N424MA1986 Fairchild SA227-AC
Safety record in brief:No NTSB accidents or incidents since 198213 ADs may apply31 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Uas Transervices INC
- Owner type
- Corporation
- City, state
- Boca Raton, FL
- Certificate issued
- Apr 30, 2007
- Expires
- Jan 31, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Feb 28, 1986
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
- 1986
- Serial number
- AC-639
- 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
- A50B8F
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- 2007 – nowUas Transervices INCBoca Raton, FL · current
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 (31)
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.
- Navigation · valve · seizedMar 14, 2017
DURING NORMAL CRUISE FLIGHT AT ABOUT 16,000 FT IN ICING CONDITIONS, THE PILOT’S AIRSPEED INDICATION WAS READING LOW AND CONTINUED TO DROP UNTIL IT REACHED ZERO. THE CREW TROUBLESHOT THE ISSUE USING THE QRH, WHEN THE PILOT ATTEMPTED TO SELECT THE ALTERNATE STATIC SOURCE, THE SELECTOR VALVE WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · hydraulic line · chafedSep 10, 2015
ON VISUAL APPROACH, PILOT SELECTED LG TO THE EXTENDED POSITION. THE LG POSITION INDICATORS LIGHTS FOR THE MLG REMAINED RED & THE LIGHT FOR NLG DID NOT ILLUMINATE. THE PILOT CYCLED THE LG & RECEIVED TWO GREEN INDICATOR LIGHTS FOR THE MLG, BUT NO LIGHT FOR THE NLG. PERFORMED AN EMER MANUAL EXTENSION…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · wire harness · damagedAug 10, 2015
EN-ROUTE THE PILOT NOTICED THE RT ENG EGT SPIKED 100 DEGREES CELSIUS, THE RT ENG FUEL BYPASS LIGHT ALSO ILLUMINATED. THE PILOT FOLLOWED THE EMER CHECKLIST & PERFORMED A PRECAUTIONARY RT ENG SHUTDOWN. DECLARED AN EMER & DIVERTED. THE PILOT LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING IS IN…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Hydraulic power · hydraulic line · crackedJun 22, 2014
ON APPROACH THE PILOT NOTICED A HIGH PITCH WHINE COMING FROM WHERE HE BELIEVED TO BE THE RT ENG. AFTER THREE SECONDS THE PILOT NOTICED BOTH HYD LOW PRESS ANNUNCIATORS ILLUMINATED. CHECKED HYD QTY GAUGE & READING WAS 0. PILOT STARTED EMER PROCEDURES OUTLINED IN QRH, DECLARED AN EMER. MANUALLY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · switch · out of adjustNov 23, 1996
FLT 3429 - ON CLIMB-OUT FROM MSP, THE NOSE GEAR WOULD NOT REMAIN UP AND LOCKED AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE ADJUSTED THE NLG UPLIMIT SWITCH. ALL CHECKS SATISFACTORY. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · switch · failedOct 2, 1996
FLT 3467 - ON APPROACH TO DTW, THE RIGHT INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. MAINTENANCE REPLACED THE RIGHT INBOARD DOWN POSITION SWITCH. ALL CHECKS SATISFACTORY. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · position ind · failedSep 18, 1996
FLT 2903 - ON APPROACH TO DTW, THE RIGHT GEAR DOWN LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. THE INDICATOR LIGHT WOULD ILLUMINATE INTERMITTENTLY WHEN WIGGLED. THE CREW PERFORMED AND EMERGENCY EXTENSION AND LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR POSITION…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · door frame · crackedJul 7, 1996
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERFORMED REPAIR TO A CRACK IN THE CARGO DOOR FRAME, P/N 27-22085, AT FS 438.060 BY REMOVING DAMAGED GAS STRUT MOUNT HOLE (1.625 BY 1.825), FABRICATED, PREPPED AND INSTALLED A REPAIR ANGLE, REPAIR PLATE, AND FILLER IAW FAIRCHILD ARP 53-20-9503…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · door frame · crackedJul 7, 1996
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERFORMED REPAIR TO A CRACK IN THE CARGO DOOR FRAME, P/N 27-22085, AT FS 491, BY REMOVING DAMAGED GAS STRUT MOUNT HOLE (1.625 BY 1.825). FABRICATED, PREPPED AND INSTALLED A REPAIR ANGLE, REPAIR PLATE, AND FILLER IAW FAIRCHILD ARP 53-20-9503 DATED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support · crackedJun 6, 1996
DURING SCHEDULED MAINTENANCE IN MSP, MAINTENANCE FOUND PILOTS SIDE SEAT TRACK SUPPORT CHANNEL AT FS 107 CRACKED BETWEEN RIVETS ON NUT PLATE. FABRICATED AND INSTALLED DOUBLER PER ARP 53-10-9322. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 31 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