Citation 500/501 and Sierra Eagle Inspections

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	Powerplants (both)	300 hrs / 24 mo.
Phase 4 A/F	Airframe Only	300 hrs / 24 mo.
Phase 5	Complete Inspection & 1200 hr. — w/o Phase 49	1200 hrs / 36 mo.
Phase 1 thru 5 — w/o Phase 49
Phase 6	Airframe Exterior Check	14 days
Phase 7	Drag Chute	90 days
Phase 10 - NiCAD	Battery Deep Cycle	100 hrs
Phase 11	Stick Shaker (Netherlands)	200 hrs
Phase 12	ACM & Spar	600 hrs
Phase 13	Nicad S/B Gyro Battery	100 hrs / 3 mo.
Phase 14	Lead Acid S/B Gyro	3 - 6 mo.
Phase 15	Empennage Structure: Crack Inspection — Tail	10K hrs, 15K hrs, then ea 1K
Phase 16	Cabin Door and Engine Mount Structure	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, FAR 91.411A/S	Every 2 years
Phase 20	Phs. 20 above, with RVSM	Every 2 years
Phase 21	CVR & Locator Beacon	Every 2 years
RVSM Yearly Inspection		Every year
Phase 23	Elevator Rate Limiter Autopilot Test	Every 5 years
Phase 24	Pressure Bulkheads & Spar C/T	10K hrs, then ea. 3K hrs
Hot Section Inspect	Pratt & Whitney	per P&W Manual
Phase 34	Portable Fire Extinguishers	every 6 mo.
Phase 37	Windows, Doors, Wing & Horizontal Stabilizer	5000 hrs
Phase 39	Camera Pod & Navigation Sight Structure	4500 hrs, then ea. Phase 5
Phase 41	Horizontal X-Ray	3,700 hrs, then ea. 1,200 hrs
Phase 48	Cockpit & Cabin Halon FE Inspection	Every 72 mo.
Phase 49	Skin Seam & Windshield / Window Inspection	1200 hrs / 36 mo.
Phase 51	Foam Voids, SL500-28-10 (Block reinstall extra)	First 10,000 hrs/10 yr, then ea. 5 yr.
Phase 52	Fwd & Aft Pressure Bulkhead	First 5000 hrs, then ea. 2000 hrs.
Phase 53	Emer. Locator Transmitter	Every 12 mos.
Phase 54	Battery Deep Cycle, Lead-Acid	100 hrs
Phase 55	Thrust Reverser Pivot Point lube	600 hrs
Phase 56	Vapor cycle system hour meter	300 hrs
Phase 57	Corrosion Inspection	6 months
Phase 58	Vapor Cycle Cooling 500 Compressor Hour (Except Compressor Motors 113404-1, -5 or FWA1134104-1, -5)	500 A/C compressor hours
Phase 59	Front Carry-Thru to Wing Spar Lugs	10,000 hours, then ea. 1200 hrs
Phase MA	Nose LG Fork -1, -3	12,000 Lndgs, then ea. 1000
Phase MD	MLG Side Brace	Every 5000 landings
Phase MF	BF Goodrich Brake Inspection - no TRs	1st 224 lndgs, then ea. 200 lndgs, remove at 749 lndgs
Phase MG	BF Goodrich Brake Inspection - w/ TRs	1st 425 lndgs, remove at 749 lndgs
Phase MH	Vapor cycle system hour meter (Compressor Motors 113404-1, -5 or FWA1134104-1, -5)	Every 300 hrs
Sierra Eagle 2,500 Hour Inspection		Every 2,500 hrs
Engine Change
Certificate of Airworthiness
Prepurchase Evaluation
Aircraft Re-weigh