# N488HA: 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: 55001
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 24, 2008
- Certificate issued: June 28, 2011
- Expires: June 30, 2027
- Mode S code: A60701
- 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=488HA
- Page: https://openairdocs.org/aircraft/N488HA

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/N488HA/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 N488HA.

## FAA accident and incident reports

None matched to N488HA.

## Service difficulty reports (52, 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 ASAA2026100367267](https://openairdocs.org/sdr/ASAA2026100367267), Oct 3, 2026: DUCT. CONTAMINATED. STRONG DIRTY SOCK SMELL ON TAKEOFF DISSIPATED BUT LINGERED ON THROUGHOUT THE FLIGHT AND CABIN. GROUNDED - YES. INSPECTED PNEMATIC SYS & NO DEFECTS NOTED. SUSPEC
- [SDR ASAA2026100267268](https://openairdocs.org/sdr/ASAA2026100267268), Oct 2, 2026: APU. ODOR. APU DIRTY SOCK SMELL WITH APU AIR ON ( AUXILIARY POWER UNIT (APU)(NOTE MANIFOLD ISOLATION VALVE MUST BE OPERATIONAL) ). GROUNDED - YES. REMOVED AND REPLACED APU
- [SDR ASAA2026100267266](https://openairdocs.org/sdr/ASAA2026100267266), Oct 2, 2026: COALESCER BAG. ODOR. DIRTY SOCK SMELL WITH ENG ON AND PACKS ON - PLANE REFUSED. GROUNDED - YES. PER AMM 21-54-00. REMOVED & REPLACED COALESCER BAGS & PERFORMED PACK BURN W/ ENG 1 & 
- [SDR ASAA2026100167208](https://openairdocs.org/sdr/ASAA2026100167208), Oct 1, 2026: COOLING FAN. FAILED. DMI 407502, STINKY SOCK SMELL W/ APU BLEED ON. ( AUXILIARY POWER UNIT (APU)(NOTE MANIFOLD ISOLATION VALVE MUST BE OPERATIONAL) ). GROUNDED - YES. REMOVED AND RE
- [SDR ASAA2026092767163](https://openairdocs.org/sdr/ASAA2026092767163), Sep 27, 2026: COALESCER BAG. ODOR. DMI# 407496 MUSTY SMELL CAUSING WATERING EYES WITH APU RUNNING. ( AUXILIARY POWER UNIT (APU)(NOTE MANIFOLD ISOLATION VALVE MUST BE OPERATIONAL) ). GROUNDED - YE
- [SDR ASAA2026091266875](https://openairdocs.org/sdr/ASAA2026091266875), Sep 12, 2026: WARNING MESSAGE. FALSE ACTIVATION. AIR RETURN, CABIN DOOR ALERT 6500 7000, & AFTER LANDING. GROUNDED - YES. PERFORMED FIM 52-70 TASK 805. FWD CABIN DOOR SENSOR INDUCTANCE GOOD. CONFIRMED PROX SEN
- [SDR ASAA2026031163805](https://openairdocs.org/sdr/ASAA2026031163805), Mar 11, 2026: COALESCER BAG. ODOR. FUMES EVENT DURING TAKEOFF DISIPITATED DURING THRUST REDUCTION. SUSTAINED FUMES DIRTY SOCK SMELL DURING WHOLE FLIGHT BUT WAS WORSE ON TAKEOFF. UTILIZED OXY MASK
- [SDR ASAA2025110261561](https://openairdocs.org/sdr/ASAA2025110261561), Nov 2, 2025: SOCKET. FAILED. SEVERAL EMERGENCY LIGHTS INOPERATIVE AT ROW 17. GROUNDED - YES. REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT ROW 17. CONDITION SAME 5742. 11/02/2025. NS 23-
- [SDR HALA20251010051](https://openairdocs.org/sdr/HALA20251010051), Oct 9, 2025: BATTERY PACK. INOPERATIVE. CENTER EXIT SIGN INOP. REPLACED EMERGENCY BATTERY AND POWER SUPPLY PER AMM 33-51-03. OPS CHECK GOOD.
- [SDR HALA20250828047](https://openairdocs.org/sdr/HALA20250828047), Aug 27, 2025: PLACARD. DAMAGED. L EXTERIOR EMERGENCY EXIT SIGN DAMAGED. REPLACED L EXTERIOR EMERGENCY EXIT PLACARD PER AMM 11-00-00. OK FOR SERVICE.
- [SDR HALA20250818045](https://openairdocs.org/sdr/HALA20250818045), Aug 17, 2025: LANDING GEAR. MALFUNCTIONED. GEAR FREE FALL FAILED. PERFORMED AMM 32-32-01OPERATIONAL TEST OF ALTERNATE LANGING GEAR EXTENSION CONTROL MECHANISM. OPS CHECK GOOD.
- [SDR HALA20250627034](https://openairdocs.org/sdr/HALA20250627034), Jun 26, 2025: WIRE. BROKEN. FWD EMERGENCY LIGHT TOGGLE SWITCH LED WIRE SEAL BROKEN. REPLACED WIRE SEAL ON FWD EMERGENCY LIGHT TOGGLE SWITCH. SECURITY CHECK GOOD. OK FOR SERVICE.
- [SDR HALA20250121001](https://openairdocs.org/sdr/HALA20250121001), Jan 19, 2025: WHEEL. ABNORMAL. LOW SPEED REJECTED TAKEOFF. EXCESSIVE NOSEWHEEL SHIMMY. REMOVED AND REPLACED BOTH NLG WHEEL/TIRE ASSEMBLYS PER AMM 32-42-01. SPIN AND SECURITY CHECK GOOD. OK FO
- [SDR HALA20241105067](https://openairdocs.org/sdr/HALA20241105067), Nov 4, 2024: BATTERY. INOPERATIVE. EXTERIOR EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED EXT EMERG. LIGHT BATTERY PER AMM 33-51-06. OPS CHECK GOOD.
- [SDR HALA20241024059](https://openairdocs.org/sdr/HALA20241024059), Oct 23, 2024: POWER SUPPLY. INOPERATIVE. DURING OVERNIGHT CK FOUND CEILING EMERGENCY EXIT LIGHT OUT AT OVERWING EXIT. REPLACED OVERWING EMER LIGHTS POWER SIUPPLY AND BATTERY POS B5-121 IAW 33-51-03. OP
- [SDR HALA20241023057](https://openairdocs.org/sdr/HALA20241023057), Oct 22, 2024: BATTERY. INOPERATIVE. DURING OVERNIGHT CK FOUND EMERGENCY EXIT LIGHT AT AFT BULKHEAD DOOR. REPLACED AFT BULKHEAD DOOR POWER SUPPLY AND BATTERY POS B5-260, FOUND LOOSE WIRE CONNECTION
- [SDR HALA20241022056](https://openairdocs.org/sdr/HALA20241022056), Oct 21, 2024: PSEU. FAULTED. GEAR DOOR OPEN INFLIGHT. TROUBLESHOT PER FIM 32-60 TASK 802. NO FAULTS EXIST ON PSEU CURRENT FAULTS. COMPLETED "FIM 32-60 TASK 802 STEP F. WIRE CHECKS PASSED. R
- [SDR HALA2023050100022](https://openairdocs.org/sdr/HALA2023050100022), Apr 29, 2023: UNKNOWN. UNKNOWN. ATB - CABIN DOOR ALERT DISPLAYED IN FLGIHT. CLEANED MED PROXIMITY SENSOR. INTERROGATED PSEU NO CURRENT OR LAST FLIGHT FAULTS SHOWN REF AMM 32-61-01. GOOD FOR SE
- [SDR HALA2020122100223](https://openairdocs.org/sdr/HALA2020122100223), Dec 20, 2020: SHUTOFF VALVE. MALFUNCTIONED. ATB-CONTINUOUS INTERMITTENT LEVEL 1 ALERT "RUDDER POWER OFF" ON CLIMBOUT THROUGH 10K. BITE FCC 1 & 2 NO FAULTS NOTED, REF FIM 27-20 TASK 810. PERFORMED OPERATIO
- [SDR HALA2020041900092](https://openairdocs.org/sdr/HALA2020041900092), Apr 18, 2020: BATTERY PACK. DISCHARGED. LEFT AND RIGHT OVER WING FWD EMERGENCY EXIT OVERHEAD "EXIT" SIGNS INOPERATIVE. // REPLACED EMERGENCY BATTERY PACK AND POWER SUPPLY (B5-121) PER AMM 33-51-03. OP
- [SDR HALA2019111100479](https://openairdocs.org/sdr/HALA2019111100479), Nov 9, 2019: PITOT TUBE. FAILED. ATB - PITOT AUX FAIL: ILLUMINATED. // INSTALLED NEW PITOT TUBE (AUX) PER AMM 34-11-01-400-801. COMPLETED UP TO STEP F (1) (J). PENDING LEAK AND OPS CHECK. LEAK 
- [SDR HALA2019110600469](https://openairdocs.org/sdr/HALA2019110600469), Nov 5, 2019: ACTUATOR. MALFUNCTIONED. GEAR DOOR OPEN ON EAD WHILE ON APPROACH.// REMOVED AND REPLACED RH MAIN LANDING GEAR DOOR ACTUATOR PER AMM 32-34-03. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVI
- [SDR HALA2019050900240](https://openairdocs.org/sdr/HALA2019050900240), Apr 7, 2019: FAIRING. CORRODED. DURING (C) CHECK THE RT INBD HORIZONTAL STAB L/E FAIRING HAS MODERATE CORROSION AROUND FASTENER HOLES. REMOVED FAIRING FROM RT INBD HORIZONTAL STAB. VERIFIED NE
- [SDR HALA2019050900239](https://openairdocs.org/sdr/HALA2019050900239), Apr 7, 2019: PAN. DAMAGED. DURING (C) CHECK THE MED PAN WAS FOUND BENT AND GOUGED AT BAYONET CUTOUT. TRIMMED OUT DAMAGE ON OUTER PAN. INNER RADIUS TO 1.25R AND TRIMMED OUT INNER PAN DAMAG
- [SDR HALA2019050800226](https://openairdocs.org/sdr/HALA2019050800226), Apr 7, 2019: SKIN. DAMAGED. DURING C CHECK FOUND THE AFT CARGO DOOR SKIN FWD LOWER L/E HAS PULLING FASTENERS AND WAVY SKIN. VERIFIED MATERIAL FOR AFT CARGO DOOR -3 LOWER SKIN REPLACEMENT U
- [SDR HALA2019050800225](https://openairdocs.org/sdr/HALA2019050800225), Apr 7, 2019: CHANNEL. CRACKED. DURING C CHECK FOUND THE LT MLG DOOR CRACKED AT FWD Z CHANNEL, O/B SIDE. REMOVED AND REPLACED LT MLG DOOR FWD Z CHANNEL, O/B SIDE.
- [SDR HALA2019050700222](https://openairdocs.org/sdr/HALA2019050700222), Apr 7, 2019: CHANNEL. CRACKED. DURING C CHECK THE LT MLG DOOR FOUND CRACKED AT FWD Z CHANNEL I/B SIDE. REMOVED CRACKED Z CHANNEL AND PICKED UP HOLES IN NEW FWD Z CHANNEL PER DWG 5910783. INST
- [SDR HALA2019050700220](https://openairdocs.org/sdr/HALA2019050700220), Apr 7, 2019: SKIN. CORRODED. DURING C CHECK THE LT LOWER WING SKIN FOUND TO HAVE CORROSION/BULGE NEAR XW 519. REAR SPAR. SEPARATED LOWER SKIN FROM REAR SPAR LOWER CAP APPROX 14" AT STATION 
- [SDR HALA2019050700219](https://openairdocs.org/sdr/HALA2019050700219), Apr 7, 2019: PANEL. DETERIORATED. S/M PNL 370KR ANTENNA SURFACE DETERIORATED. ERODED AREAS WERE BLENDED IAW SRM 51-70-09.
- [SDR HALA2018081400372](https://openairdocs.org/sdr/HALA2018081400372), Aug 13, 2018: PITOT TUBE. FAILED. CAPTAIN`S PITOT AUX FAILED. AIR TURNBACK, REMOVED AND REPLACED AUX PITOT TUBE IAW AMM 34-11-01.
- [SDR HALA2018032100117](https://openairdocs.org/sdr/HALA2018032100117), Mar 19, 2018: UNKNOWN. ODOR. F/A REPORTED SMELLING SOMETHING BURNING THROUGHOUT CABIN AT FL200. ODOR DISSIPATED BY 170. POSSIBLY ELECTRICAL. OPS CHECKED PACKS OFF OF APU BLEED AIR. NO DEFEC
- [SDR HALA2017061300153](https://openairdocs.org/sdr/HALA2017061300153), Jun 12, 2017: WARNING LIGHT. FALSE ACTIVATION. AFTER LANDING, EMERGENCY POWER ACTIVATED FOR ABOUT 10 SECONDS, RETURNED TO NORMAL, THEN FLT REC FAIL AND VIA FAIL LIGHTS ILLUMINATED AND REMAINED ON. RESET BOTH
- [SDR HALA2016091400355](https://openairdocs.org/sdr/HALA2016091400355), Sep 14, 2016: WARNING LIGHT. FALSE ACTIVATION. AFT BULKHEAD DOOR ALERT ILLUMINATED CLIMBING THROUGH APPROX 2,000 FT. ,AFT BULKHEAD DOOR VERIFIED CLOSED NO DEFECTS NOTED. INTERMITTENT INDICATION WARNING MAY O
- [SDR HALA2016061100233](https://openairdocs.org/sdr/HALA2016061100233), Jun 11, 2016: BATTERY PACK. DISCHARGED. AFTER EMERGENCY POWER TEST WE HAVE EMERGENCY POWER TEST FAIL. GATE EXTERNAL POWER DROPPED OFF WHILE PLUGGED IN. BATTERY NEEDS CHARGING. CHARGED BATTERY EMERGENC
- [SDR HALA2016050500172](https://openairdocs.org/sdr/HALA2016050500172), May 5, 2016: CYLINDER. MALFUNCTIONED. UPON GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. CREW USED THE ALT METHOD, MANUALLY EXTENDING GEARS). ACCOMPLISHED BITE CHECK, NO FAULTS NOTED. ACFT TO 
- [SDR HALA2016050300171](https://openairdocs.org/sdr/HALA2016050300171), May 5, 2016: WARNING LIGHT. FALSE ACTIVATION. ON APPROACH, DURING GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED AND CREW USED THE ALT METHOD, MANUALLY EXTENDING GEARS. ACCOMPLISHED BITE CHECK, NO FAULT
- [SDR HALA201510310022](https://openairdocs.org/sdr/HALA201510310022), Oct 31, 2015: PITOT HEAD. OBSTRUCTED. AIR DIVERSION, 10 KT. AIRSPEED DISCREPANCY AT V1. CAPTAINS AIRSPEED MATCHED STANDBY AND F/O SIDE 10-12 KTS. LOWER. REMOVED OBSTRUCTION AND FLUSHED F/O PITOT SYS
- [SDR HALA201508160159](https://openairdocs.org/sdr/HALA201508160159), Aug 16, 2015: MOTOR. INOPERATIVE. STABILIZER TRIM DOES NOT MOVE USING CAPTAIN`S OR FIRST OFFICER`S TRIM SWITCHES. TROUBLESHOT IAW FIM 27-40, TASK 801, R & R PRIMARY TRIM DRIVE MOTOR IAW AMM 27-4
- [SDR HALA2015072400142](https://openairdocs.org/sdr/HALA2015072400142), Jul 24, 2015: MOTOR. MALFUNCTIONED. PRIMARY TRIM INOPERATIVE. R & R PRIMARY STABILIZER TRIM MOTOR IAW AMM 27-41-10-400-801.
- [SDR HALA201506290121](https://openairdocs.org/sdr/HALA201506290121), Jun 29, 2015: PUMP. LEAKING. LINE SERVICE NOTED FLUID DRIPPING FROM NR 2 ENGINE. LINE MAINTENANCE FOUND RT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. TROUBLESHOT, FOUND ENGINE HYD PUMP INOPERATI
- [SDR HALA2014091200137](https://openairdocs.org/sdr/HALA2014091200137), Sep 12, 2014: UNKNOWN. SMOKE. F/A REPORTED A SMALL AMOUNT OF SMOKE FWD DOOR AREA, FOLLOWED BY RT PACK OVERHEAT AND SHUTDOWN. INSPECTED EPC FWD AND AFT SIDE, E & E COMPARTMENT. FOUND NO SMOKE
- [SDR HALA2014022200032](https://openairdocs.org/sdr/HALA2014022200032), Feb 22, 2014: BRAKE ASSY. FAILED. NR 1 BRAKE WAS DRAGGING CAUSING OVERHEAT DURING TAXI. REPLACED NR 1 BRAKE IAW AMM 32-43-01, LEAK CHECK OPS CHECK OK. BRAKE CAME APART, AND THE PIECES WEDGED THE
- [SDR HALA2012072000178](https://openairdocs.org/sdr/HALA2012072000178), Jul 20, 2012: TIRE. DISINTEGRATED. DURING TAKEOFF AT APPROX 90 KNOTS, A RT MAIN GEAR TIRE APPEARED TO FAIL. R & R NR 3 & NR 4 MAIN TIRE IAW AMM 32-41-01. SPIN & SECURITY CHECKED OK. BOROSCOPED NR
- [SDR HALA2011080500349](https://openairdocs.org/sdr/HALA2011080500349), Aug 5, 2011: STARTER. DAMAGED. LT ENGINE NO START. FOUND STARTER NR 1 ENG WITH INTERNAL DAMAGE. R & R NR 1 ENG STARTER. OPS CK GOOD. AMM 80-11-01, SECURED COWLINGS.
- [SDR HALA2011072000328](https://openairdocs.org/sdr/HALA2011072000328), Jul 20, 2011: UNKNOWN. LEAKING. DURING T/O WATER DRIPPING FROM CEILING PANEL OVER AFT F/A SEAT. ELECTRICAL SMOKE ALSO COMING FROM CEILING PANEL. RESECURED OVERHEAD AC DUCT DRAIN HOSE. OPS CHEC
- [SDR HALA2011062700293](https://openairdocs.org/sdr/HALA2011062700293), Jun 27, 2011: SKIN. DENTED. PASSENGER MAIN ENTRANCE DOOR HAS DAMAGE (DENTED IN). JUST AFT OF FWD LOWER CORNER AND FWD OF AFT LOWER CORNER. REMOVED FWD LOWER CORNER, AFT LOWER CORNER, AND C
- [SDR HALA2011052700231](https://openairdocs.org/sdr/HALA2011052700231), May 27, 2011: WIRE. DAMAGED. AUTO TRIM FAIL - BOTH ALTERNATE TRIM CB'S POPPED (D-10 & 11). REMOVED AND REPLACED THE ALTERNATE TRIM DRIVE MOTOR IAW AMM 27-43-01. COND. SAME. FOUND WIRES E940
- [SDR HALA2010110700526](https://openairdocs.org/sdr/HALA2010110700526), Nov 7, 2010: CABLE. BROKEN. FOUND FLAP BUS TO ELEVATOR SERVO FORCE LIMITER CABLE BROKEN IN RT WHEEL WELL. FOUND TO BE FLAP INPUT TO ELEVATOR SERVO LIMITER CABLE, REMOVED & FABRICATED NEW C
- [SDR HALA2009072000313](https://openairdocs.org/sdr/HALA2009072000313), Jul 20, 2009: SKIN. DENTED. ENTRY DOOR GOT JAMMED BY JETBRIDGE CAUSING POSSIBLE DAMAGE. FOUND DOOR SKIN DENT AFT SIDE 3" X 3/4" FWD SKIN DENT 6" X 1" EDDY CURRENT CK OK NO CRACKS PRESS CK 
- [SDR HALA2009041200145](https://openairdocs.org/sdr/HALA2009041200145), Apr 12, 2009: SPOILER SYS. MALFUNCTIONED. AUTO GROUND SPOILERS FAILED TO DEPLOY ON LANDING. MANUAL DEPLOYED OKAY. PERFORMED FIM 27-60 TASK 825, NO FAULTS NOTED. RETURN-TO-SERVICE TEST PASSED. OK FOR SER

All 52: https://openairdocs.org/aircraft/N488HA/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/N488HA/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.