# N808SY: 2005 Boeing 737-8BK

- Status: Valid registration
- Airframe: [Boeing 737-8BK](https://openairdocs.org/model/boeing-737-8bk) (registry code 13844FG, 149 seats)
- Engine: [CFM International CFM56-7B27 series](https://openairdocs.org/engine/cfm-international-cfm56-7b27-series) (registry code 13046)
- Serial number: 33021
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: June 15, 2014
- Certificate issued: June 15, 2020
- Expires: June 30, 2027
- Mode S code: AB013C
- 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=808SY
- Page: https://openairdocs.org/aircraft/N808SY

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 CFM56-7B27 model are included.

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

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

None in force.

### Matched by engine (CFM International CFM56-7B27 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 N808SY.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20050409007059I](https://openairdocs.org/incident/20050409007059I), Apr 9, 2005: Boeing 7378BK (N808SY), Fort Myers, FL, Minor damage. (-23) On 04/09/05, a sun country B-737-8BK, operating as flt. #381 inbound from msp, was on final approach to rsw r/w 24 when the aircraft encountered a…

## Service difficulty reports (102, 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 SCNA20261012422](https://openairdocs.org/sdr/SCNA20261012422), Oct 11, 2026: LIGHT. INOPERATIVE. LEFT FWD OVERWING EMERGECY EXIT DOOR HANDLE LIGHT INOP. OPEN
- [SDR SCNA20261012421](https://openairdocs.org/sdr/SCNA20261012421), Oct 11, 2026: LIGHT. INOPERATIVE. LEFT AFT OVERWING EMERGENCY EXIT DOOR HANDLE LIGHT INOPERATIVE. OPEN
- [SDR SCNA20260908383](https://openairdocs.org/sdr/SCNA20260908383), Sep 6, 2026: PIN. BROKEN. L2 DOOR SLIDE ASSY HAS BLOCKER, LATCH ASSY, BROKEN PIN. OPEN.
- [SDR SCNA20260831374](https://openairdocs.org/sdr/SCNA20260831374), Aug 28, 2026: ANGLE. FAULTED. R1 GIRT BAR ANGLE NOT FULLY SEATING GIRT BAR. ADJUSTED GIRT BAR CLIPS IAW AMM 25-66-01. OPS CHECKED GOOD.
- [SDR SCNA20260619252](https://openairdocs.org/sdr/SCNA20260619252), Jun 16, 2026: SLIDE. NO DISCREPANCY. BOARDING DOOR L1 SLIDE SEEMS OUT OF POSITION. INSPECTED L1 SLIDE ARM / DIDARM DOOR OPS CHECKS GOOD . REF AMM 2566-01 REV 89.
- [SDR SCNA20260505186](https://openairdocs.org/sdr/SCNA20260505186), May 4, 2026: SLIDE. NOT REPORTED. L2 DOOR OPENED BY CATERING WHILE DOOR WAS ARMED. REMOVED ESCAPE SLIDE PACK AND COVER IAW AMM 25-66-01. INSPECTED AND REINSTALLED ESAPE SLIDE PACK AND COVER IAW 
- [SDR SCNA20260428172](https://openairdocs.org/sdr/SCNA20260428172), Apr 27, 2026: LAMP. INOPERATIVE. EMERGANCY EXIT 2L, DOOR LIGHT INOP. REMOVED AND REPLACED FUSE AND LIGHT LAMP REF AMM 33-21-00. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR SCNA20260325137](https://openairdocs.org/sdr/SCNA20260325137), Mar 24, 2026: LIGHT. NO DISCREPANCY. R1 LAVATORY EMERGENCY EXIT LIGHT INOPERATIVE. PERFORMED OPS CHECK OF LAV CALL LIGHT REF. AMM 33-20-00, NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR SCNA20260119033](https://openairdocs.org/sdr/SCNA20260119033), Jan 16, 2026: LIGHT. LOOSE. FLOOR PATH LIGHT STRIP BETWEEN ROWS 10-12 ON LEFT SIDE LOOSE. RESECURED FLOOR PATH LIGHT STRIP REF AMM 33-51-16 OK FOR SERVICE
- [SDR SCNA20251024407](https://openairdocs.org/sdr/SCNA20251024407), Oct 22, 2025: BATTERY PACK. INOPERATIVE. R1 FWD DOOR, EMERGENCY EXIT LIGHTS (INTERIOR AND EXTERIOR) INOP REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD
- [SDR SCNA20251021397](https://openairdocs.org/sdr/SCNA20251021397), Oct 10, 2025: LAMP. INOPERATIVE. 14A EMERGENCY EXIT LIGHT NOT WORKING. RELAMPED 14A WINDOW LIGHT IAW AMM 33-21-00.
- [SDR SCNA20250915376](https://openairdocs.org/sdr/SCNA20250915376), Sep 4, 2025: PLATE. DAMAGED. COCKPIT DOOR POST SECURITY PLATE DAMAGED. FUSELAGE FRAME AT STA. 277 HAS A WEAR MARK FROM THE DOOR POST PLATE SHIM. COMPLIED WITH ATS ER 25-02572 REV: IR
- [SDR SCNA20250814318](https://openairdocs.org/sdr/SCNA20250814318), Aug 13, 2025: LIGHT. NO DISCREPANCY. EMERGENCY LIGHT STRIP DETACHED FROM FLOOR NEAR SEAT 12C. INSPECTED LIGHT STRIP AT 12C IAW AMM 25-27-21, NO ISSUE FOUND. OK FOR SERVICE.
- [SDR SCNA20250731293](https://openairdocs.org/sdr/SCNA20250731293), Jul 31, 2025: LIGHT. PEELING. ROW 12 -FLOOR FLORESENT STRIPS PEELING UPWARDS-BOTH SIDES. REINSTALLED FLOOR FLORESENT STRIPS AT ROW 12 BOTH SIDES REF AMM 33-51-13.
- [SDR SCNA20250707240](https://openairdocs.org/sdr/SCNA20250707240), Jul 6, 2025: BRACKET. LOOSE. DEFECT 801679: 1L DOOR GIRT BAR BRACKET IS LOOSE RESOLUTION: ADJUSTED GIRT BAR BRACKET REF AMM 25-66-00
- [SDR SCNA20250623221](https://openairdocs.org/sdr/SCNA20250623221), Jun 20, 2025: LIGHT. DETACHED. DEFECT 809392: PHOTOLUMINESCENT EMERGENCY LIGHT STRIP NEAR ROW 13 LIFTING OFF THE GROUND. RESECURED ESCAPE PATH STRIP REF AMM 25-22-00. THIS CLEARS MEL
- [SDR SCNA20250507169](https://openairdocs.org/sdr/SCNA20250507169), May 7, 2025: GLOWSTRIP. UNSECURE. LUMINESCENT STRIP LOOSE ROW 11 ABC - RE-SECURED LUMINESCENT FLOOR PATH STRIP AT ROW 11 ABC REF. AMM 33-51-16.
- [SDR SCNA20250407102](https://openairdocs.org/sdr/SCNA20250407102), Apr 4, 2025: SMOKE DETECTOR. FALSE ACTIVATION. DEFECT 769347: FWD LAV SMOKE DETECTOR WENT OFF - RESOLUTION: OPS CHECKED FWD LAV SMOKE DETECTOR REF AMM 26-14-00 OPS CHECKS GOOD.
- [SDR SCNA20250331083](https://openairdocs.org/sdr/SCNA20250331083), Mar 25, 2025: FLAP. LOOSE. WORKORDER 93998 NR00001: L2 DOOR SLIDE FLAP LOOSE AND CONTACTING SILL HARD ON CLOSING DOOR. - - RESOLUTION: REMOVED SLIDE AND REPACKED LOWER FLAP PER AMM REF 25
- [SDR SCNA20250325082](https://openairdocs.org/sdr/SCNA20250325082), Mar 24, 2025: SKIRT. LOOSE. DEFECT 769333: 2L DOOR SLIDE SKIRT SAGGING / DROOPING. HITS AIRCRAFT STRIKE PLATE WHEN CLOSING DOOR. 2L DOOR SLIDE SKIRT REPACKED REF AMM 25-66-00 GOOD FOR SERV
- [SDR SCNA20250226063](https://openairdocs.org/sdr/SCNA20250226063), Feb 24, 2025: GIRT BAR. UNPACKED. DEFECT WORK ORDER 93377 NR00004: L2 DOOR ESCAPE SLIDE GIRT NOT PROPERLY STOWED. - - RESOLUTION: REMOVED SLIDE ADJUSTED (STOWED) GIRT IN THE CORRECT POSITION.INS
- [SDR SCNA20250217054](https://openairdocs.org/sdr/SCNA20250217054), Feb 17, 2025: SMOKE DETECTOR. FALSE ACTIVATION. DEFECT 792517: FWD LAVATORY SMOKE ALLARM SOUNDED IN FLIGHT WILE PASSENGER WAS IN LAV. NO FIRE AND NO SMOKE PRESENT. PASSENGER STATED THEY WERE NOT VAPING OR SMO
- [SDR SCNA20250116020](https://openairdocs.org/sdr/SCNA20250116020), Jan 14, 2025: FITTING. CORRODED. ADAPTER PLATE OF FLOOR MOUNTED ESCAPE SLIDE BRAKETS L2 AND HARDWARE OF R2 WERE REPLACED PER B737-800 AMM 25-66-02
- [SDR SCNA20250404093](https://openairdocs.org/sdr/SCNA20250404093), Jan 13, 2025: PRESSURE BLKHD. CRACKED. INITIAL INSPECTION: CRACKS (2EAS) ON MLG WHEEL WELL PRESSURE DECK WEB STA 663 BTW LBL 33 & LBL 42. MLG WHEEL WELL PRESSURE DECK WEB STA 663 BTW LBL 33 & LBL 42 
- [SDR SCNA20250210047](https://openairdocs.org/sdr/SCNA20250210047), Jan 13, 2025: FLOORBEAM. CORRODED. WORK ORDER N808SY/2772/B737/H CHECK: - - INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR OF FLOOR STRUCTURE BEAM, STA= 986.5, STA= 986.5 BTW LBL 32 AND RBL 45 
- [SDR SCNA20250114012S](https://openairdocs.org/sdr/SCNA20250114012S), Jan 12, 2025: WINDSHIELD. NOT REPORTED. - Nº1 LH/RH WINDSHIELD WERE REPLACED PER B737-800 AMM 56-11-11
- [SDR SCNA20250114012](https://openairdocs.org/sdr/SCNA20250114012), Jan 12, 2025: WINDSHIELD. ARCED. ARCING ON HEAT FILM AT NR 1 LH/RH WINDSHIELD. RESOLUTION: (IN PROGRESS)
- [SDR SCNA20241114372](https://openairdocs.org/sdr/SCNA20241114372), Nov 3, 2024: LIGHT. DAMAGED. WORK ORDER 90968, NR00010: FLOOR SELF ILLUMINATING TRACK DAMAGED ROW 28 ABC TO 30ABC. REPAIR REF CMM 33-51-07 PAGE401 RESOLUTION: REPAIRED DAMAGED FLOOR TRACK R
- [SDR SCNA20241114371](https://openairdocs.org/sdr/SCNA20241114371), Nov 3, 2024: GLOWSTRIP. DAMAGED. WORK ORDER 90968, N/R00009: FLOOR SELF ILLUMINATING TRACK DAMAGED EXIT ROW 15DEF. RESOLUTION: REPAIRED DAMAGED FLOOR TRACK ROW 15DEF REF CMM 33-51-07.
- [SDR SCNA20240621254](https://openairdocs.org/sdr/SCNA20240621254), Jun 20, 2024: HEATER. DAMAGED. FWD CABIN CREW REPORTED SMELL OF SMOKE IN FLIGHT. FRONT 1/3 OF A/C WAS ABLE TO SMELL IT. WENT AWAY AS WE RAN THE SMOKE, FIRE OR FUMES CHECKLIST. PERFORMED FIM 2
- [SDR SCNA20240219039](https://openairdocs.org/sdr/SCNA20240219039), Feb 13, 2024: LENS. CRACKED. DEFECT WO 79966 NRC00232: SECONDARY FINDING, G 4 GALLEY BOTH L/H AND R/H EMERGENCY EXIT DOORWAY LIGHT LENS ARE CRACKED AND BROKEN. - RESOLUTION: REMOVED AND REP
- [SDR SCNA20240311148](https://openairdocs.org/sdr/SCNA20240311148), Jan 23, 2024: GUSSET. CRACKED. CRACKED GUSSET ASSY AT STA 500I, STR 19R. REMOVED GUSSET AT FCB, BS 5001, STR 19R, IAW SRM 51-40-02. 60240 01/24/2024 RECEIVED NEW GUSSET AND LOCATED AND DRILLE
- [SDR SCNA20240311147](https://openairdocs.org/sdr/SCNA20240311147), Jan 23, 2024: ATTACH BRACKET. CRACKED. LEFT WING DEFLECTION RIB ATTACH BRACKET IS CRACKED AT THE UPPER O/B FASTENER (MARKED). REMOVED AND REINSTALL LEFT WING DEFLECTION RIB BRACKET AT THE UPPER O/B I
- [SDR SCNA20240311146](https://openairdocs.org/sdr/SCNA20240311146), Jan 23, 2024: SIDEWALL SUPPORT. CORRODED. CORROSION AT SIDEWALL SUPPORT FRAME ATTACH ANGLE STA 500D, LBL 27 - LBL 36. REMOVED AND INSTALLED NEW SIDEWALL SUPPORT FRAME ATTACH ANGLE AT BS 500D, LBL 27-LBL
- [SDR SCNA20230307091I](https://openairdocs.org/sdr/SCNA20230307091I), Mar 6, 2023: NONE. NONE. DEFECT W/O 77387: 2R ESCAPE SLIDE COVER VISION WINDOW IS CRACKED IN 2 PLACES. RESOLUTION: (IN PROGRESS)
- [SDR SCNA20221021136](https://openairdocs.org/sdr/SCNA20221021136), Oct 21, 2022: NONE. NONE. DEFECT 740823: DOOR 1R GIRT BAR BRACKET LOOSE. RESOLUTION: ADJUSTED GIRT BAR BRACKET REF AMM 25-66-01.
- [SDR SCNA20221003121](https://openairdocs.org/sdr/SCNA20221003121), Sep 7, 2022: LIGHT. INOPERATIVE. DEFECT WORK ORDER N/R-00023: BURNED EMERGENCY EXIT LIGHT LATERAL WALL LAV A (1EA), CEILING PANEL GA LLEY 1 (1EA), HEADER PANEL ENTRY DOOR (1EA) AT FWD GALLEY AR
- [SDR SCNA20220622072](https://openairdocs.org/sdr/SCNA20220622072), Jun 21, 2022: DOOR LATCH. LOOSE. DEFECT 682588: FLIGHT DECK DOOR LATCH DIFFICULT TO GET BOLT TO CATCH RESOLUTION: OPENED AND CLOSED DOOR SEVERAL TIMES OPS NORMAL REF AMM 52-51-02
- [SDR SCNA20220414030](https://openairdocs.org/sdr/SCNA20220414030), Apr 13, 2022: NONE. NONE. DEFECT: AT FL 370 ENGINE #2 ROLLED BACK THRUST LEVER DID NOT RESPOND "RED EGT " BOX ILLUMINATED. RESOLUTION: PERFORMED FIM TASK 73-06 TASK 812 “AUTO DECELERATIO
- [SDR SCNA20210126004](https://openairdocs.org/sdr/SCNA20210126004), Jan 15, 2021: DOOR. WORN. PNEUMATIC ACCESS DOOR (192DR), WORN ON EDGES WHERE IT CONTACTS DOOR 192CR. FOUND DAMAGE ON HIGH PRESSURE CONNECT DOOR TO BE OUT OF LIMITS, PER SRM 53-40-70-1A-1
- [SDR SCNA20210126009](https://openairdocs.org/sdr/SCNA20210126009), Jan 12, 2021: FLOORBOARD. DAMAGED. FWD WET AREA FLOORBOARD P/N 141A5810-121 HAVE DAMAGE INSERTS. UPON FURTHER INVESTIGATION REPAIRED DAMAGE ON FWD WET AREA FLOORBOARD 141A5810-121 AND REPLACED DA
- [SDR SCNA20210126008](https://openairdocs.org/sdr/SCNA20210126008), Jan 12, 2021: FLOORBOARD. PUNCTURED. FWD WET AREA FLOORBOARD P/N 141A5810-558 HAS PUNCTURE. REPAIRED PUNCTURE ON FWD WET AREA FLOORBOARD 141A5810-558, PER SRM 53-00-50-2R-1.
- [SDR SCNA20210126007](https://openairdocs.org/sdr/SCNA20210126007), Jan 11, 2021: FLOOR PANEL. CORRODED. FLOOR PANEL BS 344-360 LBL 60 (P/N 141A5810-570) IS CORRODED AROUND FASTENER HOLES. INSTALLED NEW FLOOR PANEL P/N 141A5810-570) AT BS 344-360.
- [SDR SCNA20210126006](https://openairdocs.org/sdr/SCNA20210126006), Jan 11, 2021: SKIN. DAMAGED. HORIZONTAL STABILIZER REMOVABLE TIP 345A AFT LOWER RIVET SEPARATED FROM SKIN. REPAIRED RIVET HOLE ON AFT LOWER SEPERATED SKIN ON HORIZONTAL STABILIZER REMOVABLE
- [SDR SCNA20210126005](https://openairdocs.org/sdr/SCNA20210126005), Jan 7, 2021: ACCESS DOOR. WORN. RT ACCESS DOOR 192CR WORN WHERE PNEUMATIC DOOR (192DR) LATCHES CONTACT. REMOVED AND REPLACED ECS DOOR DOUBLER P/N 149A72244Y4 PO 804710, IAW SRM 51-40-02-0G-0.
- [SDR SCNA20190327030](https://openairdocs.org/sdr/SCNA20190327030), Mar 27, 2019: LAMP SOCKET. CORRODED. LT AFT OVERWING EMERGENCY EXIT LIGHT INOP, RT AFT GALLEY SERVICE DOOR (EXTERIOR) EMERGENCY EXIT LIGHT INOP. FOUND 465 OHMS OF RESISTANCE AT THE LAMP, CLEANED CO
- [SDR SCNA20190206026](https://openairdocs.org/sdr/SCNA20190206026), Feb 6, 2019: BATTERY PACK. DISCHARGED. R1 DOOR EMERGENCY LIGHT INOP. TROUBLESHOT, REMOVED AND REPLACED M1674 BATTERY PACK AND PERFORMED OPS CHECK. OPS CHECK GOOD.
- [SDR SCNA20190206025](https://openairdocs.org/sdr/SCNA20190206025), Feb 6, 2019: SCUFF PLATE. CRACKED. UPON REMOVAL OF AFT CARGO R/H SCUFF PLATE, FOUND PART TO BE CRACKED. LOCATED AND DRILLED NEW SERVICEABLE PART. INSTALLED.
- [SDR SCNA20190206024](https://openairdocs.org/sdr/SCNA20190206024), Feb 6, 2019: SHEAR WEB. CORRODED. R2 DOOR SHEAR WEB CORRODED AT STA 986.5 RBL32. R2 DOOR SHEAR WEB CORRODED & OUT OF LIMITS, REMOVED SHEAR WEB AND REPLACED WITH NEW.
- [SDR SCNA20190206023](https://openairdocs.org/sdr/SCNA20190206023), Feb 6, 2019: DOOR SILL. CORRODED. CORROSION FOUND UNDER SCUFF PLATE AT THE L1 DOOR LBL64 BETWEEN STA 312 AND 344. REMOVED & REPLACED CORRODED L1 DOOR MAIN LOWER SILL INNER CHORD.

All 102: https://openairdocs.org/aircraft/N808SY/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 CFM56-7B27 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 737-8BK aircraft: https://openairdocs.org/model/boeing-737-8bk/aircraft.md
- The CFM International CFM56-7B27 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b27-series.md

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