N614QX

Service difficulty reports · 465

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 = 'N614QX' 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 SWIA2021081060293Seat Track · corroded* RH FLOOR SEAT TRACK AT RBL9 BETWEEN FS830.40 AND APROX. FS985.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND REPLACED RH FLOOR SEAT TRACK AT RBL9 BETWEEN FS830.40 - FS985.00 REF CRJ700 SRM51-41-02-001-001-A01. SEE COMay 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021081060292Seat Track · corroded* LH SEAT TRACK AT LBL9 BETWEEN FS830.40 AND FS985.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND INSTALLED NEW SEAT TRACK LBL9 BETWEEN FS830 AND FS985 REF-CRJ-700 SRM 51-41-02-001-001 A01May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021081060257Stringer · corroded*CORROSION ON STGR 26R BETWEEN FS 1031.00 €“ 1047.00 (C-CHECK RO 8/9/2021) REMOVED CORROSION ON STGR 26R BETWEEN FS 1031.00 €“ 1047.00 REF. CRJ700 AMM 53-00-03-201-001-A01. EVALUATED AND FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR REF. CRJ700 AMM 51-2May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081060256Doubler · corroded*CORROSION ON DOUBLER FOR DRAIN MAST BETWEEN FS 1031.00 €“ 1051.30, STGR 27 €“ 26R (C-CHECK RO 8/9/2021) REPLACED DOUBLER AT DRAIN MAST BETWEEN FS1031-1051 STGR 27-26R REF- DWG MM670-43200 REV-N AND CRJ-700 SRM 51-42-06-001-001 A01,LEAK CHECK GOOD,NO May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021081060255Stringer Clip · corroded*CORROSION ON CLIP ATTACHED TO STGR 26L AND FS 1000.00 (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CLIP IAW CRJ700 SRM 51-42-06-001-001-A01, DRAWING# MM670-36061 REV D, SEE CONTINUATION FOR WORK ACCOMPLISHED. COMPLIED WITH TASK CARD 51-900-1002-SKYMay 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2021081060254Stringer · corroded*CORROSION ON STGR 25L BETWEEN FS 1088.00 €“ 1051.00. AREAS MARKED. (C-CHECK RO 8/9/2021) REPAIRED DAMAGED STRINGER 25L BETWEEN FS 1051 AND FS1088 IAW CRJ700 SRM 53-00-03-201-001-A01 FIG 53-00-03-991-805 SHT 2, C/W TACK CARD 51-900-1002-SKY, SEE CONTINMay 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202160253Stringer · corroded* STR.20R BETWEEN FS 310.00 AND 319.70 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND REPLACED INTERCOSTAL P/N SH670-32074-1 AT FS310-319 STGR20R REF CRJ700 SRM51-42-06-001-001-A01 AND SRM51-42-21-001-001-A01 REV 38 JUL 25/May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081060252Striker · corroded* SERVICE DOOR BOTTOM SILL SEAL STRIKER HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND REPLACED NEW SERVICE DOOR SEAL STRIKER P/N SH670-31412-1 REF- CRJ700 SRM 51-42-06-001-001-A01 AND DRAWING NO. SH670-31950 REV Y. SEE COMay 12, 2021 · N614QX · Cndair CL6002C10 · Service DoorsSDR SWIA2021081060251Bulkhead · corrodedFS 693 FWD PRESSURE BLKHD CORRODED @ BOTTOM ANGLE BTWN STGRS 26L/26R (C-CHECK RO 8/9/2021) REPAIRED LOWER MACHINED FRAME AT FS693 FWD PRESSURE BULKHEAD BTW STGR 26L-STGR 26R AND ALL STEPS COMPLETED OF REF-CRJ-700 MHI RJ REO 670-53-41-530 REV -- DATED 20May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA202160250Mount · corrodedFWD BAGG TIE DOWN MOUNT PLATE CORRODED @ FS 533 BTWN STGRS 22L/23L (C-CHECK RO 8/9/2021) REMOVED AND INSTALLED NEW FWD CARGO FLOOR MACHINED BRACKET (P/N SH670-33390) AT FS533.00 BETWEEN STGR 22L/23L. REF CRJ-700 SRM 51-42-21-001-001-A01, SRM 51-42-22-00May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021081060249Stringer · corrodedSTGR 20R CORRODED 3 PLACES BTWN FS'S 485/501 (C-CHECK RO 8/9/2021) PERFORMED A SPLICE REPAIR TO STGR 20R BETWEEN FS485-501 REF REO 670-53-31-665 REV A DATED 2021-06-11. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST FORM M-337 AND SKYWEST TASK 51-900May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081060248Stringer · corrodedSTGR 19R CORRODED BTWN FS'S 485/501 (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CORRODED STGR19R BETWEEN FS485 TO FS501 REF CRJ 700 SRM 53-00-03-201-001-A01.LEAK CHECK GOOD / COMPLIED WITH TASK 51-900-1002-SKYMay 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081060247Stringer · corrodedSTGR 20R CORRODED BTWN FS'S 565/581 (C-CHECK RO 8/9/2021) PERFORMED SPLICE REPAIR TO STGR 20R BETWEEN FS565-581 REF REO 670-53-31-665 REV A DATED 2021-06-11. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST FORM M-337 AND SKYWEST TASK 51-900-1002-SKY.May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081060283Skin · chafed* LH INBOARD FLAP UPPER SKIN IS CHAFED UNDER PANEL 584CB (C-CHECK RO 8/9/2021) BLENDED DAMAGE AREA FROM UPPER SKIN UNDER PANEL 584CB PER CRJ 700 SRM 51-12-00-001-001-A01,NO DAMAGE ALLOW AREA , RECIEVED REO 670-57-52-352 REV -- DATE 2017-03-28 , NDT AREMay 11, 2021 · N614QX · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021081060291Stop Fitting · corroded* PASSENGER DOOR LOWER STOP BOLT FITTING CORRODED (C-CHECK RO 8/9/2021) REMOVED AND REPLACED PAX DOOR LOWER STOP FITTING IAW CRJ-700 AMM 52-11-02-000-806-A01 AND 52-11-02-400-806-A01May 9, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021081060282Fitting · chafed* FWD CARGO DOOR SURROUND, UPPER FWD GUIDE FITTING CHAFED/GOUGED (C-CHECK RO 8/9/2021) REPLACED FWD CARGO DOOR SURROUNG UPPER FWD GUIDE FITTITNG IAW CRJ 700 AMM 53-31-23-400-801-A01 / OPS TEST GOODMay 9, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021081060246Bracket · loose* SERVICE DOOR HOLD OPEN BRACKET IS LOOSE (C-CHECK RO 8/9/2021) REMOVED AND REPLACED AFT STRGR 14 IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. INSTL'D SERVICE DOOR HOLD OPEN BRACKET IAW CRJ700 SRM 51-42-13-001-001-A01, LEAK May 9, 2021 · N614QX · Cndair CL6002C10 · Service DoorsSDR SWIA2021081060245Skin · chafed* FUSELAGE EXTERIOR SKIN CHAFED IN 3 LOCATIONS BETWEEN FS977 €“ FS985 STGR27 (C-CHECK RO 8/9/2021) PERFORMED REPAIR TO THE FUSELAGE EXTERIOR SKIN CHAFED AREAS BETWEEN FS977-985 AT STGR 27 REF REO 670-53-00-660 REV -- DATED 2021-05-31AND REO 670-53-00-2May 9, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2021081060290Lug · corroded* L/H #3 FLAP MECHANISM FWD LUG FITTING HAS CORRODED HARDWARE (C-CHECK RO 8/9/2021) REPLACED MOUNTING HDWR ON L/H # 3 FLAP MECHANISM FWD LUG FITTING PER REF CRJ700 AMM TASK 57-54-02-400-810 CONFIG A01 LEAK CHECK GOODMay 8, 2021 · N614QX · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021081060289Fitting · corrodedPASSENGER DOOR SURROUND STRUCTURE FITTING. LOCATED TOWARD FWD AT THE MID SECTION HAS CORRODED FASTENER AND NUTPLATE. IDENTIFIED WITH TAPE. (C-CHECK RO 8/9/2021) REPLACED HARDWARE AND NUTPLATES ON PAX DOOR SURROUND STRUCTURE FITTING IAW CRJ 700 SRM 51-May 6, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021081060288Fitting · corrodedPASSENGER DOOR SURROUNDING STRUCTURE FITTING. LOCATED TOWARD AFT AT THE MID SECTION HAS CORRODED FASTENER (1) AND NUTPLATE. IDENTIFIED WITH TAPE. (C-CHECK RO 8/9/2021) REMOVED AND REPLACED NUTPLATE AT PAX DOOR SURROUND STRUCTURE MID LOCATION REF CRJ70May 6, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2021081060281Seat Track · corrodedR/H SIDE SEAT RAIL AT APPROX. FS863.00-FS969.00 HAS MULTIPLE SPOTS OF CORROSION ,SCRATCHES AND GOUGES (C-CHECK RO 8/9/2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL AT APPROXIMATELY FS863.00 - FS969.00 IAW REF CRJ700 SRM 53-00-49-000-801-A01 AND SRM 53-0May 6, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021081060280Seat Track · corroded*L/H SIDE SEAT RAIL AT APPROX. FS879.00-FS953.00 HAS MULTIPLE SPOTS OF CORRODE HARDWARE ,SCRATCHES AND GOUGES (C-CHECK RO 8/9/2021) NO DAMAGE ALLOWED ON SIDE SEAT RAIL FS 879-953 FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 53-51-49-101-001-A01, FABRICATEMay 6, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021081060279Seat Track · corroded*R/H SIDE SEAT RAIL AT APPROX. FS379.00-FS485.00 HAS MULTIPLE SPOTS OF CORRROSION ,SCRATCHES AND GOUGES (C-CHECK RO 8/9/2021) NO DAMAGE ALLOWED ON SIDE SEAT RAIL FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 53-21-49-101-001-A01, REPLACED BY NEW SECTION FAMay 6, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021081060287Vane · corrodedL/H INBD FLAP MOVEABLE VANE UPPER MOUNTING HARDWARE CORRODED (C-CHECK RO 8/9/2021) REMOVED LHIB FLAP MOVABLE VANE UPPER MOUNTING HARDWARE REF CRJ700 AMM 27-52-23-000-801-A01 STEP 4.A.(3)(A)(B). INSTALLED NEW MOUNTING HARDWARE REF CRJ700 AMM 27-52-23-40May 5, 2021 · N614QX · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA202160244Slat Track · corrodedR/H SLAT TRACK 2-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) REMOVED PITTING CORROSION ON RH SLAT TRACK 2-2 IN 2 AREAS IAW CRJ700 SRM 51-21-06-001-001-A01 / ORIGINAL THICKNESS IS .250" / AFT TRACK L= 1.6" W= 1" REMAINING THICKNESS ISMay 5, 2021 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081060243Slat Track · corrodedL/H SLAT TRACK 3-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 3-2 REF-CRJ-700 MHIRJ REO 670-57-42-1097 REV --, DATED 2021-05-17 AND CRJ 700 SRM 51-21-06-001-001-A01 ALL STEPS COMPLETED, OPS TEST GOOD. /May 5, 2021 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081060242Slat Track · corrodedL/H SLAT TRACK 2-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 2-2 REF-CRJ-700 MHIRJ REO 670-57-42-1096 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SMay 5, 2021 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081060241Slat Track · corrodedL/H SLAT TRACK 2-1 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 2-1 REF-CRJ-700 MHIRJ REO 670-57-42-1095 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SMay 5, 2021 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081060240Slat Track · corrodedL/H SLAT TRACK 1-3 HAS WORN AREA AND PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 1-3 REF-CRJ-700 MHIRJ REO 670-57-42-1094 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASKMay 5, 2021 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081060239Slat Track · corrodedL/H SLAT TRACK 1-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 1-2 REF-CRJ-700 MHIRJ REO 670-57-42-1093 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SMay 5, 2021 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081060238Slat Track · corrodedL/H SLAT TRACK 1-1 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 1-1 REF-CRJ-700 MHIRJ REO 670-57-42-1091 REV --, DATED 2021-05-14 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SMay 5, 2021 · N614QX · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081060286Bracket · crackedGALLEY SERVICE DOOR - STABILIZER BAR BRACKET CRACKED @ UPPER STABILIZER BAR ATTACH POINT (C-CHECK RO 8/9/2021) REMOVED AND REPLACED STABILIZER BAR BRACKET P/N CC670-38380-3 WITH A NEW ONE IAW CRJ700 SRM TASK 51-41-02-001-001-A01.May 3, 2021 · N614QX · Cndair CL6002C10 · Galley DoorsSDR SWIA2021081060237Skin · chafed*RH WING LOWER EXTERNAL SKIN HAS CHAFING FROM CANOE FAIRING PANEL 695AB BETWEEN FS 797.00 €“ 847.00, APPROX. WS 202.67 (C-CHECK RO 8/9/2021) DAMAGE BLENDED-OUT IAW REO 670-57-21-913 REV -- (DATED 2021-05-12) & CRJ700 SRM 51-12-00-001-001-A01. LEAK CHK May 3, 2021 · N614QX · Cndair CL6002C10 · Wing, Plate/SkinSDR SWIA2021081060236Skin · dentedEXTERNAL FUSELAGE - SEVERAL SMALL DENTS FS 485 STGR 21R (C-CHECK RO 8/9/2021) DUE TO THE PROXIMITY OF THE SEVERAL SMALL DENTS TO EACH OTHER AT FS485 STGR 21R, THEY WERE TREATED IN EFFECT AS ONE DENT AND REWORKED REF REO 670-53-31-673 REV -- DATED 2021-Apr 30, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201712215253Angle · crackedFOUND THE BS 202.75 BULKHEAD CAP ANGLE HAS A CRACK INDICATION AT STRINGER 13AR. 1 INCH LONG, 100%FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 670-53-11-1353 AND REO 670-53-11-1353.Dec 21, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201712205252Angle · crackedFOUND THE BS 202.75 BULKHEAD CAP ANGLE HAS A CRACK INDICATION IN THE RADIUS AT STRINGER 13A . REPAIRED THE DAMAGE IAW REO 670-53-11-1351.Dec 20, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201712165251Stiffener · crackedFOUND THE BS 202.75 BULKHEAD FWD STIFFENER, AFT INBD RADIUS, LBL 30, WL 100 HAS A CRACK INDICATION, .200 INCH LONG, 80% FSH, FAILED NDT INSPECTION. REPAIRED THE STIFFENER IAW SRM 53-11-10-201-005-A01.Dec 16, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201712155250Stiffener · crackedFOUND THE BS 202.75 BULKHEAD FWD VETICAL STIFFENER BL 0, WL 100 HAS A CRACK INDICATION NOTED ON THE RT SIDE FWD RADIUS APPROXIMATELY 1 INCH LONG, 70% FSH FAILED NDT. REPAIRED THE DAMAGE IAW REO 670-53-1354, AND REO 670-53-11-1354.Dec 15, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201702181245Door Sill · corrodedLT FLOORSILL AT FS 349 IS CORRODED. REPAIRED FLOORSILL IAW EA 25-2017-028 AND EC/TC EA 25-2017-028 REV 0.Feb 18, 2017 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201702141204Angle · corrodedDURING C CHECK, FOUND PASSENGER DOOR LOWER SILL MID CAP ANGLE CORRODED. R & R PASSENGER DOOR LOWER SILL MID CAP ANGLE.Feb 14, 2017 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201702131250Floorbeam · corrodedCORROSION ON FLOORBEAM AT LBL 27.00 BETWEEN FS 1000 AND FS 1051. REPAIRED FLOORBEAM IAW EO 700-53-10-00012.Feb 13, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201702131244Floorbeam · corrodedCORROSION ON FLOORBEAM AT LBL 9.00 BETWEEN FS 1015.00 AND FS 1051.30. CONTINUATION FROM OP 74 FOUND DAMAGED CLIP AT LBL9 FS 985. REPAIRED CLIP IAW EA 26-2017-024.Feb 13, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201702131202Doubler · corrodedDURING C CHECK, FOUND CORROSION ON THE TCAS OMNI DIRECTIONAL ANTENNA DOUBLER. R & R THE DOUBLER.Feb 13, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201702081155Intercostal · corrodedCORROSION ON AVIONICS BAY INTERCOSTAL AT FS 364.00 STR 26L. REMOVED AND INSTALLED NEW SERVICEABLE INTERCOSTAL AT FS 364.00 STR 26L IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Feb 8, 2017 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201702031133Fitting · crackedCO-PILOTS WINDSHIELD SIDE POST LOWER AFT SUPPORT ANGLE IS CRACKED AT RADIUS. REMOVED AND INSTALLED A NEW SUPPORT FITTING IAW SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.Feb 3, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201702031132Frame · corrodedCORROSION ON BS 295 FRAME BETWEEN STRINGERS 25L-25R. REPAIRED THE FRAME SECTOR IAW EC/TC REO 670-53-21-799 AND REO 670-53-21-799 REV A.Feb 3, 2017 · N614QX · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201701301117Angle · corrodedSERVICE DOOR LOWER SILL, LOWER SILL ANGLE IS CORRODED. REMOVED AND REPLACED SILL ANGLE IAW SRM 51-42-06-001-001-A01.Jan 30, 2017 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201701301116Seat Track · corrodedRIGHT SIDE SEAT TRACK SEGMENT NR 6 FS 785-FS 863 HAS CORROSION AT MULTIPLE LOCATIONS. REPLACED SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801-A02.Jan 30, 2017 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201701301115Cage · damagedCARGO PANEL 281 ALC,S SMOKE DETECTOR CAGE IS BENT AND HAS ONE PIECE BROKEN OFF AND MISSING. REPAIRED CAGE IN ACCORDANCE WITH ECTC CARD NR REO 670-25-52-006 REV B DATED 2017-01-27 AND REO 670-25-52-006 REV E DATED 2016-09-09.Jan 30, 2017 · N614QX · Cndair CL6002C10 · Smoke Detection
Back to N614QX