# Service difficulty reports: N611AW, cancelled Feb 7, 2008 A list on [N611AW, cancelled Feb 7, 2008](https://openairdocs.org/deregistered/N611AW-2008-02-07.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 2 · 90 reports - [SDR A6WA200460020](https://openairdocs.org/sdr/A6WA200460020.md): Sill · corroded · Jun 7, 2004 · N611AW · Bac 146300A · Fuselage Miscellaneous Structure > L1 SILL PLATE CORRODED BEYOND LIMITS. SIL PLATE L1 REPAIRED IAW BAE SRM 51-43-00, 51-42-00 AND 51-23-00. (M) - [SDR A6WA200460019](https://openairdocs.org/sdr/A6WA200460019.md): Skin · scratched · Jun 2, 2004 · N611AW · Bag BAE146300A · Cargo/Baggage Doors > AFT CARGO DOOR SCRATCHES BEYOND THE ALLOWABLE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS. MAINTENANCE CUT DAMAGED AREA OUT IAW BAE SRM 52-32-11 FIG 201 PARA 3B PER BAE FAX BARA/AVR/6767/04-DC. HFEC INSPECTION C/O ON CUT OUT REPAIR, NO CRACKS N - [SDR A6WA200460018](https://openairdocs.org/sdr/A6WA200460018.md): Flap Track · worn · May 28, 2004 · N611AW · Bac 146300A · Trailing Edge Flaps > LT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908004. DAMAGED AREA MAPPED AND SUBMITTED TO BAE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6761/04-MK, NO CRACKS NOTED. DV - [SDR A6WA200460017](https://openairdocs.org/sdr/A6WA200460017.md): Flap Track · worn · May 28, 2004 · N611AW · Bac 146300A · Trailing Edge Flaps > RT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908003. MAINTENANCE MAPPED AND SUBMITTED TO BE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6762/04-04-MK. NO CRACKS NOTED. - [SDR A6WA200460016](https://openairdocs.org/sdr/A6WA200460016.md): Floorbeam · cracked · May 26, 2004 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam > CRACK LOCATED IN THE LOWER RADIUS OF FLOORBEAM 33B AT LBL 62.0 INCHES. MAINTENANCE REQUESTED REPAIRS FROM MFG SYSTEMS REF AVMAX FAX 611-1908002. REPAIRED IAW BAE FAX BARA/AVR/6759/04-DC AND BARA/AVR/6752/04-02. PRIMED IAW BAE 146 AMM 20-10-11. (M) - [SDR A6WA200460014](https://openairdocs.org/sdr/A6WA200460014.md): Fuel Control · fluctuates · May 9, 2004 · N611AW · Bag BAE146300A · Fuel Control/Turbine Engines > WHILE IN VMC CLIMBING THROUGH 16000 FEET THE NR 3 ENGINE N1 FLUCTUATION FOLLOWED BY FUEL FLOW DROPPING TO ZERO. ENGINE WAS SHUTDOWN, REMAINDER OF FLT MIN N2 OF 8 PERCENT, N1 26, 10 PSI, OIL QUANT 3/4 FULL. MAINTENANCE REMOVED AND REPLACED NR 3 FUEL CONTROL U - [SDR A6WA200360044](https://openairdocs.org/sdr/A6WA200360044.md): Skin · lightning strike · Oct 2, 2003 · N611AW · Bag BAE146300A · Fuselage Main, Plate/Skin > DAMAGE NOTED ON LEFT SIDE OF FUSELAGE DURING LIGHTNING STRIKE INSPECTION. EXIT BURN MARK LOCATED 8 INCHES AFT OF FRAME 19C BETWEEN STRINGER 21 AND 22 AT CENTER AND APPROX.375 INCH IN DIAMETER BY.010 INCHES DEPTH. MAINTENANCE BLENDED DAMAGE TO A SMOOTH MIRRO - [SDR A6WA200360029](https://openairdocs.org/sdr/A6WA200360029.md): Conduit · damaged · May 23, 2003 · N611AW · Bac 146300A · Fuselage Miscellaneous Structure > FLANGED CONDUIT P/N HC535B0285-000 IS KINKED AND HAS TWO HOLES. MAINTENANCE WELDED CONDUIT IAW BAE FAX BARA/AVR/6411/03-DC. (M) - [SDR A6WA200100050](https://openairdocs.org/sdr/A6WA200100050.md): Odor · detected · Aug 3, 2001 · N611AW · Bac 146300A · Air Distribution System > AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMELL IN FWD GALLEY AREA, GALLEY LOAD SHED, SMELL DISSIPATED. MAINTENANCE INSPECTED FWD CABIN AND GALLEY AREA, RAN ENGINES, USED ENGINE AIR WITH GALLEY POWER ON, NO SMELL NOTED. - [SDR A6WA200100011](https://openairdocs.org/sdr/A6WA200100011.md): Computer · malfunctioned · Feb 3, 2001 · N611AW · Bag BAE146300A · Leading Edge Slat Control System > AFTER TAKEOFF, FLAPS RETRACTED TO BETWEEN 0-18 DEGREES AND THEN STOPPED. AFTER CHECKLIST, RETRACTED TO 18 DEGREES RETURNED TO LANDING FLAP FAULT ILLUMINATED. MAINTENANCE RESET C/B L9, D24, E12, RERACKED FLAP COMPUTER, CLEARED FLAP FAULT. OP CHECKED GOOD. - [SDR A6WA200100010](https://openairdocs.org/sdr/A6WA200100010.md): Connector · disconnected · Jan 21, 2001 · N611AW · Bag BAE146300A · Emergency Lighting > THREE LIGHTS IN FRONT OF PASSENGER CABIN NOT ILLUMINATING. MAINTENANCE CLEANED AND RESECURED CONNECTOR PLUG TO EMERGENCY POWER SUPPLY ABOVE ROW 7, OPS CHECKED GOOD. - [SDR A6WA200000072](https://openairdocs.org/sdr/A6WA200000072.md): Proximity Sensor · malfunctioned · Dec 17, 2000 · N611AW · Bag BAE146300A · Landing Gear Position and Warning > UNSAFE RIGHT MLG INTRANSIT LIGHT ON WITH GEAR SELECTED UP ALSO ASSOCIATED GEAR HANDLE LIGHT ON. MAINTENANCE CLEANED DOOR UPLOCK PROXY SENSORS AND GEAR PROXY SENSORS, PERFORMED GEAR SWING, 3 CYCLES, ALL INDICATIONS NORMAL. - [SDR 99ZZZM603](https://openairdocs.org/sdr/99ZZZM603.md): Fire Bottle · damaged · Nov 11, 1998 · N611AW · Bag BAE146300A · Fire Bottle, Fixed > ENGINE NOSE COWL WO NR BY8402 HAD FIRE BOTTLE CL978M HAS WORN THREADS ON JUNCTION BOX AND CONTROL HEAD. REM AND REPLACED FIRE BOTTLE. (M) - [SDR 99ZZZM599](https://openairdocs.org/sdr/99ZZZM599.md): Mask · cracked · Jul 28, 1998 · N611AW · Bag BAE146300A · Passenger Oxygen System > FORWARD AFT FACING F/A OXYGEN BOTTLE, MASK FACE PIECE CRACKED. REPLACED OXYGEN MASK, OPS CHECKS OK. (M) - [SDR 99ZZZM600](https://openairdocs.org/sdr/99ZZZM600.md): Valve · failed · Jul 27, 1998 · N611AW · Bag BAE146300A · Passenger Oxygen System > CABIN OXYGEN SYSTEM FAILED LEAK CHECK. TROUBLESHOOT SYSTEM. REPLACED PAX ISO VLV, 5 QUICK DISC (OUTLETS), 4 RT BOX ASSY. SEE W/C'S FOR PARTS CHANGED, SYSTEM LEAK CHECKS OK. (M) - [SDR 99ZZZM591](https://openairdocs.org/sdr/99ZZZM591.md): Mask · torn · Jul 27, 1998 · N611AW · Bag BAE146300A · Passenger Oxygen System > OXYGEN MASK AT 9 RT FACE PIECE TORN. REPLACED OXYGEN MASK 9 RT, OPS AND LEAK CHECKS OK. (M) - [SDR 99ZZZM585](https://openairdocs.org/sdr/99ZZZM585.md): Outlets · leaking · Jul 27, 1998 · N611AW · Bag BAE146300A · Passenger Oxygen System > FOUND OXYGEN OUTLETS AT RT 6, 14, 17, 20, AND 21 LEAKING. REPLACED OUTLETS AT RT 6, 14, 17, 20, AND 21. LEAK CHECK OK. (M) - [SDR 99ZZZM583](https://openairdocs.org/sdr/99ZZZM583.md): Oxygen Box · leaking · Jul 27, 1998 · N611AW · Bag BAE146300A · Passenger Oxygen System > FOUND OXYGEN BOX AT 4 RT LEAKING THROUGH MASK WITH PIN INSTALLED. REPLACED OXYGEN BOX ASSY, OPS AND LEAK CHECKS OK. - [SDR 99ZZZM580](https://openairdocs.org/sdr/99ZZZM580.md): Manifold · leaking · Jul 23, 1998 · N611AW · Bag BAE146300A · Passenger Oxygen System > FOUND 4 RT OXYGEN BOX, 2 MASK LEAKING WITH PINS INSTALLED, OXYGEN MASK FACE PIECE TORN. REPLACED 4 RIGHT OXYGEN MANIFOLD, OPS AND LEAK CHECKS OK. REPLACED MASK ASSY, LEAK AND OPS CHECKS OK. (M) - [SDR 99ZZZM590](https://openairdocs.org/sdr/99ZZZM590.md): Door · chafed · Jul 21, 1998 · N611AW · Bag BAE146300A · Engine Cowling System > NR 3 ENGINE INBOARD FAN DOOR LOWER SPLITTER AREA, 2ND STIFFENER FROM FORWARD CHAFED. REPLACED THE NR 3 ENGINE INBOARD FAN DOOR LOWER SPLITTER AREA, 2ND STIFFENER FROM FORWARD. (M) - [SDR 99ZZZM589](https://openairdocs.org/sdr/99ZZZM589.md): Door · damaged · Jul 20, 1998 · N611AW · Bag BAE146300A · Engine Cowling System > NR 1 EIGNE INBOARD REAR COWL DOOR HAS A HOLE WORN THROUGH THE TOP 3RD RIB BACK FROM THE FRONT CORNER OF THE DOOR. REPLACED THE TOP THIRD RIB FROM THE FRONT EDGE OF THE NR 1 INBOARD REAR COWL DOOR SPLITTER. (M) - [SDR 99ZZZM587](https://openairdocs.org/sdr/99ZZZM587.md): Stiffener · cracked · Jul 20, 1998 · N611AW · Bag BAE146300A · Wing Miscellaneous Structure > LT WING TOP SKIN TE SHROUD OUTBOARD STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPAIRED ABOVE STIFFENER PER BAE FAX JM/RJO317/97 USING 2 024T3.050. (M) - [SDR 99ZZZM572](https://openairdocs.org/sdr/99ZZZM572.md): Intercostal · cracked · Jul 20, 1998 · N611AW · Bag BAE146300A · Entrance Stairs > AFT AIRSTAIR OUTBOARD RAIL INTERCOSTAL CRACK AT FLOOR, AFT END. REMOVED AND REPLACED AFT AIRSTAIR OUTBOARD RAIL INTERCOSTAL AT AFT END OF RAIL. WORK DONE IAW BAE MM 51-00-00. (M) - [SDR 99ZZZM596](https://openairdocs.org/sdr/99ZZZM596.md): Bracket · cracked · Jul 17, 1998 · N611AW · Bag BAE146300A · Hydraulic System, Main > LEFT WING HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR, RIB NR 3. REMOVED AND REPLACED ABOVE BRACKET. (M) - [SDR 99ZZZM592](https://openairdocs.org/sdr/99ZZZM592.md): Tread Plate · corroded · Jul 17, 1998 · N611AW · Bag BAE146300A · Fuselage Miscellaneous Structure > LEFT FORWARD TREAD PLATE (E804) HAS CORROSION ON INNER SURFACE. REMOVED CORROSION ON LT FORWARD TREAD PLATE 9E804). (M) - [SDR 99ZZZM613](https://openairdocs.org/sdr/99ZZZM613.md): Structure · corroded · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Miscellaneous Structure > FOUND CORROSION AROUND MOUNTING HOLES FOR GALLEY. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICABLE AREAS AROUND GALLEY MOUNTING HOLES. (M) - [SDR 99ZZZM612](https://openairdocs.org/sdr/99ZZZM612.md): Rivets · failed · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Miscellaneous Structure > CABIN FLOOR OUTBOARD SUPPORT ANGLE HAS 2 POPPED RIVETS AT FRAME 26 (RIGHT SIDE AFT OF FRAME). REPLACED RIVETS. (M) - [SDR 99ZZZM597](https://openairdocs.org/sdr/99ZZZM597.md): Floorbeam · cracked · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam > CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LEFT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M) - [SDR 99ZZZM588](https://openairdocs.org/sdr/99ZZZM588.md): Cowl · cracked · Jul 15, 1998 · N611AW · Bag BAE146300A · Engine Cowling System > NR 2 ENGINE PYLON SHOULDER COWL HAS CRACKED SKIN BETWEEN THE BIG HYD PIPE AND THE DRAIN TUBE. REPAIRED ABOVE CRACK USING.040 TA 2 PER FAX KG/0603-91 AND SRM. (M) - [SDR 99ZZZM582](https://openairdocs.org/sdr/99ZZZM582.md): Step · corroded · Jul 15, 1998 · N611AW · Bag BAE146300A · Entrance Stairs > AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP. - [SDR 99ZZZM579](https://openairdocs.org/sdr/99ZZZM579.md): Floorbeam · cracked · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam > CABIN PRESS FLOORBEAM NR 19 (RIGHT OUTBOARD SEAT RAIL) CRACKED AT FRAME 29. REPAIRED PER FAX REF DJR/RJO207-97 AND REPAIR DRAWING HC536H9211. (M) - [SDR 99ZZZM578](https://openairdocs.org/sdr/99ZZZM578.md): Floorbeam · cracked · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam > CABIN PRESSURE FLOORBEAM NR 13 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. - [SDR 99ZZZM577](https://openairdocs.org/sdr/99ZZZM577.md): Floorbeam · cracked · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam > CABIN PRESS FLOORBEAM NR 15 CRACKED AT FRAME 29, RIGHT INBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M) - [SDR 99ZZZM576](https://openairdocs.org/sdr/99ZZZM576.md): Floorbeam · cracked · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam > CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M) - [SDR 99ZZZM575](https://openairdocs.org/sdr/99ZZZM575.md): Floorbeam · cracked · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam > CABIN PRESS FLOORBEAMS NR 9 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M) - [SDR 99ZZZM571](https://openairdocs.org/sdr/99ZZZM571.md): Sill · corroded · Jul 15, 1998 · N611AW · Bag BAE146300A · Fuselage Miscellaneous Structure > PAX DOOR SILL PLATE SOME LIGHT SURFACE CORROSION, MARKED W/DOT. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICABLE AREA. (M) - [SDR 99ZZZM584](https://openairdocs.org/sdr/99ZZZM584.md): Door · chafed · Jul 14, 1998 · N611AW · Bag BAE146300A · Engine Cowling System > NR 3 ENGINE INBOARD FAN DOOR INNER TITANIUM DISHING CHAFED THROUGH. REPAIRED CHAGED AREA OF NR 3 ENGINE INBOARD FAN DOOR INNER SKIN IAW 146 RIL HC711H9047. (M) - [SDR 99ZZZM586](https://openairdocs.org/sdr/99ZZZM586.md): Door · chafed · Jul 13, 1998 · N611AW · Bag BAE146300A · Engine Cowling System > NR 4 ENGINE INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH JUST ABOVE DISHING AREA. REPAIRED CHAFED AREA IAW RIL HC711H9047. (M) - [SDR 99ZZZM581](https://openairdocs.org/sdr/99ZZZM581.md): Stair · corroded · Jul 13, 1998 · N611AW · Bag BAE146300A · Entrance Stairs > AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP. - [SDR 99ZZZM595](https://openairdocs.org/sdr/99ZZZM595.md): Bracket · cracked · Jul 10, 1998 · N611AW · Bag BAE146300A · Hydraulic System, Main > RIGHT WING TE HYD CLAMP BRACKET CRACKED AT FALSE SPAR, RIB 6. ALSO, HYD CLAMP LOOSE OUTBOARD OF RIB 6. REPLACED ONE RIGHT WING TRAILING EDGE HYD CLAMP BRACKET (P/N HC932HO178-003) AT FALSE SPAR, RIB 6. TIGHTENED BOLTS SECURING HYD CLAMP OUTBOARD OF RIB 6. - [SDR 99ZZZM594](https://openairdocs.org/sdr/99ZZZM594.md): Structure · worn · Jul 9, 1998 · N611AW · Bag BAE146300A · Nacelle/Pylon Structure > NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH HOLES WORN AND SLOPPY AT SHOULDER COWL STRUCTURE. REPAIR PER RI HC710H9033. REPAIRED NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH STRUCTURE HOLES IAW BAE REPAIR DRAWING HC710H9003. (M) - [SDR 99ZZZM593](https://openairdocs.org/sdr/99ZZZM593.md): Angle · cracked · Jul 9, 1998 · N611AW · Bag BAE146300A · Wing Miscellaneous Structure > RIGHT WING TE LOWER SKIN, INBOARD STIFFENER BETWEEN RIBS 8/9 TAG ANGLE CRACKED AFT END OF STIFFENER. REPLACED SAID TAG ANGLE AND FOUND SERVICEABLE. (M) - [SDR 99ZZZM573](https://openairdocs.org/sdr/99ZZZM573.md): Control Cable · corroded · Jul 9, 1998 · N611AW · Bag BAE146300A · Aileron Control System > BOTH CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER AILERON INTERCONNECT CABLES, GENERATED NEW WC FOR TRAVEL CHECKS AND FREEDOM OF MOVEMENT. (M) - [SDR 99ZZZM574](https://openairdocs.org/sdr/99ZZZM574.md): Trim Strip · corroded · Jul 7, 1998 · N611AW · Bag BAE146300A · Passenger Compartment Equipment > FRAME 18 TRIM STRIP FOR UNDER RIGHT BULKHEAD BADLY CORRODED, REPLACED. REMOVED AND REPLACED FRAME 18 TRIM STRIP. - [SDR 99ZZZM598](https://openairdocs.org/sdr/99ZZZM598.md): Slide · cracked · Jul 1, 1998 · N611AW · Bag BAE146300A · Escape Slide > LEFT FORWARD EVAC SLIDE PACK BOARD CRACKED AT TOP MOUNT PP PIN. REMOVED SLIDE ASSY AND PLACED ON W/O, P/N 31050-105, S/N 0093, REF W/C 8012 FOR INSTALLATION. (M) - [SDR 99ZZZM535](https://openairdocs.org/sdr/99ZZZM535.md): Engine · failed · Jan 16, 1998 · N611AW · Bag BAE146300A · Engine (Turbine/Turboprop) > NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN. DIVERTED TO LAS. REMOVED AND REPLACED NR 1 ENGINE IAW AWAC ENDING CHANGE CHECKLIST AND AIRCRAFT MM. (M) - [SDR 98ZZZX1197](https://openairdocs.org/sdr/98ZZZX1197.md): Engine · failed · Jan 16, 1998 · N611AW · Bag BAE146300A · Engine (Turbine/Turboprop) > SBA - FLT 586 - NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN - DIVERTED TO LAS. UNDER FURTHER INVESTIGATION. - [SDR 98ZZZM96](https://openairdocs.org/sdr/98ZZZM96.md): Valve · failed · Jul 29, 1997 · N611AW · Bag BAE146300A · Pneumatic Distribution System > NR 3 NOSE COWL FLOW CONTROL VALVE WAS FOUND TO HAVE A RIVET IN THE FAIL/SAFE MODE TO BE WORN EXCESSIVELY. REPLACED VALVE. (M) - [SDR 97ZZZX3050](https://openairdocs.org/sdr/97ZZZX3050.md): Fire Wire · chafed · Jun 26, 1997 · N611AW · Bag BAE146300A · Fire Detection > ATW - NR 2 ENGINE INBOARD FIRE EXTINGUISHER WIRES ARE CHAFED BY NOSE COWL DISCONNECT. REPLACED WIRES 2WB170 AND 2WB173. SEE ENGINE CHANGE CHECK LIST FOR TEST OF FIRE EXTINGUISHING SYSTEM. ` - [SDR 97ZZZX3109](https://openairdocs.org/sdr/97ZZZX3109.md): Skin · cracked · Apr 3, 1997 · N611AW · Bag BAE146300A · Wing, Plate/Skin > LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT FORWARD END APPROXIMATELY.75 INCH LONG LOCATED IN AREA BETWEEN WING RIBS 5 AND 6. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97. Next page: https://openairdocs.org/deregistered/N611AW-2008-02-07/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 = 'N611AW' AND deregistration_id = 'N611AW-2008-02-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N611AW-2008-02-07/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.