# Service difficulty reports: N713SY, cancelled Mar 1, 2024

A list on [N713SY, cancelled Mar 1, 2024](https://openairdocs.org/deregistered/N713SY-2024-03-01.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 4 · 196 reports

- [SDR SCNA20210302013](https://openairdocs.org/sdr/SCNA20210302013.md): Eec · faulted · Feb 28, 2021 · N713SY · Boeing 7377Q8 · Fuel Controlling System
  > BOTH EEC ALT LIGHTS WITH DISPLAY SOURCE 1 ILLUMINATED RAN QRH FOR ALT LIGHT & DISPLAY SOURCE 1. SUBSEQUENTLY INTERMITTANT LOSS OF VERT MODES VNAV, LVL CHANGE, V/S, AUTOPILOT, F/D, HYD SYS A INDICATION. SPD LMT ANNUNCIATION ILLUMINATED FMC 2 FROZE. EEC ALT LIGH
- [SDR SCNA20201117324](https://openairdocs.org/sdr/SCNA20201117324.md): Fairing · damaged · Nov 10, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > NR 1 FLAP AFT FAIRING HAS DAMAGE ON INNER SKIN. REPAIRED NR 1 FLAP AFT FAIRING INNER SKIN, IAW ER 20-03509 REV IR AND SC EA 57-0055.
- [SDR SCNA20201117298](https://openairdocs.org/sdr/SCNA20201117298.md): Skin · damaged · Nov 10, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > LT OUTBOARD FLAP LEADING EDGE PANEL 567AT DAMAGED. LT OUTBOARD FLAP LEADING EDGE PANEL 567AT FOUND TO BE OUT OF LIMITS, IAW SRM 57-53-01-1A-3 RECEIVED NEW FLAP LEAD EDGE. LOCATED, DRILLED, TOP COATED IAW SRM 51-40-05-0G-0 AMM 51-21-99-300-801.
- [SDR SCNA20201117297](https://openairdocs.org/sdr/SCNA20201117297.md): Fairing · damaged · Nov 10, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > LT WING NR 3 FLAP AFT FAIRING HAS DAMAGE ON INNER SKIN. REPAIRED LT WING NR 3 FLAP AFT FAIRING INNER SKIN, IAW ER 20-0352 REV IR AND SC EA 57-0054.
- [SDR SCNA20201117326](https://openairdocs.org/sdr/SCNA20201117326.md): Frame · damaged · Nov 9, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Frame
  > FRAME HOLE AT BS 992.8 LBL 55 WL 208 IS OUT OF ROUND. REPAIRED FRAME HOLE AT STA 992.8, LBL 55, WL 208, IAW ATS ER 20-03503 REV IR DATED 06-NOV-2020 AND SCA EA 53-0061.
- [SDR SCNA20201117325](https://openairdocs.org/sdr/SCNA20201117325.md): Frame · damaged · Nov 9, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Frame
  > FRAME HOLE AT BS 951.07 LBL 55 WL 208 IS OUT OF ROUND. REPAIRED FRAME HOLE AT STA 951.07, LBL 55, WL 208, IAW ATS ER 20-03506 REV IR DATED 06-NOV-2020 AND SCA EA 53-0062.
- [SDR SCNA20201117328](https://openairdocs.org/sdr/SCNA20201117328.md): Panel · damaged · Nov 6, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > RT WING INBOARD FLAP PANEL 653ET HAS DAMAGED HONEYCOMB ON LOWER SURFACE. REPAIRED DAMAGE TO HONEYCOMB ON LOWER (INNER) SURFACE OF RT WING INBOARD FLAP PANEL 653ET, PER SRM 51-70-10-2R-4.
- [SDR SCNA20201117327](https://openairdocs.org/sdr/SCNA20201117327.md): Panel · burned · Nov 5, 2020 · N713SY · Boeing 7377Q8 · Nacelle/Pylon, Plate/Skin
  > PYLON PANEL 441 ER IS BURNT INTO THE COMPOSITE MATERIAL. REPAIRED BURNT INTO THE COMPOSITE MATERIAL ON PYLON PANEL 441ER, IAW 737 SRM 54-50-70-2R-2 AND SRM 51-70-05 REPAIR 6.
- [SDR SCNA20201117322](https://openairdocs.org/sdr/SCNA20201117322.md): Panel · damaged · Nov 3, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 192F AFT INSIDE EDGE OF PANEL HEAVILY WORN. REPAIRED DAMAGE TO AFT INSIDE EDGE OF PANEL 192F IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 4D(1) TABLE 202.
- [SDR SCNA20201117320](https://openairdocs.org/sdr/SCNA20201117320.md): Panel · damaged · Nov 3, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 192HR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 192HR, IAW SRM 51-70-05-2R-8 PER SRM 53-40-70-2R-1 PARA 4D(1) TABLE 202.
- [SDR SCNA20201117318](https://openairdocs.org/sdr/SCNA20201117318.md): Panel · damaged · Nov 3, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 191FL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 191FL, IAW 737 SRM 53-30-70-2R-1 AND SRM 51-70-05 REPAIR 8.
- [SDR SCNA20201117302](https://openairdocs.org/sdr/SCNA20201117302.md): Floorbeam · corroded · Nov 3, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Floor Beam
  > CORROSION AROUND FASTENER ON FLOOR SUPPORT BEAM AT BS 950 LBL 50 WL 208. REMOVED DAMAGED FLOOR SUPPORT BEAM AT BS 950 LBL 50 WL 208 AND INSTALLED NEW FLOOR SUPPORT BEAM, PER SRM 51-40-02-0G-0 AND 2 EA CLIPS PER SRM 51-40-02-0G-0 AND DWG 147A5650 REV-C.
- [SDR SCNA20201117301](https://openairdocs.org/sdr/SCNA20201117301.md): Floorbeam · corroded · Nov 3, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Floor Beam
  > CORROSION AROUND FASTENER HOLE ON FLOOR SUPPORT BEAM AT BS 950 LBL 48 WL 208. REMOVED FLOOR SUPPORT BEAM AT BS 950 LBL 48 WL 208 DUE TO DAMAGE FOUND OUT OF LIMITS, PER SRM 53-70-51-1A-1. INSTALLED NEW FLOOR SUPPORT BEAM, PER SRM 51-40-02-0G-0 AND DWG 147A565
- [SDR SCNA20201117299](https://openairdocs.org/sdr/SCNA20201117299.md): Floorbeam · corroded · Nov 3, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Floor Beam
  > CORROSION AROUND FASTENER HOLE ON FLOOR BEAM AT BODY STATION 986.5 LBL 43 TO RBL 50 WL 208. REMOVED AND REPLACED FS 986.5 FLOOR BEAM "T" CAP (PREVIOUS REPAIR) RBL 55-LBL 55 WL 208, IAW SRM 51-40-02-0G-0, SRM 53-70-51-2R-4 AND SCA EC/TC ENG-53SCA-09268.
- [SDR SCNA20201117319](https://openairdocs.org/sdr/SCNA20201117319.md): Panel · damaged · Nov 2, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 192HL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 192HL, IAW SRM 51-70-05-2R-8.
- [SDR SCNA20201117317](https://openairdocs.org/sdr/SCNA20201117317.md): Panel · damaged · Nov 2, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 191FR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES ON PANEL 191FR, IAW 737 SRM 53-30-70-2R-1 AND SRM 51-70-04 REPAIR 9 AND 10.
- [SDR SCNA20201117316](https://openairdocs.org/sdr/SCNA20201117316.md): Panel · damaged · Nov 2, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 192AL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 53-40-70-2R-1, 51-70-05-2R-8.
- [SDR SCNA20201117315](https://openairdocs.org/sdr/SCNA20201117315.md): Panel · damaged · Nov 2, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 192AR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 53-40-70-2R-1, 51-70-05-2R-8.
- [SDR SCNA20201117311](https://openairdocs.org/sdr/SCNA20201117311.md): Panel · damaged · Nov 2, 2020 · N713SY · Boeing 7377Q8 · Wing, Plate/Skin
  > PANEL 671BB HAS MULTIPLE SCREW HOLES CRACKED/DAMAGED. REPAIRED DAMAGED SCREW HOLES ON PANEL 671BB, IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 4D TABLE 202.
- [SDR SCNA20201117313](https://openairdocs.org/sdr/SCNA20201117313.md): Torque Tube · chafed · Nov 1, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flap Control System
  > RT INBOARD MAIN FLAP HAS MINOR WEAR ON TORQUE TUBE AT INBOARD SIDE WITH MISSING CIC AND PRIMER. REWORK/REPAIR ACCOMPLISHED FOR TORQUE TUBE, IAW ENGINEERING TASK CARD 737-53-1264-01-GROUP 2.
- [SDR SCNA20201117323](https://openairdocs.org/sdr/SCNA20201117323.md): Fairing · damaged · Oct 31, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > NR 1 FLAP AFT FAIRING HAS DAMAGE AT LEADING EDGE. REPAIRED DAMAGE AT LEADING EDGE OF NR 1 AFT FLAP TRACK FAIRING, PER SRM 57-53-70-2R-5.
- [SDR SCNA20201117308](https://openairdocs.org/sdr/SCNA20201117308.md): Panel · damaged · Oct 30, 2020 · N713SY · Boeing 7377Q8 · Horizontal Stabilizer, Plate/Skin
  > PANEL 333EB SCREW HOLE DAMAGED. PANEL 333EB DAMAGED SCREW HOLE REPAIRED, IAW B737 SRM 55-10-01-2R-9 TABLE 203 AND IAW B737 SRM 51-70-05-2R-8.
- [SDR SCNA20201117307](https://openairdocs.org/sdr/SCNA20201117307.md): Retainer · corroded · Oct 30, 2020 · N713SY · Boeing 7377Q8 · Horizontal Stabilizer Structure
  > PANEL 333AB FIXED RUB STRIP CLAMP CORRODED IN MULTIPLE SPOTS. ORDERED AND RECEIVED NEW 186A3002-29 RETAINER AND 186A3004-3, -4 SEAL ASSEMBLYS FOR PANEL 333AB. TRANSFERED ORIGINAL HOLE PATTERN TO NEW RETAINER (RUB STRIP CLAMP), PER SRM 51-40-05 AND 51-40-08.
- [SDR SCNA20201117306](https://openairdocs.org/sdr/SCNA20201117306.md): Retainer · corroded · Oct 30, 2020 · N713SY · Boeing 7377Q8 · Horizontal Stabilizer Structure
  > PANEL 343AB FIXED RUB STRIP CLAMP CORRODED IN MULTIPLE SPOTS. ORDERED AND RECEIVED NEW 186A3002-30 RETAINER AND 186A3004-4 SEAL ASSEMBLY FOR PANEL 343AB. TRANSFERRED ORIGINAL HOLE PATTERN TO NEW RETAINER (RUB STRIP CLAMP) PER SRM 51-40-05 AND 51-40-08. INST
- [SDR SCNA20201117305](https://openairdocs.org/sdr/SCNA20201117305.md): Panel · damaged · Oct 30, 2020 · N713SY · Boeing 7377Q8 · Horizontal Stabilizer, Plate/Skin
  > PANEL 343CB HAS MULTIPLE DAMAGED SCREW HOLES. PANEL 343CB MULTIPLE DAMAGED SCREW HOLES REPAIRED, IAW B737 SRM 55-10-01-2R-9 TABLE 203 AND IAW B737 SRM 51-70-04-2R-9.
- [SDR SCNA20201117304](https://openairdocs.org/sdr/SCNA20201117304.md): Skin · worn · Oct 30, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > LT OUTBOARD AFT FLAP INBOARD EDGE HAS WEAR MARK 9 INCHES UP FROM TRAILING EDGE. REPAIRED WORN AREA 9 INCHES UP FROM TRAILING EDGE ON LT OUTBOARD AFT FLAP INBOARD EDGE, IAW SRM 57-53-01-2R-14 + SRM 51-70-10-2R-4.
- [SDR SCNA20201117303](https://openairdocs.org/sdr/SCNA20201117303.md): Skin · delaminated · Oct 30, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > LT WING OUTBOARD AFT FLAP INBOARD LOWER CORNER IS DELAMINATED. REPAIRED DELAMINATION INBOARD LOWER CORNER ON LT WING OUTBOARD AFT FLAP, IAW SRM 51-70-10-2R-4 57-53-01-2R-14.
- [SDR SCNA20201117295](https://openairdocs.org/sdr/SCNA20201117295.md): Panel · damaged · Oct 30, 2020 · N713SY · Boeing 7377Q8 · Nacelle/Pylon, Plate/Skin
  > LEFT PYLON PANEL 431ER COMPOSITE DAMAGED ALONG EDGE. LEFT PYLON PANEL 431ER COMPOSITE DAMAGE ALONG EDGE REPAIRED, IAW B737 SRM 54-50-70-2R-2 TABLE 202 AND IAW B737 SRM 51-70-05-2R-6.
- [SDR SCNA20201117321](https://openairdocs.org/sdr/SCNA20201117321.md): Panel · damaged · Oct 29, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 192E HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 51-70-04-2R-9 ON PANEL 192F.
- [SDR SCNA20201117314](https://openairdocs.org/sdr/SCNA20201117314.md): Skin · damaged · Oct 29, 2020 · N713SY · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 194CL HAS DAMAGED SCREW HOLE. REPAIRED DAMAGED SCREW HOLE ON PANEL 194CL, IAW SRM 51-70-04-2R-9.
- [SDR SCNA20201117312](https://openairdocs.org/sdr/SCNA20201117312.md): Panel · damaged · Oct 29, 2020 · N713SY · Boeing 7377Q8 · Wing, Plate/Skin
  > PANEL 671DB HAS MULTIPLE SCREW HOLES DAMAGED. REPAIRED MULTIPLE SCREW HOLES ON PANEL 671DB, PER SRM 51-70-05-2R-8.
- [SDR SCNA20201117309](https://openairdocs.org/sdr/SCNA20201117309.md): Panel · damaged · Oct 29, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > PANEL 571BB HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 57-51-01-2R-1, 51-70-05-2R-8.
- [SDR SCNA20201117296](https://openairdocs.org/sdr/SCNA20201117296.md): Skin · damaged · Oct 29, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > ACCOMPLISH PERMANENT REPAIR OF LT INBOARD FLAP OUTBOARD FAIRING CENTER SEAL FASTENER HOLES. ACCOMPLISHED PERMANENT REPAIR OF LT INBOARD FLAP TRACK FAIRING OUTBOARD CENTER BULB SEAL FASTENER HOLES, PER SRM 57-53-70-2R-2 PARA 5.
- [SDR SCNA20201117310](https://openairdocs.org/sdr/SCNA20201117310.md): Panel · damaged · Oct 28, 2020 · N713SY · Boeing 7377Q8 · Trailing Edge Flaps
  > PANEL 571AB HAS DAMAGED SCREW HOLE. REPAIRED DAMAGED SCREW HOLE ON PANEL 571AB, IAW 737 SRM 57-51-01-2R-1 AND SRM 51-70-05 REPAIR 8.
- [SDR SCNA20201117300](https://openairdocs.org/sdr/SCNA20201117300.md): Floor Panel · punctured · Oct 27, 2020 · N713SY · Boeing 7377Q8 · Fuselage Floor Panel
  > FLOOR PANEL 241YF HAS A PUNCTURE ON UPPER SURFACE. REPAIRED PUNCTURE ON UPPER SURFACE ON FLOOR PANEL 241YF, IAW SRM 53-00-50-2R-1.
- [SDR SCNA20190627107](https://openairdocs.org/sdr/SCNA20190627107.md): Closeout Panel · cracked · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CLOSE OUT PNL ON AFT SIDE OF LT WHEEL WELL CRACKED. REPAIRED CLOSE OUT PNL ON AFT SIDE OF LT WHEEL WELL.
- [SDR SCNA20190627106](https://openairdocs.org/sdr/SCNA20190627106.md): Floor Panel · damaged · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Floor Panel
  > FLOOR PANEL 222DF HAS 2 CORNERS DAMAGED. REPAIRED DAMAGED FLOOR PANEL 222DF (2 CORNERS).
- [SDR SCNA20190627105](https://openairdocs.org/sdr/SCNA20190627105.md): Floor Panel · damaged · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Floor Panel
  > FLOOR PANEL 232AF 4 CORNERS DAMAGED. REPAIRED DAMAGED FLOOR PANEL 232AF (4 CORNERS).
- [SDR SCNA20190627104](https://openairdocs.org/sdr/SCNA20190627104.md): Support Fitting · corroded · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA STA 344 LBL64 SUPPORT FITTING CORRODED. REMOVED CORRODED MOUNT AND INSTALLED NEW MOUNT.
- [SDR SCNA20190627103](https://openairdocs.org/sdr/SCNA20190627103.md): Mount · corroded · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Main, Attach Fittings
  > MAIN CABIN FWD WET AREA STA 312 LBL 64 SUPPORT MOUNT IS CORRODED. REMOVED CORRODED MOUNT AND INSTALLED NEW MOUNT.
- [SDR SCNA20190627102](https://openairdocs.org/sdr/SCNA20190627102.md): Intercostal · cracked · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA STA 270 TO 277 BL0 INTERCOSTAL CRACKED. REMOVED AND INSTALLED NEW WET AND MAIN CABIN FWD AREA STA 270 TO STA 277 BLO.
- [SDR SCNA20190627101](https://openairdocs.org/sdr/SCNA20190627101.md): Intercostal · cracked · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA STA 277 TO 294.5 BL0 INTERCOSTAL CRACKED. REMOVED AND INSTALLED NEW WET AND MAIN CABIN FWD AREA STA 277 TO 294.5 BLO.
- [SDR SCNA20190627100](https://openairdocs.org/sdr/SCNA20190627100.md): Floorbeam · corroded · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Main, Floor Beam
  > MAIN CABINFWD WET AREA STA 328 RBL 47 FLOORBEAM UPPER FLANGE SHOWS CORROSION. REMOVED AND REPLACED FLOORBEAM UPPER FLANGE AT STA 328 RBL 47.
- [SDR SCNA20190627099](https://openairdocs.org/sdr/SCNA20190627099.md): Floorbeam · corroded · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Main, Floor Beam
  > MAIN CABIN FWD WET AREA STA 328 RBL24 FLOORBEAM UPPER FLANGE CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER FLANGE ONBS 328 RBL0 TO.63.
- [SDR SCNA20190627098](https://openairdocs.org/sdr/SCNA20190627098.md): Intercostal · cracked · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA STA 312 TO 328 RBL 33 INTERCOSTAL IS CRACKED. REMOVED AND INSTALLED NEW WER IN MAIN CABIN FWD AREA STA 312-320 RBL 33.
- [SDR SCNA20190627097](https://openairdocs.org/sdr/SCNA20190627097.md): Floor Panel · damaged · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Floor Panel
  > DAMAGED FLOOR PANEL 231CF AT CORNER. REPAIRED DAMAGED FLOOR PANEL 231CF AT CORNER.
- [SDR SCNA20190627096](https://openairdocs.org/sdr/SCNA20190627096.md): Floor Panel · damaged · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Floor Panel
  > DAMAGED FLOOR PANEL 231BF AT CORNER. REPAIRED DAMAGED FLOOR PANEL 231 BF AT CORNER.
- [SDR SCNA20190627095](https://openairdocs.org/sdr/SCNA20190627095.md): Scuff Plate · cracked · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > AFT DOOR CARGO DOOR SCUFF-PLATE CRACKED. LOCATED AND DRILLED AFT DOOR CARGO DOOR SCUFF PLATE. INSTALLED NEW SCUFF PLATE.
- [SDR SCNA20190627094](https://openairdocs.org/sdr/SCNA20190627094.md): Shear Web · corroded · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > STATION 986.5 RT SIDE CLOSE OUT WEB HAS CORROSION ON TOP AND BOTTOM SIDE. REMOVED + REPLACED LT + RT SHEAR WEB FROM STATION 986-1016.
- [SDR SCNA20190627093](https://openairdocs.org/sdr/SCNA20190627093.md): Strap · corroded · Jun 27, 2019 · N713SY · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > AT STATION 1016 SHEAR WEB STRAP ON RT SIDE HAS CORROSION. REMOVED + REPLACED SHEAR WEB STRAP @ STA 1016 RT O/B.

Next page: https://openairdocs.org/deregistered/N713SY-2024-03-01/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 = 'N713SY' AND deregistration_id = 'N713SY-2024-03-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N713SY-2024-03-01/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, except the copies of manufacturers’ service documents, which belong to their rights holders.