# Service difficulty reports: N711SY, cancelled Mar 3, 2020

A list on [N711SY, cancelled Mar 3, 2020](https://openairdocs.org/deregistered/N711SY-2020-03-03.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 2 · 99 reports

- [SDR SCNA201910019183](https://openairdocs.org/sdr/SCNA201910019183.md): Skin · worn · Sep 24, 2019 · N711SY · Boeing 73773V · Leading Edge Devices
  > RH LE SLAT #7 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #7 SLAT REF AMM 27-81-21. INSPECTED INTERFACE, OK TO INSTALL. INSTALLED NEW SLAT IAW AMM 27-81-21-400-801. S
- [SDR SCNA2019100194182](https://openairdocs.org/sdr/SCNA2019100194182.md): Structure · worn · Sep 24, 2019 · N711SY · Boeing 73773V · Leading Edge Devices
  > #1 SLAT UNDER TRAILING EDGE HAS WORN ANTI ABRASION PAINT NUMEROUS SPOTS. OUTBOARD TRAILING EDGE WEAR IS BEYOND ALLOWABLE LIMIT AND WILL REQUIRE REPAIR PER SRM 57-42-01-2R-6 REPAIR 6. REPAIRED REF SRM 57-42-01-2R-6
- [SDR SCNA2019100194181](https://openairdocs.org/sdr/SCNA2019100194181.md): Skin · damaged · Sep 24, 2019 · N711SY · Boeing 73773V · Leading Edge Devices
  > RH LE SLAT #6 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND SRM REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #6 SLAT REF AMM 27-81-21. PERFORMED INTERFACE INSPECTION AND OK TO INSTALL NEW SLAT. INSTALLED NEW SLAT
- [SDR SCNA2019100194180](https://openairdocs.org/sdr/SCNA2019100194180.md): Structure · corroded · Sep 24, 2019 · N711SY · Boeing 73773V · Cargo/Baggage Doors
  > AFT CARGO DOOR, CORROSION ON LOWER AFT INSIDE CORNER NEXT TO INSULATION BUTTON. SEE SRM 52-30-01/1A01 FOR LIMITS. METAL THICKNESS.071 MATERIAL 7075T6. REMOVED CORROSION AT 2 LOCATIONS WITH CUTOUTS AT LOWER AFT CORNER AND LOWER INNER SKIN FWD OF AFT STOP FITTI
- [SDR SCNA2019100192179](https://openairdocs.org/sdr/SCNA2019100192179.md): Fastener · loose · Sep 24, 2019 · N711SY · Boeing 73773V · Wing Main, Frame Structure
  > LEFT WING, UPPER L/E 16 LOOSE FASTNERS FROM THE PYLON INBD. ALONG THE AFT SIDE OF PANEL. REMOVED 16 EA LOOSE FASTENERS ON L/H WING UPPER SKIN JUST INBD OF # 1 PYLON. REAMED HOLES TO 1ST OVER 3/16..199" OPEN HOLE AND COUNTER SINK HFEC ACCOMPLISHED BY NDI. NO C
- [SDR SCNA2019100194178](https://openairdocs.org/sdr/SCNA2019100194178.md): Spar · cracked · Sep 24, 2019 · N711SY · Boeing 73773V · Wing Spar
  > 11" CRACK ON WING CENTER SECTION REAR SPAR BETWEEN 45.64 AND 31.83 STIFFENERS. COMPLETED INTERIM REPAIR IAW SRM 57-10-10-2R-2 PARAGRAPH 6. ITEM WILL BE PLACED ON GMM/MTI FOR TRACKING PURPOSES FOR A DETAILED VISUAL INSPECTION EVERY 3,000 FLIGHT CYCLES. IF ADDIT
- [SDR SCNA201906219072](https://openairdocs.org/sdr/SCNA201906219072.md): Support · damaged · Jun 19, 2019 · N711SY · Boeing 73773V · Wing Miscellaneous Structure
  > RIGHT MLG SIDE STAY IS RUBBING INTO THE LOWER BEAM SUPPORT AND INTO THE THIRD ROD END SUPPORT MOUNT. REF TASK CARD FOR FIXED T/E PANEL WEAR. REMOVED AND REPLACED ROD SUPPORT AND RECONNECTED ROD.
- [SDR SCNA201902152027](https://openairdocs.org/sdr/SCNA201902152027.md): Battery · inoperative · Feb 12, 2019 · N711SY · Boeing 73773V · Emergency Lighting
  > FWD WINDSCREEN EMERGENCY PATH LIGHT INOP. R+R'D FORWARD L/A PWR SUPPLY BATTERY. OPS CHECK OK.
- [SDR SCNA201809176108](https://openairdocs.org/sdr/SCNA201809176108.md): Battery · discharged · Sep 16, 2018 · N711SY · Boeing 73773V · Emergency Lighting
  > EMERGENCY EXIT LIGHT L2, OVERHEAD INOP. R&R BATTERY L2 DOOR AND OVERHEAD EXIT LIGHT. OPS CHECK GOOD.
- [SDR SCNA20180830103](https://openairdocs.org/sdr/SCNA20180830103.md): Battery Pack · discharged · Aug 30, 2018 · N711SY · Boeing 73773V · Emergency Lighting
  > RT AFT EXTERIOR EMG LIGHT AND INTERER EXIT LIGHT INOP. R/R BATTERY PACK. OPS CHK GOOD.
- [SDR SCNA20180426080](https://openairdocs.org/sdr/SCNA20180426080.md): Structure · cracked · Apr 26, 2018 · N711SY · Boeing 73773V · Leading Edge Devices
  > FOUND A CRACK ON THE NR 2 LT LE SLAT. LENGTH OF CRACK IS 1.125 INCH. THE CRACK IS ACCEPTABLE TO FLY FOR 50FC. REMOVED AND REPLACED THE NR 2 LT L/E SLAT. OK FOR SERVICE.
- [SDR SCNA20180330074](https://openairdocs.org/sdr/SCNA20180330074.md): Light · inoperative · Mar 30, 2018 · N711SY · Boeing 73773V · Emergency Lighting
  > 9ABC EMERGENCY LIGHT INOP. PLACED 9ABC EMERGENCY AISLE LIGHT ON MEL. R&R THE INOP EMER LIGHT BULB AT 9ABC. OP CHECK GOOD. THIS CLEARS MEL.
- [SDR 2018F00062](https://openairdocs.org/sdr/2018F00062.md): Pump · failed · Dec 10, 2017 · N711SY · Boeing 7378Q8 · Hydraulic Pump (Electric/Engine), Main
  > LOST OF HYDRAULIC SYSTEM "B" INFLIGHT. POP OUT CIRCUIT BREAKERS ENGINE 2 PUMP DEPRESS VALVE 1 AND SYST "B" STANDBY RUDDER. (QRF RETURN TO AIRPORT). CORRECTIVE ACTION:HAS BEEN CHANGED EDP SYST "B" ENGINE 2 AND CHANGED FILTER SYSTEM B.
- [SDR SCNA20170901160](https://openairdocs.org/sdr/SCNA20170901160.md): Skin · dented · Sep 1, 2017 · N711SY · Boeing 73773V · Fuselage Main, Plate/Skin
  > FUSELAGE DENT LOCATED NEAR LAV SERVICE DOOR. REMOVED DENT DAMAGE AT LAV SERVICE DOOR STA 834 BELOW STR 22L AND REPAIRED.
- [SDR SCNA20161001231](https://openairdocs.org/sdr/SCNA20161001231.md): Light · inoperative · Oct 1, 2016 · N711SY · Boeing 73773V · Emergency Lighting
  > AFT EMERGENCY LIGHT IN HORSESHOE PANEL INOPERATIVE. REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR SCNA20161001230](https://openairdocs.org/sdr/SCNA20161001230.md): Floorboard · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Floor Panel
  > FLOORBOARD IS CORODED AT RBL 16, BS 966.
- [SDR SCNA20161001229](https://openairdocs.org/sdr/SCNA20161001229.md): Floor Panel · damaged · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Floor Panel
  > FORWARD CABIN FLOOR PANEL 141A5810-56 HAS CORNER BROKEN OFF. REPAIRED THE FLOOR PANEL.
- [SDR SCNA20161001228](https://openairdocs.org/sdr/SCNA20161001228.md): Floor Panel · damaged · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Floor Panel
  > FORWARD CABIN FLOOR PANEL 141A5810-484 HAS TWO AREAS WHERE THE UPPER LAYER OF FIBERGLASS IS MISSING. REPAIRED THE FLOOR PANEL.
- [SDR SCNA20161001227](https://openairdocs.org/sdr/SCNA20161001227.md): Floor Panel · damaged · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Floor Panel
  > FORWARD CABIN FLOOR PANEL 141A5810-464 HAS SEVERAL MISSING AND CORRODED INSERTS. REPAIRED THE CABIN FLOOR PANEL.
- [SDR SCNA20161001226](https://openairdocs.org/sdr/SCNA20161001226.md): Floor Panel · damaged · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Floor Panel
  > FWD CABIN FLOOR PANEL 141A5810-185 HAS EDGE DAMAGE. REPAIRED FWD CABIN FLOOR PANEL.
- [SDR SCNA20161001225](https://openairdocs.org/sdr/SCNA20161001225.md): Insert · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Floor Panel
  > FORWARD CABIN FLOOR PANEL 141A5810-185 HAS SEVERAL MISSING AND CORRODED INSERTS. REPAIRED FORWARD CABIN FLOOR PANEL 141A5810-185.
- [SDR SCNA20161001224](https://openairdocs.org/sdr/SCNA20161001224.md): Insert · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Floor Panel
  > FORWARD CABIN FLOOR PANEL 141A5810-245 HAS SEVERAL CORRODED INSERTS. REPLACED THE INSERTS.
- [SDR SCNA20161001223](https://openairdocs.org/sdr/SCNA20161001223.md): Crease Beam · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Main, Structure
  > CREASE BEAM CORRODED IN SEVERAL PLACES FROM BS 947.5 TO 986.5. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMIT. INSTALLED A NEW CREASE BEAM.
- [SDR SCNA20161001222](https://openairdocs.org/sdr/SCNA20161001222.md): Nut Plate · missing · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Main, Attach Fittings
  > BL 0 INTERCOSTAL MISSING ONE NUTPLATE BS 927 TO 947. INSTALLED A NEW NUT PLATE.
- [SDR SCNA20161001221](https://openairdocs.org/sdr/SCNA20161001221.md): Floor Support · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED LBL 20 UPPER FLANGE AFT HOLE BS 967 TO 947. REMOVED CORROSION, ORIGINAL T=.090, AFTER BLENDING T=.059,.031 MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.
- [SDR SCNA20161001220](https://openairdocs.org/sdr/SCNA20161001220.md): Floorbeam · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Main, Floor Beam
  > BS 986 FLOORBEAM CORRODED ON UPPER SURFACE UPPER FLANGE PREVIOUS REPAIR BL 0 TO LBL 45. REMOVED CORROSION IAW EA.
- [SDR SCNA20161001219](https://openairdocs.org/sdr/SCNA20161001219.md): Floorbeam · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Main, Floor Beam
  > BS 986 FLOORBEAM CORRODED ON UPPER SURFACE UPPER FLANGE PREVIOUS REPAIR BL 0 TO RBL 45. REMOVED CORROSION IAW EA.
- [SDR SCNA20161001218](https://openairdocs.org/sdr/SCNA20161001218.md): Floorbeam · corroded · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Main, Floor Beam
  > BS 966 FLOORBEAM CORRODED AT RBL 27. REPAIRED THE FLOORBEAM.
- [SDR SCNA20161001217](https://openairdocs.org/sdr/SCNA20161001217.md): Floorbeam · damaged · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Main, Floor Beam
  > FLOORBEAM BS 312 UPPER FLANGE HAS SCRIBE LINES AND CORROSION FROM LBL 5 TO 52. REPAIRED THE FLOORBEAM.
- [SDR SCNA20161001214](https://openairdocs.org/sdr/SCNA20161001214.md): Intercostal · cracked · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT RBL 32 STA 312 TO 328 IS CRACKED ON UPPER FLANGE AT FWD HOLE INTO THE RADIUS. REMOVED AND REPLACED INTERCOSTAL AT RBL 32 STA. 312 TO 328.
- [SDR SCNA20161001213](https://openairdocs.org/sdr/SCNA20161001213.md): Intercostal · cracked · Oct 1, 2016 · N711SY · Boeing 73773V · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STA 328 TO 312 AT RBL16 IS CRACKED AT AFT HOLE ON UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL AT STA 312 TO 328 RBL 16.
- [SDR SCNA20160930212](https://openairdocs.org/sdr/SCNA20160930212.md): Window Frame · cracked · Sep 30, 2016 · N711SY · Boeing 73773V · Fuselage Main, Structure
  > R1 WINDOW FRAME, UPPER O/B CORNER AT MOST UPPER I/B ATTACH FASTENER HOLE TO #2 WINDOW FRAME, CRACK INDICATION IN HOLE, HOLE MARKED IN BLACK. REMOVED DAMAGE TO R/H FLIGHT DECK #1 WINDOW FRAME AND REPAIRED.
- [SDR SCNA20160930211](https://openairdocs.org/sdr/SCNA20160930211.md): Window · cracked · Sep 30, 2016 · N711SY · Boeing 73773V · Flight Compartment Windows
  > R1 WINDOW HAS A CRACK INDICATION ON UPPER RIGHT HAND CORNER. END OF CRACK INDICATION MARKED IN BLACK ON FLIGHT DECK SIDE. RESTORED R/H #1 WINDOW FRAME CRACK ON UPPER R/H CORNER. OPS AND LEAK CHECK GOOD.
- [SDR SCNA20160930210](https://openairdocs.org/sdr/SCNA20160930210.md): Window Frame · cracked · Sep 30, 2016 · N711SY · Boeing 73773V · Fuselage Main, Structure
  > L1 WINDOW FRAME, UPPER O/B CORNER AT MOST UPPER I/B ATTACH FASTENER HOLE TO #2 WINDOW FRAME, CRACK INDICATION IN HOLE, HOLE MARKED IN BLACK. REPAIRED L/H FLIGHT DECK #1 WINDOW FRAME UPPER O/B CORNER.
- [SDR SCNA20160930209](https://openairdocs.org/sdr/SCNA20160930209.md): Window Frame · cracked · Sep 30, 2016 · N711SY · Boeing 73773V · Fuselage Main, Structure
  > L1 WINDOW FRAME HAS A CRACK INDICATION ON UPPER LEFT HAND CORNER. END OF CRACK INDICATION MARKED IN BLACK. RESTORED L/H #1 WINDOW FRAME CRACK ON UPPER LEFT HAND CORNER. OPS AND LEAK CHECK GOOD.
- [SDR SCNA20160930208](https://openairdocs.org/sdr/SCNA20160930208.md): Skin · delaminated · Sep 30, 2016 · N711SY · Boeing 73773V · Wing, Plate/Skin
  > RT WING LEADING EDGE PANEL 621CB DELAMINATED ON LEADING EDGE. REPAIRED RH WING LEADING EDGE PANEL 621CB.
- [SDR SCNA20160930207](https://openairdocs.org/sdr/SCNA20160930207.md): Skin · damaged · Sep 30, 2016 · N711SY · Boeing 73773V · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE PANEL 621DB DELAMINATED ON LEADING EDGE. REPAIRED RH WING LEADING EDGE PANEL 621DB.
- [SDR SCNA20160930206](https://openairdocs.org/sdr/SCNA20160930206.md): Bracket · cracked · Sep 30, 2016 · N711SY · Boeing 73773V · Stabilizer Position Indicating
  > PULLEY BRACKET AFT OF BS 1016 FOR THE LEFT HORIZONTAL STAB CABLE "STA", FAIRLEAD ON PULLEY BRACKET IS CRACKED. REMOVED CRACKED FAIRLEAD AFT OF STA 1016 FOR LH HORIZONTAL STAB CABLE & REPLACED WITH NEW.
- [SDR SCNA20160930205](https://openairdocs.org/sdr/SCNA20160930205.md): Support · corroded · Sep 30, 2016 · N711SY · Boeing 73773V · Fuselage Miscellaneous Structure
  > R1 DOOR THRESHOLD SUPPORT ATTACH TO CREASE BEAM IS CORRODED AT STA. 320 RBL 61. REMOVED CORROSION FROM R1 DOOR THRESHOLD SUPPORT ATTACH ANGLE ORIG. "T" 0.090 REMOVED 0.022 REMAINING "T" 0.068 OUT OF LIMITS. SUPPORT ANGLE WAS INSTALLED AS PART OF THE CREASE B
- [SDR SCNA20160930204](https://openairdocs.org/sdr/SCNA20160930204.md): Crease Beam · corroded · Sep 30, 2016 · N711SY · Boeing 73773V · Passenger/Crew Doors
  > R1 DOOR CREASE BEAM IS CORRODED RBL 60 STA 320 TO 358. REMOVED AND REPLACED R1 DOOR CREASE BEAM.
- [SDR SCNA20160930203](https://openairdocs.org/sdr/SCNA20160930203.md): Floor Support · corroded · Sep 30, 2016 · N711SY · Boeing 73773V · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT STA 309.9 RBL 5 CORRODED AFT OF GALLEY MOUNT. REMOVED FLOOR SUPPORT AT STA - 294.5 RBL 5. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT.
- [SDR SCNA20160930202](https://openairdocs.org/sdr/SCNA20160930202.md): Strap · corroded · Sep 30, 2016 · N711SY · Boeing 73773V · Fuselage Main, Structure
  > RIGHT HAND CREASE BEAM STRAP CORRODED AT STA 291. REMOVED & REPLACED RT CREASE BEAM STRAP STA 277 TO 312.
- [SDR SCNA20160930201](https://openairdocs.org/sdr/SCNA20160930201.md): Skin · worn · Sep 30, 2016 · N711SY · Boeing 73773V · Service Doors
  > RT A/C BAY, GROUND PNEUMATIC DOOR INNER SURFACE HAS AREAS OF WEAR AND MISSING PAINT. BLENDED DAMAGE ON GROUND PNEUMATIC DOOR, ORIGINAL T=.100 AFTER BLENDING T=.075,.025 MATERIAL LOSS, OUT OF LIMITS. FABRICATED NEW DOOR AND INSTALLED.
- [SDR SCNA20160930200](https://openairdocs.org/sdr/SCNA20160930200.md): Beam · loose · Sep 30, 2016 · N711SY · Boeing 73773V · Trailing Edge Flaps
  > NR 6 FLAP FAIRING LOOSE AT AFT CENTER ATTACHMENT. REMOVED & REPLACED NR 6 FLAP FAIRING AFT ATTACH BEAM ASSY.
- [SDR SCNA20160929199](https://openairdocs.org/sdr/SCNA20160929199.md): Skin · damaged · Sep 29, 2016 · N711SY · Boeing 73773V · Ailerons
  > LEFT WING AILERON UPPER SURFACE HAS SEVERAL AREAS OF EXPOSED COMPOSITE. REPAIRED THE LEFT WING AILERON UPPER SURFACE.
- [SDR SCNA20160929198](https://openairdocs.org/sdr/SCNA20160929198.md): Trunnion · loose · Sep 29, 2016 · N711SY · Boeing 73773V · Wing, Landing Gear Attach Fittings
  > LEFT WING MAIN LANDING GEAR, FWD TRUNION RETENTION NUTS SEALENT DISBONDED OR MISSING 4 EA. NUTS. APPLIED FILLET SEAL TO SPECIAL WASHERS NUTS ON LH WINGS MLG, FWD TRUNION RETENTION NUTS.
- [SDR SCNA20160929197](https://openairdocs.org/sdr/SCNA20160929197.md): Nose Cowl · damaged · Sep 29, 2016 · N711SY · Boeing 73773V · Engine Cowl Flaps
  > RT WING NR 2 ENGINE NOSE COWL, THUMBNAIL MATTING SURFACE HAS LIGHT WEAR AND MISSING PAINT. AREAS FROM 10 TO 2 O`CLOCK MARKED. REPAIRED NR 2 RIGHT WING ENGINE NOSE COWL.
- [SDR SCNA20160929196](https://openairdocs.org/sdr/SCNA20160929196.md): Panel · loose · Sep 29, 2016 · N711SY · Boeing 73773V · Wing Main, Frame Structure
  > RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL IS LOOSE. FOUND HOLES TO BE ELONGATED ON UPPER SUPPORT BEAM AT RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL, CUT OUT DAMAGE AND ACCOMPLISHED REPAIR.
- [SDR SCNA20160929195](https://openairdocs.org/sdr/SCNA20160929195.md): Panel · loose · Sep 29, 2016 · N711SY · Boeing 73773V · Wing Main, Frame Structure
  > LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL IS LOOSE. REMOVED 2 EACH RETAINERS ON LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL. INSTALLED SERRATED PLATE AND REINSTALLED 2EACH RETAINERS.
- [SDR SCNA20160929194](https://openairdocs.org/sdr/SCNA20160929194.md): Skin · delaminated · Sep 29, 2016 · N711SY · Boeing 73773V · Trailing Edge Flaps
  > LEFT OUTBOARD AFT FLAP, INBOARD TRAILING EDGE CORNER HAS A SMALL AREA OF DELAMINATION. REPAIRED LEFT OUTBOARD AFT FLAP INBOARD TRAILING EDGE CORNER.

Next page: https://openairdocs.org/deregistered/N711SY-2020-03-03/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 = 'N711SY' AND deregistration_id = 'N711SY-2020-03-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N711SY-2020-03-03/reports

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