N3267NBeechcraft 58
This N-number isn't registered right now. Below is its last known registration, canceled Dec 23, 2024.
Safety record in brief:No NTSB accidents or incidents since 198215 ADs may apply7 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Dlc Sky LLC
- Owner type
- LLC
- City, state
- Dover, DE
- Certificate issued
- Oct 24, 2023
- Canceled
- Dec 23, 2024
- Airworthiness
- Standard · Normal
- Airworthiness date
- Dec 26, 1995
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 dataAirframe
- Manufacturer
- Beechcraft
- Model
- 58
- Serial number
- TH-1767
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A387F4
Engine
- Make and model
- Cont Motor Io-550 Series
- Type
- Reciprocating
- Power
- 300 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2023 – 2024Dlc Sky LLCDover, DE
- 1951 – 1955Individual ownerMinneapolis, MN · different airframe: Piper J3c-65 S/N 22458
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (15)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2013-16-01 | Elevator Balance Weight | Sep 24, 2013 | Airframe (58) |
| 2012-10-02 | Hawker Beechcraft Corporation Airplanes | Jun 21, 2012 | Airframe (58)Certain serial numbers: 58 TH-1931–TH-2124; G58 TH-2125–TH-2281; G58 TH-2283; G58 TH-2284 |
| 2011-27-04 | Hawker Beechcraft Corporation Airplanes Equipped With a Certain Supplemental Type… | Dec 29, 2011 | Airframe (58)Only with: Equipped with STC SA1762SO (Foxstar modification). |
| 2009-25-01 | Hawker Beechcraft Corporation Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A… | Jan 8, 2010 | Airframe (58)Certain serial numbers: 58 TH-733–TH-1609; 58A TH-733–TH-1609; 58P TJ-3–TJ-497; 58PA TJ-3–TJ-497; 58TC TK-1–TK-151; 58TCA TK-1–TK-151; … |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO-550 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
Show all 15 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2008-13-17 | Hawker Beechcraft Corporation (Type Certificates No. 3A15, No. 3A16, No. A23CE, and No.… | Aug 6, 2008 | Airframe (58)Certain serial numbers: F33 CD-1235–CD-1304; G33 CD-1235–CD-1304; F33A CE-290–CE-1791; F33C CJ-26–CJ-179; V35B D-9069–D-10403; A36 E-185–E-3629; …. Only with: Circuit breaker toggle switch P/N 35-380132-1 through 35-380132-53 installed. |
| 2007-06-07 | Raytheon Aircraft Company Models 58 and G58 Airplanes | Apr 19, 2007 | Airframe (58)Certain serial numbers: TH-2097–TH-2150. Only with: Optional propeller unfeathering accumulators installed. |
| 2003-01-01 | Raytheon Aircraft Company Beech Models 36, A36, A36TC, B36TC, 58, and 58A Airplanes | Feb 27, 2003 | Airframe (58)Certain serial numbers: A36 E-185–E-3231; A36 E-3233; B36TC EA-242; B36TC EA-273–EA-635; 58 TH-1–TH-1811; 58 TH-1813–TH-1897; … |
| 2002-11-07 | Raytheon Aircraft Company Models E55, E55A, A56TC, 58, 58A, 58P, 58PA, 58TC, and 58TCA… | Jul 15, 2002 | Airframe (58)Certain serial numbers: E55 TE-768–TE-1201; E55A TE-768–TE-1201; A56TC TG-84–TG-94; 58 TH-1–TH-1388; 58 TH-1390–TH-1395; 58A TH-1–TH-1388; … |
| 2000-26-16 | Raytheon Aircraft Company Beech Models A36, B36TC, and 58 Airplanes | Feb 16, 2001 | Airframe (58)Certain serial numbers: A36 E-1–E-3231; A36 E-3233; B36TC EA-1–EA-635; 58 TH-1–TH-1811; 58 TH-1813–TH-1897 |
| 2000-22-18 | Raytheon Aircraft Company Beech Model 58 Airplanes | Dec 29, 2000 | Airframe (58)Certain serial numbers: 58 TH-1389; 58 TH-1396–TH-1885 |
| 2000-18-02 | Raytheon Aircraft Company Models A65, A65-8200, 65-B80, 70, 95-A55, 95-B55, 95-C55, D55… | Sep 22, 2000 | Airframe (58)Certain serial numbers: A65 LC-265–LC-272; A65 LC-325–LC-335; A65-8200 LC-273–LC-324; 65-B80 LD-349–LD-511; 70 LB-1–LB-35; 95-A55 TC-191–TC-349; … |
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (58)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798 |
| 98-04-24 | Raytheon Aircraft Company Models E55, E55A, 58, 58A, 58P, 58PA, 58TC, 58TCA Airplanes… | Mar 13, 1998 | Airframe (58) |
| 97-14-15 | Raytheon Aircraft Company (Formerly Known as Beech Aircraft Corporation) Models E33… | Sep 2, 1997 | Airframe (58) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (7)
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.
- Fuselage · channel · crackedNov 15, 2016
WHILE PERFORMING A ROUTINE INSPECTION, CRACKS WERE NOTED ON A LATERAL CHANNEL IN THE TAIL SECTION OF THE FUSELAGE. CRACKS WERE APPEARING ON THE UPPER LT AND RT CORNERS AT THE CUTOUT RELIEFS. THIS AREA IS DIFFICULT TO VIEW AND ANY DEFECTS EASILY OVERLOOKED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · bushing · deformedJul 7, 2015
FOUND NUT MISSING, RT SIDE INBD LANDING GEAR ACTUATOR ROD ATTACH POINT WHERE IT ATTACHES TO THE GEAR ACTUATOR CROSS ARM. DISCOVERED NUT AND COTTER PIN REMNANTS UNDER GEAR ACTUATOR. UPON CLOSER EXAMINATION, NOTED THAT THE ACTUATOR ROD BUSHING (56-810015-1) HAD WORN INTO THE AN 960-416 WASHERS THAT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ignition · distributor blk · out of positionOct 13, 2010
DURING A PREFLIGHT RUN-UP, THE LEFT ENGINE WAS OBSERVED TO ONLY PRODUCE ABOUT 2000 RPM. INSPECTION OF THE LEFT MAGNETO REVEALED THE BRONZE BEARING HAD BECOME LOOSE IN THE DISTRIBUTOR BLOCK ALLOWING THE DISTRIBUTOR GEAR ELECTRODE TO STRIKE AND DAMAGE SEVERAL OF THE DISTRIBUTOR BLOCK ELECTRODES.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
- Ignition · ignition switch · burnedMay 18, 2010
RIGHT ENGINE FAILED TO CRANK UPON APPLICATION OF STARTER. PILOT NOTED SMOKE AND BURNING SMELL FROM UNDER INSTRUMENT PANEL. UPON INSPECTION IT WAS FOUND THAT THE IGNITION SWITCH CUPS WERE SEVERLY WORN, AND CONTACT POINTS WERE BURNT. SWITCH WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. WE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Pneumatic · pneumatic system · contaminatedNov 23, 2005
DURING PROLONGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER ENTER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LG AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERAL OUNCES OF WATER REMAINING IN SYS. SYS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · switch · faultyJan 8, 2005
INTERNAL UPPER BRAIDED CONDUCTOR ON LINE SIDE FAILED, SEPARATED FROM ITS CONTACT OR WELD. SPRING MECHANISM FOR SWITCH BECOMES CONDUCTOR. SPRING CAN NOT HANDLE THE CURRENT OF LANDING LIGHT CIRCUIT, AND OVERHEATS. OVERHEATING OF SPRING CAUSED NYLON TOGGLE ASSY TO FAIL. TOGGLE ASSY IS RENDERED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · tube · chafedJan 13, 1999
THERE IS A SCREW HOLE DRILLED OUT IN THE PANEL DIRECTLY ABOVE ROD. AN INSTALLATION OF A LONG SCREW IN THIS HOLE WILL RESULT IN THE SCREW CHAFING THE ROD. SUBMITTER STATED THIS IS WHAT CAUSED THIS DAMAGE.
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