Electromagnetic interference (EMI) from passenger-carried portable electronic devices (PED) on commercial airplanes has been reported as being responsible for anomalous events during flight. The operation of PEDs produces uncontrolled electromagnetic emissions that could interfere with airplane systems. Airplane systems are tested to rigorous electromagnetic standards to establish and provide control of the electromagnetic characteristics and compatibility of these systems. However, PEDs are not subject to these same equipment qualification and certification processes. Though many cases of EMI have been reported over the years, with PEDs suspected as the cause, it has proven almost impossible to duplicate these events. Boeing has participated in several related activities and has revised its all-model service letter for concurrence with the U.S. Federal Aviation Administration (FAA) advisory circular (AC) on the use of cell phones while airplanes are on the ground. However, operators and their flight crews are ultimately responsible for deciding whether to allow the use of PEDs.

1. Testing and analysis of PEDs and airplane systems.
2. Resulting regulations and recommendations.
3. Operator actions for investigating and preventing PED events.
4. Ongoing related activities at Boeing.

1. TESTING AND ANALYSIS OF PEDS AND AIRPLANE SYSTEMS
Boeing has conducted several tests and investigations to better understand the effects of PED use on airplane systems. These include analysis of operator reports, investigation of specific instances of suspected PED interference, ground and airplane tests of in-seat power, and cell phone tests and analysis.

Analysis of operator reports.
Boeing has received many reports related to PEDs from operators. The majority of these reports were inquiries about PEDs in general. The remaining reports involved airplane anomalies and can be grouped into one of three categories of PED events: (1) events where PED interference was suspected (an airplane anomaly occurred when a PED was being operated), (2) events with an apparent correlation between PED operation and the airplane anomaly (the problem disappeared when the PED was turned off, either immediately or shortly thereafter), and (3) events showing a strong correlation between PED operation and the airplane anomaly (the problem disappeared when the PED was turned off, returned when PED use resumed, and disappeared when the PED was turned off again).

Of the reports involving airplane anomalies, only a few showed a strong correlation between the airplane reaction and the suspected PED.

Investigation of specific instances of suspected PED interference.
Some sample cases are included here to illustrate the variety of potential PED events.

1995, 737 airplane.
A passenger laptop computer was reported to cause autopilot disconnects during cruise. Boeing purchased the computer from the passenger and performed a laboratory emission scan from 150 kHz to 1 GHz. The emissions exceeded the Boeing emission standard limits for airplane equipment at various frequency ranges up to 300 MHz. Boeing participated with the operator on two flight tests with the actual PED, using the same airplane and flight conditions, in an attempt to duplicate the problem. Using even these extensive measures to re-create the reported event, Boeing was unable to confirm the reported interference between the PED and the airplane system.

1996/1997, 767 airplane.
Over a period of eight months, Boeing received five reports on interference with various navigation equipment (uncommanded rolls, displays blanking, flight management computer [FMC]/ autopilot/standby altimeter inoperative, and autopilot disconnects) caused by passenger operation of a popular handheld electronic game device. In one of these cases, the flight crew confirmed the interference by turning the unit on and off to observe the correlation. The same unit was used on another flight and on a different airplane, but the event could not be duplicated. Boeing purchased two of the actual suspect units through the airline and tested them in the laboratory, along with three off-the-shelf units. It was determined that these suspect units had emission profiles similar to the off-the-shelf units and that the levels from these devices were below airplane equipment emission limits.

1998, 747 airplane.
A passenger’s palmtop computer was reported to cause the airplane to initiate a shallow bank turn. One minute after turning the PED off, the airplane returned to "on course." When the unit was brought to the flight deck, the flight crew noticed a strong correlation by turning the unit back on and watching the anomaly return, then turning the unit off and watching the anomaly stop. Boeing was not able to purchase the actual PED, but contacted the PED manufacturer and purchased the same model. Boeing laboratory emission testing revealed that the unit exceeded Boeing airplane equipment emission levels by up to 37 dB by demonstrating energy levels in the frequency range of 150 to 700 kHz. In the Boeing navigation laboratory the unit was placed next to the FMCs, control display unit, and integrated display unit, but the reported anomaly could not be duplicated.

As a result of these and other investigations, Boeing has not been able to find a definite correlation between PEDs and the associated reported airplane anomalies. For future considerations and investigations, other factors are becoming significant. Qualification levels related to high-intensity radiated fields (HIRF) for new airplane equipment are higher than almost any level of emissions from passenger PEDs. The size of many PEDs is shrinking and, as a result, these units require less power to operate. Though this can increase the margin between airplane system susceptibility test levels and PED emissions, some PEDs are now operating in new frequency bands and are combining multiple functions, making it more difficult to distinguish between intentionally and non-intentionally transmitting PEDs (see below).

Consequently, some airplane systems that have not been reported as being susceptible to PEDs, such as the global positioning system, weather radar, and radio altimeter, may pick up energy from newer PEDs that operate in the high-frequency bands and whose harmonics or other noise may fall within one of these airplane systems’ operating bands.

Ground and airplane tests of in-seat power.
Operators have asked Boeing to install and certify in-seat power outlets for passenger use of laptop computers. Boeing and the FAA have three related electromagnetics concerns: (1) whether installing the outlets will increase the use of laptop computers and a corresponding number of potential PED events, (2) whether the power cord will introduce additional radiated emission effects, and (3) whether laptop connections will corrupt airplane power by conducting emissions into the airplane power system.

Boeing certifies the in-seat power system but does not certify or control the power cords and what is connected to them. The in-seat power system is qualified to the same standards as any other airplane system. Sufficient attenuation is required within the power supply to ensure that the conducted emissions from laptop computers are not fed into the airplane power system. In addition to the laboratory tests performed by the supplier, Boeing is required to conduct airplane tests where the system is fully loaded with laptop computers.

Boeing has tested in-seat power on eight airplanes: two 737s, one 747, two 767s, and three 777s. The number of laptops operating simultaneously in each test ranged from 32 to 245. Included with the laptops were a mixture of compact-disc players and electronic games. Boeing found no airplane susceptibility in these eight tests, though some emissions were found to be extremely noisy in the laboratory (up to 40 dB over the airplane equipment emission limit). The noise levels were above the airplane equipment emission levels from 150 kHz to 500 MHz. Even though these computers did not cause any airplane system anomalies, Boeing has observed airplane antenna receiver susceptibility from "noisy" systems with levels significantly lower than those recorded by the laptop computers used in the tests.

Cell phone tests and analysis.
Boeing conducted a laboratory and airplane test with 16 cell phones typical of those carried by passengers, to determine the emission characteristics of these intentionally transmitting PEDs. The laboratory results indicated that the phones not only produce emissions at the operating frequency, but also produce other emissions that fall within airplane communication/navigation frequency bands (automatic direction finder, high frequency, very high frequency [VHF] omni range/locator, and VHF communications and instrument landing system [ILS]). Emissions at the operating frequency were as high as 60 dB over the airplane equipment emission limits, but the other emissions were generally within airplane equipment emission limits. One concern about these other emissions from cell phones is that they may interfere with the operation of an airplane communication or navigation system if the levels are high enough.

Boeing also performed an airplane test on the ground with the same 16 phones. The airplane was placed in a flight mode and the flight deck instruments, control surfaces, and communication/navigation systems were monitored. No susceptibility was observed.

Telephones installed and certified on the airplane by Boeing or operators are not actually cell phones, but part of an airborne certified satellite system. These phones are electromagnetically compatible with the airplane systems because their emissions are controlled. In contrast, the emissions from passengers’ cell phones are not known or controlled in the same way as permanently installed equipment.

2. RESULTING REGULATIONS AND RECOMMENDATIONS

All electrical and electronic airplane systems are qualified to meet stringent requirements for electromagnetic susceptibility. They are tested to well-established limits during various modes of operation and with setup configurations that represent the airplane installation in terms of electromagnetic protection. Sufficient margins exist between the qualification susceptibility test level and the expected airplane environment noise levels. Compliance with these requirements provides a high level of confidence that the airplane systems will function as intended in the electromagnetic environment of the airplane. However, susceptibility can occur in the airplane if an uncontrolled source of electromagnetic energy radiates emission levels above the susceptibility level to which the airplane system was tested or if the airplane system protection has been degraded.

In addition, airplane systems with a receiving antenna component have an exception from the susceptibility requirements. The radio frequency (RF) radiated susceptibility test is performed on the system over a full frequency spectrum, but not in the designed operating frequency band of the antenna. No value is gained from performing the RF radiated susceptibility test in the operating band of the antenna because it is designed to respond to signals in this band. PEDs can radiate non-intentional noise within the airplane antenna’s operating frequency band, and this can create EMI. Because the basic function of an antenna-based system is to seek and find low-level electromagnetic signals and to respond to signals in a certain frequency band, the probability of interference to these systems is more likely than interference to systems not connected to an antenna receiver.

As a result of these conclusions, recommendations and regulations regarding PED-related anomalies have been established by several agencies, including the U.S. Radio Technical Commission for Aeronautics (RTCA), the FAA, the U.S. Federal Communications Commission (FCC), and Boeing.

RTCA.
The RTCA has focused its attention on airplane system susceptibility with the highest probability of EMI from a PED -- namely, airplane antenna receiver systems. (RTCA document DO-199, "Potential Interference to Aircraft Electronic Equipment From Devices Carried Aboard," lists the eight conditions that are required for an airplane antenna receiver system to experience interference from a PED.)

The RTCA concluded that the probability of a PED interfering with an airplane receiver system is very low. In the case of an ILS localizer antenna, the probability of PED interference was calculated as one in one million. Based on the total number of flights per year (determined in 1988), the expected ILS localizer receiver disruption is once in any two-year period.

The first national committee that investigated interference by passenger-carried PEDs was created in the early 1960s. Its activities were initiated by a report that a passenger-operated portable FM broadcast receiver caused an airplane navigation system to indicate that the airplane was off course by more than 10 deg. The airplane was actually on course and, when the portable receiver was turned off, the malfunction ceased. A final report from this committee, RTCA DO-119, was issued in 1963 and resulted in the revision of the FAA Federal Aviation Regulations (FAR) by establishing a new rule (FAR 91.19, now 91.21), which states that the responsibility for ensuring that PEDs will not cause interference with airplane navigation or communication systems remained with the operator of the airplane.

In the early 1980s, media attention focused on in-flight portable computer use and variations in airline policies. Some computer trade publications suggested that their readers avoid particular operators who restricted the use of portable computers. As a result, one operator requested that a special committee be formed to "generate a Minimum Operational Performance Standards document against which manufacturers (of computers and other portable electronic devices) marketing their products for airborne use, could test and label them as meeting this standard in a manner similar to the Underwriters Laboratories Inc. sign of approval." In 1988, a final report was released (RTCA DO-199) that recommended the following:

• Acceptable limits of radiation and associated test methods for PEDs should be established.
• The FCC should specify a new classification for PEDs that may be operated on board airplanes.
• The FAA should initiate a regulatory project to revise FAR 91.19, providing guidance for acceptable methods of compliance and to develop methods to enhance public awareness.
• Standardized reporting of suspected interference by PEDs should be implemented.

In 1992, the U.S. Government requested that the RTCA resolve outstanding questions on PEDs to ensure air safety, specifying that unnecessary restrictions should not be placed on untested PEDs, and to gain an understanding of multiple effects and those from intentional radiators such as remote control devices and cell phones. For various reasons, intentional radiators were not evaluated. In 1996, the committee issued its report, RTCA DO-233. The recommendations are as follows:

1. The FAA should modify FAR 91.19 (now 91.21), Portable Electronic Devices, so that
   1. The use of any PED is prohibited on airplanes during any critical phase of flight.
   2. The use of any PED having the capability to intentionally transmit electromagnetic energy is prohibited in an airplane at all times unless testing has been conducted to ascertain its safe use.
2. PED testing efforts should be continued and should include existing and new technology devices such as satellite communications, embedded communications devices, and two-way pagers.
3. A public awareness campaign should be initiated to educate the flying public about PEDs and especially those designed as intentional radiators.
4. More research is needed on the design and feasibility of detection devices.

FAA.
In 1993, the FAA issued AC 91.21-1, "Use of Portable Electronic Devices Aboard Aircraft." This circular provides guidance to the airlines in establishing compliance with FAR 91.21, which provides recommended procedures for airlines and test criteria for manufacturers. For the use of cell phones, the AC states that the FCC currently prohibits the use and operation of cell phones while airborne. The reason for this relates primarily to cellular ground base system susceptibility because a cell phone in the air will have greater coverage (transmitting to several cell bases simultaneously on the same frequency) than a cell phone on the ground (transmitting to one cell base). The FAA supports this airborne restriction because of the potential for interference to critical airplane systems. Currently, the FAA does not prohibit use of cell phones in airplanes while on the ground if the operator has determined that they will not cause interference with the navigation or communication system of the airplane on which they are to be used. An example might be use at the gate or during an extended wait on the ground, when specifically authorized by the captain. A cell phone must not be authorized for use while the airplane is taxiing for departure after leaving the gate. The unit must be turned off and properly stowed; otherwise, a signal from a ground cell could activate it.

FCC.
The U.S. Code of Federal Regulations, title 47, part 22, subpart H, "Cellular Radiotelephone Service," section 22.925, "Prohibition on airborne operation of cellular telephones," states that cell phones installed in or carried aboard airplanes must not be operated while such airplanes are airborne (not touching the ground). When any airplane leaves the ground, all cell phones on board that airplane must be turned off, and the use of cell phones while airborne is prohibited by FCC rules. The use of cell phones on the ground and in the airplane is also subject to FAA regulations.

Boeing.
In addition to its active participation on the last two RTCA committees, Boeing released an all-model service letter in 1993 to provide guidance to operators regarding the use of PEDs. The letter included the following statements:

• Use of intentional transmitters should be prohibited at all times.
• Use of non-intentional transmitters should be prohibited during takeoff and landing (critical stages of flight).
• Operation of non-intentional transmitters should be allowed for use during noncritical stages of flight unless the operator of the airplane has determined otherwise.
• Airline procedures should be established for PED termination if problems arise.
• Data should be recorded during a suspected PED-related event.

Boeing has revised its service letter to be in accordance with the FAA AC on the use of cell phones while the airplane is on the ground.

3. OPERATOR ACTIONS FOR INVESTIGATING AND PREVENTING PED EVENTS
Because PED interference is often named as the cause of airplane anomalies, operators should be thorough when confirming a cause-and-effect relationship. Other possibilities should always be considered, including loose cables or other maintenance issues, flight crew activity, and HIRF.

The initial reports that operators submit to Boeing about possible PED interference must contain sufficient detail to allow further investigation, if desired. Follow-up information is difficult to obtain because the passenger and the PED involved in the event are seldom available, details may not have been fully documented, and relevant data may be unknown. To support further investigation, operators should provide the following data:

• Model and make of the PED.
• Identification of peripherals used with the PED.
• Seat location of the PED.
• Operating mode of the PED.
• Name, address, and telephone number of the passenger using the PED.
• Airplane model and tail number or effectivity number.
• Identification of airplane system and description of anomaly.
• Frequency and operation mode of the airplane system, if applicable.
• Length of time between PED shutoff and airplane system recovery, and confirmation of whether the PED was cycled off and on to confirm the cause-and-effect relationship.
• Flight phase and route.
• Copy of flight data recorder output.
• Results of postmaintenance inspection.

4. ONGOING RELATED ACTIVITIES AT BOEING
Boeing continues to monitor its fleet through reports submitted by operators and to investigate these reports when possible. The company continues to share its experience and knowledge of PEDs and airplanes with the industry and the public. Boeing is committed to supporting future committee activity and investigations into PED detection devices.

BRUCE DONHAM
PRINCIPAL ENGINEER & DESIGNATED ENGINEERING REPRESENTATIVE

ELECTROMAGNETIC EFFECTS AND ANTENNAS
BOEING COMMERCIAL AIRPLANES GROUP