# N826SY: 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: 34411
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 14, 2018
- Certificate issued: June 12, 2020
- Expires: June 30, 2027
- Mode S code: AB48CC
- 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=826SY
- Page: https://openairdocs.org/aircraft/N826SY

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 N826SY.

## FAA accident and incident reports

None matched to N826SY.

## Service difficulty reports (58, newest 50)

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 SCNA20260805338](https://openairdocs.org/sdr/SCNA20260805338), Aug 4, 2026: SLIDE. MISINSTALLED. L2 DOOR ESCAPE SLIDE NOT INSTALLED CORRECT LOWER BALL NOT IN SLOT - - REINSTALLED L2 DOOR SLIDE IAW AMM 25-66-01 OK FOR SERVICE RII ACCOMPLISHED ON L2 DOOR SLID
- [SDR SCNA20260720320](https://openairdocs.org/sdr/SCNA20260720320), Jul 20, 2026: HOLDER. UNSECURE. L1 GIRT BAR HOLDER NEED TIGHTENED. GIRT BAR RETAINER CLIP ADJUSTED, GIRT BAR IS SECURE WHEN STOWED IN ARMED/UNARMED POSITIONS IAW AMM 25-66-01.
- [SDR SCNA20260629265](https://openairdocs.org/sdr/SCNA20260629265), Jun 27, 2026: GIRT BAR. DAMAGED. R2 DOOR GIRT BAR LEFT HAND SIDE OF BAR, THE PLASTIC PIECE IS BROKEN, DEBRIS FOUND WAS FROM AN OLD PIECE. RENTENSION CLIP IS INSTALLED AND SECURED AT 2R DOOR GIR
- [SDR SCNA20260601230](https://openairdocs.org/sdr/SCNA20260601230), May 31, 2026: BATTERY PACK. INOPERATIVE. FOUND RH AFT EMERGENCY OVERWING EXIT LIGHT INOP. R/R RH AFT EMERGENCY OVERWING EXIT LIGHT LAMP IAW AMM 33-51-04-960-801. NO HELP. R/R RH AFT EMER OVERWING EXIT 
- [SDR SCNA20260514198](https://openairdocs.org/sdr/SCNA20260514198), May 13, 2026: BATTERY PACK. INOPERATIVE. FWD RH AND LT EMERGENCY DOORS EMERGENCY LIGHTS DO NOT WORK. REMOVED AND REPLACE EMERGENCY BATTERY PACK IAW B737-800 MM 33-51-06 OPS CHECK GOOD ON FWD RH AND LH 
- [SDR SCNA20260310115](https://openairdocs.org/sdr/SCNA20260310115), Mar 10, 2026: TRIM PANEL. DAMAGED. 2L LAV LOWER RIGHT INSIDE LAV TRIM BROKEN AND SHARP. RESECURED 2L LAV TRIM PIECE. REF CMM 25-43-78. OK FOR SERVICE
- [SDR SCNA20260623259](https://openairdocs.org/sdr/SCNA20260623259), Mar 8, 2026: SMOKE GOGGLES. CRACKED. SMALL CRACK IN THE MIDDLE SECTION OF THE GLASS ON CAPTAINS SMOKE GOGGLES (BW #9425 MC NOTIFIED). REMOVED AND REPLACED CA SMOKE GOGGLES IN REF AMM 25-64-00. OKAY
- [SDR SCNA20260213080](https://openairdocs.org/sdr/SCNA20260213080), Feb 12, 2026: LIGHT. DETACHED. FOUND AREAS OF FLOOR PATH LIGHTING NOT ADHEREING TO CABIN FLOOR REAFIXED FLOOR PATH LIGHTING IAW 33-51-00. BUTT JOINT GAP REQUIRED PER ITEM 12 OF TASK CARD ST02
- [SDR SCNA20251218495](https://openairdocs.org/sdr/SCNA20251218495), Dec 16, 2025: LAMP. INOPERATIVE. NO SMOKING LIGHTS INOP AT THE FOLLOWING SEAT LOCATIONS: 6D, 11D, 29D, 10A, 19A RELAMPED NO SMOKING LIGHTS 6D, 11D, 29D,10A,AND 19A REF AMM 33-25-00. OK FOR SERV
- [SDR SCNA20251215485](https://openairdocs.org/sdr/SCNA20251215485), Dec 14, 2025: BRAKE. CONTAMINATED. BOTH BRAKE SMOKING ON LANDING UP TO GATE. INSP NR 1 & 2 BRAKES IAW AMM 32-41-41. NO LEAKS NOTED, SUSPECT DEICING FLUID.
- [SDR SCNA20250919382](https://openairdocs.org/sdr/SCNA20250919382), Sep 18, 2025: HANDLE. UNSECURE. LEFT FWD OVERWING EMERGENCY EXIT DOOR MAINT ASSIST STRAP MISSING TRIM RETAINING STUDS. SECURED THE LT FWD OVERWING EXIT DOOR ASSIST HANDLE TRIM ASSY. REF AMM 52
- [SDR SCNA20250917378](https://openairdocs.org/sdr/SCNA20250917378), Sep 15, 2025: BATTERY PACK. NO TEST. 6-12ABC EMERGENCY AREA LIGHTS FAILED CAPACITY CHECK RETEST. PER AMM 33-51-06-200-801 STEP 5 REMOVED AND REPLACED AFT POWER SUPPLY BATTERY PACK REF: 31-51-06-960
- [SDR SCNA20250908365](https://openairdocs.org/sdr/SCNA20250908365), Sep 7, 2025: SLIDE. NO DISCREPANCY. 1L DOOR SLIDE SAGS AND SEEMS TO MAKE A POPPING NOISE ON CLIMB OUT INSPECTED SLIDE PACK PER AMM 25-66-01 NO DEFECTS NOTED OK FOR SERVICE A&P 3353509
- [SDR SCNA20250818324](https://openairdocs.org/sdr/SCNA20250818324), Aug 17, 2025: BATTERY PACK. INOPERATIVE. 2L EMERGENCY EXIT PLACARDS (TOP AND BOTTOM) AND FLOOR EXIT LIGHTING IN THE AFT CABIN DID NOT ILLUMINATE WITH AC POWER OFF. REMOVED AND REPLACED BATTERY PACK PER
- [SDR SCNA20250811313](https://openairdocs.org/sdr/SCNA20250811313), Aug 9, 2025: LIGHT. UNSECURE. THE EMERGENCY LIGHTING STRIP ON THE FLOOR IS NOT SECURED TO THE FLOOR ROW 12 & 13. RESECURED STRIP @ ROW 12 & 13 REF AMM 25-27-31. OK FOR SERVICE.
- [SDR SCNA20250425129](https://openairdocs.org/sdr/SCNA20250425129), Apr 21, 2025: LENS. DAMAGED. ON WALKAROUND FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS PUSHED OUT & LIGHT INOP. - RESOLUTION: RELAMPED L1 DOOR EMERGENCY EXIT (SLIDE) LIGHT, CHECKS GOOD
- [SDR SCNA20250221059](https://openairdocs.org/sdr/SCNA20250221059), Feb 20, 2025: SLIDE. PARTIAL DEPLOY. L1 DOOR SLIDE PARTIALLY DEPLOYED FROM SLIDE CANISTER. GIRT BAR WAS ARMED WHEN DOOR PARTIALLY OPENED. REF LOG PAGE 797561 ITEM 2 FOR SLIDE REPLACEMENT, REF 79756
- [SDR SCNA20250130035](https://openairdocs.org/sdr/SCNA20250130035), Jan 28, 2025: LATCH. STUCK. DEFECT 797311: FORWARD ALLEY EMERGENCY CABINET EQUIPMENT DOOR LATCH STUCK. RESOLUTION: LUBED LATCH FWD GALLEY CABINET DOOR LATCH. OPS CK GOOD REF AMM 25-64-00.
- [SDR SCNA20241104356](https://openairdocs.org/sdr/SCNA20241104356), Nov 1, 2024: EXTINGUISHER. NO TEST. DEFECT 734522: #2 FIRE EXTINGUISHING TEST FAILED. - - RESOLUTION: PERFORMED OVERHEAT DETECTION TEST, OPS CHECK GOOD. REF AMM 26-10-00 THIS CLEARS MEL 26-2-2 MDD
- [SDR SCNA20240816302](https://openairdocs.org/sdr/SCNA20240816302), Aug 7, 2024: SKIN. CORRODED. WORK ORDER FS240102: COROSION FOUND ON LH SIDE EXTERNAL FUSELAGE SKIN AT STA 917 BTWN STR21 AND STR22 L, LAV VENT. - - RESOLUTION: REMOVED CORROSION ON LH SIDE 
- [SDR SCNA20240813300](https://openairdocs.org/sdr/SCNA20240813300), Aug 6, 2024: REPAIR. UNKNOWN. WWORK ORDER FS 2400102: SCRATCH FOUND ON EXISTING REPAIR, L/H SIDE EXTERNAL FUSELAGE AFT OF L2 DOOR APPROX BS 1016 BTWN STR 12L AND STR 17L. - - CORRECTIVE ACTI
- [SDR SCNA20240708263](https://openairdocs.org/sdr/SCNA20240708263), Jul 3, 2024: UNION. LEAKING. CRUZ FLIGHT HYDRAULIC QTY ON SYSTEM A DROPPED TO 22%.PRESS STAYED NORMAL TILL T/R DEPLOYED. DROPPED TILL 1700 PRESS FOR A FEW SEC. REPLACED A HYD UNION AND HOSE
- [SDR SCNA20240624255](https://openairdocs.org/sdr/SCNA20240624255), Jun 21, 2024: HOLDER. LOOSE. DOOR 1L GIRT BAR HOLDER LOOSE. REMOVED DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-66-01. SHOT NEW RIVET IN GRIT BAR HOLDER IAW SRM 51-40-02. INSTALLED ESCAPE SLIDE IA
- [SDR SCNA202405170237](https://openairdocs.org/sdr/SCNA202405170237), May 9, 2024: BRACKET. LOOSE. R1 GIRT BAR BRACKETS ON DOOR ARE LOOSE. - - : ADJUSTED GIRT BAR BRACKETS REF AMM 25-66-00
- [SDR SCNA20240219046](https://openairdocs.org/sdr/SCNA20240219046), Feb 18, 2024: SIGN. DETACHED. EXIT LIGHT ABOVE 14F FELL OFF. INSTALLED EXIT SIGN COVER REF AMM 33-51--01-960--801.
- [SDR SCNA20240219040](https://openairdocs.org/sdr/SCNA20240219040), Feb 15, 2024: SIGN. DETACHED. DEFECT 752823: 2L DOOR EXIT FELL OFF ON LANDING. - RESOLUTION: RESECURED EXIT SIGH LIGHT COVER IAW AMM 33-51-01.
- [SDR SCNA20240214038](https://openairdocs.org/sdr/SCNA20240214038), Feb 8, 2024: SIGN. DETACHED. DEFECT 752815: EXIT SIGN LEFT SIDE AFT GALLEY FELL OFF. - RESOLUTION: RESECURED LH EXIT SIGN LENS ON AFT GALLEY IAW AMM 33-51-01. OK FOR SERVICE.
- [SDR SCNA20250407105](https://openairdocs.org/sdr/SCNA20250407105), Dec 22, 2023: STRINGER. CRACKED. WORK ORDER 77245, NR00142: HIDDEN DAMAGE: AFTER REMOVED ANGLE, CRACK ON STRINGER S-26R STA 500I WAS FOUND AT FORWARD CARGO COMPARTMENT. - RESOLUTION: STRINGER S
- [SDR SCNA20231205254](https://openairdocs.org/sdr/SCNA20231205254), Dec 1, 2023: UNKNOWN. UNKNOWN. ROW 16CBA EMER LIGHT INOP. R & R ROW 16ABC EMERGENCY LIGHT HOUSING ASSY IAW AMM 33-51-00. OPS CHECK GOOD
- [SDR SCNA20231205253](https://openairdocs.org/sdr/SCNA20231205253), Dec 1, 2023: UNKNOWN. UNKNOWN. ROW 14 CBA EMER LIGHT INOP. REPLACED LAMP IAW AMM 33-51-03. OPS CK GOOD.
- [SDR SCNA20231205252](https://openairdocs.org/sdr/SCNA20231205252), Dec 1, 2023: UNKNOWN. UNKNOWN. DEFECT W/O 83430 NRC00006 RH AFT OVERWING EXIT EMER LIGHT INOP - - RESOLUTION: RELAMPED OUTSIDE AFT R/H OVERWING EXIT LIGHT IAW 33-51-00.
- [SDR SCNA20231205251](https://openairdocs.org/sdr/SCNA20231205251), Nov 20, 2023: UNKNOWN. UNKNOWN. ROW 12D EMERGENCY LIGHT LENS MISSING. INSTALLED NEW LENS AT SEAT 12 D IAW AMM 33-51-03. OK FOR SERVICE.
- [SDR SCNA20231009230S](https://openairdocs.org/sdr/SCNA20231009230S), Oct 5, 2023: UNKNOWN. UNKNOWN. ON TAKEOFF, SOUND OF LEAKING AIR BEGAN DURING CLIMBOUT NEAR L2 WINDOW AND L1 DOOR. BECAME LOUDER WITH INCREASED SPEED. OVERWEIGHT LANDING 154,500 POUNDS. TOUCHD
- [SDR SCNA20231009230](https://openairdocs.org/sdr/SCNA20231009230), Oct 5, 2023: UNKNOWN. UNKNOWN. FLIGHT SCX343: L1 DOOR SQUEAL – CREW HELD SE OF KMSP TO BURN FUEL TO GET BELOW MAX LANDING WEIGHT – FLIGHT LANDED RWY 30L AT KMSP WITHOUT INCIDENT AND TAXIED TO
- [SDR SCNA20230713202](https://openairdocs.org/sdr/SCNA20230713202), Jun 17, 2023: UNKNOWN. UNKNOWN. DEFECT 770109: FA REPORTS 1 R GRIT BAR BRACKET LOOSE. - - - RESOLUTION: ADJUSTED GRIT BAR PER AMM 25-66-00.
- [SDR SCNA20230525163](https://openairdocs.org/sdr/SCNA20230525163), May 24, 2023: UNKNOWN. UNKNOWN. DEFECT 769274: DOOR 1R SLIDE IS NOT STORED CORRECTLY. - - - RESOLUTION: REMOVED AND RE-INSTALLED 1R EMERGENCY SLIDE IAW AMM 25-66-01 FIT CHECK GOOD.
- [SDR SCNA20230501141](https://openairdocs.org/sdr/SCNA20230501141), May 1, 2023: UNKNOWN. UNKNOWN. DEFECT 722637: R1 GIRT BAR WILL NOT STAY ATTACHED TO DOOR WHEN DISARMED. - - - RESOLUTION: ADJUSTED CLIP ON DOOR THAT SECURES GIRT BAR AS REQUIRED. OK FOR SERVI
- [SDR SCNA20230412124](https://openairdocs.org/sdr/SCNA20230412124), Apr 5, 2023: UNKNOWN. UNKNOWN. DEFECT W/O 78001 NON-ROUTINE CARD 0001: AFT SERVICE DOOR (RH REAR GALLEY DOOR): EXCESSIVE DISTANCE BETWEEN GIRT BAR AND LOWER EDGE OF SLIDE COVER. RESOLUTION: R
- [SDR SCNA20221109143S](https://openairdocs.org/sdr/SCNA20221109143S), Nov 8, 2022: NONE. NONE. DEFECT 714523: EMERGENCY LIGHT( EXTERIOR L1 DOOR) DOES NOT ILLUMINATE WHEN IN ON POSITION. RESOLUTION: RR"D BATTERY AND BATTERY [OWER SUPPLY IAW AMM 33-51-00. O
- [SDR SCNA20221109143I](https://openairdocs.org/sdr/SCNA20221109143I), Nov 8, 2022: NONE. NONE. DEFECT 714523: EMERGENCY LIGHT( EXTERIOR L1 DOOR) DOES NOT ILLUMINATE WHEN IN ON POSITION: RESOLUTION:
- [SDR SCNA20221107142S](https://openairdocs.org/sdr/SCNA20221107142S), Nov 4, 2022: BALLAST. FAILED. 14A EMERGENCY EXIT DOOR DOWN LIGHT INOP. REMOVED AND REPLACED BALLAST IAW B737800 AMM 33-29-00-0960-804. OSP CHECK GOOD. NO DEFECTS NOTED.
- [SDR SCNA20221107142I](https://openairdocs.org/sdr/SCNA20221107142I), Nov 4, 2022: NONE. NONE. DEFECT 714515: 14A EMERGENCY EXIT DOOR DOWN LIGHT INOP. RESOLUTION: (IN PROGRESS)
- [SDR SCNA20221017132S](https://openairdocs.org/sdr/SCNA20221017132S), Oct 12, 2022: NONE. NONE. DEFECT WORK ORDER 74176: AFT LEFT EMERGENCY LIGHTS INTERMITTENT WHEN USING AFT FA PANEL. RESOLUTION: COULD NOT DUPLICATE PER AMM 31-51-00. OPS CHECK GOOD.
- [SDR SCNA20221017132](https://openairdocs.org/sdr/SCNA20221017132), Oct 12, 2022: NONE. NONE. DEFECT WORK ORDER 74176 : RESOLUTION: COULD NOT DUPLICATE PER AMNM 31-51-00. OPS CHECK GOOD.
- [SDR SCNA20221007124](https://openairdocs.org/sdr/SCNA20221007124), Oct 7, 2022: LIGHT. INOPERATIVE. DEFECT 725566: EMERGENCY AREA LIGHT AT 31ABC, CEILING, IS INOP. RESOLUTION: R AND R'D THE EMERG. AREA LAMP AT 31ABC, CEILING, IAW AMM 33-51-03. OP CHK GOOD, OK 
- [SDR SCNA20220527065](https://openairdocs.org/sdr/SCNA20220527065), May 18, 2022: STIFFENER. CRACKED. DEFECT: RH HORIZONTAL STAB RIB AT STA 123.85 #3 STIFFENER IS CRACKED. RESOLUTION: REPAIRED RH HORIZONTAL STAB RIB CRACK AT STA 123.85 STIFFENER PER B737 SRM 55-
- [SDR SCNA20220527064](https://openairdocs.org/sdr/SCNA20220527064), May 18, 2022: STIFFENER. CRACKED. DEFECT: RH HORIZONTAL STAB RIB AT STA 92.70 #2 STIFFENER IS CRACKED. RESOLUTION: REPAIRED RH HORIZONTAL STAB RIB CRACK AT STA 92.70 STIFFENER PER B737 SRM 55-10
- [SDR SCNA20220527063](https://openairdocs.org/sdr/SCNA20220527063), May 18, 2022: RIB. CRACKED. DEFECT: RH HORIZONTAL STAB RIB AT STA 92.70 #1 STIFFENER IS CRACKED. RESOLUTION: REPAIRED RH HORIZONTAL STAB RIB AT STA 92.70 STIFFENER PER B737 SRM 55-10-09-2R
- [SDR SCNA20220527062](https://openairdocs.org/sdr/SCNA20220527062), May 18, 2022: RIB. CRACKED. DEFECT: LH HORIZONTAL STAB RIB AT STA 92.70 #3 STIFFENER IS CRACKED. RESOLUTION: REPAIRED #3 STIFFENER ON LH HORIZONTAL STAB RIB STATION 92.70 IAW B737-800SRM55
- [SDR SCNA20220527061](https://openairdocs.org/sdr/SCNA20220527061), May 18, 2022: RIB DOUBLER. CRACKED. DEFECT: LH HORIZONTAL STAB RIB AT STA 92.70#2 STIFFENER IS CRACKED. RESOLUTION: REPAIRED #2 STIFFENER ON LH HORIZONTAL STAB RIB STATION 92.70 IAW B737-800SRM-55

All 58: https://openairdocs.org/aircraft/N826SY/reports.md

## 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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