Douglas DC-8-62

Service difficulty reports · 2,778

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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 ABXA9500639Press Switch · leakingEIGHTY MINUTES AFTER LEVEL OFF, NR 1 ENGINE OIL PRESSURE LIGHT CAME ON INTERMITTENTLY, OIL PRESSURE 44 PSI AND OIL TEMPERATURE 100 DEGREES CELSIUS. NOTED NR 1 OIL QTY DECREASING AT RATE OF 1.1 GPH. REDUCED POWER TO IDLE, CONSUMPTION DROPPED TO .6 GPH AT IDLEJul 28, 1995 · N803AX · Doug DC862 · Engine Oil PressureSDR 95ZZZX4248Retract Pin · shearedKEWR/KBWI - FLT 118 - AFTER TAKEOFF OUT OF KEWR, THE DOORS, LIGHT, AND LANDING GEAR UNSAFE LIGHT STAYED ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE AND LIGHTS STAYED ILLUMINATED. HYDRAULIC PRESSURE AND QTY NORMAL. NORMAL LANDING MADE AT KBWI. MAINTENANCE FOUNJul 21, 1995 · N990CF · Doug DC862 · Landing Gear Retraction/Extension SystemSDR 95ZZZM373Skin · crackedLEFT LEADING EDGE AFT LOWER SKIN CRACKED INBOARD OF NR 2 ENGINE PYLON AT WING STATION XS1 70.900 AT AFT ROW OF ATTACH FASTENERS, 1.5 INCH CRACK. STOP DRILLED CRACK, TREATED AND PRIMED AREA. FABRICATED AND INSTALLED 5 INCH BY 7 INCH 7075-T6 .071 INCH DOUBLER Jul 21, 1995 · N1803 · Doug DC862 · Wing, Plate/SkinSDR IXXA199567Wire · failedWSAP - ON DEPARTURE DURING UPLATCH CHECK, THE GEAR LIGHT STAYED ON WITH THE MAIN GEAR DOOR LIGHT OUT. THE LANDING GEAR WAS CYCLED ONCE, AND THE UPLATCH CHECK WAS SUCCESSFUL. INSPECTION OF THE SYSTEM IN RJTY REVEALED AN INTERMITTENT GROUND WIRE ON THE RT MLG Jul 19, 1995 · N61CX · Doug DC862 · Landing Gear System WiringSDR 95ZZZX3452Skin · corrosionLEFT WING INBOARD SLOT L/E HAS LEVEL 2 CORROSION. REPAIRED IAW SRM 57-2-1.Jul 6, 1995 · N1804 · Doug DC862 · Leading Edge DevicesSDR 95ZZZX3453Fitting · crackedDURING PRE-FLIGHT, MAINTENANCE CHECK FOUND LT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0.Jul 5, 1995 · N1804 · Doug DC862 · Elevator StructureSDR 95ZZZM266Fitting · crackedDURING PREFLIGHT MAINTENANCE CHECK, FOUND LEFT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0.Jul 5, 1995 · N1804 · Doug DC862 · Elevator StructureSDR 95ZZZX3457Floor Support · crackedDURING B-CHECK INSPECTION, FOUND RIGHT WW AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACKED AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39.Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZX3451Angle · crackedDURING B-CHECK INSPECTION, THE RT INBOARD FLAP, OUTBOARD, FORMER AND SCISSOR PANEL ATTACHMENT ANGLES FOUND CRACKED IN 2 LOCATIONS, BOTTOM AREA. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE IAW DER ARW 12565-128.Jul 3, 1995 · N1804 · Doug DC862 · Trailing Edge FlapsSDR 95ZZZX3449Floor Support · crackedDURING C-CHECK INSPECTION, FOUND THE RT W/W AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACK AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39.Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZM424Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON WING CENTER SECTION UPPER SKIN PANEL SPLICE DOUBLER AT XCW 0.000 FS 780. MECHANCICALLY REMOVED CORROSION. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DER DWG ARW 950051-5296.Jul 3, 1995 · N802BN · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM268Longeron · corrodedPOPPED RIVET HEADS AND SKIN BULGE AT FS 208.00 AT LONGERON 28R. REMOVED SECTION OF LONGERON 28R AND TWO INTERCOSTALS. FOUND LEVEL 2 CORROSION ON L-28R. REPLACED 20 INCH SECTION OF L-28R AND REINSTALLED INTERCOSTALS PICKING EXISTING HOLES IAW SRM 53-2-2 AND 5Jul 3, 1995 · N1804 · Doug DC862 · Fuselage Main, Longeron/StringerSDR 95ZZZM265Skin · corrodedLEFT ELEVATOR LOWER SKIN HAS LEVEL 2 CORROSION AT XE 195.33. SKIN SECTION REMOVED. FABRICATED NEW SKIN USING OLD AS TEMPLATE. INSTALLED NEW SKIN SECTION IAW SRM 55-2-0, 51-1-8 AND 51-1-21. REBALANCED ELEVATOR IAW SRM 51-4-4, DC8 SB 27-185 AND DOUGLAS FAX FJul 3, 1995 · N1804 · Doug DC862 · Elevator, Plate/SkinSDR IXXA199565Fire Detector · malfunctionedKWRI - ON DEPARTURE OUT OF KWRI, A NR 3 ENGINE FIRE WARNING WAS EXPERIENCED. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO KWRI FOR MAINTENANCE. WINDMILLING OIL PRESSURE WAS 30 PSI. INSPECTION AT KWRI REVEALED AN INTERMITTENTLY BAD Jun 30, 1995 · N21CX · Doug DC862 · Fire DetectionSDR IXXA199563Duct Clamp · failedLPLA/KWRI - IN CRUISE BETWEEN LPLA AND KWRI, A NR 3 ENGINE FIRE WARNING WAS EXPERIENCED WITH NORMAL ENGINE PARAMETERS OBSERVED. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE FIRE BOTTLES DISCHARGED. THE FIRE WARNING EXTINGUISHED AND THE ENGINE MAINTAINEDJun 29, 1995 · N21CX · Doug DC862 · Pneumatic Distribution SystemSDR 95ZZZM434Longeron · corrodedDURING C-CHECK INSPECTION, FOUND L31R AND FINGER DOUBLER BETWEEN FS 208.00 AND 270.00 WITH LEVEL 2 CORROSION. REMOVED AND REPLACED L31R AND FINGER DOUBLER BETWEEN FS 208.00 AND 270.00 IAW SRM 51-1-2 AND 51-2-0.Jun 20, 1995 · N802BN · Doug DC862 · Fuselage Main, Longeron/StringerSDR 95ZZZM426Skin · corrodedDURING C-CHECK, FOUND LEVEL TWO CORROSION INSIDE FORWARD ACCESSORY COMPARTMENT ON L27R BETWEEN FS 225 AND 270. REMOVED CORROSION. FABRICATED AND INSTALLED FILLER AND DOUBLER, IAW DER DWG ARW 950051-0566. MFG AND INSTALLED LONGERON IAW DAC DWG 5613861510.Jun 16, 1995 · N802BN · Doug DC862 · Fuselage Main, Plate/SkinSDR 95ZZZM423Press Floor · corrodedDURING C-CHECK INSPECTION, FOUND UNDERSIDE OF COCKPIT PRESSURE FLOOR WITH LEVEL 2 CORROSION AT FS 182 LBL 44. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW DER DWG ARW 950051-4066.Jun 16, 1995 · N802BN · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZM418Door · corrodedDURING C-CHECK, FOUND CORROSION AROUND TAILCONE LOWER DOOR. MECHANICALLY REMOVED CORROSION. TREATED AND PRIMED AREA. FABRICATED AND INSTALLED DOUBLER IAW DER DWG ARW 950051-6037.Jun 16, 1995 · N802BN · Doug DC862 · Aerodynamic FairingsSDR 95ZZZM444Doubler · damagedDURING C-CHECK INSPECTION, FOUND IMPROPER REPAIR ON THE LOWER FORWARD CARGO COMPARTMENT AFT DOOR CUTOUT AT LOWER FORWARD SAB CORNER. REMOVED IMPROPER REPAIR, FABRICATED DOUBLERS USE CLAD 7075-TL 125 AND .090 TREATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 5Jun 15, 1995 · N802BN · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZM443Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, UPPER SKIN HAD CORROSION LEVEL 2 FROM XE 219.979 TO XE 312.500 AT TRAILING EDGE. REMOVED PANEL AND ROUTED TO OUTSIDE SERVICE. PANEL WAS RESKINNED AND REINSTALLED.Jun 15, 1995 · N802BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 95ZZZM440Skin · corrodedDURING C-CHECK INSPECTION, FOUND FS 862 JUST FORWARD OF LEFT MLG DOOR (BELLY FAIRINGS) HAS A 4 INCH BY 3 INCH TEMP REPAIR. FABRICATED NEW SKIN AS PER ORIGINAL USED CLAD 7075-T6 .050 DRILLED HOLES TREATED AREAS WITH ALODINE AND F.R. PRIMER IAW SRM 51-1-8 INSTAJun 15, 1995 · N802BN · Doug DC862 · Fuselage Main, Plate/SkinSDR 95ZZZM439Support · corrodedDURING C-CHECK INSPECTION, FOUND LEFT W/W FAIRING SUPPORT FRAME BENEATH REVERSER PUMP WITH LEVEL 2 CORROSION. FABRICATED NEW SUPPORT USED 7075-T6.063 IAW 51-1-0 TREATED WITH ALODINE AND F.R. PRIMER IAW 51-1-8 INSTALLED NEW SUPPORT AS PER SRM 51-1-21 AND SRM 5Jun 15, 1995 · N802BN · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZM438Skin · corrodedDURING C-CHECK INSPECTION, FOUND THE LEFT WING LEADING EDGE WITH CORROSION AT STATION XFS 566. REMOVED FASTENERS, REMOVED CORROSION, FOUND LEVEL 2 CORROSION FABRICATED DOUBLER IAW 57-2-1 TREATED AND PRIMED IAW 51-1-8 INSTALLED FILLERS AND DOUBLER IAW SRM 57-2Jun 15, 1995 · N802BN · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM437Fitting · corrodedDURING C-CHECK INSPECTION, FOUND FLOOR BEAM TO FUSELAGE FRAME ATTACH FITTING AT RIGHT FS 235 WITH LEVEL 2 CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jun 15, 1995 · N802BN · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZM436Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, LOWER SKIN SURFACE AT TRAILING EDGE BETWEEN XE 272.00 TO STABILIZER TIP WITH LEVEL 2 CORROSION. REPLACED PANEL IAW SRM 51-1-21 PG 20-25 AND SRM 55-1-0.Jun 15, 1995 · N802BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 95ZZZM435Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN SURFACE AT TRAILING EDGE BETWEEN XE 272.00 TO STAB TIP WITH LEVEL 2 CORROSION. REMOVED DAMAGED SKIN PANELS, FABRICATED, TREATED AND INSTALLED NEW PANELS IAW SRM 51-1-8, 51-1-21 PG 20-Jun 15, 1995 · N802BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 95ZZZM433Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AROUND ATTACH FASTENERS ON UPPER SURFACE OF RT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD FROM XFS 178.00 TO XH 285.00. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-0968.Jun 15, 1995 · N802BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 95ZZZM431Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AROUND ATTACH FASTENERS ON UPPER SURFACE OF LEFT HORIZ STAB L/E OUTBOARD FROM XH 285.00 TO XFS 178.00. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-0969 SRM 51-3-0.Jun 15, 1995 · N802BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 95ZZZM429Skin · corrodedFOUND DURING C-CHECK, LEFT HORIZONTAL STABLE INBOARD FROM XAR TO XFS 178 HAS LEVEL II CORROSION ON UPPER SIDE AROUND ATTACH FASTENERS. CUT OUT CORRODED AREA, FABRICATED DOUBLERS AND FILLERS IAW DER ARW 950051-0966 AND SRM 57-2-1 FIG 38 DAC 274118/G1P1518.Jun 15, 1995 · N802BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 95ZZZM428Skin · corrodedDURING C-CHECK, FOUND RT WING UPPER LEADING EDGE BETWEEN NR 3 AND NR 4 ENGINES AREAS OF BULGING SKIN CORROSION LEVEL 2 SMALL CRACKS. REMOVED CORROSION FOUND BEYOND LIMITS IAW SRM 57-2-0 CUT OUT DAMAGE SECTION, FABRICATED DOUBLER AND FILLER IAW DER 950051-1098Jun 15, 1995 · N802BN · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM421Doubler · damagedDURING C-CHECK INSPECTION, FOUND IN PROPER REPAIR ON THE LOWER FORWARD CARGO COMPARTMENT AFT DOOR CUTOUT AT LOWER FWD SAB CORNER. REMOVED IN PROPER REPAIR, FABRICATED DOUBLERS USE CLAD 7075-TL 125 AND .090 TREATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 51-Jun 15, 1995 · N802BN · Doug DC862 · Fuselage Miscellaneous StructureSDR 95ZZZM420Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, UPPER SKIN HAS CORROSION LEVEL 2 FROM XE 219.979 TO XE 312.500 AT T/E. REMOVED PANEL AND ROUTED TO OUTSIDE SERVICE. PANEL WAS RESKINNED AND REINSTALLED. (M)Jun 15, 1995 · N802BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 95ZZZM430Skin · corrodedDURING C-CHECK INSPECTION, FOUND LIGHT CORROSION AT EXTERIOR FUSELAGE SKIN CUSP LINE AT FS 902-980 AT L21R. REMOVED CORROSION PER SRM 51-18 FOUND TO BE BEYOND LIMITS LEVEL 2 CORROSION. FABRICATED AND INSTALLED REPAIR PARTS IAW DER DWG ARW 950051-5065.Jun 14, 1995 · N802BN · Doug DC862 · Fuselage Main, Plate/SkinSDR 95ZZZM432Trap Panel · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION LEFT WING UPPER SURFACE TRAPEZOID PANEL BETWEEN AFT SPAR AND XW 19.00. FABRICATED AND INSTALLED NEW PANEL AS PER ORIGINAL IAW DER DWG ARW 950051-0203.Jun 13, 1995 · N802BN · Doug DC862 · Wing Miscellaneous StructureSDR IXXA199562Uplock Assy · lack of lubeON DEPARTURE OUT OF RJTY, THE UPLATCH CHECK WAS ACCOMPLISHED AND BOTH THE GEAR DOOR AND GEAR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO RJTY FOR MAINTENANCE. MAINTENANCE JACKED THE AIRCRAFT, CLEANED AND LUBRICATED BOTH THE LANDING GEAR AND THE GEARJun 12, 1995 · N61CX · Doug DC862 · Landing Gear Door Retract SectionSDR 95ZZZM427Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON SKIN UNDER AFT END 'C' BELLY DOOR SILL PROTECTOR. REMOVED SCUFF PLATE. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER IAW SRM 51-1-8 AND 5-1-16 PER DER DWG ARW 950051-5100.Jun 12, 1995 · N802BN · Doug DC862 · Fuselage Main, Plate/SkinSDR ABX9500531Spring · defectiveDURING MAINTENANCE INSPECTION, FOUND THAT FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT UNLOCK. ADJUSTED FORWARD UPPER STOP TO CENTER WINDOW WHICH CORRECTED UPPER LATCH ENGAGEMENT IAW DC-8 MM CHAPTER 56-10-3, AT ILN AS PRECAUTIONARY. MAINTENANCE INSTALLED NEW SJun 9, 1995 · N801AX · Doug DC862 · Flight Compartment WindowsSDR 95ZZZM267Te Skin · corrodedFOUND LEVEL 2 CORROSION LEFT ELEVATOR OUTBOARD STATIC WICK ATTACH POINT. REMOVED LEFT ELEVATOR. REMOVED DAMAGED T/E SECTION. FABRICATED AND INSTALLED NEW T/E SECTION IAW SRM 51-1-21A. INSTALLED NEW STATIC WICK BASE IAW MM 23-60-00. REINSTALLED ELEVATOR AFMay 29, 1995 · N1804 · Doug DC862 · Elevator, Plate/SkinSDR ABXA9500519Window Seal · defectiveDURING MAINTENANCE INSPECTION, DISCOVERED THAT THE CAPTAIN'S CLEAR VIEW WINDOW WOULD NOT OPEN. REMOVED EXCESS FILLER FROM THE SEAL SURFACE OF WINDOW FRAME. RESURFACED SEAL AND ADJUSTED THE UPPER LATCH IAW DC-8 MM CHAPTER 56.May 25, 1995 · N805AX · Doug DC862 · Flight Compartment WindowsSDR ABXA9500518Flap Drive Link · crackedDURING C-CHECK, COMPLIANCE OF A.D. 88-10-07 AND USING ULTRASONIC INSPECTION, FOUND THE FLAP DRIVE LINK AT STATION 98, POINT J TO BE CRACKED. REPAIRED LEFT FLAP DRIVE LINK IAW DC-8 MM CHAPTER 27.May 24, 1995 · N803AX · Doug DC862 · Trailing Edge Flap Control SystemSDR ARWR960699Skin · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT, AFT CARGO DOOR JAMB AREA, FORWARD SIDE HAS CORROSION BETWEEN FUSELAGE SKIN AND SEAL DEPRESSOR. REPAIRED IAW DAC FAX 293907 AND 297170. (X)May 16, 1995 · N8969U · Doug DC862 · Fuselage Main, Plate/SkinSDR 95ZZZW700Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROISION AT RIGHT LEADING EDGE AT XFS 291.500 TO 329.00. FOUND CORROSION BEYOND LIMIT. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER USING CLAS 7075-T6. PICKED UP EXISTING ATTACHMENTS WHERE POSSIBLE. ALL WORK DOApr 30, 1995 · N42086 · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM422Skin · damagedDURING C-CHECK, FOUND 26 INCHES BY 12 INCHES TEMP REPAIR ON RT INBOARD AILERON LOWER SURFACE. REMOVED PREVIOUS SKIN PANEL FROM XA 542.00 TO XW 563.00 CUT REAR SPAR FOR ACCESS. INSTALLED NEW SKIN PANEL AND INSTALLED REPAIR DOUBLERS ON REAR SPAR IAW DER DWG ARApr 27, 1995 · N802BN · Doug DC862 · AileronsSDR 95ZZZX3450Slot Door · corrosionON A TYPE SERVICE 'A', FOUND RT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS' HEADS. CUT OUT DAMAGED AREAS, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED IAW SRM 57-2-1, FIGURE 2H.Apr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/SkinSDR 95ZZZW658Slot Door · corrodedON 'A' CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL II CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE.Apr 25, 1995 · N1804 · Doug DC862 · Leading Edge DevicesSDR 95ZZZW657Slot Door · corrodedON 'A' CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL II CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. (W)Apr 25, 1995 · N1804 · Doug DC862 · Leading Edge DevicesSDR 95ZZZM264Slot Door · corrodedON A-CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE. REMOVED SLOT DOOR L/E SECTION, CUT OUT DAMAGED AREAS, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/E.Apr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM263Slot Door · corrodedON A-CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. REMOVED SLOT DOOR L/E. CUT OUT DAMAGED AREAS, FABRICATED ADN INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/EApr 25, 1995 · N1804 · Doug DC862 · Wing, Plate/SkinSDR 95ZZZM425Skin · damagedDURING C-CHECK, FOUND TEMP REPAIR AT FS 290.00 L26R AT TOILET DUMP ACCESS. REMOVED TEMP REPAIR. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-5011.Apr 9, 1995 · N802BN · Doug DC862 · Fuselage Main, Plate/Skin
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