# Service difficulty reports: N448AW

A list on [N448AW](https://openairdocs.org/aircraft/N448AW.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 · 184 reports

- [SDR A6WA202210138339](https://openairdocs.org/sdr/A6WA202210138339.md): None · none · Oct 13, 2022 · N448AW · Cndair CL2151A10 · Landing Gear Actuator
  > RECEIVED GEAR DISAGREE WARNING AFTER DEPARTURE, C/W QRH, MESSAGE REMAINED. TIME OF MESSAGE WAS APPROX 15-20 SECONDS AFTER GEAR SELECTED UP. RECEIVED NOSE DOOR OPEN WARNING MESSAGE WHILE C/W QRH. NOSE GEAR BOX TURNED RED ON EICAS, MANUAL DEPLOYMENT WAS REQUI
- [SDR A6WA202207298239](https://openairdocs.org/sdr/A6WA202207298239.md): Floorbeam · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Floor Panel
  > FLOOR BEAM RBL9 HAS CORROSION ALONG EDGES IN SEVERAL AREAS FROM FS559+16 TO FS559+80 ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED FLOOR BEAM P/N: 601R31119-75 AT RBL9 FROM FS559.00 TO FS559.00 + 112 PER REO 601R-53-51-619 REV -- DATED: 2022-06-14
- [SDR A6WA202207298240](https://openairdocs.org/sdr/A6WA202207298240.md): Floor Skin · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FLOOR BEAM LBL9 HAS CORROSION ALONG EDGES IN SEVERAL AREAS FROM FS559+16 TO FS559+80 ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND INSTALLED NEW LBL 9 FLOOR BEAM CAP BETWEEN FS 559.00+10 AND FS 569 REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-- 22, REO 601R-5
- [SDR A6WA202207298243](https://openairdocs.org/sdr/A6WA202207298243.md): Seat Track · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > *FS499.00 Ï¿½ AFT OF FS544.00 RH SIDE SEAT TRACK HAS CORROSION PITTING THROUGH OUT STICK (MARKED) ***AIRCRAFT REMOVED FROM SERVICE ***REPLACED SEAT TRACK REF CRJ 200 SRM 51-41-02
- [SDR A6WA202207298238](https://openairdocs.org/sdr/A6WA202207298238.md): Floor Splice · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORRODED FLOOR STRAP AT FS 559+80 RBL 9 TO RBL 27 ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED FLOOR SUPPORT PLATE BETWEEN RBL9-RBL27 DUE TO CORROSION EXCEEDING ALLOWABLE DAMAGE LIMITS. REF CRJ 200 SRM 51-42-06
- [SDR A6WA202207298244](https://openairdocs.org/sdr/A6WA202207298244.md): Floor Skin · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *FS559.00 FLOOR STRAP FROM RBL 27 TO PRESSURE FLOOR SILL CORRODED IN SEVERAL AREAS (MARKED) *****AIRCRAFT REMOVED FROM SERVICE ***** REPLACED FS559.00 FLOOR STRAP FROM RBL 27 TO PRESSURE FLOOR SILL REF CRJ 200 SRM 51-42-06
- [SDR A6WA202207298242](https://openairdocs.org/sdr/A6WA202207298242.md): Door Sill · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Structure (General)
  > *PAX DOOR LOWER SILL ANGLE CORRODED IN SEVERAL AREAS (MARKED) ***AIRCRAFT REMOVED FROM SERVICE *** REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, AND DWG 601R31527 REV -AM
- [SDR A6WA202207298241](https://openairdocs.org/sdr/A6WA202207298241.md): Frame Splice · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FRAME FS605.0 HAS CORROSION STGR24L-23R ***AIRCRAFT REMOVED FROM SERVICE *** REMOVED AND REPLACED FS 605.0 LOWER FRAME SECTOR STGR 21L - 21R REF CRJ 200 SRM 51-42-06, SRM 51-42-21, BOMBARDIER DWG 601R36026 REV. AE AND DWG 601R35005 REV AG
- [SDR A6WA202207298257](https://openairdocs.org/sdr/A6WA202207298257.md): Support Plate · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT PLATE BETWEEN RBL9 TO RBL27 AT FS559+80 HAS CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED FLOOR SUPPORT PLATE BETWEEN RBL9-RBL27 DUE TO CORROSION EXCEEDING ALLOWABLE DAMAGE LIMITS. REF CRJ 200 SRM 51-42-06
- [SDR A6WA202207298256](https://openairdocs.org/sdr/A6WA202207298256.md): Floorbeam · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL9 FLOOR BEAM HAS CORROSION IN SEVERAL SPOTS FS559+112 TO FS559+80 ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED FLOORBEAM P/N: 601R31119-75 AT RBL9 FROM FS559.00 TO FS559.00 + 112 PER REO 601R-53-51-619 REV -- DATED: 2022-06-14
- [SDR A6WA202207298254](https://openairdocs.org/sdr/A6WA202207298254.md): Floor Support · corroded · Jul 29, 2022 · N448AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > LH WINDSCREEN OTBD MOUNTING POINT SHOWS SIGNS OF EXFOLIATING CORROSION. ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE REF. CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, AND DWG 601R38673 REV. D.
- [SDR A6WA202207228234](https://openairdocs.org/sdr/A6WA202207228234.md): Floor Panel · cracked · Jul 22, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH TRU BAY (FWD EQUIPMENT COMPARTMENT) FLOOR CRACKED AT FRAME 193 ***AIRCRAFT REMOVED FROM SERVICE ***** COMPLIED WITH ALL STEPS 1-11 IAW REO 601R-53-11-081, REV NC, DATED: 97-07-02
- [SDR A6WA202207168233](https://openairdocs.org/sdr/A6WA202207168233.md): Stringer · cracked · Jul 16, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS 379.00 STRG 3LH CRACKED AT FASTENER (MARKED). ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED STRINGER 3L @ APPROX. FS379.00 WITH NEW P/N 601R31016-87 REF CRJ200 SRM 51-42-06, SRM 51-42-21 AND DWG 601R31016 REV D PERFORMED A LEAK TEST OF THE PASS
- [SDR A6WA202207078231](https://openairdocs.org/sdr/A6WA202207078231.md): Floorbeam · corroded · Jul 7, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SURFACE CORROSION FOUND ON LBL 27 FLOORBEAM NEAR FS 559+96 ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED LBL27 FLOORBEAM CAP SECTION BETWEEN FS559.00+80 AND FS569 REF CRJ200 SRM 53-00-43 REPAIR NO. 2, SRM 51-42-21, SRM 51-42-34, SRM 51-42-06 AN
- [SDR A6WA202207068236](https://openairdocs.org/sdr/A6WA202207068236.md): Floor Support · corroded · Jul 6, 2022 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > ADDITIONAL CORROSION ON CABIN FLOOR SILL FS 280.00 - FS 409.00 (AS PICTURED ON AGING AIRCRAFT INSPECTION REPORT). ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED NEW LH FLOOR SILL FROM FS 349.00 - FS 412.00 REF CRJ-200 SRM 51-42-06, 51-42-21 AND
- [SDR A6WA202206088226](https://openairdocs.org/sdr/A6WA202206088226.md): Seat Track · corroded · Jun 8, 2022 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS 439.00 - FS 449.85 RH SIDE SEAT TRACK CORRODED/GOUGED (MARKED) *****AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED NEW FABRICATED PASSENGER CABIN RH SIDE SEAT TRACK P/N: 601R-53-00-485-1 PO#: T58347 BETWEEN FS 439.00 AND FS 449.85 IAW REO 601R-53-
- [SDR A6WA202206068230](https://openairdocs.org/sdr/A6WA202206068230.md): Cleat · corroded · Jun 6, 2022 · N448AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR FWD AND AFT HAND RAIL CUPS AT THE FLOOR SILL HAVE SEVERAL AREAS OF CORROSION (MARKED). ****AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED FWD AND AFT HAND RAIL CUPS WITH 2EA NEW CLEATS REF CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV -AM.
- [SDR A6WA202009247295](https://openairdocs.org/sdr/A6WA202009247295.md): Windshield · cracked · Sep 22, 2020 · N448AW · Cndair CL6002B19 · Flight Compartment Windows
  > FIRST OFFICER'S WINDSHIELD CRACKED AT APPROXIMATELY 7,500 FEET. PRIOR TO CRACKING WE GOT A RIGHT WINDSHIELD HEAT CAUTION. AIRCRAFT REMOVED FROM SERVICE. R & R RT WINDSHIELD, IAW AMM 56-11-01. OPS CHECK GOOD. S/N OFF: 14139H5917 S/N ON: 19284H9352.
- [SDR A6WA2020011347106](https://openairdocs.org/sdr/A6WA2020011347106.md): Unknown · malfunctioned · Jan 12, 2020 · N448AW · Cndair CL6002B19 · Cabin Cooling System
  > AFTER TAKEOFF WHEN SWITCHING RH PACK TO 10TH STAGE AIR RECEIVED A RH PACK HIGH PRESSURE CAUTION, WITH THE LEFT PACK ALREADY ON MEL. CREW COMPLETED QRH AND PERFORMED AN AIR RETURN TO IAD. AIRCRAFT REMOVED FROM SERVICE PERFORMED OPS CHECK OF RH PACK WITH APU
- [SDR A6WA2019022646418](https://openairdocs.org/sdr/A6WA2019022646418.md): Warning Message · false activation · Feb 24, 2019 · N448AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING, NLG INDICATED RED. HYD P UMP 3A ON MEL. DISAGREE NEVER CLEARED. CW QRH. INDICATED GREEN. UNEVEN TFUL LANDING. DISAGREE AT APROX 28 SECONDS AFTER GEAR SELECTION. DID N OT MOVE GEAR HANDLE WITHIN 30 SECONDS. MANUAL R
- [SDR A6WA2019021846400](https://openairdocs.org/sdr/A6WA2019021846400.md): Trim System · frozen · Feb 15, 2019 · N448AW · Cndair CL6002B19 · Rudder Tab Control System
  > ON FINAL APPROACH REC'D UNCOMMANDED YAW, CONTINUED TO LANDING WHEN IN FLARE TRIED TO APPLY RT RUDDER, RT RUDDER WAS FROZEN. A/P WAS DISENGAGED. RUDDER TRIM OPERATES NORMALLY, NO ASSOCIATED MSG'S RUDDER POSITION INDICATION FLUXES LT/RT OF CENTER.
- [SDR A6WA2018101246111](https://openairdocs.org/sdr/A6WA2018101246111.md): Bpsu · malfunctioned · Oct 9, 2018 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECIEVED FLAPS FAIL CAUTION MESSAGE IMMEDIATELY FOLLOWING INITIAL DESCENT FROM FL 300. RAN QRH. LANDED FLAPS ZERO DEGREES. NO OTHER ISSUES NOTED. LANDING WAS UNEVENTFUL. PERFORMED FLAP RESET PROCEDURE IAW AWA SUPP. 98-018G BOX 12. FLAPS RESET. PLACARD
- [SDR A6WA2018101046106](https://openairdocs.org/sdr/A6WA2018101046106.md): Bpcu · malfunctioned · Oct 9, 2018 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAPS FAIL CAUTION MESSAGE DURING CLIMB THROUGH FL 210. FLAPS HAD BEEN SET TO ZERO SINCE LEAVING PATTERN ALTITUDE. NO OTHER ISSUES. DIVERTED BACK TO ORD. SUSPECT RH BPSU
- [SDR A6WA2018092146081](https://openairdocs.org/sdr/A6WA2018092146081.md): Plate · corroded · Sep 16, 2018 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD COVER PLATE CORRODED, R&R.
- [SDR A6WA2018092146082](https://openairdocs.org/sdr/A6WA2018092146082.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT FLOOR SEAT TRACK CORRODED BETWEEN FS 349 AND FS 379, R&R.
- [SDR A6WA2018091946072](https://openairdocs.org/sdr/A6WA2018091946072.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR TRACK CORRODED BETWEEN FS 379.00 AND FS 409+128. R&R.
- [SDR A6WA2018091946073](https://openairdocs.org/sdr/A6WA2018091946073.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT FLOOR SEAT TRACK CORRODED BETWEEN FS 379 AND 409+128.
- [SDR A6WA2018092146074](https://openairdocs.org/sdr/A6WA2018092146074.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT TRACK CORRODED BETWEEN FS 349 AND FS 379.
- [SDR A6WA2018091946068](https://openairdocs.org/sdr/A6WA2018091946068.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT WALL SEAT TRACK CORRODED BETWEEN FS 409+16 AND FS 409+112.
- [SDR A6WA2018091946064](https://openairdocs.org/sdr/A6WA2018091946064.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT WALL SEAT TRACK CORRODED BETWEEN FS 544 AND FS 559+16.
- [SDR A6WA2018091946070](https://openairdocs.org/sdr/A6WA2018091946070.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT WALL SEAT TRACK CORRODED BETWEEN FS 409+16 AND FS 409+112.
- [SDR A6WA2018091946071](https://openairdocs.org/sdr/A6WA2018091946071.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT FLOOR SEAT TRACK CORRODED BETWEEN FS 409+128 AND FS 559.00.
- [SDR A6WA2018091946066](https://openairdocs.org/sdr/A6WA2018091946066.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT WALL SEAT TRACK CORRODED BETWEEN FS 544.00 AND FS 559+80.
- [SDR A6WA2018091946065](https://openairdocs.org/sdr/A6WA2018091946065.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT WALL SEAT TRACK CORRODED BETWEEN FS 449.85 AND FS 499.00.
- [SDR A6WA2018091946067](https://openairdocs.org/sdr/A6WA2018091946067.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT WALL SEAT TRACK CORRODED BETWEEN FS 449.85 AND FS 499.00.
- [SDR A6WA2018091946069](https://openairdocs.org/sdr/A6WA2018091946069.md): Seat Track · corroded · Sep 12, 2018 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H WALL SEAT TRACK CORRODED AT FS 409+128
- [SDR A6WA2018072445899](https://openairdocs.org/sdr/A6WA2018072445899.md): Fire Bottle · low · Jun 10, 2018 · N448AW · Cndair CL6002B19 · Fire Bottle, Fixed
  > CARGO BOTTLE LOW CAUTION MSG. CW QRH. DIVERTED TO DAY REMOVED AND REPLACED LT CARGO FIRE BOTTLE IAW AMM SUP 10-099A. OPS CHECKED GOOD.
- [SDR A6WA2018062245899](https://openairdocs.org/sdr/A6WA2018062245899.md): Fire Bottle · low · Jun 10, 2018 · N448AW · Cndair CL6002B19 · Fire Bottle, Fixed
  > CARGO BOTTLE LOW CAUTION MSG. CW QRH. DIVERTED TO DAY REMOVED AND REPLACED LT CARGO FIRE BOTTLE IAW AMM SUP 10-099A OPS CHECKED GOOD.
- [SDR A6WA201745363](https://openairdocs.org/sdr/A6WA201745363.md): Wire Harness · damaged · Oct 15, 2017 · N448AW · Cndair CL6002B19 · Landing Gear System Wiring
  > DURING CLIMB OUT, RECEIVED A GEAR DISAGREE THROUGH 17000 FT. NLG SHOWED YELLOW HASH. COMPLIED WITH QRH. MESSAGE CLEARED ON ITS OWN. DIVERTED. ON APPROACH SELECTED GEAR DOWN, HEARD CLICKING NOISE FROM THE NOSE GEAR. GEAR INDICATED DOWN AND LOCKED. R &
- [SDR A6WA2017092245298](https://openairdocs.org/sdr/A6WA2017092245298.md): Sensor · out of limits · Sep 21, 2017 · N448AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE DURING CLIMB. COMPLIED WITH THE QRH. MESSAGE CLEARED AND REAPPEARED MULTIPLE TIMES. THEN CLEARED COMPLETELY. NLG SHOWED AMBER. DURING DESCENT GEAR EXTENDED NORMALLY. LANDED AT NEAREST SUITABLE AIRPORT IAW QRH. FOUND NLG DOWNLOCK SENSOR O
- [SDR A6WA2017020344779](https://openairdocs.org/sdr/A6WA2017020344779.md): Light · inoperative · Feb 1, 2017 · N448AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT INOPERATIVE BEHIND ROW 8
- [SDR A6WA2016111644575](https://openairdocs.org/sdr/A6WA2016111644575.md): Circuit Breaker · tripped · Nov 12, 2016 · N448AW · Cndair CL6002B19 · AC Generator-Alternator
  > FLT 3978. IN FLIGHT AC ESSENTIAL FEED CIRCUIT BREAKER TRIPPED. CIRCUIT BREAKER PANEL 1 C2 ASSOCIATED AC ESS SWITCH ILLUMINATED COMPLIED WITH QRH. GEN 1 WILL NOT RESET. RESET CIRCUIT BREAKER ON PANEL 1 C2 PERFORMED OPS CHECK OF AC BUSS 1 SYSTEM OPS CHECK GOO
- [SDR A6WA201644451](https://openairdocs.org/sdr/A6WA201644451.md): Light · inoperative · Oct 21, 2016 · N448AW · Cndair CL6002B19 · Emergency Lighting
  > AFT SECTION FLOOR EMERGENCY LIGHTS INOP. ROWS 9 -12.
- [SDR A6WA201644435](https://openairdocs.org/sdr/A6WA201644435.md): Light · inoperative · Oct 16, 2016 · N448AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT DO NOT WORK STARTING AT ROW 8 TO BACK OF PLANE. R&R EMERGENCY FLOOR TRACK LIGHTS AT ROW 12 IAW AMM 33-51-01. OPS CHECK GOOD.
- [SDR A6WA201644332](https://openairdocs.org/sdr/A6WA201644332.md): Ballast · inoperative · Sep 14, 2016 · N448AW · Cndair CL6002B19 · Passenger Compartment Lighting
  > FLIGHT 4041.ODOR IN CABIN SIMILAR TO ELECTRICAL OVERHEAT. STRONGEST MID CABIN. LT SIDE ROW 9 SIDE WALL LIGHT INOPERATIVE. INSPECTED AND FOUND LIGHT BALLAST INOPERATIVE AT SEAT 1CA. REMOVED AND REPLACED BALLAST AND SIDEWALL LIGHT BULB OPS CHECK OK. NO ODOR
- [SDR A6WA201644205](https://openairdocs.org/sdr/A6WA201644205.md): Rib · bent · Aug 8, 2016 · N448AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP RIB AT WS 106.352 BENT, REPLACED.
- [SDR A6WA201644203](https://openairdocs.org/sdr/A6WA201644203.md): Shroud · cracked · Aug 8, 2016 · N448AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT OTBD L/E SHROUD IS DENTED AND CRACKED AT WS 342-350.
- [SDR A6WA201644202](https://openairdocs.org/sdr/A6WA201644202.md): Doubler · chafed · Aug 8, 2016 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NLG DOOR CUTOUT, RT DOUBLER AT FS 206 IS CHAFED.
- [SDR A6WA201644204](https://openairdocs.org/sdr/A6WA201644204.md): Skin · chafed · Aug 8, 2016 · N448AW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON UPPER L/E SKIN CHAFED AT AREAS ALONG ENTIRE LENGTH, REPLACED.
- [SDR A6WA201644201](https://openairdocs.org/sdr/A6WA201644201.md): Web · cracked · Aug 8, 2016 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WEB BELOW PILOTS WINDSHIELD SIDE POST SUPPORT IS CRACKED.

Next page: https://openairdocs.org/aircraft/N448AW/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 = 'N448AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N448AW/reports

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