# Service difficulty reports: N415AW

A list on [N415AW](https://openairdocs.org/aircraft/N415AW.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 5 · 214 reports

- [SDR A6WA202402088712](https://openairdocs.org/sdr/A6WA202402088712.md): Control Lever · failed · Feb 8, 2024 · N415AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH, RECEIVED FLAP FAIL CAUTION MESSAGE AFTER SELECTING FLAPS TO 30. COMPLIED WITH QRH. NORMAL LANDING WEIGHT, BTMS: 3,3,2,2. COMPLIED WITH RESET OF FLAPS PER AWA SUP 98-018I, SUCCESSFULLY PERFORMED 5 FULL EXTENSION/RETRACTION CYCLES. FLAP MEL 27-50-01
- [SDR A6WA202303168514](https://openairdocs.org/sdr/A6WA202303168514.md): Unknown · corroded · Mar 16, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > R/H FLOOR SILL FROM FS 563 TO FS621 IS FOUND TO BE OUT OF LIMITS. ******AIRCRAFT REMOVED FROM SERVICE********* REPLACE R/H FLOOR SILL BETWEEN FS 563 AND FS621 REF REO 601R-53-61-5376 REV A DATED 2018-10-25
- [SDR A6WA202303158503](https://openairdocs.org/sdr/A6WA202303158503.md): Angle · corroded · Mar 15, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FLOOR ANGLE BETWEEN FS349- FS310 AT PAX DR HAS CORROSION. *******AIRCRAFT REMOVED FROM SERVICE************ REPLACED FLOOR ANGLE BETWEEN FS349- FS310 AT PAX DR REF CRJ-200-SRM 51-42-06 AND CRJ-200-SRM 51-42-21
- [SDR A6WA202303108485](https://openairdocs.org/sdr/A6WA202303108485.md): Unknown · corroded · Mar 10, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > MULTIPLE SPOTS OF CORROSION NOTED ON R/H PRESSURE FLOOR SILL PANEL BETWEEN FS 409+128 AND FS559 ****AIRCRAFT REMOVED FROM SERVICE***** REPAIRED R/H PRESSURE FLOOR SILL REF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-3127 REV A DATED 2023-03-08
- [SDR A6WA202303108486](https://openairdocs.org/sdr/A6WA202303108486.md): Floor Support · cracked · Mar 10, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > ANGLE BRACKET SECURING FS 621 BULKHEAD TO L/H FLOOR SILL MISSING RIVETS ****AIRCRAFT REMOVED FROM SERVICE******* REPLACED FLOOR SUPPORT ANGLE REF REO 601R-53-61-117 REV E DATED 2018-01-15
- [SDR A6WA202303058479](https://openairdocs.org/sdr/A6WA202303058479.md): None · corroded · Mar 5, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > R/H FLOOR SILL FROM FS 559+86 TOFS563 IS FOUND TO BE OUT OF LIMITS *********AIRCRAFT REMOVED FROM SERVICE******* REPLACE FLOOR SILL BETWEEN FS559.00 +86 FS 621.00 PER CRJ 200 SRM 51-42-21 AND 51-42-06 AND DWG # 601R31133 REV J.
- [SDR A6WA202303048478](https://openairdocs.org/sdr/A6WA202303048478.md): None · corroded · Mar 4, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > L/H FLOOR SILL FROM FS 563 TO FS 621 IS FOUND TO BE OUT OF LIMITS ****AIRCRAFT REMOVED FROM SERVICE******** INSTALLED A NEW LH FLOOR SILL, FROM FS563.00-FS621.00 WITH NEW FASTENERS. REF DRAWING 601R35011 REV-R,
- [SDR A6WA202303038476](https://openairdocs.org/sdr/A6WA202303038476.md): Floorbeam · corroded · Mar 3, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > RBL 9 FLOOR BEAM CAP HAS CORROSION AT FS 559+80 ****AIRCRAFT REMOVED FROM SERVICE********** REPLACE RBL 9 FLOOR BEAM CAP SECTION REF REO 601R-53-51-650 REV -- DATED 2023-02-28
- [SDR A6WA202303038477](https://openairdocs.org/sdr/A6WA202303038477.md): Angle · gouged · Mar 3, 2023 · N415AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ACFT EXTERIOR- FS 409+112 BETWEEN STRGRS 27/26L VERICAL PLATE FOR FWD DRAW BEAM CORROSION. ********AIRCRAFT REMOVED FROM SERVICE********* REPAIRED LOWER FRAME ANGLE AND FUSELAGE SKIN AT FS 409+112 BETWEEN STR 26L 27
- [SDR A6WA202303028473](https://openairdocs.org/sdr/A6WA202303028473.md): Skin · dented · Mar 2, 2023 · N415AW · Cndair CL6002B19 · Vertical Stabilizer, Spar/Rib
  > DENT NOTED ON R/H VERTICAL STAB BETWEEN RIB#3-RIB #4 AFT OF MID SPAR AND APPROX 14" T/E ****AIRCRAFT REMOVED FROM SERVICE******** REPAIRED PER CRJ-200 SRM 55-31-31
- [SDR A6WA202303018472](https://openairdocs.org/sdr/A6WA202303018472.md): Floor Support · corroded · Mar 1, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > L/H FLOOR SILL HAS CORROSION FROM FS 559 TO FS 559+48 ******AIRCRAFT REMOVED FROM SERVICE******** REPLACE L/H FLOOR SILL
- [SDR A6WA202302288490](https://openairdocs.org/sdr/A6WA202302288490.md): Floorbeam · corroded · Feb 28, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > OUTBOARD PORTION OF SEAT RAIL SUPPORT BEAM IS CORRODED AT BL 27 BETWEEN FS559+80 - FS621 **********AIRCRAFT REMOVED FROM SERVICE********* REMOVED CORROSION FROM O/B SEAT RAIL SUPPORT BEAM LBL27 BETWEEN FS559.00+80 TO FS621.00 PER CRJ 200 SRM 51-21-06. FOUND RE
- [SDR A6WA202302258491](https://openairdocs.org/sdr/A6WA202302258491.md): Coaming · dented · Feb 25, 2023 · N415AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AFT CARGO DOOR SURROUND COAMING IS DENTED/MISSING MATERIAL IN MULTIPLE LOCATIONS *******AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED AFT CARGO DOOR SURROUND COAMING REF CRJ200 SRM 51-41-02 AND SRM 51-42-10.
- [SDR A6WA202203028118](https://openairdocs.org/sdr/A6WA202203028118.md): None · none · Feb 28, 2022 · N415AW · Cndair CL6002B19 · Wing Structure
  > ****SUPPLEMENTAL INFORMATION ***** AFTER DOOR CLOSE AND BEFORE PUSH BACK. LH WING TIP WAS STRUCK BY GROUND SUPPORT TUG WHILE TOWING BAGGAGE CARTS. TOW BAR WAS ATTACHED TO PLANE AND PUSH BACK TUG. AIRCRAFT DID NOT SLIDE AFT IMPACT. ***AIRCRAFT REMOVED FROM S
- [SDR A6WA202110157901](https://openairdocs.org/sdr/A6WA202110157901.md): None · corroded · Oct 14, 2021 · N415AW · Cndair CL6002B19 · Doors
  > PAX DOOR FWD ANCHOR FITTING PLATE WAS BADLY CORRODED (EXFOLIATION). THE CENTER SECTION OF THIS PLATE EXPANDED DUE TO THE CORROSION WHICH CAUSED THE FORWARD ANCHOR FITTING TO CRACK. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FWD PAX DOOR ANCHOR F
- [SDR A6WA202108187859](https://openairdocs.org/sdr/A6WA202108187859.md): Control Unit · faulted · Aug 17, 2021 · N415AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH RECEIVED FLAP FAIL CAUTION MESSAGE. FLAPS FAILED AT 30 DEGREES. MX WILL ATTEMPT THE RESET AS THE CREW WAS ON A TIGHT TAIL SWAP. ***AIRCRAFT REMOVED FROM SERVICE*** T/S IAW FIM SUPP 98-018I. FAULT LOGS SHOW FECU MOST LIKELY ISSUE. R/R FECU IAW AM
- [SDR A6WA202101067515](https://openairdocs.org/sdr/A6WA202101067515.md): Skin · cracked · Jan 5, 2021 · N415AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS 235 RIGHT SIDE FUSELAGE EXTERNAL SKIN CRACKED AFT OF NOSE LANDING GEAR CUT-OUT, NEXT TO RIGHT RADIUS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CRACK ON SKIN AT FS 235 RIGHT SIDE AFT OF NOSE LANDING GEAR CUT OUT, IAW CRJ200 REO 601R-53-11-048.
- [SDR A6WA202101047512](https://openairdocs.org/sdr/A6WA202101047512.md): Seat Track · corroded · Jan 3, 2021 · N415AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT FS 559+32 TO FS 559+80, FBL 9 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 559+32 TO FS 559+80, FBL 9.
- [SDR A6WA202101047511](https://openairdocs.org/sdr/A6WA202101047511.md): Seat Track · corroded · Jan 3, 2021 · N415AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACKAT FS 409 +112 ON LBL 9 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 409+112, LBL 9.
- [SDR A6WA202101047510](https://openairdocs.org/sdr/A6WA202101047510.md): Structure · corroded · Jan 3, 2021 · N415AW · Cndair CL6002B19 · Fuselage Main, Structure
  > T-CAP EXTRUSION IN CARGO BAY ON LBL 27 AT FS 559+118 TO FS 621 IS CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP EXTRUSION IN CARGO BAY AT LBL 27, FS 559+118 TO FS 621.00.
- [SDR A6WA2020012847131](https://openairdocs.org/sdr/A6WA2020012847131.md): Connector · disconnected · Jan 23, 2020 · N415AW · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > WING OVERHEAT WARNING MSG ON CLIMBOUT. CW QRH MSG CLEARED WITH WING A TIICE OFF WITHIN 40 SECONDS. RETURNED TO MKE. LANDING WEIGHT UNDER 44 000 LBS, BTMSMAX 3,3,2,3 MC ACARS REPORTS THIS IS THE RH WING AIRCRAF
- [SDR A6WA2019111446978](https://openairdocs.org/sdr/A6WA2019111446978.md): Fuel Control · malfunctioned · Nov 5, 2019 · N415AW · Cndair CL6002B19 · APU Engine Fuel and Control
  > SUPPLEMENTAL INFORMATION, ATTEMPTED TO START APU BELOW 10000 FT FIRST ATTEMPT FAILED. UPON SECOND TRY STARTED NORMAL, HOWEVER VERY STRONG FUEL SMELL IN A/C AIRCRAFT. REMOVED FROM SERVICE, INVESTAGTED APU BAY FOIR FUEL. NONE FOUND. STARTED APU SEVERAL TIMES O
- [SDR A6WA2019093046885](https://openairdocs.org/sdr/A6WA2019093046885.md): Warning System · activated · Sep 25, 2019 · N415AW · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > ON CLIMB OUT OF DAY AT 7000 FEET THE CREW RECEIVED A RIGHT WINDSHIELD HEAT CAUTION MESSAGE. CREW COMPLIED WITH THE QRH AND THE MESSAGE PERSISTS. DUE TO ICING EN-ROUTE AND AT THE DESTINATION IT WAS DECIDED TO RETURN BACK TO DAY
- [SDR A6WA2019050846595](https://openairdocs.org/sdr/A6WA2019050846595.md): Skin · dented · May 7, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REF LP 326168 / 1 - FUSELAGE AFT OF F.S.755.00 ON BOTTOM SIDE OF FUSELAGE DAMAGED. APPROXIMATELY 28 INCHES BY 9 INCHES OF DENTED / WRINKLED SKIN. TWO STRINGERS DAMAGED ON INSIDE OF FUSELAGE APPROXIMATELY 1 INCH FROM F.S.755.00.
- [SDR A6WA2019050846596](https://openairdocs.org/sdr/A6WA2019050846596.md): Stringer · bent · May 7, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER P/N 600-21302-63 REQUIRES FABRICATION DUE TO PART AVAILABILITY.
- [SDR A6WA201904046530](https://openairdocs.org/sdr/A6WA201904046530.md): Apu · odor · Apr 2, 2019 · N415AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > DURING ARRIVAL CREW ATTEMPTED APU START WITH NO LIGHT OFF. AFTER TWO MINUTES SUCCESSFULLY STARTED APU THEN RECEIVED ODOR OF FUEL IN CABIN, SHUT DOWN APU.
- [SDR A6WA2019031346468](https://openairdocs.org/sdr/A6WA2019031346468.md): Unknown · malfunctioned · Mar 11, 2019 · N415AW · Cndair CL6002B19 · Cabin Pressure Control System
  > AFTER T/O AIRCRAFT WOULD NOT PRESSURIZE. NO ASSOCIATED MESSAGES. SWAPPED APC (PRESSURE CONTROLLERS) AND TRIED MANUAL PRESSURIZATION AIRCRAFT WOULD STILL NOT PRESSURIZE. RETURNED TO CAE.
- [SDR A6WA2019020246354](https://openairdocs.org/sdr/A6WA2019020246354.md): Frame · corroded · Feb 1, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Frame
  > LOWER FLANGE ANGLE AT FS 333 IS CORRODED. REPLACED.
- [SDR A6WA2019020246353](https://openairdocs.org/sdr/A6WA2019020246353.md): Plug · damaged · Jan 30, 2019 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 131AL HAS A PREVIOUS FREEZE PLUG DAMAGED AT THE 12 O'CLOCK POSITION. REPLACED.
- [SDR A6WA2019013146347](https://openairdocs.org/sdr/A6WA2019013146347.md): Skin · cracked · Jan 29, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LH TRU DOOR LAND SKIN HAS CRACK AT UPP AFT LATCH CUT OUT REPAIR LH TRU DOOR LAND SKIN AT UPPER AFT LATCH CUT OUT IAW AWAC SUPP# 19-016A
- [SDR A6WA2018013146351](https://openairdocs.org/sdr/A6WA2018013146351.md): Intercostal · cracked · Jan 29, 2019 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPON C/W ITEM 6 OF EO# E13/024/449 FOUND INERCOSTAL 601R35210-17 TO HAVE A CRACK IN THE FWD CORNER INSTALLED PERMANENT REPAIR ON FOWARD CORNER OF INTERCOSTAL IAW AWAC SUPP# 13-085B
- [SDR A6WA2019012946346](https://openairdocs.org/sdr/A6WA2019012946346.md): Stiffener · cracked · Jan 28, 2019 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *SUPPLEMENTAL INFORMATION* (DIFFICULTY DATE YEAR ENTERED IN ERROR, CHANGED FROM 2018 TO 2019) PAX DOOR ASSIST MOTOR OB MOUNT IS CRACKED AT LOWER RADIUS REMOVE AND REPLACED STIFFENER UAW SRM 51-52-06 AND 51-42-13.
- [SDR A6WA2019012946345](https://openairdocs.org/sdr/A6WA2019012946345.md): Intercostal · cracked · Jan 28, 2019 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AEB STRINGER 15L INTERCOSTAL CRACKED REMOVED AND REPLACED AEB STRINGER 15L INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.
- [SDR A6WA2019012846341](https://openairdocs.org/sdr/A6WA2019012846341.md): Skin · cracked · Jan 26, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED IN THE AFT LT CORNER OF THE NLG SPADE DOOR CUT OUT. REPAIRED AFT LT CORNER OF NLG SPADE CUT OUT IAW REO 601R-53-11-048 REV D.
- [SDR A6WA2019012846336](https://openairdocs.org/sdr/A6WA2019012846336.md): Attach Angle · cracked · Jan 25, 2019 · N415AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > *SUPPLEMENTAL INFORMATION* (DIFFICULTY DATE YEAR ENTERED IN ERROR, CHANGED FROM 2018 TO 2019) CARGO DOOR MEMBER AFT LOWER ATTACH ANGLE CRACKED. REPLACE MEMBER ANGLE IAW CRJ 200 SRM 51-42-21.
- [SDR A6WA2019012846339](https://openairdocs.org/sdr/A6WA2019012846339.md): Stringer · cracked · Jan 25, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER AT FS379.00, STR 3L. REPAIRED STR 3L AT FS 379.00 IAW SRM 53-00-03, 51-20-06, 51-21-11.
- [SDR A6WA2019012846335](https://openairdocs.org/sdr/A6WA2019012846335.md): Fitting · cracked · Jan 25, 2019 · N415AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR BEAM MEMBER FWD LOWER CLIP CRACKED. REPLACED CLIP IAW SRM 51-42-21.
- [SDR A6WA2019012846334](https://openairdocs.org/sdr/A6WA2019012846334.md): Attach Angle · cracked · Jan 25, 2019 · N415AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LT WING I/B LEADING EDGE O/B ATTACH ANGLE AT TRANSITION PNL IS CRACKED. REPLACED ANGLE IAW SRM 51-41-02.
- [SDR A6WA2019012846333](https://openairdocs.org/sdr/A6WA2019012846333.md): Beam · cut · Jan 25, 2019 · N415AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR BEAM MEMBER 601R35050-64 HAS A CUT ON FWD SIDE MADE BY CABLE ASSIST. REPLACED BEAM IAW SRM 51-42-06, 51-42-21.
- [SDR A6WA2019012846338](https://openairdocs.org/sdr/A6WA2019012846338.md): Vane · chafed · Jan 24, 2019 · N415AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING I/B FLAP VANE HAS 3 WORN SPOTS. (CHAFING) REPAIRED FLAP VANE IAW SRM 51-42-13 AND REO601R-57-52-004 REV-D.
- [SDR A6WA2019012846337](https://openairdocs.org/sdr/A6WA2019012846337.md): Structure · cracked · Jan 24, 2019 · N415AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER EDGE MEMBER AFT EDGE IS CRACKED. REPAIRED PAX DOOR EDGE MEMBER IAW REO 601R-52-11-279 REV-NC.
- [SDR A6WA2019012846332](https://openairdocs.org/sdr/A6WA2019012846332.md): Threshold · corroded · Jan 24, 2019 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD CORRODED. REPLACED THRESHOLD IAW SRM 51-42-06, 51-23-00.
- [SDR A6WA2019012346320](https://openairdocs.org/sdr/A6WA2019012346320.md): Rib · cracked · Jan 22, 2019 · N415AW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON RIB AT STA. 340.481 IS CRACKED. REMOVED AND REPLACED LEFT AILERON RIB AT STA 340.481 IAW CRJ 200 SRM 51-42-06 AND 51-42-13.
- [SDR A6WA2019012346323](https://openairdocs.org/sdr/A6WA2019012346323.md): Stringer Clip · cracked · Jan 21, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 280 STRINGER 3L I/B AND OB CLIPS ARE CRACKED. REMOVED AND REPLACED 2 EACH CLIPS AT FS 280 IB AND OB OF STRINGER 3L IAW SRM 51-42-21 AND 51-42-06.
- [SDR A6WA2019012346322](https://openairdocs.org/sdr/A6WA2019012346322.md): Stringer Clip · cracked · Jan 21, 2019 · N415AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 280 STRINGER 3L IB AND OB CLIPS ARE CRACKED. REMOVED AND REPLACED 2 EACHS CLIPS AT FS 280 IB AND OB OF STRINGER 3L IAW SRM 51-42-21 AND 51-42-06.
- [SDR A6WA2019012346321](https://openairdocs.org/sdr/A6WA2019012346321.md): Angle · cracked · Jan 21, 2019 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AEB RT OBLIQUE ANGLE AT STRINGER 14R IS CRACKED. REMOVED AND REPLACED AEB RT OBLIQUE ANGLE AT STRINGER 14R IAW SRM 51-42-21.
- [SDR A6WA2019012146316](https://openairdocs.org/sdr/A6WA2019012146316.md): Stiffener · cracked · Jan 20, 2019 · N415AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > EXHAUST FAIRING 446AL FWD STIFFENER RING CRACKED. REPAIRED STIFFENER RING IAW CMM 79-11-00-300-810-A01, REPAIR SRS042.
- [SDR A6WA2019012146315](https://openairdocs.org/sdr/A6WA2019012146315.md): Attach Angle · cracked · Jan 20, 2019 · N415AW · Cndair CL6002B19 · Service Doors
  > EXTERNAL POWER SERVICE PANEL LOWER ATTACH ANGLE IS CRACKED. REPLACED LOWER ATTACH ANGLE IAW SUPP. 15-039.
- [SDR A6WA2019012146310](https://openairdocs.org/sdr/A6WA2019012146310.md): Retainer · cracked · Jan 19, 2019 · N415AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PNL 422BT SEAL RETAINER IS CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.
- [SDR A6WA2019012146311](https://openairdocs.org/sdr/A6WA2019012146311.md): Stiffener · cracked · Jan 19, 2019 · N415AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > PNL 436AL HAS A CRACKED FWD STIFFENER RING. REPAIRED STIFFENER RING IAW CMM 78-11-00-300-810-A01, REPAIR SRS042.

Next page: https://openairdocs.org/aircraft/N415AW/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 = 'N415AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N415AW/reports

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