# N842QS: 2023 Textron 700 - Status: Valid registration - Airframe: [Textron 700](https://openairdocs.org/model/textron-700) (registry code 2076819, 14 seats) - Engine: [Honeywell AS907-2-1S](https://openairdocs.org/engine/honeywell-as907-2-1s) (registry code 33403) - Data sheets: [TCDS T00015WI](https://openairdocs.org/tcds/T00015WI) (Textron Aviation Inc.), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs) - Serial number: 700-0089 - Year built: 2023 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 15, 2023 - Certificate issued: April 27, 2023 - Expires: April 30, 2030 - Mode S code: AB88B6 - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=842QS - Page: https://openairdocs.org/aircraft/N842QS 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): 2 in force ### Matched by airframe (Textron 700) - [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 ### Matched by engine (Honeywell AS907-2-1S) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N842QS. ## FAA accident and incident reports None matched to N842QS. ## Service difficulty reports (10) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2026060408320](https://openairdocs.org/sdr/DXTA2026060408320), Jun 2, 2026: DOOR. OUT OF ADJUST. CLIMBING OUT OF 1000 FEET, WE HEARD A HISSING SOUND. WE THEN RECEIVED TWO COCKPIT NOTIFICATIONS: CABIN DOOR OPEN AND CHECK DOORS. WE ADVISED ATC THAT WE NEEDED - [SDR DXTA2025063004070](https://openairdocs.org/sdr/DXTA2025063004070), Jun 27, 2025: PIN. BINDING. MAIN DOOR GEAR PINS ARE VERY STIFF. TAKES A LOT OF FORCE TO PUSH THE DOOR HANDLE OPEN AND CLOSED CORRECTIVE ACTION; GAINED ACCESS TO AIRCRAFT AND FOUND DOOR PIN - [SDR DXTA2025060903787](https://openairdocs.org/sdr/DXTA2025060903787), Jun 5, 2025: DOOR. OUT OF ADJUST. MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE REPEAT WRITE UP. ADJUSTED FWD UPPER ECCENTRIC TO CORRECT MED DOOR PIN CONTACT POINT WITH REF TO CE-700 AMM 52-10- - [SDR DXTA2025051203409](https://openairdocs.org/sdr/DXTA2025051203409), May 8, 2025: STRIKER. OUT OF ADJUST. MAIN CABIN DOOR IS DIFFICULT TO LATCH CLOSED. INTERIOR AND/OR EXTERIOR HANDLE REQUIRES EXCESSIVE FORCE TO MOVE TO LATCHED POSITION. PERFORMED MULTIPLE ADJUSTMEN - [SDR DXTA2025050803409](https://openairdocs.org/sdr/DXTA2025050803409), May 8, 2025: HANDLE. BINDING. MAIN DOOR HANDLE: REPEAT WRITEUP: MAIN CABIN DOOR IS DIFFICULT TO LATCH CLOSED. INTERIOR AND/OR EXTERIOR HANDLE REQUIRES EXCESSIVE FORCE TO MOVE TO LATCHED POSI - [SDR 2025FA0000254](https://openairdocs.org/sdr/2025FA0000254), Apr 8, 2025: THRUST REVERSER. CORRODED. CORROSION ON INSIDE SURFACE OF LH AND RH ENGINE THRUST REVERSER PIVOT DOORS AND BEAMS. REMOVED CORROSION AND VERIFIED REMAINING MATERIAL THICKNESS TO BE WITHIN - [SDR DXTA2024123101780](https://openairdocs.org/sdr/DXTA2024123101780), Dec 30, 2024: PIN. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO CLOSE. LATCH PINS AND SOCKETS LUBED. OPS CHECK GOOD. IAW CE-700 AMM 52-10-00 - [SDR DXTA2024062512160](https://openairdocs.org/sdr/DXTA2024062512160), Jun 24, 2024: HANDLE. FAULTED. INTERIOR HANDLE WILL NOT CLOSE. TRIED TO CLOSE IT FROM THE OUTSIDE AND THE OUTSIDE LEVER WILL NOT CLOSE EITHER. TRIED THE DOOR RESET PROCEDURE AND IT DIDNT WORK - [SDR DXTA2024061312032](https://openairdocs.org/sdr/DXTA2024061312032), Jun 13, 2024: BATTERY. NO TEST. WHILE DOING THE POWER ON CHECKLIST EMER LIGHTS SWITCH TO ON WE GOT NO EMERG LIGHTS ON INTHE CABIN. PERFORMED THE 30 MINUTE CHARGE PROCEDURE IN THE QRH 25X THEN - [SDR DXTA2023050885490](https://openairdocs.org/sdr/DXTA2023050885490), May 5, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTING: WHEN ARRIVING AT AIRCRAFT AFTER A 12 HOUR OVERNIGHT, ALL EMER LIGHTS WERE FOUND TO BE ON, EXTERIOR AND INTERIOR. EMER LIGHT SWITCH WAS IN FA ## Service difficulty reports on N842QS not matched to an aircraft (3) They name N842QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA200702331](https://openairdocs.org/sdr/DXTA200702331), Jul 11, 2007: PUMP. LOW PRESSURE. AT CRUISE, TRANSFERRING FUEL AS RT PUMP WAS TURNED OFF AIRCRAFT SHUDDERED WITH LOUD BANG NOISE. ELECTED TO STOP THE TRANSFER: AS PUMP WAS TURNED ON AGAIN AIRCRA - [SDR DXTA200400496](https://openairdocs.org/sdr/DXTA200400496), Dec 25, 2004: PITCH CONTROL. FROZEN. PITCH TRIM FROZEN IN FLIGHT. ON CLIMBOUT FROM MINNEAPOLIS 10 DEG CELSIUS APPROX AUTOPILOT BEGAN 300-500 FT +- PITCH EXCURSIONS. UPON DESCENT, PITCH TRIM BEGAN W - [SDR DXTA200400358](https://openairdocs.org/sdr/DXTA200400358), Aug 14, 2004: WARNING LIGHT. ILLUMINATED. NUMBER 2 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF ROLL AT 100 KNTS, REJECTED TAKEOFF. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FUEL FILTER ELEMENTS WITH NEW EL ## STCs that may be installed (OpenAirDocs) (11) 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 700) - [STC ST12145SE](https://openairdocs.org/stc/ST12145SE): Installation of Starlink Aviation System. AeroMech Incorporated - [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC - [STC ST00415BO](https://openairdocs.org/stc/ST00415BO): Installation of an NVIS/NVG compatible lighting system and infrared capable exterior lighting. ATI Engineering Services LLC - [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc - [STC ST02812LA](https://openairdocs.org/stc/ST02812LA): Installation of the Honeywell EDG-100 Connected Engine Data Access System. Honeywell International Inc - [STC ST04572CH](https://openairdocs.org/stc/ST04572CH): Installation of an Airborne Terminal System and a Ka Radome. StandardAero Business Aviation Services LLC - [STC ST02746SE](https://openairdocs.org/stc/ST02746SE): Installation of external aerodynamic modifications, interior furnishings and equipment, including provisions for additional non-essential systems. Textron Aviation Inc - [STC ST02694SE](https://openairdocs.org/stc/ST02694SE): Group Reduced Vertical Separation Minimum (RVSM) airworthiness approval. AeroMech Incorporated - [STC ST04211NY](https://openairdocs.org/stc/ST04211NY): Installation of of NSM UNIFIS 3000 G2 Flight Inspection System. Aerospace Design & Compliance LLC - [STC ST01971WI](https://openairdocs.org/stc/ST01971WI): Installation of the Garmin G5000 Software Changes & GH-3900 Standby Configuration Updates. Textron Aviation Inc - [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 ## Related - Other Textron 700 aircraft: https://openairdocs.org/model/textron-700/aircraft.md - The Honeywell AS907-2-1S engine: https://openairdocs.org/engine/honeywell-as907-2-1s.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.