# N5153A: 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: 32884 - Year built: 2002 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 5, 2019 - Certificate issued: April 1, 2019 - Expires: April 30, 2029 - Mode S code: A676C4 - 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=5153A - Page: https://openairdocs.org/aircraft/N5153A 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 N5153A. ## FAA accident and incident reports None matched to N5153A. ## Service difficulty reports (31) 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 SCNA20260716307S](https://openairdocs.org/sdr/SCNA20260716307S), Jul 14, 2026: SMOKE GOGGLES. MISSING. FWD FACING SUPERNUMERARY SEATS MISSING SMOKE GOGGLES ( SUPERNUMERARY SEATS ) PLACED SMOKE GOOGLE ON EACH FWD FACING SEATS IAW AMM 25-64-00 THIS CLEARS MEL 25-31 - [SDR SCNA20260716307](https://openairdocs.org/sdr/SCNA20260716307), Jul 14, 2026: SMOKE GOGGLES. MISSING. FWD FACING SUPERNUMERARY SEATS MISSING SMOKE GOGGLES. OPEN - [SDR SCNA20260323133](https://openairdocs.org/sdr/SCNA20260323133), Mar 22, 2026: LIGHT. ARCED. PILOT SIDE (FO) MAP LIGHT ARC'D WHEN THE FOS HEADSET MADE ONCTACT. HAPPENED MORE THAN ONCE. CONCERNED ABOUT FAULTY WIRING ( WORK IN OROGRESS) - [SDR SCNA20250904355](https://openairdocs.org/sdr/SCNA20250904355), Sep 3, 2025: BULB. INOPERATIVE. INOPERATIVE BULB ON THE EMER EXIT LIGHT NOT ARMED LIGHT. RELAMPED OPS CHECK GOOD IAW AMM 33-11-00 - [SDR UIEA2025061200741](https://openairdocs.org/sdr/UIEA2025061200741), Jun 18, 2025: SKIN. SCRATCHED. LOWER LOBE, FWD CARGO DOOR EXTERNAL SKIN WITH SCRATCHES LOCATED BETWEEN BEAM D AND LOWER FRAME.(

REPLACED FWD CARGO COMPARTMENT DOOR EXTERNAL SKIN I.A.W B737- - [SDR UIEA2025061200743](https://openairdocs.org/sdr/UIEA2025061200743), Jun 18, 2025: SKIN. SCRATCHED. LOWER LOBE, AFT CARGO COMPARTMENT DOOR, EXTERNAL SKIN WITH SEVERAL SCRATCHES BETWEEN BEAM B AND LOWER FRAME.(

REPLACED AFT CARGO COMPARTMENT DOOR EXTERNAL SKI - [SDR UIEA2025061200744](https://openairdocs.org/sdr/UIEA2025061200744), Jun 18, 2025: CARGO TRACK. CRACKED. FWD CARGO COMPARTMENT, CARGO TRACK-TIE DOWN AT STA 460 RBL 13.84 WITH CRACK.(

REPAIRED TIE DOWN CARGO TRACK AT FWD CARGO COMPARTMENT RBL 13.84", SECTION BETWE - [SDR UIEA2025061200746](https://openairdocs.org/sdr/UIEA2025061200746), Jun 18, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRUCTURE AT STA 727+13" RBL3 RAIL CHANNEL WITH CORROSION.(

REPAIRED RAIL FLOOR BEAM SECTION AT AFT CARGO COMPARTMENT FLOOR STRUCT - [SDR UIEA2025061200747](https://openairdocs.org/sdr/UIEA2025061200747), Jun 18, 2025: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR STRUCTURE FROM STA 747 TO STA 847 AT LBL 21" SIDE PLATE-SUPPORT ZEE WITH CORROSION IN SEVERAL PLACES.(

REPAIRED AFT CARGO COMPARTM - [SDR UIEA2025061200748](https://openairdocs.org/sdr/UIEA2025061200748), Jun 18, 2025: SUPPORT ANGLE. CRACKED. UPPER FUSELAGE AT STA 303.9 LBL 57 WL 208.1, FWD ENTRY AREA SILL SUPPORT ANGLE WITH CRACK.(

REPAIRED FWD ENTRY DOOR LOWER SILL INNER CHORD SECTION AT B/S 303. - [SDR UIEA2025061200749](https://openairdocs.org/sdr/UIEA2025061200749), Jun 18, 2025: FRAME. UNKNOWN. PER CUSTOMER INSTRUCTIONS IN REFERENCE AT BOEING RECOMENDATION REPLACE RH FRAME FITTING AND FAIL SAFE STRAP ASSY AT STATION 663.75 PER ENGINEERING DRAWING 144A2 - [SDR UIEA2025061200750](https://openairdocs.org/sdr/UIEA2025061200750), Jun 18, 2025: FAILSAFE. DAMAGED. IN REFERECE AT COOPESA´S NRI 1-23 REPLACE LH FRAME FITTING AND FAIL SAFE STRAP ASSY AT STATION 663.75 PER ENGINEERING DRAWING 144A2400-27 FRAME INSTALLATION.(< - [SDR UIEA2025061200751](https://openairdocs.org/sdr/UIEA2025061200751), Jun 18, 2025: STRINGER. NONE. PERFORM CUTTING AND SPLICING OF STRINGER 10 L/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0061 DATED 08 MAY 25 AND BOEING - [SDR UIEA2025061200752](https://openairdocs.org/sdr/UIEA2025061200752), Jun 18, 2025: STRINGER. NONE. PERFORM CUTTING AND SPLICING OF STRINGER 14 L/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0062 DATED 08 MAY 25 AND BOEING - [SDR UIEA2025061200753](https://openairdocs.org/sdr/UIEA2025061200753), Jun 18, 2025: STRINGER. NONE. PERFORM CUTTING AND SPLICING OF STRINGER 10 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0063 DATED 08 MAY 25 AND BOEING - [SDR UIEA2025061200754](https://openairdocs.org/sdr/UIEA2025061200754), Jun 18, 2025: STRINGER. NONE. PERFORM CUTTING AND SPLICING OF STRINGER 14 R/H FOR STA 663.75 FRAME FITTING ASSEMBLY REPLACEMENT AS PER BOEING REF COO-TLS -25-0064 DATED 08 MAY 25 AND BOEING - [SDR UIEA2025061200755](https://openairdocs.org/sdr/UIEA2025061200755), Jun 18, 2025: SKIN. DENTED. ENGINE #2, INLET COWL, INNER BARREL, LOWER ACUSTICAL SKIN WITH DENTS (2 EA) AT 6 O'CLOCK POSITION. PERFORMED PERMANENT REPAIR AT ENGINE N°2 INLET COWL INNER BA - [SDR UIEA2025061200756](https://openairdocs.org/sdr/UIEA2025061200756), Jun 18, 2025: SKIN. CRACKED. LEFT WING, INBOARD L/E (FIXED L/E) SKIN CRACKED AT KRAS 217.5 AROUND FASTENER HOLE (1EA) AND AT SEAL RIB (REF: KRAS 224.82) BETWEEN THE NOSE BEAM AND FIRST STRI - [SDR UIEA2025061200757](https://openairdocs.org/sdr/UIEA2025061200757), Jun 18, 2025: SUPPORT BEAM. WORN. LOWER FUSELAGE, LOWER SUPPORT BEAM AT RBL 40.875, STA 547 LOWER CHORD WITH WEAR. REPAIRED WING CENTER SECTION LOWER SUPPORT BEAM LOWER CHORD SECTION AT RBL 40.8 - [SDR UIEA2025022700181](https://openairdocs.org/sdr/UIEA2025022700181), Feb 25, 2025: BOTTLE. LOW PRESSURE. L1 DOOR SLIDE LOW PRESSURE.(

LP 1820629 M2: REMOVED AND REPLACED L1 DOOR SLIDE IAW B737 AMM 25-66-01. INFLATION CYLINDER CHECKED PER 25-66-01, CHECKS GOOD. TH - [SDR UIEA2024123001194](https://openairdocs.org/sdr/UIEA2024123001194), Dec 30, 2024: NONE. NONE. HIT BIRDS ON TAKE OFF. HIGH SPEED REJECT AT 110 KTS(

PERFORMED HIGH ENERGY STOP CONDITIONAL INSPECTION IAW AMM 05-51-07, NO DEFECTS NOTED. PERFORMED BIRD STRI - [SDR UIEA2024092100912](https://openairdocs.org/sdr/UIEA2024092100912), Sep 21, 2024: POWER SUPPLY. INOPERATIVE. R1 DOOR EMERGENCY LIGHTING INOP(

R/R DOOR EMERGENCY LIGHT BATTERY SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD. NO FURTHER DEFECTS

) - [SDR UIEA2024061900550](https://openairdocs.org/sdr/UIEA2024061900550), Jun 19, 2024: SPRING. FAILED. ITEM 1 - AFT CARGO LIGHT ILLUMINATED DURING TAKEOFF ROLL. ITEM 2 - A/C REJECTED TAKEOFF(

ITEM 1 - TRANSFERRED TO MDDR 211037 IAW DDG 52-03-01. "M" ACTIONS C/W - [SDR UIEA2023042000373](https://openairdocs.org/sdr/UIEA2023042000373), Apr 26, 2023: UNKNOWN. UNKNOWN. LOWER FUSELAGE, AFT CARGO COMPARTMENT, AT BS 727G +18", LBL 21.5", ZEE CHANNEL WITH CRACK.(

REPAIRED SIDEPLATE SECTION AT LBL 21.5 BETWEEN BS727E+6.5" AND BS7 - [SDR UIEA2023042000374](https://openairdocs.org/sdr/UIEA2023042000374), Apr 26, 2023: UNKNOWN. UNKNOWN. LOWER FUSELAGE, FWD CARGO COMPARTMENT, AT BS 540, STGR 27L, STRINGER WITH CORROSION.(

REPAIRED FUSELAGE STRINGER 27LH BETWEEN BS500G+1.5" AND BS540 I/A/W B737 - [SDR UIEA2023042000375](https://openairdocs.org/sdr/UIEA2023042000375), Apr 26, 2023: UNKNOWN. UNKNOWN. LOWER FUSELAGE, FWD CARGO COMPARTMENT, AT BS 540, STGR 27R, STRINGER WITH CORROSION.(

REPAIRED FUSELAGE STRINGER 27RH BETWEEN BS500G+6.750" AND BS540 I/A/W B7 - [SDR UIEA2023042000376](https://openairdocs.org/sdr/UIEA2023042000376), Apr 26, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPT. STRINGER 26R BETWEEN BS 500B AND BS 500G WITH CORROSION.NOTE: WHEN PERFORMED ACCESS WITH NRI 1-126 WAS DETECTED.(

REPAIRED FUSELAGE STRINGER - [SDR UIEA2023042000377](https://openairdocs.org/sdr/UIEA2023042000377), Apr 26, 2023: UNKNOWN. UNKNOWN. FWD CARGO COMPT. STRINGER 26L BETWEEN BS 500B AND BS 500G WITH CORROSION.NOTE: WHEN PERFORMED ACCESS WITH NRI 1-127 WAS DETECTED.(

REPAIRED FUSELAGE STRINGER - [SDR UIEA2023042700389](https://openairdocs.org/sdr/UIEA2023042700389), Apr 26, 2023: ANTENNA. UNKNOWN. DURING ELT OPERATIONAL TEST WAS FOUND ELT SHOWING 3 FLASHES FAULT CODE(

PERFORMED T/S AND FOUND ELT ANTENNA DAMAGED. REPLACED AND TESTED ELT ANTENNA I/A/W B73 - [SDR Q2SA20210808453](https://openairdocs.org/sdr/Q2SA20210808453), Aug 8, 2021: PROXIMITY SENSOR. INOPERATIVE. AIRCRAFT GROUNDED. LE FLAP TRANSIT LIGHT CAME ON AT FLIGHT LEVEL 400. RAN QRH AND LIGHT WENT OUT. REMOVED AND REPLACED LE FLAP 1 PROXIMITY SENSOR IAW B737 AMM 2 - [SDR Q2SA20190702423](https://openairdocs.org/sdr/Q2SA20190702423), Jul 2, 2019: GCU. MALFUNCTIONED. AIRCRAFT GROUNDED. DURING THE "BEFORE START CHECKLIST", THE APU GEN TRIPPED OFF AND A STRONG ELECTRICAL SMELL FILLED THE COCKPIT. RESET APU GCU IAW AMM 24-21-81 ## 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 N5153A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5153A before. - [Cancelled 2012-09-10](https://openairdocs.org/deregistered/N5153A-2012-09-10): Cessna P210N, S/N P21000832, built 1983. Sale reported, pending cancellation. Owner: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - [Cancelled 1965-05-20](https://openairdocs.org/deregistered/N5153A-1965-05-20): Cessna 172, S/N 28153. Owner: [Hightower Earl](https://openairdocs.org/faa-owner/HIGHTOWER%20EARL), [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles) ## 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.