p

Equipped with the Metro Aviation, Inc. 

EMERGENCY MEDICAL Y TEM 

Kit No. 155M-I 00 

Document No.: RFM 155M- I 00 

Rev.:!\ 

Date: 05 Oct 20 12 

REGI TRATIONNO.: ____ _ 

ERIAL NO.: ___ _ 

Please visit the Metro Aviation Product upport website at 

""" .mctroproduct'>upport.com for the latest revision of thi manual. 

This supplement must be attached to the ECF/FAA approved Rotorcraft Flight Manual. The Metro 

Aviation, Inc., Emergency Medical Sy tem Kit No. 155M-100 is installed in accordance with TC NO. 

R0959 1 RC. The information contained herein supplements or supersedes the basic Rotorcraft Flight 

Manual only in those areas listed. For limitations, procedures, and performance information not 

contained in thi upplement, consult the ba ic Rotorcraft Flight Manual. 

FAAAPPROVED· 

-"J .. tcatAHo ~~rn / #oi!!::!J­ /f1" Acting Manager. Rotorcran Certifi cation Office 

Fort Worth. Te¥s 76 137-4298 

Date: Q= ..frJ bu- 2, 2.0 12.. 

- PIWPHIE'I i\R\' OTI 1111' lXKliMI N'l \NO l llr INI OR\1ATI0'< II[ RII'- IRL I'ROI'RII I IRY ll•\1 10 \Ill RO ~VI~ 110'. "-C 11\ll ,\I.L DF,IG' 11•\NIJI A( RI~G Rli'ROOl CliO!\, 11\F PAff"'l 

KIC.In '> 11\ll :,.\II·' II.IGIII RI•(;,IRI>I"'t.lll[ q111 •IRI [XI'RI '51 Y Rl RVII) 1111\ D•ITA SLIO~IriHD l "-DER ( ONHDI·!\1 1<\1 RH A 110''>1 111' I ()R A C'IH\ RI'O~l I ND 'flniFR l.)()(l \II Vf '0R 1111 1"1 ()It~ I•\ liON ('ON I 'iNIIl I~ SIIAll U[ R[rRODLC"~D LSED OR ~C'I O~I 10 0 1111 RS 
IR 22 Dec 201 1 

A 05 Oct 20 12 

g

All 

7 

9 

16-17 

20 

25 

INITIAL R LEA E 

I. Revised 2.5(e) verbiage 

to include ''E'' size 

cylinder. 

2. Revised 2.5(1) to add 

PIN ISSM-400-2 

3. Revised 7.0 to add 

Mar1in Baker scats 

4. Revised 8.1 (k) verbiage 

to inc Jude ·•o·· or "E" 

size cylinder. 

5. Revised 8.1 (v) verbiage 

to include Martin Baker 

seats. 

Efrain E. Esparza 

By colt A. Horn 

Manager. 

Rotorcran Certification Orfiec 

For1 Worth, Texas 76193-0 170 

Date: December 22, 20 II 

c 

Acting Manager, 

Rotorcra rt Certification Orfice 

Fort ~:s 76 137-4298 

Date: a '.IH ~ 2Dl2.. 

U ISTC MANUALSIEC155\EMS\FMS\Current\To AGO RFMS 26 Jui2012\RFMS15SM-100A 05 Oct 2012.doc 2 of40 
1.0 

2.0 

3.0 

4.0 

5.0 

6.0 

7.0 

8.0 

9.0 

10.0 

Figure: I 

Figure:2 

F'igure:3 

RECORD OF REVISION 

TABLE OF CONTENTS 

GENERAL 

LIMITATION 

EM ERGENCY PROCEDURES 

NORMAL PROCEDURES 

PERFORMANC 

ELECTRICAL LOA DING 

WEIGHT /\N O BAL/\NC 

Y TEM FU CTIONALIOPERATION/\L DE CRIPTION 

EMS CONTROL SYSTEM OPERATION PROCEDURES 

PIVOTING LITTER SYSTEM OPERATION PROCEDURE 

FIGURE 

TROLLEY 

UPPER DECK 

GENERAL EM A RRANGEM ENT 

U:\STC MANUALSIEC1551EMS\FMS\Current\To ACO RFMS 26 Jui2012\RFMS155M-100A 05 Oct 2012.doc 

2 

3 

4 

4 

13 

13 

14 

15 

16 

18 

28 

36 

24 

24 

37 

3 of 40 
2.0 LIM ITATIONS 

2. 1 Equipment-Attendants/Pas engers-Patients: 

(a) Medical Equipment 

All equipment mu t be towed and/or secured in appropriate mounts or storage 

compartment during taxi, take-off and landing. 

(b) A ttcndants/Passenger 

All attendant/passenger eat must be locked in tracks during all phase of night. 

All attendant/passengers must remain in scats during all phases of night unless approved 

by pilot in command. 

All attendant/passengers in seats must be seated facing forward or aft. du ri ng taxi, takeoff and landing with safety belt and shoulder harness secured. 

(c) Pivoting Litter System (PL ) 

MedDeck 4x quick relea e pins mu t be installed during all phases of night. 

Aero led (litter) must be locked in position for taxi, take-ofT and landing unless 

movement approved by pilot in command. 

(d) Patients 

Occupant of litter mu t be po itioned head forward. and be ecured in harnesses during 

all phases of night. 

econd patient u ing the upplemental patient restraint must be positioned head lorward, 

remain on backboard and be secured in torso and leg restraints during all phases of flight 

per placard instructions in Para. 2.5. 

(c) upplemental Strobe Lights 

During Night or in IM C fl ight condilions. the trobe lights may cause reflections. which 

may affect the pi lot. The strobe lights must be switched off per placard instructions in 

Para. 2.5. 

U ISTC MANUALSIEC1551EMSIFMS\Current\To ACO RFMS 26 Jui 2012\RFMS155M-100A 05 Oct2012.doc 4 of40 
facing position For Taxi, Take-off and Landing. 

The two aft cabin (#3LII & #4RII) seats will be, locked in the fwd-facing position 

For Taxi. Take-off and Landing. 

NOTE 

Any seat or combination or eats may be removed as necessary to fac ilitate operations. 

(b) The (#4RH & #5RH) attcndant/pa enger seats shall be removed when nece sary to 

transport a econd patient u ing the supplementa l pati ent restraint. 

2.3 Flight Envelope Limits 

(a) This STC reduces the maximum seat/litter to less than nine. Therefore. the 

lleight/Vclocity diagram in the Rotorcraft Flight Manual is no longer a limitation and 

hould be u ed for performance planning as long as the aircrall remains in the TC 

configuration. 

2.4 Mass and Center of Gravity Limitations 

The helicopter empty weight shall be computed from the most current weight and balance 

info rmation and the fo llowing patient, attendant, and equipment locations. 

U:ISTC MANUALS\EC1551EMS\FMS\Current\To ACO RFMS 26 Jul 2012\RFMS155M· 100A 05 Oct 2012.doc 5 of 40 
(a) For blackout curtain PIN 155M- I 05- 1: 

BLACKOUT CURTA I REQUIRED FOR 

NVG NIGHT OPERATION 

UNLESS ALL PED ARE OFF OR 

DEMO TRATED NVG FRIENDLY 

Location: In full view of the pilot 

(b) For accessory bar mount PIN 155M- 129-I: 

WEIGHT OF ANY INGLE ITEM OF 

EQUIPME T NOT TO EXCEED 15 LBS. 

TOTAL BAR MOUNT WEIGHT NOT TO 

EXCEED 25 LB . EQUALLY PACED. 

MAX CG 4 INCHES FROM BAR MOUNT 

Location: Aft cabin bu lkhead adjacent to mount in plain view 

EQUIPME T M UST BE SECURED 

DURING ALL PHA E OF FLIGHT 

Location: Art cabin bulkhead adjacent to mount in plain vie\) 

(c) For fwd storage cabinet PIN 155M- 133-I : 

ORA WER M UST BE LATCIIED 

CLO ED FOR TAXI, 

TAKE-OFF, AND LANDING 

CONTENT OTTO 

EXCEED 10 LB 

Location: Fwd storage cabinet drawer face, 2 pl. in plain view 

WEBB! G MUST BE IN TALLED FOR 

TAXI. TAKE-OFF. AND LANDING 

LOWER TORAGE CONTE T NOT 

TO EXCEED 25 LB 

Location: Fwd storage cabinet in plai n view 

U:\STC MANUALSIEC1551EMS\FMS\Current\To ACO RFMS 26 Jul 2012\RFMS 155M·100A 05 Oct 2012.doc 6 of 40 
CONTENTS NOT TO 

EXCEED I 0 LBS 

Location: A ft cabin storage system door face, 2 pl. in plain view 

FOR LOWER STORAGE USAGE. WEBB! G MU T BE 

IN TALLED FOR TAXI, TAKE-OFF A D LANDING. 

LOWER TORAGE CONTENTS OT 

TO EXCEED 40 LB 

Location: Aft storage sy tem in plain view 

(d) For aft cargo net PIN 155M- 136- 1: 

CA RGO NOT TO 

EXCEED 150 LB 

Location: Adj acent to ex isting art baggage door ·'NET IS MANDATORY 

TO SE URE CARGO" placard 2pts 

(c) For portable oxygen mount PIN 155M- 140- I /-2: 

''D" or ·'E" izc cylinder only. All cylinders in tailed 

in this mount must meet the requirements of 49 CFR. 

part 171, 172 and 173 except 173.24 

(a)(l ). Max cylinder weight 15 lb each. 

Location: Fwd storage cabinet above mount in plain view 

(f) For loading light PIN 155M- 166- I : 

LOADING LIGIIT FOR 

GROUNDU EONLY 

Locat ion: Ceiling panel adjacent to l ight in plain view 

(g) For Venti lator M ount PIN I SSM - 198- 1 

EQUIPMENT MUST BE F.CURED 

DURING ALL PHA E OF FLIGHT 

Location: Ventilator mount in plain view 

U:\STC MANUALS\EC155\EMS\FMS\Current\To ACO RFMS 26 Jui2012\RFMS155M-100A 05 Oct2012.doc 

7 of 40 
, 

TIIROUGH CLOUD, FOG OR I lAZE. 

TANDARD PO ITION LIGHT TO BE 

ON FOR ALL NIGHT OPERATION 

(black w/silver letters) 

Location: Instrument panel in full view of the pilot 

(i) For upcr ightscanner searchlight P/N 155M- 195-I: 

CAUTION 

EXTENSION OF THE LANDING & EARCI-ILIGHT 

ABOVE 70 KNOT IS NOT RECOMM ENDED 

Location: Instrument panel in full view of the pilot 

(j) For pivoting litter system P/N 155M-300- 1: 

Location: Cabin overhead module in full view of crew 

OCCUPANT OF LITTER MU T BE I lEAD 

FWD AND SeCURED IN HARNE E 

DURI GALL PIIA E OF FLIGIIT 

Location: Cabin overhead module in full view of crew 

MED DECK QUICK RELE/1. E PIN 

MUST BE IN T/\ LLED DURI NG ALL 

PHASES OF OPERATION 

Location: Cabin overhead module in ful l view of crew 

U·ISTC MANUALSIEC 155\EMS\FMS\Current\To ACO RFMS 26 Jul 2012\RFMS 155M·100A 05 Oct 2012.doc 

8 of40 
~ 1. REMOVE #4 & #5 RH SEAT IF INSTALLED. 

2. PUT 4 POINT RESTRAINT BELT ENDS AND TRACK STUDS IN POSITION 

ON RH FLOOR TRACKS AND TORQUE CAP NUTS SNUG + 1/8 TURN. 

POSITION PADS OVER CAP NUTS. 

3. PUT LEG RESTRAINT TIE DOWN FITTINGS IN POSITION ON RH FLOOR 

TRACKS AND ENGAGE FITTING. 

4. POSITION PATIENT AT DESIRED LOCATION WITH HEAD FWD AND 

INSERT SHOULDER STRAPS AND LEG RESTRAINT THROUGH THE 

BACKBOARD ACCESS HOLES. PATIENT SHOULD BE SNUG AGAINST 

SHOULDER STRAPS SO THAT THE PATIENT CANNOT SLIDE FWD 

UNDER CRASH LOADS. 

5. SECURE PATIENT UPPER TORSO WITH 4 POINT RESTRAINT. 

6. SECURE PATIENT LOWER BODY WITH LEG RESTRAINT. 

Location: Upper right hand /\fl cabin bulkhead in full view of crew 

(I) For seating PIN ISSM-400-1 /-2: 

OCCUPANTS IN EAT MU T BE EATED 

FACING FWD OR AFT, DURING TAXI. 

TAKE-OFF OR LANDING WITH SAFETY 

BELT AND IIARNE ECURED 

EATS MU T BE LOCKED IN TRACKS 

DURI GALL PitA ES OF FLIGHT 

Location: Cabin overhead 1110dule in full view of crew 2 pies 

U.\STC MANUALS\EC155\EMS\FMS\Current\To ACO RFMS 26 Jui2012\RFMS155M-100A 05 Oct 2012.doc 9 of40 
Location: Equipment rack, accessory bar mount in plain view 

EQU IPMENT MU T BE ECUREO 

DURING ALL PHA E OF FLIGHT 

Location: Equipment rack, acce sory bar mount in pla in view 

(n) For LOX PIN 155M-640-I: 

NO STORAGE FWD OF 

LOX CONTAINER BOX 

(Green fi eld w/white letters) 

Location: LOX Box door in plain view 

CAUTION 

LIQUID OXYGEN VENT 

(Green fi eld w/whitc letters) 

Location: Right ide of aircraft adjacent to LOX vent in plain view 

CAUTION 

LOX INSIDE 

(Green fi eld w/whitc letters) 

Location: Right baggage compartment door in plain view 

CAUTI ON 

KEEP CLEAN, DRY 

AND FREE FROM OILS 

(Green field w/whitc letters) 

Location: LOX Box door in plain view 

U:ISTC MANUALSIEC155\EMS\FMS\Current\To ACO RFMS 26 Jui2012\RFMS155M-100A 05 Oct2012.doc 

I 0 of 40 
Location: Overhead module adjacent to switch in plain view 

(o) For remote equipment mount P/N ISSM-700-1: 

Location: torage system back panel in plain view 

(p) For IV Support P/N I SSM-8 10- 1: 

MAX WEJGIIT NOT TO 

EXCEED 10 LB 

Location: Cabin overhead module adjacent to IV support in plain view 

(q) For medical inverter electrical outlet P/N ISSM-900- 1: 

110 VAC 60Hz 

10 A MPS 

Location: Fwd storage cabinet and aft storage system adjacent to outlets 

CONNECT GROUND FAULT 

PROTECTED POWER 0 LY 

Location: Right side of aircraft fwd of boom adjacent to inverter ystcm external outlet 

(r) For shore power external/internal electrical outlets PIN ISSM-900- 1: 

GROUND USE ONLY 

11 0 VAC 6011z 

10 AMPS 

Location: Lower right hand aft cabin bulkhead adjacent to internal shore power outlet 

0 ECTGROUND FAULT 

PROTECTED POWER ONLY 

Location: Right side of aircraft fwd of boom adjacent to externa l shore power outlet 

U:\STC MANUALS\EC155\EMS\FMS\Curreni\To ACO RFMS 26 Jui2012\RFMS155M-100A 05 Oct 2012.doc II of40 
The Metro detachable Blackout urtain (MAl P/N 155M - I 050- 1) must be installed during night 

operations, un less the aft cabin has been demonstrated to be NVG compliant and all carry-on 

equipment has al so been demonstrated not to cause interference when N ight Vision goggles are 

in u e by night crew or only approved N VI cabin lighting is util ized during NVG operations. 

Operation of suction pump over I 04° F OAT prohibited. 

Operation or air pump over I 04° F OAT prohibited. 

U:\STC MANUALS\EC155\EMS\FMS\Current\To ACO RFMS 26 Jul 2012\RFMS155M·100A 05 Oct2012.doc 12 of 40 
(2) Land as soon as possible. 

3.2 Loss of Engine Power 

( I) All non-essentia l li ghts and EM equipment arc shed automatically in this aircraft on loss 

of an engine, no pilot action required. 

(2) Stow all loose equipment. 

3.3 Generator Failure 

( I) A II non-essential medical equipment are shed automatically in this aircra ft on loss of a 

generator, no pilot action required. 

4.0 NORMAL PROCEDURES 

No change. 

U:\STC MANUALS\EC155\EMSIFMS\Current\To ACO RFMS 26 Jui2012\RFMS155M·100A 05 Oct 2012.doc 13 of 40 
200 

50 100 150 

· APPROVED ENVELOPE AT TAKEnf.F AND l ""'"G I'·' "G£ 3 "GUA£ >C.JI 

2 

200 

! ,-,-. 

I ' 

150 

so 

250 lAS 300( km I h) 

j HEIGHT I VELOCITY DIAGRAM 

1 

I 

U:\STC MANUALS\EC 155\EMS\FMS\Current\To ACO RFMS 26 Jul 2012\RFMS155M-100A 05 Oct 2012.doc 14 of 40 
/\ft torage System Lights 

Cabin Flood (Blue-White) Lighting 

Cabin Reading Lighting 

Load Lights 

Aft a bin Dimmer 

upplemental trobe Lights 

uper Nightscanner earchlight 

LOX 

Medical /\ir 

Medical uction 

Medical Inverter 

U:ISTC MANUALSIEC1551EMSIFMS\Current\To ACO RFMS 26 Jui 20121RFMS155M· 100A 05 Oct 2012.doc 

0.14 

0.75 

0.40 

0.50 

0.4 1 

3.50 

2 1.0 

1.00 

4.50 

7.70 

50.00 

15 of40 
Wt. Ar m Mom 

Item lbs In In 

(MM) 

155M- lOS Blackout Curtain 3.3 86.65 285.95 ( 1.50) (2200.9 1) (330 1.37) 

155M-300 Pivoting Liller System: 

MedDeck and Trolley 39.0 137.28 5353 .92 (17.69) (3486.9 1) (6 1683.44) 

AeroSied CF Stretcher 28.0 137.28 3843.84 ( 12.70) (3486.91 ) (44283.76) 

155M-320 Supplemental Patient Restraint 4.5 143.84 647.28 J.2.04l _(3653.542 (7453.22) 

155M-400 Fischer & Entwicklungen (F & E) eating ( 155M-400- 1) 

# I LH F & E P/N 9613-0-33-

OX004B20X0002X (seat w/black restraint & 32.8 94. 12 3087. 14 

black headre t) MODEL: 230/305 equipped (1 4.88) (2390.65) (35572.87) 

with the Fischer swivel unit PIN 97 15- 1-21-1 5 

#2 RH F & E PIN 96 13-0-33-

OX004B20X0002X (seat w/black restraint & 32.8 94. 12 3087. 14 

black headrest) MODEL; 230/305 equipped ( 14.88) (2390.65) (35572.87) 

with the Fischer swivel unit P/N 9715- 1-2H5 

#3 Ll l F & E P/N 96 13-0-33-

OX004B20X0002X (seat w/black restraint & 32.8 174.85 5735.08 

black headrest) MODEL; 230/305 equipped ( 14.88) (444 1. 19) (66084.9 1) 

with the Fischer swivel unit P/N 97 15- 1-21-1 5 

#4 RH F & E PIN 96 13-0-33-

OX004B20X0002X (seat w/black restraint & 32.8 174.85 5735 .08 

black headrest) MODEL; 230/305 equ ipped ( 14.88) (444 1. 19) (66084.9 1) 

with the Fischer swivel unit PIN 97 15-1-21-1 5 

#5 Rll F & E PIN 96 13-0-33-

OX004B20X0002X (seat w/black restrai nt & 32.8 138.72 4550.02 

black headrest) MODEL: 230/305 equipped ( 14.88) (3523.49) (52429.53) 

with the Fischer swivel unit P/N 97 15-1-21-1 5 

155M-400 Martin Baker eating: ( ISSM-400-2) 

U:ISTC MANUALSIEC1551EMSIFMSICurrent\To ACO RFMS 26 Jui 20121RFMS155M-100A OS Ocl 2012.doc 16 of 40 
#2 RH Martin Baker seat w/swivcl unit 

Martin Baker P/N MB S 12650AC04 (seat 

w/black restraint & black headrest) 

#3 LH Martin Baker seat w/swivel unit 

Martin Baker P/N MBC 126SOAC04 (seat 

w/black restraint & black headrest) 

#4 RH Martin Baker eat w/ wivcl unit 

Martin Baker PfN MBC 12650AC04 ( eat 

w/black restraint & black headrest) 

#5 RH Martin Baker seat w/ wive! unit 

Martin Baker PfN M BC I 2650AC04 (seat 

w/black restraint & black headrest) 

155M-640 RTI-526 LOX ystem 

15SM-720 uetion Pump 

ISSM-730 Air Pump 

ISSM-900 60 liz Inverter 

40.0 

(I 8. I 4) 

40.0 

( 18. 14) 

40.0 

( 18. 14) 

40.0 

( I 8. 14) 

43.0 

( 19.50) 

6.5 

(2.95) 

4.5 

(2.04) 

7.7 

(3.49) 

94. 12 

(2390.65) 

174.85 

(4441. I 9) 

174.85 

(4441.19) 

138.72 

(3523.49) 

239.57 

(6085.08) 

254.69 

(6469. 13) 

254.69 

(6469. 13) 

192.9 1 

(4899.9 1) 

3764.8 

(43366.39) 

6994 

(80563 . I 9) 

6994 

(80563.19) 

5548.8 

(639 I 6. I I) 

1030 1.51 

(I I 8659.06) 

I 655.49 

(19083.93) 

I 146.1 I 

( I 3 197.03) 

1485.41 

( I 7 1 00.69) 

Note: Moment (For each item) = Weight of item X di Lance from aircraft. datum (Arm). 

U:ISTC MANUALSIEC1551EMSIFMS\Curreni\To ACO RFMS 25 Jul 20121RFMS155M·100A 05 Oct 2012.doc 17 of 40 
155M-1 10 

155M- Ill 

155M-1 25 155M- 126 

155M-1 29 

155M- I 33 155M- 135 155M- 136 

155M- 140 

155M- 164 155M- 165 155M- 166 

ISSM- 180 

ISSM- 195 

155M- 197 

155M-198 155M-250 

ISSM-300 ISSM-320 

ISSM-400 

155M-500 

155M-55 I 

ISSM-640 

155M-700 

ISSM-720 

155M-730 

ISSM-800 ISSM-810 ISSM-900 

JUNCTION BOX INSTALL 

CIRCUIT BREAKER PANEL INSTALL 

ELECTRICAL SCHEMATIC 

WIRE ROUTING 

ACCESSORY BAR MOUNT INSTALL 

FWD STORAGE CABINET INSTALL 

AFTSTORAGESYSTEM INSTALL AFT CARGO NET INSTALL 

PORTABLE 02 MOUNT INSTALL 

CABIN FLOOD L IGHTS INSTALL CABIN READING LIGHTS INSTALL 

LOAD LIGHTS INSTALL 

SUPPLEMENTAL STROBE LIGI ITS INSTALL 

SUPER NIGHTSCANNER INSTALL 

PROPAQ MD MOUNT IN TALL 

VENTILATOR MOUNT INSTALL 

CABIN FLOOR INSTALL 

PIVOTING LITTER SYSTEM INSTALL 

SECONDARY PATIENT RESTRA INT I STALL 

EATING IN TALL 

CABIN OVERHEAD MODULE INSTALL 

EQUIPMENT RACK INSTALL 

LOX INSTALL 

REMOTE EQUIPM ENT MOUNT INSTALL 

MEDICAL UCTION INSTALL 

MEDICAL AIR I TALL 

GA TOWER INSTALL 

IV UPPORT IN TALL 

MEDICAL INVERTER INSTALL 

U:\STC MANUALS\EC155\EMS\FMS\Current\To ACO RFMS 26 Jul 2012\RFMS155M·1 OOA 05 Oct 2012.doc 18 of 40 
(b) 

(c) 

(d) (e) 

(f) 

(g) 

155M-lOS Blackout Curtain Install 

The blackout curtain is deployable and will isolate the flight crew from the cabin lighting 

during low visibi lity and night operations. Suitable placards will be provided in the cabin 

and in the cockpit to ensure the appropriate use of the blackout curtain during taxi, 

takeoff, and landing operations. 

155M-II O Junction Box I nsta II 

The junction box will be the central location for electrical distribution for the EM 

equipment. 

155M-Ill Circuit Breaker Panel Insta ll 

The circuit breaker panel will be the central location for electrical power distribution for 

the EMS equipment. 

ISSM-125 Electrical chematic 

The EMS electrical system wiring wi ll be completely documented in the Electrical 

system schematic. 

155M- 126 Wire Routing 

The EM electrical system wiring routing will be completely documented in the Wire 

Routing Insta ll . 

155M-1 29 Accessory Bar Mount 

The accessory bar mount installed on the aft cabin bulkhead used to support various 

medical equipment (not to exceed 25 lbs) with easily removable mounts. 

U:\STC MANUALSIEC1551EMSIFMS\Current\To ACO RFMS 26 Jui 20121RFMS155M-100A 05 Oct 2012 doc 19 of 40 
(i) 

(k) 

forward outboard sides of the cabinet/gas tower installation wil l be mounted two medical 

oxygen cylinder mounts. The top of the cabinet can be adapted to support medical life 

support/ monitoring equipment. All compa11mcnts will be individually placarded for 

maximum weight of contents. 

155M- 135 Aft to rage y tem I nsta II 

The aft storage system will be positioned in the ECF aft cabin bulkhead access opening, 

between the two forward facing eat , the torage system will extend aft into the baggage 

compartment. and will be insta lled nu h with the cabin bulkhead panel as to not protrude 

into the cabin space. torage compartment will face forward and prov ide easy access to 

additional medical equipment. Three lights will be used to provide illumination of the 

cabinet area during operation, and the four control pane ls, located in the cabin overhead 

modul e wi II allow passengers/attendants to control cabinet I ighting. !\II compartments 

will be placarded for maximun1 weight of contents. 

155M-1 36 Aft Cargo Net Install 

The cargo net designed specifically for cargo (not to exceed 150 lbs.) wi ll be located in 

the left hand aft baggage compartment. 

ISSM-140 Portable Oxygen Mount Install 

Two Portable Oxygen Mount for a ··o·· or ·'E .. size cylinder will be located on the 

forward outboard side of the fwd storage cabinet. Mounts are to store the cylinders only, 

and should not be used for d i pen i ng. 

U:ISTC MANUALSIEC1551EMSIFMS\Current\To ACO RFMS 26 Jul 2012\RFMS155M-100A 05 Oct 2012.doc 20 or 40 
(m) 

(n) 

(o) 

(p) 

155M- 165 Cabin Reading Lights Install 

Cabin LED reading lights with touch control and dimming capability will be used at the 

(# I, #2, #3 & #4) seat locations. 

155M- 166 Load Lights Install 

The Load Lights consists of a si ngle LED light located above the right and left hand side 

door that is used fOI' illuminating the area when loading the aircraft. 

NOTE 

The load lights are lo r ground use only. 

155M- ISO upplemental Strobe Lights Install 

The upplemcntal Strobe Light ystem consi ts of a switch in the overhead console 

labe led "STROBE L TS", and a combination strobe and LED position light assembly 

Whelen PIN 01-0771 11 0-03 & -04 (TCO-C96a/T O-C30c) that replace the type certified 

position lights on the end or the horizontal tabilizer. The type certified position lights 

system control remains unchanged. Next, a power supply is mounted on the L/1-1 FWD 

existing equipment mount plate in the tail boom area aft of the horizontal stabilizer and a 

5 amp circuit breaker labeled ''STROBES'' located in the 4 ALPHA panel. 

Additionally, during night or in IMC tlight conditions. the strobe lights may cause 

reflections, which may affect the pilot. The strobe lights must be switched off. 

NOTE 

The type certified reel anti-collision light on the top of the vertical fi n remains unchanged. 

155M- 195 Super Nightscanner Install 

The uper Nightscanner consis1s of an 800.000 candle power incandescent searchlight 

.. Non-I R .. , existing overhead mounted switches for on-off, stow and existing cyclic 

mounted switches. The search light is powered by one 25 amp CB labeled "SUPER NCAN'' on the# l shed buss in the nose bay and one 5 amp CB labeled ''L T CTL" located 

on the 3 ALPHA panel # I shed buss in the nose bay. The Super Nightscanner mounted in 

forward be lly (chin panel) and operated by the activation of the cyclic mounted switches. 

There arc two switches, one toggle switch for on. stow, and off. One "Chinese hat" 

switch for elevation and azimuth control. The uper Nightscanner allows the pilot to 

perform reconnaissance of a landing area at night. 

U:\STC MANUALSIEC 155\EMSIFMS\Current\To ACO RFMS 26 Jul 2012\RFMS 155M-1 OOA 05 Oct 2012.doc 21 or 40 
(r') 

(s) 

(t) 

155M-198 Venti Ia tor Mount Install 

The Ventilator mount designed specifically for the LTV ventilator (not to exceed 16 lbs.) 

will be located on the fwd storage cabinet 155M- 133. 

l55M-250 Cabin Floor Install 

Tht:. floor pallet assembly will be installed in the aircraft to provide for the protection of 

the airframe and provide mounting for the litter assembly components. and the standard 

seats. The noor pallet will be machined aluminum with a hard anodized surface. A fluid 

dam/trough will be machined into the tloor to contain spilled 1luids. The Jloor pallet will 

overlay the existing aircraft lloor and mount to the existing cargo attachment fittings. 

Scats and litters wi ll mount directly to the floor pallet. Recessed longitudinal 

.. Brownline'' floor tracks will be integrated into the floor pallet to accommodate a number 

of interior seating/litter arrangements. 

155M-300 Pivoting Litter ystem Install 

A single patient litter along with a loading system capable of tracking and pivoting will 

be installed. The litter wi ll be installed in -line with the tlight direction. with the patient 

head positioned forward for all interior arrangements. 

The single patient I itter system consists of the fol lowing: 

I. .J-Rail Mount Assembly - The .J-Rail Mount assembly consists of a plate on which 

two pieces of track arc mounted. The tracks are for the rollers on the lower plate 

of the Trolley Assembly. The lower retractable pins of the Trolley engage the JRail Mount tracks to stop the travel of the Tro lley. The J-Rail Mount assembly is 

attached to the cabin floor with a quick pin at each end of the track which keeps 

the Trolley Assembly from coming out of the tracks wllen the lower pins are 

retracted. 

2. AeroSled CF -The AeroSied CF (TSO-C39b) is a carbon libcr patient litter. The 

AeroSled CF is made of a carbon tiber main body and backrest with an aluminum 

tube and machined component frame that wraps around the perimeter of the body. 

It is equipped with fittings on the bottom to engage the locking towers on the 

upper deck. The backrest is adjustable and activated by paddles on the backrest 

that acti vate a gas spring. The stretcher is also equipped with shoulder and body 

restraints as we ll as a foot bag to restrain the patient in a crash situation. The litter 

U·ISTC MANUALSIEC1551EMSIFMS\Current1To ACO RFMS 26 Jul 2012\RFMS155M-1 OOA 05 Oct 2012.doc 22 of40 
for the LifcPort AcroSicd. The trolley can translate and rotate to numerous 

positions prior to night for ease of loading non-ambulatory patients. The 

MedDeck System is made up of a Trolley Assembly and Upper Deck Assembly. 

5. Trolley - The trolley consists of an upper and lower plate, each with cam rollers 

(Reference Figure 25- 1 ). The center cylinder has an upper and lower retractable 

pin. The lower pins engage and lock into holes in the J-Rail Mount tracks. The 

upper pins engage and lock into holes in the upper deck. The cam rollers on the 

lower plate ride in the tracks on the J-Ra il Mount tracks. The cam rollers on the 

upper plate ride in the tracks on the upper deck. The trolley release hand le on the upper deck retracts both pins <md allows the trolley to roll inboard and outboard 

and the upper deck to translate along its long axis with respect to the trolley. The 

hand le also allows the upper deck and upper plate to rotate with respect to center 

cyli nder. 

6. Upper Deck - The upper deck is an aluminum structure that supports the 

Aero led. It is equipped with locking towers that retain the stretcher. The 

underside has two tracks for the cam rollers in the upper plate of the trolley and a 

series of locking holes to engage the upper retractable pins of the trolley. 

The trolley release handle turns a belt and drive shaft system that creates or 

removes tension in the cable to release or lock the trolley. The AeroSied Release 

Handles activates the cams in the locking towers and releases the AeroSied. 

U:ISTC MANUALSIEC1551EMSIFMS\Current\To AGO RFMS 26 Jui2012\RFMS155M-100A 05 Oct 2012.doc 23 of 40 
..... mtln 

.... "'1/olJ 

Lower Plot 

Figure I Trolley 

Trolley/Upper Deck Release 

Lever (Both Ends & Sides) 

Belt / 1 ( Cable 

milD m 

1- "" . v -

!---• - .__ 

,., 

t-· 

........ 

Figure 2 Upper Deck 

Manual UppPr 

p,n R!'leosP 

Monvol Lower Pin 

<Be th Sides 

Lower Ret,..oc table P1n <Both Sides) 

AeroSied Release 

Lever (Both Ends & Sides) 

U:\STC MANUALS\EC155\EMSIFMS\Current\To ACO RFMS 26 Jul 20121RFMS155M-100A 05 Oct 2012.doc 24 of 40 
(v) 

(w) 

(x) 

NOTE 

The right hand #4 & #5 attendant/passenger seats shall be removed when it is necessary 

to transport a second patient. 

155M-400 Seating Insta ll 

The EMS seating arrangement includes fi ve (5) attendant/passenger scats. The scats are 

longitudinal tracking and swivel-capable seats. The seats may either be Martin Baker P/N 

MBC 12650AC04 (seat w/black restra int & black headrest) or F & E PIN 961 3-0-33-

0X004B20X0002X (seat w/black restraint & black headrest) MODEL; 230/305 equipped 

with the Fischer swivel unit P/N 97 15- 1-21-1 5. The seats must meet the requirements of 

TSO-C39b Type IV seats or TS0- 127 for a FAR 29 Rotorcraft in a fwd and aft-fac ing 

configuration for Taxi, Take-off, Landing and Emergency Procedures (TTOL & EP). The 

seats will be directly mounted to the MAl floor pallet in recessed longitudina l fl oor tracks 

that meet MS33601 integrated into the floor pal let to accommodate a number of interior 

seating/litter arrangements. For Taxi. Take-off and Landing the forward cabin (# I LH & 

#2RH) seats will be locked in the aft-facing position. The single mid-cabin (#5RH) seat 

wi ll either be locked in the fwd-facing or aft-facing position. The remaining two aft cabin 

(#3LH & #4RH) seats will be locked in the fwd-facing position. 

NOTE 

Any seat or combination of seats may be removed as necessary to faci litate operations. 

155M-500 Cabin Overhead Mod ule Install 

The overhead module is positioned centerline longitudinally in the an cabin. The module 

will serve as a mounting location for the IV support, cabin nood (blue-white) lights, EMS 

equ ipment control touch panel, audio panels and miscellaneous other mission specific 

contro ls. 

155M-55 I Medical Equipment Rack Install 

The Medica l EqLr ipment Rack is ··manufactured from machined aluminum" and insta lled 

on the fwd storage cabinet. The racks support variou medical equipment secured to the 

rack with casi ly removable mount . 

U:ISTC MANUALSIEC155\EMSIFMS\Current\To ACO RFMS 26 Jui2012\RFMS155M· 100A 05 Oct 2012.doc 25 or 40 
(z) 

526-RTI LOX ystem, 

I 0 Liter DEWAR" Container 

Fill, Bui ldup, Vent Valve 

Build up Coil 

Pressure Control Valve 

Flow Modulator 

upply Heat Exchanger 

P1-essure Regulator 

Solenoid Valve 

Pressure Relief Devices 

The DEW /\R 'S Container and the Supply Heat Exchanger allows the liquid 02 to 

convert to gas prior to entering the cabin an in line electrical shut off va lve is installed 

adjacent to the DEWAR'S Container on the low pressure supply line. The valve is 

controlled by three switch system: Pilot master cutoff switch. Emergency oxygen 

override in the cabin if touch screens fa ils. Touch screens four for normal on/off 

operation, located in the cabin overhead multipurpose module. The touch screens also 

have annunciation of low oxygen pressure below 27 psi. A Flow Control Oxygen Outlet 

is located in the cabin Gas Panel and contents gauge is located in the overhead module. 

The Flow Control Oxygen Outlet is a self-sea l in g. duplex, oxygen outlet station, and the 

contents gauge allows the crew to monitor [he amount of oxygen available for use. 

ervice the 526-RTI LOX ystem by removing the unit and serv icing orr the aircraft. 

Low pressure oxygen is supplied on demand at 45 to 65 PSI depending on altitude, 

temperature and remaining contents in the DEWAR'S Container. 

155M-700 Remote EqL1i pmcnt Mount Install 

The remote equipment mount consists of a \12" thick aluminum honeycomb panel attached 

to the aft storage system. This mount provides a place for EMS equipment; such as, the jbox, circuit breaker panel. and inverter. Access to the equipment is gained from the right 

hand baggage compartment door. 

U;\STC MANUALS\EC155\EMS\FMSICurreni\To ACO RFMS 26 Jui20121RFMS155M-100A 05 Oct2012.doc 26 of 40 
(ab) 155M-730 Medica l Air Install 

(ac) 

The Medical Air Pump installation provides an electrical pump for the purpose of 

powering various carry on equipment. Operation is controlled with the touch panels, 

located in the overhead module. Low pressure annunciated on the touch screens when 

below 27 psi. The pump's air is regulated and filtered. 

155M-800 Gas Tower lnsta II 

Two medical gas towers will be located on the an outboard sides of the fwd storage 

cabinet. The gas towers contain oxygen, air and suction outlets. 

(ad) 155M-8 1 0 IV SL1pport Install 

An intravenous solution (IV) bag support will be provided in the overhead module to 

provide attachment points for medical hoses and IV solution bags in close proximity to 

the patient. 

(ae) 155M-900 Medical Inverter Install 

The Medical Inverter installed to provide an II OVAC source for carry on equipment 

rotor turning. The Inverter is a TSO-C73 unit and tne unit output is limited to I 0.0 amps 

AC. 

A Direct AC ource system (ground outlet) that allows the crew while on the ground and 

connected to the external II 0 Vac receptac le to operate high load carry on equipment 

with rotors not turning will be incorporated into the EM installation. 

U:\STC MANUALS\EC1551EMSIFMS\Current\To ACO RFMS 26 Jul 2012\RFMS155M-100A 05 Oct 2012.doc 27 of40 
Touch Panel 

Touch Panel 

Touch Panel 

Touch Panel 

Power Switch 

Module 

I I I I I I I I 

Patient Storage Flood Load Oxygen J I Suction II A ir II Inverter I llcadset Lt Lt Lt 

U:\STC MANUALS\EC155\EMS\FMS\Current\To ACO RFMS 26 Jui 2012\RFMS155M-100A 05 Oct 2012.doc 28 of 40 
NOTE 

T he annunciations and associated menus are available on all screens at all times. T he Medical M enu is 

displayed above. 

Annunciations and Menus 

Function DESCRIPTION 

INT (indicator only) AnnLmciator is highlighted when the I I 0 VAC source is internal. 

Note 

Whenever the Medical Inverter is supply ing I I 0 V AC to the 

aircraft, this annunciator will be illuminated. 

EXT (indicator only) Annunciator is highlighted when the I I 0 VAC source is external. 

Note 

Whenever an external source of II 0 Y AC is plugged into the 

aircraft and is providing power this annunciator will be illuminated. 

PA TM IC (indicator only) Annunciator is highlighted when the " Patient Microphone" is 

active. 

Annunciator is shadowed when the '·Patient M icrophone'' is 

inactive. 

PATPHO (indicator only) Annunciator is highlighted when the "Patient Earphones'' are 

active. 

Annunciator is shadowed when the ··Patient Earphones'' are 

inactive. 

Annunciator is highlighted " AMBER"' when air pressure is below 

AIR (indicator only) 27psi Annunciator is highlighted "GREEN" when air pressure is above 

27psi 

Indicator is highlighted " RED"' when oxygen pressure is be low 

OXYGEN (indicator only) 27psi 

Indicator is highlighted "GREEN'' when oxygen pressure is above 

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U:IS

TC MANUALSIEC155\EMS\FMS\Current1To ACO RFMS 26 Jul 20121RFMS155M·1 OOA 05 Oct 2012.doc 30 of40 
AIR 

.. 

-

. 

- -. 

.. 

,-- ,_.. ,....-. 

Air SucHan Oxygen lmerter 

• • 

NOTE 

When a medica l system switch is activated, the annunciator light will change from neutral co lor to white 

or green. This indicates that the switch is in an "ON" state. 

Function DESCRIPTION 

Medical To access the medical menu touch the single action Medical button, that 

brings the user to the medical menu from any screen. 

Air To turn on the medical air pump touch the alternate action A IR button that 

turns pump on/off. 

NOTE 

If there is a loss, of power or the pump, fails there will be no "Air" 

but the switch annunciator wil l remain green indicating the switch is 

in the ''ON"' position. 

Suction To turn on the Medical Suction Pump touch the alternate action Suction 

button that turns the air pump on/off. 

NOTE 

l f there is a loss or power or the pump fails there will be no "Suction" bLit the 

switch annunciator wil l remain green indicating the switch is in the ''ON'' 

position. 

Oxygen To turn on the medical oxygen touch the alternate action Oxygen button that 

turns the medical oxygen on/off. 

NOTE 

If there is a loss of power or the cutoff valve fai ls there wi ll be no "Oxygen" 

but the switch annunciator will remain green, indicating the switch is in the 

"ON'' position. 

If the Touch Panel fails, turn on oxygen with the momentary '·Emergency 

Oxygen"' switch located on the center aft overhead module and use the pilots 

oxygen override switch to turn the oxygen off. 

Stop flow of oxygen by removing all power from aircraft. or by 

tLirning the pilots oxyp,en override switch to off. 

U:ISTC MANUALSIEC 155\EMSIFMSICurrent\To ACO RFMS 26 Jul 20121RFMS155M-100A 05 Oct 2012.doc 3 1 of 40 
NOTE 

The " INT" annunciator should be highlighted i f there is power 

available. If there is a loss. of power or the inverter, fails there will 

be no " Inverter" but the switch annunciator wi ll remain green 

indicating the switch is in the ''ON" position. 

U:\STC MANUALSIEC1551EMSIFMS\Current1To ACO RFMS 26 Jul 20121RFMS155M·100A 05 Oct 2012.doc 32 o f 40 
NOTE 

When the annunciator light is on the associated button changes from neutral color to white or green. 

This indicates that the switch is in an ''ON" state. 

Function DESCRIPTION 

Lights To access the Lights Menu touch the single action Lights button, which brings the user to the I ights menu from any screen. 

Load L ight To turn on the load lights touch the alternate action Load Light button that 

tums the load I ights on/off. 

To turn on the 4x audio panels and RC-7000 remote control panel lighting 

Day Night witch touch the alternate action Day Night Switch button. This controls the 4x audio panels and RC-7000 remote control panel l ighting in the overhead 

module only. 

Storage Lights To turn on the Storage Lights touch the alternate action Storage Light button that turns the aft cabinet lights on/orr. 

M edical Lights 

ON/OFF To turn on/off the medical I ights touch the alternate action ON/OFF button that turns the medical lights on/off. 

BLUE To change the light setting to blue touch the momentary BLUE button that turns the light setting t o blue by actuating WI liTE/BLUE relay. 

WHITE To change the light setting to white touch the momentary WHITE button that turns the light setting to white by relaxing WHITE/BLUE relay. 

HIGH To change the light intensity setting to high touch the momentary HIGH button that sets the white/blue lights to its high setting by closing a rela)l_. 

To change the light intensity setting to medium touch the momentary 

MEDIUM M EDIUM button that sets the white/blue lights to its low setting by closing a 

relay. 

LOW To change the light intensity setting to low touch the momentary LOW 

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U:IS

TC MANUALSIEC1551E

MS\FMS\Current1To ACO RFMS 26 Jul 20121RFMS1 55

M-1 OOA 05 Oct 2012.doc 34 of 40 
NOTE 

When the annunciator light on the associated button changes from neutra l color to white or green. This 

indicates that the switch is in an ''ON" state. 

·Function DESCRIPTION M ise To access the Mise Menu touch the single action Mise button, 

which brings the user to the M ise menu from any screen. 

Pat Mic To turn the Patient microphone on or off touch the alternate action 

Pat Mic button. 

Pat Pho To turn the Patient phones on or off touch the alternate action Pat Pho button. 

•Intensity To increase the screen brightness touch the momentary • Intensity button. 

To decrease the screen brightness touch the momentary 

button. 

U:\STC MANUALSIEC1551EMS\FMS1Current\To ACO RFMS 26 Jui2012\RFMS155M-100A 05 Oct 2012.doc 35 o f 40 
and push down on the backrest. 

(b) Aero led Deck Release: To remove the Aero led pull the AeroSied release handle on the 

upper deck and slide the AcroSied aft or forward until the fi ttings on the stretcher clear 

the locking towers. To in tall the Aero led, slide it forward onto the deck o that the 

stretcher fittings engage. 

(c) Trolley Release: The McdOcck can rotate and translate to facil itate loading the Aero led. 

Moving the trolley relea e handle to the ·'traver e'' position as indicated on the placard 

allows the trolley to translate laterally. Moving the release handle to the "rotate" position 

allows the trol ley to rotate about the center cylinder. 

U.\STC MANUALS\EC1551EMSIFMS\Current\To ACO RFMS 26 Jul 2012\RFMS155M·1 OOA OS Oct 2012.doc 36 of 40 
PORTABLE 02 MOUNT _/ "' 

1 55M-140 EXIl 

CABIN FLOOR 

155M-250 

EXIT 

t 

EXIT 

GENERAL ARRANGEMENT 

(VIEW LOOKING DOWN) 

EXIT 

MEDICAL AIR 

15511.4-730 

LOX 

15511.4- 640 

AFT CARGO NET 

15511.4- 136 

AFT STORAGE SYSTEM 

155M- 135 

PNOTING LITTER SYSTEM 

155M- 300 

SEATING 

155M-400 

SECONDARY PATIENT RESTRAINT 

15511.4-320 

GENERAL ARRANGEMENT 

(ALTERNATE VIEW LOOKING DOWN) 

Figure 3 "General EMS Arrangement'" provides an overview of the EMS seating arrangements and the 

locations of the eq uipment installation locations. 

U;\STC MANUALSIEC155\EMS\FMS\Current\To ACO RFMS 26 Jui20121RFMS155M-100A 05 Oct2012.doc 37 of 40 
... jiiiiiii.[ID 

.... 

f W'p STORAGE CABINET RACK. MOUNTS 

& MED GAS TOWER 

(VIEW rACING FWD) 

AfT STORAGE SYStEM & MOUNT 

(VI[W rACING AFi) 

Figure 3 ·'General EM S Arrangement"' (conti nued) 

D 

ACCESSORY 9AR MOUNT 

155M- 129 

ArT STORAGE SYSTEM 

155M- 1.35 

U:\STC MANUALSIEC1551EMSIFMSICurrent\To ACO RFMS 26 Jul 2012\RFMS155M-100A 05 Oct 2012.doc 38 o f 40 
' 

EMS OVERHEAD LIGHTING & IV SUPPORT 

(VIEW LOOKING UP) 

SUPPLEMENTAL 

STROBE LJCHTS 

155M-180 

REMOTE EQUIPMENT MOUNT 

AND 

AFT STORACE SYSTEM 

I !)SM- 13!) 

MEDICAL SUCTION 

155M-720 

MEDICAL AIR 

155M-730 

(REF.) R/H SIDE VIEW 

Figure 3 ·'General EMS Arrangement'' (continued) 

CABIN OVERHEAD MODULE 

155M-500 

(REF.) 

SUPPORT 

155M- 810 

SUI'ER NICHTSCANNER 

155M-195 

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MEDICAL INVERTER 

155M- 900 

@ 

CIRCUIT BREAKER PANEL --........._ @ 

155M-111 "'-._ 

REMOTE EQUIPMENT MOUNT 

155M-700 

JUNCTION BOX~ 

155M- 11 0 

@ 

@ 

• 

000®® 

. 

---

.. 

00000 

I 

• 

0· 

REMOTE EQUIPMENT MOUNT & EQUIPMENT 

(R/H SIDE VIEW FACING INBOARD) 

Figure 3 ··General EM Arrangement" · (continued) 

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