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Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
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COMPONENT LUBRICANT FREQUENCY
1. ENGINE OIL SUMPS (CONTINENTAL) CONTINENTAL SPECIFI-
PA-28RT-201T ONLY CATION MHS-24A AND
SERVICE BULLETIN M75-2 100 HRS
2. OIL FILTER 50 HRS
3. INDUCTION AIR FILTERS CLEAN AS OFTEN AS
NECESSARY, EVERYDAY
UNDER SEVERE
CONDITIONS
4. ALTERNATE AIR DOOR MIL-L-7870 100 HRS
5. PROPELLER ASSEMBLY MIL-G-23827 100 HRS
6. ENGINE CONTROL AND ENVIRONMENTAL
CONTROL PIVOT POINTS MIL-L-7870 100 HRS
7. FRESH AIR VENT SHAFTS MIL-G-7711 500 HRS
SPECIAL INSTRUCTIONS
1. Air Filter - To clean filter, tap gently to remove dirt particles. Do not blow out with compressed air or use oil; replace filter if punctured or
damaged.
2. See latest revision of TCM Service Bulletin M75-2 for recommended oil and filter change period. The engine lubricating oil system is
serviced with MIL-C-6529. Type II for the initial fill and for the first 25 hours engine time per TCM Operator’s Manual and MHS-184. Service
engine thereafter with oil per MHS-24A and latest revision of TCM Service Bulletin M75-2.
3. Ascertain that oil filter complies with specifications of latest revision of TCM Service Bulletin M75-7.
4. Propeller - Remove one of two grease fittings for each blade. Apply grease through fitting until fresh grease appears at hole of removed
fitting.
Figure 12-9. Lubrication Chart (Continental Power Plant, Propeller and Control Pivot Points)
12-20-32
Page 12-26
December 1, 1978
1E10
PIPER AIRCRAFT
PA-28RT-201 / 201T
*MAINTENANCE MANUAL

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Piper Arrow IV Turbo Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelArrow IV Turbo
Horsepower200 hp
Seating Capacity4
Landing GearRetractable tricycle
Range773 nautical miles
Service Ceiling20, 000 ft
Fuel Capacity72 gallons
Propeller2-blade constant speed
Max Takeoff Weight2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)55 knots
Rate of Climb1, 000 ft/min

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