# N380WL: 1985 Boeing 737-3G7, registration cancelled 2006-03-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 21, 2006
- Exported to: Indonesia
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-3G7](https://openairdocs.org/model/boeing-737-3g7) (registry code 138447J)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 23218
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 20, 1985
- Certificate issued: March 14, 2001
- Last registry action: April 14, 2005
- Mode S code: A45D49
- Owner when cancelled: [East Trust Sub-12](https://openairdocs.org/faa-owner/EAST%20TRUST%20SUB-12)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N380WL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=380WL
- Page: https://openairdocs.org/deregistered/N380WL-2006-03-21

From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-3G7: https://openairdocs.org/model/boeing-737-3g7.md

## Service difficulty reports (16)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR PIDA06007](https://openairdocs.org/sdr/PIDA06007), Jan 15, 2006: ATTACH ANGLE. CRACKED. UPPER O/B ATTACH ANGLE FOR THE LEFT RAM AIR DUCT IS CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-02 AND 51-40-00.
- [SDR PIDA06004](https://openairdocs.org/sdr/PIDA06004), Jan 12, 2006: SKIN. CRACKED. CRACK IN FUSELAGE SKIN AT BS 380 ABOVE STR 4 RT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.
- [SDR PIDA06005](https://openairdocs.org/sdr/PIDA06005), Jan 10, 2006: SKIN. CRACKED. CRACK IN FUSELAGE SKIN AT BS 500A ABOVE STR 4 LT SKIN LAP JOINT. REPAIRED DAMAGE PER SRM 53-00-01.
- [SDR PIDA06002](https://openairdocs.org/sdr/PIDA06002), Dec 31, 2005: ACTUATOR. BROKEN. LOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOIL
- [SDR PIDAS06002](https://openairdocs.org/sdr/PIDAS06002), Dec 31, 2005: ACTUATOR. BROKEN. LOSS OF -A- SYSTEM HYDRAULIC PRESSURE; QUANTITY ZERO; ISOLATED SYSTEM, PERFORMED MANUAL GEAR EXTENSION & FLAPS 25 LANDING, NO FURTHER INCIDENT. FOUND NR 1 SPOIL
- [SDR PIDA20050201](https://openairdocs.org/sdr/PIDA20050201), Dec 23, 2005: AUTOPILOT SYS. MALFUNCTIONED. B-CHANNEL AUTO PILOT CAPTURES PRESELECTED ALTITUDE 300 FEET HIGH ON DESCENT BELOW FLIGHT LEVEL 20,000. A-CHANNEL WORKS FINE. PLACED B-AUTO PILOT ON MEL 22-1.
- [SDR PIDA20050200](https://openairdocs.org/sdr/PIDA20050200), Dec 21, 2005: CONTROL PANEL. MALFUNCTIONED. AUTO PILOT LEVELING OFF 300 FEET ABOVE SELECTED MCP ALTITUDE. REPLACED MODE SELECT PANEL PER MM 22-11-00. OPS CHECKS OK.
- [SDR PIDA20050193](https://openairdocs.org/sdr/PIDA20050193), Nov 22, 2005: LAP JOINT. CRACKED. DURING "A CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST AFT OF BS 440.
- [SDR PIDA20050192](https://openairdocs.org/sdr/PIDA20050192), Nov 22, 2005: LAP JOINT. CRACKED. DURING "A CHECK, FOUND TWO CRACKS ABOVE STR 10 RT SKIN LAP, ONE JUST AFT OF BS 500A AND ONE JUST FORWARD OF BS 500B.
- [SDR PIDA20050191](https://openairdocs.org/sdr/PIDA20050191), Nov 22, 2005: LAP JOINT. CRACKED. DURING A-CHECK, FOUND CRACK ABOVE STR 10 RT SKIN LAP JUST FORWARD OF BS 520.REPAIRED PER SRM 53-00-01.
- [SDR PIDA20050194](https://openairdocs.org/sdr/PIDA20050194), Nov 22, 2005: SKIN. CRACKED. DURING "A" CHECK, FOUND CRACK IN FUSELAGE SKIN JUST BELOW STR 22RT BETWEEN BS 727D AND BS 727E.
- [SDR PIDA20050182](https://openairdocs.org/sdr/PIDA20050182), Oct 24, 2005: POWER LEVER. OUT OF ADJUST. LEFT POWER LEVER DID NOT GO TO FLIGHT IDLE WITH LEVEL CHANGE SELECTED, THUS RESULTING IN ASYMMETRICAL THRUST. PERFORMED CABLE LUB PER MM 12-26-00.
- [SDR PIDA20050050](https://openairdocs.org/sdr/PIDA20050050), Jun 6, 2005: ENGINE. BIRD INGESTION. INGESTED BIRD IN RIGHT ENGINE AT ROTATION. VIBRATION INDICATION 4.0 UNITS AT POWER REDUCTION. INSPECTED ENGINE PER MM 71-00-47. UNSHINGLED BLADES NR 20, 21, 22,
- [SDR 380WL0002](https://openairdocs.org/sdr/380WL0002), Mar 7, 2005: INDICATOR. MALFUNCTIONED. NR 2 NAV-ILS, FLAGS WHEN IN VOR/ILS/AP MODE. PLACED ON MEL 22-15-7 AND 8. PERFORMED TROUBLE-SHOOTING PROCEDURE FOR VOR/ILS SYSTEM PER MM 34-31-00. NO DEFECTS NO
- [SDR 380WL0003](https://openairdocs.org/sdr/380WL0003), Mar 5, 2005: CABLE. OUT OF RIG. AUTOTHROTTLE KICKS OFF DURING FLIGHT. RIGGED LEFT THROTTLE FLEX CABLE PER MM 76-11-00. AUTOTHROTTLE CHECKS GOOD.
- [SDR 380WL0001](https://openairdocs.org/sdr/380WL0001), Aug 20, 2004: COMPUTER. MALFUNCTIONED. AUTO THROTTLE DOES NOT ACHIEVE REQUESTED TAKE OFF THRUST AND DISENGAGES DURING ALL PHASES OF FLIGHT. REPLACED AUTO THROTTLE COMPUTER IAW MM 22-31-10. TEST NORMA

## 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 20050516010729I](https://openairdocs.org/incident/20050516010729I), May 16, 2005: Boeing 7373G7 (N380WL), Lancaster, PA. (-23) On 05/16/2005 at approximately 0035 UTC, PCE402, while descending to 15,000 feet, southwest of Lancaster, Pennsylvania, requested priority landing to…

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