# Service difficulty reports: N718SK

A list on [N718SK](https://openairdocs.org/aircraft/N718SK.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 3 · 112 reports

- [SDR SWIA2026070276444](https://openairdocs.org/sdr/SWIA2026070276444.md): Acm · seized · Jul 2, 2026 · N718SK · Cndair CL6002C10 · Cabin Cooling System
  > RIGHT PACK AUTO FAIL. BURNING SMELL WITH HAZE THROUGH OUT THE AIRCRAFT. MEL 21-51-1ACAT C DUE 7/11/26 (FLIGHT 6215) MCI--DEFERRED PER MEL 21-51-1A. AIR-CONDITIONING PACKS FOR RT PACK INOPERATIVE. COMPLIED WITH ACCORDING TO MEL VERIFIED THAT RAM AIR
- [SDR SWIA2025111201](https://openairdocs.org/sdr/SWIA2025111201.md): Windshield · cracked · Nov 10, 2025 · N718SK · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT WINDSHIELD OUTER LAYER CRACKED. NO PRESSURIZATION CHANGE. (FLIGHT 4935) REMOVED AND REPLACED RT WINDSHIELD IAW AMM 56-11-01. NO DEFECTS NOTED, ACFT OK FOR CONTINUED SERVICE.
- [SDR SWIA202503310029](https://openairdocs.org/sdr/SWIA202503310029.md): Stringer · chafed · Mar 29, 2025 · N718SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CHAFING FOUND ON STGR 7 AT FS1144.00-1162.00 (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR ON R/H STGR 7 AT FS1144.00-1162.00 IN REFERENCE TO CRJ700 SRM 53-00-03-21 AND REO 670-53-61-292 REV E.
- [SDR SWI2025F00150](https://openairdocs.org/sdr/SWI2025F00150.md): Oxygen Mask · burst · Feb 12, 2025 · N718SK · Cndair CL6002C10 · Crew Oxygen System
  > FO 02 MASK BURST CAUSING COMPLETE LOSS OF OXYGEN WITH SUBSEQUENT OXY LO PRESS CAUTION MESSAGE (FLIGHT 6203 - FILED CLOSED) TROUBLESHOT OXY LO PRESS CAUTION MESSAGE REF CRJ700 FIM 35-10-00. REMOVED AND REPLACED FIRST OFFICER'S CREW OXYGEN MASK REF CRJ700
- [SDR SWIA202412160014](https://openairdocs.org/sdr/SWIA202412160014.md): Shutoff Valve · faulted · Dec 14, 2024 · N718SK · Cndair CL6002C10 · Airfoil Anti/De-ice System
  > LH AND RH WING ANTI-ICE CAUTION MESSAGE. (FLIGHT 4818 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29317448 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT WING A/I FAULT MESSAGE IN REFERENCE TO FIM 30-12-00-810-801. SEE CP 29318473
- [SDR SWIA20231101003](https://openairdocs.org/sdr/SWIA20231101003.md): Hinge · corroded · Oct 3, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > CORROSION FOUND BEHIND THE RIGHT NLG AFT HINGE FITTING ON THE NLG GEAR BOX (C-CHECK RO 11/4/2023) BLENDED CORROSION ON THE NLG GEAR BOX WHERE THE RIGHT NLG AFT HINGE FITTING IS ATTACHED, FOUND TO BE OUT OF LIMITS SINCE NO ALLOWABLE DAMAGE LIMITS FOR AREA
- [SDR SWI2023F00460](https://openairdocs.org/sdr/SWI2023F00460.md): Unknown · damaged · Sep 19, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGE FOUND AT SEAT TRACK RBL9 FS581 - FS680 (C-CHECK RO 11/4/2023) REPLACED CABIN FLOOR SEAT TRACK RBL9 FS581 - FS680 REF CRJ700 AMM 53-00-49-400-801-A03
- [SDR SWI2023F00459](https://openairdocs.org/sdr/SWI2023F00459.md): Unknown · damaged · Sep 19, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGE FOUND AT SEAT TRACK LBL9 FS581 - FS680 (C-CHECK RO 11/4/2023) REPLACED THE CABIN FLOOR SEAT TRACK LBL9 FS581 - FS680 REF CRJ700 AMM 53-00-49-400-801-A03
- [SDR SWI2023F00458](https://openairdocs.org/sdr/SWI2023F00458.md): Unknown · damaged · Sep 19, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGE FOUND AT SEAT TRACK RBL9 FS485 - FS581 (C-CHECK RO 11/4/2023) REPLACED CABIN FLOOR SEAT TRACK RBL9 FS485 - FS581 REF CRJ700 AMM 53-00-49-400-801-A03
- [SDR SWIA202311010919](https://openairdocs.org/sdr/SWIA202311010919.md): Unknown · damaged · Sep 19, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGE FOUND AT SEAT TRACK LBL9 FS485 - FS581 (C-CHECK RO 11/4/2023) REPLACED THE CABIN FLOOR SEAT TRACK LBL9 FS485 - FS581 REF CRJ700 AMM 53-00-49-400-801-A03
- [SDR SWI2023F00457](https://openairdocs.org/sdr/SWI2023F00457.md): Unknown · corroded · Sep 11, 2023 · N718SK · Cndair CL6002C10 · Wing, Attach Fittings
  > AFTER REMOVAL OF PANEL 642AZ FOUND THE FWD ATTACH ANGLE TO BE CORRODED (C-CHECK RO 11/4/2023) REMOVED CORROSION ON PANEL 642AZ - FWD ATTACH ANGLE AND FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 57-22-32-101-001-A01. REPLACED WITH NEW SUPPORT ANGLE PN CC670-1
- [SDR SWI2023F00456](https://openairdocs.org/sdr/SWI2023F00456.md): Unknown · corroded · Sep 11, 2023 · N718SK · Cndair CL6002C10 · Wing, Attach Fittings
  > AFTER REMOVAL OF PANEL 542AZ FOUND THE FWD ATTACH ANGLE TO BE CORRODED (C-CHECK RO 11/4/2023) REMOVED CORROSION ON PANEL 542AZ - FWD ATTACH ANGLE AND FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 57-22-32-101-001-A01. REPLACED WITH NEW SUPPORT ANGLE PN CC670-1
- [SDR SWIA202311010911](https://openairdocs.org/sdr/SWIA202311010911.md): Unknown · damaged · Sep 11, 2023 · N718SK · Cndair CL6002C10 · Engine Thrust Reverser
  > WHILE BACK DRILLING POTTED "Z" STIFFENER HOLES ON L/H ENGINE UPPER TRANSCOWL, THE UPPER MOST FASTENER HOLE WAS DOUBLE DRILLED. (C-CHECK RO 11/4/2023) L/H ENGINE UPPER TRANSCOWL DOUBLE DRILLED HOLE LOCATION HAS BEEN REPAIRED REF REO# 670-54-21-1574, REV --
- [SDR SWIA202311010906](https://openairdocs.org/sdr/SWIA202311010906.md): Unknown · corroded · Sep 6, 2023 · N718SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > 2 EA CLEATS THAT ATTACH TO FORMER FS323.963 ARE CORRODED (C-CHECK RO 11/4/2023) REMOVED AND REPLACED 2 EA CLEATS THAT ATTACH TO FORMER FS323.963. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2023F00455](https://openairdocs.org/sdr/SWI2023F00455.md): Unknown · corroded · Sep 5, 2023 · N718SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR CLEAT @ AFT SIDE OF FS338.00 AND INTERCOSTAL DD6 IS CORRODED (C-CHECK RO 11/4/2023) INSTALLED NEW PAX DOOR CLEAT @ AFT SIDE OF FS338.00 AND INTERCOSTAL DD6. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH TASK CARD
- [SDR SWIA202311010905](https://openairdocs.org/sdr/SWIA202311010905.md): Unknown · corroded · Sep 5, 2023 · N718SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR CLEAT @ FWD SIDE OF FS320.00 AND INTERCOSTAL DD6 IS CORRODED (C-CHECK RO 11/4/2023) REMOVED AND REPLACED PAX DOOR CLEAT @ FWD SIDE OF FS320.00 AND INTERCOSTAL DD6. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH TA
- [SDR SWIA202311010831](https://openairdocs.org/sdr/SWIA202311010831.md): Unknown · cracked · Aug 31, 2023 · N718SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H ENGINE LOWER TRANS COWL LATCH COAMING CRACKED BY AFT LATCH BEARING PAD CHANNEL. (C-CHECK RO 11/4/2023) REMOVED AND INSTALLED WITH NEW LATCH DOOR COAMING REF REO 670 54-21-1207 REV. (A) DATED 2015-08-27. PERFORMED OPS TEST AND TEST PASSED. COMPLIED WITH
- [SDR SWI2023F00454](https://openairdocs.org/sdr/SWI2023F00454.md): Unknown · dented · Aug 29, 2023 · N718SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FLIGHT COMPARTMENT FLOOR DENTED/GOUGED BETWEEN COPILOT SEAT TRACKS (C-CHECK RO 11/4/2023) REPAIRED FLIGHT COMPARTMENT FLOOR BETWEEN COPILOT SEAT TRACKS IAW REO 670-53-11-1881 REV. -- DATED 2023-09-08 STEPS 1 THROUGH 11. COMPLIED WITH TASK CARD 51-900-1002-
- [SDR SWI2023F00453](https://openairdocs.org/sdr/SWI2023F00453.md): Unknown · corroded · Aug 29, 2023 · N718SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD3 BETWEEN FS320 & FS338 HAS CORROSION (C-CHECK RO 11/4/2023) REMOVED AND INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD3 BETWEEN FS320 & FS338. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 6
- [SDR SWIA202311010829](https://openairdocs.org/sdr/SWIA202311010829.md): Unknown · corroded · Aug 29, 2023 · N718SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD2 BETWEEN FS320 & FS338 HAS CORROSION (C-CHECK RO 11/4/2023) REMOVED AND INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD2 BETWEEN FS320 & FS338. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING
- [SDR SWI2023F00452](https://openairdocs.org/sdr/SWI2023F00452.md): Unknown · cracked · Aug 28, 2023 · N718SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H ENGINE UPPER TRANS COWL INBD A-BRACKET CRACKED (C-CHECK RO 11/4/2023) REMOVED R/H ENGINE UPPER TRANS COWL INBD. STAND OFF (A BRACKET) AND INSTALLED 1 EA. NEW STAND OFF P/N CN 624-2082-201, REF. REO 670-54-21-971, REV. A, DATED 2017/05/11 STEPS 1-3. COM
- [SDR SWI2023F00451](https://openairdocs.org/sdr/SWI2023F00451.md): Unknown · chafed · Aug 28, 2023 · N718SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H ENGINE LOWER TRANS COWL INBD SLIDER CHAFED (C-CHECK RO 11/4/2023) REMOVED CHAFING ON THE R/H ENGINE LWR TRANS COWL, INBD SLIDER AND FOUND OUT OF LIMITS PER CRJ700SRM 54-21-00-101-001-A01. RECEIVED AND COMPLIED WITH REO 670-54-21-1573 REV -- DATED 2023-
- [SDR SWI2023F00450](https://openairdocs.org/sdr/SWI2023F00450.md): Unknown · cracked · Aug 28, 2023 · N718SK · Cndair CL6002C10 · Wing Structure
  > RH WING SLAT TRACK CANNISTER 1-3 ATTACH STRAP INSIDE FUEL PANEL 651AB POSSIBLY CRACKED (MARKED) 27088818 (C-CHECK RO 11/4/2023) COMPLIED WITH PERMANENT REPAIR TO RH WING SLAT TRACK CANNISTER 1-3 REF REO 670-57-42-577 REV -- 2016-12-02, CRJ-700 SRM 51-42-06
- [SDR SWIA2023110100828](https://openairdocs.org/sdr/SWIA2023110100828.md): Unknown · cracked · Aug 28, 2023 · N718SK · Cndair CL6002C10 · Wing Structure
  > LH WING SLAT TRACK CANNISTER 1-3 ATTACH STRAP INSIDE FUEL PANEL 551AB POSSIBLY CRACKED (MARKED) 27088815 (C-CHECK RO 11/4/2023) PERFORMED REPAIR TO THE LH WING SLAT TRACK CANNISTER 1-3 ATTACH STRAP INSIDE FUEL PANEL 551AB REF CRJ700 SRM 51-42-06-001-001-A0
- [SDR SWI2023F00449](https://openairdocs.org/sdr/SWI2023F00449.md): Unknown · gouged · Aug 27, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE (FUSELAGE SIDE) LANDINGS 23 & 27 HAVE GOUGES (C-CHECK RO 11/4/2023) PERFORMED REPAIR OF PASSENGER DOOR PIANO HINGE LANDINGS 23 AND 27 IAW ALL STEPS OF REO 670-53-21-582 REV -F, DATED 2017-08-02 REPAIR TYPE: IV.. COMPLIED WITH TAS
- [SDR SWI2023F00448](https://openairdocs.org/sdr/SWI2023F00448.md): Unknown · corroded · Aug 27, 2023 · N718SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT FS 333.00 AND STGR 25R IS CORRODED. (C-CHECK RO 11/4/2023) REMOVED AND INSTALLED NEW STRINGER SPLICE AT FS333.00 STGR 25R. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. ALL CHECKS GOOD AT THIS TIME. COMPLIED WITH TASK 5
- [SDR SWIA20230827](https://openairdocs.org/sdr/SWIA20230827.md): Unknown · corroded · Aug 27, 2023 · N718SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CLIP AT FS 295.00 AND STGR 18L IS CORRODED. (C-CHECK RO 11/4/2023) REPLACED CORRODED CLIP P/N SH670-31969-2 WITH NEW. REF. CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG SH670-31550 REV G. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWI2023F00447](https://openairdocs.org/sdr/SWI2023F00447.md): Unknown · corroded · Aug 26, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SEAT TRACK FLOOR BEAM AT LBL9 BETWEEN FS1000.00 TO FS1069.75 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 11/4/2023) REMOVED AND REPAIRED L/H SEAT TRACK FLOOR BEAM AT LBL9 FS1000.00 TO FS1069.75 CRJ700 SRM 53-00-41-201-001-A01 REV. 38 ISSUED 07/25/
- [SDR SWI2023F00446](https://openairdocs.org/sdr/SWI2023F00446.md): Unknown · corroded · Aug 26, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SEAT TRACK FLOOR BEAM AT LBL27 BETWEEN FS1000.00 TO FS1069.75 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 11/4/2023) REPAIRED LH FLOOR BEAM LBL27 BETWEEN FS1000 - FS1069.75 REF CRJ700 SRM 53-00-41-201-001-A01 REPAIR FIGURE 53-00-41-991-830. COMPLI
- [SDR SWI2023F00445](https://openairdocs.org/sdr/SWI2023F00445.md): Unknown · corroded · Aug 26, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SEAT TRACK FLOOR BEAM AT RBL9 BETWEEN FS1000.00 TO FS1069.75 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 11/4/2023) NO CORROSION NOTED ON FLOOR BEAM RBL9 FS1037 - FS1069.75. REMOVED CORROSION AT RH FLOOR BEAM RBL9 BETWEEN FS1000 - FS1037, FOUND FL
- [SDR SWI2023F00444](https://openairdocs.org/sdr/SWI2023F00444.md): Unknown · corroded · Aug 26, 2023 · N718SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SEAT TRACK FLOOR BEAM AT RBL27 BETWEEN FS1000.00 TO FS1069.75 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 11/4/2023) REPAIRED R/H SEAT TRACK FLOOR BEAM AT RBL27 BETWEEN FS1000.00 TO FS1069.75 REF REO NO. 670-53-61-2164 REV -- DATED 2023-09-08. CO
- [SDR SWIA2023110100826](https://openairdocs.org/sdr/SWIA2023110100826.md): Unknown · corroded · Aug 26, 2023 · N718SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT HANDRAIL CAP (CLEAT) BETWEEN FS333.00 TOFS349.00 HAS CORROSION (MARKED) (C-CHECK RO 11/4/2023) REMOVED AND REPLACED CLOSING FITTING "HANDRAIL CAP (CLEAT)" WITH NEW ASSY FOR STGR 18L AT FS342.00 IAW CRJ700 SRM 51-42-06-001-001-A01 & DWG NO.SH67
- [SDR SWI2023F00443](https://openairdocs.org/sdr/SWI2023F00443.md): Unknown · corroded · Aug 25, 2023 · N718SK · Cndair CL6002C10 · Galley Doors
  > SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AROUND THE FASTENER HOLES. (MARKED) (C-CHECK RO 11/4/2023) REMOVED AND INSTALLED NEW SERVICE DOOR LOWER SEAL STRIKER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV Y. ALL CHECKS GOOD AT THIS TIM
- [SDR SWIA2023110100825](https://openairdocs.org/sdr/SWIA2023110100825.md): Unknown · corroded · Aug 25, 2023 · N718SK · Cndair CL6002C10 · Service Doors
  > SERVICE DOOR MOUNTING ANGLE ON THE LOWER SILL HAS CORROSION. (MARKED) 27074154 (C-CHECK RO 11/4/2023) REMOVED AND INSTALLED NEW SERVICE DOOR MOUNTING ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND DWG SH670-31950 REV.
- [SDR SWIA2023110100824](https://openairdocs.org/sdr/SWIA2023110100824.md): Unknown · gouged · Aug 24, 2023 · N718SK · Cndair CL6002C10 · Ailerons
  > RIGHT AILERON HINGE FITTING #3 LOWER SURFACE HAS TWO AREAS WITH GOUGING DAMAGE. (MARKED) (C-CHECK RO 11/4/2023) BLENDED OUT GOUGE ON RIGHT AILERON HINGE FITTING #3 LOWER SURFACE AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF CRJ700SRM 51-12-00-001-001
- [SDR SWIA2023110100821](https://openairdocs.org/sdr/SWIA2023110100821.md): Unknown · chafed · Aug 21, 2023 · N718SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > RH AILERON UPPER LEADING EDGE SKIN SHROUD CHAFFING FROM INBOARD TO OUTBOARD SIDES (C-CHECK RO 11/4/2023) REPLACED RH AILERON UPPER LEADING EDGE SKIN REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DWG: CC670-13000 REV D. COMPLIE
- [SDR SWIA202311010002](https://openairdocs.org/sdr/SWIA202311010002.md): Unknown · elongated · Aug 20, 2023 · N718SK · Cndair CL6002C10 · Fuselage Main, Frame
  > PANEL 642AT HAS ELONGATED BOLT HOLE( MARKED) AND ON THE STRUCTURE OF THE PANEL AREA HAS A STUCK SHANK MARKED). (C-CHECK RO 11/4/2023) PERFORMED REPAIR TO ELONGATED HOLE ON PANEL 642AT REF REO 670-57-21-954 REV -- DATE 2023-09-07 ALL STEPS COMPLIED WITH. C
- [SDR SWIA202311010001](https://openairdocs.org/sdr/SWIA202311010001.md): Unknown · chafed · Aug 17, 2023 · N718SK · Cndair CL6002C10 · Passenger/Crew Doors
  > CHAFE LOCATED JUST BELOW PAX DOOR (IN SCOPE 1C 53-900-308). (C-CHECK RO 11/4/2023) PERFORMED REPAIR TO CHAFE DAMAGE LOCATED JUST BELOW PAX DOOR. REF CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-53-21-2316 REV -- DATED 2023-09-06 ALL STEPS OF REO COMPLIED WI
- [SDR SWIA202266141](https://openairdocs.org/sdr/SWIA202266141.md): None · odor · Jul 20, 2022 · N718SK · Cndair CL6002C10 · Air Conditioning System
  > FAINT BURNT RUBBER SMELL COMING THROUGH FO VENT, FA REPORTS SAME SMELL IN FIRST CLASS (FLIGHT #3196 FILED CLOSED) UPON ARRIVAL TALKED WITH FLIGHT CREW AND VERIFIED FAINT SMELL TO COME FROM FO VENT AND MOMENTARILY LASTED A COUPLE OF MINUTES. CYCLED BOTH PAC
- [SDR SWIA202265260](https://openairdocs.org/sdr/SWIA202265260.md): None · delaminated · Apr 1, 2022 · N718SK · Cndair CL6002C10 · Window/Windshield System
  > FO SIDE WINDOW MORE HOT THAN USUAL AND DELAMINATED IN THE FAR RIGHT CORNER (FLIGHT 3075 - FILED CLOSED) REMOVED AND REPLACED RH SIDE WINDOW PER CRJ AMM 56-12-01. PERFORMED OPS CHECK OF WINDOW HEAT AND LEAK CHECK OF SIDE WINDOW, OPS CHECK AND LEAK CHECK G
- [SDR SWIA202264767](https://openairdocs.org/sdr/SWIA202264767.md): None · none · Feb 28, 2022 · N718SK · Cndair CL6002C10 · Aircraft Fuel System
  > FUEL IMBALANCE CAUTION. UP TO 1200LBS IN FLIGHT. BOTH BOOST PUMPS ON PER CSL 1978. LEFT TANK LOWER. WITH RIGHT TANK QUANTITY INCREASING. (FLIGHT 3092 - FILED CLOSED) PERFORMED OPERATIONAL CHECK OF FUEL TRANSFER AND CROSS FLOW SYSTEM IAW AMM 28-13-00. SYS
- [SDR SWIA2022011463766](https://openairdocs.org/sdr/SWIA2022011463766.md): Ballast · failed · Jan 13, 2022 · N718SK · Cndair CL6002C10 · Passenger Compartment Lighting
  > FAS REPORT HAZE AND BURNING RUBBER SMELLED ON DESCENT. NO OTHER SECONDARY ISSUES OBSERVED. PACK OUTFLOW TEMPS WERE 35 - 40C ALL OTHER SYSTEMS AND INDICATIONS NORMAL (FLIGHT 3058 - FILED CLOSED) TROUBLE SHOT SMELL IN AIRCRAFT AND TALKING TO BOTH FLIGHT ATT
- [SDR SWIA201642219](https://openairdocs.org/sdr/SWIA201642219.md): Stringer · corroded · Jun 1, 2016 · N718SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 20R BETWEEN FS 501 TO 517 CORRODED. REPAIRED THE STRINGER IAW EA. PRESSURIZATION LEAK CHECKED GOOD.
- [SDR SWIA201642218](https://openairdocs.org/sdr/SWIA201642218.md): Stringer · corroded · May 16, 2016 · N718SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > LT FUSELAGE INTERNAL JUST AFT OF BS 349, STR 20L HAS CORROSION ON TOP. REPAIRED STR 20L JUST AFT OF FS349 IAW STS EA. LEAK CHECK GOOD.
- [SDR SWIA201642222](https://openairdocs.org/sdr/SWIA201642222.md): Door Sill · corroded · May 15, 2016 · N718SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL CORROSION OUT OF LIMITS. REMOVED THE CORRODED OUT OF LIMITS AFT CARGO DOOR SILL AND INSTALLED A NEW AFT CARGO DOOR SILL IAW SRM. COMPLIED WITH PRESSURIZATION CHECK OF THE AFFECTED AREA IAW AMM, PRESSURE LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA201642221](https://openairdocs.org/sdr/SWIA201642221.md): Frame · corroded · May 14, 2016 · N718SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY LOWER FRAME AT BS 349 CORRODED OUT OF LIMITS. R & R THE LOWER FRAME IAW SRM. PRESSURIZATION LEAK CHECKED GOOD.
- [SDR SWIA201642220](https://openairdocs.org/sdr/SWIA201642220.md): Frame · corroded · May 14, 2016 · N718SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY LOWER FRAME AT BS 333 CORRODED. R & THE LOWER FRAME IAW REO. PRESSURE LEAK CHECKED GOOD.
- [SDR SWIA201642217](https://openairdocs.org/sdr/SWIA201642217.md): Frame · corroded · May 14, 2016 · N718SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY LOWER FRAME AT BS 319 HAD OUT OF LIMITS CORROSION. REPAIRED IAW REO. LEAK CHECKED GOOD.
- [SDR SWIA201642216](https://openairdocs.org/sdr/SWIA201642216.md): Frame · corroded · May 13, 2016 · N718SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY LOWER FRAME AT BS 364 CORRODED BETWEEN STR 25L AND STR 26L. R & R FRAME SECTOR AT FS 364 BETWEEN STR 24L AND 24R IAW REO.
- [SDR SWIA201439290](https://openairdocs.org/sdr/SWIA201439290.md): Structure · damaged · Sep 21, 2014 · N718SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUND BIRD STRIKE ON LT WING, NR 2 SLAT TO BE DAMAGED BETWEEN SS 293.75 AND SS 306.75. REPAIRED IAW REO.

Next page: https://openairdocs.org/aircraft/N718SK/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 = 'N718SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N718SK/reports

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