# Service difficulty reports: N607SK

A list on [N607SK](https://openairdocs.org/aircraft/N607SK.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 · 163 reports

- [SDR SWI2025F00149](https://openairdocs.org/sdr/SWI2025F00149.md): Windshield · cracked · Feb 1, 2025 · N607SK · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAINS WINDSHIELD CRACKED (FLIGHT 6273 - FILED CLOSED) PLEASE REFERENCE AML 1528716 PLEASE REFERENCE AML 1528718 PLEASE REFERENCE AML 1528719 PLEASE REFERENCE AML 1528720 REMOVED AND REPLACED THE LH WINDSHIELD IN REFERENCE TO AMM 56-11-01 AND COM
- [SDR SWIA202266088](https://openairdocs.org/sdr/SWIA202266088.md): None · corroded · Jun 20, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FUSELAGE FRAME FS265 REINFORCEMENT ANGLE CORRODED BETWEEN STGR 26L AND 26R. (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED THE NEW STIFFENER ANGLE TO FRAME FS.265 LOWER SECTION REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG #CC670-34020 REV.-A. COMPLIED
- [SDR SWIA202266087](https://openairdocs.org/sdr/SWIA202266087.md): None · corroded · Jun 6, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON VERTICAL POST AT RBL 12.0 FS 280.0 AT FLOOR LEVEL (C-CHECK RO 7/8/2022) COMPLIED WITH REPAIR ON VERTICAL POST AT RBL 12.0 FS 280.0 AT FLOOR LEVEL REF CRJ 700 SRM 53-11-10-201-006-A01. / COMPLIED WITH SKYWEST TASKCARD 51-900-1002-
- [SDR SWIA202266086](https://openairdocs.org/sdr/SWIA202266086.md): None · corroded · May 26, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 21L BACK UP SILL ATTACH ANGLE (PN SH670-31828-1) COMMON TO FS349.00 FRAME CORRODED (C-CHECK RO 7/8/2022) EVALUATED ATTACH ANGLE AT STR21L COMMON TO FS349.00, EXFOLIATE CORROSION WAS FOUND OUT OF LIMITS. REMOVED AND INSTALLED NEW MA
- [SDR SWIA202266085](https://openairdocs.org/sdr/SWIA202266085.md): None · corroded · May 26, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY FS349.00 FRAME CORRODED BETWEEN STR 26L AND STR 26R (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW FS349.00 FRAME FROM STR 23L TO STR 24R REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG:SH690-31350 REV M. COMPLIED WITH TASK CARD 51-900-
- [SDR SWIA202266084](https://openairdocs.org/sdr/SWIA202266084.md): None · corroded · May 24, 2022 · N607SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > LBL 27 FLOOR BEAM CORRODED AT APPROX. FS1031. (C-CHECK RO 7/8/2022) DAMAGE FOUND TO BE OUT OF LIMITS, REF: CRJ700 SRM 53-61-43-101-001-A01. INSTALLED NEW LBL27 FLOOR BEAM SECTION FROM APPROX. FS1005 - FS1035 WITH SPLICES AND SHIMS. REF: CRJ700 SRM
- [SDR SWIA202266083](https://openairdocs.org/sdr/SWIA202266083.md): None · corroded · May 21, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 CORRODED (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED 1EA NEW STR 23RH SPLICE AT FS333.00 IAW CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWIA202266082](https://openairdocs.org/sdr/SWIA202266082.md): None · cracked · May 20, 2022 · N607SK · Cndair CL6002C10 · Fuselage Floor Panel
  > CRACKED AND CORRODED RH COCKPIT FLOOR SUPPORT ANGLE, FS.274. (C-CHECK RO 7/8/2022) REMOVED AND REPLACED NEW RH COCKPIT FLOOR SUPPORT ANGLE AT FS 265.00 - FS 280.00 CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV -G. COMPLIED WITH TASK CARD 51-90
- [SDR SWIA202266081](https://openairdocs.org/sdr/SWIA202266081.md): None · gouged · May 20, 2022 · N607SK · Cndair CL6002C10 · Ailerons
  > * R/H INBOARD FLAP, OUTBOARD HINGE ARM LOWER LUG IS GOUGED, MARKED. (C-CHECK RO 7/8/2022) BLENDED OUT GOUGE ON R/H INBOARD FLAP OUTBOARD HINGE ARM LOWER LUG REF CRJ 700 SRM 51-12-00-001-001-A01. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS
- [SDR SWIA202266080](https://openairdocs.org/sdr/SWIA202266080.md): None · corroded · May 18, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Frame
  > 2 EA CLEATS @ FS339.963 AND LOWER CHANNEL HAVE INTERGRANULAR CORROSION (C-CHECK RO 7/8/2022) REMOVED 2 EA CLEATS @ FS339.963 AND LOWER CHANNEL REF CRJ700 SRM51-42-06-001-001-A01 / AND INSTALLED NEW (2EA) CLEATS @ FS339.963 AND LOWER CHANNEL REF: CRJ-7
- [SDR SWIA202266079](https://openairdocs.org/sdr/SWIA202266079.md): None · cracked · May 17, 2022 · N607SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > R/H VERTICAL STAB AFT DRAG ANGLE IS CRACKED (C-CHECK RO 7/8/2022) REMOVED DAMAGED AND INSTALLED REPAIR DOUBLER AND FILLER ON R/H AFT DRAG ANGLE. REF: CRJ700 SRM 55-31-00-201-001-A01. / COMPLIED WITH TASKCARD 51-900-1002-SKY
- [SDR SWIA202266078](https://openairdocs.org/sdr/SWIA202266078.md): None · corroded · May 17, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON ANGLE COMMON WITH INTERCOSTAL BETWEEN FS 517.00 - FS 533. AND BETWEEN STGR 22LH - 23LH (C-CHECK RO 7/8/2022) REMOVED CORROSION ON ANGLE COMMON WITH INTERCOSTAL BETWEEN FS517.00-FS533.00 AND BETWEEN STGR 22L AND STGR 23L REF. CRJ-
- [SDR SWIA202266077](https://openairdocs.org/sdr/SWIA202266077.md): None · corroded · May 17, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > DURING REMOVAL CORROSION WAS FOUND ON INTERCOSTAL BETWEEN FS 517.00 - FS 533. AND BETWEEN STGR 22LH - 23LH (C-CHECK RO 7/8/2022) REMOVED CORROSION ON INTERCOSTAL BETWEEN FS517.00-FS533.00 BETWEEN STGR 22L AND STGR 23L REF. CRJ-700 SRM, 51-21-06-001-001
- [SDR SWIA202266076](https://openairdocs.org/sdr/SWIA202266076.md): None · corroded · May 16, 2022 · N607SK · Cndair CL6002C10 · Doors
  > PAX DOOR FORMER FS329.41, DD5 AND DD6 HAS INTERGRANULAR CORROSION ON MORE THAN ONE ELEMENT (C-CHECK RO 7/8/2022) INSTALLED NEW PAX DOOR FORMER FS329.41, DD5 AND DD6. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH SKYWES
- [SDR SWIA202266075](https://openairdocs.org/sdr/SWIA202266075.md): None · corroded · May 16, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY FS319.70 FRAME CORRODED ON SEVERAL ATTACH FLANGES BETWEEN STR 21L AND STR 26R (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW FS319.70 FRAME FROM STR 21L TO STR 23R REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A0
- [SDR SWIA202266074](https://openairdocs.org/sdr/SWIA202266074.md): None · corroded · May 14, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS310.00 AND FS319.70 (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW STR 23R FROM FS280.00 TO FS333.00 REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND DWG:SH670-31630 REV K. COMPLIE
- [SDR SWIA202266073](https://openairdocs.org/sdr/SWIA202266073.md): None · corroded · May 14, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 22R CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW STR 22R FROM FS280.00 TO FS333.00 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV K. COMPLIED
- [SDR SWIA202266072](https://openairdocs.org/sdr/SWIA202266072.md): None · corroded · May 14, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS310.00 AND FS319.70 (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW STR 21R FROM FS280.00 TO FS333.00 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV K. COMPLIED
- [SDR SWIA202266071](https://openairdocs.org/sdr/SWIA202266071.md): None · corroded · May 13, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Frame
  > 2 EA CLEATS @ FS320.00 FRAME AND LOWER CHANNEL HAS INTERGRANULAR CORROSION (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW 2 EA CLEATS @ FS320.00 FRAME AND LOWER CHANNEL. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH
- [SDR SWIA202266070](https://openairdocs.org/sdr/SWIA202266070.md): None · corroded · May 13, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > 2 EA CLEATS @ INTERCOSTAL DD4 BETWEEN FS311.74 AND FS320.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 7/8/2022) REMOVED AND REPLACED 2 EA CLEATS @ INTERCOSTAL DD4 BETWEEN FS311.74 AND FS320.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 R
- [SDR SWIA202266069](https://openairdocs.org/sdr/SWIA202266069.md): None · corroded · May 13, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > 1 EA CLEAT @ INTERCOSTAL DD6 AND FS320.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 7/8/2022) REMOVED DAMAGED 1 EA CLEAT @ INTERCOSTAL DD6 AND FS320.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 / AND INSTALLED NEW 1 EA CLEAT @ INTERCOSTAL DD6 AND FS320.00.
- [SDR SWIA202266068](https://openairdocs.org/sdr/SWIA202266068.md): None · corroded · May 13, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE €“ CORROSION ON STRINGER @ FS 533 AND STGR23L (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW STRINGER 23L BETWEEN FS533 AND FS477. REF. CRJ700 SRM 51-42-06-001-001-A01 AND DWG # SH670-33200 REV. G. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202266067](https://openairdocs.org/sdr/SWIA202266067.md): None · cracked · May 12, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > *R/H WINDSHIELD SIDE POST IS CRACKED (MARKED) (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW WINDSHIELD SIDE POST P/N 601R33223-2. REF: DWG CC670-33055, REV: F, CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. OPERATIONAL AND L
- [SDR SWIA202266066](https://openairdocs.org/sdr/SWIA202266066.md): None · cracked · May 12, 2022 · N607SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > *R/H VERTICAL STAB DRAG ANGLE IS CRACKED (MARKED) (C-CHECK RO 7/8/2022) REMOVED DAMAGED AND: INSTALLED REPAIR DOUBLER AND FILLER ON R/H FWD DRAG ANGLE. REF: CRJ700 SRM 55-31-00-201-001-A01. / COMPLIED WITH TASKCARD 51-900-1002-SKY
- [SDR SWIA202266065](https://openairdocs.org/sdr/SWIA202266065.md): None · corroded · May 12, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 21L BACK-UP SILL CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW STR 21L BACK-UP SILL BETWEEN FS319.70 AND FS333.00 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG
- [SDR SWIA202266064](https://openairdocs.org/sdr/SWIA202266064.md): None · corroded · May 11, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE - STGR 23L CORRODED BTWN FS'S 581/597 (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW STGR 23L SECTION BETWEEN FS581 AND FS603.5. REF. CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-33200 REV. G. AND REO 670-53-31-783 REV -- DATED 2022-05-31
- [SDR SWIA202266063](https://openairdocs.org/sdr/SWIA202266063.md): None · corroded · May 11, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 24L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 7/8/2022) REMOVED AND REPLACED NEW STGR 24L FROM FS 280.00 - FS 333.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV -K. COMPLIED
- [SDR SWIA202266062](https://openairdocs.org/sdr/SWIA202266062.md): None · corroded · May 11, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 7/8/2022) REMOVED AND REPLACED STR 23L BETWEEN FS280.00 AND FS333.00 REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV K. COMPLIE
- [SDR SWIA202266061](https://openairdocs.org/sdr/SWIA202266061.md): None · corroded · May 11, 2022 · N607SK · Cndair CL6002C10 · Doors
  > PAX DOOR LOWER CHANNEL P/N 601R318074-5 IS CORRODED (C-CHECK RO 7/8/2022) INSTALLED NEW PAX DOOR LOWER CHANNEL P/N 601R318074-5. 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 SKYWEST T
- [SDR SWIA202266060](https://openairdocs.org/sdr/SWIA202266060.md): None · corroded · May 11, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > PAX DOOR FRAME FS320.00 P/N 601R318032-5 HAS INTERGRANULAR CORROSION (C-CHECK RO 7/8/2022) INSTALLED NEW PAX DOOR FRAME FS320.00 P/N 601R318032-5. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N. COMP
- [SDR SWIA202266059](https://openairdocs.org/sdr/SWIA202266059.md): None · corroded · May 11, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 7/8/2022) REMOVE AND INSTALLED NEW STRINGER 24R FROM FS333 TO FS352.00 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 53-00-03-201-001-A01. COMPLIED WITH TASK CARD 51-900
- [SDR SWIA202266058](https://openairdocs.org/sdr/SWIA202266058.md): None · corroded · May 11, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 7/8/2022) REMOVED STR 23R FROM FS333.00 TO FS379.00 REF. CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED NEW STR 23R FROM FS333.00 TO FS379.00 REF. CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202266057](https://openairdocs.org/sdr/SWIA202266057.md): None · corroded · May 10, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL DD2 FS320.163 - FS338.963 IS CORRODED (C-CHECK RO 7/8/2022) INSTALLED NEW PAX DOOR INTERCOSTAL DD2 FS320.163 - FS338.963. 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
- [SDR SWIA202266056](https://openairdocs.org/sdr/SWIA202266056.md): None · corroded · May 10, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION ON STGR19R BETWEEN FS549.00-FS581.00 (MARKED) (C-CHECK RO 7/8/2022) REMOVED CORROSION ON STGR19R BETWEEN FS549.00-FS581.00 PER CRJ700 SRM 51-21-06-001-001-A01, OUT OF LIMITS / REPAIRED AND INSTALLED ALL REPAIR PARTS FOR STRINGER 19R REPAIR BE
- [SDR SWIA202266055](https://openairdocs.org/sdr/SWIA202266055.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > RH FS.280 LOWER BULKHEAD WEB HAS CORROSION AT RBL 12 FLOOR LEVEL. (C-CHECK RO 7/8/2022) REPAIRED RH FS.280 LOWER BULKHEAD REF CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM M-337. SEE CONTINUE CARD FO MORE DETAILS.
- [SDR SWIA202266054](https://openairdocs.org/sdr/SWIA202266054.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LH FS.280 LOWER BULKHEAD WEB HAS CORROSION AT LBL 12 FLOOR LEVEL. (C-CHECK RO 7/8/2022) REPAIRED LH FS.280 LOWER BULKHEAD REF CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM M-337. SEE CONTINUE CARD FO MORE DETAILS.
- [SDR SWIA202266053](https://openairdocs.org/sdr/SWIA202266053.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Galley Doors
  > *SERVICE DOOR SEAL STRIKER HAS MULTIPLE SPOTS OF CORROSION AROUND THE FASTENER HOLES (MARKED) (C-CHECK RO 7/8/2022) REPLACED SERVICE DOOR SEAL STRIKER REF CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND DWG SH670-31950, REV Y LEAK CHECK GOO
- [SDR SWIA202266052](https://openairdocs.org/sdr/SWIA202266052.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > *LH PRESSURE FLOOR SILL HAS CORROSION PRESENT AT APPROX. FS.745.00 (MARKED) (C-CHECK RO 7/8/2022) REMOVED CORROSION ON LH PRESSURE FLOOR SILL AT APPROX. FS 745.00 IAW CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH
- [SDR SWIA202266051](https://openairdocs.org/sdr/SWIA202266051.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > *RH PRESSURE FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION AT APPROX. FS.773.50 (MARKED) (C-CHECK RO 7/8/2022) REMOVED CORROSION FOR RH PRESSURE FLOOR SILL ANGLE AT FS 773.5 AND FS 780.00 (AS MARKED) PER REFERENCE CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO
- [SDR SWIA202266050](https://openairdocs.org/sdr/SWIA202266050.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > *LH PRESSURE FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION AT APPROX. FS.773.50 (MARKED) (C-CHECK RO 7/8/2022) REMOVED MULTIPLE SPOTS OF CORROSION ON LH PRESSURE FLOOR SILL AT APPROX. FS.773.50 IAW CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS
- [SDR SWIA202266049](https://openairdocs.org/sdr/SWIA202266049.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE - TIEDOWN PLATE CORRODED BTWN FS'S 549/565 AND BTWN STGRS 26L/27 (C-CHECK RO 7/8/2022) REPLACED FWD BAGGAGE - TIEDOWN PLATE FS 549/565 AND BTWN STGRS 26L/27 WITH NEW PN SH670-33574-5 PO# T-64024 REF CRJ 700 SRM 51-42-06-001-001-A01 AND BOMB
- [SDR SWIA202266048](https://openairdocs.org/sdr/SWIA202266048.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE - TIEDOWN PLATE CORRODED FS 581 AND BTWN STGRS 22L/23L (C-CHECK RO 7/8/2022) REPLACED FWD BAGGAGE - TIEDOWN PLATE FS 581 AND BTWN STGRS 22L/23L WITH NEW PN SH670-33390-2 PO# T-63304 REF CRJ 700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH6
- [SDR SWIA202266047](https://openairdocs.org/sdr/SWIA202266047.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE - TIEDOWN PLATE CORRODED FS 581 AND BTWN STGRS 26L/27 (C-CHECK RO 7/8/2022) REPLACED FWD BAGGAGE - TIEDOWN PLATE FS 581 AND BTWN STGRS 26L/27 WITH NEW PN SH670-33389-2 PO# T-61666 REF CRJ 700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670
- [SDR SWIA202266046](https://openairdocs.org/sdr/SWIA202266046.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE - TIEDOWN PLATE CORRODED FS 549 AND BTWN STGRS 24R/25R (C-CHECK RO 7/8/2022) INSTALLED ALL PARTS, TIE DOWN PLATE, STIFFENER AND INTERCOSTAL AND FRAME CLIPS FROM FS 549 TO FS 565 BETWEEN STR 24R AND STR 25R PER REFERENCE CRJ 700 SRM 51-42-21-
- [SDR SWIA202266045](https://openairdocs.org/sdr/SWIA202266045.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE - TIEDOWN PLATE CORRODED FS 533 AND BTWN STGRS 26L/27 (C-CHECK RO 7/8/2022) REMOVED AND REPLACED CORRODED TIE-DOWN PLATE AT FS 533 AND BETWEEN STR 27 - 26L WITH NEW UNIT. REF CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING# SH670-33600 REV AD.
- [SDR SWIA202266044](https://openairdocs.org/sdr/SWIA202266044.md): None · corroded · May 7, 2022 · N607SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD BAGGAGE - TIEDOWN PLATE CORRODED JUST FORWARD OF FW 533 AND BTWN STGRS 22L/23L (C-CHECK RO 7/8/2022) REMOVED CORROSION IN FWD BAGGAGE BAY TIE-DOWN FITING/MACHINED BRACKET FWD OF FS533.00 BETWEEN STGR 22L AND STGR 23L REF. CRJ-700 SRM, 51-21-06-001-0
- [SDR SWIA202266043](https://openairdocs.org/sdr/SWIA202266043.md): None · corroded · May 6, 2022 · N607SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > RH FS.280 FLOOR CROSSBEAM HAS CORROSION BETWEEN BL0 AND RBL12. (C-CHECK RO 7/8/2022) REMOVED AND REPLACED NEW RH CROSSBEAM AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 AND DWG CC670-
- [SDR SWIA202266042](https://openairdocs.org/sdr/SWIA202266042.md): None · corroded · May 6, 2022 · N607SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > LH FS.280 FLOOR CROSSBEAM HAS CORROSION BETWEEN BL0 AND LBL12. (C-CHECK RO 7/8/2022) REMOVED AND REPLACED NEW LH CROSSBEAM AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 AND DWG CC670-
- [SDR SWIA202266041](https://openairdocs.org/sdr/SWIA202266041.md): None · corroded · May 6, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > RH NOSE JACKING PAD INTERCOSTAL BETWEEN FS.265 AND FS.280 HAS CORROSION. (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW R/H JACK PAD INTERCOSTAL P/N: CC670-32179-2. REF: DWG CC670-32050, REV: NC, CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21
- [SDR SWIA202266040](https://openairdocs.org/sdr/SWIA202266040.md): None · corroded · May 6, 2022 · N607SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > LH NOSE JACKING PAD INTERCOSTAL BETWEEN FS.265 AND FS.280 HAS CORROSION. (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW L/H JACK PAD INTERCOSTAL P/N CC670-32179-1. REF: DWG CC670-32050, REV: NC, CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-

Next page: https://openairdocs.org/aircraft/N607SK/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 = 'N607SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N607SK/reports

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