# Service difficulty reports: N555NN

A list on [N555NN](https://openairdocs.org/aircraft/N555NN.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR VNAA2025112811102](https://openairdocs.org/sdr/VNAA2025112811102.md): Selector Valve · faulted · Nov 26, 2025 · N555NN · Cndair CL6002D24 · Landing Gear Steering System
  > GEAR DISAGREE WARNING W/ LOSS OF STEERING ON LANDING. /REMOVED AND REPLACED MLG SELECTOR VALVE ASSEMBLY IAW AMM 32-10-000/400-801-A01. BLED HYD SYSTEM 3 IAW AM 29-10-00-870-802-A01.
- [SDR VNAA2024090311101](https://openairdocs.org/sdr/VNAA2024090311101.md): Light · burned out · Aug 30, 2024 · N555NN · Cndair CL6002D24 · Passenger Compartment Lighting
  > FLIGHT ATTENDANT REPORTED ELECTRICAL FUMES IN BACK OF AIRCRAFT. ON GND WAITING AT GATE APU BLEEDS ONLY / TROUBLESHOT PER FIM 21-22-00-810-806. FOUND AFT LAV VANITY LIGHT LED BURNT OUT. REMOVED AND REPLACED AFT LAV VANITY LIGHT LED IAW CRJ 900 AMM 33-25-03-000/
- [SDR VNAA202310100009](https://openairdocs.org/sdr/VNAA202310100009.md): Skin · dented · Sep 25, 2023 · N555NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENTS BTW FS 1162.00 TO FS 1181.00 AND BTW STGR 25LH TO STGR 25RH. REPAIRED PER EA 23-C9-53-1365 REV.IR SECTION III - PERMANENT REPAIR.
- [SDR VNAA202310100002](https://openairdocs.org/sdr/VNAA202310100002.md): Skin · worn · Sep 24, 2023 · N555NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 597AB) AT LH WING LOWER SKIN. REPAIRED PER EA 23-C9-57-1243 REV IR, EA 23-C9-57-1276 REV.A, EA 23-C9-57-1277 REV.IR, EA23-C9-57-1278 REV.IR SECTION III-PERMANENT REPAIR.
- [SDR VNAA202310080003](https://openairdocs.org/sdr/VNAA202310080003.md): Bushing · corroded · Sep 24, 2023 · N555NN · Cndair CL6002D24 · Wing Structure
  > CORROSION ON BUSHINGS SETTLEMENT AREA (8 LOCATIONS) HINGE 1,2, 3, 4 (INBD AND OUTBD) WAS FOUND. CORROSION ON BUSHINGS SETTLEMENT AREA (8 LOCATIONS) HINGE 1,2, 3, 4 (INBD AND OUTBD) WERE REPAIRED PER REO 690-57-51-299 REV. --
- [SDR VNAA202310090005](https://openairdocs.org/sdr/VNAA202310090005.md): Intercostal · corroded · Sep 23, 2023 · N555NN · Cndair CL6002D24 · Passenger/Crew Doors
  > INTERCOSTAL DD3 WAS REPLACED AND ANGLE-TO-SKIN OF INTERCOSTAL BTW FORMER FS 320.163 AND FWD SUPPORT ANGLE OF PASSENGER DOOR INTERNAL STRUCTURE (INSIDE ACCESS PANEL 832DL) WAS CLEANED AND RE-INSPECT AND CORROSION WAS NOT FOUND PER CRJ-900 SRM 51-42-06-001-001-A
- [SDR VNAA2023100910006](https://openairdocs.org/sdr/VNAA2023100910006.md): Intercostal · worn · Sep 19, 2023 · N555NN · Cndair CL6002D24 · Passenger/Crew Doors
  > WEAR ON INTERCOSTAL 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. INTERCOSTAL 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS REPLACED PER EA 23-C9-53-1282 REV. IR
- [SDR VNAA202310080004](https://openairdocs.org/sdr/VNAA202310080004.md): Hinge · corroded · Sep 18, 2023 · N555NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > ORROSION ON BUSHINGS (7 EA) OF AILERON HINGE 1 (OUTBD), HINGE 2,3, 4 (INBD AND OUTBD) AT LH WING REAR SPAR. AILERON HINGE 1 (OUTBD), HINGE 2,3, 4 (INBD AND OUTBD) AT LH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-298 REV. - & EA 23-C9-57-1242 REV. A
- [SDR VNAA202310080002](https://openairdocs.org/sdr/VNAA202310080002.md): Bushing · corroded · Sep 18, 2023 · N555NN · Cndair CL6002D24 · Wing Structure
  > AFTER BUSHINGS REMOVAL OF AILERON HINGE LH IN REF NRC 00125, CORROSION ON BUSHINGS SETTLEMENT AREA (7 LOCATIONS) HINGE 1 (OUTBD), HINGE 2, 3, 4 (INBD AND OUTBD) WAS FOUND. SETTLEMENT AREA (8 LOCATIONS) HINGE 1,2, 3, 4 (INBD AND OUTBD) WERE REPAIRED PER REO 69
- [SDR VNAA202310100005](https://openairdocs.org/sdr/VNAA202310100005.md): Support Plate · corroded · Sep 11, 2023 · N555NN · Cndair CL6002D24 · Fuselage Structure (General)
  > CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/R
- [SDR VNAA202310100007](https://openairdocs.org/sdr/VNAA202310100007.md): Strut · corroded · Sep 10, 2023 · N555NN · Cndair CL6002D24 · Main Landing Gear Strut/Axle/Truck
  > AFTER REMOVAL OF LEFT MLG PISTON AXLE, CORROSION ON SHOCK STRUT THREADS. SHOCK STRUT LH SIDE WAS REPAIRED PER REO 690-32-11-163 REV. - -
- [SDR VNAA202310100006](https://openairdocs.org/sdr/VNAA202310100006.md): Landing · corroded · Sep 10, 2023 · N555NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT SETTLEMENT AREA OF ACCESS PANEL 195AB. REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ-900 SRM 53-83-55-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01
- [SDR VNAA202310090010](https://openairdocs.org/sdr/VNAA202310090010.md): Hinge Fitting · bent · Sep 10, 2023 · N555NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > BENT AFT HINGE ON FWD BAGGAGE BAY DOOR STRUCTURE. DUE NOT ALLOWABLE DAMAGE AT AFT HINGE ON FWD BAGGAGE BAY DOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 53-31-23-101-001-A02 AND SRM 51-41-02-001-001-A01
- [SDR VNAA202310100010](https://openairdocs.org/sdr/VNAA202310100010.md): Angle · cracked · Sep 7, 2023 · N555NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER ACCESS PANEL REMOVAL WITH NRC 00030, CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUC
- [SDR VNAA202310100008](https://openairdocs.org/sdr/VNAA202310100008.md): Bracket · cracked · Sep 3, 2023 · N555NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > DURING DVI SERVICE DOOR STABILIZATION BRACKET ASSY STEP 4. BRACKET ASSEMBLY WAS FOUND CRACKED. BRACKET ASSY SERVICE DOOR P/N:CC670-38380-1 WAS REPLACED PER CRJ900 AMM 52-41-27
- [SDR VNAA2023100910004](https://openairdocs.org/sdr/VNAA2023100910004.md): Floorbeam · cracked · Sep 3, 2023 · N555NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1596 REV.--
- [SDR VNAA202310100003](https://openairdocs.org/sdr/VNAA202310100003.md): Fitting · worn · Aug 28, 2023 · N555NN · Cndair CL6002D24 · Fuselage Structure (General)
  > PERM REPAIR - JACKING PAD HELICOIL INSERT, RHS CW PERM REPAIR PER REO INSTRUCTIONS. JACK FITTING PAD RH WING WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR VNAA202310080010](https://openairdocs.org/sdr/VNAA202310080010.md): Seat Track · corroded · Aug 28, 2023 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS OF RBL9 AND LBL9 BTW FS847.00 TO FS977.00. DUE NOT DAMAGE ALLOWED ON SEAT RAILS OF RBL9 AND LBL9 BTW FS847.00 TO FS977.00 (2E/A) WRE REPLACED PER CRJ-900 SRM 53-51-49-101-001-A02 AND CRJ/900 AMM 53-00-49 CONFIG. (A12)
- [SDR VNAA202310080001](https://openairdocs.org/sdr/VNAA202310080001.md): Skin · dented · Aug 23, 2023 · N555NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%. DENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZE
- [SDR VNA2023F00006](https://openairdocs.org/sdr/VNA2023F00006.md): Drag Angle · cracked · Aug 22, 2023 · N555NN · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01
- [SDR VNAA202310080009](https://openairdocs.org/sdr/VNAA202310080009.md): Seat Track · corroded · Aug 22, 2023 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL 9 BTW F.S.581.00 TO F.S.661.00. SEAT RAIL RBL 9 BTW F.S.581.00 TO F.S.661.00 WAS EVALUATED PER CRJ-900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202310080008](https://openairdocs.org/sdr/VNAA202310080008.md): Seat Track · corroded · Aug 22, 2023 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 485.00. SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 485.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02; CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)
- [SDR VNAA202310080007](https://openairdocs.org/sdr/VNAA202310080007.md): Seat Track · corroded · Aug 22, 2023 · N555NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL 9 BTW FS 379. SEAT RAIL LBL 9 BTW FS379 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202310080006](https://openairdocs.org/sdr/VNAA202310080006.md): Bracket · corroded · Aug 22, 2023 · N555NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET MACHINED (6EA) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO BELOW FLOOR BETWEEN STGR 23RH/23LH AND FS501.00 TO FS661.00+32.00. BRACKET MACHINED (6EA) AT INTERNAL STRUCTURE FWD BAGGAGE BAY CARGO BELOW FLOOR BETWEEN STGR 23RH/23LH AND FS501
- [SDR VNAA202310080005](https://openairdocs.org/sdr/VNAA202310080005.md): Hinge Fitting · excess play · Aug 22, 2023 · N555NN · Cndair CL6002D24 · Rudder Structure
  > AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. RUDDER HINGE FITTINGS NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR, WERE REPLACED PER RIL #2103 REV. B
- [SDR VNA2023F00007](https://openairdocs.org/sdr/VNA2023F00007.md): Drag Angle · cracked · Aug 20, 2023 · N555NN · Cndair CL6002D24 · Vertical Stabilizer
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR VNAA202310100004](https://openairdocs.org/sdr/VNAA202310100004.md): Striker · worn · Aug 18, 2023 · N555NN · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR SEAL STRIKER WITHIN 1,374.07 FH (BEFORE 20,312.15 FH). REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND EA 23-C9-53-0145 REV.IR
- [SDR VNAA202310100001](https://openairdocs.org/sdr/VNAA202310100001.md): Skin · worn · Aug 17, 2023 · N555NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON FIXED LEADING EDGE (522AL, 522BL) AT LH WING. REPAIRED PER EA 23-C9-57-1196 REV.IR SECTION III PERMANENT REPAIR.
- [SDR VNAA202310090014](https://openairdocs.org/sdr/VNAA202310090014.md): Skin · worn · Aug 17, 2023 · N555NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON FIXED LEADING EDGE (631AR) AT RH WING. WEAR ON FIXED LEADING EDGE (631AR) AT RH WING WAS REPAIRED PER EA 23-C9-57-1191 REV.IR SECTION III PERMANENT REPAIR
- [SDR VNAA202310090013](https://openairdocs.org/sdr/VNAA202310090013.md): Skin · nicked · Aug 17, 2023 · N555NN · Cndair CL6002D24 · Trailing Edge Flaps
  > SEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE REMOVED PER CRJ900 SRM 51-12-00-001-001-A01; WERE EVALUATED WITHIN LIMITS BTW FLS 45 TO FLS 65 AND WERE E
- [SDR VNAA202310090012](https://openairdocs.org/sdr/VNAA202310090012.md): Skin · worn · Aug 17, 2023 · N555NN · Cndair CL6002D24 · Wing, Plate/Skin
  > WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. REPAIRED PER EA 23-C9-57-1258 REV IR, EA 23-C9-57-1259 REV IR, EA 23-C9-57-1260 REV IR, EA 23-C9-57-1261 REV IR, EA 23-C9-57-1262 REV IR.
- [SDR VNAA202310090011](https://openairdocs.org/sdr/VNAA202310090011.md): Access Panel · corroded · Aug 17, 2023 · N555NN · Cndair CL6002D24 · Passenger/Crew Doors
  > CORROSION ON PASSENGER DOOR ACCES PANEL 832EL. CORROSION ON ACCESS PANEL 832EL WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01; WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 52-11-32-101-001-A01; AND WAS VERIFIED PER CRJ900 AIPC 52-11-32-20
- [SDR VNAA202209081112](https://openairdocs.org/sdr/VNAA202209081112.md): None · none · Sep 5, 2022 · N555NN · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE RED WARNING AFTER GEAR SELECTED UP AFTER TAKE OFF. RAN QRF, RTF. DECLARED EMERGENCY. UPON INSPECTION OF PX22 FOUND UPPER DRAG BRACE BRACKET FOR PX22 AND PX21 LOOSE AND WIGGLING FROM SIDE TO SIDE AND UP AND DOWN. INSTALLED NEW WASHERS ON DRAG BRAC
- [SDR VNAA202110051111](https://openairdocs.org/sdr/VNAA202110051111.md): Seal · sticking · Oct 2, 2021 · N555NN · Cndair CL6002D24 · Emergency Exits
  > DURING SCHEDULED INSPECTIONS, MX WAS UNABLE TO OPEN THE LH FWD EMERGENCY EXIT DOOR (FROM THE INSIDE SEAT 15A). LH FWD EMERGENCY DOOR REQUIRES DVI AND LEAK CHECK DUE TO SEALANT FOUND AROUND FLAPPER DOOR. / REMOVED AND REPLACED EMERGENCY DOOR FLAP SEAL IAW CRJ 9
- [SDR VNAA202107051114](https://openairdocs.org/sdr/VNAA202107051114.md): Door · damaged · Jul 5, 2021 · N555NN · Cndair CL6002D24 · Landing Gear Doors
  > OPERATOR HAS REPORTED DAMAGE TO RHS FWD NOSE LANDING GEAR DOOR & RHS ADG FUSELAGE SKIN PANEL (DWG. CC670-33109, REF) BETWEEN FS169 AND FS193. / WITNESSED CONSTANT AVIATION PERFORM REMOVAL AND REPLACEMENT OF THE RH FORWARD AIR DRIVEN GENERATOR SKIN PANEL (P/N:
- [SDR VNAA202106041112](https://openairdocs.org/sdr/VNAA202106041112.md): Skin · damaged · Jun 3, 2021 · N555NN · Cndair CL6002D24 · Elevator, Plate/Skin
  > DURING OVERNIGHT MAINTENANCE AT CHARLOTTE NC, (CLT), MX REPORTS BURN MARK DAMAGE TO THE RH ELEVATOR P/N AV670-24100-040 SN MH570. THE DAMAGE DIMENSIONS ARE AS FOLLOWS.75"L X.5"W X.25"D AND IS LOCATED AT THE TRAILING EDGE BETWEEN RIBS 19 AND 20. THE ELEVATOR
- [SDR VNAA2020073011101](https://openairdocs.org/sdr/VNAA2020073011101.md): Bleed Valve · failed · Jul 27, 2020 · N555NN · Cndair CL6002D24 · Compressor Bleed Valve
  > L ENG DEGRADED, L ENG SURGE OPEN CAUTION, L ENG ITT EXCEEDED. CREW SENT ACARS TO DISPATCHER STATING THEY WERE RETURNING TO FIELD, DUE TO MX. CREW DID DECLARE AN EMERGENCY. CREW STATES THEY RECEIVED L ENGINE DEGRADED MESSAGE AND L ENGINE SURGE OPEN CAUTION
- [SDR VNAA2020021751102](https://openairdocs.org/sdr/VNAA2020021751102.md): Sign · cracked · Feb 15, 2020 · N555NN · Cndair CL6002D24 · Emergency Lighting
  > SERVICE DOOR EXIT SIGN CRACKED. R/R SERVICE DOOR EXIT SIGN LENS
- [SDR VNAA2020021511101](https://openairdocs.org/sdr/VNAA2020021511101.md): Housing · failed · Feb 15, 2020 · N555NN · Cndair CL6002D24 · Emergency Lighting
  > INTERIOR EMERGENCY LIGHT TO THE LEFT OF PAX DOOR (UPPER) ON THE FWD WARDROBE WONT ILLUMINATE. MX R+R EMERGENCY EXIT SIGN LIGHT ASSY DS156 IAW CRJ-900 AMM 33-51-05-000/400-801, CRJ-900 WM 33-23-04, AND CRJ-900 ESPM 20-26-11. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR VNAA201911299907](https://openairdocs.org/sdr/VNAA201911299907.md): Intercostal · corroded · Nov 29, 2019 · N555NN · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTALS BETWEEN FS 323 TO FS 335 3 INTER COSTALS CORRODED FROM THE TOP OF DOOR MARKED WITH TAPE. REMOVED INTERCOSTALS PAX DOOR FS 323 TO FS 335 3EA IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED 3EA NEW PAX DOOR MID INTERCOSTALS BETWEEN FS 323 F
- [SDR VNAA2019062651103](https://openairdocs.org/sdr/VNAA2019062651103.md): Actuator · failed · Jun 25, 2019 · N555NN · Cndair CL6002D24 · Trailing Edge Flap Actuator
  > DURING AN OCF FLIGHT FOR A FLAPS FAIL MESSAGE CREW RECEIVED THE SAME MESSAGE. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. R&R RH INBD FLAP ACTUATOR, OPS CHECK GOOD.
- [SDR VNAA201906221103](https://openairdocs.org/sdr/VNAA201906221103.md): Flap System · malfunctioned · Jun 21, 2019 · N555NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > FLAP FAIL IN FLIGHT. PERFORMED OPS CHECK FOR FLAP AND SLAT SYST IAW AMM. OPS CHECK GOOD
- [SDR VNAA201906221101](https://openairdocs.org/sdr/VNAA201906221101.md): Flap System · malfunctioned · Jun 21, 2019 · N555NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > DURING THE APPROACH, THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE FLAPS WERE INDICATING 8 DEGREES. WHEN THE CREW TRIED TO PUT THE FLAPS DOWN TO 20 DEGREES THE FLAPS WOULD NOT GO DOWN. CREW RAN THE QRH AND DECLARED AN EMERGENCY. LANDED, CHECKED TIRES A
- [SDR VNAA2016091700019](https://openairdocs.org/sdr/VNAA2016091700019.md): Unknown · smoke · Sep 17, 2016 · N555NN · Cndair CL6002D24 · Air Distribution System
  > CREW REPORTED SMOKE IN THE CABIN AT AROUND 11000 FEET. DECLARED AN EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK OF ALL SYSTEMS, OPS CHECKED GOOD. FOUND NO EVIDENCE OF BURNT WIRES OR COMPONENTS. THE AI
- [SDR VNAA2016020100002](https://openairdocs.org/sdr/VNAA2016020100002.md): Controller · failed · Feb 1, 2016 · N555NN · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > CREW REPORTED LT WIDOW HEAT CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDOW TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015072800037](https://openairdocs.org/sdr/VNAA2015072800037.md): Warning Light · illuminated · Jul 28, 2015 · N555NN · Cndair CL6002D24 · Door Warning System
  > CREW REPORTED CENTER CARGO DOOR AMBER CAUTION MESSAGE DURING INITIAL CLIMB. RETURNED TO FIELD DUE TO NOT BEING ABLE TO PRESSURIZE CABIN AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF CENTER CARGO DOOR INDICATING SYS AND OPS CHECK OF CABIN PR

## 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 = 'N555NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N555NN/reports

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