Inspection Document | Description | Time Interval |
---|---|---|
Phase B | General Airframe & Engine | 150 hrs. |
Phase 1 | Nose, Cockpit, Interior | 300 hrs / 24 mo. |
Phase 2 | Wings, Gear, Empennage | 300 hrs / 24 mo. |
Phase 3 | Tailcone | 300 hrs / 24 mo. |
Phase 4 | Airframe and Powerplants (both) | 300 hrs / 24 mo. |
Phase 4 A/F | Airframe Only | 300 hrs / 24 mo. |
Phase 5 | Complete Inspection & 1200 hr. | 1200 hrs / 36 mo. |
Phase 1 thru 5 | Complete Inspection (w/o Phase 49) | |
Phase 6 | Corrosion | 14 days |
Phase 8 | Portable Fire Extinguisher | 6 mo. |
Phase 11 | Standby Gyro Battery Pack | 3 to 6 mo. |
Phase 12 | Cargo Door / Frame Inspection | 3600 hours |
Phase 13 | Window Structure/Horiz Stab. | 5000 hrs |
Phase 14 | Fuselage/Wing Structure | 10K, then 3000 hrs thereafter |
Phase 15 | Crack Inspection — Empennage/Tail | 10K hrs, 15K hrs, then ea 1K |
Phase 16 | Crack Inspection — Door & Pylon | 10K hrs, 15K hrs then ea 3K |
Phase 17 | Crack Inspection — Cabin Structure | 10,000 hrs |
Phase 18 | Emergency Equipment | Every Year |
Phase 20 | A/S, Alt, ADC & Static with RVSM | Every 2 years |
Phase 20 | Phase 20 w/o RVSM | Every 2 years |
RVSM Yearly Inspection | Every year | |
Phase 21 | Transponder & CVR Beacon | Every 2 years |
Phase 22 | Nitrogen Hydro | Every 3 years |
Phase 23 | Engine Fire Extinguisher Bottles Hydro | Every 5 years |
Hot Section Inspections | per P&W Manual | |
Phase 26 | TKS Strainers | 3000 hrs / 24 mo. |
Phase 27 | Battery Recondition - NiCad | 100 hrs |
Phase 30 | Hamilton Standard ACM Oil Change | 600 hrs |
Phase 31 | Flap Bell Crank Mounts | 4000 landings / 2000 landings thereafter |
Phase 32 | Aileron Drive Bracket | 15,000 landings / 7500 landings thereafter |
Phase 33 | Aileron Yokes Inspection | 15,000 landings / 10,000 landings thereafter |
Phase 39 | Camera Pod & Nav. Sight Structure | 4500 hrs, then 8100, then 450 thereafter |
Phase 47 | Cockpit & Cabin Halon FE Hydro | Every 12 years |
Phase 48 | Cockpit & Cabin Halon FE Inspection | Every 72 mo. |
Phase 49 | Skin Joint & Doubler Inspection | 1200 hrs / 36 mo. |
Phase 51 | O2 Cyl. Hydrostatic Test | 5 years |
Phase 52 | ELT Inspection | 12 mo. |
Phase 53 | Wing L/E | 2400 hrs / 72 mo. |
Phase 54 | I/B Lower Wing Spar | 13,200 hrs, 1200 hrs thereafter |
Phase 55 | O/B Lower Wing Spar | 15,600 hrs, 1200 hrs thereafter |
Phase 56 | Wing Spar Cap inspection | 15,600 hrs, 2400 hrs thereafter |
Phase 57 | Front Carry-Thru to Wing Spar Lugs - Inspection | 10,000 hrs, 1200 hrs thereafter |
Phase 58 | Vapor Cycle Cooling Hour Meter Check | 300 hrs |
Phase 59 | Vapor Cycle Cooling 500 Compressor Maint. | 500 hrs Compressor hrs. |
Phase MA | Vapor cycle system hour meter | 300 hrs |
Phase MB | Nose Fork Inspection (5542300-2) | 10,000 landings, then ea 1,000 landings |
Engine Change | ||
Certificate of Airworthiness | ||
Prepurchase Evaluation | ||
Aircraft Re-weigh |
Citation S550 InspectionsLynnFleck2019-05-21T12:45:30-05:00