# Service difficulty reports: N652BR, cancelled Nov 3, 2023

A list on [N652BR, cancelled Nov 3, 2023](https://openairdocs.org/deregistered/N652BR-2023-11-03.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 · 155 reports

- [SDR SWIA202266736](https://openairdocs.org/sdr/SWIA202266736.md): None · failed · Nov 4, 2022 · N652BR · Cndair CL6002B19 · Landing Gear Door Actuator
  > D:GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR UP ABOVE SPEED 200KTS. GEAR RETRACTION SPEED LIMIT EXCEEDED. / C: MEL 32-30-1 / CAT A DUE WITHIN 1 FLIGHT DAY / NOTE: MX ACTION CW AND CAT II DOWNGRADED / GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR U
- [SDR SWIA2021091561081](https://openairdocs.org/sdr/SWIA2021091561081.md): A/C Pack · failed · Sep 14, 2021 · N652BR · Cndair CL6002B19 · Cabin Cooling System
  > WHILE CLIMBING THROUGH 23000 FT RIGHT PACK TURNED OFF. RAN CHECKLISTS AND DESCENDED TO 15000. DO TO THE TERRAIN AND NOT BEING ABLE TO GET LOWER THE PASSENGER MASKS DEPLOYED AND CABIN HIGH ALT OCCURRED. (FLIGHT 5488 - FILED CLOSED) THIS DISCREPANCY WAS TR
- [SDR SWIA2021072659748](https://openairdocs.org/sdr/SWIA2021072659748.md): Skin · damaged · Jul 12, 2021 · N652BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN BETWEEN FS 265.00 - FS 280.00 BETWEEN STR 25L AND STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS265.00 - FS280.00 AND STR24L - STR25R IN REF TO REO 601R-53-11-3715, REV--, DATED 2021-07-21
- [SDR SWIA202159747](https://openairdocs.org/sdr/SWIA202159747.md): Skin · damaged · Jul 12, 2021 · N652BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN AND REPAIR DOUBLER AT FS 235.00, BETWEEN STR 25L - STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS227.74 - FS250.00 AND STR24R - STR24L IN REF TO REO 601R-53-11-3714, REV--, DATED 2021-07-
- [SDR SWIA2021062591000](https://openairdocs.org/sdr/SWIA2021062591000.md): Apu · shutdown · Jun 25, 2021 · N652BR · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > APU INFLIGHT SHUTDOWN WHILE ENROUTE. SINGLE GENERATOR. VERIFIED APU INTAKE DOOR CLOSED AND ALL MX ACTION HAS BEEN COMPLIED WITH. REACTIVATED APU PER MEL 49-10-1A TROUBLESHOT APU INFLIGHT SHUTDOWN IAW FIM 49-10-00. REMOVED AND REPLACED APU ECU IAW AMM 49-6
- [SDR SWIA202158148](https://openairdocs.org/sdr/SWIA202158148.md): Bracket · bent · May 12, 2021 · N652BR · Cndair CL6002B19 · Main Landing Gear
  > GEAR DISAGREE EMERGENCY MESSAGE. NOSE GEAR REMAINED DOWN. RAN QRH AND EXTENDED ALL GEAR SUCCESSFULLY AND COMPLETED RTF. (FLIGHT 5289 - FILED CLOSED) FOUND NOSE LANDING GEAR WOW SENSOR BRACKET BENT, REPLACED BRACKET AND ADJUSTED WOW SENSOR IN REFERENCE TO
- [SDR SWIA202053019](https://openairdocs.org/sdr/SWIA202053019.md): Heat Shield · cracked · Oct 4, 2020 · N652BR · Cndair CL6002B19 · APU Exhaust System
  > APU HEAT EXHAUST SHIELD HAS A CRACK BETWEEN THE 7 O`CLOCK AND 8 O`CLOCK POSITION. FILED CLOSED RO 10/5/2020. REMOVED AND REPLACED APU HEAT EXHAUST SHIELD, IN REF TO CRJ200 AMM.
- [SDR SWIA2020060950959](https://openairdocs.org/sdr/SWIA2020060950959.md): Skin · dented · May 29, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENT LABELED 18 BETWEEN FS654.50 & FS672.20 AND STR 1R - STR 2R REQUIRES REPAIR. (C-CHECK) RO 4/27/2020 REPAIRED FUSELAGE SKIN DENT LABELED 18 BETWEEN FS654.50 - FS672.20 AND STR 1R - STRG 2R REF REO.
- [SDR SWIA2020060950958](https://openairdocs.org/sdr/SWIA2020060950958.md): Bulkhead · damaged · May 17, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE PERFORMING REPLACEMENT OF RBL 18 VERTICAL POSTS (INBOARD AND OUTBOARD) AT FS 409+128, FOUND 4 EACH HOLES ELONGATED ON BULKHEAD WEB AND 1 EACH DENT. (C-CHECK) RO 4/27/2020 REPAIR DAMGED AT RBL 18 VERTICAL POSTS (INBOARD AND OUTBOARD) AT FS 409+128 REF RE
- [SDR SWIA2020060950957](https://openairdocs.org/sdr/SWIA2020060950957.md): Skin · dented · May 15, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENTS FOUND IN MULTIPLE LOCATIONS ON TOP SIDE OF FUSELAGE BETWEEN FS 621.00 AND FS 755.00 PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/27/2020 REWORKED AND REPAIRED
- [SDR SWIA2020060950956](https://openairdocs.org/sdr/SWIA2020060950956.md): Floor Support · worn · May 14, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3) REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 REMOVED THE DAMAGED BEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3), REF SRM. INSTALLED NEW BEAM CAP P/N 601R35031-3 FROM FS569 TO FS621 LBL27 REF SRM
- [SDR SWIA2020060950946](https://openairdocs.org/sdr/SWIA2020060950946.md): Strap · worn · May 13, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT STRAP FS559.0 RBL 40 AND 27 APPROX REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 ORDERED AND RECEIVED, DRILLED AND LOCATED NEW PART, INSTALLED NEW STRAP ON THE RT SIDE AT FS559.00 RBL 27 - 40. REF SRM, DRAWING. COMPLIED WITH TASK CARD.
- [SDR SWIA2020060950955](https://openairdocs.org/sdr/SWIA2020060950955.md): Post · cracked · May 9, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 LBL 18.0 OUTBD VERTICAL POST AFT RADIUS IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED 2 EA PLATES ATTACHED TO VERTICAL STIFFENER FS 409+128 LBL18 AT WL 65.90 & WL 53.42 FOM. REF SRM. REMOVED I/B STIFFENER AND O/B CRACKED STIFFENER OF OUTBOARD VERTICA
- [SDR SWIA2020060950954](https://openairdocs.org/sdr/SWIA2020060950954.md): Stiffener · cracked · May 9, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 BL 0.0 RT VERTICAL POST UPPER STIFFENER IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT VERTICAL POST AT BL 0.0 FS 409.00+128 INSTALLED REF SRM AND DRAWING.
- [SDR SWIA2020060950953](https://openairdocs.org/sdr/SWIA2020060950953.md): Post · cracked · May 9, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 RBL 18.0 INBD AND OUTBD VERTICAL POST HAVE CRACKS IN AFT RADIUS. (C-CHECK) RO 4/27/2020 REMOVED AND INSTALLED NEW FS 409+128 RBL 18.0 INBD AND OUTBD VERTICAL POST. REF DWG, REO AND SRM. ALL CHECKS GOOD AT THIS TIME.
- [SDR SWIA2020060950972](https://openairdocs.org/sdr/SWIA2020060950972.md): Stop Fitting · chafed · May 8, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Structure
  > THE AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING IS CHAFED. (C-CHECK) RO 4/27/2020 REPLACED AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING REF SRM TUC4200 DUE:30-SEP-20 SEE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA2020060950971](https://openairdocs.org/sdr/SWIA2020060950971.md): Stop Fitting · chafed · May 8, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Structure
  > THE AVIONICS BAY DOOR CUTOUT SURROUND FWD LT STOP FITTING IS CHAFFED. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT LIMITS REF SRM. REMOVED AND REPLACED NEW AVIONICS BAY DOOR CUTOUT SORROUND FWD LT STOP FITTING. REF SRM.
- [SDR SWIA2020060950965](https://openairdocs.org/sdr/SWIA2020060950965.md): Fitting · cracked · May 8, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE AVIONICS BAY DOOR SURROUND AFT LT GUIDE FITTING IS BROKEN/CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED WITH NEW1 EACH AFT LT GUIDE FITTING ON AVIONICS BAY DOOR REF SRM.
- [SDR SWIA2020060950952](https://openairdocs.org/sdr/SWIA2020060950952.md): Frame · corroded · May 8, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Frame
  > THE FRAME AT FS349.00 HAS CORROSION FROM STRINGER 26R TO 26L. (C-CHECK) RO 4/27/2020 BLENDED OUT CORROSION ON LOWER FRAME SECTION AT FS349 FROM STR 26R TO 26L. REF SRM. ORIGINAL MATERIAL THICKNESS IS.063" PER SRM. MATERIAL LOSS IS.005 WITH.058" REMAININ
- [SDR SWIA2020060950974](https://openairdocs.org/sdr/SWIA2020060950974.md): Strap · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT STRAP FS559.0 LBL 40 AND 27 APPROX HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION AND RT STRAP FS559.0 WAS FOUND TO BE OUT OF LIMITS REF SRM. REPLACED ON MX#20971547, JOB 2742971. SEE CONTINUTION CARD FOR DETAILS.
- [SDR SWIA2020060950967](https://openairdocs.org/sdr/SWIA2020060950967.md): Seat Track · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK SECTION FROM APPROX FS559.00 TO FS559.00+80 AT RBL9.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND REPLACED NEW PASSENGER FLOOR SEAT RAIL AY FS 559.00 TO 559.00+80 RBL 9.0 REF AMM A
- [SDR SWIA2020060950966](https://openairdocs.org/sdr/SWIA2020060950966.md): Seat Track · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS559.00+112 - 574.00 (APPROXIMATE) AT RBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM 53-61-49. REMOVED AND INSTALLED NEW CARGO SEAT TRACK INSTALLED ATFS 559.00+112 TO FS 574.00 AT RBL 9.0 REF AMM.
- [SDR SWIA2020060950962](https://openairdocs.org/sdr/SWIA2020060950962.md): Floor Skin · cracked · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE PRESSURE FLOOR SKIN BETWEEN LBL 9.00 AND BL 0 AT APPROX FS 461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.06LBS. WEIGHT OF REPAIR PARTS IS 2.42LBS. TOTAL WEIGHT ADDED = 2.36LB. PRESSURE CHECKS GOOD AT THIS TIM
- [SDR SWIA2020060950951](https://openairdocs.org/sdr/SWIA2020060950951.md): Panel · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE RT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED RT PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 REF REO, SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD AT THIS TI
- [SDR SWIA2020060950950](https://openairdocs.org/sdr/SWIA2020060950950.md): Panel · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE LT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED LT PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 REF REO, AND REO. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOO
- [SDR SWIA2020060950949](https://openairdocs.org/sdr/SWIA2020060950949.md): Floor Skin · cracked · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE PRESSURE FLOOR SKIN BETWEEN RBL 9.00 AND BL 0 AT APPROX FS461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.05LBS. WEIGHT OF REPAIR PARTS IS 2.42LBS. TOTAL WEIGHT ADDED = 2.37LB. PRESSURE CHECKS GOOD AT THIS T
- [SDR SWIA2020060950947](https://openairdocs.org/sdr/SWIA2020060950947.md): Crossbeam · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE CROSSBEAM CAP AT FS559.00+48 BETWEEN RBL27.00 AND RBL9.00 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE FLOOR SUPPORT PLATE. REF SRM, DRAWING.
- [SDR SWIA2020060950945](https://openairdocs.org/sdr/SWIA2020060950945.md): Strap · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT STRAP FS559.0 LBL 35 AND 27 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION ON LT STRAP AT FS559 BETWEEN LBL27 - LBL35 REF SRM. LT STRAP AT FS 559.00 BETWEEN LBL 27 AND LBL 35 HAS AN ORIGINAL THICKNESS OF 0.050? REF SRM 53-41-43 FIG 1. MIN REMAINI
- [SDR SWIA2020060950944](https://openairdocs.org/sdr/SWIA2020060950944.md): Bracket · cracked · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 484 INBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 INBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT FS484 INBOARD PULLEY ANGLE BRACKET PART 601R-51-41-059-2 REF PREVIOUSLY INCORPERATED RE. INSTALLED L
- [SDR SWIA2020060950943](https://openairdocs.org/sdr/SWIA2020060950943.md): Bracket · cracked · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 484 OUTBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 OUTBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT FS484 OUTBOARD PULLEY ANGLE BRACKET PART 601R-51-41-059-1 REF: PREVIOUSLY INCORPERATED REO. INSTA
- [SDR SWIA2020060950942](https://openairdocs.org/sdr/SWIA2020060950942.md): Floor Support · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOORBEAM FS 409.00+128 TO 599.0 RBL 9 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED THE CORROSION, ENSURED REMAINING MATERIAL THICKNESS (NDT) - FOUND OUT OF LIMITS. RECEIVED ENGINEERING SUPPORT, COMPLIED WITH REO - PART IN LIMITS. REF REO.
- [SDR SWIA2020060950941](https://openairdocs.org/sdr/SWIA2020060950941.md): Doubler · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT GALLEY INBRD FWD DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED FWD DOUBLER PLATE AT FS295 AND RBL 4.25 REF SRM AND DWG. SEE CONTINUATIO CARD FOR DETAILS.
- [SDR SWIA2020060950940](https://openairdocs.org/sdr/SWIA2020060950940.md): Doubler · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT GALLEY INBRD AFT DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED AFT DOUBLER PLATE AT FS324 AND RBL 4.25 REF SRM AND DWG. CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020060950939](https://openairdocs.org/sdr/SWIA2020060950939.md): Doubler · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT GALLEY OUTBRD DOUBLER PLATE APPROX FS 319 RBL 35 HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED O/B DOUBLER PLATE AT FS319 AND RBL 35 REF SRM AND DWG. CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020060950938](https://openairdocs.org/sdr/SWIA2020060950938.md): Floorbeam · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 RBL 9. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE RT FLOORBEAM AT RBL 9 BETWEEN FS409.00+05 TO 409.00+121. REF REO.
- [SDR SWIA2020060950937](https://openairdocs.org/sdr/SWIA2020060950937.md): Floorbeam · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 LBL 9. (C-CHECK) RO 4/27/2020 BLENDED CORROSION ON LT FLOOR BEAM AT FS409.00+05 TO FS409.00+121 REF. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020060950936](https://openairdocs.org/sdr/SWIA2020060950936.md): Door Sill · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL HAS CORROSION RT FS 319- 349. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND REPLACED NEW MID SUPPORT ANGLE P/N 601R38303-253 AT RT FS319.00 TO FS 349.00 REF SRM AND DRAWING.
- [SDR SWIA2020060950935](https://openairdocs.org/sdr/SWIA2020060950935.md): Seat Track · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS559.00+112 - 574.00 (APPROXIMATE) AT LBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED SEAT TRACK FROM FS559+112 -FS574 LBL9 REF SRM.
- [SDR SWIA2020060950934](https://openairdocs.org/sdr/SWIA2020060950934.md): Seat Track · corroded · May 7, 2020 · N652BR · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS559.00+112 - 621.00 SEAT RAIL BEAM CAP AT LBL27 CORRODED IN NUMEROUS AREAS. (C-CHECK) RO 4/27/2020 REMOVED CORROSION FROM SEAT RAIL BEAM CAP AT LBL27 FS559.00+112 - 621.00. BLEND OUT AT FLOORBEAM FS559+112 - FS569.00, INBD LBL27 WAS FOUND TO BE WITHIN LIMI
- [SDR SWIA2020060950970](https://openairdocs.org/sdr/SWIA2020060950970.md): Connecting Rod · chafed · May 2, 2020 · N652BR · Cndair CL6002B19 · Landing Gear Door Retract Section
  > RT MLG LWR/OTBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF INBD END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REMOVED RT MLG DOOR STRUT. REF AMM - INSTALLED NEW RT MLG DOOR STRUT (WITH ONE EACH NEW BOLT, ONE NEW WASHER AND ONE NEW NUT AT
- [SDR SWIA2020060950969](https://openairdocs.org/sdr/SWIA2020060950969.md): Connecting Rod · chafed · May 2, 2020 · N652BR · Cndair CL6002B19 · Landing Gear Door Retract Section
  > RT MLG UPPER/INBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF LWR END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REPLACED RT MLG DOOR PUSH/PULL ROD REF AMM. OPS TEST GOOD.
- [SDR SWIA2020060950968](https://openairdocs.org/sdr/SWIA2020060950968.md): Support · chafed · May 1, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CENTER VERTICAL SUPPORT POST (AFT SIDE) REAR PRESS BULKHEAD FS 621.00, BL 0.00, IS CHAFED FROM MECHANICAL CONTACT WITH 10TH STAGE BLEED AIR SOV APROX 10' FROM TOP OF POST. (C-CHECK) RO 4/27/2020 REPAIRED CENTER VERTICAL SUPPORT POST (AFT SIDE) REAR PRESS BULK
- [SDR SWIA2020060950964](https://openairdocs.org/sdr/SWIA2020060950964.md): Attach Fitting · cracked · May 1, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND CRACKED ATTACHING (CLIP) AFT R/H SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14R LEVEL, AFT EQUIPMENT BAY. (C-CHECK) RO 4/27/2020 REMOVED, LOCATED, DRILLED, REPLACED AND RESTORED FINISH ON ATTACH
- [SDR SWIA2020060950963](https://openairdocs.org/sdr/SWIA2020060950963.md): Attach Fitting · cracked · May 1, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND CRACKED ATTACHING (CLIP) AFT LT SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14L LEVEL, AFT EQUIPMENT BAY. (C-CHECK) RO 4/27/2020 REMOVED, LOCATED, DRILLED, REPLACED AND RESTORED FINISH ON ATTACHI
- [SDR SWIA2020060950973](https://openairdocs.org/sdr/SWIA2020060950973.md): Stringer · gouged · Apr 30, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > SMALL SECTION OF STRINGER ATTACHED TO AFT PRESSURE BULKHEAD FS 621.00 THAT SPANS FROM THE AFT CARGO DOOR AFT TRACK OTBD TO FS 621.00, FOUND GOUGED/BENT FROM PROBABLE PREVIOUS MECHANICAL CONTACT WITH AFT CARGO DOOR AFT LOCK BOLT. (C-CHECK) RO 4/27/2020 REMOVED
- [SDR SWIA2020060950961](https://openairdocs.org/sdr/SWIA2020060950961.md): Attach Angle · cracked · Apr 30, 2020 · N652BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > (AFT) ATTACHING ANGLE (BOTTOM SIDE) AT FS 621.00 AND COMMON TO THE PRESSURE BULKHEAD, FOR ATTACHMENT OF THE CARGO DOOR CAM TRACK SUPPORT ASSY FOUND CRACKED. (C-CHECK) RO 4/27/2020 REPLACED CRACKED AFT ATTACHING ANGLE WITH NEW ONE P/N 601R35050-109 AT FS 621.0
- [SDR SWIA2020060950933](https://openairdocs.org/sdr/SWIA2020060950933.md): Skin · dented · Apr 29, 2020 · N652BR · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT FUSELAGE SKIN HAS DENT OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT APPROX FS 232 / BL 8 RT. (C-CHECK) RO 4/27/2020 REPAIRED THE DENT AT THE RT FUSELAGE SKIN, OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT. REF REO. REFERENCE THE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020060950932](https://openairdocs.org/sdr/SWIA2020060950932.md): Skin · chafed · Apr 28, 2020 · N652BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584FT. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E OUTBOARD SECTION WITH NEW PN 601R14303-43 PO# T-54677 REF DWG AND SRM. COMPLIED WITH CARD.
- [SDR SWIA2020060950931](https://openairdocs.org/sdr/SWIA2020060950931.md): Skin · chafed · Apr 28, 2020 · N652BR · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584ET. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E CENTER SECTION WITH NEW PN 601R14303-51 PO# 7426-00010 REF DWG AND SRM. COMPLIED WITH CARD.
- [SDR SWIA2020060950930](https://openairdocs.org/sdr/SWIA2020060950930.md): Skin · chafed · Apr 28, 2020 · N652BR · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP VANE SKIN IS CHAFED OUTBOARD OF PANEL 684FT. (C-CHECK) RO 4/27/2020 REPLACED RT INBOARD FLAP VANE SKIN OUTBOARD OF PANEL 684FT PN 601R14303-44S REF DWG SRM, SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Next page: https://openairdocs.org/deregistered/N652BR-2023-11-03/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 = 'N652BR' AND deregistration_id = 'N652BR-2023-11-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N652BR-2023-11-03/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.