# Service difficulty reports: N820NK, cancelled May 9, 2005 A list on [N820NK, cancelled May 9, 2005](https://openairdocs.org/deregistered/N820NK-2005-05-09.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 · 156 reports - [SDR GTIA050126](https://openairdocs.org/sdr/GTIA050126.md): Fuel Control · out of trim · Apr 10, 2005 · N820NK · Doug DC982 · Fuel Controlling System > NR 1 ENGINE IDLE IS TO LOW WITH BLEED 45-47 PERCENT N2 ENGINE EXTREMELY SLOW TO ACCELERATE, EGT IS 490 AT IDLE, MUST MOVE THROTTLE 1 KNOB FORWARD TO MAINTAIN 50 PERCENT N2, NR 2 ENGINE IDLE IS TO LOW WITH BLEED ON 48 PERCENT N2 ENGINE IS VERY SLOW TO ACCELERAT - [SDR GTIA050072](https://openairdocs.org/sdr/GTIA050072.md): Indicator · intermittent · Mar 14, 2005 · N820NK · Doug DC982 · Rate of Climb Indicator > F/O`S VSI INDICATOR GOES ON AND OFF, INTERMITTENT. TAIL SWAP WITH AC N819. REMOVED AND REPLACED VSI INDICATOR. (K) - [SDR GTIA050058](https://openairdocs.org/sdr/GTIA050058.md): Cover · damaged · Mar 10, 2005 · N820NK · Doug DC982 · Ailerons > LT AILERON IB UPPER ATTACH FITTING COVER DAMAGED, AIRCRAFT TAIL SWAP WITH 819NK. INSTALLED LT AILERON IB UPPER ATTACH FITTING COVER. (K) - [SDR GTIA050044](https://openairdocs.org/sdr/GTIA050044.md): Windshield · cracked · Feb 20, 2005 · N820NK · Doug DC982 · Flight Compartment Windows > F/O WINDSHIELD CRACKED IN FLIGHT, OUTER PANE ONLY. AIRCRAFT TAIL SWAP WITH N835NK. REMOVED AND REPLACED WINDSHIELD. (K) - [SDR GTIA050010](https://openairdocs.org/sdr/GTIA050010.md): Strut · iced · Jan 18, 2005 · N820NK · Doug DC982 · Main Landing Gear Strut/Axle/Truck > FLT 202 - DTW - AFTER TAKEOFF GEAR WOULD NOT RETRACT, RETURNED TO DTW, NORMAL LANDING WEIGHT FOR LANDING, AIRCRAFT TAIL SWAP. UPON INSPECTION, FOUND NOSE STRUT PACKED WITH ICE, CLEANED, REPACKED AND SERVICED. (M) - [SDR GTIA050005](https://openairdocs.org/sdr/GTIA050005.md): Lanyard · broken · Jan 11, 2005 · N820NK · Doug DC982 · Escape Slide > FLL - L1 ESCAPE SLIDE LANYARD BROKEN. INSTALLED NEW LANYARD ON L1 DOOR SLIDE. (M) - [SDR GTIA040860](https://openairdocs.org/sdr/GTIA040860.md): Lanyard · disconnected · Dec 13, 2004 · N820NK · Doug DC982 · Escape Slide > DTW - FOUND L1 DOOR EVAC SLIDE DEPLOYMENT LANYARD DISCONNECTED FROM SLIDE ASSY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE. (M) - [SDR GTIA040828](https://openairdocs.org/sdr/GTIA040828.md): Engine · malfunctioned · Oct 27, 2004 · N820NK · Doug DC982 · Engine (Turbine/Turboprop) > LT 283881; INFLIGHT SHUTDOWN - DIVERSION, SHUTDOWN LT ENGINE DUE TO LOW OIL PRESSURE, LOW OIL QTY. REMOVED AND REPLACED NR 1 ENGINE. - [SDR GTIA040816](https://openairdocs.org/sdr/GTIA040816.md): Spring · broken · Oct 17, 2004 · N820NK · Doug DC982 · Service Doors > R1 SVC, DOOR BAYONET ROLLER HELICAL TORSION SPRING BROKEN. REMOVED AND REPLACED R1 DOOR BAYONET ROLLER HELICAL TORSION SPRING. OPS CHECK GOOD IAW 52-41-00. - [SDR GTIA040742](https://openairdocs.org/sdr/GTIA040742.md): Bearing · failed · Aug 22, 2004 · N820NK · Doug DC982 · Landing Gear Retraction/Extension System > FLT 380 - LT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. GEAR RECYLE SATISFACTORY. REPLACED BEARING ON LEFT TORQUE TUBE VERIFIED PROPER RIGGING. PERFORMED MULTIPLE GEAR SWINGS CHECKS GOOD. (M) - [SDR GTIA040741](https://openairdocs.org/sdr/GTIA040741.md): Control Valve · malfunctioned · Aug 19, 2004 · N820NK · Doug DC982 · Landing Gear Retraction/Extension System > AFTER TAKEOFF, AIRCRAFT SPEED APPROX 150 KNOTS THERE WAS NO DRAG 100 FEET AGL 12 DEGREE PITCH UPLEFT MAIN GEAR, GEAR WAS UP RED LIGHT STAYED ON AFTER GEAR RETRACTION GEAR DOOR OPEN LIGHT WAS NOT ON AND NOSE AND RIGHT MAIN GEAR LIGHTS NOT ON AT SPEED 200 KNOTS - [SDR GTIA040725](https://openairdocs.org/sdr/GTIA040725.md): Conduit · out of position · Aug 17, 2004 · N820NK · Doug DC982 · Landing Gear System Wiring > DTW - FLT 563 - AFTER TAKEOFF LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON/RED FOR ONE MINUTE AFTER ALL OTHER LANDING GEAR LIGHTS OUT. AS SLOWED TO 230 KIAS FOR QRH PROCEDURE LIGHT WENT OUT AND REMAINED OUT FOR REMAINDER OF FLIGHT. FOUND WIRE CONDUIT FROM GEAR UP - [SDR GTIA040748](https://openairdocs.org/sdr/GTIA040748.md): Roller · out of adjust · Aug 17, 2004 · N820NK · Doug DC982 · Landing Gear Door Retract Section > DURING CRUISE FLIGHT, GEAR DOOR OPEN LIGHT CAME ON, PUT HYDRAULIC PUMPS ON HIGH AND LIGHT WENT OUT AFTER APPROXIMATELY 3 MINUTES. FOUND DOOR ROLLER TO HOOK CLEARANCE OUT OF ADJUSTMENT. ADJUSTED CLEARANCE. (M) - [SDR GTIA040722](https://openairdocs.org/sdr/GTIA040722.md): Proximity Sensor · malfunctioned · Aug 16, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > LGA - FLT 779 - FOUND LEFT MAIN GEAR UNSAFE LIGHT CAME ON AND STAYED ON IN FLIGHT. FOLLOW QRH PROCEDURES CONT TO FLL AT.700 MACH. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. (M) - [SDR GTIA040723](https://openairdocs.org/sdr/GTIA040723.md): Proximity Sensor · malfunctioned · Aug 14, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > ORD - FLT 1525 - LEFT MAIN LANDING GEAR INDICATOR STAYED RED AFTER GEAR RETRACTION FOLLOWED QRH AND HAD NORMAL INDICATIONS AFTER. REMOVED AND REPLACED LEFT MLG UPLOCK PROX SENSOR. PERFORMED OPS CHECK OF SENSOR THROUGH PROX SWITCH ELECT. (M) - [SDR GTIA040629](https://openairdocs.org/sdr/GTIA040629.md): Line · leaking · Jun 26, 2004 · N820NK · Doug DC982 · Hydraulic System, Main > LGA - FLT 779 - JUST AFTER TAKEOFF LGA, STRANGE ODOR CAME THROUGH VENTS. BRAKE TEMP INDICATOR LIGHT WAS FLASHING AND TEMP NEEDLE MOVING, LEFT LANDING GEAR DOWN TO MAKE SURE NO BRAKE HEAT, LIGHT WENT OUT, ODOR WENT AWAY. FOUND NR 2 BRAKE AFT HYD LINE LOOSE AN - [SDR GTIA040579](https://openairdocs.org/sdr/GTIA040579.md): Warning Light · malfunctioned · Jun 19, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > FOUND LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. (M) - [SDR GTIA040563](https://openairdocs.org/sdr/GTIA040563.md): Latch · stuck · Jun 7, 2004 · N820NK · Doug DC982 · Emergency Exits > LGA - FLT 1174 - FLIGHT ATTENDANT SAYS THAT AFT CABIN DOOR IS VERY HARD TO CLOSE. AFT FLIGHT ATTENDANT REPORTED SAFETY DOOR FOR TAIL CONE HANDLE ABOVE FLIGHT ATTENDANT SEAT WOULD NOT LATCH. FREED LATCH, OPS CHECK NORMAL. NO FAULT REPORTED OR FOUND WITH AFT - [SDR GTIA040549](https://openairdocs.org/sdr/GTIA040549.md): Uplock Sensor · out of adjust · May 28, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > ORD - FLT 1525 - FOUND LEFT MAIN GEAR INDICATES UNSAFE, RED LIGHT, WITH GEAR HANDLE UP DURING CLIMB AND CRUISE ONLY. T/S LEFT INDICATING SYSTEM CHECKED AIR GAPS ON MAIN GEAR LEFT UPLOCK, DOOR OPEN, AND DOWNLOCK PROX SENSORS. FOUND LEFT UPLOCK SENSOR OUT OF A - [SDR GTIA040512](https://openairdocs.org/sdr/GTIA040512.md): Sensor · inoperative · May 23, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > RT MAIN GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RAISED. GEAR WAS CYCLED AND LIGHT EXTINGUISHED. ADJUSTED RT MLG UP LATCH PROXIMITY SENSOR TO TARGET CLEARANCE. JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS. ALL INDICATIONS NORMAL. - [SDR GTIA040470](https://openairdocs.org/sdr/GTIA040470.md): Proximity Switch · out of limits · May 20, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > ON CLIMBOUT CENTER GER RED LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE (CYCLED GEAR DOWN AND UP) LIGHTS WENT OUT. JACKED AC NOSE GEAR AND PERFORMED NOSE GEAR RETRACTION TEST FOR UP/DOWN POSITION LIGHTS. NO FAULTS WERE NOTED ON SEVERAL - [SDR GTIA040469](https://openairdocs.org/sdr/GTIA040469.md): Control Valve · loose · May 14, 2004 · N820NK · Doug DC982 · Landing Gear Retraction/Extension System > IN CLIMB AT GEAR RETRACT LT MAIN GEAR UNSAFE LIGHT STAYED ON WITH GEAR HANDLE UP. CK QRH AND FOLLOWED PROCEDURE WITH NO CHANGE. LEAVING 10,000 FT AND PUTTING HYD. PUMPS TO LOW AND OFF THE GEAR DOOR OPEN LIGHT ALSO CAME ON. SELECTED ENGINE PUMPS TO HIGH AND - [SDR GTIA040453](https://openairdocs.org/sdr/GTIA040453.md): Proximity Switch · inoperative · May 13, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > LT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. DURING ARRIVAL INTO FLL. QRH C/W GEAR DOOR OPEN EXTINGUISH WITH HYDRAULIC SYSTEM HI. 3000 GEAR DOOR LIGHT ILLUMINATED AGAIN WITH HYDRAULIC SYSTEM IN 1500 PSI LOW POSITION. CLEANED AND ADJUSTED LT GE - [SDR GTIA040449](https://openairdocs.org/sdr/GTIA040449.md): Strap · frayed · May 4, 2004 · N820NK · Doug DC982 · Escape Slide > AFT TAIL SLIDE PACK COVER HOLD DOWN STRAP FRAYED AND PRESS GAUGE NOT IN WINDOW. REMOVED AND REPLACED FRAID COVER HOLD DOWN STRAP ON AFT TAILCONE SLIDEPACK. ADJUSTED PACK COVER SO GAUGE WAS VISIBLE. - [SDR GTIA040221](https://openairdocs.org/sdr/GTIA040221.md): Liner · loose · Mar 18, 2004 · N820NK · Doug DC982 · Engine Air Intake System > ACY - NR 2 ENGINE INTAKE LINER LOOSE FOUND ON WALKAROUND. REMOVED DAMAGED ACOUSTIC PANEL LINER. INLET COWL INSPECTION AND REPAIR OF THE DYNA ROHR ACOUSTIC PANELS ACOUSTIC LINING MISSING BETWEEN 4 O'CLOCK AND 8 O'CLOCK POSITION NOSE COWL TO BE REPLACED ON C/O - [SDR GTIA040141](https://openairdocs.org/sdr/GTIA040141.md): Warning Light · illuminated · Feb 21, 2004 · N820NK · Doug DC982 · Landing Gear Position and Warning > RSW - FLT 1605 - AFTER GEAR HANDLE SELECTED UP LT MAIN GEAR UNSAFE LIGHT (RED) REMAINED ON. CONSULTED QRH, GEAR UNSAFE LIGHT REMAINED ON ALL OTHER AIRCRAFT INDICATION NORMAL. INSPECTED LEFT MLG POSITION INDICATION SYSTEM. NO DEFECTS NOTED AT THIS TIME. (M) - [SDR GTIA030895](https://openairdocs.org/sdr/GTIA030895.md): Odor · detected · Nov 5, 2003 · N820NK · Doug DC982 · Air Distribution System > LEFT AND RIGHT AIR COND SUPPLY TEMP HIGH LIGHTS CAME ON WITH BURNING ODOR IN CABIN WHEN AIRFOIL ANTI-ICE TURNED ON. ACCOMPLISHED QRH PROCEDURES LIGHTS WENT OUT, CONTINUED FLIGHT. PER COMPANY REQUEST AND ITEM ABOVE PERF EXTRA ENGINE RUN UP AT CRUISE PLUS POWE - [SDR GTIA030883](https://openairdocs.org/sdr/GTIA030883.md): Wire · loose · Oct 27, 2003 · N820NK · Doug DC982 · Light System Wiring > FTW - FOUND EMERGENCY LIGHTS INOPERATIVE O/H STATION 800-1200 AND LEFT SIDEWALL LIGHTS INOPERATIVE IN VENTRAL STAIRWELL AREA. TROUBLE SHOT, FOUND LOOSE WIRE. RE-INSTALL LOOSE TERMINAL. (M) - [SDR GTIA030872](https://openairdocs.org/sdr/GTIA030872.md): Floorbeam · corroded · Oct 20, 2003 · N820NK · Doug DC982 · Fuselage Main, Floor Beam > FOUND CABIN FLOORBEAM, IN MID PIT, CHAFING AND CORRODED. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. (M) - [SDR GTIA030874](https://openairdocs.org/sdr/GTIA030874.md): Fitting · cracked · Oct 20, 2003 · N820NK · Doug DC982 · Fuselage Miscellaneous Structure > AFT PIT DOOR UPPER STOP, FORWARD FITTING CRACKED. REMOVED DAMAGED FITTING. REPLACED FITTING. (M) - [SDR GTIA030873](https://openairdocs.org/sdr/GTIA030873.md): Web · corroded · Oct 19, 2003 · N820NK · Doug DC982 · Fuselage Miscellaneous Structure > FOUND PAX CABIN SUBFLOOR CORRODED AT RBL 40 TO 54 STATION 180 TO 200. REMOVED DAMAGED WEB. FABRICATED NEW WEB. FABRICATED NEW SPLICE. INSTALLED NEW WEB AND SPLICE. (M) - [SDR GTIA030884](https://openairdocs.org/sdr/GTIA030884.md): Floor Panel · corroded · Oct 17, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FTW - FOUND CABIN FLOOR WEB CORRODED UNDER GALLEY DRAIN PAN STATION 158 RBL - 44 INCHES. (M) - [SDR GTIA030857](https://openairdocs.org/sdr/GTIA030857.md): Longeron · damaged · Oct 15, 2003 · N820NK · Doug DC982 · Fuselage Main, Longeron/Stringer > FTW - FOUND DAMAGED LONGERON STATION FS 1271 L24L. REMOVED DAMAGED LONGERON AT L24L FS 1322-1271. FABRICATED NEW LONGERON. LOCATED AND DRILLED SPLICE. INSTALLED SPLICE AND LONGERON. (M) - [SDR GTIA030859](https://openairdocs.org/sdr/GTIA030859.md): Skin · dented · Oct 13, 2003 · N820NK · Doug DC982 · Fuselage Main, Plate/Skin > FTW - FOUND DENT AT FS 1276 TO FS 1315 BETWEEN LONGERONS 23 AND 24L, REQUIRES REPAIR. DENT AT FS 1276 SHOULD BE INCORPORATED INTO THIS REPAIR. CUT OUT DAMAGED SECTION OF SKIN FROM STATION 1276-1315. FABRICATED INNER DOUBLERS, FINGER DOUBLER AND NEW SKIN. I - [SDR GTIA030860](https://openairdocs.org/sdr/GTIA030860.md): Floorboard · delaminated · Oct 12, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FTW - FOUND PAX CABIN FLOORBOARD DELAMINATED AT FORWARD F/A SEAT AREA. FABRICATED NEW FLOORBOARD. (M) - [SDR GTIA030844](https://openairdocs.org/sdr/GTIA030844.md): Floor Support · corroded · Oct 11, 2003 · N820NK · Doug DC982 · Fuselage Miscellaneous Structure > FOUND FLOOR SUPPORT AT FS 146 TO 154 LBL 53 HAS CORROSION. FLOOR SUPPORT REMOVED. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) - [SDR GTIA030814](https://openairdocs.org/sdr/GTIA030814.md): Fitting · corroded · Oct 10, 2003 · N820NK · Doug DC982 · Fuselage Main, Attach Fittings > FOUND MID PIT STATION 693 TEE FITTING CORRODED/ELONGATED HOLES. FABRICATED NEW T-FITTING. (M) - [SDR GTIA030851](https://openairdocs.org/sdr/GTIA030851.md): Plate · corroded · Oct 10, 2003 · N820NK · Doug DC982 · Fuselage Miscellaneous Structure > FTW - FOUND TWO CORRODED FLOOR PLATES AT FS 160, 18 INCHES LBL. FABRICATED FLOOR PLATE. TWO FLOOR PLATES ARE REMOVED AND INSTALLED ON SAS W/C B00104 18-R-15. (M) - [SDR GTIA030843](https://openairdocs.org/sdr/GTIA030843.md): Web · corroded · Oct 10, 2003 · N820NK · Doug DC982 · Fuselage Miscellaneous Structure > FOUND SUBFLOOR CORRODED STATION 195 LBL 50. REMVOED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M) - [SDR GTIA030885](https://openairdocs.org/sdr/GTIA030885.md): Yoke · damaged · Oct 9, 2003 · N820NK · Doug DC982 · Engine Mount Section > FTW - NR 2 YOKE ASSEMBLY UPPER ISOLATOR CONICAL SURFACE WORN. REMOVED NR 2 UPPER FORWARD ISOLATOR. INSTALLED NEW ISOLATOR. UPON INSTALLATION OF YOKE ASSEMBLY FOUND UPPER ISOLATOR INNER ASSEMBLY LOOSE. FOUND ISOLATOR INNER ASSEMBLY STILL LOOSE. REMOVED UPP - [SDR GTIA030834](https://openairdocs.org/sdr/GTIA030834.md): Floorboard · broken · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FOUND FORWARD CABIN STATION 200 TO 256 LBL 21 TO LBL 44 FLOORBOARD HAS SEVERAL INSERTS BROKEN OUT/CORRODED SOFT/MUSHEY AND DAMAGE ALONG EDGE. FABRICATED NEW FLOORBOARD. (M) - [SDR GTIA030835](https://openairdocs.org/sdr/GTIA030835.md): Floor Panel · corroded · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FTW - FOUND FORWARD CABIN FLOOR PANEL STATION 160-200 CENTER HAS SEVERAL INSERTS BROKEN OUT/CORRODED AND SOFT/MUSHEY. FABRICATED NEW FLOOR PANEL. (M) - [SDR GTIA030832](https://openairdocs.org/sdr/GTIA030832.md): Floorboard · corroded · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FORWARD CABIN STATION 200 TO 256 CENTER FLOORBOARD HAS SEVERAL INSERTS BROKEN OUT/CORRODED SOFT/MUSHEY AND DAMAGED ALL CORNERS. FABRICATED NEW FLOORBOARD. (M) - [SDR GTIA030833](https://openairdocs.org/sdr/GTIA030833.md): Floor Panel · cracked · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FORWARD CABIN STATION 200 TO 256 RBL 45.5 TO RBL 55 METALLIC PANEL HAS CRACKED/DAMAGED AT HAT CHANNEL AND EXPANSION JOINT CRACK/DISBONDED. FABRICATED REPAIRS. INSTALLED HAT CHANNEL REPAIRS. REPAIRED DISONDED AREA. (M) - [SDR GTIA030836](https://openairdocs.org/sdr/GTIA030836.md): Floorboard · corroded · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FTW - FOUND FORWARD CABIN STATION 200 TO STATION 180 RBL 8 INCHES TO RBL 44 FLOOR PANEL HAS SEVERAL INSERTS BROKEN OUT/CORRODED/SOFT/MUSHEY. FABRICATED NEW FLOORBOARD. (M) - [SDR GTIA030842](https://openairdocs.org/sdr/GTIA030842.md): Floorboard · corroded · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FTW - FOUND FORWARD CABIN FLOORBOARD STATION 200 TO STATION 256 LBL 14.5 TO LBL 21 HAS SEVERAL INSERTS BROKEN OUT, CORRODED, SOFT/MUSHEY. FABRICATED NEW FLOOR BOARD. (M) - [SDR GTIA030837](https://openairdocs.org/sdr/GTIA030837.md): Floorboard · corroded · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FOUND FORWARD CABIN FLOORBOARD STATION 180 TO STATION 160 RBL 8 INCHES TO RBL 44 HAS SEVERAL INSERTS BROKEN OUT, CORRODED AND SOFT/MUSHEY. FABRICATED NEW FLOOR BOARD. (M) - [SDR GTIA030838](https://openairdocs.org/sdr/GTIA030838.md): Floorboard · corroded · Oct 6, 2003 · N820NK · Doug DC982 · Fuselage Floor Panel > FORWARD CABIN FLOOR BOARD STATION 200 TO STATION 160 RBL 44 TO RBL 55 HAS SEVERAL INSERTS CORRODED/SOFT MUCHEY. FABRICATED NEW FORWARD CABIN FLOOR BOARD. (M) - [SDR GTIA030862](https://openairdocs.org/sdr/GTIA030862.md): Beam · cracked · Oct 2, 2003 · N820NK · Doug DC982 · Fuselage Main, Structure > FOUND L1 DOOR FORWARD VERTICAL BEAM AND STRAP CRACKED/BENT. REMOVED T-ANGLE. REMOVED CRACKED STRAP. REMOVED FORWARD VERTICAL BEAM. FABRICATED REPLACEMENT VERTICAL BEAM AND STRAP. INSTALLED NEW VERTICAL BEAM, NEW STRAP AND T-ANGLE. (M) - [SDR GTIA030879](https://openairdocs.org/sdr/GTIA030879.md): Cap · cracked · Oct 2, 2003 · N820NK · Doug DC982 · Leading Edge Devices > FOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP IS CRACKED. REMOVED END CAP. LOCATED AND DRILLED NEW PART. INSTALLED NEW END CAP. (M) Next page: https://openairdocs.org/deregistered/N820NK-2005-05-09/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 = 'N820NK' AND deregistration_id = 'N820NK-2005-05-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N820NK-2005-05-09/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.