Owner type
Government
Serial number
85
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
Mode S code
A134A6

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.

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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.

1968In forceSuperseded2026
ADs by the year they took effect: 102 ADs
19681
19691
19701
19751
19771
19782
19804
19811
19821
19832
19841
19851
19864
19876
19881
19905
19915
19925
19939
19947
19951
19965
19976
19981
19993
20003
20013
20022
20041
20052
20062
20071
20091
20101
20112
20121
20142
20151
20161
20221
20231
20241
20261
See all 103 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N177RAMatched 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 2019FA0000111Bracket · crackedPILOT'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 AApr 9, 2019 · N177RA · Dhav DHC7102 · Rudder Control SystemSDR QM7R201904020003Bracket · crackedONE 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 SystemSDR 99ZZZX1127Cvr · failedCVR 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 MonitoringSDR 98ZZZX4770Oxygen Bottle · failedOXYGEN 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 THEOct 30, 1998 · N177RA · Dhav DHC7102 · Crew Oxygen SystemSDR PAYA95D7003Retract Mech · malfunctionedPHL-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.

See all 156 STCs