Safety record in brief:1 NTSB incident (minor damage, Oct 2014)5 ADs may apply2 service difficulty reports
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The failure of the main landing gear tire, which resulted in separation of the servo block and subsequent total loss of all hydraulic system pressure and prevented the landing gear from extending before landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN15IA014)
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 |
|---|---|---|---|
| 2016-07-02 | Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc.… | May 5, 2016 | Engine (TFE731-5BR)Serial numbers per Table 2 of Honeywell Service Bulletin TFE731-72-3789, Revision 0. Only with: Engines with interstage turbine transition (ITT) duct P/N 3075292-4 installed with a serial number listed in the SB. |
| 2014-12-52 | Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc.… | Jul 28, 2014 | Engine (TFE731-5BR)Only with: Engines with LPT2 blades P/N 3075424-1, -2, or -3 installed. |
| 2012-17-05 | Honeywell International Inc. Turbofan Engines | Oct 2, 2012 | Engine (TFE731-5BR)Only with: Applies only with specific first stage low-pressure turbine (LPT1) rotor assembly P/Ns installed: TFE731-5 with P/N 3075184-2, -3, or -4; TFE731-5AR/-5BR with P/N 3075447-1, -2, -4, 3075713-1, -2, -3, or 3074748-5; TFE731-4, -4R, -5AR, -5BR, -5R with P/N 3074748-4, -5, 3075447-1, -2, -4, 3075713-1, -2, or -3. |
| 2008-19-12 | Honeywell International Inc. TFE731-4, -4R, -5, -5AR, -5BR, and -5R Series Turbofan… | Oct 27, 2008 | Engine (TFE731-5BR)Only with: Interstage turbine transition (ITT) duct P/N 3075292-1, 3075292-3, 3074766-1, 3077063-1, 3075655-1, 3075655-2, 3075699-1, or 3075699-3 installed. |
| 2000-24-25 | Raytheon Model Hawker 800A (U-125A) and Hawker 800XP Series Airplanes | Jan 16, 2001 | Airframe (HAWKER 800XP)Serial numbers per Raytheon Aircraft Service Bulletin SB 32-3274, dated August 1999 |
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.
NR 1 TIRE FAILED AT TAKEOFF AND DISABLED THE RIT MAIN GEAR SHUTTLE VALVE RESULTING IN A LOSS OF HYD FLUID FROM THE MAIN AND AUX SYSTEMS. A GEAR UP LANDING RESULTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.LOSS OF HYD PRESS IN PRIMARY SYS, LOSS OF QTY IN AUX SYS. UNABLE TO EXTEND GEAR. PERFORMED GEAR UP LANDING.
From FAA Service Difficulty Reports; matched by N-number and serial number.