Approved Oxygen Systems
Cirrus SR22T G7 · Weight & Balance
Overview
This document provides critical information regarding the weight and balance of the Cirrus SR22T, particularly when equipped with an oxygen system. It outlines the responsibilities of the pilot to ensure that the aircraft's weight and balance are within limits before flight. The document includes specific weight and moment data for the oxygen system and details on deicing fluid capacity and weight. It serves as a supplement to the Pilot's Operating Handbook (POH) and is essential for safe flight operations involving the oxygen system.
- Total weight of the oxygen system is 6.4 lb.
- Empty weight of the aircraft is 17.4 lb; full weight is 23.8 lb.
- Deicing fluid tank capacity is 8.5 gallons (32 liters).
- Deicing fluid weight is 9.2 lb per gallon.
- Pilot must verify weight and balance with oxygen system installed before flight.
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 takeflightsandiego.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight & Balance
- Year ·
- 2013
- Pages ·
- 2
- File size ·
- 820 KB
- Copy found at ·
- takeflightsandiego.com
Specifications & performance
Extracted from this document.
Specifications
- Empty weight (lb) ·
- 17.4
- Fuel capacity (gal) ·
- 8.5
What is the Approved Oxygen Systems?
The Approved Oxygen Systems is a weight & balance for the Cirrus SR22T G7, dated 2013.
How many pages is the Approved Oxygen Systems?
The copy of the Approved Oxygen Systems on file runs 2 pages.
What year was the Approved Oxygen Systems published?
The Approved Oxygen Systems — the Cirrus SR22T G7 weight & balance on file — is dated 2013.
Common. More common than 99% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cirrus SR22T G7.
- 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
Weight & Balance Information
The document specifies the weight, arm, and moment for the oxygen system when fully charged (1800 psig). The total weight of the oxygen system is 6.4 lb. Table 4 provides detailed weight and balance information, including the empty and full weights of the aircraft.
Oxygen System Installation
It is the pilot's responsibility to verify that the weight and balance of the aircraft are within limits with the oxygen system installed prior to flight. The installation does not affect the performance characteristics of the airplane.
Deicing Fluid Capacity
The document provides information on deicing fluid, stating that the total fluid tank capacity is 8.5 gallons (32 liters) and the weight of the deicing fluid is 9.2 pounds per gallon. This information is crucial for completing the loading form in the weight and balance section of the POH.
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
- Pilot's responsibility to ensure weight and balance are within limits with the oxygen system installed.
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
Cirrus Design SR22 SR22T Approved Oxygen Systems Precise Flight, lnc. Fixed Oxyoen System Section 9 Supplements Duration Chart Notes: o Bottle Capacity has been reduced 5% forsafety . The installation of this equipment does not affect or change the performance ':J characteristics of the airplane, which are detailed in Section 5 oithe primary portion of the Prlot's Operating Handbook. No change from basic Handbook. Section 6 - Weight & Balance lf the aircraft is equipped with and the Oxygen System is installed, it is the -_, Pilot's responsibility to verify the weight and balance of the aircraft is within limits with the System installed prior to flight. The weight, arm, and moment for fully charged systems (1800psig),are provided in Table 4. The total weight of oxygen in the system is 6.41b and the actual weight and moment can be determined by oxygen pressure per Figure 24. Tahla 4 - Waiohf and Balanee lnformafion Table 4 - Weight and Balance Information Weioht - lb Arm Momenul000 Empty 17.4 262.3 4565.7 Full 23.8 265.3 6316.4 Section 7 - System Description The general operating procedures for use of the Fixed Oxygen System discussed in the Section 1 - General System Overview of this Supplement. IS '--,--l FAA Approval Date: Document No.: 102NMAN000'l Rev.: Page 45 of 49 Section I Supplements Cirrus Design SR22T Section 6 - Weight & Balance Flefer to Section 6 - Weight and Balance pf the basic POH for current weight and balance data. Use the following table to determine the MomenU1000 for deicing fluid to complete the Loading Form in the Weight and Balance Section of the basic POH. . Total fluid tank capacity is 8.5 gallon (32L). . Deicing fluid weight is 9.2 pounhs per gallon. P/N 13772-151 Original lssue: 02-01-13 Gailon$ Weishr :: LB ilnll'rI : ioooe ,::: f46ft (FS148.0 G[allifis \treight : LB. llofirI l0ooe fdnk (F$148.0) Gallona' Wdght ..tB :, ilom/ 10000 : fhnk tFsr48.0) U.I u.y u,t 4 J.3 JU"tl 4.49 o,5 !v.o o,oo o.2 t.8 o.27 3.4 31.3 4,63 6.6 60.7 8,99 0.3 2.8 0.41 3.5 32.2 4.77 . 6.7 61"6 9.12 0.4 3.7 0.54 3.6 33.1 4,90 6.8 62.6 9.26 0.5 4.6 0.68 3.7 34.0 5.04 6.9 63,5 9.40 0.6 5.5 0.82 3.S 35.0 5.17 7.0 64.4 s.53 a,t 6.4 0.ss 3.9 3s.9 5.31 65.3 9.67 0.8 7.4 1.09 4.0 36.8 5.45 7.2 66.2 9.AO o.9 4.3 1.23 4.r ot.l 5,5U t,5 67.2 9.94 .o 9.2 LJO 4.2 36,6 5.72 7.4 ou. r 'r o.o8 tu.t I ,TU 4.3 39.6 5.85 7,5 69.0 "t 0.2'l ,2 1.0 1.63 4.4 40.5 5.99 7.6 05.v r 0.35 .t 12.O 4.5 41,4 o. r5 70.E 10,46 + I2.9 '1.91 4.6 42.3 tr.ztt 7,8 1.8 'r 0.62 .5 I3.E z,o4 4.f 44,2 tt.40 /,u I t.t 10^76 ,6 '14,7 z. ru 4,8 4{.2 It,54 o.o 73.6" 1o.89 I5.6 2,31 4,9 45.1 6.67 E,.' 74,5 't.03 .E I6.6 2.45 5.O 46.O* 6.EI E.Z 75.4 I,Y I7.5 8.59 5.I ,*o,v 6.94 9.3 76.4 1.30 2.Q IE,4 t.t z 5.2 47.4 t.u6 8.4 77.3 1.44 2.1 19.3 2.86 5.3 48.8 7.22 8.5 78.2 1.57 2.2 2A.2 5.00 5.4 49.7 7.35 *Minimum Dispatch Fluid 0ty 2.3 21.2 3.13 5.5 50.6 7.49 **Usable Tank Capacity a,.t ?2.1 a,2f 5.{i 51.5 7.62 4,' z3^o 3.40 5,t 52.4 7.76 2.4 23.9 3,54 5.4 53,4 7.90 4.t 24.8 3.68 5.9 54.3 8.03 ?.4 25.6 3.E1 6.O 85.2 E.I7 t.v 26.7 rt.vt 6.I ao. r 8.01 3.0 27.6 4.08 6.2 57.O 8,44 3.I zE.5 4.22 6,t 56.0 E.5E 3.2 29.4 4.36 6,4 0u.Y 4.7't 40 ol 52