# Service difficulty reports: N816SK

A list on [N816SK](https://openairdocs.org/aircraft/N816SK.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 6 · 294 reports

- [SDR SWIA2026050175990](https://openairdocs.org/sdr/SWIA2026050175990.md): Controller · warning message · May 1, 2026 · N816SK · Cndair CL6002D24 · Pitot/Static Anti-Ice System
  > L PITOT HEAT CAUTION DURING CLIMB OUT IN ICING CONDITIONS. RAN QRH, PROBLEM DID NOT RESOLVE. (FLIGHT 3589) REMOVED AND REPLACED L PITOT HEAT ADS HEAT CONTROLLER PER CRJ 900 AMM 30-31-15. OPERATIONAL TEST GOOD. PERFORMED OPERATIONAL TEST OF ICE DETECTOR SENS
- [SDR SWIA2026031075903](https://openairdocs.org/sdr/SWIA2026031075903.md): Skin · damaged · Mar 10, 2026 · N816SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SIGNS OF LIGHTENING DAMAGE BETWEEN RIVET AND SKIN FWD OF BS 453 ABOVE STR 2L. REPAIRED DAMAGE ON EXTERIOR FUSELAGE SKIN BS 453, STR 2L IAW REO 690-53-21-2117, REV - (P1), AND SRM 51-42-06, 53-00-00, 51-12-00, 51-25-01, AMM 21-31-00. NDT PERFORMED.
- [SDR SWIA2025121975902](https://openairdocs.org/sdr/SWIA2025121975902.md): Rib · cracked · Dec 19, 2025 · N816SK · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > RIGHT WING L/E RIB AT WS 58.41 CRACKED. PERFORMED REPAIR ON RT WING L/EDGE RIB AT WS58.41 IAW SRM 51-42-15, AMM 57-41-32, REO 690-57-41-582 REV--(P1), REO 690-57-41-582, REV-. PERFORMED INSPECTION.
- [SDR SWIA2025121975900](https://openairdocs.org/sdr/SWIA2025121975900.md): Rib · cracked · Dec 19, 2025 · N816SK · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > LEFT L/E RIB AT WS 58.41 CRACKED. PERFORMED REPAIR AT LT LE RIB IAW SRM 53-24-15, 51-25-16, AMM 57-41-32, &REO 690-57-41-581, REV -. PERFORMED NDT INSPECTION.
- [SDR SWIA2025121875899](https://openairdocs.org/sdr/SWIA2025121875899.md): Bulkhead Web · corroded · Dec 18, 2025 · N816SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > SIGNS OF CORROSION BETWEEN THE LT 280 WEB AND THE POST AT LBL 12. R & R BULKHEAD LOWER WEB IAW AMM 20-70-00, SRM 53-00-00, 51-42-06, 51-42-13, 51-42-21, 53-11-10, 51-21-11, 51-25-06, & 51-42-24.
- [SDR SWIA2025121675901](https://openairdocs.org/sdr/SWIA2025121675901.md): Door Frame · gouged · Dec 16, 2025 · N816SK · Cndair CL6002D24 · Fuselage Main, Structure
  > PASSENGER DOOR CUTOUT AT STR 5L, BS 310 GOUGED. REPAIRED THE DAMAGE ON THE PAX DOOR CUTOUT AT STR 5L BS 310 IAW REO 690 53-21-2122, REV-- DATE 2026-04-04 AND SRM 53-21-01. NDT PERFORMED
- [SDR SWI2023120600565](https://openairdocs.org/sdr/SWI2023120600565.md): Unknown · leaking · Dec 5, 2023 · N816SK · Cndair CL6002D24 · Flight Compartment Windows
  > DUE TO RH SIDE WINDOW FAILING LEAK CHECK RH SIDE WINDOW MUST BE REMOVED. (FILED CLOSED)REMOVED RH SIDE WINDOW IN REF WITH CRJ900 AMM 56-12-01. REF ML 27508670 FOR INSTALLATION OF RH SIDE WINDOW.
- [SDR SWIA202266850](https://openairdocs.org/sdr/SWIA202266850.md): None · cracked · Oct 13, 2022 · N816SK · Cndair CL6002D24 · Doors
  > PAX DOOR LINTEL STGR3L FS280 CRACKED (C-CHECK RO 11/10/2022) REPAIRED PAX DOOR LINTEL STGR3L FS280 REF REO 670-53-21-493, REV -D, 2015-07-10. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWIA202265747](https://openairdocs.org/sdr/SWIA202265747.md): None · corroded · Apr 12, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STGR 21R JOINT PIECE CORRODED AT LAV DRAIN UPPER DIAPHRAGM. (C CHECK RO 5/23/22) REMOVED AND REPLACED NEW STGR21R JOINT PIECE AT LAV DRAIN UPPER DIAPHRAGM REF. CRJ-900 AMM, 51-42-06-001-001-A01 AND DWG SH670-32280 REV H. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA202265746](https://openairdocs.org/sdr/SWIA202265746.md): None · corroded · Apr 11, 2022 · N816SK · Cndair CL6002D24 · Water and Waste System
  > CHANNEL ON LAV DRAIN LOWER DIAPHRAGM CORRODED. (C CHECK RO 5/23/22) REMOVED AND REPLACED IMPACT CHANNEL FROM LOWER DIAPHRAGM ON LAV DRAIN REF. CRJ-900 SRM, 51-42-06-001-001-A01 AND DWG SH670-32280 REV H. COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK CH
- [SDR SWIA202265745](https://openairdocs.org/sdr/SWIA202265745.md): None · corroded · Apr 11, 2022 · N816SK · Cndair CL6002D24 · Water and Waste System
  > UPPER DIAPHRAM AT LAV DRAIN CORRODED. (C CHECK RO 5/23/22) REMOVED AND INSTALLED NEW UPPER DISPHRAGM AT LAV DRAIN AND SUPPORT ANGLE REF. CRJ-900 SRM, 51-42-06-001-001-A01 AND DWG SH670-32280 REV H. COMPLIED WITH TASK CARD 51-900-1002-SKY, LEAK CHECKS G
- [SDR SWIA202265744](https://openairdocs.org/sdr/SWIA202265744.md): None · corroded · Apr 10, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CLEAT ON STR 20R AT FS 453 IS CORRODED. (C CHECK RO 5/23/22) FOUND CLEAT ON STGR 20R AT FS453 TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-21-03-101-006-A04. REPLACED CLEAT AT STGR 20R AT FS453 REF. CRJ-900 SRM, 51-42-06-001-001-A01 AND DWG SH670-31401 REV A
- [SDR SWIA202265743](https://openairdocs.org/sdr/SWIA202265743.md): None · corroded · Apr 10, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CLEAT ON STR 20R AT FS 364 IS CORRODED. (C CHECK RO 5/23/22) FOUND CLEAT ON STGR 20R AT FS364 TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-21-03-101-006-A04. REPLACED CLEAT AT STGR 20R AT FS364 REF. CRJ-900 SRM, 51-42-06-001-001-A01 AND DWG SH670-31950 REV Y
- [SDR SWIA202265742](https://openairdocs.org/sdr/SWIA202265742.md): None · corroded · Apr 10, 2022 · N816SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > AVIONICS BAY WEB ATTACHMENT STRINGER 26L CORRODED, BETWEEN FS333.00 AND FS364.00. (C CHECK RO 5/23/22) REPLACED AVIONICS BAY WEB ATTACHMENT STRINGER 26L BETWEEN FS333.00 AND FS364.00 REF DWG SH670-32050 REV. J AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIE
- [SDR SWIA202265741](https://openairdocs.org/sdr/SWIA202265741.md): None · corroded · Apr 9, 2022 · N816SK · Cndair CL2151A10 · Fuselage Main, Keel
  > AVIONICS BAY STRINGER 27 CORRODED, BETWEEN FS333.00 AND FS364.00. (C CHECK RO 5/23/22) REPLACED AVIONICS BAY STRINGER 27 BETWEEN FS333.00 TO FS364.00 REF DWG SH690-31350 REV. M, CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK
- [SDR SWIA202265801](https://openairdocs.org/sdr/SWIA202265801.md): None · damaged · Apr 8, 2022 · N816SK · Cndair CL6002D24 · Fuselage Structure (General)
  > AFT FACE BULKHEAD AT FS280.00 ANGLE DEFORMED / CRACKED AT WL97.70. (C CHECK RO 5/23/22) REMOVED AND REPLACED ANGLE ON AFT FACE BULKHEAD AT FS280.00 AT WL97.70 IAW CRJ 900 SRM 51-42-06-001-001-A01 / DRAWING #CC670-34010 REV K. (SEE CONTINUATION SHEET FOR
- [SDR SWIA202265800](https://openairdocs.org/sdr/SWIA202265800.md): None · damaged · Apr 8, 2022 · N816SK · Cndair CL6002D24 · Fuselage Structure (General)
  > AFT FACE BULKHEAD AT FS280.00 ANGLE DEFORMED / CRACKED AT WL85.60. (C CHECK RO 5/23/22) REMOVED AND REPLACED NEW ANGLE ON AFT FACE BULKHEAD AT FS280.00 AT WL85.60 IAW CRJ 900 SRM 51-42-06-001-001-A01 / DRAWING # CC670-34010 REV K. (SEE CONTINUATION SHEET
- [SDR SWIA202265740](https://openairdocs.org/sdr/SWIA202265740.md): None · cracked · Apr 4, 2022 · N816SK · Cndair CL6002D24 · Nacelle/Pylon Structure
  > AFTER REMOVAL OF "Z" STIFFENER FROM R/H UPPER TRANSCOWL, IT WAS DISCOVERED THAT A CRACK EXISTS AT THETOP HOLE LOCATIION ON THE SKIN DIRECTLY UNDER THE "Z" STIFFENER. (C CHECK RO 5/23/22) PERMANENTLY REPAIRED R/H UPPER TRANSCOWL INNER SKIN CRACK REF MHIR
- [SDR SWIA202265805](https://openairdocs.org/sdr/SWIA202265805.md): None · corroded · Apr 2, 2022 · N816SK · Cndair CL6002D24 · Fuselage Structure (General)
  > AFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41512-1, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODED. (C CHECK RO 5/23/22) AFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41512-1, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODED
- [SDR SWIA202265804](https://openairdocs.org/sdr/SWIA202265804.md): None · corroded · Apr 2, 2022 · N816SK · Cndair CL6002D24 · Fuselage Structure (General)
  > AFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41511-5, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODED. (C CHECK RO 5/23/22) AFT GALLEY 2 SUPPORT BRACKET, PART# SH670-41511-5, ATTACHED TO STRG 21R AND STRG. 20R APPROX. FS 372.00 IS CORRODED
- [SDR SWIA202265739](https://openairdocs.org/sdr/SWIA202265739.md): None · damaged · Mar 30, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > REMOVE FRAME SEGMENT AT FS629 FROM STGR 20R TO STGR 16R TO FACILITATE STGRS 18R, 19R, 20R AND 21R REPLACEMENT, AFTER STRINGERS REPLACEMENT, REINSTALL FRAME SEGMENT BY SPLICE REPAIR. REF MHI 690-53-00-478, REV --(P1), DATED ON 2022-03-29 AND CAMPS MX TRANS #€™
- [SDR SWIA202265738](https://openairdocs.org/sdr/SWIA202265738.md): None · cracked · Mar 30, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Frame
  > REMOVE FRAME SEGMENT AT FS613 FROM STGR 20R TO STGR 16R TO FACILITATE STGRS 18R, 19R, 20R AND 21R REPLACEMENT, AFTER STRINGERS REPLACEMENT, REINSTALL FRAME SEGMENT BY SPLICE REPAIR. REF MHI 690-53-00-478, REV --(P1), DATED ON 2022-03-29 AND CAMPS MX TRANS #€™
- [SDR SWIA202265737](https://openairdocs.org/sdr/SWIA202265737.md): None · corroded · Mar 30, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Frame
  > STRINGER JOINT SPLICE 26RH CORRODED AT FS333.00. (C CHECK RO 5/23/22) REPLACED STRINGER JOINT SPLICE AT 26RH AT FS333 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV. E. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202265736](https://openairdocs.org/sdr/SWIA202265736.md): None · corroded · Mar 29, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME 942 BETWEEN STR24R AND STR21R. (C CHECK RO 5/23/22) BLENDED OUT CORROSION ON FRAME FS942, BETWEEN STGR 24R AND 21R. REF. CRJ900 SRM 51-21-06-001-001-A01 /. ORIGINAL FRAME WEB THICKNESS AT BLENDED AREAS = 0.050€? PER REF CRJ 900 SRM
- [SDR SWIA202265735](https://openairdocs.org/sdr/SWIA202265735.md): None · corroded · Mar 28, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Frame
  > UPON REMOVAL OF FS295 FRAME FOUND CORROSION AT APPROX 24R. (C CHECK RO 5/23/22) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FS295 FRAME BETWEEN STGR 15RH TO 25RH AND FRAME SPLICE AT STGR 25RH REF CRJ900 SRM
- [SDR SWIA202265734](https://openairdocs.org/sdr/SWIA202265734.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER JOINT SPLICE 22R CORRODED AT FS333. (C CHECK RO 5/23/22) INSTALLED NEW 22R STRINGER SPLICE AT FS333.00 IAW CRJ900 SRM 51-42-06-001-001-A01 AND DWG:SH670-32420 REV E. SEE CONTINUATION CARD FOR DETAILS. PRESSURE LEAK CHECK OF REPAIR AREA CHECKED G
- [SDR SWIA202265733](https://openairdocs.org/sdr/SWIA202265733.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER JOINT SPLICE 21R CORRODED AT FS333. (C CHECK RO 5/23/22) EVALUATED SPLICE AT STGR 21R, FS333.00 HAS PITTING CORROSION THROUGH PART. 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS. REF. CRJ 900 SRM 53-00-00-101-001-A01. REMOVED AND REPLACED DAMAGE
- [SDR SWIA202265732](https://openairdocs.org/sdr/SWIA202265732.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER JOINT SPLICE 27 CORRODED AT FS333. (C CHECK RO 5/23/22) JOINT SPLICE 27 FS333 FOUND TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-00-00-101-001-A01. REMOVED AND REPLACED STRINGER JOINT SPLICE 27 AT FS333 REF. CRJ-900 SRM, 51-42-06-001-001-A01 AND DWG
- [SDR SWIA202265731](https://openairdocs.org/sdr/SWIA202265731.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER JOINT SPLICE 26L CORRODED AT FS333. (C CHECK RO 5/23/22) INSTALLED NEW STRINGER JOINT SPLICE 26L AT FS333.00 IAW CRJ900 SRM 51-42-06-001-001-A01 AND DWG: SH670-32420 REV E. PRESSURE LEAK CHECK OF REPAIR AREA CHECKED GOOD, NO LEAKS NOTED REF. CRJ
- [SDR SWIA202265730](https://openairdocs.org/sdr/SWIA202265730.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER JOINT SPLICE 25L CORRODED AT FS333. (C CHECK RO 5/23/22) REPLACED STRINGER JOINT SPLICE 25L AT FS333 REF DWG SH670-32420 REV. E, CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202265729](https://openairdocs.org/sdr/SWIA202265729.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER JOINT SPLICE AT 24L CORRODED AT FS333. (C CHECK RO 5/23/22) REPLACED STRINGER JOINT SPLICE AT 24L AT FS333 REF DWG SH670-32420 REV. E, CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202265728](https://openairdocs.org/sdr/SWIA202265728.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STGR 23R CORRODED BETWEEN FS333 - FS379. (C CHECK RO 5/23/22) REPLACED STGR 23R BETWEEN FS333 TO FS379 REF DWG SH670-31350 REV. A, CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202265727](https://openairdocs.org/sdr/SWIA202265727.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER JOINT SPLICE CORRODED AT 22L / FS333. (C CHECK RO 5/23/22) CORROSION ON JOINT SPLICE AT STGR 22L, FS333 TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-00-00-101-001-A01. REMOVED AND REPLACED STRINGER JOINT SPLICE 22L AT FS333 REF. CRJ-900 SRM 51-42-0
- [SDR SWIA202265726](https://openairdocs.org/sdr/SWIA202265726.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STGR 22R CORRODED BETWEEN FS333 - FS349. (C CHECK RO 5/23/22) REPLACED STGR 22R BETWEEN FS333 TO FS349 REF DWG SH670-31350 REV. A, AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202265725](https://openairdocs.org/sdr/SWIA202265725.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STGR 21R CORRODED BETWEEN FS333 - FS349. (C CHECK RO 5/23/22) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE BE OUT OF LIMITS. REMOVED AND REPLACED STRINGER 21R SECTION FROM FS333 - FS349, P/N SH670-31383-1, REF: CRJ900 SRM 51-42-06-001-001-A01,
- [SDR SWIA202265724](https://openairdocs.org/sdr/SWIA202265724.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > 25L CORRODED BETWEEN FS333 -FS349. (C CHECK RO 5/23/22) REPLACED STRINGER 25L FROM FS333 TO FS364 REF DWG SH670-32050 REV. J, CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202265723](https://openairdocs.org/sdr/SWIA202265723.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STGR 24L CORRODED BETWEEN FS333 - FS349. (C CHECK RO 5/23/22) CORROSION ON STGR 24L BETWEEN FS333-FS349 FOUND TO BE OUT OF LIMITS IN REF TO CRJ900 SRM 53-21-03-101-006-A04. CUT AWAY SECTION OF STGR 24L FROM APPROX FS370-FS333 AND INSTALLED NEW STRINGER S
- [SDR SWIA202265722](https://openairdocs.org/sdr/SWIA202265722.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STGR 22L CORRODED BETWEEN FS349 / FS364. (C CHECK RO 5/23/22) CORROSION ON STGR 22L BETWEEN FS349-FS364 FOUND TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-21-03-101-006-A04. REPAIRED AND INSTALLED STGR 22L NEW SECTION AND REPAIR SPLICE FROM FS333-FS370.50
- [SDR SWIA202265721](https://openairdocs.org/sdr/SWIA202265721.md): None · corroded · Mar 27, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STGR 21L CORRODED BETWEEN FS349 / FS364. (C CHECK RO 5/23/22) REPLACED STRINGER 21LH BETWEEN FS333 TO FS379 IN REF TO CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV M. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202265720](https://openairdocs.org/sdr/SWIA202265720.md): None · corroded · Mar 26, 2022 · N816SK · Cndair CL6002D24 · Fuselage Structure (General)
  > TCAS DOUBLER CORRODED BETWEEN FS295.00 AND FS310.00. (C CHECK RO 5/23/22) EVALUATED DAMAGE OF TCAS DOUBLER AND FOUND IT TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-21-01-101-002-A02. REMOVED AND REPLACED TCAS DOUBLER BETWEEN FS295.00 TO FS310.00 REF. CRJ-90
- [SDR SWIA202265719](https://openairdocs.org/sdr/SWIA202265719.md): None · corroded · Mar 26, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER 27 CORRODED BETWEEN FS310.00/FS333.00. (C CHECK RO 5/23/22) REPLACED STRINGER 27 BETWEEN FS310.00 TO FS333.00 REF DWG SH670-31630 REV. K, CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK
- [SDR SWIA202265718](https://openairdocs.org/sdr/SWIA202265718.md): None · corroded · Mar 26, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER 27 CORRODED BETWEEN FS280.00/FS295.00. (C CHECK RO 5/23/22) INSTALLED NEW STRINGER 27 FROM FS280.00 TO FS303.00 IN REF TO CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV K. SEE CONTINUATION CARD FOR DETA
- [SDR SWIA202265717](https://openairdocs.org/sdr/SWIA202265717.md): None · corroded · Mar 26, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER 26RH CORRODED BETWEEN FS295.00/FS310.00. (C CHECK RO 5/23/22) REPLACED STRINGER 26RH BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV.K. COMPLIED WITH 51-900-1002-SKY. L
- [SDR SWIA202265716](https://openairdocs.org/sdr/SWIA202265716.md): None · damaged · Mar 25, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > REMOVE AND REPLACE STR21R FROM FS477.00 TO FS621.00. (C CHECK RO 5/23/22) REMOVED STRINGER STGR21R FROM FS477.00 TO FS 693.00 REF. CRJ900 SRM 51-42-06-001-001-A01 / INSTALLED NEW STRINGER P/N: 690-33211-3A PO: T57891 STGR21R FROM FS477.00 TO FS 693.00 R
- [SDR SWIA202265715](https://openairdocs.org/sdr/SWIA202265715.md): None · damaged · Mar 25, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > REMOVE AND REPLACE STR18R FROM FS477.00 TO FS661.00 +96. (C CHECK RO 5/23/22) - REMOVED STGR18R SECTION FROM FS477 TO FS661+96, REFERENCE CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01. / - INSTALLED NEW REPLACEMENT STGR18R SECTION
- [SDR SWIA202265819](https://openairdocs.org/sdr/SWIA202265819.md): None · corroded · Mar 24, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > RH STRINGER 18 BETWEEN FS. 485.00 AND FS. 517.00 HAS CORROSION. (C CHECK RO 5/23/22) REMOVED CORROSION FROM STR 18R REF. CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS OF STR 18R BETWEEN FS485.00 AND FS517.00 IS.080 REF. CRJ 900 SRM 53-31
- [SDR SWIA202265818](https://openairdocs.org/sdr/SWIA202265818.md): None · corroded · Mar 24, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > RH STRINGER 18 BETWEEN FS. 565.00 AND FS. 581.00 HAS CORROSION. (C CHECK RO 5/23/22) REMOVED CORROSION FROM STR 18R REF. CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS OF STR 18R BETWEEN FS565.00 AND FS581.00 IS.080 REF. CRJ 900 SRM 53-31
- [SDR SWIA202265817](https://openairdocs.org/sdr/SWIA202265817.md): None · corroded · Mar 24, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > RH STRINGER 18 BETWEEN FS. 613.00 AND FS. 629.00 HAS CORROSION. (C CHECK RO 5/23/22) REMOVED CORROSION FROM STR 18R REF. CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS OF STR 18R BETWEEN FS613.00 AND FS629.00 IS.080 REF. CRJ 900 SRM 53-31
- [SDR SWIA202265816](https://openairdocs.org/sdr/SWIA202265816.md): None · corroded · Mar 24, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Keel
  > RH STRINGER 18 BETWEEN FS. 661.00+32 AND FS. 661.00+74 HAS CORROSION. (C CHECK RO 5/23/22) REMOVED CORROSION FROM STR 18R REF. CRJ 900 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS OF STR 18R BETWEEN FS661.00+32 AND FS661.00+74 IS.080 REF. CRJ 9
- [SDR SWIA202265714](https://openairdocs.org/sdr/SWIA202265714.md): None · corroded · Mar 24, 2022 · N816SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CLEAT ON FS310.00 FRAME AND STR20R INTERCOSTAL IS HEAVILY CORRODED. (C CHECK RO 5/23/22) NTERGRANULAR CORROSION NOTED ON CLEAT, DAMAGE 100% THROUGH PART AND IS ON MORE THAN ONE ELEMENT, MAKING CLEAT OUT OF LIMITS REF. CRJ900 SRM 53-21-23-101-002-A02 WHIC

Next page: https://openairdocs.org/aircraft/N816SK/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 = 'N816SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N816SK/reports

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