# Boeing 737-2A3

- Type: Aircraft model (FAA registry)
- Registry code: 138441B
- Manufacturer (registry): BOEING
- Model: 737-2A3
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 139
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-737-2a3

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (6)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA020418005](https://openairdocs.org/sdr/CA020418005), Apr 16, 2002: CIRCUIT BREAKER. OVERHEATED. (CAN) A/C ON GROUND AND ALL PAX BOARDED WHEN F/A INFORMED CAPTAIN SMOKE COMING FROM FLOOR VENTS AT ROW 1. AT SAME TIME CREW NOTICED SMOKE ON FLIGHT DECK. STAIRS
- [SDR CA001122019](https://openairdocs.org/sdr/CA001122019), Nov 3, 2000: O-RING. DAMAGED. (CAN) CREW REPORTED A LOSS OF B SYSTEM HYDRAULIC FLUID EN ROUTE FROM ABBOTTSFORD TO CALGARY. UPON ARRIVAL IN CALGARY THE NR 1 BRAKE WAS FOUND TO BE LEAKING AT Q
- [SDR CA001103017](https://openairdocs.org/sdr/CA001103017), Oct 18, 2000: INDICATOR. FAILED. (CAN) ON APPROACH THE FLAPS FAILED TO EXTEND BEYOND 5 UNITS AND INDICATED AN ASYMMETRICAL CONDITION. THE AIRCRAFT LANDED WITHOUT INCIDENT. FLAP POSITION INDICAT
- [SDR CA000414008](https://openairdocs.org/sdr/CA000414008), Apr 8, 2000: TUBE. CHAFED. (CAN) NO 2 SYS A LOW PRESS WARNING LIGHT ON IN FLIGHT WITH A LOSS OF SYS QTY ON APPROACH. NO 1 A SYS LOW PRESS WARNING LIGHT ON RESULTING IN LOSS OF SYS HYD. CH
- [SDR CA970319001](https://openairdocs.org/sdr/CA970319001), Mar 10, 1997: TUBE ASSY. BROKEN. (CAN) #2 ENGINE E.P.R. GAUGE WAS READING LOW. MAINTENANCE FOUND THE PT7 MANIFOLD LINE BROKEN. THE LINE WAS REPLACED AND THE ENGINE GROUND RUN SERVICEABLE. THE A
- [SDR CA961009006](https://openairdocs.org/sdr/CA961009006), Sep 11, 1996: DETECTOR UNIT. INTERMITTENT. (CAN) ON APPROACH MASTER CAUTION LIGHT AND #2 ENGINE OVERHEATING LIGHT ON. THE ENGINE OVERHEAT AND FIRE CHECKLIST WAS COMPLETED. SINGLE ENGINE APPROACH CARRIED 

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