N704CFairchild SA227-AC
This N-number isn't registered right now. Below is its last known registration, canceled Feb 12, 2004.
Safety record in brief:No NTSB accidents or incidents since 198213 ADs may apply25 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Corrales & Associates INC
- Owner type
- Corporation
- City, state
- Simi Valley, CA
- Certificate issued
- Feb 4, 2004
- Canceled
- Feb 12, 2004
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 23, 1988
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
- Serial number
- AC-704
- 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
- A9639C
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- 2004Corrales & Associates INCSimi Valley, CA
- 1950 – 1953Individual ownerBurbank, CA · different airframe: Stinson 108-3 S/N 108-3704
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 (25)
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 · rod · out of adjDec 21, 2000
FLT 2568 - BIL - FOUND CABIN DOOR WARNING LIGHT CAME ON AT 2,000 AGL, CREW RETURNED TO BASE. ADJUSTED CENTER BAYONET, GROUND OPS CHECK AND TEST FLIGHT WERE GOOD. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · rivet · looseOct 3, 2000
FLT 2564 - BIL - PASSENGER REPORTED TO CREW HE SAW FUEL OR LIQUID COMING OFF TOP OF WING. CREW VERIFIED, AND RETURNED TO BASE WITH NO FURTHER INCIDENT. FOUND FUEL TO BE COMING FROM RIVET ON TOP OF WING. REPLACED AND RESEALED 4 LEAKING RIVETS ON TOP SIDE OF WING OUTBOARD OF RT ENGINE NACELLE. NO…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · acm · failedOct 1, 2000
FLT 2565 - SDY - THE CABIN STARTED TO FILL WITH SMOKE SHORTLY AFTER LANDING. CREW FOLLOWED CHECKLIST PROCEDURES AND TURNED OFF ACM''S. AIRCRAFT DEPLANED AT GATE WITH NO FURTHER PROBLEMS. LEFT ACM HAD FAILED. DEFERRED LEFT ACM, THE REPLACED LATER. NO FURTHER DEFECTS NOTED. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Engine fuel and control · computer · malfunctionedMar 4, 2000
HLN - FLT 2585 - LEFT ENGINE BYPASS LIGHT CAME ON. TORQUE REDUCED TO 35 PERCENT, THEN BYPASS LIGHT CYCLED ON AND OFF. CREW DECLARED EMERGENCY AND RETURNED TO HELENA. LEFT ENGINE SRL COMPUTER FAILURE. SRL COMPUTER WAS DEFERRED PER MEL, FLIGHT RESUMED AND COMPLETED WITH NO FURTHER PROBLEM. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · bearing · wornFeb 7, 1997
DURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE COPILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · control rod · creasedFeb 7, 1997
DURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE ELEVATOR CONTROL ROD, BETWEEN CONTROL COLUMN AND WALKING BEAM, ROD END BEARING RETAINER/DUST COVER WAS FOUND CREASED. THE ROD END WAS REPLACED WITH A NEW PART.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · control rod · creasedFeb 7, 1997
DURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE ELEVATOR CONTROL ROD, BETWEEN CONTROL COLUMN AND WALKING BEAM, ROD END BEARING RETAINER/DUST COVER WAS FOUND CREASED. THE ROD END WAS REPLACED WITH A NEW PART.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · torque tube · corrodedJan 28, 1997
DURING COMPLIANCE OF AD 96-21-05, THE LT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE INTERNAL CORROSION BEYOND ACCEPTABLE LIMITS. THE TORQUE TUBE WAS REPLACED WITH A NEW PART.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · torque tube · corrodedJan 28, 1997
DURING COMPLIANCE OF AD 96-21-05, THE RT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE INTERNAL CORROSION BEYOND ACCEPTABLE LIMITS. THE TORQUE TUBE WAS REPLACED WITH A NEW PART.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · engine · failedNov 10, 1996
RT ENGINE TORQUE ROLL BACK DURING TAKEOFF. REPLACED RT ENGINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 25 reports.
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