# N816SY: 2001 Boeing 737-8Q8

- Status: Valid registration
- Airframe: [Boeing 737-8Q8](https://openairdocs.org/model/boeing-737-8q8) (registry code 13844BX, 189 seats)
- Engine: [CFM International CFM56-7B26 series](https://openairdocs.org/engine/cfm-international-cfm56-7b26-series) (registry code 13045)
- Serial number: 30637
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 13, 2011
- Certificate issued: March 4, 2021
- Expires: March 31, 2028
- Mode S code: AB214D
- 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=816SY
- Page: https://openairdocs.org/aircraft/N816SY

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 737-8Q8)

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 N816SY.

## 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 20121120025649I](https://openairdocs.org/incident/20121120025649I), Nov 20, 2012: Boeing 737-8Q8 (N816SY), Minneapolis, MN, Minor damage. The aircraft was parked at gate H3 of the msp airport terminal 2 (humphrey terminal). Deicing operations to remove frost were in process when a portion of the…

## Service difficulty reports (178, 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 SCNA20261015432](https://openairdocs.org/sdr/SCNA20261015432), Oct 14, 2026: LATCH. FAULTED. L2 DOOR SLIDE BUSTLE LATCH ASSY. WILL NOT BREAK OVER AND LOCK. REMOVED AND REPLACED LATCH ASSY AT DOOR L2 IAW AMM 25-66-01.
- [SDR SCNA20260713296](https://openairdocs.org/sdr/SCNA20260713296), Jul 12, 2026: ENGINE. FOD. NR 1 ENG VIB WENT TO 4.0 - RAN CHKLST, RETURNED TO MSP. DECLARED EMERGENCY BLEW OUTER MLG TIRE ON T/O. COMPLTD TIRE TREAD/BURST INSP IAW AMM 05-51-54. NO DEFECT
- [SDR SCNA20260623255](https://openairdocs.org/sdr/SCNA20260623255), Jun 19, 2026: SMOKE GOGGLES. CRACKED. SMOKE GOOGLES HAVE CRACK ON NOSE. PRIMARY OBSERVER SMOKE GOGGLES R&R REF AMM 25-64-00 OK FOR SERVICE THIS CLEARS MEL 25-11-1 MDDR# 139614
- [SDR SCNA20260603236](https://openairdocs.org/sdr/SCNA20260603236), Jun 3, 2026: LIGHT. UNSECURE. PHOTOLUMINESCENT ESCAPE PATH MARKING SYSTEM ALONG FLOUR AT ROWS 13-14 STRIP IS LOSE. RESECURED PHOTOLUMINESCENT FLOOR PATH AT SEATS 13 AND 14 DEF REF AMM 33-51-
- [SDR SCNA20260518203](https://openairdocs.org/sdr/SCNA20260518203), May 15, 2026: SKIN. DAMAGED. LIGHTING STRIKE STA 243.7 STR 1L. REMOVED AND REPLACED 1 SOLID RIVET AT FUSELAGE SKIN BS 234.7 STR 1L IAW SRM 53-00-01-2R-40 REPAIR 40 PARAG 4.
- [SDR SCNA20260518201](https://openairdocs.org/sdr/SCNA20260518201), May 15, 2026: NOT REPORTED. DAMAGED. LIGHTNING STRIKE TRANSFERRED TO W/O 104619 N/R-0001. COMPLETED PHASE 1 AND 2 AMM 05-51-19-210-804 AND AMM 05-51-19-210-805. ALL LIGHTING STRIKES ARE ON NON-ROUT
- [SDR SCNA20260513196](https://openairdocs.org/sdr/SCNA20260513196), May 12, 2026: GIRT BAR. NO DISCREPANCY. FA REPORTS DIFFICULTY WITH UNSEATING FWD ENTRY GIRT BAR FROM HANGER DURING ARMING PROCEDURE - - REMOVED AND INSTALLED GIRT BAR SMOOTH OPERATION IAW AMM 25-66-01
- [SDR SCNA20260102001](https://openairdocs.org/sdr/SCNA20260102001), Dec 31, 2025: SWITCH. BROKEN. EMERGENACY EXIT LIGHT SWITCH IN COCKPIT HAS BROKEN BLACK SWITCH GUARD. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GAURD IAW AMM 33-51-00.
- [SDR SCNA20251212483](https://openairdocs.org/sdr/SCNA20251212483), Dec 12, 2025: LIGHT. UNSECURE. ROW 12 ABC EMERGENCY FLOOR LIGHTING STRIP NEEDS TO BE RESECURED TO FLOOR
- [SDR SCNA20250828341](https://openairdocs.org/sdr/SCNA20250828341), Aug 25, 2025: STRIP. UNSECURE. FLOOR STRIP IN FWD GALLEY BETWEEN NICKLE BOARD AND AISLE RUNNER DAMAGED, TRIP HAZARD. REPLACED STRIP BETWEEN NICKLE BOARD AND AISLE RUNNER IAW AMM25-27-15 OK FO
- [SDR SCNA20250807296](https://openairdocs.org/sdr/SCNA20250807296), Aug 2, 2025: DOOR. STUCK. FWD GALLEY EMERGENCY EQUIPMENT DOOR STUCK CLOSED- PUSHED IN TO FAR. UNJAMMED DOOR OPERATED NORMALLY. OK FOR SERVICE REF AMM 25-24-15
- [SDR SCNA20250618218](https://openairdocs.org/sdr/SCNA20250618218), Jun 17, 2025: BRACKET. OUT OF ADJUST. DEFECT 814016: GIRT BAR BRACKETS STIFF ON L1 AND R1 DOORS. ADJUSTED GIRT BAR BRACKETS AND OPS CHECKS GOOD REF AMM 25-66-01.
- [SDR SCNA20250611204](https://openairdocs.org/sdr/SCNA20250611204), Jun 10, 2025: BRACKET. LOOSE. DEFECT 814002: BOTH FOWARD DOOR GIRT BAR BRACKETS LOOSE - RESOLUTION: ADJUSTED L1 AND R1 GIRT BAR BRACKETS REF AMM 25-66-01. OK FOR SERVICE
- [SDR SCNA20250423121](https://openairdocs.org/sdr/SCNA20250423121), Apr 16, 2025: DOOR. OPEN. LOUD VIBRATION HEARD AFTER TAKEOFF SUSPECTED GROUND CREW HEADSET AUDIOPANEL DOOR WAS LEFT OPEN OR CAME OPEN. - RESOLUTION: GROUND CREW REPORTED GROUND SERVICE D
- [SDR SCNA20250408107](https://openairdocs.org/sdr/SCNA20250408107), Apr 7, 2025: SKIRT. OUT OF POSITION. WORK ORDER 94406, NR00009: AFT GALLEY ENTRY DOOR , ESCAPE SLIDE SKIRT EXTENDS MORE THAN 10 INCHS AT BOTTOM OF DOOR AND CATCHES ON DOOR SILL. - RESOLUTION: REPOS
- [SDR SCNA20250321079](https://openairdocs.org/sdr/SCNA20250321079), Mar 21, 2025: LIGHT. LOOSE. SCNA20250321079 DEFECT 712156 AC 816: EXIT PATH FLOOR LIGHTING IS LOOSE NEAR 2 DEF. SECURED EXIT PATH FLOOR LIGHTING AT ROW 2 DEF REF AMM 35-27-31
- [SDR SCNA20250110010](https://openairdocs.org/sdr/SCNA20250110010), Jan 10, 2025: LIGHT. DETACHED. DEFECT 794782: AC RIGHT ROW 12 EMERGENCY TRACK LIGHTING SEPERATING FROM FLOOR. RESOLUTION: RESECURED EMER. TRACK LIGHTING REF AMM 33-51-16.
- [SDR SCNA20250807302](https://openairdocs.org/sdr/SCNA20250807302), Nov 23, 2024: RIB. CRACKED. CRACKS ON RIB STAB STA= 249.10 AT RH HORIZONTAL STABILIZER. CRACKS ON RIB STAB STA= 249.10 AT RH HORIZONTAL STABILIZER WERE REPAIRED PER ETI-737-24-176 REV 4 AN
- [SDR SCNA20241125376](https://openairdocs.org/sdr/SCNA20241125376), Nov 22, 2024: WIRE. ARCED. WORKORDER 80746, NON-ROUTINE 00004: INITIAL INSPECTION: SIGN OF ARCING ON BRAID WIRE UPPER EDGE OF WINDOW 1 RH AT FLIGHT COMPARTMENT.
- [SDR SCNA202405207240](https://openairdocs.org/sdr/SCNA202405207240), May 13, 2024: BUMPER. BROKEN. DOOR 2L SLIDE BUMPER PART BROKE OFF SLIDE BUMPER. (OPEN)
- [SDR SCNA202405170236](https://openairdocs.org/sdr/SCNA202405170236), May 7, 2024: BUMPER. BROKEN. : DOOR 2L SLIDE BUMPER PART BROKE OFF SLIDE BUMPER - - RESOLUTION: (OPEN DEFECT)
- [SDR SCNA20240429222](https://openairdocs.org/sdr/SCNA20240429222), Apr 28, 2024: SLIDE. DISLODGED. DOOR 1L SLIDE DROPPED OUT OF CASEING WHILE DOOR WAS BEING OPENED. REINSTALLED SLIDE PACK AND COVER 1L DOOR REF AMM 25-66-01.
- [SDR SCNA20240206029](https://openairdocs.org/sdr/SCNA20240206029), Feb 4, 2024: BRACKET. OUT OF ADJUST. GIRT BAR ON MAIN DOOR LOOSE FALLS OUT. ADJUSTED TENSION ON GRIT BAR HOLD BRACKET REF AMM 25-66-02.
- [SDR SCNA20230202052S](https://openairdocs.org/sdr/SCNA20230202052S), Feb 1, 2023: NOT ENTERED. NOT ENTERED. SCNA20230202052 SUPPLEMENT
- [SDR SCNA20230202052](https://openairdocs.org/sdr/SCNA20230202052), Feb 1, 2023: NOT ENTERED. NOT ENTERED. DEFECT 756124: NOSE GEAR CAME DOWN ON THE AFTER TAKEOFF CHECKLIST. NOSE GEAR LIGHT DISPLAYED RED THEN ONLY GREEN. LANDING GEAR DISAGREE CHECKLIST/QRH COMPLETE. 
- [SDR SCNA20221011127](https://openairdocs.org/sdr/SCNA20221011127), Oct 10, 2022: OVEN. SMOKE. DEFECT 725184: OVEN SMOKING WHILE COOKING SMELLS ELECTRICAL. RESOLUTION: CATERING REPLACED OVEN RACKS AND INSERT WITH CLEAN UNITS OPS CHECK GOOD IAW AMM 25-30-6
- [SDR SCNA20220926110](https://openairdocs.org/sdr/SCNA20220926110), Sep 22, 2022: HMU. FAULTED. NR 2 ENGINE HIGH VIB (MORE THAN 4.0) AND MOMENTARY SURGE. PERFORMED BORESCOPE OF #2 ENGINE BOOSTER SECTION AND LPT BLADES REF. AMM 72-00-00-200-803-F00, AND AMM
- [SDR SCNA20221003112](https://openairdocs.org/sdr/SCNA20221003112), Jun 1, 2022: BATTERY. INOPERATIVE. DEFECT WORK ORDER N/R-00016: EMERGENCY BATTERY AT M1694 INOP RESOLUTION: REMOVED, REPLACED AND TESTED EMERGENCY BATTERY AT M1694 IAW AMM B737 33-51-06-960-805, 
- [SDR SCNA20220414026](https://openairdocs.org/sdr/SCNA20220414026), Mar 17, 2022: NONE. NONE. DEFECT: AT ROWS 10 AND 11, LUMINESCENT LIGHT STRIP IS LOOSE RESOLUTION: REINSTALLED EMERGENCY FLOOR PATH STRIP REF. AMM 33-51-16.
- [SDR SCNA20220427040](https://openairdocs.org/sdr/SCNA20220427040), Feb 25, 2022: GIRT BAR. LOOSE. L2 GIRT BAR HOLDER LOOSE. RESOLUTION: ADJUSTED HOLDER REF AMM 25-66-00
- [SDR SCNA202217003](https://openairdocs.org/sdr/SCNA202217003), Feb 12, 2022: NONE. NONE. DEFECT SECTION 43 FUSELAGE SKIN GOUGED FROM BS414 TO BS438 AT S-20R. RESOLUTION: DAMAGE WAS TRIMMED OUT FROM BS414 TO BS438 AT STRINGER 20R. STRINGER 20R WAS FO
- [SDR SCNA20220217001](https://openairdocs.org/sdr/SCNA20220217001), Feb 12, 2022: NONE. NONE. TASK: TEMPORARY SKIN REPAIR INSTALLED STA 420 STR 20R. RESOLUTION: REMOVED TEMPORARY SKIN REPAIR AT BS 420 STR 20 AND INSTALLED 1 DOUBLER 2024-T3 .063", -2 TRIP
- [SDR SCNA20211208099SU](https://openairdocs.org/sdr/SCNA20211208099SU), Dec 5, 2021: WIRE. CHAFED. VERIFY THE WIRE INTEGRITY AT THE BELOW LISTED CONNECTORS AND MEGGER THE WIRING LOOKING FOR SHORTS. WHILE USING THE MEGGER METER. FOUND 3 TWISTED SHIELDED PAIR W
- [SDR SCNA20211208099](https://openairdocs.org/sdr/SCNA20211208099), Dec 5, 2021: SENSOR. FAULTED. DEFECT: HAD TRAILING EDGE FLAP DISAGREE ON APPROACH AFTER VECTORS INDICATED 0 WHEN LEVER SAET AT 15 RAN QRH THEN RECEIVED ASYMETRY RAN QRH AND LANDED RESOLUTION
- [SDR SCNA20211208098](https://openairdocs.org/sdr/SCNA20211208098), Nov 24, 2021: SENSOR. FAULTED. DEFECT: ON DEPARTURE THE FLAPS WOULD NOT RETRACT, PER QRH ALTERNATE FLAP EXTENSION WAS ATTEMPTED IMEDIATELY A TRAILING EDGE ASSYMETRY DEVELOPED ALT FLAP EXTENSI
- [SDR SCNA20211124097](https://openairdocs.org/sdr/SCNA20211124097), Nov 24, 2021: CIRCUIT BREAKER. TRIPPED. ON ARRIVAL FLAPS FAILED TO EXTEND. PER THE QRH ALETERNATE FLAP EXTENISON WAS ATTEMPTED. LEADING EDGE DEVICES EXTENTED BUT TRAILING EDGE FLAPS DID NOT. NOTIFIED 
- [SDR SCNA20211018084](https://openairdocs.org/sdr/SCNA20211018084), Oct 14, 2021: NONE. NONE. DEFECT: LANDING GEAR LEVER WILL NOT MOVE UP AFTER TAKEOFF RESOLUTION: FOUND GROUND SPOILER INTERLOCK VALVE LOWER SLIDER ASSY. DISCONNECTED . CONEECTED LOWER SLI
- [SDR SCNA2020031911013](https://openairdocs.org/sdr/SCNA2020031911013), Mar 11, 2020: CREASE BEAM. CORRODED. CORROSION ON SEVERAL POINTS AT LH CREASE BEAM WL 208 FROM STA 968 TO STA 1016 REMOVED AND REPLACED ON BS 1016 TO 900 LH CREASE BEAM PER B737-800 SRM 51-40-02.
- [SDR SCNA2020031903012](https://openairdocs.org/sdr/SCNA2020031903012), Mar 8, 2020: FLOORBEAM. CORRODED. CORROSION ON TCAP AT STA 986.5 FROM BL 0 TO BL 45L .REMOVED CORROSION ON T CAP BS986BL0TO BL45L FOUND TO BE OUT OFF LIMITS REPLACED T CAP PER WORK ORDERR 350084
- [SDR SCNA2020031916003](https://openairdocs.org/sdr/SCNA2020031916003), Feb 16, 2020: STRINGER. CORRODED. CORROSION FOUND AT AFT CARGO, AFT BULKHEAD UNDER WATER TANK.REPAIRED STRINGER CORROSION IN AFT CARGO UNDER WATER TANK PER B737-800 SRM 53-00-03 FIG 201 REINSTAL
- [SDR SCNA2020031915042](https://openairdocs.org/sdr/SCNA2020031915042), Feb 15, 2020: RIB. DAMAGED. LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB TURNBUCKLE LUG DAMAGED REPAIRED L/H WING I/B FIXED F/E DEFLECTION CONTROL RIB PER B737-800 SRM 57-5
- [SDR SCNA2020031914018](https://openairdocs.org/sdr/SCNA2020031914018), Feb 14, 2020: CREASE BEAM. CORRODED. CORROSION ON SEVERAL POINTS AT R1 DOOR CREASE BEAM BTW STA 328 TO STA 291.5REMOVED AND REPLACED R1 DOOR CREASE BEAM AT STA 328 TO STA 291.5 ALL WORK DONE IAW B7
- [SDR SCNA2020031914004](https://openairdocs.org/sdr/SCNA2020031914004), Feb 14, 2020: COUNTERBALANCE. CORRODED. RUDDER COUNTER BALANCE HAS EVIDENCE OF CORROSION.REMOVED AND REPLACED RUDDER COUNTER BALANCE WEIGHT IAW B737 SRM 51-40-02 REFER TO NR 3500849/3000/0009 FOR BALA
- [SDR SCNA2020031913041](https://openairdocs.org/sdr/SCNA2020031913041), Feb 13, 2020: CHANNEL. CORRODED. RAIL CHANNELS AT ST 767 LBL 3.0, LBL 8.1, LBL 12.5 AND LBL 17.24 HAVE SURFACE CORROSION AFT CARGO BAY REPAIRED RAIL CHANNELS AT ST 767, LBL 3.0, LBL 8-1, LBL 12
- [SDR SCNA2020031913038](https://openairdocs.org/sdr/SCNA2020031913038), Feb 13, 2020: FRAME. CORRODED. SURFACE CORROSION ON 3 EA FRAME ON COMPARTMENT FLOOR AT ST 767 REPAIRED 3EA CHANNEL FRAMES ON AFT COMPARTMENT AT S-1 767 ALL WORK DONE IAW B737-800 SRM 51-10-02
- [SDR SCNA2020031913006](https://openairdocs.org/sdr/SCNA2020031913006), Feb 13, 2020: CHANNEL. CORRODED. CORROSION ON Z CHANNEL BTW STA 986.5 AND STA 1006 AT BL 40R WL 208.REMOVED AND REPLACED Z CHANNEL ON BS986.5 AND 1006. AT BL 40 WLZ08. PER B737-800 SRM 51-40-02
- [SDR SCNA2020031913005](https://openairdocs.org/sdr/SCNA2020031913005), Feb 13, 2020: FLOORBEAM. CORRODED. CORROSION ON TCAP OF BEAM STA 986.5 FROM BL 0 TO BL 45R WL 208 REMOVED AND REPLACED TCAP ON BS 986.TO RBL 45 TO LBL 45, PER B7374 800 SRM 53-10-51 REP 4.
- [SDR SCNA2020031909023](https://openairdocs.org/sdr/SCNA2020031909023), Feb 9, 2020: INSERT. DAMAGED. MULTIPLE CORRODED INSERTS ON FLOOR PANEL 242 UF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 242UF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE ARR-ASR FORM SH
- [SDR SCNA2020031908040](https://openairdocs.org/sdr/SCNA2020031908040), Feb 8, 2020: DOOR FRAME. CRACKED. R1 DOOR CUT OUT FRAME LOWER SIDE FWD IS CRACK. REMOVED AND INSTALLED R1 DOOR FRAME IAW B737-800 SRM 51-40-02 STEP 4 AND 7.
- [SDR SCNA2020031908039](https://openairdocs.org/sdr/SCNA2020031908039), Feb 8, 2020: SCUFF PLATE. CRACKED. R1 SCUFF PLATE HAS A CRACK ON THE PLATE.R1 SCUFF PLATE P/N 141A8431-1 REPAIRED ON REPAIR ORDER 412614 IAW BAC5975 REV (N) DATED 12 SEP 2019 8130-3 FORM TRACKING

All 178: https://openairdocs.org/aircraft/N816SY/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 737-8Q8 aircraft: https://openairdocs.org/model/boeing-737-8q8/aircraft.md
- The CFM International CFM56-7B26 series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b26-series.md

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