- Registered owner
- Destiny Venture LLC
- Location
- Brownsville, TX
- Owner type
- LLC
- Serial number
- RK-107
- Year built
- 1995
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 15, 1995
- Certificate issued
- April 23, 2013
- Expires
- April 30, 2029
- Mode S code
- AC89FA
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D 5 model are included below.
On this page
Airworthiness directives that may apply · 29
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 1 |
|---|---|
| 1991 | 1 |
| 1992 | 2 |
| 1993 | 2 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 2 |
| 1998 | 2 |
| 1999 | 1 |
| 2001 | 3 |
| 2002 | 1 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 1 |
| 2014 | 2 |
| 2022 | 1 |
| 2023 | 1 |
| 2026 | 1 |
See all 31 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Beech 400
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-18-24Flap Cable InspectionEngine · Pratt & Whitney Canada JT15D 5 series
SAIB NE-07-03Dual-engine flameoutsNTSB investigations
No NTSB investigations matched to N907JEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech 400 aircraft
FAA incident reports
No FAA accident or incident reports matched to N907JEMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech 400 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2008FA0000155Rib · crackedFOUND SEVERAL CRACKS (25) IN RIB TO LOWER SKIN ATTACH FLANGES, AT RIVET HOLES , IN 3 LT , AND 4 RT HORIZONTAL STABILIZER INNER SPAR RIBS. RIBS NR 234 ON LT SIDE, AND NR 2345 ON RT SIDE AFFECTED.SDR 2008FA0000154Rib · crackedFOUND SEVERAL CRACKS (25) IN RIB TO LOWER SKIN ATTACH FLANGES, AT RIVET HOLES , IN 3 LT, AND 4 RT HORIZONTAL STABILIZER INNER SPAR RIBS. RIBS NR 234 ON LT SIDE, AND NR 2345 ON RT SIDE. AFFECTED.SDR 2006FA0000648Connector · damagedINVESTIGATED REPORT OF FLAP ASYMMETRY ANNUNCIATOR LIGHT FLICKERING IN-FLIGHT. FOUND WIRE C458A22 ROUTED SO THAT EXCESSIVE WIRE TENSION AT P156 PLUG WAS CAUSING INTERMITTENT CONTACT WITH A156 PC BOARD J1 CONNECTOR. REROUTED WIRING AS REQUIRED FOR REVEALING WISDR 2006FA0000422Tube · brokenDURING RECURRING 400 HR INSPECTION REQUIRED BY AD, FOUND AFT FUSELAGE RT BLEED AIR DUCT ASSY. BELLOWS BRAIDED WIRE MESH BLOWN OUT OF END FITTINGS. SUSPECTED TO BE CAUSED BY BLEED AIR LEAK FROM EITHER CRACKED BELLOWS OR FATIGUE/TUBING MIS-ALIGNMENT STRESS. RSDR 2006FA0000421Screw · wrong partDURING INSPECTION IAW MFG SB, FOUND BRAKE HYDRAULIC LINE DAMAGED BY FLOOR PANEL ATTACHING SCREW. REPAIRED TUBING AND MODIFIED FLOOR PANELS IAW SB. HAVE FOUND THIS SAME CONDITION ON OTHER AIRCRAFT. (K)SDR 2005FA0001321Line · damagedDURING COMPLIANCE WITH INSPECTION PORTION OF SB NOTED CHAFE DAMAGE TO PN 128580101-1 NOTED CHAFE DAMAGE TO PN 128-580101-1 HYDRAULIC BRAKE LINE FROM ADJACENT FLOORBOARD ATTACH SCREW. DAMAGE FOUND LESS THAN 10 PERCENT OF TUBING WALL THICKNESS. RECOMMEND THATSDR 2005FA0001308Fastener · looseDURING SCHEDULED 1ST (D) INSPECTION FOUND HI-LOK PIN COLLAR LOOSE (UPPER HEX SECTION STILL INTACT) FOR (1) FASTENER (OF 3) ATTACHING PN 454A23202-3 LT VERTICAL STABILIZER PIVOT PLATE TO VERTICAL STABILIZER AFT SPAR, UPPER LT SIDE. AREA IS JUST BELOW WHERE PN
STCs that may be installed · 117
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 400
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST04187NYInstallation of of Enode Engine Data Acquisition Unit & Ionode Digital Data RecorderSTC ST12344IBReplacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher