# Service difficulty reports: N825SY

A list on [N825SY](https://openairdocs.org/aircraft/N825SY.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SCNA20261014427](https://openairdocs.org/sdr/SCNA20261014427.md): Skin · cracked · Oct 8, 2026 · N825SY · Boeing 7378F2 · Horizontal Stabilizer, Plate/Skin
  > 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.md): Skin Panel · cracked · Sep 28, 2026 · N825SY · Boeing 7378F2 · Wing, Plate/Skin
  > 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. (CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTION) IN REFERENCE JOB # 581. CARD: ENG-57SCA-11486. CRACK O
- [SDR SCNA20261014424](https://openairdocs.org/sdr/SCNA20261014424.md): Skin · cracked · Sep 28, 2026 · N825SY · Boeing 7378F2 · Wing, Plate/Skin
  > 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 PANEL KRAS 206, RIGHT WING. (CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTION) REF JOB 581. CARD:
- [SDR SCNA20261014429](https://openairdocs.org/sdr/SCNA20261014429.md): Skin · cracked · Sep 27, 2026 · N825SY · Boeing 7378F2 · Horizontal Stabilizer, Plate/Skin
  > 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 REFERENCE TO TASK CARD ENG-55SCA-11150-RH, THE HORIZONTAL STAB WAS REPAIRED IAW SRM 55-10-01-2R-11, REPA
- [SDR SCNA20261014428](https://openairdocs.org/sdr/SCNA20261014428.md): Skin · cracked · Sep 27, 2026 · N825SY · Boeing 7378F2 · Horizontal Stabilizer, Plate/Skin
  > 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-11150-RH,
- [SDR SCNA20260928413](https://openairdocs.org/sdr/SCNA20260928413.md): Light Sys · faulted · Sep 27, 2026 · N825SY · Boeing 737800* · Emergency Lighting
  > 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 ON.
- [SDR SCNA20261020437](https://openairdocs.org/sdr/SCNA20261020437.md): Skin · cracked · Sep 26, 2026 · N825SY · Boeing 7378F2 · Horizontal Stabilizer, Plate/Skin
  > 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 LOWER SKIN AT STAB STA 129.50 COMMON TO THE HORIZONTAL RIBS, CRACK (1EA) AT STAB STA 138.70 COMMON TO TH
- [SDR SCNA20261014426](https://openairdocs.org/sdr/SCNA20261014426.md): Skin · cracked · Sep 26, 2026 · N825SY · Boeing 7378F2 · Horizontal Stabilizer, Plate/Skin
  > 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 REFERENCE TO TASK CARD ENG-55SCA-11150-LH, CRACK OF: L=0.750IN LENGTH ON LH HORIZONTAL STABILIZER LOWER
- [SDR SCNA20260914392](https://openairdocs.org/sdr/SCNA20260914392.md): Brake · leaking · Sep 14, 2026 · N825SY · Boeing 7378F2 · Landing Gear Brake System
  > 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.md): Lamp · inoperative · Aug 17, 2026 · N825SY · Boeing 7378F2 · Emergency Lighting
  > 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.md): Skirt · misinstalled · Jun 5, 2026 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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.md): Skirt · unpacked · May 29, 2026 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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.md): Downlock Sensor · faulted · May 15, 2026 · N825SY · Boeing 7378F2 · Landing Gear Position and Warning
  > AFTER TAKEOFF FWD GREEN RIGHT GEAR LIGHT REMAINED ILLUMINATED. OVHD GEAR LIGHTS WERE EXTINGUISHED. REMOVED AND REPLACED R/H GEAR DOWNLOCK SENSOR S0073. SENSOR ADJUSTMENT AND OPS TEST CHECKS GOOD. REF AMM 32-61-31. (EMRGENCY DECLARED)
- [SDR SCNA20260420163](https://openairdocs.org/sdr/SCNA20260420163.md): Wire · broken · Apr 19, 2026 · N825SY · Boeing 7378F2 · Light System Wiring
  > 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 REF AMM 33-21-00.
- [SDR SCNA20260420162](https://openairdocs.org/sdr/SCNA20260420162.md): Elec Connector · dirty · Apr 19, 2026 · N825SY · Boeing 7378F2 · Door System Wiring
  > 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 CONNECTOR D11072. NO VOLTAGE. REMOVED AND REPLACED BATTERY POWER SUPPLY REF AMM 33-51-06. NO HELP. BUT NOW
- [SDR SCNA20260420161](https://openairdocs.org/sdr/SCNA20260420161.md): Battery Pack · inoperative · Apr 19, 2026 · N825SY · Boeing 7378F2 · Emergency Lighting
  > 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.md): Lanyard · unsecure · Feb 12, 2026 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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. OK FOR SERVICE.
- [SDR SCNA20260210070](https://openairdocs.org/sdr/SCNA20260210070.md): Seat Back · damaged · Feb 9, 2026 · N825SY · Boeing 7378F2 · Passenger Compartment Equipment
  > SEAT BACK METAL PROTRUDING AND POCKET TORN. OPEN
- [SDR SCNA20251226508](https://openairdocs.org/sdr/SCNA20251226508.md): Retainer · unsecure · Dec 26, 2025 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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.md): Window Frame · cracked · Aug 26, 2025 · N825SY · Boeing 7378F2 · Fuselage Main, Structure
  > 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.md): Lens · broken · Jul 6, 2025 · N825SY · Boeing 737800* · Emergency Lighting
  > CENTER EMERGENCY EXIT LENS BROKEN - R & R CENTER EMERGENCY EXIT ROW LENS IAW AMM 33-51-01
- [SDR SCNA20250625229](https://openairdocs.org/sdr/SCNA20250625229.md): Retainer · loose · Jun 24, 2025 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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 SLIDE IAW AMM 25-66-01.INSPECTED SLIDE WHEN ITS INSTALLED REF AMM 25-66-01.
- [SDR SCNA20250407101](https://openairdocs.org/sdr/SCNA20250407101.md): Fire Detector · false activation · Apr 4, 2025 · N825SY · Boeing 7378F2 · Fire Detection
  > 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. - RESOLUTION: PERFORMED FIM 26-16 TASK 801 NO DEFECTS NOTED. REMOVED AND REPLACED AFT CARGO CEU IN REF. T
- [SDR SCNA20250128033](https://openairdocs.org/sdr/SCNA20250128033.md): Cover · broken · Jan 27, 2025 · N825SY · Boeing 7378F2 · Escape Slide
  > 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.md): Girt Bar · loose · Jan 16, 2025 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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. OPS CHECK GOOD OK FOR SERVICE.
- [SDR SCNA20250102001](https://openairdocs.org/sdr/SCNA20250102001.md): Aileron · lack of lube · Jan 1, 2025 · N825SY · Boeing 7378F2 · Aileron Control System
  > 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. CONTROLS REMAINED STIFF ON ROLL OUT UNTIL FLAPS RETRACTED. LUBRICATED AILERON POGO QUADRANT PER A
- [SDR SCNA20240725281](https://openairdocs.org/sdr/SCNA20240725281.md): Pressure Deck · cracked · Jul 12, 2024 · N825SY · Boeing 7378F2 · Fuselage Main, Structure
  > 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 REPAIR 6.
- [SDR SCNA20240725282](https://openairdocs.org/sdr/SCNA20240725282.md): Panel · damaged · Jul 11, 2024 · N825SY · Boeing 7378F2 · Wing, Plate/Skin
  > 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) ON BOTTOM SIDE OF PANEL WAS REPAIRED PER B737-800 SRM 51-70-05-2R-0 REPAIR GENERAL WITH REFERENCE T
- [SDR SCNA20241114367](https://openairdocs.org/sdr/SCNA20241114367.md): Light · detached · Jul 3, 2024 · N825SY · Boeing 7378F2 · Emergency Lighting
  > 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.md): Light · detached · Jul 3, 2024 · N825SY · Boeing 7378F2 · Emergency Lighting
  > 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.md): Door · cracked · Apr 23, 2024 · N825SY · Boeing 7378F2 · Accessory Compartment Doors
  > 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 53-10-15-2R-5 REPAIR 5
- [SDR SCNA20240329169](https://openairdocs.org/sdr/SCNA20240329169.md): Unknown · faulted · Mar 28, 2024 · N825SY · Boeing 7378F2 · Trailing Edge Flap Control System
  > 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.md): Unknown · unknown · May 9, 2023 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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.md): Girt Bar · out of adjust · Sep 15, 2022 · N825SY · Boeing 7378F2 · Emergency Equipment
  > 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.md): Light · inoperative · Sep 6, 2022 · N825SY · Boeing 7378 · Emergency Lighting
  > 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.md): Elevator System · interference · May 30, 2022 · N825SY · Boeing 7378F2 · Elevator Control System
  > 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 BITE. FOUND #1 SMYD FAULTED 3 TIMES ON LAST FLT LEGRPLACED #1 SYMD PER AMM 27-32-42 SND TESTED
- [SDR SCNA20220601](https://openairdocs.org/sdr/SCNA20220601.md): Elevator System · intermittent · May 30, 2022 · N825SY · Boeing 7378F2 · Elevator Control System
  > 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 BITE. FOUND #1 SMYD FAULTED 3 TIMES ON LAST FLT LEGRPLACED #1 SYMD PER AMM 27-32-42 SND TESTED
- [SDR SCNA202205044046](https://openairdocs.org/sdr/SCNA202205044046.md): Girt Bar · loose · Apr 30, 2022 · N825SY · Boeing 7378F2 · Passenger/Crew Doors
  > 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 BAR CLAMP TO SLIDE COVER. REINSTALLED SLIDE ON DOOR PER AMM 25-66-07.
- [SDR SCNA20220427035](https://openairdocs.org/sdr/SCNA20220427035.md): Girt Bar · loose · Apr 6, 2022 · N825SY · Boeing 7378F2 · Escape Slide
  > 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.md): None · none · Oct 12, 2021 · N825SY · Boeing 7378F2 · Fuselage Main, Structure
  > 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. 986.5 FLOOR BEAM PER SRM 53-70-51-2R-4, FIG 204.
- [SDR SCNA20211028092](https://openairdocs.org/sdr/SCNA20211028092.md): None · none · Oct 11, 2021 · N825SY · Boeing 7378F2 · Fuselage Structure (General)
  > 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 REPLACEMENT SHEER WEB PER PO 839525-SCA. LOCATED AND DRILLED REPLACEMENT SHEAR WEB PER SRM 51-40-05-0G-0
- [SDR SCNA20211028090](https://openairdocs.org/sdr/SCNA20211028090.md): None · none · Oct 9, 2021 · N825SY · Boeing 7378F2 · Fuselage Main, Structure
  > 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 BOEING DWG'S 140A9870 REV A AND DWG 147A7500 REV
- [SDR SCNA20211028088](https://openairdocs.org/sdr/SCNA20211028088.md): None · none · Oct 8, 2021 · N825SY · Boeing 7378F2 · Fuselage Main, Structure
  > 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.B, 7,D REV 73 AND DWG # 147A5700 REV. B
- [SDR SCNA20211028093](https://openairdocs.org/sdr/SCNA20211028093.md): None · none · Oct 6, 2021 · N825SY · Boeing 7378F2 · Fuselage Structure (General)
  > 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. 53-80-08-1A-1, 4F DETAIL D REV 73. REMOVED AND REPLACED NEW REPLACEMENT INTERCOSTAL IAW-B-737-SRM-51-40-
- [SDR SCNA20211028089](https://openairdocs.org/sdr/SCNA20211028089.md): None · none · Oct 6, 2021 · N825SY · Boeing 7378F2 · Fuselage Main, Structure
  > 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 FOUND IN SRM. REMOVED FLOOR SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED NEW FLOOR SUPPORT P/O# 839922/1 I

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N825SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N825SY/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
