# Service difficulty reports: N675BR

A list on [N675BR](https://openairdocs.org/aircraft/N675BR.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 2 · 72 reports

- [SDR SWIA20190405670](https://openairdocs.org/sdr/SWIA20190405670.md): Reservoir · malfunctioned · Mar 28, 2019 · N675BR · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > GOT GEAR DISAGREE WARNING MESSAGE WHEN LOWERING THE GEAR. LEFT MAIN SHOWED RED. APPROX 30 SECONDS LATER, MESSAGE CLEARED WITH A GREEN INDICATION ON THE LEFT MAIN GEAR. (FLT#3521) REMOVED AND REPLACED SYSTEM 3 HYDRAULIC RESERVOIR, NLG PRIORITY VALVE AND RESIS
- [SDR SWIA2019032645660](https://openairdocs.org/sdr/SWIA2019032645660.md): Hydraulic System · contaminated · Mar 26, 2019 · N675BR · Cndair CL6002B19 · Hydraulic System, Main
  > LEFT MAIN LANDING GEAR DID NOT SHOW DOWN ON FINAL. DURING GO AROUND WE GOT ALL THREE WHEELS TO INDICATE DOWN. (FLT#7363) CLOSED FOUND AIR IN SYSTEM NR 3 HYDRAULIC SYSTEM BLED NR 3 HYDRAULIC SYSTEM IAW AMM. PERFORMED MULTIPLE GEAR SWINGS ON EACH NR 3 HYD PUMP A
- [SDR SWIA2018101145133](https://openairdocs.org/sdr/SWIA2018101145133.md): Strut · low · Oct 11, 2018 · N675BR · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING MESSAGE, NOSEGEAR DID NOT RETRACT, WOW CAUTION, WOW INPUT STATUS, NOSEWHEEL STEERING INOP CAUTION MESSAGE. (FLT 4291) CLOSED SERVICED NLG SHOCK STRUT IAW TASK CARD. PERFORMED NLG SWING IAW AMM. ALL OPS CHECKS GOOD.
- [SDR SWIA2018040544472](https://openairdocs.org/sdr/SWIA2018040544472.md): Mount · corroded · Mar 26, 2018 · N675BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT INBD WARDROBE MOUNT PLATE COMMON TO FLOOR STRUCTURE IS CORRODED. AFT MOUNTING PLATE WAS REMOVED AND REPLACED IAW REO.
- [SDR SWIA201844471](https://openairdocs.org/sdr/SWIA201844471.md): Mount · corroded · Mar 26, 2018 · N675BR · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FWD AND AFT INBD GALLEY MOUNT PLATES COMMON TO FLOOR STRUCTURE ARE CORRODED. BOTH MOUNTING PLATES WERE REMOVED AND REPLCED IAW SRM.
- [SDR SWIA2018040544470](https://openairdocs.org/sdr/SWIA2018040544470.md): Cargo Track · corroded · Mar 14, 2018 · N675BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 CARGO TRACK, BS 559 + 90 TO 559 + 96 HAS CORROSION. REMOVED, AND REPLACED THE CARGO TRACK IAW REO AND AMM.
- [SDR SWIA2018040544469](https://openairdocs.org/sdr/SWIA2018040544469.md): Cargo Track · corroded · Mar 14, 2018 · N675BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 CARGO TRACK, BS 559 + 112 HAS CORROSION. REMOVED AND REPLACED THE CARGO TRACK IAW SRM.
- [SDR SWIA2018040544468](https://openairdocs.org/sdr/SWIA2018040544468.md): Cargo Track · corroded · Mar 14, 2018 · N675BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 CARGO TRACK, BS 559 + 112 HAS CORROSION. REMOVED AND REPLACED THE CARGO TRACK IAW SRM AND AMM.
- [SDR SWIA201844467](https://openairdocs.org/sdr/SWIA201844467.md): Cargo Track · corroded · Mar 14, 2018 · N675BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK HAS CORROSION, BS 615, LBL 9. REPLACED THE CARGO TRACK IAW AMM.
- [SDR SWIA2018040544466](https://openairdocs.org/sdr/SWIA2018040544466.md): Floor Support · corroded · Mar 14, 2018 · N675BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CARGO FLOOR SUPPORT, BS 559+84 TO 559+114 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM. OPS CHECKED GOOD.
- [SDR SWIA2018040544465](https://openairdocs.org/sdr/SWIA2018040544465.md): Skin · dented · Mar 13, 2018 · N675BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT BS 654.5, BETWEEN STRINGERS 20L AND 21L DENTED. REPAIRED THE SKIN IAW REO.
- [SDR SWIA201844464](https://openairdocs.org/sdr/SWIA201844464.md): Vane · chafed · Mar 10, 2018 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE SKIN CHAFED ON THE INBD SIDE. INSTALLED A NEW FLAP VANE, INBD CAP IAW SRM AND REO.
- [SDR SWIA201844463](https://openairdocs.org/sdr/SWIA201844463.md): Door Sill · corroded · Mar 9, 2018 · N675BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE SERVICE DOOR SILL PLATE AFTER REMOVAL. REPLACED THE DOOR SILL IAW SRM.
- [SDR SWIA201642034](https://openairdocs.org/sdr/SWIA201642034.md): Skin · dented · Mar 23, 2016 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP DENTED. REMOVED AND INSTALLED NEW SERVICEABLE RT FLAP AT WS 80.50 AND WS 127.25 IAW AMM.
- [SDR SWIA201642033](https://openairdocs.org/sdr/SWIA201642033.md): Skin · dented · Mar 23, 2016 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP DENTED. REMOVED AND INSTALLED NEW SERVICEABLE LT FLAP AT WS 80.50 AND 127.25 IAW AMM.
- [SDR SWIA201642038](https://openairdocs.org/sdr/SWIA201642038.md): Floorbeam · corroded · Mar 21, 2016 · N675BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE AT BS 349.5 BETWEEN LBL 41.0, LBL 30.0 HAS EVIDENCE OF CORROSION. REPLACED CORRODED FLOOR SUPPORT ANGLE, PN 601R38673-43 WITH NEW PART IAW SRM.
- [SDR SWIA201642037](https://openairdocs.org/sdr/SWIA201642037.md): Angle · corroded · Mar 19, 2016 · N675BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL LOWER ANGLE EVIDENCE OF CORROSION. REPLACED CORRODED ANGLE WITH NEW ANGLE, IAW SRM.
- [SDR SWIA201642036](https://openairdocs.org/sdr/SWIA201642036.md): Vane · chafed · Mar 19, 2016 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE L/E INBD CAP CHAFED. REMOVED AND INSTALLED NEW RT INBD FLAP VANE L/E INBD CAP, PN: 601R14303-54 IAW SRM.
- [SDR SWIA201642035](https://openairdocs.org/sdr/SWIA201642035.md): Structure · chafed · Mar 17, 2016 · N675BR · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LOWER L/E FIXED INBD SECTION HAS CHAFING. REMOVED AND INSTALLED NEW PANEL ON LT AILERON LOWER L/E INBD FIXED POSITION IAW SRM.
- [SDR SWIA201642032](https://openairdocs.org/sdr/SWIA201642032.md): Skin · chafed · Mar 17, 2016 · N675BR · Cndair CL6002B19 · Ailerons
  > CHAFING ON LT WING AILERON PANEL 599AB. R & R. LT WING AILERON PANEL.
- [SDR SWIA201437928](https://openairdocs.org/sdr/SWIA201437928.md): Bearing · galled · May 29, 2014 · N675BR · Cndair CL6002B19 · Engine Mount Section
  > RIGHT ENGINE FWD MOUNT YOKE HAS STIFF BEARINGS AND GALLED. REMOVED RT ENGINE FWD MOUNT YOKE AND REPLACED WITH A SERVICEABLE FWD MOUNT YOKE IAW AMM.
- [SDR SWIA201437927](https://openairdocs.org/sdr/SWIA201437927.md): Bushing · galled · May 29, 2014 · N675BR · Cndair CL6002B19 · Engine Mount Section
  > RIGHT ENGINE FWD MOUNT LINK AND CLAMP-UP BUSHING GALLED. REMOVED RT ENGINE FWD MOUNT LINK AND CLAMP-UP BUSHING AND REPLACED WITH A SERVICEABLE LINK AND CLAMP-UP BUSHING IAW AMM.
- [SDR SWIA201437926](https://openairdocs.org/sdr/SWIA201437926.md): Housing · galled · May 29, 2014 · N675BR · Cndair CL6002B19 · Engine Mount Section
  > RIGHT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING HAS GALLEING, SERVICE REMOVED RT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING AND REPLACED WITH A SERVICEABLE SPHERICAL BUSHING HOUSING IAW AMM.
- [SDR SWIA201437925](https://openairdocs.org/sdr/SWIA201437925.md): Bolt · galled · May 29, 2014 · N675BR · Cndair CL6002B19 · Engine Mount Section
  > RT ENGINE FWD YOKE MOUNT PYLON UPPER AND LOWER BOLTS HAVE DEEP SCRATCHES AND GALLING, SERVICE REMOVED RT ENGINE FWD YOKE MOUNT PYLON UPPER AND LOWER BOLTS AND REPLACED WITH A SERVICEABLE UPPER AND LOWER BOLTS IAW AMM.
- [SDR SWIA201437717](https://openairdocs.org/sdr/SWIA201437717.md): Lamp · inoperative · May 23, 2014 · N675BR · Cndair CL6002B19 · Emergency Lighting
  > RIGHT NR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.
- [SDR SWIA201436862](https://openairdocs.org/sdr/SWIA201436862.md): Floor Support · corroded · Mar 18, 2014 · N675BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON CARGO BAY FLOOR SUPPORT CAP FROM BS 559+112 - 621 AT LBL 27. C-CHECK, REPLACED CARGO BAY FLOOR SUPPORT IAW REO AND SRM.
- [SDR SWIA201436861](https://openairdocs.org/sdr/SWIA201436861.md): Floor Support · corroded · Mar 18, 2014 · N675BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON CARGO BAY FLOOR SUPPORT FROM BS 559+112 - 621 AT LBL 9. C-CHECK, REPLACED CARGO BAY FLOOR SUPPORT 9 IAW REO AND SRM.
- [SDR SWIA201436864](https://openairdocs.org/sdr/SWIA201436864.md): Intercostal · cracked · Mar 16, 2014 · N675BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT LBL 36.20, AFT SIDE OF PRESSURE BULKHEAD FS 621, BELOW ENGINE BOX BEAM, IS CRACKED. C-CHECK, INSTALLED INTERCOSTAL, IAW SRM.
- [SDR SWIA201436863](https://openairdocs.org/sdr/SWIA201436863.md): Vane · chafed · Mar 16, 2014 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE MID-SECTION CHAFED. C-CHECK, INSTALLED NEW FLAP VANE IAW SRM.
- [SDR SWIA201436867](https://openairdocs.org/sdr/SWIA201436867.md): Skin · corroded · Mar 15, 2014 · N675BR · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK ACCESS ORIFICE 640BB HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION IAW REO.
- [SDR SWIA201436866](https://openairdocs.org/sdr/SWIA201436866.md): Skin · corroded · Mar 15, 2014 · N675BR · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK ACCESS 540BB ORIFICE HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION FROM LT LOWER WING PLANK ACCESS ORIFICE IAW REO.
- [SDR SWIA201436865](https://openairdocs.org/sdr/SWIA201436865.md): Skin · corroded · Mar 15, 2014 · N675BR · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK ACCESS PANEL 510AB ORIFICE HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION FROM LT LOWER WING PLANK ACCESS PANEL ORIFICE 510AB IAW REO.
- [SDR SWIA201436876](https://openairdocs.org/sdr/SWIA201436876.md): Skin · chafed · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Landing Gear Doors
  > LEFT MLG DOOR HAS A CHAFE ON THE INTERNAL SKIN AT THE DOOR L/E. C-CHECK, REPAIRED CHAFED AREA OF LT MLG DOOR REO.
- [SDR SWIA201436875](https://openairdocs.org/sdr/SWIA201436875.md): Skin · chafed · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Ailerons
  > LEFT AILERON UPPER L/E IS CHAFED FROM OTBD EDGE IN ABOUT.3333 OF L/E. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201436874](https://openairdocs.org/sdr/SWIA201436874.md): Vane · chafed · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE L/E CENTER BUMPER CONTACT POINT IS CHAFED. C-CHECK, INSTALLED NEW LT INBD FLAP VANE CAP MID SECTON IAW SRM.
- [SDR SWIA201436873](https://openairdocs.org/sdr/SWIA201436873.md): Vane · chafed · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE L/E OTBD BUMPER CONTACT POINT IS CHAFED. C-CHECK, INSTALLED NEW RT INBD FLAP, OTBD VANE CAP IAW SRM.
- [SDR SWIA201436872](https://openairdocs.org/sdr/SWIA201436872.md): Vane · chafed · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE L/E OTBD BUMPER CONTACT POINT IS CHAFED. C-CHECK, REPLACED LT FLAP VANE L/E SKIN IAW SRM.
- [SDR SWIA201436871](https://openairdocs.org/sdr/SWIA201436871.md): Channel · cracked · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK NOTED AT BS 409+128 VERTICAL POST, LBL 18 OTBD C-CHANNEL, AFT RADIUS. C-CHECK, REPLACED CHANNEL IAW SRM AND REO.
- [SDR SWIA201436870](https://openairdocs.org/sdr/SWIA201436870.md): Floorbeam · cracked · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM AT LBL 9 INBD AND OTBD ANGLES ARE CRACKED. C-CHECK, REPLACED CRACKED INBD AND OTBD ANGLES IAW SRM.
- [SDR SWIA201436869](https://openairdocs.org/sdr/SWIA201436869.md): Floorbeam · cracked · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM AT RBL 9 OTBD AND INBD ANGLES ARE CRACKED. C-CHECK, REPLACED CRACKED ANGLES AT FS 280 FLOORBEAM IAW SRM.
- [SDR SWIA201436868](https://openairdocs.org/sdr/SWIA201436868.md): Floorbeam · cracked · Mar 13, 2014 · N675BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM RT LOWER RADIUS CRACKED AT RBL 11. C-CHECK, REPLACED DAMAGED FLOORBEAM RADIUS SECTION IAW REO.
- [SDR SWIA201333316](https://openairdocs.org/sdr/SWIA201333316.md): Light · inoperative · Apr 26, 2013 · N675BR · Cndair CL6002B19 · Emergency Lighting
  > FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 7394) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201333317](https://openairdocs.org/sdr/SWIA201333317.md): Light · inoperative · Apr 23, 2013 · N675BR · Cndair CL6002B19 · Emergency Lighting
  > REAR CEILING EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4764) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332674](https://openairdocs.org/sdr/SWIA201332674.md): Fixture · inoperative · Jan 26, 2013 · N675BR · Cndair CL6002B19 · Emergency Lighting
  > SIDEWALL LIGHTS AT ROW 3 A/B DO NOT ILLUMINATE. (C-CHECK) REPLACED LIGHT FIXTURE AT ROW 2 AND 3 A/B IAW AMM.
- [SDR SWIA201232230](https://openairdocs.org/sdr/SWIA201232230.md): Selector Valve · failed · Nov 24, 2012 · N675BR · Cndair CL6002B19 · Landing Gear Selector
  > GEAR DISAGREE WARNING AND NOSE DOOR WARNINGS, AFTER QRH, GEAR CAME DOWN NORMALLY. (FLT 4659) REPLACED NOSE GEAR SELECTOR VALVE. P/N: 750006000 S/N ON: 0465T S/N OFF: 1434
- [SDR SWIA201232182](https://openairdocs.org/sdr/SWIA201232182.md): Fan · malfunctioned · Nov 16, 2012 · N675BR · Cndair CL6002B19 · Air Distribution Fan
  > ON APPROACH TO LAND, SMELLED STRONG BURNING ODOR IN COCKPIT DISCOVERED CIRCUIT BREAKER GALLEY FAN TRIPPED. (FLT 4732) REPLACED GALLEY FAN IAW AMM. P/N ON: AE0607D00 P/N OFF: AE0405A03 S/N ON: L0323 S/N OFF: 260
- [SDR SWIA201230118](https://openairdocs.org/sdr/SWIA201230118.md): Bulkhead · cracked · Mar 21, 2012 · N675BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > (C-CHECK) CRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD. REPAIRED CRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD.
- [SDR SWIA201126368](https://openairdocs.org/sdr/SWIA201126368.md): Adc · malfunctioned · May 19, 2011 · N675BR · Cndair CL6002B19 · Air Data Computer
  > FIRST OFFICER'S ALTITUDE FLUCTUATES +/- 100' IN LEVEL FLIGHT; VSI FLUCTUATES +/- 1000'/MIN IN LIGHT TURBULENCE. (FLT 1361) REPLACED NR 2 AIR DATA COMPUTER. P/N ON GMT4190-020 S/N OFF 1220
- [SDR COMA2010062350133](https://openairdocs.org/sdr/COMA2010062350133.md): Skin · dented · Jun 23, 2010 · N675BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > A 3.5 INCH LONG DENT FOUND BELOW CARGO DOOR SCUFF PLATE, FS 574.00, STRINGER 18L-19L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-3701.
- [SDR COMA2010061850131](https://openairdocs.org/sdr/COMA2010061850131.md): Bulkhead · cracked · Jun 17, 2010 · N675BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AT FS 621.00 (REAR PRESSURE BULKHEAD) THE AREA AROUND THE CARGO DOOR LINTEL FITTING IS CRACKED. REPAIRED IAW REO 601R-53-61-1230.

Next page: https://openairdocs.org/aircraft/N675BR/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 = 'N675BR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N675BR/reports

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