# N715TW: 2018 Honda HA-420 - Status: Valid registration - Airframe: [Honda HA-420](https://openairdocs.org/model/honda-ha-420) (registry code 4400000, 8 seats) - Engine: [GE Honda HF-120](https://openairdocs.org/engine/ge-honda-hf-120) (registry code 30200) - Data sheets: [TCDS A00018AT](https://openairdocs.org/tcds/A00018AT) (Honda Aircraft Company LLC), [TCDS E00085EN](https://openairdocs.org/tcds/E00085EN) (GE Honda Aero Engines) (OpenAirDocs) - Serial number: 42000102 - Year built: 2018 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, normal - Airworthiness date: April 3, 2020 - Certificate issued: May 9, 2026 - Expires: May 31, 2033 - Mode S code: A9905E - Registered owner: [Mhi Aviation LLC](https://openairdocs.org/faa-owner/MHI%20AVIATION%20LLC) - Location: [Saint Rose, LA](https://openairdocs.org/faa-place/LA/Saint%20Rose) - Owner type: LLC - Owner's area on the map: 29.9940° N, 90.3208° W: Placed by OpenAirDocs at the center of ZIP code 70087, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=715TW - Page: https://openairdocs.org/aircraft/N715TW 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): 9 in force ### Matched by airframe (Honda HA-420) - [AD 2026-10-02](https://openairdocs.org/ad/2026-10-02): Fuselage Main, Plate/Skin · Honda HA-420. Effective Jul 2, 2026 - [AD 2026-06-71](https://openairdocs.org/ad/2026-06-71): Trailing Edge Flap Actuator · Honda HA-420. Effective May 8, 2026 - [AD 2026-01-01](https://openairdocs.org/ad/2026-01-01): Aileron Control System · Honda HA-420. Effective Feb 17, 2026 - [AD 2023-11-03](https://openairdocs.org/ad/2023-11-03): Windshield/Door Rain/Ice Removal · Honda HA-420. Effective Jun 16, 2023 - [AD 2022-18-03](https://openairdocs.org/ad/2022-18-03): Windshield/Door Rain/Ice Removal · Honda HA-420. Effective Sep 22, 2022 - [AD 2020-04-14](https://openairdocs.org/ad/2020-04-14): Landing Gear · Honda HA-420. Effective Apr 6, 2020 - [AD 2018-21-13](https://openairdocs.org/ad/2018-21-13): Landing Gear · Honda HA-420. Effective Nov 27, 2018 - [AD 2018-15-06](https://openairdocs.org/ad/2018-15-06): Time Limits · Honda HA-420. Effective Aug 13, 2018 ### Matched by engine (GE Honda HF-120) - [AD 2019-16-02](https://openairdocs.org/ad/2019-16-02): Fuel Control/ Turbine Engines · GE Honda Aero Engines HF120. Effective Sep 13, 2019 ### Historical (superseded or no longer in force) - [AD 2022-05-13](https://openairdocs.org/ad/2022-05-13) (historical): Windshield/Door Rain/Ice Removal · Honda HA-420. Effective Apr 18, 2022 - [AD 2021-22-12](https://openairdocs.org/ad/2021-22-12) (historical): Trailing Edge Flap Actuator · Honda HA-420. Effective Nov 19, 2021 - [AD 2018-11-05](https://openairdocs.org/ad/2018-11-05) (historical): Landing Gear · Honda HA-420. Effective May 29, 2018 - [AD 2018-06-10](https://openairdocs.org/ad/2018-06-10) (historical): Landing Gear · Honda HA-420. Effective Apr 13, 2018 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N715TW. ## FAA accident and incident reports None matched to N715TW. ## Reports on N715TW not matched to an aircraft (1) They name N715TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19990710039209I](https://openairdocs.org/incident/19990710039209I), Jul 10, 1999: Boeing 757231 (N715TW), Orlando, FL. On t/o from stl. Aircraft left nose tire separated from the aircraft. Aircraft landed mco without incident. ## 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 N715TW not matched to an aircraft (20) They name N715TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR P9RA20050097](https://openairdocs.org/sdr/P9RA20050097), Aug 28, 2005: CONNECTOR. CONTAMINATED. SFB FORWARD EMERGENCY LIGHTS INOP IN FIRST CLASS CABIN. FOUND MOISTURE IN SEVERAL LIGHT STRIP HOOK UP POINTS. CLEANED CONTACTS. OPS CHECKED GOOD PER MM. NO PART - [SDR P9RA20050074](https://openairdocs.org/sdr/P9RA20050074), Apr 4, 2005: PACKING. SPLIT. CRUISE FLT FL390, EICAS MESSAGE FOR LEFT SYSTEM HYDRAULIC FLUID LOW. FOLLOWED QRH PROCEDURE BUT FLUID LEVEL CONTINUED TO DECREASE. ALTERNATE EXTEND ON GEAR AND - [SDR P9RA20040042](https://openairdocs.org/sdr/P9RA20040042), Sep 24, 2004: SLIDE. DEPLOYED. AT GATE IN TOL, R1 DOOR SLIDE DEPLOYED BY GROUND SERVICE PERSONNEL INADVERTENTLY. REMOVED AND REPLACED R1 SLIDE PER MM. - [SDR P9RA20040037](https://openairdocs.org/sdr/P9RA20040037), Sep 3, 2004: IDG. INOPERATIVE. SYR. RT GENERATOR DRIVE LIGHT CAME ON AT APPROX. 60 KNOTS. REJECTED TAKE OFF AND RETURNED TO GATE. ISSUED MEL 24001. MAINTENANCE ENTRY 9/4/2004. REMOVED AND REP - [SDR P9RA20040030](https://openairdocs.org/sdr/P9RA20040030), Aug 8, 2004: BULB. BURNED OUT. AIRCRAFT IN MAINTENANCE, SAT R4 DOOR SLIDE (ARMED) LIGHT FAILED TO ILLUMINATE.RELAMPED SOCKET. LIGHT WORKS NORMAL IAW MM 331100. - [SDR ZW0A0303203](https://openairdocs.org/sdr/ZW0A0303203), Mar 19, 2003: LIGHT. DISCONNECTED. THE MOST FORWARD SECTION OF EGRESS LIGHTS WERE INOPERATIVE. RECONNECTED THE FWD LAMP ASSEMBLY. CHECK-C 3-29-2002. - [SDR ZWOA0207002](https://openairdocs.org/sdr/ZWOA0207002), Jul 8, 2002: BULB. BURNED OUT. EGRESS LIGHTING AT SEAT 19C INOP. RELAMPED LIGHT. LAST CHECK C PERFORMED 10/14/2000 AT LAX. --CLOSED-- - [SDR ZW0A0204001](https://openairdocs.org/sdr/ZW0A0204001), Mar 31, 2002: LAMP. THE LEFT AFT CABIN DOOR SLIDE LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-14-00 LAX. --CLOSED-- - [SDR ZW0A0203902](https://openairdocs.org/sdr/ZW0A0203902), Mar 27, 2002: SKIN. CRACKED. DURING CHECK-C MAINT THE LT WING OTBD T/E FOREFLAP HAD 6 INCH LONG CRACK IN THE LOWER SURFACE, NEXT TO THE OTBD END. INSTALLED NEW PANEL PER SRM 51-10-02. - [SDR ZW0A0100801](https://openairdocs.org/sdr/ZW0A0100801), Apr 25, 2001: LIGHT. INOPERATIVE. THE EMERGENCY LIGHT ABOVE CABIN SEAT 6C WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-14-00 LAX. - [SDR ZW0A0100312](https://openairdocs.org/sdr/ZW0A0100312), Apr 13, 2001: SKIN. DAMAGED. ON THE LT WING, THE LOWER INBD CORNER OF THE INBD AFT FLAP HAD BOTTOM SURFACE WITH IMPACT DAMAGE. AREA WAS APPROX 8 IN BY 6 IN WITH CRACK. INSTALLED 14 BY 15 IN - [SDR TWAA0105802](https://openairdocs.org/sdr/TWAA0105802), Mar 31, 2001: LIGHT. INOPERATIVE. THE EGRESS LIGHT WAS INOPERATIVE AT ROW 1. REPLACED THE FLEX LAMP. CHECK-C 10-14-2000 LAX. - [SDR TWAA0104607](https://openairdocs.org/sdr/TWAA0104607), Mar 10, 2001: ENGINE. FAILED. DURING CLIMB AT 10,000 FEET A LOUD BANG WAS HEARD FROM THE RT ENG AND IT STARTED TO SPOOL DOWN. THE ENG WAS SHUT DOWN AND THE FLIGHT RETURNED TO AUA. THE ENGINE - [SDR TWAA0018801](https://openairdocs.org/sdr/TWAA0018801), Dec 1, 2000: LENS. OUT OF POSITION. THE EXIT LIGHT COVER ON THE RT SIDE MOST FORWARD DOOR HAD FALLEN OFF. INSTALLED SET SCREW AND COVER. CHECK-C 10-14-00 LAX. - [SDR TWAA0015706](https://openairdocs.org/sdr/TWAA0015706), Oct 3, 2000: SKIN. DENTED. FOUND DENT FWD OF AFT LT PASSENGER DOOR, STA 1616, BELOW STRINGER 18L. DENT WAS 2.75 IN BY 3.5 IN BY 0.127 DEEP. INSTALLED EXTERIOR DOUBLER REPAIR 11.5 BY 9.5 P - [SDR TWAA0003501](https://openairdocs.org/sdr/TWAA0003501), Feb 28, 2000: BULB. FAILED. AN EGRESS LIGHT WAS INOPERATIVE AT THE RT AISLE JUST BEFORE THE AFT LAV. REPLACED THE BULB, PN 767, AND A JUMPER CABLE, PN 5912-8. CHECK-C 4-24-99 LAX. - [SDR TWAA9917501](https://openairdocs.org/sdr/TWAA9917501), Dec 28, 1999: BOTTLE. DISCHARGED. THE FORWARD LEFT CABIN DOOR ASSIST BOTTLE PRESSURE WAS FOUND TO BE ZERO. REPLACED THE BOTTLE. CHECK-C 4-24-99 LAX. - [SDR TWAA9907601](https://openairdocs.org/sdr/TWAA9907601), May 27, 1999: GEARBOX. FAILED. THE LEFT ENGINE OIL PRESSURE DROPPED TO ZERO. OIL CONSUMPTION WAS NORMAL. SHUT THE ENGINE DOWN AND RETURNED TO STL. FOUND METAL IN THE OIL SYSTEM. REPLACED THE - [SDR TWAA9903401](https://openairdocs.org/sdr/TWAA9903401), Mar 5, 1999: ENGINE. FAILED. DURING ETOPS FLIGHT SEGMENT, THE LT ENG OIL PRESSURE DROPPED TO ZERO AND LOW OIL PRESSURE LIGHT CAME ON. SHUT DOWN THE ENG AND MADE UNSCHEDULED LANDING AT SFO. - [SDR TWAA9817501](https://openairdocs.org/sdr/TWAA9817501), Oct 28, 1998: WIRE. DAMAGED. THE FORWARD CABIN 26 INCH LONG EGRESS LIGHT STRIP WAS FOUND INOPERATIVE WHILE ON THE GROUND. THE STRIP HAD TORN LOOSE. STL SECURED THE LIGHT STRIP AND DEFERRED ## STCs that may be installed (OpenAirDocs) (5) 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 (Honda HA-420) - [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc - [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc - [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH - [STC SA04214NY](https://openairdocs.org/stc/SA04214NY): Installation of the Gogo AVANCE L3 System. Banyan Air Service - [STC SA01855WI](https://openairdocs.org/stc/SA01855WI): Installation of the Send Solutions Airtext Router in 14 CFR Part 23 Aircraft. 3S Certification LLC ## Related - Other Honda HA-420 aircraft: https://openairdocs.org/model/honda-ha-420/aircraft.md - The GE Honda HF-120 engine: https://openairdocs.org/engine/ge-honda-hf-120.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.