# Service difficulty reports: N701BR

A list on [N701BR](https://openairdocs.org/aircraft/N701BR.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 4 · 165 reports

- [SDR SWIA2023072401](https://openairdocs.org/sdr/SWIA2023072401.md): Unknown · dented · Jul 20, 2023 · N701BR · Cndair CL6002B19 · Fuselage Structure (General)
  > TRANSFER FROM EAML 1176225: EXT AIR START PANEL DOOR DISCOVERED OPEN ON TAXI IN, SEE EAML 1175774.TWO (2) DENTS (1.20" L X 1.00" W X 0.0375" DEEP & 2.10" L X 1.70" W X 0.0725" DEEP) TO LOWER FUSELAGE SKIN (DWG 601R35005, AL ALLOY CLAD 2024-T42, 0.036"+/-0.002
- [SDR SWIA2023072101](https://openairdocs.org/sdr/SWIA2023072101.md): Unknown · dented · Jul 20, 2023 · N701BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1176225: EXT AIR START PANEL DOOR DISCOVERED OPEN ON TAXI IN, SEE EAML 1175774.TWO (2) DENTS (1.20" L X 1.00" W X 0.0375" DEEP & 2.10" L X 1.70" W X 0.0725" DEEP) TO LOWER FUSELAGE SKIN (DWG 601R35005, AL ALLOY CLAD 2024-T42, 0.036"+/-0.002
- [SDR SWIA202265990](https://openairdocs.org/sdr/SWIA202265990.md): None · failed · Jul 10, 2022 · N701BR · Cndair CL6002B19 · Landing Gear Door Actuator
  > WHILE CONFIGURING FOR LANDING AND SELECTING GEAR DOWN RECEIVED €˜GEAR DISAGREE€™ WARNING MESSAGE. RAN QRH FOR GEAR DISAGREEMENT MESSAGE CLEARED AND CONFIRMED GEAR DOWN AND LOCKED. (FLIGHT 5310 - FILED CLOSED) TROUBLESHOT GEAR DISAGREE MESSAGE IN REF TO
- [SDR SWIA202264579](https://openairdocs.org/sdr/SWIA202264579.md): None · none · Feb 21, 2022 · N701BR · Cndair CL6002B19 · Landing Gear System
  > ON APPROACH, AFTER SELECTING LANDING GEAR DOWN, GEAR DISAGREE WARNING, WITH NOSE WHEEL INDICATING DOWN AND GREEN, WITH BOTH MAINS RED. SIMULTANEOUSLY, HYD 3 LOPRESS CAUTION POPULATED. INITIATED MISSED APPROACH. DURING INITIAL CLIMB BOTH MAINS CHANGED TO INDICA
- [SDR SWIA2021073059791](https://openairdocs.org/sdr/SWIA2021073059791.md): Skin · cracked · Jul 25, 2021 · N701BR · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE SKIN AT WS 199.0 HAS A 2.25 INCH VERTICAL CRACK. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 WILL BE REQUIRED. REFERENCE CP 23174513 FOR ORIGINAL WRITE UP. (FILED CLOSED) REPLACED R/H WING LEADING EDGE SKIN IN REFE
- [SDR SWIA202157105](https://openairdocs.org/sdr/SWIA202157105.md): Window · cracked · Mar 26, 2021 · N701BR · Cndair CL6002B19 · Flight Compartment Windows
  > CAPTAIN WINDOW CRACKED ON CLIMB OUT REMOVED AND REPLACED LH SIDE WINDOW IN REF TO AMM 56-12-01, OPS AND LEAK CHECK GOOD AT THIS TIME. / PLEASE REFERENCE AML 606661 PLEASE REFERENCE AML 606670
- [SDR SWIA202155508](https://openairdocs.org/sdr/SWIA202155508.md): Servo · overserviced · Jan 19, 2021 · N701BR · Cndair CL6002B19 · Flight Control System
  > FIRST OFFICER LEG, ON FINAL APPROACH AFTER DISCONNECTING AUTOPILOT, FLIGHT CONTROLS LOCKED UP AND FO HAD TO APPLY FAIRLY STRONG FORCE TO GET PITCH MOVEMENT OF YOKE TO UNLOCK. THEN TO MAKE ROLL ADJUSTMENTS IN FLIGHT, HAD TO APPLY SIMILAR FORCE TO UNLOCK ROLL M
- [SDR SWIA202055493](https://openairdocs.org/sdr/SWIA202055493.md): Crossbeam · corroded · Dec 28, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Structure
  > CROSSBEAM CAP STRIP AT FS 589.00, BETWEEN LBL 9.0 AND LBL 27.00 IS CORRODED AROUND NUTPLATES AND THE NUTPLATE ATTACHING RIVETS AND SCORED ACROSS THE CENTER FROM LBL 9.00 TO LBL 27.00. C-CHECK RO 1/16/2021. COMPLIED WITH REMOVAL AND REPLACEMENT OF CROSSBEAM C
- [SDR SWIA202055507](https://openairdocs.org/sdr/SWIA202055507.md): Stiffener · cracked · Dec 16, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE WORKING F.S.621 BULKHEAD REPAIR FOUND STIFFENER OUTBOARD OF LBL 36 JUST ABOVE FLOOR LEVEL IN AFT SIDE OF BULKHEAD CRACKED. C-CHECK RO 1/16/2021. INSTALLED STIFFNER P/N 601R36008-51 COMMON TO AFT BULKHEAD AT FS 621 LBL 36, IAW CRJ-200 SRM 51-42-06 REV 3
- [SDR SWIA202055506](https://openairdocs.org/sdr/SWIA202055506.md): Trunnion · out of tolerance · Dec 14, 2020 · N701BR · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > FOUND INDICATION RT MLG TRUNNION 1ST HOLE AFT OF STRAP 55% FSH.25 UP TRUNNION FAILS NDT. C-CHECK RO 1/16/2021. PERFORMED REPAIR, IAW REO 601R-57-21-3386 REV- DATED 2020-12-30. M377 AND MAJOR REPAIR TASK CARD ATTACHED NO WEIGHT CHANGE, REFERENCE CONTINUATIO
- [SDR SWIA202055505](https://openairdocs.org/sdr/SWIA202055505.md): Trunnion · out of tolerance · Dec 14, 2020 · N701BR · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > FOUND INDICATION LT MLG TRUNNION 3RD HOLE FROM FRONT OF STRAP 60% FSH.5 UP TRUNNION FAILS NDT. C-CHECK RO 1/16/2021. PERFORMED REPAIR OF LT MLG TRUNNION, IAW REO 601R-57-21-3384 REV - DATED 2020-12-30. FORM M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY.
- [SDR SWIA202055504](https://openairdocs.org/sdr/SWIA202055504.md): Trunnion · damaged · Dec 14, 2020 · N701BR · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RT TRUNNION HAS ONE OVERSIZE HOLE AT AFT HOLE ON STRAP. C-CHECK RO 1/16/2021. PERFORMED REPAIR, IAW REO 601R-57-21-3386 REV - DATED 2020-12-30. TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. NO WEIGHT AND BALANCE CHANGE.
- [SDR SWIA202055497](https://openairdocs.org/sdr/SWIA202055497.md): Trunnion · failed · Dec 14, 2020 · N701BR · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > FOUND INDICATION LT MLG TRUNNION AFT HOLE IN STRAP 60% FSH.5 UP TRUNNION FAILS NDT. C-CHECK RO 1/16/2021. PERFORMED REPAIR IAW REO 601R-57-21-3384 REV - DATED 2020-12-30. TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. WEIGHT AND BALANCE NOT AFE
- [SDR SWIA202055530](https://openairdocs.org/sdr/SWIA202055530.md): Floorbeam · corroded · Dec 3, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 349 RBL 9 TO RBL 27 IS CORRODED. C-CHECK RO 1/16/2021. FOUND CORROSION ON FS 349 RBL 9 TO RBL 27 TO ONLY BE ON FASTENERS. REMOVED AND REPLACED FASTENERS, IAW CRJ200 SRM 51-42-13. REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202055529](https://openairdocs.org/sdr/SWIA202055529.md): Floorbeam · corroded · Dec 3, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 349 LBL 27 TO LBL 9 IS CORRODED. C-CHECK RO 1/16/2021. UPON EVAL FOUND TO ONLY BE CORROSION ON FASTENERS. REMOVED AND REPLACED CORRODED FASTENERS AND NUTPLATES ON LBL 9 FS 349, IAW CRJ 200 SRM 51-42-13 AND 51-42-15. REFERENCE CONTINUE CARD FOR DETAILS O
- [SDR SWIA202055528](https://openairdocs.org/sdr/SWIA202055528.md): Floorbeam · corroded · Dec 3, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 349 LT FLOOR SILL TO LBL 27 IS CORRODED. C-CHECK RO 1/16/2021. FASTENERS AND NUTPLATES WERE FOUND TO BE CORRODED. REMOVED AND REPLACED WITH SERVICABLE HARDWARE, IAW CRJ 200 SRM 51-42-10.
- [SDR SWIA202055515](https://openairdocs.org/sdr/SWIA202055515.md): Floorbeam · cracked · Dec 3, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 LBL 9 INBOARD CLIP AND RBL 9 OUTBOARD CLIP ARE CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED TWO EACH CLIPS LBL 9 INBOARD AND RBL OUTBOARD AT FS 280, IAW CRJ 200 SRM 51-24-36, 51-25-21, 51-25-06 AND 51-42-21 MATERIAL TYPE USED PER REO 601R-53-11
- [SDR SWIA202055503](https://openairdocs.org/sdr/SWIA202055503.md): Not Reported · corroded · Dec 3, 2020 · N701BR · Cndair CL6002B19 · Fuselage Structure (General)
  > LBL 9 BETWEEN FS 409+128 AND FS 424 HAS AREAS OF CORROSION. C-CHECK RO 1/16/2021. RBL 9 WAS CORRECT DISCREPANT AREA. REPAIRED RBL 9 FROM FS 409+128-FS 424, IAW MHIRJ REO 601R-53-41-2829 REV- DATED 2020-12-22. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED
- [SDR SWIA202055491](https://openairdocs.org/sdr/SWIA202055491.md): Floor Support · corroded · Dec 3, 2020 · N701BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THERE ARE SEVERAL AREAS OF CORROSION ON RBL 9 BETWEEN FS 409 AND FS 409+64. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FLOOR CAP CHANNEL AT RBL 9 FS 409 TO FS 409+112, IAW CRJ200 SRM 51-42-06 AND 51-42-21. C/W MAJOR REPAIR TASK CARD AND 377 FORM. NO WEIGHT
- [SDR SWIA202055514](https://openairdocs.org/sdr/SWIA202055514.md): Mount Bracket · cracked · Dec 2, 2020 · N701BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR COVER PLATE AFT MOUNTING BRACKET INBOARD IS CRACKED NEEDS REPLACED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CRACKED MOUNTING BRACKET, IAW CRJ 200 AMM 52-70-04-000-801 AND SRM 51-41-02. OPERATIONS CHECK GOOD AT THIS TIME.
- [SDR SWIA202055527](https://openairdocs.org/sdr/SWIA202055527.md): Floor Support · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 559.00 +96 TO FS 559.00 +112. C-CHECK RO 1/16/2021. RT FLOOR SILL REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE SILL, IAW CRJ-200 SRM 51-40-11. RECEIVED REO 601R-53-51-539 REV P1 DATED 2020-
- [SDR SWIA202055526](https://openairdocs.org/sdr/SWIA202055526.md): Spacer · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Elevator Structure
  > RT ELEVATOR OB HINGE ANTI ROTATION DEVICE HARDWARE AND BONDING WIRE HARDWARE CORRODED. C-CHECK RO 1/16/2021. RT ELEVATOR OUTBOARD HINGE ANTI ROTATION HW AND BONDING WIRE HW REPLACED, IAW CRJ 200 AMM 27-34-01-000-801.
- [SDR SWIA202055525](https://openairdocs.org/sdr/SWIA202055525.md): Bolt · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Elevator Structure
  > RT ELEVATOR PCU MOUNTING HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT ELEVATOR PCU MOUNT HARDWARE, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOOD.
- [SDR SWIA202055524](https://openairdocs.org/sdr/SWIA202055524.md): Bolt · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Elevator Structure
  > LT ELEVATOR OUTBOARD HINGE MOUNTING HARDWARE AND ANTI ROTATION DEVICE HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED LT ELEVATOR OUTBOARD HINGE MOUNTING HARDWARE AND ANTI-ROTATION HARDWARE, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOO
- [SDR SWIA202055523](https://openairdocs.org/sdr/SWIA202055523.md): Mount · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Elevator Structure
  > LT ELEVATOR CENTER HINGE MOUNTING HARDWARE, PCU MOUNTING HARDWARE AND BONDING WIRE HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CORRODED HARDWARE ON FLUTTER DAMPER AND BONDING WIRE, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOOD.
- [SDR SWIA202055522](https://openairdocs.org/sdr/SWIA202055522.md): Floorbeam · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING INSPECTION OF 36M TASK CARD 53-170-500, FOUND CORROSION BETWEEN RBL 9 AND RBL 27 AT 559+80. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FLOOR SUPPORT, IAW CRJ200 SRM 51-42-06 AND 51-42-11.
- [SDR SWIA202055521](https://openairdocs.org/sdr/SWIA202055521.md): Strap · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LT CABIN FLOOR BEAM SUPPORT STRAP AT FS 559.00 BETWEEN LBL 36 AND LBL 44 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. REMOVED DAMAGED SUPPORT STRAP AT FS 559 BETWEEN LBL 36 AND LBL 44 AND INSTALLED NEW SERVICEABLE STRAP, IAW CRJ200-SRM-51-42-06, 51
- [SDR SWIA202055513](https://openairdocs.org/sdr/SWIA202055513.md): Support Bracket · cracked · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD LOWER CAM TRACK SUPPORT BRACKET IS CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CARGO DOOR FWD LOWER CAM TRACK SUPPORT BRACKET, IAW CRJ200 SRM 51-42-06.
- [SDR SWIA202055512](https://openairdocs.org/sdr/SWIA202055512.md): Angle · cracked · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 2 EA INTERCOSTAL CLIPS CRACKED AT FS 484.00 BETWEEN LBL 27 AND LBL 36. C-CHECK RO 1/16/2021. REMOVED AND REPLACED 2 EA INTERCOSTAL CLIPS, IAW CRJ 200 SRM 51-42-21, REFERENCING STEP 14 OF PREVIOUSLY ACCOMPLISHED REO 601R-53-41-059 REV C DATED 2020-03-11 FOR F
- [SDR SWIA202055511](https://openairdocs.org/sdr/SWIA202055511.md): Attach Angle · cracked · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > INTERCOSTAL CLIP CRACKED AT FS 484.00 BETWEEN RBL 27 AND RBL 36. C-CHECK RO 1/16/2021. REMOVED AND REPLACED WITH A SERVICEABLE INTERCOSTAL CLIP AT FS 484.00 BETWEEN RBL 27 AND RBL 36, IAW CRJ 200 SRM 51-42-21.
- [SDR SWIA202055510](https://openairdocs.org/sdr/SWIA202055510.md): Attach Angle · cracked · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > INTERCOSTAL CLIP CRACKED AT FS 484.00 BETWEEN RBL 9 AND RBL 18. REMOVED AND REPLACED UNSERVICEABLE INTERCOSTAL CLIP AT FS 484.00 BETWEEN RBL 9 AND RBL 18 WITH NEW SERVICEABLE INTERCOSTAL CLIP PN: 601R31171-9, IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21.
- [SDR SWIA202055492](https://openairdocs.org/sdr/SWIA202055492.md): Floor Support · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SILL FROM FS 409.00 +128 TO FS 559.00 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. COMPLIED WITH BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 FOR CORROSION REPAIR OF LT FLOOR SILL AT FS 409+128-FS 559. REFERENCE CONTINUATION CARD
- [SDR SWIA202055490](https://openairdocs.org/sdr/SWIA202055490.md): Floor Support · corroded · Dec 1, 2020 · N701BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL FROM FS 409.00 +128 TO FS 559.00 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. REPAIRED RT FLOOR SILL AT FS 409+128 TO FS 559.00, PER REO 601R-53-41-666 REV C DATED 2012-11-06. C/W FORM M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY
- [SDR SWIA202055502](https://openairdocs.org/sdr/SWIA202055502.md): Frame · corroded · Nov 30, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 349.00 FROM STGR 25L TO 25R HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/16/2021. INSTALLED NEW FRAME AT FS 349 FROM STR 25L TO 25R, IAW SRM 51-42-06, 51-42-21. TASK CARD 51-900-1003-SKY COMPLETED. FORM M-337 ATTACHED, NO WEIGHT AND BALANCE CHANGE.
- [SDR SWIA202055487](https://openairdocs.org/sdr/SWIA202055487.md): Intercostal · corroded · Nov 30, 2020 · N701BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 2 EA INTERCOSTALS AT FS 349.00 TO FS 364.00 BETWEEN STRINGERS 26L AND 26R HAVE MULTIPLE SPOT OF CORROSION. C-CHECK RO 1/16/2021. REMOVED AND REPLACED 2 EA INTERCOSTALS AT FS 349 TO FS 364 BETWEEN STR 26L AND 26R, IAW SRM 51-42-06, 51-42-21, 51-40-11. COMPLE
- [SDR SWIA202055509](https://openairdocs.org/sdr/SWIA202055509.md): Shear Tie · cracked · Nov 26, 2020 · N701BR · Cndair CL6002B19 · Passenger/Crew Doors
  > FORWARD UPPER INNER SKIN CORNER ATTACHMENT ANGLES (2 EA) ON PAX DOOR FOUND TO BE CRACKED. C-CHECK RO 1/16/2021. REMOVED, LOCATED AND DRILLED UP NEW SERVICEABLE CORNER ATTACHMENT ANGLES PN 601R38122-1 AND 601R38122-2, IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-40
- [SDR SWIA202055520](https://openairdocs.org/sdr/SWIA202055520.md): Bolt · corroded · Nov 23, 2020 · N701BR · Cndair CL6002B19 · Spoilers
  > LT SPOILERON AND FLIGHT SPOILER PCU LOWER MOUNTING HARDWARE CORRODED. C-CHECK RO 1/16/2021. REPLACED LT SPOILERON AND FLIGHT SPOILER PCU MOUNTING HARDWARE, IAW CRJ 200 AMM 27-62-01-400-801 SUBTASK 27-62-01-420-001 STEPS (2)-(7). REF CONT CARD FOR WORK PERFO
- [SDR SWIA202055519](https://openairdocs.org/sdr/SWIA202055519.md): Washer · corroded · Nov 23, 2020 · N701BR · Cndair CL6002B19 · Spoilers
  > RT SPOILERON AND FLIGHT SPOILER PCU LOWER MOUNTING HARDWARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT FLIGHT SPOILER PCU LOWER MOUNTING HARDWARE, IAW CRJ 200 AMM 27-62-01-000/400-801.
- [SDR SWIA202055518](https://openairdocs.org/sdr/SWIA202055518.md): Control Lever · corroded · Nov 21, 2020 · N701BR · Cndair CL6002B19 · Elevator Control System
  > LT AND RT ELEVATOR CONTROL LEVER ASSEMBLIES HAS EVIDENCE OF CORROSION AT UPPER AND LOWER LEVERS. C-CHECK RO 1/16/2021. REMOVE AND REPLACED LT AND RT ELEVATOR CONTROL LEVER UPPER AND LOWER LEVERS, IAW CRJ-200 AMM 27-31-35-000-801 AND 27-31-35-400-801. OPERAT
- [SDR SWIA202055517](https://openairdocs.org/sdr/SWIA202055517.md): Nut · corroded · Nov 21, 2020 · N701BR · Cndair CL6002B19 · Elevator Structure
  > RT ELEVATOR FLUTTER DAMPERS HAVE CORRODED HARDWARE AT ELEVATOR ATTACH POINTS. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT ELEVATOR FLUTTER DAMPERS CORRODED HARDWARES WITH SERVICEABLE PARTS, IAW CRJ200 AMM 27-34-05-400-801.
- [SDR SWIA202055516](https://openairdocs.org/sdr/SWIA202055516.md): Nut · corroded · Nov 21, 2020 · N701BR · Cndair CL6002B19 · Elevator Structure
  > LT FLUTTER DAMPERS HAVE CORRODED NUTS AT ELEVATOR ATTACH POINTS. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CORRODED HARDWARE ON LT FLUTTER DAMPERS, IAW CRJ200 AMM 27-34-01-400-801. OPERATIONS TEST GOOD.
- [SDR SWIA202055498](https://openairdocs.org/sdr/SWIA202055498.md): Vane · dented · Nov 20, 2020 · N701BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE LEADING EDGE IS DENTED AT WS 140 APPROXIMATELY.250 IN DIAMETER X.030 IN DEEP. C-CHECK RO 1/16/2021. REMOVED AND REPLACED DAMAGED LT INBOARD FLAP VANE LEADING EDGE WITH NEW SERVICEABLE PN 601R14303-43S, IAW CRJ 200 SRM 51-42-13, FORM 33
- [SDR SWIA202055496](https://openairdocs.org/sdr/SWIA202055496.md): Vane · chafed · Nov 20, 2020 · N701BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS 56 APPROXIMATELY 1 IN LONG X.5 IN WIDE X.015 DEEP. C-CHECK RO 1/16/2021. REPLACED THE LT INBOARD FLAP VANE INBOARD LEADING EDGE SKIN, IAW CRJ 200 SRM 51-42-13 AND 51-40-11 REV B DATED 11/25/2020, TASK CARD
- [SDR SWIA202055495](https://openairdocs.org/sdr/SWIA202055495.md): Vane · chafed · Nov 20, 2020 · N701BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS 105 APPROXIMATELY 1 IN LONG X.5 IN WIDE X.015 IN DEEP. C-CHECK RO 1/16/2021. INSTALLED NEW SERVICEABLE LT FLAP VANE LEADING EDGE, IAW CRJ 200 SRM 51-42-13 AND SKYWEST TASK CARD 51-900-1003-SKY. FORM M-337
- [SDR SWIA202055494](https://openairdocs.org/sdr/SWIA202055494.md): Mount Bracket · cracked · Nov 19, 2020 · N701BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > EXTERNAL SERVICES PANEL LOWER MOUNTING BRACKET IS CRACKED. C-CHECK RO 1/16/2021. REPLACED BRACKET, IAW CRJ SRM 51-42-06. REF CONT CARD FOR WORK PREFORMED.
- [SDR SWIA202055531](https://openairdocs.org/sdr/SWIA202055531.md): Skin · corroded · Nov 18, 2020 · N701BR · Cndair CL6002B19 · Ailerons
  > LT AILERON UPPER HINGE LINE SKIN IS CHAFED FROM WS 311 TO WS 353 APPROXIMATELY.25 IN WIDE X.020 IN DEEP. C-CHECK RO 1/16/2021. REMOVED AND REPLACED LT AILERON UPPER LEADING EDGE, IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13. PAINTED TOP COAT, IAW CRJ 200 SRM
- [SDR SWIA202055533](https://openairdocs.org/sdr/SWIA202055533.md): Housing · gouged · Nov 16, 2020 · N701BR · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS BAY DOOR OUTER HANDLE HOUSING IS GOUGED AT (3) LOCATIONS. C-CHECK RO 1/16/2021. MAIN AVIONICS BAY DOOR OUTER HANDLE HOUSING IS GOUGED AT (3) LOCATIONS FOUND TO BE OUT OF LIMITS, IAW REO 601R-52-42-052 REV- DATED 2014-04-25. LOCATED AND DRILLED
- [SDR SWIA202055532](https://openairdocs.org/sdr/SWIA202055532.md): Housing · chafed · Nov 15, 2020 · N701BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR OUTER HANDE HOUSING IS CHAFED. C-CHECK RO 1/16/2021. REMOVED CHAFE DAMAGE FROM PAX DOOR OUTER SKIN AND HANDLE HOUSING ASSEMBLY, IAW CRJ-200 SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR, IAW REO 601R-52-11-2844 REV-- DATED 2020-12-11
- [SDR SWIA202055489](https://openairdocs.org/sdr/SWIA202055489.md): Skin · dented · Nov 15, 2020 · N701BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORWARD AND AFT, UPPER INNER SKIN CORNERS ARE DENTED WITH DAMAGED FASTENERS. C-CHECK RO 1/16/2021. REMOVED AND REPLACED PAX DOOR FWD AND AFT UPPER INNER SKIN CORNERS WITH NEW SERVICEABLE PARTS, IAW SRM 51-42-06, 51-42-13,51-40-11. TASK CARD 51-900-
- [SDR SWIA202055488](https://openairdocs.org/sdr/SWIA202055488.md): Housing · chafed · Nov 15, 2020 · N701BR · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR HANDLE HOUSING IS CHAFED AT THE FORWARD UPPER EDGE. C-CHECK RO 1/16/2021. CARGO DOOR HANDLE HOUSING IS OUT OF ALLOWABLE LIMITS, IAW REO 601R-52-31-086 REV- DATED 05-NOV-07. REPLACED CARGO DOOR HANDLE HOUSING, IAW CRJ-700 SRM 51-42-21 INSTALLED NE

Next page: https://openairdocs.org/aircraft/N701BR/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 = 'N701BR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N701BR/reports

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