# Service difficulty reports: N726SK

A list on [N726SK](https://openairdocs.org/aircraft/N726SK.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 · 220 reports

- [SDR SWIA2026022675603](https://openairdocs.org/sdr/SWIA2026022675603.md): Panel · loose · Feb 26, 2026 · N726SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > RIGHT WING LEADING EDGE PANEL 622BR HAS SEVERAL LOOSE FASTENERS AND THREE PULLED THROUGH FASTNERS 0N THE INBOARD SIDE, COMPLIED WITH TEMPORARY REPAIR OF MULTIPLE DAMAGED HOLES FOR RIGHT WING LEADING PANEL 622BR REF. REO 670-57-41-682 REV.-A,
- [SDR SWIA2026020475611](https://openairdocs.org/sdr/SWIA2026020475611.md): Intercostal · cracked · Feb 4, 2026 · N726SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING THE LH TRU LANDING INSTALLATION CRACK FOUND ON LH INTERCOSTAL ELECTRIC BAY FLOOR BETWEEN FS 173.00 AND FS 193.00 MX# 31653855 (C-CHECK RO 03/28/2026)REMOVED AND REPLACED INTERCOSTAL P/N CC670-33194-7. REF. CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-1
- [SDR SWIA2026020275609](https://openairdocs.org/sdr/SWIA2026020275609.md): Vane · chafed · Feb 2, 2026 · N726SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE OUTBD LEADING EDGE CAP CHAFED IN MULTIPLE SPOTS. REMOVED AND REPLACED CHAFED LT INBD FLAP VANE, OUTBD LEADING EDGE CAP WITH NEW CAP USING ALL NEW FASTENERS, IAW DWG CC670-14010 REV -F AND SRM 51-42-10-001-001 A01.
- [SDR SWIA2026012975619](https://openairdocs.org/sdr/SWIA2026012975619.md): Hinge Arm · chafed · Jan 29, 2026 · N726SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT INBOARD FLAP OUTBOARD HINGE ARM BOTH FAIRING PLATES CHAFED. REMOVED AND REPLACE LEFT INBOARD FLAP OUTBOARD HINGE ARM, IB FAIRING AND OB (2EA.) FAIRING PLATES WITH NEW REF. CRJ700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-45-00-001-001-A01.
- [SDR SWIA2026012975618](https://openairdocs.org/sdr/SWIA2026012975618.md): Plate · chafed · Jan 29, 2026 · N726SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT INBOARD FLAP INBOARD HINGE ARM BOTH FAIRING PLATES CHAFED REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD HINGE ARM BOTH FAIRING PLATES P/N: CC670-14138-1 AND CC670-14138-2 REF. CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-15-001-001-A01.
- [SDR SWIA2026012975601](https://openairdocs.org/sdr/SWIA2026012975601.md): Angle · corroded · Jan 29, 2026 · N726SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SURROUND STRUCTURE KICK PLATE ANGLE (STGR 17L TO 18L) HAS CORROSION (C-CHECK RO 03/28/2026)REMOVED AND REPLACED CORRODED KICKPLATE ANGLE WITH NEW KICK PLATE ANGLE (P/N: SH670-31875-3) USING NEW FASTENERS, REF CRJ700 SRM 51-42-21-001-001-A01, SR
- [SDR SWIA2026012675610](https://openairdocs.org/sdr/SWIA2026012675610.md): Latch Catch · cracked · Jan 26, 2026 · N726SK · Cndair CL6002C10 · Fuselage Main, Structure
  > POSSIBLE CRACK ON LEFT TRU LANDING AFT LATCH CATCH. REMOVED AND REPLACED LEFT TRU LANDING. REF. SRM 51-42-06-001-001-A01, REO 670-53-11-2268 REV.- AND DWG CC670-33040 REV. -G SHEET 2.
- [SDR SWIA2026012475615](https://openairdocs.org/sdr/SWIA2026012475615.md): Slat Track · worn · Jan 24, 2026 · N726SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-1, LOWER FACE HAS WORN AREA AND FORWARD OUTBOARD IS SCUFFED/SCRATCHES, BLENDED OUT WORN AREA AND SCRATCH ON LT WING SLAT TRACK 1-1, LOWER FACE AND FORWARD OUTBOARD SIDE ( TOTAL 5 BLENDS) REF. SRM 51-12-00-001-001-A01.FOUND TO BE OUT OF LIMI
- [SDR SWIA2026012475614](https://openairdocs.org/sdr/SWIA2026012475614.md): Skin · scratched · Jan 24, 2026 · N726SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN, FS977 STGR 27 HAS SCUFFING COMPLIED WITH CRJ700 MHIRJ REO 670-53-00-290 REV -F DATED: 2019/04/26 (SOLUTION 2, FIGURE 8) & (SOLUTION 1 FIGURE 7)SEE CONTINUE CARD FOR DETAILS,LEAK CHECK GOOD,COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2026012375604](https://openairdocs.org/sdr/SWIA2026012375604.md): Fitting · worn · Jan 23, 2026 · N726SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR, EXTERNAL SURROUND, AFT CAM FITTING WORN, REMOVED AND REPLACED PAX DOOR, EXTERNAL SURROUND FS.349, AFT UPPER CAM FITTING SH670-31913-3 WITH NEW REF. SRM 51-42-21-001-001-A01 AND DWG# SH670-31810 REV. AE.
- [SDR SWIA2026012375602](https://openairdocs.org/sdr/SWIA2026012375602.md): Skin · worn · Jan 23, 2026 · N726SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR, EXTERNAL SURROUND, FORWARD CAM FITTING WORN, REMOVED AND REPLACE PAX FWD DOOR SURROUND CAM FITTING (FS310) WITH NEW REF. SRM 51-42-21-001-001-A01 AND DWG #SH670-31810 REV. AE.
- [SDR SWIA2026011975606](https://openairdocs.org/sdr/SWIA2026011975606.md): Stand Off · cracked · Jan 19, 2026 · N726SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RH UPPER TRANSCOWL INBD A BRACKET STANDOFF IS CRACKED. REMOVED CRACKED INBD A BRACKET STANDOFF FROM RT UPPER TRANSCOWL AND INSTALLED 1 EA NEW INBD A BRACKET STANDOFF, ON RT UPPER TRANSCOWL, REF. GREO #670-54-21-971, REV (-B),
- [SDR SWIA2026011975605](https://openairdocs.org/sdr/SWIA2026011975605.md): Floorbeam · cracked · Jan 19, 2026 · N726SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > S 280 CROSSBEAM AND RIGHT FWD OTBD, RBL 9 HAS A CRACKED ANGLE, REMOVED AND REPLACED THE ANGLE TO RBL 12, FS.280 FLOOR BEAM WITH NEW REF. SRM 51-42-21-001-001-A01, & DWG CC670-34010, REV.-K.
- [SDR SWIA2026011375612](https://openairdocs.org/sdr/SWIA2026011375612.md): Drag Angle · cracked · Jan 13, 2026 · N726SK · Cndair CL6002C10 · Vertical Stabilizer
  > VERTICAL STAB. LH SIDE AFT DRAG ANGLE HAS POSSIBLE CRACKED. REPLACED VERTICAL STAB. LH SIDE AFT DRAG ANGLE REF CRJ700 51-42-21-001-001-A01, CRJ700 51-42-13-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01 AND DWG BA670-35002 REV: F. COMPLIED WITH 51-900-1002-S
- [SDR SWIA2026011375607](https://openairdocs.org/sdr/SWIA2026011375607.md): Vane · chafed · Jan 13, 2026 · N726SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LT INBD FLAP VANE, LEADING EDGE CHAFED AT MULTIPLE SPOTS. R & R LT INBD FLAP VANE LEADING EDGE WITH NEW IAW SRM 51-42-10-001-001-A01, & DWG CC670-14010 REV -F.
- [SDR SWIA2026010675613](https://openairdocs.org/sdr/SWIA2026010675613.md): Door · dented · Jan 6, 2026 · N726SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > ADM# N726SK-8479 - 6 O'CLOCK POSITION LT ENGINE COWL FAN DOOR. 6 O"CLOCK POSITION LT ENGINE LOWER COWL FAN DOOR 3 INCH LONG DENT BY 1.5" WIDE. 0.020 DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDA
- [SDR SWIA2026010575608](https://openairdocs.org/sdr/SWIA2026010575608.md): Hinge · gouged · Jan 5, 2026 · N726SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > FOUND GOUGING DAMAGE ON FWD SIDE OF PAX DOOR HINGE, DOOR SIDE AT BS 320. COMPLIED WITH REO 670-52-11-511 TYPE 1 REPAIR. COMPLY WITH PERMANENT REPAIR OF FWD SIDE OF PAX DOOR HINGE LUG AT FS320.00,WITHIN 5000 FLIGHT CYCLES. COMPLIED WITH PERMANENT REPAIR OF FW
- [SDR SWIA2025081375617](https://openairdocs.org/sdr/SWIA2025081375617.md): Roller · out of limits · Aug 13, 2025 · N726SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 700 RH - DISCARD THE RH SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2 (P/N CC670-12272-1 OR PN YR1319). REMOVE AND REPLACE IAW TASK CARD 27-630-809 (MRB 27-81-43-717), DISCARDED THE RH SLAT T
- [SDR SWIA2025081375616](https://openairdocs.org/sdr/SWIA2025081375616.md): Roller · out of limits · Aug 13, 2025 · N726SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 700 LH - DISCARD THE LH SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2 (P/N CC670-12272-1. REMOVE AND REPLACE IAW TASK CARD 27-530-809 (MRB 27-81-43-717), REMOVED AND INSTALLED NEW L/H TRACK SE
- [SDR SWIA202505300029](https://openairdocs.org/sdr/SWIA202505300029.md): Hinge · gouged · May 29, 2025 · N726SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > FOUND GOUGING DAMAGE ON FWD SIDE OF PAX DOOR HINGE DOOR SIDE AT FS320.00 (FILED CLOSED)FOUND PAX DOOR HINGE DOOR SIDE LUG AT FS 320.00 TO BE.1545" IN LENGTH,.0016" IN DEPTH, AND.0305" IN WIDTH. BLENDED GOUGING DAMAGE ON FWD SIDE OF PAX DOOR HINGE SIDE AT FS
- [SDR SWI2024F00111](https://openairdocs.org/sdr/SWI2024F00111.md): Seat Track · missing · Feb 2, 2024 · N726SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK EXTRUSION MISSING AT SEAT 2A (FILED CLOSED)INSTALLED SERVICEABLE SEAT TRACK EXTRUSION AT SEAT 2A, REFERENCE APPLICABLE STEPS IN CRJ700AMM 25-21-01
- [SDR SWIA202264757](https://openairdocs.org/sdr/SWIA202264757.md): None · corroded · Feb 21, 2022 · N726SK · Cndair CL600* · Ailerons
  > L/H INBD FLAP. UPPER FLAP VANE ACTUATOR MOUNT HARDWARE CORRODED, UNDER 584AB ACCESS PANEL. (C CHECK RO 02/25/2022) INSTALLED NEW SERVICEABLE HARDWARE PER CRJ700 AMM 27-52-23-400-801-A01 OPS CHECK GOOD AT THIS TIME
- [SDR SWIA202264756](https://openairdocs.org/sdr/SWIA202264756.md): None · corroded · Feb 3, 2022 · N726SK · Cndair CL600* · Ailerons
  > L/H INBD FLAP. UPPER FLAP VANE ACTUATOR MOUNT HARDWARE CORRODED, UNDER 584AB ACCESS PANEL. (C CHECK RO 02/25/2022) REMOVED AND REPLACED LH INB FLAP VANE ACTUATOR HARDWARE UNDER PANEL 584AB REF CRJ 700 AMM 27-52-23-400-801-A01 OPS TEST GOOD
- [SDR SWIA202264725](https://openairdocs.org/sdr/SWIA202264725.md): None · chafed · Jan 29, 2022 · N726SK · Cndair CL600* · Powerplant System
  > ON R/H UPPER TRANSCOWL, INNER COAMING HAS CHAFE DAMAGE AT FWD EDGE. (C CHECK RO 02/25/2022) ON R/H UPPER TRANSCOWL, REPAIRED CHAFE DAMAGE ON INNER COAMING AT FWD EDGE, REF. REO 670-54-21-1514, REV. --, 2022-02-03 ALL STEPS CW. COMPLIED WITH TASK CARD 5
- [SDR SWIA202264724](https://openairdocs.org/sdr/SWIA202264724.md): None · corroded · Jan 28, 2022 · N726SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > 1 EA CLEAT ON PAX DOOR @ DD1A AND FS320.00 HAS CORROSION (C CHECK RO 02/25/2022) REMOVED AND REPLACED CLEAT @ DD1A AND FS320.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202264723](https://openairdocs.org/sdr/SWIA202264723.md): None · corroded · Jan 28, 2022 · N726SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > 1 EA CLEAT ON PAX DOOR @ DD1A AND FS323.00 HAS CORROSION (C CHECK RO 02/25/2022) REMOVED AND REPLACED CLEAT @ DD1A AND FS323.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA202264755](https://openairdocs.org/sdr/SWIA202264755.md): None · cracked · Jan 26, 2022 · N726SK · Cndair CL600* · Doors
  > PAX DOOR AFT COUNTER-BALANCE BEAM IS CRACKED (C CHECK RO 02/25/2022) REMOVED DAMEGED BEAM, LOCATED, DRILLED, AND INSTALLED NEW PAX DOOR AFT COUNTE-RBALANCE BEAM. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31707 REV -E
- [SDR SWIA202264741](https://openairdocs.org/sdr/SWIA202264741.md): None · damaged · Jan 25, 2022 · N726SK · Cndair CL600* · Doors
  > AFT CARGO DOOR - THE AFT LOWER TRACK STOP IS UNSERVICEABLE (C CHECK RO 02/25/2022) REMOVED AND REPLACED AFT CARGO DOOR AFT LOWER TRACK STOP REF CRJ 700 AMM 52-31-23-400-802-A01 OPS TEST GOOD
- [SDR SWIA202264722](https://openairdocs.org/sdr/SWIA202264722.md): None · damaged · Jan 24, 2022 · N726SK · Cndair CL600* · Nacelle/Pylon, Frame/Spar/Rib
  > SPLICE FRAME AT FS 469 STGR 16 RH TO FOM (C CHECK RO 02/25/2022) ACCOMPLISHED SPLICE FRAME REPAIR AT FS 469 STGR 16 RH TO FOM REF REO 670-53-21-2226 REV -- 2022-01-25 COMLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202264740](https://openairdocs.org/sdr/SWIA202264740.md): None · worn · Jan 22, 2022 · N726SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > SLAT-TRACK SIDE ROLLER 3-2, BOTH TOP AND BOTTOM SIDE ROLLERS HAVE DAMAGE. P/N: CC670-12459-3 ROLLER, CC670-12459-4 ROLLER, CC670-12087-1 SHIM. (C CHECK RO 02/25/2022) DICREPANCY MISSING LOCATION. REMOVED AND INSTALLED 4 NEW ROLLERS ON LH SLAT TRACK 3-2 REF
- [SDR SWIA202264739](https://openairdocs.org/sdr/SWIA202264739.md): None · worn · Jan 22, 2022 · N726SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > SLAT-TRACK SIDE ROLLER 2-2, BOTH TOP AND BOTTOM SIDE ROLLERS HAVE DAMAGE. P/N: CC670-12048-3 ROLLER, CC670-12027-3 ROLLER, CC670-12087-1 SHIM, CC670-12098-1 SHIM (C CHECK RO 02/25/2022) REMOVED AND REPLACED LH SLAT TRACK 2-2 TOP AND BOTTOM SIDE ROLLERS R
- [SDR SWIA202264738](https://openairdocs.org/sdr/SWIA202264738.md): None · worn · Jan 22, 2022 · N726SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > SLAT-TRACK SIDE ROLLER 1-2, BOTH TOP AND BOTTOM SIDE ROLLER HAVE DAMAGE. P/N: CC670-12027-3 ROLLER, CC670-12048-3 ROLLER, CC670-12087-1 SHIM, CC670-12098-1 SHIM. (C CHECK RO 02/25/2022) DISCREPANCY MISSING LOCATION. REMOVED AND INSTALLED 4 NEW ROLLERS ON
- [SDR SWIA202264754](https://openairdocs.org/sdr/SWIA202264754.md): None · cracked · Jan 19, 2022 · N726SK · Cndair CL600* · Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED (C CHECK RO 02/25/2022) REMOVED AND REPLACED PAX DOOR AFT DOOR DRAG ANGLE P/N 601R31772-5S. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, DRAWING 601R31707 REV -E, AND DRAWING 601R31702 REV N
- [SDR SWIA202264753](https://openairdocs.org/sdr/SWIA202264753.md): None · corroded · Jan 19, 2022 · N726SK · Cndair CL600* · Doors
  > EMERGENCY DOOR, L/H LOWER FORWARD STOP FITTING HAS DAMAGED HOLE, PITTING, CORROSION INSIDE BORE. PART NO. SH670-36041-3. (C CHECK RO 02/25/2022) REMOVED AND REPLACED 1EA. DAMAGED\CORRODED EMERGENCY DOOR, L/H LOWER FORWARD STOP FITTING, WITH 1EA. NEW EMERGE
- [SDR SWIA202264737](https://openairdocs.org/sdr/SWIA202264737.md): None · worn · Jan 19, 2022 · N726SK · Cndair CL600* · Ailerons
  > LH FLAP STUB FAIRING 171DL, RETAINING PLATE WORN/CHAFFED AND HINGED ATTACH POINT WORN. (C CHECK RO 02/25/2022) REMOVED AND REPLACED 1EA HINGE ASSY P/N CC670-39239-1 ON LH FLAP STUB FAIRING 171DL. CRJ-700 SRM 51-42-21-001-001-A01.
- [SDR SWIA202264721](https://openairdocs.org/sdr/SWIA202264721.md): None · missing · Jan 19, 2022 · N726SK · Cndair CL600* · Powerplant System
  > RH LOWER TRANSCOWL I/B STANDOFF MISSING MATERIAL. (C CHECK RO 02/25/2022) REMOVED AND REPLACED RH LOWER TRANSCOWL INBD STANDOFF P/N CN624-2082-201. REF. REO 670-54-21-971 REV A, DATED 2017/05/11. WEIGHT REMOVED = 0.04LBS. WEIGHT INSTALLED = 0.04LBS. NO WEI
- [SDR SWIA202264720](https://openairdocs.org/sdr/SWIA202264720.md): None · missing · Jan 19, 2022 · N726SK · Cndair CL600* · Powerplant System
  > RH UPPER TRANSCOWL Z ANGLE MISSING FASTENERS & DISBONDED FROM INNER PERFORATE. (C CHECK RO 02/25/2022) REPAIRED R/H UPPER TRANSCOWL Z ANGLE REF MHIRJ REO 670-54-21-1513 REV -- 2022-02-07. COMPLIED WITH SKYCARD 51-900-1002
- [SDR SWIA202264719](https://openairdocs.org/sdr/SWIA202264719.md): None · cracked · Jan 19, 2022 · N726SK · Cndair CL600* · Powerplant System
  > LH LOWER TRANSCOWL OUTER SKIN CRACKED FROM FWD LATCH CUTOUT AFT TOWARDS THE LATCH DOOR CUTOUT. (C CHECK RO 02/25/2022) L/H LOWER TRANSCOWL OUTER SKIN CRACK @ FWD LATCH CUTOUT HAS BEEN REPAIRED REF REO# 670-54-21-1207, REV A, DATED 8/27/15, REO# 670-54-21-1
- [SDR SWIA202264718](https://openairdocs.org/sdr/SWIA202264718.md): None · chafed · Jan 19, 2022 · N726SK · Cndair CL600* · Fuselage Main, Keel
  > STGR8L BETWEEN FS1144 & FS1162 HAS CHAFE DAMAGE NEAR THE WATER INJECTION LINE TUBE. (C CHECK RO 02/25/2022) REMOVED AND REPLACED STRINGER 8L BETWEEN FS1144.00 TO FS1162.00 REF REO 670-53-61-2053, REV --, DATED 2022-02-11, COMPLIED WITH ALL STEPS OF REO, OP
- [SDR SWIA202264717](https://openairdocs.org/sdr/SWIA202264717.md): None · cracked · Jan 19, 2022 · N726SK · Cndair CL600* · Fuselage Floor Panel
  > CRACK FOUND ON R/H COCKPIT FLOOR SUPPORT ANGLE AT RBL 12 FWD OF FS 280 (C CHECK RO 02/25/2022) REMOVED AND REPLACED NEW RH COCKPIT FLOOR SUPPORT ANGLE AT RBL 12.00 BETWEEN FS 250.00 - FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV -G
- [SDR SWIA202264716](https://openairdocs.org/sdr/SWIA202264716.md): None · cracked · Jan 19, 2022 · N726SK · Cndair CL600* · Fuselage Floor Panel
  > CRACK FOUND ON L/H COCKPIT FLOOR SUPPORT ANGLE AT LBL 12 FWD OF FS 280 (C CHECK RO 02/25/2022) REMOVED AND REPLACED NEW LH COCKPIT FLOOR SUPPORT ANGLE AT LBL 12.00 BETWEEN FS 250.00 - FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV -G
- [SDR SWIA202264715](https://openairdocs.org/sdr/SWIA202264715.md): None · corroded · Jan 18, 2022 · N726SK · Cndair CL600* · Doors
  > CORROSION FOUND ON SERVICE DOOR SILL BETWEEN FS319 AND FS347 (C CHECK RO 02/25/2022) COMPLIED WITH REO 670-53-21-2225 REV -- DATE 2022-01-25 STEP1 TO 9 ON SERVICE DOOR SILL BETWEEN FS 319.00 - FS 347.00. SEE CONTINUE CARD FOR MORE DETAILS.
- [SDR SWIA202264714](https://openairdocs.org/sdr/SWIA202264714.md): None · corroded · Jan 18, 2022 · N726SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL DD1 FS323.00 - FS335.00 HAS CORROSION (C CHECK RO 02/25/2022) REMOVED AND REPLACED INTERCOSTAL DD1 FS323.00 €“ FS335.00 / REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N / COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202264713](https://openairdocs.org/sdr/SWIA202264713.md): None · corroded · Jan 18, 2022 · N726SK · Cndair CL600* · Fuselage Main, Frame
  > PAX DOOR AFT FORMER FS347.25 HAS CORROSION (C CHECK RO 02/25/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 /, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N. COMPLIED WITH TASK 51-900-1002-SK
- [SDR SWIA202264765](https://openairdocs.org/sdr/SWIA202264765.md): None · worn · Jan 17, 2022 · N726SK · Cndair CL600* · Rudder/Tab, Attach Fittings
  > * BOTH CENTER RUDDER HINGES ( MOUNTED TO REAR SPAR OF VERTICAL STABILIZER) LOOSE IN / BEARING MOUNT. WORN TO LIMITS. (C CHECK RO 02/25/2022) REPLACED NEW BEARING IN RUDDER HINGE FITTING #2 & RUDER HINGE FITTING #3 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ
- [SDR SWIA202264752](https://openairdocs.org/sdr/SWIA202264752.md): None · cracked · Jan 14, 2022 · N726SK · Cndair CL600* · Fuselage Structure (General)
  > *PASSENGER DOOR €“ LOWER ATTACH ANGLE FOR POWER ASSIST MOTOR (DOOR OPEN POSITION) IS CRACKED. (C CHECK RO 02/25/2022) REMOVED AND REPLACED PAX DOOR MOTOR MOUNTING STIFFENER P/N 601R317745-7. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31707 REV
- [SDR SWIA202264712](https://openairdocs.org/sdr/SWIA202264712.md): None · corroded · Jan 14, 2022 · N726SK · Cndair CL600* · Fuselage Main, Frame
  > *PASSENGER DOOR €“ CORROSION ON FORMER AT FS329.41 BETWEEN DD5 AND DD6. (C CHECK RO 02/25/2022) BLENDED OUT CORROSION AND RESTORED FINISH ON FORMER AT FS329.41 BETWEEN DD5 AND DD6. REF: CRJ-700 SRM 51-21-06-001-001-A01 / AND CRJ-700 SRM 51-25-16-001-001-A
- [SDR SWIA202264711](https://openairdocs.org/sdr/SWIA202264711.md): None · corroded · Jan 14, 2022 · N726SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *PASSENGER DOOR €“ POSSIBLE CORROSION ON CLIP COMMON TO DD6 AND FORMER AT FS329.41. (C CHECK RO 02/25/2022) REMOVED AND REPLACED CLEAT @ DD6 AND FORMER AT FS329.41. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N C/W 51-900-1002-SKY
- [SDR SWIA202264710](https://openairdocs.org/sdr/SWIA202264710.md): None · corroded · Jan 14, 2022 · N726SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *PASSENGER DOOR €“ CORROSION ON DD4 BETWEEN FORMER AT FS338.963 AND FORMER AT FS347.25. (C CHECK RO 02/25/2022) REMOVED AND REPLACED INTERCOSTAL DD4 FS338.963 €“ FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N COMPLIED WITH 5
- [SDR SWIA202264709](https://openairdocs.org/sdr/SWIA202264709.md): None · corroded · Jan 14, 2022 · N726SK · Cndair CL600* · Fuselage Structure (General)
  > *PASSENGER DOOR €“ POSSIBLE CORROSION ON CLIP COMMON TO DD6 AND FORMER AT FS338.963. (C CHECK RO 02/25/2022) REMOVED AND REPLACED CLEAT @ DD6 AND FS338.963. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N C/W 51-900-1002-SKY

Next page: https://openairdocs.org/aircraft/N726SK/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 = 'N726SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N726SK/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.