# Service difficulty reports: N413AW

A list on [N413AW](https://openairdocs.org/aircraft/N413AW.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 · 159 reports

- [SDR A6WA202406248769](https://openairdocs.org/sdr/A6WA202406248769.md): Idg · underserviced · Jun 24, 2024 · N413AW · Cndair CL6002B19 · AC Generator-Alternator
  > RTO AT 60 KTS DUE TO IDG 2 CAUTION MSG, CLEARED AFTER 5 SECONDS. DID NOT RECEIVE BRAKE OVHT WARNING MSG ***** AIRCRAFT REMOVED FROM SERVICE ***** SERVICED #2 IDG IAW SUP 16-364A. PERFORMED OPS CHECK OF #2 IDG IN REF TOO AMM 24-11-01. OPS CHECK GOOD AT THIS TI
- [SDR A6WA202406238768](https://openairdocs.org/sdr/A6WA202406238768.md): Drive Assy · faulted · Jun 23, 2024 · N413AW · Cndair CL6002B19 · Engine Thrust Reverser
  > RT REV UNLOCKED CAUTION AT FL240 FEET. PRESSED EMER STOW, MESSAGE DID NOT CLEAR. NO YAW NOTED. AMBER REV DISPLAYED IN N1 GAUGE. TR APPEARS STOOD ON WALK AROUND. COMPLIED WITH DEACTIVATION OF RH THRUST REVERSE NO PDU ADJUSTMENT REQUIRED IAW AMM AWA SUP 15-046D
- [SDR A6WA202404288734](https://openairdocs.org/sdr/A6WA202404288734.md): Control Lever · failed · Apr 28, 2024 · N413AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL 7 DEG ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R FLAP LEVER PER AMM SUP 09-038A. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND FROM MEL
- [SDR A6WA202310268665](https://openairdocs.org/sdr/A6WA202310268665.md): Unknown · unknown · Oct 26, 2023 · N413AW · Cndair CL6002B19 · Electrical Power System
  > LOW SPEED ABORT FOR IDG 2 CAUTION MSG CLEARED WHEN POWER REDUCED. ******AIRCRAFT REMOVED FROM SERVICE******** C/W M ACTION FOR MEL 24-11-01-01 REF 363019/2 FOR MEL. T.S. PER FIM 24-10-00. FOUND #2 IDG OIL LEVEL LOW. PERFORMED LEAK CHECK OF RH IDG OIL
- [SDR A6WA202307168642](https://openairdocs.org/sdr/A6WA202307168642.md): Eec · unknown · Jul 16, 2023 · N413AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION MESSAGE ON APPROACH WHEN EXTENDING TO 45 DEGREES. GAUGS INDICATED 45 DEGREES. QRH C/W AND NORMAL LANDING. PREFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ******AIRCRAFT REMOVED FROM SERV
- [SDR A6WA202306108629](https://openairdocs.org/sdr/A6WA202306108629.md): Unknown · unknown · Jun 10, 2023 · N413AW · Cndair CL6002B19 · Landing Gear System
  > ON TO RCVD GEAR DISAGREE AND NLG DOOR OPEN WARNING MSGS C/W QRH FOR NLG DOOR OPEN BOTH MSGS DISAPPEARED. RETURNED DAYTON.NO EMER DECLARED. **********AIRCRAFT REMOVED FROM SERVICE********* SERV NLG IAW AMM 1
- [SDR A6WA202305288615](https://openairdocs.org/sdr/A6WA202305288615.md): Engine · damaged · May 28, 2023 · N413AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ITT ON RIGHT ENGINE INCREASED TO 840C ON 85% N1 ON BOTH ENGINES, WITH VIBRATIONS AT FLIGHT LEVEL 190. REDUCED POWER VIBRATION ON N2 TWICE FOR 1 SEC EACH. AND N1 VIBE AT 2.7MIL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED BOROSCOPE INSPECTION OF RH ENGINE COLD S
- [SDR A6WA202110217916](https://openairdocs.org/sdr/A6WA202110217916.md): None · none · Oct 19, 2021 · N413AW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > ON T/O RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MSG'S. C/W QRH LOWERED GEAR AND RETURNED TO FIELD. AFTER SELECTING HANDLE UP WARNING CAME ON IMMEDIATELY. RECEIVED INBD A-SKID AND NWS INOP MSG'S BRIEFLY. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVE
- [SDR A6WA202110197915](https://openairdocs.org/sdr/A6WA202110197915.md): None · none · Oct 18, 2021 · N413AW · Cndair CL6002B19 · Main Landing Gear Attach Section
  > AFTER SELECTING LANDING GEAR UP, GOT GEAR DISAGREE MSG, C/W QRH LANDING GEAR DOWN 3 GREENS. NLG DID NOT COME UP. RETURNED TO ORIGINATING AIRPORT. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW AMM 32-22-20. OPS CHECK GO
- [SDR A6WA202101047502](https://openairdocs.org/sdr/A6WA202101047502.md): Control Unit · malfunctioned · Jan 1, 2021 · N413AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > RECEIVED LT AND RT WING ANTI-ICE CAUTION MESSAGES DURING CRUISE. C/W QRH, MESSAGES PERSISTED. WING ANTI-ICE ON ADVISORY MESSAGE NOT PRESENT. DIVERTED TO PIT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TEMP CONTROL UNIT, IAW AMM 30-12-19. OPERATI
- [SDR A6WA202011307430](https://openairdocs.org/sdr/A6WA202011307430.md): Hinge · corroded · Nov 28, 2020 · N413AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR UPPER STEP PLATFORM TO SILL HINGE CORRODED. AIRCRAFT REMOVED FROM SERVICE. LOCATED AND DRILLED NEW HINGE. REMOVED AND REPLACED UPPER STEP PLATFORM TO HINGE, IAW SRM 51-40-11.
- [SDR A6WA202011247427](https://openairdocs.org/sdr/A6WA202011247427.md): Seat Track · corroded · Nov 23, 2020 · N413AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK CORRODED AT LBL 9 FS 364 THRU FS 409. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK. INSTALL NEW SEAT TRACK AT LBL 9.00 FS 364 THRU FS 409, IAW REO 601R-53-00-764.
- [SDR A6WA202011307433](https://openairdocs.org/sdr/A6WA202011307433.md): Seat Track · corroded · Nov 16, 2020 · N413AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK AT RIGHT BUTT LINE 9 FS 364-FS 409. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW REO-601R-53-00-764 REPAIR B STEP 1.
- [SDR A6WA202011307432](https://openairdocs.org/sdr/A6WA202011307432.md): Seat Track · corroded · Nov 16, 2020 · N413AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK CORRODED AT LBL 9 FS 409 THRU FS 559. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SEAT TRACK, PER REO 601R-53-00-764 REPAIR B STEP 1.
- [SDR A6WA2019080546769](https://openairdocs.org/sdr/A6WA2019080546769.md): Skin · damaged · Jul 30, 2019 · N413AW · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR UPPER FORWARD CORNER INNER SKIN DAMAGED. REPAIRED.
- [SDR A6WA2019032646519](https://openairdocs.org/sdr/A6WA2019032646519.md): Intercostal · corroded · Mar 26, 2019 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL IS CORRODED JUST AFT OF FS 310 FRAME AT STGR 21L.
- [SDR A6WA2019101746931](https://openairdocs.org/sdr/A6WA2019101746931.md): Hinge · damaged · Mar 19, 2019 · N413AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON FUSELAGE SIDE HAS MULTIPLE HOLES OUT OF ROUND.
- [SDR A6WA2019031246469](https://openairdocs.org/sdr/A6WA2019031246469.md): Angle · corroded · Mar 12, 2019 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER FLOOR SILL ANGLE IS CORRODED.
- [SDR A6WA2019030746454](https://openairdocs.org/sdr/A6WA2019030746454.md): Door Sill · corroded · Mar 5, 2019 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR SILL IS CORRODED AT F.S.449.85.
- [SDR A6WA2019030146435](https://openairdocs.org/sdr/A6WA2019030146435.md): Frame · cracked · Feb 28, 2019 · N413AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333.00 FRAME IS CRACKED AT STRINGER 0.
- [SDR A6WA2019022546414](https://openairdocs.org/sdr/A6WA2019022546414.md): Floor Panel · cracked · Feb 24, 2019 · N413AW · Cndair CL6002B19 · Fuselage Floor Panel
  > LH FWD EQUIPMENT COMPARTMENT FLOOR IS CRACKED AT FS 193.00.
- [SDR A6WA2019022546415](https://openairdocs.org/sdr/A6WA2019022546415.md): Floor Support · corroded · Feb 24, 2019 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOORBOARD SUPPORT ANGLE OVER THE PRESSURE FLOOR SILL IS CORRODED AT FS 559.
- [SDR A6WA2018112546167](https://openairdocs.org/sdr/A6WA2018112546167.md): Valve · leaking · Nov 20, 2018 · N413AW · Cndair CL6002B19 · APU Engine Fuel and Control
  > ON APPROACH APPROXIMATELY 10 MINUTES AFTER APU START WITH LCV OPEN RECEIVED FUEL SMELL IN COCKPIT. ON GROUND APU DOOR SHOWED DASHES. BOTH PACKS RUNNING WITH BLEEDS ON ENGINES. AFTER APU SHUTDOWN SMELL WENT AWAY. INSPECTED AND FOUND FUEL SHUTOFF VALVE/SOLENOID
- [SDR A6WA2018071845934](https://openairdocs.org/sdr/A6WA2018071845934.md): Wire Harness · crushed · Jul 13, 2018 · N413AW · Cndair CL6002B19 · Landing Gear System Wiring
  > UPON SELECTING LANDING GEAR UP RECEIVED GEAR DISAGREE WARNING AND NOSE DOOR OPEN WARNING MESSAGES C/W QRH MESSAGES CLEARED ON GEAR EXTENSION. PLAN TO CHANGE CRUSHED NLG HARNESS.
- [SDR A6WA2018071345934](https://openairdocs.org/sdr/A6WA2018071345934.md): Wire Harness · crushed · Jul 13, 2018 · N413AW · Cndair CL6002B19 · Landing Gear System Wiring
  > UPON SELECTING LANDING GEAR UP RECEIVED GEAR DISAGREE WARNING AND NOSE DOOR OPEN WARNING MESSAGES. C/W QRH MESSAGES CLEARED ON GEAR EXTENSION PLAN TO CHANGE CRUSHED NLG HARNESS.
- [SDR A6WA2018012445588](https://openairdocs.org/sdr/A6WA2018012445588.md): Control Unit · malfunctioned · Jan 21, 2018 · N413AW · Cndair CL6002B19 · AC Generation System
  > AFTER TAKEOFF, THE AIR DRIVEN GENERATOR DEPLOYED UNCOMMANDED. COMPLIED WITH QRH, GENERATORS DID NOT PICK UP THE LOAD, AND POWER TRANSFER OVERRIDE SWITCH DID NOT WORK. DIVERTED. THE GENERATOR TRANSFER OCCURRED BELOW 80 KNOTS AFTER LANDING. REPLACED ADG AUTO
- [SDR A6WA2018012545571](https://openairdocs.org/sdr/A6WA2018012545571.md): Autopilot Sys · malfunctioned · Jan 16, 2018 · N413AW · Cndair CL6002B19 · Autopilot System
  > 3843 ON APPROACH SWITCHING FROM NAV TO HEADING TO APPROACH MODE A/C TRIED TO CLIMB IN PITCH MODE WITH AUTO PILOT ON FOLLOWED BY C-CORD AURAL ALERT TURNED AUTO PILOT OFF AND BACK ON A/C BEGAN TO CLIMB IN PITCH MODE AGAIN. AUTO PILOT DISCONTINUED FOR APPROACH.
- [SDR A6WA2018011845571](https://openairdocs.org/sdr/A6WA2018011845571.md): Autopilot Sys · malfunctioned · Jan 16, 2018 · N413AW · Cndair CL6002B19 · Autopilot System
  > ON APPRACH SWITCHING FROM NAV TO HEADING TO APPROACH MODE A/C TRYED TO CLIMB IN PITCH MODE WITH AUTO PILOT ON FOLLOWED BY C-CORD AURAL ALERT TURNED AUTO PILOT OFF AND BACK ON A/C BEGAN TO CLIMB IN PITCH MODE AGAIN. AUTO PILOT DISCONTINUED FOR APPROACH. AURAL W
- [SDR A6WA2017091345270](https://openairdocs.org/sdr/A6WA2017091345270.md): Actuator · malfunctioned · Sep 8, 2017 · N413AW · Cndair CL6002B19 · Auto Flight System
  > RECEIVED AN UNCOMMANDED YAW IN FLIGHT, 2 BALL WIDTHS ON THE SIDE SLIP INDICATOR. COMPLIEC WITH QRH. YD 1 AND 2 OFF UNCOMMANDED YAW CONTINUED FOR 10 MINUTES THEN CLEARED. COULD FEEL YAW MOTION IN RUDDER PEDALS. REMOVED AND REPLACED THE NR 1 YAW DAMPER ACTUAT
- [SDR A6WA2017082245215](https://openairdocs.org/sdr/A6WA2017082245215.md): Frame · cracked · Aug 20, 2017 · N413AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND A DENT UNDER CARGO DOOR. BS 605 FRAME WAS CRACKED
- [SDR A6WA2017040644906](https://openairdocs.org/sdr/A6WA2017040644906.md): Unknown · odor · Apr 5, 2017 · N413AW · Cndair CL6002B19 · Cabin Cooling System
  > STRONG BURNING ODOR FROM PACKS, WHILE ON APU BLEED, RIGHT AFTER TAKEOFF, IN CABIN AND COCKPIT.
- [SDR A6WA2017022444817](https://openairdocs.org/sdr/A6WA2017022444817.md): Skin · chafed · Feb 23, 2017 · N413AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND CHAFE DAMAGE THAT EXCEED ALLOWABLE LIMITS IAW EO E16/011/453 REV:A ON RT APRON SKIN PANEL.
- [SDR A6WA2017022444814](https://openairdocs.org/sdr/A6WA2017022444814.md): Floorbeam · corroded · Feb 23, 2017 · N413AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > TWO NUT PLATE LOCATIONS ON THE FLOORBEAM CORRODED AT LBL 27, BS 559+90 TO 559+112. REPAIRED THE FLOORBEAM IAW SRM 53-00-43, REPAIR 2.
- [SDR A6WA2017022444815](https://openairdocs.org/sdr/A6WA2017022444815.md): Skin · dented · Feb 23, 2017 · N413AW · Cndair CL6002B19 · Rudder, Plate/Skin
  > RUDDER IS DENTED ON RT SIDE. REPAIRED IAW SRM 55-40-00.
- [SDR A6WA2017022444813](https://openairdocs.org/sdr/A6WA2017022444813.md): Floor Support · corroded · Feb 23, 2017 · N413AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT OTBD FLOOR SUPPORT CORRODED AT BS 559+80 TO 559+112. REMOVER AND REPLACED THE FLOOR SUPPORT IAW EA 253-00638 REV-IR.
- [SDR A6WA2017022444816](https://openairdocs.org/sdr/A6WA2017022444816.md): Vane · chafed · Feb 23, 2017 · N413AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE LE CHAFED IN MULTIPLE AREAS. REPLACED THE FLAP VANE.
- [SDR A6WA2017022444811](https://openairdocs.org/sdr/A6WA2017022444811.md): Doubler · corroded · Feb 22, 2017 · N413AW · Cndair CL6002B19 · Fuselage Main, Structure
  > AFT INBD DOUBLER ON WARDROBE IS CORRODED. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-42-10.
- [SDR A6WA2017022444806](https://openairdocs.org/sdr/A6WA2017022444806.md): Intercostal · cracked · Feb 18, 2017 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 1013972-3000-0023 - INTERCOSTAL AT STGR 13L AND FS 625 IS CRACKED
- [SDR A6WA2017022444808](https://openairdocs.org/sdr/A6WA2017022444808.md): Skin · chafed · Feb 18, 2017 · N413AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT WING TE FLAP VANE CTR LE IS CHAFED.
- [SDR A6WA201744807](https://openairdocs.org/sdr/A6WA201744807.md): Skin · chafed · Feb 18, 2017 · N413AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING TE FLAP VANE IS CHAFED
- [SDR A6WA201744805](https://openairdocs.org/sdr/A6WA201744805.md): Intercostal · cracked · Feb 17, 2017 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 14L, BS 625 CRACKED.
- [SDR A6WA201744803](https://openairdocs.org/sdr/A6WA201744803.md): Seat Track · corroded · Feb 15, 2017 · N413AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT AISLE SEAT TRACK NR 3 HAS CORROSION AND IS GOUGED BETWEEN BS 409+128 AND 559.
- [SDR A6WA2017022444804](https://openairdocs.org/sdr/A6WA2017022444804.md): Seat Track · corroded · Feb 15, 2017 · N413AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT AISLE SEAT TRACK NR 2 HAS CORROSION BETWEEN BS 394 THRU 409+128
- [SDR A6WA2017022444802](https://openairdocs.org/sdr/A6WA2017022444802.md): Angle · cracked · Feb 13, 2017 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE INBD SIDE OF RBL 36 AT BS 473.15 CRACKED. REPLACED THE ANGLE.
- [SDR A6WA2017021544800](https://openairdocs.org/sdr/A6WA2017021544800.md): Angle · cracked · Feb 13, 2017 · N413AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ANGLE ON THE OTBD SIDE OF RBL 9 AND AFT SIDE OF FLOORBEAM BS 280 IS CRACKED
- [SDR A6WA201744798](https://openairdocs.org/sdr/A6WA201744798.md): Bracket · cracked · Feb 12, 2017 · N413AW · Cndair CL6002B19 · Nacelle/Pylon, Attach Fittings
  > STANDOFF BRACKET AT 7 O'CLOCK POSITION ON RH ENGINE NOSE INLET COWL
- [SDR A6WA2017021544797](https://openairdocs.org/sdr/A6WA2017021544797.md): Bracket · cracked · Feb 12, 2017 · N413AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STANDOFF BRACKET AT 8 O'CLOCK POSITION ON LH ENGINE NOSE INLET COWL IS CRACKED
- [SDR A6WA2017010544727](https://openairdocs.org/sdr/A6WA2017010544727.md): Door · binding · Jan 5, 2017 · N413AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR IS DIFFICULT TO OPEN FROM INSIDE.
- [SDR A6WA2016122844679](https://openairdocs.org/sdr/A6WA2016122844679.md): Engine · unserviceable · Dec 20, 2016 · N413AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > APROXIMATELY 10500 FT, HEARD A LOUD BANG WITH VIBRATION. RT ENGINE ITT PEGGED. RETARDED THROTTLE ITT REMAINED PEGGED. CW QRH FOR SEVERE ENGINE DAMAGE. ENGINE WAS SHUT DOWN BY FLIGHT CREW. DIVERTED TO LGA. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. LANDING W
- [SDR A6WA2016080144130](https://openairdocs.org/sdr/A6WA2016080144130.md): Warning Message · illuminated · Jul 20, 2016 · N413AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE AND NOSE DOOR OPEN WARNING MESSAGE AFTER GEAR SELECTED UP. NOSE GEAR REMAINED DOWN. NWS CAUTION MESSAGE. COMPLIED WITH QRH.

Next page: https://openairdocs.org/aircraft/N413AW/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 = 'N413AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N413AW/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.