Incident · minor damage
Nov 11, 1993 · Sugar Land, TXTHE PARTIAL FAILURE OF THE HYDRAULIC PUMP (POWER PACK).
- Damage
- Minor
- Injuries
- None
- Report
- FTW94IA032
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW94IA032)
Safety record in brief:1 NTSB incident (minor damage, Nov 1993)13 ADs may apply2 service difficulty reports
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Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
THE PARTIAL FAILURE OF THE HYDRAULIC PUMP (POWER PACK).
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW94IA032)
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; … |
| 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.
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.
IDLER GEAR [PN: 896804-2] TEETH GALLED DUE TO BEARINGS (2EA) [PN: 3103035-1, SN: 10-151725-07307 & 10-151725-07323, TSN: 5,558.3] WORN AND SPALLING. RESULTED IN UNCOMMANDED SHUTDOWN OF ENGINE DUE TO FUEL PRESSURE LOSS.
From FAA Service Difficulty Reports; matched by N-number and serial number.APPROXIMATLY 100 MILES FROM THE DESTINATION OF THE FLIGHT, THE PILOT NOTICED A OIL PRESSURE LOW CAUTION LIGHT FOR THE LT ENGINE. THE PILOT SECURED THE ENGINE AND FEATHERED THE PROPELLER, ACFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE FOUND THE ENGINE OIL LEVEL LOW. OIL WAS SERVICED TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.