# N5693A: 1999 Boeing 737-84P

- Status: Valid registration
- Airframe: [Boeing 737-84P](https://openairdocs.org/model/boeing-737-84p) (registry code 13844ZZ, 189 seats)
- Engine: [CFM International CFM56-7B24 series](https://openairdocs.org/engine/cfm-international-cfm56-7b24-series) (registry code 13044)
- Serial number: 29947
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 12, 2020
- Certificate issued: June 17, 2020
- Expires: June 30, 2027
- Mode S code: A74B1B
- 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=5693A
- Page: https://openairdocs.org/aircraft/N5693A

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 737-84P)

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 N5693A.

## FAA accident and incident reports

None matched to N5693A.

## Service difficulty reports (36)

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 SCNA20261016434S](https://openairdocs.org/sdr/SCNA20261016434S), Oct 15, 2026: SLIDE. PARTIAL DEPLOY. CATERING OPENED L1 DOOR AFTER CLOSED AND ARMED. SLIDE PARTIALLY DEPLOYED. INSTALLED L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01 A/C GOOD FOR SERVICE.
- [SDR SCNA20261016434](https://openairdocs.org/sdr/SCNA20261016434), Oct 15, 2026: SLIDE. PARTIAL DEPLOY. CATERING OPENED L1 DOOR AFTER CLOSED AND ARMED. SLIDE PARTIALLY DEPLOYED. OPEN
- [SDR SCNA20261015430](https://openairdocs.org/sdr/SCNA20261015430), Oct 14, 2026: CHARGER. ODOR. FLT CREW REPORTS BURING PLASTIC ODOR IN SUPERNUMERARY AREA. FOUND SOURCE OF SMELL TO BE BATTERY CHARGER. REMOVED AND REPLACED BATTERY CHARGER IAW AMM 23-31-21. 
- [SDR SCNA20261006416](https://openairdocs.org/sdr/SCNA20261006416), Oct 4, 2026: BATTERY PACK. INOPERATIVE. ALL EMERGENCY LIGHTS ON LH SIDE INOP. SUSPECT BATTERY. REMOVED AND REPLACED LT BATTERY PACK REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR SCNA20260812355](https://openairdocs.org/sdr/SCNA20260812355), Aug 10, 2026: BATTERY. INOPERATIVE. AFT FACING OTBD SUPERNUMERARY SEAT EMERGENCY LIGHT NOT FLASHING. REPLACED THE BATTERY IN AFT FACING OTBD FLASHLIGHT IAW AMM 25-64-00. OPS CHKD GOOD.
- [SDR SCNA20250923388](https://openairdocs.org/sdr/SCNA20250923388), Sep 4, 2025: FAILSAFE. CORRODED. WO 98143, NR00005 FAS# 4686 WHILE WORKING TASK CARD 737-53A1414-01-NDT_UT FOUND CORROSION ON FAILSAFE STRAP AT STA 663.75 LH SIDE (AD RELATED) - FAS#6574COMPLIE
- [SDR SCNA20250818321](https://openairdocs.org/sdr/SCNA20250818321), Aug 14, 2025: DOOR. OUT OF ADJUST. DEFECT 750237: L1 DOOR SLIDE NEEDS TO BE ADJUSTED. FOUND L1 DOOR SLIDE MISALIGNED. RESOLUTION: REINSTALLED L1 DOOR SLIDE IAW AMM 25-66-00. OK FOR SERVICE.
- [SDR SCNA20250707244](https://openairdocs.org/sdr/SCNA20250707244), Jun 27, 2025: SKIN. CORRODED. R/H FUSELAGE FROM STA663 TO AFT PRESSURE BULKHEAD HAS SIGNS OF CORROSION ALONG LAP SEAM. ACCOMPLISHED EA 737-5360-72-B0528 P1, EA 737-5360-72-B0528 REV I/R AND 
- [SDR SCNA20250626233](https://openairdocs.org/sdr/SCNA20250626233), Jun 9, 2025: FITTING. WORN. L/H WING FOUND WEAR MARKING I/B SIDES OF FACE ON O/B FITTING I/B FLAP .
- [SDR SCNA20250627235](https://openairdocs.org/sdr/SCNA20250627235), Jun 8, 2025: FLAP TRACK. EXCESS PLAY. UPON DISASSEMBLY OF THE R/W I/B AFT FLAP TRACK FOR EXCESSIVE AXIAL PLAY. FOUND O/B TRACK, I/B SIDE, O/B FACE HAS EXCESSIVE WEAR. O/B FLAP FITTING I/B LUG AT R/W
- [SDR SCNA20250626232](https://openairdocs.org/sdr/SCNA20250626232), Jun 6, 2025: FLAP. CRACKED. CRACKED RH WING INBD KRUEGER FLAP T/E. REMOVED SEAL FOR ACCESS AT RH WING INBD KRUEGER FLAP IAW B737-800 BCF SRM 51-40-02-0G-0. REMOVED DAMAGE AT RH WING INBD K
- [SDR SCNA20250627236](https://openairdocs.org/sdr/SCNA20250627236), May 22, 2025: LAP JOINT. CORRODED. L/H FUSELAGE FROM STA 663 TO AFT PRESSURE BULKHEAD HAS NOTEABLE CORROSION ALONG LAPSEAM AS MARKED. ACCOMPLISHED EA 737-5360-72-B0508 IR ON L/H FUSELAGE AT AREA 
- [SDR SCNA20250623226](https://openairdocs.org/sdr/SCNA20250623226), May 22, 2025: PRESSURE BLKHD. CORRODED. L/H FUSELAGE FROM STA 663 TO AFT PRESSURE BULKHEAD HAS NOTEABLE CORROSION ALONG LAPSEAM AS MARKED. ACCOMPLISHED EA 737-5360-72-B0508 IR ON L/H FUSELAGE AT AREA 
- [SDR SCNA20250127028](https://openairdocs.org/sdr/SCNA20250127028), Jan 24, 2025: FASTENER. LOOSE. MULTIPLE SMOKED FASTENERS ON THE R/H WING JUST INBOARD OF THE #2 ENGINE PYLON WHEN PRESSING ON PANEL IT APPEARS THAT THE FASTENERS ARE LOOSE AND MAYBE SHEARED. 
- [SDR SCNA20241104354](https://openairdocs.org/sdr/SCNA20241104354), Nov 3, 2024: LIGHT. ARCED. DEFECT 749919: FO MAP LIGHT SPARKED POPPED C/B, RESET MAP AND KIT C/B, STATIC FEEDBACK CAN BE HEARD ON FO HEADSET.
- [SDR SCNA20240625256](https://openairdocs.org/sdr/SCNA20240625256), Jun 25, 2024: GIRT BAR. LOOSE. GIRT BAR LOOSE WHILE IN DOOR BRACKETS. ADJUSTED GIRT BAR 2 RETAINING CLIPS ON L1 DOOR REF AMM 25-66-01. GIRT BAR RESECURED
- [SDR SCNA2024052000242](https://openairdocs.org/sdr/SCNA2024052000242), May 14, 2024: CONTROLLER. FAILED. UNABLE TO CONTROL FLIGHT DECK TEMP. EXESSIVE HEAT. FOLLOWED QRH PROCEDURE TURNED OFF TRIM AIR SWITCH STILL UNCONTROLLABLE THEN TURNED OFF L- PACK PER QRH A/C TE
- [SDR SCNA20231106245](https://openairdocs.org/sdr/SCNA20231106245), Nov 4, 2023: UNKNOWN. UNKNOWN. R1 WINDOW CRACKED REMOVED AND REPLACED R1 WINDOW. OPS CHECKED GOOD. LEAK CHECKED GOOD
- [SDR SCNA20230531168](https://openairdocs.org/sdr/SCNA20230531168), May 25, 2023: FRAME. CORRODED. DEFECT NR00261: CORROSION FWD CARGO COMPARTMENT, FRAME AT WL 160, BS 500I BETWEEN S-25L TO S-26L HAS CORROSION. - - - RESOLUTION: CORROSION ON STA 500I FRAME BE
- [SDR SCNA20230530164](https://openairdocs.org/sdr/SCNA20230530164), May 16, 2023: BAFFLE. DAMAGED. DEFECT NR00577: FWD CARGO COMPPARTMENT, BAFFLE IS DAMAGED BETWEEN BS 400 AND BS 420, S-26L. - - - RESOLUTION: REMOVED AND REPLACED BAFFLE ON AFT CARGO FWD BETWE
- [SDR SCNA20230531167](https://openairdocs.org/sdr/SCNA20230531167), Apr 17, 2023: PLATE. CORRODED. DEFECT NR00513: CORROSION FWD CARGO COMPARTMENT BS440 FRAME ATTACH PLATE FROM STRINGER 22L TO 24L AT NUT PLATE HOLES. - - - RESOLUTION: REMOVED AND REPLACED NEW
- [SDR SCNA20230515148](https://openairdocs.org/sdr/SCNA20230515148), Apr 14, 2023: WEB. CORRODED. DEFECT NR00421: STA 420-440 STR 26R INTERCOSTAL. - - - RESOLUTION: CORROSION ON INTERCOSTAL STA 420-440 STR 26 FOUND TO BE OUT OF LIMITS IAW B737 53-30-15-1A-1 
- [SDR SCNA20230519157](https://openairdocs.org/sdr/SCNA20230519157), Apr 13, 2023: CHANNEL. CORRODED. DEFECT NR00254: CORROSION FWD CARGO COMPARTMENT, ZEE CHANNEL AT WL 160, BS 500A TO BS 500I, S-26R, HAS CORROSION (MARKED). - - - REMOVED AND INSTALLED REPLACEME
- [SDR SCNA20230531171](https://openairdocs.org/sdr/SCNA20230531171), Apr 12, 2023: SUPPORT. CORRODED. DEFECT NR00255: FWD COMPARTMENT SIDEWALL SUPPORT AT BS500D FROM S20R TO S26R HAS CORROSION. - - - RESOLUTION: REMOVED AND REPLACED SIDEWALL SUPPORT AT ST 500D F
- [SDR SCNA20230531170](https://openairdocs.org/sdr/SCNA20230531170), Apr 12, 2023: SHIELD. CORRODED. DEFECT NR00271: FWD CARGO COMPARTMENT, SHIELD AT WL 160 BS 440 AND S26R HAS CORROSION. - - - RESOLUTION: REMOVED AND REPLACED SHIELD AT WL 160 BS440 AND S26R IA
- [SDR SCNA20230531169](https://openairdocs.org/sdr/SCNA20230531169), Apr 12, 2023: SHIELD. CORRODED. DEFECT NR00257: FWD CARGO COMPARTMENT, SHIELD AT WL 160, S26R, BS 500 HAS CORROSION. - - - RESOLUTION: REMOVED AND REPLACED SHIELD WL 160 S26R, BS 500 PER B737-
- [SDR SCNA20230530165](https://openairdocs.org/sdr/SCNA20230530165), Apr 12, 2023: STRINGER. CORRODED. DEFECT NR00258: CORROSION FWD CARGO COMPARTMENT STRINGER AT WL 160, BS400, S-26R HAS CORROSION (MARKED). - - - RESOLUTION: CORROSION DAMAGE EVALUATED AND FOUND 
- [SDR SCNA20230519159](https://openairdocs.org/sdr/SCNA20230519159), Apr 12, 2023: BAFFLE. CORRODED. DEFECT NR00259: FWD CARGO COMPARTMENT, BAFFLE AT WL 160, S-26R, BETWEEN BS 400 AND BS 420 IS CRACKED. - - - RESOLUTION: REMOVED AND INSTALLED REPLACEMENT BAFFLE
- [SDR SCNA20230519158](https://openairdocs.org/sdr/SCNA20230519158), Apr 12, 2023: CHANNEL. CORRODED. DEFECT NR00262: CORROSION FWD CARGO COMPARTMENT, Z CHANNEL AT WL 160, BS 500B TO BS 500I, S-26L HAS CORROSION. - - - RESOLUTION: REMOVED AND REPLACE FWD CARGO C
- [SDR SCNA20230515150](https://openairdocs.org/sdr/SCNA20230515150), Apr 12, 2023: BAFFLE. CORRODED. DEFECT NR00253: FWD CARGO COMPARTMENT, BAFFLE AT WL 160, BETWEEN BS 500F AND BS 500G, S-26R FASTENER HOLES DAMAGED. (MARKED) - - - RESOLUTION: REPLACED AND REPA
- [SDR SCNA20230515149](https://openairdocs.org/sdr/SCNA20230515149), Apr 12, 2023: BAFFLE. CORRODED. DEFECT NR00269: FWD COMPARTMENT, BAFFLE AT WL 160 S-26L, BETWEEN BS.500F TO 500G AFT UPPER HOLE IS ELONGATED. (MARKED) - - - RESOLUTION: REPLACED AND REPAIRED B
- [SDR SCNA20230522161](https://openairdocs.org/sdr/SCNA20230522161), Apr 11, 2023: WEB. CORRODED. DEFECT NR00232: CORROSION FOUND ON FWD CARGO DOOR SUB THRESHILD WEB WHILE ACCESSING FOR NDI INSPECTION. - - - RESOLUTION: FWD CARGO DOOR SUB THRESHOLD FOUND TO 
- [SDR SCNA20230502142](https://openairdocs.org/sdr/SCNA20230502142), Apr 11, 2023: UNKNOWN. UNKNOWN. DEFECT ID 00229: BS 663 LOWER VAPOR BARRIER CRACKED OUTBORD OF RBL 55 APPROX. WL150 - - - RESOLUTION: REMOVED R/H 663 CRACKED VAPOR BARRIER IAW SRM 51-40-07-0G-
- [SDR SCNA20230216082](https://openairdocs.org/sdr/SCNA20230216082), Feb 16, 2023: NONE. NONE. DEFECT 735769: L1 DOOR SLIDE GIRT BAR LOOSE RESOLUTION: REINSTALLED L1 SLIDE IAW B737 AMM 25-66-01. NO FURTHER DEFECTS NOTED BY MX.
- [SDR SCNA20221128148](https://openairdocs.org/sdr/SCNA20221128148), Nov 22, 2022: RETAINER. OUT OF ADJUST. L1 DOOR SLIDE GIRT BAR WON'T STAY ON RETAINER FOR DOOR. ADJUSTED GIRT BAR HOLDER AS NEEDED.
- [SDR SCNA20200721049](https://openairdocs.org/sdr/SCNA20200721049), Jul 18, 2020: PRESSURE SWITCH. MALFUNCTIONED. DURING CLIMB OUT FROM MSP APU LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY #2 SOURCE OFF LIGHT ILLUMINATING. DECLARED AN EMERGENCY- AIR RETURN. REMOVED AND RE

## 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 N5693A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N5693A before.

- [Cancelled 2000-04-28](https://openairdocs.org/deregistered/N5693A-2000-04-28): Enstrom Helicopter 280C, S/N 1190. Exported to Canada. Owner: [Powis Mary M](https://openairdocs.org/faa-owner/POWIS%20MARY%20M), [Pocahontas, AR](https://openairdocs.org/faa-place/AR/Pocahontas)
- [Cancelled 1956-02-20](https://openairdocs.org/deregistered/N5693A-1956-02-20): Cessna 172, S/N 28293. Owner: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## Related

- Other Boeing 737-84P aircraft: https://openairdocs.org/model/boeing-737-84p/aircraft.md
- The CFM International CFM56-7B24 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b24-series.md

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