# Presentation: 009392

## Louise C. Speitel
Fire Safety Branch AAR-440FAA W.J. Hughes Technical Center
Atlantic City International Airport, NJ  08405  USA

- Fire Safety Branch AAR-440FAA W.J. Hughes Technical Center
- Atlantic City International Airport, NJ  08405  USA

**THE DEVELOPMENT OF GUIDANCE FOR THE USE OF NEW AGENTS IN HANDHELD EXTINGUISHERS FOR AIRCRAFT CABINS**

- Aircraft Systems Fire Protection Working Group Meeting Ottawa, Canada
- February 15-16, 2005

## OUTLINE OF TALK

-   FAR requirements for hand-held extinguishers
-   Minimum performance standard (MPS) for transport category aircraft
-   Purpose of handheld advisory circular (AC)
-   Approach
-   Extinguisher ratings
-   Throw range
-   Fixed nozzle/ hose/ adjustable wand
-   Toxicity: decomposition products, agent, low oxygen hypoxia
-   Ventilation nomograms
-   A/C language for halocarbon fire extinguishers
-  Caveats

## FEDERAL AVIATION REGULATION (FAR) REQUIREMENTS FOR HAND FIRE EXTINGUISHERS

-   Specifies the minimum number of Halon 1211 or equivalent extinguishers for various size aircraft.
-   Specifies the location and distribution of extinguishers on an aircraft.
-   Each extinguisher must be approved.
-   Each extinguisher intended for use in a personnel compartment must be designed to minimize the hazard of toxic gas concentration.
-   The type and quantity of extinguishing agent, if other than Halon 1211, must be appropriate for the kinds of fires likely to occur.
-   The FAR does not give extinguisher ratings. This is done in the AC.

## THE MINIMUM PERFORMANCE STANDARD (MPS)

-   Provides requirements for equivalency to Halon 1211 5 B:C extinguishers to satisfy Federal Aviation Regulations citing “Halon 1211 or equivalent”:
-   UL rated 5 B:C Halocarbon extinguishers that will be used in transport category aircraft must pass 2 tests identified in DOT/FAA/AR-01/37 _Development of a Minimum Performance Standard (MPS) for Hand-Held Fire Extinguishers as a replacement for Halon 1211 on Civilian Transport Category Aircraft_.
-   Hidden Fire Test
-   Seat Fire/Toxic_i_ty Test
-   The MPS guarantees extinguishers to replace halon 1211 will have equal fire performance and an acceptable level of toxicity (for decomposition products of the agent). Guidance for agent toxicity can be found in the advisory circular.
-   The MPS requires that a  permanent label be  affixed to the extinguisher identifying FAA approval for use on board commercial aircraft.

## PURPOSE OF ADVISORY CIRCULAR: Safety

*“**Provide methods for showing compliance with the hand fire extinguisher provisions in parts 21. 25, 29, 91,121, 125, 127 and 135 of the Federal Aviation Regulations (FAR 14)”.   (Other avenues exist for showing compliance.)*

-    21      Certification procedures for products and parts
-    25	Airworthiness standards - Transport category airplanes
-    29	Airworthiness standards - Transport category rotorcraft
-    91	General operating and flight rules
-  121	Operating requirements - Domestic, flag and supplemental operations
-  125	Certification & operations- Airplanes having a seating capacity of 20 or more passengers or a maximum payload capacity of 6000 pounds or more
-  127	Certification and Operations of Scheduled Air Carriers with Helicopters ?
-  135	Air Taxi Operators and commercial operators

##  While this AC is not mandatory, it offers a method of demonstrating compliance with the applicable airworthiness requirements. ....

-  This AC does not constitute a regulation and is not intended to require anything beyond that specifically required by the regulations.

**PURPOSE OF ADVISORY CIRCULAR (cont.)**

## PURPOSE OF ADVISORY CIRCULAR (cont.)

-   Provide safety guidance for halon replacement agents.
-  Effectiveness in fighting onboard fires.
-  Toxicity to passengers and crew
-   Provides updated general information.
-   Applies to aircraft and rotorcraft.
-   Requires adherence to outside documents:
-  ASTM specifications
-  MPS for hand fire extinguisher for transport category aircraft** **
-  CFR Title 40: Protection of the Environment, Part 82- Protection of Stratospheric Ozone, Subpart G, Significant New Alternatives Program and Subpart H- Halon Emissions Program.

**PURPOSE OF ADVISORY CIRCULAR (cont.)**

## RELATED SECTIONS

**FEDERAL AVIATION REGULATIONS (FARS)**

-   21.305     Certification procedures for products and parts
-   23.561      Normal, utility, acrobatic, and commuter category airplanes
-   25.561; 25.851    Transport category airplanes
-   27.561                 Normal category rotorcraft
-   29.561; 29.851; 29.853 (e) and (f)
-   91.193 (c)    ?
-   121.309 (c)
-   125.119 (b) and (c)** **
-   127.107 (c)  ?
-   135.155

## RELATED TITLES: CODE OF FEDERAL REGULATIONS (CFRs)

-   Title 40: Protection of the Environment
-   Title 46  Shipping
-   Title 49  Transportation
-          **OTHER RELATED INFORMATION (ACs and ADs)**
-    AC-120-80    In-Flight Fires
-    AC 20-42C   Hand Fire Extinguishers for Use in Aircraft
-    AD 93-07-15 (2)(i)   Airworthiness Directives:
-    Boeing Models 707, 727, 737, 747, and 757
-    McDonnell Douglas Models DC-8, DC-9, and DC-10

## APPROACH 

-     The FAA Fire Safety Section is providing guidance material to the FAA Aircraft Certification Office. The guidance material includes a draft AC for halocarbon hand-held extinguishers.
-    The Aircraft Certification Office will be tasked to write the advisory circular.
-    Recommend a separate AC for Halon Replacement Extinguishers.
-   This AC will be revised as new agents are introduced.
-    Use science-based approach published in peer-reviewed literature and adapted in NFPA 2001 Standard for Clean Agent Extinguishing Systems.
-    Conservative
-    More accurate than approach used for halons** **
-   The safe-use guidance is based on an assessment of the relationship between halocarbons in the blood and any adverse toxicological or cardiac sensitization event.

## APPROACH (cont.)

-   Safe human exposure limits, up to 5 minutes are derived using a Physiologically-based Pharmacokinetic (PBPK) modeling of measured agent levels in blood .
-   Assume 8,000 ft or 14,000 ft P altitude, 70F (21.1C) cabin temperature & perfect mixing.
-   Non-ventilated aircraft: The allowed concentration would be based on the 5-minute PBPK safe human concentration if available. Otherwise,  the “No Observable Adverse Effect Level” (NOAEL) may be used.
-  Ventilated aircraft: Tables /graphs will be included if PBPK data is available for that agent.
-  Agent manufacturers may provide PBPK data and tables for ventilated aircraft at their expense.
-   Operators of non-transport category aircraft should become familiar with the information in this AC
-  The proposed AC is subject to toxicological review & change/ rewrite by the FAA Aircraft Certification Office.

## COMBINED OR SEPARATE A/C?

-   **ONE A/C FOR ALL HANDHELD EXTINGUISHERS:**
-  The safe-use guidance for Halons would be changed to match the safe-use guidance for halon replacements.
-   New guidance for the halons would restrict Halon 1211 from being used in small aircraft.
-   Adoption would take years, or may never happen due to resistance from industry to lower the allowed weights of halon.

-   **SEPARATE  A/C FOR HALON REPLACEMENTS:**
-   A separate A/C for halon replacements may be adapted relatively quickly. Halon replacements are available meeting UL and MPS requirements: Halotron I, HFC236fa, and HFC227ea.
-   The Montreal Protocol and U.S. Clean Air Act require phase out of ozone depleting halons and transition to available alternatives.
-   Current A/C 20-42C for halons will be revised later.

## EXTINGUISHER RATINGS FOR HALONS

**   ****AC 20-42C:**
-  A minimum UL rated 5 B:C sized extinguisher was recommended for Halon 1211 for all sized aircraft.
-  A minimum UL rated 2 B:C extinguisher was recommended for Halon 1301 for aircraft with a maximum certificated occupant capacity (MCOC) of 4 including the pilot.
** **Recommends a minimum 2A, 40B:C rating for accessible cargo compartments of combination passenger/cargo and cargo aircraft.
-    NFPA 408 allows 2 B:C UL rated bottle of Halon 1211 in aircraft with a MCOC of 4.

## EXTINGUISHER RATINGS FOR HALOCARBONS

**   ****Proposed Halocarbon  Extinguisher Advisory Circular:**
-   Recommends a minimum 5B:C UL rating.
-    For transport category aircraft, extinguishers with a minimum UL 5 B:C rating must meet the Minimum Performance Standard. A permanent label is required, indicating  FAA approval for use on-board commercial aircraft.
-  Recommends a minimum 2A, 40B:C rating for accessible cargo compartments of combination passenger/cargo and cargo aircraft.

## THROW RANGE

-   The MPS requires a minimum throw range of 6-8 feet
-   A throw range of 10 feet or greater is recommended for 5 B:C halocarbon extinguishers with a maximum certificated occupant capacity (MCOC) of 19 or more persons including the pilot.
-  A longer throw range is needed to fight seat fires in large aircraft cabins and narrow body fuselages where  the heat radiating from the ceiling may make it more difficult to get close to the fire.
-   A throw range of 3 feet or greater is recommended for halocarbon extinguishers  with a MCOC of less than 19 passengers.
** **A lower velocity discharge is less likely to cause splashing &/ or splattering of the burning material. Consider a shorter throw range for very small aircraft
-  Select a range that would allow the firefighter to effectively fight fires likely to occur.

## FIXED NOZZLE/HOSE/ ADJUSTABLE WAND

-   For access to underseat, overhead and difficult to reach locations, it is recommended that extinguishers be equipped with a discharge hose or adjustable wand.
-   An extinguisher with a discharge hose or adjustable wand is more likely to result in the extinguisher being properly held during use.
-   Provides a means of directing a stream of agent to more inaccessible areas.
-   An extinguisher with an adjustable wand allows one-handed use.

## USER PREFERENCE SURVEY

**USER PREFERENCE SURVEY**

*The toxicity issues for extinguishing agents in portable fire extinguishers is the most important concern of the airline industry as indicated in over 111 responses to the User Preference Survey conducted by the FAA sponsored IASFPWG.*

## TOXICITY CONSIDERATIONS

** ****Toxicity of the halocarbon itself**
-   Cardiotoxicity
-   Anesthetic Effects
-   Guidelines in the proposed AC are stricter than UL 2129 “Halocarbon Clean Agent Fire Extinguishers”. Immediate egress assumed for UL 2129 standard.
**  ****Low oxygen hypoxia: Very small aircraft**
** **Aircraft pressurized to 8,000 ft Altitude
-  Nonpressurized Aircraft: Much greater concern up to 14,000 ft.
**  ****Toxicity of halocarbon** **decomposition products**
** **Guidelines set in the Minimum Performance Standard for Handheld Extinguishers

## AGENT TOXICITY :

**SAFE CLEAN AGENT CONCENTRATION**

- Total agent available from all required extinguishers should not be capable (assuming perfect mixing) of producing concentrations in the compartment by volume, at _**70oF (21.1oC)**__ __**when discharged at altitude**_   (8,000 ft. P, pressurized Aircraft and 14,000 ft P, nonpressurized aircraft), that exceeds the agent’s safe exposure guidelines. *(Note: Designing for altitude provides a large safety factor for ground use. No need for 120**o**F correction)*
**Nonventilated passenger or crew compartments:**
- PBPK derived 5 minute safe human exposure concentration, if known.
- If PBPK data is not available, the agent No Observable Adverse Effect Level **(NOAEL)**  is to be used. *(Note: UL 2129 allows use of a (sometimes higher) LOAEL Concentration)*
**  ****Ventilated Compartments:**
- Use graphs or tables to obtain maximum weight per cubic foot. Tables are based on PBPK modeling of theoretical concentration decay curves & perfect mixing. If tables are not available, follow concentration guidelines for nonventilated compartments.

## SAFE EXTINGUISHER WEIGHTS FOR AVIATION       (NO VENTILATION, 8000 FT. ALTITUDE , 70oF)

| Agent |  CAlt 
 (%) |   S  
(ft3/lb) |    W         
  (lb) | One 5BC Ext.   (lb) | X1bottle
(ft3) | Max. No. 5BC Ext for 1000 ft3 = V/X = 1000/X |
| --- | --- | --- | --- | --- | --- | --- |
| Halotron 1 |   1.0 |  2.597 |  |        5.0 | 1730.3 | 0.6 |
| HFC 236fa | 12.5 |  2.4574 |  |        4.75 | 114.6 | 8.7 |
| Halon 1211 |   1.0 |  2.248 |  |        2.5 | 748.9 | 1.3 |
| HFC 227ea | 10.5 | 2.2075 |  |       5.75 | 145.6 | 6.7 |

-   C**Altitude** is the maximum FAA allowed clean agent concentration (%) *discharged at altitude*
-   W is the maximum FAA allowed weight of clean agent (lb) ***(all extinguishers)*** for volume X
-   X is the minimum FAA allowed volume of a compartment (ft3) ***(all extinguishers)***** **
-   S is the specific volume of the agent at sea level at 70oF (21.1o C) (ft3/lb)

**7x**

**0.5x**

**5 x**

- Where A= Altitude correction factor for S
- At 8000 ft:**     **A= 760mmHg/564.59mmHg = 1.346
- (At 14,000 ft: A= 760mmHg/446.63mmHg = 1.702)

**X = X****1bottle**** x No. Bottles**

## SAFE EXTINGUISHER WEIGHTS FOR AVIATION

**(NO VENTILATION, ****14,000 FT.**** ALTITUDE ****, 70oF****)**

| Agent |  CAlt 
 (%) |   S  
(ft3/lb) |    W         
  (lb) | One 5BC Ext.   (lb) | X1bottle
(ft3/lb) | Max. No. 5BC Ext. for 1000 ft3 =  V/X= 1000/X |
| --- | --- | --- | --- | --- | --- | --- |
| Halotron 1 |   1.0 |  2.597 |  |        5.0 | 2188.0 | 0.5 |
| HFC 236fa | 12.5 | 2.4574 |  |        4.75 | 144.9 | 6.9 |
| Halon 1211 |   1.0 | 2.248 |  |        2.5 | 947.0 | 1.1 |
| HFC 227ea | 10.5 | 2.2075 |  |       5.75 | 184.1 | 5.4 |

-   C**Altitude** is the maximum FAA allowed clean agent concentration (%) ***discharged at altitude***
-   W is the maximum FAA allowed weight of clean agent (lb) ***(all extinguishers)***** **for volume X
-   X is the minimum FAA allowed volume of a compartment (ft3) ***(all extinguishers)***** **
-   S is the specific volume of the agent at sea level at 70oF (21.1o C) (ft3/lb)

**6x**

**0.4x**

**5 x**

- Where A= Altitude correction factor for S
- (At 8000 ft:**     **A= 760mmHg/564.59mmHg = 1.346)
- At 14,000 ft: A= 760mmHg/446.63mmHg) = 1.702

**X = X****1bottle**** x No. Bottles**

## AGENT TOXICITY: MINIMUM SAFE COMPARTMENT VOLUME    (NO VENTILATION, 70oF) 

- The toxicity guidelines in the proposed halocarbon advisory circular allow the following minimum compartment volumes for the following 5 B:C extinguishers, released at 70oF: (21.1oC)

| Agent | Notes | Agent Weight (lbs) | Minimum Volume of Compartment (ft3) 1 |  |  |
| --- | --- | --- | --- | --- | --- |
|  |  |  | For Sea Level
(For info only) | For 8,000 ft P Altitude
(Pressurized A/C) | For 14,000 ft   P Altitude (NonPressurized A/C) |
| HFC236fa |  | 4.75 | 85 | 115 | 145 |
| Halotron I | 2 | 5.0 | 1286 | 1730 | 2188 |
| HFC227ea |  | 5.75 | 108 | 146 | 184 |
| Halon 1211 | 2, 3 | 2.5 | 556 | 749 | 947 |
| Halon 1301 | 2, 3 | 5.0 | 243 | 327 | 414 |

***Multiply this number by the number of extinguishers in the aircraft***
***Do not use in small spaces***
***(If the proposed halocarbon extinguisher AC was applied to the Halons)***

## AGENT TOXICITY: NO. OF 5BC BOTTLES ALLOWED

**(NO VENTILATION, 8000 FT ALTITUDE, ****70oF****)**

| Aircraft/ Helicopter | Vol (ft3) | Max No. Seats | Halon 1211 |  |  | HFC-236fa | Halotron 1 | HFC-227ea |
| --- | --- | --- | --- | --- | --- | --- | --- | --- |
|  |  |  | AC20-42C & UL1093 | AC20-42C
1 air-change /min | New AC | New AC | New AC | New AC |
| Cessna 152- | 77 | 2 | 0.3 | 0.4 | 0.1 | 0.6 | 0.04 | 0.5 |
| Cessna 210C | 140 | 6 | 0.5 | 0.7 | 0.2 | 1.2 | 0.08 | 1.0 |
| Cessna C421B | 217 | 10 | 0.7 | 1.1 | 0.3 | 1.9 | 0.1 | 1.5 |
| Sikorsky S76 | 204 | 14 | 0.7 | ___ | 0.2 | 1.8 | 0.1 | 1.4 |
| B727-100 | 5,333 | 131 | 17 | ___ | 6.4 | 47 | 3.1 | 37 |
| B767-200 | 11,265 | 255 | 36 | ___ | 14 | 98 | 6.5 | 77 |
| B 747 | 27,899 | 500 | 90 | ___ | 34 | 243 | 16 | 192 |

|  | Less than one 5 B:C extinguisher allowed |
| --- | --- |

## TOXICITY GUIDELINES FOR HANDHELDS

**(NO VENTILATION)**

| Agent  | AC 20-42C 
If Egress is possible within 1 minute | A/C20-42C
Otherwise,
Max Design Concentration | Max Safe Concentration (Constant Concentration) | Guidance for New A/Cs
(Altitude) |
| --- | --- | --- | --- | --- |
| Halon 1211 | 4%  at sea level
(basis for nomograms- used for ventilated compartments at 8,000 ft) | 2% at sea level | 2.8% for 15 sec
1.8% for 30 sec
1.3% for 1 min
1 % for 5 min | 1% for 5 min |
| Halon 1301 | 10%  at sea level
(basis for nomograms- used for ventilated compartments at 8,000 ft) | 5% at sea level | 10% for ~15 sec
6% for 5 min | 6% for 5 min |
| HCFC Blend B | N/A | N/A | Between 1% and 2% for 5 min | 1% for 5 min |
| HFC 236fa | N/A | N/A | 15% for 30 sec
12.5% for 5 min | 12.5% for 5 min |
| HFC 227ea | N/A | N/A | 12% for 30 sec
10.5% for 5 min | 10.5% for 5 min |

## KINETIC MODELING OF ARTERIAL HALON 1211 

**BLOOD CONCENTRATION (No Ventilation)**

**FAA cuurently allows up to 4% for 1 minute at sea level ****(7% at 14,000 ft)**** **
**FAA currently allows up to 8% for vent A/C at 8000 ft  ****(10% at 14,000 ft)**

**Allowed  &**
** ****Unsafe**

**Halon 1211 Gas Concentrations**

## VENTILATION

-    ***WARNING***:  Small increase in concentration above the Safe 5 Minute Human Exposure Concentration results in a much shorter  time to effect:
- Safe human exposure to constant concentration:
- HFC 236fa : 12.5% for 5 min, 15% for 30 sec.
- HFC 227ea: 10.5% for 5 min, 12.0% for 30 sec.,
-   Development of  Ventilation Tables:
-   Based on total weight of agent on aircraft for ***all*** extinguishers.
-   Stratification of agents is a realistic expectation but is not included due to lack of acceptable methodology. Perfect mixing is assumed
-   Agent manufacturers may apply pharmacokinetic modeling  of blood concentration data to perfect mixing agent decay concentration curves.
-   Tables for ventilated aircraft can be developed from that data.
-   This work is to be preformed at the manufacturers expense.
-   A limited number of laboratories have capability of performing this modeling.

## (assuming perfect mixing)

##    dB/dt = k1 C(t) - k2B(t)

**   ****dB/dt = k****1**** C(t) - k****2****B(t)**

- Blood
- B(t)

- Waste

**k****1**

**k****2**

- C(t)

**Lung**

## MODELING ARTERIAL BLOOD CONCENTRATIONS OF HALOCARBONS USING 1st ORDER KINETICS

## KINETIC MODELING OF ARTERIAL HALON 1211 BLOOD CONCENTRATION IN VENTILATED AIRCRAFT

**Critical Arterial Concentration**

**As ******** increases, arterial concentration (at t = ********) approaches 0.37x arterial conc with no air change) **

****** ****=1 minute**

****** ****=6 minutes**

****** ****= Air Change Time **

## KINETIC MODELING OF ARTERIAL HFC236fa BLOOD CONCENTRATION IN VENTILATED AIRCRAFT

**As ******** increases, arterial concentration (at t = ********) approaches 0.37x arterial conc with no air change) **

*k**1**= 27.73*
*k**2**= 3.924*

****** ****= Air Change Time**

## For any  , get the maximum safe concentration,C from the curve :

**KINETIC MODELING OF ARTERIAL BLOOD ****HFC236fa ****CONCENTRATION IN VENTILATED AIRCRAFT**

***(=12.75 with no ventilation)***** **

***Perfect mixing assumed***

*For any **** , get the maximum safe concentration,C from the curve :*

## KINETIC MODELING OF ARTERIAL BLOOD HFC236fa CONCENTRATION IN VENTILATED AIRCRAFT

## KINETIC MODELING OF ARTERIAL BLOOD CONCENTRATIONS  IN VENTILATED AIRCRAFT

***Perfect mixing assumed***

**S = Specific volume of the agent at sea level:    **
**         **At  70oF (21.1oC):  S= 2.4574 ft3/lb
**A = Altitude correction factor for S:**
-          At 8000 ft:**              **A= 1.346
-          At 14,000 ft:           A= 1.702

***Solve equation or use  graph or table:***

| Altitude
(ft) | Temp
(oF) | Specific Volume = S x A
(ft3/lb) | Maximum Safe Weight for Hazard Volume, W/V (lb/ft3)   
         Maximum Safe Concentration  at Altitude (% by Volume) |  |  |  |  |  |  |  |  |  |  |  |  |  |
| --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- |
|  |  |  | 14 | 15 | 16 | 17 | 18 | 19 | 20 | 21 | 22 | 23 | 24 | 25 | 26 | 27 |
|   8, 000
 | 70 | S=2.4574       A=1.346
3.3077 | .0492 |  |  |  |  |  |  |  |  |  |  |  |  |  |
| 14,000
 | 70 | S= 2.4574      A=1.702
4.1825 |  |  |  |  |  |  |  |  |  |  |  |  |  | .0884 |

**Maximum Safe Weight HFC236fa**

## 1st ORDER KINETIC MODELING OF ARTERIAL 

**BLOOD CONCENTRATION HISTORIES**

-    Provides a ***simple mathematical solution***  to obtain data needed to develop perfect mixing ventilation tables which will provide maximum safe extinguishing agent weights for a range of compartment volumes and air change times.
-     Monte Carlo simulations of arterial blood concentration histories for 5 minute exposures to constant agent concentrations are used as input data for developing equations (95% confidence) for each extinguishing agent.
-   PBPK arterial blood data has been published for HFC 236fa and HFC 237fa which accounts for 95% (two standard deviations) of the simulated population having 5 minute arterial  blood concentrations below the target concentration.
-  Equations can be developed for each agent, which transform agent concentration histories to arterial blood concentration histories in ventilated spaces.
-   Demonstrated to work for predicting blood concentration histories for exposures to a constant concentration of agent.
-   Must be validated for predicting blood concentration histories for exposures to changing concentrations of agent.

## LOW OXYGEN HYPOXIA AT ALTITUDE: Very Small Aircraft  (Min. Safe Vol. = 53.5 cubic feet for 1 5BC HFC236fa extinguisher at 

***14,000 ft. if ************ ******= 0.5 min, C******0 ******= 27%)******  ******TENTATIVE HYPOXIA GUIDANCE 1:***

**Agent design concentration ****at *****FAA allowed maximum P altitudes***** can not exceed:**
**For all pressurized aircraft *****(at 8,000 ft P):*****   ****30 %****  *****(independent of cabin temperature)***
**For all unpressurized aircraft *****(at 14,000 ft P):*****  ****30%**** if aircraft descends to  8,000 ft. **
**within 1 minute. or 30% if cabin ventilates at least 1 air change/minute & descends to **
**12,000 ft. in 1 min.**** **

| Altitude (ft) | P            (mm Hg) | PO2             (mm Hg) | PAO2
(mmHg) | PAO2 with 30% 
Halocarbon
(mm Hg) | PAO2 with 30% Halocarbon (mm Hg)
after ventilating for  minutes,  when  ≤ 1 minute |
| --- | --- | --- | --- | --- | --- |
| 0 | 760 | 159.21 | 103.0 | 72.1 | =72.1+(103-72.1)*.63 = 91.6 |
| 8,000 | 564.64 | 118.29 | 68.9 | 48.2     | =48.2+(68.9-48.2)*.63= 61.2 |
| 9,000 | 543.31 | 113.82 | 65.0 | 45.5 | =45.5+(65.0-45.5)*.63= 58.1 |
| 10,000 | 522.73 | 109.51 | 61.2 | 42.8 | =42.8+(61.2-42.8)*.63= 54.4 |
| 11,000 | 502.92 | 105.36 | 57.8 | 40.5 | =40.5+(57.8-40.5)*.63= 51.4 |
| 12,000 | 483.36 | 101.26 | 54.3 | 38.0 | =38.0+(54.3-38.0)*.63= 48.3 |
| 13,000 | 464.82 | 97.38 | 51.0 | 35.7 | =35.7+(51.0-35.7)*.63= 45.3 |
| 14,000 | 446.53 | 93.55 | 47.9 | 33.5 | =33.5+(47.9-33.5)*.63= 42.6 |

*Unpressurized aircraft currently allowed to fly at 14,000 ft. P for 30 minutes.*

## LOW OXYGEN HYPOXIA AT ALTITUDE  Very Small Aircraft   

**(*****Min. Safe Vol. = 59 cubic feet for 1 5BC HFC236fa extinguisher at ***
***14,000 ft. if ************ = 0.5 min, C0 = 22%)***** *****TENTATIVE HYPOXIA GUIDANCE 2:***

- Agent design concentration **at *****FAA alowed maximum P altitudes*** can not exceed:
- For all pressurized aircraft ***(at 8,000 ft):***   **22 %**  *(independent of cabin temperature)*
- For all unpressurized aircraft ***(at 14,000 ft):***  **22%** if aircraft descends to  8,000 feet
- within 1 minute. or **22%** if cabin ventilates at least 1 air change/minute & descends to
- 12,500 ft. in 1 minute.

| Altitude (ft) | P            (mm Hg) | PO2             (mm Hg) | PAO2
(mmHg) | PAO2 with 22% 
Halocarbon
(mm Hg) | PAO2 with 30% Halocarbon (mm Hg)
after ventilating A/C  for  minutes, when  ≤ 1 minute |
| --- | --- | --- | --- | --- | --- |
| 0 | 760 | 159.21 | 103.0 | 80.3 | =80.3+(103-80.3)*.63 = 94.6 |
| 8,000 | 564.64 | 118.29 | 68.9 | 53.7     | =53.7+(68.9-53.7)*.63= 63.3 |
| 9,000 | 543.31 | 113.82 | 65.0 | 50.7 | =50.7+(65.0-50.7)*.63= 59.7 |
| 10,000 | 522.73 | 109.51 | 61.2 | 47.7 | =47.7+(61.2-47.7)*.63= 56.2 |
| 11,000 | 502.92 | 105.36 | 57.8 | 45.1 | =45.1+(57.8-45.1)*.63= 53.1 |
| 12,000 | 483.36 | 101.26 | 54.3 | 42.4 | =42.4+(54.3-42.4)*.63= 49.9 |
| 13,000 | 464.82 | 97.38 | 51.0 | 39.8 | =39.8+(51.0-39.8)*.63= 46.9 |
| 14,000 | 446.53 | 93.55 | 47.9 | 37.4 | =37.4+(47.9-37.4)*.63= 44.0 |

*Unpressurized aircraft currently allowed to fly at 14,000 ft. for 30 minutes.*

## A/C LANGUAGE FOR HALOCARBON FIRE EXTINGUISHERS

-  Provide safety guidance for halocarbon extinguishers.
-  Recommends a minimum UL rated 5 B:C sized extinguisher for occupied spaces
-  The proposed A/C requires adherence to the handheld Minimum Performance Standard for occupied spaces on transport category aircraft.
-  Recommends throw ranges for various sized aircraft
-  Recommends discharge hose or adjustable wand.
-  Provides guidance for minimizing risk of low oxygen hypoxia when released at altitude.

## A/C LANGUAGE FOR HALOCARBON FIRE EXTINGUISHERS

-    States the maximum weight that ***all*** extinguishers should not exceed, based on agent toxicity, size of compartment, and maximum FAA-allowed altitude of the cabin.
-    May allow increased halocarbon clean agent concentrations in ventilated compartments:
-  Consideration of allowing use of ventilation tables for small aircraft only.
-  Tables can be developed if PBPK data is available.
-  Tables would provide the maximum safe weight of agent based on safe concentration at altitude, compartment volume, time for an air change, and hypoxia considerations.
-  Provides updated safe handling guidelines based on adverse toxicological or cardiac sensitization events and PBPK modeling.
-    Operators of non-transport category aircraft should become familiar with the information in this A/C.
-    The proposed AC is subject to change/ rewrite by the FAA Aircraft Certification Office.

## CAVEATS

-    The contents of this presentation have not had a complete toxicological review.
-   The validity of applying existing kinetic models to high air change rates is uncertain at this moment.
-   The hypoxic guidelines need to be reviewed by aeromedical experts with experience with high altitude, low oxygen hypoxia issues.
-    The proposed AC is subject to change/ rewrite by the FAA Aircraft Certification Office.

## WORKING GROUP PARTICIPANTS

-  Louise Speitel	FAA
-  Rich Mazzone	Boeing
-  Bradford Colton	American Pacific Corp
-  Howard Hammell	Dupont
-  Steve Happenny    FAA
-  Gary Jepson	Dupont
-  Bella Maranion	EPA
-  Reva Rubenstein	ICF Consulting

## http://www.fire.tc.faa.gov

- _[http://www.fire.tc.faa.gov](http://www.fire.tc.faa.gov/)_

## HANDHELD TASK GROUP

**Wednesday 12:30- 3:00**
**Open Meeting**