# N484HA: 2001 Boeing 717-200

- Status: Valid registration
- Airframe: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (registry code 1383700, 100 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 55129
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 28, 2001
- Certificate issued: June 29, 2011
- Expires: June 30, 2027
- Mode S code: A5F825
- Registered owner: [Hawaiian Airlines Inc](https://openairdocs.org/faa-owner/HAWAIIAN%20AIRLINES%20INC)
- Location: [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu)
- Owner type: Corporation
- Owner's area on the map: 21.3477° N, 157.8767° W: Placed by OpenAirDocs at the center of ZIP code 96819, 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=484HA
- Page: https://openairdocs.org/aircraft/N484HA

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. The registry lists only the engine series, so ADs for every Rolls-Royce BR-700 model are included.

## ADs that may apply (OpenAirDocs): 78 in force

### Matched by airframe (Boeing 717-200)

- [AD 2026-13-15](https://openairdocs.org/ad/2026-13-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jul 1, 2026
- [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 2025-21-05](https://openairdocs.org/ad/2025-21-05): Landing Gear · Boeing 717-200. Effective Jan 2, 2026
- [AD 2025-02-07](https://openairdocs.org/ad/2025-02-07): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Mar 17, 2025
- [AD 2024-21-01](https://openairdocs.org/ad/2024-21-01): Wings · Boeing 717-200. Effective Nov 7, 2024
- [AD 2024-20-02](https://openairdocs.org/ad/2024-20-02): Fuselage · Boeing 717-200, DC-9-11, DC-9-12 and 16 more. Effective Oct 21, 2024
- [AD 2023-12-15](https://openairdocs.org/ad/2023-12-15): Navigation · Boeing 707-100 Long Body, 707-200, 707-100B Long Body and 74 more. Effective Jun 21, 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 2021-12-12](https://openairdocs.org/ad/2021-12-12): Wings · Boeing 717-200. Effective Jul 29, 2021
- [AD 2021-02-16](https://openairdocs.org/ad/2021-02-16): Ice and rain protection · Boeing 717-200. Effective Mar 30, 2021
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-10-08](https://openairdocs.org/ad/2018-10-08): Stabilizers · Boeing 717-200. Effective May 31, 2018
- [AD 2018-03-04](https://openairdocs.org/ad/2018-03-04): Airspeed/Mach Indicator · Boeing 717-200, DC-9-11, DC-9-12 and 23 more. Effective Mar 16, 2018
- [AD 2017-09-09](https://openairdocs.org/ad/2017-09-09): Passenger Compartment Equipment · Boeing 717-200, MD-90-30, CL-600-2C10 (Regional Jet Series 700) and 17 more. Effective Jun 28, 2017
- [AD 2017-01-03](https://openairdocs.org/ad/2017-01-03): Standard practices/structures · Boeing 717-200. Effective Mar 14, 2017
- [AD 2015-02-05](https://openairdocs.org/ad/2015-02-05): Navigation · Boeing 717-200, DC-10-10, DC-10-10F and 13 more. Effective Mar 5, 2015
- [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014
- [AD 2014-05-22](https://openairdocs.org/ad/2014-05-22): Fuselage · Boeing 717-200. Effective Apr 15, 2014
- [AD 2013-19-22](https://openairdocs.org/ad/2013-19-22): JASC Code 53, Fuselage · Boeing 717-200. Effective Nov 6, 2013
- [AD 2012-12-09](https://openairdocs.org/ad/2012-12-09): Horizontal Stabilizer Structure · Boeing 717-200. Effective Jul 23, 2012
- [AD 2011-12-01](https://openairdocs.org/ad/2011-12-01): Equipment/Furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 268 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-07-07](https://openairdocs.org/ad/2009-07-07): Main landing gear (MLG) · Boeing 717-200. Effective May 5, 2009
- [AD 2008-18-05](https://openairdocs.org/ad/2008-18-05): Elevator standby cable system · Boeing 717-200. Effective Oct 14, 2008
- [AD 2008-11-15](https://openairdocs.org/ad/2008-11-15): Fuel tank systems · Boeing 717-200, DC-9-11, DC-9-12 and 21 more. Effective Jul 3, 2008
- [AD 2008-11-06](https://openairdocs.org/ad/2008-11-06): Gray water drain hose · Boeing 717-200. Effective Jul 3, 2008
- [AD 2008-02-12](https://openairdocs.org/ad/2008-02-12): Center fuel tank · Boeing 717-200. Effective Feb 28, 2008
- [AD 2008-02-08](https://openairdocs.org/ad/2008-02-08): Main fuel tanks · Boeing 717-200. Effective Feb 26, 2008
- [AD 2007-19-15](https://openairdocs.org/ad/2007-19-15): Flight management system (FMS) · Boeing 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Oct 26, 2007
- [AD 2007-19-03](https://openairdocs.org/ad/2007-19-03): Power conversion distribution unit (PCDU) · Boeing 717-200. Effective Oct 17, 2007
- [AD 2007-17-11](https://openairdocs.org/ad/2007-17-11): In-line fuel float switch fuses · Boeing 717-200. Effective Oct 2, 2007
- [AD 2007-13-09](https://openairdocs.org/ad/2007-13-09): Fuel boost pump container · Boeing 717-200. Effective Aug 3, 2007
- [AD 2007-13-01](https://openairdocs.org/ad/2007-13-01): Wiring of the first officer's pitot static heater system · Boeing 717-200. Effective Jul 25, 2007
- [AD 2007-05-06](https://openairdocs.org/ad/2007-05-06): Bulkhead nipple assemblies of the left and right wing vent boxes · Boeing 717-200. Effective Apr 9, 2007
- [AD 2006-20-12](https://openairdocs.org/ad/2006-20-12): Replaces clamp bases on fuel tank vent systems. · Boeing 717-200. Effective Nov 8, 2006
- [AD 2006-10-14](https://openairdocs.org/ad/2006-10-14): Stop pad support fittings · Boeing 717-200, DC-9-11, DC-9-12 and 22 more. Effective Jun 21, 2006
- [AD 2005-16-08](https://openairdocs.org/ad/2005-16-08): Oxygen release system in the forward cabin · Boeing 717-200. Effective Sep 13, 2005
- [AD 2005-11-03](https://openairdocs.org/ad/2005-11-03): Brake fuses. · Boeing 717-200. Effective Jul 1, 2005
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2004-08-02](https://openairdocs.org/ad/2004-08-02): Left and right hand horizontal stabilizer hinge fitting bolts · Boeing 717-200. Effective May 19, 2004
- [AD 2004-03-21](https://openairdocs.org/ad/2004-03-21): Inboard Ends of Outer Skin Panels of Horizontal Stabilizer at Station Xh=7.234 · Boeing 717-200. Effective Mar 17, 2004
- [AD 2004-01-15](https://openairdocs.org/ad/2004-01-15): Auxiliary hydraulic pump · Boeing 717-200. Effective Feb 17, 2004
- [AD 2003-14-05](https://openairdocs.org/ad/2003-14-05): Main spoiler actuators · Boeing 717-200. Effective Jul 31, 2003
- [AD 2003-10-10](https://openairdocs.org/ad/2003-10-10): Rear spar · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-10-08](https://openairdocs.org/ad/2003-10-08): Upper center fuselage · Boeing 717-200. Effective Jul 1, 2003
- [AD 2003-04-24](https://openairdocs.org/ad/2003-04-24): Support Fitting Assemblies and Stop Pads of Main Spoiler Actuators · Boeing 717-200. Effective Mar 17, 2003
- [AD 2002-21-01](https://openairdocs.org/ad/2002-21-01): Electrical terminal contact pins · Airbus A319-111, A319-112, A319-113 and 66 more. Effective Nov 27, 2002
- [AD 2002-16-09](https://openairdocs.org/ad/2002-16-09): Solenoid operated shut-off valve (SOV) · Boeing 717-200. Effective Sep 3, 2002
- [AD 2002-14-16](https://openairdocs.org/ad/2002-14-16): Spoiler Hold-Down Actuator Supports on Left and Right Wing Rear Spar · Boeing 717-200. Effective Aug 16, 2002
- [AD 2001-18-11](https://openairdocs.org/ad/2001-18-11): Rudder Trim · Boeing 717-200. Effective Oct 1, 2001

### Matched by engine (Rolls-Royce BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

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

- [AD 2022-09-18](https://openairdocs.org/ad/2022-09-18) (historical): Navigation · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 72 more. Effective May 23, 2022
- [AD 2020-03-20](https://openairdocs.org/ad/2020-03-20) (historical): Navigation · Modification of Rockwell Collins, Inc. Multi-Mode Receiver (STC ST01883WI or 4 others). Effective Feb 18, 2020
- [AD 2016-09-05](https://openairdocs.org/ad/2016-09-05) (historical): Stabilizers · Boeing 717-200. Effective Jun 8, 2016
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2007-11-13](https://openairdocs.org/ad/2007-11-13) (historical): Principal structural elements (PSEs) · Boeing 717-200. Effective Jun 29, 2007
- [AD 2004-18-04](https://openairdocs.org/ad/2004-18-04) (historical): Airplane Flight Manual (AFM) · McDonnell Douglas 717-200, MD-10-10F, MD-10-30F and 2 more. Effective Sep 20, 2004
- [AD 2003-17-01](https://openairdocs.org/ad/2003-17-01) (historical): Flap system · McDonnell Douglas 717-200. Effective Sep 23, 2003
- [AD 2000-03-51](https://openairdocs.org/ad/2000-03-51) (historical): Jackscrew Assembly · McDonnell Douglas 717-200, DC-9 Series (all), MD-88 and 1 more. Effective Mar 6, 2000
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 92: https://openairdocs.org/aircraft/N484HA/ads.md

## Information bulletins (advisory) (4 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-18-33](https://openairdocs.org/saib/NM-18-33): Engine Fuel and Control. Issued Dec 17, 2018
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006

## NTSB investigations

None matched to N484HA.

## FAA accident and incident reports

None matched to N484HA.

## Service difficulty reports (72, 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 ASAA2026050264582](https://openairdocs.org/sdr/ASAA2026050264582), May 2, 2026: DOOR. NO DISCREPANCY. MAIN CABIN DOOR 1L HARD TO OPEN WOULD GET STUCK HALF WAY. GROUNDED - YES. VISUAL CHECK OF 1L DOOR NORMAL NO DEFECTS NOTED OPERATED DOOR MULTIPLE TIMES FUNCTIONA
- [SDR ASAA2026022263509](https://openairdocs.org/sdr/ASAA2026022263509), Feb 22, 2026: TEST BUTTON. INOPERATIVE. CARGO SMOKE TEST BUTTON DOESN'T WORK. GROUNDED - YES. RESET VIA AND CARGO SMOKE DETECTION PER FIM 26-13 TASK 807. TEST, NO FAULTS NOTED. OK FOR SVC.
- [SDR ASAA2026011962923](https://openairdocs.org/sdr/ASAA2026011962923), Jan 19, 2026: DOOR. NO DISCREPANCY. MAIN CABIN DOOR HARD TO OPEN IAW FA. GROUNDED - YES. MAIN CABIN DOOR OPS CHKD OK, NO DEFECTS NOTED, ACFT OK FOR SVC.
- [SDR ASAA2025122362495](https://openairdocs.org/sdr/ASAA2025122362495), Dec 23, 2025: HANDLE. BINDING. L1 DOOR HANDLE HARD TO OPEN. GROUNDED - YES. PERFORM FIM 52-10 TASK 801 TO STEP C.(1)(B) DOOR NOT HARD TO UNLOCK NO DEFECTS NOTED OK FOR SVC.
- [SDR ASAA2025121562350](https://openairdocs.org/sdr/ASAA2025121562350), Dec 15, 2025: BAYONET. LACK OF LUBE. 1L DOOR HARD TO OPEN. GROUNDED - YES. LUBRICATED DOOR BAYONET INSPECTED SEALS AND HANDLES. OPS CHECK GOOD OK FOR SVC.
- [SDR HALA20250731042](https://openairdocs.org/sdr/HALA20250731042), Jul 30, 2025: VANE. DENTED. DENT ON LH WING FLAP FIXED VANE INBOARD DENETIONS 5" X 1 ". REPLACED LT WING INBRD FLAP FIXED VANE PER AMM 27-50-02 OPS CHECK GOOD.
- [SDR HALA2023040100015](https://openairdocs.org/sdr/HALA2023040100015), Apr 1, 2023: UNKNOWN. UNKNOWN. OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD. OK FOR SERVICE
- [SDR HALA202211010004](https://openairdocs.org/sdr/HALA202211010004), Oct 29, 2022: COMPRESSOR. STALLED. ATB-RH ENG COMPRESSOR STALL WITH LOUD BANG AND FLUTTER. REMOVED AND REPLACED NUMBER TWO ENGINE PER T/C E1128-717-72-003-REMOVAL W/O 236088
- [SDR HALA2022072500136](https://openairdocs.org/sdr/HALA2022072500136), Jul 23, 2022: NONE. NONE. ATO - L ENG COMPRESSOR STALL ON TAKEOFF.// L/H ENG REMOVED AND REPLACED PER TC E1128-717-72-003-REMOVAL AND 71-HWI-00-02. OK FOR SERVICE.
- [SDR HALA2021012700012](https://openairdocs.org/sdr/HALA2021012700012), Jan 25, 2021: LINE. LEAKING. ATO-ATO/BTB: HYD L QTY LO ALERT ON T/O ROLL. INSTALLED NR 1 EDP HYD LOW PRESSURE SWITCH LINE, PER AMM 20-10-13-911-801 AND AMM 29-34-01-000-801. PERFORMED IDLE 
- [SDR HALA2020070700139](https://openairdocs.org/sdr/HALA2020070700139), Jul 6, 2020: VANE. CORRODED. ON OVERNIGHT, FOUND LEFT WING OUTBOARD FIXED FLAP VANE CORRODED AT THE INBOARD EDGE. REMOVED AND REPLACED LEFT OUTBOARD FIXED FLAP VANE IAW AMM 27-50-02. ADJUST
- [SDR HALA2020060800123](https://openairdocs.org/sdr/HALA2020060800123), Jun 7, 2020: PITOT TUBE. DENTED. FOUND F/O PITOT TUBE DAMAGED IN INLET. REMOVED AND REPLACED DAMAGED F/O PITOT TUBE PER AMM 34-11-01. OPS CHECK AND LEAK CHECK GOOD.
- [SDR HALA2020013110024](https://openairdocs.org/sdr/HALA2020013110024), Jan 30, 2020: ELECTRICAL SYS. UNKNOWN. POWER INTERUPTION WHEN EXTERNAL POWER WAS DISCONECTED, RESET AND RTS PASSED.
- [SDR HALA2019090300359](https://openairdocs.org/sdr/HALA2019090300359), Sep 1, 2019: LENS. DAMAGED. 1ST CLASS EXIT SIGN COVER DAMAGED. ( EMERGENCY EXIT LIGHT ). REPLACED EXIT SIGN LENS.
- [SDR HALA2019060700281](https://openairdocs.org/sdr/HALA2019060700281), Jun 6, 2019: ACTUATOR. MALFUNCTIONED. ATB - ON APPROACH, AFTER GEAR EXTENSION "GEAR DOOR OPEN" ALERT CAME ON. RECYCLED THE GEAR AGAIN AND ALERT CAME ON. GEAR WAS DOWN AND 3 GREEN. NORMAL GEAR INDICA
- [SDR HALA2019041200188](https://openairdocs.org/sdr/HALA2019041200188), Apr 9, 2019: SKIN. DENTED. DENT FOUND AT STA 218, L26L.// CUT OUT DAMAGE AREA PER SRM 53-03-01-2R-1 REPAIR 1 FIGURE 206 SHEET 3 CLASS 2 REPAIR. HFEC OK. FOUND LONGERON DAMAGED. THE DAMAGE
- [SDR HALA2019012600033](https://openairdocs.org/sdr/HALA2019012600033), Jan 26, 2019: BRACKET. CORRODED. RIGHT HAND FLAP UPPER MOVABLE VANE INBOARD GUIDE BRACKET HAS EXFOLIATION CORROSION. REPLACED AND PICKED UP HOLES ON RIGHT HAND FLAP UPPER MOVABLE VANE INBD GUID
- [SDR HALA2019011800031](https://openairdocs.org/sdr/HALA2019011800031), Jan 18, 2019: STOP FITTING. CORRODED. RIGHT HAND FLAP TRACK STOP HAS EXFOILATION CORROSION. 1. REPLACED FLAP TRACK STOP PER DWG #5913134.
- [SDR FOTR20181022001](https://openairdocs.org/sdr/FOTR20181022001), Oct 22, 2018: DOUBLER. CRACKED. RUDDER HAS AN EDGE CRACK ON THE LOWER SIDE OF THE LT RUDDER DURING REMOVAL.
- [SDR HALA2018062600302](https://openairdocs.org/sdr/HALA2018062600302), Jun 24, 2018: SMOKE DETECTOR. FAULTY. LAVATORY SMOKE MESSAGE. REPLACED LAV SMOKE DETECTOR PER FIM 26-14 TASK 801. OPS GOOD OK FOR SVC.
- [SDR HALA2018060600279](https://openairdocs.org/sdr/HALA2018060600279), Jun 5, 2018: WARNING MESSAGE. FALSE ACTIVATION. CARGO SMOKE AFT FAIL ALERT DURING GROUND TEST. PERFORMED FIM 26-13 TASK 802, OPS CHECKED GOOD. NO DEFECTS NOTED. AFT CARGO REACTIVATED BACK TO NORMAL.
- [SDR HALA2018060500277](https://openairdocs.org/sdr/HALA2018060500277), Jun 5, 2018: SMOKE DETECTOR. NO TEST. AFT CARGO BAY, AFT SMOKE DETECTOR DOES NOT TEST. REPLACED THE SMOKE DETECTOR ASSY IAW AMM 26-13-01. SMOKE DETECTOR TESTED OK.
- [SDR HALA2017102500260](https://openairdocs.org/sdr/HALA2017102500260), Oct 24, 2017: WARNING MESSAGE. FALSE ACTIVATION. CARGO SMOKE AFT FAIL, AFTER TEST. TESTED CARGO SMOKE SYSTEM, TEST PASSED, OK FOR SERVICE.
- [SDR HALA2017100400250](https://openairdocs.org/sdr/HALA2017100400250), Oct 4, 2017: O-RING. LEAKING. ATB, RIGHT HYDRAULIC QUANTITY LEAK. REPLACED LT BUNGEE CYLINDER ACTUATOR O-RING.
- [SDR HALA2017032800088](https://openairdocs.org/sdr/HALA2017032800088), Mar 28, 2017: PITOT HEAD. OBSTRUCTED. AIR TURN BACK FOR MULTIPLE ALERTS BEING DISPLAYED, STICK PUSHER FAIL, A/P NOT AVAILABLE, IAS ANOMALY BETWEEN CAPTAIN & FIRST OFFICER, RUDDER LIMITER FAIL. FOUND
- [SDR HALA2016122600562](https://openairdocs.org/sdr/HALA2016122600562), Dec 26, 2016: CONTROL UNIT. FAILED. ANTI-SKID FAIL ALERT ON LANDING GEAR EXTENSION. DIVERTED. REMOVED AND REPLACED BCU IAW AMM 32-45-01. PERFORMED RTS. RTS PASSED. OK FOR SERVICE.
- [SDR HALA2016102600377](https://openairdocs.org/sdr/HALA2016102600377), Oct 26, 2016: WARNING SYSTEM. ACTIVATED.  OPEN - ATO - TANK L AFT PUMP LO LIGHT ILLUMINATED ON THROTTLE ADV FOR T/O, MAIN TANK FUEL AC BOOST PUMPS. DEFERRED USING MEL 28-22-01.
- [SDR HALA2016082800337](https://openairdocs.org/sdr/HALA2016082800337), Aug 28, 2016: PROXIMITY SENSOR. OUT OF ADJUST. AFTER TAKE OFF WHEN GEAR WAS RETRACTED LEFT MAIN GEAR "UNSAFE" "RED" LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. FOUND LEFT MLG UP AND LATCHED PROXIMITY 
- [SDR HALA2016072500293](https://openairdocs.org/sdr/HALA2016072500293), Jul 25, 2016: INTERFACE UNIT. MALFUNCTIONED. DURING TAKEOFF AT APPROX 70 KNTS, TAKE OFF CONFIGURATION WARNING FOR STAB TRIM ENUNCIATED. STAB TRIM WAS SET PROPERLY. PERFORMED CAWS SYSTEM TEST PER FIM 31-51 
- [SDR HALA2016071400273](https://openairdocs.org/sdr/HALA2016071400273), Jul 14, 2016: ADIRU. FAILED. AFTER TAKE OFF, IAS-AMBER, NO COMMAND BARS ON PFD, AUTOPILOT INOPERATIVE, RUDDER LIMITER RESTRICTED, RUDDER LIMITER FAILED. REPLACED NR 1 ADIRU PER FIM 34-16- T
- [SDR HALA2016051900200](https://openairdocs.org/sdr/HALA2016051900200), May 18, 2016: DOWNLOCK SENSOR. FAILED. WHEN RAISING GEAR LT MAIN INDICATED UNSAFE, RED. DID NOT FEEL ANY TURBULENCE WHEN UNSAFE INDICATION WAS ON. R & R LT MAIN GEAR DOWN/LOCKED PROXIMITY SENSORS IAW
- [SDR 2016FA0000250](https://openairdocs.org/sdr/2016FA0000250), May 18, 2016: POSITION SENSOR. FAILED. LEFT GEAR UNSAFE LIGHT WITH GEAR HANDLE IN UP POSITION. REPLACED SENSOR LINK & CHECK ADJUSTMENT OF LT MLG GEAR UP & LATCHED PROXIMITY SENSOR. GND OPERATIONS CHE
- [SDR HALA2016051000176](https://openairdocs.org/sdr/HALA2016051000176), May 10, 2016: TIRE. FAILED. RIGHT OTBD TIRE, NR 4, TREAD SEPARATED. VERIFIED TIRE PRESSURE PRIOR TO REMOVAL, FOUND AT 185 PSI, TIRE WARM. R & R NR 4 MAIN WHEEL AND TIRE ASSY IAW AMM 32-41-
- [SDR HALA201506240114](https://openairdocs.org/sdr/HALA201506240114), Jun 24, 2015: SLIDE. NO TEST. AFTER TAIL CONE SLIDE FUNCTIONAL TEST FOUND TAIL CONE SLIDE PACKED IMPROPERLY UNABLE TO SEE THE PRESSURE GAUGE. REPLACED AFT TAIL CONE SLIDE IAW AMM 25-61-02.
- [SDR HALA201506100108](https://openairdocs.org/sdr/HALA201506100108), Jun 9, 2015: LONGERON. CRACKED. FOUND CRACK ON BOTTOM OF LONGERON BY VERTICAL FRAME OF NR 2 ENGINE APRON. FOUND CRACK TO BE ON PREVIOUS REPAIR ANGLE. REMOVED REPAIR ANGLE INSPECTED AND HFEC AR
- [SDR HALA2015051200072](https://openairdocs.org/sdr/HALA2015051200072), May 12, 2015: COMPRESSOR. STALLED. AIR DIVERSION, NR 1 ENGINE COMPRESSOR STALL IN FLIGHT. ENGINE CHANGED.
- [SDR HALA2015042600065](https://openairdocs.org/sdr/HALA2015042600065), Apr 26, 2015: PACKING. LEAKING. "HYD RT QTY LO" SYS FAILURE. R & R LT MLG BUNGEE CYLINDER B-NUT LINE FITTING PACKING IAW AMM 32-33-02 STEP 2, D, 1, H AND STEP 3, E, P. LEAK CHECK GOOD.
- [SDR HALA2014050500061](https://openairdocs.org/sdr/HALA2014050500061), May 5, 2014: SLIDE. OPEN. TAILCONE SLIDE OPENED, UNRAVELLED, DURING TAIL CONE DEPLOYMENT TEST. R & R THE TAIL CONE SLIIDE ASSY IAW AMM 25-61-02, SECURITY CHECKED GOOD.
- [SDR HALA2012022300070](https://openairdocs.org/sdr/HALA2012022300070), Feb 23, 2012: POWER SUPPLY. FAILED. EMERGENCY LIGHTS ROW 1-5 INOPERATIVE. REPLACED B5-115, IAW AMM 33-51-03. OPS CHECKED OK.
- [SDR HALA2012022000065](https://openairdocs.org/sdr/HALA2012022000065), Feb 20, 2012: WARNING LIGHT. FALSE ACTIVATION. GEAR DOOR OPEN LIGHT ILLUMINATED INTERMITTENTLY ON APPROACH. PERFORMED FIM TASK 32-60-802, STEPS E1, B2, 3, 4, B. OPERATED GEAR, ALERT DOES NOT SHOW. ALL SENSOR
- [SDR HALA201202090052](https://openairdocs.org/sdr/HALA201202090052), Feb 9, 2012: PROXIMITY SENSOR. FALSE INDICATION. AFTER TAKEOFF PLACED GEAR HANDLE UP, LT MAIN UNSAFE INDICATION LIGHT AND LEVEL PSEU FAIL LIGHT. REPLACED LT MLG DOWN LOCK PROXIMITY SENSORS IAW AMM 32-61-04. RE
- [SDR HALA2011092000415](https://openairdocs.org/sdr/HALA2011092000415), Sep 20, 2011: LAMP. INOPERATIVE. AISLE EMERGENCY LIGHT BY SEAT NR1 INOPERATIVE. RELAMPED AISLE LIGHT AT SEAT NR 1, OPS CHECKED OK.
- [SDR HALA2011060800255](https://openairdocs.org/sdr/HALA2011060800255), Jun 8, 2011: LATCH. BROKEN. MLG DOOR LATCH ON RT SIDE UPLOCK MECHANICAL LATCH BROKEN. R & R RT MLG DOOR LATCH IAW AMM 32-34-01. CLEARANCE AND OPS CHECK OK. REMOVED NLG & MLG PINS. OK FOR S
- [SDR HALA2011053100242](https://openairdocs.org/sdr/HALA2011053100242), May 31, 2011: DOOR. DAMAGED. OPEN - PASSENGER/CREW ENTRANCE DOOR WAS LIFTED BY THE JETWAY BRIDGE CAUSING DAMAGE TO THE BOTTOM OF THE DOOR. REPAIR IN WORK.
- [SDR HALA2011052400223](https://openairdocs.org/sdr/HALA2011052400223), May 24, 2011: CONTROL UNIT. BINDING. AILERON CONTROL IS BINDING, REPEAT WRITE UP. LUBRICATED LT & RT CONTROL TAB CABLES & PULLEYS IAW AMM12-24-00, OPS CK OK, NO BINDING NOTED. ACCOMP RTS ON SECU AL
- [SDR HALA2011052300216](https://openairdocs.org/sdr/HALA2011052300216), May 23, 2011: AILERON SYS. LACK OF LUBE. AILERON CONTROL IS BINDING. LUBRICATED CONTROL TAB IAW MM 12-24--00 SECURITY AND CONTROL CHECK GOOD.
- [SDR HALA2011022700118](https://openairdocs.org/sdr/HALA2011022700118), Feb 27, 2011: ENGINE. FAILED. NR 1 ENGINE FAILED. SHUT DOWN ENGINE. ENGINE CHANGE IN WORK. OPEN
- [SDR HALA2010110100512](https://openairdocs.org/sdr/HALA2010110100512), Nov 1, 2010: POWER SUPPLY. INOPERATIVE. SEAT MOUNTED EXIT LIGHTS ROW 2 EF INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY B5-118 IAW AMM 33-54-03 OPS CHECK OK.
- [SDR HALA2010100800459](https://openairdocs.org/sdr/HALA2010100800459), Oct 8, 2010: DISPLAY. MALFUNCTIONED. AIR TURN BACK - UNABLE TO SELECT OTHER PAGES ON MCDU OTHER THAN /TO/APPR PG SWITCHES MOMENTARILY - REVERTS BACK. RESET BOTH VIA NR1 AND NR2 - OPS CHECK OK IAW A
- [SDR HALA2010051700249](https://openairdocs.org/sdr/HALA2010051700249), May 17, 2010: CONTROL CABLE. DISLODGED. RT WING SLAT CONTROL CABLE JUMPED OUT OF PULLEY AND DAMAGED RIBS, 2 EA AT SLAT CONTROL MECHANISM OTBD SUPPORT. REMOVED R/W SLAT CONTROL CABLES, 2,3,4,AND 5 SLAT

All 72: https://openairdocs.org/aircraft/N484HA/reports.md

## STCs that may be installed (OpenAirDocs) (71, first 50)

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 (Boeing 717-200)

- [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 ST02463AT](https://openairdocs.org/stc/ST02463AT): Installation of an Intrusion/Penetration Resistance Flightdeck Door and Reinforced Flightdeck Door Surround. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04122AT](https://openairdocs.org/stc/ST04122AT): Installation of an oven. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST04816NY](https://openairdocs.org/stc/ST04816NY): Installation of Electronically Steerable (ESA) Antenna and Power Supply. ALOFT AeroArchitects
- [STC ST12026AT](https://openairdocs.org/stc/ST12026AT): Installation of Portable Emergency Locator Transmitter. Delta Flight Products LLC
- [STC ST02478NY](https://openairdocs.org/stc/ST02478NY): Installation of an advertisement container on the bottom of a seat back tray table on Weber Model 5300 passenger seats (Weber Part Numbers 852454, 852455, 852456, 852457, 852458, and 852459). Atin OOH, LLC
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST04813NY](https://openairdocs.org/stc/ST04813NY): Installation of Hughes Satellite Connectivity and Wifi Cabin Distribution System. ALOFT AeroArchitects
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [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 ST03682AT](https://openairdocs.org/stc/ST03682AT): Installation of an Aircell Broadband Service (ABS) Passenger Cabin Air-To-Ground (ATG) Voice/Data Communication System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST11388DS](https://openairdocs.org/stc/ST11388DS): Expansion of the Delta Comfort+® Passenger Seating Section. Aircraft Systems and Manufacturing Inc
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST02637AT](https://openairdocs.org/stc/ST02637AT): Installation of SafTGlo Inc. photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [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 ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC SA9024NM-D](https://openairdocs.org/stc/SA9024NM-D): Installation of Scandinavian Bellyloading Company, sliding carpet loading system. SBC-America LLC
- [STC ST04416AT](https://openairdocs.org/stc/ST04416AT): Installation of the Rockwell Collins Multi-Mode Receiver (MMR). Woven Electronics LLC
- [STC ST04418AT](https://openairdocs.org/stc/ST04418AT): Installation of the Rockwell Collins Automatic Dependent Surveillance - Broadcast (ADS-B) Out System. Woven Electronics LLC
- [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC
- [STC ST01465LA-D](https://openairdocs.org/stc/ST01465LA-D): Installation of B/E Aerospace, Inc. Air Chiller Part Number 374-8. B/E Aerospace Inc
- [STC ST01023SE](https://openairdocs.org/stc/ST01023SE): Installation of a the TPA-81A Traffic Alert and Collision Avoidance System (TCAS) Processor in accordance with Master Drawing List 756-0119-001, Revision D, dated November 21, 2003, or later FAA approved revisions. Honeywell International Inc
- [STC ST01096SE](https://openairdocs.org/stc/ST01096SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST01640SE](https://openairdocs.org/stc/ST01640SE): Installation of the Mark III Aircraft Communications Addressing and Reporting System (ACARS). Honeywell International Inc
- [STC ST03418NY](https://openairdocs.org/stc/ST03418NY): Installation of a UTC Electronic Flight Bags. Rockwell Collins Inc
- [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc
- [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04029CH](https://openairdocs.org/stc/ST04029CH): Modification of an existing Aircell Broadband Services (ABS) System with ATG4 Enhancements. Intelsat Inflight LLC
- [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC
- [STC ST04425CH](https://openairdocs.org/stc/ST04425CH): Installation of a Honeywell One Aero Edge Node (1AEN) in accordance with StandardAero Master Data List 1037081, Revision (B), dated June 9, 2020 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04424CH](https://openairdocs.org/stc/ST04424CH): TPED Compatibility Test in accordance with StandardAero Master Data List 1037140, Revision (B), dated June 1, 2020 or later FAA approved revision. Standard Aero Business Aviation Services LLC
- [STC ST04468NY](https://openairdocs.org/stc/ST04468NY): Installation of Honeywell ADS-B Transponder Upgrade. H4 Aerospace (UK) Ltd
- [STC ST02152LA](https://openairdocs.org/stc/ST02152LA): Installation of AmSafe Aviation Inflatable Restraint (AAIR) System. AMSAFE Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA8339SW](https://openairdocs.org/stc/SA8339SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST04229NY](https://openairdocs.org/stc/ST04229NY): Introduction of a 16G New Generation Stretcher XL P/N 1120030-Series. Bucher Leichtbau AG
- [STC ST04167NY](https://openairdocs.org/stc/ST04167NY): Installation of TCAS System upgrade to Change 7.1. H4 Aerospace (UK) Ltd
- [STC ST03846NY](https://openairdocs.org/stc/ST03846NY): Installation of SuperSeal UltraLite (SSUL) PHOTOLUMINESCENT AISLE PATH MARKING SYSTEM. STG Aerospace Ltd
- [STC ST04242CH](https://openairdocs.org/stc/ST04242CH): Installation of ACSS Automatic Dependent Surveillance-Broadcast (ADS-B) compliant Mode S Transponders. Canard Aerospace Corporation
- [STC ST04186CH](https://openairdocs.org/stc/ST04186CH): Retrofit installation of Rosemount Aerospace Model 0861EW2 Angle of Attack (AOA) Sensors. Rosemount Aerospace Inc
- [STC ST02479SE](https://openairdocs.org/stc/ST02479SE): Installation of class dividers and cross aisle curtain headers. Northwest Aerospace Technologies Inc
- [STC SA7076NM](https://openairdocs.org/stc/SA7076NM): Installation of Stretcher Carrier. Air Medic LLC
- [STC ST02991AT](https://openairdocs.org/stc/ST02991AT): Installation of LiveTV XM Satellite Radio System. Thales Avionics Inc
- [STC ST03449CH](https://openairdocs.org/stc/ST03449CH): Installation of LH and RH Passenger Window - STA 218 to STA 237. AAR Aircraft Services
- [STC ST04206AT](https://openairdocs.org/stc/ST04206AT): Interior reconfiguration. Delta Air Lines Inc
- [STC ST03442CH](https://openairdocs.org/stc/ST03442CH): Installation of New Interior Arrangement. AAR Aircraft Services
- [STC ST03817AT](https://openairdocs.org/stc/ST03817AT): Installation of a Thales-KANNAD Emergency Locator Transmitter. Avionics Support Group Inc

All 71: https://openairdocs.org/aircraft/N484HA/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce BR-700 series engine: https://openairdocs.org/engine/rolls-royce-br-700-series.md

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