# Service difficulty reports: N505AE

A list on [N505AE](https://openairdocs.org/aircraft/N505AE.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 3 · 125 reports

- [SDR VNAA2024121711101](https://openairdocs.org/sdr/VNAA2024121711101.md): Engine · fumes · Oct 26, 2024 · N505AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > ON DESCENT, THE FLIGHT CREW REPORTED FUMES IN COCKPIT IN FLIGHT, SMELLING OF TIRES AND OCCASIONAL BURNING. THE LOCATION OF THE FUMES WAS IN THE COCKPIT AND FORWARD JUMP SEAT AREA. THE CAPTAIN WAS EVALUATED BY PARAMEDICS DUE TO THE HEADACHE THAT FORMED FROM THE
- [SDR VNAA2024102211101](https://openairdocs.org/sdr/VNAA2024102211101.md): Acm · odor · Oct 20, 2024 · N505AE · Cndair CL6002C10 · Cabin Cooling System
  > ON TAKEOFF BRIEFLY SMELLED BURNING SMELL FOR 10 SEC. SMELL DISSIPATED AND ALL INDICATIONS FINE. DURING DESCENT CA AND FO BOTH WERE FEELING FAINT. POSSIBLE FUME ISSUE. EMERGENCY WAS DECLARED / REMOVED AND REPLACED THE LH ACM IAW CRJ 700 AMM 21-51-08-400-801-A01
- [SDR VNAA2024071511104](https://openairdocs.org/sdr/VNAA2024071511104.md): Windshield · unserviceable · Jul 14, 2024 · N505AE · Cndair CL6002C10 · Flight Compartment Windows
  > SPARK ON WINDSHIELD SENSOR CA SIDE LOWER SENSOR (BOTTOM) / T/S AND MEASURED THE RESISTANCE BETWEEN THE HEATER POWER TERMINALS (P1 AND P2) ON THE CA SIDE WINDSHIELD AND FOUND 40M OHMS (EXPECTED RESISTANCE WAS FROM 11OHMS TO 13.5OHMS) IAW CRJ700 AMM 56-11-01-400
- [SDR VNAA2024032711102](https://openairdocs.org/sdr/VNAA2024032711102.md): Acm · smoke · Mar 24, 2024 · N505AE · Cndair CL6002C10 · Cabin Cooling System
  > SMOKE/HAZE IN CABIN AFTER ENGINE START / PERFORMED ENGINE RUN AND TAXI FOR SMOKE/HAZE IN CABIN FOUND NO EVIDENCE IN CABIN.IAW CRJ 700 AMM 09-20-585-801-A01. PERFORMED MOC REQUESTED ENGINE RUNS IAW CRJ 700 AMM FIM 21-21-00-810-806-A01. CRJ 700 FIM 21-22-00-810-
- [SDR VNAA2024032711101](https://openairdocs.org/sdr/VNAA2024032711101.md): Acm · odor · Mar 24, 2024 · N505AE · Cndair CL6002C10 · Cabin Cooling System
  > STRONG BURNING ODOR ON T/O FA REPORTED HAZE IN THE CABIN. SLOWLY DISSIPATED OVER 30 MIN. SMELL REOCCUR ON APPROACH 4000 FT UNTIL TAXI IN / TROUBLESHOT IAW CRJ 700 FIM 21-21-00-810-806-A01. NO FAULTS FOUND AT THIS TIME. NO ODORS OR HAZE NOTED AT THIS TIME. APPL
- [SDR VNAA2024031311101](https://openairdocs.org/sdr/VNAA2024031311101.md): Probe · faulted · Mar 10, 2024 · N505AE · Cndair CL6002C10 · Overheat Detection
  > BRAKE OVHT WARNING MSG IN FLIGHT, L OUTBD SENSOR APPEARS ERRONEOUS AT 20 / PERFORMED TROUBLESHOOTING OF BRAKE OVHT WARNING MSG IAW FIM 32-46-01-810-802 A01. REMOVED LH OB THERMOCOUPLE SENSOR IAW 32-46-01-000-801 A01. REPLACED LH OB THERMOCOUPLE SENSOR IAW CRJ
- [SDR VNAA2024030511101](https://openairdocs.org/sdr/VNAA2024030511101.md): Acm · odor · Mar 1, 2024 · N505AE · Cndair CL6002C10 · Cabin Cooling System
  > FAINT ELECTRICAL BURNING SMELL COMING FROM COCKPIT / UPON FURTHER T/S PER FIM 21-21-00-810-806-AO1 FOUND LH PAC CUASING SMELL REMOVED AND REPLACED AIR CYCLE MACHINE IAW CRJ 700 AMM 21-52-08-000/400-801-A01. OPS CHECK GOOD. LEAK TEST GOOD.
- [SDR VNAA2024013011101](https://openairdocs.org/sdr/VNAA2024013011101.md): Unknown · odor · Jan 27, 2024 · N505AE · Cndair CL6002C10 · Air Distribution System
  > OIL SMELL COMING THROUGH THE PACKS WHEN USING APU BLEEDS / PERFORMED OPERATIONS CHECK ON LH/RH PACKS WITH APU IAW CRJ 700 AMM 21ˆ’50ˆ’00ˆ’862ˆ’801. OPERATIONS CHECK OF LH/RH PACKS IAW CRJ 700 AMM 21-51-00-710-801, NO OIL SMELL PRESENT AT THIS TIME. OPERATI
- [SDR VNAA2023122611101](https://openairdocs.org/sdr/VNAA2023122611101.md): Unknown · unknown · Dec 24, 2023 · N505AE · Cndair CL6002C10 · Hydraulic System, Main
  > DECREASING DURING FLIGHT, HYD SYSTEM OFF IN FLIGHT. MANUAL EXTENSION./ SERVICED HYDRAULIC SYSTEM NO 3 IAW CRJ700 AMM 12-12-29-611-802-A01.PRESSURIZED HYDRAULIC SYSTEM NO 3 IAW CRJ700 AMM 12-00-06-862-803, FOUND LOOSE B- NUT ON THE SELECTOR VALVE PRESSURE LINE.
- [SDR VNAA2023111411101](https://openairdocs.org/sdr/VNAA2023111411101.md): Fan · failed · Nov 11, 2023 · N505AE · Cndair CL6002C10 · Indicating/Recording System
  > DISPLAY COOL FAN CAUTION MSG UPON LANDING AND SMELL OF ELECTRICAL IN FLIGHT DECK / PERFORM SMOKE INSP FOR FLIGHT DECK IAW CRJ 700 FIM 21-21-00-810-806-A01. NO FIRE FOUND. SMOKE SMELL DISIPATED. REMOVED AND REPLACED DISPLAY SUPPLY FAN 2 (GROUND FAN) IAW CRJ-7
- [SDR VNAA202207211111](https://openairdocs.org/sdr/VNAA202207211111.md): Torque Link · disconnected · Jul 20, 2022 · N505AE · Cndair CL6002C10 · Nose/Tail Landing Gear Attach Section
  > WE WERE NOTIFIED BY FUSION/DIVERSION TRACKER THAT FLIGHT 5062 WAS RETURNING TO RTF. OUR DISPATCHER ACARSD THE CREW AND THEY TOLD US THEY WERE RTF DUE TO AN INPUT GEAR RETRACTION ISSUE. ATC DID END UP DECLARING AN EMERGENCY FOR THE A/C AS THE CREW ASKED IF THEY
- [SDR VNAA202204011111](https://openairdocs.org/sdr/VNAA202204011111.md): None · unknown · Mar 30, 2022 · N505AE · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > AFTER TAKE OFF, CREW COMMANDED GEAR UP, AND GOT A GEAR DISAGREE MESSAGE. THEY LEVELED OFF AT 3000' AND RAN THE QRH. QRH SAID LAND NEAREST SUITABLE. CREW DECLARED AN EMERGENCY AND DECIDED TO BURN OFF FUEL BEFORE DIVERTING TO IAD. ONCE AIRCRAFT WAS NO LONGER OVE
- [SDR VNAA202203291111](https://openairdocs.org/sdr/VNAA202203291111.md): Selector Valve · failed · Mar 26, 2022 · N505AE · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MSG IN FLIGHT, CAME ON IN 6 SECS OR LESS / C/W FIM TASK 32-31-00-810-803-A01 POSSIBLE CAUSE #3 FOUND PINS A TO PIN B FAILED/OPEN CIRCUIT. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ700 AMM 32-32-10-000/400-801-A01.
- [SDR VNAA202112281111](https://openairdocs.org/sdr/VNAA202112281111.md): Acm · smoke · Dec 24, 2021 · N505AE · Cndair CL6002C10 · Cabin Cooling System
  > UPON STARTING UP THE LH PACK THERE WAS A SMELL THE CREW NOTICED. WHEN THEY LOOKED BACK INTO THE CABIN THEY BECAME AWARE THERE WAS A SLIGHT HAZE. THEY THEN SHUT DOWN THE LH PACK, DEPLANED THE PAX IN A NORMAL MANNER. NO EMERGENCY WAS DECLARED. CREW CALLED MX CON
- [SDR VNAA202112011112](https://openairdocs.org/sdr/VNAA202112011112.md): Door Seal · popped · Nov 29, 2021 · N505AE · Cndair CL6002C10 · Passenger/Crew Doors
  > ENROUTE TO DCA AT FL330, CREW RECEIVED INDICATION OF A PASSENGER DOOR SEAL SQUEALING. CREW INITIALLY DECLARED EMERGENCY AND DIVERTED TO CLT. CREW CANCELLED EMERGENCY PRIOR TO LANDING CLT. MAIN CABIN DOOR SEAL POPPED IN FLIGHT / INSP. PAX DOOR SEAL AND FOUND
- [SDR VNAA202109081111](https://openairdocs.org/sdr/VNAA202109081111.md): Pcu · faulted · Sep 3, 2021 · N505AE · Cndair CL6002C10 · Drag Control System
  > INBOUND TO CAK, THE CREW RECEIVED A CAUTION MESSAGE FOR SPOILERONS OB AND OB FLT SPOILERS, SO THEY DECLARED AN EMERGENCY WITH ATC. MX HAS BEEN NOTIFIED, AND THEY REQUESTED TO SWAP THE RETURN TRIP ONTO A DIFFERENT AIRCRAFT SO THEY COULD TROUBLESHOOT THIS ISSUE.
- [SDR VNAA2020072979996](https://openairdocs.org/sdr/VNAA2020072979996.md): Intercostal · corroded · Jul 29, 2020 · N505AE · Bombdr CL6002D15 · Passenger/Crew Doors
  > PAX DOOR FOUND TO HAVE INTERNAL CORROSION. REPAIRED AS NECESSARY
- [SDR VNAA202007279995](https://openairdocs.org/sdr/VNAA202007279995.md): Floor Support · corroded · Jul 27, 2020 · N505AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > LEFT HAND OUTBOARD TOP CAP BETWEEN FS1000 TO FS1047 IS CORRODED. REPLACED CAP.
- [SDR VNAA202007279994](https://openairdocs.org/sdr/VNAA202007279994.md): Floor Support · corroded · Jul 27, 2020 · N505AE · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > LEFT HAND INBOARD TOP CAP BETWEEN FS1000 TO FS1047 IS CORRODED. REPLACED TOP CAP.
- [SDR VNAA202007279993](https://openairdocs.org/sdr/VNAA202007279993.md): Structure · corroded · Jul 27, 2020 · N505AE · Bombdr CL6002D15 · Passenger/Crew Doors
  > PASSENGER DOOR FOUND TO HAVE SEVERAL AREAS OF LOCALIZED CORROSION. EVALUATED AND FOUND CORROSION IN SOME AREAS TO BE OUT OF SRM LIMITS AND SENT DOOR TO VENDOR FOR REPAIRS.
- [SDR VNAA202007279992](https://openairdocs.org/sdr/VNAA202007279992.md): Seat Track · corroded · Jul 27, 2020 · N505AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > NUMBER 1 RIGHT FLOOR SEAT TRACK HAS NUMEROUS SPOTS OF PITTING CORROSION AND GOUGES THOUGH OUT ITS LENGTH. EVALUATED AND FOUND NUMBER 1 RIGHT FLOOR SEAT TRACK TO BE OUT OF LIMITS. REPLACED SEAT TRACK.
- [SDR VNAA202007279991](https://openairdocs.org/sdr/VNAA202007279991.md): Seat Track · corroded · Jul 27, 2020 · N505AE · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > NUMBER 1 LEFT FLOOR SEAT TRACK HAS NUMEROUS SPOTS OF PITTING CORROSION AND GOUGES THOUGH OUT ITS LENGTH. EVALUATED AND DETERMINED NUMBER 1 LEFT FLOOR SEAT TRACK TO BE BEYOND LIMITS. REPLACED SEAT TRACK.
- [SDR VNAA2020041411101](https://openairdocs.org/sdr/VNAA2020041411101.md): Manifold · failed · Apr 13, 2020 · N505AE · Cndair CL6002C10 · Landing Gear Steering System
  > ON T/O AFTER SELECTING GEAR UP THE CREW RECEIVED AN AMBER NOSEHWEEL STEERING INOP CAUTION MESSAGE. THE CREW CONTINUED TO CLIMB TO FL230. ONCE LEVEL, CREW DECLARED AN EMERGENCY WITH ATC AND DIVERTED TO CLT. - REMOVED AND REPLACE NOSE WHEEL STEERING MANIFOLD, OP
- [SDR VNAA2020040221101](https://openairdocs.org/sdr/VNAA2020040221101.md): Unknown · malfunctioned · Mar 29, 2020 · N505AE · Cndair CL6002C10 · Cabin Pressure Control System
  > AUTO PRESS CAUTION MSG, DID NOT PRESSURIZE, RETURNED TO FIELD. AUTO PRESS CAUTION MSG NOT PRESENT UPON ARRIVAL. T/S PER CRJ 700 FIM. NO CURRENT FAULTS OR FAULT HISTORY. PRESSURIZED A/C PER CRJ 700 AMM. NO DEFECTS NOTED. OKAY FOR SERVICE.
- [SDR VNAA2019112201101](https://openairdocs.org/sdr/VNAA2019112201101.md): Control Unit · failed · Nov 20, 2019 · N505AE · Cndair CL6002C10 · Stabilizer Control System
  > CREW HAD AN INTERMITTENT PITCH FEEL CAUTION MESSAGE. THEY DECLARED A PRECAUTIONARY EMERGENCY WITH CLT APPROACH AND LANDED WITHOUT INCIDENT. TRUCKS WERE ROLLED BUT THE CABIN WAS NOT BRACED. MX R&R SSCU1 IAW CRJ 700 AMM 27-61-05-000/400-801, OPS CHECK GOOD.
- [SDR VNAA2019111521103](https://openairdocs.org/sdr/VNAA2019111521103.md): Warning Message · false activation · Nov 12, 2019 · N505AE · Cndair CL6002C10 · Elevator Control System
  > FLIGHT 5513 RECEIVED MULTIPLE PITCH FEEL FAULT CAUTION MESSAGES IN FLIGHT. THE CREW RAN THE QRH AND CONTINUED TO DCA WHERE THEY LANDED WITHOUT INCIDENT BUT DID DECLARED AN EMERGENCY AS A PRECAUTION, EMERGENCY VEHICLES DID RESPOND BUT WERE CALLED OFF AFTER THE
- [SDR VNAA2019101181101](https://openairdocs.org/sdr/VNAA2019101181101.md): Flashlight · failed · Oct 8, 2019 · N505AE · Cndair CL6002C10 · Emergency Equipment
  > AFT FA FLASHLIGHT NOT CHARGING. R/R FLASHLIGHT IAW CRJ 700 AMM 25-61-02-400/000-801-A22. AND PERFORMED OPERATIONAL TEST OF THE FLASH LIGHT IAW CRJ 700 AMM 25-61-00-710-801(CONFIG A02). OPS CHECK IS GOOD AT THIS TIME. THIS CLEARS MEL.
- [SDR VNAA2019100321101](https://openairdocs.org/sdr/VNAA2019100321101.md): Outflow Valve · malfunctioned · Oct 2, 2019 · N505AE · Cndair CL6002C10 · Pressure Regulator/Outflow Valve
  > WHILE CLIMBING THROUGH FL250 THE CREW RECEIVED A CABIN ALTITUDE WARNING MESSAGE. CREW IMMEDIATELY PUT ON THEIR OXYGEN MASK AND RAN THE QRH. THEY BEGAN A DECENT OF 2,500FT PER MINUTE DOWN TO 10,000FT. CREW DECIDED TO DIVERT TO DULLES DUE TO THE LONG RUNWAYS AND
- [SDR VNAA2019080411102](https://openairdocs.org/sdr/VNAA2019080411102.md): Housing · defective · Aug 4, 2019 · N505AE · Cndair CL6002C10 · Emergency Lighting
  > #5 CEILING EMERGENCY FLOOD LIGHT WILL NOT ILLUMINATE REMOVED AND REPLACED LAMP HOUSING OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2019052899902](https://openairdocs.org/sdr/VNAA2019052899902.md): Angle · cracked · May 28, 2019 · N505AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280 FWD J ANGLE HAS MINOR CORROSION ON UPPER SURFACE RBL TO LBL 12 ALONG WITH A GOUGE THAT IS OUT OF SRM LIMITATIONS C/A: INSTALLED NEW J ANGLE AT FS 280 IAW SRM 51-42-06-001-001-A01.
- [SDR VNAA2019052899901](https://openairdocs.org/sdr/VNAA2019052899901.md): Tee Fitting · cracked · May 28, 2019 · N505AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280 RBL 9.0 T FITTING CRACKED ON UPPER OTBD CORNER. C/A: REMOVED AND REPLACED T FITTING AT FS 280 RBL 9 IAW SRM 51-42-06-001-001-A01.
- [SDR VNAA2019040511101](https://openairdocs.org/sdr/VNAA2019040511101.md): Control Unit · failed · Apr 5, 2019 · N505AE · Cndair CL6002C10 · Stabilizer Control System
  > ENROUTE, THE CREW RECIEVED A PITCH FEEL FAULT AND A RUDDER LIMIT FAULT MESSAGE. THEY DECLARED AN EMERGENCY AND THE TRUCKS WERE DISPATCHED. THE A/C WAS ABLE TO TAXI TO THE GATE WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE #1 SSCU. OPS CHECK GOOD.
- [SDR VNAA2019031511101](https://openairdocs.org/sdr/VNAA2019031511101.md): Circuit Breaker · tripped · Mar 15, 2019 · N505AE · Cndair CL6002C10 · Autopilot System
  > DURING APPROACH THE CREW RECEIVED MULTIPLE PITCH FEEL CAUTION AND RUDDER / LIMIT FAULT MESSAGES. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT / INCIDENT. THE AIRCRAFT WAS ABLE TO TAXI TO THE GATE. TRUCKS ROLLED. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE FOR
- [SDR VNAA2019011111101](https://openairdocs.org/sdr/VNAA2019011111101.md): Unknown · malfunctioned · Jan 11, 2019 · N505AE · Cndair CL6002D24 · Engine Vibration Analyzer
  > DURING CRUISE THE CREW REPORTED A RIGHT ENGINE VIB OF 1.9. ATC DECLARED AN EMERGENCY FOR THEM AND THEY LANDED IN DCA WITHOUT ISSUE. THE CREW GROUND RAN THE AIRCRAFT WITH MAITENANCE AND THE VIBE CHECK WAS WITHIN LIMITS
- [SDR SIMA2018062518005](https://openairdocs.org/sdr/SIMA2018062518005.md): Frame · corroded · Jun 18, 2018 · N505AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 319.7 WAS CORRODED BETWEEN STRINGERS 25L AND 25R. REPAIRED IAW ERS-CR-53MR-3322.
- [SDR SIMA20180618004](https://openairdocs.org/sdr/SIMA20180618004.md): Angle · cracked · Jun 18, 2018 · N505AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT 2ND FROM INBD VERTICAL ANGLE AT FS 2800.00 IS CRACKED. R&R ANGLE IAW ETN-CR-043RI AND SRM 51-42-06.
- [SDR SIMA20180612007](https://openairdocs.org/sdr/SIMA20180612007.md): Crossmember · corroded · Jun 12, 2018 · N505AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT SIDE OF CROSSMEMBER AT FS280.00 IS CORRODED. REPLACED LEFT SIDE CROSSMEMBER AT FS280 IAW SRM 51-42-06 AND 51-42-13.
- [SDR SIMA20180605007](https://openairdocs.org/sdr/SIMA20180605007.md): Tee Fitting · cracked · Jun 5, 2018 · N505AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "T" FITTING FROM LEFT INBD FLOOR SUPPORT TO CROSSMEMBER AT FS280.00 APPEARS TO HAVE 1/4" CRACK ON UPPER INBD RADIUS. INSTALLED NEW FABRICATED BRACKETS IAW SRM 51-42-21 AND 51-42-06.
- [SDR SIMA20180324003](https://openairdocs.org/sdr/SIMA20180324003.md): Flashlight · inoperative · Mar 24, 2018 · N505AE · Cndair CL6002C10 · Emergency Equipment
  > FA REPORTED THE AFT FLASHLIGHT IS NOT CHARGING. REMOVED AND REPLACED THE FLASHLIGHT. PERFORMED AN OPS CHECK IAW AMM 25-61-00. OPS CHECKED GOOD.
- [SDR SIMA20180211004](https://openairdocs.org/sdr/SIMA20180211004.md): Computer · failed · Feb 11, 2018 · N505AE · Cndair CL6002C10 · Autopilot System
  > AUTOPILOT WILL NOT MAINTAIN LATERAL NAVIGATION. REMOVED AND REPLACED THE AILERON SERVO IAW AMM 22-11-21. REMOVED AND REPLACED THE FCC IAW AMM 22-12-14. OPS CHECKED GOOD. REMOVED AND REPLACED AILERON SERVO MOUNT AND CABLES IAW AMM 22-11-11. OPS CHECKED G
- [SDR SIMA20171015002](https://openairdocs.org/sdr/SIMA20171015002.md): Wire · disconnected · Oct 15, 2017 · N505AE · Cndair CL6002C10 · Light System Wiring
  > ROW 16 EMERGENCY CEILING DOME LIGHT INOPERATIVE. FOUND A WIRE PULLED OUT AND CONTACT PIN BROKEN OFF IN THE CONNECTOR. INSTALLED A NEW PIN ON WIRE AND INSTALLED IN CONNECTOR IAW ESPM 20-33-00. OPS CHECKED GOOD.
- [SDR SIMA20170604003](https://openairdocs.org/sdr/SIMA20170604003.md): Transducer · failed · Jun 4, 2017 · N505AE · Cndair CL6002C10 · Brake Anti-Skid Section
  > ANTI SKID INBD CAUTION MESSAGE. REMOVED AND REPLACED WHEEL SPEED TRANSDUCER IAW AMM 32-44-01. OPS CHECKED GOOD
- [SDR SIMA20170221002](https://openairdocs.org/sdr/SIMA20170221002.md): Manifold · failed · Feb 21, 2017 · N505AE · Cndair CL6002C10 · Landing Gear Steering System
  > "STEERING INOP" CAUTION MSG POSTED AFTER TAKE OFF AND GEAR RETRACTION. REMOVED AND REPLACED NLG STEERING MANIFOLD IAW AMM 32-51-50. PERFORM OPS TEST OF NLG STEERING MANIFOLD IAW AMM 32-51-00 NO DEFECTS NOTED. PERFORMED NLG EXTENSION AND RETRACTION IAW AMM 32-
- [SDR SIMA20170219001](https://openairdocs.org/sdr/SIMA20170219001.md): Circuit Breaker · open · Feb 19, 2017 · N505AE · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP MSG AFTER TAKEOFF DURING GEAR RETRACTION. RESET NOSE STEER CB'S IAW FIM 32-50-00, STEERING INOP MESSAGE DID NOT SHOW. CHECKS GOOD.
- [SDR SIMA20170107007](https://openairdocs.org/sdr/SIMA20170107007.md): Wire · pulled · Jan 7, 2017 · N505AE · Cndair CL6002C10 · Light System Wiring
  > CEILING LEVEL EMERGENCY FLOOD LIGHT NR 3 INOPERATIVE. PINNED WIRE PULLED FROM CONNECTOR J361 IAW ESPM. REMOVED AND REPLACED THE BULB IAW AMM 33-51-09. OPS CHECKED GOOD.
- [SDR SIMA20161020002](https://openairdocs.org/sdr/SIMA20161020002.md): Sign · inoperative · Oct 20, 2016 · N505AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHT NEAR PAX DOOR FLOOR IS INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-05. OPS CHECKED GOOD.
- [SDR SIMA20160918006](https://openairdocs.org/sdr/SIMA20160918006.md): Support Fitting · cracked · Sep 18, 2016 · N505AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ADG DOOR ROD AFT LEVER SUPPORT FITTING CRACKED ON OUTBOARD SIDE OF THE PIVOT HOLE. EVALUATED ADG DOOR ROD AFT LEVER SUPPORT FITTING AND FOUND IT TO BE NOT CRACKED, NDI PERFORMED AND REINSTALLED ORIGINAL FITTING BACK IN AIRCRAFT IAW SRM 51-42-20, AND INSTALLE
- [SDR SIMA20160918007](https://openairdocs.org/sdr/SIMA20160918007.md): Drag Angle · cracked · Sep 18, 2016 · N505AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACKED BY THE POWER ASSIST CABLE-C/A-REPAIRED PAX DOOR AFT DRAG ANGLE IAW CRJ SRM 52-11-04.
- [SDR SIMA20160918004](https://openairdocs.org/sdr/SIMA20160918004.md): Floorbeam · cracked · Sep 18, 2016 · N505AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RIGHT SIDE OF FLOORBEAM AT BS 280 HAS CORROSION ON UPPER SURFACE THE ENTIRE LENGTH. AND A 1 INCH CRACK ON UPPER SURFACE JUST OUTBD OF RBL 9. REMOVED AND INSTALLED NEW RIGHT HAND SECTION OF THE FLOORBEAM IAW SRM 51-42-06 AND 51-42-13.
- [SDR SIMA20160918005](https://openairdocs.org/sdr/SIMA20160918005.md): Floorbeam · cracked · Sep 18, 2016 · N505AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > ANGLE ATTACHED TO FORWARD SIDE OF FLOORBEAM BS 280 AT LBL 9 HAS A 1/2 INCH CRACK. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE IAW SRM 53-11-41.

Next page: https://openairdocs.org/aircraft/N505AE/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 = 'N505AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N505AE/reports

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