# Boeing 737-200A

- Type: Aircraft model (FAA registry)
- Registry code: 1384416
- Manufacturer (registry): BOEING
- Model: 737-200A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 100
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-737-200a

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 (2)

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 20000711035649I](https://openairdocs.org/incident/20000711035649I), Jul 11, 2000: Boeing 737200A (N120NJ), Kansas City, MO. (-23) On July 11, 2000, at 0959 (LCL), vanguard airlines, flight 584, aircraft N120NJ, was scheduled to enroute from mci to mdw. The captain reported that…
- [Incident 20000104000559I](https://openairdocs.org/incident/20000104000559I), Jan 4, 2000: Boeing 737200A (N120NJ), Kansas City, MO. (-23) On January 4, 2000, vanguard airlines, flight 819, a Boeing 737, was enroute from mci to dfw. Upon taxi, the number two engine epr indicator failed. No…

## Service difficulty reports (5)

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

- [SDR SROM201203200001](https://openairdocs.org/sdr/SROM201203200001), Mar 16, 2012: STRINGER CLIP. CRACKED. STRINGER CLIP AT BS 663 S10L CRACKED.
- [SDR DHL2003741552](https://openairdocs.org/sdr/DHL2003741552), Mar 22, 2003: WEB. CRACKED. DURING C-CHECK, LT MLG W/W STA 950 LOWER AFT MLG DOOR STOP AT LATCH POINT, WEB IS CRACKED. REMOVED NR 1 & 2 HYD SYS B-PUMPS. DISCONNECTED 3 HYD LINES LT MLG W/W
- [SDR P2EA01166](https://openairdocs.org/sdr/P2EA01166), Aug 18, 2001: BULKHEAD. CRACKED. SJO - DURING Q-CHECK, INSPECTION PER S/B 737-53A1173, BS 178 FORWARD PRESSURE BULKHEAD WEB WITH CRACK AT WL 210 AND RBL 8.5. FORWARD PRESSURE BULKHEAD BS 178, V
- [SDR P2EA01168](https://openairdocs.org/sdr/P2EA01168), Aug 14, 2001: SKIN. DAMAGED. DURING Q-CHECK, EXTERNAL FUSELAGE, SKIN WITH SCRATCH AND DENT FROM BS 306 TO BS 307, BETWEEN STRINGER 20 AND 21 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 29
- [SDR P2EA01161](https://openairdocs.org/sdr/P2EA01161), Aug 13, 2001: SKIN. CRACKED. SJO - DURING Q-CHECK, R1 DOOR, LOWER AFTER CORNER CUT OUT WITH CRACK. REPAIRED FUSELAGE SKIN FORWARD GALLEY DOOR CUT OUT FROM BS 314 TO BS 340, BETWEEN STRINGER

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