# N5179A: 2002 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: 32614 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 29, 2019 - Certificate issued: June 25, 2019 - Expires: June 30, 2029 - Mode S code: A67F04 - 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=5179A - Page: https://openairdocs.org/aircraft/N5179A 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 N5179A. ## FAA accident and incident reports None matched to N5179A. ## Service difficulty reports (33) 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 SCNA20260615248](https://openairdocs.org/sdr/SCNA20260615248), Jun 14, 2026: POWER SUPPLY. INOPERATIVE. GALLEY EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR AND L1 DOOR INOP. REMOVED & REPLACED GALLEY EMERGENCY EXIT SIGN POWER PACK IAW AMM 33-51-06. OPS CHECK GOOD AT THI - [SDR SCNA20251211481](https://openairdocs.org/sdr/SCNA20251211481), Dec 10, 2025: PLACARD. MISSING. FO SIDE EMERGENCY ESCAPE ROPE PLACARD MISSING. - [SDR SCNA20251211480](https://openairdocs.org/sdr/SCNA20251211480), Dec 10, 2025: PLACARD. MISSING. CA SIDE EMERGENCY ESCAPE ROPE PLACARD MISSING. INSTALLED PROPER PLACARD IAW AMM 11-32-02. - [SDR SCNA20251030419](https://openairdocs.org/sdr/SCNA20251030419), Oct 27, 2025: DOOR. NOT REPORTED. REMOVE & REINSTALL RT LOWER HP AIR DOOR. REMOVED RT LOWER HP AIR DOOR & INSTALLED NEW HP AIR DOOR WITH NEW HINGES AND LATCHES. - [SDR SCNA20251030418](https://openairdocs.org/sdr/SCNA20251030418), Oct 27, 2025: PLATE. WORN. REPLACE STRIKER PLATE (DOUBLER) ON RT PACK DOOR FWD INNER SURFACE WORN. REMOVED & REPLACED (DOUBLER) STRIKER PLATE ON RT PACK ACCESS DOOR FWD INNER SURFACE IAW - [SDR SCNA20251028413](https://openairdocs.org/sdr/SCNA20251028413), Oct 26, 2025: PLACARD. MISSING. AFT CARGO CAUTION DO NOT BLOCK SMOKE DETECTOR MISSING IN 2 AREAS. INSTALLED 2EA. CAUTION SMOKE DETECTOR DO NOT BLOCK IN AFT CARGO CEILINGS ADJACENT TO SMOKE DET - [SDR SCNA20251030417](https://openairdocs.org/sdr/SCNA20251030417), Oct 22, 2025: SUPPORT BEAM. DAMAGED. GROUND CREW FOUND HP AIR DOOR PARTIALLY HANGING. LATCH AND LANDING DAMAGED. PERFORMED PERMANENT REPAIR ON WING CENTOR SECTION LWR SUPPORT BEAM LWR CHORD AT RBL - [SDR SCNA20250808310](https://openairdocs.org/sdr/SCNA20250808310), Aug 8, 2025: FLAP SYSTEM. FAULTED. FLIGHT NUMBER 3080. DURING LAND FLAPS WERE STUCK AT 15 AND WOULD NOT RETRACT UP OR EXTEND RAN QRH PROCEDURE TRAILING EDGE FLAP DISAGREE. PERFORMED FIM 27-51 TAS - [SDR UIEA2025061200742](https://openairdocs.org/sdr/UIEA2025061200742), Jun 11, 2025: CHANNEL. CORRODED. AFT CARGO COMP RAIL-CHANNEL LBL 8.10 CORROSION NOTED BETWEEN STA 787 TO STA 767.(

REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL LBL 8.10 BETWEEN STA 787 TO - [SDR UIEA2025061200745](https://openairdocs.org/sdr/UIEA2025061200745), Jun 11, 2025: CHANNEL. CORRODED. AFT CARGO COMP RAIL-CHANNEL RBL 8.10 CORROSION NOTED BETWEEN STA 787 TO STA 767.(

REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL RBL 8.10 BETWEEN STA 787 TO - [SDR UIEA2025061300759](https://openairdocs.org/sdr/UIEA2025061300759), Jun 11, 2025: SKIN. CRACKED. RH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 120.30 +10" FROM AFT SPAR, CRACK LENGTH 1.25".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMI - [SDR UIEA2025061300760](https://openairdocs.org/sdr/UIEA2025061300760), Jun 11, 2025: SKIN. CRACKED. RH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 129.50 +34.25" FROM AFT SPAR, CRACK LENGTH 1.0".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALU - [SDR UIEA2025061300761](https://openairdocs.org/sdr/UIEA2025061300761), Jun 11, 2025: SKIN. CRACKED. LH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 120.30+10" FROM AFT SPAR, CRACK LENGTH 1.0".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINU - [SDR UIEA2025061300762](https://openairdocs.org/sdr/UIEA2025061300762), Jun 11, 2025: SKIN. CRACKED. LH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 129.50+26" FROM AFT SPAR, CRACK LENGTH 1.0".(

ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINU - [SDR UIEA2025061300763](https://openairdocs.org/sdr/UIEA2025061300763), Jun 11, 2025: CHANNEL. CORRODED. AFT CARGO COMP RAIL-CHANNEL RBL 3.00 CORROSION NOTED BETWEEN STA 787 TO STA 767.(

REMOVED CORROSION ON AFT CARGO COMP RAIL-CHANNEL RBL 3.00 BETWEEN STA 787 TO - [SDR UIEA2025061300764](https://openairdocs.org/sdr/UIEA2025061300764), Jun 11, 2025: FLOORBEAM. CORRODED. MDCC, FLOOR STRUCTURE, BS 986.5 BETWEEN LBL 24.75 TO L2 DOOR INNER CHORD WITH SURFACE CORROSION.(

PERFORMED PERMANENT REPAIR AT TRANSVERSAL FLOOR BEAM STA 986 - [SDR UIEA2025061300765](https://openairdocs.org/sdr/UIEA2025061300765), Jun 11, 2025: RIB. CRACKED. DURING VISUAL INSPECTION OF RH HORIZONTAL STABILIZER IN THE INSPAR RIB, LOWER CHORD STAB STA 92.70 WERE FOUND 2 CRACKS AT STIFFENER #2 AND STIFFENER #3.(

ACCO - [SDR UIEA2025061300766](https://openairdocs.org/sdr/UIEA2025061300766), Jun 11, 2025: RIB. CRACKED. CRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 95.96.(

REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 95.96 AND INSTALLED SAME - [SDR UIEA2025061300767](https://openairdocs.org/sdr/UIEA2025061300767), Jun 11, 2025: RIB. CRACKED. CRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 105.26.(

REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 105.26 AND INSTALLED SAM - [SDR UIEA2025061300768](https://openairdocs.org/sdr/UIEA2025061300768), Jun 11, 2025: TAIL CONE. DENTED. REF DMI #194100: PERFORM PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM SECTION.(

PERMANENT REPAIR FOR DENT FOUND ON TAIL CONE STA 1200 BOTTOM S - [SDR UIEA2025061300769](https://openairdocs.org/sdr/UIEA2025061300769), Jun 11, 2025: RIB. CRACKED. CRACK FOUND ON R/H FIXED HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 114.55.(

REMOVED R/H HORIZONTAL STABILIZER L/E RIB CHORD L/E STA 114.55 AND INSTALLED SAM - [SDR UIEA2025061300770](https://openairdocs.org/sdr/UIEA2025061300770), Jun 11, 2025: PANEL. CORRODED. COVER OF AFT BULKHEAD OF FWD CARGO COMPARTMENT, INTERNAL SQUARE WITH CORROSION ON HOLES FOR FASTENERS.(

UPON EVALUATION ON FWD CARGO AFT BULKHEAD PANEL WAS FO - [SDR UIEA2025061300771](https://openairdocs.org/sdr/UIEA2025061300771), Jun 11, 2025: BATTERY PACK. INOPERATIVE. RH SIDE EMERGENCY LIGHTS INOP.(

REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 REV 86. OPERATIONAL TEST SATISFACTORY.

) - [SDR UIEA2025021200131](https://openairdocs.org/sdr/UIEA2025021200131), Feb 12, 2025: LENS. DAMAGED. RH EXTERNAL EMERGENCY LENS & LIGHT INOP AFT OF RIGHT WING.(

EMERGENCY LIGHT L00548 DEACTIVATED ELECTRICALLY INOP REF AMM 33-51-04. THIS CLOSES MDDR 225774. PL - [SDR UIEA2024092700961](https://openairdocs.org/sdr/UIEA2024092700961), Sep 27, 2024: INDICATION SYS. FALSE INDICATION. AFT CARGO DOOR OPEN LIGHT ON TAKE OFF ROLL(

FOUND DOOR SWITCH STICKS. CLEANED AFT CARGO DOOR OPEN MECHANISM AND DOOR SWITCH TESTED PER BOEING AMM TASK 52-31-0 - [SDR UIEA2024092200914](https://openairdocs.org/sdr/UIEA2024092200914), Sep 22, 2024: PROXIMITY SENSOR. FAULTED. LE FLAP TRANSIT ILLUMINATED DURING T/O. IMMEDIATELY AT THRUST, LEVER INCREASE. DISCONTINUED TAKEOFF(

R/R LE FLAP PROXIMITY SENSOR POSITION F4 IAW B737 AMM 27- - [SDR UIEA2023122001007](https://openairdocs.org/sdr/UIEA2023122001007), Dec 20, 2023: PUMP. UNKNOWN. LEFT CENTER FUEL PUMP "LOW PRESSURE ILLUMINATED IN FLIGHT. RAN QRH ACCORDINGLY(

21DEC23 - 1699547 - ITEMS M1-M3- PDX - FOUND BOOST PUMP TANK CTR LEFT C/B TRIP - [SDR UIEA2023063000673](https://openairdocs.org/sdr/UIEA2023063000673), Aug 13, 2023: DOUBLER. UNKNOWN. LOWER FUSELAGE, EXTERNAL POWER RECEPTACLE, INNER DOUBLER WITH CRACK.(

R/R INNER DOUBLER P/N: 141A3722-12 AT EXTERNAL POWER RECEPTABLE IAW B737-800 BCF SRM 51- - [SDR UIEA2023063000674](https://openairdocs.org/sdr/UIEA2023063000674), Aug 13, 2023: UNKNOWN. UNKNOWN. LH WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT RBL 7 WITH CRACK (FOUND DURING ACCESS PROCESS TO THE W/O A1N080-7-522)(

PERFORMED PERMANENT REP - [SDR UIEA2023063000675](https://openairdocs.org/sdr/UIEA2023063000675), Aug 13, 2023: RADIO ALTIMETER. UNKNOWN. NAVIGATION - RADIO ALTIMETER SYSTEM - INSTALLATION OF COLLINS LRA-900 LOW RANGE RADIO ALTIMETERS - STC ST02002WI - AD 2021-23-12 IAW ATLAS AIR EO 3834A029 REV.0 - [SDR UIEA2023063000676](https://openairdocs.org/sdr/UIEA2023063000676), Aug 13, 2023: UNKNOWN. UNKNOWN. FUSELAGE - STRUCTURE AROUND OPENINGS - NUMBER 1 WINDOW FRAME - POST PREVENTIVE MODIFICATION INSPECTION - SB 737-53-1335 - AD 2013-19-23 AMOC IAW ATLAS AIR EO 38 - [SDR UIEA2023072800763](https://openairdocs.org/sdr/UIEA2023072800763), Aug 13, 2023: UNKNOWN. UNKNOWN. RT WING FUEL TANK STIFFENER WITH CRACK, BETWEEN RIB 21 & RIB 22 (OBSERVED WHILE PERFORMING THE 20 YEARS INSPECTION)(

PERFORMED PERMANENT REPAIR ON RH OUTBOARD - [SDR Q2SA20210224443](https://openairdocs.org/sdr/Q2SA20210224443), Feb 24, 2021: WIRE. DAMAGED. AIRCRAFT GROUNDED. SELECTED FLAPS 1 WITH NO MOVEMENT. RAN VARIOUS FLAP QRH PROCEDURES AND EVENTUALLY ENDED WITH ALL FLAPS UP LANDING QRH PROCEDURE. NO ABNORMALL ## 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 N5179A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5179A before. - [Cancelled 1957-07-11](https://openairdocs.org/deregistered/N5179A-1957-07-11): Cessna 172, S/N 28179. Exported to Canada. Owner: [Hoffmaster V D](https://openairdocs.org/faa-owner/HOFFMASTER%20V%20D), [Edinburg, TX](https://openairdocs.org/faa-place/TX/Edinburg) ## 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 --- 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.