# Service difficulty reports: N447AW A list on [N447AW](https://openairdocs.org/aircraft/N447AW.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 · 175 reports - [SDR A6WA202210058313](https://openairdocs.org/sdr/A6WA202210058313.md): None · none · Oct 5, 2022 · N447AW · Cndair CL2151A10 · Landing Gear System > ON LADING ROLL OUT ON RNW 24 LEFT IN DAY I VEER IN TO THE RIGHT IN THE GRASS AND HIT SOMETHING THAT CAUSED DAMAGE TO THE LEFT WING. WITH REVERSER OUT, IT STARTED TO SLOWLY VEER TO THE RIGHT, I TOOK THE REVERS OUT THINKING THIS WILL HELP THE SITUATION AND THEN - [SDR A6WA202105247784](https://openairdocs.org/sdr/A6WA202105247784.md): Strut · discharged · May 22, 2021 · N447AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle > AFTER TO NWS CAU MSG. C/W QRH MSG CLEARED. AIR RETURN TO DAY. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND NLG STRUT EXTENSION LOW, DE-SERVICED AND SERVICED NLG STRUT WITH NITROGEN IAW 12-12-32. PERFORMED RIG CHECK OF LH AND RH FEEDBACK RVDT PER AMM 32-51-20. - [SDR A6WA202105047769](https://openairdocs.org/sdr/A6WA202105047769.md): Valve · malfunctioned · May 3, 2021 · N447AW · Cndair CL6002B19 · Landing Gear Steering System > RECEIVED NWS INOP CAUTION AFTER GEAR RETRACTION DURING DEPARTURE. C/W QRH. MSG PERSISTED. NO OTHER ASSOCIATED MSGS. SELECTED NWS AFTER LANDING, SEEMED TO BE OPERATIVE AND MSG CLEARED. AIRCRAFT REMOVED FROM SERVICE, REMOVED AND REPLACED EHSV IAW AMM 32- - [SDR A6WA202011097405](https://openairdocs.org/sdr/A6WA202011097405.md): Door · unknown · Nov 6, 2020 · N447AW · Cndair CL6002B19 · Passenger/Crew Doors > ON ARRIVAL AT GATE, PAX DOOR UNABLE TO OPEN FROM INSIDE OR OUTSIDE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST, IAW AMM 52-11-00-05. OPERATIONS CHECK OK, INSIDE AND OUTSIDE OPERATIONAL NORMAL. - [SDR A6WA202010217346](https://openairdocs.org/sdr/A6WA202010217346.md): Bonding Jumper · out of position · Oct 20, 2020 · N447AW · Cndair CL6002B19 · Ice/Rain Protection System Wiring > REVIVED ANTI ICE DUCT WARNING MESSAGE ON DEPARTURE RAN QRH MESSAGE CLEARED. ANTI-ICE WAS SELECTED OFF. MESSAGE CLEARED WHEN 14TH STAGE VALVES WERE CLOSED. AIRCRAFT REMOVED FROM SERVICE. FOUND PICALO TUBE BONDING JUMPER BEHIND ACCESS PANNEL 630MZ LOOSE AND - [SDR A6WA202010197343](https://openairdocs.org/sdr/A6WA202010197343.md): Attach Angle · cracked · Oct 19, 2020 · N447AW · Cndair CL6002B19 · Passenger/Crew Doors > SUSPECTED CRACK ON EXISTING REPAIR OF PAX DOOR AFT DRAG ANGLE INBOARD OF MOTOR ASSIST PULLEY. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND FOUND TO BE CRACKED 1.25''L. REMOVED EXISTING REPAIR, REF CRJ 200 SRM 51-42-22. FABRICATED REPAIR SPLICE FROM 601R190 - [SDR A6WA202010207335](https://openairdocs.org/sdr/A6WA202010207335.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL ANGLE AT FS 502 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 502 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010207329](https://openairdocs.org/sdr/A6WA202010207329.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL PANEL AT FS 556 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 556 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010207334](https://openairdocs.org/sdr/A6WA202010207334.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL PANEL AT FS 428 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 428 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010207331](https://openairdocs.org/sdr/A6WA202010207331.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL PANEL AT FS 555.5 AND RBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 555.5 AND RBL 47, PER REO 601R-53-41-666 AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.77''L X 0.50''W. - [SDR A6WA202010207328](https://openairdocs.org/sdr/A6WA202010207328.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL PANEL AT FS 494 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 494 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010207337](https://openairdocs.org/sdr/A6WA202010207337.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL ANGEL AT FS 507 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 507 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010207325](https://openairdocs.org/sdr/A6WA202010207325.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT PRESSURE FLOOR SILL ANGLE AT FS 452 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 452 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010207336](https://openairdocs.org/sdr/A6WA202010207336.md): Floor Support · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage, Stabilizer Attach Fittings > RT PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010207333](https://openairdocs.org/sdr/A6WA202010207333.md): Pressure Deck · corroded · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Main, Structure > LT PRESSURE FLOOR SILL PANEL AT FS 537 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 537 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES - [SDR A6WA202010197338](https://openairdocs.org/sdr/A6WA202010197338.md): Skin · gouged · Oct 17, 2020 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > PROTRUDING DENT ON AFT FUSELAGE AT FS 682.00 BETWEEN STR 23R AND 24R. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CIRCULAR CUTOUT 1.5''D ON REPAIR AREA FS 682.00 BETWEEN STR 23R AND STR 24R, REF EA: AWAC-CRJ253-01514 REV IR DATED 10/13/20. PERFORMED HFEC INSPE - [SDR A6WA202010197327](https://openairdocs.org/sdr/A6WA202010197327.md): Intercostal · cracked · Oct 14, 2020 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CLIP (INTERCOSTAL) CRACKED ON AFT SIDE OF PRESSURE BULKHEAD BETWEEN RBL 36.20 & S15R. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CLIP (INTERCOSTAL) ON AFT SIDE OF PRESSURE BULKHEAD AT FS 625.30 BETWEEN RBL 36.20 AND S15R, IAW CRJ 200 SRM 51-42-21 RE - [SDR A6WA202010197332](https://openairdocs.org/sdr/A6WA202010197332.md): Bulkhead Web · cracked · Oct 9, 2020 · N447AW · Cndair CL6002B19 · Fuselage Main, Bulkhead > ACCOMPLISHED SDI OF AFT PRESSURE BULKHEAD FWD FACE 2 EA INDICATIONS FOUND. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HFEC INSPECTION ON THE FWD SURFACE OF THE AFT PRESSURE BULKHEAD WEB AT FS 621.00 BETWEEN LBL 36.20 AND RBL 36.20 FROM WL 73.00 TO WL 150.00, I - [SDR A6WA2020021947187](https://openairdocs.org/sdr/A6WA2020021947187.md): Gearbox · cracked · Feb 18, 2020 · N447AW · Cndair CL6002B19 · Humidity Control System > AFTER SELECTING PACKS ON FOLLOWING UNPRESSURIZED TAKEOFF SMOKE IN COCKPIT AND REPORTS OF CHEMICAL BURNING SMELL IN THE CABIN. SMOKE DISSIPATED QUICKLY FROM COCKPIT. SUPP 09-037 REQUIRED. AIRCRAFT REMOVED FROM SERVICE APU ON MEL FOUND OIL IN APU ENCLOSURE RE - [SDR A6WA2019080246765](https://openairdocs.org/sdr/A6WA2019080246765.md): A/C Pack · inoperative · Jul 14, 2019 · N447AW · Cndair CL6002B19 · Cabin Temperature Control System > UNABLE TO COOL CABIN WITH RIGHT PACK ON MEL, CABIN TEMP ONLY WENT FROM 31C TO 28C ON 1HR 20 MINUTE FLIGHT. FLIGHT IS DIVERTING TO DAY WHERE WE HAVE A SPARE AIRCRAFT TO CONTINUE TO ORD WITH. - [SDR A6WA2018091446051](https://openairdocs.org/sdr/A6WA2018091446051.md): Skin · cracked · Sep 13, 2018 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN AND DOUBLER IN THE FWD LOWER CORNER OF PAX DOOR CUTOUT DAMAGED. REPAIRED. - [SDR A6WA2018091446050](https://openairdocs.org/sdr/A6WA2018091446050.md): Frame · corroded · Sep 10, 2018 · N447AW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME 589 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGER 20L AND 26L IN THE CARGO BAY. REPAIRED FRAME 589 FROM STRINGER 20L TO 26L. - [SDR A6WA2018091046046](https://openairdocs.org/sdr/A6WA2018091046046.md): Skin · gouged · Sep 8, 2018 · N447AW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT I/B FLAP, LOWER SKIN HAS GOUGE AND DENT. REPAIRED RIGHT I/B FLAP LOWER SKIN IAW REO 601R-57-52-1544 REV-. - [SDR A6WA2018091046048](https://openairdocs.org/sdr/A6WA2018091046048.md): Frame · cracked · Sep 8, 2018 · N447AW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME 605.00 CRACKED AT LBL9. REPAIRED FRAME 605.00 AT LBL9 IAW REO 601R-53-61-5214 REV-A. - [SDR A6WA2018091046047](https://openairdocs.org/sdr/A6WA2018091046047.md): Frame · corroded · Sep 8, 2018 · N447AW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME 605.00 CORRODED BETWEEN STR20L AND 20R. REPLACED FRAME IAW CRJ200 SRM 51-42-06, 51-42-21, 53-61-15. - [SDR A6WA2018091046044](https://openairdocs.org/sdr/A6WA2018091046044.md): Cleat · corroded · Sep 7, 2018 · N447AW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR LOWER AFT HANDRAIL CLEAT CORRODED. REPLACED CLEAT IAW SRM 51-42-06, TR51-42, 51-42-13, 51-21-06, 53-21-23. - [SDR A6WA2018091046043](https://openairdocs.org/sdr/A6WA2018091046043.md): Bracket · corroded · Sep 7, 2018 · N447AW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR AFT HANDRAIL CUP CORRODED FROM FS 340.00 AND LBL38. REPLACED CUP BRACKET IAW SRM 51-42-06, 51-42-13, TR51-42, 51-21-06, 53-21-23. - [SDR A6WA2018091046045](https://openairdocs.org/sdr/A6WA2018091046045.md): Retainer · cracked · Sep 7, 2018 · N447AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure > LEFT PYLON PANEL 412DB HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06. - [SDR A6WA2018091046042](https://openairdocs.org/sdr/A6WA2018091046042.md): Skin · cracked · Sep 6, 2018 · N447AW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT I/B FLAP LOWER SKIN HAS POSSIBLE CRACK ON CENTER TRAILING EDGE. REPAIRED SKIN IAW SRM 57-52-00. - [SDR A6WA2018091046041](https://openairdocs.org/sdr/A6WA2018091046041.md): Beam · damaged · Sep 3, 2018 · N447AW · Cndair CL6002B19 · Cargo/Baggage Doors > CARGO DOOR BEAM MEMBER PN: 601R35050-64 CUT BY CARGO DOOR CABLES. REPLACED BEAM IAW SRM 51-42-21, 51-42-06. - [SDR A6WA2018090446037](https://openairdocs.org/sdr/A6WA2018090446037.md): Retainer · cracked · Sep 2, 2018 · N447AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure > RIGHT PYLON PNL 422BT HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06. - [SDR A6WA2018090446038](https://openairdocs.org/sdr/A6WA2018090446038.md): Retainer · cracked · Sep 2, 2018 · N447AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure > RIGHT PYLON PNL 422DB HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06. - [SDR A6WA2018090446039](https://openairdocs.org/sdr/A6WA2018090446039.md): Fitting · damaged · Sep 2, 2018 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CARGO DOOR FWD SIDE SURROUND STRUCTURE HAS BENT/ TORN CLIP. REPLACED CLIP IAW SRM 51-42-21. - [SDR A6WA2018070545915](https://openairdocs.org/sdr/A6WA2018070545915.md): Bpsu · malfunctioned · Jun 30, 2018 · N447AW · Cndair CL6002B19 · Trailing Flap Position Indicating System > ON APPROACH FLAPS FAILED AT O DEGREES. PERFORMED FLAPS RESET PROCEDURE IAW SUP 98-18G BOX 12. PLACARDED AND PLACED ON MEL. CHANGED BPSU. - [SDR A6WA2018060845874](https://openairdocs.org/sdr/A6WA2018060845874.md): Skin · gouged · Jun 7, 2018 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > DURING AN INSPECTION, A GOUGE WAS FOUND IN THE FUSELAGE SKIN MEASURING 0.006 INCHES DEEP LOCATED AT BS 265, 0.1875 INCHES BELOW STRINGER 22L. THE GOUGE WAS REPAIRED IAW EA CRJ253-00968, REV IR. - [SDR A6WA2018042745787](https://openairdocs.org/sdr/A6WA2018042745787.md): Oil Cooler · malfunctioned · Apr 26, 2018 · N447AW · Cndair CL6002B19 · APU Oil System > APU OIL TEMP CAUTION ILLUMINATED INFLIGHT WITH THE NR 2 IDG ON MEL REPLACED OIL COOLER FOR BEING CLOGGED AND REPLACED APU. - [SDR A6WA2018021245615](https://openairdocs.org/sdr/A6WA2018021245615.md): Bulkhead · cracked · Feb 5, 2018 · N447AW · Cndair CL6002B19 · Fuselage Main, Bulkhead > WHILE PERFORMING SPECIAL DETAILED INSPECTION OF THE AFT PRESSURE BULKHEAD FORWARD FACE A CRACK WAS FOUND AT FS621.0, LBL 27.5, WL 132.0 THAT WAS 1.5 INCHES LONG. - [SDR A6WA2017072445113](https://openairdocs.org/sdr/A6WA2017072445113.md): Connector · unsecure · Jul 21, 2017 · N447AW · Cndair CL6002B19 · Light System Wiring > EMERGENCY LIGHTS BLINKING IN BACK OF CABIN SECURED LIGHT CONNECTOR IAW AMM 33-51-00. OP CHECKED GOOD. - [SDR A6WA201644419](https://openairdocs.org/sdr/A6WA201644419.md): Connector · loose · Oct 7, 2016 · N447AW · Cndair CL6002B19 · Light System Wiring > FLOOR LEVEL EMERGENCY LIGHTING AFT OF ROW 8 INITIALLY DID NOT TURN ON, WHEN DID TURN ON LIGHTS WERE VERY DIM. CONNECTED AND SECURED ROW 8 FLOOR TRACK LIGHTING CONNECTORS IAW SUP 13-022. OPS TEST GOOD. - [SDR A6WA201644333](https://openairdocs.org/sdr/A6WA201644333.md): Unknown · malfunctioned · Sep 13, 2016 · N447AW · Cndair CL6002B19 · Autopilot System > ON CLIMBOUT, EXPERIENCED SEVERAL OCCURRENCES OF UNCOMMANDED YAW. ACFT WOULD YAW TO ALMOST FULL BRICK OF DEFECTION, THEN JOLT BACK TO CENTER, FOLLOWED BY SMALL JOLT LT AND RT WITH INDICATION FCC-AMP-Y, RT: 6547, REPAIR RT: 008000, INTERROGATED FCC AND FOUND - [SDR A6WA201644268](https://openairdocs.org/sdr/A6WA201644268.md): Panel · cracked · Aug 27, 2016 · N447AW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR FOWARD RISER PANEL CRACKED AT LOWER CORNER, FOUND DURING REPAIR OF AFT RISER PANEL. - [SDR A6WA201644250](https://openairdocs.org/sdr/A6WA201644250.md): Rib · cracked · Aug 21, 2016 · N447AW · Cndair CL6002B19 · Elevator, Spar/Rib > LEFT ELEVATOR RIBLET AT ES 62.02 CRACKED. - [SDR A6WA201644253](https://openairdocs.org/sdr/A6WA201644253.md): Post · cracked · Aug 21, 2016 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > VERTICAL POST RBL 18 AT FS 409+128 IS CRACKED AT BOTTOM OTBD FLANGE. - [SDR A6WA201644249](https://openairdocs.org/sdr/A6WA201644249.md): Skin · damaged · Aug 21, 2016 · N447AW · Cndair CL6002B19 · Trailing Edge Flaps > RIGHT INBD FLAP LOWER SKIN HAS 2 EA LARGE AREAS HEAVILY PITTED, DEBRIS DAMAGE ON INBD SIDE. - [SDR A6WA201644244](https://openairdocs.org/sdr/A6WA201644244.md): Intercostal · cracked · Aug 19, 2016 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS 484, CLIP AT RBL 36 IS CRACKED. R & R CLIP, REPAIRED INTERCOSTAL AT FS 484.00 AND RBL36 IAW EA AWAC-CRJ253-00482, REV-A DATED 8/17/2016. - [SDR A6WA201644246](https://openairdocs.org/sdr/A6WA201644246.md): Skin · chafed · Aug 19, 2016 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > RIGHT MLG APRON STRUCTURE SKIN OUTER SURFACE GOUGED JUST FWD OF FS 554. - [SDR A6WA201644243](https://openairdocs.org/sdr/A6WA201644243.md): Post · cracked · Aug 19, 2016 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > VERTICAL POST LBL18, OTBD OF FS 409+128 IS CRACKED AT BOTTOM END. REPAIRED VERTICAL POST AT FS 409+128 AND LBL18 IAW REO 601R-53-41-056, REV-F DATED 2011/09/02. - [SDR A6WA201644245](https://openairdocs.org/sdr/A6WA201644245.md): Skin · damaged · Aug 19, 2016 · N447AW · Cndair CL6002B19 · Trailing Edge Flaps > LEFT INBD FLAP LOWER SKIN HAS 2 LARGE AREAS WITH CHIPPED PAINT AND PITTING. - [SDR A6WA201644242](https://openairdocs.org/sdr/A6WA201644242.md): Floorbeam · cracked · Aug 18, 2016 · N447AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > BS 280 FLOORBEAM AFT UPPER ANGLE CRACKED AT OTBD RBL 9. REPAIRED THE FLOORBEAM ANGLE IAW REO601R-53-11-137 REV-A. - [SDR A6WA201644240](https://openairdocs.org/sdr/A6WA201644240.md): Attach Bracket · cracked · Aug 17, 2016 · N447AW · Cndair CL6002B19 · Cargo/Baggage Doors > ATTACH BRACKET AT LOWER END OF FWD CARGO DOOR TRACK IS CRACKED. Next page: https://openairdocs.org/aircraft/N447AW/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 = 'N447AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N447AW/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.