N801MX

Cancelled 2000

Deregistered aircraft · Dehavilland DHC-8-102

Cancelled
June 27, 2000
Exported to
Australia
Status when cancelled
Valid registration
Serial number
008
Type
Fixed wing multi engine
Certificate issued
April 20, 2000
Last registry action
April 20, 2000
Mode S code
AAE6BD
Owner when cancelled
First Security Bank Na Trustee
Owner type
Corporation

From the FAA registry file of October 28, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N801MX and the event date: up to this one’s cancellation.

Service difficulty reports · 6

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

SDR PCAA9600291Bolt · crackedDHC TASK 5310/08F DUE. PERFORMED ULTRASONIC TEST OF RIGHT BOLT, TEST REVEALED 30 PERCENT BACK REFLECTION. REMOVED AND REPLACED BOTH LEFT AND RIGHT FORWARD BOLTS. SUBSEQUENT ULTRASONIC TEST ON BOLT REMOVED FROM LEFT SIDE REVEALED 10 PERCENT BACK REFLECTION. Jun 30, 1996 · N801MX · Dhav DHC8102 · Fuselage Miscellaneous StructureSDR PCAA9600280Upper Arm Assy · wornDURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INSTALL CORRECTLY DUE TO THE HOLES BEING OVERSIZED. REMOVED AND REPLACED UPPER AND LOWER CENTER HINGE Apr 7, 1996 · N801MX · Dhav DHC8102 · Rudder StructureSDR 96ZZZM881Lower Arm Assy · wornDURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INSTALL CORRECTLY DUE TO THE HOLES BEING OVERSIZED. REMOVED AND REPLACED UPPER AND LOWER CENTER HINGE Apr 7, 1996 · N801MX · Dhav DHC8102 · Rudder StructureSDR PCAA9500206Seq Valve · failedWHEN LANDING GEAR WAS RETRACTED, NOSE GEAR ADVISORY LIGHT REMAINED ON. THE GEAR WAS SELECTED DOWN PER THE CHECK LIST; THE MAIN GEAR CAME DOWN AND LOCKED, THE NOSE GEAR INDICATED UNSAFE. THE CREW PERFORMED AN ALTERNATE EXTENSION. INSPECTED WIRING HARNESS FORMar 17, 1995 · N801MX · Dhav DHC8102 · Landing Gear Retraction/Extension SystemSDR PCAA9500204Prox Cont Box · failedAFTER DEPARTURE AND SELECTING GEAR UP, NOSE GEAR DOOR AMBER LIGHT STAYED LIT, FOLLOWED CHECK LIST, RECYCLED GEAR, NOSE WHEEL DID NOT COME DOWN. PERFORMED ALT GEAR EXT CHECK LIST, THEN RECEIVED 3 GREEN. REMOVED AND REPLACED PSEU DUE TO VARIOUS FAULT INDICATIOMar 8, 1995 · N801MX · Dhav DHC8102 · Landing Gear Position and WarningSDR PCAA9500196Prox Cont Box · failedTHE LT DOOR OPEN ADVISORY LIGHT ILLUMINATED IN FLIGHT. CREW VERIFIED DOOR IS CLOSED. REMOVED AND REPLACED LT FWD GEAR DOOR ACTUATOR AND PSEU IAW MM, OPERATIONAL CHECK GOOD. ACFT RETURNED TO SERVICE. (W)Feb 8, 1995 · N801MX · Dhav DHC8102 · Landing Gear Position and Warning