FAA APPROVED AIRPLANE FLIGHT MANUAL Cessna 350 (LC42-550FG) with Garmin Integrated Flight Display

6A-13 I 6A-14 I 6A-15 I 6A-16 I 6-A17 I 6-Al8 I Weight & Balance (Appendix B) Installed Equipment List 6B-I I 6B-2 I 6B-3 I 6B-4 I 6B-5 I 6B-6 I 6B-7 I 6B-8 I 6B-B I 6B-I0 I SECTION 7 (Description of Airplane & Systems) 7-1 7-2 7-3 7-4 7-5 7-6 7-7 7-8 7-9 7-10 RB050005 X I H H H H H H H H H Cessna 350 (LC42-550FG) LIST OF EFFECTIVE PAGES Reissue Added Pages Page Rev Page Rev 7-11 H 7-12 H 7-13 H 7-14 H 7-15 I 7-16 H 7-17 H 7-18 H 7-19 H 7-20 H 7-21 H 7-22 H 7-23 H 7-24 H 7-25 H 7-26 H 7-27 H 7-28 H 7-29 H 7-30 H 7-31 H 7-32 H 7-33 H 7-34 I 7-35 H 7-36 H 7-37 H 7-38 H 7-39 H 7-40 H 7-41 H 7-42 H 7-43 H 7-44 H Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 Cessna 350 (LC42-550FG) LIST OF EFFECTIVE PA~E Reissue Added Pa 1 Page Rev Page 7-45 H 7-46 H 7-47 H 7-48 H 7-49 H 7-50 H 7-51 H 7-52 H 7-53 I 7-54 H 7-55 H 7-56 H 7-57 H 7-58 H 7-59 H 7-60 H 7-61 H 7-62 H 7-63 H 7-64 H 7-65 H 7-66 H 7-67 I 7-68 I SECTION 8 (Handling, Servicing & Maintenance) 8-1 I 8-2 I 8-3 I 8-4 I 8-5 I 8-6 I 8-7 I Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 8-8 8-9 8-10 8-1 I 8-12 8-13 8-14 8-15 8-16 8-17 8-18 8-19 8-20 9-1 9-2 List of Effective Pages H H H H H H H H H SECTION 9 (Supplements) H H RB050005 xi List of Effective Pages Cessna 350 (LC42-550FG) This Page Intentionally Left Blank RB050005 xii Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 Cessna 350 (LC42-550FG) Narrative Discussion of Revisions NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level No. - All Initial revision. Title Page, iii, Revised to indicate Revision A. A vii through xi, Revised LOEP. xvi Revised Narrative Discussion of Revisions. A 1-2 Revised the Empty Weight in Figure 1-2. A 1-9 Changed "Limit Load" to "Limit Load Factor" and "Ultimate Load" to "Ultimate Load Factor". Revised maneuvering speed in Figure 2-1. Described airspeed markings on the PFD in the Airspeed Indicator Markings section. A 2-4 to 2-7 Deleted Maximum Manifold Pressure for Idle from the Powerplant Limitations section. Changed "on the Garmin GI 000 system" to "on the MFD" in the Powerplant Gauge Markings section. Revised Figure 2-3. Revised Figure 2-5 2-9, 2-15, 3-7, 3-9, 3-1 I, 3-13, 3- 15, 3-17, 4-9 A through Revised footer. 4-17, 6-12, 6- 14, 6-16, 6-18, 6-20, and 6A- IO Revised table of GI 000 software versions, , and changed "limit" to "minimum height" in no. 8 in the Garmin GI 000 System Limitations section. Changed ", flight director or manual electric trim" to "or flight director" and the "PFT" annunciation description for the GFC 700 in no. 6 of the Garmin GI000 System Limitations section. Added explanation of automatic switching caution to no. 2 of the Approach Operation Limitations in the Garmin GI 000 System A 2-9to2-14 Limitations section. Deleted 14 CFR Part 121 from no. 2 of the GTX33 Mode S Transponder Limitations section. Deleted no. 4 in the Garmin GFC 700 Automatic Flight Control System Limitations section. Added a Warning to verify proper operation of the oxygen system and revised the Warning against use of lipstick, chapstick, and etc. in the Oxygen Limitations section. Reoaginated pages. A 2-17 Revised maneuvering speed placard. A 2-18 Revised location of compass placard. Added panel light dimmer placard. A 3-1 to 3-3 Revised Table of Contents. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 xiii Narrative Discussion of Revisions Cessna 350 (LC42-550FG) Revision Level A A A A A A A A A A A RB050005 xiv NARRATIVE DISCUSSION OF REVISIONS Page No. 3-5 through 3- 34 4-1 to 4-3 4-6 through 4- 18 4-20 to 4-23 4-27 through 4-37 5-6 6-1 and 6-2 6-4 to 6-20 6-Al through 6-AI0 6-B I through 6-86 7-2 through 7- s Comment Revised maneuvering speed in Figure 3-1. Revised Emergency Procedure checklists. Changed "Boost" to "Fuel" in the Emergency Backup Boost Pump title and section. Changed "Boost" to "Fuel" in the Critical Issues (Backup Boost Pump) title and section. Revised the Failure of Engine Driven Fuel Pump section. Changed "Emergency Landing Without Engine Power" to "Forced Landing (Engine Out and Partial Power)"in the Engine Docs Not Restart paragraph in the Engine Failure and Forced Landings section and in the Low Oil Pressure paragraph of the Engine and Propeller Problems section. Changed "engine" to "System" in the Electrical Problems section. Revised Table of Contents. Revised the Normal Procedures checklists. Indicated ammetcr/loadmetcr is displayed on MFD System page in the Normal Starting paragraph of the Engine Starting section. Revised description of the tab in the Fuel Quantity section. Changed "auxiliary boost pumps are off' to "auxiliary fuel pump is off' in the Over Priming section. Changed "If the airplane" to "The airplane" in the first sentence of the Ground Power Operations section. Rcpaginated pages. Added Oxygen System paragraph to the Before Takeoff section. Added paragraph directing fuel pump switch be off for descent and landing and revised the SpcedBrakes paragraph in the Descent section. Added paragraph on propeller speed intermodulation and Note on flaps use to the Glidcslope Flight Procedure with Autopilot discussion under the Approach section. Changed "boost" to "fuel" in the Balked Landings section. Added Oxygen System paragraph to the Landings section. Changed "boost pumps" to "fuel pump" in the third paragraph of the Hot Weather Operations section. Revised Figure 5-5. Revised Table of Contents. Added Caution and example regarding specific weight of Aviation Gasoline. Rcpaginatcd pages. Deleted model #sand size from Items 34-35, 34-36, and 34-37. Deleted model #sand size from Items 34-35, 34-36, and 34-37. Revised Table of Contents. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: l/10-22-2008 Cessna 350 (LC42-550FG) Narrative Discussion of Revisions NARRATIVE DISCUSSION OF REVISIONS Revision Level A A A Page No. 7-10 through 7-14 7-17 to 7-19 7-23 through 7-74 Comment Changed "convenience" to "inconvenience" in the Control Lock section. Changed "Engine Indication System (EIS) page" to "various pages" in the Elevator and Aileron section. Revised the Hat Switches section. Revised Trim Position Indicator section. Deleted the last sentence from the Autopilot/Trim Master Switch (A/P Trim) section. Changed "flaps does" to "flaps switch docs" in the 6th sentence of the 2nd paragraph of the Wing Flaps section. Changed "on the left side" to "at the front" in the Front Seat Adjustment section. Revised Fi2:urc7-3. Revised Fi2:ure7-4. Revised 2nd paragraph of the Baggage Door section. Changed "clockwise" to "inboard", and deleted "90° counterclockwise or" in the Parking Brake section. Changed "IO-550-N25" to "1O-550-N" in the Engine Specification section. Added a Note about airspace penetration and Warning in event of AHRS failure to the Garmin GI000 Integrated Cockpit System section. Added MFD Map Scale, MFD Holding Pattern Depiction, and VOR Frequency Display on the MFD paragraphs. Added GCU 476 Remote Keypad. Added Figure 7-6 and renumbered following figures. Changed "Boost" to "Fuel" in the Backup Boost Pump and Vapor Suppression section title. Changed "Boost" to "Fuel" in the Primer section. Added tables to the Aircraft Alerts, Caution Alerts, Annunciation Advisory, and Message Advisory Alerts sections. Revised the Backup Attitude Indicator section. Added AFCS Alerts, TA WS Alerts, and TA WS System Status Annunciations and Other Annunciations sections. Revised description of the Kollsman Window in the Backup Altimeter section. Changed "MFD EIS page" to "MFD System page" in the 3rd paragraph of the Fuel Quantity Indication section. Revised the Alerts Window paragraph and the Alert Level Definitions paragraph in the Annunciations and Alerts section. Revised the Oxygen annunciations in the Caution Alerts section. Added OXYGEN ON to the Annunciations Advisory section. Revised Figure 7-13 and renumbered it to Figure 7-14. Revised Figure 7-14 and renumbered it to Figure 7-15. Revised the Pilot-Static System section. Revised the Fuel System section and changed "MFD EIS page" to "MFD System page" in the Fuel Selector paragraph. Revised location of the backup pump and vapor suppression switches in the Backup Fuel Pump and Vapor Suppression section. Deleted "single speed" from the Airflow and Operation paragraph of the Environmental Control System section. Revised switch operation in the Overhead Reading Lights and Instrument Flood Bar sections. Revised Upper Instruments section. Revised Lower Instruments, Circuit Breaker and Master Switches Panels section. Revised Figure 7-18 and renumbered it to Figure 7-19. Revised the Flaos Panel and 5 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 xv Narrative Discussion of Revisions Cessna 350 (LC42-550FG) Revision Level A B B B B B B B RB050005 xvi NARRATIVE DISCUSSION OF REVISIONS Page No. 8-11 Title Page, iii, vii through xi, xvi 2-6 2-9to2-12 3-19 3-31 4-19 4-30 to 4-32 Comment Pack Switches (Press-to-Test PTT) section and renamed it to Press-to-Test PTT Button. Added a Note on the GDL 69A to, and revised the Rudder Limiter Test paragraph in, the Stall Warning System section. Revised the Control Stick Switches and Headset Plug Positions section. Revised the Autopilot Disconnect/Trim Interrupt Switch section. Revised the description of condition required for ELT activation, and the location of the ELT switch in the Emergency Locator Transmitter section. Changed "EIS page" to "System page", revised the Oxygen Flow Controls paragraph, revised lipstick, chapstick, etc. use Warning, and added a Preflight Testing paragraph in the Precise Flight Fixed Oxygen System section. Changed "EIS" to "System" and revised description of Test/Reset button in the CO Guardian Carbon Monoxide Detector section. Added Reference to Garmin Cockpit Reference Guide for operating instructions in the XM Weather (WX) Data System section. Revised the Ryan Model 9900BX TCAD section. Added titles to Figure 7-24 and 7-25 and renumbered to 7-25 and 7-26. Deleted the Acknowledge/Traffic Button section. Changed "maximum performance" to "maximum ACCS performance" in the 5'h General Hint for ACCS Operation. Deleted GT A 82 Trim Adapter, revised CWS (Control Wheel Steering) Button paragraph, and added two Warning notes in the Garmin GFC 700 Automatic Flight Control System section. Added Go Around information to the GA (Go Around Button paragraph in the Additional AFCS Controls section. Rcpaginatcd pages and revised cross references. Added pages 7-69 through 7- 74. Revised Figure 8-4. Revised to indicate Revision B. Revised LOEP. Revised Narrative Discussion of Revisions. Revised Figure 2-3. Revised software versions table and No. IO under the Garmin GI 000 System Limitations section. Reformatted No. 2 under the Approach Operation Limitations section into a caution. Revised the Garmin GFC 700 Automatic Flight Control Systems Limitations section. Revised Fii?ure 2-7. Changed "backup fuel pump" to "backup fuel pump switch" in the third paragraph under the Emergency Backup Fuel Pump section. Changed ", or annunciation" to ", or annunciated" in the first note under the Oxygen System section. Changed "stall warning" to "stall warning tone" in the last sentence of the Rudder Limiter Test section. Revised Mixture Settings paragraphs under the Cruise section. Revised the Glideslope Flight Procedure with Autopilot section. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 Cessna 350 (LC42-550FG) Narrative Discussion of Revisions NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level No. B 7-5 Revised Table of Contents. B 7-24 Added "for the identified station" to the end of the last sentence in the VOR Frequency Display on the MFD section. Deleted item 2.h. "OXYGEN PRES" and deleted last row from the following table. B 7-30 Revised the description of the "Fuel Pump" message. Changed "Fuel Pump On" to "Fuel Pump" and "Fuel pump is operating" to "Backup fuel pump is operating" in the Alerts table. B 7-32 Changed "Fuel Pump On" to "Fuel Pump" and revised the description in the Audio Alert/Voice Message section. B 7-47 and 7-48 Deleted duplicate sentences in the Press-to-Test PTT Button section. Indicated engine driven or electrically driven compressor. Added section System Operation Using Ground Power describing use of ACCS to pre-cool cabin of the aircraft. This is B 7-64 to 7-74 possible only by ACCS equipped with electric compressor powered by ground power. Added "above 400 AGL" to the last sentence of the first paragraph describing GA Mode operation. Rcpaginated pages. Title Page, iii, Revised to Title Page to indicate Revision C. C Revised LOEP. vii to xi, xvi Revised Narrative Discussion of Revisions. C 2-4 Revised Figure 2-1. C 2-17 Revised Maneuvering Speed placard. Reformatted entire manual to 5.5 x 8.5. Page numbers indicated D All for Revision Level D were made prior to reformatting of the manual; refer to Rev. C manual to compare changes. Title Page, iii, Revised Title Page to indicate Revision C. D Revised LOEP. vii to xi, xvi Revised Narrative Discussion of Revisions. D 2-7 Revised the Maximum Empty Weight from 2580 lbs. to 2568 lbs. D 2-18 Revised compass placard. D 3-1 Revised Table of Contents. D 3-16 and 3-17 Added Something Stuck in or Interfering With a Doorjamb checklist. Revised Circuit Breaker Panel section. D 3-19 Revised the 4th paragraph under the Emergency Backup Fuel Pump section. D 3-27 and 3-28 Revised the Under Voltage section .. Revised the last sentence in the Master Switches section. Revised the location of the static air source switch under the D 3-30 and 3-3 I Static Air Source Blockage section. Revised the bullet list in the first paragraph of the Oxygen System section. Added Note to the Crosswind Operations section. D 4-15 to4-18 Changed "85%" to "80%" in the Cruise checklist. Repaginated pages. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 xvii NarrativeDiscussionof Revisions Cessna 350 (LC42-550FG) Revision Level D D D D D D D D D D D D D D D D D RB050005 xviii NARRATIVE DISCUSSION OF REVISIONS Page No. 4-20 4-22 to 4-24 4-27 and 4-28 4-32 to 4-38 5-20 6-12 and 6-13 6-16 6-18 and 6-19 6A-l to 6A-10 6B-l to 6B-6 7-1 7-8 7-15to7-19 7-21 7-30 7-39 7-47 and 7-48 Comment Revised location of the blue dots in the Fuel Selector section. Deleted the second paragraph and revised the Over Priming paragraph of the Engine Starting section. Revised the Battery Recharging section. Changed "there may be no point" to "there is no ooint" in the Crosstie Oocrations Checklist section. Revised the 3rd paragraph under the Engine Runup section. Changed "descent speed" to "airspeed" in the 2nd sentence of the Glidcslope Flight Procedure with Autopilot section. Revised the 3rd paragraph under the Hot Weather Operations section. Revised the Crosswind Landings section. Rcoaginated oage. Revised the Lean of Peak Engine Operation section. Deleted indication of an optional restraint system from the Baggage Nets section. Revised the Maximum Empty Weight section. Revised Figure 6-19. Revised Figure 6-20. Changed "five through eight" to "four through seven" in the Flight Operation Requirements on the first page. Added optional Oregon Aero scats, optional McCauley propeller, spinner and blade heaters, optional Precise Flight semi-portable oxygen system, Artex ME406 ELT, electrically driven compressor, interlock assembly, and accessories alternator. Indicated !FR for Items 34-11 and 34-18. Added optional Oregon Aero seats, optional McCauley propeller, spinner, and blade heaters, optional Precise Flight semi-portable oxygen system, Artcx ME406 ELT, electrically driven compressor, interlock assembly, and accessories alternator. Revised the POHi AFM weight. Revised the GTX 33 weight. Revised Table of Contents Revised the description of the wing cuffs in the Wings and Fuel Tanks section. Added Warning to the Door section. DO NOT open door during flight. Changed "Door Open" to "DOOR OPEN" in the Latching Mechanism and Door Seal System sections. Changed "manifold gauge" to "manifold pressure indicator" in the Throttle paragraph under the Engine Controls section. Changed "pilot's left knee" to "pilot's right knee" and "fuel manifold" to "intake manifold" in the Induction section. Changed "or pressure is above 18 psi" to "or a pressure differential greater than 18 psi is detected" in the Engine Oil section. Changed all occurrences of "L-LOW" to "L LOW" in the Caution Alerts section. Changed "L-LOW" to "L LOW" in the Fuel Low Annunciation Messages section. Revised the first paragraph of the Backup Fuel Pumo and Vaoor Suooression section. Revised Figure 7- 19. Revised the first sentence of the Airplane Exterior Lighting Svstem section. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) Narrative Discussion of Revisions NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level No. Revised the Emergency Locator Transmitter (ELT) section to include the Artex ME406 ELT. Revised the last paragraph in the Oxygen Display section. Changed "test/reset" to "reset" and two occurrences of "50" to "75" in the CO Guardian Carbon Monoxide Detector section. Indicated the location of the XM antenna in the XM Weather (WX) Data System section. Added GTA 82 Trim Adapter to the list of LRU in the GRC 700 AFCS. D 7-54 to 7-78 Changed "GA" to "GO AROUND" in the Additional AFCS Controls section. Added a Note to delay after turning off the system before turning it back on again in the System Operation paragraph of the Automatic Climate Control System (ACCS) section. Revised the Note in the System Operation Using Ground Power Supply paragraph to indicate 24 V ground power supply and 100 amps, and added Note to delay after turning off the system before turning it back on again. D 8-8 and 8-9 Revised Figure 8-3. Revised the Oxygen System Servicing section. Title Page, iii, Revised Title Page. E Revised LOEP. vii to xi, xix Revised Narrative Discussion of Revisions. E 1-1 Revised Table of Contents. E 1-22 Added atmospheric pressure relationships Figure 1-17. E 2-9 Revised paragraph 3.b. under the Garmin GI000 System Limitations section. E 2-11 Added A5 Flowmeters to the Oxygen Limitations section. E 5-1 Revised Table of Contents. E 5-32 to 5-34 Added Figure 5-27 for A5 Flowmeter and revised Figure 5-26. Revised cross references. Added pages 5-33 and 5-34. Added Item 52-01 Remote Keyless Entry System to the E 6A-3 to 6A-18 Equipment for Types of Operation List. Revised Item 34-37. Changed shaded blocks to check marks. E 68-1 to 68-10 Added Item 52-01 Remote Keyless Entry System to the Installed Equipment List. E 7-1 to 7-4 Revised Table of Contents. E 7-14 and 7-15 Added paragraph for description of the remote keyless entry system. E 7-27 Revised description of Elevator Mistrim Up and Down, and Aileron Mistrim Left and Right in the AFCS Alerts table. Added A5 Flowmcters under the Oxygen Flow Controls section. E 7-54 to 7-57 Added use of soap and water solution to get rid of static charge in the A5 Flowmeter. Removed all occurrences of Columbia, Columbia Aircraft F All Manufacturing Corporation, etc. and replaced with Cessna as applicable. Repaginated pages. Title Page, iv, G vii to xi, xix to Revised administrative pages. xxii Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 xix Narrative Discussion of Revisions Cessna 350 (LC42-550FG) Revision Level G G G G G G G G G G G G G G G G G G G G G RB050005 xx NARRATIVE DISCUSSION OF REVISIONS Page No. 1-4 and 1-5 2-1 2-6 2-9to2-13 2-17 2-19 2-21 3-3 3-13 3-19 3-24 4-2 4-4 and 4-5 4-9 to 4-1 I 4-17 4-19 to 4-21 5-11 5-23 and 5-24 5-32 6-13 6-A3 to 6-AI8 Comment Revised the Total Fuel Capacity section. Pages 1-4 and 1-5 rcpaginatcd. Revised Table of Contents. Revised the Fuel Quantity Row in Figure 2-3. Revised the Fuel Limitations section. Added Item 12. Flight Plan WARNING note to page 2-10. Added SafcTaxi Limitations section. Added Wide Arca Augmentation System (WAAS) Limitations section. Repaginatcd pages. Revised the Engraved On Fuel Selector Knob and Upper Plate placard. Indicated "(when air conditioning is installed)" for the Air Conditioning System Bay Access Cover placard. Revised the On Bottom of Baggage Compartment Door Joggle placard. Revised the Near Fill Cap of Fuel Tank placard. Changed maneuvering speed from "158" to "148" in Figure 3-1. Changed "75" to "50" in the Carbon Monoxide Detection procedure Note. Changed "right bus" to "essential bus" in the first sentence of the last paragraph of the Trim Tab Malfunctions section. Revised Figure 3-5. Revised Table of Contents. Added item 17 Induction Heated Air to Area I, and ", bushing in place" to Item 7 of Area 3 and to Item 2 of Arca 5 in the Preflight Insoection checklist. Added Item I and Item 14 regarding Air Conditioning to the Crosstie Operation checklist. Repaginated pages. Revised the Fuel Quantity section. Added description of the battery charging circuit. Rcpaginated pages. Removed the list of fuel flows from Figure 5-7. "Full Fuel Tanks" changed to Fuel Tanks Filled to" under conditions in Figure 5-20 and Figure 5-21. Revised Figure 5-26 and Figure 5-27. Revised the Fuel row and footnote in Figure 6-12. Revised 24-04 and added 24-05 to 24-07 Battery, 28 Volt. Deleted Item 21-26 Lower Hose Cover. Added items 33-8 to 33- 11 for Precise Flight Landing and Taxi Lights. Added 34-02 GA 35 GPS Antenna, 34-03 GA 37 GPS and XM Satellite Radio Antenna, and 34-26 GDU I 044 MFD with connector. Renumbered following Item Nos. Changed "GIA 63" to "GIA 63/GIA 63W" in Item Nos. 34-24, 34-25, and 34-26, and renumbered them to 34-27, 34-28, and 34-29. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) Narrative Discussion of Revisions NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level No. Revised 24-04 and added 24-05 to 24-07 Battery, 28 Volt. Deleted Item 21-26 Lower Hose Cover. Added items 33-8 to 33- 11 for Precise Flight Landing and Taxi Lights. G 6-B I to 6-B 10 Added 34-02 GA 35 GPS Antenna, 34-03 GA 37 GPS and XM Satellite Radio Antenna, and 34-26 GDU I 044 MFD with connector. Renumbered following Item Nos. Changed "GIA 63" to "GIA 63/GIA 63W" in Item Nos. 34-24, 34-25, and 34-26, and renumbered them to 34-27, 34-28, and 34-29. G 7-1 to 7-4 Revised Table of Contents. G 7-7 Deleted the Control Lock section. G 7-17 Revised footer to match LOEP. Revised the System Description list ofLRUs. Changed all occurrences of "GDU 1042" to "GDU 1042/GDU 1044" and GIA 63" to "GIA 63/GIA 63W" in the GDU 1040 PFD and GDU 1042 MFD, GMA 1347 Audio Panel, GIA 63, GDL 69A Data Link Receiver, GRS 77, GDC 74A, GEA 71, and G 7-19 to 7-24 GTX 33 sections, as applicable. Described the function of the GDU 1044 and GIA 63W in the sections listed above, as applicable. Indicated reference to "the latest revision" of the Garmin GI 000 Cockpit Reference Guide. Also changed "190-00567-00" to "I 90-00567-01", where applicable. Indicated reference to "the latest revision" of the Garmin GI 000 G 7-28 Cockpit Reference Guide. Also changed "190-00567-00" to "190-00567-01". Added SmartView, FliteCharts, SafeTaxi, and Wide Area Augmentation System (WAAS) descriptions. G 7-29 to 7-32 Corrected formatting in first paragraph of the Fuel System section. Rcpaginated pages. G 7-34 Revised the Fuel Low Annunciation messages section. G 7-38 and 7-39 Added Battery Charging Circuit description. Revised Figure 7-17. G 7-46 Changed "I 90-00567-00" to" 190-00567-01". Indicated reference to "the latest revision" of the Garmin GI 000 G 7-56 Cockpit Reference Guide and changed "190-00567-00" to "190- 00567-01" in the XM Weather (WX) Data System section. Indicated reference to "the latest revision" of the Garmin G 1000 Cockpit Reference Guide and changed "190-00567-00" to "190- G 7-59 00567-0 l" in the TCAD Display on the G 1000 section. Added interlock assembly to the general description of the Automatic Climate Control System section. Indicated reference to "the latest revision" of the Garmin G 1000 Cockpit Reference Guide and changed "190-00567-00" to "190- G 7-65 to 7-67 00567-01". Changed "GOU 1042" to "GDU 1042/GDU 1044" and "GIA 63" to "GIA 63/GIA 63W" throughout the Garmin GFC 700 Automatic Flight Control System (AFCS) section. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 xxi Narrative Discussion of Revisions Cessna 350 (LC42-550FG) Revision Level G H H H H H H H H H I I I I I I RB050005 xxii NARRATIVE DISCUSSION OF REVISIONS Page No. 8-4 to 8-6 All Title Page, iv, vii to xi, xxii 1-2 2-1 2-5 to 2-14 6-A3 to 6-A18 6-Bl to 6-BI0 7-37 9-1 and 9-2 Title Page, iv, vii to xii, xxii to xxiv 2-8 2-18 2-23 3-1 and 3-2 3-4 to 3-30 Comment Changed "190-00567-00" to "190-00567-01" in the Customer Delivery Package section. Revised the Fuel Capacities under the Fuel Servicing section. Revised due to company change to Cessna. Revised administrative pages. Revised Figure 1-1 to indicate horizontal stabilizer span is 14.1 ft. Revised the Table of Contents. Indicated "70 amp" for the Plane Power alternator in the Alternator Output Limitations section. Added color-coded range arc definitions to the Powerplant Gauge Markings section. Repaginated pages. Indicated Kelly alternator on Item 24-01, added Item 24-02 for Plane Power alternator, and renumbered following items. Added Item 71-03 for the Wintcrization Kit. Indicated Kelly alternator on Item 24-0 I, added Item 24-02 for Plane Power alternator, and renumbered following items. Added Item 71-03 for the Winterization Kit. Added "(70 amp for Plane Power alternator)" to the General Description paragraph. Simplified and revised the section to include optional equipment and/or devices manufactured by Cessna. Revised administrative pages. Deleted statement related to gyros under the Approved Acrobatic Maneuvers section. Indicated that the Under All Scats placard is not required under Oregon Aero scats. Added Jack Point placard. Revised the Table of Contents. "1.3.1" changed to "3.1" in step 3 and "3-16" to "3-17" in step 3.2 of the Procedures After an Engine Restart checklist. Changed "Step 4" to "Step 5" in Step 4 under the Engine Driven Fuel Pump (EDFP) - Partial Failure checklist. Changed "3-28" to "3- 30" in step 9 of the Ditching checklist. Revised the Electrical Fire in Flight and the Cabin Fire in Flight checklists. "6.1" and "6.2" changed to "3.1" and "3.2", respectively, in step 3, and "Alt Off'" changed to "Alt Off' in step 6 of the Alternator Failure - Electrical System Discharging checklist. Added Starter Motor Engaged in Flight Checklist. "No. 6" changed to "6" in step I of the Rudder Limiter Malfunction checklist. Changed "3- 26" to "3-29", "3-28" to "3-30", and "3-27" to "3-29" in the Evacuating the Airplane checklist. Revised Figure 3-2. Added Starter Motor Engaged in Flight discussion to the Amplified Emergency Procedures section. Added oagcs 3-29 and 3-30. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 Cessna 350 (LC42-550FG) Narrative Discussion of Revisions NARRATIVE DISCUSSION OF REVISIONS Revision Page Comment Level No. I 4-2 Revised the Table of Contents. I 4-3 Revised Figure 4-1. Revised item I and 14, and switched item 6 with item 7 and item I 4-9 and 4-10 12 with item 13 under the Crosstie Operation procedure. Revised the Autopilot Autotrim Operations checklist. Revised item 3 and 4 under the Taxiim1 checklist. I 4-22 Revised the first paragraph under the Taxiing section. Added Caution and explanation about use ofrapid forward stick I 4-27 to 4-32 movement with flaps fully extended at forward cg. Repaginated following pages. I 6A-l Deleted statement on headsets as optional items. I 6A-3 to 6A-18 Added Item No. 25-31 Rosen Sunvisor. I 68-1 to 68-10 Added Item No. 25-31 Rosen Sunvisor. I 7-1 Revised the Table of Contents. Deleted the Step (Not Installed) paragraph. Revised the Handles I 7-15 paragraph. Deleted "red lettered" from the Parking Brake paragraph_ I 7-34 Deleted "with red letters" and "with "amber letters". From the Backun Fuel Pumn and Vapor Sunorcssion section. Deleted Item 4 Automatic Stowage Due to Stall Warning I 7-53 Activation from the Precise Flight Specdbrake 2000 System section. I 7-67 to 7-70 Added description ofVNV Key. Revised Figure 7-32. Deleted oa!!cS7-69 and 7-70. Revised the Table of Contents. Revised all paragraphs in the Introduction section and added Airplane File paragraph. Revised the Cessna Advisory Service section and renamed it to "Cessna Owner Advisories". Deleted the Customer Delivery Package I 8-1 to 8-11 section. Revised the Preventive Maintenance section and renamed it to "Pilot Conducted Preventive Maintenance". Deleted sections Warranty Work and ADLOGTM Maintenance Rccordkccping System (MRS). Revised, renamed to "Airplane File", and moved section Airplane Documentation to page 8-4. Added section Cessna Customer Care Pro11ram. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 RB050005 xxiii Narrative Discussion of Revisions Cessna 350 (LC42-550FG) This Page Intentionally Left Blank RB050005 xxiv Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 Cessna 350 (LC42-550FG) TABLE OF CONTENTS Section 1 General Section 1 General THREE-VIEW ORA WING OF THE AIRPLANE ....................................................................... 1-2 INTRODUCTION ......................................................................................................................... 1-3 DESCRIPTIVE DATA .................................................................................................................. 1-4 Engine ................................................................................................................................... 1-4 Propeller ................................................................................................................................ 1-4 Fuel ....................................................................................................................................... 1-4 Oil ......................................................................................................................................... 1-5 Maximum Certificated Weights ........................................................................................... 1-5 Typical Airplane Weights ..................................................................................................... 1-5 Cabin and Entry Dimensions ................................................................................................ 1-5 Space and Entry Dimensions of Baggage Compartment ..................................................... 1-5 Specific Loadings ................................................................................................................. 1-5 ABBREVIATIONS, TERMINOLOGY, AND SYMBOLS ......................................................... 1-7 Airspeed Terminology .......................................................................................................... 1-7 Meteorological Terminology ................................................................................................ 1-8 Engine Power and Controls Terminology ............................................................................ 1-8 Airplane Performance and Flight Planning Terminology .................................................... 1-9 Weight and Balance Terminology ...................................................................................... 1-10 REVISIONS AND CONVENTIONS USED IN THIS MANUAL ........................................... 1-13 Supplements ........................................................................................................................ 1-13 Use of the terms Warning, Caution, and Note .................................................................... 1-13 Meaning of Shall, Will, Should, and May .......................................................................... 1-13 Meaning of Land as Soon as Possible or Practicable ......................................................... 1-13 CONVERSION CHARTS ........................................................................................................... 1-13 Kilograms and Pounds ........................................................................................................ 1-14 Feet and Meters .................................................................................................................. 1-15 Inches and Centimeters ........................................................................................................ 1-16 Knots, Statute Miles, and Kilometers .................................................................................. 1-17 Liters, Imperial Gallons, and U.S. Gallons ........................................................................ 1-18 Temperature Relationship (Fahrenheit and Cclsius) ........................................................... 1-21 Fuel Weights and Conversion Relationships ..................................................................... 1-22 Atmospheric Pressure Relationships (In. Hg and Hectopascal) ........................................ 1-22 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 1-1 Section 1 General Cessna 350 (LC42-550FG) THREE-VIEWDRAWINGOF THE AIRPLANE Wing Area Wing Span Length Empty Weight (±) Gross Weight Stall Speed Maneuvering Speed Cruising Speed Never Exceed Speed Engine Propeller Governor SPECIFICATIONS 141.2 ft. 2 (13.1 m2 ) 35.8 ft. (10.9 m) 25.2 ft. (7.68 m) 2450 lbs. (1111.1 kg) 3400 lbs. (1542 kg) 57 KIAS 148 KIAS 190 KTAS 235 KIAS 310 HP Continental 1O-550-N Hartzell McCauley *Note: Wingspan is 36 ft.± with position lights. t--------35.8 FT.*--------, 14.1 FT. >---+----+-4 .17 FT. Figure I - I RB050005 1-2 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) Section 1 General INTRODUCTION Section 1 General This handbook is written in nine sections and includes the material required to be furnished to the pilot by Federal Aviation Regulations and additional information provided by the manufacturer and constitutes the FAA Approved Airplane Flight Manual. Section I contains generalized descriptive data about the airplane including dimensions, fuel and oil capacities, and certificated weights. There are also definitions and explanations of symbols, abbreviations, and commonly used terminology for this airplane. Finally, conventions specific to this manual are detailed. NOTE Federal Aviation Regulations require that a current Handbook be in the airplane during flight. It is the operator's responsibility to maintain the Handbook in a current status. The manufacturer provides the registered owner(s) of the airplane with revisions. In countries other than the United States, FAA operating rules may not apply. Operators must ensure that the aircraft is operated in accordance with national operating rules. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 1-3 Section 1 General Cessna 350 (LC42-550FG) DESCRIPTIVE DAT A ENGINE Number of Engines: I Engine Manufacturer: Teledyne Continental Engine Model Number: 1O-550-N Engine Type: Normally aspirated, direct drive, air-cooled, horizontally opposed, fuel-injected, six- cylinder engine with 550 in. 3 (9013 cm 3) displacement Takeoff Power: 310 BHP at 2700 RPM. Maximum Continuous Power: 3 JO BHP at 2700 RPM Maximum Normal Operating Power: Same as maximum continuous power. Maximum Climb Power: Same as maximum continuous power. Maximum Cruise Power: Same as maximum continuous power. PROPELLER Propeller Manufacturer: Hartzell Propeller Hub and Blade Model Number: PHC-J3YF-IRF and F7691D-l Number of Blades: 3 Propeller Diameter: 76 in. (193 cm) minimum, 77 in. (I 96 cm) maximum Propeller Type: Constant speed and hydraulically actuated, with a low pitch setting of 14.1° ± 0.2° and a high pitch setting of34.7°± 1.0° (30 inch station) FUEL The following fuel grades, including the respective colors, are approved for this airplane. IO0LL Grade Aviation Fuel (Blue) 100 Grade Aviation Fuel (Green) Total Fuel Capacity - 106 Gallons (401 L) Total Capacity Each Tank: 53 Gallons (201 L) Total Usable Fuel: SIN 42502 to 42567 49 Gallons US (186 L)/Tank, 98 Gallons US (371 L) Total SIN 42568 and on Standard: 43 Gallons US (163 L)/Tank, 86 Gallons US (326 L) Total Long Range: 51 Gallons US (193 L)/Tank, 102 Gallons US (386 L) Total NOTE Under certain atmospheric conditions, ice can form along various segments of the fuel system. Under these conditions, isopropyl alcohol, ethylene glycol monomethyl ether, or diethylene glycol monomethyl ether may be added to the fuel supply. Additive concentrations shall not exceed 3% for isopropyl alcohol or 0.15% for ethylene glycol monomethyl ether and diethylene glycol monomethyl ether (military specification MIL-1- 27686E). See Figure 8 - 1 in Section 8 for a chart of fuel additive mixing ratios. RB050005 1-4 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) OIL Section 1 General Specification or Oil Grade (the first 25 engine hours) - Aviation Grade Straight Mineral Oil (MIL-L-6082) shall be used during the first 25 hours of flight operations. Specification or Oil Grade (after 25 engine hours) - Teledyne Continental Motors Specification MHS-24D and MHS-25 (latest revisions). An ashless dispersant oil shall be used after 25 hours. Viscosity Recommended for Various Average Air Temperature Ranges Below 40°F (4°C)-SAE 30, I0W30, !5W50, or 20W50 Above 40°F (4°C)- SAE 50, I 5W50, 20W/50, or 20W60 Total Oil Capacity Sump: 8 Quarts (7.6 L) Total: IO Quarts (9.5 L) Drain and Refill Quantity: 8 Quarts (7.6 L) Oil Quantity Operating Range: 6 to 8 Quarts (5.7 to 7.6 L) NOTE The first time the airplane is filled with oil, additional oil is required for the filter, oil cooler, and propeller dome. At subsequent oil changes, this additional oil is not drainable from the system, and the added oil is mixed with a few quarts of older oil in the oil system. MAXIMUM CERTIFICATED WEIGHTS Ramp Weight: Takeoff Weight: Landing Weight: Baggage Weight: TYPICAL AIRPLANE WEIGHTS 3400 lbs. (1542 kg) 3400 lbs. (1542 kg) 3230 lbs. (1465 kg) 120 lbs. (54.4 kg) The empty weight of a typical airplane offered with four-place seating, standard interior, avionics, accessories, and equipment has a standard empty weight of about 2300 lbs. (1043 kg). Maximum Useful Load: 1100 lbs.* (498.9 kg) *(The useful load varies for each airplane. Please sec Section 6 for specific details.) CABIN AND ENTRY DIMENSIONS Maximum Cabin Width: 50 inches (127 cm) Maximum Cabin Length (Firewall to aft limit of baggage compartment): • 139.6 inches (354.6 cm) Maximum Cabin Height: 49 inches (124.5 cm) Minimum Entry Width: 33 inches (83.8 cm) Minimum Entry Height: 33 inches (83.8 cm) Maximum Entry Clearance: 46 inches (116.8 cm) SPACE AND ENTRY DIMENSIONS OF BAGGAGE COMPARTMENT Maximum Baggage Compartment Width: 38.5 inches (97.8 cm) Maximum Baggage Compartment Length: 52 inches (132 cm) (Including Shelf) Maximum Baggage Compartment Height: 34.5 inches (87.6 cm) Maximum Baggage Entry Width: 28 inches (71.1 cm) (Diagonal Measurement) SPECIFIC LOADINGS Wing Loading: 24.08 lbs./sq. ft. Power Loading: I 0.97 lbs./hp. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 1-5 Section 1 General RB050005 1-6 Cessna 350 (LC42-550FG) This Page Intentionally Left Blank Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) Section 1 General ABBREVIATIONS, TERMINOLOGY, AND SYMBOLS AIRSPEED TERMINOLOGY CAS KCAS GS !AS KIAS TAS Vo Vrn Vso Vx Vv Calibrated Airspeed means the indicated speed of an aircraft, corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level. Calibrated Airspeed expressed in knots. Ground Speed is the speed of an airplane relative to the ground. Indicated Airspeed is the speed of an aircraft as shown on the airspeed indicator when corrected for instrument error. !AS values published in this Handbook assume zero instrument error. Indicated Airspeed expressed in knots. True Airspeed is the airspeed of an airplane relative to undisturbed air, which is the CAS, corrected for altitude, temperature and compressibility. This term refers to the maximum speed in level flight with maximum continuous power. The maximum operating maneuvering speed of the airplane. Do not apply full or abrupt control movements above this speed. If a maneuver is entered gradually at V0 with maximum weight and full forward CG, the airplane will stall at limit load. However, limit load can be exceeded at VO if abrupt control movements arc used or the CG is farther aft. Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. Never Exceed Speed is the speed limit that may not be exceeded at any time. Maximum Structural Cruising Speed is the speed that must not be exceeded except in smooth air and then only with caution. Stalling Speed or the minimum steady flight speed at which the airplane is controllable. Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the landing configuration. Best Angle-of-Climb Speed is the airspeed that delivers the greatest gain of altitude in the shortest possible horizontal distance. Best Rate-of-Climb Speed is the airspeed that delivers the greatest gain in altitude in the shortest possible time. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 1-7 Section 1 General Cessna 350 (LC42-550FG) METEOROLOGICAL TERMINOLOGY ISA International Standard Atmosphere in which: Standard Temperature OAT Indicated Pressure Altitude Pressure Altitude (PA) Station Pressure Wind I. The air is a dry perfect gas; 2. The temperature at sea level (SL) is 15° C (59° F); 3. The pressure at SL is 29.92 inches of Hg (1013.2 mb); 4. The temperature gradient from SL to an altitude where the temperature is -56.5°C (-69.7°F) is -0.00198°C (-.003564°F) per foot, and zero above that altitude. Standard Temperature is 15°C (59°F) at sea level pressure altitude and decreases 2°C (3.2°F) for each 1000 feet of altitude. Outside Air Temperature is the free air static temperature obtained either from in-flight temperature indications or ground meteorological sources, adjusted for instrument error and compressibility effects. The number actually read from an altimeter when the barometric subscalc has been set to 29.92 inches of Hg (1013.2 mb). Altitude measured from standard sea level pressure (29.92 inches of Hg) by a pressure or barometric altimeter. It is the indicated pressure altitude corrected for position and instrument error. In this Handbook, altimeter instrument errors arc assumed to be zero. Actual atmospheric pressure at field elevation. The wind velocities recorded as variables on the charts of this handbook arc to be understood as the headwind or tailwind components of the reported winds. ENGINE POWER & CONTROLS TERMINOLOGY BHP EGTGaugc MP MCP Maximum Cruise Power MNOP Mixture Control Propeller Control RB050005 1-8 Brake Horsepower is the power developed by the engine. The Exhaust Gas Temperature indicator is the instrument used to identify the lean fuel flow mixtures for various power settings. Manifold Pressure is the pressure measured in the intake system of the engine and is depicted as inches of Hg. Maximum Continuous Power is the maximum power for abnormal or emergency operations. The maximum power recommended for cruise. Maximum Normal Operating Power is the maximum power for all normal operations (except takeoff). This power, in most situations, is the same as Maximum Continuous Power. The Mixture Control provides a mechanical linkage with the fuel control unit of fuel injection engines, to control the size of the fuel feed aperture, and thus, the air/fuel mixture. It is also a primary means to shut down the engine. The lever used to select a propeller speed. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) Section 1 General Propeller Governor RPM Stall Strip Tachometer Throttle Wing Cuff The device that regulates the RPM of the engine and propeller by increasing or decreasing the propeller pitch, through a pitch change mechanism in the propeller hub. Revolutions Per Minute is a measure of engine and/or propeller speed. A small triangular strip installed along the leading edge of an airplane wing near the root. The stall strips force the roots of the wing to stall before the tips. The strips allow complete control throughout the stall. An instrument that indicates propeller rotation and is expressed as revolutions per minute (RPM). The lever used to control engine power, from the lowest through the highest power, by controlling propeller pitch, fuel flow, engine speed, or any combination of these. Specially shaped composite construction on the outboard leading edge of the wing. The cuff increases the camber of the airfoil and improves the slow- flight and stall characteristics of the wing. AIRPLANE PERFORMANCE & FLIGHT PLANNING TERMINOLOGY Demonstrated Crosswind Velocity G GPH Limit Factor NMPG PPH Load Unusable Fuel Ultimate Factor Load Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane can be maintained during takeoff and landing. The value shown is not considered limiting. A unit of acceleration equal to the acceleration of gravity at the surface of the earth. The term is frequently used to quantify additional forces exerted on the airplane and is expressed as multiples of the basic gravitational force, e.g., a I. 7-g force. Gallons Per Hour is the quantity of fuel consumed in an hour expressed in gallons. The limit load factor is expressed in multiples of gravity (g) which the airplane can safely withstand. If the limit load factor is exceeded, the airplane may be damaged. Nautical Miles per Gallon is the distance (in nautical miles) which can be expected per gallon of fuel consumed at a specific power setting and/or flight configuration. Pounds Per Hour is the quantity of fuel consumed in an hour expressed in pounds. Unusable Fuel is the amount of fuel expressed in gallons that cannot safely be used in flight. Unusable Fuel is the fuel remaining after a runout test has been completed in accordance with governmental regulations. The ultimate load factor is 1.5 times the limit load factor. If the ultimate load factor is exceeded, the airplane can fail catastrophically. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 1-9 Section 1 General Usable Fuel Cessna 350 (LC42-550FG) Usable Fuel is the quantity available that can safely be used for flight planning purposes. WEIGHTAND BALANCE Arm The Arm is the horizontal distance from the reference datum to the center of gravity (C.G.) ofan item. Basic Weight Empty The Basic Empty Weight is the Standard Empty Weight plus optional equipment. CG CG Arm CG Limits Maximum Empty Weight Maximum Gross Weight Maximum Landing Weight Maximum Ramp Weight Maximum Takeoff Weight Maximum Zero- Fuel Weight Minimum Flight Weight Minimum Useful Load RB050005 1-10 The Center of Gravity is the point at which the airplane will balance if suspended. Its distance from the datum is found by dividing the total moment by the total weight of the airplane. The arm obtained by adding the individual moments of the airplane and dividing the sum by the total weight. The extreme center of gravity locations within which the airplane must be operated at a given weight. This is the maximum allowable weight of the airplane when empty, before fuel, passengers, and baggage arc added. Subtracting the minimum useful load from the maximum gross weight produces the maximum empty weight. The amount of additional equipment that can be added to the airplane is determined by subtracting the standard empty weight from the maximum empty weight. Sec page 6-16 for an example. The maximum loaded weight of an aircraft. Gross weight includes the total weight of the aircraft, the weight of the fuel and oil, and the weight of all the load it is carrying. The maximum weight approved for landing touchdown. The maximum weight approved for ground maneuver. (It includes the weight of the fuel used for startup, taxi, and runup.) The maximum weight approved for the start of the takeoff run. The maximum weight authorized for an aircraft that docs not include the weight of the fuel. This weight includes the basic empty weight plus the weight of the passengers and baggage. The maximum zero-fuel weight can change depending on the center of gravity location. Sec Figure 2 - 4 for an example. This is the minimum weight permitted for flight operations and includes the basic empty weight plus fuel, pilot, passengers, and baggage. The minimum flight weight can change depending on the center of gravity location. Sec Figure 2 - 4 for an example. For utility category airplanes, certified for night or IFR operations, a weight of 190 pounds for each installed scat plus the fuel weight for 45 minutes at maximum continuous power. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) Section 1 General Moment Reference Datum Standard Empty Weight Station Useful Load MISCELLANEOUS Flight Time- Airplanes Time in Service The moment of a lever is the distance, in inches, between the point at which a force is applied and the fulcrum, or the point about which a lever rotates, multiplied by the force, in pounds. Moment is expressed in inch-pounds. This is an imaginary vertical plane from which all horizontal distances arc measured for balance purposes. This is the weight of a standard airplane including unusable fuel, full operating fluids, and full oil. The Station is a location along the airplane's fuselage usually given in tenns of distance from the reference datum, i.e., Station 40 would be 40 inches from the reference datum. The Usefitl Load is the difference between Takeoff Weight or Ramp Weight, if applicable, and Basic Empty Weight. Pilot time that commences when an aircraft moves under its own power for the purpose of flight and ends when the aircraft comes to rest after landing. Time in service, with respect to maintenance time records, means the time from the moment an aircraft leaves the surface of the earth until it touches it at the next point oflanding. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 1-11 Section 1 General RB050005 1-12 Cessna 350 (LC42-550FG) This Page Intentionally Left Blank Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) SUPPLEMENTS Section 1 General Equipment, which is not covered in Sections 1 through 8 of the Information Manual, is included in Section 9, as applicable. USE OF THE TERMS WARNING, CAUTION, AND NOTE The following conventions will be used for the terms, Warning, Caution, and Note. fi'ARNING! The use of a Warning symbol means that information which follows is of critical importance and concerns procedures and techniques which could cause or result in personal injury or death if not carefully followed. !CAUTION! The use of a Caution symbol means that information which follows is of significant importance and concerns procedures and techniques which could cause or result in damage to the airplane and/or its equipment if not carefully followed. NOTE The use of the term "NOTE" means the information that follows is essential to emphasize. MEANING OF SHALL, WILL, SHOULD, AND MAY The words shall and will arc used to denote a mandatory requirement. The word should denotes something that is recommended but not mandatory. The word may is permissive in nature and suggests something that is optional. MEANING OF LAND AS SOON AS POSSIBLE OR PRACTICABLE The use of these two terms relates to the urgency of the situation. When it is suggested to land as soon as possible, this means to land at the nearest suitable airfield after considering weather conditions, ambient lighting, approach facilities, and landing requirements. When it is suggested to land as soon as practicable, this means that the flight may be continued to an airport with superior facilities, including maintenance support, and weather conditions. CONVERSION CHARTS On the following pages arc a series of charts and graphs for conversion to and from U.S. weights and measures to metric and imperial equivalents. The charts and graphs arc included to help pilots who live in countries other than the United States or pilots from the United States who arc traveling to or within other countries. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 1-13 Section 1 General Cessna 350 (LC42-550FG) KILOGRAMS AND POUNDS . 99.l!YERTIN§ K!LOG~S TO PO!J":1!>5- Kilograms 0 2 3 4 5 6 7 8 9 0 2.205 4.409 6.614 8.818 11.023 13.228 15.432 17.637 19.842 IO 22.046 24.251 26.455 28.660 30.865 33.069 35.274 37.479 39.683 41.888 20 44.092 • 46.297. 48.502 50.706. 52.911 55.116 57.320 59:525 61.729 63.934 30 66.139 68.343 70.548 72.753 74.957 77.162 79.366 81.571 83.776 85.980 40 88.185 90:390 92.594 94.799 ; 97.003 99.208 101.413 103.617: 105.822 !08.026 50 110.231 112.436 114.640 116.845 119.050 121.254 123.459 125.663 127.868 130.073 60 • 132.2T7: 134.482 136.687 138.891 141.096 143.300 145.505 147.710 149.914 152.119 70 154.324 156.528 158.733 160.937 163.142 165.347 167.551 169.756 171.961 174.165 80 176.370 j 178.574 180.779 182.984 185.188 : 187.393 189.597 191.802 194.007 196.211 90 198.416 200.621 202.825 205.030 207.234 209.439 211.644 213.848 216.053 218.258 JOO 220.462 2.n6ii' 224.811 227.076. 229.281 231.485 233.690 ,235.895 238.099 240.304 Example: Convert 76 kilograms to pounds. Locate the 70 row in the first column and then move right, horizontally to Column No. 6 and read the solution, 167.551 pounds. Figure I - 2 <;ONVERTINGPOUNDSTC>KILOGRAMS Pounds 0 2 3 4 5 6 7 8 9 0 0.454 0.907 1.361 1.814 2.268 2.722 3.175 3.629 4.082 10 4.536 4.990 5.443 5.897 6.350 6.804 7.257 7.711 8.165 8.618 20 9.072 9.525 9.979 10.433 I0.886 11.340 11.793 12.247 12.701 13.154 30 13.608 14.061 14.515 14.969 15.422 15.876 16.329 16.783 17.236 17.690 40 18.144 18.597 19.051 19.504 19.958 . 20.412 20.865 21.319 21.772 • 22.226 50 22.680 23.133 23.587 24.040 24.494 24.948 25.401 25.855 26.308 26.762 60 27.216 27.669 28.123 28.576 29.030 29.483 29.937 30.391 30.844 31.298 70 31.751 32.205 32.659 33.112 33.566 34.019 34.473 34.927 35.380 35.834 80 36.287 36.741 37.195 37.648 38.102 38.555 39.009 39.463 39.916 40.370 90 40.823 41.277 41.730 42.184 42.638 43.091 43.545 43.998 44.452 44.906 100 45.359 45.813 46.266 46.720 47.174 47.627 48.081 48.534 48.988 49.442 Example: Convert 40 pounds to kilograms. Locate the 40 row in the first column and then move right one column to Column No. 0 and read the solution, 18.144 kilograms. Figure I - 3 RB050005 1-14 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Section 1 Cessna 350 (LC42-550FG) General FEET AND METERS CONVERTING METERS TO FEET Meters 0 2 3 4 5 6 7 8 9 0 3.281 6.562 9.843 13.123 16.404 19.685 22.966 26.247 29.528 10 32.808 36.089 39.370 42.651 45.932 49.213 52.493 55.774 59.055 62.336 20 65.617 68.898 72.178 75.459 78.740 82.021 85.302 88.583 91.864 95.144 30 98.425 101.706 104.987 108.268 111.549 114.829 118.110 121.391 124.672 127.953 40 131.234 134.514 137.795 141.076 .144.357 147.638 150.919 _154.i99 157.480 160.761 50 164.042 167.323 170.604 173.885 177.165 180.446 183.727 187.008 190.289 193.570 60 196.850 200.131 203.412 • :Zo6.693 209.974 213.255 216.535 219.81? ;#3.097 L226.378 70 229.659 232.940 236.220 239.501 242.782 246.063 249.344 252.625 80 262.467 265.748 269.029 272.310 275.591 278.871 282.152 _285.433 90 295.276 298.556 301.837 305.118 308.399 311.680 314.961 318.241 100 328.084 "331.365 334.646 337.927 341.207 344.488 347.769 351.050 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 4 CONVERTING FEE_TTQ ME"[E~~- Feet 0 2 3 4 5 6 7 0 0.305 0.610 0.914 1.219 1.524 1.829 2.134 10 3.048 3.353 3.658 3.962 4.267 4.572 4.877 5.182 20 6.096 6.401 6.706 7.010 7.315 7.620 7.925 8.230 30 9.144 9.449 9.754 10.058 10.363 10.668 10.973 11.278 40 12.192 12.497 12;802 13.106 13.411 13.716 14.021 14.326 50 15.240 15.545 15.850 16.154 16.459 16.764 17.069 17.374 60 18.288 18.593 18.898 19.202 19.507 19.812 20.117 20.422 70 21.336 21.641 21.946 22.250 22.555 22.860 23.165 23.470 80 24.384 24.689 24.994 25.298 25.603 25.908 26.213 26.518 90 27.432 27.737 28.042 28.346 28.651 28.956 29.261 29.566 100 30.480 30.785 31.090 31.394 31.699 32.004 32.309 32.614 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 5 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 255.906 259.186 :288.714 \?91.995 321.522 324.803 354.331 357.612 8 9 2.438 2.743 5.486 5.791 8.534 8.839 11.582 11.887 14.630 14.935 17.678 17.983 20.726 21.031 23.774 24.079 26.822 27.127 29.870 30.175 32.918 33.223 RB050005 1-15 Section 1 General Cessna 350 (LC42-550FG) INCHES AND CENTIMETERS CONVERTING CENTIMETERS TO INCHES Centimeters 0 1 2 3 4 5 6 7 8 9 0 0.394 0.787 1.181 1.575 1.969 2.362 2.756 3.150 3.543 10 3.937 4.331 4.724 5.118 5.512 5.906 6.299 6.693 7.087 7.480 20 7.874 8.268 8.661 9.055 9.449 9.843 10.236 10.630 1Lo24 11.417 30 11.811 12.205 12.598 12.992 13.386 13.780 14.173 14.567 14.961 15.354 40 15.748 16.142 16.535 16.929 17.323 17.717 18.110 18.504 18.898 19.291 50 19.685 20.079 20.472 20.866 21.260 21.654 22.047 22.441 22.835 23.228 60 23.622 24.016 24.409 24.803 25.197 25.591 25.984 _ -~6.378 26.772 27.165 70 27.559 27.953 28.346 28.740 29.134 29.528 29.921 30.315 30.709 31.102 80 31.496 31.890 32.283 32.677 33.071 33.465 33.858 34.252 34.646 35.039 .. 90 35.433 35.827 36.220 36.614 37.008 37.402 37.795 38.189 38.583 38.976 100 39.370 39.764 40.157 40.551 40.945 41.339 , 41.732 42.126 42.520 42.913 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 6 CONVJ:RTING !~CHES TO_CE~TiMETERS Inches 0 2 3 4 5 6 7 8 9 0 2.54 5.08 7.62 10.16 12.70 15.24 17.78 20.32 22.86 10 25.40 27.94 30.48 33.02 35.56 38.10 40.64 43.18 45.72 48.26 20 50.80 53.34 55.88 5,8J_2 60.96 63.50 66.04 68.58 71.12 73.66 30 76.20 78.74 81.28 83.82 86.36 88.90 91.44 93.98 96.52 99.06 40 101.60 104.14; 106.68 109.22 111.76 114.30 116.84 119.38 121.92 124.46 50 127.00 129.54 132.08 134.62 137.16 139.70 142.24 144.78 147.32 149.86 60 152.40 154.94 157.48 160.02 162.56 165.10 167.64 170.18 172.72 175.26 70 177.80 180.34 182.88 185.42 187.96 190.50 193.04 195.58 198.12 200.66 80 203.20 205.74 208.28 210.82 213.36 215.90 218.44 220.98 223.52 226.06 90 228.60 231.14 233.68 236.22 238.76 241.30 243.84 246.38 248.92 251.46 100 254.00 256.54 259.08 261.62 264.16 266.70 269.24 271.78 274.32 276.86 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 7 RB050005 1-16 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) NAUTICAL MILES, STATUTE MILES, AND KILOMETERS Nautical Statute Kilo- Nautical 'Statute Kilo- Miles Miles meters, Miles Miles meters 5 6 9 175 202 324 10 12 19 180 207 333 15 17 28 185 213 343 20 23 37 190 219 352 25 29 46 195 225 361 30 35 56 200 230 370 35 40 65 205 236 380 40 46 74 210 242 389 45 52 83 215 248 398 50 58 93 220 253 407 55 63 102 225 259 417 60 69 111 230 265 426 65 75 120 235 271 435 70 81 130 240 276 444 75 86 139 245 282 454 80 92 148 250 288 463 85 98 157 255 294 472 90 104 167 260 299 482 95 109 176 265 305 491 100 115 185 270 311 500 105 121 194 275 317 509 l!il 127 204 280 322 519 115 132 213 285 328 528 120 138 222 290 jj4 537 125 144 232 295 340 546 130 150 241 300 345 556 135 155 250 305 351 565 140 161 259 310 357 574 145 167 269 315 363 583 ISO 173 278 320 369 593 155 178 287 325 374 602 160 184 296 330 380 611 165 190 306 335 386 620 170 196 315 340 392 630 Figure I - 8 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Nautical Statute Miles Miles 345 397 350 403 355 409 360 415 365 420 370 426 375 432 380 438 385 443 390 449 395 455 400 461 405 466 410 472 415 478 420 484 425 489 430 495 435 501 440· 507 445 512 450 5fs 455 524 460 530 465 535 470 541 475 547 480 553 485 559 490 564 495 570 500 576 505 582 5io 587 Section 1 General Kilo- lllet~r,s 639 648 657 667 676 685 695 704 713 722 732 741 750 759 769 778 787 796 806 815 824 833 843 852 861 870 880 889 898 907 917 926 935 945 RB050005 1-17 Section 1 General Cessna 350 (LC42-550FG) LITERS,IMPERIALGALLONS,AND U.S. GALLONS CONVERTIN-GLITER.STO IMPER.JALGALLONS_ Liters 0 2 3 4 5 6 7 8 9 () 0.66 0.88 ·. 0.22 0.44 LIO L32 1.54 l.76 1.98 10 2.20 2.42 2.64 2.86 3.08 3.30 3.52 3.74 3.96 4.18 20 4:40 4.62 4.84 5.06 5.28 5.50 5.72 5.94 6.16 6.38 30 6.60 6.82 7.04 7.26 7.48 7.70 7.92 8.14 8.36 8.58 .40 8.80 9:02 9.24 9.46 9.68 9.90 10.12 10.34 10.56 10.78 50 11.00 11.22 11.44 11.66 11.88 12.10 12.32 12.54 12.76 12.98 60 .13.20 13.42 13.64 13.86 14.08 14.30 14.52 14.74 14.96 15.18 70 15.40 15.62 15.84 16.06 16.28 16.50 16.72 16.94 17.16 17.38 80 17.60 17.82 18.04 18.26 18.48 18.70 18.92 19.14 19.36 19.58 90 19.80 20.02 20.24 20.46 20.68 20.90 21.12 21.34 2L56 21.78 100 22.00 • 22.22 22.44 22.66 22.88 23.10 23.32 23.54 23.76 23.98 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 9 CONVERTl~G IMPERIAL GALLONS TO LITERS Imperial 0 2 3 4 5 6 7 8 9 Gallons 0 0.00 4.55 9.09 13.64 18.18 22.73 27.28 31.82 36.37 40.91 10 45.46 50.01 54.55 59.10 63.64 68.19 72.74 77.28 81.83 86.37 20 90.92 95.47 100.01 104.56 109.10 113.65 118.20 122.74 127.29 131.83 30 136.38 140.93 145.47 150.02 154.56 159.11 163.66 168.20 172.75 177.29 40 181.84 186.39 190.93 195.48 200.02 204.57 209.12 213.66 218.21 222.75 50 227.30 231.85 236.39 240.94 245.48 250.03 254.58 259.12 263.67 268.21 60 272.76 277.31 281.85 286.40 290.94 295.49 300.04 304.58 309.13 313.67 70 318.22 322.77 327.31 331.86 336.40 340.95 345.50 350.04 354.59 359.13 80 363.68 368.23 ' 372.77 377.32 381.86 386.41 390.96 395.50 400.05 404.59 90 409.14 413.69 418.23 422.78 427.32 431.87 436.42 440.96 445.51 450.05 100 454.60 459.15 463.69 468.24 472.78 477.33 481.88 486.42 490.97 495.51 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. RB050005 1-18 Figure I - 10 . Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) LITERS, IMPERIAL GALLONS, AND U.S. GALLONS (Continued) coNVERTJf.lGLI!F::RSTo_U.s'.GALbQN§ Liters 0 2 3 4 5 6 7 0 0.00 0.26 0.53 0.79 1.06 1.32 1.59 I.85 10 2.64 2.91 3.17 3.43 3.70 3.96 4.23 4.49 20 5.28 5.55 5.81 6.08 6.34 6.60 6.87 7.13 30 7.93 8.19 8.45 8.72 8.98 9.25 9.51 9.77 40 10.57 10.83 11.10 11.36 11.62 11.89 12.15 12.42 50 13.21 13.47 13.74 14.00 14.27 14.53 14.79 15.06 60 15.85 16.11 16.38 16.64 16.91 17.17 17.44 17.70 70 18.49 18.76 19.02 19.28 19.55 19.81 20.08 20.34 80 21.13 2L40 21.66 21.93 22.19 22.45 22.72 22.98 90 23.78 24.04 24.30 24.57 24.83 25.10 25.36 25.62 100 26.42 26.68 26.95 · 27.21 27.47 27.74 28.00 28.27 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 11 CO,t,,VE:R,JIN,G U.S._GALLONSTC>LITER,~ U.S. Gallons 0 2 3 4 5 6 7 .. 0 0.00 3.79 7.57. 11.36 15.14 18.93 22.71 26.50 10 37.85 41.64 45.42 49.21 52.99 56.78 60.56 64.35 20 75.70 79.49 83.27 87.06 90.84 94.63 98.41 102.20 30 113.55 117.34 121.12 124.91 128.69 132.48 136.26 140.05 40 151.40 155.19 158.97 162.76 166.54 170.33 174.11 177.90 50 189.25 193.04 196.82 200.61 204.39 208.18 211.96 215.75 60 227.10 230.89 234.67 238.46 242.24 246.03 249.81 253.60 70 264.95 268.74 272.52 276.31 280.09 283.88 287.66 291.45 80 302.80 306.59 310.37 314.16 317.94 321.73 325.51 329.30 90 340.65 344.44 348.22 352.01 355.79 359.58 363.36 367.15 100 378.50 382.29 386.07 389,86 393.64 397 ..43 401.21 405.00 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 12 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Section 1 General 8 9 2.11 2.38 4.76 5.02 7.40 7.66 10.04 10.30 12.68 12.94 15.32 15.59 17.96 18.23 20.61 20.87 23.25 23.51 25.89 26.15 28.53 2?-79 8 9 30.28 34.07 68.13 71.92 105.98 109.77 143.83 147.62 181.68 185.47 219.53 223.32 257.38 261.17 295.23 299.02 3~3.08 336.87 370.93 374.72 .. 408.z~ 41t57 RB050005 1-19 Section 1 General Cessna 350 (LC42-550FG) LITERS,IMPERIALGALLONS,AND U.S. GALLONS(Continued) CONYERTiNG IMPE_RiAL~ALLONS T_()U.S. GALLONS Imperial 0 2 3 4 Gallons 5 6 7 8 9 0 0.00 l.~0 2.40 3.60 4.80 6.01 7.21 8.41 9.61 10.81 10 12.01 13.21 14.41 15.61 16.81 18.02 19.22 20.42 21.62 22.82 20 • 24.02 25.22 26.42 27.62 28.82 30.03 fl.23 32.43 33.63 34.83 30 36.03 37.23 38.43 39.63 40.83 42.04 43.24 44.44 45.64 46.84 ., 40 48.04 49.24 50.44 51.64 52.84 54.05 55.25 56.45 57.65 58.85 50 60.05 61.25 62.45 63.65 64.85 66.06 67.26 68.46 69.66 70.86 60 72.06 • 73:26 74.46 75.66 76.86 78.07 79.27 80.47 81.67 82.87 70 84.07 85.27 86.47 87.67 88.87 90.08 91.28 92.48 93.68 94.88 80 96.08 97.28·. 98.48 99.68 100.88 102.09 103.29 104.49 105.69 106.89 90 108.09 109.29 110.49 111.69 112.89 114.10 115.30 116.50 117.70 118.90 100 120.10 121.30 122.50 123.70 124.90 126.11 127.31 128.51 129.71 130.91 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 13 £.O_NVERTlNGU.S. GALLONS TO IMPERIAL GALL,ONS U.S. Gallons 0 l 2 3 4 5 6 7 8 9 0 0.00 0.83 1.67 2.50 3.33 4.16 5.00 5.83 6.66 7.49 10 8.33 9.16 9.99 10.82 11.66 12.49 13.32 14.16 14.99 15.82 20 16.65 17.49 18.32 19.15 19.98 20.82 21.65 22.4~ 23.32 24.15 30 24.98 25.81 26.65 27.48 28.31 29.14 29.98 30.81 31.64 32.47 40 33.31 34.14 34.97 35.81 36.64 37.47 38.30 39.14 39.97 40.80 50 41.63 42.47 43.30 44.13 44.96 45.80 46.63 47.46 48.30 49.13 60 49.96 50.79 51.63 52.46 53.29 54.12 54.96 55.79 56.62 57.45 70 58.29 59.12 59.95 60.79 61.62 62.45 63.28 64.12 64.95 65.78 80 66.6.1 67.45 68.28 69.11 69.95 70.78 71.61 72.44 73.28 74.11 90 74.94 75.77 76.61 77.44 78.27 79.10 79.94 80.77 81.60 82.44 100 83.27 84.10 84.93 85.77 86.60 87.43 88.26 89.10 89.93 90.76 Example: Refer to Figure 1-2 and Figure 1-3 for examples of how to use these types of tables. Figure I - 14 RB050005 1-20 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) TEMPERATURE RELATIONSHIPS (FAHRENHEIT AND CELSIUS) Fahrenheit Celsius Fahrenheit Celsius -40F -40C 145F 63C -35F -37C ISOF 66C -JOF -34C 155F 68C -25F -32C 160F 71C -20F -29C 165F 74C -!SF -26C 170F 77C -IOF -23C 175F 79C -SF -21C 180F 82C OF -18C 185F 85C SF -!SC 190F 88C !OF -12C 195F 91C 15F -9C i00F 93C 20F -7C 205F 96C 25F -4C 2IOF 99C 30F -IC 215F !02C 35F 2C 220F !04C 40F 4C 225F 107C 45F 1c 230F !IOC 50F IOC 235F 113C 55F .13C 2401' 116t 60F 16C 245F !!SC 65F isc 250F 121c 70F 21C 255F 124C 75F 24C 260F 127C 80F 27C 265F 129C 85F 29C 270F 132C 90F 32C 275F 135C 95F 35C 280F 138C IOOF 38C 285F 141C IOSF 41C 290F 143C llOF 43C 295F 146C !!SF 46C 300F 149C 120F 49C 305F 152C 125F 52C 310F 154C 130F 54C 315F 157C 135F 57C 3201' 160C 140F 60C 325F 163C Figure I - 15 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Fahrenheit 330F 335F 340F 345F 350F 355F 360F 365F 370F 375F 380F 385F 390F 395F 400F 405F 4IOF 415F 420F ·425F 430F 435F 440F 445F 450F 4551' 460F 465F 470F 475F 480F 4851' 490F 495F 500F 5051' S!OF Section 1 General Celsius. !66C !68C !71C 174C 177C .179C 182C !85C !88C 191c 193C 196C 199C ·202c 204C 207C 210C iUc 216C 218C 221C 224c 227C ii9c 232C 235C: 238C 241C 243C 246c 249C 2s2c 254C 257C 260C 263C 266C RB050005 1-21 Section 1 General Cessna 350 (LC42-550FG) FUEL WEIGHTS AND CONVERSION RELATIONSHIPS The table below summarizes the weights and conversion relationships for liters, U.S. Gallons, and Imperial Gallons. The chart values arc only to two decimal places. The table is intended to provide approximate values for converting from one particular quantity of measurement to another. Qu;ntity iii~~ Imperial Gallons u.i'.dall~ns·· Wtiigiit• Kg. Lbs. 3.72 7.2 ConvertingTo U:S. G,ll,llnS ConvertingTo Imp_e~i:ilGallons . ·convertingTo Liters 26% of theliter quantity 22% of the liter quantity 1.2 times the numberof ImperialGallons Figure I - 16 83%of the U.S. Gallon • quanjity 4.55 timesthe numberof ImperialGallons 3.•78 timesthe numberof U.S. Gallo11s ATMOSPHERIC PRESSURE RELATIONSHIPS {IN. HG AND HECTOPASCAL) In.Hg 27.70 27.75 27.80 27.85 27.90 27.95 28.00 28.05 28.10 28.15 28.20 28.25 28.30 28.35 28.40 28.45 28.50 28.55 28.60 28.65 RB050005 1-22 hPa 938 940 941 943 945 946 948 950 952 953 955 957 958 960 962 963 965 967 969 970 In. Hg 28.70 28.75 28.80 .. 28.85 28.90 28.95 29.00 29.05 29.10 29.15 29.20 29.25 29.30 29.35 29.40 29.45 29.50 29.55 29.60 29.65 .• Pressure hPa In.Hg hPa In. Hg hPa 972 29.70 1006 30.65 1038 974 29.75 1007 30.70 1040 975 29.80 1009 30.75 1041 977 29.85 1011 "30.80 1043 979 29.90 1013 30.85 1045 980 29.92 1013 30.90 1046 982 29.95 1014 30.95 1048 984 30.00 1016 31.00 1050 985 30.05 1018 31.05 1051 987 30.10 1019 31.10 1053 989 30.15 1021 31.15 1055 991 30.20 1023 31.20 1057 992 30.25 1024 31.25 1058 994 30.30 1026 31.30 1060 996 30.35 1028 31.35 1062 997 30.40 1029 31.40 1063 999 30.45 1031 31.45 1065 1001 30.50 1033 31.50 1067 1002 30.55 1035 31.55 1068 1004 30.60 1036 31.60 1070 Figure I - 17 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) TABLE OF CONTENTS Section 2 Limitations Section 2 Limitations INTRODUCTION .......................................................................................................................... 2-3 LIMITATIONS ............................................................................................................................... 2-4 Airspeed Limitation ............................................................................................................... 2-4 Airspeed Indicator Markings ................................................................................................. 2-4 Powcrplant Limitations ......................................................................................................... 2-5 Powcrplant Fuel and Oil Data ............................................................................................... 2-5 Oil Grades Recommended for Various Average Temperature Ranges ....................... 2-5 Oil Tcmpcraturc ............................................................................................................ 2-5 Oil Pressure ................................................................................................................... 2-5 Approved Fuel Grades .................................................................................................. 2-5 Fuel Flow and Fuel Pressure ........................................................................................ 2-5 Alternator Output Limitations ............................................................................................... 2-5 Powcrplant Gauge Markings ................................................................................................. 2-6 Propeller Data and Limitations .............................................................................................. 2-7 Propeller Diameters ...................................................................................................... 2-7 Propeller Blade Angles at 30 Inches Station Pressure ................................................. 2-7 Power Setting Limitations ..................................................................................................... 2-7 Weight Limits ........................................................................................................................ 2-7 Other Weight Limitations ...................................................................................................... 2-7 Center of Gravity Limits ....................................................................................................... 2-7 Center of Gravity Table ......................................................................................................... 2-8 Maneuvering Limits .............................................................................................................. 2-8 Utility Category ............................................................................................................ 2-8 Approved Acrobatic Maneuvers ........................................................................................... 2-8 Spins ....................................................................................................................................... 2-8 Flight Load Factor Limits ...................................................................................................... 2-9 Utility Category ............................................................................................................ 2-9 Kinds of Operation Limits and Pilot Requirements .............................................................. 2-9 Icing Conditions .................................................................................................................... 2-9 Fuel Limitations ................................................... :................................................................. 2-9 Garmin GI000 System Limitations .....,................................................................................. 2-9 Approach Operation Limitations ................................................................................ 2-11 SafcTaxi Limitations .................................................................................................. 2-I I Wide Arca Augmentation System (WAAS) Limitations ........................................... 2-11 GTX 33 Mode S Transponder Limitations ......................................................................... 2-12 Garmin GFC 700 Automatic Flight Control System Limitations ....................................... 2-12 Oxygen Limitations ............................................................................................................. 2-12 Ryan Model 9900BX TCAD Limitations ........................................................................... 2-13 Other Limitations ................................................................................................................. 2-14 Altitude ....................................................................................................................... 2-14 Flap Limitations .......................................................................................................... 2-14 Passenger Seating Capacity ........................................................................................ 2-14 Rudder Limiter ........................................................................................................... 2-14 PLACARDS .................................................................................................................................. 2-15 General ................................................................................................................................. 2-15 Interior Placards ................................................................................................................... 2-15 Exterior Placards .................................................................................................................. 2-21 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 2-1 Section 2 Limitations RB050005 2-2 Cessna 350 (LC42-550FG) This Page Intentionally Left Blank Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) Section 2 Limitations Section 2 Limitations INTRODUCTION Section 2 contains the operating limitations of this airplane. TI1eFederal Aviation Agency approves the limitations included in this Section. These include operating limitations, instrument markings, and basic placards necessary for the safe operation of the airplane, the airplane's engine, the airplane's standard systems, and the airplane's standard equipment. NOTE This section covers limitations associated with the standard systems and equipment in the airplane. Refer to Section 9 for amended operating procedures, limitations, and related performance data for equipment installed via an STC. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 2-3 Section 2 Limitations AIRSPEEDLIMITATIONS Cessna 350 (LC42-550FG) LIMITATIONS The airspeed limitations below arc based on the maximum gross takeoff weight of 3400 lbs ( 1542 kg). The maximum operating maneuvering speeds (V0 ) and applicable gross weight limitations arc shown in Figure 2 - I. SPEED KCAS KIAS, REMARKS Max. Operating Maneuvering Speed Do not apply full or abrupt control movements Vo 2500 Pounds Gross Weight 128 127 above this speed. 3400 Pounds Gross Weight 149 148 VFE Maximum Flap Extended Speed 120 119 Do not exceed this speed with full flaps. Takeoff ' , (Down or 40° Flap Setting) flaps can be extende.d at 130 KCAS (129 KIAS). Max. Structural Cruising Speed Do not exceed this speed except in smooth air V,-o *Decrease 4 knots for each I 000-ft 180* 179* and then only with caution. above 12,000 feet (Press. Alt.) Neve; Exceed Speed v~'E *Decrease 5 knots for each 1000-ft 235* 235* Do not exceed this speed in any operation. above 12,000 feet (Press. Alt.) Figure 2 - 1 AIRSPEED INDICATOR MARKINGS The airspeed is shown on both the PFD and backup airspeed indicator. The airspeed on the PFD is indicated with an airspeed tape and colored bands (see discussion in Section 7). The outer circumference of the backup airspeed indicator has four colored arcs. The meaning and range of each arc is tabulated in Figure 2 - 2. MARKING White Arc Green Arc Yellow Arc Red Line RB050005 2-4 KIASVALUE ORRANGE 57 - 119 71 • 179 179-235 235 SIGNIFICANCE Full Flap Operating Range - Lower limit is maximum weight stalling speed in the landing configuration. Upper limit is maximum speed pennissible with flaps extended. Nonna! Operating Range - Lower limit is maximum weight stalfing speed· . •with flaps-retracted. Upp~r limit _ismaximum structural£_ruisingspeed. Operations must be conducted with caution and only in smooth air. Maximum speed for all operations Figure 2 - 2 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) POWERPLANT LIMITATIONS Number of Engines: One (I) Engine Manufacturer: Teledyne Continental Engine Model Number: 1O-550-N Recommended Time Between Overhaul: 2000 Hours (Time in Service) Maximum Power: 310 BHP at 2700 RPM Maximum Manifold Pressure: Full power at sea level Maximum Recommended Cruise: 248 BHP (80%) Maximum Cylinder Head Temperature: 460°F (238°C) POWERPLANT FUEL AND OIL DATA Oil Grades Recommended for Various Average Air Temperature Ranges Below 40°F (4°C)-SAE 30, I0W30, 15W50, or 20W50 Above 40°F (4°C)- SAE 50, 15W50, 20W/50, or 20W60 Oil Temperature Maximum Allowable: 240°F ( I I 6°C) Recommended takeoff minimum: 100°F (38°C) Recommended flight operations: 170°F to 200°F (77°C to 93°C) Oil Pressures Normal Operations: 30-60 psi (pounds per square inch) Idle, minimum: IO psi Maximum allowable (cold oil): 100 psi Approved Fuel Grades IO0LL Grade Aviation Fuel (Blue) 100 Grade Aviation Fuel (Green) Fuel Flow and Fuel Pressure Normal Operations: IO to 22 GPH (38 to 83 LPH) (7 to 16 psi) Idle, minimum: I to 2 GPH (3.8 to 7.6 LPH) (4 psi) Maximum allowable: 28 GPH (106 LPH) (22 psi) ALTERNATOR OUTPUT LIMITATIONS Section 2 Limitations At altitude above 12,000 ft., with high angle of attack, and low airspeeds the alternator outputs arc limited as shown below. Left, belt driven alternator: Kelly Aerospace alternator: 65 amp Plane Power alternator: 70 amp Right, gear driven alternator: 52 amp Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 2-5 Section 2 Limitations POWERPLANT GAUGE MARKINGS Cessna 350 (LC42-550FG) The following table; Figure 2 - 3, shows applicable color-coded ranges for the various powerplant gauges displayed on the MFD. Green Arc - Nonna\ operating range. Red Line or Arc - Operation within the red line or arc is prohibited by the engine manufacturer. Yellow Arc -Operation within the yellow arc is permitted for a limited time during normal operations such as at idle, warm-up, and take-off. Also indicates precautionary zones where operation should be minimized by pilot action. White Arc - Operation within the white arc is permitted, take-off RPM for example. Extended operation in the white arc may reduce the engine's ability to reach Time Between Overhaul (TBO). GAUGE Tachometer Manifold ,Pressμrc Oil Temperature Oil Pressure Fuel Quantity Fuel Flow Cylinder Head Temperature RB050005 2-6 REDLINE Minimum Limit Minimum for idle 600RPM Minimum for idle JOpsi A red line at '"zero"indicates the remaining four gallons (SIN 42502 to 4 2567), or two gallons (SIN 42568 and on), in each tank cannot be used safely in flight YELLOW/ GREEN ARC YELLOW/ REDLINE WHITE ARC Normal WHITE ARC Limit Operating 2000 - 2500 RPM 2500 - 2700 RPM 2700-3000 RPM IO - 30 Inches Hg 100°F- 170°F l 70°F - 220°F 220°F - 240°F 240°F - 250°F (38°C - 77°C) (77°C - I 04°C) (104°C- 116°C) (116°C-121°C) lOOpsi 10-30psi 30 - 60 psi (Cold Oil) 10-22GPH 28GPH (38-83 LPH) (10<5,l,PH) I 00°F - 240°F 240°F - 420°F 420°F - 460°F 460°F - 500°F (38°C-116°C) (116°C-216°C) (216°C - 238°C) (238°C - 260°C) Figure 2 - 3 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 Cessna 350 (LC42-550FG) PROPELLER DATA AND LIMITATIONS Number of Propellers: I Propeller Manufacturer: Hartzell Propeller, Inc. Hartzell Propeller Hub and Blade Model Numbers: PHC-J3YF-IRF and F769ID-1 Propeller Diameters Minimum: 76 in. (193.cm) Maximum: 77 in. (196 cm) Propeller Blade Angle at 30 inch Station Low: 14.1°±0.2° High: 34.7° ± 1.0° POWER SETTING LIMITATIONS Section 2 Limitations Do not exceed 20 inches of Hg of manifold pressure below 2200 RPM. This requirement is not an engine limitation, but rather a propeller harmonic condition inherent in the Cessna 350 (LC42- 550FG). WEIGHT LIMITS Utility Category Maximum Ramp Weight: Maximum Empty Weight: Maximum Takeoff Weight: Maximum Landing Weight: Maximum Baggage Weight:* 3400 lbs. (I 542 kg) 2568 lbs. (I I 65 kg) 3400 lbs. ( 1542 kg) 3230 lbs. {I465 kg) 120 lbs. (54.4 kg) *The baggage compartment has two areas, the main area and the hat rack area. The combined weight in these areas cannot exceed 120 pounds (54.4 kg). The main area is centered at station 166.6 with maximum weight allowance of 120 pounds (54.4 kg). The hat rack area, which is centered at station 199.8, has a maximum weight allowance of20 pounds (9.1 kg). When loading baggage in the main baggage compartment, Zone A (the forward portion of the main baggage area) must always be loaded first. Sec page 6-13 for a table ofloading stations and baggage zones. OTHER WEIGHT LIMITATIONS TYPE OF WEIGHT FORWARDDATUM •AFT DATUM POINT VARIATION LIMITATION POINTAND WEIGHT AND WEIGHT Minimum Flying Weight I 03 inches and 2240 lbs. I IO inches and 2500 lbs. Straight Line Maximum Zero Fuel Weight 103 inches and 2725 lbs. 110 inches and 3228 lbs. Straight Line ReferenceDatum:The referencedatum is locatednear the tip of the propellerspinner.As distancefrom the datum increases, there is an increase in weight for each of the two limi_tationcategories. The variationis linearor straightline from the fore to the aft positions. • Figure2-4 CENTER OF GRAVITY LIMITS Figure 2 - 5 specifies the center of gravity limits for utility category operations. The variation along the arm between the forward and aft datum points is linear or straight line. The straight-line variation means that at any given point along the arm, an increase in moments changes directly according to the variations in weight and distance from the datum. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 2-7 Section 2 Limitations Cessna 350 (LC42-550FG) CENTER OF GRAVITY TABLE CATEGORY Utility Category FORWARDDATUM POINTAND WEIGHT I 03 inches - 2240 to 2500 lbs. I 07 inches - 3400 lbs. AFT DATUMPOINT AND WEIGHT 110 inches 2500 to 3400 lbs. VARIATION Straight Line Reference Datum: The reference datum is located at the tip of the propeller spinner. This location causes all arm distances and moments (the product of arm and weight) to be positive values. Figure 2 -5 MANEUVER LIMITS Utility Category - This airplane is certified in the utility category. Only the acrobatic maneuvers shown in Figure 2 - 6 arc approved. APPROVED ACROBATIC MANEUVERS MANEUVER ENTRY SPEED Chandelles 150 KIAS Lazy Eights 150 KIAS Steep Tums 150 KIAS Stalls Slow Deceleration* * Ensure that maximum fuel imbalance does not exceed 10 gallons (38 L). SPINS PROHIBITED Figure 2 - 6 While there are no limitations to the performance of the acrobatic maneuvers listed in Figure 2 - 6, it is important to remember that the airplane accelerates quite rapidly in a nose down attitude, such as when performing a lazy eight. SPINS The airplane, as certified by the Federal Aviation Agency, is not approved for spins of any duration. During the flight test phase of the airplane's certification, spins and/or spin recovery techniques were not performed or demonstrated. It is not known if the airplane will recover from a spin. !WARNING! Do not attempt to spin the airplane under any circumstances. The airplane, as certified by the Federal Aviation Agency, is not approved for spins of any duration. During the flight test phase of the airplane's certification, spins were not performed. It is not known if the airplane will recover from a spin. RB050005 2-8 Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: 1/10-22-2008 Cessna 350 (LC42-550FG) FLIGHT LOAD FACTOR LIMITS Utility Category - Maximum flight load factors for all weights are: Flaps Position Up (Cruise Position) Down (Landing Position) Max. Load Factor +4.4g and -l.76g +2.0g and -0.0g KINDS OF OPERATION LIMITS AND PILOT REQUIREMENTS Section 2 Limitations The airplane has the necessary equipment available and is certified for daytime and nighttime VFR and !FR operations with only one pilot. The operational minimum equipment and instrumentation for the kinds of operation arc detailed in Part 91 of the FARs. ICING CONDITIONS Flight into known icing is prohibited. FUEL LIMITATIONS Total Capacity: 106 US Gallons (401 L) Total Capacity Each tank: 53 US Gallons (201 L) Maximum Fuel Imbalance: IO gallons US (38 L) between left and right fuel tanks Total Usable Fuel SIN 42502 to 42567 49 Gallons US (I 86 L)/Tank, 98 Gallons US (371 L) Total SIN 42568 and on Standard: 43 Gallons US (163 L)/Tank, 86 Gallons US (326 L) Total Long Range: 51 Gallons US (193 L)/Tank, 102 Gallons US (386 L) Total GARMIN G1000 SYSTEM LIMITATIONS I. The GI000 must utilize the following or later FAA approved software versions: Sub-System Software Version PFD 6.13 MFD 6.13 COM 7.00 GCU 2.01 GDC 2.05 GMA 2.1 I GDL 3.02.00 GMU 2.01 GIA 4.50 GEA 2.07 GPS 3.03 GRS 2.06 GSA 2.09 GTA 2.01 The database version is displayed on the MFD power-up page immediately after system power- up and must be acknowledged. The remaining system software versions can be verified on the AUX group sub-page 5, "AUX- SYSTEM STATUS". 2. !FR enroute, oceanic and terminal navigation predicated upon the GI000 GPS Receiver is prohibited unless the pilot verifies the currency of the database or verifies each selected waypoint for accuracy by reference to current approved navigation data. Initial Issue of Manual: December 9, 2005 Latest Revision Level/Date: H/03-20-2008 RB050005 2-9 Section 2 Limitations Cessna 350 (LC42-550FG) 3. Instrument approach navigation predicated upon the G 1000 GPS Receiver must be accomplished in accordance with approved instrument approach procedures that arc retrieved from the GPS equipment database. The GPS equipment database must incorporate the current update cycle or be verified for accuracy using current approved navigation data. a. Instrument approaches utilizing the GPS receiver must be conducted in the approach mode and Receiver Autonomous Integrity Monitoring (RAIM) must be available at the Final Approach Fix. b. Accomplishment of!LS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for GPS overlay using GPS for lateral guidance on the final approach segment is not authorized .. c. Use of the GI 000 VOR/ILS receiver to fly approaches not approved for GPS require VOR/ILS navigation data to be valid on the PFD display. d. When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS navigation, the aircraft must have the operational equipment capable of using that navigation aid, and the required navigation aid must be operational. e. VNA V information may be utilized for advisory infonnation only. Use of VNAV information for Instrument Approach Procedures does not guarantee step-down fix altitude protection, or arrival at approach minimums in nonnal position to land. VNAV also does not guarantee compliance with intermediate altitude constraints between the top of descent and the waypoint where the VNAV path tenninates in tenninal or enroute operations. 4. If not previously defined, the following default settings must be made in the "SYSTEM SETUP" menu of the GI 000 prior to operation (refer to Pilot's Cockpit Reference Guide for procedure if necessary): n a. DIS, SPD m kt (sets navigation units to "nautical miles" and "knots") b. ALT, VS ft fpm (sets altitude units to "feet" and "feet per minute") c. MAP DATUM WGS 84 (sets map