# N390WL: 1985 Boeing 737-3G7, registration cancelled 2006-04-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 5, 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: 23219
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 13, 1985
- Certificate issued: March 15, 2001
- Last registry action: April 14, 2005
- Mode S code: A484C8
- 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/N390WL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=390WL
- Page: https://openairdocs.org/deregistered/N390WL-2006-04-05

From the FAA registry file of November 5, 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 (12)

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

- [SDR PIDA06001](https://openairdocs.org/sdr/PIDA06001), Dec 29, 2005: WEB. CRACKED. INNER WEB OF THE FORWARD CARGO DOOR IS CRACKED. REPAIRED DAMAGE IAW SRM 52-00-01 AND 51-70-13.
- [SDR PIDA20050204](https://openairdocs.org/sdr/PIDA20050204), Dec 29, 2005: FITTING. CRACKED. RIGHT MAIN LANDING GEAR ACTUATOR OUTBOARD LOWER FORWARD ATTACH FITTING ON WING LOWER SPAR IS CRACKED. REPLACED ATTACH FITTING PER SRM 51-10-2.
- [SDR PIDA20050203](https://openairdocs.org/sdr/PIDA20050203), Dec 27, 2005: SKIN. CRACKED. L2 DOOR SKIN CRACKED IN THE LOWER AFT CORNER OF THE TOP HINGE CUTOUT. REPAIRED DAMAGE AREA PER SRM 52-00-01.
- [SDR PIDA2005O188](https://openairdocs.org/sdr/PIDA2005O188), Nov 8, 2005: SKIN. CRACKED. ON WALK AROUND, NOTED SMALL SECTION OF PAINT MISSING ABOVE PAX WINDOW, RIGHT SIDE OF FUSELAGE. CLOSER INSPECTION FOUND CRACK IN FUSELAGE SKIN PARALLEL TO SKIN L
- [SDR PIDA20050170](https://openairdocs.org/sdr/PIDA20050170), Oct 8, 2005: CONTROL PANEL. MALFUNCTIONED. MCP COURSE DISPLAY SKIPS NUMBERS. REPLACED MODE CONTROL PANEL PER MM 22-01-00. GROUND OPS CHECKS GOOD.
- [SDR PIDA20050062](https://openairdocs.org/sdr/PIDA20050062), Aug 5, 2005: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHT IN OVERHEAD BIN AT SEAT 4RT IS INOP. RELAMPED, OPS NORMAL.
- [SDR PIDA20050061](https://openairdocs.org/sdr/PIDA20050061), Jul 25, 2005: SKIN. CRACKED. CRACK IN FUSELAGE SKIN JUST BELOW STR.18LT AT APROXIMATE BS797. REPAIRED IN ACCORDANCE WITH SRM 53-00-01.
- [SDR PIDA20050058](https://openairdocs.org/sdr/PIDA20050058), Jul 12, 2005: REFLECTOR. DEFECTIVE. L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. FOUND REFLECTOR ASSEMBLY LIGHT SOCKET BAD. REPLACED REFLECTOR ASSEMBLY. OPS CHECKS NORMAL PER MM 33-51.
- [SDR PIDA2005004](https://openairdocs.org/sdr/PIDA2005004), Apr 17, 2005: LIGHT. INOPERATIVE. LEFT EMERGENCY OVERHEAD LIGHT INOP (3RD ONE BACK). REPLACED OVERHEAD EMERGENCY LIGHT ASSY PER MM 33-51-12. OPS CHECKS GOOD.
- [SDR PIDA2005334](https://openairdocs.org/sdr/PIDA2005334), Apr 17, 2005: LIGHT. INOPERATIVE. LEFT EMERGENCY OVERHEAD LIGHT INOP (3RD ONE BACK). REPLACED OVERHEAD EMERGENCY LIGHT ASSY PER MM 33-51-12. OPS CHECKS GOOD.
- [SDR 390WL0002](https://openairdocs.org/sdr/390WL0002), Mar 28, 2005: LIGHT. BROKEN. EMERGENCY OVERHEAD LIGHT AT SEAT 21 ABC IS BROKEN. PLACED OVERHEAD LIGHT ON MEL 33-15-3. REPLACED BROKEN RETAINER ON LIGHT FIXTURE AND RETURNED LIGHT TO NORMAL.
- [SDR 390WL0001](https://openairdocs.org/sdr/390WL0001), Feb 7, 2005: SELECTOR. UNKNOWN. AUTO FLIGHT MODE CONTROL PANEL VERTICAL SPEED SELECTOR INOP. PLACED ON MEL 22-14-(1). NO FAILURES OR IN FLIGHT FAULTS NOTED. PASSED AUTO PILOT TESTS FOR DFCS GR

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