# Service difficulty reports: N776SK

A list on [N776SK](https://openairdocs.org/aircraft/N776SK.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 · 134 reports

- [SDR SWIA2026052276030](https://openairdocs.org/sdr/SWIA2026052276030.md): Window · cracked · May 22, 2026 · N776SK · Cndair CL6002C10 · Flight Compartment Windows
  > CP SIDE WINDOW HAS ~3 INCH CRACK IN THE INNER PANE (FLIGHT 3792) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32308780 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED THE CA SIDE WINDOW WITH REFERENCE TO AMM 56€“12€“01 & TASK CARD 56-220-1000-SK
- [SDR SWIA2025031105](https://openairdocs.org/sdr/SWIA2025031105.md): Window · failed · Mar 5, 2025 · N776SK · Cndair CL6002C10 · Flight Compartment Windows
  > L WINDOW SHATTERED IN FLIGHT (FLIGHT 4011) REMOVED AND REPLACED CAPTAINS SIDE WINDSHIELD AND PERFORMED OPS CHECKS IN REFERENCE TO CRJ700 AMM 56-11-01. OPS CHECK AND LEAK TEST GOOD. TORGUE WRENCH S/N USED 202407010030077 DUE DATE 02/26.
- [SDR SWIA202503060015](https://openairdocs.org/sdr/SWIA202503060015.md): Window · cracked · Mar 5, 2025 · N776SK · Cndair CL6002C10 · Flight Compartment Windows
  > L WINDOW SHATTERED IN FLIGHT (FLIGHT 4011 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024121900011](https://openairdocs.org/sdr/SWIA2024121900011.md): Winglet · ground damage · Dec 11, 2024 · N776SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > TRANSFER FROM EAML 1489329: LH WINGLET IMPACT DAMAGE HAS BROKEN THE MOST OUTBOARD TIP OF THE CLOSING SPAR AND QTY-2 OF THE LENS ATTACHMENT NUTPLATES HOLES LOCATED ON CLOSING SPAR HAVE BECAME UNUSABLE. (FLIGHT 3939 - FILED CLOSED) 1.) REMOVED AND REPLACE
- [SDR SWIA202411250916](https://openairdocs.org/sdr/SWIA202411250916.md): Roller · worn · Sep 16, 2024 · N776SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H #1 SLAT #1 SLAT TRACK HAS ROLLER WARE. REPAIRED DAMAGE TO LH #1 SLAT #1 SLAT TRACK IAW REO 670-57-42-1808 REV-- DATE 2024-10-29 AND CRJ 700 SRM 51-11-00 & 51-12-00. NDT,. SEE REPORT FOR DETAILS. REQUIRES REPEAT INSPECTION WITH A THRESHOLD 40K FC, REPEAT
- [SDR SWIA2024112501286](https://openairdocs.org/sdr/SWIA2024112501286.md): Frame · corroded · Sep 15, 2024 · N776SK · Cndair CL6002C10 · Fuselage Main, Frame
  > SIGNS OF CORROSION IN FWD BAGGAGE BAY AT FS565.0 STGR 26LH, LOCATED ON AFT SIDE OF THE FRAME. (C-CHECK RO 11/23/2024) REPAIRED FRAME IN FWD BAGGAGE BAY AT FS565.0, STGR26L, LOCATED ON AFT SIDE OF FRAME IAW CRJ700 SRM 51-42-06, 53-31-06, REO 670-53-31-94
- [SDR SWIA202411250915](https://openairdocs.org/sdr/SWIA202411250915.md): Bracket · cracked · Sep 15, 2024 · N776SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H #1 SLAT #3 SLAT TRACK BOX BRACKET CRACKED. (C-CHECK RO 11/23/2024) REPAIRED SLAT TRACK BOX #3 ON RH #1 SLAT IAW REO 670-57-42-577 REV-- DATE 2016-12-02 AND CRJ700 AMM 28-11-00 AND 57-41-05. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT#
- [SDR SWIA202411250903](https://openairdocs.org/sdr/SWIA202411250903.md): Fairing · cracked · Sep 3, 2024 · N776SK · Cndair CL6002C10 · Aerodynamic Fairings
  > AFT WING TO BODY L/H DIAPHRAGM HAS A CRACK AT FS909. (C-CHECK RO 11/23/2024) REPAIRED AREA ON AFT WTB LH DIAPHRAGM AT 909.00 IAW REO 670-53-82-478 REV-A DATE: 2014-11-12NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S102524-4 PO# 174025 DATE
- [SDR SWIA202411250831](https://openairdocs.org/sdr/SWIA202411250831.md): Floorbeam · cracked · Aug 31, 2024 · N776SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL12 COCKPIT FLOOR BEAM IS CRACKED ON OTBD SIDE AT FS280.00 (C-CHECK RO 11/23/2024) PERFORMED REPAIR ON LBL12 COCKPIT FLOOR BEAM OTBD SIDE AT FS280.00 IAW REO 670-53-11-896 REV-- DATE: 2015-03-17, AMM 20-70-00. PERFORMED INSPECTION BY BARON NDT, LLC FA
- [SDR SWIA202411250828](https://openairdocs.org/sdr/SWIA202411250828.md): Hinge · gouged · Aug 28, 2024 · N776SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER- DOOR PIANO HINGE ON FUSELAGE HAS A GOUGE ON AFT SIDE AT SPRING PIN (C-CHECK RO 11/23/2024) PEFORMED BLENDED OUT AND EVALUATED AREA ON PASSENGER DOOR PIANO HINGE ON FUSELAGE AFT SIDE SPRING PIN MESUAREMENTS AREA: MATERIAL LOSS: 0.025", MAXIMUM
- [SDR SWIA202162865](https://openairdocs.org/sdr/SWIA202162865.md): None · damaged · Oct 30, 2021 · N776SK · Cndair CL600* · Air Conditioning System
  > 2 SECTIONS OF ORANGE DUCTING ON R/H SIDE OF FUSELAGE FROM FWD OF WING BOX NEEDS TO BE REPLACED. FS 527-629. (C-CHECK RO 11/28/2021) REPLACED UNDERFLOOR EXHAUST DUCT FROM F.S. 609.00 - F.S. 667.00 IAW CRJ-700 AMM 21-23-53-000/400-803-A01. REMOVED DUCT F
- [SDR SWIA202162882](https://openairdocs.org/sdr/SWIA202162882.md): None · worn · Oct 14, 2021 · N776SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > WHILE REPLACING TOP FWD ROLLERS ON RH WING FOUND SLAT TRACK 3-3 WORN BEYOND LIMITS. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED RH SLAT TRACK 3-3 IAW CRJ 700 AMM 27-81-41-000/400-803-A01. REF ATTACHED CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202162864](https://openairdocs.org/sdr/SWIA202162864.md): None · corroded · Oct 14, 2021 · N776SK · Cndair CL600* · Doors
  > PAX DOOR KICKPLATE ANGLE FS 310- FFS349 STGR 17L-18L FOUND CORRODED (C-CHECK RO 11/28/2021) REMOVED AND REPLACED PAX DOOR KICKPLATE ANGLE FS 310- FFS349 STGR 17L-18L IAW CRJ 200 SRM 51-42-06-001-001-A01.
- [SDR SWIA202162881](https://openairdocs.org/sdr/SWIA202162881.md): None · worn · Oct 6, 2021 · N776SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > WHILE REPLACING TOP FWD ROLLERS ON LH WING FOUND SLAT TRACK 3-3 WORN BEYOND LIMITS. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED LH SLAT TRACK 3-3 IW CRJ 700 AMM 27-81-41-000/400-803-A01. REF ATTACHED CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202162863](https://openairdocs.org/sdr/SWIA202162863.md): None · chafed · Oct 5, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > PAX DOOR HINGE LUGS AND LANDINGS ON (FUESLAGE SIDE) FOUND CHAFFING ON ALL LUGS AND LANDINGS. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED PAX DOOR HINGE FUSELAGE SIDE IAW CRJ-700 SRM 53-21-23-201-007-A01, 51-42-21-001-001-A01. COMPLETED TASK CARD 51-900
- [SDR SWIA202162862](https://openairdocs.org/sdr/SWIA202162862.md): None · chafed · Oct 5, 2021 · N776SK · Cndair CL600* · Fuselage, Equipment Attach Fittings
  > PAX DOOR PIANO HINGE LUGS (ON DOOR SIDE) FOUND CHAFFING ON ALL LUGS OUTER SURFACE FACE. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED PAX DOOR HINGE (DOOR SIDE) IAW CRJ-700 SRM 52-11-01-201-002-A01. COMPLETED TASK CARD 51-900-1002-SKY AND M-337. NO CHANG
- [SDR SWIA202162880](https://openairdocs.org/sdr/SWIA202162880.md): None · worn · Oct 4, 2021 · N776SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH WING SLAT TRACK 3-2 HAS TOP INBOARD SIDE ROLLER WORN BEYOND LIMITS. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED LH WING SLAT TRACK 3-2 TOP INBD SIDE ROLLER IAW CRJ 700 AMM 27-81-44-000/400-803-A01 REF ATTACHED CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202162879](https://openairdocs.org/sdr/SWIA202162879.md): None · worn · Oct 4, 2021 · N776SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH WING SLAT TRACK 2-2 HAS TOP INBOARD SIDE ROLLER WORN BEYOND LIMITS. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED LH SLAT TRACK 2-2 TOP INBD SIDE ROLLER IAW CRJ 700 AMM 27-81-44-000/400-802-A01 REF ATTACHED CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202162878](https://openairdocs.org/sdr/SWIA202162878.md): None · corroded · Oct 3, 2021 · N776SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH WING SLAT TRACK 1-2 HAS OB TOP AFT, INBOARD TOP AFT AND INB BOTTOM FWD ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED LH SLAT TRACK 1-2 OUTBD TOP AFT, INBD TOP AFT AND INBD BOTTOM FWD SIDE ROLLERS IAW CRJ 700 AMM 27-81-44-0
- [SDR SWIA2021113062861](https://openairdocs.org/sdr/SWIA2021113062861.md): Floorbeam · corroded · Sep 29, 2021 · N776SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND R/H BEAM TO BE CORRODED UNDER PANEL 194AB. (C-CHECK RO 11/28/2021) REPAIRED RH BEAM UNDER PANEL 194AB IAW MHIRJ REO 670-53-42-051 REV -- DATED 2021-11-08. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED. WEIGHT CHANGES A
- [SDR SWIA202162888](https://openairdocs.org/sdr/SWIA202162888.md): Bolt · corroded · Sep 27, 2021 · N776SK · Cndair CL600* · Elevator Tab, Attach Fittings
  > RH ELEVATOR INBD PCU (SYST. #3), AFT HANGER BEAM BOLT/WASHER CORRODED. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED THE RH ELEVATOR IB PCU SYS #3 AFT HANGER BEAM BOLT AND WASHER IAW CRJ 700 AMM27-33-01-000/400-802-A01
- [SDR SWIA202162887](https://openairdocs.org/sdr/SWIA202162887.md): None · corroded · Sep 26, 2021 · N776SK · Cndair CL600* · Passenger/Crew Doors
  > PAX DOOR STOP BRACKET CORRODED AT FS338.963 AND BETWEEN DD6 AND DD5. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED PAX DOOR STOP BRACKET AT F.S 338.963 IAW CRJ 700 SRM 51-42-13-001-001-A01. REFER TO MX TRAN # 23635257 JOB 91024195 OP 109 FOR OPS CHECK OF
- [SDR SWIA202162886](https://openairdocs.org/sdr/SWIA202162886.md): None · corroded · Sep 23, 2021 · N776SK · Cndair CL600* · Wing, Landing Gear Attach Fittings
  > RH OUTBD FLAP CENTER HINGE ARM UPPER AND LOWER BOLTS AND BUSHING CORRODED (C-CHECK RO 11/28/2021) REPLACED UPPER AND LOWER BUSHINGS OM THE RH OB FLAP CENTER HINGE ARM IAW CRJ 700 AMM 20-31-00-400-802 CONFIG A01, ATTACHED NEW HARDWARE TO HINGE ARM ASSEMB
- [SDR SWIA202162877](https://openairdocs.org/sdr/SWIA202162877.md): None · corroded · Sep 23, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > L/H SIDE SEAT ARAIL IS CORRODED BETWEEN F.S. 708 TO F.S. 752. (C-CHECK RO 11/28/2021) REMOVED CORRODED LH SIDE SEAT RAIL IAW CRJ 700 AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE UNIT IAW CRJ 700 AMM 53-00-49-400-801-A03
- [SDR SWIA202162876](https://openairdocs.org/sdr/SWIA202162876.md): None · corroded · Sep 23, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 485 TO F.S. 565. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED CORRODED RH SIDE SEAT RAIL BETWEEN FS 485 TO 565 WITH NEW SERVICEABLE RH SIDE SEAT RAIL PN: SH670-32234-3 IAW CRJ 700 AMM 53-00-49-000/400-801-A03
- [SDR SWIA202162875](https://openairdocs.org/sdr/SWIA202162875.md): None · corroded · Sep 23, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 565 TO F.S. 661. (C-CHECK RO 11/28/2021) R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 565 TO F.S. 661 WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 700 AMM 53-00-49-000/400-801-A03. SEE ATTACHED CONTINUATION C
- [SDR SWIA202162874](https://openairdocs.org/sdr/SWIA202162874.md): None · corroded · Sep 23, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > L/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 579 TO F.S. 677. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED THE LH SIDE SEAT RAIL BETWEEN FS 579 AND FS 677 IAW CRJ 700 AMM 53-00-49-000/400-801-A03. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWIA202162860](https://openairdocs.org/sdr/SWIA202162860.md): None · corroded · Sep 23, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 379 TO F.S. 485. (C-CHECK RO 11/28/2021) R/H SIDE SEAT TRACK BETWEEN F.S. 379 TO F.S. 485 WAS REMOVED AND REPLACED IAW CRJ 700 AMM 53-00-49-000/400-801-A03. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK
- [SDR SWIA202162873](https://openairdocs.org/sdr/SWIA202162873.md): None · corroded · Sep 21, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > LBL 27, FLOOR SEAT TRACK BETWEEN FS 581 - FS 693 IS CORRODED. (C-CHECK RO 11/28/2021) REMOVED CORRODED FLOOR SEAT TRACK BETWEEN FS581- FS693 AT LBL 27 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK IAW CRJ 70
- [SDR SWIA202162872](https://openairdocs.org/sdr/SWIA202162872.md): None · corroded · Sep 21, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > LBL 27, FLOOR SEAT TRACK BETWEEN FS 485 - FS 581 IS CORRODED. (C-CHECK RO 11/28/2021) UNDER FURTHER INVESTIGATION FOUND THERE TO BE NO CORROSION FOUND ON FLOOR SEAT TRACK BETWEEN FS485- FS581 ON LBL 27 IAW CRJ 700 SRM 51-26-00-001-001-A01
- [SDR SWIA202162871](https://openairdocs.org/sdr/SWIA202162871.md): None · corroded · Sep 21, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > RBL 9, FLOOR SEAT TRACK BETWEEN FS 581 - FS 691.50 IS CORRODED. (C-CHECK RO 11/28/2021) REMOVED CORRODED FLOOR SEAT TRACK AT RBL 9 BETWEEN FS581- FS691.50 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND REPLACED WITH NEW SERVICEABLE FLOOR SEAT TRACK IAW
- [SDR SWIA202162870](https://openairdocs.org/sdr/SWIA202162870.md): None · corroded · Sep 21, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > LBL 9, FLOOR SEAT TRACK BETWEEN FS 581 - FS 691.50 IS CORRODED. (C-CHECK RO 11/28/2021) REMOVED CORRODED FLOOR SEAT TRACK AT LBL 9 BETWEEN FS581- FS691.50 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND REPLACED WITH NEW SERVICEABLE FLOOR SEAT TRACK IAW
- [SDR SWIA202162869](https://openairdocs.org/sdr/SWIA202162869.md): None · corroded · Sep 21, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > RBL 9, FLOOR SEAT TRACK BETWEEN FS 485 - FS 581 IS CORRODED (C-CHECK RO 11/28/2021) REMOVED CORRODED FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 485- FS 581 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK IAW CRJ 700
- [SDR SWIA202162868](https://openairdocs.org/sdr/SWIA202162868.md): None · corroded · Sep 21, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > LBL 9, FLOOR SEAT TRACK BETWEEN FS 485 - FS 581 IS CORRODED. (C-CHECK RO 11/28/2021) REMOVED CORRODED FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 485- FS 581 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK IAW CRJ 700
- [SDR SWIA202162867](https://openairdocs.org/sdr/SWIA202162867.md): None · cracked · Sep 21, 2021 · N776SK · Cndair CL600* · Fuselage Main, Frame
  > F.S. 280 LBL9 OUTBOARD SUPPORT CLIP IS CRACKED. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED F.S. 280 LBL9 OUTBOARD SUPPORT CLIP IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR SWIA202162885](https://openairdocs.org/sdr/SWIA202162885.md): None · corroded · Sep 20, 2021 · N776SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > F.S. 333 TO F.S. 349 STGR 20L INTERCOSTAL IS CORRODED. (C-CHECK RO 11/28/2021) BLENDED CORROSION ON INTERCOSTAL AT STRINGER 20L BETWEEN FS 333 AND FS 349 IAW CRJ 700 SRM 51-26-06-001-001-A01 AND FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLACED INTERCOSTAL
- [SDR SWIA202162866](https://openairdocs.org/sdr/SWIA202162866.md): None · corroded · Sep 20, 2021 · N776SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > RBL 9 FLOOR SEAT RAIL IS CORRODED BETWEEN F.S. 349 TO F.S. 485. (C-CHECK RO 11/28/2021) REMOVED CORRODED FLOOR SEAT TRACK BETWEEN F.S.349- F.S.693 AT LBL 9 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A03 AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK IAW C
- [SDR SWIA202162859](https://openairdocs.org/sdr/SWIA202162859.md): None · corroded · Sep 20, 2021 · N776SK · Cndair CL600* · Standard Practices/Structures
  > PAX DOOR UPPER SILL ANGLE IS CORRODED BETWEEN F.S. 310 TO F.S. 349. (C-CHECK RO 11/28/2021) PAX DOOR SILL ANGLE WAS REMOVED AND A NEW PART SH670-31825-9 WAS INSTALLED IAW CRJ 700 SRM 51-41-04-01-001-A01 ALL OPS CHECKS GOOD
- [SDR SWIA2021113062858](https://openairdocs.org/sdr/SWIA2021113062858.md): Frame · corroded · Sep 20, 2021 · N776SK · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 295 FRAME IS CORRODED BETWEEN STGR26L TO 25L. (C-CHECK RO 11/28/2021) F.S. 295 STGR26L TO 25L WAS REPAIRED AS REQUIRED IAW CRJ 700 SRM 53-00-06-201-006. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED, NO WEIGHT CHANGE,
- [SDR SWIA202162857](https://openairdocs.org/sdr/SWIA202162857.md): Frame · corroded · Sep 20, 2021 · N776SK · Cndair CL600* · Fuselage Main, Frame
  > F.S. 319 FRAME IS CORRODED BETWEEN STGR 18L TO 19L. (C-CHECK RO 11/28/2021) REMOVED AND REPLACED FRAME SECTION AT F.S. 319.00 STRINGER 17L - 20L IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. COMPLETED TASK CARD 51-900-1002-SKY AND FORM
- [SDR SWIA202162884](https://openairdocs.org/sdr/SWIA202162884.md): None · corroded · Sep 19, 2021 · N776SK · Cndair CL600* · Wing, Landing Gear Attach Fittings
  > LH OB FLAP CENTER HINGE ARM UPPER AND LOWER BUSHINGS AND ATTACHING HARDWARE IS CORRODED REQUIRES REPLACEMENT (C-CHECK RO 11/28/2021) REPLACED BUSHINGS IAW CRJ 700 AMM 20-31-00-400-802 CONFIG A01, ATTACHED NEW HARDWARE TO HINGE ARM ASSEMBLY SEE CAMP# 234
- [SDR SWIA202162883](https://openairdocs.org/sdr/SWIA202162883.md): None · corroded · Sep 19, 2021 · N776SK · Cndair CL600* · Fuselage Structure (General)
  > CORRODED DOUBLERS AT FS 533 AND FS 581 STGR 25L-26L (C-CHECK RO 11/28/2021) CORROSION ON DOUBLERS AT FS 533 AND FS 581 STGR 25L-26L WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DOUBLERS WITH NEW SERVICEABLE PARTS IAW CRJ 700 SRM 51-42-22-001-00
- [SDR SWIA201910146463](https://openairdocs.org/sdr/SWIA201910146463.md): Angle · damaged · Sep 21, 2019 · N776SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS202.75 AFT SIDE OF BULKHEAD LH CAP ANGLE HAS AN INDICATION.4" LONG IN THE RADIUS JUST BELOW STGR13. FAILED NDT INSPECTION. (C-CHECK) RO: 10/11/2019 INSTALLED NEW CAP ANGLE AND PERFORMED NDT AND RESTORED FINISH IAW REO.
- [SDR SWIA2019101446462](https://openairdocs.org/sdr/SWIA2019101446462.md): Frame · cracked · Sep 21, 2019 · N776SK · Cndair CL6002C10 · Fuselage Main, Frame
  > LH FS220 FRAME HAS AN INDICATION.75" LONG THRU THE 3RD FASTENER DOWN FROM STGR13. FAILED NDT INSPECTION. (C-CHECK) RO: 10/11/2019 REMOVED AND INSTALLED SERVICEABLE FRAME SECTOR IAW SRM.
- [SDR SWIA2019082246195](https://openairdocs.org/sdr/SWIA2019082246195.md): Landing Gear · malfunctioned · Aug 22, 2019 · N776SK · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > CREW REPORTS AFTER TAKE OFF RECEIVED THE LANDING GEAR DISAGREEMENT NOSE LANDING GEAR WOULD NOT RETRACT. PERFORMED REPACK OF NLG STRUT IAW AMM. PERFORMED EXTENSION AND RETRACTION CHECK OF NLG IAW AMM. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA2018061144757](https://openairdocs.org/sdr/SWIA2018061144757.md): Loop · failed · Jun 11, 2018 · N776SK · Cndair CL6002C10 · Overheat Detection
  > RECEIVED A LT BLEED DUCT CAUTION MESSAGE. DECLARED EMERGENCY. REMOVED AND REPLACED THE LEFT BLEED LOOP A SENSING ELEMENT, MT 139 IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA2017102543918](https://openairdocs.org/sdr/SWIA2017102543918.md): Intercostal · corroded · Oct 8, 2017 · N776SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BS 319.7, STRINGER 20R INTERCOSTAL HAS CORROSION. REMOVED & REPLACED THE INTERCOSTAL IAW SRM.
- [SDR SWIA2017102543917](https://openairdocs.org/sdr/SWIA2017102543917.md): Threshold · corroded · Oct 7, 2017 · N776SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD HAS AN AREA OF CORROSION BELOW FLOORBOARD AREA AT NUTPLATE LOCATIONS. REMOVED AND REPLACED AFT CARGO DOOR THRESHOLD IAW SRM.
- [SDR SWIA2017102543916](https://openairdocs.org/sdr/SWIA2017102543916.md): Floorbeam · corroded · Oct 7, 2017 · N776SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM UPPER SPLICE HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM UPPER SPLICE IAW SRM.
- [SDR SWIA201743915](https://openairdocs.org/sdr/SWIA201743915.md): Nut Plate · corroded · Oct 6, 2017 · N776SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON LATCH PIN FITTING ATTACH PLATE ON FWD SIDE OF BS 364, STRINGER 27. REMOVED AND REPLACED THENUTPLATE ASSY IAW SRM.

Next page: https://openairdocs.org/aircraft/N776SK/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 = 'N776SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N776SK/reports

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