Safety record in brief:1 NTSB accident (substantial damage, Aug 1990)10 ADs may apply6 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
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.
DOUBLE POWER LOSS DUE TO IMPROPER FUELING PROCEDURES. FACTORS RELATING TO THE ACCIDENT WERE: IMPROPER PRE-FLIGHT ACTIONS BY THE PILOT AND WRONG FUEL.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC90LA182)
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 |
|---|---|---|---|
| 2013-16-01 | Elevator Balance Weight | Sep 24, 2013 | Airframe (58P) |
| 2009-25-01 | Hawker Beechcraft Corporation Models 58, 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A… | Jan 8, 2010 | Airframe (58P)Certain serial numbers: 58 TH-733–TH-1609; 58A TH-733–TH-1609; 58P TJ-3–TJ-497; 58PA TJ-3–TJ-497; 58TC TK-1–TK-151; 58TCA TK-1–TK-151; … |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 2008-13-17 | Hawker Beechcraft Corporation (Type Certificates No. 3A15, No. 3A16, No. A23CE, and No.… | Aug 6, 2008 | Airframe (58P)Certain serial numbers: F33 CD-1235–CD-1304; G33 CD-1235–CD-1304; F33A CE-290–CE-1791; F33C CJ-26–CJ-179; V35B D-9069–D-10403; A36 E-185–E-3629; …. Only with: Circuit breaker toggle switch P/N 35-380132-1 through 35-380132-53 installed. |
| 2007-21-02 | Raytheon Aircraft Company Models 58P and 58TC Airplanes | Nov 15, 2007 | Airframe (58P)Certain serial numbers: TJ-177; TJ-178; TJ-180; TJ-211; TJ-213; TJ-247; …. Only with: Airplanes used as lead airplanes by the United States Forest Service for firefighting missions. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2002-11-07 | Raytheon Aircraft Company Models E55, E55A, A56TC, 58, 58A, 58P, 58PA, 58TC, and 58TCA… | Jul 15, 2002 | Airframe (58P)Certain serial numbers: E55 TE-768–TE-1201; E55A TE-768–TE-1201; A56TC TG-84–TG-94; 58 TH-1–TH-1388; 58 TH-1390–TH-1395; 58A TH-1–TH-1388; … |
| 2002-10-13 | Raytheon Aircraft Company Model 58P, 60, A60, B60, and 65-88 Airplanes | Jul 8, 2002 | Airframe (58P)Certain serial numbers: 58P TJ-3–TJ-497; 60 P-4–P-122; 60 P-124–P-126; A60 P-123; A60 P-127–P-246; B60 P-247–P-596; … |
| 2000-18-02 | Raytheon Aircraft Company Models A65, A65-8200, 65-B80, 70, 95-A55, 95-B55, 95-C55, D55… | Sep 22, 2000 | Airframe (58P)Certain serial numbers: A65 LC-265–LC-272; A65 LC-325–LC-335; A65-8200 LC-273–LC-324; 65-B80 LD-349–LD-511; 70 LB-1–LB-35; 95-A55 TC-191–TC-349; … |
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (58P)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798 |
| 98-04-24 | Raytheon Aircraft Company Models E55, E55A, 58, 58A, 58P, 58PA, 58TC, 58TCA Airplanes… | Mar 13, 1998 | Airframe (58P) |
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.
RIGHT INSTRUMENT AIR PUMP FAILED.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT INSTRUMENT AIR PUMP FAILED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING AN ANNUAL INSPECTION, FOUND LEFT INSTRUMENT AIR PUMP INOPERATIVE. REMOVED PUMP, FOUND DRIVE COUPLING SHEARED. FOUND PUMP VANE DEBRIS IN PRESSURE SIDE AIR HOSE. SINCE O/H, ALL FILTERS WERE REPLACED WITH NEW WHEN PUMP WAS INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number.OWNER REPORTED LT FUEL PRESSURE WAS LOW WHEN OPERATING BOOST PUMP. TESTED FUEL PRESSURE, FOUND PRESSURE LOW. PUMP REMOVED. FUEL SYS COMPONENTS WERE INSPECTED AND NO EVIDENCE OF DEBRIS OR CONTAMINATION WAS FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ANNUAL INSPECTION, PERFORMED A DIFFERENTIAL COMPRESSION CHECK. FOUND NR 6 CYLINDER COMPRESSION 32 PSI/80 PSI. COMPRESSION LEAK PAST EXHAUST VALVE. REMOVED CYLINDER ASSY AND SENT TO MFG FOR REPAIRS.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING LT AND RT ENGINE CHANGE THE LT AND RT ENGINE MOUNT TRUSSES WERE INSPECTED. SEVERE HEAT EROSION WAS FOUND ON THE LT BEAM BELOW THE FWD INDUCTION AIR BOX MOUNT BRACKET. THIS AREA IS NEAR THE LT EXHAUST ELBOW. BOTH MOUNTS SHOW THE SAME AMOUNT OF EROSION. MFG TECH SUPPORT SHOWS REPAIR INFO AS…
From FAA Service Difficulty Reports; matched by N-number and serial number.