N592BA1984 Fairchild SA227-AC
This N-number isn't registered right now. Below is its last known registration, canceled Dec 27, 2021.
Safety record in brief:No NTSB accidents or incidents since 198213 ADs may apply4 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Wca Aircraft Services LLC
- Owner type
- LLC
- City, state
- Wilmington, DE
- Certificate issued
- Oct 30, 2012
- Canceled
- Dec 27, 2021
- Airworthiness
- Standard · Normal
- Airworthiness date
- Sep 5, 1984
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
- Fairchild
- Model
- SA227-AC
- Year
- 1984
- Serial number
- AC-592
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 12
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A7A4EF
Engine
- Make and model
- Airesearch Tpe331 Series
- Type
- Turbo-prop
- Power
- 904 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2012 – 2021Wca Aircraft Services LLCWilmington, DE
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (13)
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 |
|---|---|---|---|
| 2003-19-10 | Fairchild Aircraft, Inc., SA226 Series and SA227 Series Airplanes | Nov 7, 2003 | Airframe (SA227-AC) |
| 2002-08-01 | Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes | Jun 6, 2002 | Airframe (SA227-AC)Certain serial numbers: SA227-AC 420–583; SA227-AT 420–583; SA227-TT 420–583 |
| 2001-20-14 | Fairchild Aircraft, Inc., Models SA226 and SA227 Series Airplanes | Nov 21, 2001 | Airframe (SA227-AC)Certain serial numbers: SA226-T T201–T248; SA226-T(A) T(A)249–T(A)-291; SA226-T(B) T(B) 276; SA226-T(B) T(B) 292–T(B) 417; SA226-AT AT001–AT074; SA226-TC TC201–TC419; … |
| 2000-17-11 | Fairchild Aircraft, Inc., SA226 Series and SA227 Series Airplanes | Sep 22, 2000 | Airframe (SA227-AC)Only with: Incorporating Ozone Industries MLG assembly P/N OAS5453-1 (Rev H, J, K, or N) or OAS5453-5 (SA226), or P/N OAS5453-5 (SA227), with P/N OAS5501-1 MLG drag brace assembly. |
| 2000-17-01 | Fairchild Aircraft, Inc. Models SA226-T, SA226-AT, SA226-T(B), SA226-TC, SA227-AT… | Oct 6, 2000 | Airframe (SA227-AC)Certain serial numbers: SA226-T T201–T275; SA226-T T277–T291; SA226-T(B) T(B) 276; SA226-T(B) T(B) 292–T(B) 417; SA226-AT AT001–AT074; SA226-TC TC201–TC419; … |
Show all 13 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-03-17 | Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes | Apr 10, 2000 | Airframe (SA227-AC) |
| 98-19-15 R1 | Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes | Mar 3, 2000 | Airframe (SA227-AC)Only with: Equipped with Barber-Colman pitch trim actuators P/N 27-19008-001/-004 or P/N 27-19008-002/-005. |
| 98-06-25 | Fairchild Aircraft Inc. Models SA226- AT, SA226-TC, SA227-AC, and SA227-AT Airplanes | Apr 27, 1998 | Airframe (SA227-AC)Certain serial numbers: SA226-AT AT001–AT074; SA226-TC TC201–TC419; SA227-AC AC406; SA227-AC AC415; SA227-AC AC416; SA227-AC AC420–AC456; … |
| 97-11-13 | Fairchild Aircraft SA226 and SA227 Series Airplanes | Jul 11, 1997 | Airframe (SA227-AC)Certain serial numbers: SA226-T T201–T275; SA226-T T277–T291; SA226-T(B) T(B)276; SA226-T(B) T(B)292–T(B)417; SA226-AT AT001–AT074; SA226-TC TC201–TC419; … |
| 97-10-13 | Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes | Jul 8, 1997 | Airframe (SA227-AC)Certain serial numbers: SA226-T T201–T275; SA226-T T277–T291; SA226-T(B) T(B)276; SA226-T(B) T(B)292–T(B)417; SA226-AT AT001–AT074; SA226-TC TC201–TC419; …. Only with: Applies to airplanes that do not incorporate an elevator torque tube P/N 27-44026-005, 27-44026-007, or 27-44026-SEO-1-03. |
| 96-19-05 | Fairchild Aircraft SA226 and SA227 Series Airplanes | Oct 1, 1996 | Airframe (SA227-AC)Only with: Equipped with Ozone Industries MLG yoke (MLG assembly P/N OAS5453, dash numbers up to and including -19) or NLG yoke (NLG assembly P/N OAS5451, dash numbers up to and including -17). |
| 94-07-10 R1 | Fairchild Aircraft SA226 and SA227 Series Airplanes | Mar 25, 1996 | Airframe (SA227-AC)Certain serial numbers: SA226-T T201–T275; SA226-T T277–T291; SA226-T(B) T(B)276; SA226-T(B) T(B)292–T(B)417; SA226-AT AT001–AT074; SA226-TC TC201–TC419; … |
| 93-15-02 R1 | Fairchild Aircraft SA226 and SA227 Series Airplanes | Apr 17, 1995 | Airframe (SA227-AC)Only with: Equipped with a Simmonds-Precision pitch trim actuator P/N DL5040M5. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (4)
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.
- Ice and rain protection · lead · brokenSep 22, 2011
FOUND 3 DEFECTIVE LEADS ON RT PROP. ALL 3 FAILED AT THE GROUND WIRE AT THE SAME LOCATION AS PREVIOUS FAILED LEADS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · wire · brokenNov 4, 2008
ON TUESDAY 11/4/08, FLIGHT RETURNED TO RAMP AFTER DEPARTURE. PILOT IN COMMAND STATED THAT AFTER ROTATION AND STANDARD DEPARTURE, HE SELECTED FLAPS UP. NO CHANGE IN ACFT CONFIGURATION WAS NOTED AND NO MOVEMENT ON THE FLAP INDICATOR. HYDR PRESSURE AND ALL CIRCUIT BREAKERS WERE CHECKED AND FOUND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Windows · windshield · crackedFeb 25, 2002
THE RIGHT COPILOTS HEATED WINDSHIELD CRACKED AT APPROX 20,000 FEET WITH THE AIRCRAFT PRESSURIZED TO APPROXIMATELY 4.5 PSI. THE WINDSHIELD IS SPIDER CRACKED ACROSS THE ENTIRE SURFACE. THE WINDSHIELD SHOWS NO EVIDENCE OF IMPACT CAUSING THE CRACKING.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reportsShow fewer reports
- Windows · windshield · crackedFeb 25, 2002
THE RT COPILOTS HEATED WINDSHIELD CRACKED AT APPROX. 20,000 FEET WITH THE AIRCRAFT PRESSURIZED TO APPROXIMATELY 4.5 PSI. THE WINDSHIELD IS SPIDER CRACKED ACROSS THE ENTIRE SURFACE. THE WINDSHIELD SHOWS NO EVIDENCE OF IMPACT CAUSING THE CRACKING.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026