this variant: up to 2260 nm range, 232 kt cruise, 4400 kg MTOW, 10 passengers, 35000 ft ceiling.
- SB 55-004 (stabilizer rear bolts) is mandatory. Bolts replaced since July 24, 2018 on a PC-12/47 may be affected.
- SB 32-029 covers nose landing gear corrosion. Due within 660 flying hours or 13 months of the Rev 1 release.
- Check the logbooks for any Hartzell five-blade propeller (STC SA03466CH) and any brake conversion kit.
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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 ·
- 48 KB
- Copy found at ·
- sprinkle.com
What are the headline figures for the PILATUS PC-12/47?
The supplied data has no variant-specific figures for the PILATUS PC-12/47. The PC-12 family reaches up to 2260 nm range, 232 kt cruise, 4400 kg MTOW, 10 passengers and 35000 ft ceiling.
Which service bulletins matter for a PILATUS PC-12/47?
For a PILATUS PC-12/47, check compliance with SB 55-004 (horizontal stabilizer rear attachment bolts) and SB 32-029 (nose landing gear fork and cylinder pipe corrosion). Both name PC-12/47 series aircraft in their effectivity.
Does a PILATUS PC-12/47 need special propeller care?
A PILATUS PC-12/47 with the Hartzell five-blade composite propeller (STC SA03466CH) needs care with de-ice testing. Heating the boots for more than 10 seconds can severely damage the composite blades.
What is the PILATUS PC-12/47 Model Guide?
The PILATUS PC-12/47 Model Guide is a model guide for the PILATUS PC-12/47, dated 2026.
What year was the PILATUS PC-12/47 Model Guide published?
The PILATUS PC-12/47 Model Guide — the PILATUS PC-12/47 model guide on file — is dated 2026.
Common. More common than 99% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the PILATUS PC-12/47.
- 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
Service bulletins to verify
SB 55-004 requires a check of the horizontal stabilizer rear attachment bolts at the 12 Months Inspection. Bolts with incorrect heat treatment are replaced (1.5 man-hours). SB 32-029 Rev 1 requires inspection of the nose-wheel fork assembly for corrosion on the cylinder pipe. Repair takes 5.0 man-hours and replacement 7.0. Ask for logbook entries showing both were done.
Propeller and brake modifications
Hartzell HC-E5A-3A/NC10245B five-blade composite propellers are approved on the PC-12 under STC SA03466CH. They have their own de-ice and lightning-strike inspection requirements. An Aircraft Wheel and Brake conversion kit (part 199-241) lists PC-12/47 among its series. Confirm which wheel and brake and propeller are fitted and that the paperwork matches.
Avionics and electrical options
The Mid-Continent and True Blue Power catalog lists TA202 Series high power USB chargers as standard equipment for the Pilatus PC-12. It also lists STC-approved TB40 and TB44 lithium-ion batteries, a TS835 emergency battery power supply, an MD302 SAM standby attitude module and an MD23 digital ACU. Check which are installed.
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Safety notes
- With the Hartzell composite propeller, never heat the de-ice boots for more than 10 seconds on the ground. Wait 2 minutes between tests.
- SB 55-004: bolts without correct heat treatment have reduced material properties and could fail from fatigue.
- SB 32-029: exposed raw material and corrosion on the nose gear cylinder pipe are visible without disassembling the gear.
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-12/47 Model Guide PILATUS PC-12/47 is a turboprop in the Pilatus PC-12 family (PC-12, PC-12/45, PC-12/47, PC-12/47E, PC-12/47G). No variant-specific specifications were supplied, so confirm figures against the aircraft's own handbook. This guide gives family-level maxima and the service bulletin and modification points in the supplied documents. • Family-level maxima, not this variant: up to 2260 nm range, 232 kt cruise, 4400 kg MTOW, 10 passengers, 35000 ft ceiling. • SB 55-004 (stabilizer rear bolts) is mandatory. Bolts replaced since July 24, 2018 on a PC-12/47 may be affected. • SB 32-029 covers nose landing gear corrosion. Due within 660 flying hours or 13 months of the Rev 1 release. • Check the logbooks for any Hartzell five-blade propeller (STC SA03466CH) and any brake conversion kit. Service bulletins to verify SB 55-004 requires a check of the horizontal stabilizer rear attachment bolts at the 12 Months Inspection. Bolts with incorrect heat treatment are replaced (1.5 man-hours). SB 32-029 Rev 1 requires inspection of the nose-wheel fork assembly for corrosion on the cylinder pipe. Repair takes 5.0 man-hours and replacement 7.0. Ask for logbook entries showing both were done. Propeller and brake modifications Hartzell HC-E5A-3A/NC10245B five-blade composite propellers are approved on the PC-12 under STC SA03466CH. They have their own de-ice and lightning-strike inspection requirements. An Aircraft Wheel and Brake conversion kit (part 199-241) lists PC-12/47 among its series. Confirm which wheel and brake and propeller are fitted and that the paperwork matches. Avionics and electrical options The Mid-Continent and True Blue Power catalog lists TA202 Series high power USB chargers as standard equipment for the Pilatus PC-12. It also lists STC-approved TB40 and TB44 lithium-ion batteries, a TS835 emergency battery power supply, an MD302 SAM standby attitude module and an MD23 digital ACU. Check which are installed. Safety notes: • With the Hartzell composite propeller, never heat the de-ice boots for more than 10 seconds on the ground. Wait 2 minutes between tests. • SB 55-004: bolts without correct heat treatment have reduced material properties and could fail from fatigue. • SB 32-029: exposed raw material and corrosion on the nose gear cylinder pipe are visible without disassembling the gear.