N810BN, cancelled Aug 7, 2012

Service difficulty reports · 79

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N810BN' AND deregistration_id = 'N810BN-2012-08-07'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ARWA20040805Switch · failedON ENGINE START, NR 4 ENGINE WOULD NOT LIGHT UP WITH A & B AND BOTH IGNITERS. T/S DOWN TO FUEL SHUT-OFF LEVER SWITCH TRANSFERRED TO DMI 18678 IN ACCORDANCE WITH MEL 74-1 CATEGORY-C, PLACARD INSTALLED. REPLACED START LEVER SWITCH PER MM 74-00; OPERATIONAL NORAug 24, 2004 · N810BN · Doug DC862 · Ignition SystemSDR ARWA20040702Actuator · inoperativeFUEL DUMPED PER ABNORMAL CHECKLIST AT MAXIMUM LANDING WEIGHT SWITCH PUT IN DRAIN POSITION, BUT CONTINUED DUMPING MANUALLY PUT IN DRAIN POSITION FOR 5 MINUTES, REMAINDER OF ELECTRICAL CYCLE OK. TRANSFERRED TO DMI 18610 IN ACCORDANCE WITH MEL 28-9-1. MANUAL FUJul 14, 2004 · N810BN · Doug DC862 · Fuel Dump SystemSDR ARWA20040701Linkage · vibrationAFTER TAKEOFF HEAVY NOISE VIBRATION EXPERIENCE. CYCLE GEAR SEVERAL TIMES WITH NO CHANGE, RETURNED TO FIELD. FUEL DUMPED PER ABNORMAL CHECKLIST. CHECKED NOSE GEAR DOOR LINKAGE IN ACCORDANCE WITH MM 32-22-2; OPERATIONS AND TESTED IN ACCORDANCE WITH MM 32-21-1Jul 14, 2004 · N810BN · Doug DC862 · Landing Gear Door Retract SectionSDR ARWA20040507Actuator · malfunctionedUNABLE TO EXTEND FUEL DUMP CHUTES ELECTRICALLY, MOTOR STOPPED APPROXIMATELY 3300 FULL EXTENDED. TRANSFERRED TO DMI NR 18536 CATEGORY (C) IAW MEL 28-9-1. INSTALLED CAT (C) PLACARD; PENDING CLOSING OF DMI. PERFORMED OPERATIONAL CHECK OF FUEL DUMP CHUTE ELECT MMay 21, 2004 · N810BN · Doug DC862 · Fuel Dump SystemSDR ARWA20040506Gyro · faultyCAPTAIN'S COMPASS FAILED IN FLIGHT. REMOVED AND REPLACED CAPTAIN'S PICTORIAL DEVIATION INDICATOR (PDI) AND DIRECTIONAL GYRO (DG) IAW MM 31-10-1 AND MM 34-21-1. SWAPPED INSTRUMENT AMPS IAW 34-00. SYSTEM GROUND TEST NORMAL IAW 34-21-0, 34-52-0 AND 34-28-0.May 21, 2004 · N810BN · Doug DC862 · Directional Gyro and Indicating SystemSDR ARWA20040106Switch · inoperativeSTARTED TAKE-OFF ROLL, AILERON POWER LIGHT CAME ON. REMOVED AND REPLACED MANUAL CONTROL IND SWITCH IAW MM 27-11-14; OPERATIONAL CHECK NORMAL IAW MM 27-11-14 AND 27-11-0.Jan 27, 2004 · N810BN · Doug DC862 · Aileron Control SystemSDR ARWA20031204Spar · crackedDURING ACCOMPLISHMENT OF RB 17284 SB 57-090 INSPECTION. LEFT WING FRONT SPAR XFS 517 & XFS 518, LOWER CAP HOLES (2 EACH) WITH CRACKS.Dec 6, 2003 · N810BN · Doug DC862 · Wing SparSDR ARWA20030201Gyro · malfunctionedNR 2 RADIO MAGNETIC INDICATOR (RMI) HAS "OFF" FLAG AND CAPTAIN'S HORIZONTAL SITUATION INDICATOR (HSI) HAS "OFF" FLAG. FLAGS COME IN VIEW INTERMITTENTLY "CONTINOUSLY" AND IN TURNS. NO HEADING MOVEMENT WITH "OFF" FLAGS IN VIEW. REMOVED AND REPLACED NR 1 DIRECTFeb 2, 2003 · N810BN · Doug DC862 · Directional Gyro and Indicating SystemSDR ARWA20030108Smoke Detector · malfunctionedLOWER CARGO SMOKE AND FIRE DETECTION MAINTENANCE LIGHT ON; CODE F15231: FALSE ALARM. LOWER CARGO AND FIRE DETECTOR MAINTENANCE LIGHT ON; ENTERED ON DMI 17416 IAW MEL 26-10-1-R-A CAT "C". REMOVED AND REPLACED SMOKE DETECTOR FORWARD CENTER; OPERATIONAL CHECK OJan 27, 2003 · N810BN · Doug DC862 · Smoke DetectionSDR ARWA20020914Splice · crackedDURING C-CHECK, MAIN CARGO COMPARTMENT FLOORBEAM SPLICES CRACKED AT STA 320, 340, 360, 380, 400, 420, 440 & 460 L-21 LONGITUDE.Sep 12, 2002 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA20020705O-Ring · defectiveAPPROXIMATELY ONE AND HALF (1.5) HOURS AFTER TAKE OFF, HYDRAULIC QUANTITY DROPPED TO THE STAND PIPE. FOUND DEFECTIVE O-RING ON ENGINE DRIVEN PUMP PRESSURE LINE FITTING RT ENGINE DRIVEN PUMP. REMOVED AND REPLACED O-RING IAW MM 29-10-12; OPS CHECKED NORMAL ON Jul 16, 2002 · N810BN · Doug DC862F · Hydraulic System, MainSDR ARWA20020704Duct · looseAFTER TAKEOFF, HEAVY VIBRATION / NOISE FELT COMING FROM THE COCKPIT FLOOR AREA, CAPTAIN'S SIDE. INSPECTED NOSE WHEEL WELL AREA AND FOUND LT AIR DUCT BOOT LOOSE FOR FLOW CONTROL SYSTEM; REINSTALLED BOOT AND SECURED CLAMPS AND CHECK RT SIDE TOO FOR CONDITION FOJul 7, 2002 · N810BN · Doug DC862 · Air Distribution SystemSDR ARWA20020604Cylinder · faultyAFTER T/O, HYD TEMP CLIMBED TO 83 DEG C, PERFORMED ABNORMAL CHECKLIST, NO CHANGE. RETURNED TO RAMP. REMOVED & REPLACED NR 3 ENG HYD DRIVEN PUMP, PERFORMED OPERATIONS CHECK, CHECKED NORMAL IAW MM 29-30-0. DURING TAXI FOR T/O, HYDRAULIC OIL TEMP CLIMBED TO 8Jun 21, 2002 · N810BN · Doug DC862 · Steering UnitSDR ARWA20020503Garlock Seal · leakingNR 4 ENGINE OIL QUANTITY 3/4 OF A GALLON. PERFORMED INFLIGHT SHUT DOWN ABNORMAL. OIL PRESS WINDMILLING 20 PSI. SERVICED ENGINE OIL IAW DC-8 MM 12-20-1 AND PERFORMED ENGINE RUN-UP; FOUND OIL LEAK AT MAIN FUEL PUMP DRAIN. REMOVED AND REPLACED MAIN FUEL PUMP May 8, 2002 · N810BN · Doug DC862 · Turbine Engine Oil SystemSDR ARWA20020208Transformer · faultyAFTER LANDING ROLL IN MGGT, HEAVY SMOKE WAS SEEN COMING OUT FROM BEHIND F/O'S INSTRUMENT PANEL. AREA WAS INSPECTED, FOUND THE GLARESHIELD LIGHT BALLAST (B6) AT FAULT. REMOVED AND REPLACED BALLAST TRANSFORMER IAW MM 33-12-0, PERFORMED OPERATIONAL CHECK IAW MMFeb 27, 2002 · N810BN · Doug DC862 · Flight Compartment LightingSDR ARWA20020104Switch · brokenWHILE STARTING ENGINE NR 4 STARTER SWITCH BROKE. REMOVED AND REPLACED NR 4 ENGINE STARTER SWITCH IAW MM 20-50-01. OPS CHECK ON ENGINE IDLE RUN UP IAW 71-00 FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE.Jan 4, 2002 · N810BN · Doug DC862 · Engine CrankingSDR ARWA20011213Hydraulic Line · leakingLOSS OF HYDRAULIC FLUID DURING LANDING ROLL IN SKBO. COMPLETED ABNORMAL EMERGENCY CHECKLIST, LEAK STOPPED. TAXIED UNEVENTFUL TO CARGO RAMP. T/S AND FOUND STANDBY RUDDER ACCUMULATOR PRESSURE HYDRAULIC HOSE TO PUMP LEAKING. REMOVED AND REPLACED HIGH PRESSURE Dec 27, 2001 · N810BN · Doug DC862 · Hydraulic System, MainSDR ARWA20011204Limiter · out of adjWHILE SETTING MAX POWER TAKEOFF, NR 4 ENGINE OIL PRESSURE MAXED OUT. PERFORMED ENGINE RUN IAW MM 71-00; FOUND OIL PRESSURE AT TAKEOFF 58 PSI WITHIN LIMITS IAW AA DC8 MM PAGES 5-35-90. ADJUSTED UPPER LIMIT TO 54 PSI IAW MM 79-20-5. OPS NORMAL, 41 PSI AT IDLEDec 5, 2001 · N810BN · Doug DC862 · Engine Oil PressureSDR ARWA20011202Gyro · failedFIRST OFFICER'S COMPASS INOPERATIVE AFTER 1000 FEET. AIRCRAFT RETURNED TO KMIA AND PERFORMED OVERWEIGHT LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 PDI, INSTRUMENT AMPLIFIER AND DIRECTIONAL GYRO IAW MM 34-00. PERFORMED OPERATIONAL CHECK COMPASS SYSTDec 3, 2001 · N810BN · Doug DC862 · Directional Gyro and Indicating SystemSDR ARWA0011005PinLOG PAGE 105745. DISCREPANCY:GEAR NOT LATCHED LIGHT ON, DOOR NOT LATCHED LIGHT ON, AIRCRAFT DIVERTED TO SJU AND ACCOMPLISHED AN UNEVENTFULL LANDING.AIRCRAFT PERFORMED AN OVERWEIGHT LANDING. CORRECTIVE ACTION:FOUND LEFT HAND MAIN GEAR RETRACT ACTUATOR PIN BROKEOct 10, 2001 · N810BN · Doug DC862 · Landing Gear ActuatorSDR ARWA0010902EngineLOG PAGE 106168. DISCREPANCY: ON CLIMB OUT OF KMIA NBR-3 ENG OIL PRESS LIGHT CAME ON AND OIL PRESS ERRATIC. PERFORMED PRECAUTIONARY SHUT DOWN. TOTAL WINDMILLING TIME 25 MIN. LANDING WT 240.0 LBS ENG SHUT DOWN AT 0536Z.AIRCRAFT LANDED WITHOUT INCIDENT. CORRECTISep 18, 2001 · N810BN · Doug DC862 · Engine Oil PressureSDR ARWA0010808Boot · out of adjDURING UPLATCH CK DOORS NOT LATCHED LIGHT ILUMINATED. ACCOMPLISHED ABNORMAL CK LIST AND NO HELP. SLIGHT VIBRATION ON COCKPIT FLOOR DURING ENTIRE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. CHECK ADJUSTMENT LT MAIN DOOR UPLATCH MECHANISM IAW MM 32-31-4, OPS CAug 18, 2001 · N810BN · Doug DC862 · Air Distribution SystemSDR ARWA0010605Engine · malfunctionedDURING TAKEOFF ROLL LOSS POWER ON NR 1 ENGINE. ABORTED TAKEOFF AT 70 KNOTS. REFERRED TO PERFORMANCE MANUAL BRAKE ENERGY CHART OK TO TAXI. CHECKED ALL TANK CROSSFEED VALVES AND SELECTOR VALVES FOR OPERATION FOUND NORMAL IAW MM 28-22-2,3. INSPECTED FUEL FILTJun 19, 2001 · N810BN · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWA0010307O-Ring · leakingAT TOP OF DESCENT NR 3 ENGINE OIL PRESSURE GAUGE FLICKERS FULL SCALE HIGH AND LOW AND NR 3 ENGINE OIL PRESSURE LIGHT FLICKERS ON AND OFF. ALL OTHER ENGINE PARAMETERS NORMAL. PRECAUTIONARY ENGINE SHUTDOWN. ON INSPECTION OF ENGINE, FOUND TOWER SHAFT SEAL LEAKMar 20, 2001 · N810BN · Doug DC862 · Turbine Engine Accessory DriveSDR ARWA0001203Uplock · dirtyAFTER GEAR RETRACTION GEAR NOT LATCHED UP LIGHT ON, ON UPLATCH CHECK LANDING GEAR FALLS OUT. FOUND MLE UPLATCH MECHANISM DRY; CLEANED & LUBRICATED MLE UPLATCH MECHANISM IAW MM 12-81-1; PERFORMED LANDING GEAR SWING IAW 32-11-1 CHECK OK.Dec 21, 2000 · N810BN · Doug DC862 · Landing Gear Position and WarningSDR ARWA0001201Uplock Switch · failedDOOR NOT LATCHED LIGHT ILLUMINATED AFTER TAKEOFF PERFORMED ABNORMAL CKLIST LIGHT REMAIN ON. REMOVED AND REPLACED RT MAIN LANDING GEAR DOOR UPLOCK SWITCH, OPERATIONAL CHECK LANDING GEAR DOOR INDICATION SYSTEM IAW 32-60-0 AND FOUND NORMAL.Dec 6, 2000 · N810BN · Doug DC862 · Door Warning SystemSDR ARWA991002Switch · failedMIA - FLT 751 - AIR TURNBACK, ON GER RETRACT DOOR NOT LATCHED. LIGHT REMAINS ILLUMINATED. PERFORMED ABNORMAL CHECKLIST 4 TIMES. LIGHT REMAINS ON. TROUBLESHOT, FOUND LEFT MAIN GEAR DOOR SWITCH FAULTY. REMOVED AND REPLACED SWITCH. OPS CHECK NORMAL IAW MM 3Oct 24, 1999 · N810BN · Doug DC862 · Landing Gear Door Retract SectionSDR ARWA990306Retract Mech · lack of lubeMIA - FLT 656 - AIR TURNBACK, ON UPLATCH CHECK, GEAR NOT LATCHED LIGHT ON. PROCEEDED WITH ABNORMAL CHECKLIST. WITH ENGINE PUMPS OFF, GEAR NOT LATCHED LIGHT CAME ON ABOUT 1 OR 2 MINUTES LATER. UNABLE TO DUMP FUEL ELECTRICALLY, MANUAL STARTED THEN GOT EXTREMELYMar 19, 1999 · N810BN · Doug DC862 · Landing Gear Retraction/Extension SystemSDR ARWA990107Uplock · lack of lubeMIA - FLT 1628 - AFTER TAKEOF IN SEGU, GEAR NOT LATCHED LIGHT ILLUMINATED, RECYCLED GEAR SEVERAL TIMES. COULD NOT GET SATISFACTORY UPLATCH CHECK, DOOR NOT LATCHED, LIGHT DID NOT ILLUMINATE, PROCEEDED TO DESTINATION IN ACCORDANCE OF ABNORMAL CHECKLIST. CHECKEJan 14, 1999 · N810BN · Doug DC862 · Landing Gear Door Retract SectionSDR ARWA981204Wire · brokenGEAR DOOR NOT LATCHED, LIGHT ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE, LIGHT REMAINED ON. RETURNED TO MIAMI, NO FUEL DUMPED. FOUND BROKEN WIRE AT LT MLG DOOR UPLATCH SWITCH CANNON PLUG. REPAIRED SAME PER MM 20-50-00, OPS CHECK NORMAL PER MM 32-61-4.Dec 5, 1998 · N810BN · Doug DC862 · Landing Gear System WiringSDR ARWA981201Switch · inopPRECAUTIONARY SHUT DOWN DUE ENGINE OIL PRESSURE LIGHT FOR NR 1 ENGINE. FOLLOWED ABNORMAL CHECKLIST FOR ENGINE OIL PRESS. LIGHT ON, OIL PRESS 48 PSI, OIL TEMPERATURE MAX 105 DEGREE AFTER THROTTLE RETARD DURING CLIMB 80 PSI, OIL PRESS WHEN ENGINE WINDMILLING, Dec 2, 1998 · N810BN · Doug DC862 · Engine Oil Indicating SystemSDR ARWA981125Skin · corrodedC-CHECK, CORROSION FOUND BETWEEN LOWER SKIN AND RIBS ON LT I/B AILERON. REMOVED DAMAGED LOWER SKIN, FABRICATED REPAIR SKIN PER EO DRAWING NR 98-0924-3, ON 8110-3, DATED SEPT 25, 1998 UNDER WORK ORDER NR 1299.Nov 19, 1998 · N810BN · Doug DC862 · AileronsSDR ARWA981124Fasteners · misinstalledC-CHECK, NR 1 AND NR 2 PYLON'S HAVE WRONG FASTENERS INSTALLED IN PLANKS. OPENED REPLACEMENT HOLES TO .260 DIA AND INSTALLED PER EO DRAWING NR 98-014 ON 8110-3, DATED SEPT 28, 1998 UNDER WORK NR 1299.Nov 19, 1998 · N810BN · Doug DC862 · Nacelle/Pylon StructureSDR ARWA981123Frame · misdrilledC-CHECK, FRAME 1340 AT LT CUSP ABOVE FLOOR FITTING HAS DRILLED HOLE AT EDGE OF ANGLE. REMOVED DAMAGED AREA AND INSTALLED DOUBLERS PER DRAWING NR 98-012 ON 8110-3 DATED SEPT 09, 1998 UNDER WORK ORDER NR 1392.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, FrameSDR ARWA981122Floorbeam · corrodedC-CHECK, CORROSION BLISTERS ON FLOORBEAM TOP FWD EDGE AT NUT PLATES STA 1140 BETWEEN NR 2 AND NR 4 SEAT TRACKS. REMOVED ENTIRE UPPER SECTION AND INSTALLED DOUBLER PER EO NR 98-924-04 0N 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, Floor BeamSDR ARWA981121Doubler · corrodedC-CHECK, FINGER DOUBLER CORRODED AT CUSP LINE RT O/B OF F/E POSITION SUBFLOOR PRESSURE PANEL STA 168 TO 188. REMOVED DAMAGED SKIN AND INSTALLED DOUBLERS PER EO NR 98-0924 ON 8110-3 DATED SEPT 24, 1998 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981120Skin · crackedC-CHECK, 1.75 INCH CRACK IN LEFT WING SKIN UPPER SURFACE AT STA 74.86. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 57-2-1 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Wing, Plate/SkinSDR ARWA981119Spar · crackedC-CHECK, CENTER WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS STA 857 LBL 37, 51, 61 LT W/W. STOP DRILLED CRACKS AND INSTALLED DOUBLERS PER DRAWING NR 98-013 ON 8110-3 DATED SEPT 22, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Wing SparSDR ARWA981118Spar · crackedC-CHECK, WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS 33 TO 35 RIGHT OF CENTER LINE AND 53 TO 54 STA 857 RT W/W. STOP DRILLED AND INSTALLED DOUBLERS PER DRAWING NR 98-015 ON 8110-3, DATED SEPT 30, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Wing SparSDR ARWA981117Angle · crackedC-CHECK, 4.5 INCH CRACK TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN336. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER EO NR 98-0924-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Nacelle/Pylon StructureSDR ARWA981116Angle · crackedC-CHECK, 8 INCH CRACK IN RADIUS OF TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN310. STOP DRILLED CRACK, INSTALLED DOUBLER PER EO NR 98-0926-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Nacelle/Pylon StructureSDR ARWA981115Longeron · crackedC-CHECK, CORROSION BLISTER/CRACK ON LONGERON 27R FUSELAGE FRAME 1060. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER DRAWING NR 98-012 ON 8110-3 DATED SEPT 04, 1998 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, Longeron/StringerSDR ARWA981114Skin · corrodedC-CHECK, FUSELAGE SKIN CORRODED AND SHEAR FOOT BULGED AFT SIDE FUSELAGE FRAME STA 1320 BETWEEN LONGERON 29L-31L. REMOVED DAMAGED SKIN, FABRICATED DOUBLERS AND INSTALLED PER SRM 53-2-1 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, Plate/SkinSDR ARWA981113Skin · corrodedC-CHECK, LT HORIZ STAB L/E I/B LITE CORROSION AT FASTENERS XFS 180. REMOVED CORROSION AND INSTALLED DOUBLERS PER EO NR 98-0924-02 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR ARWA981112Skin · corrodedC-CHECK, LT HORIZONTAL STAB L/E CORROSION AT SCREW HOLES O/B END UPPER SURFACE. REMOVED CORROSION AND INSTALLED DOUBLERS PER EO NR 98-0924-02 ON 8110-3 DATED SEPT 24, 1998 UNDER WORK NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR ARWA981111Rib · crackedC-CHECK, 3.5 INCH CRACK IN RT WING L/E RIB STA XFS 422. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 57-2-0 UNDER WORK ORDER NR 1299.Nov 19, 1998 · N810BN · Doug DC862 · Wing, Rib/BulkheadSDR ARWA981110Fitting · crackedC-CHECK, 4.5 INCH CRACK IN LONGERON SPLICE FITTING 25R STA 1090. REPLACED LONGERON FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981109Fitting · crackedC-CHECK, LONGERON 22R END CAP 6.5 INCH CRACK STA 990. REPLACED END CAP FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981108Fitting · crackedC-CHECK, LONGERON 23R END CAP FITTING 5 INCH CRACK STA 990. REPLACED FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981107Fitting · crackedC-CHECK, 6 INCH CRACK IN LONGERON END CAP FITTING 22L STA 990. REPLACED FITTING PER SRM 51-1-20 UNDER WORK NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous Structure
Back to N810BN, cancelled Aug 7, 2012