# Service difficulty reports: N612QX

A list on [N612QX](https://openairdocs.org/aircraft/N612QX.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 9 · 415 reports

- [SDR SWIA2026052776234](https://openairdocs.org/sdr/SWIA2026052776234.md): Intercostal · chafed · May 27, 2026 · N612QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ON STGR-9L, BETWEEN FS1162.00 AND FS1181.00 SHOWING SIGNS OF CHAFING (AFT EQUIPMENT BAY) PERFORMED REPAIR AREA ON INTERCOSTAL STGR9L BETWEEN FS1162.00 TO FS1181.00 IAW CRJ700 SRM 53-61-04, 51-42-06, AMM20-70-00, 29-11-30, 21-52-06, MHI RJ REO 670-
- [SDR SWIA2026032976238](https://openairdocs.org/sdr/SWIA2026032976238.md): Skin · damaged · Mar 29, 2026 · N612QX · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EVIDENCE OF LIGHTNING DAMAGE IN AREA OF BS 354, S27. REPAIRED DAMAGED AREAS ON EXTERIOR FUSELAGE SKIN AT BS 354, S27 IAW REO 670-53-21-2895, REV --, AND SRM 51-42-06, 53-00-00, 51-40-11, 51-12-00; AMM 05-51-07.
- [SDR SWIA2026032976232](https://openairdocs.org/sdr/SWIA2026032976232.md): Skin · gouged · Mar 29, 2026 · N612QX · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > PAX DOOR CUTOUT-FWD LOWER CORNER HAS GOUGE (BS 319.7 AND BS 333, STGR17L AND WL 71) PERFORMED REPAIR AREA ON PAX DOOR CUTOUT FWD LOWER CORNER AT BS 319.7 TO BS 333, STGR17L AND W L71 IAW SRM 51-26-01, 51-11-00. 53-21-01. THIS TEMPORARY REPAIR MUST BE REPLACED
- [SDR SWIA2026032876233](https://openairdocs.org/sdr/SWIA2026032876233.md): Floorbeam · cracked · Mar 28, 2026 · N612QX · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLIGHT COMPARTMENT LBL12 FLOORBEAM CRACKED AT FS280. REPAIRED DAMAGED FLOORBEAM AT LBL12, BS 280 IAW SRM 51-42-20, 51-42-06, 51-42-21, 53-11-43, AMM 20-70-00, 32-22-07, 32-22-00, E-STR-12-004 REV -NC.
- [SDR SWIA2026032576237](https://openairdocs.org/sdr/SWIA2026032576237.md): Rod · gouged · Mar 25, 2026 · N612QX · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT WING INBD FLAP NR 2 FLAP VANE ACTUATOR ROD IS GOUGED BLENDED OUT DAMAGE ON THE LT WING INBD FLAP NR 2 VANE ACTUATOR ROD IAW REO 670-57-52-257, REV -B, AMM 27-52-00.
- [SDR SWIA2026032576236](https://openairdocs.org/sdr/SWIA2026032576236.md): Web · cracked · Mar 25, 2026 · N612QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR WEB (RIGHT OF ADG PUMP) CRACKED AT PREVIOUS REPAIR. REMOVED AND REPLACED RT FLOOR WEB REPAIR AT FWD EQUIPMENT COMPARTMENT IAW REO 670-53-11-509, REV -E.
- [SDR SWIA2026032576235](https://openairdocs.org/sdr/SWIA2026032576235.md): Rod · gouged · Mar 25, 2026 · N612QX · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT WING INBD FLAP NR 4 VANE ACTUATOR ROD HAS GOUGES. BLENDED OUT DAMAGE ON THE LT WING INBD FLAP 4 FLAP VANE ACTUATOR ROD IAW, REO 670-57-52-257, REV -B, AMM 27-52-00.
- [SDR SWIA2026032576231](https://openairdocs.org/sdr/SWIA2026032576231.md): Vane · gouged · Mar 25, 2026 · N612QX · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT WING INBD FLAP NR 3 FLAP VANE ACTUATOR ROD IS GOUGED. BLENDED OUT DAMAGE ON THE LT WING INBD FLAP 3 FLAP VANE ACTUATOR ROD IAW REO 670-57-52-257, REV -B, AMM 27-52-00 MATERIAL LOSS NEGLIGIBLE. NO CHANGE TO AIRCRAFT WEIGHT.
- [SDR SWIA2026012776240](https://openairdocs.org/sdr/SWIA2026012776240.md): Roller · out of limits · Jan 27, 2026 · N612QX · Cndair CL6002C10 · Leading Edge Devices
  > TRACK ROLLER SLAT 1-2 700 RT, DISCARD THE RH SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2. REMOVE AND REPLACE IAW TASK CARD 27-630-809. COMPLIED WITH SKYWEST TASK CARD: 27-630-809.
- [SDR SWIA2026012776239](https://openairdocs.org/sdr/SWIA2026012776239.md): Roller · out of limits · Jan 27, 2026 · N612QX · Cndair CL6002C10 · Leading Edge Devices
  > TRACK ROLLER, SLAT 1-2 700 LT, DISCARD THE LT SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2. REMOVE AND REPLACE IAW TASK CARD 27-530-809. COMPLIED WITH SKYWEST TASK CARD: 27-530-80.
- [SDR SWI2025F01825](https://openairdocs.org/sdr/SWI2025F01825.md): Safety Pin · installed · Dec 14, 2025 · N612QX · Cndair CL6002C10 · Main Landing Gear
  > GEAR DISAGREE IN AIR RAN QRH. GEAR PINS STILL INSTALLED. (FLIGHT 6218) REMOVED LT/RT AND NLG SAFETY PINS AND INSTALLED THE SAFETY PINS IN THE HOLDER BEHIND THE FOS SEAT AND VERIFIED ALL 4 SAFETY PINS ARE PRESENT. PERFORMED A GVI OF THE LT/RT AND NLG AND ASSO
- [SDR SWIA2025012000119](https://openairdocs.org/sdr/SWIA2025012000119.md): Skin · dented · Jan 19, 2025 · N612QX · Cndair CL6002C10 · Trailing Edge Flaps
  > TRANSFER FROM EAML 1516947: DENTS TO R/H OUTBD FLAP LOWER SKIN (DWG: 601R14536, AL ALLOY 2024-T3, 0.040€? POCKET THICKNESS, 0.050€? PAD-UP THICKNESS, REF). DENTS ARE LOCATED BETWEEN FS235.965- FS254.96 AND 10.00€? FWD OF FLAP TRAILING EDGE (BETWEEN FRONT S
- [SDR SWIA2024120901360](https://openairdocs.org/sdr/SWIA2024120901360.md): Unknown · odor · Dec 6, 2024 · N612QX · Cndair CL6002C10 · Air Distribution System
  > BURNING SMELL FOR ABOUT 5 MINS AFTER 30 MINUTES IN FLIGHT. IT CAME ON INTENSELY TWICE DURING THOSE 5 MINUTES. THE WAS NO ANY INDICATION OF SMOKE OR ANY EICAS MESSAGE. THE NEXT 40 MINUTES OF FLYING WAS UNEVENTFUL. (FLIGHT 1300 - FILED CLOSED)COMPLIED WITH FIM
- [SDR SWIA202412090006](https://openairdocs.org/sdr/SWIA202412090006.md): Windshield · arced · Dec 6, 2024 · N612QX · Cndair CL6002C10 · Flight Compartment Windows
  > CA SIDE WINDSHIELD MAY HAVE ARCED. BURNING SMELL IN THE COCKPIT. APPEARS TO BE COMING FROM THE BOTTOM LEFT CORNER OF THE CA SIDE WINDSHIELD. EN-ROUTE AND THE SMELL LASTED ABOUT 5 MINUTES. (FLIGHT 6423 - FILED CLOSED) REMOVED AND REPLACED CA SIDE WINDSHIE
- [SDR SWIA202266223](https://openairdocs.org/sdr/SWIA202266223.md): None · odor · Aug 9, 2022 · N612QX · Cndair CL6002C10 · Air Conditioning System
  > TRANSIENT BRIEF ACRID ODOR SIMILAR TO BURNT RUBBER SMELT BY PASSENGERS IN ROW 6-8. ALL CABIN LIGHTS SELECTED OFF AT TIME OF ODOR. OVERHEAD BINS WERE OPENED AND NO SOURCE OF LION BATTERY RUNAWAY WAS DETECTED. POST FLIGHT INSPECTION OF OVERHEADS BY CREW IN ROW 6
- [SDR SWIA202265832](https://openairdocs.org/sdr/SWIA202265832.md): None · odor · May 29, 2022 · N612QX · Cndair CL6002C10 · Air Conditioning System
  > FLIGHT CREW AND PASSENGERS REPORT A BURNING SMELL IN THE AREA OF THE 4TH ROW OF SEATS. FLIGHT ATTENDANT REMARKED THAT THE BALLAST DOOR OVER SEATS 4 DC WAS ABNORMALLY HOT COMPARED TO OTHER BALLAST DOORS. ( FLIGHT 3278 - FILED CLOSED) / REFERENCED SERVICE
- [SDR SWIA2021082060543](https://openairdocs.org/sdr/SWIA2021082060543.md): Windshield · delaminated · Aug 19, 2021 · N612QX · Cndair CL6002C10 · Flight Compartment Windows
  > COPILOT FORWARD WINDSCREEN APPEARS DELAMINATED, UPPER RIGHT CORNER AND LOWER LEADING EDGE. (FLIGHT 2958 - FILED CLOSED) REMOVED AND REPLACED FO WINDSHIELD PER CRJ700 AMM 56-11-01 AND TASK CARD 56-220-1000-SKY. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA202159325](https://openairdocs.org/sdr/SWIA202159325.md): Thrust Reverser · damaged · Jun 17, 2021 · N612QX · Cndair CL6002C10 · Engine Thrust Reverser
  > DAMAGE FOUND ON LH LOWER FAN COWL UPON RIGGING OF LH THRUST REVERSERS. (C-CHECK RO 7/5/2021) REPAIRED LH LOWER FAN COWL. REF CRJ-700 SRM 54-14-00-201-004-A01. RESTORED FINISH. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2021070759326](https://openairdocs.org/sdr/SWIA2021070759326.md): Floorbeam · damaged · Apr 25, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *MISSING FASTENER HEAD, UNDERSIDE OF FLOOR BEAM RBL9 AFT OF FS 280.00 (C-CHECK RO 7/5/2021) REMOVED AND REPLACED FASTENER WITH MISSING HEAD, LOCATED UNDERSIDE OF FLOOR BEAM RBL 9 AFT OF FS 280.00 REF. CRJ-700 SRM 51-42-13-001-001-A01
- [SDR SWIA2021070759319](https://openairdocs.org/sdr/SWIA2021070759319.md): Skin · corroded · Apr 20, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR OUTER SKIN ( INNER SIDE) FOUND EXFOLIATED CORROSION BETWEEN MID DD3 AND MID DD4 INTERCOSTAL (C-CHECK RO 7/5/2021) BLENDED OUT CORROSION ON PAX DOR OUTER SKIN (INNER SIDE) IAW CRJ700 SRM 51-21-06-001-001-A01, FOUND TO BE WITH IN LIMITS OF REO 67
- [SDR SWIA2021070759318](https://openairdocs.org/sdr/SWIA2021070759318.md): Door Frame · corroded · Apr 20, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FORMER F/S 329.41 IS CORRODED BETWEEN MID DD5 AND MID DD6 INTERCOSTAL (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR FORMER FS329.41 BETWEEN MID DD5 AND MID DD6 INTERCOSTAL PER CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 R
- [SDR SWIA2021070759317](https://openairdocs.org/sdr/SWIA2021070759317.md): Skin · gouged · Apr 18, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGE AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R (C-CHECK RO 7/5/2021) REPAIRED GOUGE AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R REF REO 670-53-00-290 REV -F DATED 2019/04/26 SOLUTION 2 ALL STEPS COMPLIED WITH. COMPLIED WITH 51-900-1002-SKY R
- [SDR SWIA2021070759316](https://openairdocs.org/sdr/SWIA2021070759316.md): Skin · corroded · Apr 18, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR OUTER SKIN HAS CORROSION BETWEEN MID DD5 AND MID DD6 INTERCOSTAL ( INNNER SIDE) (C-CHECK RO 7/5/2021) REPAIRED PASSENGER DOOR OUTER SKIN BETWEEN DD5 AND DD6. REF REO 670-52-11-1226 REV -- DATED 2021-05-03 ALL STEPS COMPLIED WITH. COMPLIED WITH
- [SDR SWIA2021070759315](https://openairdocs.org/sdr/SWIA2021070759315.md): Door Frame · corroded · Apr 17, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FRAME F/S 327.763 IS CORRODED (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR FRAME FS327.763 PER CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND BOMBARDIER DWG 601R31702 REV. N. RESTORED FINISH AND REAPPLIED CIC TO THE AREA.
- [SDR SWIA2021070759314](https://openairdocs.org/sdr/SWIA2021070759314.md): Support Angle · corroded · Apr 16, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD ANGLE SUPPORT IS CORRODED (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR FWD ANGLE SUPPORT WITH A SERVICEABLE UNIT PER CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. RESTORED FINISH AND REAPPLIED CIC TO REPAIR LOC
- [SDR SWIA2021070759313](https://openairdocs.org/sdr/SWIA2021070759313.md): Skin · chafed · Apr 16, 2021 · N612QX · Cndair CL6002C10 · Trailing Edge Flaps
  > THE R/H INBOARD FLAP LOWER SKIN IS CHAFED WHERE BOTH THE INBOARD AND OUTBOARD CANOE FAIRING SEALS CONTACT IT. (C-CHECK RO 7/5/2021) COMPLIED WITH THE BLENDOUT REPAIR TO THE R/H INBOARD FLAP LOWER SKIN BETWEEN FLAP STA 48.000 AND FLAP STA 64.000 PER REO
- [SDR SWIA2021070759312](https://openairdocs.org/sdr/SWIA2021070759312.md): Skin · chafed · Apr 16, 2021 · N612QX · Cndair CL6002C10 · Trailing Edge Flaps
  > THE L/H INBOARD FLAP LOWER SKIN IS CHAFED WHERE THE INBOARD CANOE FAIRING SEAL CONTACTS IT. (C-CHECK RO 7/5/2021) COMPLIED WITH THE BLENDOUT REPAIR TO THE L/H INBOARD FLAP LOWER SKIN BETWEEN FLAP STA 48.000 AND FLAP STA 64.000 PER REO 670-57-52-483 REV
- [SDR SWIA2021070759311](https://openairdocs.org/sdr/SWIA2021070759311.md): Intercostal · corroded · Apr 16, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR AFT DD4 INTERCOSTAL WITH A SERVICEABLE UNIT PER CRJ700 SRM 51-42-06-001-001-A01 & BOMBARDIER DWG 601R31702 REV. N. RESTORED FINISH AND REAPPLIED CIC AT REPAIRED
- [SDR SWIA2021070759310](https://openairdocs.org/sdr/SWIA2021070759310.md): Cleat · corroded · Apr 16, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD CLEAT IS CORRODED COMMON TO DD4 INTERCOSTAL (C-CHECK RO 7/5/2021) REMOVED AND INSTALLED NEW CLEAT COMMON TO AFT DD4 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV. N AND RESTORED FINISH AND APPLY C.I.C AT REPAIRED LOCAT
- [SDR SWIA2021070759309](https://openairdocs.org/sdr/SWIA2021070759309.md): Former · corroded · Apr 13, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER HAS CORROSION (C-CHECK RO 7/5/2021) REPLACED PASSENGER DOOR AFT FORMER WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 DRAWING 601R31702 REV N. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2021070759308](https://openairdocs.org/sdr/SWIA2021070759308.md): Stringer · corroded · Apr 11, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 20L APPROXIMATELY AT FS 324.00 - 327.00 COMMON TO TRANSPONDER CANNON PLUG AND CABLE BRACKET (C-CHECK RO 7/5/2021) REPLACED STGR 20L WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31810 RE
- [SDR SWIA2021070759307](https://openairdocs.org/sdr/SWIA2021070759307.md): Stringer Splice · corroded · Apr 9, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > SPLICE ANGLE AT FS 333.00 ATTACHED TO STGR 21L COMMON TO INTERCOSTAL HAS EVIDENCE OF CORROSION (C-CHECK RO 7/5/2021) REPLACED SPLICE ANGLE AT FS 333.00 ATTACHED TO STGR 21L COMMON TO INTERCOSTAL. REF: CRJ-700 S.R.M. 51-42-06-001-001-A01, DWG SH670-31
- [SDR SWIA2021070759305](https://openairdocs.org/sdr/SWIA2021070759305.md): Stringer Splice · corroded · Apr 7, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON SPLICE STGR 24L FS333.00 (C-CHECK RO 7/5/2021) BLENDED CORROSION REF CRJ 700 SRM 51-12-00-001-001-A01 100% MATERIAL LOSS, AFTER BLEND. SPLICE REQUIRES REPLACEMENT. REF CRJ 700 SRM 53-00-00-101-001-A01 REPLACED STRG 24L SPLICE ATTATC
- [SDR SWIA2021070759304](https://openairdocs.org/sdr/SWIA2021070759304.md): Hinge Fitting · gouged · Apr 7, 2021 · N612QX · Cndair CL6002C10 · Fuselage, Door Hinge
  > * FOUND A GOUGE ON FUSELAGE SIDE OF THE PAX DOOR HINGE LUG(AREA MARKED) (C-CHECK RO 7/5/2021) REPAIRED GOUGE ON FUSELAGE SIDE OF THE PAX DOOR HINGE LUG. BOMBARDIER REO 670-53-21-582 REV -F DATED 2017-08-02. COMPLIED WITH SKYWEST TASK 51-900-1002-SKY.
- [SDR SWIA2021070759303](https://openairdocs.org/sdr/SWIA2021070759303.md): Door Sill · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON GALLEY DOOR SILL. AREA MARKED. (C-CHECK RO 7/5/2021) REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SILL ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG# SH670-31950 REV.Y. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.
- [SDR SWIA2021070759302](https://openairdocs.org/sdr/SWIA2021070759302.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 25L, BETWEEN FS 421.00 €“ 437.00. MARKED. (C-CHECK RO 7/5/2021) REPLACED STRINGER 25L BETWEEN FS409-FS453 REF CRJ 53-00-03-201-001-A01 AND DRAWING SH670-31350 REV A. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CA
- [SDR SWIA2021070759301](https://openairdocs.org/sdr/SWIA2021070759301.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 19R BETWEEN FS 349.00 €“ 394.00. MARKED. (C-CHECK RO 7/5/2021) REPLACED STGR 19R FROM FS349-FS394.00 REF SRM 51-42-06-001-001-A01 DWG SH670-31070 REV J RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY & M-337
- [SDR SWIA2021070759300](https://openairdocs.org/sdr/SWIA2021070759300.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 20R BETWEEN FS 364.00 €“ 379.00. MARKED. (C-CHECK RO 7/5/2021) REMOVED CORROSION ON STGR 20R BETWEEN FS364.00-FS379.00. WITHIN LIMITS. RESTORED FINISH PRESSURE CHECK GOOD. REF REO 670-53-21-2021 REV -- DATED 2021-04-27. COMPLIED WITH
- [SDR SWIA2021070759299](https://openairdocs.org/sdr/SWIA2021070759299.md): Intercostal · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON INTERCOSTAL ATTACHED TO STGR 21L BETWEEN FS 310.00 €“ 349.00. (C-CHECK RO 7/5/2021) REPLACED INTERCOSTAL BETWEEN F.S. 310.00 - F.S. 349.00 WITH NEW ONE'S P/N SH670-31822-1, SH670-31823-1 REF CRJ 700 SRM 51-42-06-001-001-A01. DWG SH670-31
- [SDR SWIA2021070759298](https://openairdocs.org/sdr/SWIA2021070759298.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 22L BETWEEN FS 333.00 €“ 349.00. MARKED. (C-CHECK RO 7/5/2021) REPAIRED STR 22L BETWEEN FS333-FS379. REF CRJ 700 SRM 53-00-03-201-001-A01, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DWG SH670-31366 REV NC, DW
- [SDR SWIA2021070759297](https://openairdocs.org/sdr/SWIA2021070759297.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 19R BETWEEN FS 280.00 €“ 295.00, AND FS 310.00 €“ 319.00 (C-CHECK RO 7/5/2021) REMOVED COROSION ON STGR 19 R BETWEEN FS 280.00 - 295.00 AND FS 310.00 - 319.00 REF REO 670-53-21-2060 REV -- DATED 2021-06-05 ALL STEPS COMPLIED WITH. F
- [SDR SWIA2021070759296](https://openairdocs.org/sdr/SWIA2021070759296.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 27 BETWEEN FS 319.00 €“ 333.00 ON LH AND RH SURFACES. AREA MARKED. (C-CHECK RO 7/5/2021) REMOVED AND REPLACED STGR27 SECTION BETWEEN F.S315.00 AND 333.00 IAW CRJ-700 SRM 51-42-06-001-001-A01 REV.38 25JULY2020 AND BOMBARDIER DWG# SH67
- [SDR SWIA2021070759295](https://openairdocs.org/sdr/SWIA2021070759295.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 20R BETWEEN FS 295.00 €“ 310.00 (C-CHECK RO 7/5/2021) REPLACED STR 20RH FROM FS280-FS319.00 WITH NEW. REF CRJ-700 SRM 53-00-03-201-001-A01. 51-42-06-001-001-A01 AND DRAWING SH670-31630 REV K / COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2021070759294](https://openairdocs.org/sdr/SWIA2021070759294.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 24L BETWEEN FS 319.00 €“ 333.00. MARKED. (C-CHECK RO 7/5/2021) REMOVED AND REPLACED STGR24L SECTION F.S.280.00-333.00 IAW CRJ-700 SRM 51-42-06-00-001-A01 REV38 25JULY2020 AND CRJ-700 SRM 51-42-21-00-001-A01 REV38 25JULY2020 AND BOM
- [SDR SWIA2021070759293](https://openairdocs.org/sdr/SWIA2021070759293.md): Stringer · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 19L, BETWEEN FS 295.00 €“ 310.00. MARKED. (C-CHECK RO 7/5/2021) REPLACED STGR 19L BETWEEN FS295.00-FS310.00 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31550 REV G. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH
- [SDR SWIA2021070759292](https://openairdocs.org/sdr/SWIA2021070759292.md): Floorbeam · corroded · Apr 3, 2021 · N612QX · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *MULTIPLE AREAS OF CORROSION ON FS 280.00 FLOOR SUPPORT BEAM BETWEEN LBL9 €“ RBL9 (C-CHECK RO 7/5/2021) REMOVED AND REPLACED COCKPIT FLOOR SUPPORT BEAM P/N CC670-34095-1 AT FS280 LBL9 - RBL9 REF DWG NO. CC670-33052 REV -G, CRJ700 SRM51-42-06-001-001-A0
- [SDR SWIA2021070759291](https://openairdocs.org/sdr/SWIA2021070759291.md): Intercostal · corroded · Apr 2, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > *PASSENGER DOOR - INTERCOSTAL DD6 HAS CORROSION, MULTIPLE AREAS. (MARKED) (C-CHECK RO 7/5/2021) REPLACED PASSENGER DOOR INTERCOSTAL MID DD6 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 CRJ-700 SRM 51-42-21-001-001-A01 AND DRAWING 601R31702 REV N. REST
- [SDR SWIA2021070759290](https://openairdocs.org/sdr/SWIA2021070759290.md): Intercostal · corroded · Apr 2, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > *PASSENGER DOOR €“ INTERCOSTAL DD3 HAS CORROSION, MULTIPLE AREAS. (MARKED) (C-CHECK RO 7/5/2021) REPLACED PASSENGER DOOR MID DD3 INTERCOSTAL REF CRJ--700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DRAWING 601R31702 REV N. RESTORED F
- [SDR SWIA2021070759289](https://openairdocs.org/sdr/SWIA2021070759289.md): Former · corroded · Apr 2, 2021 · N612QX · Cndair CL6002C10 · Passenger/Crew Doors
  > *PASSENGER DOOR €“ FORWARD FORMER HAS CORROSION ON INNER WEB, UNDER PANEL 832FL. (MARKED) (C-CHECK RO 7/5/2021) REPLACED PASSENGER FOWARD FORMER WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. RESTORED FINISH. PRESSURE CHECK
- [SDR SWIA2021070759288](https://openairdocs.org/sdr/SWIA2021070759288.md): Slat Track · corroded · Mar 30, 2021 · N612QX · Cndair CL6002C10 · Leading Edge Devices
  > R/H SLAT TRACK 1-2 HAS CORROSION ON LWR SIDE (MARKED WITH RED) (C-CHECK RO 7/5/2021) DAMAGE TO R/H SLAT TRACK 1-2 BLENDED IAW MHI REO 670-57-42-1059 REV -- DATED 2021-04-27. ALL STEPS COMPLIED WITH. OPS CHECK GOOD. RIG CHECK GOOD. COMPLIED WITH 51-900-

Next page: https://openairdocs.org/aircraft/N612QX/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 = 'N612QX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N612QX/reports

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