# N825SY: 2006 Boeing 737-8F2

- Status: Valid registration
- Airframe: [Boeing 737-8F2](https://openairdocs.org/model/boeing-737-8f2) (registry code 13844DA, 149 seats)
- Engine: [CFM International CFM56-7B26 series](https://openairdocs.org/engine/cfm-international-cfm56-7b26-series) (registry code 13045)
- Serial number: 34410
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2018
- Certificate issued: June 15, 2020
- Expires: June 30, 2027
- Mode S code: AB4515
- Registered owner: [Sun Country Inc](https://openairdocs.org/faa-owner/SUN%20COUNTRY%20INC)
- Location: [Minneapolis, MN](https://openairdocs.org/faa-place/MN/Minneapolis)
- Owner type: Corporation
- Owner's area on the map: 44.8723° N, 93.2328° W: Placed by OpenAirDocs at the center of ZIP code 55450, 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=825SY
- Page: https://openairdocs.org/aircraft/N825SY

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 CFM56-7B26 model are included.

## ADs that may apply (OpenAirDocs): 19 in force

### Matched by airframe (Boeing 737-8F2)

None in force.

### Matched by engine (CFM International CFM56-7B26 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 N825SY.

## FAA accident and incident reports

None matched to N825SY.

## Service difficulty reports (45)

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 SCNA20261014427](https://openairdocs.org/sdr/SCNA20261014427), Oct 8, 2026: SKIN. CRACKED. CRACK WAS FOUND OF 0.125IN LENGTH IN RIB HOLE AT STAB STA 129.50 OF LT HORIZONTAL STAB LOWER SURFACE. REPAIR: IAW SRM REF 55-10-09-2R-5, REPAIR 5.
- [SDR SCNA20261014425](https://openairdocs.org/sdr/SCNA20261014425), Sep 28, 2026: SKIN PANEL. CRACKED. INITIAL INSPECTION: CRACK WAS FOUND IN THE SKIN OF HOLE #6 SKIN AND COUNTERSINK BTW 12 O CLOCK POSITION AT LEADING EDGE SKIN PANEL KRAS 206, LEFT WINGS. (CONTAC
- [SDR SCNA20261014424](https://openairdocs.org/sdr/SCNA20261014424), Sep 28, 2026: SKIN. CRACKED. CRACKS WERE FOUND IN THE SKIN OF HOLE #4 SKIN & COUNTERSINK BTW 10 O CLOCK POSITION AND HOLE #5 SKIN & COUNTERSINK BTW 11 O CLOCK POSITION AT LEADING EDGE SKIN 
- [SDR SCNA20261014429](https://openairdocs.org/sdr/SCNA20261014429), Sep 27, 2026: SKIN. CRACKED. WO 98046 NR00014 INITIAL / CRACK WAS FOUND OF: L=0.688IN LENGTH ON RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 138.70 COMMON TO THE HORIZONTAL RIB IN REFERE
- [SDR SCNA20261014428](https://openairdocs.org/sdr/SCNA20261014428), Sep 27, 2026: SKIN. CRACKED. CRACK WAS FOUND OF: L=0.625IN LENGTH ON RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 184.70 COMMON TO THE HORIZONTAL RIB IN REFERENCE TO TASK CARD ENG-55SCA-
- [SDR SCNA20260928413](https://openairdocs.org/sdr/SCNA20260928413), Sep 27, 2026: LIGHT SYS. FAULTED. DURING EMERGENCY LIGHTS CHECK, EMERGENCY LIGHTS AT OVERHEAD BINS 6L AND 8L POSITION, R1 DOOR AND FWD RT OVERWING EMERGENCY EXIT DOOR AT CABIN PAX DOES NOT TURN 
- [SDR SCNA20261020437](https://openairdocs.org/sdr/SCNA20261020437), Sep 26, 2026: SKIN. CRACKED. A CRACK WAS FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 138.70 COMMON TO THE HORIZONTAL RIB IAW TASK CARD ENG-55SCA-11150-LH, CRACKS (2EAS) AT LOWE
- [SDR SCNA20261014426](https://openairdocs.org/sdr/SCNA20261014426), Sep 26, 2026: SKIN. CRACKED. WO 98046 NR00012, INITIAL / CRACK WAS FOUND OF: L=0.750IN LENGTH ON LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 147.90 COMMON TO THE HORIZONTAL RIB IN REFER
- [SDR SCNA20260914392](https://openairdocs.org/sdr/SCNA20260914392), Sep 14, 2026: BRAKE. LEAKING. RIGHT MAIN/RIGHT BRAKE WET/ SMOKING. FOUND NR 4 MLG BRAKE PISTON LEAKING REMOVED AND REPLACED NUMBER 4 MLG BRAKE REF AMM 32-41-41.
- [SDR SCNA20260818367](https://openairdocs.org/sdr/SCNA20260818367), Aug 17, 2026: LAMP. INOPERATIVE. AREA EMERGENCY LIGHT INOPERATIVE AT ROW 28DEF. RELAMPED AREA EMERGENCY LIGHT IAW AMM 33-51-03-960-801.
- [SDR SCNA20260608242](https://openairdocs.org/sdr/SCNA20260608242), Jun 5, 2026: SKIRT. MISINSTALLED. R-1 DOOR SLIDE, GILT BAR SKIRT IMPROPERLY STOWED. PERFORMED ADJUSMENT R-1 DOOR SLIDE, GILT BAR SKIRT IAW AMM 25-66-01
- [SDR SCNA20260601228](https://openairdocs.org/sdr/SCNA20260601228), May 29, 2026: SKIRT. UNPACKED. L1 DOOR SLIDE GIRT BAR SKIRT IMPROPERLY STOWED. RESECURED L1 DOOR SLIDE GIRT BAR SKIRT IAW AMM 25-66-01-400-803.
- [SDR SCNA20260518207](https://openairdocs.org/sdr/SCNA20260518207), May 15, 2026: DOWNLOCK SENSOR. FAULTED. AFTER TAKEOFF FWD GREEN RIGHT GEAR LIGHT REMAINED ILLUMINATED. OVHD GEAR LIGHTS WERE EXTINGUISHED. REMOVED AND REPLACED R/H GEAR DOWNLOCK SENSOR S0073. SENSOR A
- [SDR SCNA20260420163](https://openairdocs.org/sdr/SCNA20260420163), Apr 19, 2026: WIRE. BROKEN. AFT RIGHT OVERWING DOOR EMERGENCY LIGHTS INOP FOUND BROKEN WIRE ON AFT R/H OVERWING EXIT WINDOW LIGHT, REMOVED AND REPLACED AFT R/H OVERWING WINDOW LIGHT ASSY R
- [SDR SCNA20260420162](https://openairdocs.org/sdr/SCNA20260420162), Apr 19, 2026: ELEC CONNECTOR. DIRTY. L1 DOOR EXTERIOR EMERGENCY DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT BATTERY PACK REF 33-51-06. NO HELP. CHECKED FOR POWER AT CONNECT
- [SDR SCNA20260420161](https://openairdocs.org/sdr/SCNA20260420161), Apr 19, 2026: BATTERY PACK. INOPERATIVE. R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 EMERGENCY LIGHTS BATTERY PACK REF AMM 33-51-06. OPS CHK GOOD
- [SDR SCNA20260213076](https://openairdocs.org/sdr/SCNA20260213076), Feb 12, 2026: LANYARD. UNSECURE. CREW REPORTED, THE LT FWD EMERGENCY OVERWING EXIT DOOR LANYARD POUCH HANGING DOWN. INSTALLED TWO STUDS FOR LT FWD OVERWING EXIT DOOR LANYARD IAW AMM 52-22-51. O
- [SDR SCNA20260210070](https://openairdocs.org/sdr/SCNA20260210070), Feb 9, 2026: SEAT BACK. DAMAGED. SEAT BACK METAL PROTRUDING AND POCKET TORN. OPEN
- [SDR SCNA20251226508](https://openairdocs.org/sdr/SCNA20251226508), Dec 26, 2025: RETAINER. UNSECURE. L1 ESCAPE SLIDE VERY LOOSE WHEN DISARMED AND GIRT BAR IS IN RETAINER CLIP. TIGHTENED L1 SLIDE GIRT BAR HOLDER REF AMM 25-61-06
- [SDR SCNA20250905362](https://openairdocs.org/sdr/SCNA20250905362), Aug 26, 2025: WINDOW FRAME. CRACKED. L1 WINDOW FRAME CRACK - PERMANENT REPAIR - LH - - C/W BY ATS 80761C ACCOMPLISHED SB 737-53-1336 REV 1 DATED OCT 23, 2014
- [SDR SCNA20250708248](https://openairdocs.org/sdr/SCNA20250708248), Jul 6, 2025: LENS. BROKEN. CENTER EMERGENCY EXIT LENS BROKEN - R & R CENTER EMERGENCY EXIT ROW LENS IAW AMM 33-51-01
- [SDR SCNA20250625229](https://openairdocs.org/sdr/SCNA20250625229), Jun 24, 2025: RETAINER. LOOSE. L1 DOOR SLIDE GIRT BAR RETAINING LOOPS LOOSE IN COVER, REMOVED SLIDE IAW AMM 25-66-01 TO TIGHTEN RIVETS ON GIRT BAR RETAINING LOOPS IAW SRM 51-40-02. INSTALLED 
- [SDR SCNA20250407101](https://openairdocs.org/sdr/SCNA20250407101), Apr 4, 2025: FIRE DETECTOR. FALSE ACTIVATION. DEFECT 714466: EXPERIENCED 4 INNTERMITTENT , AFT CARGO FIRE ALERTS FROM 37,000 FT TO 8000 FT. LONGEST OF 10 SECOND DURATION. ALWAYS WENT OUT ON ITS OWN. - RESOL
- [SDR SCNA20250128033](https://openairdocs.org/sdr/SCNA20250128033), Jan 27, 2025: COVER. BROKEN. DEFECT 796983: 2L SLIDE HOUSING COVER BROKEN. RESOLUTION: REAPPLIED 2L SLIDE HOUSING COVER REF AMM 25-66-00 OK FOR SERVICE
- [SDR SCNA20250116017](https://openairdocs.org/sdr/SCNA20250116017), Jan 16, 2025: GIRT BAR. LOOSE. DEFECT 796963: 1R DOOR BRACKET FOR GIRT BAR LOOSE. RESOLUTION: FOUND DEBRIS IN GIRT BAR BRACKET AND ON GIRT BAR REMOVED CLEANED AND REINSTALLED REF AMM 25-66-01
- [SDR SCNA20250102001](https://openairdocs.org/sdr/SCNA20250102001), Jan 1, 2025: AILERON. LACK OF LUBE. ON APPROACH WITH FLAPS 30, GEAR EXTENDED, HYD B QTY WAS 69-70% AND PRESSURE AT 2870. AILERONS BEOND 10-15 DEGREES OF BANK WERE VERY STIFF AND HARD TO GET BEOND.
- [SDR SCNA20240725281](https://openairdocs.org/sdr/SCNA20240725281), Jul 12, 2024: PRESSURE DECK. CRACKED. CRACK AT WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB ON STA 663 BTW LBL 31.83 AND LBL 45.64. REPAIRED PER B737-800 SRM 57-10-10 REPAIR 3 PAR 5 AND 
- [SDR SCNA20240725282](https://openairdocs.org/sdr/SCNA20240725282), Jul 11, 2024: PANEL. DAMAGED. RH WING TE FIXED UPPER PANEL BTW #7 GROUND SPOILER AND #8 FLIGHT SPOILER DAMAGE. FIXED UPPER PANEL BETWEEN #7 GROUND SPOILER AND #8 FLIGHT SPOILER (W.S. 278.50)
- [SDR SCNA20241114367](https://openairdocs.org/sdr/SCNA20241114367), Jul 3, 2024: LIGHT. DETACHED. DEFECT 7533444: 12D EMERGENCY EXIT LIGHT COMING OFF FLOOR. RESOLUTION: SECURED FLOOR PROXIMITY LIGH AT ROW 12D REF AMM 33-51-15. OK FOR SERVICE.
- [SDR SCNA20240708264](https://openairdocs.org/sdr/SCNA20240708264), Jul 3, 2024: LIGHT. DETACHED. 12D EMERGENCY EXIT LIGHT COMING OFF FLOOR. SECURED FLOOR PROXIMITY LIGH AT ROW 12D REF AMM 33-51-15. OK FOR SERVICE
- [SDR SCNA20240531247](https://openairdocs.org/sdr/SCNA20240531247), Apr 23, 2024: DOOR. CRACKED. CRACK ON INNER SKIN OF FWD CUTOUT AT EXTERNAL POWER RECEPTACLE DOOR.INNER SKIN OF FWD CUTOUT AT EXTERNAL POWER RECEPTACLE DOOR WAS REPAIRED PER B737-800 SRM 53-
- [SDR SCNA20240329169](https://openairdocs.org/sdr/SCNA20240329169), Mar 28, 2024: UNKNOWN. FAULTED. FLAPS LOCKED AT 25 DEGREES PRIOR TO LANDING. PERFORMED FIM 27-51 TASK 801. NO ACTIVE FAULTS. PERFORMED OPS CHK OF TE FLAPS REF AMM 27-51-00. NO FAULTS NOTED.
- [SDR SCNA20230510145](https://openairdocs.org/sdr/SCNA20230510145), May 9, 2023: UNKNOWN. UNKNOWN. DEFECT 763214: 1L BOARDING DOOR SLIDE IS EXPOSED AND COMING OUT BY GIRT BAR. - - - RESOLUTION: RE-STOWED L1 SLIDE PER AMM TASK 25-66-01. A/C OK FOR SERVICE.
- [SDR SCNA20220926109](https://openairdocs.org/sdr/SCNA20220926109), Sep 15, 2022: GIRT BAR. OUT OF ADJUST. DEFECT 715333: GIRT BAR AT DOOR 1L WILL NOT STAY STOWED IN DISARMED POSITION. RESOLUTION: ADJUSTED GIRT BAR LATCH PER AMM 12-25-41. OPS CHECK GOOD.
- [SDR SCNA20221003120](https://openairdocs.org/sdr/SCNA20221003120), Sep 6, 2022: LIGHT. INOPERATIVE. DEFECT WORK ORDER N/R-00003 EXTERIOR RH AFT R2 DOOR EMERG LIGHT INOP. RESOLUTION: RE-LAMPED R2 DOOR EMERGENCY EXIT LIGHT. REF AMM 33-51-04.
- [SDR SCNA20220601066](https://openairdocs.org/sdr/SCNA20220601066), May 30, 2022: ELEVATOR SYSTEM. INTERFERENCE. DEFECT: SPD LIM AMBER INDICATION ON CA PFD AFTER TAKE-OFF WITH INTERMITTENT STICK SHAKER. LOW SPEED LIMIT TAPE CAME UP TO 280 KIAS. RESOLUTION: ACOMPLISHED DFCS
- [SDR SCNA20220601](https://openairdocs.org/sdr/SCNA20220601), May 30, 2022: ELEVATOR SYSTEM. INTERMITTENT. DEFECT: SPD LIM AMBER INDICATION ON CA PFD AFTER TAKE-OFF WITH INTERMITTENT STICK SHAKER. LOW SPEED LIMIT TAPE CAME UP TO 280 KIAS. RESOLUTION: ACOMPLISHED DFCS
- [SDR SCNA202205044046](https://openairdocs.org/sdr/SCNA202205044046), Apr 30, 2022: GIRT BAR. LOOSE. DEFECT: DOOR 1L GIRT BAR BRACKET ON DOOR SWIVELS BACK AND FORTH WHEN BAR IS NOT INSTALLED MX NOTIFIED 8340. RESOLUTION: REMOVED SLIDE FROM DOOR AND SECURED GIRT
- [SDR SCNA20220427035](https://openairdocs.org/sdr/SCNA20220427035), Apr 6, 2022: GIRT BAR. LOOSE. FWD ENTRY DOOR (1L) LHS GIRT BAR BRACKET LOOSE. RESOLUTION: REPLACED GIRT BAR ASSY REF M/M 25-66-00
- [SDR SCNA20211028087](https://openairdocs.org/sdr/SCNA20211028087), Oct 12, 2021: NONE. NONE. CORROSION FOUND IN NUTPLATE @STA. 986.5, LBL 43, WL 208. CORROSION FOUND OUT OF LIMITS @ STA. 986.5, LBL 43 WL 208 PER SRM 53-70-51-1A-1, FIG 104. REPAIRED STA.
- [SDR SCNA20211028092](https://openairdocs.org/sdr/SCNA20211028092), Oct 11, 2021: NONE. NONE. CORROSION FOUND ON SHEAR WEB @STA. 986.5, RBL 44, WL 208. CORROSION FOUND TO BE OUT OF LIMITS @ STA. 986.5, RBL 44, WL 208 PER SRM HAS NO LIMITS. MACHINED REPLA
- [SDR SCNA20211028090](https://openairdocs.org/sdr/SCNA20211028090), Oct 9, 2021: NONE. NONE. CORROSION FOUND ON SHEAR WEB AROUND NUTPLATE @STA. 1016, LBL 37, WL 208. REMOVED AND REPLACED SHEAR WEB @ STA 1016, LBL 37, WL 208 IAW SRM 51-10-02-0G-0 AND BOE
- [SDR SCNA20211028088](https://openairdocs.org/sdr/SCNA20211028088), Oct 8, 2021: NONE. NONE. CORROSION FOUND ON SHEAR WEB @STA. 986.5, LBL 44, WL 208. REMOVED DAMAGED SHEAR WEB @ STA 986.5 LBL 44 AND INSTALLED NEW WEB PER .B737 S.R.M 51-40-02-0G PARA 4.
- [SDR SCNA20211028093](https://openairdocs.org/sdr/SCNA20211028093), Oct 6, 2021: NONE. NONE. CORROSION ON INTERCOSTAL ( FLEX SEAL WEB) ,FWD SIDE OF AFT PRESSURE BULKHEAD AT STA1028, RBL 28, WL209. INTERCOSTAL FOUND DAMAGE OUT OF LIMITS PER IAW-SRM. 53-8
- [SDR SCNA20211028089](https://openairdocs.org/sdr/SCNA20211028089), Oct 6, 2021: NONE. NONE. CORROSION FOUND ON FLOOR SUPPORT @STA. 947+11, LBL 49, WL 208. CORROSION ON FLOOR SUPPORT STA 947+11 LBL 49 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS FO

## 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 CFM56-7B26 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

## Related

- Other Boeing 737-8F2 aircraft: https://openairdocs.org/model/boeing-737-8f2/aircraft.md
- The CFM International CFM56-7B26 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b26-series.md

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