# N458MC: 2019 Textron 680A

- Status: Valid registration
- Airframe: [Textron 680A](https://openairdocs.org/model/textron-680a) (registry code 2076814, 10 seats)
- Engine: [Pratt & Whitney Canada PW306D1](https://openairdocs.org/engine/pratt-whitney-canada-pw306d1) (registry code 51850)
- Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (Textron Aviation Inc.), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 680A0187
- Year built: 2019
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 20, 2019
- Certificate issued: June 23, 2023
- Expires: June 30, 2030
- Mode S code: A590EA
- Registered owner: [Mclane Company Inc](https://openairdocs.org/faa-owner/MCLANE%20COMPANY%20INC)
- Location: [Temple, TX](https://openairdocs.org/faa-place/TX/Temple)
- Owner type: Corporation
- Owner's area on the map: 31.1423° N, 97.3746° W: Placed by OpenAirDocs at the center of ZIP code 76504, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=458MC
- Page: https://openairdocs.org/aircraft/N458MC

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 3 in force

### Matched by airframe (Textron 680A)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2018-07-13](https://openairdocs.org/ad/2018-07-13): Landing Gear · Textron 510, 680 and 680A. Effective May 15, 2018

### Matched by engine (Pratt & Whitney Canada PW306D1)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N458MC.

## FAA accident and incident reports

None matched to N458MC.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N458MC not matched to an aircraft (18)

They name N458MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR UIEA2015050500255](https://openairdocs.org/sdr/UIEA2015050500255), May 5, 2015: RELAY. FAULTY. LEFT CDU INTERMITTENT UPPER EICAS BLANK. R & R STDBY POWER TRANSFORMER RELAY R7227 IAW AMM 24-29-03 401. OPERATIONS CHECKED OK.
- [SDR UIEA2014120200624](https://openairdocs.org/sdr/UIEA2014120200624), Dec 1, 2014: AUTOPILOT SYS. MALFUNCTIONED. DESCENDING ACFT ABRUPTLY PITCHED UP & STARTED TO CLIMB ON AUTOPILOT. DISCONNECT AUTOPILOT & RE-ENGAGED LATER & OPERATIONS WERE NORMAL. VERIFIED NO CMC ACTIVE FA
- [SDR UIEA2013061100325](https://openairdocs.org/sdr/UIEA2013061100325), Jun 10, 2013: LAMP. BURNED OUT. EMERGENCY LIGHT IN STAIRWELL TO UPPER DECK DOES NOT ILLUMINATE. RELAMPED EMERGENCY LIGHT IN STAIRWELL TO UPPER DECK IAW AMM 33-51-07-962-001. TEST GOOD.
- [SDR UIEA2013022500105](https://openairdocs.org/sdr/UIEA2013022500105), Feb 25, 2013: STRUCTURE. CHAFED. LT WING L/E NR 9 L/C FLAP BULLNOSE INBD EDGE FOUND CHAFED. LT WING L/E NR 9 L/C FLAP BULLNOSE INBD EDGE REPAIRED IAW R1-57-44-16155, REV A.
- [SDR UIEA2013022500104](https://openairdocs.org/sdr/UIEA2013022500104), Feb 23, 2013: STIFFENER. CRACKED. LEFT WING OTBD REFUELING PANEL, ATTACH STIFFENING ANGLE OTBD CORNER FOUND CRACKED. LT WING OTBD REFUELING PANEL, ATTACH STIFFENING ANGLE REPLACED IAW R1-52-49-1
- [SDR UIEA2013022500103](https://openairdocs.org/sdr/UIEA2013022500103), Feb 21, 2013: STRUCTURE. CHAFED. LT WING L/E NR 10 L/C FLAP BULL NOSE OTBD EDGE FOUND CHAFED. LT WING L/E NR 10 L/C FLAP BULL NOSE OTBD EDGE REPAIRED IAW R1-57-44-10156, REV A.
- [SDR UIEA2012070300294](https://openairdocs.org/sdr/UIEA2012070300294), Jul 3, 2012: STOWAGE BOX. DAMAGED. CREW OXYGEN WAS FOUND TO BE LOW. ON INSPECTION AND LEAK CHECK AFTER BOTTLE REPLACEMENT IAW AMM 12-15-08, THE CAPTAIN'S OXYGEN MASK STOWAGE BOX WAS FOUND TO BE D
- [SDR UIEA2012022300057](https://openairdocs.org/sdr/UIEA2012022300057), Feb 22, 2012: STRUCTURE. DAMAGED. DURING MX WALKAROUND, FOUND DAMAGE TO THE NR 2 ENGINE THRUST REVERSER CORE COWL AFT EXTRUSION.
- [SDR UIEA2011122100726](https://openairdocs.org/sdr/UIEA2011122100726), Dec 20, 2011: SEAL. PUNCTURED. DURING A-3 CHECK AT BFM, MX FOUND DAMAGE TO THE LT INBD T/E MID FLAP-RUBBING SHEET/STRIP (PN 65B08436-35) OF THE COMPRESSION SEAL AT WBL 129.30, MEASURING 2.3 I
- [SDR UIEA2011103100633](https://openairdocs.org/sdr/UIEA2011103100633), Oct 30, 2011: INSULATION. DELAMINATED. DURING WALKAROUND, MX FOUND THE NR 4 RT T/R INSULATION DAMAGE AS FOLLOWS (REF FIG 1) DELAMINATIONS AND PUNCTURE OF INSULATION FROM HONEYCOMB STRUCTURE IS AS FOL
- [SDR UIEA2011041200245](https://openairdocs.org/sdr/UIEA2011041200245), Apr 12, 2011: LANDING GEAR. MISINSTALLED. DURING D-CHECK AT SIN, LANDING GEARS WERE REPLACED; UPON OPS CHECKS, MX FOUND THE LT AMP; RT BODY GEARS- UPPER JURY STRUT PLATES MOUNTING BOLTS BEING INSTALLED 
- [SDR UIEA2011032800168](https://openairdocs.org/sdr/UIEA2011032800168), Mar 28, 2011: FRAME. UNKNOWN. DURING SB 747-53A2507 INSP AT BS 1220, S8L LOCATION COMMON TO FRAME WEB, FRAME DOUBLER AND FRAME CHORD. (THE REPAIR WAS ACCOMPLISHED IAW RI NR N458MC-11-002 IAW
- [SDR UIEA2011032500165](https://openairdocs.org/sdr/UIEA2011032500165), Mar 25, 2011: FRAME. CRACKED. DURING D INSPECTION OF DATUM ACFT IAW EO 4453A197, CRACK WAS FOUND ON FRAME AT BS 1160 (RT AT STR 9). (THE DAMAGED FRAME WAS REPAIRED IAW PART 5 OF EO 4453A197,
- [SDR UIEA2011031800158](https://openairdocs.org/sdr/UIEA2011031800158), Mar 18, 2011: FRAME. CRACKED. THE LT NR 4 FAN REVERSER EXHIBITED A CRACK ON THE TORQUE BOX FWD FRAME. (IN THIS INSTANCE THE CRACK HAD BEEN STOP DRILLED AND REGULARLY INSPECTED BY THE PRIOR O
- [SDR UIEA2011030600154](https://openairdocs.org/sdr/UIEA2011030600154), Mar 6, 2011: SKIN. DAMAGED. THE LIGHTNING STRIKE DAMAGE TO 65B07656-259 SKIN WAS DETECTED AT BS 385 AND S31AL. THE DEPTH OF LIGHTNING STRIKE DAMAGE WAS .015 INCHES AS RECORDED IAW SIAEC NR
- [SDR UIEA2011022400178](https://openairdocs.org/sdr/UIEA2011022400178), Feb 24, 2011: SKIN. DAMAGED. FUSELAGE SKIN INSP DURING "D-CHECK", FOUND LIGHTNING STRIKE ON CROWN SKIN AT STA 345 BETWEEN STR 1R AND 2R (SOLID FASTENER REPAIR CARRIED OUT IAW B744SF SRM 53-
- [SDR UIEA2011022400145](https://openairdocs.org/sdr/UIEA2011022400145), Feb 24, 2011: SKIN. DAMAGED. DURING D-CHECK OF THE DATUM AIRPLANE, A LIGHTNING STRIKE DAMAGE WAS FOUND ON RT FUSELAGE SKIN AT BS 345, S1R-2R . DAMAGE WAS FOUND TO BE BEYOND THE ALLOWABLE LI
- [SDR UIEA2011022300142](https://openairdocs.org/sdr/UIEA2011022300142), Feb 23, 2011: SKIN. DAMAGED. LIGHTNING STRIKE DAMAGE FOUND AT STA 385 LT, S-31A, DEPTH FOUND APPROX 0.015, LENGTH APPROX 1" TO C/OUT FUSELAGE SKIN EXTERNAL REPAIR IAW SRM 53-00-01. CAT B RE

## STCs that may be installed (OpenAirDocs) (16)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Textron 680A)

- [STC ST04765NY](https://openairdocs.org/stc/ST04765NY): Unprepared (Grass/Sod) Runway Operations. Textron Aviation Inc
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC ST122244IB](https://openairdocs.org/stc/ST122244IB): Installation of Gogo Galileo system, including HDX Antenna. Alamo Engineering GmbH
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST11983SE](https://openairdocs.org/stc/ST11983SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST02037WI](https://openairdocs.org/stc/ST02037WI): Installation of Gogo Business Aviation AVANCE L5 System with MB 13 Antennas. Duncan Aviation Inc
- [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST04367CH](https://openairdocs.org/stc/ST04367CH): Installation of a Medical Interior in accordance with LifePort Master Data List EGR-887-000-001, Revision (B), dated April 18, 2019 or later FAA approved revision and LifePort Master Drawing List MDL-887-00, Revision (D), dated April 11, 2019 or later FAA approved revision.". LifePort LLC
- [STC ST01027DE](https://openairdocs.org/stc/ST01027DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries. MarathonNorco Aerospace Inc
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST11168SC](https://openairdocs.org/stc/ST11168SC): Installation of a Pratt & Whitney Flight Data Acquisition, Storage, and Transmission System (FAST). Pratt & Whitney Engine Services Inc

## Earlier aircraft with N458MC

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N458MC before.

- [Cancelled 2007-05-29](https://openairdocs.org/deregistered/N458MC-2007-05-29): Cessna T182T, S/N T18208458, built 2005. Owner: [Mid Continent Aircraft Corp](https://openairdocs.org/faa-owner/MID%20CONTINENT%20AIRCRAFT%20CORP), [Hayti, MO](https://openairdocs.org/faa-place/MO/Hayti)

## Related

- Other Textron 680A aircraft: https://openairdocs.org/model/textron-680a/aircraft.md
- The Pratt & Whitney Canada PW306D1 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw306d1.md

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