# Service difficulty reports: N702BR, cancelled Oct 2, 2023

A list on [N702BR, cancelled Oct 2, 2023](https://openairdocs.org/deregistered/N702BR-2023-10-02.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 · 158 reports

- [SDR SWIA202266607](https://openairdocs.org/sdr/SWIA202266607.md): None · noisy · Oct 9, 2022 · N702BR · Cndair CL6002B19 · Doors
  > THROUGH 15,000 UNTIL APPROXIMATELY FL210, A LOUD WHISTLING/SQUEALING NOISE WAS HEARD IN THE FLIGHT DECK AND CABIN. FA STATES SHE WAS PRETTY POSITIVE THAT THE NOISE WAS ORIGINATING FROM THE MAIN CABIN DOOR. NOISE WAS MUFFLED WHEN SHE CLOSED THE MCD CURTAIN AND
- [SDR SWIA202266485](https://openairdocs.org/sdr/SWIA202266485.md): None · gouged · Sep 5, 2022 · N702BR · Cndair CL6002B19 · Doors
  > TRANSFER FROM EAML 983820: REF AML 983236, 2-OFF GOUGE DAMAGE (APROXIMATIVE 0.065€?D & 0.035€?D AT THE EDGE,REF) ON CARGO DOOR OUTER SKIN (DWG. 601R35027; 0.095" +/- 0.002" NOMINAL THK, REF) LOCATED AT UPPER EDGE BETWEEN FS589.00 - FS621.00. (FLIGHT
- [SDR SWIA202162461](https://openairdocs.org/sdr/SWIA202162461.md): None · smoke · Nov 8, 2021 · N702BR · Cndair CL6002B19 · Window/Windshield System
  > SMOKE OFF OFF LEFT WINDSHIELD WAS FOLLOWED BY WINDSHIELD CRACKING. LEFT SIDE. (FLIGHT 4255 - FILED CLOSED) PLEASE REFERENCE AML 776009 PLEASE REFERENCE AML 776106. REMOVED AND REPLACED LEFT WINDSHIELD PER AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220
- [SDR SWIA202161613](https://openairdocs.org/sdr/SWIA202161613.md): None · cracked · Oct 3, 2021 · N702BR · Cndair CL6002B19 · Doors
  > DURING THE INSPECTION OF THE PASSENGER DOOR FITTINGS ON THE FUSELAGE, FOUND THE PASSENGER DOOR STOP BRACKET ON THE FORWARD SIDE OF THE PASSENGER DOOR CUTOUT IN THE FUSELAGE TO BE CRACKED ON THE LOWER SIDE OF THE BRACKET. (FILED CLOSED) REMOVED AND REPLAC
- [SDR SWIA202158379](https://openairdocs.org/sdr/SWIA202158379.md): Flap System · failed · May 24, 2021 · N702BR · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION APPEARED DURING CLIMB OUT 17000', FLAP FAIL AT 0 DEGREES RAN QRH FSI LESS THEN 400 FPM TOUCH DOWN ARE SPEED LESS THEN MAX TIRE SPEED (FLIGHT 4291) COMPLIED WITH AD 2009-06-12/09 FOR TROUBLESHOOTING. FLIGHT LEG 1589 LRU PROBABLES ARE
- [SDR SWIA202155051](https://openairdocs.org/sdr/SWIA202155051.md): Engine · fluctuates · Jan 4, 2021 · N702BR · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > LARGE N1 FLUCTUATIONS AT HIGH POWER SETTINGS AFTER TAKEOFF. ERRATIC FUEL FLOW, POWER FLUCTUATIONS COULD BE FELT. RETURNED TO FIELD. MEL 76-11-1 CAT: C DUE: 14JAN2021. LARGE N1 FLUCTUATIONS AT HIGH POWER SETTINGS AFTER TAKEOFF. ERRATIC FUEL FLOW, POWER FLU
- [SDR SWIA2020080451636](https://openairdocs.org/sdr/SWIA2020080451636.md): Seat Track · corroded · Jul 13, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SMALL SEAT TRACK SEGMENT LOCATED BETWEEN FS559+80 TO FS559+96 AT RBL9 IS CORRODED. REMOVED & REPLACED SMALL SEAT TRACK LOCATED FS559+80 TO FS559+96 WITH NEW STOCK IAW REO.
- [SDR SWIA2020080451592](https://openairdocs.org/sdr/SWIA2020080451592.md): Seat Track · corroded · Jul 13, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 2 EACH CABIN SEAT TRACK SEGMENTS LOCATED AT RBL9 AND LBL9 FROM FS559 TO FS559+80 AR CORRODED. (C-CHECK) RO 7/31/2020 REMOVED/FABRICATED AND INSTALLED NEW SEAT TRACK FABRICATED FROM 20276-288-0-0A IAW REO
- [SDR SWIA2020080451635](https://openairdocs.org/sdr/SWIA2020080451635.md): Floor Support · corroded · Jul 6, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL IN CARGO BAY HAS 4 AREAS OF CORROSION AROUND NUT PLATES, LOCATED FROM FS559+112 TO FS621.00. REMOVED AND REPLACED 4 NUTPLATES AT RT FLOOR SILL LOCATED BETWEEN FS559+112 TO FS621.00 IAW SRM. REMOVED PEALED PAINT NO CORROSION FOUND AT THIS TIM
- [SDR SWIA2020080451634](https://openairdocs.org/sdr/SWIA2020080451634.md): Seat Track · corroded · Jul 6, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT LOCATED FROM FS 559+64 TO 559+80 AT RLB27 IS CORRODED. UPON FURTHER INVESTIGATION FOUND SEAT TRACK SEGMENT TO BE LOCATED AT F.S. 559+48 TO F.S. 559+64 RBL 27. REMOVED CORRODED SEAT TRACK SEGMENT IAW AMM. LOCATED, DRILLED AND INSTALLED NE
- [SDR SWIA2020080451605](https://openairdocs.org/sdr/SWIA2020080451605.md): Floorbeam · corroded · Jul 6, 2020 · N702BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT RBL9 HAS A SMALL AREA OF CORROSION AROUND FLOORBOARD NUT PLATE AT FS 589.00. REMOVED AND REPLACED RBL 9 FLOORBEAM IAW SRM, AND GREO.
- [SDR SWIA2020080451581](https://openairdocs.org/sdr/SWIA2020080451581.md): Seat Track · corroded · Jul 6, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > 3 EACH SEAT TRACK SEGMENTS ARE CORRODED IN CARGO BAY AREA, LOCATED BETWEEN FS574.00 TO FS559+80 AT RBL9 AND LBL9 AS MARKED. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED 3 SEAT TRACK IN CARGO BAY AREA BETWEEN F.S.574.00 TO F.S. 599+80RBL9 AND LBL9 IAW CRJ20
- [SDR SWIA2020080451633](https://openairdocs.org/sdr/SWIA2020080451633.md): Seat Track · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER FLOOR SEAT TRACK BETWEEN FS 409 AND FS 409+128 AT LBL 9 IS CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED PASSENGER FLOOR SEAT TRACK BETWEEN F.S. 409 AND F.S. 409+128 AT LBL9 IAW AMM.
- [SDR SWIA2020080451632](https://openairdocs.org/sdr/SWIA2020080451632.md): Seat Track · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER FLOOR SEAT TRACK BETWEEN FS 364 AND FS 409 AT RBL 9 IS CORRODED SEVERAL LOCATIONS. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SERVICEBLE PASSENGER SEAT TRACK BETWEEN F.S. 364 AND F.S. 409 AT RBL 9 IAW AMM
- [SDR SWIA2020080451631](https://openairdocs.org/sdr/SWIA2020080451631.md): Seat Track · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER FLOOR SEAT TRACK BETWEEN FS 364 AND FS 409 AT LBL9 IS CORRODED SEVERAL LOCATIONS. (C-CHECK) RO 7/31/2020 REMOVED FLOOR SEAT TRACK BETWEEN F.S. 364 AND F.S. 409 AT LBL9 IAW CRJ200 AMM. FABRAICATED WITH ALT MATERIAL AND INSTALLED IAW BOMBARDIER RE
- [SDR SWIA2020080451630](https://openairdocs.org/sdr/SWIA2020080451630.md): Fastener · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 349 FLOORBEAM DOUBLER BETWEEN LBL 27 AND LBL 42 HAD CORRODED FASTENERS. REPLACED THE FASTENERS IAW SRM.
- [SDR SWIA2020080451629](https://openairdocs.org/sdr/SWIA2020080451629.md): Seat Track · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER FLOOR SEAT TRACK BETWEEN FS 409+128 AND FS 559 AT RBL9 IS CORRODED SEVERAL LOCATIONS. REMOVED CORRODED FLOOR SEAT TRACK BETWEEN F.S. 409+128 AND F.S. 559 AT RBL 9 IAW AMM. INSTALLED NEWLY FABRICATED SEAT TRACK IAW AMM.
- [SDR SWIA2020080451628](https://openairdocs.org/sdr/SWIA2020080451628.md): Seat Track · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER FLOOR SEAT TRACK BETWEEN FS 409+128 AND FS 559 AT LBL9 WAS CORRODED AT SEVERAL LOCATIONS. REMOVED CORRODED FLOOR SEAT TRACK BETWEEN F.S. 409+128 AND F.S. 559 AT LBL 9 IAW AMM. INSTALLED NEWLY FABRICATED SEAT TRACK IAW AMM.
- [SDR SWIA2020080451606](https://openairdocs.org/sdr/SWIA2020080451606.md): Attach Bracket · cracked · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BS 621.00 REAR PRESSURE BULKHEAD, L/H UPPER INTERCOSTAL ANGLE BETWEEN F.S. 621.00 AND F.S. 625.00 IS CRACKED. (C-CHECK) RO 7/31/2020 REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ-200 SRM.
- [SDR SWIA2020080451604](https://openairdocs.org/sdr/SWIA2020080451604.md): Panel · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL PANEL CORRODED AT 7EA. LOCATIONS BETWEEN FS 409+128 AND FS 559. REPAIRED LH FLOOR SILL PANEL AT 7EACH LOCATIONS IAW REO.
- [SDR SWIA2020080451603](https://openairdocs.org/sdr/SWIA2020080451603.md): Panel · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL PANEL IS CORRODED AT 6EA. LOCATIONS BETWEEN FS 409+128 AND FS 559. REPAIRED RH PRESSURE FLOOR SILL PANEL AT 6EACH LOCATIONS IAW REO.
- [SDR SWIA2020080451584](https://openairdocs.org/sdr/SWIA2020080451584.md): Seat Track · corroded · Jul 3, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER FLOOR SEAT TRACK BETWEEN FS 409 AND FS 409+128 AT RBL 9 IS CORRODED SEVERAL LOCATIONS. REMOVED CORRODED FLOOR SEAT TRACK BETWEEN F.S.409 AND F.S. 409+128 AT RBL 9 IAW CRJ 200 AMM. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK P/N
- [SDR SWIA2020080451627](https://openairdocs.org/sdr/SWIA2020080451627.md): Gusset · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > SERVICE DOOR SURROUND LWR FRAME GUSSET AT FS 349 IS CORRODED. REMOVED AND REPLACED CORRODED GUSSET AT BS 349 SERVICE DOOR WITH NEW SERVICEABLE GUSSET IAW SRM
- [SDR SWIA2020080451626](https://openairdocs.org/sdr/SWIA2020080451626.md): Anchor Fitting · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD ANCHOR FITTING SERRATED PLATE AT FS 310 IS CORRODED. REMOVED AND REPLACED PAX DOOR FWD ANCHOR FITTING AND GUSSET IAW AMM. ADJUSTMENT CHECK GOOD
- [SDR SWIA2020080451625](https://openairdocs.org/sdr/SWIA2020080451625.md): Doubler · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SILL CANNON PLUG DOUBLERS 2EA. ARE BOTH CORRODED BETWEEN FS319 AND FS333. REMOVED AND REPLACED THE DOUBLERS IAW SRM.
- [SDR SWIA2020080451624](https://openairdocs.org/sdr/SWIA2020080451624.md): Angle · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SILL LWR ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR SILL LOWER ANGLE IAW SRM.
- [SDR SWIA2020080451602](https://openairdocs.org/sdr/SWIA2020080451602.md): Trunnion · cracked · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LH MLG TRUNNION HAS AN INDICATION IN EACH FASTENER HOLE (2ND HOLE(1" LONG BY 55%FSH), (3RD HOLE (.1" LONG BY 15% FSH), (MOST AFT INBD HOLE (.15" BY 90% FSH). FAILED NDT INSPECTION. (C-CHECK) RO 7/31/2020 REPAIRED LH MLG TRUNNION 2ND AND 3RD HOLE IAW REO
- [SDR SWIA2020080451601](https://openairdocs.org/sdr/SWIA2020080451601.md): Trunnion · cracked · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RH MLG TRUNNION FASTENER HOLE HAS AN INDICATION.1" LONG BY 55% FSH IN 7TH FASTENER HOLE AFT(MARKED WITH SHARPIE). FAILED NDT INSPECTION. REPAIRED MLG TRUNNION FASTENER HOLE 7TH FASTENER HOLE AFT IAW REO.
- [SDR SWIA2020080451600](https://openairdocs.org/sdr/SWIA2020080451600.md): Not Reported · damaged · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Structure (General)
  > WHILE PERFORMING SB601R-57-046, FOUND 9TH HOLE FROM FRONT ON R/H SIDE TO BE OVERSIZED. REPAIRED 9TH HOLE FROM FRONT ON RH SIDE IAW REO.
- [SDR SWIA2020080451595](https://openairdocs.org/sdr/SWIA2020080451595.md): Intercostal · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND INTERCOSTAL BETWEEN FS 295 AND FS 310 STGR 14L IS CORRODED. (C-CHECK) RO 7/31/2020 REPLACED PAX DOOR SURROUND INTERCOASTAL BEWEEN FS 295 ABD FS 310 STR 14L IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT C
- [SDR SWIA2020080451593](https://openairdocs.org/sdr/SWIA2020080451593.md): Floor Support · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SILL UPPER ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR SILL UPPER ANGLE IAW CRJ 200 SRM.
- [SDR SWIA2020080451591](https://openairdocs.org/sdr/SWIA2020080451591.md): Gusset · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LWR SURROUND, FWD UPPER GUSSET AT FS 310 IS CORRODED. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED PAX DOOR LWR SURROUND FWD UPPER GUSSET AT F.S.310 IAW CRJ 200 SRM.
- [SDR SWIA2020080451588](https://openairdocs.org/sdr/SWIA2020080451588.md): Floor Support · corroded · Jul 2, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IS CORRODED JUST FWD OF SERVICE DOOR CUTOUT AT FS 319.70. REMOVED AND REPLACED R/H FLOOR SILL P/N 601R-31148-79 IAW SRM.
- [SDR SWIA2020080451599](https://openairdocs.org/sdr/SWIA2020080451599.md): Bulkhead · chafed · Jun 30, 2020 · N702BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS621 BULKHEAD FORWARD SIDE REPAIR DOUBLERS CHAFED FROM CONTACT WITH SCREWS AT WL103 AT RBL36, RBL27, RBL18, LBL7, LBL9, LBL18, LBL27 WITH DEEPEST CHAFE AT.005" (C-CHECK) RO 7/31/2020 REPAIRED F.S 621 BULKHEAD FORWARD SIDE REPAIR DOUBLER CHAFES IAW REO.
- [SDR SWIA2020080451623](https://openairdocs.org/sdr/SWIA2020080451623.md): Seat Track · corroded · Jun 29, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT RAIL BETWEEN BS 409+112 AND 449.85 WAS CORRODED AT SEVERAL PLACES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.
- [SDR SWIA2020080451622](https://openairdocs.org/sdr/SWIA2020080451622.md): Seat Track · corroded · Jun 29, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL BETWEEN F.S. 544.00 AND F.S. 559.00+80 IS CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED LEFT SIDE SEAT RAIL IAW AMM.
- [SDR SWIA2020080451621](https://openairdocs.org/sdr/SWIA2020080451621.md): Seat Track · corroded · Jun 29, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LEFT SIDE SEAT RAILS BETWEEN BS 409.00+112 AND BS 499.00 ARE CORRODED IN SEVERAL PLACES. REPLACED THE SIDEWALL SEAT TRACK IAW AMM.
- [SDR SWIA2020080451620](https://openairdocs.org/sdr/SWIA2020080451620.md): Seat Track · corroded · Jun 29, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL BETWEEN BS 409+16 AND 409+112 WAS CORRODED AT SEVERAL PLACES. REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA2020080451590](https://openairdocs.org/sdr/SWIA2020080451590.md): Seat Track · corroded · Jun 29, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT RAILS BETWEEN F.S. 499.00 AND F.S. 559.00+80 IS CORRODED IN SEVERAL AREAS. REMOVED AND INSTALLED SERVICABLE SEAT TRACK BETWEEN 499.00 AND 559.00+80 IAW AMM, REFERENCE CAMP 21201733 FOR PART FABRICATION
- [SDR SWIA2020080451582](https://openairdocs.org/sdr/SWIA2020080451582.md): Seat Track · corroded · Jun 29, 2020 · N702BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT RAIL BETWEEN F.S. 364.00 AND F.S. 409.00+16 IS CORRODED IN SEVERAL PLACES. (C-CHECK) RO 7/31/2020 REMOVED CORRODED R/H SIDE SEAT RAIL BETWEEN F.S. 364.00 AND F.S. 409.00+16 IAW CRJ 200 AMM. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE SID
- [SDR SWIA2020080451598](https://openairdocs.org/sdr/SWIA2020080451598.md): Angle · cracked · Jun 27, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 RH & LH SIDE OF BL0 VERTICAL POST HAS ONE EACH INDICATION.15" LONG BY 80% FSH IN THE UPPER AFTER RADIUS @ WL69. FAILED NDT INSPECTION. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED FS 409+128 VERTICAL POST AT RH AND LH OF BL0 IAWE CRJ 200 SRM AN
- [SDR SWIA2020080451589](https://openairdocs.org/sdr/SWIA2020080451589.md): Post · cracked · Jun 27, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 RBL18 VERTICAL POST HAS AN INDICATION.13" LONG BY 75% FSH IN THE UPPER AFT RADIUS @ WL69. FAILED NDT INSPECTION. REPAIRED AREA IAW SRM AND REO.
- [SDR SWIA2020080451583](https://openairdocs.org/sdr/SWIA2020080451583.md): Attach Angle · cracked · Jun 27, 2020 · N702BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 280 STGR 3L ATTACH ANGLE IS CRACKED APPROX..500" IN LENGTH. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED ATTACH ANGLE AT FS 280 STRG 3L IAW CRJ-200 SRM
- [SDR SWIA2020080451587](https://openairdocs.org/sdr/SWIA2020080451587.md): Track · gouged · Jun 26, 2020 · N702BR · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK AT FS 574 IS GOUGED 1.5" IN LENGTH,.156" IN WIDTH, AND APPROX..075" IN DEPTH. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED CARGO DOOR FWD TRACK IAW CRJ 200 SRM NO DEFECTS NOTED OPS TEST GOOD
- [SDR SWIA2020080451586](https://openairdocs.org/sdr/SWIA2020080451586.md): Channel · chafed · Jun 26, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SURROUND STRUCTURE FWD UPPER WEB CHANNEL AT FS 574 IS CHAFED APPROX..750" IN LENGTH,.062" IN WIDTH, AND.030" IN DEPTH. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED CARGO DOOR SURROUND STRUCTURE UPPER WEB CHANNEL IAW SRM.
- [SDR SWIA2020080451585](https://openairdocs.org/sdr/SWIA2020080451585.md): Channel · cracked · Jun 26, 2020 · N702BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SURROUND STRUCTURE, FWD/LWR C-CHANNEL IS CRACKED 1" IN LENGTH. REMOVED DAMAGED CARGO DOOR SURROUND STRUCTURE FWD/LWR C-CHANNEL, LOCATED AND DRILLED NEW C-CHANNEL, AND INSTALLED IAW CRJ200 SRM
- [SDR SWIA2020080451619](https://openairdocs.org/sdr/SWIA2020080451619.md): Nut · corroded · Jun 25, 2020 · N702BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT OTBD FLAP CENTER HINGE BOX FWD NUT WAS CORRODED. REMOVED AND INSTALLED A NEW NUT IAW AMM.
- [SDR SWIA2020080451618](https://openairdocs.org/sdr/SWIA2020080451618.md): Bolt · corroded · Jun 25, 2020 · N702BR · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT SPOILERON INBD HINGE HARDWARE WAS CORRODED. REPLACED THE HARDWARE IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA2020080451617](https://openairdocs.org/sdr/SWIA2020080451617.md): Nut · corroded · Jun 25, 2020 · N702BR · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT FLIGHT SPOILER INBD AND OTBD HINGE HARDWARE WAS CORRODED. REPLACED HARDWARE IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA2020080451616](https://openairdocs.org/sdr/SWIA2020080451616.md): Bolt · corroded · Jun 25, 2020 · N702BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP INBD FWD FLAP FITTING TWO FWD HARDWARE WAS CORRODED. REMOVED HARDWARE IAW AMM AND INSTALLED NEW HARDWARE IAW AMM.

Next page: https://openairdocs.org/deregistered/N702BR-2023-10-02/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 = 'N702BR' AND deregistration_id = 'N702BR-2023-10-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N702BR-2023-10-02/reports

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