# Service difficulty reports: N605NW, cancelled May 5, 2008 A list on [N605NW, cancelled May 5, 2008](https://openairdocs.org/deregistered/N605NW-2008-05-05.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 · 54 reports - [SDR 0602479605](https://openairdocs.org/sdr/0602479605.md): Rod End · bent · Nov 16, 2006 · N605NW · Doug DC932 · Aileron Tab Control System > DURING THE CLIMB TO ALTITUDE AFTER TAKEOFF, THE AILERON TRIM FELT LOCKED UP OR FROZEN AND WAS INOPERATIVE AND UNUSABLE. THE FLIGHT CREW DIVERTED THE AIRCRAFT TO DTW AND NOTED THAT THE TRIM FREED UP AS THE AIRCRAFT DESCENDED BELOW 10,000 FEET. THE LANDING AT - [SDR 0601939605](https://openairdocs.org/sdr/0601939605.md): Rod End · broken · Sep 3, 2006 · N605NW · Doug DC932 · Leading Edge Devices > AS THE AIRCRAFT WAS ON APPROACH FOR LANDING AT BIS THE SLAT DEPLOYMENT WAS ASYMMETRICAL AND THE AIRCRAFT EXPERIENCED AND UNCOMMANDED ROLL. CREW RETRACTED THE LEADING EDGE DEVICES AND RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT MSP. MAINTENANCE FOUND - [SDR 0400559605](https://openairdocs.org/sdr/0400559605.md): Controller · failed · Apr 17, 2004 · N605NW · Doug DC932 · Cabin Pressure Controller > DURING CRUISE AT FL350 THE CABIN BEGAN AN UNCONTROLLED CLIMB. MANUAL CONTROL HAD NO EFFECT SO THE FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET. IT IS NOTED THE CREW WAS ABLE TO REGAIN MANUAL CONTROL DURING THE DESCENT. FLIGHT DIVERTED TO DTW AND L - [SDR 0400269605](https://openairdocs.org/sdr/0400269605.md): Skin · cracked · Jan 16, 2004 · N605NW · Doug DC932 · Fuselage Main, Plate/Skin > DURING (L) CHECK FOUND CRACK IN SKIN AS BS 996 BETWEEN L7L AND L8L. REPAIRED IAW EA 96-197817. - [SDR 0201949605](https://openairdocs.org/sdr/0201949605.md): Skin · cracked · May 20, 2002 · N605NW · Doug DC932 · Fuselage Main, Plate/Skin > During Hck in DHN, a crack was found in the skin common to the fasteners picking up the APB tee cap. Repaired per EA 96-190036. - [SDR 0003179605](https://openairdocs.org/sdr/0003179605.md): Skin · cracked · Sep 7, 2000 · N605NW · Doug DC932 · Fuselage Main, Plate/Skin > FUSELAGE EXTERIOR.25 INCH LONG CRACK 9 O''CLOCK POSITION AT NR 2 AFT DOOR STOP ADJUST HOLE. TRIMMED OUTER SKIN, CRACK REMOVED. FABRICATED DOUBLER AND FILLER. REPAIRED PER EA 96-179114 AND SRM 53-05 FIG 114. LOGPAGE 1491024. - [SDR 9809599605](https://openairdocs.org/sdr/9809599605.md): Engine · failed · May 23, 1998 · N605NW · Doug DC932 · Engine (Turbine/Turboprop) > DURING CLIMB AT 1500 FEET, THE LEFT ENGINE EXPERIENCED A CONTAINED FAILURE. AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK. - [SDR 9807109605](https://openairdocs.org/sdr/9807109605.md): Apu · oil leak · Apr 23, 1998 · N605NW · Doug DC932 · APU Oil System > LEFT AFT LAVATORY SMOKE ALARM ACTIVATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. PROBLEM COULD NOT BE DUPLICATED ON GROUND. IT IS SUSPECTED THAT RESIDUAL OIL FROM THE APU LEAKED INTO THE PNEUMATIC SYSTEM. AIRCRAFT WAS RETURNED - [SDR 9807209605](https://openairdocs.org/sdr/9807209605.md): Apu · failed · Apr 22, 1998 · N605NW · Doug DC932 · APU Oil System > AFTER ENGINE START SMOKE BEGAN TO ENTER CABIN. PLANE WAS AT THE GATE AND PASSENGERS WERE DEPLANED THROUGH THE GATEWAY. MAINTENANCE ISOLATED SOURCE OF SMOKE TO OIL IN PNEUMATIC SYSTEM FROM THE APU. PLACED APU ON MEL AND REPLACED WATER SEPARATORS. - [SDR 9807389605](https://openairdocs.org/sdr/9807389605.md): Bulkhead Doubler · cracked · Apr 16, 1998 · N605NW · Doug DC932 · Fuselage Main, Bulkhead > DURING LINE CHECK, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER ABOVE THE LEFT DOOR STOP FITTING. REPAIRED PER EA 96-156476. - [SDR 9805199605](https://openairdocs.org/sdr/9805199605.md): Fuse · blown · Mar 29, 1998 · N605NW · Doug DC932 · Emergency Lighting > DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT FORWARD GALLEY DOOR AND BETWEEN ROWS 1 THRU 4 INOPERATIVE. REPLACED FUSE IN EMERGENCY EXIT SIGN AT FORWARD GALLEY DOOR, OPERATIONAL CHECK NORMAL. - [SDR 9720479605](https://openairdocs.org/sdr/9720479605.md): Skin · cracked · Oct 20, 1997 · N605NW · Doug DC932 · Fuselage Main, Plate/Skin > DURING L-CHECK, FOUND CRACK IN FUSELAGE SKIN AT FASTENER LOCATED APPROXIMATELY 2 INCHES FORWARD OF COPILOT'S WINDSHIELD WIPER BASE. REPAIRED PER EA 96-151773. - [SDR 9719589605](https://openairdocs.org/sdr/9719589605.md): Batteries · discharged · Oct 18, 1997 · N605NW · Doug DC932 · Emergency Lighting > DURING PERIODIC CHECK, EMERGENCY LIGHTS AT FORWARD ENTRY, SERVICE ENTRY, AND COCKPIT OVERHEAD FAILED TEN MINUTE TEST. REPLACED BATTERIES IN BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9719579605](https://openairdocs.org/sdr/9719579605.md): Battery Packs · discharged · Oct 18, 1997 · N605NW · Doug DC932 · Emergency Lighting > DURING PERIODIC CHECK, RIGHT NACELLE, LEFT NACELLE, AND EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEN MINUTE TEST. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. - [SDR 9720469605](https://openairdocs.org/sdr/9720469605.md): Press Panel · cracked · Oct 17, 1997 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 83, LEFT SIDE AT VERTICAL FRAME FITTING. REPAIRED PER EA 96-151763. - [SDR 9719719605](https://openairdocs.org/sdr/9719719605.md): Press Panel · cracked · Oct 16, 1997 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING L CHECK, FOUND CRACKS IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 110 AT THE INBOARD AND OUTBOARD VERTICAL FITTINGS. REPAIRED PER EA 96-151761. - [SDR 9717139605](https://openairdocs.org/sdr/9717139605.md): Batteries · discharged · Sep 8, 1997 · N605NW · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 5 THRU 9 WOULD NOT TEST. REPLACED BATTERIES AT POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9717136305](https://openairdocs.org/sdr/9717136305.md): Batteries · discharged · Sep 8, 1997 · N605NW · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 5 THRU 9 WOULD NOT TEST. REPLACED BATTERIES AT POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9716859605](https://openairdocs.org/sdr/9716859605.md): Downlock Sw · failed · Sep 5, 1997 · N605NW · Doug DC932 · Landing Gear Position and Warning > LEFT MAIN LANDING GEAR FAILED UPLATCH CHECK WITH GEAR UNSAFE LIGHT ON AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH, OPERATIONAL CHECK NORMAL. - [SDR 9716079605](https://openairdocs.org/sdr/9716079605.md): Egt Indicator · corroded · Aug 20, 1997 · N605NW · Doug DC932 · Engine EGT/TIT Indicating System > DURING TAKEOFF ROLL AT 90 KNOTS, THE LEFT ENGINE EGT INDICATION EXCEEDED NORMAL OPERATING LIMITS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE EGT INDICATOR, NR 5 EGT THERMOCOUPLE, AND EGT BALANCE RESISTOR. ENGINE OPER - [SDR 9710789605](https://openairdocs.org/sdr/9710789605.md): Servo · malfunctioned · Jun 3, 1997 · N605NW · Doug DC932 · Autopilot Main Servo > ELEVATOR LOCKED UP DURING CRUISE FLIGHT AT 31,000 FEET WITH AUTO-PILOT INOPERATIVE. CREW DECLARED AN EMERGENCY AND FLIGHT DIVERTED TO STL. AIRCRAFT LANDED WITHOUT INCIDENT. NOTE: FREE MOVEMENT OF ELEVATOR WAS ACCOMPLISHED AT 3,000 FEET AND 140 KNOTS AIRSPE - [SDR 9707599605](https://openairdocs.org/sdr/9707599605.md): Switch · malfunctioned · Apr 15, 1997 · N605NW · Doug DC932 · Landing Gear Position and Warning > LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR WITH SAME RESULTS. SPEED WAS INCREASED TO 290 KNOTS AND GEAR DOOR OPEN LIGHT ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT - [SDR 9704739605](https://openairdocs.org/sdr/9704739605.md): Battery Pack · discharged · Mar 6, 1997 · N605NW · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AND LEFT AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9700169605](https://openairdocs.org/sdr/9700169605.md): Uplock Switch · malfunctioned · Jan 6, 1997 · N605NW · Doug DC932 · Landing Gear Position and Warning > DURING CLIMBOUT, THE LEFT AND RIGHT MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR WITH SAME RESULTS. FLIGHT CONTINUED TO DESTINATION AT REDUCED SPEED AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES, DISC - [SDR 9700259605](https://openairdocs.org/sdr/9700259605.md): Slide · low pressure · Jan 4, 1997 · N605NW · Doug DC932 · Escape Slide > DURING LINE MAINTENANCE INSPECTION, FOUND AFT TAIL COMPARTMENT EMERGENCY EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. - [SDR 9626699605](https://openairdocs.org/sdr/9626699605.md): Starter · failed · Dec 17, 1996 · N605NW · Doug DC932 · Engine Starter > DURING CLIMB, THE RIGHT ENGINE FIRE WARNING SYSTEM ILLUMINATED. CREW PULLED THE RIGHT ENGINE FIRE HANDLE AND FIRED ONE BOTTLE. THE A/C RETURNED TO AUS AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION, MAINTENANCE FOUND THE RIGHT ENGINE STARTER HAD EXPER - [SDR 9622649605](https://openairdocs.org/sdr/9622649605.md): Latch Assy · failed · Oct 21, 1996 · N605NW · Doug DC932 · Landing Gear Door Retract Section > LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAITNENANCE REPLACED LEFT MAIN GEAR DOOR UPLATCH ASSEMBLY, OPERATIONAL CHECK NORMAL. - [SDR 9620779605](https://openairdocs.org/sdr/9620779605.md): Downlock Switch · malfunctioned · Sep 27, 1996 · N605NW · Doug DC932 · Landing Gear Position and Warning > DURING CLIMBOUT ON GEAR RETRACTION, GOT LEFT GEAR UNSAFE LIGHT. RECYCLED GEAR AND RETURNED TO SLC. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LEFT DOWNLOCK SWITCH, CHECKED WIRING AND UPLOCK SWITCH, RAN GEAR SEVERAL TIMES AND OPERATIONAL CHECK GOOD. - [SDR 9620869605](https://openairdocs.org/sdr/9620869605.md): Connectors · dirty · Sep 26, 1996 · N605NW · Doug DC932 · Landing Gear Position and Warning > LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR WITH SAME RESULTS. FLIGHT RETURNED TO SLC AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND RESEATED ELECTRICAL CONNECTORS TO SWITCHES. OPERATIONAL CHECK NORMAL ON GEAR SWING. - [SDR 9620609605](https://openairdocs.org/sdr/9620609605.md): Slide · low pressure · Sep 26, 1996 · N605NW · Doug DC932 · Escape Slide > DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. - [SDR 9620559605](https://openairdocs.org/sdr/9620559605.md): Radar System · malfunctioned · Sep 25, 1996 · N605NW · Doug DC932 · Weather Radar System > WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RADAR TRANSCEIVER AND INDICATOR, OPERATIONAL CHECK NORMAL. - [SDR 9618809605](https://openairdocs.org/sdr/9618809605.md): Uplock Switch · malfunctioned · Aug 26, 1996 · N605NW · Doug DC932 · Landing Gear Position and Warning > LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME RESULTS. FLIGHT RETURNED TO YYC AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO MSP. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK SWITCH, OPERATIONAL CHECK - [SDR 9617259605](https://openairdocs.org/sdr/9617259605.md): Wire · broken · Aug 5, 1996 · N605NW · Doug DC932 · Light System Wiring > DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT SEAT 3C INOPERATIVE. REPAIRED BROKEN WIRE, OPERATIONAL CHECK NORMAL. - [SDR 9611989605](https://openairdocs.org/sdr/9611989605.md): Power Supply · inoperative · May 24, 1996 · N605NW · Doug DC932 · Emergency Lighting > DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 18 TO 21 AND AFT ENTRY INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9606179605](https://openairdocs.org/sdr/9606179605.md): Socket · shorted · Mar 15, 1996 · N605NW · Doug DC932 · Landing Gear Position and Warning > DURING CLIMBOUT AT APPROXIMATELY 28,000 FEET, THE LEFT MAIN LANDING GEAR GREEN LIGHT ILLUMINATED. NO VIBRATION OR YAW WAS FELT. HYDRAULIC PUMP WAS SWITCHED TO HIGH WITH NO CHANGE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. LIGHT REMAINED ON THROUG - [SDR 9606549605](https://openairdocs.org/sdr/9606549605.md): Bulkhead · corroded · Feb 22, 1996 · N605NW · Doug DC932 · Fuselage Main, Bulkhead > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 1046 CANTED BULKHEAD UPPER CAP BETWEEN LONGERONS 3L TO 6L. REPAIRED CAP PER EA 99-108995. - [SDR 9606529605](https://openairdocs.org/sdr/9606529605.md): Frame · corroded · Feb 20, 1996 · N605NW · Doug DC932 · Fuselage Main, Frame > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION AT THE FS 1121 WEB JUST OUTBOARD OF LONGERON 1 LOOKING AFT. REPAIRED THE WEB (P/N 9911839-117) PER EA 99-108851. - [SDR 9604529605](https://openairdocs.org/sdr/9604529605.md): Fitting · corroded · Feb 15, 1996 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 26R END FITTING AT FS 996. REPLACED FITTING PER SRM 51-01. - [SDR 9606519605](https://openairdocs.org/sdr/9606519605.md): Spar Web · corroded · Feb 12, 1996 · N605NW · Doug DC932 · Vertical Stabilizer, Spar/Rib > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE VERTICAL STABILIZER AFT SPAR WEB AT ZRS 65 AND 75. REPAIRED WEB (P/N 9911834-175) PER EA 99-108802. - [SDR 9603869605](https://openairdocs.org/sdr/9603869605.md): Fitting · corroded · Feb 9, 1996 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 22L SPLICE AT FS 863. REPLACED SPLICE FITTING PER SRM 51-01. - [SDR 9603859605](https://openairdocs.org/sdr/9603859605.md): Fitting · corroded · Feb 9, 1996 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 19L END FITTING AT FS 996. REPLACED FITTING PER SRM 51-01. - [SDR 9606509605](https://openairdocs.org/sdr/9606509605.md): Longeron · corroded · Feb 8, 1996 · N605NW · Doug DC932 · Wing, Longeron/Stringer > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION AND CRACKS IN THE CENTER WING TANK STR 19 AND 21 AT THE WS 58.5 BULKHEAD. REPAIRED STRINGERS PER EA 99-108792. - [SDR 9606499605](https://openairdocs.org/sdr/9606499605.md): Spar · corroded · Feb 6, 1996 · N605NW · Doug DC932 · Wing Spar > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER T-CAP BETWEEN XRS 470 TO 531. REPAIRED T-CAP (P/N 5911302-502) PER EA 99-108804. - [SDR 9606489605](https://openairdocs.org/sdr/9606489605.md): Skin · corroded · Feb 6, 1996 · N605NW · Doug DC932 · Fuselage Main, Plate/Skin > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 1095, LONGERON 18R. REPAIRED SKIN PER EA 99-108841. - [SDR 9603289605](https://openairdocs.org/sdr/9603289605.md): Fitting · cracked · Feb 6, 1996 · N605NW · Doug DC932 · Nacelle/Pylon, Attach Fittings > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT PYLON AFT SPAR UPPER FORWARD INBOARD FITTING APPROXIMATELY FS 1038. REPLACED FITTING PER SRM 51-30-25. - [SDR 9606479605](https://openairdocs.org/sdr/9606479605.md): Trapezoidal Pnl · cracked · Feb 4, 1996 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT TRAPEZOIDAL PANEL AFT FLANGE AT LONGERON 20R. REPAIRED PANEL (P/N 9919402-2) PER EA 99-103135. - [SDR 9602439605](https://openairdocs.org/sdr/9602439605.md): Fitting · cracked · Jan 29, 1996 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE KEEL WEB ATTACH FITTING FS 744 TO 756, IN THE LOWER INBOARD AFT CORNER OF THE LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED FITTING PER SRM 51-01. - [SDR 9602379605](https://openairdocs.org/sdr/9602379605.md): Fitting · cracked · Jan 26, 1996 · N605NW · Doug DC932 · Fuselage Miscellaneous Structure > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE KEEL WEB TO FLOORBEAM ATTACH FITTING AT FS 718. REPLACED FITTING PER SRM 51-01. - [SDR 9606469605](https://openairdocs.org/sdr/9606469605.md): Frame · corroded · Jan 23, 1996 · N605NW · Doug DC932 · Fuselage Main, Frame > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION AT THE FS 148 FRAME AT LONGERON 8R. REPAIRED FRAME (P/N 9911514) PER EA 99-108799. - [SDR 9606459605](https://openairdocs.org/sdr/9606459605.md): Skin · corroded · Jan 23, 1996 · N605NW · Doug DC932 · Fuselage Main, Plate/Skin > DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 389 TO 406, LONGERONS 27R TO 28R. REPAIRED PANEL ASSEMBLY (P/N 5911412) PER EA 99-108803. Next page: https://openairdocs.org/deregistered/N605NW-2008-05-05/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 = 'N605NW' AND deregistration_id = 'N605NW-2008-05-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N605NW-2008-05-05/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.