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 SWIA2021091060873Fitting · chafed*EVALUATE CHAFE ON RH WHEEL WELL WING LINK FITTING ATTACHED TO REAR SPAR. MARKED (C-CHECK RO 9/8/21) REPAIRED CHAFE ON RH WHEEL WELL WING LINK FITTING (ATTACHED TO REAR SPAR) BY COMPLYING WITH ALL STEPS OF REO 670-57-11-180 REV -- DATED 2021-07-30. COMPLJul 3, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021091060871Fitting · chafed*EVALUATE CHAFE ON LH WHEEL WELL WING LINK FITTING ATTACHED TO REAR SPAR. MARKED (C-CHECK RO 9/8/21) REPAIRED CHAFE ON LH WHEEL WELL WING LINK FITTING (ATTACHED TO REAR SPAR) BY COMPLYING WITH ALL STEPS OF REO 670-57-11-179 REV -- DATED 2021-07-30. COMPLJul 3, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021091060868Door Frame · crackedFWD EQUIPMENT COMPARTMENT - L/H DOOR FRAME - AFT DOOR LATCH CUTOUT HAS SUSPECTED CRACK IN RADIUS (C-CHECK RO 9/8/21) REMOVED AND REPLACED L/H ELECTRICAL BAY DOOR LANDING REF CRJ700 SRM 51-42-06-001-001-A01 AND REO 670-53-11-1721 REV-- DATED 2021-08-12 COMJul 3, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021091060866Door Frame · crackedFWD EQUIPMENT COMPARTMENT - R/H DOOR FRAME - AFT DOOR LATCH CUTOUT CRACKED IN RADIUS (C-CHECK RO 9/8/21) TRANSFERED FROM CO: 101451221 JOB:: 710145121 OP: 123 / REMOVED CRACKED RH TRU BAY LANDING, REF CRJ700 SRM 51-42-06-001-001 A01.INSTALLED NEW R/H TRJul 3, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021091060863Door Frame · crackedFWD EQUIPMENT COMPARTMENT - L/H DOOR FRAME - LWR AFT CORNER OF DOOR CUTOUT HAS SUSPECTED CRACK (C-CHECK RO 9/8/21) REPLACED FWD EQUIPTMENT COMPARTMENT SKIN FOR L/H DOOR FRAME, LWR AFT CORNER CUTOUT CRACK REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 AMM 5Jul 3, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021091060862Slat Track · worn* L/H SLAT TRACK 3-3 HAS EVIDENCE OF RUBBING ABBRASION TOP SIDE (C-CHECK RO 9/8/21) PERFORMED PERMANENT REPAIR REO 670-57-42-1151 REV -- DATED 2021-08-24 ON LH SLAT TRACK 3-3. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. OPS CHECKS GOODJul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060859Slat Track · corroded* L/H SLAT TRACK 3-2 HAS FRETTING TOP AND BTM (C-CHECK RO 9/8/21) SLAT TRACK BLENDED W/IN LIMITS IAW REO 670-57-42-1150 REV-- DATED 2021-08-23. €ŒALL STEPS C/W€?. REINSTL'D LH 3-2 SLAT TRACK IAW CRJ700 AMM 27-81-41-400-802-A01. ALL CHK GOOD. SKYCARD 5Jul 3, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060857Hinge Fitting · corroded* R/H #4 FLAP HINGE LUGS HAVE EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) INSTALLED NEW HARDWARES ON RH #4 HINGE LUGS REF CRJ700 AMM 57-53-27-400-802-A01 FROM STEP 1. TO 4. AND STEP 4. A. (4) TO (16) AND STEP5.Jul 3, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060856Slat Track · worn* L/H SLAT TRACK 2-1 HAS UN-EVEN WARE 1 PLC ON I/B SIDE AND 1 PLC O/B SIDE ( MARKED ) (C-CHECK RO 9/8/21) L/H SLAT TRACK 2-1 HAS UN-EVEN WARE 1 PLC ON I/B SIDE AND 1 PLC O/B SIDE. REPAIRED PER MHIRJ REO 670-57-42-1148 REV -- DATE 2021-08-23, "ALL STEPS C/Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060855Hinge Fitting · corroded* R/H #5 FLAP HINGE LUGS HAVE EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) REMOVED AND INSTALLED NEW HARDWARE ON RH #5 FLAP HINGE LUGS REF CRJ700 AMM 57-53-27-400-803-A01 STEP 4. A. (7) (B).Jul 3, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060854Hinge Box · corroded* R/H I/B FLAP HINGE BOX #1 HAS EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) REMOVED AND INSTALLED NEW HARDWARES ON I/B FLAP HINGE BOX #1 REF CRJ700 AMM 57-54-02-400-801-A01 STEP 4. A. (1)(D) (5) (7) ONLY.Jul 3, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060853Slat Track · corroded* L/H SLAT TRACK 2-2 HAS EVIDENCE OF CORROSION ON BTM SIDE 2 PLC'S ( MARKED ) (C-CHECK RO 9/8/21) CORROSION REMOVED W/IN LIMITS IAW REO 670-57-42-1136 REV-- DATED 2021-08-03. €ŒALL STEPS C/W€?. REINSTL'D LH 2-2 SLAT TRACK IAW CRJ700 AMM 27-81-41-400-80Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060852Hinge Fitting · corroded* R/H #4 FLAP HINGE LUGS HAVE EVIDENCE OF CORRODED HARDWARE (C-CHECK RO 9/8/2021) REMOVED AND INSTALLED NEW R/H # 4 FLAP HINGE LUGS REF CRJ 700 SRM 51-41-02-001-001-A01Jul 3, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060851Slat Track · corroded* L/H SLAT TRACK 2-3 HAS EVIDENCE OF CORROSION ON TOP SIDE 2 PLC'S ( MARKED ) (C-CHECK RO 9/8/21) CORROSION REMOVED W/IN LIMITS IAW REO 670-57-42-1169 REV-- DATE 2021-08-25. €ŒALL STEPS C/W€?. REINSTL'D LH 2-3 SLAT TRACK IAW CRJ700 AMM 27-81-41-400-801Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060850Bolt · corrodedPASSENGER DOOR: NOTED CORROSION ON TWO OF THE BOLTS FOR THE LOWER TENSION TIES ALIGNMENT PLATE ON THE FORWARD SIDE OF THE DOOR(MARKED WITH RED GREASE PENCIL) (C-CHECK RO 9/8/2021) REMOVED AND REPLACED 2EA. BOLTS FOR THE LOWER TENSION TIES ALIGNMENT PLATJul 3, 2021 · N705SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2021091060848Slat Track · corroded* L/H SLAT TRACK 1-3 HAS EVIDENCE OF CORROSION ON TOP SIDE 2 PLC'S ( MARKED ) (C-CHECK RO 9/8/21) CORROSION REMOVED W/IN LIMITS IAW REO 670-57-42-1168 REV-- DATED 2021-08-26. €ŒALL STEPS C/W€?. REINSTL'D LH 1-3 SLAT TRACK IAW CRJ700 AMM 27-81-41-400-801Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060845Slat Track · corroded* L/H SLAT TRACK 1-2 HAS EVIDENCE OF CORROSION ON BTM SIDE 1 PLC ( MARKED ) (C-CHECK RO 9/8/21) CORROSION REMOVED WITH IN LIMITS REF REO 670-57-42-1135 REV-- DATED 2021-07-12. €ŒALL STEPS C/W€?. REINSTL'D LH 1-2 SLAT TRACK IAW CRJ700 AMM 27-81-41-400-80Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060844Skin · gougedLH INBOARD FLAP SKIN HAS DENT WITH GOUGE WS 126 AND LOWER SPAR INTERCOSTAL AS MARKED (C-CHECK RO 9/8/2021) L/H INBD FLAP LOWER SKIN DAMAGE OUT OF LIMITS, APPROX LOCATION, INTERSECTION RIB WS120.00 AND INTERCOSTAL SPART, REPAIRED ON JOB 710145125 OP 107Jul 3, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060843Link · gouged* R/H SLAT TRACK 3-1 HAS GOUGE IN LOWER LINK (C-CHECK RO 9/8/2021) REMOVED DAMAGED AND INSTALLED "NEW" R/H OUTBD SLAT TRACK 3-1 LOWER LINK AS REQ'D REF. CRJ700 AMM 57-42-01-400-807-A01. OPERATION TEST OF THE SLATS IS GOOD.Jul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060842Pin · migrated* L/H SLAT TRACK 2-3 HAS EVIDENCE OF MIGRATION OF ECCENTRIC PIN (C-CHECK RO 9/8/2021) REMOVED OLD AND INSTALLED NEW ECCENTRIC PIN AND HARDWARE TO THE L/H 2-3 SLAT TRACK REF CRJ 700 AMM 57-42-01-400-806-A01 / . RIGGING AND OPERATIONAL CHECK OF THE LH SLAJul 3, 2021 · N705SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021091060841Stand Off · cracked* LEFT SIDE UPPER TRANS COWL STANDOFF HAS SUSPECT CRACK AT TOP FASTENER ON INBOARD END OF COWL. (C-CHECK RO 9/8/21) REMOVED AND REPLACED LH UPPER TRANSCOWL STANDOFF ON THE INBOARD END REF REO 670-54-21-971 REV A DATED 2017/05/11, CRJ700 SRM 51-42-14-001-0Jul 2, 2021 · N705SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2021091060840Vane · chafed*RIGHT WING INBOARD FLAP VANE LEADING EDGE IS CHAFED ON PANEL 684ET. (FLAGGED) (C-CHECK RO 9/8/2021) REMOVED AND REPLACED WITH NEW PANEL P/N CC670-14027-3. REF CRJ 700 SRM 51-40-06-001-001-A01.Jul 1, 2021 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021091060838Skin · chafedLH AILERON UPPER L/E HAS CHAFING DAMAGE (C-CHECK RO 9/8/21) REPLACED LH AILERON UPPER L/E WITH A SERVICEABLE UNIT REF CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42--21-001-001-A01, COMPLIED WITH TASK CARD 51-900-1002-SKY, SEE CONTINUATION CARD FOJul 1, 2021 · N705SK · Cndair CL6002C10 · AileronsSDR SWIA2021091060835Skin · dentedADM# N750SK-1285 / THERE IS A DENT APPROXIMATELY 15" AFT OF SVC DOOR AS FS 364 AND 17" UP FROM BOTTOM OF SERVICE DOOR AT STRINGER 15R. PLEASE PLOT/MAP AND EVALUATE THE DAMAGE. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFJun 24, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021091060833Skin · dentedTHERE IS A DENT ON THE BOTTOM EDGE OF THE SVC DOOR, MARKED WITH RED GREASE PENCIL. PLEASE PLOT/MAP AND EVALUATE THE DAMAGE. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. (C-CHECK RO 9/8/2Jun 24, 2021 · N705SK · Cndair CL6002C10 · Service DoorsSDR SWIA2021091060830Door · dentedTHERE ARE DENTS/NICKS AROUND THE LOW PRESSURE GROUND AIR CONNECTION DOOR, MARKED WITH RED GREASE PENCIL. PLEASE PLOT/MAP AND EVALUATE THE DAMAGE. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDUREJun 24, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202160641Stringer · corrodedSTRINGER 21R HAS CORROSION JUST FWD OF FS 349.0 (C-CHECK RO 8/31/21) REMOVED AND REPLACED STRINGER 21R IAW CRJ700 SRM 51-42-06-001-001-A01 AND MHI REO 670-53-21-2067 REV. --, DATED 6/30/21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED ANApr 13, 2021 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202155678Hinge · wornPASSENGER DOOR PIANO HINGE ASSEMBLY ON FUSELAGE IS WORN. REPAIR HAS BEEN CLASSIFIED AS A MAJOR REPAIR PER GMM 3-26 FORM M-337 REQUIRED FILED CLOSED. REMOVED AND REPLACED PIANO TYPE HINGE PN SH670-31876-13 IAW CRJ700 SRM 51-77-00 AND FASTENER 51-42-20 SEALINGJan 20, 2021 · N705SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2018092445092Seal · failedGEAR DISAGREE ON TAKEOFF FOLLOWED BY A WOW INPUT CAUTION MSG. (FLT 3259) FO: 09/24/2018 CLOSED. REMOVED THE NLG PISTON ASSY AND INSTALLED THE SCRAPER SEAL IN THE GLAND NUT AND INSTALLED GLAND NUT ON PISTON/AXLE ASSY IAW AMM. REPLACED ALL NLG SEALS IAW AMM. INSSep 23, 2018 · N705SK · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/AxleSDR SWIA2018051744637Unknown · smokeAFT LAV SMOKE WARNING MESSAGE DURING CLIMB. SMOKE FILLING CABIN REPORTED BY FAS. RETURNED TO FIELD. PERFORMED A COMPRESSOR WASH RINSE CYCLE IAW AMM. OPERATED PACKS AND ENGINE AT CRUISE POWER, NO DEFECTS NOTED.May 7, 2018 · N705SK · Cndair CL6002C10 · Air Distribution SystemSDR SWIA201744037Stringer · crackedCRACK AT FS 280 STG 3L TO THE 3RD FASTENER HOLE. (C-CHECK) C/W REPAIR IAW REO.Nov 21, 2017 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201744036Post · crackedLBL30 VERTICAL POST ON FWD SIDE OF FS202 HAS ON CRACK INDICATION NOTED AT THE TOP (IN AFT I-BEAM WEB-FLANGE INTERSECTION) .250" LONG. (C-CHECK) REPAIRED LBL30 VERTICAL POST ON FWD SIDE OF FS202 IAW SRM.Nov 16, 2017 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2017120544033Post · crackedRBL30 VERTICAL POST ON FWD SIDE OF FS202 HAS ON CRACK INDICATION NOTED AT THE TOP (IN AFT I-BEAM WEB-FLANGE INTERSECTION) .300" LONG. (C-CHECK) REPAIRED RBL30 VERTICAL POST ON FWD SIDE OF FS202 IAW SRM.Nov 16, 2017 · N705SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2017120544035Frame · crackedRT FS 220 FRAME HAS A CRACK INDICATION NOTED AT FASTENER HOLE ADJACENT TO LIGHTING HOLE JUST BELOW STR 13A ON RT SIDE. THE INDICATION IS .300" LONG. (C-CHECK) REMOVED CRACKED RT 220 FRAME SECTOR AND REPLACE WITH NEW SERVICEABLE FRAME IAW SRM.Nov 14, 2017 · N705SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2017120544034Frame · crackedLT FS 220 FRAME HAS A CRACK INDICATION NOTED AT FASTENER HOLE ADJACENT TO LIGHTING HOLE JUST BELOW STG 13A ON LT SIDE. THE INDICATION IS .300" LONG. (C-CHECK) REMOVED CRACK LT 220 UPPER FRAME SECTOR AND REPLACED WITH NEW SERVICEABLE FRAME IAW SRM.Nov 14, 2017 · N705SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201743441Skin · corrodedUPON REMOVAL OF PASSENGER DOOR INNER SKIN, FOUND CORROSION ON INTERCOSTAL IN THE UPPER MID SECTION OF THE DOOR. REMOVED AND INSTALLED NEWINTERCOSTAL, WITH ALL NEW FASTENERS IAW SRM. ALL CHECKS GOOD.Jun 15, 2017 · N705SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA201743440Skin · chafedLEFT INBOARD FLAP INSIDE OF PANEL 584DB, INTERNAL SIDE OF SKIN IS CHAFED.REMOVED AND REPLACED PANEL IAW SRM AND REO.Jun 15, 2017 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA201743439Skin · chafedLEFT INBOARD FLAP INSIDE OF PANEL 584CB, INTERNAL SIDE OF SKIN IS CHAFED. REPLACED THE PANEL IAW SRM AND REO.Jun 15, 2017 · N705SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA201743433Intercostal · crackedON REMOVAL OF PASSENGER DOOR INNER SKIN FOUND A CRACK IN THE RADIUS OF INTERCOSTAL ON UPPER AFT CORNER OF DOOR. REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL IAW SRM. ALL CHECKED GOOD.Jun 15, 2017 · N705SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA201743438Hinge · gougedPAX DOOR HINGE HALF DOOR SIDE HAS GOUGES. (C-CHECK) RO: 06/29/2017 REMOVED & INSTALLED NEW HINGE HALF ON PAX DOOR, ALL CHECKS GOOD.Jun 13, 2017 · N705SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA201743437Stringer Splice · corrodedSTRINGER SPLICE 25R AT BS 333 HAS CORROSION. REMOVED AND INSTALLED A NEW STRINGER SPLICE IAW SRM.Jun 11, 2017 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201743436Stringer · corrodedCORROSION FOUND BETWEEN BS 333 AND 349, STRINGER 26R. REMOVED & REPLACED THE STRINGER IAW SRM. ALL CHECKED GOOD.Jun 11, 2017 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201743435Stringer · corrodedCORROSION FOUND BETWEEN BS 333 AND 349, STRINGER 25R. REMOVED & INSTALLED NEW STRINGER IAW SRM. ALL CHECKED GOOD.Jun 11, 2017 · N705SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA201743434Structure · dentedINLET COWL OF RIGHT ENGINE INNER BARREL HAS NUMEROUSE DENTS. (C-CHECK) RO: 06/29/2017 REPAIRED 7 DENTS IN RH INLET ACOUSTIC INNER PANEL IAW SRM.Jun 9, 2017 · N705SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA201743432Scuff Plate · scratchedVERTICAL SCRATCH DAMAGE TO THE AFT CARGO DOOR SCUFF PLATE. INSTALLED A NEW AFT CARGO DOOR SCUFF PLATE IAW SRM.Jun 8, 2017 · N705SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA201641866Unknown · smokeRETURNED TO FIELD WITH REPORT OF SMOKE IN THE CABIN AFTER TAKEOFF. PLANE LANDED WITHOUT INCIDENT. INSPECTED INTERIOR OF CABIN, COCKPIT, AVIONICS, FWD CARGO COMPARTMENT, AFT CARGO COMPARTMENT, APU AND APU COMPARTMENT. NO SMOKE IN CABIN AND COCKPIT NOTED AT TFeb 8, 2016 · N705SK · Cndair CL6002C10 · Air Distribution SystemSDR SWIA201541332Skin · chafedRIGHT AILERON TOP L/E HAS CHAFE MARK. C-CHECK, REPLACED RT AILERON TOP L/E PANEL IAW SRM.Jun 5, 2015 · N705SK · Cndair CL6002C10 · AileronsSDR SWIA201540598Connector · unsecureMOST FORWARD CEILING EMERGENCY FLOOD LIGHT IS INOPERATIVE. FOUND MOST FORWARD CEILING EMERGENCY FLOOD LIGHT CONNECTOR LOOSE. INSTALLED CONNECTOR IAW AMM.Jan 14, 2015 · N705SK · Cndair CL6002C10 · Light System WiringSDR SWIA201335808Sensor · faultyBRAKE OVER TEMPERATURE WARNING. FLT 4966 REPLACED NR 1 BTMS THERMOCOUPLE SENSOR IAW AMM 32-46-01. OPERATIONS CHECKED GOOD AT THIS TIME.Dec 28, 2013 · N705SK · Cndair CL6002C10 · Landing Gear Brake SystemSDR SWIA201335667Wire Harness · chafedCHAFE ON ELECTRICAL HARNESS IN RT MLG WW. C-CHECK REPAIRED THE RT MLG WW HARNESS CHAFE OTBD IAW REO.Dec 18, 2013 · N705SK · Cndair CL6002C10 · Landing Gear System Wiring
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