# N5261A: 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: 32348
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 2020
- Certificate issued: July 22, 2019
- Expires: July 31, 2029
- Mode S code: A6A1B4
- 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=5261A
- Page: https://openairdocs.org/aircraft/N5261A

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 N5261A.

## FAA accident and incident reports

None matched to N5261A.

## Service difficulty reports (34)

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 SCNA20260709288](https://openairdocs.org/sdr/SCNA20260709288), Jul 8, 2026: LAMP. INOPERATIVE. MULTIPLE LAMPS INOPERATIVE ON EMERGENCY LIGHT ABOVE R1 DOOR. REG LOGPAGE 834780 ITEM 1 FOR REPLACEMENT.
- [SDR SCNA20260113028](https://openairdocs.org/sdr/SCNA20260113028), Jan 12, 2026: RIVET. LOOSE. MAIN CARGO CABIN R1 FWD GALLEY DOOR ESCAPE SLIDE COVER FWD GIRT BAR RETAINER CLIP WITH SOLID RIVETS LOOSE. REPLACED SOLID RIVET IAW B737-800 BCF SR 51-40-02-06-
- [SDR SCNA20260113027](https://openairdocs.org/sdr/SCNA20260113027), Jan 12, 2026: BRACKET. STUCK. MAIN CARGO CABIN, R1 FWD GALLEY DOOR ESCAPE SLIDE COVER LATCH BRACKET IS STUCK. REPLACED FWD GALLEY (R1) DOOR ESCAPE SLIDE COVER LATCH BRACKT IAW B737-800 AMM T
- [SDR SCNA20251202458](https://openairdocs.org/sdr/SCNA20251202458), Dec 1, 2025: SLIDE. DISCHARGED. L1 SLIDE DISCHARGED. INSTALLED SERVICEABLE SLIDE IAW AMM 25-66-01 MEL 52-16-1 CLEARED.
- [SDR SCNA20251103425](https://openairdocs.org/sdr/SCNA20251103425), Oct 31, 2025: OIL SYSTEM. EMPTY. AFTER TAKEOFF ENG 2 OIL QTY WENT TO ZERO THEN ENG OIL PRESSURE DECREASED TO RED RANGE THEN TO ZERO PRECAUTIONARY SHUT DOWN NR 2 ENG. REMOVED AND REPLACED #2 ENG
- [SDR SCNA20251103424](https://openairdocs.org/sdr/SCNA20251103424), Oct 31, 2025: CARPET. UNSECURE. AFT EDGE OF CARPET LH ISLE IS A TRIP HAZARD AT FWD SIDE OF LAV. AFT EDGE OF CARPET LT AISLE CARPET STRIP AT FWD SIDE OF LAV WAS REALIGNED AND SECURED IAW CARPET
- [SDR SCNA20251022404S](https://openairdocs.org/sdr/SCNA20251022404S), Oct 20, 2025: SLIDE. DISLODGED. L1 SLIDE DETACHED ( MAIN CABIN EXIT/SLIDE L-1 DOOR SLIDE INOPERATIVE OR MISSING PROVIDED R1 OPERATES NORMALLY. ) RESCURED L1 DOOR GIRT BAR CDLIP IAW AMM 25-66-0
- [SDR SCNA20251022404](https://openairdocs.org/sdr/SCNA20251022404), Oct 20, 2025: SLIDE. DETACHED. L1 SLIDE DETACHED. OPEN
- [SDR SCNA20250909367](https://openairdocs.org/sdr/SCNA20250909367), Sep 8, 2025: WINDOW. ARCED. ARCING ON UPPER LH CORNER OF L1 WINDSCREEN WITH SMALL BURN SPOT R&R L1 WINDOW PER AMM 56-11-11 LEAK CHECK AND OPS CHECK GOOD REMOVED COLLARS AND RESET BREAKERS 
- [SDR SCNA20250609200](https://openairdocs.org/sdr/SCNA20250609200), Jun 2, 2025: CARGO TRACK. DAMAGED. WORK ORDER 95745, NR0004: DAMAGED TRACK ASSY CARGO SPORT IN AFT CARGO AT LBL 17.2 STA 787 - RESOLUTION: REMOVED AND REPLACED CARGO SUPPORT RAIL IN AFT CARGO AT 
- [SDR SCNA20241216397](https://openairdocs.org/sdr/SCNA20241216397), Dec 13, 2024: RING. MISSING. ONE OF THE RETAINING RINGS ON THE L1 GIRT BAR IS MISSING MC NOTIFIED BW9425. REPLACED MISSING GIRT BAR STOP ASSY PER AMM 25-66-01 THIS CLEARS MEL 52-16-2 MDDR #
- [SDR SCNA20240309062](https://openairdocs.org/sdr/SCNA20240309062), Jan 16, 2024: INTERCOSTAL. CRACKED. AFT CARGO COMPARTMENT FROM STA 827 TO STA 847 AT LBL20 INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL I-A-W BOEING SRM 51-10-02-0G-0 PARAG 9A.
- [SDR SCNA20240309070](https://openairdocs.org/sdr/SCNA20240309070), Jan 12, 2024: SHEAR TIE. CRACKED. FWD CARGO COMPARTMENT AT STA 500I BETWEEN STR-25L STR-26L FRAME WITH CRACK. REPLACED (SHEAR TIE) P/N # 143A3010-69 FWD CARGO COMPARTMENT AT STA 500I BETWEEN STG
- [SDR SCNA20240309061](https://openairdocs.org/sdr/SCNA20240309061), Jan 11, 2024: STIFFENER. CRACKED. REPLACED TOP STIFFENER P/N 111A2401-2 AND 111A2401-1 AT B%S 550 BETWEEN RBL 6" AND RBL 54" IAW B737-800 BFC SRM 51-10-02-0G-0 PARG 9 AND BOEING INST DWG 111A200
- [SDR SCNA20240308060](https://openairdocs.org/sdr/SCNA20240308060), Jan 11, 2024: ANGLE. CRACKED. MAIN CARGO DECK FLOOR TRANSVERSAL ANGLE FLANGE IS CRACKED AT BS 540, RBL 24. EMP# 157 QC# 25 REPLACED BREAK IAW B737-800 BCF SRM 51-10-02-0G-0 PARG 9 AND BOEING
- [SDR SCNA20240308059](https://openairdocs.org/sdr/SCNA20240308059), Jan 9, 2024: SPAR WEB. CORRODED. EMP# 157 QC# 25 RII# QC25 PERFORMED PERMANENT REPAIR OF RH WING FRONT SPAR WEB AT FWD FUEL BOOST PUMP DUE TO CORROSION OUT LIMITS IAW COOPESA EO# 600-EO-2024-19
- [SDR SCNA20240311149](https://openairdocs.org/sdr/SCNA20240311149), Jan 8, 2024: BULKHEAD. CRACKED. AFT CARGO COMPARTMENT, FWD BULKHEAD PANELS: 141JW, 142MW WITH CRACKS. BULKHEAD PANELS DAMAGE WERE FOUND GREATER THAN THE LIMITS I.A.W BOEING 737-800 AMM SCA TAS
- [SDR SCNA20240309066](https://openairdocs.org/sdr/SCNA20240309066), Jan 7, 2024: BULKHEAD. CORRODED. FWD CARGO COMPARTMENT AFT BULKHEAD AT 500I THE LEFT RAIL, CENTER RAIL AND RIGHT RAIL WITH CORROSION. REPLACED SUPPORT AND ANGLES P/N143A9495Y23, 143A9485-35 AND
- [SDR SCNA20240309065](https://openairdocs.org/sdr/SCNA20240309065), Jan 6, 2024: INTERCOSTAL. CRACKED. AFT CARGO COMPARTMENT FROM STA 747 TO STA 767 AT RBL20 INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL AFT CARGO COMPARTMENT FROM STA 747 TO STA 767 AT RBL 20 I.A.
- [SDR SCNA20240309064](https://openairdocs.org/sdr/SCNA20240309064), Jan 6, 2024: INTERCOSTAL. CRACKED. AFT CARGO COMPARTMENT FROM STA 727A TO STA 727B AT LBL20 AND RBL20 INTERCOSTAL WITH CRACK. REPLACED INTERCOSTAL IAW B-737-800 SRM 51-10-02-0G-0 PARAG 9
- [SDR SCNA20240309063](https://openairdocs.org/sdr/SCNA20240309063), Jan 6, 2024: CARGO TRACK. CRACKED. AFT CARGO COMPARTMENT FROM STA 787 TO STA 807 AT LBL 17.24 DOWN TRACK-TIE CARGO SECTION WITH CRACK. PERFORMED PERMANENT REPAIR AT CARGO TRACK SECTION FROM STA72
- [SDR SCNA20240309069](https://openairdocs.org/sdr/SCNA20240309069), Jan 5, 2024: BAFFLE. CORRODED. LOWER FUSELAGE, FWD CARGO COMPARTMENT. FROM STA 500H TO STA 500I AT RBL 21 AND LBL 21 THE INTERCOSTALS (BAFLES) WITH CORROSION. REPLACED (BAFLES) INTERCOSTALS F
- [SDR SCNA20240309068](https://openairdocs.org/sdr/SCNA20240309068), Jan 5, 2024: BAFFLE. CORRODED. LOWER FUSELAGE, FWD CARGO COMPARTMENT. FROM STA 500A TO STA 500I AT RBL 21 THE INTERCOSTALS (BAFLES) WITH CORROSION. REPLACED (BAFLES) INTERCOSTALS FROM STA 500
- [SDR SCNA20240309067](https://openairdocs.org/sdr/SCNA20240309067), Jan 5, 2024: BAFFLE. CORRODED. MRO ZONE 1 NR# 10 EMP# 6434 W/O:77911,TASK CARD #538200000:LOWER FUSELAGE, FWD CARGO COMPARTMENT. FROM STA 400 TO STA 500H AT LBL 21 THE INTERCOSTALS (BAFLES) W
- [SDR SCNA20240305058](https://openairdocs.org/sdr/SCNA20240305058), Dec 27, 2023: FLOOR SUPPORT. CORRODED. AFTER GILL LINER REMOVAL IN LEFT BELLY AFT CARGO, CORROSION WAS FOUND ON FLOOR SUPPORT AT APPROX STA 792 TO STA 787. PER ENGINEERING, AFT CARGO DEPT SHALL REMAI
- [SDR SCNA20230420131](https://openairdocs.org/sdr/SCNA20230420131), Apr 19, 2023: UNKNOWN. UNKNOWN. DEFECT 735992: DOOR SLIDE OUT OF POSITION L1 - - - RESOLUTION: REINSTALLED L1 DOOR ESCAPE SLIDE. REF. AMM 25-66-01.
- [SDR SCNA20230412123](https://openairdocs.org/sdr/SCNA20230412123), Mar 24, 2023: UNKNOWN. UNKNOWN. DEFECT 735954: DOOR 1L AFT GIRT BAR HOLDER LOOSE. RESOLUTION: RESECURED L1 AFTR GIRT BAR HOLDERR AND REINSTALLED SLIDE IAW AMM 25-66-01. NO FURHTER DEFECTS NOTE
- [SDR SCNA20230227088](https://openairdocs.org/sdr/SCNA20230227088), Feb 27, 2023: NONE. NONE. DEFECT 716061: LE FLAP TRANSIT LIGHT ILLUMINATED PRIOR TO APPROACH (ON DESCENT) LANDING FLAP 15 AS PER QRH. RESOLUTION: PEFORMED FIM 27-88 TASK 820 NO FAULTS FO
- [SDR SCNA20230227](https://openairdocs.org/sdr/SCNA20230227), Feb 27, 2023: NONE. NONE. DEFECT 716061: LE FLAP TRANSIT LIGHT ILLUMINATED PRIOR TO APPROACH (ON DESCENT) LANDING FLAP 15 AS PER QRH. EMERGENCY DECLARED. RESOLUTION: PEFORMED FIM 27-88 T
- [SDR SCNA20220727087](https://openairdocs.org/sdr/SCNA20220727087), Jul 21, 2022: RIVET. BROKEN. DEFECT: DOOR 1L SLIDE BAR STOWAGE HOOK BROKEN RIVET, HOOK LOOSE. RESOLUTION: REPLACED BROKEN RIVET ON 1L SIDE BAR STOWAGE HOOK REF AMM 25-66-01.
- [SDR SCNA20220321005](https://openairdocs.org/sdr/SCNA20220321005), Feb 21, 2022: NONE. NONE. DEFECT: R/H WING. L/E UPPER SKIN, I/B OF NACELLE HAS 12X SMOKING RIVETS (MARKED). RESOLUTION: REPAIRED R/H WING FIXED L/E SKIN, JUST IB OF NO.2 ENGINE PER ATSER
- [SDR SCNA20220321004](https://openairdocs.org/sdr/SCNA20220321004), Feb 21, 2022: NONE. NONE. DEFECT: L/H WING, L/E UPPER SKIN, I/B OF NACELLE HAS 12X SMOKING RIVETS (MARKED). RESOLUTION: REPAIRED L/H WING, L/E UPPER SKIN, I/B OF NACELLE IAW ER 22-01301 
- [SDR SCNA20210302012](https://openairdocs.org/sdr/SCNA20210302012), Feb 27, 2021: TIRE. FAILED. BLEW 2 MAIN LEFT TIRES ON LANDING TAXI OFF RUNWAY. TRANSFERRED LOG PAGE 644446 ITEM 1 TO W-O 58267. [REMOVED AND REPLACED #1 MAIN TIRE AND WHEEL ASSYS. REF. AMM
- [SDR SCNA20200612045](https://openairdocs.org/sdr/SCNA20200612045), Jun 12, 2020: SENSOR. FAULTY. FLAP TRAILING EDGE ASSYMETRY PRIOR TO FLAPS 1. FOUND FLAP NR 2 SKEW FAULT CODE 27-53251 PERFORMED FIM 27-59 TASK 802. REMOVED AND REPLACED NR 2 FLAP SKEW SENSOR

## 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 N5261A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5261A before.

- [Cancelled 2014-10-27](https://openairdocs.org/deregistered/N5261A-2014-10-27): Cessna 310, S/N 35461, built 1956. Registration expired, pending cancellation. Owner: [Twin Flyers Inc](https://openairdocs.org/faa-owner/TWIN%20FLYERS%20INC), [Winston, GA](https://openairdocs.org/faa-place/GA/Winston)

## 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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