PILATUS PC-9A Model Guide
PILATUS PC-9A · Model Guide
Overview
PILATUS PC-9A is a Pilatus turboprop aircraft, part of the PC-9 family. The registry data gives no performance, weight or seating figures for it. The two documents supplied are a PC-9 service bulletin on the rear fuselage Frame 11 (FR11) fittings and the PC-9 maintenance manual time-limits chapter. A buyer's checks should centre on structural records and the inspection schedule.
- PILATUS PC-9A is a turboprop; the supplied data has no range, speed, weight or seat-count figures.
- Service Bulletin 53-022 covers replacing the FR11 fittings, which can crack from stress corrosion.
- Ask for proof that SB 53-022 was done, or that the repetitive FR11 crack inspections are current.
- Never extend a scheduled inspection beyond the permitted tolerance; the maintenance manual is firm on this.
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
Does the supplied data give PILATUS PC-9A performance figures?
No. For PILATUS PC-9A the registry entry has no range, cruise speed, weight, ceiling or seat data, so none are quoted. Get these from the aircraft's flight manual and records.
What is the main structural item to check on a PILATUS PC-9A?
The FR11 fittings in the rear fuselage. SB 53-022 says the original AA2024-T351 fittings can crack from stress corrosion. Check whether the fittings were replaced or the repetitive inspections are current.
How much work is the FR11 fitting replacement on a PILATUS PC-9A?
SB 53-022 lists 19.0 man-hours: 5.0 for preparation, 7.0 for replacing the fittings and 7.0 for close-up. It needs Modification Kit 500.50.09.270, and the bulletin says weight and moment do not change.
How should inspection tolerances be treated on a PILATUS PC-9A?
The manual allows limited tolerances, subject to local regulations, but says never to extend an inspection beyond them. Example: a 100 hour inspection done at 260 hours gives next inspections at 360, 460 and 560 hours.
What is the PILATUS PC-9A Model Guide?
The PILATUS PC-9A Model Guide is a model guide for the PILATUS PC-9A, dated 2026.
What year was the PILATUS PC-9A Model Guide published?
The PILATUS PC-9A Model Guide — the PILATUS PC-9A model guide on file — is dated 2026.
Common. More common than 70% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the PILATUS PC-9A.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
PILATUS PC-9A for sale now
Free — save the PC-9 to your watchlist and track it in one place.
More PILATUS PC-9Amanuals & documents
Related documents
If you fly the PILATUS PC-9A, you may also be researching these.
In this document
Frame 11 fitting service bulletin
SB 53-022 (dated Feb 25/16) applies to MSN 101 thru 248 and 501 thru 567. A mandatory crack inspection of the left and right FR11 fittings made from AA2024-T351 can lead to replacement. The cause of the cracks is stress corrosion. Pilatus rates compliance 'Highly recommended'. Check the aircraft's MSN against these ranges.
What the fix involves
The new fittings use material more resistant to stress corrosion cracking, supplied in Modification Kit 500.50.09.270. The job takes 19.0 man-hours and includes removing the horizontal stabilizer. Weight and moment change is none. Once the fittings are replaced, the repetitive mandatory inspections are cancelled. Old fittings must not be refitted to a post-bulletin aircraft.
Maintenance manual time limits
The time limits chapter covers airworthiness limitations, overhaul limits, and scheduled and unscheduled checks. It lists life-limited and overhauled components, and the airframe is designed to the safe life concept. A wash and corrosion control program is recommended. Tropical or arctic operation may need more frequent inspections. Engine and propeller limits are in the Pratt & Whitney Canada and Hartzell documents.
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
- Both ejection seats must have safety pins installed in the safe-for-servicing locations before anyone enters the cockpit for SB 53-022 work.
- Put 'DO NOT OPERATE THE FLIGHT CONTROLS' warning signs in both cockpits during the FR11 work and follow the flight control safety precautions.
- Never extend an inspection or component life by more than the permitted tolerance.
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-9A Model Guide PILATUS PC-9A is a Pilatus turboprop aircraft, part of the PC-9 family. The registry data gives no performance, weight or seating figures for it. The two documents supplied are a PC-9 service bulletin on the rear fuselage Frame 11 (FR11) fittings and the PC-9 maintenance manual time-limits chapter. A buyer's checks should centre on structural records and the inspection schedule. • PILATUS PC-9A is a turboprop; the supplied data has no range, speed, weight or seat-count figures. • Service Bulletin 53-022 covers replacing the FR11 fittings, which can crack from stress corrosion. • Ask for proof that SB 53-022 was done, or that the repetitive FR11 crack inspections are current. • Never extend a scheduled inspection beyond the permitted tolerance; the maintenance manual is firm on this. Frame 11 fitting service bulletin SB 53-022 (dated Feb 25/16) applies to MSN 101 thru 248 and 501 thru 567. A mandatory crack inspection of the left and right FR11 fittings made from AA2024-T351 can lead to replacement. The cause of the cracks is stress corrosion. Pilatus rates compliance 'Highly recommended'. Check the aircraft's MSN against these ranges. What the fix involves The new fittings use material more resistant to stress corrosion cracking, supplied in Modification Kit 500.50.09.270. The job takes 19.0 man-hours and includes removing the horizontal stabilizer. Weight and moment change is none. Once the fittings are replaced, the repetitive mandatory inspections are cancelled. Old fittings must not be refitted to a post-bulletin aircraft. Maintenance manual time limits The time limits chapter covers airworthiness limitations, overhaul limits, and scheduled and unscheduled checks. It lists life-limited and overhauled components, and the airframe is designed to the safe life concept. A wash and corrosion control program is recommended. Tropical or arctic operation may need more frequent inspections. Engine and propeller limits are in the Pratt & Whitney Canada and Hartzell documents. Safety notes: • Both ejection seats must have safety pins installed in the safe-for-servicing locations before anyone enters the cockpit for SB 53-022 work. • Put 'DO NOT OPERATE THE FLIGHT CONTROLS' warning signs in both cockpits during the FR11 work and follow the flight control safety precautions. • Never extend an inspection or component life by more than the permitted tolerance.