N194US

Cancelled 2016

Deregistered aircraft · 1967 Douglas DC-9-15F · Pratt & Whitney JT8D-1

Cancelled
March 24, 2016
Status when cancelled
First renewal notice
Serial number
47016
Year built
1967
Type
Fixed wing multi engine
Engine
Turbo-jet
Airworthiness
Standard
Certificate issued
February 26, 1997
Last registry action
July 15, 2013
Mode S code
A178DA
Owner when cancelled
USA Jet Airlines Inc
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 · 2

FAA accident and incident reports matched to this aircraft by N194US and the event date: up to this one’s cancellation.

Service difficulty reports · 9

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

SDR Y2PA04023Ground Wire · brokenNO GEAR INDICATION ON LT MAIN GEAR, EITHER RED OR GREEN. CREW DECLARED AN EMERGENCY AND DIVERTED. CREW FOLLOWED COM PROCEDURES WITH NO HELP. LT GEAR INDICATION DOES NOT TEST (RED AND GREEN LIGHTS INOPERATIVE). AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC SESep 23, 2004 · N194US · Doug DC915F · Landing Gear System WiringSDR Y2PA96088Skin · cannedYIP - LEFT TAIL SECTION SKIN 'OIL CANNED'. SKIN IS IN THE AREA ADJACENT TO THE AFT AIR STAIRS. SKIN PANEL IS IN AN 'UNPRESSURIZED AREA'. REPLACED SKIN PANEL. (M)Oct 16, 1996 · N194US · Doug DC915F · Fuselage Main, Plate/SkinSDR Y2PA96087Frame · crackedYIP - LEFT MAIN FRAME CRACKED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED MAIN FRAME. (M)Oct 16, 1996 · N194US · Doug DC915F · Fuselage Main, FrameSDR Y2PA96086Skin · corrodedYIP - SMALL AREA OF CORROSION NOTED ON THE FORWARD FUSELAGE SKIN, BELOW THE FORWARD BAGGAGE COMPARTMENT OPENING. REMOVAL OF INITIAL CORROSION REVEALED MORE EXTENSIVE (LEVEL 2) AREAS OF CORROSION. REMOVED CORROSION, CLEANED AND TREATED AREA. FABRICATED AND IOct 16, 1996 · N194US · Doug DC915F · Fuselage Main, Plate/SkinSDR Y2PA96048Door Switch · failedLRD - GEAR DOOR OPEN LIGHT REMAINING ON IN FLIGHT AFTER PERFORMING UPLATCH CHECK. REPLACED RIGHT MAIN GEAR DOOR SWITCH, AND ADJUSTED DOOR STOP BOLT ON GEAR DOOR IAW DC9 MM 32-70-0, 32-31-4. GEAR CYCLED AND CHECKED OK. (M)Aug 9, 1996 · N194US · Doug DC915F · Landing Gear Position and WarningSDR Y2PA96045Actuator · failedYIP - WITH GEAR RAISED AFTER TAKEOFF RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON, GEAR WAS CYCLED AND LIGHTS REMAINED ON. REMOVED AND REPLACED RT MLG ACTUATOR. FOUND LOOSE RIGHT GEAR DOOR SWITCH, TIGHTENED MOUNTING BOLTS. OPS CHECK GOOD. (M)Jun 25, 1996 · N194US · Doug DC915F · Landing Gear ActuatorSDR Y2PA96015Longeron · crackedYIP - CRACKS IN NR 1 (.375 INCH) AND NR 2 (.5 INCH) LONGERONS, AT FUSELAGE STATION NR 332. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FLIGHT VEHICLES, INC DRAWING 'FUS-LONGERON 1 AND 2 R AT STATION 332 REPAIR'. THESE DATA DER, ON FAA FORM 8110-3, DATED 3/3Apr 2, 1996 · N194US · Doug DC915F · Fuselage Main, Longeron/StringerSDR Y2PA96013Airspeed Ind · inoperativeYIP - NR 1 FIRST OFFICERS AIRSPEED INDICATOR INOP. DUPLICATED MALFUNCTION, REMOVED AND REPLACED FIRST OFFICERS AIRSPEED INDICATOR. SYSTEM OPERATIONAL CHECKS GOOD IAW DC9 MM CHAPTER 34-10-01. (M)Mar 27, 1996 · N194US · Doug DC915F · Airspeed/Mach IndicatorSDR Y2PA950011Rib · brokenYIP - DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS NOTED THAT THE LEFT WING OUTBOARD SPOILER SUPPORT UPPER RIB ASSEMBLY WAS BROKEN, AND A SECTION OF THE RIB WAS MISSING. REMOVED AND REPLACED RIB ASSEMBLY. NEW RIB WAS PROCURED PRE-DRILLED AND THE HOLES DIDJul 12, 1995 · N194US · Doug DC915F · Wing, Rib/Bulkhead