DYNAMIC VENTURES INC
Also recorded as: DYNAMIC VENTURES INC
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
No FAA enforcement actions linked to this operator.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal. To verify a report, search its control number at the FAA SDRS site.
Reports span 1996–2009. Most-reported systems: Landing gear (32) — 3; Doors (52) — 1; Wings (57) — 1; Engine air (75) — 1. Most-common natures of condition, as filed: OTHER — 5; SMOKE/FUMES/ODORS/SPARKS — 1.
6 reports on file.
Part: HINGE — CORRODED (CABIN DOOR) · airframe 4,946 hrs · 4,210 cycles
DURING THE SID INSP THE UPPER CABIN DOOR WAS REMOVED FOR INSP. THE HINGE PIVOT BOLTS COULD NOT BE REMOVED BECAUSE THE BOLTS, BUSHINGS AND BRGS WERE ALL RUSTED SOLID. THIS CAUSED THE BOLTS TO PIVOT IN THE FUSELAGE STRUCTURE INSTEAD OF THE BEARINGS CAUSING EXCESSIVE WEAR OF THE FUSELAGE DOOR MOUNT HOLES. THERE IS NO REQUIREMENT TO REMOVE THE UPPER DOOR EXCEPT DURING THE SID INSP CALLED OUT IN THE LATEST MANUAL REVISION NR 16.
Part: DRAG BRACE — DAMAGED (NLG) · airframe 4,946 hrs · 4,210 cycles
DURING THE SID INSP THE NLG WAS REMOVED FOR INSP. THE DRAG BRACE RT BRG PLATE HOLES WERE ALL FOUND EXCESSIVLY ELONGATED REQUIRING STRUCTURAL REPAIR. SUSPECT DAMAGE WAS CAUSED BY NORMAL TOWING OVER THE LIFE OF THE ACFT. THIS WOULD NOT BE DETECTED UNLESS THE NOSE GEAR IS REMOVED AS REQUIRED BY THE SID INSP CALLED OUT IN THE LATEST MANUAL REVISION 16.
Part: PIVOT — CORRODED (MLG) · airframe 4,946 hrs · 4,210 cycles
DURING THE SID INSP OF THE MLG TRAILING LINK, THE PIVOT PIN WAS FOUND TO HAVE EXCESSIVE AMOUNTS OF RUST AND PITS.
Part: BEARING — LOOSE (L TMLG TRUNNION) · airframe 4,946 hrs · 4,210 cycles
WITH THE LT MAIN GEAR REMOVED FROM THE WING FOR SID INSP, THE AFT TRUNNION BRG WAS FOUND VERY LOOSE IN THE AFT TRUNNION SUPPORT.
Part: CLAMP — CRACKED (BLEED SUPPLY)
REPORTED SMOKE IN COCKPIT UPON TAKEOFF. A/C RETURNED IMMEDIATELY AND PERFORMED NORMAL LANDING. INSP REVEALED A CRACKED V-BRAND CLAMP CONNECTING BLEED AIR SUPPLY LINES IN RT WING ROOT AREA ADJACENT TO SURFACE DEICE PRESSURE REGULATORS. SMOKE WAS DETERMINED TO ORIGINATE FROM A PLASTIC/VINYL HOSE INSIDE CABIN ADJACENT TO FUSELAGE SKIN WHICH HAD BURNED AND MELTED. SUSPECT HEAT FROM BLEED AIR SUPPLY LINES CAUSED LOCAL AREA TO CONDUCT HEAT THROUGH THE SKIN TO THE EXTENT NECESSARY TO MELT THE TUBING. INSP REVEALED NO OTHER APPARENT HEAT RELATED DAMAGE. SUBMITTER NOTES THAT THE CRACK IN THE V-BAND CLAMP OCCURRED AT JUNCTION OF BARREL BOLT, AND NO SAFETY DEVICES WERE INCORPORATED ON ANY OF CLAMPS IN AREA.
Part: FITTING — CHAFED SKIN (RT INBD FLAP)
INBOARD FORWARD SIDE OF RIGHT INBOARD FLAP IS CHAFING INTO THE SKIN AT THE WING STUB. FITTING PN 5825017-1 OR PN 5825017-2, WHICH IS RIVETED TO THE FORWARD INBOARD SIDE OF THE RIGHT INBOARD FLAP, IS CHAFING AGAINST THE WING SKIN.