# N17309: 2023 Boeing 737-8

- Status: Valid registration
- Airframe: [Boeing 737-8](https://openairdocs.org/model/boeing-737-8) (registry code 13844FZ, 175 seats)
- Engine: [CFM International LEAP-1B28 series](https://openairdocs.org/engine/cfm-international-leap-1b28-series) (registry code 13120)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company), [TCDS E00088EN](https://openairdocs.org/tcds/E00088EN) (CFM International S.A.) (OpenAirDocs)
- Serial number: 67563
- Year built: 2023
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 12, 2023
- Certificate issued: July 20, 2023
- Expires: July 31, 2030
- Mode S code: A126CC
- Registered owner: [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.6171° N, 111.6866° W: Placed by OpenAirDocs at the center of ZIP code 84121, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17309
- Page: https://openairdocs.org/aircraft/N17309

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 CFM International LEAP-1B28 model are included.

## ADs that may apply (OpenAirDocs): 47 in force

### Matched by airframe (Boeing 737-8)

- [AD 2026-18-07](https://openairdocs.org/ad/2026-18-07): Fuselage · Boeing 737-8, 737-9 and 737-8200. Effective Oct 22, 2026
- [AD 2026-15-11](https://openairdocs.org/ad/2026-15-11): Fuselage · Boeing 737-8, 737-9 and 737-8200. Effective Sep 10, 2026
- [AD 2026-14-11](https://openairdocs.org/ad/2026-14-11): Air Conditioning · Boeing 737-8, 737-9 and 737-8200. Effective Jul 13, 2026
- [AD 2026-13-17](https://openairdocs.org/ad/2026-13-17): Navigation · Boeing 737-8, 737-9 and 737-8200. 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 2025-25-04](https://openairdocs.org/ad/2025-25-04): Equipment/furnishings · Boeing 737-600 Series, 737-700 Series, 737-700C Series and 6 more. Effective Jan 16, 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 2024-23-11](https://openairdocs.org/ad/2024-23-11): Flight controls · Boeing 737-8, 737-9 and 737-8200. Effective Jan 6, 2025
- [AD 2024-19-06](https://openairdocs.org/ad/2024-19-06): Ice/Rain Protection System · Boeing 737-8 and 737-9. Effective Nov 26, 2024
- [AD 2024-13-02](https://openairdocs.org/ad/2024-13-02): Oxygen · Boeing 737-8, 737-9, 737-8200 and 3 more. Effective Jul 25, 2024
- [AD 2024-06-03](https://openairdocs.org/ad/2024-06-03): Electrical Power · Boeing 737-8 and 737-9. Effective May 22, 2024
- [AD 2024-03-04](https://openairdocs.org/ad/2024-03-04): Flight controls · Boeing 737-8, 737-9 and 737-8200. Effective Feb 12, 2024
- [AD 2023-15-05](https://openairdocs.org/ad/2023-15-05): Ice and Rain Protection, Powerplant · Boeing 737-8, 737-9 and 737-8200. Effective Aug 25, 2023
- [AD 2023-12-11](https://openairdocs.org/ad/2023-12-11): Navigation · Boeing 737-8, 737-9 and 737-8200. 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 2023-05-06](https://openairdocs.org/ad/2023-05-06): Fuel · Boeing 737-8, 737-9 and 737-8200. Effective May 10, 2023
- [AD 2023-04-17](https://openairdocs.org/ad/2023-04-17): Fuel · Boeing 737-600 Series, 737-700 Series, 737-700C Series and 5 more. Effective May 1, 2023
- [AD 2023-06-10](https://openairdocs.org/ad/2023-06-10): Ice and Rain Protection, Powerplant · Boeing 737-8, 737-8200 and 737-9. Effective Apr 11, 2023
- [AD 2022-24-09](https://openairdocs.org/ad/2022-24-09): Air conditioning · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 12 more. Effective Jan 26, 2023
- [AD 2022-16-09](https://openairdocs.org/ad/2022-16-09): Wings · Boeing 737-8. Effective Oct 20, 2022
- [AD 2022-06-06](https://openairdocs.org/ad/2022-06-06): Flight controls · Boeing 737-600 Series, 737-700 Series, 737-700C Series and 5 more. Effective Jun 16, 2022
- [AD 2021-13-18](https://openairdocs.org/ad/2021-13-18): Powerplant · Boeing 737-8, 737-8200 and 737-9. Effective Sep 3, 2021
- [AD 2021-16-15](https://openairdocs.org/ad/2021-16-15): Air conditioning · Boeing 737-8, 737-800 Series, 737-8200 and 2 more. Effective Aug 9, 2021
- [AD 2021-12-13](https://openairdocs.org/ad/2021-12-13): Fuel · Boeing 737-8 and 737-9. Effective Jul 29, 2021
- [AD 2021-10-07](https://openairdocs.org/ad/2021-10-07): Autoflight, Flight controls · Boeing 737-8 and 737-9. Effective Jul 8, 2021
- [AD 2021-08-04](https://openairdocs.org/ad/2021-08-04): Oxygen · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 23 more. Effective May 26, 2021
- [AD 2021-09-08](https://openairdocs.org/ad/2021-09-08): Electrical power system · Boeing 737-8 and 737-9. Effective Apr 30, 2021
- [AD 2021-01-04](https://openairdocs.org/ad/2021-01-04): Doors · Boeing 737-600 Series, 737-700 Series, 737-700C Series and 5 more. Effective Mar 29, 2021
- [AD 2020-24-02](https://openairdocs.org/ad/2020-24-02): Auto flight, Flight controls, and Indicating/recording systems · Boeing 737-8 and 737-9. Effective Nov 20, 2020
- [AD 2020-21-02](https://openairdocs.org/ad/2020-21-02): Fire protection · Airbus Canada Limited Partnership BD-500-1A10, BD-500-1A11, A330-201 and 45 more. Effective Nov 19, 2020
- [AD 2020-11-12](https://openairdocs.org/ad/2020-11-12): Nacelles/pylons · Boeing 737-8 and 737-9. Effective Jul 30, 2020
- [AD 2020-14-09](https://openairdocs.org/ad/2020-14-09): Fuel storage · Boeing 737-8 and 737-9. Effective Jul 15, 2020
- [AD 2020-03-10](https://openairdocs.org/ad/2020-03-10): Fuselage · Boeing 737-600 Series, 737-700 Series, 737-700C Series and 5 more. Effective Mar 27, 2020
- [AD 2019-18-03](https://openairdocs.org/ad/2019-18-03): Exhaust · Boeing 737-600 Series, 737-700 Series, 737-700C Series and 5 more. Effective Oct 3, 2019
- [AD 2019-14-12](https://openairdocs.org/ad/2019-14-12): Flight Controls · Boeing 737-8 and 737-9. Effective Aug 30, 2019
- [AD 2019-14-02](https://openairdocs.org/ad/2019-14-02): Hydraulic power · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 11 more. Effective Aug 27, 2019
- [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 2018-20-13](https://openairdocs.org/ad/2018-20-13): Fuel · Boeing 757-200 Series, 757-200CB Series, 757-200PF Series and 13 more. Effective Nov 15, 2018

### Matched by engine (CFM International LEAP-1B28 series)

- [AD 2025-14-08](https://openairdocs.org/ad/2025-14-08): Turbine Section · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Aug 25, 2025
- [AD 2025-04-12](https://openairdocs.org/ad/2025-04-12): Turbine Section · CFM International LEAP-1A23, LEAP-1A24, LEAP-1A24E1 and 24 more. Effective Apr 8, 2025
- [AD 2024-25-02](https://openairdocs.org/ad/2024-25-02): Turbine Engine Compressor Section · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Feb 12, 2025
- [AD 2023-07-11](https://openairdocs.org/ad/2023-07-11): Turbine Engine Compressor Section · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Jun 13, 2023
- [AD 2022-17-02](https://openairdocs.org/ad/2022-17-02): Turbine Engine Accessory Drive · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Oct 20, 2022
- [AD 2022-11-02](https://openairdocs.org/ad/2022-11-02): Turbine Engine Compressor Section, Turbine Section · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Jul 8, 2022
- [AD 2021-10-06](https://openairdocs.org/ad/2021-10-06): Engine Controls · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective May 10, 2021
- [AD 2020-06-01](https://openairdocs.org/ad/2020-06-01): Turbine/Turboprop · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Apr 16, 2020
- [AD 2018-20-01](https://openairdocs.org/ad/2018-20-01): Turbine Section · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Dec 17, 2018

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

- [AD 2026-13-05](https://openairdocs.org/ad/2026-13-05) (historical): Air conditioning · Boeing 737-8, 737-9 and 737-8200. Effective Jul 16, 2026
- [AD 2026-04-05](https://openairdocs.org/ad/2026-04-05) (historical): Electrical Power · Boeing 737-8, 737-9 and 737-8200. Effective Feb 24, 2026
- [AD 2023-09-04](https://openairdocs.org/ad/2023-09-04) (historical): Equipment/furnishings · Boeing 737-600 Series, 737-700 Series, 737-700C Series and 5 more. Effective Jun 29, 2023
- [AD 2022-03-20](https://openairdocs.org/ad/2022-03-20) (historical): Navigation · Boeing 737-8, 737-9 and 737-8200. Effective Jan 31, 2022
- [AD 2021-14-20](https://openairdocs.org/ad/2021-14-20) (historical): Cabin Altitude Pressure Switches · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 12 more. Effective Jul 20, 2021
- [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 2018-23-51](https://openairdocs.org/ad/2018-23-51) (historical): Flight controls · Boeing 737-8 and 737-9. Effective Dec 21, 2018
- [AD 2023-23-12](https://openairdocs.org/ad/2023-23-12) (historical): Turbine Section · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Jan 16, 2024
- [AD 2019-12-01](https://openairdocs.org/ad/2019-12-01) (historical): Turbine Engine Accessory Drive · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Jul 3, 2019
- [AD 2018-25-09](https://openairdocs.org/ad/2018-25-09) (historical): Engine Controls · CFM International LEAP-1B21, LEAP-1B23, LEAP-1B25 and 8 more. Effective Dec 26, 2018

## Information bulletins (advisory) (7 in force)

- [SAIB 2026-17](https://openairdocs.org/saib/2026-17): VNAV Approach Disconnect Following Missed Approach, Anomaly on Airplanes with FMC U14.0/14.1. Issued Oct 3, 2026
- [SAIB NM-20-02](https://openairdocs.org/saib/NM-20-02): Fire Protection. Issued Mar 11, 2020
- [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-18-18](https://openairdocs.org/saib/NM-18-18): Equipment/Furnishings - First Observer's Seat Cup Holder. Issued Jul 2, 2018
- [SAIB NM-17-17](https://openairdocs.org/saib/NM-17-17): Oxygen System. Issued Jun 19, 2017
- [SAIB NM-17-10](https://openairdocs.org/saib/NM-17-10): Maintenance Practices. Issued Apr 13, 2017

## NTSB investigations

None matched to N17309.

## NTSB investigations on N17309 not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DEN86FA080](https://openairdocs.org/ntsb/DEN86FA080), Feb 20, 1986: Boeing 737-300 (N17309), Denver, CO, substantial damage

## FAA accident and incident reports

None matched to N17309.

## Service difficulty reports (5)

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 CALA2025081507809](https://openairdocs.org/sdr/CALA2025081507809), Aug 15, 2025: UNKNOWN. ODOR. BAD ODOR COMING FROM AC SYSTEM. FOUND APU RUNNING AND EXTERNAL AIR HOOKED UP ON ARRIVAL. DISCONNECTED EXT AIR AND RAN BOTH PACKS. WALKED CABIN AND FLIGHT DK NOT
- [SDR CALA2025052805051](https://openairdocs.org/sdr/CALA2025052805051), May 26, 2025: WARNING MESSAGE. FALSE INDICATION. ANTI-ICE MASTER CAUTION DURING TAKEOFF ROLL DEBRIEFED CREW. ON TAKEOFF ROLL AT 80 KT RECEIVED ANTI ICE MASTER CAUTION MOMENTARILY. NOTED NO FAULTS ON MASTER CAU
- [SDR CALA2025043004340](https://openairdocs.org/sdr/CALA2025043004340), Apr 27, 2025: DOOR. NONE. BATHROOM DOOR 2R JAMMED. FOUND LAV E OPENING AND CLOSING NORMAL. ALSO CHECKED LAV D AND A DOORS. ALL OPERATING NORMAL. FOUND LAV E OPENING AND CLOSING NORMAL. A
- [SDR CALA2025031402839](https://openairdocs.org/sdr/CALA2025031402839), Mar 14, 2025: NONE. NONE. PRESS GAUGE ON 2L/2R ARE BORDERLINE INSPECTED DOOR SLIDE PRESSURES. BOTH ARE WITHIN LIMITS REF. AMM 25-66-01.
- [SDR CALA2024071700230](https://openairdocs.org/sdr/CALA2024071700230), Jul 12, 2024: WINDSHIELD. CRACKED. POSSIBLE CRACK ON R1 LOWER SIDE REMOVED R2 WINDSHIELD IAW AMM 56-11-11. AND INSTALLED R2 WINDSHIELD UP TO STEPS 8-B IAW AMM 56-11-11. STEPS 9 THRU CLOSE UP NEED

## Service difficulty reports on N17309 not matched to an aircraft (44)

They name N17309, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR CALA0500056](https://openairdocs.org/sdr/CALA0500056), Feb 23, 2005: CHANNEL. CRACKED. INSPECTION FOUND A 10 INCH CRACK IN STIFFENER CHANNEL IN FORWARD CARGO BAY AT VOR ANTENNA, STA 500 BETWEEN S28L AND S28R. THE CHANNEL WAS REMOVED AND REPLACED I
- [SDR CALA0500052](https://openairdocs.org/sdr/CALA0500052), Feb 22, 2005: SHEAR TIE. CORRODED. INSPECTION FOUND SKIN CLIP CORRODED AT STA 500, RBL 2 IN FORWARD BAGGAGE BIN FLOOR AREA. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07 FIGURE 207.
- [SDR CALA0500048](https://openairdocs.org/sdr/CALA0500048), Feb 20, 2005: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L CORRODED AT RIVET HOLES BETWEEN STA 500 AND 500B. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 
- [SDR CALA0500047](https://openairdocs.org/sdr/CALA0500047), Feb 20, 2005: FRAME. CORRODED. INSPECTION FOUND STA 500 FRAME CORRODED AT SKIN ATTACH POINT BETWEEN S27R AND S28R, RBL 11-RBL 16. A FRAME REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 203.
- [SDR CALA0300568](https://openairdocs.org/sdr/CALA0300568), Sep 29, 2003: WIRE. BROKEN. INSPECTION FOUND EMERGENCY AISLE LIGHTS AT ROW S 12-20 INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT STA 378 EMERGENCY LIGHT BATTERY PACK. THE BROKEN WIRE WAS
- [SDR CALA0300560](https://openairdocs.org/sdr/CALA0300560), Sep 26, 2003: BATTERY PACK. INOPERATIVE. THE INTERIOR EMERGENCY AISLE LIGHTS AT ROWS 14R, 16L, 19L, 21R, AND 23L WERE FOUND INOPERATIVE. REPLACED BATTERY PACKS AT M1135 AND M1136 POWER SUPPLIES IAW MM 
- [SDR CALA0300371](https://openairdocs.org/sdr/CALA0300371), Jul 8, 2003: PRESSURE PANEL. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN PRESSURE DECK AT STA 665, RBL 35, JUST O/B OF J-BOX IN RT WHEEL WELL CEILING. THE PRESSURE DECK WAS REPAIRED IAW SRM 53-60-51
- [SDR CALA0300335](https://openairdocs.org/sdr/CALA0300335), Jun 25, 2003: UPLOCK. INOPERATIVE. THE RT MLG FAILED TO EXTEND ON FIRST ATTEMPT WHILE ON APPROACH TO IAH. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE RT MLG RED WARNING LIGHT. A TOWER FLY-
- [SDR CALA0300077](https://openairdocs.org/sdr/CALA0300077), Feb 28, 2003: BEAM. CORRODED. INSPECTION FOUND ALL TORQUE BOX MOUNTING HOLES ELONGATED ON L-2 DOOR. REPAIRED IAW ECRA 5210-01658.
- [SDR CALA0300070](https://openairdocs.org/sdr/CALA0300070), Feb 26, 2003: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN L-2 DOOR AT WEB OPENING ON INTERIOR SKIN ABOVE INSTALLED TORQUE TUBE. INSTALLED REPAIR IAW ECRA 5210-01653.
- [SDR CALA0300099](https://openairdocs.org/sdr/CALA0300099), Feb 23, 2003: STRAP. CORRODED. INSPECTION FOUND R/H FLOOR SUPPORT STRAP CORRODED AT STA 793. THE FLOOR SUPPORT STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300067](https://openairdocs.org/sdr/CALA0300067), Feb 23, 2003: WEB. CORRODED. INSPECTION FOUND THE FORWARD I/B CORNER OF WEB CORRODED AT AFT CARGO DOOR LOWER THRESHOLD. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 53-60-
- [SDR CALA0300066](https://openairdocs.org/sdr/CALA0300066), Feb 23, 2003: STRAP. CORRODED. INSPECTION FOUND STRAP CORRODED UDER VERTICAL WEB AT STA 780-800, RBL 20. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300065](https://openairdocs.org/sdr/CALA0300065), Feb 23, 2003: STRAP. CORRODED. INSPECTION FOUND CORROSION ON AFT LOWER STRAP ON BOTTOM SIDE OF VERTICAL WEB UPPER FLANGE AT STA 840-853, RBL 19. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-
- [SDR CALA0300064](https://openairdocs.org/sdr/CALA0300064), Feb 23, 2003: WEB. CORRODED. INSPECTION FOUND VERTICAL WEB CORRODED IN AFT BAGGAGE BIN AT STA 791-800, RBL 20. A NEW WEB WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA0300063](https://openairdocs.org/sdr/CALA0300063), Feb 22, 2003: FRAME. CORRODED. INSPECTION FOUND BELTFRAME CORRODED AT STA 793. THE CORRODED AREA WAS REMOVED AND A TYPICAL FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11.
- [SDR CALA0300058](https://openairdocs.org/sdr/CALA0300058), Feb 19, 2003: SEAT TRACK. CORRODED. INSPECTION FOUND L/H O/B SEAT TRACK AT BS 907-947.5 CORRODED. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-52, F
- [SDR CALA0300051](https://openairdocs.org/sdr/CALA0300051), Feb 17, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R AND 29L CORRODED AT STA 323 AT FORWARD SIDE OF E&E DOOR JAMB. THE STRINGER SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300098](https://openairdocs.org/sdr/CALA0300098), Feb 16, 2003: PAN. CORRODED. INSPECTION FOUND LAV FLOOR PAN FASTENER CORRODED AT STA 1016, RBL 13. A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-20-02.
- [SDR CALA0300050](https://openairdocs.org/sdr/CALA0300050), Feb 16, 2003: STRAP. CORRODED. INSPECTION FOUND H-STRAP CORRODED AT STA 1006, BL 0. THE H-STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300049](https://openairdocs.org/sdr/CALA0300049), Feb 15, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, BL 0 TO LBL 18. THE UPPER CHORD OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851, REV. B.
- [SDR CALA0300097](https://openairdocs.org/sdr/CALA0300097), Feb 14, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 344 BETWEEN LBL 36 AND RBL 12. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-5
- [SDR CALA0300034](https://openairdocs.org/sdr/CALA0300034), Feb 10, 2003: GALLEY TRACK. CORRODED. INSPECTION FOUND GALLEY FLOOR TRACK CORRODED BETWEEN BS 277 - 294 AT RBL 36. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300031](https://openairdocs.org/sdr/CALA0300031), Feb 10, 2003: STIFFENER. CORRODED. INSPECTION FOUND STIFFENER CORRODED AT LEFT SIDE AND RIGHT SIDE OF BL0 BELOW FLOOR LINE AT STA 1016. REPAIRED IAW EA 5310-04045, POS 2.
- [SDR CALA0300029](https://openairdocs.org/sdr/CALA0300029), Feb 10, 2003: SKIN. GOUGED. INSPECTION FOUND THE R/H UPPER FUSELAGE SKIN GOUGED BELOW FORWARD R/H SIDE DORSAL FIN MOUNT POINT AT STA 880, STRINGER 2R. A DOUBLER REPAIR WAS INSTALLED IAW SR
- [SDR CALA0300001](https://openairdocs.org/sdr/CALA0300001), Jan 1, 2003: SKIN. CRACKED. INSPECTION FOUND A 1.5" CRACK IN R/H FUSELAGE SKIN AFT OF TRAILING EDGE OF FLAP, BS 727E, S18R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01 AND ECRA 5330-03191.
- [SDR CALA0101019](https://openairdocs.org/sdr/CALA0101019), Dec 4, 2001: SKIN. CRACKED. INSPECTION FOUND A 1/4" CRACK AT LOWER HINGE OF R-1 DOOR EXTERIOR SKIN. A REPAIR WAS INSTALLED IAW ECRA 5210-01458.
- [SDR CALA0101017](https://openairdocs.org/sdr/CALA0101017), Nov 30, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND CABIN L/H O/B SEAT TRACK CORRODED AT STA 887-907. REPAIRED SEAT TRACK IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA0101016](https://openairdocs.org/sdr/CALA0101016), Nov 28, 2001: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 1006 BETWEEN S16R AND S15R. A FRAME REPAIR SECTION AND SPLICES WERE INSTALLED IAW SRM 53-00-07, FIGURE 201.
- [SDR CALA0101013](https://openairdocs.org/sdr/CALA0101013), Nov 27, 2001: SKIN. CRACKED. INSPECTION FOUND A 1/2" CRACK IN #1 PYLON SKIN PANEL #5727L. REPAIRED IAW ECRA 5430-01230.
- [SDR CALA0101009](https://openairdocs.org/sdr/CALA0101009), Nov 23, 2001: BRACKET. CRACKED. INSPECTION FOUND A 1/4" CRACK IN R/H WING #6 FLAP TRACK FAIRING I/B SUPPORT BRACKET. A NEW BRACKET WAS INSTALLED IAW MM 51-10-02.
- [SDR CALA9901256](https://openairdocs.org/sdr/CALA9901256), Sep 18, 1999: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FORWARD LOWER FUSELAGE SKIN AT BS 373 AT GROUND BLOWER EXHAUST. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED
- [SDR CALA9900499](https://openairdocs.org/sdr/CALA9900499), May 7, 1999: STRINGER. CORRODED. STRINGER 26L IS CORRODED FROM STA 500 TO 500D ALONG WITH STRINGER ATTACH CLIP AT STA 500D FORWARD CARGO PIT. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-00-03
- [SDR CALA9900468](https://openairdocs.org/sdr/CALA9900468), May 3, 1999: SKIN. CRACKED. FUSELAGE SKIN CRACKED UPPER LEFT CORNER OF CAPTAINS WINDSHIELD 1/2 TO RIVET. CONFIRMED WITH HFEC. REPAIRED PER EC/RA 5330-02802.
- [SDR CALA9900460](https://openairdocs.org/sdr/CALA9900460), Apr 30, 1999: FLOORBEAM. CRACKED. HOU - FLOORBEAM WEB CRACKED .35 INCH AT STATION 328 LBL 1. INSTALLED REPAIR PER EC/RA 5310-03847. (M)
- [SDR CALA9900445](https://openairdocs.org/sdr/CALA9900445), Apr 26, 1999: SEAT TRACK. CORRODED. CABIN RIGHT O/B SEEAT TRACK HEAVY CORROSION AT STA 907 - 917. REMOVED CABIN SEAT TRACK AT STA 907 TO END OF TRACK PER SRM 53-00-52.
- [SDR CALA9900440](https://openairdocs.org/sdr/CALA9900440), Apr 23, 1999: SEAT TRACK. CORRODED. CABIN RIGHT SIDE INBOARD SEAT TRACK HEAVY CORROSION BS 907 - BS 930. SPLICED IN NEW SEAT TRACK SECTION AT STA 827 - 947 PER SRM 5300-00-52 FIG 204.
- [SDR CALA9900424](https://openairdocs.org/sdr/CALA9900424), Apr 19, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 344, BL 0 TO LBL 15. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-51, FIGURE 20
- [SDR CALA9802189](https://openairdocs.org/sdr/CALA9802189), Dec 21, 1998: SWITCH. INOPERATIVE. THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING AT PBI. THE GEAR WAS CYCLED, BUT THE RED LIGHT DID NOT EXTINGUISH. A MANU
- [SDR CALA9801964](https://openairdocs.org/sdr/CALA9801964), Oct 16, 1998: POWER SUPPLY. INOPERATIVE. AFT 4 SEATS AND AFT 3 LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY IN AFT CEILING, STA 920 PER MM 33-51-51.
- [SDR CALA9700318](https://openairdocs.org/sdr/CALA9700318), Mar 11, 1997: HYD LINE. LEAKING. THE HYDRAULIC B NR 1 ELECTRIC LOW PRESSURE LIGHT CAME ON FOLLOWED BY NR 2 ENGINE LOW PRESSURE AND HYDRAULIC B QUANTITY DROPPED TO ZERO. THE A/C WAS RETURNED TO 
- [SDR CALA9601257](https://openairdocs.org/sdr/CALA9601257), Sep 2, 1996: HYD LINE. BROKEN. THE B-SYSTEM LOW PRESSURE LIGHT FOR NR 2 ENGINE HYDRAULIC PUMP ILLUMINATED FOLLOWED BY B-SYSTEM HYDRAULIC QUANTITY DROP TO 0.5 GALLONS WHILE APPROACHING CLE. TH
- [SDR CAL950407](https://openairdocs.org/sdr/CAL950407), May 19, 1995: HYD LINE. LEAKING. FLT NR 0419 - CLE - THE 'A' SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE IN FLIGHT. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 ENGINE DRIVEN HYDRAUL
- [SDR CAL950044](https://openairdocs.org/sdr/CAL950044), Jan 17, 1995: CIRCUIT BREAKER. FAILED. CLE - FLT 1835 - THE ACFT EXPERIENCED AN ELECTRICAL FAILURE WHILE EN ROUTE TO MDW. THE APU WAS STARTED, BUT IT WOULD ONLY POWER THE LT SIDE. THE TRANSFER BUS OF

## STCs that may be installed (OpenAirDocs) (166, 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 737-8)

- [STC ST03438NY](https://openairdocs.org/stc/ST03438NY): Installation of Adams Rite Lavatory Equipment. Delta Engineering Corporation
- [STC ST12515IB](https://openairdocs.org/stc/ST12515IB): Potable Water System Tank Usable Volume Change, from 40 U.S. gallon to 60 U.S. gallon capacity. Boeing Brasil Serviços Técnicos Aeronáuticos
- [STC ST04669CH](https://openairdocs.org/stc/ST04669CH): Installation of Honeywell Advanced Communications and Entertainment System (ACES). Honeywell Aerospace
- [STC ST09941AC](https://openairdocs.org/stc/ST09941AC): Installation of a Gables SATVOICE Annunciator Panel. L2 Aviation
- [STC ST02269NY](https://openairdocs.org/stc/ST02269NY): Installation of Self Illuminating Floor Path Marking System. Lufthansa Technik AG
- [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 ST12445IB](https://openairdocs.org/stc/ST12445IB): nstallation of ACRO Series 6 ‘X’ passenger seats in 189Y seating configuration i. Eirtech Aviation Services Limited
- [STC ST12443LA](https://openairdocs.org/stc/ST12443LA): Installation of Teledyne Controls Edge Computing Platform (ECP). Teledyne Controls, LLC
- [STC ST12437IB](https://openairdocs.org/stc/ST12437IB): Installation of a new VIP cabin interior for 19 passengers and two required Cabin Crew for private operation. AMAC Aerospace Switzerland AG
- [STC ST04474NY](https://openairdocs.org/stc/ST04474NY): Activation of Wireless Local Area Network (WLAN) system. Jet Aviation AG
- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST04281NY](https://openairdocs.org/stc/ST04281NY): Replacement of Aft Lavatories. B/E Aerospace Limited
- [STC ST09927AC](https://openairdocs.org/stc/ST09927AC): Installation of a Gables Audio Management System. L2 Aviation
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST12005SE](https://openairdocs.org/stc/ST12005SE): Installation of Starlink Aviation System. Space Exploration Technologies Corp./Starlink Aviation
- [STC ST04040CH](https://openairdocs.org/stc/ST04040CH): Activation of Smart Runway and Smart Landing (SRSL) Runway Awareness Advisory System (RAAS) Functions for Honeywell Mark V and Mark V-A Enhanced Ground Proximity Warning Systems (EGPWS). Honeywell International Inc
- [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series
- [STC ST04363AT](https://openairdocs.org/stc/ST04363AT): Interior reconfiguration installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04393AT](https://openairdocs.org/stc/ST04393AT): Interior Reconfiguration installation. 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 ST04667CH](https://openairdocs.org/stc/ST04667CH): Installation of Southwest Airlines Interior Reconfiguration for Extended Leg Room (ELR) Cabin. Astronics Connectivity Systems and Certification Corp
- [STC ST03738NY](https://openairdocs.org/stc/ST03738NY): Modification of the ALOFT AeroArchitects Auxiliary Fuel System. ALOFT AeroArchitects
- [STC ST03735NY](https://openairdocs.org/stc/ST03735NY): Installation of a ViaSat KA SATCOM Antenna System. ALOFT AeroArchitects
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST04593CH](https://openairdocs.org/stc/ST04593CH): Installation of Astronics EmPower In-Seat Power System. Astronics Connectivity Systems and Certification Corp
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc
- [STC ST03405NY](https://openairdocs.org/stc/ST03405NY): Installation (with demod option) of an Connectivity Antenna. Delta Engineering Corporation
- [STC ST09848DS](https://openairdocs.org/stc/ST09848DS): Guam Interim 14F Configuration. United Airlines
- [STC ST04758NY](https://openairdocs.org/stc/ST04758NY): Installation of single cockpit USB charger. Eirtech Aviation Services Inc
- [STC ST09844DS](https://openairdocs.org/stc/ST09844DS): This project installs a new Next-IS media server and installation provisions to interface with the Starlink IFC system. United Airlines
- [STC ST04380AT](https://openairdocs.org/stc/ST04380AT): Installation of Row 44 Broadband Antenna provisions on a Boeing 737-8 aircraft. Anuvu IFC Corporation
- [STC ST12279IB](https://openairdocs.org/stc/ST12279IB): Installation of B737-8 MAX Printer, In-Seat Power supply (ISPS), and Power Outlets. Elisen & associés Inc
- [STC ST04052NY](https://openairdocs.org/stc/ST04052NY): ViaSat KA Cabin Distribution System Installation. ALOFT AeroArchitects
- [STC ST03218CH](https://openairdocs.org/stc/ST03218CH): Modify aircraft interior to match standard passenger cofigurations, IAW Global Onboard Partners MDL # 252013-737-MDL-02, Rev. N, dtd 1/4/22 or later FAA approved revisions. Atin OOH LLC
- [STC ST02908NY](https://openairdocs.org/stc/ST02908NY): Installation of a Panasonic Avionics Corporation Global Communications Suite (GCS) and/or In-Flight Entertainment (IFE). Delta Engineering Corporation
- [STC ST01143LA](https://openairdocs.org/stc/ST01143LA): Installation of Aerocon Engineering Company (AEC) Airstar. Aircraft Technical Development Inc. dba Aerocon Engineering Company
- [STC ST04381AT](https://openairdocs.org/stc/ST04381AT): Activation of the Row 44 Broadband System on a Boeing 737-8 aircraft. Anuvu IFC Corporation
- [STC ST11087SC](https://openairdocs.org/stc/ST11087SC): Installation of Heads-Up Technologies Pre,Recorded Announcement Machine (PRAM). American Airlines, Inc., M&E Engineering Division
- [STC ST04051NY](https://openairdocs.org/stc/ST04051NY): ViaSat KA SATCOM Antenna System Installation. ALOFT AeroArchitects
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12136AT](https://openairdocs.org/stc/ST12136AT): Installation of Cabin Interior Reconfiguration. Delta Flight Products (DFP)
- [STC ST12102IB](https://openairdocs.org/stc/ST12102IB): Installation of a Honeywell Aspire 400 SBB Satcom and/or an AMT-3800 high gain antenna. Jet Aviation AG
- [STC ST12059IB](https://openairdocs.org/stc/ST12059IB): Installation of Seat to Floor Interface - isotropic intercostals for installation of seats and divans. JET AVIATION AG
- [STC ST12056IB](https://openairdocs.org/stc/ST12056IB): The Manufacture and Installation of External Printed Aircraft Graphics Film. Libellule Monde Inc
- [STC ST11915IB](https://openairdocs.org/stc/ST11915IB): Installation of the AFIRS (Automated Flight Information Reporting System) Edge system. FLYHT Aerospace Solutions Ltd
- [STC ST04261NY](https://openairdocs.org/stc/ST04261NY): Installation of an Executive Interior. ALOFT AeroArchitects
- [STC ST04368AT](https://openairdocs.org/stc/ST04368AT): Installation of a Rockwell Collins CMU-900 ACARS/CPDLC Communication Management Unit P/N 822-1239-151 to provide Data Link communications via existing data link capable VHF Mode 2 (VDLM2), HF and/or SATCOM systems and host the CPDLC application which support EASA Link 2000+ communications. LB Aircraft Engineering Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH

All 166: https://openairdocs.org/aircraft/N17309/stcs.md

## Earlier aircraft with N17309

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N17309 before.

- [Cancelled 1940-08-09](https://openairdocs.org/deregistered/N17309-1940-08-09): Lockheed 12A, S/N 1209. Exported to Canada. Owner: [Charles H Babb Company](https://openairdocs.org/faa-owner/CHARLES%20H%20BABB%20COMPANY), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)

## Related

- Other Boeing 737-8 aircraft: https://openairdocs.org/model/boeing-737-8/aircraft.md
- The CFM International LEAP-1B28 series engine: https://openairdocs.org/engine/cfm-international-leap-1b28-series.md

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