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FLIGHT MANUAL

C-141CUSAF SERIES AIRCRAFT

NOTE: PERFORMANCE DATA IS CONTAINED IN TO 1C-141B-1-1SEE TECHNICAL ORDER INDEX TO 0-1-1-3 AND ITS SUPPLEMENTS FOR CURRENT STATUSOF FLIGHT MANUALS, SAFETY SUPPLEMENTS, OPERATIONAL SUPPLEMENTS, AND FLIGHTCREW CHECKLISTS.COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTIONOF ALL AIR FORCE PERSONNEL CLEARED FOR OPERATION OF SUBJECT AIRCRAFT.THIS PUBLICATION SUPERSEDED TO 1C-141C-1SS-3; TO 1C-141C-1SS-4; TO 1C-141C-1SS-5; TO1C-141C-1SS-6; TO 1C-141C-1SS-9; TO 1C-141C-1SS-10; TO 1C-141C-1SS-11; TO 1C-141C-1SS-12;AND TO 1C-141C-1SS-12 ERRATA IN CHANGE 1 DATED, 17 OCTOBER 2001. TO 1C-141C-1SS-7WAS SUPERCEDED BY TO 1C-141C-1SS-12, AND TO 1C-141C-1SS-8 HAS BEEN RESCINDED.DISTRIBUTION STATEMENT - Distribution authorized to the Department of Defense and U.S. DoD

( > contractors only (Administrative or Operational Use) (1 August 2002). Other requests for thisw document shall be referred to WR-ALC/LJET, Robins AFB GA 31098

WARNING - This document contains technical data whose export is restricted by the Arms Exportft Control Act (Title 22, U.S.C., Sec. 2751 et seq.) or the Export Administration Act of 1979, as|| amended (Title 50, U.S.C., App. 2401 et seq.). Violations of these export laws are subject to^ s e v e r e c r i m i n a l p e n a l t i e s .

HANDLING AND DESTRUCTION NOTICE - Comply with the distribution statement and destroy byQ any method that will prevent disclosure of the contents or reconstruction of the document.

PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE AIR FORCE

23 AUGUST 1999CHANGE 2-1 AUGUST 2002

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USAF

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<£&?TABLE OF CONTENTS

SECTION I D E S C R I P T I O N A N D O P E R AT I O N 1 - 1

SECTION II N O R M A L P R O C E D U R E S 2 - 1

SECTION III E M E R G E N C Y P R O C E D U R E S 3 - 1

SECTION IV C R E W D U T I E S 4 - 1

% ^ SECTION V O P E R A T I N G L I M I T A T I O N S 5 - 1

^ / 'SECTION VI F L I G H T C H A R A C T E R I S T I C S 6 - 1

SECTION VI I ADVERSE WEATHER OPERATIONS 7-1

APPENDIX I PERFORMANCE DATA SEE TO 1C-141B-1-1

INDEX A L P H A B E T I C A L I N D E X - 1

T01C-141C-1

Read Carefully Don't Learn By Accident

D304970ISCOPE.This manual contains information which will provide you with a general knowledge of the aircraft, its characteristics,and specific normal operating procedures. Your flying experience is recognized; therefore, basic flight principlesare avoided. Multiple emergencies, adverse weather, terrain or extenuating circumstances may require modificationof any procedure(s) presented in this manual.

PERMISSIBLE OPERATIONS.The flight manual takes a positive approach and normally states only what you can do. Unusual operations orconfigurations which exceed the limitations as specified in this manual must be approved, through Commandchannels, by the flight manual manager (WR-ALC/LFLET). Clearance must be obtained from the Major Command(with information to the flight manual manager) before any questionable operation is attempted which is not specifically permitted in this manual.

In some cases, the limits and tolerances presented in the flight manual are not precisely identical to those presentedin the maintenance manuals. The numerical values in the flight manual are to be used as operating guides byflight personnel.

HOW TO BE ASSURED OF HAVING LATEST DATA.

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You must be constantly aware of the latest manual, checklist and status of supplements. The latest formal supplement(safety or operational) will have a supplement status page which provides the current status of your flight manual.If you should have any doubts concerning the status of your flight manual, check with your flight manual distributionofficer.

TO 1C-141C-1

SAFETY AND OPERATIONAL SUPPLEMENTS.Safety supplements are issued as an expeditious means of reflecting safety information when hazardous safetyconditions exist. These supplements contain operational, precautionary and restrictive instructions that affect safetyand safety modifications. Operational supplements are issued as an expeditious means of reflecting informationwhen mission essential operational procedures are involved. Supplements are issued by teletype (interim) or byprinted copy (formal) depending upon the urgency. Interim supplements are formalized and replaced with a newnumber within 30 days. Formal printed supplements are identified by red letters "SS" for safety supplementsand black letters "OS" for operational supplements printed around the borders of the title pages. In accordancewith TO 00-5-1, both Safety and Operational supplements are numbered sequentially using the same block numbers.They will be filed in reverse numerical sequence in front of the manual. The flyleaf page will be retained withsupplements until rescinded or incorporated.CHECKLISTS.The flight manual contains amplified normal and emergency procedures. Checklists contain these procedures inabbreviated form and are issued as separate technical orders. Line items in the flight manual and checklists areidentical with respect to arrangement and item number. If authorized by an interim safety operational supplementthat affects a checklist, write in the applicable change on the affected checklist Within 40 days, a formal supplementwill be issued with the revised checklist page attached.HOW TO GET PERSONAL COPIES.Each flight crewmember is entitled to personal copies of the Flight Manual, Safety Supplements, and Checklists.The required quantities should be ordered before you need them to assure their prompt receipt. Check with yourpublications personnel; it is their job to fulfill your Technical Order requests. Basically, you must order the requiredquantities on the Publication Requirements Table (TO 0-1-1-3). Technical order 00-5-2 gives detailed informationfor properly ordering these publications. Make sure a system is established at your base to deliver these publicationsto the flight crews immediately upon receipt.FLIGHT MANUAL BINDERS.Looseleaf binders and sectionalized tabs are available for use with your manual. They are obtained through localpurchase procedures and are listed in the Federal Supply Schedule (FSC Group 75, Office Supplies Part I). Checkwith your supply personnel for assistance in procuring these items.DEFINITIONS.The following definitions apply to the use of the words "shall," "will," "should," and "may."

shall - Construed to mean that the requirements are binding or mandatory.

will - Construed to mean that the requirements are binding or mandatory.

should - Used to express a non-mandatory desire or preferred method of accomplishment, and shall be construedas a non-mandatory provision.

may - Used to express an acceptable or suggested means of accomplishment and shall be construed as a non-mandatoryprovision.

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WARNINGS, CAUTIONS, AND NOTES.Warnings, Cautions and Notes will always appear in the text where appropriate and will always follow the numberedline items (steps or procedures) and/or amplifications to which they apply.

The following definitions apply to "Warnings," "Cautions" and "Notes" found throughout the manual.

WARNING

Operating procedures, techniques, etc., which could result in personal injury orloss of life if not carefully followed.

In Sections II, III, and IV, capital letters enclosed by quotation marks are reserved for spoken responses. Switchand control positions are shown in capital letters without quotation marks, items being operated arc shown withinitial capital letters only, while the crew member making the spoken response is identified by an abbreviationin parentheses.

Example:Windshield Heat - "OFF" (CP)

If an item is normally identified by a capitalized abbreviation, such as CADC, MTC, APU, etc., this identificationis used.

Example:APU Control Switch - START/RUN

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Operating procedures, techniques, etc., which could result in damage to equipmentif not carefully followed.

NOTEAn operating procedure, technique, etc., which it is considered necessary to emphasize.

U S E O F C A P I T A L L E T T E R S A N D Q U O T A T I O N M A R K S . ^

In Section I of this manual, where most of the descriptive material is located, control or switch positions areidentified by the use of capital letters reflecting the identification visible in the aircraft, enclosed by quotation )marks, and the placarded name of the item is shown in capital letters without quotation marks. v ^J

Example:

T h e t h r o t t l e i s m o v e d t o " I D L E S T A R T * p o s i t i o n , J

The unmarked neutral position of certain switches, when mentioned specifically, is identified by capital letterswithout quotation marks.

Example:

The switch is placed successively in the "NORM" and OFF positions

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EFFECTIVITY.

This manual incorporates TCTO 1C-141B-541 and TCTO 1C-141-768 and pertains to the following 62 tail numbers: |

63-8080,63-8084,63-8085,64-0614,64-0620,64-0622,64-0627,64-0632,64-0637,64-0640,64-0645,65-0216,65-0222, |65-0225,65-0226,65-0229,65-0232,65-0237,65-0245,65-0248,65-0249,65-0250,65-0256,65-0258,65-0261,65-0271,65-9409,65-9412,65-9414,66-0130,65-0132,66-0134,66-0136,66-0139,66-0148,66-0151,66-0152,664)153,66-0157,66-0164,66-0167,664174,664)177,66-0181,66-0182,66-0185,664)190,66-0191,66-0193,66-0201,66-7950,66-7952,66-7953, 66-7954, 66-7957, 66-7959, 67-0015, 67-0021, 67-0024, 67-0027, 67-0029, 67-0031

TIME COMPLIANCE TECHNICAL ORDERS.

The following Time Compliance Technical Orders have been incorporated in this manual.

N U M B E R T I T L E

1C-141-542 INSTALLATION OF AN/ALE-47 COUNTERMEASURES DISPENSING SYSTEM ANDAN/AAR-47 MISSILE WARNING SET.

1C-141-550 REPLACEMENT OF NO. 1 KY-75 (PARK-HILL COMSEC EQUIP.) WITH ADVANCEDNARROWBANDDIGITAL VOICETERMINAL ON C-141B AIRCRAFT.

1C-141-555 INSTAIlAl!ONOFL-BANDSATELIJriECOMMUM(^TIONSYSONC-141AmCRAFr.

1C-141-559 INSTAIIATIONOFSECONDOOMFORTPAIiCTRECBPTACLE.1C-141-576 INSTAUATIONOFSEIJBCITvT3CALL(SELCAL) ONC-141 AIRCRAFT.

1C-141-763 FUELQUANT1TYINDICATIONSYS REPLACEMENT.1C-141-768 INSTAUATIONOFALLWEATHERFUGHTCONTROLSYSTEM/GCASONC-MIAIRC^^

1C-141-801 REMOVERADIORECEIVER-TRANSMITrBRRT-1341 (V)3/5 ANZARC-190 AND REPLACEWITH RT-1341 (V) 8 AN/ARC-190 ON C-141 AIRCRAFT.

1C-141B-520 INSTALIATIONOFFIRSINTEGRAT10NOFAN/APN-169ENHANC^1C-141B-541 mSTAIlATIONOFGLOBALPOSmONINGSYSTEMENHANCEDNAVIGATIONSYSTEM

ONC-141 AIRCRAFT.1C-141B-588 INSTALLAllONOFTRAIMCALBRTANDCOLIJSIONAVOmANCESYSTEMANDINCT

LATIONOFTERRAIN AWARENESS AND WARNING SYSTEM, C-141C AIRCRAFT.IC-141-853 REMOVALOFMODES/IFFAPX-100CONTROLPANEL,PARTNUMBBR4070741-0506AND

INSTAIIATIONOFMODES/nTAPX-100CONTROLPANEL,PARTNUMBER4070741-0507AND REMOVAL OF MODE S/IFF APX-100 TANSPONDER, PART NUMBER 4070740-0508AND INSTALLATION OFMODE S/OFF APX-IOOTRANSPONDER, PARTNUMBER4070740-0510 ON C-141B/C AIRCRAFT.

YOUR RESPONSIBILITY TO LET US KNOW.

Every effort is made to keep the Flight Manual current Review conferences with operating personnel and a constant reviewof accident and flight test reports assure inclusion of the latest data in the manual. However, we cannot correct an error unlesswe know of its existence. La this regard, it is essential that you do your part Comments, corrections, and questions regardingthis manual or any phase of the Flight Manual program are welcomed. These should be submitted in accordance with API11-215 and forwarded through your Command Headquarters to Warner Robins Air Logistics Center, Robins AFB, Georgia31098, Attn: UET.

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GLOSSARY OF TERMS.

CUSTOM DATABASE - All database files contained in theNP, except the Navigation Database.

NAVTGATIONDATABASE - The Navigation database forwhich the identifier is displayed on the Power-Up page.

I

J=AAAAAAAABA/CACCACSACTADCADDRADFADIADSADU.ABCAECC

AEOO

AERP

AETAFCPAFCSAHDAHRSAIAI/ONAIUATALEALOGALTALTNA MAMLCD

Not equal toAltitudeAbsolute AltitudeAir-to-AirAt or AboveAt or BelowAir ConditioningAccuracy Warning AnnunciatorAutomatic Communications SystemActiveAir Data ComputerAddressAutomatic Direction FinderAttitude Director IndicatorAirdrop SystemAir Data UnitAeromedical Evacuation CrewAeromedical Evacuation ControlCenterAeromedical Evacuation OperationsOfficerAircrew Eye and RespiratoryProtectionAeromedical Evacuation TechnicianAutomatic Flight Control ProcessorAutomatic Flight Control SystemAheadAttitude Heading Reference SystemAnti-iceAnti-ice <onAuxiliary Interface UnitAnti-JamAutomatic Link EstablishmentAnalogAltitudeAlternateAmplitude ModulationActive Matrix Liquid Crystal Display

ANDVT Advanced Narrowband Digital VoiceTerminal

A N G A n g l eA N N U N C A n n u n c i a t o rA D A A n g l e o f A t t a c kA P A u t o p i l o tA P P A p p r o a c hA P P R A p p r o a c hA P T A i r p o r tA P U A u x i l i a r y P o w e r U n i tA R R A r r i v a lA / S A i r s p e e dA / T A u t o t h r o t t l eA T A A c t u a l T i m e o f A r r i v a lAT C C A i r Tr a f fi c C o n t r o l C e n t e rATCRBS Air Traffic Control Radar Beacon

SystemATGL Ai r Transpor tab le Gal ley /LavatoryAT S A u t o m a t i c T h r o t t l e S y s t e mA U T O A u t o m a t i cA V A v i o n i c sA V A I L A v a i l a b l eAWLS A l l Weather Land ing Sys temB A L B a l l i s t i cB A R O B a r o m e t r i cBDHI Bearing Distance Heading IndicatorB H D B e h i n dB I T B u i l t - i n T e s tB I T E B u i l t - i n Te s t E q u i p m e n tB M A X B r a k i n g M a x i m u mB O D B o t t o m o f D e s c e n tB R G B e a r i n gBRGW Brake Release Gross WeightB T U B a r i c T e r m i n a l U n i tB U B a t t e r y U n i tC C e l s i u sC / A C o u r s e / A c q u i s i t i o nCADC Cen t ra l A i r Da ta Compute rC A L C C a l c u l a t e dCARA Combined Al t i tude Radar Al t imeter

SystemCARP Computed A i r Re lease Po in tC A R T C a r t r i d g eC A S C a l i b r a t e d A i r s p e e d

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C-BITCBCCBRecuCDICDSCDSCDU

ICEFSCFCFLCGCHAN

| C H KCICIVCLBCMCMDCMDSCMTC/N0

COMMCP

| C P ACPUCRCCRSCRZCSDCVRCWCWACWFSCWSDADADAMU

DBDCDECELDEPDESDESCDESEL

Continuous Built-in TestCDS Brightness ControlCalifornia Bearing RatioCockpit Control UnitCourse Deviation IndicatorContainer Delivery SystemControl Display SystemControl Display UnitCritical Engine Failure SpeedCourse to a FixCritical Field LengthCenter of GravityChannelCheckControl IndicatorCarousel IV INSClimbCOMSEC ModuleCommandCountermeasures Dispensing SetCharge Medical TechnicianCanier-to-Noise Power SpectralDensity RatioCommunicationCurved PathClosest Point of ApproachComputer Processing UnitCyclic Redundancy CheckCourseCruiseConstant Speed DriveCockpit Voice RecorderContinuous WaveCaution/Warning/AdvisoryColumn/Wheel Force SensorControl Wheel SteeringDescent AltitudeDescent AngleDisplay Avionics ManagementUnitDatabaseDirect ControlDecelerationDepartureDescentDescriptionDeselect

DESTDFDFDRDHDICUDIRDISABDISCDISTDIUDLDLRDLSDLYDMEDOMDPUDRDRFDROPDRPDRUDSPYDSRV

DTDDTGDTKDUDZDZESCEEAIECEFECONEEBD

EFCEGREGTEHEEHEELELEVELTEMBEMER

DestinationDirect to a FixDigital Flight Data RecorderDecision HeightDisplay Interface Control UnitDirectDisableDiscreteDistanceDisplay Interface UnitDownloadData Loader ReceptacleData Loader System

DelayDistance Measuring EquipmentDay-of-MonthDisplay Processor UnitDead ReckoningDriftDroppedDropData Receptacle UnitDisplayDeep Submergence RescueVehicleData Transfer DeviceDistance To GoDesired TrackDisplay UnitDrop ZoneDrop Zone EscapeEastEngine Anti-IceEarth-Centered Earth-FixedEconomyEmergency Escape BreathingDeviceExpect Further ClearanceEmbedded GPS ReceiverExhaust Gas TemperatureEstimated Heading ErrorEstimated Horizontal ErrorElectroluminescentElevationEmergency Locator TransmitterExpanded Memory BoardEmergency

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EMI Electro Magnetic Interference GPSD G r o u n d S p e e d |

| ENCDR Encoder GRAD Gradient

ENG Engine GRD Ground

| ENS Enhanced Navigation System GS GlideslopeEO Engine Out GS Ground SpeedEOD End of Descent GTRK Ground Track

EPOS Emergency Passenger Oxygen HoursSystem HA High Altitude

EPR Engine Pressure Ratio HARP High Altitude Release PointEQUIP Equipment HAT Height Above TouchdownEREO Emergency Retract Emergency Off HDG HeadingESC Escape HE Heavy EquipmentETA Estimated Time of Arrival HF High FrequencyETD Estimated Time of Departure HG MercuryETE Estimated Time Enroute HGT HeightETI Elapsed Time Indication HH High Altitude/High PowerETP Equal Time Point HIALTRF High Altitude Rate of FallEVI Engine Vibration Indicator HIST History

| E W P Emergency War Planning HP H e c t o P a s c a l 1F Fahrenheit HS Heading SelectFA Course from a Fix to an Altitude HSI Horizontal Situation IndicatorFAF Final Approach Fix HTR Turn RadiusFC Frequent Tracked/Tracking Code IAA Indicated Absolute AltitudeFCI Flight Command Indicator IAF Initial Approach FixFCP Flight Control Panel IAS Indicated AirspeedFCR Flight Command Repeater B IT Initiated Built-in TestFF Fuel Flow ICAO International Civil AviationFL Flight Level Organization

I n d e n t i fi e r 1FLC Flight Level Change IDFLT Flight ID Inner Diameter

I d e n t i f y / I d e n t i fi e r *FMS Flight Management System IDENTFMT Frequency Managed Training IDTK Instantaneous Desired TrackFN Flight Nurse IF Initial FixFOB Fuel on Board ILS Instrument Landing SystemFOD Foreign Object Damage ILSDME JLS/DMEFOM Figure of Merit IN InchesFP Flight Plan INAV Integrated NavigationFPM Feet per Minute INBD InboundFPS Feet per Second INDX Index

FQI Fuel Quantity Indicator INIT I n i t i a l i z a t i o n 1

FT Feet INS Inertia! Navigation System

FTD Forward Travel Distance INV Invalid

FTT Forward Travel Time INU Inertial Navigation Unit

G Grid DP Initial Point

| GAGPS

Go-Around ITA Indicated True Altitude

Global Positioning System ISA International Standard AtmosphereK Kilo (Thousand)

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K E Y B D K e y b o a r dK F D K e y fi l l D e v i c eK H Z K i l o h e r t zKNS Kalman Navigat ion Solut ionK T K n o tK V A K i l o v o l t - A m p e r eL A L o w A l t i t u d eLAT/LON Lati tude/LongitudeL B P o u n dL D R L e a d e rL G L o n gL B L L a b e lL D G L a n d i n gL L L a t i t u d e / L o n g i t u d e

| L I M L i m i t e rL G T H L e n g t hLNAV Lateral Navigation (or Lateral

Guidance)L O C L o c a l i z e rL Q A L i n k Q u a l i t y A n a l y s i sL R C L o n g R a n g e C r u i s eL R U L i n e R e p l a c e a b l e U n i tL S K L i n e S e l e c t K e yL T L e f tL V L L e v e lL Z L a n d i n g Z o n eLZ/NPA Landing Zone/Non-Precision

ApproachesM M i n u t e sMAC Mean Aerodynamic ChordMAG VAR Magnetic VariationM A I N T M a i n t e n a n c e

I M A N M a n u a lM A P M i s s e d A p p r o a c h P o i n tM A X M a x i m u mM B M i l l i b a r sMBIT Maintenance Bui l t - in TestM C M e d i c a l C r e wM C D M e d i c a l C r e w D i r e c t o rMDA Min imum Descen t A l t i t udeM D B M i s s i o n D a t a b a s eM D F M i s s i o n D a t a F i l eMFCDU Multi-function Control Display

UnitM F D M u l t i - f u n c t i o n D i s p l a yMFP Miss ion F l ight ParameterMFSI Multifunction Standby InstrumentMGRS Military Grid Reference SystemM H Z M e g a h e r t z

MIN ACCEL Minimum AccelerationML Master LostMLG Main Landing GearMLS Microwave Landing SystemMLSDME MLS/DMEMmo Maximum Allowable MachMOD ProvisionalMOPS Minimum Operational PerformanceMS ModeSMSL Mean Sea LevelMSN MissionMSP Mode Select PanelMSTR MasterMSU Mode Selector UnitMWOD Multiple-Word-of-DayMWS Missile Warning SystemN NorthNAR Non-Altitude ReportingNAV NavigationNDB Navigation DatabaseNDB Non-Directional BeaconNE NortheastNM Nautical MilesNOD Nurse of the DayNP Navigation ProcessorNPA Non-Precision ApproachNS Navigation SolutionNTA Number of TCAS-Equipped

AircraftNVG Night Vision GogglesNVIS Night Vision Imaging SystemNVM Non-Volatile MemoryNW NorthwestOAT Outside Air TemperatureOB OutboardOBS ObstacleOBSTR ObstructionOD Outer DiameterOPER OperationOPT OptimumPA Pressure AltitudePAV Pressure Altitude VariationPAYLD PayloadPBD Place/Bearing/DistancePBPB Place/Bearing/Place/BearingPDB Performance Data BasePER PersonnelPERF Peformance

Change 1 ix

TO 1C-141C-1

PFBIT Preflight Built-in-Test RTN R e t u r n |PFD Primary Flight Display RW RunwayPI Point of Impact RWYS RunwaysPIREPS Pilot Reports RZ RendezvousPOBIT Power-on Built-in Test SecondsPPOS Present Position SouthPPP Patient Positioning Plans SurfacePPS Precise Positioning System SAT Static Air TemperaturePREV Previous SCADC Standard Central Air Data ComPRS Position Reporting System puterPVT Position, Velocity, and Time SD Slow DownP-P Point-to-point SE Southeast

QFE Field Elevation Barometric Setting SEL SelectONE Standard Atmosphere Setting SELCAL Selective CallQNH MSL Barometric Setting SEQ SequenceQTY Quantity SFC Surface

QUAD Quadrant SFD Secondary Flight DisplayQUOT Quotient SH Short

I R A Resolution Advisory SID Standard Instrument Departure| r a Runway Available SIGMETS Significant Meteorological Infor

RAIM Receiver Autonomous Integrity mationMonitoring SKE Station Keeping Equipment

|ram Random Access Memory SLEN Slot EnableRCR Runway Condition Reading SN C/NoRCU Remote Control Unit SOC Start of ClimbRCVR Receiver SOP Speed On PitchRDR Rotary Function Switch SPD SpeedREC Receive SPO System Program Office■ REDI ref

Reduced EPR Takeoff SPR Single Point Refueling SystemReference SRCU Split Remote Control Unit

REFGS Reference Ground Speed SRS Software Requirements SpecificaREMAIN Remaining tion

IREQIrev

Required ST State

Reverse STAB S t a b i l i z e r |

RF Radio Frequency STAR Standard Terminal Arrival RouteS t a t u s ■R/G-A Rotation/Go-Around STAT

RNDZ Rendezvous STBY Standby

RNG Range STC Sensitivity Time ControlSet Prior To Brake Release TRT 1E P R T a k e o f f ■I R O T

| r rRotate STRT

Rain Removal SU Sensor UnitRSC Runway Surface Covering SV Satellite NumberRSP Reference Set Panel SVS Secure Voice SystemRSS Root Sum Square SW SouthwestRT Receiver-Transmitter TerminalRT Right TrueRTA Required Time of ArrivalRTE Route TA T r a f fi c A l e r t |

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| TATACAN

L |

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TCAS

TASTAWS

TAVTDTDZETEKTEMPTFTHR

I TLSTOTOATOCTODTODTOLDTOTT-OUTTPTRTRANSTR-RECTRTTSPTTFFTTG

| TWTWSUARRSI

UHFUPSURUTCUTMVAVALIVAPPVHFVMCA

True AltitudeTactical Air NavigationTraffic Alert and CollisionAvoidance SystemTrue AirspeedTerrain Awareness and WarningSystemTemperature Altitude VariationTouchdownTouchdown Zone ElevationTraffic Encryption KeyTemperatureTrack to a FixThresholdTire Limit SpeedTakeoffTime of ArrivalTop of ClimbTime of DayTop of DescentTakeoff and Landing DataTime Over TargetTime OutTurn PointTransformer RectifierTransitionTransmit-ReceiveTakeoff Rated ThrustThrust Speed ParameterTime to First FixTime to GoTailwindTrack-While-ScanUniversal Aerial RefuelingReceptacle SlipwayInstallationUltra High FrequencyUniversal Polar StereographicUnrestrictedUniversal Time CoordinatesUniversal Transversal MercatorHeading from a Fix to an AltitudeVariable Altitude Limit IndexVelocity Approach SpeedVery High FrequencyVelocity Minimum ControlAirspeed

VMCG Velocity Minimum Control GroundSpeed

VMCO Velocity Minimum ClimboutSpeed

VMFR Velocity Minimum Flap RetractionSpeed

Vino Maximum Al lowable IndicatedAirspeed

VNAV Vertical Navigation (or VerticalGuidance)

V O R V H F O m n i - R a n g eV O R D M E V O R / D M EV O R TA C V O R / TA C A NV P T H V e r t i c a l P a t hV R O T R o t a t e A i r s p e e dV S I Ve r t i c a l S c a l e I n d i c a t o rV T K V e r t i c a l T r a c kVV I Ve r t i ca l Ve loc i t y I nd i ca to rW W e s tW A I W i n g A n t i - I c e |WGS-84 World Geodetic System 1984W O D W o r d - o f - D a yW O W W e i g h t o n W h e e l sW P / W P T W a y p o i n tWSE Waypoint Select Page Exclusion |W T W e i g h tW/V/L Wind Bearing/Wind Speed/Wind

LimitX C r o s sX F E R T r a n s f e rXTK/XTRK CrosstrackX W C r o s s w i n d IZ F W Z e r o F u e l W e i g h tZ M Z o n e M a r k e r

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