# Service difficulty reports: N771SK

A list on [N771SK](https://openairdocs.org/aircraft/N771SK.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 · 177 reports

- [SDR SWIA2025022101](https://openairdocs.org/sdr/SWIA2025022101.md): A/C Pack · smoke · Feb 20, 2025 · N771SK · Cndair CL6002C10 · Cabin Cooling System
  > D: PACK 2 INOP, CAUSING SMOKE IN CABIN.C: MEL 21-51-1ACAT "C" DUE 3/2/2025**DO NOT RTS WITHOUT SMOD APPROVAL**SMOKE IN THE CABIN (FLIGHT 4921 - FILED CLOSED) FEB 20, 2025 STATION: PHX--UPON ARRIVAL TO AIRCRAFT PERFORMED TROUBLESHOOTING OF SMOKE AND ABNO
- [SDR SWI2024F00181](https://openairdocs.org/sdr/SWI2024F00181.md): Skin · damaged · Feb 13, 2024 · N771SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DAMAGE TO FUSELAGE SKIN AND INTERCOSTAL LOCATED AT STR12A BETWEEN FS220.0 - FS235.0, LHS. THE DENT DIMENSIONS ARE: 6€? (L) X 4.5€? (W) X 0.032€? DEEP. SEE EAML 1296554 (FLIGHT 4827 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27816391 WITH THE
- [SDR SWIA2024021500003](https://openairdocs.org/sdr/SWIA2024021500003.md): Skin · dented · Feb 13, 2024 · N771SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT INFRONT OF PORT SIDE STANDBY PITOT PROBE BELOW LH WINDSHIELD. (FLIGHT 4827 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27816382 WITH THE FOLLOWING CORRECTIVE ACTION: "PLEASE SEE ML 27816384 FOR CORRECTIVE ACTIONS "
- [SDR SWIA202402140003](https://openairdocs.org/sdr/SWIA202402140003.md): Skin · dented · Feb 13, 2024 · N771SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT INFRONT OF PORT SIDE STANDBY PITOT PROBE BELOW LH WINDSHIELD. (FLIGHT 4827 FILED OPEN)DAMAGE FOUND TO BE OUT OF LIMITS, SEE EAML 1296795 FOR DAMAGE DESCRIPTION.
- [SDR SWIA202265571](https://openairdocs.org/sdr/SWIA202265571.md): None · failed · May 7, 2022 · N771SK · Cndair CL6002C10 · Cabin Pressure Indicator
  > CABIN ALT WARNING AT FL250. CABIN PRESSURE LOST. WAS ON PRESS CONTROLLER 2 WHEN IT HAPPENED. FA REPORTED LITTLE TO NO AIRFLOW IN THE CABIN SHORTLY BEFORE THE CABIN ALT CAUTION CAME ON FOLLOWED BY THE WARNING MSG. (FLIGHT 3191 - FILED CLOSED) PLEASE REF
- [SDR SWIA202264529](https://openairdocs.org/sdr/SWIA202264529.md): None · cracked · Feb 1, 2022 · N771SK · Cndair CL6002C10 · Electrical Power System
  > EXTERNAL POWER PROVISIONS BOX IS CRACKED. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW SERVICEABLE EXTERNAL POWER PROVISION BOX, REF. DRAWING#CC670-33092 REV.A AND CRJ700 SRM 51-42-06-001-001-A01, OPS TEST GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-
- [SDR SWIA202264542](https://openairdocs.org/sdr/SWIA202264542.md): None · damaged · Jan 27, 2022 · N771SK · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > LH MOST AFT PAX SEAT DOES NOT SECURE IN SEAT TRACK LOCATION 17AB. (TRACK REPLACEMENT REQUIRED) (C CHECK RO 2/17/2022) REMOVED AND INSTALLED WITH NEW L/H FLOOR SEAT TRACK FROM ROW 13B/A TO 17B/A REF. CRJ-700 AMM 53-00-49-000-801-A17 AND CRJ-700 AMM 53-00-49
- [SDR SWIA202264528](https://openairdocs.org/sdr/SWIA202264528.md): None · cracked · Jan 24, 2022 · N771SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > RH GUSSET AT RBL12 ATTACHED TO COCKPIT FLOOR SUPPORT AND FS280 BEAM IS CRACKED (C CHECK RO 2/17/2022) REMOVED AND REPLACE RH GUSSET AT RBL12 ATTACHED TO COCKPIT FLOOR SUPPORT FS280 REF CRJ700 SRM 51-42-06-001-001-A01, BOMBARDIER DRAWING CC670-33052 REV -G.
- [SDR SWIA202264527](https://openairdocs.org/sdr/SWIA202264527.md): None · cracked · Jan 24, 2022 · N771SK · Cndair CL6002C10 · Fuselage Floor Panel
  > RH COCKPIT FLOOR SUPPORT ANGLE AT RBL12 FS280 IS CRACKED (C CHECK RO 2/17/2022) REMOVED AND REPLACED RH COCKPIT FLOOR SUPPORT ANGLE AT RBL12 FS280 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, BOMBARDIER DRAWING CC670-33199 REV - B. COMPL
- [SDR SWIA202264526](https://openairdocs.org/sdr/SWIA202264526.md): None · cracked · Jan 17, 2022 · N771SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > LH GUSSET IS CRACK COMMON TO STIFFENER AT LBL12 FS280 (C CHECK RO 2/17/2022) REMOVED AND REPLACED THE LH GUSSET COMMON TO STIFFENER AT LBL12 FS280 REF CRJ700 SRM 51-42-06-001-001-A01, BOMBARDIER DRAWING CC670-33052 REV -G. COMPLIED WITH ST 51-900-1002-SKY
- [SDR SWIA202264525](https://openairdocs.org/sdr/SWIA202264525.md): None · cracked · Jan 17, 2022 · N771SK · Cndair CL6002C10 · Fuselage Main, Frame
  > LH STIFFENER IS CRACK COMMON TO FLOOR BEAM AT LBL 12 FS274 (C CHECK RO 2/17/2022) REMOVED AND REPLACED LH STIFFENER COMMON TO FLOOR BEAM AT LBL12 FS274 REF SRM 51-42-06-001-001-A01, BOMBARDIER DRAWING CC670-33199 REV -B, DRAWING CC670-33052 REV -G. COMPLI
- [SDR SWIA202264524](https://openairdocs.org/sdr/SWIA202264524.md): None · cracked · Jan 5, 2022 · N771SK · Cndair CL6002C10 · Fuselage Floor Panel
  > CENTER COCKPIT FLOOR BEAM AT RBL12 FS274 CRACK (C CHECK RO 2/17/2022) CUT OUT DAMAGED COCKPIT FLOOR BEAM SECTION AT RBL 12, FS274.00. FABRICATED AND INSTALLED NEW FLOOR BEAM SECTION. REF. CRJ700 SRM 53-11-43-201-003-A01 REPAIR TYPE 4, FIG. 53-11-43-995-819
- [SDR SWIA202264523](https://openairdocs.org/sdr/SWIA202264523.md): None · cracked · Jan 5, 2022 · N771SK · Cndair CL6002C10 · Fuselage Floor Panel
  > CENTER COCKPIT FLOOR BEAM AT LBL12 FS274 CRACK (C CHECK RO 2/17/2022) INSTALLED ALL REPAIR PARTS LH COCKPIT FLOOR BEAM SECTOR, 2EA ANGLE AND 2EA SPLICES AT LBL12 FS274 REF. CRJ700 SRM 53-11-43-201-003-A01 TYPE 4. ALSO COMPLIED WITH 51-900-1002-SKY. SEE CON
- [SDR SWIA202264522](https://openairdocs.org/sdr/SWIA202264522.md): None · corroded · Jan 5, 2022 · N771SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > L/H FS280 LOWER WEB HAS CORROSION (C CHECK RO 2/17/2022) FABRICATED, LOCATED AND INSTALLED NEW L/H FS 280 LOWER WEB REF CRJ 700 SRM 53-11-10-201-004-A01, CRJ 700 SRM 51-42-13-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01. ALSO COMPLIED WITH 51-900-1002
- [SDR SWIA202264521](https://openairdocs.org/sdr/SWIA202264521.md): None · corroded · Jan 5, 2022 · N771SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > L/H FS280 FLOOR BEAM HAS CORROSION (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW L-H FS280 FLOOR BEAM, REF. DRAWING CC670-34010 REV K, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-22-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01 AND CRJ 700 SRM 5
- [SDR SWIA202264520](https://openairdocs.org/sdr/SWIA202264520.md): None · cracked · Jan 4, 2022 · N771SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR BEAM BL12L OUTBOARD ANGLE ATTACHING TO FS280.00 BEAM IS CRACKED, (C CHECK RO 2/17/2022) REMOVED AND REPLACED FLOORBEAM LBL12 OUTBOARD ANGLE ATTACHING TO FS280 REF CRJ700 SRM 51-42-21-001-001-A01, DRAWING CC670-33052 REV -G. COMPLIED WITH ST 51-900-
- [SDR SWIA202264519](https://openairdocs.org/sdr/SWIA202264519.md): None · corroded · Jan 3, 2022 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION FOUND ON STRINGER 22R BETWEEN FS364.00 AND FS379.00 (C CHECK RO 2/17/2022) REMOVED AND REPLACED STGR22R BETWEEN FS379.00 - FS364.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31350 REV A. LEAK CHECK OF REPAIR AREA GOOD REF CRJ700 AMM 21-31
- [SDR SWIA202264518](https://openairdocs.org/sdr/SWIA202264518.md): None · damaged · Jan 3, 2022 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > REMOVE AND REINSTALL FRAME AT FS645.00 FROM STRINGER 19R TO 25R TO FACILITATE REPAIR OF STRINGER 21R ON JOB 710244114 OP67 CAMP 23959538. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED FRAME SECTION FS645.00 FROM STRINGER 25R TO STRINGER 19R THROUGH FUSELAGE
- [SDR SWIA202264517](https://openairdocs.org/sdr/SWIA202264517.md): None · corroded · Jan 2, 2022 · N771SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME SECTOR AT FS379.00 BETWEEN STGR 22R AND STGR 23R. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW FRAME SECTOR AT FS379.00 BETWEEN STGR 25R AND STGR 20R. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32050 REV J. COMPLIED WIT
- [SDR SWIA202264516](https://openairdocs.org/sdr/SWIA202264516.md): None · corroded · Jan 2, 2022 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION FOUND ON STRINGER 23R BETWEEN FS333.00 AND FS379.00. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW STGR 23R BETWEEN FS333 - FS379 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31350 REV A. COMPLIED WITH TASK CARD 51-900-1002-SKY. AALL CHE
- [SDR SWIA202164515](https://openairdocs.org/sdr/SWIA202164515.md): None · corroded · Dec 31, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > STRINGER 24L BETWEEN FS517-FS533 CORRODED. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW INTERCOSTAL AND STRINGER COMMON TO STGR-24L AT FS517.00 - FS333.00. REF CRJ-700 SRM 51-42-06-001-001-A01. SRM 51-42-21-001-001-A01.DWG SH670-33200 REV-G AND DWG SH6
- [SDR SWIA202164514](https://openairdocs.org/sdr/SWIA202164514.md): None · corroded · Dec 30, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FS517-FS533 STGR24L INTERCOSTAL CORRODED. (C CHECK RO 2/17/2022) CORROSION FOUND OUT OF LIMITS REF CRJ-700 SRM 53-31-23-101-001-A01, RECEIVED AND WET INSTALLED NEW INTERCOSTAL AT FS517.00 STRG 24L, REF CRJ700 SRM 51-42-06-001-001-A01. DWG SH670-33083 REV-A
- [SDR SWIA202164513](https://openairdocs.org/sdr/SWIA202164513.md): None · corroded · Dec 30, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS319.70 LH BETWEEN STGR18L AND 21L CORRODED. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW REPLACEMENT FRAME AT FS319.70 BETWEEN STGR18L AND 21L USING ALL NEW FASTENERS. REF BOMBARDIER DWG# SH670-31810 REV AE AND CRJ700 SRM 51-42-21-001-001-A
- [SDR SWIA202164512](https://openairdocs.org/sdr/SWIA202164512.md): None · corroded · Dec 30, 2021 · N771SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > BACKUP SILL BETWEEN FS333.00 AND FS349.00 AT STGR21L CORRODED. (C CHECK RO 2/17/2022) REMOVED AND REPLACED CORRODED BACK UP SILL ON STGR21L BETWEEN FS333.00 AND FS349.00 WITH NEW BACK UP SILL (P/N SH670-31823-1) USING ALL NEW FASTENERS. REF BOMBARDIER DWG#
- [SDR SWIA202164511](https://openairdocs.org/sdr/SWIA202164511.md): None · corroded · Dec 28, 2021 · N771SK · Cndair CL6002C10 · Doors
  > GALLEY SERVICE DOOR UPPER SILL ANGLE HAS EXFOLIATED CORROSION. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW GALLEY SERVICE DOOR UPPER SILL ANGLE REF CRJ700 SRM 51-42-06-001-001-A01 DRW # SH670-31950 REV Y. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-90
- [SDR SWIA202164510](https://openairdocs.org/sdr/SWIA202164510.md): None · damaged · Dec 24, 2021 · N771SK · Cndair CL6002C10 · Fuselage Structure (General)
  > REMOVE AND REPLACE C-CHANNEL DOUBLER P/N CN624-2048-201 ON R/H LWR TRANSCOWL (C CHECK RO 2/17/2022) REMOVED DAMAGED C CHANNEL & INSTALLED NEW C CHANNEL DOUBLER P/N CN624-2048-201 ON R/H LOWER TRANSCOWL, REF DRAWING CN624-2003, REV Y. COMPLIED WITH ST 51-9
- [SDR SWIA202164509](https://openairdocs.org/sdr/SWIA202164509.md): None · damaged · Dec 24, 2021 · N771SK · Cndair CL6002C10 · Powerplant System
  > REMOVE AND REPLACE LATCH DOOR COAMING ON R/H LWR TRANSCOWL (C CHECK RO 2/17/2022) REMOVED DAMAGED LATCH DOOR COAMING & INSTALLED NEW LATCH DOOR COAMING P/N CN624-2060-S0401 (WAS: P/N CN624-2060-209) ON R/H LOWER TRANSCOWL, REF DRAWING CN624-2003, REV. Y.
- [SDR SWIA202164508](https://openairdocs.org/sdr/SWIA202164508.md): None · cracked · Dec 22, 2021 · N771SK · Cndair CL6002C10 · Rudder Actuator
  > RH RUDDER FEEL UNIT SUPPORT STRUCTURE OTBD LOWER CHANNEL AT APPROX. FS202.75 - FS222.76 RBL26.00 IS CRACKED. (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW FABRICATED RH RUDDER FEEL UNIT SUPPORT STRUCTURE OTBD LOWER CHANNEL PN: CC670-94231-4 AT APPROX.
- [SDR SWIA202164547](https://openairdocs.org/sdr/SWIA202164547.md): None · corroded · Dec 21, 2021 · N771SK · Cndair CL6002C10 · Ailerons
  > R/H INBOARD FLAP MOVEABLE VANE ACTUATORS 1 AND 2, FWD TRUNNION ATTACH HARDWARE ARE CORRODED (C CHECK RO 2/17/2022) REMOVED AND REPLACED CORRODED HARDWARE ON R/H I/B FLAP MOVEABLE VANE ACTUATORS 1 AND 2 FWD TRUNNION ATTACH WITH 9 NEW BOLTS, 9 WASHERS, AND 5
- [SDR SWIA202164507](https://openairdocs.org/sdr/SWIA202164507.md): None · corroded · Dec 20, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > *STGR20R HAS CORROSION FS364.00 - FS379.00. (C CHECK RO 2/17/2022) BLENDED AND TREATED CORROSION ON STGR20R BETWEEN FS364.00 AND FS379.00 PER MHIRJ REO 670-53-21-2216 REV --, DATED 2022-01-11. ALL STEPS OF REO COMPLIED WITH IN ITS ENTIRETY. SEE CONTINUATI
- [SDR SWIA202164506](https://openairdocs.org/sdr/SWIA202164506.md): None · gouged · Dec 17, 2021 · N771SK · Cndair CL6002C10 · Fuselage Structure (General)
  > EXTERNAL FUSELAGE SKIN AT APPROX. FS969-FS985 STGR27 HAS 1EA CHAFE AND 1 EA GOUGE. (C CHECK RO 2/17/2022) COMPLIED WITH FUSELAGE SKIN REPAIR AT FS977-FS985 STGR27 REF BOMBARDIER REO 670-53-00-290 REV -F DATED 2019/04/26. COMPLIED WITH TASK CARD 51-900-1002
- [SDR SWIA202164541](https://openairdocs.org/sdr/SWIA202164541.md): None · corroded · Dec 15, 2021 · N771SK · Cndair CL6002C10 · Fuselage Structure (General)
  > AVIONICS FLOORBOARD ANGLE ON AFT FACE OF FS280 FRAME APPEARS CORRODED. (C CHECK RO 2/17/2022) REMOVED AND REPLACED WITH NEW THE AVIONICS BAY CRAWLWAY FLOORBOARD SUPPORT ANGLE ON THE AFT FACE OF FS280.00 IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42
- [SDR SWIA202164505](https://openairdocs.org/sdr/SWIA202164505.md): None · corroded · Dec 15, 2021 · N771SK · Cndair CL6002C10 · Fuselage Structure (General)
  > PAX DOOR LOWER KICK PLATE ANGLE CORRODED (C CHECK RO 2/17/2022) REMOVED CORROSION FROM PAX DOOR LOWER KICK PLATE ANGLE, AND EVALUATED AS OUT-OF-LIMITS. INSTALLED NEW PAX DOOR LOWER KICK PLATE ANGLE. REF. BOMBARDIER DWG SH670-31810 REV AE AND CRJ700 SRM 51-
- [SDR SWIA202164504](https://openairdocs.org/sdr/SWIA202164504.md): None · corroded · Dec 15, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION FOUND ON STRINGER25R BETWEEN FS280.00 AND FS333.00. (C CHECK RO 2/17/2022) REPLACED STR 25R BETWEEN FS280 - FS333. REF CRJ700 SRM 51-42-06-001-001-A01, REF CRJ700 SRM 51-42-12-001-001-A01 AND DWG SH670-31630 REV K.
- [SDR SWIA202164503](https://openairdocs.org/sdr/SWIA202164503.md): None · corroded · Dec 15, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON FS333.00 STRINGER JOINT PIECE COMMON TO STRINGER 25R. (C CHECK RO 2/17/2022) REMOVED AND REPLACED STGR25R JOINT/SPLICE AT FS333.00 REF CRJ700 SRM 51-42-06-001-001-A01, AND DWG SH670-32420 REV E. LEAK CHECK OF THE REPAIR AREA GOOD REF CRJ
- [SDR SWIA202164502](https://openairdocs.org/sdr/SWIA202164502.md): None · corroded · Dec 15, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON LATCH PIN INTERCOSTAL 27 L/H BETWEEN FS349.00 AND FS364.00. (C CHECK RO 2/17/2022) REMOVED AND REPLACED LATCH PIN INTERCOSTAL 27L BETWEEN FS349 - FS364 REF CRJ700 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, DRAWING SH670-32050 RE
- [SDR SWIA202164501](https://openairdocs.org/sdr/SWIA202164501.md): None · corroded · Dec 15, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION FOUND ON R/H LONGERON 25R BETWEEN FS333.00 AND FS349.00. (C CHECK RO 2/17/2022) REMOVED AND REPLACED R/H LONGERON 25R BETWEEN FS333.00 - FS349.00 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-32050 REV J. LEAK CHECK
- [SDR SWIA202164500](https://openairdocs.org/sdr/SWIA202164500.md): None · corroded · Dec 15, 2021 · N771SK · Cndair CL6002C10 · Fuselage Floor Panel
  > FS280 FWD COCKPIT SUPPORT ANGLE CORRODED (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE P/N CC670-34095-1 REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 WITH ALTERNATE FASTENERS CALLED OUT IN PREVIOU
- [SDR SWIA202164499](https://openairdocs.org/sdr/SWIA202164499.md): None · corroded · Dec 14, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION FOUND ON STRINGER 26R BETWEEN FS280.00 AND FS333.00. (C CHECK RO 2/17/2022) REMOVED AND REPLACED STGR26R BETWEEN FS280.00 - FS333.00 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. LEAK CHECK OF REPAIR ARE
- [SDR SWIA202164498](https://openairdocs.org/sdr/SWIA202164498.md): None · dented · Dec 14, 2021 · N771SK · Cndair CL6002C10 · Wing Structure
  > DENT FOUND ON L/H I/B FLAP LOWER SKIN APPROX 26" FROM I/B EDGE AND 6" FROM T/E (MARKED) (C CHECK RO 2/17/2022) ACCOMPLISHED REPAIR TO L/H I/B FLAP LOWER SKIN. REF CRJ700 SRM 57-52-01-201-005-A01 SPLICE REPAIR FIGURE 57-52-01-995-802 AND COMPLIED WITH SKY
- [SDR SWIA202164497](https://openairdocs.org/sdr/SWIA202164497.md): None · damaged · Dec 13, 2021 · N771SK · Cndair CL6002C10 · Powerplant System
  > LH UPPER TRANSCOWL HAS 1EA LOSE FASTENER ON Z STIFFENER FOR LATCH DOOR DOMAINING (C CHECK RO 2/17/2022) L/H UPPER TRANSCOWL HAS BEEN REPAIRED REF REO# 670-54-21-1499, REV --. DATED 12/22/21. COMPLIED FULLY W/SKYCARD 51-900-1002 SKY.
- [SDR SWIA202164496](https://openairdocs.org/sdr/SWIA202164496.md): None · damaged · Dec 13, 2021 · N771SK · Cndair CL6002C10 · Powerplant System
  > RH LOWER TRANSCOWL FWD "Z" STIFFENER HAS SEVERAL SHEARED FASTENERS (C CHECK RO 2/17/2022) REPAIRED R/H LWR TRANSCOWL Z STIFFNER AND INNER SKIN REF MHIRJ REO 670-54-21-1500 REV -- 2021-12-22. COMPLIED WITH SKYCARD 51-900-1002
- [SDR SWIA202164495](https://openairdocs.org/sdr/SWIA202164495.md): None · chafed · Dec 13, 2021 · N771SK · Cndair CL6002C10 · Powerplant System
  > LH UPPER TRANSCOWL EXTERNAL SKIN CHAFED AT AFT SIDE OF LATCH DOOR OPINING (C CHECK RO 2/17/2022) REPAIRED CHAFED EXTERNAL SKIN ON AFT SIDE OF LATCH DOOR OPENING OF THE LH UPPER TRANSCOWL PER MHIRJ REO 670-54-21-1505 REV --, DATED 2022-01-11. ALL STEPS OF
- [SDR SWIA202164494](https://openairdocs.org/sdr/SWIA202164494.md): None · corroded · Dec 13, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON PAX DOOR INTERCOSTAL AFT DD4. (C CHECK RO 2/17/2022) PAX DOOR INTERCOSTAL DD4 FROM FS338.96 TO FS347.25 HAS INTERGRANULAR CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMITS. REF REO 670-52-11-010 REV NC, DATED 2002-02-25 AND CRJ200 SRM 52-00-00
- [SDR SWIA202164493](https://openairdocs.org/sdr/SWIA202164493.md): None · corroded · Dec 12, 2021 · N771SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON LOWER FRAME SECTOR FS364.00 BETWEEN STGR 25R AND STGR 27 (C CHECK RO 2/17/2022).COMPLIED WITH FRAME SPLICE REPAIR REF CRJ700 SRM 53-21-23-201-008-A01. LEAK CHECK OF THE REPAIR AREA GOOD REF CRJ700 AMM 21-31-00-910-801-A01. SEE CONTINUE
- [SDR SWIA202164540](https://openairdocs.org/sdr/SWIA202164540.md): None · worn · Dec 10, 2021 · N771SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > RH WING SLAT TRACK 3-2 FWD INBD SIDE ROLLER RATCHETS (C CHECK RO 2/17/2022) REMOVED AND REPLACED R/H SLAT 3-2 FWD I/B SIDE ROLLER REF CRJ700 AMM 27-81-44-000-803-A01 AND AMM 27-81-44-400-803-A01. OPS CHECK GOOD REF CRJ700 AMM 27-52-00-864-801-A01
- [SDR SWIA202164539](https://openairdocs.org/sdr/SWIA202164539.md): None · worn · Dec 10, 2021 · N771SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > RH WING SLAT TRACK 1-2 FWD OTBD SIDE ROLLER HAS FLAT SPOT BEYOND LIMITS (C CHECK RO 2/17/2022) REMOVED AND REPLACED R/H WING SLAT TRACK 1-2 FWD O/B SIDE ROLLER REF. CRJ-700 AMM 27-81-44-000-801-A01 AND 27-81-44-400-801-A01
- [SDR SWIA202164538](https://openairdocs.org/sdr/SWIA202164538.md): None · seized · Dec 10, 2021 · N771SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > RH WING SLAT TRACK 3-2 BOTTOM AFT ROLLER SEIZED (C CHECK RO 2/17/2022) REMOVED AND REPLACED R/H WING SLAT TRACK 3-2 BOTTOM AFT ROLLER WITH NEW ROLLER REF CRJ 700 AMM 27-81-43-000-804-A01 AND 27-81-43-400-804-A01. TUC 4980 CAL DUE DATE 31-SEP-22.
- [SDR SWIA202164550](https://openairdocs.org/sdr/SWIA202164550.md): None · corroded · Dec 9, 2021 · N771SK · Cndair CL6002C10 · Doors
  > *LH OVERWING EMER DOOR HAS CORRODED INTERIOR HARDWARE FOR ATTACHING HANDLE MECHANISM. MARKED. (C CHECK RO 2/17/2022) REMOVED CORRODED AND INSTALLED NEW INTERIOR HARDWARE FOR ATTACHING HANDLE MECHANISM IN LH OVERWING EMERGENCY DOOR IAW CRJ700 AMM 52-21-02-0
- [SDR SWIA202164537](https://openairdocs.org/sdr/SWIA202164537.md): None · worn · Dec 9, 2021 · N771SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > LH WING SLAT TRACK 3-2 FWD INBD SIDE ROLLER SEIZED (C CHECK RO 2/17/2022) REMOVED AND REPLACED L/H SLAT TRACK 3-2 FWD INBD SIDE ROLLER WITH NEW ROLLER REF CRJ 700 AMM 27-81-44-000-803-A01 & 27-81-44-400-803-A01.

Next page: https://openairdocs.org/aircraft/N771SK/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 = 'N771SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N771SK/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.