Owner type Government
Year built 1982
Type Fixed wing multi engine
Engine Turbo-prop
Airworthiness Standard, normal
Airworthiness date August 27, 2003
Certificate issued September 30, 1999
Expires May 31, 2028 From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page Registration Potential ADs 99 Information bulletins 5 NTSB investigations 0 FAA incident reports 4 Difficulty reports 5 Potential STCs 156 Related links Airworthiness directives that may apply · 99 Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
1968 In force Superseded2026 ADs by the year they took effect: 102 ADs 1968 1 1969 1 1970 1 1975 1 1977 1 1978 2 1980 4 1981 1 1982 1 1983 2 1984 1 1985 1 1986 4 1987 6 1988 1 1990 5 1991 5 1992 5 1993 9 1994 7 1995 1 1996 5 1997 6 1998 1 1999 3 2000 3 2001 3 2002 2 2004 1 2005 2 2006 2 2007 1 2009 1 2010 1 2011 2 2012 1 2014 2 2015 1 2016 1 2022 1 2023 1 2024 1 2026 1
See all 103 ADs Information bulletins that may apply · 5 Advisory, not mandatory.
NTSB investigations No NTSB investigations matched to N177RA Matched 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 Dehavilland DHC-7-102 aircraft FAA incident reports · 4 FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 5 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2019FA0000111 Bracket · cracked PILOT'S RUDDER PEDAL CONTROL MECHANISM BRACKET ASSY CRACKED. IPC 27-20-00, FIG 10, ITEM 50, PN # 72710086-001. REPORTED A BRACKET HAD BROKEN ON THEIR AIRCRAFT AND RECOMMENDED "ONE TIME INSPECTION" FOR MAINTENANCE TO INSPECT THEIR ASSIGNED AIRCRAFT. INSPECTED A Apr 9, 2019 · N177RA · Dhav DHC7102 · Rudder Control System SDR QM7R201904020003 Bracket · cracked ONE TIME INSPECTION FOR CRACK/BREAK OF THE RUDDER CONTROL MECHANISM BRACKET. THE INSPECTION RESULTED IN IDENTIFYING A CRACK AT BOTTOM OF RADIUS. Apr 2, 2019 · N177RA · Dhav DHC7102 · Rudder Control System SDR 99ZZZX1127 Cvr · failed CVR WAS SENT OUT FOR A READ-OUT AND RE-CERTIFICATION. ALLIED SIGNAL INFORMED THAT THE TAPE DID NOT RECORD, THEY SAID THAT THIS PART NUMBERED CVR IS KNOWN TO FAIL. Jan 25, 1999 · N177RA · Dhav DHC7102 · Audio/Video Monitoring SDR 98ZZZX4770 Oxygen Bottle · failed OXYGEN BOTTLE WAS RECEIVED FROM VENDOR FULLY SERVICED AND WAS INSTALLED ON AIRCRAFT WITHOUT CONNECTING THE SUPPLY LINES. OXYGEN BOTTLE SITTING STATICALLY, THE MALE CONNECTION FITTING SEPARATED INTERNALLY CAUSING EXPLOSION LIKE SOUND AND DISSIPATING ALL OF THE Oct 30, 1998 · N177RA · Dhav DHC7102 · Crew Oxygen System SDR PAYA95D7003 Retract Mech · malfunctioned PHL-JFK - FLT 7707 - THE LT MAIN GEAR FAILED TO EXTEND NORMALLY. EMERGENCY GEAR EXTENSION PERFORMED NORMAL. JACKED ACFT AND CYCLED GEAR 20 TIMES WITH NO DEFECTS NOTED. RELEASED ACFT FOR TEST FLIGHT AND CYCLED GEAR AT ALTITUDE. NO DEFECTS NOTED. (W) Jan 23, 1995 · N177RA · Dhav DHC7102 · Landing Gear Retraction/Extension System STCs that may be installed · 156 Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Dehavilland DHC-7-102 See all 156 STCs