# N89304: 2014 Embraer S A ERJ 170-200 LL

- Status: Valid registration
- Airframe: [Embraer S A ERJ 170-200 LL](https://openairdocs.org/model/embraer-s-a-erj-170-200-ll) (registry code 326041A, 88 seats)
- Engine: [GE CF34-8E5](https://openairdocs.org/engine/ge-cf34-8e5) (registry code 30061)
- Data sheets: [TCDS A56NM](https://openairdocs.org/tcds/A56NM) (Embraer S.A.), [TCDS E00063EN](https://openairdocs.org/tcds/E00063EN) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 17000406
- Year built: 2014
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 12, 2025
- Certificate issued: June 16, 2014
- Expires: June 30, 2027
- Mode S code: AC52EE
- Registered owner: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=89304
- Page: https://openairdocs.org/aircraft/N89304

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): 30 in force

### Matched by airframe (Embraer S A ERJ 170-200 LL)

- [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 2025-14-05](https://openairdocs.org/ad/2025-14-05): Nacelles/Pylons · Embraer ERJ 170-100 LR, ERJ 170-100 STD, ERJ 170-100 SE and 12 more. Effective Aug 25, 2025
- [AD 2025-01-05](https://openairdocs.org/ad/2025-01-05): Time Limits/Maintenance Checks · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Mar 17, 2025
- [AD 2024-14-08](https://openairdocs.org/ad/2024-14-08): Pneumatic System · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Sep 25, 2024
- [AD 2024-12-08](https://openairdocs.org/ad/2024-12-08): Landing gear · Embraer ERJ 170-100 LR, ERJ 170-100 STD, ERJ 170-100 SE and 5 more. Effective Jul 11, 2024
- [AD 2023-13-02](https://openairdocs.org/ad/2023-13-02): Flight controls · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Sep 5, 2023
- [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 2023-03-19](https://openairdocs.org/ad/2023-03-19): Instruments · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Apr 7, 2023
- [AD 2022-16-01](https://openairdocs.org/ad/2022-16-01): Windows · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Aug 15, 2022
- [AD 2022-11-51](https://openairdocs.org/ad/2022-11-51): Wing structure · Embraer ERJ 170-200 STD, ERJ 170-200 LR, ERJ 170-200 SU and 1 more. Effective Jun 21, 2022
- [AD 2020-25-08](https://openairdocs.org/ad/2020-25-08): Flight controls · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Jan 21, 2021
- [AD 2020-07-21](https://openairdocs.org/ad/2020-07-21): Landing gear · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective May 26, 2020
- [AD 2020-05-22](https://openairdocs.org/ad/2020-05-22): Indicating/recording systems · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Apr 24, 2020
- [AD 2019-19-03](https://openairdocs.org/ad/2019-19-03): Fuselage · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Oct 31, 2019

### Matched by engine (GE CF34-8E5)

- [AD 2026-21-11](https://openairdocs.org/ad/2026-21-11): Turbine Engine Compressor Section · General Electric Company GE Aerospace CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 27, 2026
- [AD 2025-12-08](https://openairdocs.org/ad/2025-12-08): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jul 23, 2025
- [AD 2023-02-05](https://openairdocs.org/ad/2023-02-05): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 9 more. Effective Mar 14, 2023
- [AD 2022-21-06](https://openairdocs.org/ad/2022-21-06): Turbine Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 15, 2022
- [AD 2022-09-14](https://openairdocs.org/ad/2022-09-14): Compressor Bleed Valve · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jun 24, 2022
- [AD 2022-08-06](https://openairdocs.org/ad/2022-08-06): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Apr 29, 2022
- [AD 2021-26-19](https://openairdocs.org/ad/2021-26-19): Turbine Section · General Electric CF34-8C5, CF34-8C5B1, CF34-8E2 and 6 more. Effective Jan 25, 2022
- [AD 2021-23-51](https://openairdocs.org/ad/2021-23-51): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Dec 29, 2021
- [AD 2021-18-13](https://openairdocs.org/ad/2021-18-13): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 22, 2021
- [AD 2018-17-14](https://openairdocs.org/ad/2018-17-14): Thrust Reverser · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 7, 2018
- [AD 2017-20-09](https://openairdocs.org/ad/2017-20-09): Turbine Engine Bypass Section · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 13, 2017
- [AD 2017-17-18](https://openairdocs.org/ad/2017-17-18): Turbine Engine Compressor Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 6, 2017
- [AD 2013-06-06](https://openairdocs.org/ad/2013-06-06): Operability bleed valves (OBV) · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective May 8, 2013
- [AD 2009-24-06](https://openairdocs.org/ad/2009-24-06): Full authority digital electronic controls · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Dec 28, 2009
- [AD 2008-05-01](https://openairdocs.org/ad/2008-05-01): Fuel metering units (FMU) · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 8 more. Effective Apr 3, 2008
- [AD 2005-07-09](https://openairdocs.org/ad/2005-07-09): Master variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Apr 20, 2005

### Historical (superseded or no longer in force)

- [AD 2022-25-07](https://openairdocs.org/ad/2022-25-07) (historical): Time Limits/Maintenance Checks, Flight controls, Fuel, Doors, Fuselage, Nacelles/pylons, Stabilizers, Wings, Powerplant, Exhaust · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Jan 23, 2023
- [AD 2020-12-12](https://openairdocs.org/ad/2020-12-12) (historical): Nacelles/pylons · Yaborã Indústria Aeronáutica ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 12 more. Effective Aug 13, 2020
- [AD 2019-25-16](https://openairdocs.org/ad/2019-25-16) (historical): Flight controls · Embraer ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD and 5 more. Effective Feb 10, 2020
- [AD 2008-16-01](https://openairdocs.org/ad/2008-16-01) (historical): Full authority digital engine controls (FADECs) · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Aug 15, 2008
- [AD 2004-04-04](https://openairdocs.org/ad/2004-04-04) (historical): Master Variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Mar 9, 2004

## Information bulletins (advisory) (1 in force)

- [SAIB NM-20-12](https://openairdocs.org/saib/NM-20-12): Powerplant System - Operating in Icing Conditions. Issued Jun 18, 2020

## NTSB investigations

None matched to N89304.

## FAA accident and incident reports

None matched to N89304.

## Service difficulty reports (100, newest 50)

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 MASA2026101800049](https://openairdocs.org/sdr/MASA2026101800049), Oct 18, 2026: MAU. FAULTED. ACFT RETURNED TO FIELD, DECLARED AN EMERGENCY AFTER TAKEOFF, WHEN MULTIPLE MESSAGES APPEARED. AT FAIL/FMS SPEED ON PFD WILL NOT SHOW. SECURED CONTROL I/O MODULE
- [SDR MASA2026042300017](https://openairdocs.org/sdr/MASA2026042300017), Apr 23, 2026: FLASHLIGHT. INOPERATIVE. FWD FA FLASHLIGHT IS INOP/PLACED ON MEL
- [SDR JR2R20251222666](https://openairdocs.org/sdr/JR2R20251222666), Dec 22, 2025: FAIRING. DAMAGED. LIGHTNING STRIKE DAMAGE TO LH #3 FLAP FAIRING. REPAIRED
- [SDR JR2R20251209775](https://openairdocs.org/sdr/JR2R20251209775), Dec 9, 2025: TRUNNION. CHAFED. NOSE LANDING GEAR TRUNNION BORE HAS EVIDENCE OF DAMAGE. BLEND DAMAGED AREA.
- [SDR JR2R20251126745](https://openairdocs.org/sdr/JR2R20251126745), Nov 26, 2025: SEAT TRACK. CORRODED. EXISTING SEAT TRACK REPAIR DOUBLER AT FR84 RBL11 IS CORRODED. REPLACED
- [SDR JR2R20251118258](https://openairdocs.org/sdr/JR2R20251118258), Nov 18, 2025: SKIN. ERODED. RIGHT WING SLAT 4 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20251118107](https://openairdocs.org/sdr/JR2R20251118107), Nov 18, 2025: SKIN. ERODED. RH WING SLAT 4 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20251118105](https://openairdocs.org/sdr/JR2R20251118105), Nov 18, 2025: SKIN. ERODED. RH WING SLAT 3 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20251118104](https://openairdocs.org/sdr/JR2R20251118104), Nov 18, 2025: SKIN. ERODED. RH WING SLAT 2 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE
- [SDR JR2R20251118103](https://openairdocs.org/sdr/JR2R20251118103), Nov 18, 2025: SKIN. ERODED. RIGHT WING SLAT 1 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20251118102](https://openairdocs.org/sdr/JR2R20251118102), Nov 18, 2025: SKIN. ERODED. LEFT WING SLAT 4 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20251118101](https://openairdocs.org/sdr/JR2R20251118101), Nov 18, 2025: SKIN. ERODED. LEFT WING SLAT 3 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20251118100](https://openairdocs.org/sdr/JR2R20251118100), Nov 18, 2025: SKIN. ERODED. LEFT WING SLAT 2 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20251118199](https://openairdocs.org/sdr/JR2R20251118199), Nov 18, 2025: SKIN. ERODED. RIGHT WING SLAT 1 HAS SEVERAL AREAS OF EROSION DAMAGE ON LEADING EDGE.
- [SDR JR2R20250210268](https://openairdocs.org/sdr/JR2R20250210268), Feb 10, 2025: NUT PLATE. DAMAGED. RIGHT HAND OUTBAD FLAP LOWER SIDEHAS A DAMAGED NUTPLATE WITH NO ACCESS TO CHANGE IT. INSTALLE RIVNUT IAW ENGINEERING DATA.
- [SDR JR2R20250209260](https://openairdocs.org/sdr/JR2R20250209260), Feb 9, 2025: SUPPORT ANGLE. ELONGATED. MID WING TO BODY FAIRING AFT L-SUPPORT ANGLE, RIGHT HAND SIDE TOP SCREWHOLE WAS ELONGATED.
- [SDR JR2R20250206869](https://openairdocs.org/sdr/JR2R20250206869), Feb 6, 2025: RIB. CRACKED. RIGHT HAND HORIZONTAL STAB, RIB 12 CRACKED ON UPPER FLANGE AFT OF FRONT SPAR.
- [SDR JR2R20250129766](https://openairdocs.org/sdr/JR2R20250129766), Jan 29, 2025: SEAL REST. CORRODED. FORWARD CARGO CUT OUT; FORWARD LOWER SEAL REST CORRODED
- [SDR JR2R20250129765](https://openairdocs.org/sdr/JR2R20250129765), Jan 29, 2025: SEAL REST. CORRODED. FORWARD CARGO CUT OUT; CENTER LOWER SEAL REST CORRODED
- [SDR JR2R20250129764](https://openairdocs.org/sdr/JR2R20250129764), Jan 29, 2025: SEAL REST. CORRODED. FORWARD CARGO CUT OUT; AFT LOWER SEAL REST CORRODED
- [SDR JR2R20250128182](https://openairdocs.org/sdr/JR2R20250128182), Jan 28, 2025: SPLICE STRAP. CORRODED. AFT WING TO BODY, FUSELAGE FAIRING STRAP SPLICE IS CORRODED.
- [SDR JR2R20250127183](https://openairdocs.org/sdr/JR2R20250127183), Jan 27, 2025: BEAM. CORRODED. CARGO DOOR CUTOUT LOWER BEAM UNDER LOWER SEAL RESTS CORRODED IN MULTPLE PLACES.
- [SDR JR2R20250127169](https://openairdocs.org/sdr/JR2R20250127169), Jan 27, 2025: FRAME. CORRODED. FRAME 83 IS CORRODED BETWEEN STRINGERS 27R TO 28R.
- [SDR JR2R20250127029](https://openairdocs.org/sdr/JR2R20250127029), Jan 27, 2025: SHEAR TIE. CORRODED. FWD CARGO. FRAME 26, STRINGER 27L TO 28L. CENTER FLOOR SUPPORT SHEAR TIE CORRODED
- [SDR JR2R20250127035](https://openairdocs.org/sdr/JR2R20250127035), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO. FRAME 74, STRINGER 28R TO 27R. SHEAR TIE CORRODED
- [SDR JR2R20250127030](https://openairdocs.org/sdr/JR2R20250127030), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO. FRAME 81, STRINGER 26R TO 27R. SHEAR TIE CORRODED
- [SDR JR2R20250127033](https://openairdocs.org/sdr/JR2R20250127033), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO, FRAME 76, STRINGERS 27R TO 28R, SHEAR TIE CORRODED.
- [SDR JR2R20250127181](https://openairdocs.org/sdr/JR2R20250127181), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO, FRAME 83, STRINGERS 28R TO 29R, SHEAR TIE CORRODED.
- [SDR JR2R20250127032](https://openairdocs.org/sdr/JR2R20250127032), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO, FRAME 83, STRINGERS 26R TO 27R, SHEAR TIE CORRODED.
- [SDR JR2R20250127180](https://openairdocs.org/sdr/JR2R20250127180), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO, FRAME 82, STRINGERS 29R TO 28R, SHEAR TIE CORRODED.
- [SDR JR2R20250127034](https://openairdocs.org/sdr/JR2R20250127034), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO, FRAME 75, STRINGERS 27R TO 28R, SHEAR TIE CORRODED.
- [SDR JR2R20250127031](https://openairdocs.org/sdr/JR2R20250127031), Jan 27, 2025: SHEAR TIE. CORRODED. AFT CARGO, FRAME 82, STRINGERS 26R TO 27R, SHEAR TIE CORRODED.
- [SDR JR2R20250124186](https://openairdocs.org/sdr/JR2R20250124186), Jan 24, 2025: STRINGER. CORRODED. SPLICES ON STRINGER 29 BETWEEN FAMES 73 AND 74 CORRODED.
- [SDR JR2R20250124170](https://openairdocs.org/sdr/JR2R20250124170), Jan 24, 2025: STRINGER. CORRODED. STRINGER AND MULTIPLE FASTERNES CORRODED AWAY IN MULTIPLE PLACES IN THE AFT CARGO, STRINGER 29R, FROM FRAME 74 TO FRAME 83.
- [SDR JR2R20250124167](https://openairdocs.org/sdr/JR2R20250124167), Jan 24, 2025: FRAME. CORRODED. CORROSION FOUND ON THE AFT SIDE OF FRAME 82 UNDER THE SHEAR TIE BETWEEN STRINGERS 27R AND 28R.
- [SDR JR2R20250119870](https://openairdocs.org/sdr/JR2R20250119870), Jan 19, 2025: RIB. CRACKED. RH HORIZ STAB RIB 11 CRACKED ON UPPER FLANGE IN TWO PLACES, AFT OF FRONT SPAR
- [SDR JR2R20250119874](https://openairdocs.org/sdr/JR2R20250119874), Jan 19, 2025: RIB. CRACKED. LH HORIZ STAB RIB 11 CRACKED ON UPPER FLANGE IN TWO PLACES, AFT OF FRONT SPAR
- [SDR JR2R20250119873](https://openairdocs.org/sdr/JR2R20250119873), Jan 19, 2025: RIB. CRACKED. LH HORIZ STAB RIB 12 CRACKED ON UPPER FLANGE IN TWO PLACES, AFT OF FRONT SPAR
- [SDR JR2R20250119076](https://openairdocs.org/sdr/JR2R20250119076), Jan 19, 2025: BEAM. CORRODED. LONG BEAM AT LBL 10 BETWEEN FRAMES 87 AND 88 IS CORRODED.
- [SDR JR2R20250119072](https://openairdocs.org/sdr/JR2R20250119072), Jan 19, 2025: SHEAR PANEL. CORRODED. RH SHEAR PANEL IS CORRODED.
- [SDR JR2R20250119079](https://openairdocs.org/sdr/JR2R20250119079), Jan 19, 2025: GUSSET. CORRODED. CENTER GUSSET AT FRAME 90, BL 0 IS CORRODED
- [SDR JR2R20250119796](https://openairdocs.org/sdr/JR2R20250119796), Jan 19, 2025: SKIN. CHAFED. LH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS
- [SDR JR2R20250119807](https://openairdocs.org/sdr/JR2R20250119807), Jan 19, 2025: SKIN. CHAFED. RH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS
- [SDR JR2R20250119877](https://openairdocs.org/sdr/JR2R20250119877), Jan 19, 2025: RIB. CRACKED. L/H HORIZONTAL STAB TIP FAIRING, PANEL 335AL, END RIB IS CRACKED IN RADIUS.
- [SDR JR2R20250119994](https://openairdocs.org/sdr/JR2R20250119994), Jan 19, 2025: BONDING JUMPER. CORRODED. CENTER LOWER FUSELAGE, SKIN AND BONDING JUMPER CLIP CORRODED AFT OF FR31 STR27R
- [SDR MAS2025F00000](https://openairdocs.org/sdr/MAS2025F00000), Jan 19, 2025: BONDING JUMPER. CORRODED. CENTER LOWER FUSELAGE, SKIN AND BONDING JUMPER CLIP CORRODED AFT OF FR31 STR27R
- [SDR JR2R20250119001](https://openairdocs.org/sdr/JR2R20250119001), Jan 19, 2025: BONDING JUMPER. CORRODED. CENTER LOWER FUSELAGE SKIN AND BONDING JUMPER CLIP CORRODED AFRT OF FR 31, ON STR 27L
- [SDR JR2R20250119078](https://openairdocs.org/sdr/JR2R20250119078), Jan 19, 2025: GUSSET. CORRODED. TOP GUSSET AT FR90 LBL10 CORRODED
- [SDR JR2R20250119077](https://openairdocs.org/sdr/JR2R20250119077), Jan 19, 2025: DOUBLER. CORRODED. EXISITNG DOUBLER AT FRAME 87 ON LONG BEAM AT RBL 10 IS CORRODED
- [SDR JR2R20250119048](https://openairdocs.org/sdr/JR2R20250119048), Jan 19, 2025: SILL DRAIN. CORRODED. AFT WET AREA, FR89 O/B MOP SILL CORRODED

All 100: https://openairdocs.org/aircraft/N89304/reports.md

## STCs that may be installed (OpenAirDocs) (20)

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 (Embraer S A ERJ 170-200 LL)

- [STC ST04801NY](https://openairdocs.org/stc/ST04801NY): Installation (including Demod option) of Connectivity Antenna. Delta Engineering Corporation
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST04748NY](https://openairdocs.org/stc/ST04748NY): Installation of the SpaceX Starlink Aviation System. Space Exploration Technologies Corp. / Starlink Aviation
- [STC ST02722LA](https://openairdocs.org/stc/ST02722LA): Updates the aircraft recording system by replacing the forward Cockpit Voice and Data Recorder (CVDR) with a new SRVIVR25 CVDR with Recorder Independent Power Supply (RIPS). Acron Aviation Inc
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST11372DS](https://openairdocs.org/stc/ST11372DS): De-modification of Air-To-Ground (A TG) antennas and associated cabin equipment i. Altitude Aerospace USA
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12138CH](https://openairdocs.org/stc/ST12138CH): Installation of Universal Avionics KAPTURE Combined Cockpit Voice and Flight Data Recorders i. GoAeroMx, LLC
- [STC ST02402LA](https://openairdocs.org/stc/ST02402LA): Interior Installations and Modifications. Safran Cabin Inc
- [STC ST02534SE](https://openairdocs.org/stc/ST02534SE): Installation and maintenance of a Crane Aerospace & Electronics Tire Pressure Sensor Assembly. ELDEC Corporation
- [STC ST09900AC](https://openairdocs.org/stc/ST09900AC): installation of an Electronic Flight Bag (EFB) power system. L2 Aviation
- [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 ST04820NY](https://openairdocs.org/stc/ST04820NY): Installation (including Demod option) of Cabin Connectivity. Delta Engineering Corporation
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04535AT](https://openairdocs.org/stc/ST04535AT): Installation of the CES-170 Emergency Light Power Unit (ELPU). Chippewa Aerospace Inc
- [STC ST03422NY](https://openairdocs.org/stc/ST03422NY): Update of Intelsat components. Delta Engineering Corporation
- [STC ST00957DE](https://openairdocs.org/stc/ST00957DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery. MarathonNorco Aerospace Inc
- [STC ST04435AT](https://openairdocs.org/stc/ST04435AT): Installation of Astronics Passenger In-Seat Power in the Embraer ERJ-170-100, ERJ-170-200, ERJ-190-100 and ERJ-190-200 Series Aircraft. Chippewa Aerospace Inc
- [STC ST03406NY](https://openairdocs.org/stc/ST03406NY): Installation of a gogo Cabin Connectivity System. Delta Engineering Corporation

## Earlier aircraft with N89304

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N89304 before.

- [Cancelled 1974-04-24](https://openairdocs.org/deregistered/N89304-1974-04-24): Cessna 140, S/N 8332. Owner: [Smith Orlin W](https://openairdocs.org/faa-owner/SMITH%20ORLIN%20W), [Colorado Springs, CO](https://openairdocs.org/faa-place/CO/Colorado%20Springs)

## Related

- Other Embraer S A ERJ 170-200 LL aircraft: https://openairdocs.org/model/embraer-s-a-erj-170-200-ll/aircraft.md
- The GE CF34-8E5 engine: https://openairdocs.org/engine/ge-cf34-8e5.md

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