# Service difficulty reports: N705SK

A list on [N705SK](https://openairdocs.org/aircraft/N705SK.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 · 205 reports

- [SDR SWIA20240809703](https://openairdocs.org/sdr/SWIA20240809703.md): Frame Splice · damaged · Jul 3, 2024 · N705SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 319 SPLICE REPAIR REQUIRED FOR FOM OF STR 25R REPLACEMENT (C-CHECK RO 8/7/2024) PERFORMED REPAIR ON DAMAGE FRAME 319 BETWEEN STR 25L TO STR 24R IAW CRJ 700 SRM 51-41-02,SRM -51-42-06,SRM 53-00-06,REO 670-53-21-1308 REV -- DATED 2016-09-06,SRM 51-4
- [SDR SWIA20240809611](https://openairdocs.org/sdr/SWIA20240809611.md): Skin · chafed · Jun 11, 2024 · N705SK · Cndair CL6002C10 · Wing, Plate/Skin
  > BOTTOM SKIN ON RH AT WS128.00 CHAFFED. (C-CHECK RO 8/7/2024) PERFORMED BLENDED OUT AND EVALUATED DAMAGE AT BOTTOM SKIN RH WS128.00, MESUAREMENTS ARE: ORIGINAL THICKNESS: 0.125", MATERIAL LOSS: 0.005", REMAINING MATERIAL: 0.120", FOUND TO BE WHITH IN LIM
- [SDR SWIA20240809610](https://openairdocs.org/sdr/SWIA20240809610.md): Stringer · corroded · Jun 10, 2024 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25R BETWEEN FS 295 TO 310 HAS SIGNS OF CORROSION (C-CHECK RO 8/7/2024) REMOVED AND REPLACED DAMAGED STGR 25R BETWEEN FS295.00 TO FS310.00 IAW CRJ-700 SRM 51-42-06, SRM 51-40-06, SRM 51-21-11, SRM 51-25-06, SRM 51-21-11, SRM 51-25-16, CRJ 700 AMM
- [SDR SWIA20240809605](https://openairdocs.org/sdr/SWIA20240809605.md): Skin · chafed · Jun 5, 2024 · N705SK · Cndair CL6002C10 · Wing Miscellaneous Structure
  > LH WING LOWER SKIN WS128.00 AT THE NOSE OF FLAP FAIRING 586AB THE SKIN IS CHAFFED (C-CHECK RO 8/7/2024) PERFORMED BLENDED OUT AND EVALUATED DAMAGE ON LH WING LOWER SKIN WS128.00 AT THE NOSE OF FLAP FAIRING 586AB THE SKIN, MESUAREMENTS ARE: ORIGINAL THIC
- [SDR SWIA20240809604](https://openairdocs.org/sdr/SWIA20240809604.md): Skin · chafed · Jun 4, 2024 · N705SK · Cndair CL6002C10 · Aileron Tabs
  > RH OB FLAP MIDDLE AFT HINGE BOX SUPPORT FITTING WS220.00 CENTER LUGS HAVE CHAFE DAMAGE (C-CHECK RO 8/7/2024) PERFORMED REPAIR ON RH OB FLAP MIDDLE AFT HINGE BOX SUPPORT FITTING WS220.00 CENTER LUGS PER MHIRJ REO 670-57-21-981. REV. --. DATE: 2024-07-04
- [SDR SWIA202312140003](https://openairdocs.org/sdr/SWIA202312140003.md): Unknown · haze · Dec 13, 2023 · N705SK · Cndair CL6002C10 · Air Distribution System
  > ON TAKEOFF FROM PSP THE FLIGHT ATTENDANTS REPORTED A HAZE FILLING THE CABIN WITH A SLIGHT OIL SMELL. THIS OCCURRED IMMEDIATELY AFTER TAKEOFF AND DISSIPATED WITHIN A COUPLE MINUTES. WE DID NOT EXPERIENCE IT ON THE FLIGHT DECK. (FLIGHT 6361 FILED CLOSED)UPON A
- [SDR SWIA202304120002](https://openairdocs.org/sdr/SWIA202304120002.md): Unknown · smoke · Apr 12, 2023 · N705SK · Cndair CL6002C10 · Humidity Control System
  > FA€™S REPORTED SMOKE IN CABIN DURING TAKEOFF ALONG WITH SMELL OF €ŒBURNT POTATO€™S€? SMOKE WAS GRAYISH WHITE AND TRANSLUCENT, IN THE LOWER PART OF CABIN, FROM GALLEY TO MID-CABIN. SMOKE AND SMELL DISSIPATED WITHIN A COUPLE OF MINUTES. NO HEAT OR SMOKE NOT
- [SDR SWIA2022111466852](https://openairdocs.org/sdr/SWIA2022111466852.md): Windshield · cracked · Nov 7, 2022 · N705SK · Cndair CL6002C10 · Flight Compartment Windows
  > LEFT WINDSHIELD HEAT AT 12000FT. RAN QRH AND MSG OUT. AT 7000FT NOTICED CRACK IN CAPT WINDSHIELD SO TURNED LT WSHLD HEAT OFF FOR REMAINDER OF APPROACH. (FLIGHT 4916) REMOVED AND REPLACED CAPT SIDE WINDSHEILD IAW AMM 56-11-01. OPS CHECK OF HEAT AND PRESSURE
- [SDR SWIA202266448](https://openairdocs.org/sdr/SWIA202266448.md): None · odor · Sep 11, 2022 · N705SK · Cndair CL6002C10 · Air Conditioning System
  > ON DESCENT THROUGH 20000 FEET FLIGHT ATTENDANTS SMELLED BURNING ODOR EMITTING FROM GALLEY AREA BOTH PILOTS ALSO SMELLED SAME ODOR EMITTING FROM BEHIND THEM. NO SMOKE OR ANY PHYSICAL SIGNS OF THE ODOR WHERE IDENTIFIED. FLIGHT ATTENDANT AS A PRECAUTION TURNED
- [SDR SWIA202265541](https://openairdocs.org/sdr/SWIA202265541.md): None · defective · Apr 28, 2022 · N705SK · Cndair CL6002C10 · Doors
  > D: DURING DEPLANING RECEIVED ?R EMER DOOR? CAUTION MESSAGE. RIGHT SIDE EMER INDICATION IS AMBER ON DOORS PAGE. / PN: SH670-36500-1 MR# 1948816 / C: MEL 52-70-3 / CAT C EXP 4-27-22 (FLIGHT 3167 - FILED CLOSED) REMOVED AND REPLACED RT EMERGENCY OVER WING D
- [SDR SWIA202163107](https://openairdocs.org/sdr/SWIA202163107.md): None · cracked · Dec 20, 2021 · N705SK · Cndair CL600* · Window/Windshield System
  > RIGHT SIDE OF WINDSHIELD HAD ARCING THROUGHOUT FLIGHT IN TOP RIGHT CORNER WITH NO VISIBLE DAMAGE. SHORTLY BEFORE LANDING THERE WAS SIGNIFICANT ARCING AND THE OUTER SURFACE CRACKED (FLIGHT 3064 - FILED CLOSED) REMOVED AND REPLACED FO SIDE WINSDHIELD ASSY R
- [SDR SWIA2021091360889](https://openairdocs.org/sdr/SWIA2021091360889.md): Strut · discharged · Sep 10, 2021 · N705SK · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE ON DEPARTURE FOLLOWED BY STEERING INOP. RAN GEAR DISAGREE QRH AND GOT LANDING GEAR DOWN AND LOCKED. THE STEERING INOP MESSAGE PERSISTED SO WE RAN THAT QRH AS WELL AND LANDED BACK IN LAX WITHOUT NOSE WHEEL STEERING. UPON POST FLIGHT INSPECTION, FO
- [SDR SWIA2021091060846](https://openairdocs.org/sdr/SWIA2021091060846.md): Seat Track · corroded · Aug 24, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL FS712.00 TO FS762.00 HAS CORROSION. REMOVED AND REPLACED LEFT SIDE SEAT RAIL FROM FS712.00-FS762.00 WITH NEW PART.REF.CRJ700 AMM53-00-49-400-801-A03,AMM 53-00-49-400-802-A03.
- [SDR SWIA2021091060839](https://openairdocs.org/sdr/SWIA2021091060839.md): Floor Support · corroded · Aug 13, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOORBEAM LBL27 BETWEEN APPROXIMATELY FS1015 TO FS1031 (C-CHECK RO 9/8/2021) REPAIRED FLOOR BEAM BETWEEN AFT OF FS1031.00 LBL27 REF. CRJ700 SRM 53-00-41-201-001-A01 FIGURE 53-00-41-991-830. COMPLIED WITH ST 51-900-1002-SKY
- [SDR SWIA2021091060837](https://openairdocs.org/sdr/SWIA2021091060837.md): Floorbeam · corroded · Aug 13, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LBL9 AT APPROXIMATELY FS1031 (MARKED) (C-CHECK RO 9/8/2021) REPAIRED FLOOR BEAM LBL9 AT APPROXIMATELY FS1031.00 REF. CRJ700 SRM 53-00-41-201-001-A01, FIGURE 53-00-41-991-803 SHEET 1 AND 4.COMPLIED WITH ST 51-900-1002-SKY
- [SDR SWIA2021091060867](https://openairdocs.org/sdr/SWIA2021091060867.md): Seat Track · corroded · Aug 12, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SIDE SEAT RAIL ON L/H SIDE APPROX FS690 TO FS718 (C-CHECK RO 9/8/2021) REMOVED CORROSION ON LEFT SIDE SEAT RAIL PN SH670-36255-3 APPROX. FS690.00 €“ FS718.00 REF. CRJ700 SRM 51-21-06-001-001-A01. EVALUATED DAMAGE REMOVAL, DAMAGE SEPARATION IS
- [SDR SWIA2021091060836](https://openairdocs.org/sdr/SWIA2021091060836.md): Intercostal · cracked · Aug 12, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge Flaps
  > ON L/H I/B FLAP, REMOVE & REPLACE CRACKED INTERCOSTAL P/N CC670-14152-1. (C-CHECK RO 9/8/2021) ON L/H I/B FLAP, REMOVED CRACKED INTERCOSTAL. RECEIVED, LOCATED, DRILLED & INSTALLED NEW INTERCOSTAL P/N CC670-14152-1, REF. CRJ700 SRM 51-42-06-001-001
- [SDR SWIA2021091060832](https://openairdocs.org/sdr/SWIA2021091060832.md): Stand Off · cracked · Aug 4, 2021 · N705SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > DURING REMOVAL OF STANDOFF ON LEFT UPPER TRANSCOWL,A CRACK WAS FOUND ON UNDERLAYING STRUCTURE (C-CHECK RO 9/8/2021) REPAIRED CRACK ON UPPER LEFT TRANSCOWL BY COMPLYING WITH ALL STEPS OF REO 670-54-21-1463 REV-- DATED 2021-08-12, COMPLIED WITH TASK CARD
- [SDR SWIA2021091060831](https://openairdocs.org/sdr/SWIA2021091060831.md): Drag Angle · elongated · Aug 2, 2021 · N705SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STAB RH SIDE HAS (3) ELONGATED HOLES ON LOWER BOTTOM UNDER AFT DRAG ANGLE. (C-CHECK RO 9/8/2021) VERTICAL STAB RH SIDE (3) ELONGATED HOLES ON LOWER BOTTOM UNDER AFT DRAG ANGLE REPAIRED PER MHIRJ REO 670-55-31-146 REV €“ DATE 2021-08-05. COMPL
- [SDR SWIA2021091060829](https://openairdocs.org/sdr/SWIA2021091060829.md): Skin · dented · Aug 2, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge Flaps
  > L/H INBD FLAP, LOWER SKIN IS DAMAGE OUT OF LIMITS DUE TO DENT WITH GOUGE APPROX LOCATION, INTERSECTION RIB WS120.00 AND INTERCOSTAL SPAR. REQUIRES REPAIR. (C-CHECK RO 9/8/2021) REPAIRED L/H I/B FLAP LOWER SKIN AT FLS112.300 & FLS120.200 (WS120.00), REF
- [SDR SWIA2021091060828](https://openairdocs.org/sdr/SWIA2021091060828.md): Cargo Track · corroded · Aug 2, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RETRIEVAL SYSTEM L/H TRACK OUTBOARD (MARKED) (C-CHECK RO 9/8/2021) REPLACED CORRODED FWD CARGO RETRIEVAL SYSTEM L/H TRACK OUTBOARD WITH A FABRICATED SERVICEABLE REPLACEMENT REF MHIRJ REO 670-25-51-050 REV -- DATED 2021-08-09, STEP 1,
- [SDR SWIA2021091060826](https://openairdocs.org/sdr/SWIA2021091060826.md): Stringer · corroded · Jul 29, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FS364-379 STRG 23 R/H HAS CORROSION. (C-CHECK RO 9/8/2021) REPLACED STR 23 R/H FROM FS 333-379 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020, CRJ 700 SRM 51-42-20-001-001-A01 REV. 38 DATED JUL 25/2020, CRJ 700 SRM 51-42-21-001-001-A01 R
- [SDR SWIA2021091060825](https://openairdocs.org/sdr/SWIA2021091060825.md): Channel · corroded · Jul 29, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON DRAIN MAST INNER CHANNEL @ APPROX. STRG27 & FS1031.00 (C-CHECK RO 9/8/2021) CORROSION IS EXFOLIATION. REMOVED AND REPLACED DRAIN MAST CHANNEL P/N MM670-43255-001 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DRAWING MM670-43200 REV N. POT
- [SDR SWIA2021091060823](https://openairdocs.org/sdr/SWIA2021091060823.md): Support · corroded · Jul 23, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SILL FWD OF FS310 IS CORRODED. (C-CHECK RO 9/8/2021) COMPLIED WITH ALL THE STEPS OF REO 670-53-21-2110 REV -- DATED 2021-08-28, INSTALLED -1 WEB SPLICE, -2 FILLER ANGLE, -3 AND -4 FILLER ON R/H FLOOR SILL REPAIR BETWEEN FS295.00 AND FS310.00. TASK CA
- [SDR SWIA2021091060822](https://openairdocs.org/sdr/SWIA2021091060822.md): Window Post · cracked · Jul 21, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Structure
  > SUSPECTED CRACK ON PILOT€™S WINDSHIELD POST, AT UPPER BARREL NUT HOLE. (C-CHECK RO 9/8/2021) REPLACED PILOTS WINDSHIELD POST IAW DWG 601R33007 REV.-U, AND DWG 601R33223 REV. J. LEAK CHECK GOOD, COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION
- [SDR SWIA2021091060865](https://openairdocs.org/sdr/SWIA2021091060865.md): Roller · worn · Jul 20, 2021 · N705SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT SIDE ROLLER 1-2 AFT OTBD WORN OUT OF LIMIT. (C-CHECK RO 9/8/2021) REMOVED WORN AND - INSTALLED NEW RH WING SLAT SIDE ROLLER 1-2 AFT OTBD REF CRJ700 AMM 27-81-44-400-801-A01. FREEDOM OF MOVEMENT CHECKS GOOD.
- [SDR SWIA2021091060887](https://openairdocs.org/sdr/SWIA2021091060887.md): Housing · cracked · Jul 19, 2021 · N705SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > * LH WING, UNDER FUEL PNL 551AB, SLAT TUBE HOUSING IS CRACKED. FLAGGED (C-CHECK RO 9/8/21) REPLACED SLAT TUBE HOUSING SUPPORT BRACKET BOMBARDIER REO 670-57-42-577 REV€”2016-12-02. LEAK CHECKED GOOD PER CRJ 700 AMM 28-11-00-790-801-A01; LEAK CHECKED GO
- [SDR SWIA2021091060886](https://openairdocs.org/sdr/SWIA2021091060886.md): Skin · chafed · Jul 17, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN IS CHAFED AT STGR27 FS977.00 - FS985.00 (MARKED) (C-CHECK RO 9/8/21) BLENDED CHAFED AREA AT FS977-985 STR27, "WITHIN LIMITS" REF CRJ700 REO 670-53-00-290 REV-F DATED 2019/04/26. RESTORED FASTENERS AND FINISH.
- [SDR SWIA2021091060885](https://openairdocs.org/sdr/SWIA2021091060885.md): Angle · corroded · Jul 9, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *GALLEY SERVICE DOOR LOWER SILL ANGLE HAS EVIDENCE OF CORROSION (C-CHECK RO 9/8/21) --BLENDED SERVICE DOOR LOWER SILL ANGLE "OUT OF LIMITS" REF CRJ700 SRM 53-21-23-101-002-A01, SRM 51-21-06-001-001-A01. / --REMOVED AND REPLACED THE SERVICE DOOR LOWER SIL
- [SDR SWIA2021091060888](https://openairdocs.org/sdr/SWIA2021091060888.md): Bolt · corroded · Jul 8, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > RT NR 1 FLAP VANE ACTUATOR HAS MULTIPLE CORRODED HARDWARE COMMON TO ATTACH POINT TO FLAP (C-CHECK RO 9/8/21) INSTALLED NEW R/H #1 FLAP VANE ACTUATOR HARDWARE COMMON TO ATTACH POINT TO FLAP REF. CRJ-700 AMM 27-52-23-400-801-A01. / OPS CHECK GOOD.
- [SDR SWIA2021091060884](https://openairdocs.org/sdr/SWIA2021091060884.md): Floor Support · corroded · Jul 8, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * R/H FLOOR SILL FROM APROX F/S 1045-1069 HAS MULTIPLE AREAS OF CORROSION ( MARKED) (C-CHECK RO 9/8/21) REPLACED R/H FLOOR SILL FROM APROX S 1045 - 1069 IAW REO 670-53-61-1935 REV. -- DATED 2021-08-09. PRESSURE CHECK GOOD, COMPLIED WITH TASK CARD 51-900-
- [SDR SWIA2021091060883](https://openairdocs.org/sdr/SWIA2021091060883.md): Beam · gouged · Jul 8, 2021 · N705SK · Cndair CL6002C10 · Engine Thrust Reverser
  > *RIGHT ENGINE, LOWER TR FIXED STRUCTURE LATCH BEAM (OTBD) IS GOUGED NEAR THE LATCHES (MARKED). (C-CHECK RO 9/8/21) REPAIRED GOUGED DAMAGE ON RIGHT ENGINE, LOWER TR FIXED STRUCTURE LATCH BEAM NEAR LATCHES REF MHIRJ REO 670-54-22-041 REV -- DATED 2021-08-06
- [SDR SWIA2021091060847](https://openairdocs.org/sdr/SWIA2021091060847.md): Vane · corroded · Jul 8, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge Flaps
  > * R/H I/B FLAP INTERNAL STRUCTURE HAS EVIDENCE OF SUSPECTED CORROSION APROX 7" FROM I/B EDGE OF FLAP AND IN BTM QUADRANT I/B SIDE OF FIRST INNER RIB (C-CHECK RO 9/8/2021) REMOVED AND REPLACED WITH NEW RH INBD FLAP. REF CRJ 700 AMM 27-52-21-400-801-A01 O
- [SDR SWIA2021091060882](https://openairdocs.org/sdr/SWIA2021091060882.md): Door Sill · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * PAX DOOR ENTRY SILL HAS AREAS OF CORROSION FROM APPROX FS310.0 TO FS 349.0 (C-CHECK RO 9/8/21) REMOVED LOWER SILL ANGLE AND INSTALLED NEW PAX DOOR ENTRY LOWER SILL ANGLE PN SH670-31875-3 REF DWG SH670-31810 REV Y AND CRJ700 SRM 51-42-06-001-001-A01, SRM
- [SDR SWIA2021091060881](https://openairdocs.org/sdr/SWIA2021091060881.md): Door Sill · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *SERVICE DOOR AFT FLOOR SILL AT APPROX. 349 HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 9/8/21) REMOVED CORROSION ON SERVICE DOOR AFT FLOOR SILL AT APPROX. FS349 REF CRJ-700 SRM 51-21-06-001-001-A01, REMAINING MATERIAL WITHIN LIMITS REF CRJ-700 S
- [SDR SWIA2021091060880](https://openairdocs.org/sdr/SWIA2021091060880.md): Floorbeam · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > * COCK PIT FLOOR BOARD LANDING CORRODED IN MULTIPLE SPOTS FROM RBL9 TO LBL9 AT FS 280.00 (MARKED). (C-CHECK RO 9/8/21) REMOVED AND REPLACED WITH NEW COCK PIT FLOOR BOARD LANDING AT FS280, RBL9 - LBL9 REF CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-
- [SDR SWIA2021091060879](https://openairdocs.org/sdr/SWIA2021091060879.md): Stringer · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *STRG 21R AT APPROX. FS.364-FS.379 HAS CORROSION (C-CHECK RO 9/8/21) REPLACED STR 21 R/H AT APROX FS 364 - 379 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV. 38 DATED JUL 25 2020, AND BOMBARDIER DWG SH670-31350 REV.A. LEAK CHECK GOOD, COMPLIED WITH TASK CARD 5
- [SDR SWIA2021091060874](https://openairdocs.org/sdr/SWIA2021091060874.md): Retainer · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > *SIDE SEAT RAIL MOUNTING RETAINER AT APPROX. FS.785 LH SIDE HAS CORROSION (MARKED) (C-CHECK RO 9/8/2021) EVALUATED DAMAGE ON LH SIDE SEAT RAIL TRIM RETAINER AT APPROX. FS785.00, ORIGINAL MATERIAL THICKNESS IS 0.040€? REF. CRJ700 SRM 53-41-49-001-001-A
- [SDR SWIA2021091060872](https://openairdocs.org/sdr/SWIA2021091060872.md): Retainer · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > *SIDE SEAT RAIL MOUNTING RETAINER AT APPROX. FS.785 RH SIDE HAS CORROSION (MARKED) (C-CHECK RO 9/8/2021) EVALUATED DAMAGE ON RH SIDE SEAT RAIL TRIM RETAINER AT APPROX. FS785.00, ORIGINAL MATERIAL THICKNESS IS 0.040€? REF. CRJ700 SRM 53-41-49-001-001-A
- [SDR SWIA2021091060870](https://openairdocs.org/sdr/SWIA2021091060870.md): Seat Track · chafed · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *SIDE SEAT RAIL AT APPROX. FS.785 HAS CHAFFING DAMAGE JUST AFT OF RH EMER EXIT DOOR (MARKED) (C-CHECK RO 9/8/2021) EVALUATED SIDE SEAT RAIL FS785.00 RH SIDE, MULTIPLE AREAS OF CORROSION AND DAMAGE FOUND IN A SINGLE CROSS-SECTION FOUND TO BE OUT OF LIMIT
- [SDR SWIA2021091060869](https://openairdocs.org/sdr/SWIA2021091060869.md): Seat Track · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *SIDE SEAT RAIL MOUNTING AT APPROX. FS.724 LH SIDE HAS CORROSION (MARKED) (C-CHECK RO 9/8/2021) SIDE SEAT RAIL MOUNTING(RETAINER) REMOVED AND REPLACED WITH NEW RETAINERS FROM FS675-FS725 AND FS712-FS762 ALSO INSTALLED NEW REPLACEMENT SIDE SEAT RAIL FROM
- [SDR SWIA2021091060864](https://openairdocs.org/sdr/SWIA2021091060864.md): Roller · worn · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT SIDE ROLLER 2-2 FWD OTBD WORN OUT OF LIMITS. (C-CHECK RO 9/8/2021) REMOVED WORN AND INSTALLED NEW LH WING SLAT SIDE ROLLER 2-2 FWD OTBD REF CRJ700 AMM 27-81-44-400-802-A01 /. FREEDOM OF MOVEMENT CHECKS GOOD.
- [SDR SWIA2021091060861](https://openairdocs.org/sdr/SWIA2021091060861.md): Roller · worn · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT SIDE ROLLER 1-2 (FWD INBD AND FWD OTBD) WORN OUT OF LIMIT. (C-CHECK RO 9/8/2021) REMOVED WORN AND INSTALLED NEW L/H WING SLAT SIDE ROLLER1-2 FWD INBD AND FWD OTBD REF CRJ 700 AMM 27-81-44-400-801-A01. OPERATIONAL TEST OF THE FLAPS AND SLAT
- [SDR SWIA2021091060860](https://openairdocs.org/sdr/SWIA2021091060860.md): Roller · worn · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT SIDE ROLLER 1-2 (AFT INBD AND AFT OTBD) WORN OUT OF LIMIT. (C-CHECK RO 9/8/2021) REMOVED WORN AND INSTALLED 2EA NEW LH WING SLAT SIDE ROLLERS AT 1-2 (AFT INBD AND AFT OTBD) REF CRJ700 AMM 27-81-44-400-801-A01. FREEDOM OF MOVEMENT CHECKS GOO
- [SDR SWIA2021091060858](https://openairdocs.org/sdr/SWIA2021091060858.md): Roller · worn · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT SIDE ROLLER 1-1 AFT OTBD WORN OUT OF LIMIT. (C-CHECK RO 9/8/2021) INCORRECT DISCRAPENCY, SEE MX23153161, JOB 710145121 OP 327 FOR CORRECTIVE ACTION.
- [SDR SWIA2021091060849](https://openairdocs.org/sdr/SWIA2021091060849.md): Door Sill · corroded · Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *SERVICE DOOR FWD FLOOR SILL DOUBLER PLATE AT APPROX. 319 HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 9/8/2021) REMOVED AND REPLACED SERVICE DOOR FLOOR SILL DOUBLER AT FS 319.7 IAW CRJ700 SRM 51-42-13-001-001-A01 AND CRJ700 SRM 51-42-21-001-001
- [SDR SWIA2021091060878](https://openairdocs.org/sdr/SWIA2021091060878.md): Door Sill · corroded · Jul 6, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * AFT CARGO BAY LOWER SIL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 9/8/21) / REMOVED AND INSTALLED NEW AFT CARGO DOOR SILL BETWEEN FS1000.00 - 1047.00 REF. CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWIA2021091060877](https://openairdocs.org/sdr/SWIA2021091060877.md): Drag Angle · cracked · Jul 6, 2021 · N705SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > *VERTICAL STAB HAS A CRACKED DRAG ANGLE ON RH SIDE (MARKED) (C-CHECK RO 9/8/21) REPLACED CRACKED VERTICAL STAB DRAG ANGLE WITH NEW, REF BOMBARDIER DWG BA670-35002 REV -F, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM
- [SDR SWIA2021091060876](https://openairdocs.org/sdr/SWIA2021091060876.md): Drag Angle · cracked · Jul 6, 2021 · N705SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > *VERTICAL STAB HAS A CRACKED DRAG ANGLE ON LH SIDE (MARKED) (C-CHECK RO 9/8/21) REMOVED CRACKED VERTICAL STAB LH SIDE DRAG ANGLE AND REPLACED WITH A SERVICEABLE UNIT (P/N: A670-21186-003) REF CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-13-001-001
- [SDR SWIA2021061060875](https://openairdocs.org/sdr/SWIA2021061060875.md): Cotter Pin · deformed · Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge Devices
  > * L/H SLAT TRACK 2-1 HAS EVIDENCE OF MIGRATION OF ECCENTRIC PIN (C-CHECK RO 9/8/2021) INSPECTED TORQUE OF NUT ON L/H SLAT TRACK 2-1 ECCENTRIC PIN.TORQUE WITHIN RANGE. REMOVED AND INSTALLED NEW SERVICABLE COTTER PIN TO ECCENTRIC PIN. REF CRJ 700 AMM 57-

Next page: https://openairdocs.org/aircraft/N705SK/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 = 'N705SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N705SK/reports

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