AGL Component Library By Precision AGL Academy

Portable PAPI

A transportable, rapidly deployable Precision Approach Path Indicator system designed for temporary airfields, military operations, disaster relief, and emergency landing strips. Portable PAPI offers the same intuitive red/white visual glide slope guidance as fixed PAPI, but in a rugged, self‑contained package that can be set up in minutes without permanent infrastructure.

Portable PAPI transportable red/white glide slope indicator for temporary airfields

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Overview

What Is It?

The Portable PAPI is a self‑contained, transportable version of the standard Precision Approach Path Indicator. It consists of four light units (or sometimes two, in a portable APAPI configuration) mounted on a lightweight, collapsible tripod or base, with integrated power sources (batteries, solar panels, or portable generators) and control electronics. The system is designed to be rapidly deployed and calibrated without the need for permanent foundations, underground cabling, or fixed power infrastructure.

Portable PAPI is ideal for temporary airfields, military forward operating bases, humanitarian relief operations, emergency landing strips, and any situation where a permanent visual glide slope system is not feasible. Despite its portable nature, it delivers the same high‑intensity, precision beam pattern and colour‑transition accuracy as its fixed counterpart, ensuring safe approaches for both fixed‑wing and rotary‑wing aircraft.

Purpose

Purpose & Function

A portable PAPI exists to bring precision glide slope guidance to places where a permanent installation isn't possible or isn't yet justified — a disaster relief strip, a forward operating base, or a temporary runway supporting an event or emergency. Without it, pilots approaching an unfamiliar or hastily prepared airstrip would have to rely on non-visual approach aids or judgement alone, both of which carry a much higher margin for descent-angle error, especially in poor light or unfamiliar terrain.

By replicating the same red/white colour transition and beam accuracy as a fixed installation, the portable system lets a pilot approach with the same confidence and technique they'd use anywhere else, without needing special training or procedures just because the glide slope indicator happens to be sitting on a tripod rather than a permanent foundation.

Application

Where Is It Used?

Portable PAPI is used in a wide range of temporary and rapidly changing operational environments:

  • Military forward operating bases – where runways are temporary and need rapid setup.
  • Humanitarian relief operations – after natural disasters, where permanent infrastructure is damaged.
  • Emergency landing strips – for medical evacuation or disaster response.
  • Temporary airfields for events – airshows, firefighting, or construction projects.
  • Remote or austere locations – where power and cabling are not available.
  • As a backup or supplement to fixed PAPI – for maintenance or contingency operations.
Placement

Installation & Location

Rather than a fixed frangible mount on a permanent base can, Portable PAPI units sit on ground-bearing skids, trailers, or tripod-style frames that can be positioned directly on the surface without excavation or cut-in works. Set-out still follows the same principle as fixed PAPI — a wing bar at a set lateral offset from the runway edge and a setback from the threshold chosen to give the correct glide angle over the aiming point — but the position is established with a portable survey or GPS reference rather than a permanent as-built survey, and the bar is levelled unit-by-unit using built-in bubble levels or self-levelling mounts. Power is typically supplied by an integral battery pack, solar panel, or portable generator rather than mains-fed constant current regulators, allowing the whole system to be set out, aligned, and made operational within a short window, then struck and relocated once the runway or task is no longer needed.

Function

How Does It Work?

Portable PAPI functions on the same optical principles as fixed PAPI, but with integrated power and control systems:

  • Optical Design: Each light unit contains a high‑intensity LED array or halogen lamp with precision optics that project a beam with a sharp red/white transition. The transition angle is set to the desired glide path (typically 3° but adjustable).
  • Colour Indication: The four‑light display provides the standard red/white combination:
    • All white – well above the glide path.
    • 3 white / 1 red – slightly above.
    • 2 white / 2 red – on the correct glide path.
    • 1 white / 3 red – slightly below.
    • All red – well below.
  • Power and Control: The system is typically powered by rechargeable batteries (with solar panels for extended operations) or a portable generator. A built‑in control unit provides intensity adjustment (day, twilight, night) and may include remote control or wireless monitoring capabilities.
  • Deployment: The units are placed on a level surface at the required distance from the runway threshold, aligned using a built‑in compass and spirit level or a portable theodolite. The entire system can be set up by two people in under 30 minutes.
Architecture

System Architecture & Control Logic

Portable PAPI keeps the same fixed-optics signal as permanent PAPI — each unit's lens/shutter is still tilted to a specific elevation so the red/white transition sits at the right point — but replaces the CCR series circuit with a self-contained power and control chain. A battery bank (charged by solar panel, mains, or topped up by a portable generator) feeds a built-in control unit, which is the electronic equivalent of the CCR: it sets one shared brightness level across all four units for day, twilight, or night, and on models with wireless monitoring, reports state of charge and unit status to a handheld or remote link rather than to an ALCMS. Because there's no buried series loop, there's also no loop-voltage fault detection — each unit is typically wired to the control unit individually, so a lamp or driver failure is more often caught by directly checking that unit than inferred from circuit behaviour. The part that still has to be done by hand, every deployment, is optical alignment: units are levelled and aimed using a built-in compass and spirit level or a portable theodolite, since the elevation that encodes the glide path is set fresh each time the array is placed rather than fixed permanently in the ground.

Battery / Solar / Generator → Built-in Control Unit → Per-Unit Wiring → Light Unit (elevation re-aimed on each deployment)

BATTERY / SOLAR / GENERATOR 12V / 24V, 8–12 hr runtime BUILT-IN CONTROL UNIT Sets shared brightness; may report status wirelessly PER-UNIT WIRING (NO SERIES LOOP) Each unit addressed individually, not looped LIGHT UNIT (×4) Aimed fresh each deployment with theodolite/level Elevation not permanent — re-set on relocation NO LOOP FEEDBACK — CHECK UNITS DIRECTLY Without a series circuit, a lamp/driver fault is found by inspection, not inferred from loop voltage
System Architecture

No Permanent Infrastructure Required

The thing that actually makes this "portable" isn't the optics — it's identical to fixed PAPI. It's that nothing here needs to be buried, poured, or wired in: a tripod and a battery replace the foundation and the CCR series circuit, so two people can have it aligned and running in under 30 minutes.

FIXED PAPI Permanent Foundation Poured base, fixed alignment Underground CCR Circuit 6.6A series loop, buried cabling Fixed 4‑Unit PAPI Array Permanent, pre‑surveyed position NO CIVIL WORKS PORTABLE PAPI Tripod / Collapsible Base Level surface, no digging Battery / Solar / Generator 12V / 24V, 8–12 hr runtime Deployed & Aligned Under 30 min, two‑person crew
Fixed PAPI — permanent civil & electrical works
Portable PAPI — self‑contained, no fixed infrastructure
Construction

Physical Construction

Each portable unit is a compact, weatherproof housing in lightweight aluminium or high-impact polymer, built around the same lower red-filter / upper white-glass optical split as a fixed PAPI, with a built-in spirit level and pitch-adjustment mechanism for setting the glide-path angle in the field without survey equipment. The housing sits on a folding tripod or ballasted skid base rather than a buried frangible mast, so the whole unit can be man-carried, levelled, and aimed by two people without excavation or concrete footings. Power comes from an integrated 12V/24V battery pack, charged by an attached solar panel or a portable generator rather than a mains-fed isolating transformer, and units link back to a small field controller for step-brightness or on/off control. This self-contained design is intended for temporary glide-path guidance — during runway works, at deployed or expeditionary airfields, or as a fallback when a fixed PAPI is out of service — and is designed to be struck and removed rather than left as a permanent installation.

Specification

Technical Parameters

ParameterTypical Value
Light SourceHigh‑intensity LED array (or 100W halogen)
ColourWhite (upper beam) and Red (lower beam) per unit
Luminous IntensityUp to 20,000 cd (white) and 10,000 cd (red)
Intensity Steps3‑step (day, twilight, night) – manually or remotely controlled
Glide Path AngleTypically 3° (2.5° to 4° adjustable)
Beam PatternNarrow vertical beam with sharp red/white transition
Number of Units4 (standard portable PAPI) or 2 (portable APAPI)
Power SourceIntegrated batteries (12V/24V), solar panels, or portable generator
Battery Life8–12 hours (continuous use) with solar recharging option
Weight per Unit10–15 kg (22–33 lbs) including tripod/base
Deployment TimeLess than 30 minutes for two persons
Protection ClassIP65 / IP67 (weather‑resistant, dustproof)
Operating Temperature-20°C to +50°C
Power Supply

Electrical Requirements

RequirementTypical Value
Power SourceIntegrated battery bank (12V/24V DC), solar panel trickle charge, or portable petrol/diesel generator
Battery TypeSealed lead-acid or LiFePO4, sized to the stated 8–12 hour runtime
ChargingSolar panel (typically 50W–100W per unit) or mains/generator battery charger
Inter-Unit CablingLow-voltage DC cable between units, or self-contained units with no shared series loop
Voltage12V or 24V DC per unit (no isolating transformer or airfield series circuit required)
Fault ProtectionBattery management system with low-voltage disconnect and short-circuit protection
Earthing/GroundingLocal earth spike/rod per unit where required by the site risk assessment
Protection Class (Electrical)IP65 / IP67 sealed battery and control compartment
Remote/Manual ControlStep selection via local control panel or remote handset, independent of any fixed CCR
Optical Performance

Photometric Requirements

ParameterTypical Value
Main Beam Intensity (White)≥ 14,000 cd on-axis per unit, up to 20,000 cd at full intensity
Main Beam Intensity (Red)≥ 7,000 cd on-axis per unit, up to 10,000 cd at full intensity
Transition Sharpness (Red/White)≤ 3 arc-minutes vertical transition band per unit
Vertical Beam Spread4 units (or 2 for portable APAPI) splayed about the site-set 3° reference
Horizontal Beam Spread± 5° to ± 10° either side of runway centreline plane
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-28 figures
Chromaticity (White)Within ICAO Annex 14 white boundary (CIE coordinates)
Chromaticity (Red)Within ICAO Annex 14 red boundary (CIE coordinates)
Intensity Tolerance± 25% of rated value at each control-unit step (field measurement)
Maintenance Factor≥ 50% of new-fixture intensity before LED/lens replacement is due
Test MethodPortable photometer or fixed test bench, verified after each deployment
Compliance

Applicable Standards

ICAO Annex 14

PAPI specifications – applicable to portable systems

FAA AC 150/5345-28

Precision Approach Path Indicator (PAPI) systems – includes portable PAPI guidance

FAA AC 150/5345-50B

Specification for Portable Runway and Taxiway Lights

IEC/TS 61827

Characteristics of inset and elevated luminaires used on aerodromes and heliports (photometric & electrical performance)

Prerequisites

Installation Requirements

Portable Survey/GPS Reference Setout
Site

Establish the lateral offset from the runway edge and setback from the threshold using a portable survey or GPS reference rather than a permanent as-built survey, following the same glide-angle principle as fixed PAPI.

Skid/Tripod Placement & Levelling
Mechanical

Position each ground-bearing skid, trailer, or tripod frame directly on the surface without excavation, levelling unit-by-unit using built-in bubble levels or self-levelling mounts.

Unit-by-Unit Aiming
Mechanical

Aim each unit to place the on-slope indication correctly over the aiming point at the required glide angle.

Power Source Connection
Power

Connect the integral battery pack, solar panel, or portable generator for each unit in place of a mains-fed isolating transformer.

Inter-Unit Spacing & Alignment Check
Mechanical

Confirm equal spacing and alignment across the bar, since there is no permanent fixing to hold the units in relation to each other.

Stability & Anchoring for Site Conditions
Mechanical

Secure skids or tripods against wind and any propeller or jet blast expected for the deployment duration.

Pre-Deployment Sign-off
Documentation

Record the GPS/survey reference, unit positions, and battery or charge state before the system is declared operational.

Recovery & Site Restoration Plan
Documentation

Confirm the strike-and-relocate procedure and site restoration steps for once the deployment period ends.

Verification

Testing & Commissioning

Battery & Charging System Check
Pre-Deployment

Verify each unit's battery charge state and confirm the solar panel or portable generator is correctly maintaining charge before the units are taken to site.

Deployment Stability Verification
Deployment

Confirm the tripod or ballasted skid base sits level and stable on the ground surface, since there is no buried footing to compensate for an uneven set-up.

Glide Path Angle & Unit Aiming Verification
Deployment

Set each unit's red/white transition to the design glide-path angle using the built-in spirit level and pitch adjuster, staggering units by the design increment without survey equipment.

Field Controller Step Response
Deployment

Cycle each unit through its day/twilight/night brightness steps from the field controller and confirm correct, synchronised response across all units.

Inter-Unit Alignment Check
Deployment

Sight along the row of deployed units to confirm consistent lateral alignment and spacing, since units are hand-placed rather than fixed on surveyed masts.

Photometric Verification
Deployment

Measure red and white beam intensity, colour, and transition sharpness on each unit with a calibrated photometer against the applicable commissioning tolerances.

Battery Life Endurance Check
Deployment

Confirm the expected 8–12 hour runtime under continuous use, or verify solar recharging keeps pace with planned operating hours for extended deployments.

Deployment Record & Sign-off
Deployment

Log unit positions, aiming angles, and photometric readings for the deployment period, since the temporary set-up has no permanent as-built record.

Upkeep

Inspection & Maintenance

Post-Deployment Alignment Check
Every deployment

Verify glide path angle with a theodolite or laser level after each setup, since integrated levels and compasses alone may not meet precision-approach tolerance.

Battery & Solar Panel Check
Every deployment

Test battery charge level and solar panel output before and during operation, since cloudy weather or high-intensity night use can drain batteries faster than expected.

Lens Cleaning
Every deployment

Clean dust, dirt, and moisture from each lens before use, since temporary and austere sites expose optics to contamination more readily than fixed installations.

Transport Case & Housing Inspection
Quarterly

Inspect transport cases, tripods, and unit housings for damage from repeated handling and transportation that could affect optics or electronics.

Wind Stability Check
Every deployment

Confirm tripods or bases are adequately secured against wind, adding ballast or guy ropes in high-wind conditions to maintain alignment.

Photometric Intensity Check
Annual

Verify white and red beam intensity against ICAO thresholds using a calibrated photometer to confirm the unit still meets performance specification.

Weatherproof Seal Inspection
Quarterly

Check housing seals and gaskets for wear so the IP65/IP67 rating is maintained across repeated field deployments.

Storage Charge Maintenance
Monthly

Top up integrated batteries during storage periods to prevent deep-discharge degradation ahead of the next deployment.

Field Notes

Common Field Issues

Rapid Deployment Calibration

Portable PAPI must be calibrated quickly and accurately in the field. The use of integrated levels and compasses helps, but precise alignment may require a theodolite or laser level, especially if the system is used for precision approaches. Regular practice and pre‑deployment checks are essential.

Battery Life and Power Management

Depending on the intensity setting and ambient conditions, battery life can be limited. Solar panels help extend operation, but cloudy weather or high‑intensity night operations may drain batteries quickly. Power management and backup batteries are critical for sustained operations.

Lens Contamination and Optical Degradation

In temporary or austere environments, lenses are more prone to dust, dirt, and moisture. Regular cleaning with appropriate materials is essential to maintain light output and colour transition integrity.

Transportation Damage

Frequent transportation can cause damage to optics, electronics, or mechanical components. Robust transport cases and careful handling are necessary to ensure the system remains operational when needed.

Wind and Environmental Stability

Portable tripods or bases must be adequately secured against wind and vibration. In high‑wind conditions, additional ballast or guy ropes may be required to maintain alignment.

Diagnostics

Troubleshooting Guide

One Unit Dark, Others Normal
Likely Cause
Failed LED module / lamp in that unit, a discharged or faulty individual battery connection, or a broken per-unit wiring link back to the control unit.
Diagnostic Steps
Check the unit's individual power connection and cable back to the control unit; verify battery voltage at the unit; swap in a known-good lamp/LED module if available to isolate the fault.
Corrective Action
Replace the failed lamp/LED module or repair the per-unit wiring connection; since there is no buried loop, faults are typically found by directly checking the affected unit rather than by loop testing.
Entire Array Dark / Control Unit Not Responding
Likely Cause
Depleted battery bank, a failed solar charge controller, or a fault in the built-in control unit that distributes power and brightness commands to all units.
Diagnostic Steps
Check battery state of charge and solar panel/generator input; verify the control unit powers on and reports status (via wireless monitoring if fitted); check the main power link from battery to control unit.
Corrective Action
Recharge or replace the battery bank, repair or replace the solar charge controller, or swap the control unit; confirm the array powers up before re-deployment.
Short or Degraded Runtime Between Charges
Likely Cause
Reduced battery capacity from age or temperature, insufficient solar input in overcast conditions, or higher-than-expected power draw at a high intensity step.
Diagnostic Steps
Check battery health and charge cycles; review solar panel output against expected conditions; confirm the intensity step in use matches operational need rather than defaulting to maximum brightness.
Corrective Action
Replace aging batteries, add or reposition solar panels for better exposure, or step down brightness when full intensity isn't required; keep charged spare batteries on hand for extended operations.
Misleading Red/White Split After Deployment
Likely Cause
Because alignment is re-established at every deployment rather than fixed permanently, a unit may have been leveled or aimed incorrectly using the built-in compass/spirit level, or ground settlement after placement has shifted the tripod or skid.
Diagnostic Steps
Re-check each unit's level and aim using a portable theodolite or laser level against the intended glide-path angle; verify the base/tripod hasn't settled or shifted on soft ground.
Corrective Action
Re-level and re-aim the affected unit(s), add ballast or wider footing on soft ground to prevent settlement, and re-verify alignment before returning the system to service.
Lens Contamination or Optical Degradation
Likely Cause
Temporary or austere deployment sites expose lenses to more dust, dirt, and moisture than permanent installations.
Diagnostic Steps
Inspect lenses for visible contamination and check light output against expected values.
Corrective Action
Clean lenses with appropriate materials on a more frequent schedule than a fixed installation would require, particularly after deployment in dusty or wet conditions.
Physical Damage After Transport
Likely Cause
Frequent transportation and handling can damage optics, electronics, or mechanical components, particularly if transport cases are inadequate or handling is rushed.
Diagnostic Steps
Inspect each unit after transport and before deployment for cracked lenses, loose fasteners, or damaged mounting hardware; power-test before final placement.
Corrective Action
Repair or replace damaged components before deployment, and use robust, well-padded transport cases with careful handling procedures to prevent recurrence.
Reliability

Failure Modes & Root Causes

Battery Depletion / Degradation
High Severity
Root Cause
Insufficient solar charging during extended overcast periods, an aging or deep-cycled battery pack past its usable capacity, or a unit left deployed longer than its power budget was planned for.
Effect
Dimming output as voltage sags, reduced operating hours, or complete loss of the unit overnight — a failure mode fixed PAPI, powered from mains-fed CCRs, does not share.
Detection Method
Battery state-of-charge check at each site visit, monitoring output intensity for gradual dimming, and logging deployment duration against the system's rated power autonomy.
LED Module / Lamp Failure
High Severity
Root Cause
Vibration damage sustained in transit, thermal cycling in exposed field conditions, or ordinary end-of-life lumen depreciation.
Effect
Single unit goes dark or drops below minimum intensity within the two- or four-light tripod-mounted array.
Detection Method
Visual confirmation that all units are alight at setup and during routine checks, and a photometric spot-check where equipment is available.
Tripod / Base Instability
High Severity
Root Cause
Soft or uneven ground at the rapidly-prepared deployment site, wind loading on the lightweight collapsible base, or ground stakes that were not adequately secured during setup.
Effect
Unit tilts or shifts out of aim tolerance, producing a misleading glide-slope indication — more likely here than on a fixed, surveyed foundation.
Detection Method
Visual level check at setup and after any high-wind event, and periodic re-verification of aim against the design glide angle during extended deployments.
Solar Panel / Charge Controller Fault
Medium Severity
Root Cause
Dust or debris accumulation on the panel surface, a failed or miswired charge controller, or panel damage from transport and rough handling.
Effect
Battery fails to recharge adequately during daylight hours, shortening the unit's effective night-time operating window.
Detection Method
Checking charge controller status indication and panel output current against expected values in daylight, and inspecting the panel surface for contamination.
Lens Contamination
Low Severity
Root Cause
Dust, sand, or debris typical of austere or disaster-relief sites settling on the lens during transport and deployment.
Effect
Reduced or hazy light output and a softened colour transition, harder to correct in the field without cleaning equipment on hand.
Detection Method
Visual inspection of the lens at setup and during routine checks, and a photometric spot-check where equipment is available.
Control Electronics / Enclosure Ingress
Medium Severity
Root Cause
Seal wear from repeated setup/teardown cycling, or exposure to conditions (rain, sand, humidity) beyond the enclosure's rated ingress protection during prolonged field use.
Effect
Erratic operation, corrosion of internal contacts, or complete failure of the control electronics driving the unit.
Detection Method
Inspection of enclosure seals and fasteners before each deployment, and checking for condensation or corrosion inside the housing after extended field use.
Precautions

Safety & Operational Notes

Battery Handling
Electrical Safety

Handle the sealed battery pack per the manufacturer's guidance, avoid puncturing or crushing it during transport, and check for swelling, heat, or leakage before each deployment rather than assuming a fully-charged pack is a healthy one.

Airside Work Coordination
Operational

Deployment or recovery of a portable PAPI on or near an active runway requires ATC/airside coordination and a NOTAM covering the period the unit is being set up, moved, or is otherwise not providing a reliable indication.

Tripod Stability in Wind
Operational

Stake down and, where provided, guy the tripod base at every deployment; a lightweight collapsible base on soft or uneven ground is more prone to wind-induced tip-over than a fixed foundation, which can drop the unit out of aim tolerance or cause injury if it topples.

Aim Verification After Every Setup
Operational

Because the unit is set up fresh at each deployment rather than surveyed into a fixed foundation, verify level and elevation setting against the design glide-path angle every time it is deployed, not only after maintenance.

Solar Panel Orientation & Access
Operational

Position the solar panel for clear sky exposure and out of ground-crew shadow paths, and confirm the charge controller is functioning at setup, since an unnoticed charging fault only becomes apparent as the unit dims overnight.

FOD Control on the Movement Area
Operational

Account for all stakes, guy lines, fasteners, and packing material during setup and teardown, and remove the unit and its hardware completely if the deployment is temporary, to prevent foreign object debris on the movement area.

Manual Handling
Personnel Safety

Use correct lifting technique and, where available, a second person when carrying and erecting the unit, particularly in the austere or disaster-relief conditions the equipment is often deployed into.

Restore to Compliant State
Compliance

Do not leave a unit out of aim tolerance, at reduced intensity, or otherwise non-compliant while in service; monitor battery state of charge and photometric output through the deployment period and stand the unit down before it falls below minimum requirements.

Field Insight

Engineering & Expert Notes

Repeated Setup and Teardown Wears the Mounting Interface
Mechanical

A portable unit's mounting hardware goes through far more assembly cycles than a permanent installation ever sees; inspect threads and locking mechanisms for wear at every deployment, not just at an annual service interval.

Field Re-Aim Needs a Repeatable Reference, Not a By-Eye Setup
Alignment

Because the unit is re-levelled and re-aimed at every new site, carry a dedicated aim jig or inclinometer calibrated to the system rather than relying on operator judgement, which introduces inconsistency from one deployment to the next.

Track Actual Hours Against Rated Runtime, Not Just Capacity
Power

Battery or generator sources are sized for an expected runtime, but an unexpected extended deployment quietly draws down reserve capacity; log actual hours in service against the rated runtime rather than assuming the power source will signal a low charge in time.

Ground Settling Undermines Long-Term Level Mid-Deployment
Siting

Soft or uneven ground that seemed adequate at setup can settle under the unit's own weight over several days, shifting the calibrated angle without any fault at the fixture itself; recheck level and aim partway through an extended deployment, not only at initial setup.

Storage-Rated Weatherproofing Isn't the Same as Continuous Field Exposure
Durability

Some portable units are weatherproofed assuming intermittent deployment between stints in storage; if a unit is left in place for an extended operation, inspect seals and connectors on a shorter cycle than the standard maintenance interval.

Solar-Powered Units Need a Full-Day Shading Check
Power

A site that looks unshaded at setup can fall under moving shadows from trees or structures at different times of day; verify solar charging through a complete daily cycle before relying on the unit for night operations.

Quick Answers

Frequently Asked Questions

Short answers about portable PAPI systems: power options, deployment, alignment, standards and maintenance.

Q1What is a portable PAPI?

A portable PAPI is a self-contained, transportable version of the Precision Approach Path Indicator. It has four light units (or two in a portable APAPI configuration) on lightweight collapsible tripods or bases with integrated batteries, solar panels or a portable generator.

Q2Why use a portable PAPI?

It brings precision glide slope guidance to places where a permanent installation is not possible or justified, such as a disaster relief strip, a forward operating base or a temporary runway.

Q3Where are portable PAPI systems used?

Military forward operating bases, humanitarian relief operations after natural disasters, emergency landing strips and other temporary or rapidly changing operational environments.

Q4How is a portable PAPI powered?

Each unit uses integrated 12 V or 24 V batteries (sealed lead-acid or LiFePO4), solar panels (typically 50-100 W per unit) or a portable generator. Battery life is typically 8-12 hours of continuous use, and no isolating transformer or airfield series circuit is required.

Q5How quickly can a portable PAPI be set up?

Typically in under 30 minutes for two people, with units weighing about 10-15 kg including the tripod or base.

Q6What intensity and photometric performance does it have?

Up to 20,000 cd white and 10,000 cd red, with typical on-axis minimums of 14,000 cd and 7,000 cd, a red/white transition of 3 arc-minutes or less, and 3-step intensity control set manually or by remote handset.

Q7Which standards apply to portable PAPI?

ICAO Annex 14, FAA AC 150/5345-28 (PAPI systems, including portable guidance), FAA AC 150/5345-50B (Specification for Portable Runway and Taxiway Lights) and IEC/TS 61827.

Q8Why must the glide angle be verified after each deployment?

Integrated levels and compasses alone may not meet precision-approach tolerance, so verify the glide path angle with a theodolite or laser level after every setup.

Q9How do you keep portable PAPI units stable in wind?

Secure tripods or bases against wind, adding ballast or guy ropes in high-wind conditions so alignment is maintained.

Q10What maintenance does a portable PAPI need?

Every deployment: alignment check, battery and solar panel check, lens cleaning and wind stability check. Quarterly: inspect transport cases, tripods and housings for handling damage. Annually: verify white and red beam intensity.

Q11What if one portable PAPI unit is dark?

Likely causes are a failed LED module or lamp, a discharged or faulty individual battery connection, or a broken per-unit wiring link to the control unit. Check the unit's power connection and battery voltage first.

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