200M 400M 200M
RNG: 2.4 KM
BRG: 047°
ALT: 3,200 FT
SPD: 480 KTS
HDG: 012° N
TGT: ALPHA-7
MODE: SEARCH
PWR: NOMINAL
FREQ: X-BAND
STATUS: LOCK
NAVTGTWPNDEFRDRCOM
MIL-STD-1553IFF: ACTIVELINK-16: SYNC
SECTOR: ALPHA
THREAT: CLEAR
RADAR: ACTIVE
TRACK: 6 TGT
LAT 28.6213°N LON 77.3873°E
NX
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NMX‑APSTR‑001 / Part No. 001749000 / IJT‑LSP · Altitude Switch · 7600 m / MIL‑Grade · Aviation Noida · India · 2026
NMX-APSTR-001

Altitude switch test rig. 7600 m.

Specialized absolute pressure switch test rig (Part No. 001749000) for evaluating the performance, accuracy, and durability of the altitude switch used in the IJT‑LSP (Intermediate Jet Trainer – Limited Series Production) Project — MIL-grade construction, real-time LED indication.

Absolute Pressure Switch Test Rig — Neometrix, Noida
Fig · 01 Front panel — DC supply, insulation tester, ammeter, indicator lamps
Altitude Threshold
7600m
Tolerance
±150m
DC Output
32V DC
Insulation Test
1KV DC
Standard
MIL-grade
01
Overview

Precision altitude switch validation.

The Absolute Pressure Switch Test Rig evaluates the altitude switch — a critical avionic component that activates or deactivates an electrical circuit based on atmospheric pressure — at its design threshold of 7600 m (±150 m).

Absolute Pressure Switch Test Rig — instrument panel detail
Fig · 02 Instrument panel — toggle switches, indicator lamps, ammeter

The rig is purpose-built to support the IJT-LSP (Intermediate Jet Trainer – Limited Series Production) Project, providing a complete electrical and pneumatic test environment for the altitude switch (Part No. 001749000). It validates switch activation pressure, insulation integrity, and circuit continuity in a single integrated bench.

The altitude switch functions on a bellow-and-micro-switch principle: atmospheric pressure change causes the bellow assembly to expand, deflecting the adjusting cap nut until the normally-open micro switch closes and completes the electrical circuit. The rig replicates this stimulus environment precisely and measures the switch-over point.

One bench. Altitude threshold verification, insulation test, and circuit continuity — all MIL-grade.

Real-time feedback is provided via front-panel green and red LED indicator lamps (28 V DC), with a calibrated digital ammeter monitoring the switched circuit. All instruments are supplied with test and calibration certificates.

02
Unit Under Test

The altitude switch anatomy.

The UUT — absolute pressure altitude switch — is a five-component assembly. Understanding its construction is essential to interpreting test results.

Component · 01

Pipe Union

Connects the altitude switch to the pneumatic test circuit. Serves as the pressure inlet point for applying the simulated atmospheric pressure stimulus to the bellow assembly.

Pneumatic Interface · Pressure Inlet
Component · 02

Bellow Assembly

Expands or contracts in response to pressure variations. Converts the absolute pressure signal into a mechanical displacement that drives the micro switch actuation mechanism.

Pressure-to-Motion Transducer
Component · 03

Adjusting Cap Nut

Regulates the travel of the bellow assembly, setting the precise pressure threshold at which the micro switch activates. Factory-set to correspond to 7600 m altitude pressure.

Threshold Setting · Factory Calibrated
Component · 04

Micro Switch

A normally-open (N/O) switch that closes when the bellow displacement reaches the threshold corresponding to pressure below the 7600 m altitude equivalent, completing the aircraft electrical circuit.

N/O · Activates below 7600 m
Component · 05

Electrical Connector

MIL-grade electrical interface (mating plug: MIL D 38999/26 FA 35 SN) providing the aircraft wiring harness connection. The rig uses a matched mating plug for standardised electrical interfacing during test.

MIL D 38999/26 FA 35 SN · Shielded PTFE
Operating Principle

Switch Sequence

1. Pressure applied to pipe union.
2. Bellow assembly expands.
3. Micro switch closes when pressure falls below 7600 m equivalent.
4. Electrical signal sent — confirmed by rig indicator lamp and ammeter.

Pneumatic → Mechanical → Electrical
04
Key Features

What the rig delivers.

Four core capabilities that make this rig suitable for defence aviation test programmes.

Feature · 01

Accurate Altitude Threshold Sensing

Tests the altitude switch at its precise design activation pressure — equivalent to 7600 m ±150 m altitude. The calibrated DC power supply and instruments ensure the switch-over point is measured with traceable accuracy.

Feature · 02

Aircraft Safety Enhancement

Validates that the altitude switch will perform reliably in service, preventing electrical failures in altitude-dependent aircraft systems. Catches defective switches before aircraft integration.

Feature · 03

Leak-Proof Pressure Verification

Confirms zero pressure loss at the test pressure level, verifying the bellow assembly and pipe union sealing integrity. Essential for confirming that the switch will hold calibration in service at altitude.

Feature · 04

Real-Time Monitoring

Front-panel green/red LED indicators (28 V DC) and a calibrated DPI switch provide the operator with instant visual confirmation of switch state. 3½-digit ammeter displays switched circuit current in real time.

05
Specifications

Full instrument complement.

All instruments are supplied with individual test and calibration certificates. MIL-grade wiring and connectors throughout.

System ReferenceAbsolute Pressure Switch Test Rig  ·  Part No. 001749000  ·  NMX-APSTR-001
DC Power SupplyInput: 230 V ±10%, 1-Phase, 50 Hz AC  ·  Output: 0–32 V DC, 2 A rated  ·  Display: Voltage & Current (3½-digit)  ·  Supplied with test & calibration certificate
Insulation TesterMeasurement range: 0–20 GΩ  ·  Test voltages: 500 V DC & 1000 V DC  ·  Supplied with test & calibration certificate
AmmeterRange: 0–2 A  ·  Accuracy: 0.1%  ·  Display: 3½-digit with external shunt  ·  Supplied with test & calibration certificate
Mating PlugMIL D 38999/26 FA 35 SN
Toggle SwitchesDPST & SPST types
Indicator LampsGreen (28 V DC)  ·  Red (28 V DC)
WiringShielded PTFE wire  ·  Ferrule and thimble terminations throughout
Potentiometer0–270 Ω  ·  10 W rated
UUT Altitude Threshold7600 m ±150 m (micro switch activates when pressure falls below this altitude equivalent)
UUT Switch TypeNormally Open (N/O) micro switch — closes at threshold
ApplicationIJT-LSP (Intermediate Jet Trainer – Limited Series Production) Project, Indian Air Force
06
Applications

Where it matters.

Defence aviation, aerospace R&D, and avionics quality assurance — wherever altitude-dependent electrical switching components must be validated before aircraft integration.

A · 01Aviation & Aerospace — ensures altitude switches function reliably at design pressure thresholds
A · 02Defence & Military — qualification testing for IJT-LSP Project and other military aircraft programmes
A · 03Flight Safety Systems — verifies altitude-dependent switching mechanisms in avionic circuits
A · 04Quality Control — production-line testing of altitude switches before aircraft integration
A · 05R&D Laboratories — validation of new altitude switch designs at operating pressure conditions
A · 06MRO & Overhaul — recertification of repaired or overhauled altitude switches post-maintenance
07
In Depth

The complete technical read.

Engineering narrative for test engineers and procurement teams specifying altitude switch test equipment for defence aviation programmes.

Background: the altitude switch in IJT-LSP

The Intermediate Jet Trainer — Limited Series Production (IJT-LSP) is an advanced trainer aircraft programme. The altitude switch is a safety-critical avionic component that monitors cabin altitude and provides an electrical signal when the aircraft descends below a critical altitude threshold (7600 m ±150 m). This signal drives warning systems or activates protective circuits depending on the aircraft configuration.

Because the switch operates on absolute atmospheric pressure rather than gauge pressure, it must be tested under controlled low-pressure conditions that replicate the atmospheric pressure at 7600 m. The Absolute Pressure Switch Test Rig provides this environment with precision and traceability.

Test methodology

Step 1 — Electrical setup

The UUT altitude switch is connected to the rig via the MIL D 38999/26 FA 35 SN mating plug. The DC power supply is set to the required test voltage and the ammeter monitors the switch circuit. The insulation tester verifies dielectric integrity of the connector and wiring before pressurisation.

Step 2 — Pneumatic pressurisation

Pressure is applied to the altitude switch pipe union. The bellow assembly expands in response. The operator monitors the pressure stimulus until the micro switch closes — confirmed by the green indicator lamp illuminating and a current reading on the ammeter.

Step 3 — Threshold verification

The pressure at which switch-over occurs is recorded and compared against the 7600 m ±150 m specification. Pass/fail is determined by whether the switch activates within the tolerance band. Out-of-tolerance switches are rejected; in-tolerance switches are accepted and logged against their part and serial number.

Instrument calibration and traceability

All three primary instruments — DC power supply, insulation tester, and ammeter — are supplied with individual test and calibration certificates traceable to national standards. This satisfies the traceability requirements of defence procurement quality plans and allows the test data to be submitted as part of the component acceptance record.

MIL-grade construction

The rig uses shielded PTFE wiring throughout — the standard for defence avionics test equipment — with ferrule and thimble terminations at all connection points. The mating plug (MIL D 38999/26 FA 35 SN) is the correct series for the IJT-LSP altitude switch connector, ensuring proper mating without adapter risk.

08
FAQ

Common questions.

Plain-language answers from the engineering team.

Q · 01 What altitude threshold does the rig test?
The rig tests the altitude switch activation point at 7600 m ±150 m. This corresponds to the atmospheric pressure at which the bellow assembly deflects sufficiently to close the normally-open micro switch and complete the aircraft electrical circuit.
Q · 02 What electrical supply does the rig need?
The rig requires 230 V ±10%, single-phase, 50 Hz AC supply. The integrated DC power supply then provides 0–32 V DC at up to 2 A for the test circuit.
Q · 03 Are the instruments calibrated and certified?
Yes. The DC power supply, insulation tester, and ammeter are each supplied with individual test and calibration certificates traceable to national standards. This meets the traceability requirements of defence quality plans.
Q · 04 Which mating connector does the rig use?
The rig uses a MIL D 38999/26 FA 35 SN mating plug — the correct series for the IJT-LSP altitude switch connector. Shielded PTFE wiring and ferrule/thimble terminations are used throughout.
Q · 05 Can the rig be adapted for other altitude switches?
Yes. Neometrix can configure the rig for different altitude thresholds, connector types, and switch specifications. Contact us with the UUT part number and test requirement for a feasibility review.
Q · 06 What after-sales support does Neometrix provide?
Neometrix provides installation, commissioning, operator training, preventive maintenance, and on-site service. Standard 12-month warranty on manufacturing defects. Annual maintenance contracts and remote support available post-warranty.
09
Downloads

Technical documents.

Product catalogue and engineering design documents for the NMX-APSTR-001.

10
Presentation

Product overview deck.

Seven-slide summary of the NMX-APSTR-001 — design, UUT anatomy, specifications, and applications.

NMX‑APSTR‑001  ·  Part No. 001749000

Absolute Pressure
Switch Test Rig

IJT‑LSP Altitude Switch  ·  7600 m  ·  MIL‑Grade

Neometrix Engineering Pvt Ltd  ·  Noida, India

Absolute Pressure Switch Test Rig
02 / 07

What is it?

A specialized test rig for evaluating the performance, accuracy, and durability of the altitude switch used in the IJT‑LSP (Intermediate Jet Trainer – Limited Series Production) project.

What it tests
Altitude switch switch-over pressure at 7600 m altitude equivalent
Why it matters
The switch activates/deactivates aircraft electrical circuits based on atmospheric pressure — a safety-critical function
What it delivers
Threshold verification  +  insulation test  +  circuit continuity — one bench, three checks
03 / 07

Unit Under Test — Altitude Switch Anatomy

01
Pipe Union Connects switch to pneumatic test circuit — pressure inlet point
02
Bellow Assembly Expands/contracts with pressure — converts pressure to mechanical displacement
03
Adjusting Cap Nut Sets the precise activation threshold — factory-calibrated to 7600 m
04
Micro Switch (N/O) Closes when pressure falls below 7600 m equivalent — sends aircraft electrical signal
05
Electrical Connector MIL D 38999/26 FA 35 SN — aircraft harness interface
04 / 07

Operating Principle

1
Pressure applied to the altitude switch pipe union through the rig pneumatic circuit
2
Bellow assembly expands in response to the changing absolute pressure
3
Micro switch closes when pressure corresponds to altitude below 7600 m ± 150 m
4
Rig confirms switch-over via green LED lamp and digital ammeter reading
Pneumatic → Mechanical → Electrical — validated in one cycle.
05 / 07

Key Specifications

7600m
Altitude Threshold
±150m
Tolerance
32V DC
DC Supply Output
1000V DC
Insulation Test Voltage
20
Insulation Range
2A
Ammeter Range
All instruments supplied with test & calibration certificates  ·  Mating plug: MIL D 38999/26 FA 35 SN  ·  Shielded PTFE wiring
06 / 07

Features

  • Accurate altitude threshold sensing at 7600 m ±150 m
  • Insulation integrity test up to 1000 V DC / 20 GΩ
  • Real-time LED indication (green/red, 28 V DC)
  • Calibrated 3½-digit ammeter with external shunt
  • MIL-grade PTFE wiring & MIL-D 38999 connector
  • Traceable calibration certificates for all instruments

Applications

  • IJT‑LSP altitude switch qualification testing
  • Aviation & aerospace production QC
  • Defence & military aircraft programmes
  • Flight safety system validation
  • MRO & overhaul recertification
  • R&D prototype validation
07 / 07

Ready to specify?

Tell us your UUT part number, altitude threshold, and test programme. We configure the rig and walk through the test procedure before you commit.

Neometrix Engineering Pvt Ltd  ·  Noida, India  ·  neometrixgroup.com
1 / 7
Related

Other test systems from Neometrix.

Defence, aerospace, and industrial test equipment designed and manufactured at our Noida facility.

Get a proposal

Tell us your UUT and
test programme requirement.

We review the altitude switch specification, configure the rig, and walk through the test procedure with your engineering team before you commit.

Request proposal +91 7777 876 876

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