# Service difficulty reports: N709SK

A list on [N709SK](https://openairdocs.org/aircraft/N709SK.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 · 207 reports

- [SDR SWIA2026022575290](https://openairdocs.org/sdr/SWIA2026022575290.md): Windshield · cracked · Feb 16, 2026 · N709SK · Cndair CL6002C10 · Flight Compartment Windows
  > WINDSHIELD CRACKED ENROUTE. RAN QRH. NO PRESSURIZATION ISSUES. (FLIGHT 6394 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31750315. REMOVED AND REPLACED LH CA WINDSHIELD IAW TASK CARD 56-220-1000-SKY AND REFERENCING APPLICABLE STEPS OF AMM 56
- [SDR SWIA2026021765290](https://openairdocs.org/sdr/SWIA2026021765290.md): Windshield · cracked · Feb 16, 2026 · N709SK · Cndair CL6002C10 · Flight Compartment Windows
  > CA, WINDSHIELD CRACKED ENROUTE. RAN QRH. NO PRESSURIZATION ISSUES. (FLIGHT 6394) OPEN.
- [SDR SWIA2025111400001](https://openairdocs.org/sdr/SWIA2025111400001.md): Windshield · arced · Nov 11, 2025 · N709SK · Cndair CL6002C10 · Flight Compartment Windows
  > CA SIDE OUTER WINDSCREEN ARCING THEN SHATTERED WHEN WINDSHIELD HEAT WAS TURNED OFF (FLIGHT 4908 - FILED CLOSED) REPLACED CA SIDE WINDOW IN REF TO AMM 56-12-01-400-801, SEE ATTACHED TASK CARD 56-220-1000-SKY. WINDOW HEAT AND PRESSURIZATION CHECK GOOD.
- [SDR SWIA2025111100001](https://openairdocs.org/sdr/SWIA2025111100001.md): Windshield · cracked · Nov 11, 2025 · N709SK · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAIN SIDE OUTER WINDSCREEN ARCING THEN SHATTERED WHEN WINDSHIELD HEAT WAS TURNED OFF. (FLIGHT 4908) OPEN.
- [SDR SWI2025F00703](https://openairdocs.org/sdr/SWI2025F00703.md): Wire Harness · broken · May 30, 2025 · N709SK · Cndair CL6002C10 · Engine Bleed Air System Wiring
  > L BLEED DUCT WARNING IN FLIGHT AT ABOUT 16,000FT. QRH COMPLIED WITH. RETURNED TO FIELD. PASSENGER O2 MASKS DEPLOYED. (FLIGHT 6221) TROUBLESHOT L BLEED DUCT AND FOUND CONNECTOR AT MT137 UNSERVICEABLE AND PIG TAIL WIRING HARNESS AT CONNECTOR MT203P1 BRO
- [SDR SWI2025F00652](https://openairdocs.org/sdr/SWI2025F00652.md): Extractor · faulted · May 21, 2025 · N709SK · Cndair CL6002C10 · Engine Bleed Air System
  > L BLEED DUCT WARNING MESSAGE ON CLIMB OUT (FLIGHT 6200 - FILED CLOSED)INTERROGATED MDC AND FOUND CHANNEL A FLAGGING MT137 AT 80%. PERFORMED INSPECTION OF L/H BLEED DUCTING SYSTEM IN REFERENCE WITH FIM 36-21-01 AND FOUND MULTIPLE LEAK POINTS. FOUND L/H WATER EX
- [SDR SWIA20250113111](https://openairdocs.org/sdr/SWIA20250113111.md): Light · smoke · Jan 11, 2025 · N709SK · Cndair CL6002C10 · Flight Compartment Lighting
  > SMOKE EMITTED FROM FO FORWARD FLOOD LIGHT DURING CLIMB OUT. (FLIGHT 5005 - FILED CLOSED) TROUBLESHOT SMOKE IN THE COCKPIT IN REFERENCE TO FIM 21-21-00-810-806. FOUND SMOKE TO BE COMING FROM THE FO SIDE FACIA PANEL FLOOD LIGHT. INSPECTED THE FLOOD LIGHT A
- [SDR SWIA202501130049](https://openairdocs.org/sdr/SWIA202501130049.md): Door Frame · corroded · Nov 7, 2024 · N709SK · Cndair CL6002C10 · Fuselage Main, Structure
  > SERVICE DOOR SURROUND STRUCTURE FS319.00 TO FS349.00 STR 18R HAS SIGNS OF CORROSION AS MARKED (C-CHECK RO 12/31/2024 - FILED CLOSED) BLENDED CORROSION ON SERVICE DOOR LOWER MOUNTING ANGLE IAW CRJ700 SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM
- [SDR SWIA2025011307](https://openairdocs.org/sdr/SWIA2025011307.md): Door · gouged · Nov 7, 2024 · N709SK · Cndair CL6002C10 · Landing Gear Doors
  > DEEP BARE METAL GOUGE WEAR IN RH MAIN LANDING GEAR DOOR ON THE AFT OUTBOARD CORNER OF THE DOOR ADJACENT TO THE SWEEP BELT BRUSHES (C-CHECK RO 12/31/2024 - FILED CLOSED) BLENDED DAMAGE ON RH MLG DOOR AT AFT OUTBOARD CORNER AND FOUND TO BE IN LIMITS IAW C
- [SDR SWIA20250102004](https://openairdocs.org/sdr/SWIA20250102004.md): Door Frame · corroded · Nov 7, 2024 · N709SK · Cndair CL6002C10 · Fuselage Main, Structure
  > SERVICE DOOR SURROUND STRUCTURE FS319.00 TO FS349.00 STR 18R HAS SIGNS OF CORROSION AS MARKED (C-CHECK RO 12/31/2024 - FILED OPEN) BLENDED CORROSION ON SERVICE DOOR LOWER MOUNTING ANGLE IAW CRJ700 SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 5
- [SDR SWIA202501020107](https://openairdocs.org/sdr/SWIA202501020107.md): Door · gouged · Nov 7, 2024 · N709SK · Cndair CL6002C10 · Landing Gear Doors
  > DEEP BARE METAL GOUGE WEAR IN RH MAIN LANDING GEAR DOOR ON THE AFT OUTBOARD CORNER OF THE DOOR ADJACENT TO THE SWEEP BELT BRUSHES (C-CHECK RO 12/31/2024 - FILED OPEN) BLENDED DAMAGE ON RH MLG DOOR AT AFT OUTBOARD CORNER AND FOUND TO BE IN LIMITS IAW CRJ
- [SDR SWIA2025011306](https://openairdocs.org/sdr/SWIA2025011306.md): Slat Track · cracked · Nov 6, 2024 · N709SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 1-3 HOUSING BRACKET CRACKED (C-CHECK RO 12/31/2024 - FILED CLOSED) PERFORMED REPAIR ON RH SLAT TRACK 1-3 HOUSING PER BOMBARDIER REO 670-57-42-577. REV. --. DATE: 2016-12-02. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S1118
- [SDR SWIA202501020106](https://openairdocs.org/sdr/SWIA202501020106.md): Slat Track · cracked · Nov 6, 2024 · N709SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 1-3 HOUSING BRACKET CRACKED (C-CHECK RO 12/31/2024 - FILED OPEN) PERFORMED REPAIR ON RH SLAT TRACK 1-3 HOUSING PER BOMBARDIER REO 670-57-42-577. REV. --. DATE: 2016-12-02. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S111824
- [SDR SWIA2025011300001](https://openairdocs.org/sdr/SWIA2025011300001.md): Hinge · gouged · Nov 1, 2024 · N709SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE DOOR SIDE LUG #1 GOUGED (C-CHECK RO 12/31/2024 - FILED CLOSED) REPAIRED DAMAGE ON LUG #1 OF PASSENGER DOOR PIANO HINGE, DOOR SIDE IAW BOMBARDIER REO 670-52-11-511 REV.C DATE: 2017/03/09. NDT PERFORMED BY BARON NDT, LLC FAA
- [SDR SWIA202501020101](https://openairdocs.org/sdr/SWIA202501020101.md): Hinge · gouged · Nov 1, 2024 · N709SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE DOOR SIDE LUG #1 GOUGED (C-CHECK RO 12/31/2024 - FILED OPEN) REPAIRED DAMAGE ON LUG #1 OF PASSENGER DOOR PIANO HINGE, DOOR SIDE IAW BOMBARDIER REO 670-52-11-511 REV.C DATE: 2017/03/09. NDT PERFORMED BY BARON NDT, LLC FAA C
- [SDR SWIA202266599](https://openairdocs.org/sdr/SWIA202266599.md): None · failed · Oct 9, 2022 · N709SK · Cndair CL2151A10 · Landing Gear Door Actuator
  > GEAR DISAGREE AFTER SELECTING GEAR UP. NOSE WHEEL NOT LOCKED. (FLIGHT 4923 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25627409 WITH THE FOLLOWING CORRECTIVE ACTION: "INTERROGATED MDC FOUND GEAR DISAGREE B1- 007437. TROUBLESHOT IN REF T
- [SDR SWIA202266219](https://openairdocs.org/sdr/SWIA202266219.md): None · cracked · Aug 4, 2022 · N709SK · Cndair CL6002C10 · Fuselage Structure (General)
  > LH INTERCOSTAL PN CC670-33194-7 FOUND CRACKED UPON INSTALLATION OF THE HYDRAULIC COMPARTMENT SKIN. (FILED CLOSED) REMOVED DAMAGED INTERCOSTAL PN CC670-33194-7. FABRICATED NEW INTERCOSTAL SAME AS ORIGINAL REF CRJ 700 SRM 51-24-21-001-001-A01 AND DWG CC670-3
- [SDR SWIA202266350](https://openairdocs.org/sdr/SWIA202266350.md): None · cracked · Jul 28, 2022 · N709SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA77564-670-53-11-1796 N709SK MXCODEID61545-PR - LEFT FORWARD ELECTRICAL BAY DOOR 211AL SURROUND SKIN AFT LOWER CORNER SHOWING EVIDENCE OF CRACK. COMPLIED WITH TEMPORARY DISPOSITION FOR CRACKS TO HYDRAULIC SKIN PANEL AND
- [SDR SWIA2021081060227](https://openairdocs.org/sdr/SWIA2021081060227.md): Skin · damaged · Jul 21, 2021 · N709SK · Cndair CL6002C10 · Rudder, Plate/Skin
  > ADDITIONAL DAMAGE FOUND ON RUDDER L/H SKIN BTWN. RS98.750 & RS110.278. (C-CHECK RO 8/6/2021) REPAIRED L/H SIDE RUDDER SKIN DAMAGE REF REO 670-55-41-090 REV -- 2021-07-26. COMPLIED WITH SKYCARD 51-900-1002
- [SDR SWIA2021081060226](https://openairdocs.org/sdr/SWIA2021081060226.md): Angle · debonded · Jul 9, 2021 · N709SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LT UPPER TRANSCOWL, Z ANGLE DISBONDED AND HAS THREE LOOSE FASTENERS. (C-CHECK RO 8/6/2021) PERFORMED REPAIR FOR CRACK DAMAGE TO THE LH ENGINE UPPER TRANSCOWL INNER SKIN IAW ALL STEPS OF REO 670-54-21-1458 REV -- DATED 2021-07-23. / C/W TASK CARD 51-900-
- [SDR SWIA2021081060225](https://openairdocs.org/sdr/SWIA2021081060225.md): Stringer · corroded · Jul 6, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON UPPER SURFACE OF STGR17R AT APPROXIMATE FS310.00 -5". (C-CHECK RO 8/6/2021) REPAIRED CORROSION TO UPPER SURFACE OF STGR17R AT FS310.00-5" IAW REO 670-53-21-2080 REV-- 2021-07-10. COMPLIED WITH SKYWET TASK CARD 51-900-1002-SKY
- [SDR SWIA2021081060228](https://openairdocs.org/sdr/SWIA2021081060228.md): Intercostal · corroded · Jun 24, 2021 · N709SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION PRESENT ON INTERCOSTAL BETWEEN FS581.00-FS597.00 AND STGR 23L-22L (C-CHECK RO 8/6/2021) BLENDED, EVALUATED: ORIGINAL THICKNESS- 0.080", REMAING THICKNESS- 0.069", MATERIAL LOSS- 0.011", MATERIAL LOSS ALLOWABLE- NONE. OUT OF LIMITS. REF CRJ700
- [SDR SWIA2021081060233](https://openairdocs.org/sdr/SWIA2021081060233.md): Drag Angle · cracked · Jun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED NEAR POWER ASSIST PULLEY (C-CHECK RO 8/6/2021) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE, P/N 601R31772-5S. REF CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA2021081060224](https://openairdocs.org/sdr/SWIA2021081060224.md): Intercostal · corroded · Jun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD5 (FWD) CORRODED (C-CHECK RO 8/6/2021) REPLACED PAX DOOR INTERCOSTAL AT DD5 (FWD) REF DWG 601R31702 REV N, CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOOD
- [SDR SWIA2021081060223](https://openairdocs.org/sdr/SWIA2021081060223.md): Cleat · corroded · Jun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR ATTACH CLEAT AT FS313.56 FRAME AND DD4 (FWD) CORRODED (C-CHECK RO 8/6/2021) REPLACED PAX DOOR ATTACH CLEAT AT FS313.56 AND DD4 FWD, REF CRJ700 SRM 51-42-06-001-001-A01 C/W TASK CARD 51-900-1002-SKY, ALL CHECKS GOOD
- [SDR SWIA2021081060222](https://openairdocs.org/sdr/SWIA2021081060222.md): Door Frame · corroded · Jun 18, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FRAME AT FS313.56 BETWEEN DD4 AND DD5 (FWD) CORRODED (C-CHECK RO 8/6/2021) PAX DOOR FRAME AT FS313.56 BETWEEN DD4-DD5 FWD REPLACED REF DWG 601R31702 REV N, CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOOD
- [SDR SWIA2021081060221](https://openairdocs.org/sdr/SWIA2021081060221.md): Intercostal · corroded · Jun 18, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD2 (FWD) CORRODED (C-CHECK RO 8/6/2021) REPLACED PAX DOOR INTERCOSTAL DD2 (FWD) REF DWG 601R31702 REV. N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOOD
- [SDR SWIA2021081060220](https://openairdocs.org/sdr/SWIA2021081060220.md): Hinge Fitting · chafed · Jun 18, 2021 · N709SK · Cndair CL6002C10 · Rudder Structure
  > *VERTICAL STABILIZER. RUDDER LOWER CENTER HINGE FITTING, IS CHAFED ON THE UPPER SURFACE OF THE "BEARING HOUSING" AREA. (MARKED (C-CHECK RO 8/6/2021) REPAIRED CHAFE ON VERTICAL STABILIZER CENTER HINGE FITTING UPPER SURFACE. REF MHI RJ AVIATION REO 670-55
- [SDR SWIA2021081060235](https://openairdocs.org/sdr/SWIA2021081060235.md): Web · corroded · Jun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *AREAS OF CORROSION ON PAX DOOR FWD WEB STEP PANEL LANDINGS (C-CHECK RO 8/6/2021) REMOVED CORROSION ON PAX DOOR FWD WEB. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACE PAX DOOR FWD WEB PANEL P/N 601R317071-11. REF CRJ 700 SRM 51-42-06-001-001-A01 AND C
- [SDR SWIA2021081060232](https://openairdocs.org/sdr/SWIA2021081060232.md): Angle · corroded · Jun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *CORROSION PAX DOOR STOPPER BOLT MOUNT CLIP (C-CHECK RO 8/6/2021) REMOVED CORROSION ON PAX DOOR STOPPER BOLT MOUNT CLIP. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED PAX DOOR STOPPER BOLT MOUNT CLIP. SEE CONTINUATION FOR DETAILS. REF CRJ 700 SRM 51-4
- [SDR SWIA2021081060219](https://openairdocs.org/sdr/SWIA2021081060219.md): Intercostal · corroded · Jun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *CORROSION ON PAX DOOR INTERCOSTAL FWD DD3 (C-CHECK RO 8/6/2021) PAX DOOR INTERCOSTAL AT DD3 FWD REPLACED, REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, C/W TASK CARD 51-900-1002-SKY, ALL CHECKS GOOD
- [SDR SWIA2021081060218](https://openairdocs.org/sdr/SWIA2021081060218.md): Intercostal · corroded · Jun 15, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *CORROSION ON PAX DOOR INTERCOSTAL AFT DD5 (C-CHECK RO 8/6/2021) REPLACED PAX DOOR INTERCOSTAL AT AFT DD5 REF DWG 601R31702 REV N, CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY, ALL CHECKS GOOD
- [SDR SWIA2021081060217](https://openairdocs.org/sdr/SWIA2021081060217.md): Stringer · corroded · Jun 14, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR21R IS CORRODED BETWEEN FS349.00 TO FS364.00 (C-CHECK RO 8/6/2021) REMOVED AND REPLACED NEW STGR 21R P/N SH670-31383 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH 670-31350 REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM M M-337 PERFORME LE
- [SDR SWIA2021081060216](https://openairdocs.org/sdr/SWIA2021081060216.md): Angle · corroded · Jun 11, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT CAP ANGLE P/N: SH670-31821-4 FOUND CORRODED. (C-CHECK RO 8/6/2021) REMOVED AND REPLACED WITH NEW PAX DOOR AFT CAP ANGLE IAW BOMBARDIER DWG SH670-31810 REV. AE AND SRM TASK 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2021081060215](https://openairdocs.org/sdr/SWIA2021081060215.md): Angle · corroded · Jun 11, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD CAP ANGLE P/N: SH670-31821-3 FOUND CORRODED. (C-CHECK RO 8/6/2021) REMOVED AND REPLACED WITH NEW PAX DOOR FWD CAP ANGLE IAW BOMBARDIER DWG SH670-31810 REV. AE AND SRM TASK 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2021081060214](https://openairdocs.org/sdr/SWIA2021081060214.md): Angle · corroded · Jun 11, 2021 · N709SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER KIKPLATE ANGLE FOUND CORRODED. (C-CHECK RO 8/6/2021) REMOVED AND REPLACED WITH NEW PAX DOOR LWR KIKPLATE ANGLE IAW BOMBARDIER DWG SH670-31810 REV. AE, CRJ700 SRM TASK 51-42-10-001-001-A01 AND SRM TASK 51-42-21-001-001-A01. COMPLIED WITH T
- [SDR SWIA2021081060213](https://openairdocs.org/sdr/SWIA2021081060213.md): Floorbeam · cracked · Jun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK ON COCKPIT LH FLOORBEAM AT LBL12 JUST FWD OF FS280.00 (C-CHECK RO 8/6/2021) CRACK VERIFIED. REMOVED AND INSTALLED NEW SECTION OF LH FLOORBEAM FROM FS 280.00 TO FS 268.00 REF CRJ700 SRM 53-11-43-201-003-A01. NO NDT DEFECTS NOTED. COMPLIED
- [SDR SWIA2021081060212](https://openairdocs.org/sdr/SWIA2021081060212.md): Floorbeam · cracked · Jun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK ON COCKPIT RH FLOORBEAM AT RBL12 JUST FWD OF FS280.00 (C-CHECK RO 8/6/2021) CRACK VERIFIED. REMOVED AND INSTALLED NEW SECTION OF RH FLOORBEAM FROM FS 280.00 TO FS 268.00 AT RBL12 REF CRJ700 SRM 53-11-43-201-003-A01. NO NDT DEFECTS NOTED.
- [SDR SWIA2021081060211](https://openairdocs.org/sdr/SWIA2021081060211.md): Floorbeam · corroded · Jun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON LH CROSSBEAM FS 280.00 (C-CHECK RO 8/6/2021) REMOVED AND REPLACED LH CROSSBEAM P/N CC670-34094-1. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-22-001-001-
- [SDR SWIA2021081060210](https://openairdocs.org/sdr/SWIA2021081060210.md): Floorbeam · corroded · Jun 11, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON RH CROSSBEAM FS 280.00 (C-CHECK RO 8/6/2021) REMOVED AND REPLACED RH CROSSBEAM P/N CC670-34094-2S @ FS280.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 SRM 51-42-22-001-001-A01, AND DRAWING CC670
- [SDR SWIA2021081060209](https://openairdocs.org/sdr/SWIA2021081060209.md): Skin · corroded · Jun 9, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR26R-STGR25R. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT AT FS 280.00 - FS 282.86 BETWEEN STGR 26R - STGR 25R REF REO 670-53-21-2066 REV -- DATED 2021-06-28 AND CRJ700 SRM
- [SDR SWIA2021081060208](https://openairdocs.org/sdr/SWIA2021081060208.md): Skin · damaged · Jun 9, 2021 · N709SK · Cndair CL6002C10 · Horizontal Stabilizer, Plate/Skin
  > REPAIR THE L/H HORIZONTAL STABILIZER UPPER SKIN PER REO 670-5-11-330 REV -- DATED 2017-08-24 (C-CHECK RO 8/6/2021) COMPLIED WITH REPAIR TO THE L/H UPPER HORIZIONTAL STABILIZER SKIN PER REO 670-55-11-330 REV -A DATED 2021-06-30. SEE CONTINUE CARD FOR DET
- [SDR SWIA2021081060207](https://openairdocs.org/sdr/SWIA2021081060207.md): Skin · damaged · Jun 9, 2021 · N709SK · Cndair CL6002C10 · Horizontal Stabilizer, Plate/Skin
  > REPAIR THE R/H HORIZONTAL STABILIZER UPPER SKIN PER REO 670-55-11-330 REV -- DATED 2017-08-24 (C-CHECK RO 8/6/2021) C/W REPAIR TO THE R/H UPPER HORIZIONTAL STABILIZER SKIN PER REO 670-55-11-330 REV -A DATED 2021-06-30, CRJ 700 SRM 51-42-06-001-001-A01,
- [SDR SWIA2021081060204](https://openairdocs.org/sdr/SWIA2021081060204.md): Skin · corroded · Jun 8, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR25R-STGR23R. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT FS 280.00 - FS 282.86 BETWEEN STGR 23R - STGR 25R REF REO 670-53-21-2066 REV -- DATED 2021-06-28 AND CRJ700 SRM 51-
- [SDR SWIA2021081060203](https://openairdocs.org/sdr/SWIA2021081060203.md): Skin · corroded · Jun 8, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR24L-STGR23L. (C-CHECK RO 8/6/2021) REPAIRED CIRCUNFERENTIAL JOINT AT FS 280.00 BETWEEN STGR 24L - STGR 23L REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-21-06-001-001-A01 RE
- [SDR SWIA2021081060202](https://openairdocs.org/sdr/SWIA2021081060202.md): Skin · corroded · Jun 8, 2021 · N709SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FS280-FS282.86 CIRCUMFERENTIAL JOINT HAS EVIDENCE OF CORROSION FROM STGR26L-STGR26R. (C-CHECK RO 8/6/2021) REMOVED CORROSION AT FS280-FS282.86 CIRCUMFERENTIAL JOINT FROM STRG26L-STRG26R. FOUND TO BE WITHIN LIMITS PER MHIRJ REO 670-53-21-2066 REV -- DATE
- [SDR SWIA2021081060234](https://openairdocs.org/sdr/SWIA2021081060234.md): Door Sill · corroded · Jun 7, 2021 · N709SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *MULTIPLE AREAS OF CORROSION ON FWD CARGO DOOR SILL. AREAS MARKED. (C-CHECK RO 8/6/2021) BLENDED, EVALUATED: ORIGINAL MATERIAL THICKNESS OF FWD CARGO DOOR SILL (INNER SKIN) P/N SH670-33773-7 IS.080€? PER CRJ700 SRM 53-31-23-001-001-A01. MINIMUM REMAIN
- [SDR SWIA2021081060201](https://openairdocs.org/sdr/SWIA2021081060201.md): Drag Angle · cracked · Jun 7, 2021 · N709SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > *RH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPLACED R/H AFT DRAG ANGLE AT THE VERTICAL/FUSELAGE ATTACHMENT AREA REF. CRJ 700 SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01 DWG BA670-35002 REV F / C/W
- [SDR SWIA2021081060200](https://openairdocs.org/sdr/SWIA2021081060200.md): Drag Angle · cracked · Jun 7, 2021 · N709SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > *RH SIDE VERTICAL/FUSELAGE FWD DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REPAIRED THE R/H VERTICAL/FUSELAGE FWD DRAG ANGLE, CUT AWAY DAMAGE, FABRICATED AND INSTALLED ALL REPAIR PARTS, REF. CRJ 700 SRM 55-31-00-201-001-A01 AND CRJ 700 SRM 51-42-21-001-
- [SDR SWIA2021081060199](https://openairdocs.org/sdr/SWIA2021081060199.md): Drag Angle · cracked · Jun 7, 2021 · N709SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > *LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE IS CRACKED (C-CHECK RO 8/6/2021) REMOVED AND REPLACED NEW *LH SIDE VERTICAL/FUSELAGE AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 AND DWG

Next page: https://openairdocs.org/aircraft/N709SK/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 = 'N709SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N709SK/reports

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