# N5479A: 2001 Boeing 737-83N

- Status: Valid registration
- Airframe: [Boeing 737-83N](https://openairdocs.org/model/boeing-737-83n) (registry code 13844HI, 149 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 32578
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 18, 2020
- Certificate issued: July 26, 2019
- Expires: July 31, 2029
- Mode S code: A6F581
- 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=5479A
- Page: https://openairdocs.org/aircraft/N5479A

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 737-83N)

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 N5479A.

## FAA accident and incident reports

None matched to N5479A.

## Service difficulty reports (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 SCNA20260928414](https://openairdocs.org/sdr/SCNA20260928414), Sep 28, 2026: OXYGEN MASK. DAMAGED. FOUND AFT SUPERNUMERARY SEAT PORTABLE O2 BOTTLE FACE MASK DAMAGED ( SUPERNUMERARY SEATS ) FOUND PORTABLE O2 MASK CRACKED THIS CLEARS MEL 25-31 MDDR # 141727 APP
- [SDR SCNA20260916399](https://openairdocs.org/sdr/SCNA20260916399), Aug 18, 2026: SPOILER SYS. FAULTED. 805497 GND SPOILERS DID NOT AUTO DEPLOY ON LANDING. WAS ARMED WITH GREEN LIGHT. PERFORMED FIM 27-62 TASK 804 AUTO SPEED BRAKE OPS CHECK GOOD AT THIS TIME. NO DE
- [SDR SCNA20260810342](https://openairdocs.org/sdr/SCNA20260810342), Jul 28, 2026: SKIN. CORRODED. W/O 96513 NR00050: -FUSELAGE SKIN, BS 727 - 907, S14R - S17R, CORROSION AND SCRIBE LINE. PERFORMED EA 53-0375 5479A, FUSELAGE SKIN BS 727 - 907, S14R. CORROSION
- [SDR SCNA20260811349](https://openairdocs.org/sdr/SCNA20260811349), Jul 22, 2026: SKIN. CORRODED. FUSELAGE SKIN, BS 727 TO 887, S4L - CORRODED REPAIR. PERFORMED EA 53-0313, FUSELAGE SKIN REPAIR BS 727 - 887 STR.4L REPAIRED.
- [SDR SCNA20260811345](https://openairdocs.org/sdr/SCNA20260811345), Jul 20, 2026: SKIN. DAMAGED. FUSELAGE SKIN, BS 351 TO 380, S23R TO S25R, CORROSION AND SCRIBE LINE. PERFORMED ENGINEERING TASK CARD NUMBER ENG-53SCA-11906 N5479A FUSELAGE SKIN STA 351 TO 38
- [SDR SCNA20260529218](https://openairdocs.org/sdr/SCNA20260529218), May 27, 2026: BATTERY PACK. NO TEST. FWD ENTRY AREA LH SIDE EMERGENCY LIGHT BATTERY PACK IS INOP.(OBSERVED WHILE PERFORMING FINAL CHECKS WITH ITEM 7-44). REPLACED AND TESTED FWD ENTRY AREA LH POWER
- [SDR SCNA20260810341](https://openairdocs.org/sdr/SCNA20260810341), May 20, 2026: LAP JOINT. CRACKED. EXTERNAL FUSELAGE, LAP JOINT AT STRINGER 14R, BS 727I+2, LOWER SKIN CRACKED. THIS CONDITION WAS FOUND DURING THE HFEC HOLE PROBE INSPECTION PER EO COO-EO-2026-2
- [SDR SCNA20260814360](https://openairdocs.org/sdr/SCNA20260814360), Apr 7, 2026: SKIN. CORRODED. UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT SECTION 43 FROM 
- [SDR SCNA20260811354](https://openairdocs.org/sdr/SCNA20260811354), Apr 7, 2026: SKIN. CORRODED. LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 361, STA 418, STRA 442 ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR LOWER FUSELAG
- [SDR SCNA20260811353](https://openairdocs.org/sdr/SCNA20260811353), Apr 7, 2026: SKIN. DAMAGED. LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 421 ON STR-24R SKIN WITH SCRIBE LINE. PERFORMED PERMANENT REPAIR LOWER FUSELAGE EXTERNAL SKIN S
- [SDR SCNA20260811352](https://openairdocs.org/sdr/SCNA20260811352), Apr 7, 2026: SKIN. CORRODED. LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE
- [SDR SCNA20260811348](https://openairdocs.org/sdr/SCNA20260811348), Apr 7, 2026: SKIN. CORRODED. LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. - - MRO EMP# 5323-PERFORMED PERMANENT REPAIR
- [SDR SCNA20260811347](https://openairdocs.org/sdr/SCNA20260811347), Apr 7, 2026: SKIN. DAMAGED. UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 500I + 18.375 ON STR-4L SKIN WITH SCRIBE LINES. PERFRORMED PERMANENT REPAIR AT BS 500I THRU BS 
- [SDR SCNA20260811346](https://openairdocs.org/sdr/SCNA20260811346), Apr 7, 2026: SKIN. CORRODED. UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT STA 43 FROM STA 
- [SDR SCNA20260810343](https://openairdocs.org/sdr/SCNA20260810343), Apr 7, 2026: SKIN. CORRODED. UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN BS 887 - 1016, STRINGER 4L, CORRODED. PERFORMED PERMANENT REPAIR AT EXTERNAL FUSELAGE SKIN PANEL FROM 
- [SDR SCNA20260811351](https://openairdocs.org/sdr/SCNA20260811351), Apr 4, 2026: SKIN. CORRODED. UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 727 TO STA 887 ON STR-14R SKIN WITH CORROSION AND SCRIBE LINES. PERFORMED PERMANENT REPAIR AT E
- [SDR SCNA20260811350](https://openairdocs.org/sdr/SCNA20260811350), Apr 3, 2026: SKIN. DAMAGED. UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 727C ON STR-4L SKIN WITH SCRIBE LINE. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION FROM 
- [SDR SCNA20260325136](https://openairdocs.org/sdr/SCNA20260325136), Mar 23, 2026: LENS. DAMAGED. L1 FWD ENTRY DOOR ESCAPE SLIDE COVER WITH LENS DAMAGED.
- [SDR SCNA20260325135](https://openairdocs.org/sdr/SCNA20260325135), Mar 23, 2026: RETAINER. LOOSE. L1 FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR RETAINER CLIPS HAVE THE RIVETS LOOSE.
- [SDR SCNA20260317127](https://openairdocs.org/sdr/SCNA20260317127), Mar 13, 2026: COWL DOOR. UNLATCHED. ABNORMAL ACFT VIBRATION AFTER TAKEOFF. ACFT REQUIRED SUBSTANTIAL RT AILERON TO MAINTAIN WINGS LEVEL. RETURNED TO LAL. POST FLT REVEALED NR 1 ENG COWL UNLATCHED 
- [SDR SCNA20260213081](https://openairdocs.org/sdr/SCNA20260213081), Feb 13, 2026: SLIDE. DETACHED. FOUND L1 DOOR OPEN, SLIDE RESTING ON MAINTENANCE STAND. MAIN CABIN EXIT/SLIDE L-1 DOOR SLIDE INOPERATIVE OR MISSING PROVIDED R1 OPERATES NORMALLY. REPLACED L1 E
- [SDR SCNA20260129021](https://openairdocs.org/sdr/SCNA20260129021), Jan 11, 2026: WINDOW. OVERTEMP. R3 WINDOW VERY HOT TO THE TOUCH ( ELECTRICALLY HEATED WINDSHIELDS; NO. 3 WINDOW HEAT SYSTEM(S) . REF GMM/MTI MDDR#136262 WINDOW OVERHEAT OVER REF AMM 30-41-00 R
- [SDR SCNA20251230513](https://openairdocs.org/sdr/SCNA20251230513), Dec 30, 2025: ENGINE. FIRE. AFTER ENGINE SHUTDOWN NUMBER TWO ENGINE FLARED UP OUTISDE OF PLUG, HAND HELD FIRE EXTINGUSHER WAS APPLIED TO SUPPRESS FIRE. REMOVED & REPLACED #2 ENG PER TASK C
- [SDR SCNA20251103423](https://openairdocs.org/sdr/SCNA20251103423), Oct 31, 2025: SMOKE DETECTOR. MALFUNCTIONED. SMOKE ALARM WENT OFF WHEN WE WERE ON BASE TO FINAL LAVATORY SMOKE DETECTION SYSTEMS. REPLACED LAVATORY SMOKE DETECTOR IAW AMM 26-14-01, OPS CHECK GOOD,
- [SDR SCNA20250716262](https://openairdocs.org/sdr/SCNA20250716262), Jul 15, 2025: NUT. UNDERTORQUED. DURING CLIMB OUT, OIL QUANTITY IN #2 ENGINE DECREASED TO ZERO, DID NOT MOVE FROM ZERO FOR REST OF FLIGHT, ALL OTHER INDICATIONS REMAINED NORMAL. RETORQUED ENGIN
- [SDR SCNA20250317076](https://openairdocs.org/sdr/SCNA20250317076), Mar 14, 2025: LAMP. INOPERATIVE. DEFECT 782438: RH EMERGENCY LAMP OUT. - - RESOLUTION: REMOVED AND REPLACED RH EMERGENCY LAMP IAW B737 AMM 33-51-04-960-801 OPS TEST OK AT THIS TIME.
- [SDR SCNA20250217053](https://openairdocs.org/sdr/SCNA20250217053), Feb 17, 2025: SLIDE. OUT OF POSITION. DEFECT 732333: L1 DOOR SLIDE PACKAGE OUT OF POSITION. - - RESOLUTION: (IN PROGRESS)
- [SDR SCNA20240903310](https://openairdocs.org/sdr/SCNA20240903310), Aug 31, 2024: FLAP SYSTEM. MALFUNCTIONED. DEFECT : APON APPROCH AT FLAPS 30 AND THEN FLAPS 15 AIRSPEED LOW AURAL WARNING SOUNDED UNABLE TO CONFIGURE FOR NORMAL LANDING. (EMERGENCY DECLARED) - - RESOLUTI
- [SDR SCNA20240708269](https://openairdocs.org/sdr/SCNA20240708269), Jun 30, 2024: FIRE WARNING. FALSE INDICATION. #3 BRAKE FIRE / OVERHEAT AFTER A FLAPS 15 LDG W REF 150 KTS.AND REVERSER SLOW & STIFF IN DEPLOYING. THRUST REVERSER LEVERS VERY STIFF AND SLOW IN DEPLOYING TR'S
- [SDR SCNA20240429224](https://openairdocs.org/sdr/SCNA20240429224), Apr 16, 2024: FLOORBEAM. CORRODED. AFT CARGO COMPARTMENT @STA. 772 BETWEEN RBL 21 AND LBL 21 FLOOR TEE SUPPORT WITH CORROSION. REPALCED FLOOR SUPPORT TEE.
- [SDR SCNA20240425198](https://openairdocs.org/sdr/SCNA20240425198), Apr 7, 2024: ACCESS DOOR. CORRODED. RIGHT WING, MAIN TANK ACCESS DOOR 632MB WITH CORROSION. REPLACED DOOR
- [SDR SCNA20240425201](https://openairdocs.org/sdr/SCNA20240425201), Apr 6, 2024: WEB. CRACKED. UPPER FUSELAGE MAIN CARGO CABIN AREA AT STA 540, WL 208, LBL 48 TRANSVERSAL FLOOR SUPPORT WEB WITH CRACK. REPALCED FLOOR SUPPORT WEB.
- [SDR SCNA20240425200](https://openairdocs.org/sdr/SCNA20240425200), Apr 6, 2024: WEB. CRACKED. UPPER FUSELAGE MAIN CARGO CABIN AREA AT STA 540 LBL 35 TRANSVERSAL FLOOR SUPPORT WEB WITH CRACK. REPLACED FLOOR SUPPORT WEB.
- [SDR SCNA20240425199](https://openairdocs.org/sdr/SCNA20240425199), Apr 6, 2024: WEB. CRACKED. UPPER FUSELAGE MAIN CARGO CABIN AREA AT STA 540 RBL 31 TRANSVERSAL FLOOR SUPPORT WEB WITH CRACK. REPLACED FLOOR SUPPORT WEB.
- [SDR SCNA20240429228](https://openairdocs.org/sdr/SCNA20240429228), Apr 5, 2024: ANGLE. CRACKED. LOWER FUSELAGE AFT CARGO COMPARTMENT, AT STA 867 RBL 16, VERTICAL SUPPORT LOWER ANGLE LIGHT WITH CRACK. REPLACED ANGLE PN# 149A8109U114 LOCATED AT STA. 867 RBL 
- [SDR SCNA20240429227](https://openairdocs.org/sdr/SCNA20240429227), Apr 4, 2024: SUPPORT BRACKET. CRACKED. LH WING REAR SPAR AT RSS 207 SUPPORT WITH RACK . REPLACED SUPPORT BRACKET CLIP ASSY P/N 115A5552-1 IAW B737-800 BCF SRM 51-10-02 PARA. 9 AND REFERENCE AIPC 57-5
- [SDR SCNA20240429226](https://openairdocs.org/sdr/SCNA20240429226), Apr 4, 2024: SUPPORT ANGLE. DAMAGED. UPPER FUSELAGE FWD ENTRY DOOR TORQUE TUBE ACCESS STRUCTURE WITH ELONGED HOLE. REPLACED STRUCTURE SUPPORT ANGLE
- [SDR SCNA20240429225](https://openairdocs.org/sdr/SCNA20240429225), Apr 4, 2024: TEE ANGLE. CORRODED. LOWER FUSELAGE, COMMON TO ACCESS PANEL #193AL, AFT CURVED ANGLE AND LOWER TEE ANGLE WITH CORROSION AND WEAR AT SEVERAL PLACES. REPLACED ANGLES
- [SDR SCNA20240425197](https://openairdocs.org/sdr/SCNA20240425197), Apr 2, 2024: FLOORBEAM. CORRODED. AFT CARGO COMPARTMENT AT STA 727I+10"BETWEEN RBL 12"-LBL 21"FLOOR SUPPORT TEE WITH CORROSION. REPALCED FLOOR SUPPORT TEE
- [SDR SCNA20240429230](https://openairdocs.org/sdr/SCNA20240429230), Mar 31, 2024: DOUBLER. CRACKED. LOWER FUSELAGE EXTERNAL POWER RECEPTACLE DOOR CUTOUT AREA INTERNAL DOUBLER CRACKED. REPLACED INTERNAL DOUBLER PN: 141A3722-12
- [SDR SCNA20220705075SU](https://openairdocs.org/sdr/SCNA20220705075SU), Jun 23, 2022: FLANGE. CORRODED. SUPPLEMENTAL: CORROSION AT FLOOR SUPPORT UPPER CHORD FLANGE. CAUSE OF CORROSION: MOISTURE.
- [SDR SCNA20221003116SU](https://openairdocs.org/sdr/SCNA20221003116SU), Jun 21, 2022: BATTERY PACK. INOPERATIVE. SUPPLEMENT SCNA20221003116: WORK ORDER NR-00183: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: PERFORMED INSTALLATION POWER SUPPLY BATTERY PACK FWD LH 
- [SDR SCNA20221003116](https://openairdocs.org/sdr/SCNA20221003116), Jun 21, 2022: BATTERY PACK. INOPERATIVE. DEFECT 690301: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: PERFORMED INSTALLATION POWER SUPPLY BATTERY PACK FWD LH AND RH ZONE IAW AMM TASK 33-51-06-
- [SDR SCNA20220624074](https://openairdocs.org/sdr/SCNA20220624074), Jun 21, 2022: BATTERY PACK. INOPERATIVE. WORK ODER 61170: FWD AND RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: (IN PROGRESS)
- [SDR SCNA20220634074](https://openairdocs.org/sdr/SCNA20220634074), Jun 21, 2022: BATTERY PACK. INOPERATIVE. WORK ORDER 61170: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: (IN PROGRESS)
- [SDR SCNA20220712078](https://openairdocs.org/sdr/SCNA20220712078), Jun 16, 2022: STRAP. CRACKED. DEFECT: FOUND STRAP DAMAGED UNDER EXTERNAL SKIN AT STA 1138 RH. BEHIND PANEL 343AT SLIDING SEAL (STRAP N/N REF 148A8713-8) RESOLUTION: 7/10/2022 - REMOVED AND R
- [SDR SCNA20220712077](https://openairdocs.org/sdr/SCNA20220712077), Jun 10, 2022: SKIN PANEL. CRACKED. DEFECT: EXTERNAL SKIN DAMAGE WAS FOUND TO BE DAMAGED AT STA 1138 RH BEHIND PANEL 343AT SLIDING SEAL. RESOLUTION: 7/10/2022 - ACCOMPLISHED REPAIR TO EXTERNAL SKI
- [SDR SCNA20220603067](https://openairdocs.org/sdr/SCNA20220603067), May 27, 2022: FLOOR SUPPORT. CRACKED. DEFECT: BAFFLE CRACKED AT BS500A-500B R/H SIDE. RESOLUTION: REMOVED AND REPLACED BAFFLE AT BS500A-500B R/H SIDE IN ACCORDANCE WITH B737 SRM 51-40-02-04-0 PART B
- [SDR SCNA20220705075](https://openairdocs.org/sdr/SCNA20220705075), May 23, 2022: FLOOR SUPPORT. CORRODED. DEFECT: CORROSION AT FLOOR SUPPORT STA 986.5 4IN INBD OF L2. RESOLUTION: CORROSION DAMAGE ON 986.5 FLOOR BEAM FOUND TO BE OUT OF LIMITS PER B737 SRM 53-70-51-1A
- [SDR SCNA20220712076](https://openairdocs.org/sdr/SCNA20220712076), May 20, 2022: SPAR. CRACKED. DEFECT: CORROSION. RH WING, FWD OF FWD SPAR HAS CORROSION WHERE REFUELING PANEL LATCH CONTACTS STRUCTURE, WS 372 APPROX. (MARKED). RESOLUTION: 7/09/2022 REPAIRE

## 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 N5479A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5479A before.

- [Cancelled 2014-10-27](https://openairdocs.org/deregistered/N5479A-2014-10-27): Cessna T210N, S/N 21063462, built 1979. Registration expired, pending cancellation. Owner: [Groger Richard F](https://openairdocs.org/faa-owner/GROGER%20RICHARD%20F), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco)

## Related

- Other Boeing 737-83N aircraft: https://openairdocs.org/model/boeing-737-83n/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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