# N5683A: 2001 Boeing 737-84P

- Status: Valid registration
- Airframe: [Boeing 737-84P](https://openairdocs.org/model/boeing-737-84p) (registry code 13844ZZ, 189 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 32601
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 21, 2020
- Certificate issued: July 8, 2019
- Expires: July 31, 2029
- Mode S code: A74764
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5683A
- Page: https://openairdocs.org/aircraft/N5683A

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 CFM56-7B24 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-84P)

None in force.

### Matched by engine (CFM International CFM56-7B24 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998

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

- [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021
- [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019
- [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018
- [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018
- [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018
- [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014
- [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000

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

- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations

None matched to N5683A.

## FAA accident and incident reports

None matched to N5683A.

## Service difficulty reports (26)

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 SCNA20260630273](https://openairdocs.org/sdr/SCNA20260630273), Jun 29, 2026: FAULT LIGHT. FALSE ACTIVATION. DETECTOR FAULT ILLUMINATES ON CARGO FIRE TEST. COMPLETED TEST ON SYSTEM A&B CARGO FIRE TEST. OPS CHECK GOOD. IAW AMM 26-23-00.
- [SDR SCNA20260304108](https://openairdocs.org/sdr/SCNA20260304108), Mar 3, 2026: FITTING. CRACKED. LOWER FUSELAGE, MAIN WHEEL WELL, BS 727, LBL 16 - 49, FUEL LINE FITTING CRACKED, FOUND DURING PERFORMANCE OF ITEM 1-23. REPLACED FUEL FEED LINESHROUD DRAIN AT L
- [SDR SCNA20260210067S](https://openairdocs.org/sdr/SCNA20260210067S), Feb 9, 2026: RETAINER. DAMAGED. REPLACED RETAINER GIRT BAR CLIPS P/N: 65C16820-12 (2EA) IAW B737-800 BCF SRM 51-10-02-06-0 PARAG 4 ATTACHED WITH SOLID RIVETSIAW B737-800 BCF SRM 51-40-02 PARAG
- [SDR SCNA20260210069](https://openairdocs.org/sdr/SCNA20260210069), Feb 9, 2026: COVER. DAMAGED. UPPER FUSELAGE, PASSENGER COMPARTMENT, FORWARD ENTRY DOOR SLIDE COVER WITH SHARP EDGES AND PEELING PAINT. IAW B737-84P BAC 5300-1 SECTION 11.2.2 REV K DATED 05-
- [SDR SCNA20260210068](https://openairdocs.org/sdr/SCNA20260210068), Feb 9, 2026: RETAINER. LOOSE. FWD ENTRY AREA, FWD ENTRY DOOR L1, ESCAPE SLIDE COVER FWD RETAINER CLIP WITH SOLID RIVETS LOOSE. REPLACED SOLID RIVETS IAW B737-84P SRM 51-40-02-0G-0 PARAG 4E,4
- [SDR SCNA20260210067](https://openairdocs.org/sdr/SCNA20260210067), Feb 9, 2026: RETAINER. DEFORMED. FWD ENTRY AREA, GALLEY SERVICE DOOR R1, ESCAPE SLIDE RETAINER GIRT BAR CLIPS ARE DEFORMED 2EA. (WORK IN PROGRESS)
- [SDR SCNA20260210066](https://openairdocs.org/sdr/SCNA20260210066), Feb 9, 2026: LENS. CRACKED. FWD ENTRY AREA ,GALLEY SERVICE DOOR R1, ESCAPE SLIDE COVER WITH LENS CRACKED. REPLACED FWD ENTRY AREA GALLERY SERVICE DOOR R1 ESCAPE SLIDE COVER LENS IAW B737 S
- [SDR SCNA20250217055](https://openairdocs.org/sdr/SCNA20250217055), Feb 15, 2025: WINDOW. FIRE. DEFECT 793137: @FL 300 LITTLE FIRE STARTED AT THE TP LEFT CORNER OF R1 WINDOW LED TO CRACKED WINDSHIELD, PERFORMED QRH IT MELTED ON SOME POINT, AND IT KEEPED CR
- [SDR SCNA20240903308](https://openairdocs.org/sdr/SCNA20240903308), Sep 3, 2024: WIRE. PINCHED. DURING PREFLIGHT HEARD AN ELECTRICAL POP AND SAW ELECTRICAL FLASH SOMEWHERE NEAR MASTER CAUTION AND VISOR, AFTERWARDS SMELLED ELECTRICAL BURNING FOR A MOMENT. D
- [SDR SCNA20240309087](https://openairdocs.org/sdr/SCNA20240309087), Feb 12, 2024: CHANNEL. CORRODED. EMP# 6434 AFT CARGO COMPARTMENT FROM 727 TO 847 AT RBL21 ZEE CHANNEL WITH CORROSION. EMP# 168 QC# 25 RII# QC25 REPAIRED ZEE CHANNEL FROM 727 TO STA 847 AT RBL21
- [SDR SCNA20240309079](https://openairdocs.org/sdr/SCNA20240309079), Feb 11, 2024: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE MAIN CARGO CABIN FLOOR STRUCTURE BETWEEN BS 663 TO BS 640 LH UPPER AILERON CONTROL CABLE WITH CORROSION. REPLACED UPPER FUSELAGE MAIN CARGO CABIN
- [SDR SCNA20240309077](https://openairdocs.org/sdr/SCNA20240309077), Feb 11, 2024: FLOORBEAM. CORRODED. UPPER FUSELAGE MAIN CARGO CABIN, AFT ENTRY AREA, AT STA 986.5 LBL AND RBL 43 FLOOR STRUCTURE WITH CORROSION AROUND FASTENER HOLE. PERFORMED PERMANENT REPAIR AT 
- [SDR SCNA20240309071](https://openairdocs.org/sdr/SCNA20240309071), Feb 10, 2024: STIFFENER. CRACKED. UPPER FUSELAGE MAIN CARGO CABIN FLOOR STRUCTURE AREA AT BODY STATION 540 CENTER FUEL TANK STIFFENERS WITH CRACK AT FOLLOWING POSITIONS. RBL AND LBL7, 15, 32, 41
- [SDR SCNA20240309078](https://openairdocs.org/sdr/SCNA20240309078), Feb 8, 2024: SKIN. CORRODED. LOWER FUSELAGE, BETWEEN STA 727A AND 727B AND BETWEEN STR 27LH AND 27RH, SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION FROM STA 727A 
- [SDR SCNA20240309076](https://openairdocs.org/sdr/SCNA20240309076), Feb 8, 2024: ANGLE. CRACKED. EMP# 6268 LOWER FUSELAGE MAIN WHEEL WELL RIGHT SIDE FWD BULKHEAD LOWER WEB ANGLE WITH CRACK AT RBL 24.92. EMP# 168 QC# 25 REPLACED ANGLE P/N 111A1308-9 IAW B737
- [SDR SCNA20240309075](https://openairdocs.org/sdr/SCNA20240309075), Feb 8, 2024: BULKHEAD. CRACKED. LOWER FUSELAGE MAIN WHEEL WELL LEFT SIDE FWD BULKHEAD LOWER WEB ANGLE WITH CRACK AT LBL 24.92. REPLACED ANGLE P/N 111A1308-7 IAW B737-800 SRM 51-10-02-0G-0 PAR 
- [SDR SCNA20240309074](https://openairdocs.org/sdr/SCNA20240309074), Feb 8, 2024: BULKHEAD. CRACKED. LOWER FUSELAGE MAIN WHEEL WELL LEFT SIDE FWD BULKHEAD LOWER WEB WITH CRACK AT LBL 40.00. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE MAIN WW LH SIDE FWD BULKHE
- [SDR SCNA20240309073](https://openairdocs.org/sdr/SCNA20240309073), Feb 8, 2024: PRESSURE DECK. CORRODED. LOWER FUSELAGE RIGHT MAIN WHEEL WELL PRESSURE FLOOR STRUCTURE WITH CORROSION ARROUND GROUND STUD #G310DC LOCTED AT BS 717 RBL 30. PERFORMED PERMANENT REPAIR AT 
- [SDR SCNA20240309072](https://openairdocs.org/sdr/SCNA20240309072), Feb 8, 2024: BULKHEAD WEB. CRACKED. LOWER FUSELAGE MAIN WHEEL WELL RIGHT SIDE, FWD BULKHEAD LOWER WEB WITH CRACK AT RBL 9. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE MAIN W/W R/H SIDE FWD BULKHE
- [SDR SCNA20240103003](https://openairdocs.org/sdr/SCNA20240103003), Dec 31, 2023: UNKNOWN. UNKNOWN. DEFECT 717600: L1 ESCAPE SLIDE PACK BUSTLE LOOSE. - - - RESOLUTION: INSTALLED GIRT BAR INTO RETAINING CLIPS REF AMM 25-66-01. READY FOR SERVICE.
- [SDR SCNA20230215081](https://openairdocs.org/sdr/SCNA20230215081), Feb 15, 2023: NONE. NONE. DEFECT 743511: L1 DOOR OPENED WITH SLIDE ARMED, SLIDE PACK PARTIALLY PULLED FROM COVER. RESOLUTION: REINSTALLED SLIDE AND COVER ON L1 DOOR IAW TASK 25-66-01-400
- [SDR SCNA20221017133](https://openairdocs.org/sdr/SCNA20221017133), Oct 13, 2022: NONE. NONE. DEFECT 725095: FOUND L1 DOOR GUIDE ARM MISSING HARDWARE. RESOLUTION: INSTALLED L1 DOOR GUIDE ARM HARDWARE IAW AMM 52-11-21 OPS CHECK GOOD.
- [SDR SCNA20221003118](https://openairdocs.org/sdr/SCNA20221003118), Jun 24, 2022: BATTERY PACK. INOPERATIVE. DEFECT WORK ORDER N/R-N/R-00001: FOUND R/H EMERGENCY EXIT LIGHTS INOP. RESOLUTION: REMOVED AND REPLACED THE R/H EMERGENCY LIGHTS BATTERY PACK REF. AMM 33-51-06.
- [SDR SCNA20220414031](https://openairdocs.org/sdr/SCNA20220414031), Apr 13, 2022: NONE. NONE. DEFECT: LE TRANSIT LIGHT ILLUMINATED ON APPROACH. RESOLUTION: R&R #8 IB SLAT PROX SENSOR OPS CHECK GOOD REF AMM 27-88-11 ACCOMPLISHED BITE CHECK OF FSEU NO FAUL
- [SDR SCNA20211101096](https://openairdocs.org/sdr/SCNA20211101096), Oct 29, 2021: CONNECTOR. DIRTY. DEFECT: INFLIGHT "ANTISKID INOP" LIGHT ILLUMINATED. RAN QRH PROCEDURE 14-1. RESOLUTION: PERFORMED AACU BITE REF FIM 32-42 TASK 801. FOUND FAULT VLV2, CLEANED CO
- [SDR SCNA202009085051](https://openairdocs.org/sdr/SCNA202009085051), Sep 5, 2020: AUDIO PANEL. SMOKE. NR 1 RADIO PANEL SMOKING IN FLIGHT. DIVERSION TO IFP. SOURCE OF SMOKE DETERMINED ON NR 1 ACP, NR 1 ADF SELECTOR AND INDICATOR LIGHT. REMOVED AND REPLACED NR 1 A

## STCs that may be installed (OpenAirDocs) (2)

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 engine (CFM International CFM56-7B24 series)

- [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC
- [STC SE03036CH](https://openairdocs.org/stc/SE03036CH): Application of a deep compressive stress layer using a Low Plasticity Burnishing (LPB) process on CFM56-7 Series Engines Stage 1 High Pressure Compressor (HPC) Blade Dovetails in accordance with Delta Air Lines Inc. Drawing No. 72-0396, Revision B, dated November 3, 2011, or later FAA Approved revision. Delta Air Lines Inc

## Earlier aircraft with N5683A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5683A before.

- [Cancelled 2014-10-29](https://openairdocs.org/deregistered/N5683A-2014-10-29): Cessna 172, S/N 28283, built 1956. Registration expired, pending cancellation. Owner: [Lenz Daniel](https://openairdocs.org/faa-owner/LENZ%20DANIEL), [West Orange, NJ](https://openairdocs.org/faa-place/NJ/West%20Orange)

## Related

- Other Boeing 737-84P aircraft: https://openairdocs.org/model/boeing-737-84p/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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