# Service difficulty reports: N422AW, cancelled Nov 7, 2018 A list on [N422AW, cancelled Nov 7, 2018](https://openairdocs.org/deregistered/N422AW-2018-11-07.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 · 196 reports - [SDR A6WA201744762](https://openairdocs.org/sdr/A6WA201744762.md): Actuator · malfunctioned · Jan 20, 2017 · N422AW · Cndair CL6002B19 · Landing Gear Actuator > INFLIGHT, AFTER SELECTING GEAR LEVER UP, NOSE GEAR LOCK AND DOOR CYCLED FOR 1 MINUTE THEN LOCKED IN UP POSITION. GEAR EXTENDED NORMALLY AND LOCKED AFTER GEAR LEVER SELECTED DOWN. AIR RETURN UNDER 47,000LBS, LANDING NORMAL, BTMS 2-2-3-3. REF WO 255898 FOR WORK - [SDR A6WA201644263](https://openairdocs.org/sdr/A6WA201644263.md): Light · inoperative · Aug 26, 2016 · N422AW · Cndair CL6002B19 · Emergency Lighting > DURING FIRST FLIGHT ACCEPTANCE INSPECTION CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE FROM ROW 1-5. - [SDR A6WA201644257](https://openairdocs.org/sdr/A6WA201644257.md): Downlock Sensor · failed · Aug 22, 2016 · N422AW · Cndair CL6002B19 · Landing Gear Position and Warning > AFTER CLIMB OUT REC GEAR DISAGREE WARNING, NLG RED HASHES RAN QRH MSGS CLEARED RETURNED TO DEPARTURE IAW QRH. MESSAGES RECEIVED AT AROUND 7,000 FT AND 250 KTS GEAR WAS UP SLOWED TO C/W QRH WHEN HYD 2 AND 3B SEL ON MSG CLEARED. HYDS WERE IN AUTO AND INDICATIO - [SDR A6WA2016080144127](https://openairdocs.org/sdr/A6WA2016080144127.md): Door · lack of lube · Jul 18, 2016 · N422AW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBRICATED PAX DOOR IAW SUP 15-053. OPS CHECKED GOOD. - [SDR A6WA2016071944127](https://openairdocs.org/sdr/A6WA2016071944127.md): Door · lack of lube · Jul 18, 2016 · N422AW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR WILL NOT OPEN FROM OUTSIDE. LUBRICATED PAX DOOR PER 15-053. OPS CHECKED GOOD. - [SDR A6WA201643862](https://openairdocs.org/sdr/A6WA201643862.md): Roller · damaged · May 8, 2016 · N422AW · Cndair CL6002B19 · Passenger/Crew Doors > NUMBER 1 PAX DOOR VERY DIFFICULT TO MOVE TO THE OPEN POSITION FROM THE OUTSIDE. FOUND INSIDE HANDLE ROLLER DAMAGED, ROLLER HAS MULTIPLE FLAT SPOTS CAUSING ROLLER TO HANG UP IN DETENT. REPLACED THE ROLLER ON THE INNER PAX DOOR HANDLE RETENTION MECHANISM IAW A - [SDR A6WA201643847](https://openairdocs.org/sdr/A6WA201643847.md): Fuel · leaking · May 5, 2016 · N422AW · Cndair CL6002B19 · APU Engine Fuel and Control > FLIGHT 3914, 3930 STRONG FUEL ODOR COMING FROM THE PACKS. NOTED FUEL LEAK AROUND APU FUEL MANIFOLD & FILTER AREA. WIPED EXCESS FUEL IAW 299136 4 FOR MEL. DID NOT SMELL USING ENG BLEED AIR. - [SDR A6WA201643623](https://openairdocs.org/sdr/A6WA201643623.md): Light · inoperative · Feb 28, 2016 · N422AW · Cndair CL6002B19 · Emergency Lighting > FLIGHT 3791 EMER LIGHTS ROW 1 INOPERATIVE & UNSECURE. R & R EMER LIGHT COVER IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME. - [SDR A6WA201643458](https://openairdocs.org/sdr/A6WA201643458.md): Light · inoperative · Jan 15, 2016 · N422AW · Cndair CL6002B19 · Emergency Lighting > EMERGENCY FLOOR TRACK LIGHT ROW 5 - 7 ARE NOT WORKING;. - [SDR A6WA201543415](https://openairdocs.org/sdr/A6WA201543415.md): Rod · out of adjust · Dec 29, 2015 · N422AW · Cndair CL6002B19 · Galley Doors > GALLEY SERVICE DOOR DIFFICULT TO OPEN FROM INSIDE & OUTSIDE. ADJUSTED UPPER STABILIZER ROD IAW AMM 52-41. OPERATIONS CHECKED GOOD. REMOVED PLACARD & FROM MEL. - [SDR A6WA201543413](https://openairdocs.org/sdr/A6WA201543413.md): Rod · out of adjust · Dec 27, 2015 · N422AW · Cndair CL6002B19 · Service Doors > CREW REPORTED SERVICE DOOR DIFFICULT TO OPEN AFTER UNLATCHING HANDLE INSIDE & OUTSIDE OF ACFT. INSPECTED DOOR FOR SAFETY & SECURITY. PLACED SERVICE DOOR ON MEL 52-21-01. REPOSITIONED ACFT TO MAKE FOR REPAIR. MX ADJUSTED UPPER STABILIZER ROD IAW AMM 52-41. - [SDR A6WA201543394](https://openairdocs.org/sdr/A6WA201543394.md): Seal · torn · Dec 21, 2015 · N422AW · Cndair CL6002B19 · Galley Doors > GALLEY SERVICE DOOR DIFFICULT TO OPEN & CLOSE. INSPECTED GALLEY SERVICE DOOR & FOUND LOWER AFT SECTION TORN IN TWO PLACES APPROX 1" LONG. R & R SERVICE DOOR SEAL, INSPECTED & OPERATED SERVICE DOOR, VERIFIED DOOR OPERATES, CLOSES & LOCKS NORMALLY. - [SDR A6WA201543288](https://openairdocs.org/sdr/A6WA201543288.md): Mount Bracket · cracked · Nov 25, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > EXTERNAL SERVICE INSTRUMENT PANEL, LOWER ANGLE MOUNTING BRACKET IS CRACKED, REPLACED. - [SDR A6WA201543285](https://openairdocs.org/sdr/A6WA201543285.md): Support · cracked · Nov 24, 2015 · N422AW · Cndair CL6002B19 · Spoilers > SPOILER ADAPTER OTBD SUPPORT CRACKED, REPLACED. - [SDR A6WA201543284](https://openairdocs.org/sdr/A6WA201543284.md): Mount Bracket · cracked · Nov 24, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > AC POWER RECEPTACLE MOUNT BRACKET IS CRACKED AT THE FWD FASTENER HOLE, REPLACED. - [SDR A6WA201543280](https://openairdocs.org/sdr/A6WA201543280.md): Bracket · chafed · Nov 22, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > BRACKET FOR RT BRAIDED HYD LINE RUNNING THRU INTERCOSTAL AT STRINGER 9R, BETWEEN FRAMES 645 & 672 IN THE AFT EQUIPMENT BAY IS CHAFED, REPAIRED. - [SDR A6WA201543281](https://openairdocs.org/sdr/A6WA201543281.md): Intercostal · cracked · Nov 22, 2015 · N422AW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR AFT UPPER INTERCOSTAL CRACKED, REPLACED. - [SDR A6WA201543270](https://openairdocs.org/sdr/A6WA201543270.md): Support Bracket · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > RIGHT DUEL HEAT EXCHANGER, SUPPORT BRACKET CLIP IS CRACKED. R & R CRACKED BRACKET ON RT DUEL HEAT EXCHANGER SUPPORT WITH SERVICEABLE FABRICATED BRACKET IAW SRM 51-42-06, 51-11-20. - [SDR A6WA201543277](https://openairdocs.org/sdr/A6WA201543277.md): Skin · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > LOWER FWD FUSELAGE SKIN AT NLG AFT DOOR CUT OUT, AFT RT RADIUS IS CRACKED. REPAIRED DAMAGED FUSELAGE SKIN CRACK AT NLG CUT OUT, AFT RADIUS RT SIDE IAW REO 601R-53-11-048 REV D. - [SDR A6WA201543276](https://openairdocs.org/sdr/A6WA201543276.md): Floorbeam · corroded · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > ON RBL 27, THE OTBD FLOOR LANDING HAS CORROSION, BETWEEN FS 605.0 & FS 621.0, IN THE CARGO BAY. REMOVED CORRODED FLOORBEAM CAP & REPLACED WITH NEW SERVICEABLE BEAM CAP IAW EA 40-2015-229 ISSUED 11 10 15. - [SDR A6WA201543272](https://openairdocs.org/sdr/A6WA201543272.md): Web · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Wing Miscellaneous Structure > RIGHT WING OTBD LE WEB IS CRACKED, BETWEEN ACCESS PANELS 630KZ & 630LZ. R & R RT OTBD LE WEB, BETWEEN ACCESS PANELS 630KZ & 630LZ IAW SRM 51-42-13. - [SDR A6WA201543268](https://openairdocs.org/sdr/A6WA201543268.md): Intercostal · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Cargo/Baggage Doors > CARGO DOOR LOWER AFT VERTICAL MEMBER IS CRACKED FROM TOP TO BOTTOM, CRACK 6" LONG. R & R CARGO DOOR LOWER AFT VERTICAL MEMBER, INTERCOSTAL, IAW SRM 51-42-06 & 51-42-21. - [SDR A6WA201543265](https://openairdocs.org/sdr/A6WA201543265.md): Seat Track · corroded · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SMALL SEAT TRACK ON LBL9, JUST FWD OF THE AFT PRESS BULKHEAD HAS CORROSION, IN THE CARGO BAY. R & R SMALL SEAT TRACK, PN 601R31032-51 ON LBL 9, JUST FWD OF THE AFT PRESS BULKHEAD IAW AMM 53-01-11. - [SDR A6WA201543271](https://openairdocs.org/sdr/A6WA201543271.md): Attach Angle · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > APU ENCLOSURE SUPPORT STRUCTURE, RT FWD VERTICAL POST AFT ATTACH ANGLE CRACKED. R & R CRACKED ANGLE FROM RT VERTICAL POST AFT SIDE OF FWD POST OF APU ENCLOSURE WITH SERVICEABLE ANGLE IAW SRM 51-42-13 & 51-11-20. - [SDR A6WA201543266](https://openairdocs.org/sdr/A6WA201543266.md): Seat Track · corroded · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK ON LBL 9, BETWEEN FS 559+112 & 574.00 HAS CORROSION, IN THE CARGO BAY. R & R SEAT TRACK, PN 601R38779-5, ON LBL 9, BETWEEN FS 559+112 & 574.00 IAW AMM 53-01-11. - [SDR A6WA201543269](https://openairdocs.org/sdr/A6WA201543269.md): Skin · chafed · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FUSELAGE SKIN IS CHAFED NEXT TO PREVIOUS REPAIR CUT OUT, JUST FWD OF PAX DOOR OPENING & JUST ABOVE WL 79.50. REPAIRED FUSELAGE SKIN JUST FWD OF PAX DOOR OPENING & JUST ABOVE WL 79.50 IAW REO 601R-53-21-180 REV A. - [SDR A6WA201543267](https://openairdocs.org/sdr/A6WA201543267.md): Seat Track · corroded · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK ON RBL 9 HAS CORROSION, BETWEEN FS 559+80 & FS 559+96 IN THE CARGO BAY. R & R SEAT TRACK IAW AMM 53-01-11. - [SDR A6WA201543274](https://openairdocs.org/sdr/A6WA201543274.md): Drag Angle · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Wing Miscellaneous Structure > LEFT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R LT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & SUP 15-287. - [SDR A6WA201543275](https://openairdocs.org/sdr/A6WA201543275.md): Drag Angle · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Wing Miscellaneous Structure > RIGHT MLG WW DRAG ANGLE COMMON TO BAT RIB IS CRACKED IN THE AFT RADIUS. R & R RT MLG DRAG ANGLE COMMON TO BAT RIB IAW SRM 51-42-21. - [SDR A6WA201543273](https://openairdocs.org/sdr/A6WA201543273.md): Drag Angle · cracked · Nov 21, 2015 · N422AW · Cndair CL6002B19 · Wing Miscellaneous Structure > RIGHT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IS CRACKED. R & R RT MLG WW DRAG ANGLE FWD MOUNT STRUCTURE IAW EA 30-2015-523 & AWAC SUPPLEMENT 15-287. - [SDR A6WA201543264](https://openairdocs.org/sdr/A6WA201543264.md): Attach Angle · cracked · Nov 20, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > APU ENCLOSURE SUPPORT STRUCTURE, RT AFT ATTACH ANGLE SUPPORT BRACKET CRACKED. REMOVED CRACKED ATTACH ANGLE ON APU SUPPORT STRUCTURE, RT AFT SIDE & REPLACED WITH NEW SERVICEABLE BRACKET PN 601-97049-2 IAW SRM 51-42-06. - [SDR A6WA201543258](https://openairdocs.org/sdr/A6WA201543258.md): Frame Splice · bent · Nov 17, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME SPLICE AT FS 736.00, STRINGER 6L - 7L BENT. - [SDR A6WA201543248](https://openairdocs.org/sdr/A6WA201543248.md): Seat Track · corroded · Nov 15, 2015 · N422AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT AISLE SEAT TRACK STICK NR 1 HAS CORROSION, BETWEEN FS 364 & 394, REPLACED. - [SDR A6WA201543249](https://openairdocs.org/sdr/A6WA201543249.md): Seat Track · corroded · Nov 15, 2015 · N422AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT AISLE SEAT TRACK STICK NR 4 HAS CORROSION, BETWEEN FS 559 & 559+96, REPLACED. - [SDR A6WA201543251](https://openairdocs.org/sdr/A6WA201543251.md): Floorbeam · corroded · Nov 15, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > FLOORBEAM 589 CAP HAS CORROSION ON THE TOP SIDE, BETWEEN RBL 27 & THE RT FLOOR SILL, REPLACED. - [SDR A6WA201543250](https://openairdocs.org/sdr/A6WA201543250.md): Floorbeam · corroded · Nov 15, 2015 · N422AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > FLOORBEAM 559+80 CAP HAS CORROSION ON THE TOP SIDE, BETWEEN LBL 9 & RBL 9, REPLACED. - [SDR A6WA201543247](https://openairdocs.org/sdr/A6WA201543247.md): Seat Track · corroded · Nov 15, 2015 · N422AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT AISLE SEAT TRACK STICK NR 3 HAS CORROSION, BETWEEN 409+128 & 559, REPLACED. - [SDR A6WA201543252](https://openairdocs.org/sdr/A6WA201543252.md): Structure · cracked · Nov 15, 2015 · N422AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PLATFORM SKIN IS CRACKED NEXT TO ADG RETRACTION PUMP, OTBD SIDE AT FRAME CUT OUT, REPAIRED. - [SDR A6WA201543234](https://openairdocs.org/sdr/A6WA201543234.md): Fitting · cracked · Nov 10, 2015 · N422AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > OUTBOARD CLIP ON STRINGER 3L CRACKED AT FS 280, IN CABIN. - [SDR A6WA201543233](https://openairdocs.org/sdr/A6WA201543233.md): Fitting · cracked · Nov 10, 2015 · N422AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INBOARD CLIP ON STRINGER 3L CRACKED AT FS 280, IN CABIN. - [SDR A6WA201542972](https://openairdocs.org/sdr/A6WA201542972.md): Strip · misinstalled · Aug 9, 2015 · N422AW · Cndair CL6002B19 · Emergency Lighting > FLIGHT 3737, 3884 EMER FLOOR TRACK LIGHTING ARROWS POINT BACKWARDS, LAST SECTION. FOUND EMER FLOOR AFT STRIP BY LAVATORY INSTALLED INCORRECTLY. REINSTALLED EMER FLOOR LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD ARROWS POINT IN CORRECT POSITION. - [SDR A6WA201542727](https://openairdocs.org/sdr/A6WA201542727.md): Light · inoperative · May 12, 2015 · N422AW · Cndair CL6002B19 · Emergency Lighting > FLIGHT 3862, STRIP OF EMERGENCY FLOOR LIGHT NOT WORKING ROW 12. REPLACED ROW 12 FLOOR TRACK EMERGENCY STRIP IAW AMM 33-50. OPERATIONS CHECKED GOOD. - [SDR A6WA201542592](https://openairdocs.org/sdr/A6WA201542592.md): Actuator · failed · Apr 6, 2015 · N422AW · Cndair CL6002B19 · Trailing Edge Flap Actuator > WHEN SELECTING FLAPS FROM 8 DEG TO 20 DEG, AT 17 LT & 15 RT INDICATED, FLAPS FAILED. COMPLIED WITH FLAP CIRCUIT BREAKER RESET. ON 3RD RETRACTION FLAPS FAILED WHEN SELECTED TO 20 DEG, INDICATION LT 22 & RT 20, FELT SLIGHT RUMBLE WHEN FAILED. FOUND LT NR 3 FL - [SDR A6WA201542522](https://openairdocs.org/sdr/A6WA201542522.md): Connector · missing · Mar 15, 2015 · N422AW · Cndair CL6002B19 · Light System Wiring > REQUIRES INSPECTION OF FLOOR TRACK LIGHTING AT ROW 1D-F, PULLED FROM FLOOR BY PAX. INSPECTED FLOOR TRACK LIGHTING AT ROW 1 D & F, FOUND TRACK PULLED UP FROM FLOOR & CONNECTORS & CONNECTORS MISSING. SECURED WIRE WITH TAPE IAW 280733 3 FOR OPEN WRITE UP FOR FE - [SDR A6WA201442081](https://openairdocs.org/sdr/A6WA201442081.md): Warning System · false activation · Oct 23, 2014 · N422AW · Cndair CL6002B19 · Landing Gear Position and Warning > ON TAKEOFF SELECTED GEAR UP & RECEIVED GEAR DISAGREE WARNING. COMPLIED WITH QRH & MSG CLEARED. GEAR EXTENDED NORMALLY ON EXTENSION. - [SDR A6WA201310214288](https://openairdocs.org/sdr/A6WA201310214288.md): Drag Angle · cracked · Oct 21, 2013 · N422AW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings > LEFT MLG DRAG ANGLE IS CRACKED, COMMON TO UPPER SKIN. R & R ANGLE IAW SRM 51-46-11 & 51-42-21. - [SDR A6WA201310214267](https://openairdocs.org/sdr/A6WA201310214267.md): Frame · corroded · Oct 21, 2013 · N422AW · Cndair CL6002B19 · Fuselage Main, Frame > FS 319 FRAME CORRODED. R & R LWR FRAME SEGMENT. - [SDR A6WA201310214266](https://openairdocs.org/sdr/A6WA201310214266.md): Frame · corroded · Oct 21, 2013 · N422AW · Cndair CL6002B19 · Fuselage Main, Frame > FS 333 FRAME CORRODED. R & R FRAME SEGMENT. - [SDR A6WA201310214265](https://openairdocs.org/sdr/A6WA201310214265.md): Frame · corroded · Oct 21, 2013 · N422AW · Cndair CL6002B19 · Fuselage Main, Frame > FS 349 FRAME CORRODED. R & R FRAME SEGMENT. - [SDR A6WA201310214264](https://openairdocs.org/sdr/A6WA201310214264.md): Frame · corroded · Oct 21, 2013 · N422AW · Cndair CL6002B19 · Fuselage Main, Frame > FS 310 FRAME HAS CORROSION. R & R FRAME SEGMENT. Next page: https://openairdocs.org/deregistered/N422AW-2018-11-07/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 = 'N422AW' AND deregistration_id = 'N422AW-2018-11-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N422AW-2018-11-07/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.