# Service difficulty reports: N614QX

A list on [N614QX](https://openairdocs.org/aircraft/N614QX.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 10 · 465 reports

- [SDR SWIA2026080376720](https://openairdocs.org/sdr/SWIA2026080376720.md): Stringer · corroded · Jul 2, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R HAS SIGNS OF CORROSION BETWEEN FS 295 AND FS 310. REMOVED AND REPLACED THE STGR 19R BETWEEN FS 295 AND FS 310 IAW SRM 53-21-03, SRM 51-42-06, SRM 51-42-13, SRM 51-42-21, SRM 51-40-11, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16, AMM 20-70-00, REO 67
- [SDR SWIA2026070276719](https://openairdocs.org/sdr/SWIA2026070276719.md): Frame · fom · Jul 2, 2026 · N614QX · Cndair CL6002C10 · Standard Practices/Structures
  > REQUIRED FOM ON FRAME BS 333 TO FACILITATE MULTIPLE STRINGERS REPLACEMENT. PERFORMED REPAIR ON FRAME AT BS 333 BETWEEN STRINGER 25R TO STRINGER 25L IAW REO 670-53-21-799, REV -A, SRM 51-42-06, AND SRM 51-42-21, PERFORMED NDT INSPECTION IAW AMM 21-21-00.
- [SDR SWIA2026063076727](https://openairdocs.org/sdr/SWIA2026063076727.md): Frame Splice · damaged · Jun 30, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 421 REQUIRES SPLICE REPAIR FOR STRINGER 26L SPLICE, REPAIR TO FOM. PERFORMED FRAME SPLICE AT BS 421 IAW REO 670-53-21-2927, REV --(P1), AMM 21-31-00.
- [SDR SWIA2026080376721](https://openairdocs.org/sdr/SWIA2026080376721.md): Stringer · corroded · Jun 23, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L, BTWN BS 409 - 421 HAS SIGNS OF CORROSION. R & R THE STRINGER 19R BETWEEN FS 295 AND FS 310 IAW SRM 53-21-03, SRM 51-42-06, SRM 51-42-13, SRM 51-42-21, SRM 51-40-11, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16, AMM 20-70-00, REO 670-53-21-2929, REV.
- [SDR SWIA2026062276723](https://openairdocs.org/sdr/SWIA2026062276723.md): Skin · corroded · Jun 22, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE LWR SKIN EXTERIOR FOUND SIGNS OF CORROSION BTWN BS 501 - 549, AROUND ADF ANTENNA CUT-OUT. REMOVED DAMAGE ON FUSELAGE LOWER SKIN EXTERIOR BETWEEN BS 501 - 549 AROUND ADF ANTENNA CUTOUT, FOUND TO BE STRUCTURALLY ACCEPTABLE IAW SRM 53-31-01, 51-42-06, R
- [SDR SWIA2026061176715](https://openairdocs.org/sdr/SWIA2026061176715.md): Seat Track · corroded · Jun 11, 2026 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > UPON REMOVAL OF RT SEAT TRACK, CLEANED AREA AT BS 469 - 581, HAD MULTIPLE SIGNS OF CORROSION. PERFORMED REPAIR BETWEEN BS 469 - 581, FOUND TO BE WITHIN LIMITS IAW REO 670-53-31-1223, REV-, SRM 53-31-43, 51-11-00, 51-42-06, 51-42-13, 51-42-21, 53-00-41, 51-
- [SDR SWIA2026052876714](https://openairdocs.org/sdr/SWIA2026052876714.md): Seat Track · corroded · May 28, 2026 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > UPON REMOVAL OF RT SEAT TRACK, BS 581 - 685, SIGNS OF CORROSION NOTED AT BS 581. PERFORMED REPAIR BS 581 - 685, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-41, 51-12-00, 51-21-06, 53-31-43, 51-21-11, 51-25-06, 51-25-16, 51-42-06, 51-42-13, 51-42-21, & REO 670-
- [SDR SWIA2026052176724](https://openairdocs.org/sdr/SWIA2026052176724.md): Stringer · corroded · May 21, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 20L HAD SIGNS OF CORROSION BTWN BS 319 - 333. PERFORMED BLENDED OUT AND EVALUATED AREA ON S20L BETWEEN BS 319 TO 333, REWORKED CONDITION STRUCTURALLY ACCEPTABLE REMAINING THICKNESS ARE NOT LESS THAN REPORTED IAW REO 670-53-21-2918, REV-, SRM 51-12-00
- [SDR SWIA2026050576725](https://openairdocs.org/sdr/SWIA2026050576725.md): Post · corroded · May 5, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT BULKHEAD BS 280 COCKPIT POST HAS SIGNS OF CORROSION AT FLOOR LEVEL. PERFORMED REPAIR ON THE RT DOOR POST, IAW SRM 51-42-06, SRM 51-42-13, SRM 51-12-00, SRM 53-00-00, REO 670-53-11-745, REV -A.
- [SDR SWIA2026050576722](https://openairdocs.org/sdr/SWIA2026050576722.md): Post · corroded · May 5, 2026 · N614QX · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT BULKHEAD BS 280 COCKPIT POST HAS SIGNS OF CORROSION AT FLOOR LEVEL. PERFORMED A REPAIR AT FLIGHT COMPARTMENT LT DOOR POST IAW, SRM 51-42-13, SRM 51-12-00, AMM 20-70-00, RE0 670-53-11-745, REV -A, PERFORMED NDT.
- [SDR SWIA2026042576726](https://openairdocs.org/sdr/SWIA2026042576726.md): Drag Angle · cracked · Apr 25, 2026 · N614QX · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > RIGHT AFT VERTICAL DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE AT RH AFT VERTICAL IAW REO 670-55-31-018, REV-A, SRM 51-26-01.
- [SDR SWIA2026042576718](https://openairdocs.org/sdr/SWIA2026042576718.md): Drag Angle · cracked · Apr 25, 2026 · N614QX · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > LEFT AFT VERTICAL DRAG ANGLE IS CRACKED. PERFORMED REPAIR DRAG ANGLE ON LT AFT VERTICAL IAW REO 670-55-31-018, REV-A, SRM 51-26-01, NDT PERFORMED.
- [SDR SWIA2026042576716](https://openairdocs.org/sdr/SWIA2026042576716.md): Drag Angle · cracked · Apr 25, 2026 · N614QX · Cndair CL6002C10 · Vertical Stabilizer
  > RIGHT FWD DRAG ANGLE VERTICAL CRACKED. REPAIR PERFORMED DRAG ANGLE AT RH FWD VERTICAL IAW REO 670-55-31-211, REV--, REO 670-55-31-018, REV-A, SRM 51-26-01, NDT PEFORMED.
- [SDR SWIA2026042176717](https://openairdocs.org/sdr/SWIA2026042176717.md): Web · cracked · Apr 21, 2026 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR WEB IN FWD EQUIPMENT COMPARTMENT, RIGHT SIDE ADJACENT TO THE ADG PUMP. PERFORMED A REPAIR OF CRACKED FLOOR WEB IN FWD EQUIPMENT COMPARTMENT IAW REO 670-53-11-509 REV -E, AND AMM 20-70-00.
- [SDR SWIA2025111000005](https://openairdocs.org/sdr/SWIA2025111000005.md): Antenna · damaged · Nov 5, 2025 · N614QX · Cndair CL6002C10 · VHF Communications System
  > COMPLY WITH M-93 CRJ700-53-25-01 AND EA11125 REV A FOR THE MAJOR REPAIR TO THE FUSELAGE VHF ANTENNA, STA 629-645, STR 1L-1R COMPLIED WITH REPAIR PER INTELSAT EA11125 REV. A
- [SDR SWIA2025110600005](https://openairdocs.org/sdr/SWIA2025110600005.md): Antenna · damaged · Nov 5, 2025 · N614QX · Cndair CL6002C10 · VHF Communications System
  > COMPLY WITH M-93 CRJ700-53-25-01 AND EA11125 REV A FOR THE MAJOR REPAIR TO THE FUSELAGE/VHF ANTENNA/STA 629-645, STR 1L-1R (FILED OPEN)
- [SDR SWI202403110188](https://openairdocs.org/sdr/SWI202403110188.md): Steering Sys · uncontrollable · Mar 9, 2024 · N614QX · Cndair CL6002C10 · Landing Gear Steering System
  > CREW REPORTED THAT UPON LANDING AIRCRAFT BEGAN TO SWERVE UNCONTROLABLY (FLIGHT 4939 FILED CLOSED)UPON ARRIVAL TO AIRCRAFT INTERROGATED MDC FOUND NO CURRENT FAULTS AT THIS TIME. PERFORMED VISUAL INSPECTION OF BOTH LEFT AND RIGHT MLG SHOCK STRUT AND UPPER AND LO
- [SDR SWI2024F00114](https://openairdocs.org/sdr/SWI2024F00114.md): Seat Track · broken · Feb 10, 2024 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT FLOOR TRACK AT 10B IS BROKEN. (FILED CLOSED)REMOVED AND REPLACED FLOOR TRACK AT 10B IAW AMM 25-21-01.
- [SDR SWIA202311270006](https://openairdocs.org/sdr/SWIA202311270006.md): Unknown · warning message · Nov 26, 2023 · N614QX · Cndair CL6002C10 · Landing Gear System
  > DURING CLIMB OUT OF AEX AT 8000 FT AND 250KTS RECEIVED BRAKE OVHT WARNING MESSAGE AND ASSOCIATED AURAL WARNING. FO NOTICED BRAKE INDICATOR #4 SHOWED 7 AND THEN JUMPED UP TO 11 THEN RETURNED BACK TO 1. ALL OTHER INDICATORS SHOWED 1. COMPILED WITH QRH AND DETERM
- [SDR SWIA202108160312](https://openairdocs.org/sdr/SWIA202108160312.md): Window Post · failed insp · Aug 13, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Structure
  > FO'S WINDOW/WINDSHIELD I POST FAILED LEAK CHECK. REQUIRES REMOVAL, CLEANING, AND PROPERLY RE-SEALING/REINSTALLATION. (FILED CLOSED) REMOVED AND REINSTALLED THE I-STRAP ON THE FO WINDSHEILD AND SIDE WINDOW PER AMM 56-11-07. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA202108160311](https://openairdocs.org/sdr/SWIA202108160311.md): Windshield · cracked · Aug 11, 2021 · N614QX · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAINS WINDSHIELD IS CRACKED IN THE UPPER LH CORNER NEAR THE TERMINAL BLOCK. (FILED CLOSED) REMOVED AND REPLACED THE CAPTAINS SIDE WINDSHILED PER AMM 56-11-07 AND TASK CARD 56-220-1000-SKY. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME. / TO
- [SDR SWIA2021081060298](https://openairdocs.org/sdr/SWIA2021081060298.md): Cleat · corroded · Jun 14, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Structure
  > STRINGER TO FRAME ATTACHMENT CLEAT AT FS1031 STR24R HAS CORROSION (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CLEAT AT FS1031 STR24R IAW CRJ 700 SRM 51-42-21-001-001-A01, SEE CONTINUATION FOR SPECIFIC WORK ACCOMPLISHED
- [SDR SWIA2021081060277](https://openairdocs.org/sdr/SWIA2021081060277.md): Frame · damaged · Jun 8, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Frame
  > PERFORM FRAME SPLICE REPAIR AT FS1047, STR22L TO PROVIDE ACCESS FOR REPAIR OF STR 25L AT FS 1040 (C-CHECK RO 8/9/2021) INSTALLED NEW FRAME SPLICE AT FS1047 STGR 22L REF-CRJ-700 MHI RJ REO 670-53-61-1921 REV -- DATED 2021-06-26, SRM 51-42-06-001-001 A01
- [SDR SWIA2021081060276](https://openairdocs.org/sdr/SWIA2021081060276.md): Frame · damaged · Jun 7, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Frame
  > SPLICE REPAIR OF FRAME SECTOR FS501.00 AT STGR -16R COMMON TO JOB 71004994 OP 63 MX # 22779504 (C-CHECK RO 8/9/2021) PERFORMED SPLICE REPAIR OF THE FRAME SECTOR AT FS501.00 STGR 16R REF REO 670-53-31-671 REV -- DATED 2021-06-05. PRESSURE LEAK CHECK GO
- [SDR SWIA2021081060275](https://openairdocs.org/sdr/SWIA2021081060275.md): Frame · damaged · Jun 7, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Frame
  > SPLICE REPAIR OF FRAME SECTOR FS565.00 AT STGR-16R COMMON TO JOB 71004994 OP 61 MX# 22779485 (C-CHECK RO 8/9/2021) PERFORMED SPLICE REPAIR OF FRAME SECTOR FS 565 AT STGR 16R REF REO 670-53-31-671 REV-- DATED 2021-06-05 / COMPLIED WITH TASK CARD 51-900-
- [SDR SWIA2021081060297](https://openairdocs.org/sdr/SWIA2021081060297.md): Stop Fitting · cracked · Jun 6, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR, STOP BRACKET ASSY AT FS310.00 BETWEEN STGR 4LH/5LH CRACKED (C-CHECK RO 8/9/2021) REPLACED PAX DOOR STOPO BRACKET ASSY AT F.S 310.00 BETWEEN STRG 4LH/ 5LH IAW CRJ 700 SRM 51-42-21-001-001-A01
- [SDR SWIA2021081060274](https://openairdocs.org/sdr/SWIA2021081060274.md): Cleat · corroded · May 30, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CLEAT COMMON TO 1051 FRAME AND STRINGER 26R IS CORRODED (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CLEAT IAW CRJ 700 SRM 51-42-06-001-001-A01, SEE CONTINUATION FOR WORK ACCOMPLISHED. COMPLIED WITH SKYCARD 51-900-1002-SKY.
- [SDR SWIA2021081060273](https://openairdocs.org/sdr/SWIA2021081060273.md): Door · bent · May 29, 2021 · N614QX · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LH ENGINE UPPER FAN COWL DOOR THE I/B AFT EDGE IS BENT (C-CHECK RO 8/9/2021) REMOVED AND REPLACED 1EA INBOARD EDGE MEMBER ANGLE P/N CN622-0312-209 ON LH ENGINE UPPER FAN COWL DOOR REF: DWG CN622-0101 REV "K", DWG # CN622-0312 REV D. CRJ-700 SRM 51-4
- [SDR SWIA2021081060272](https://openairdocs.org/sdr/SWIA2021081060272.md): Door · bent · May 28, 2021 · N614QX · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RH ENGINE UPPER FAN COWL DOOR I/B AFT EDGE BENT (C-CHECK RO 8/9/2021) REMOVED AND REPLACED 1EA BENT INBOARD EDGE MEMBER P/N CN622-0312-0210 WITH NEW EDGE MEMBER ON THE R/H ENGINE UPPER FAN COWL DOOR REF: DWG# CN622-0201 REV L, CRJ-700 SRM 51-42-06-001-0
- [SDR SWIA2021081060301](https://openairdocs.org/sdr/SWIA2021081060301.md): Skin · dented · May 26, 2021 · N614QX · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > RH LOWER TRANSCOWL OUTER SKIN DENT. 6 O€™CLOCK. (C-CHECK RO 8/9/2021) EVALUATED RH LOWER TRANSCOWL OUTER SKIN DENT. 6 O€™CLOCK DEPTH.036" LENGTH.300"WIDTH.300" FOUND TO BE OUT OF LIMITS DUE TO THE FACT ONLY ALLOWED A DEPTH OF.028" TOOL #TUC8531 DUE
- [SDR SWIA2021081060271](https://openairdocs.org/sdr/SWIA2021081060271.md): Retainer · corroded · May 24, 2021 · N614QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FOWD SEAL RETAINER CORRODED AROUND MORE THAN HALF HOLES AND MATING SURFACE. (C-CHECK RO 8/9/2021) REMOVED AND REPLACED PAX DOOR FWD SEAL RETAINER REF-CRJ-700 SRM 51-42-06-001-001 A01 AND DWG 601R31702 REV N,LEAK CHECK GOOD. / COMPLIED WITH TASK
- [SDR SWIA2021081060269](https://openairdocs.org/sdr/SWIA2021081060269.md): Frame · corroded · May 23, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 1051 CORRODED BETWEEN STR 26 LH AND 26 RH (C-CHECK RO 8/9/2021) REPAIRED FRAME FS1051 BETWEEN STGR 26LH & 26RH AND COMPLIED WITH ALL STEPS OF REF-CRJ-700 MHI RJ REO 670-53-61-1914 REV -- DATED 2021-06-16. / COMPLIED WITH THE TASK 51-900-1002-SKY
- [SDR SWIA2021081060268](https://openairdocs.org/sdr/SWIA2021081060268.md): Angle · corroded · May 22, 2021 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE ATTACHED TO INTERCOSTAL FS310 - FS319.70 AT STGR 20R AND FRAME FS310 HAS MULTIPLE AREAS OF CORROSION (C-CHECK RO 8/9/2021) REMOVED AND REPLACED ANGLE P/N SH670-32046-3 AT FRAME FS310 STGR20R INTERCOSTAL REF CRJ700 SRM51-42-06-001-001-A01 REV 38 JU
- [SDR SWIA2021081060267](https://openairdocs.org/sdr/SWIA2021081060267.md): Support Angle · corroded · May 21, 2021 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING REMOVEL OF AFT FORMER FOUND AFT SUPPORT ANGLE CORROED (C-CHECK RO 8/9/2021) REMOVED OLD AFT SUPPORT ANGLE & INSTALLED NEW AFT FORMER SUPPORT ANGLE PER CRJ-700-SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 & DWG 601R31702 REV N. LEAK CHECK
- [SDR SWIA2021081060266](https://openairdocs.org/sdr/SWIA2021081060266.md): Support Angle · corroded · May 21, 2021 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF FWD FORMER FOUND FWD SUPPORT ANGLE CORRODED. (C-CHECK RO 8/9/2021) REMOVED OLD ANGLE AND INSTALLED NEW FWD FORMER SUPPORT ANGLE PER CRJ-700 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 & DWG 601R31702 REV N. LEAK CHECK GOOD. CO
- [SDR SWIA2021081060265](https://openairdocs.org/sdr/SWIA2021081060265.md): Former · corroded · May 20, 2021 · N614QX · Cndair CL6002C10 · Passenger/Crew Doors
  > AFT FORMER ON *PAX DOOR HAS CORROSION ON MULTIPLE ELEMENTS (C-CHECK RO 8/9/2021) REMOVED OLD AFT FORMER & REPLACE WITH NEW AFT FORMER PER CRJ-700-SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SK
- [SDR SWIA2021081060264](https://openairdocs.org/sdr/SWIA2021081060264.md): Intercostal · cracked · May 18, 2021 · N614QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD7 INTERCOSTAL BETWEEN F.S.338-347.25 HAS CRACK IN RADIUS. (C-CHECK RO 8/9/2021) REMOVED OLD INTERCOSTAL & REPLACED WITH NEW INTERCOSTAL PER CRJ-700-SRM 51-42-06-001-001-A01 & DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SKY CARD 51-900
- [SDR SWIA2021081060263](https://openairdocs.org/sdr/SWIA2021081060263.md): Intercostal · corroded · May 18, 2021 · N614QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL BETWEEN F.S.338-347.25 BELOW DD3 HAS CORROSION ON MULTIPLE ELEMENTS(AS MARKED) (C-CHECK RO 8/9/2021) REMOVED OLD INTERCOSTAL & REPLACE WITH NEW INTERCOSTAL PER CRJ-700-SRM 51-42-06-001-001-A01 & DWG 601R31702 REV N. LEAK CHK GOOD. C
- [SDR SWIA2021081060262](https://openairdocs.org/sdr/SWIA2021081060262.md): Intercostal · cracked · May 18, 2021 · N614QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD1 INTERCOSTAL HAS CRACK IN RADIUS.(AS MARKED) (C-CHECK RO 8/9/2021) REMOVED AND REPLACED INTERCOSTAL W/NEW PARTS IAW CRJ700 SRM 51-42-06-001-001-A01 & DWG 601R31702 REV N. LEAK CHK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY
- [SDR SWIA2021081060261](https://openairdocs.org/sdr/SWIA2021081060261.md): Former · corroded · May 18, 2021 · N614QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER HAS CORROSION ON MULTIPLE ELEMENTS. (C-CHECK RO 8/9/2021) REMOVED OLD FWD FORMER & REPLACE WITH NEW FWD FORMER PER CRJ-700-SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 DWG 601R31702 REV N. LEAK CHK GOOD. COMPLIED WITH SKY CARD
- [SDR SWIA2021081060260](https://openairdocs.org/sdr/SWIA2021081060260.md): Hinge · worn · May 15, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Door Hinge
  > *PAX DOOR PIANO HINGE ON FUSELAGE SIDE, LUG ON FWD PORTION HAS WEAR. MARKED. (C-CHECK RO 8/9/2021) NEW HINGE HALF INSTALLED IAW CRJ700 SRM 53-21-23-201-007-A01 WITH REFERENCE TO DWG #SH670-31810 REV-NC. LEAK CHECK GOOD / 51-900-1002-SKY COMPLIED WITH
- [SDR SWIA2021081060259](https://openairdocs.org/sdr/SWIA2021081060259.md): Hinge · worn · May 15, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Door Hinge
  > *PAX DOOR PIANO HINGE ON DOOR SIDE HAS MULTIPLE LUG LANDINGS WITH WEAR MARKS. (C-CHECK RO 8/9/2021) REMOVED AND REPLACED PIANO HINGE W/NEW PARTS IAW CRJ700 SRM 52-11-01-201-002-A01 & DWG 601R31702 REV.- N. LEAK CHK GOOD. COMPLIED WITH SKY CARD 51-900-
- [SDR SWIA2021081060296](https://openairdocs.org/sdr/SWIA2021081060296.md): Cleat · corroded · May 14, 2021 · N614QX · Cndair CL6002C10 · Passenger/Crew Doors
  > SUSPECTED CORROSION IDENTIFIED 2 PLACES ON INNER DOOR STRUCTURE UNDER ACCESS PANEL 832FL - AS MARKED (C-CHECK RO 8/9/2021) REMOVED AND REPLACED 1EA CLEAT IAW CRJ-700 SRM 51-42-06-001-001-A01
- [SDR SWIA2021081060295](https://openairdocs.org/sdr/SWIA2021081060295.md): Floorbeam · corroded · May 13, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *CORROSION ON FLOOR BEAM PACKER SANDWICHED BETWEEN FS 333.00 FLOOR SUPPORT BEAM AND RBL 9 FLOOR BEAM. (C-CHECK RO 8/9/2021) REMOVED AND REPLACE PACKERS (2EA) ON FLOOR BEAM AT FS333.00 RBL9 IAW RJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA2021081060294](https://openairdocs.org/sdr/SWIA2021081060294.md): Seat Track · corroded · May 13, 2021 · N614QX · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H O/B SEAT TRACK AT LBL 27 FROM APPROX F/S 364 TO 477 HAS MULTIPLE AREAS OF CORROSION (C-CHECK RO 8/9/2021) L/H O/B SEAT TRACK LBL27 FOUND TO BE OUT OF LIMITS DUE TO MULTIPLE DISCREPANT LOCATIONS ONLY ONE TYPE OF DAMAGE IS ALLOWED AT ANY TYPICAL CROS
- [SDR SWIA2021081060285](https://openairdocs.org/sdr/SWIA2021081060285.md): Floorbeam · corroded · May 13, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *RH FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. RBL 45 HAS CORROSION (C-CHECK RO 8/9/2021) REPLACED NEW RH FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. RBL 45 REF CRJ7
- [SDR SWIA2021081060284](https://openairdocs.org/sdr/SWIA2021081060284.md): Floorbeam · corroded · May 13, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *LH FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. LBL 45 HAS CORROSION (C-CHECK RO 8/9/2021) REPLACED NEW L/H FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. LBL 45 REF CRJ
- [SDR SWIA2021081060258](https://openairdocs.org/sdr/SWIA2021081060258.md): Floorbeam · corroded · May 13, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *CORROSION ON FLOOR SUPPORT BEAM FS 333.00 AT APPROX. RBL 18. MARKED. (C-CHECK RO 8/9/2021) DAMAGE #1 BLENDOUT DAMAGE PER CRJ 700 SRM 51-21-16-001-001-A01, NO REWORK PERMITTED ON THIS AREA FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 53-21-43-101-001-A01,
- [SDR SWIA2021081060300](https://openairdocs.org/sdr/SWIA2021081060300.md): Plate · corroded · May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD BAGG FLOOR MOUNT DBLR PLATE CORRODED @ FS 533 STGR 27 (C-CHECK RO 8/9/2021) REMOVED AND INSTALLED NEW FWD CARGO FLOOR MOUNT PLATE SH670-33376-3. REF CRJ-700 SRM 51-42-06-001-001-A01. SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA2021081060299](https://openairdocs.org/sdr/SWIA2021081060299.md): Plate · corroded · May 12, 2021 · N614QX · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD BAGG FLOOR PLATE CORRODED @ FS 517 BTWN STGRS 26R/27 (C-CHECK RO 8/9/2021) BLENDED THEN REPLACED CORRODED OUT OF LIMITS FLOOR PLATE WITH NEW FABRICATED PART AT FS 517 BETWEEN STGRS 26R/27 REF CRJ700 SRM 51-42-06-001-001-A01

Next page: https://openairdocs.org/aircraft/N614QX/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 = 'N614QX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N614QX/reports

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