# N5147A: 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: 32882
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 7, 2019
- Certificate issued: August 15, 2025
- Expires: August 31, 2032
- Mode S code: A67399
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Slat Lake City, UT](https://openairdocs.org/faa-place/UT/Slat%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=5147A
- Page: https://openairdocs.org/aircraft/N5147A

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 N5147A.

## FAA accident and incident reports

None matched to N5147A.

## Service difficulty reports (29)

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 SCNA20260623256](https://openairdocs.org/sdr/SCNA20260623256), Jun 20, 2026: SMOKE GOGGLES. BROKEN. CAPTAINS SMOKE GOGGLES BROKEN INSTALLED NEW SMOKE GOGGLES PER AMM 25-64-00
- [SDR SCNA20260623262](https://openairdocs.org/sdr/SCNA20260623262), Jun 8, 2026: SMOKE GOGGLES. MISSING. SMOKE GOGGLES MISSING FROM FWD FLT ATTENDENT SEAT I/B & O/B POS ( SUPERNUMERARY SEATS ) INSTALLED 2 MISSING SMOKE GOGGLES IN THE AFT FACING SEAT REFERENCING AMM
- [SDR SCNA20251230512](https://openairdocs.org/sdr/SCNA20251230512), Dec 29, 2025: SCREW. MISSING. L1 SLIDE COVER MISSING SCREW. INSTALLED SCREW ON L1 SLIDE IAW AMM 25-66-01
- [SDR UIEA2025030400197](https://openairdocs.org/sdr/UIEA2025030400197), Mar 4, 2025: CARGO TRACK. CORRODED. FORWARD CARGO COMPARTMENT - FLOOR STRUCTURE STA 500H TO STA 500I LBL17" CARGO TRACK CORRODED AROUND ANCHOR NUTS.(<P>PERFORMED PERMANENT REPAIR AT TIEDOWN TRACK 
- [SDR UIEA2025030400196](https://openairdocs.org/sdr/UIEA2025030400196), Mar 4, 2025: CARGO TRACK. CORRODED. FWD CARGO COMPARTMENT FROM STA 400 TO STA 460 LBL 18.2" TIE DOWN TRACK WITH CORROSION.(<P>PERFORMED PERMANENT REPAIR AT TIEDOWN TRACK SECTION FROM STA 360 TO ST
- [SDR UIEA2025030400195](https://openairdocs.org/sdr/UIEA2025030400195), Mar 4, 2025: CHANNEL. CORRODED. FWD CARGO COMPARTMENT FROM STA 420 TO STA 500D LBL 24" ZEE CHANNEL WITH CORROSION INCLUDING SPLICE AREA AND AROUND ANCHOR NUTS.(<P>PERFORMED PERMANENT REPAIR AT
- [SDR UIEA2025030400194](https://openairdocs.org/sdr/UIEA2025030400194), Mar 4, 2025: STRINGER. CORRODED. FWD CARGO COMPARTMENT FROM STA 500C+5" TO STA 500F STRINGER 28LH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(<P>PERFORMED PERMANENT REPAIR AT STRINGER 28LH 
- [SDR UIEA2025030400193](https://openairdocs.org/sdr/UIEA2025030400193), Mar 4, 2025: STRINGER. CORRODED. FWD CARGO COMPARTMENT FROM STA 500+12" AND FROM STA 500C + 12" TO STA 500F STRINGER 26LH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(<P>PERFORMED PERMANENT 
- [SDR UIEA2025030400192](https://openairdocs.org/sdr/UIEA2025030400192), Mar 4, 2025: FLOOR SUPPORT. CORRODED. FWD CARGO COMPARTMENT STA 495 LBL 8.10" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS.(<P>PERFORMED PERMANENT REPAIR AT FLOOR SUPPORT CHANNEL ON FWD CARGO 
- [SDR UIEA2025030400191](https://openairdocs.org/sdr/UIEA2025030400191), Mar 4, 2025: FLOOR SUPPORT. CORRODED. FWD CARGO COMPARTMENT STA 495 RBL 8.10" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS.(<P>PERFORMED PERMANENT FLOOR SUPPORT CHANNEL REPAIR AT FWD CARGO COM
- [SDR UIEA2025030400190](https://openairdocs.org/sdr/UIEA2025030400190), Mar 4, 2025: CARGO TRACK. CORRODED. FORWARD CARGO COMPARTMENT - FLOOR STRUCTURE FROM STA 460 TO STA 500 AND STA 500H TO STA 500I RBL13" CARGO TRACK CORRODED AROUND ANCHOR NUTS.(<P>PERFORMED PERMAN
- [SDR UIEA2025030400189](https://openairdocs.org/sdr/UIEA2025030400189), Mar 4, 2025: STRINGER. CORRODED. FWD CARGO COMPARTMENT FROM STA 500B+12" TO STA 500C+13" AND FROM STA 500D TO STA 500F STRINGER 27LH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(<P>PERFORMED
- [SDR UIEA2025030400188](https://openairdocs.org/sdr/UIEA2025030400188), Mar 4, 2025: STRINGER. CORRODED. FWD CARGO COMPARTMENT AT STA 500D+2", STA 500D+18" AND BETWEEN STA 500E-STA 500G STRINGER 26RH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(<P>PERFORMED PERM
- [SDR UIEA2025030400187](https://openairdocs.org/sdr/UIEA2025030400187), Mar 4, 2025: STRINGER. CORRODED. FWD CARGO COMPARTMENT FROM STA 500B+10" TO STA 500E+16" STRINGER 27RH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(<P>PERFORMED PERMANENT REPAIR AT STRINGER 
- [SDR UIEA2025030100186](https://openairdocs.org/sdr/UIEA2025030100186), Mar 4, 2025: FLOOR SUPPORT. CORRODED. FWD CARGO COMPARTMENT STA 495 RBL 3" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS.(<P>PERFORMED PERMANENT REPAIR AT FLOOR CARGO STRUCTURE ZEE SUPPORT FROM
- [SDR UIEA2025030100185](https://openairdocs.org/sdr/UIEA2025030100185), Mar 4, 2025: FLOOR SUPPORT. CORRODED. FWD CARGO COMPARTMENT STA 495 LBL 3" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS. PERFORMED PERMANENT REPAIR AT FLOOR CARGO STRUCTURE ZEE SUPPORT FROM ST
- [SDR UIEA2025022700179](https://openairdocs.org/sdr/UIEA2025022700179), Mar 4, 2025: STRINGER. CORRODED. LOWER FUSELAGE, FWD CARGO COMPARTMENT FROM BS 440 TO BS 490 STRNGER-27R WITH CORROSION. PERFORMED PERMANENT REPAIR AT STRINGER 27R DUE TO CORROSION OUT LIMITS I
- [SDR UIEA2025022700177](https://openairdocs.org/sdr/UIEA2025022700177), Mar 4, 2025: STRINGER. CORRODED. LOWER FUSELAGE, AFT CARGO COMPARTMENT FROM BSTA 727H TO BSTA 727I AND BSTA 727F TO BSTA 727G STRINGER 26R WITH CORROSION. PERFORMED PERMANENT REPAIR ON STRINGER
- [SDR UIEA2025022700175](https://openairdocs.org/sdr/UIEA2025022700175), Mar 4, 2025: FLOOR SUPPORT. CORRODED. LOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR STRUCTURE FROM BS 727 TO BS 767 AT RBL 21 SIDE PLATE WITH CORROSION. REPAIRED SIDEPLATE FROM BS 727 TO BS 767 AT RBL 
- [SDR UIEA2025022700170](https://openairdocs.org/sdr/UIEA2025022700170), Mar 4, 2025: FLOOR SUPPORT. CORRODED. LOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR STRUCTURE FROM BS 757+4 TO BS 847 AT LBL 25,SIDE PLATE WITH CORROSION. PERFORMED PERMANENT REPAIR AT SIDE PLATE FROM 
- [SDR UIEA2025022700169](https://openairdocs.org/sdr/UIEA2025022700169), Mar 4, 2025: SKIN. DENTED. LOWER FUSELAGE, FWD COMPARMENT CARGO DOOR EXTERNAL SKIN AT BS 462 BETWEEN BEAM B AND BEAM C SKIN WITH DENT.(<P>PERFORMED PERMAMENT REPAIR AT AFT CARGO DOOR COMP
- [SDR UIEA2025022700167](https://openairdocs.org/sdr/UIEA2025022700167), Mar 4, 2025: SKIN. DENTED. LOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR EXTERNAL SKIN AT BS 821 BETWEEN BEAM D AND BEAM E SKIN WITH DENT.<BR>(<P>PERFORMED PERMANENT REPAIR AT AFT CARGO DOOR
- [SDR UIEA2023021100104](https://openairdocs.org/sdr/UIEA2023021100104), Feb 16, 2023: NONE. NONE. WHILE PERFORMING ELT FIXED TYPE OPERATIONAL TEST, IT FAILED DURING TEST "THE LED FLASHES 4 TIMES"(<P>CLEANED ELT COAX CONNECTOR ANTENNA CABLE I/A/W B737-800 SWP
- [SDR UIEA2023021100105](https://openairdocs.org/sdr/UIEA2023021100105), Feb 16, 2023: NONE. NONE. LOWER EXTERNAL FUSELAGE AT BS 218.500, WL 192.750 LEFT SIDE SKIN FASTENER WITH DOUBLE HOLE(<P>PERFORM REPAIR AT SECTION 41, FUSELAGE BS 218, WL192.750, L/H SIDE
- [SDR UIEA2023021100106](https://openairdocs.org/sdr/UIEA2023021100106), Feb 16, 2023: NONE. NONE. LOWER EXTERNAL FUSELAGE AT BS 188, WL 194 LEFT SIDE SKIN FASTENER WITH DOUBLE HOLE(<TABLE STYLE="WIDTH: 775PX;" BORDER="0" WIDTH="639" CELLSPACING="0" CELLPADDI
- [SDR Q2SA20210909455](https://openairdocs.org/sdr/Q2SA20210909455), Sep 9, 2021: TRANSMITTER. FAULTED. WHEN COMPLETING BEFORE LANDING CHECKLIST, FLAP HANDLE SELECTED TO 30, FLAP INDICATOR NEEDLE INDICATED 8 + 10 DEGREES. ON THE GO AROUND, THE FLAP NEEDLES MATCHED
- [SDR Q2SA20210804450](https://openairdocs.org/sdr/Q2SA20210804450), Aug 4, 2021: INLET. CONTAMINATED. ON DESCENT, PASSING THROUGH 11,000 FEET, SMELLED CHLORINE. PUT ON OXYGEN MASK. INSPECTED PACKS WITH APU BLEED AND ALSO WITH BOTH ENGINES RUNNING. COULD NOT DUPL
- [SDR Q2SA20210712448](https://openairdocs.org/sdr/Q2SA20210712448), Jul 12, 2021: FLAP SYSTEM. MALFUNCTIONED. AIRCRAFT LANDED WITHOUT INCIDENT. CREW REPORTED ON APPROACH SELECTED FLAP 30 AND THEY REMAINED AT FLAP 15. CYCLED FLAP LEVER TO 15 THEN BACK TO 30, FLAPS WOULD 
- [SDR Q2SA20210331445](https://openairdocs.org/sdr/Q2SA20210331445), Mar 31, 2021: SWITCH. OUT OF ADJUST. AIRCRAFT GROUNDED. GEAR WOULD NOT RETRACT AFTER TAKE-OFF. RAN QRH, GEAR WOULD NOT RETRACT. RETURNED TO AFW. INSPECTED AND FOUND MANUAL RELEASE EXTENSION DOOR SW

## 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 N5147A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5147A before.

- [Cancelled 2013-03-25](https://openairdocs.org/deregistered/N5147A-2013-03-25): Cessna 172, S/N 28147, built 1955. Registration expired, pending cancellation. Owner: [Duke Thomas A](https://openairdocs.org/faa-owner/DUKE%20THOMAS%20A), [Byesville, OH](https://openairdocs.org/faa-place/OH/Byesville)

## 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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