# N489HA: 1998 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 Deutschland BR700-715A130](https://openairdocs.org/engine/rolls-royce-deutschland-br700-715a130) (registry code 54006)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (The Boeing Company), [TCDS E00061EN](https://openairdocs.org/tcds/E00061EN) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 55002
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 17, 2008
- Certificate issued: June 28, 2011
- Expires: June 30, 2027
- Mode S code: A60AB8
- 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=489HA
- Page: https://openairdocs.org/aircraft/N489HA

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): 64 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 Deutschland BR700-715A130)

- [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 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 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 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 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 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 2005-16-12](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

### 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 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

All 74: https://openairdocs.org/aircraft/N489HA/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 N489HA.

## FAA accident and incident reports

None matched to N489HA.

## Service difficulty reports (59, 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 ASAA2026092066990](https://openairdocs.org/sdr/ASAA2026092066990), Sep 20, 2026: DOOR. LACK OF LUBE. BOARDING DOOR HARD TO OPEN AND CLOSE. GROUNDED - YES. LUBRICATED AND CLEANED FWD PASSENGER ENTERANCE DOOR ASSEMBLY PER AMM 52-11-1-88277 OPS CHECK GOOD OK FOR S
- [SDR ASAA2026091966988](https://openairdocs.org/sdr/ASAA2026091966988), Sep 19, 2026: SLIDE. OUT OF POSITION. AFTER DISARMING DOOR, SLIDE PACK FELL OUT OF THE 1L DOOR. SLIDE DID NOT DEPLOY. GROUNDED - YES. RE INSTALLED SERVICEABLE EVAC SLIDE ON 1L DOOR PER AMM 25-61-+01
- [SDR ASAA2026091066874](https://openairdocs.org/sdr/ASAA2026091066874), Sep 10, 2026: FLT CONTROLS. FAULTED. AIRCRAFT HAD HARD ROLL TO THE RIGHT, 10 DEGREES AT GEAR EXTENSION, FLAPS 18 UNIT, 170KTS 2100FT. ASA1074 HNL LDG RWY 26L ON AS1074 ON 9/9/2026. GROUNDED - YES. 
- [SDR ASAA2026082966644](https://openairdocs.org/sdr/ASAA2026082966644), Aug 29, 2026: FLT CONTROLS. FAULTED. UNCONTROLLED ROLL ON SHORT FINAL. REPEAT WRITE UP, FLAPS 40, VAPP 143, 400 FEET, AUTOPILOT/AUTO THROTTLES OFF. GROUNDED - YES. COMPLIED WITH TSI-00723 ITEM 1, A
- [SDR ASAA2026080966254](https://openairdocs.org/sdr/ASAA2026080966254), Aug 9, 2026: ACTUATOR. FAULTED. ACFT ROLLED 15*, RT WING DOWN WITH CLEAN CONFIG TRIM (AILERON& RUDDER) WITH FLAPS 40* & GEAR DOWN AFTER HANDS OFF CONTROLS FOR 10 SECS. GROUNDED - YES. PERFORME
- [SDR ASAA2026080566153](https://openairdocs.org/sdr/ASAA2026080566153), Aug 5, 2026: ACTUATOR. UNSERVICEABLE. ON LANDING, ACFT GAVE AN UNCOMMANDED LT WING DOWN. PILOT FLYING ABLE TO COUNTER WITH RT INPUT. WING ROLLED A FEW DEGREES BUT THE YOKE DID AN UNCOMMANDED LT INPU
- [SDR HALA20250606031](https://openairdocs.org/sdr/HALA20250606031), Jun 4, 2025: LAVATORY. PAX ERROR. INFO TO MX FA REPORTED SOMEONE SMOKING IN LAV/STARTED A SMALL FIRE. FA EXTINGUISHED WITH WATER, NO AGENT DISCHARGE. PERFORMED PRECAUTIONARY CHECK OF LAV FIRE EX
- [SDR HALA202401132003](https://openairdocs.org/sdr/HALA202401132003), Jan 11, 2024: UNKNOWN. UNKNOWN. UPON PRE-FLIGHT FOUND OVHD EMER EXIT LTS FWD 1/2 INOP-DO NOT ILLUMINATE. REMOVED AND REPLACED EMER LIGHT BATTERY POWER SUPPLY PER AMM 35-51-03. OPS CHECK GOOD. 
- [SDR HALA202201310032](https://openairdocs.org/sdr/HALA202201310032), Jan 30, 2022: NONE. NONE. LOUD SQUEAL FROM SERVICE DOOR (R1) DURING CLIMB // REPOSITION SPONGE FILLER TO 1R DOOR PER AMM SUBTASK 52-42-00-420-001 AND APPLIED NEW SEALANT TO 1R DOOR SCUFF
- [SDR HALA2021122700202](https://openairdocs.org/sdr/HALA2021122700202), Dec 25, 2021: DOOR. DAMAGED. EMER EQ - DOOR - FOUND DENT/GOUGE BELOW LEADING EDGE OF 1R SERVICE DOOR. // EDDY CURRENT SHOWS NO CRACK. #8089 12/24/21. BLEND GOUGE PER SRM 53-01-01-1A-1. MEAS
- [SDR HALA2021111600162](https://openairdocs.org/sdr/HALA2021111600162), Nov 14, 2021: NONE. NONE. 3 REDS AFTER GEAR HANDLE WAS DROPPED USED ALT GEAR HANDLE GOT 3 GREEN TRIED TO STOW THE AGH BUT GOT 3 REDS AGAIN // FOUND LANDING GEAR HANDLE STICKY, AND NOT GO
- [SDR HALA2021102600146](https://openairdocs.org/sdr/HALA2021102600146), Oct 25, 2021: UNKNOWN. ODOR. BTB ON PUSH BACK STARTING LEFT ENGINE FA'S SMELLED SMOKE IN CABIN // INSPECTED PAX PSU @1-2AB, NO DEFECTS NOTED, PERFORMED ENGINE RUN, COULD NOT DUPLICATE SMELL
- [SDR HALA2021091500117](https://openairdocs.org/sdr/HALA2021091500117), Sep 15, 2021: DOOR. BINDING. EMER EQ - FWD ENTRY DOOR HARD TO OPEN AND CLOSE // PERFORMED INSPECTION OF 1L DOOR PER AMM 52-11-01-220-801. FOUND MULTIPLE SPOTS OUT OF SPEC. NEED TO CHECK RIG
- [SDR HALA2021040600043](https://openairdocs.org/sdr/HALA2021040600043), Apr 5, 2021: BATTERY PACK. INOPERATIVE. EMER EQ - AFT CABIN EMERGENCY LIGHT INOP // REMOVED AND REPLACED BATTERY PACK , EMER B5-231 PER WDM 33-51-12-3.1. OPS CHECK GOOD
- [SDR HALA2021030400025](https://openairdocs.org/sdr/HALA2021030400025), Mar 3, 2021: BAYONET. OUT OF ADJUST. EMER EQ - DURING OVERNIGHT FOUND MAIN ENTRY DOOR COULD NOT CLOSE FROM OUTSIDE HANDLE. PUSH PULLGAUGE SHOWS 120LBS TO CLOSE FROM OUTSIDE HANDLE AND 80LBS TO CLOS
- [SDR HALA2021031200031](https://openairdocs.org/sdr/HALA2021031200031), Mar 1, 2021: RIB. CRACKED. CRACK - RIGHT SIDE UNDERWING BARREL KEEL AREA (INSIDE) RIB CRACKED OTBD SIDE STA. 674 // REPAIR FORMER PER E105-B10214-PERM 1/25/21 MECH 13377 INSP 4884
- [SDR HALA2021031200030](https://openairdocs.org/sdr/HALA2021031200030), Mar 1, 2021: FORMER. CRACKED. CRACK - RH MLG DOOR FORMER P/N 9923450-504 CRACKED STA 750.2729 (M) // INSTALLED REPLACEMENT MLG DOOR FORMER P/N 9923450-504 IAW DWG# 5910783.
- [SDR HALA2021031200029](https://openairdocs.org/sdr/HALA2021031200029), Mar 1, 2021: FORMER. CRACKED. CRACK - RH MLG DOOR FORMER P/N 9923450-502 CRACKED UNDER REPAIR FILLER STA 745.027 (M) // INSTALLED REPLACEMENT MLG DOOR FORMER P/N 9923450-502 AT STA 745.027 I
- [SDR HALA2021030100023](https://openairdocs.org/sdr/HALA2021030100023), Feb 28, 2021: BATTERY PACK. INOPERATIVE. EMER EQ - OVERWING EMERGENCY LIGHTS DO NOT ILLUMINTAE WITH EMER LT SWITCH ON // REMOVED AND REPLACED OVERWING EMER. EVAC BATTERY POWER SUPPLY PER AMM 33-51-06. 
- [SDR HALA2020030900056](https://openairdocs.org/sdr/HALA2020030900056), Mar 7, 2020: SMOKE WARNING. ACTIVATED. AFT CARGO SMOKE INDICATED AT THE GATE. DISCHARGED AGENT 1. // REMOVED AND REPLACED AGENT 1 FIRE EXTINGUISHER CONTAINER IN ACCORDANCE WITH AMM 26-22-01/401 E(2)(
- [SDR HALA2019120400503](https://openairdocs.org/sdr/HALA2019120400503), Dec 3, 2019: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT EXIT HATCHES DONT TURN ON WHEN SWITCH IS ON//REMOVED AND REPLACED EMERGENCY POWER BATTERY AT LOCATION B-5-121. OPS CK GOOD PER AMM 33-51-00.
- [SDR HALA2019101500414](https://openairdocs.org/sdr/HALA2019101500414), Oct 14, 2019: TRANSDUCER. DIRTY. L HYD PRESS LOW ON LDG. STEERING RESTRICTED. R(PRESSURE DROPPED TO 800PSI). // PERFORMED FIM 29-30 TASK 802. CLEANED L HYD PRESS XDCR. RAN NO.1 ENGINE. OPS CHEC
- [SDR HALA2019101100409](https://openairdocs.org/sdr/HALA2019101100409), Oct 10, 2019: SIGN. DETACHED. EXIT SIGN NEAR FORWARD ENTRANCE WILL NOT STAY ATTACHED. SECURED EXIT SIGN REF AMM 25-60-00 SECURITY CHECK GOOD.
- [SDR HALA2019031100110](https://openairdocs.org/sdr/HALA2019031100110), Mar 10, 2019: DOWNLOCK SENSOR. DAMAGED. AFTER ENGINE SHUT DOWN PSEU ENGINE FAULT LIGHT ON. REMOVED AND REPLACED BOTH DAMAGED RT MLG DOWNLOCK SENSOR ASSEMBLIES, PER AMM 32-61-04-400-801. PERFORMED PSEU
- [SDR HALA2018101200494](https://openairdocs.org/sdr/HALA2018101200494), Oct 11, 2018: LIGHT. MALFUNCTIONED. FA REPORTS ON TAXI OUT AND TAXI IN, EMERGENCY LIGHT SYSTEM CAME ON FOR A COUPLE MINUTES. PERFORMED FIM TASK 33-50 TASK 801. NO FAULTS NOTED, NO 10 DAY HISTORY O
- [SDR HALA2018090500412](https://openairdocs.org/sdr/HALA2018090500412), Sep 4, 2018: WIRE. BROKEN. AFT BULKHEAD DOOR EXIT MARKER SIGN INOPERATIVE. FOUND WIRE C9302-263-16 BROKEN. REPAIRED THE WIRE IAW SWPM 20-10-03, AND WDM 33-51-12. EMERGENCY LIGHTING SYSTEM
- [SDR HALA2018072600406](https://openairdocs.org/sdr/HALA2018072600406), Jul 25, 2018: INVERTER. MALFUNCTIONED. WHEN ARMING EMERGENCY PWR, EMER AC COMES OFFLINE. REMOVED AND REPLACED STATIC INVERTER PER AMM 24-24-01. OK FOR SVC.
- [SDR HALA2018072300330](https://openairdocs.org/sdr/HALA2018072300330), Jul 21, 2018: INVERTER. INOPERATIVE. WHEN TESTING ELEC EMERGENCY POWER GOT A/C EMER BUS OFF LT. REMOVED AND REPLACED STATIC INVERTER PER AMM 24-24-01. OPS CHECK GOOD PER AMM 24-24-00-720-803.
- [SDR HALA2018072000326](https://openairdocs.org/sdr/HALA2018072000326), Jul 19, 2018: SMOKE DETECTOR. NO TEST. FWD CARGO SMOKE DETECTOR NR 8 FAILED TO TEST. REMOVED AND REPLACED THE SMOKE DETECTOR IAW AMM 26-13-01. OPS CHECKED AND SECURITY CHECKED GOOD.
- [SDR HALA2018072000327](https://openairdocs.org/sdr/HALA2018072000327), Jul 19, 2018: SMOKE DETECTOR. FALSE ACTIVATION. CARGO SMOKE FWD FAILED. PERFORMED AN OPS TEST OF THE SMOKE DETECTION SYSTEM IAW FIM 26-13 TASK 801. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2018042400185](https://openairdocs.org/sdr/HALA2018042400185), Apr 23, 2018: SMOKE DETECTOR. UNKNOWN. TESTED CARGO SMOKE DETECTOR & DID NOT TEST WITH PUSH BUTTON DEPRESSED. PERFORMED CARGO SMOKE TEST IAW AMM 26-13-01. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA2017010300575](https://openairdocs.org/sdr/HALA2017010300575), Jan 3, 2017: COTTER PIN. UNSECURE. LANDING GEAR LEVER WOULD NOT MOVE TO DOWN POSITION, ON SUBSEQUENT ATTEMPTS LANDING GEAR LEVER DID NOT MOVE TO DOWN POSITION. FOUND COTTER KEY ON LANDING GEAR HA
- [SDR HALA2016040400101](https://openairdocs.org/sdr/HALA2016040400101), Apr 4, 2016: PSEU. MALFUNCTIONED. WHEN LANDING GEAR EXTENDED, INDICATORS REMAINED 3 RED. RECYCLED, THEN 3 GREEN. COMPLIED WITH OPS TEST OF LANDING GEAR POSITION INDICATOR IAW AMM 32-61-06-700-80
- [SDR HALA2016021300041](https://openairdocs.org/sdr/HALA2016021300041), Feb 13, 2016: SMOKE DETECTOR. MALFUNCTIONED. CARGO SMOKE TEST INOPERATIVE. RESET NR 1 AND NR 2 VIA'S. PERFORMED RTS. BOTH VIA'S PASSES. PERFORMED AMM CARGO SMOKE DETECTOR TESTS 26-13-01-710-801 AND 26-13-0
- [SDR HALA2015051500080](https://openairdocs.org/sdr/HALA2015051500080), May 15, 2015: BATTERY. FAILED. DURING THE REPLACEMENT OF THE DUEL CELL LIFE VEST, PN 63600-101 WITH 66601-101 SINGLE CELL VESTS IN OUR FLEET, IS WAS DISCOVERED THAT THE BATTERIES WERE SWOLLEN
- [SDR HALA2015040500057](https://openairdocs.org/sdr/HALA2015040500057), Apr 5, 2015: SMOKE DETECTOR. FALSE INDICATION. LEVEL 1, LAV SMOKE DISPLAYED ON AIR SYNOPTIC PAGE. RESET THE CIRCUIT BREAKER AND PERFORMED FIM 26-14 TASK 801. OPS CHECKED OK.
- [SDR HALA2015030100026](https://openairdocs.org/sdr/HALA2015030100026), Mar 1, 2015: COMPRESSOR. STALLED. OPEN-ATO-ENGINE RT COMPRESSOR STALL. REPAIR IN WORK.
- [SDR HALA2014101800174](https://openairdocs.org/sdr/HALA2014101800174), Oct 18, 2014: UNKNOWN. ODOR. AIR DIVERSION, ODOR OF FUMES IN COCKPIT AND CABIN. THE ACFT DIVERTED TO THE NEAREST AIRPORT, WHERE AN EVENTFUL LANDING WAS MADE. REPAIRS ARE IN WORK.
- [SDR HALA2013112600172](https://openairdocs.org/sdr/HALA2013112600172), Nov 26, 2013: WIRE. DAMAGED. RIGHT LANDING GEAR UNSAFE, INTERMITTENT THREE TIMES DURING CRUISE. FOUND RT MLG DOWNLOCK SENSOR CONDUIT KINKED NEAR R5-3732. PIN B OF BOTH P1-1152 PUSHED BACK. 
- [SDR HALA2012072500182](https://openairdocs.org/sdr/HALA2012072500182), Jul 25, 2012: CYLINDER. LEAKING. RIGHT HYD FAILED DURING FLIGHT. FILTER POP-UP INDICATOR OK. MAN SYS FILTER CLEAN-REINSTALLED. TRANSFER CYLINDER LEAKING. R & R TRANSFER CYLINDER IAW AMM 32-33-0
- [SDR HALA2012032000118](https://openairdocs.org/sdr/HALA2012032000118), Mar 20, 2012: SKIN. UNKNOWN. LIGHTING STRIKE ON RT SIDE OF FUSELAGE AT APPROX STA 614 AT LONG 27 AND LONG 26. OPEN
- [SDR HALA2012032000117](https://openairdocs.org/sdr/HALA2012032000117), Mar 20, 2012: ANTENNA. DAMAGED. LIGHTING STRIKE ON VHF NR 2 ANTENNA. REPLACED VHF NR 2 ANTENNA. PERFORMED RESISTANCE CHECK IAW SPM 20-50-01, OPS CHECKED OK MM 23-72-00, SEALED ANTENNA.
- [SDR HALA2012032000116](https://openairdocs.org/sdr/HALA2012032000116), Mar 20, 2012: SKIN. DAMAGED. LIGHTING STRIKE ON LT ELEVATOR T/E END CAP AND STATIC WICK BASE PLATE, AT APPROX LOCATION XHR 218.76. OPEN
- [SDR HALA2012030100091](https://openairdocs.org/sdr/HALA2012030100091), Mar 1, 2012: DISPLAY. MALFUNCTIONED. DURING CLIMB-OUT BOTH MCDU'S WENT TO STANDBY & LOCKED. PERFORMED MM TASK 31-43-00 RTS TEST ON NR 1 & NR 2 VIA'S. NO FAULT FOUND. TEST PASSED. OK FOR SERVICE.
- [SDR HALA2011112700541](https://openairdocs.org/sdr/HALA2011112700541), Nov 27, 2011: CHARGER. FAILED. BATTERY CHARGER FAILED IN FLIGHT. AFTER BLOCK IN STRONG BURNING ODOR IN CABIN. R & R BATTERY CHARGER IAW AMM 24-34-03. OPS CHECK TASK 24-34-03-710-801 PASSED OK
- [SDR HALA2010100500455](https://openairdocs.org/sdr/HALA2010100500455), Oct 5, 2010: SILL. DAMAGED. AFT CARGO DOOR AFT SILL SUSTAINED GROUND DAMAGE. REPAIRED SEAL IAW SRM 53-20-15-2R-4.
- [SDR HALA2010091500419](https://openairdocs.org/sdr/HALA2010091500419), Sep 15, 2010: SKIN. CRACKED. LEFT WING INBD DOOR 530 GB UPPER SURFACE CRACKED 1.5" LONG, VERIFIED WITH EDDY CURRENT. REPAIRED CRACK IAW SRM 57-00-00.
- [SDR HALA2010090800420](https://openairdocs.org/sdr/HALA2010090800420), Sep 8, 2010: DRAG ANGLE. CRACKED. CRACK ON RT SIDE DRAG ANGLE, VERIFIED BY EDDY CURRENT. REPAIR IN WORK. TRIMMED OUT CRACKED AREA IAW SRM 53-30-01-2R-1. REPAIR 1. REPAIRED IAW HAL M105 FILE NR 4
- [SDR HALA2010090700418](https://openairdocs.org/sdr/HALA2010090700418), Sep 7, 2010: STRINGER CLIP. CRACKED. 1.2500" CRACK ON CLIP AT STATION 1152, L2L. R & R CRACKED CLIP AT STA 1152 L2L. R & R CRACKED CLIP AT STA 1152, LONG 2L. PAINTED FUSE AT AREA OF R & R FASTENERS
- [SDR HALA2010030200083](https://openairdocs.org/sdr/HALA2010030200083), Mar 2, 2010: CONTROL UNIT. NO TEST. DURING ENGINE FIRE DETECTION FAULT TEST,"ENGINE RT FIRE" AURAL WARNING/ LIGHTS ARE DISPLAYED. REPLACED RT ENGINE FIRE DETECTOR CONTROL UNIT IAW AMM 26-11-01. OP

All 59: https://openairdocs.org/aircraft/N489HA/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/N489HA/stcs.md

## Related

- Other Boeing 717-200 aircraft: https://openairdocs.org/model/boeing-717-200/aircraft.md
- The Rolls-Royce Deutschland BR700-715A130 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-715a130.md

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