# Service difficulty reports: N801SY

A list on [N801SY](https://openairdocs.org/aircraft/N801SY.md).

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

Page 1 of 5 · 217 reports

- [SDR SCNA20261008417](https://openairdocs.org/sdr/SCNA20261008417.md): Glowstrip · damaged · Oct 7, 2026 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > SELF-ILLUMINATING FLOOR PATH MARKING SYSTEM SECTION AT ROW 12 DEF IS PARTLY LOOSENED. FOUND TORN & SEPARATED FOAM FILLER. REPLACED SELF-ILLUMINATING FLOOR PATH MARKING SYSTEM SECTION FOAM FILLER AT ROW 12/13 DEF. REF AMM 33-51-16/401 AND CMM 33-51-07.
- [SDR SCNA20260717314](https://openairdocs.org/sdr/SCNA20260717314.md): Access Panel · worn · Jun 18, 2026 · N801SY · Boeing 7378Q8 · Vertical Stabilizer
  > WEAR ON LOWER SETTLEMENT AREA AT VERTICAL STABILIZER ACCESS PANEL NUMBER 323AL STA 1006 TO 1016 ORIGINAL THICKNESS: IS 0.063 IN AND MINIMUM REMAINING THICKNESS: IS 0.030 IN THEREFORE IT'S OUT LIMITS PER B737-800 SRM 55-30-01-1A-2 ALLOWABLE DAMAGE 2 PAR 4.B DE
- [SDR SCNA20260717313](https://openairdocs.org/sdr/SCNA20260717313.md): Access Panel · worn · Jun 18, 2026 · N801SY · Boeing 7378Q8 · Vertical Stabilizer
  > IN REFERENCE NRC 00216: WEAR ON LOWER SETTLEMENT AREA AT VERTICAL STABILIZER ACCESS PANEL NUMBER 323AL STA 1006 TO 1016 ORIGINAL THICKNESS: IS 0.063 IN AND MINIMUM REMAINING THICKNESS: IS 0.030 IN THEREFORE IT'S OUT LIMITS PER B737-800 SRM 55-30-01-1A-2 ALLOWA
- [SDR SCNA20260615247](https://openairdocs.org/sdr/SCNA20260615247.md): Bracket · corroded · Jun 13, 2026 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > AFTER REMOVAL FLOOR MOUNTED ESCAPE SLIDE BRACKETS, BRACKETS (8 EAS) WAS FOUND WITH CORROSION. REPLACED AND VERIFIED PER B737-800 AIPC 25-66-02-01 AND B737-800 AIPC 25-66-02-02
- [SDR SCNA20260715302](https://openairdocs.org/sdr/SCNA20260715302.md): Frame · cracked · Jun 10, 2026 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > WO 94270 NR00210: CRACK IN FRAME AT STA 312 & BTW S-5L & S-6L, PASSENGER CABIN. - - CRACK IN FRAME AT STA 312 & BTW S-5L & S-6L, PASSENGER CABIN WAS REPAIRED PER B737-800 SRM 53-10-07-2R-1 REPAIR 1.
- [SDR SCNA20260715301](https://openairdocs.org/sdr/SCNA20260715301.md): Skin · corroded · Jun 10, 2026 · N801SY · Boeing 7378Q8 · Fuselage Main, Plate/Skin
  > WO SEVERAL CORROSIONS ON UPPER FUSELAGE SKIN BETWEEN S-4L & S-4R AND B STA 1016 & B STA 1088, AREA COVERED PER VERTICAL STABILIZER. - - CORROSION ON UPPER FUSELAGE SKIN BETWEEN S-4L & S-4R AND B STA 1016 & B STA 1088, AREA COVERED PER VERTICAL STABILIZER WAS R
- [SDR SCNA20260715300](https://openairdocs.org/sdr/SCNA20260715300.md): Frame Angle · corroded · Jun 10, 2026 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > CORROSION FRAME CLIP (4EAS) ON STA 500H AND STGR26L TO 26R, (2EAS) ON STA 500G AND STGR 28L TO 26R, (1EA) ON STA 500C AND STGR 28R TO 27R, (2EAS) ON STA 500B AND STGR 27L TO 27R, (1EA) ON STA 500A AND STGR 28L TO 27L, (1EA) ON STA 500 AND STGR 28R TO 27R AT FW
- [SDR SCNA20260625263](https://openairdocs.org/sdr/SCNA20260625263.md): Frame · cracked · Jun 10, 2026 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > CRACK IN FRAME AT BS 312 & BTW S-5L & S-6L, PASSENGER CABIN. CRACK IN FRAME AT BS 312 & BTW S-5L & S-6L, PASSENGER CABIN WAS REPAIRED PER SRM 53-10-07-2R-1 REPAIR 1.
- [SDR SCNA20260715304](https://openairdocs.org/sdr/SCNA20260715304.md): Skin · cracked · Jun 9, 2026 · N801SY · Boeing 7378Q8 · Horizontal Stabilizer, Plate/Skin
  > WO 94270 NR00178: CRACK ON LOWER SKIN STAB STA = 101.90 AT RH HORIZONTAL STABILIZER. - - CRACK ON LOWER SKIN STAB STA = 101.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55--10-01-2R-11 REPAIR 11
- [SDR SCNA20260715303](https://openairdocs.org/sdr/SCNA20260715303.md): Stringer · corroded · Jun 9, 2026 · N801SY · Boeing 7378Q8 · Fuselage Main, Longeron/Stringer
  > WO 94270 NR0179: CORROSION ON STRINGER AT STA 847+10IN, S-23R. AFT CARGO COMPT. - - REJECT: PHYSICAL: WORK SIGNED OFF BUT NOT ACCOMPLISHED/OR PARTIALLY ACCOMPLISHED - IN REFERENCE TO WIP #2 WAS FOUND ELONGATED HOLES (6 LOCATIONS) ON EXTERNAL SKIN BTW STA 887+5
- [SDR SCNA20260529220](https://openairdocs.org/sdr/SCNA20260529220.md): Panel · detached · May 29, 2026 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > ROW 24-25 DEF EMERGENCY LIGHTNING PANEL FALLING DOWN. REATTACHED LOOSE PANEL REF MM 25-21-00. OK FOR SERVICE.
- [SDR SCNA20260424164](https://openairdocs.org/sdr/SCNA20260424164.md): Lamp · inoperative · Apr 21, 2026 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > LEFT FWD EMERG EXIT DOOR OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED LT FWD EMERG DOOR OVERWING LIGHT LAMP IAW 33-51-04. OPS CHECKED GOOD.
- [SDR SCNA20260213079](https://openairdocs.org/sdr/SCNA20260213079.md): Ring · dirty · Feb 12, 2026 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > R2 DOOR GIRT BAR STOWAGE RING BROKEN. INSPECTED GIRT BAR STOWAGE RING IAW AMM 25-66-01, FOUND TO BE DIRTY. CLEANED THE RING, NO OTHER DEFECTS FOUND. OK FOR SERVICE.
- [SDR SCNA20250905361](https://openairdocs.org/sdr/SCNA20250905361.md): Skin · cracked · Aug 28, 2025 · N801SY · Boeing 7378Q8 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED IN 2 SPOTS, 1 3/8, 1 1/4 AT STAB STATION 147.90 APPROX 24" AND 31" AFT OF FRONT SPAR. ACCOMPLISHED REPAIR OF CRACKED SPOTS ON 2 AREAS ON LEFT HORIZONTAL STABILIZER IAW B737 SRM 55-10-01-2R-11 AT STAB STATION 147.9
- [SDR SCNA20250829342](https://openairdocs.org/sdr/SCNA20250829342.md): Attach Angle · damaged · Aug 27, 2025 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > EMERGENCY LIGHT PANEL AT SEAT ROW 24, 25 DEF SAGGING / LOOSE. REPLACED MISSING BROKEN ATTACH CLIPS IAW MM 25-21-00. REATTACHED PANEL. OK FOR SERVICE.
- [SDR SCNA20250827339](https://openairdocs.org/sdr/SCNA20250827339.md): Battery Pack · no test · Aug 26, 2025 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > ROWS 12-22 DEF FAILED EMERGENCY BATTERY PACK FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR SCNA20250827337](https://openairdocs.org/sdr/SCNA20250827337.md): Battery Pack · no test · Aug 26, 2025 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROW 16-21 ABC FAILED EMERGENCY LIGHT BATTERY FUNCTION CHECK REMOVED AND REPLACED BATTERY PACK (M1694) AT ROW 13 ABC REF: AMM 33-51-06, REQUIRES OPERATIONAL CHECK. NOTE: EMERGENCY BATTERIES ON CHARGE UNTILL 1630 HRS. OPS CHECKED IAW MM 33-
- [SDR SCNA20250827336](https://openairdocs.org/sdr/SCNA20250827336.md): Battery Pack · no test · Aug 26, 2025 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > EMERGENCY LIGHTING FAILS 15 MINUTE MINIMUM ILLUMINATION CHECK ROWS 13-23 R/H CABIN. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE
- [SDR SCNA20250827335](https://openairdocs.org/sdr/SCNA20250827335.md): Battery Pack · no test · Aug 26, 2025 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > EMERGENCY LIGHTING FAILS 15 MINUTE MINIMUM ILLUMINATION CHECK ROWS 16-23 L/H CABIN. REMOVED AND REPLACED BATTERY PACK (M1694) AT ROW 13 ABC REF: AMM 33-51-06, REQUIRES OPERATIONAL CHECK. EMERGENCY BATTERIES ON CHARGE UNTILL 1630 HRS. OPS CHECKED IAW MM 33-51
- [SDR SCNA20250827334](https://openairdocs.org/sdr/SCNA20250827334.md): Battery Pack · no test · Aug 26, 2025 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > EMERGENCY LIGHTING FAILS 15 MINUTE MIMIMUM ILLUMINATION CHECK AT DOOR 1L. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR SCNA20250725271](https://openairdocs.org/sdr/SCNA20250725271.md): Girt Bar · loose · Jul 25, 2025 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > BOARDING DOOR GIRT BARS ARE LOOSE AND THE APRON IS TOO LONG ON THE RIGHT - TIGHTENED CLIP AND SECURED L1 DOOR GIRT BAR IAW AMM 25-66-01. GIRT BAR IS SECURED TO DOOR. OK FOR SERVICE.
- [SDR SCNA202507252271](https://openairdocs.org/sdr/SCNA202507252271.md): Girt Bar · loose · Jul 25, 2025 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > BOARDING DOOR GIRT BARS ARE LOOSE AND THE APRON IS TOO LONG ON THE RIGHT. - RESOLUTION: TIGHTENED CLIP AND SECURED L1 DOOR GIRT BAR IAW AMM 25-66-01. GIRT BAR IS SECURED TO DOOR. OK FOR SERVICE.
- [SDR SCNA20250617216](https://openairdocs.org/sdr/SCNA20250617216.md): Light · inoperative · Jun 17, 2025 · N801SY · Boeing 7378 · Emergency Lighting
  > 14ABC EMERGENCY EXIT ROW SIDE WALL LIGHT INOP. REPLACED LIGHT ASSY FOR 14ABC EMERGENCY EXIT ROW SIDE WALL LIGHT OPS CHECK GOOD REF AMM 33-21-00-960-807
- [SDR SCNA20250611205](https://openairdocs.org/sdr/SCNA20250611205.md): Flap System · faulted · Jun 10, 2025 · N801SY · Boeing 7378Q8 · Trailing Edge Flap Control System
  > DEFECT 808881: DURING APPROACH WHEN FLAPS SET TO FLAPS 30S, FLAP STOPPED AT 25 AND SHOWED AN ASSEMTRY QRH COMPLETED AND FLAPS LEFT IN POSITION AFTER LANDING (EMERGENCY DECLARED) - RESOLUTION: PERFORMED FSEU BITE NO ACTIVE FAULTS FOUND REF FIM 27-51 TASK 801 FO
- [SDR SCNA20240819303](https://openairdocs.org/sdr/SCNA20240819303.md): Hook · unsecure · Jul 29, 2024 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > DEFECT684360: BOARDING DOOR GIRT BAR HOOK ON DOOR (RT SIDE) NEEDS TIGHTINING. - - RESOLUTION: ADJUSTED L1 DOOR AFT GIRT BAR RETAINTER REF AMM 25-66-01. OK FOR SERVICE
- [SDR SCNA20240702261](https://openairdocs.org/sdr/SCNA20240702261.md): Girt Bar · loose · Jun 27, 2024 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > L1 GIRT BAR HOLDER IS LOOSE. ADJUSTED FWD GIRT BAR HOLDER ON L1 SLIDE CANISTER. REF AMM 25-66-00.
- [SDR SCNA20231010231](https://openairdocs.org/sdr/SCNA20231010231.md): Unknown · unknown · Oct 5, 2023 · N801SY · Boeing 7378Q8 · Escape Slide
  > DEFECT 758319: - L1 SLIDE COMING OUT OF THE TOP BOTTOM OF DOOR - - - RESOUTION - GIRT BAR HANGING OUT TO FAR RESECURED GIRT BAR VELCRO. REINSTALLED SLIDE PACK AND COVER IAW AMM 25-66-01
- [SDR SCNA20230622192](https://openairdocs.org/sdr/SCNA20230622192.md): Unknown · unknown · Jun 21, 2023 · N801SY · Boeing 7378Q8 · Pneumatic Distribution System
  > DEFECT 701216: CABIN ALTITUDE CLIMBING AT 300-400 FEET PER MINUTE AT FL240. WE CAUGHT THE RISING ALTITUDE. EMERGENCY DESCENT STARTED AND CABIN ALTITUDE WARNING SOUNDED. CABIN ALTITUDE CLIMBING AT 300-400 FEET PER MINUTE AT FL240. WE CAUGHT THE RISING ALTITU
- [SDR SCNA20230412125](https://openairdocs.org/sdr/SCNA20230412125.md): Unknown · unknown · Apr 6, 2023 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > DEFECT 745168: 2L EVACUATION SLIDE GRIT BAR WILL NOT STAY IN THE RETAINER. RESOLUTION: ADJUSTED RETAINER REF. AMM 25-61-00.
- [SDR SCNA20230123043S](https://openairdocs.org/sdr/SCNA20230123043S.md): Cabin Pressure · faulted · Jan 20, 2023 · N801SY · Boeing 7378Q8 · Cabin Pressure Control System
  > LOSS OF CABIN ALTITUDE, DIVERTING TO KMSY, MASKS WERE DEPLOYED. NO INJURIES TO PAX OR CREW. FLIGHT LANDED SAFELY, TAXIED TO GATE WITHOUT FURTHER ISSUE. MX ARRIVING ON SCENE TO TROUBLESHOOT.
- [SDR SCNA20230123043](https://openairdocs.org/sdr/SCNA20230123043.md): Warning Light · illuminated · Jan 20, 2023 · N801SY · Boeing 7378Q8 · Cabin Pressure Control System
  > CABIN ALTITUDE LIGHT ILLUMINATED IN FLIGHT WITH ACCOMPANYING CABIN DECOMPRESSION, UNABLE TO MANUALY MAINTAIN CABIN PRESSURE. PERFORMED FIM TASK 21-31 TASK 823 LEFT PACK PRESSURE SYSTEM WITHIN THE CHART ALSO DUAL PACK PRESSURIZE SYSTEM LEAK DOWN WAS HIGH ON
- [SDR SCNA20221031138](https://openairdocs.org/sdr/SCNA20221031138.md): None · none · Oct 30, 2022 · N801SY · Boeing 7378Q8 · Emergency Equipment
  > DEFECT 740681: F/A REPORTS DOOR 1R GIRT BAR BRACKET NEEDS TIGHTENING. RESOLUTION: SECURED GIRTBAR CLIPS REF AMM 25-66-01 OK FOR SERVICE.
- [SDR SCNA20221017130](https://openairdocs.org/sdr/SCNA20221017130.md): None · none · Sep 29, 2022 · N801SY · Boeing 7378Q8 · Emergency Lighting
  > DEFECT 721342: 15A EMERGENCY EXIT WALL LIGHT INOP. RESOLUTION: REPLACED 15A EMERGENCY WALL LAMP REF AMM 33-20-00. THIS CLEARS MEL 33-15-02 MDDR# 114273
- [SDR SCNA20221003122](https://openairdocs.org/sdr/SCNA20221003122.md): Light · inoperative · Sep 29, 2022 · N801SY · Boeing 7378 · Emergency Lighting
  > DEFECT 721342: 15A EMERGENCY EXIT WALL LIGHT INOP RESOLUTION: (IN PROGRESS)
- [SDR SCNA20223025020](https://openairdocs.org/sdr/SCNA20223025020.md): None · none · Jan 6, 2022 · N801SY · Boeing 7378 · Emergency Lighting
  > DEFECT: EMERGENCY EXIT LIGHTS GUARD OVER SWITCH DAMAGED. RESOLUTION: REMOVED AND REPLACED EMERGENCY EXIT LIGHT SW. GUARD. OPS CHECK NORMAL
- [SDR SCNA20211220102](https://openairdocs.org/sdr/SCNA20211220102.md): Flap System · faulted · Dec 12, 2021 · N801SY · Boeing 7378 · Trailing Edge Flap Control System
  > FLAP DISAGREE UNCOMMANDED FLAP RETRACTI0ON FROM,30 TO 25 AT 200 ON LANDING PERFORMED FIM TASK 27-51 TASK 830, NO DEFECTS NOTED. R & R FSEU PRECATUINARY REF AMM 27-51-01. OPS CHECKS GOOD FLAP DISAGREE- GO AROUND EXECUTED. LANDED SAFELY IN RFD
- [SDR SCNA20211220101](https://openairdocs.org/sdr/SCNA20211220101.md): Flap System · unknown · Dec 12, 2021 · N801SY · Boeing 7378 · Trailing Flap Position Indicating System
  > FLAP DISAGREE ON APPROACH. SELECTED FLAPS 30 AND FLAPS WERE VERIFIED AT 30. LATER WITHOUT EXCESSIVE SPEED FLAPS WENT TO 25 AND LOCKED OUT. PERFORMED FSEU BITE PROCEDURE. FOUND FAULT TE FLAP UC MSG NO. 27-51351. RESET FAULT AND PERFORMED TE ASSYM SKEW INDICATI
- [SDR SCNA20210208020](https://openairdocs.org/sdr/SCNA20210208020.md): Smoke Detector · false activation · Feb 6, 2021 · N801SY · Boeing 7378 · Smoke Detection
  > AFT LEFT LAVATORY SMOKE DETECTOR WHEN OFF ON APPROACH IN TO PUJ ABOUT 3000 AGL DECLAFRED EMERGENCY. FLIGHT ATTENDANT RESET SMOKE DETECTOR AND ALARM SILENCED. FLIGHT ATTENDANT SAID THERE WAS A SMELL ALSO ( LAVATORY SMOKE DETECTION SYSTEMS) R+R AFT LEFT SMOKE
- [SDR SCNA20201008141](https://openairdocs.org/sdr/SCNA20201008141.md): Strap · corroded · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Structure (General)
  > CORROSION FWD SERVICE DOOR INNER CHORD, INBOARD ATTACH STRAP BS 277-300 RBL 50 WL 207. REMOVED AND REPLACED FWD SERVICE DOOR INNER CHORD, INBOARD ATTACH STAP AT BS 277-300 RBL 50 WL 207, IAW DWG 141A8310 REV L AND SRM 51-40-02-0G-0.
- [SDR SCNA20201008140](https://openairdocs.org/sdr/SCNA20201008140.md): Frame · cracked · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > FRAME STA 480 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME BS 480 STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C 53SCA-10615 REV 00.
- [SDR SCNA20201008139](https://openairdocs.org/sdr/SCNA20201008139.md): Frame · cracked · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > FRAME STA 400 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8R. REPAIRED FRAM STA 400 STRINGER 8 RT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
- [SDR SCNA20201008138](https://openairdocs.org/sdr/SCNA20201008138.md): Frame · cracked · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > FRAME STA 480 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8R. REPAIRED FRAME BS 480 RT STRINGER 8, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
- [SDR SCNA20201008137](https://openairdocs.org/sdr/SCNA20201008137.md): Frame · cracked · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > FRAME STA 440 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8R. REPAIRED FRAME BS 440 STR 8 RT, PER ATS ER 20-03227 REV IR AND SCA ENG-53SCA-10615 REV 00.
- [SDR SCNA20201008136](https://openairdocs.org/sdr/SCNA20201008136.md): Frame · cracked · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > FRAME STA 500D IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME BS 500D STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C 53SCA-10615 REV 00.
- [SDR SCNA20201008135](https://openairdocs.org/sdr/SCNA20201008135.md): Frame · cracked · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > FRAME STA 440 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME STA 440 STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
- [SDR SCNA20201008134](https://openairdocs.org/sdr/SCNA20201008134.md): Frame · cracked · Sep 28, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Frame
  > FRAME STA 400 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME BS 400 STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
- [SDR SCNA20201008133](https://openairdocs.org/sdr/SCNA20201008133.md): Floorbeam · corroded · Sep 27, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM UPPER CAP BS 947 RBL 50 WL 208. REMOVED & REPLACED UPPER T CAP PREVIOUS REPAIR AT STA 947.5 RBL 50 WL 208, IAW SCA EA 53-0054 REV 00 AND ATS ER 20-03209 REV IR.
- [SDR SCNA20201008132](https://openairdocs.org/sdr/SCNA20201008132.md): Floorbeam · corroded · Sep 27, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT BS 947.5 HAS CORROSION AT RBL 5. REMOVED & REPLACED BS 947.5 UPPER T CAP PREVIOUS REPAIR AT RBL 5, IAW SCA EA 53-0054 REV 00 AND ATS ER 20-03209 REV IR.
- [SDR SCNA20201008131](https://openairdocs.org/sdr/SCNA20201008131.md): Floorbeam · corroded · Sep 27, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT BS 947.5 HAS CORROSION ON PREVIOUS REPAIR AT LBL 4. REMOVED & REPLACED BS 947.5 UPPER T CAP PREVIOUS REPAIR AT LBL 4, IAW SCA EA 53-0054 REV 00 AND ATS ER 20-03209 REV IR.
- [SDR SCNA20201008130](https://openairdocs.org/sdr/SCNA20201008130.md): Floorbeam · corroded · Sep 25, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT BS 986.5 HAS CORROSION FROM LBL 43 TO RBL 47.5. ACCOMPLISHED FLOOR BEAM REPAIR STA 986.5 RBL 50-LBL 50, IAW ATS ER 20-03204 REV IR DATED 09/24/2020 AND SUN COUNTRY EA 53-0053 REV 00.

Next page: https://openairdocs.org/aircraft/N801SY/reports.md?page=2

## 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 = 'N801SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N801SY/reports

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