N705SK

Service difficulty reports · 205

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA20240809703Frame Splice · damagedFRAME 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 51-4Jul 3, 2024 · N705SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA20240809611Skin · chafedBOTTOM 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 LIMJun 11, 2024 · N705SK · Cndair CL6002C10 · Wing, Plate/SkinSDR SWIA20240809610Stringer · corrodedSTGR 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 Jun 10, 2024 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA20240809605Skin · chafedLH 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 THICJun 5, 2024 · N705SK · Cndair CL6002C10 · Wing Miscellaneous StructureSDR SWIA20240809604Skin · chafedRH 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: 2024-07-04Jun 4, 2024 · N705SK · Cndair CL6002C10 · Aileron TabsSDR SWIA202312140003Unknown · hazeON 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 ADec 13, 2023 · N705SK · Cndair CL6002C10 · Air Distribution SystemSDR SWIA202304120002Unknown · smokeFA€™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 NOTApr 12, 2023 · N705SK · Cndair CL6002C10 · Humidity Control SystemSDR SWIA2022111466852Windshield · crackedLEFT 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 PRESSURENov 7, 2022 · N705SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA202266448None · odorON 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 Sep 11, 2022 · N705SK · Cndair CL6002C10 · Air Conditioning SystemSDR SWIA202265541None · defectiveD: 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 DApr 28, 2022 · N705SK · Cndair CL6002C10 · DoorsSDR SWIA202163107None · crackedRIGHT 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 RDec 20, 2021 · N705SK · Cndair CL600* · Window/Windshield SystemSDR SWIA2021091360889Strut · dischargedGEAR 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, FOSep 10, 2021 · N705SK · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/AxleSDR SWIA2021091060846Seat Track · corrodedLEFT 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.Aug 24, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021091060839Floor Support · corrodedCORROSION 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-SKYAug 13, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060837Floorbeam · corrodedCORROSION 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-SKYAug 13, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2021091060867Seat Track · corrodedCORRODED 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 ISAug 12, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021091060836Intercostal · crackedON 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 51-42-06-001-001Aug 12, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060832Stand Off · crackedDURING 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 Aug 4, 2021 · N705SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2021091060831Drag Angle · elongatedVERTICAL 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. COMPLAug 2, 2021 · N705SK · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SWIA2021091060829Skin · dentedL/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), REFAug 2, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060828Cargo Track · corrodedCORROSION 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,Aug 2, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021091060826Stringer · corrodedFS364-379 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 RJul 29, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021091060825Channel · corrodedCORROSION 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. POTJul 29, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060823Support · corrodedLH 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 CAJul 23, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060822Window Post · crackedSUSPECTED 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 CONTINUATIONJul 21, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021091060865Roller · wornRH 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.Jul 20, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060887Housing · cracked* 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 GOJul 19, 2021 · N705SK · Cndair CL6002C10 · Wing Main, Frame StructureSDR SWIA2021091060886Skin · chafedEXTERNAL 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.Jul 17, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021091060885Angle · corroded*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 SILJul 9, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060888Bolt · corrodedRT 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.Jul 8, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge Flap ActuatorSDR SWIA2021091060884Floor Support · corroded* 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-Jul 8, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060883Beam · gouged*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 2021-08-06Jul 8, 2021 · N705SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2021091060847Vane · corroded* 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 OJul 8, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060882Door Sill · corroded* 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, SRMJul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060881Door Sill · corroded*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 SJul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060880Floorbeam · corroded* 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-Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2021091060879Stringer · corroded*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 5Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021091060874Retainer · corroded*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-AJul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2021091060872Retainer · corroded*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-AJul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2021091060870Seat Track · chafed*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 LIMITJul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021091060869Seat Track · corroded*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 FROMJul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021091060864Roller · wornLH 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.Jul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060861Roller · wornLH 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 Jul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060860Roller · wornLH 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 GOOJul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060858Roller · wornRH 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.Jul 7, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060849Door Sill · corroded*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 51-42-21-001-001Jul 7, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060878Door Sill · corroded* 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 GOODJul 6, 2021 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2021091060877Drag Angle · cracked*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 Jul 6, 2021 · N705SK · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SWIA2021091060876Drag Angle · cracked*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 51-42-13-001-001Jul 6, 2021 · N705SK · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SWIA2021061060875Cotter Pin · deformed* 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-Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge Devices
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