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N405DD

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Raytheon C90A

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Registered owner
Vineripe Inc
Location
Delano, CA
Owner type
Corporation
Serial number
LJ-1748
Type
Fixed wing multi engine
Engine
Turbo-prop
Certificate issued
April 22, 2022
Expires
April 30, 2029
Mode S code
A4BF83
Raytheon C90AAirframe model · 9 seats · 2 engines · 155 registeredTCDS 3A20Airframe · Raytheon C90A

From the FAA registry file of October 24, 2026.

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Airworthiness directives that may apply · 32

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1987In forceSuperseded2026
See all 36 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

Historical bulletins · 2
SAIB CE-10-34R1Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08Issued Aug 20, 2013SAIB CE-10-34Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and AD 89-25-08Issued May 18, 2010

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

NTSB CEN09CA470Accident · No injuriesData collectionFinal reportBismarck, NDThe cabin entry door inadvertently opening during initial climb.Jul 23, 2009 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Accident 20090723020189ATakeoff · Bismarck, NDOn July 23, 2009 at 1235 local time, a Beechcraft BE-C90, N405DD owned and operated by the university of north dakota sustained substantial damage during takeoff at Bismarck, ND. No injuries were reported to the crew of two or passenger on board the aircraft.…Jul 23, 2009 · Substantial damage

Service difficulty reports · 4

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2006FA0000894Bolt · overtorquedDURING 1ST SCHEDULED PHASE 1 AND PHASE 2 INSPECTION INVESTIGATED PILOT COMPLAINT OF STIFF NOSEWHEEL STEERING. VERIFIED COMPLAINT, FOUND NOSEWHEEL STEERING STIFF AND LOUD POPPING NOISES COMING FROM COCKPIT UNDER FLOOR AREA WHEN TAXIED FROM COPILOTS POSITION. Aug 24, 2006 · N405DD · Beech C90A · Rudder Control SystemSDR 2006FA0000893Fastener · overtorquedFOUND OTHER LT SIDE RUDDER CONTROL ATTACHING HARDWARE TIGHT OR OVERTIGHTENED. EXAMINED LT RUDDER CONTROL SYSTEM HARDWARE FOR SERVICEABILITY AND REINSTALLED AS REQUIRED WITH NORMAL RECOMMENDED TORQUES, ADJUSTED INTERCONNECT ROD AS REQUIRED WITH NORMAL RECOMMENAug 24, 2006 · N405DD · Beech C90A · Rudder Control SystemSDR 2006FA0000892Mount · distortedDURING FIRST SCHEDULED 1ST AND 2ND PHASE INSPECTIONS NOTED SQUEAKING AND METAL TO METAL CONTACT NOISES WHEN RUDDER MOVED SIDE TO SIDE. FOUND RUDDER SERVO CABLE RUBBING ON SMT-65 SERVO MOUNT CABLE DRUM COVER. REPLACED SMT-65 UNIT AND REINSTALLED, RIGGED SERVOAug 24, 2006 · N405DD · Beech C90A · Autopilot Main ServoSDR 2006FA0000890Control Cable · out of adjustDURING 1ST SCHEDULED PHASE 1 AND PHASE 2 INSPECTIONS NOTED ELEVATOR CONTROL SYSTEM CABLE TENSIONS OUT OF MM SERVICE LIMITS. FOUND ELEVATOR NEUTRAL POSITIONS OUT OF LIMITS FOLLOWING CABLE TENSION ADJUSTMENTS (WITH FORWARD AND AFT RIG PINS INSTALLED). FOUND FOAug 24, 2006 · N405DD · Beech C90A · Elevator Control System

STCs that may be installed · 260

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 260 STCs