Skip to content
KnownTail
Aircraft record

N505QS2016 Textron Aviation INC 680A

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply18 service difficulty reports

Registration
Valid
expires Oct 31, 2033
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
18
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Co-owners
Certificate issued
Oct 5, 2026
Expires
Oct 31, 2033
Airworthiness
Standard · Transport
Airworthiness date
Aug 16, 2016

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Textron Aviation INC
Model
680A
Year
2016
Serial number
680A0042
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
10
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A64DF2

Engine

Make and model
P&W Canada Pw306d
Type
Turbo-fan
Power
5,907 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2026 – nowCo-ownerscurrent

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (1)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2018-07-13Landing GearMay 15, 2018Airframe (680A)Serial numbers per UTC Service Bulletins 2-1706-1-32-1 Rev 1 and 2-1675-32-2 Rev 1 (brake assembly serial numbers). Only with: Equipped with brake assembly P/N 2-1706-1 (Model 510) or P/N 2-1675-1 (Models 680/680A) with serial number listed in table 1 of the applicable UTC service bulletin.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (18)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Lights · battery pack · faultedJan 20, 2026

    EMER LIGHTS DO NOT COME ON IN THE ARM POSITION ON PREFLIGHT. REMOVED NR 1 EMERGENCY LIGHT POWER SUPPLY AND INSTALLED A NEW #1 OUTRIGHT EMERGENCY LIGHT POWER SUPPLY IAW MM 33-50-06. OPS TEST IS GOOD AND NO DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · failedDec 10, 2025

    INTERIOR REAR EMERGENCY LIGHT ON LAV BULKHEAD & EXIT LIGHT BELOW LAV SEAT INOP WHEN USING BATTERY PACK. BOTH FUNCTION ON SHIPS MAIN BATTERY POWER. POSITIONED THE ACFT INSIDE HANGAR. APPLIED POWER & ALLOWED ACFT TO BOOT UP & VERIFIED THE WRITE-UP. REMOVED THE BATTERY PACK NR 4 DUE TO INTERNAL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · light · inoperativeDec 2, 2025

    EMERGENCY FLOOR LIGHT BELOW LAV SEAT INOPERATIVE. REMOVED AND REPLACED LAV SEAT TOEKICK LIGHT ASSEMBLY IAW SPM 20-30-0A PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS YAW IAW AMM 33-50-00, OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Lights · battery · no testApr 17, 2024

    ON PREFLIGHT EMER LIGHTS WERE ARMED AND FAILED TO ILLUMINATE. PER MCC PROCEDURE, THE APU WAS STARTED AND GIVEN 30MIN TO CHARGE. THEN, THE AIRCRAFT POWERED DOWN AND EMER LIGHT FAILED TO ILLUMINATE AGAIN. REMOVED AND REPLACED EMERGENCY BATTERY PACKS 1,2,3 AND 4. OPS CHECKS OF BATTERIES AND EMERGENCY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery · faultedJan 11, 2024

    LAV OVERHEAD LIGHT. LAV EMER LIGHT UNDER TOILET. LAV FLOOR LIGHT. AND REAR BULKHEAD EXIT SIGN ARE ALL INOP IN ARM MODE. IN ON MODE ALL EMER LIGHTS ARE INOP. TRIED TO CHARGE SYSTEM PER NOTE WITH LIGHT SWITCH IN OFF POSITION FOR 30 MINUTES WITH NO CHANGES. REMOVED FAULTY #4 EMERGENCY BATTERY P/N…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · wire harness · defectiveFeb 14, 2023

    NLG LANDING GEAR RETRACTION: ON APPROACH, AFTER GEAR HAD BEEN EXTENDED FOR A WHILE AND FLAPS HAD BEEN SELECTED TO FULL, WE GOT THE AMBER WOW MISCOMPARE CAS. WE INITIATED A MISSED APPROACH, DURING WHICH WE BROUGHT THE GEAR HANDLE UP, BUT GEAR WOULD NOT RETRACT. WE DIVERTED TO A LONGER RUNWAY; GEAR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · door · unknownDec 3, 2022

    MAIN DOOR: CABIN DOOR INTERMITTENTLY CLOSES HALF WAY THEN STOPS AND FALLS OPEN WITH EXTERIOR AMBER CHECK DOOR HANDLE LIGHT ILLUMINATED. TURNING DOOR SWITCH OFF, AMBER LIGHT EXTINGUISHES AND DOOR CLOSES NORMALLY. OPS CHECKED THE DOOR MULTIPLE TIMES AND WE WERE UNABLE TO DUPLICATE THE DISCREPANCY.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · gougedJul 30, 2022

    NDI REQUIRED ON FUSELAGE SKIN SCRATCH BEHIND RH FORWARD OVER WING FUSELAGE FAIRING SPLICE STRAP AT FS 354. COMPLIED WITH TEXTRON AVIATION ENGINEERING ORDER, DQ35681M1, FUSELAGE (RIGHT SIDE) DAMAGE (SCRATCH), DATED: JULY 28, 2022.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · gougedJul 30, 2022

    R/H INBOARD FLAP HAS A GOUGE ON THE UPPER SURFACE APPROXIMATELY 14" FROM OUTBOARD EDGE AND 1" FROM TRAILING EDGE, MEASURING .5" IN LENGTH AND .03 IN WIDTH, FROM A TOOL FALLING ON THE FLAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING ORDER, DQ35433M1, DATED: JULY 5, 2022. RIGHT WING INBOARD FLAP…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · gougedJul 26, 2022

    R/H INBOARD FLAP HAS A GOUGE ON THE UPPER SURFACE APPROXIMATELY 14" FROM OUTBOARD EDGE AND 1" FROM TRAILING EDGE, MEASURING .5" IN LENGTH AND .03 IN WIDTH, FROM A TOOL FALLING ON THE FLAP.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 18 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

Request owner name removalReport an error in this record