- Registered owner
- Sun Country Inc
- Location
- Minneapolis, MN
- Owner type
- Corporation
- Serial number
- 34410
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 27, 2018
- Certificate issued
- June 15, 2020
- Expires
- June 30, 2027
- Mode S code
- AB4515
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-7B26 model are included below.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1998 | 3 |
|---|---|
| 2000 | 1 |
| 2001 | 2 |
| 2002 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2014 | 1 |
| 2015 | 2 |
| 2018 | 4 |
| 2019 | 2 |
| 2021 | 2 |
| 2022 | 1 |
| 2023 | 1 |
Engine · CFM International CFM56-7B26 series
AD 2023-05-05Turbine Engine Compressor SectionAD 2022-02-03Turbine Engine Accessory DriveAD 2021-16-08Turbine SectionInformation bulletins that may apply · 1
Advisory, not mandatory.
Engine · CFM International CFM56-7B26 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairNTSB investigations
No NTSB investigations matched to N825SYMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 737-8F2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N825SYMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 737-8F2 aircraft
Service difficulty reports · 45
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SCNA20261014427Skin · crackedCRACK 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 SCNA20261014425Skin Panel · crackedINITIAL 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. (CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTION) IN REFERENCE JOB # 581. CARD: ENG-57SCA-11486. CRACK OSDR SCNA20261014424Skin · crackedCRACKS 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 PANEL KRAS 206, RIGHT WING. (CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTION) REF JOB 581. CARD:
See all 45 reportsSTCs that may be installed · 2
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · CFM International CFM56-7B26 series
STC SE04840NYInstallation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engineSTC SE03036CHApplication 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.