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Aircraft record

N344HA1959 Lockheed 188A

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jan 14, 2011.

Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply6 service difficulty reports

Registration
Deregistered
Last based in
Crofton, MD
owner city / state
Owners
1
since 2009
NTSB events
None
since 1982
ADs may apply
2
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Rockland Aerospace INC
Owner type
Corporation
City, state
Crofton, MD
Certificate issued
Sep 29, 2009
Canceled
Jan 14, 2011
Airworthiness
Standard
Airworthiness date
Apr 1, 1959

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Lockheed
Model
188A
Year
1959
Serial number
1038
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
102
Engines
4
Max takeoff weight
20,000 and over lb
Mode S code
A3CCDA

Engine

Make and model
Allison 501-D13 Ser
Type
Turbo-prop
Power
3750 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2009 – 2011Rockland Aerospace INCCrofton, MD

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (2)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2006-25-12Rolls-Royce Corporation 501-D Series Turboprop EnginesJan 23, 2007Engine (501-D13 SER)
2000-23-10Lockheed Model 188A and 188C Series AirplanesDec 27, 2000Airframe (188A)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (6)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Doors · fitting · wornSep 28, 2000

    YIP - FORWARD CARGO DOOR, DOOR MOUNTED LINK ARM HAS EXCESS MOTION AT DOOR ATTACH POINT. REPAIRED FORWARD CARGO DOOR ATTACH POINTS IAW ZANTOP DRAWING NR L84-R01. REF ZIAA00013. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · corrodedSep 28, 2000

    YIP - LONGERON NR 29 ON RIGHT FUSELAGE STATION 416 FOUND CORRODED. REPAIRED LONGERON PER L-188 DRAWING NR L55-R01. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · fitting · wornSep 28, 2000

    YIP - FORWARD CARGO DOOR, DOOR MOUNTED LINK ARM HAS EXCESS MOTION AT DOOR ATTACH POINT. REPAIRED FORWARD CARGO DOOR ATTACH POINTS IAW ZANTOP DRAWING NR L84-R01. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Fuselage · skin · corrodedSep 14, 2000

    YIP - EVIDENCE OF CORROSION ON SEVERAL AREAS OF SKIN BETWEEN FS 445-588 RIGHT SIDE. NUMEROUS AREAS OF SURFACE CORROSION ON STRINGERS UNDER SKIN. REMOVED SKIN SECTION, FOUND CORROSION TO BE BEYOND LIMITS. FABRIATED NEW SKIN PANEL. REPLACED SKIN PER L-188 SRM 51-2-2. REMOVED CORROSION, FOUND TO BE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · crackedSep 13, 2000

    YIP - FOUND FUSELAGE STATION 549 BELOW STRINGER 51 CRACKED ON RIGHT SIDE. REPAIRED CRACKED STRINGER IAW L-188 53-2-3 SRM. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · crackedMar 18, 1996

    YIP - DURING INSPECTION, FOUND RIGHT WING NR 1 PLANK CRACKED AT WS 275 ON LOWER SURFACE AT THE LEADING EDGE. FABRICATED, INSTALLED AND SEALED A REPAIR PER L-188 SRM 57-2-1, FIGURE 3, SHEET 37. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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