Douglas DC-8-62

Service difficulty reports · 2,778

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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 aircraft_model_key = 'DC862'
  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 ARWA9608001Skin · puncturedWHILE LOADING AIRCRAFT, CARGO PERSONNEL PUNCTURED SKIN APPROXIMATELY 2 FORWARD OF BELLY DOOR. REPAIRED 2 TO 3 HOLE AT FUSELAGE STA 480, LONGERON 29/30R IN ACCORDANCE WITH DER DRAWING ARW960173-0001.Aug 7, 1996 · N802BN · Doug DC862 · Cargo/Baggage DoorsSDR IXXA96137Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE EXTERNAL PLATING WAS FOUND TO BE CORRODED AT FUSELAGE STATION 1495 AND LONGERON 32 RIGHT. REPAIR OF THE PLATING WAS ACCOMPLISHED BY CUTTING OUT THE DAMAGED AREA, FABRICATING AND INSTALLING REPAIR FILLERS AND DOUBLERS IAWAug 6, 1996 · N61CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA96136Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, THE LEFT OUTBOARD AILERON LOWER PLATING SURFACE WAS FOUND TO BE CORRODED BETWEEN STATIONS XW500 AND 577. THE PLATING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL 51-1-21 AND FAA DER APPROVED SKETCH A89-R05. (M)Aug 6, 1996 · N61CX · Doug DC862 · AileronsSDR IXXA96135Spar · crackedWHILE ACCOMPLISHING THE REPLACEMENT OF THE RIGHT MAIN LANDING GEAR FITTING, THE RIGHT LOWER REAR SPAR WAS FOUND TO BE CRACKED BETWEEN WING STATION S XRS 13 AND XRS 20. THE REPAIR OF THE SPAR WAS ACCOMPLISHED IAW DOUGLAS DRAWINGS 5613917, 5613918, 5613919, 561Aug 6, 1996 · N61CX · Doug DC862 · Wing SparSDR CKSA96081Fire Bottle · dischargedNR 4 ENGINE OUTBOARD BOTTLE DID NOT INDICATE LOW PRESSURE WHEN DISCHARGED FOR FIRE WARNING INDICATION. REMOVED AND REPLACED NR 3 AND NR 4 FIRE BOTTLES. PERFORMED SYSTEM CHECK, SYSTEM CHECKS OUT NORMAL IAW 26-3-0.Aug 3, 1996 · N801MG · Doug DC862 · Fire Bottle, FixedSDR CKSA96080Fire Loop · chafedNR 4 ENGINE FIRE WARNING CAME ON AT CRUISE ALT 37.0, ALL ENGINE PARAMETERS APPEARED NORMAL. OIL PRESSURE AND TEMPERATURE MIN OIL 25 PSI. SHUTDOWN ENGINE INFLIGHT IAW AIA FOM PROCEDURES, WINDMILL TIME 47 MINUTES. REMOVED AND REPLACED NR 4 ENGINE FIRE LOOP ANAug 3, 1996 · N801MG · Doug DC862 · Fire DetectionSDR ARWR9607003Floor Beam · corrodedFLOOR BEAM AT STA 235 AT LBL 66 CORRODED SECTION AT DUCT CUT-OUT. MECHANICALLY REMOVED CORRODED SECTION. FABRICATED AND INSTALLED 7075.T6 .090 INCH DOUBLER IAW MHA ENGINEERING, INC., E. O. MHA-3067 UNDER AMRC W.O. 960165. (X)Jul 30, 1996 · N1808E · Doug DC862 · Fuselage Main, Floor BeamSDR ARWR9607002Angle · corrodedFLOOR PANEL SUPPORT ANGLE AT FS 225R TO FS 273R CORRODED AT FLOOR LEVEL. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED 2024.T3 .063 INCH FILLER AND 2024.T3 .071 INCH DOUBLER IAW MHA ENG. INC., E. O. MHA-3065 UNDER AMRC W. O. 960165. (X)Jul 30, 1996 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWR9607001Skin · corrodedINNER SKIN BETWEEN FS 255 AND FS 265 CORRODED AT LONGERON 21R. CUT OUT AREA OF CORROSION, FABRICATED AND INSTALLED 7075.T6 .025 INCH FILLER AND 7075.T6 .032 INCH DOUBLER IAW MHA ENGINEERING, INC., E. O. MHA-3066 UNDER AMRC W. O. 960165. (X)Jul 30, 1996 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA96145Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL FUSELAGE PLATING AT THE FORWARD UPPER CORNER OF THE FORWARD LOWER CARGO DOOR OPENING. THE CRACK WAS REMOVED BY CUTOUT, AND FABRICATION AND INSTALLATION OF A FILLER AND REPAIR DOUBLERS IAW THJul 23, 1996 · N61CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA96144Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT OUTBOARD AILERON LOWER PLATING ON THE INBOARD SIDE WAS FOUND TO BE CORRODED. REPAIR TO THE AREA WAS ACCOMPLISHED IAW THE STRUCTURAL REPAIR MANUAL 57-10-0. (M)Jul 23, 1996 · N61CX · Doug DC862 · AileronsSDR IXXA96138Bus Links · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON, INBOARD BUS LINKS WERE FOUND TO BE CRACKED. THE BUS LINKS WERE REPLACED IAW THE DOUGLAS SRM AND MM. (M)Jul 23, 1996 · N61CX · Doug DC862 · Aileron Control SystemSDR IXXA96146Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL PLATING A FUSELAGE STATION 225 BETWEEN LONGERONS 29 AND 30 LEFT. THE CRACK WAS REPAIRED IAW THE STRUCTURAL REPAIR MANUAL. (M)Jul 22, 1996 · N61CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA96143Plating · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING LEADING EDGE PLATING WAS FOUND CRACKED AT THE INBOARD STUB WING, INBOARD END. THE CRACK WAS REPAIRED IAW THE DOUGLAS SRM 57-2-1. (M)Jul 22, 1996 · N61CX · Doug DC862 · Wing, Plate/SkinSDR IXXA96142Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW THE DOUGLAS SRM AND FITTING REPLACEMENT GUIDE. (M)Jul 22, 1996 · N61CX · Doug DC862 · Wing, Landing Gear Attach FittingsSDR IXXA96141Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR TORQUE TUBE SUPPORT FITTING WAS FOUND TO BE CRACKED. THE FITTING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL. (M)Jul 22, 1996 · N61CX · Doug DC862 · Wing Miscellaneous StructureSDR IXXA96140Bulkhead · crackedDURING ROUTINE C-CHECK INSPECTION, THE PRESSURE BULKHEAD (CABLE FEED THROUGH) AT FUSELAGE STATION 680 WAS FOUND TO BE CRACKED AT LONGERON 27 LEFT. THE BULKHEAD WAS REPLACED IAW THE AIRCRAFT SRM. (M)Jul 22, 1996 · N61CX · Doug DC862 · Fuselage Main, BulkheadSDR IXXA96139Longeron · crackedDURING ROUTINE C-CHECK INSPECTION, THE LEFT LONGERON 24 WAS FOUND CRACKED IN THE WING ATTACH BOTTLE BOLT AREA. THE LONGERON WAS REPLACED IAW THE DOUGLAS REPLACEMENT GUIDE AND THE SRM. (M)Jul 22, 1996 · N61CX · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA96124Pt2 System · contaminatedON TAKEOFF FROM COF, NR 3 AND NR 4 ENGINE PRESSURE RATIO INDICATION SYSTEMS READ HIGH COMPARED TO N1 AND THE NR 1 AND NR 2 ENGINES. THE FLIGHT ELECTED TO RETURN TO THE FIELD. MAINTENANCE REMOVED INSECT DEBRIS FROM BOTH ENGINE PT2 SYSTEMS, ACCOMPLISHED A HIGHJul 7, 1996 · N31CX · Doug DC862 · Engine Pressure Ratio (EPR)SDR 96ZZZX3649Seal · defectiveON RIA FLT 1712 (CDG/MIA) - DURING CRUISE AT APPROXIMATELY 1830Z, NR 4 ENGINE WAS SHUT DOWN DUE TO OIL PRESSURE LIGHT ON, ENGINE OIL PRESSURE FLUCTUATING AND DECREASING BELOW 35 PSI. AT MIA ON GROUND, MAINTENANCE FOUND LEAKING GEARBOX TOWER SHAFT SEAL. SEAL Jul 4, 1996 · N772CA · Doug DC862 · Turbine Engine Accessory DriveSDR CKSA96065Fuel Tube · crackedFUEL LEAK NR 3 ENGINE ON LANDING. REMOVED AND REPLACED FUEL CONTROL FUEL PRESSURE RETURN LINE. OPS CHECKS NORMAL PER MM CHAPTER 73-0, NO LEAKS NOTED DURING RUNUP.Jun 30, 1996 · N818CK · Doug DC862 · Fuel Controlling SystemSDR TC8A96047Ps4 Line · looseADVANCING NR 4 THROTTLE FOR T/O, COULD ONLY REACH 75 PERCENT N1 89.5 PERCENT N2 AND EPR OF 1.24. FOUND PS4 LINE LOOSE, TIGHTENED AND SECURED, OPS CKD ASPER MM 71-00 NORMAL.Jun 27, 1996 · N181SK · Doug DC862 · Fuel Controlling SystemSDR ARWA9606071Dir Gyro · inoperativeAFTER TAKEOFF, NR 2 COMPASS SYSTEM OFF FLAG INTERMITTENT. RETURNED TO MIAMI. REMOVED AND REPLACED DIRECTIONAL GYRO. SYSTEM OPS CHECKED NORMAL IAW 34-20-00.Jun 21, 1996 · N1803 · Doug DC862 · Attitude and Direction Data SystemSDR IXXA9699Panel · corrodedDURING ROUTINE C-CHECK AND CPCP INSPECTION, CORROSION OF THE EXTERIOR PLATING WAS IDENTIFIED AT FUSELAGE STATION 296 BETWEEN LONGERONS 34 AND 35 RIGHT. THE CORRODED AREA WAS CUT OUT AND REPAIR WAS ACCOMPLISHED BY FABRICATION AND INSTALLATION OF A FILLER AND EJun 19, 1996 · N31CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA9698Panel · crackedDURING RUOTINC C-CHECK INSPECTION, AN EXTERNAL FUSELAGE SKIN CRACK WAS IDENTIFIED AT FUSELAGE STATION 1529, LONGERON 17 RIGHT. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE CRACK, CUT OUT, FABRICATION AND INSTALLATION OF A FILLER AND EXTERNAL DOUBLER IAW THE DOUGJun 19, 1996 · N31CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA9697Panel · crackedDURING ROUTINE C-CHECK INSPECTION OF THE UPPER AFT FUSELAGE EXTERIOR PLATING, A CRACK WAS IDENTIFIED AT FUSELAGE STATION 1559, LONGERON 17 RIGHT. THE CRACK WAS REMOVED BY CUT OUT. THE REPAIR FILLER AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLED IAW THE DJun 19, 1996 · N31CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA9696Panel · crackedDURING ROUTINE C-CHECK INSPECTION OF THE UPPER AFT FUSELAGE EXTERNAL PLATING, A CRACK WAS IDENTIFIED AT FUSELAGE STATION 1541, LONGERON 17 RIGHT. REPAIR WAS ACCOMPLISHED BY CRACK CUT OUT, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBLER IAJun 19, 1996 · N31CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA9695Panel · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS IDENTIFIED IN THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 1583 AND LONGERON 22 LEFT. THE CRACK WAS REMOVED BY CUTOUT, THE REPAIR WAS ACCOMPLISHED BY FABRICATING AND INSTALLING A FILLER AND EXTERNAL DOUBLER Jun 19, 1996 · N31CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA9694Angle · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AND CORRODED AT THE FRONT SPAR. REPAIR OF THE ANGLE WAS ACCOMPLISHED IAW FAA DER APPROVED DRAWING A62-R112. (M)Jun 19, 1996 · N31CX · Doug DC862 · Vertical StabilizerSDR IXXA9693Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE RIGHT WING LEADING EDGE EXTERNAL PLATING AT STATION XW 761.695. THE CRACK WAS REMOVED BY CUT OUT. THE REPAIR WAS ACCOMPLISHED BY FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBELR Jun 19, 1996 · N31CX · Doug DC862 · Wing, Plate/SkinSDR IXXA9692Upper Mid Panel · crackedDURNG ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL STABILIZER CENTER SECTION, THE UPPER MID PANEL WAS FOUND CRACKED. THE INSPECTION WAS ACCOMPLISHED IAW DOUGLAS SERVICE BULLETIN 55-15, USING THE NDT METHODS. THE PANEL WAS REPLACED. (M)Jun 19, 1996 · N31CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA9691Panel · crackedDURING ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL CENTER SECTION, THE LOWER FORWARD PANEL WAS FOUND TO BE CRACKED. THE INSPECTION WAS ACCOMPLISHED IAW DOUG SERVICE BULLETING 55-15, USING THE NDT METHODS. THE PANEL WAS REPLACED. (M)Jun 19, 1996 · N31CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA9690Panel · crackedDURING ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL STABILIZER CENTER SECTION, THE FORWARD UPPER PANEL WAS FOUND TO BE CRACKED. THE INSPECTION WAS WITHIN THE SCOPE OF DOUGLAS SERVICE BULLETIN 55-15, USING THE NDT METHODS CALLED OUT. THE PANEL WAS REPLACED. Jun 19, 1996 · N31CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA96100Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION OF THE EXTERIOR PLATING AT FUSELAGE STATION 1590, LONGERON 35 LEFT TO 35 RIGHT WAS IDENTIFIED. THE PANEL WAS REMOVED AND REPLACED FROM STATION 1530 TO 1730, LONGERONS 31 LEFT TO 31 RIGHT. (M)Jun 19, 1996 · N31CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA9686Clamp · brokenINVESTIGATION OF THIS EVENT FOUND AN ENGINE ANTI-ICE DUCT CLAMP BOLT HAD FAILED ALLOWING BLEED AIR TO ENTER THE ENGINE COWLING. THE HOT AIR DAMAGED THE ENGINE WIRING HARNESS WHICH CAUSED SEVERAL ENGINE INDICATION SYSTEM MALFUNCTIONS. INSPECTION OF THE REMAINJun 18, 1996 · N51CX · Doug DC862 · Engine Anti-Icing SystemSDR ARWA9606070Clamp · looseDURING CLIMB, UNABLE TO MAINTAIN PRESSURIZATION WITH FOUR T/C'S OPERATING AT 24,000 FT. CABIN DIFFERENTIAL KEPT CLIMBING, RETURNED TO JFK. FOUND LEFT SIDE TURBO COMPRESSOR HOT AIR DUCT CLAMP LOOSE BY BULKHEAD IN UNPRESSURIZED AREA. RETIGHTENED CLAMP, PRESSUJun 18, 1996 · N802BN · Doug DC862 · Cabin Compressor SystemSDR AWRA9606004Dir Gyro · inoperativeNR 1 COMPASS SYSTEM FAILED AFTER TAKEOFF, RETURNED TO MIA. REMOVED AND REPLACED DIRECTIONAL GYRO IAW 34-20-00, OPS CHECKED NORMAL.Jun 12, 1996 · N802BN · Doug DC862 · Directional Gyro and Indicating SystemSDR ARWA9606003Locking Valve · inoperativeAFTER TAKEOFF, MAIN CARGO DOOR LIGHT ILLUMINATED AT 8 PSI. INSTALLED THREE GEAR AT DOOR LATCHES, RETURNED TO MIAMI. TROUBLESHOT SYSTEM, FOUND BAD LOCKING VALVE. REMOVED AND REPLACED LOCKING VALVE IAW 52-30-00, OPS CHECKED NORMAL.Jun 8, 1996 · N1803 · Doug DC862 · Cargo/Baggage DoorsSDR ARWA9606001Vert Gyro · failedAFTER TAKEOFF, CAPT'S ADI INDICATED 15 TO 20 DEGREE BANK IN LEVEL FLIGHT AND INDICATED PITCH 20 DEGREES NOSE-UP IN FLIGHT LEVEL TURN. AIRCRAFT RETURNED TO MIAMI. REMOVED AND REPLACED CAPT'S VERTICAL GYRO, OPS CHECKED NORMAL IAW DAC MM 34-25-00.May 31, 1996 · N810BN · Doug DC862 · Directional Gyro and Indicating SystemSDR ABXA9600500Window Trim · out of positionFIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN COMPLETELY. REPOSITIONED WINDOW TRIM AROUND THE FIRST OFFICER'S CLEARVIEW WINDOW, OPS CHECK GOOD.May 31, 1996 · N804AX · Doug DC862 · Flight Compartment WindowsSDR ABXA9600498Seat · unlockedDURING CRUISE, FLIGHT ENGINEER'S SEAT DROPPED FROM THE MID VERTICAL RANGE TO THE LOWEST POSITION. INSPECTED AND LUBED THE VERTICAL ADJUSTMENT MECHANISM OF THE FLIGHT ENGINEER'S SEAT, OPS CHECK GOOD.May 29, 1996 · N802AX · Doug DC862 · Flight Compartment EquipmentSDR IXXA9682Control Amp · intermittentEN ROUTE BETWEEN ELP AND TOL IN CRUISE FLIGHT AT FL 37, THE MAIN CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED. ATC WAS ADVISED, AND THE AIRCRAFT DIVERTED TO OKC. ON THE GROUND IN OKC, AND AIRCRAFT WAS CHECKED FOR SIGNS OF FIRE, SMOKE, OR ODORS OF COMBUMay 25, 1996 · N51CX · Doug DC862 · Smoke DetectionSDR ARWR960657Skin · corrodedDURING C-CHECK INSPECTION, FOUND UPPER FUSELAGE SKIN AROUND FASTENERS HAS CORROSION AND WORKING FASTENERS, RT FUSELAGE, STA 980.000 TO STA 1000.000. REPAIRED IAW DER DRAWING NR GLP 1681/96-22-14-003. TREATED AND PRIMED IAW SRM 51-1-8.May 22, 1996 · N8969U · Doug DC862 · Fuselage Main, Plate/SkinSDR ARWR960606Window Frame · crackedDURING C-CHECK, FOUND WORKING FASTENERS AND CRACK AROUND WINDOW FRAME, RT STA 1020.00. REPAIRED IAW DER DRAWING NR GLP 1681, SRM 51-1-8 AND SRM 51-11-40. (X)May 22, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR ABXA9600496Engine · malfunctionedNR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED DURING CRUISE. THE OIL TEMPERATURE INDICATED 125 DEGREES CELSIUS AND BEGAN TO INCREASE WHILE THE OIL PRESSURE AND OIL QUANTITY INDICATIONS WERE NORMAL. SHUTDOWN THE NR 3 ENGINE AT 0203Z AND THE ENGINE WINDMILLED AT May 22, 1996 · N801AX · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWR961744Skin · crackedDURING C-CHECK, FOUND LT OUTBOARD AILERON UPPER SURFACE AT OUTBOARD ATTACHING FITTING, L/E SKIN HAS A CRACK. CUT DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER IAW DER NR 950082-1567. TREATED AND PRIMED IAW SRM 51-1-8. (X)May 15, 1996 · N8969U · Doug DC862 · AileronsSDR ARWR961141Cap · corrodedDURING C-CHECK, FOUND FUSELAGE RT SIDE FRAME AT FS 208 HAS CORROSION APPROXIMATELY BETWEEN L21R AND 36R. REMOVED AND CUT CAP AT FS 208 FROM L17R AND L23R. FABRICATED NEW IAW DAC 288851 AND DER 950087-0035A. HEAT TREATED, TREATED AND PRIMED IAW SRM 51-1-8. May 15, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWR961076Skin · corrodedDUE TO EXCESSIVE REPAIRS AND CORROSION ON SKIN FROM FS 173R TO FS 270R, STR 21R TO STR 31R, REMOVED AND REPLACED SKIN. REMOVED SKIN FROM FS 178.R TO FS 270.R FROM L21R TO L31 AND INSTALLED NEW SKIN IAW DER 950087-0028. (X)May 15, 1996 · N8969U · Doug DC862 · Fuselage Main, Plate/SkinSDR ARWR960818Skin · corrodedDURING C-CHECK, FOUND RT WING UPPER SURFACE NR 3 STUB WING T/E HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED DOUBLER IAW DER ARW 950082-1011, TREATED AND PRIMED IAW SRM 51-1-8 AND INSTALLED IAW DER NR ARW 950082-1011. (X)May 15, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR ARWR960706Skin · corrodedDURING C-CHECK, FOUND UPPER FUSELAGE SKIN HAS CORROSION BETWEEN FS 822.500 AND FS 857.125, L22R. CUT OUT DAMAGED SECTION, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR IAW DER NR ARW 95 0082-1004. TREATED AND PAINTED AREA IAW SRM 51-1-8. SEALED AREAS AREMay 15, 1996 · N8969U · Doug DC862 · Fuselage Main, Plate/Skin
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