# Boeing 737-2H6

- Type: Aircraft model (FAA registry)
- Registry code: 1384604
- Manufacturer (registry): BOEING
- Model: 737-2H6
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 124
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-737-2h6

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA95RA051](https://openairdocs.org/ntsb/DCA95RA051), Aug 10, 1995: Boeing 737-200 (N125GU), San Vicente, El Salvador, 65 fatal

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19970820027069I](https://openairdocs.org/incident/19970820027069I), Aug 20, 1997: Boeing 737200 (N123GU), Miami, FL, Minor damage. Narrative: belt-loader operated by johnny stanley of dynair backed into #2 engine thrust reverser causing slight scratch/dent to its actuator fairing.…

## Service difficulty reports (10)

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

- [SDR 2006FA0000300](https://openairdocs.org/sdr/2006FA0000300), Mar 15, 2006: BOLT. BROKEN. DURING A CHECK FOUND LOWER AFT BOLT HEAD BROKEN AT ACTUATOR TO MANIFOLD MOUNT FLANGE. NO OTHER DAMAGE FOUND AND NO LEAK SEEN.
- [SDR 20010425AP006](https://openairdocs.org/sdr/20010425AP006), Mar 19, 2001: SOLENOID VALVE. FAILED. MSY - FLT 671 - AFTER TAKEOFF, AT MSY STATION THE LANDING GEAR DIDN''T RETRACTED, THE AIRCRAFT RETURNED TO MSY STATION FOR MAINTENANCE. AT EL SALVADOR STATION, 
- [SDR 20010425AP005](https://openairdocs.org/sdr/20010425AP005), Mar 19, 2001: ACCESSORY UNIT. FAILED. MSY - FLT 671 - AFTER TAKEOFF, AT MSY STATION THE LANDING GEAR DIDN''T RETRACTED, THE AIRCRAFT RETURNED TO MSY STATION FOR MAINTENANCE. AT EL SALVADOR STATION, 
- [SDR 20010409SG008](https://openairdocs.org/sdr/20010409SG008), Feb 9, 2001: HYDRAULIC LINE. DAMAGED. CCS - FLT TA610 - DURING CRUISE, THE HYDRAUIC SYSTEM ''A'' WAS LOSS, DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO CARACAS AIRPORT. AFTER LANDING, MAINTENANCE
- [SDR 20001113SH017](https://openairdocs.org/sdr/20001113SH017), Sep 30, 2000: VALVE. FAILED. SAI/BZE - FLT TA410 - DURING CRUISE, RIGHT ENGINE COWL VALVE FAILED IN THE OPEN POSITION AND THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO EL SALVADO
- [SDR 20001012SH002](https://openairdocs.org/sdr/20001012SH002), Sep 25, 2000: SWITCH. DEFECTIVE. SAL/TGU - FLT TA211 - DURING CRUISE STAGE FLIGHT, THE THRUST REVERSER NR 2 ISOLATION VALVE LIGHT CAME ON. ACFT RETURNED FOR MAINT. UPON LANDING, THE LIGHT WENT 
- [SDR 20001012SH001](https://openairdocs.org/sdr/20001012SH001), Sep 25, 2000: PIN. DAMAGED. SAL/TGU - FLT TA211 - DURING CRUISE STAGE FLIGHT, THE THRUST REVERSER NR 2 ISOLATION VALVE LIGHT CAME ON. ACFT RETURNED FOR MAINT. UPON LANDING, THE LIGHT WENT 
- [SDR 20001004AP003](https://openairdocs.org/sdr/20001004AP003), Jun 28, 2000: BULKHEAD. BIRD STRIKE. HAV-SJO-PTY - FLT LR653 - DURING TAKEOFF, A BIRD HIT THE RIGHT SIDE OF THE RADOME. THE AIRCRAFT RETURNED TO PTY STATION. AT PTY STATION MAINTENANCE TECHNICIANS 
- [SDR RJEF598H](https://openairdocs.org/sdr/RJEF598H), Jun 6, 2000: CONTROLLER. MALFUNCTIONED. DURING CRUISE, THE PRESSURIZATION SYSTEM ON AUTOMATIC AND STANDBY MODE WERE UNABLE TO HOLD THE A/C PRESSURE AND OUTFLOW VALVE INDICATIONS WERE ERRATIC. THE A/C 
- [SDR 20000703AP010](https://openairdocs.org/sdr/20000703AP010), May 18, 2000: SENSOR. CHAFED. SAL-MIA - FLT TA310 - DURING DESCENT, ENGINE NR 2 OVERHEAT LIGHT CAME ON. THE FLIGHT CREW PERFORMED QUICK REFERENCE HANDBOOK PROCEDURE FOR ENGINE OVERHEAT INDIC

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