# Service difficulty reports: N8533D A list on [N8533D](https://openairdocs.org/aircraft/N8533D.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 · 57 reports - [SDR REXA2014091700958](https://openairdocs.org/sdr/REXA2014091700958.md): Seal · missing · Sep 17, 2014 · N8533D · Cndair CL6002B19 · Emergency Equipment > SEAL MISSING ON PBE LOCATED BEHIND CAPTAINS SEAT. REPLACED PBE SECURITY SEAL IAW AMM 25-20-00. OK FOR SERVICE. - [SDR REXA2014082800848](https://openairdocs.org/sdr/REXA2014082800848.md): Roller · lack of lube · Aug 28, 2014 · N8533D · Cndair CL6002B19 · Passenger/Crew Doors > THE MAIN CABIN DOOR HANDLE WOULDN'T GO ALL THE WAY UP, HARD TO OPEN THE DOOR. LUBED DOOR ROLLERS & L1 PAX DOOR. OPERATIONS NORMAL IAW AMM 52-11-25. - [SDR REXA2014072000723](https://openairdocs.org/sdr/REXA2014072000723.md): Hook And Loop · unsecure · Jul 20, 2014 · N8533D · Cndair CL6002B19 · Emergency Equipment > CAPTAINS SIDE SMOKE GOGGLES NEED SECURING. REPLACED HOOK & LOOP IAW SRM 51-22-76. OPERATIONS CHECKED GOOD, OK FOR SERVICE. - [SDR REXA2014071200693](https://openairdocs.org/sdr/REXA2014071200693.md): Sign · broken · Jul 12, 2014 · N8533D · Cndair CL6002B19 · Emergency Lighting > WINDSCREEN EMER SIGN BROKEN. R & R WINDSCREEN EMER SIGN IAW AMM 33-51-14. - [SDR REXA2014041400060](https://openairdocs.org/sdr/REXA2014041400060.md): Hinge Fitting · damaged · Apr 4, 2014 · N8533D · Cndair CL6002B19 · Trailing Edge Flaps > LEFT OTBD FLAP AFT HINGE LUG FITTING AT FLS234.25 GOUGED & HAS OVERSIZED HOLES, OTBD LUG 0.4680 WITH REMAINING THICKNESS 0.218 INCHES, INBD LUG 0.4540 WITH REMAINING THICKNESS 0.203 INCHES. REPAIRED IAW REO 601R-57-53-1001. - [SDR REXA2014041400059](https://openairdocs.org/sdr/REXA2014041400059.md): Hinge Fitting · gouged · Apr 4, 2014 · N8533D · Cndair CL6002B19 · Horizontal Stabilizer Structure > LEFT HORIZONTAL STAB NR 2 HINGE FITTING AT BL 55.8865 GOUGED OTBD LUG & PLATE 0.770 INCHES X 0.213 INCHES X 0.015 INCHES DEEP & INBD LUG PLATE 0.980 INCHES X 0.213 INCHES X 0.006 INCHES DEEP. REPAIRED IAW REO 601R-55-11-485. - [SDR REXA2014041400058](https://openairdocs.org/sdr/REXA2014041400058.md): Hinge Fitting · gouged · Apr 4, 2014 · N8533D · Cndair CL6002B19 · Horizontal Stabilizer Structure > RIGHT HORIZONTAL STAB NR 2 HINGE FITTING AT BL 55.8865 GOUGED OTBD LUG & PLATE 1 INCH X 0.214 INCHES X 0.005 INCHES DEEP & INBD LUG PLATE 1.1 INCHES X 0.214 INCHES X 0.026 INCHES DEEP. REPAIRED IAW REO 601R-55-11-485. - [SDR REXA2014040200040](https://openairdocs.org/sdr/REXA2014040200040.md): Skin · corroded · Mar 29, 2014 · N8533D · Cndair CL6002B19 · Fuselage Main, Plate/Skin > CORROSION TO THE LOWER SKIN PANEL. REPAIRED IAW EA CRJ253-02383. - [SDR REXA2014032900038](https://openairdocs.org/sdr/REXA2014032900038.md): Hinge Fitting · damaged · Mar 26, 2014 · N8533D · Cndair CL6002B19 · Wing, Control Surface Attach Fittings > LEFT OTBD FLAP CTR HINGE ARM, CTR FITTING THAT ATTACHES TO THE WING DAMAGED. REPAIRED IAW REO 601R-57-53-1001. - [SDR REXA2014032700037](https://openairdocs.org/sdr/REXA2014032700037.md): Post · cracked · Mar 26, 2014 · N8533D · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LEFT VERTICAL POST AT FS 409+128, LBL 18 IS CRACKED AT LOWER OTBD SIDE. REPAIRED IAW REO 601R-53-41-056. - [SDR REXA2014032700036](https://openairdocs.org/sdr/REXA2014032700036.md): Stringer Clip · cracked · Mar 26, 2014 · N8533D · Cndair CL6002B19 · Fuselage Main, Attach Fittings > CLIP ON STRINGER 3R AT FS 280 CRACKED. REPAIRED IAW SRM 51-24-21, 51-42-21, 51-42-06, 51-40-11, 51-25-06, 51-25-16 & 51-21-11. - [SDR REXA2014032700035](https://openairdocs.org/sdr/REXA2014032700035.md): Stringer Clip · cracked · Mar 26, 2014 · N8533D · Cndair CL6002B19 · Fuselage Main, Attach Fittings > CLIP ON STRINGER 3L AT FS 280 CRACKED. REPAIRED IAW SRM 51-24-21, 51-42-21, 51-42-06, 51-40-11, 51-25-06, 51-25-16 & 51-21-11. - [SDR REXA2013121602403](https://openairdocs.org/sdr/REXA2013121602403.md): Battery · discharged · Dec 16, 2013 · N8533D · Cndair CL6002B19 · Emergency Equipment > FIRST OFFICER`S FLASHLIGHT NOT FLASHING. REPLACED FIRST OFFICER`S FLASHLIGHT BATTERY IAW AMM 25-61-01. OPERATIONS CHECKED OK, OK FOR SERVICE. - [SDR REXA2013092501752](https://openairdocs.org/sdr/REXA2013092501752.md): Feeder Cable · damaged · Sep 24, 2013 · N8533D · Cndair CL6002B19 · Light System Wiring > ROWS 9-12 EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY CABLE IAW AMM 33-51-01. OPS CHECK GOOD. - [SDR REXA2013080601561](https://openairdocs.org/sdr/REXA2013080601561.md): Oxygen Mask · no test · Aug 6, 2013 · N8533D · Cndair CL6002B19 · Crew Oxygen System > F/O SIDE OXYGEN MASK WILL NOT TEST. STOWED F/O OXYGEN MASK. OPS CHECKED GOOD IAW AMM 35-11-12. OK FOR SERVICE. - [SDR REXA2013073101399](https://openairdocs.org/sdr/REXA2013073101399.md): A/C Pack · overheated · Jul 31, 2013 · N8533D · Cndair CL6002B19 · Cabin Cooling System > RIGHT PACK OVERTEMPED TO 120 CAUSING SMOKE IN CABIN. - [SDR REXA2013031600564](https://openairdocs.org/sdr/REXA2013031600564.md): Life Vest · unserviceable · Mar 16, 2013 · N8533D · Cndair CL6002B19 · Life Jacket > OBSERVER LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED OBSERVER LIFE VEST IAW AMM 25-61-03. - [SDR REXA2013022800429](https://openairdocs.org/sdr/REXA2013022800429.md): Pdu · malfunctioned · Feb 28, 2013 · N8533D · Cndair CL6002B19 · Trailing Edge Flap Actuator > ON FLIGHT 3932 (SYR TO JFK) ON APPROACH WHEN FLAP SELECTOR WAS MOVED TO 8 DEGREE DESCENT, THE FLAPS FAIL CAUTION MESSAGE APPEARED. RAN QRH LANDED WITHOUT INCIDENT. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I) AMOC - [SDR REXA2013011900155](https://openairdocs.org/sdr/REXA2013011900155.md): Life Vest · unserviceable · Jan 19, 2013 · N8533D · Cndair CL6002B19 · Life Jacket > INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A. - [SDR REXA2012061100832](https://openairdocs.org/sdr/REXA2012061100832.md): Battery Pack · inoperative · Jun 11, 2012 · N8533D · Cndair CL6002B19 · Emergency Lighting > BOTH EXTERIOR NR 3 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD. - [SDR REXA2012060900693](https://openairdocs.org/sdr/REXA2012060900693.md): Angle · corroded · Jun 8, 2012 · N8533D · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 280 LOWER WEB CRACKED OUTBOARD OF RBL9. FORWARD ANGLE HAS CORROSION RBL 9 INBOARD AND OUTBOARD CLIPS ARE CRACKED, LBL 9 IN CLIP CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-171. - [SDR REXA2012060900692](https://openairdocs.org/sdr/REXA2012060900692.md): Floor Support · corroded · Jun 8, 2012 · N8533D · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LBL 27 FLOOR SUPPORT CAP CORRODED AROUND NUTPLATE HOLES BETWEEN FS 574- 621. REPAIRED IAW REO 601R-53-61-3778. - [SDR REXA2012060900691](https://openairdocs.org/sdr/REXA2012060900691.md): Stiffener · chafed · Jun 8, 2012 · N8533D · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL0 CHAFED FROM ISOLATION VALVE 0.4 INCH BY 0.2 INCH BY 0.053 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523. - [SDR REXA2012060900690](https://openairdocs.org/sdr/REXA2012060900690.md): Access Panel · corroded · Jun 8, 2012 · N8533D · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING LOWER WING PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 5 CORRODED 0.003 INCH DEEP IN FWD CRITICAL AREA, 0.001 INCH DEEP IN AFT CRITICAL AREA, AND 0.003 INCH DEEP IN NON-CRITICAL AREA. REPAIRED IAW BOMBARDIER REO 601R-57-21-030. - [SDR REXA2012060900689](https://openairdocs.org/sdr/REXA2012060900689.md): Access Panel · corroded · Jun 8, 2012 · N8533D · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUTS CORRODED. HOLE NR 1 0.001 INCH DEEP IN CRITICAL REGION. HOLE NR 4 0.001 INCH DEEP IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030. - [SDR REXA201206090688](https://openairdocs.org/sdr/REXA201206090688.md): Access Panel · corroded · Jun 8, 2012 · N8533D · Cndair CL6002B19 · Wing, Plate/Skin > RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUTS HAVE CORROSION. HOLES NR 10 0.002 INCH IN CRITICAL REGION. HOLE NR 12 0.002 INCH IN CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030. - [SDR REXA2012060900687](https://openairdocs.org/sdr/REXA2012060900687.md): Access Panel · corroded · Jun 8, 2012 · N8533D · Cndair CL6002B19 · Wing, Plate/Skin > LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 1 CORRODED 0.004 INCH DEEP IN THE NON-CRITICAL REGION AND HOLE NR 2 CORRODED 0.017 INCH DEEP IN CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030. - [SDR REXA2012051500733](https://openairdocs.org/sdr/REXA2012051500733.md): Selector Valve · malfunctioned · May 15, 2012 · N8533D · Cndair CL6002B19 · Nose/Tail Landing Gear > AIR RETURN, NOSE DOOR WARNING MESSAGE AFTER GEAR RETRACTION. MESSAGE WENT OUT AFTER 20 SECONDS. REMOVED AND REPLACED THE NOSE GEAR DOOR SELECTOR VALVE PER AMM 32-22-20. FIM 32-60-00 COMPLETED. PERFORMED GEAR SWINGS. ALL CHECKED GOOD AT THIS TIME. AIRCRA - [SDR REXA2012051400726](https://openairdocs.org/sdr/REXA2012051400726.md): Control Rod · out of adjust · May 14, 2012 · N8533D · Cndair CL6002B19 · Landing Gear Door Retract Section > NOSE DOOR WARNING MESSAGE ON TAKEOFF, QRH COMPLETE. ADJUSTED NOSE LANDING GEAR DOOR CENTER CONTROL ROD TO LIMITS IAW AMM 32-22-15. REMOVED NOSE GEAR DOOR RIGS PINS. LANDING GEAR EXTENSION RETRACTION SYSTEM AND NOSE DOOR OPERATING MECHANISM OPS CHECKS NORMA - [SDR REXA2012051300732](https://openairdocs.org/sdr/REXA2012051300732.md): Landing Gear · noisy · May 13, 2012 · N8533D · Cndair CL6002B19 · Nose/Tail Landing Gear > AFTER TAKEOFF, STRANGE GRINDING SOUND FROM NOSE GEAR AREA FOLLOWED BY A NOSE DOOR MASTER WARNING. MESSAGE EVENTUALLY WENT AWAY AFTER ABOUT 15 SECONDS SOUND STOPPED SHORTLY AFTER. THE REST OF THE FLIGHT WAS UNEVENTFUL ALSO FIRST OFFICE DID NOT NOTICE ANYTHING - [SDR REXA2012051000715](https://openairdocs.org/sdr/REXA2012051000715.md): Lamp · inoperative · May 10, 2012 · N8533D · Cndair CL6002B19 · Emergency Lighting > FORWARD CEILING EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-10. OPS CHECKED GOOD. - [SDR REXA2012041800527](https://openairdocs.org/sdr/REXA2012041800527.md): Latch · lack of lube · Apr 18, 2012 · N8533D · Cndair CL6002B19 · Accessory Compartment Doors > F/A FORWARD EMERGENCY EQUIPMENT CLOSET DOOR IS HARD TO OPEN. CLEANED & LUBED LATCHES TO F/A'S FWD CLOSET. OPS CHECKS NORMAL. - [SDR REXA2012033000378](https://openairdocs.org/sdr/REXA2012033000378.md): Skin · damaged · Mar 29, 2012 · N8533D · Cndair CL6002B19 · Fuselage Main, Plate/Skin > AIRCRAFT WAS HIT BY A JET BRIDGE IN DTW, RESULTING IN SKIN DAMAGE BETWEEN FS 250 AND FS 265 BELOW THE PRODUCTION SKIN BUTT SPLICE AT S-16L. REPAIRED IAW EA CRJ253-00448B AS APPROVED BY ASSOCIATED 8110-3 DATED MARCH 29, 2012. - [SDR REXA2012020700212](https://openairdocs.org/sdr/REXA2012020700212.md): Light · inoperative · Feb 7, 2012 · N8533D · Cndair CL6002B19 · Emergency Lighting > NR 2 SECTION OF EMER FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BAD SECTION OF FLOOR EMER LIGHT TRACK IAW AMM 33-51-01, OP CHECKS GOOD. - [SDR REXA201100914](https://openairdocs.org/sdr/REXA201100914.md): Light · loose · Dec 7, 2011 · N8533D · Cndair CL6002B19 · Emergency Lighting > THREE SECTIONS OF FLOOR TRACK LIGHT INOP. RE-SECURED EMER FLOOR TRACK LIGHT IAW AMM 33-51-01. OPC GOOD OK FOR SVC. - [SDR REXA201100763](https://openairdocs.org/sdr/REXA201100763.md): Sensing Element · defective · Oct 20, 2011 · N8533D · Cndair CL6002B19 · Pneumatic Indicating System > ANTI-ICE DUCT MESSAGE (WARNING) CAME ON AT INITIAL APLICATION OF WING A-ICE. CLEARED W/ IN 10 SEC. TWICE. REMOVED AND REPLACED RT FUSELAGE SENSING ELEMENT A38WK IAW AMM 36-21-04. OPC GOOD. VERIFIED PART EFFECTIVITY. - [SDR REXA201100762](https://openairdocs.org/sdr/REXA201100762.md): Warning System · false activation · Oct 20, 2011 · N8533D · Cndair CL6002B19 · Airfoil Anti/De-ice System > ANTI ICE DUCT WARNING JUST AFTER TAKEOFF. PERFORMED OP CHECK OF ANTI ICE DUCT WARNING SYSTEM IAW AMM 30-11-00, OP CHECK COULD NOT DUPLICATE DISCREPANCY. - [SDR REXA201100610](https://openairdocs.org/sdr/REXA201100610.md): Fuel Line · loose · Sep 27, 2011 · N8533D · Cndair CL6002B19 · APU Engine Fuel and Control > FUEL FUMES WITH BOTH PAXS OPERATING IN FLIGHT AND ON APPROACH. INSPECTED LT AND RT ENG FOUND NO FUEL OR OIL LEAKS FROM ENGINES. COULD NOT FIND SOURCE OF FUEL LEAK REMOVED AND RESEATED FUEL LINES ON APU FUEL CONTROL NO FUEL LEAK FOUND. REMOVED DUCTS FROM WAT - [SDR REXA201100605](https://openairdocs.org/sdr/REXA201100605.md): Light · inoperative · Sep 17, 2011 · N8533D · Cndair CL6002B19 · Emergency Lighting > EMERGENCY FLOOR TRACK NR 1 PARTIALLY INOP. REMOVED AND REPLACED NR 1 FLOOR TRACK LIGHTING NR 1 IAW AMM33-51-01/ VERFIED PARTS EFFECTIVITY. OPS CHECK GOOD RETURN TO SERVICE. - [SDR REXA201100604](https://openairdocs.org/sdr/REXA201100604.md): Battery Pack · discharged · Sep 17, 2011 · N8533D · Cndair CL6002B19 · Emergency Lighting > EMERGENCY 2 TO 4 LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-04 VERIFIED PART EFFECTIVITY. OPS CHECK GOOD. - [SDR REXA201100566](https://openairdocs.org/sdr/REXA201100566.md): Fuel Line · loose · Sep 17, 2011 · N8533D · Cndair CL6002B19 · APU Engine Fuel and Control > STRONG SMELL OF FUEL IN THE COCKPIT AT CRUISE ALTITUDE. WHEN ON THE GROUND STARTED THE APU WITH THE MECHANIC IN THE AFT EQUIPMENT BAY. FUEL BEGAN POURING OUT OF A FUEL LINE THAT WAS NOT TIGHTENED DOWN. IN 1 MINUTE OF RUNNING THE APU HAD APPROXIMATELY 2-3 IN - [SDR REXA201100601](https://openairdocs.org/sdr/REXA201100601.md): Battery · discharged · Sep 16, 2011 · N8533D · Cndair CL6002B19 · Emergency Lighting > LT FORWARD FUSE, RT FORWARD FUSE AND AFT FUSE, FORWARD CEILING AND SERVICE DOOR LOWER EXIT EMERGENCY FLOODLIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY NR 1 IAW AMM 33-51-04. OPS CHECK GOOD VERIFY PART EFFECTIVITY. - [SDR REXA201100507](https://openairdocs.org/sdr/REXA201100507.md): Ecu · malfunctioned · Aug 3, 2011 · N8533D · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAPS FAIL AT 30 DEGREE POSITION DURING APPROACH PERFORMED FIM PROCEDURE. REMOVED AND REPLACED FECU IAW AMM 27-51-05, AND PERFORMED OPS CHECK IAW AMM 27-54-00 AND 27-51-01, OPS CHECK GOOD, OK FOR SERVICE. - [SDR REXA201100108](https://openairdocs.org/sdr/REXA201100108.md): Bulkhead · cracked · Feb 12, 2011 · N8533D · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 559.00 BULKHEAD WEB WAS FOUND CRACKED AND REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-260 REV E AND REO 601R-53-41-609 REV B DEVIATION E. - [SDR REXA201100039](https://openairdocs.org/sdr/REXA201100039.md): Warning System · false activation · Jan 17, 2011 · N8533D · Cndair CL6002B19 · Landing Gear Position and Warning > GEAR DISAGREE. C/W PA 05-018A, PERFORMED GEAR SWING IAW AMM 32-30-00. OP/C GOOD, NO DEFECTS FOUND AT THIS TIME. - [SDR REXA201000327](https://openairdocs.org/sdr/REXA201000327.md): Wire · damaged · Dec 23, 2010 · N8533D · Cndair CL6002B19 · Ice/Rain Protection System Wiring > ON CLIMBOUT OF KBDL FOR KCVG, THE WING ANTI-ICE MASTER WARNING ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND REQUESTED TO RETURN TO KBDL. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KBDL. MAINTENANCE FOUND WIRE NUMBER 2WK26YY20 TO BE BAD FROM - [SDR REXA201000324](https://openairdocs.org/sdr/REXA201000324.md): Wire · damaged · Dec 23, 2010 · N8533D · Cndair CL6002B19 · Ice/Rain Protection System Wiring > ON CLIMBOUT OF KBDL FOR KCVG THE WING ANTI-ICE MASTER WARNING ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND RTF, NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE FOUND WIRE NR 2WK26YY20 TO BE BAD BETWEEN SP2WK AND THE WING ROOT. THE WIRE WAS REPLACED - [SDR REXA201000277](https://openairdocs.org/sdr/REXA201000277.md): Receptacle · damaged · Nov 24, 2010 · N8533D · Cndair CL6002B19 · Fuselage Main, Structure > THE GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE WAS DAMAGED. THE DAMAGE CONSISTS OF THE POWER RECEPTACLE BEING PULLED FROM THE INSTALLED POSITION IN THE RECESSED PAN AREA AND BENT DOOR LAND. TEMPORARY REPAIR IAW ENGINEERING EA 5-2010-282. - [SDR REXA201000160](https://openairdocs.org/sdr/REXA201000160.md): Retainer · corroded · Sep 25, 2010 · N8533D · Cndair CL6002B19 · Electrical/Electronic Compartment Doors > AVIONICS DOOR SEAL RETAINERS HAVE CORROSION. REMOVED 4EA SEAL RETAINERS FROM AVIONICS DOOR IAW CRJ-200 SRM 51-42-06. LOCATED, DRILLED, AND INSTALLED 4EA SEAL RETAINERS (P/N'S CC670-38662-5, CC670-38675-3, CC670-38674-3, AND CC670-38663-5) IAW CRJ-200 SRM 51- - [SDR REXA201000155](https://openairdocs.org/sdr/REXA201000155.md): Retainer · corroded · Sep 19, 2010 · N8533D · Cndair CL6002B19 · Electrical/Electronic Compartment Doors > AVIONICS DOOR SEAL RETAINERS HAVE CORROSION. REMOVED AND REPLACED 4EA SEAL RETAINERS, P/N'S CC670-38662-5, CC670-38675-3, CC670-38674-3, AND CC670-38663-5, FROM AVIONICS DOOR IAW CRJ-200 SRM 51-42-06 AND 51-23-00. Next page: https://openairdocs.org/aircraft/N8533D/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 = 'N8533D' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8533D/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.