Douglas DC-8-62F

Service difficulty reports · 1,163

Newest first. General aviation reporting is voluntary.

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 = 'DC862F'
  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 CKSA96040Service Panel · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5600-0551 AREA, AFT ACCESSORY COMPARTMENT, AFT LAVATORY WASTE DRAIN INNER SERVICE PANEL CORRODED. LEVEL 2 TASK NR 74998. REMOVED AND REPLACED INNER SERVICE PANEL AFT LAVATORY WASTE DRAIN IAW DC-May 2, 1996 · N3931A · Doug DC862F · Fluid Service DoorsSDR CKSA96038Skin · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5570-0551 AREA, FORWARD LOWER CARGO BILGE, FS 560 L35L, BULGE IN SKIN. LEVEL 2 TASK NR 59700. REMOVED CORRODED AREA AND INSTALLED REPAIR AS IT REQUIRED IAW DC-8 SRM 51-1-8. SKETCH NR AIA/E/2182 May 2, 1996 · N3931A · Doug DC862F · Fuselage Main, Plate/SkinSDR CKSA96037Stiffener · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 574L-0551 AREA, LT MLG WHEELWELL, LT MLG WHEELWELL CEILING PANEL LONGITUDINAL STIFFENER EXFOLIATING CORROSION APPROXIMATELY STA 950, 3RD STIFFENER OUTBOARD FROM KEEL BEAM LEVEL 2 TASK NR 74823. May 2, 1996 · N3931A · Doug DC862F · Fuselage Miscellaneous StructureSDR CKSA96036Fitting · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND CARD NR 573L-0551 AREA, UPPER SURFACE OF LT CUSP, LT FRAME TO CUSP FITTING AT STA 640 CORRODED. LEVEL 2 TASK NR 73562. REMOVED AND REPLACED FITTING IAW 51-1-20D. (X)May 2, 1996 · N3931A · Doug DC862F · Fuselage Miscellaneous StructureSDR CKSA96035Fitting · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 573L-0551 AREA, UPPER SURFACE OF LT CUSP, LT FRAME TO CUSP FITTING AT STA 600 CORRODED. LEVEL 2 TASK NR 73552. REMOVED AND REPLACED CUSP FITTING IAW DC-8 SRM'S 53-2-0, 51-1-20D, 51-1-3. (X)May 2, 1996 · N3931A · Doug DC862F · Fuselage Miscellaneous StructureSDR CKSA96034Fitting · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 573L-0551 AREA, UPPER SURFACE OF LT CUSP; LT FRAME TO CUSP FITTING AT STA 620 CORRODED. LEVEL 2 TASK NR 73553. REMOVED AND REPLACED FITTING PER DC8 SRM 51-1-20D AND SRM 51-3-0. (X)May 2, 1996 · N3931A · Doug DC862F · Fuselage Miscellaneous StructureSDR CKSA96033Fitting · crackedKOSC - FLT 72016 - DURING 'C-1' INSPECTION FOUND CARD NR 559L-0552 AREA, LOWER SURFACE OF LT CUSP; CRACK IN FLOOR SUPPORT FITTING AT LOWER CUSP LT SIDE STA 1120. LEVEL 2 TASK NR 60892. REMOVED AND REPLACED SHEAR TIE FITTING AS REQUIRED. INSTALLED IAW SRM 51-May 2, 1996 · N3931A · Doug DC862F · Fuselage Miscellaneous StructureSDR CKSA96032Spoiler · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND NR 121R-0552 AREA RIGHT WING EXTERIOR; NR 3 SPOILER INBOARD END CAP CORRODED. LEVEL 2 TASK NR 59624. REMOVED NR 3 SPOILER IAW DC8 MM CHAPTER 27. REPAIRED AND INSTALLED NR 3 SPOILER PANEL IAW DC8 MM CHAPMay 2, 1996 · N3931A · Doug DC862F · SpoilersSDR CKSA96031Skin · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND CARD NR 116L-0551 AREA LEFT WING LEADING EDGE; LEADING EDGE FORWARD OF OUTBOARD SLOTS INBOARD END, GOUGED AND CORRODED. LEVEL 2 TASK NR 74937. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC-8, SRMay 2, 1996 · N3931A · Doug DC862F · Wing, Plate/SkinSDR CKSA96015Ballast · burnedKOSC - FLT 72016 - SMOKE OF UNKNOWN ORIGIN ESCAPING FROM F/O PNEUMATIC RAIN REMOVAL LEVER. INSPECTED AND FOUND ORIGIN OF SMOKE COMING FROM LIGHT BALLAST AT F/O RT CONSOLE. FOUND BALLAST AT FAULT, DISCONNECT BALLAST AND TRANSFERRED TO DMI NR 22 IAW AIA MEL 33Apr 20, 1996 · N3931A · Doug DC862F · Flight Compartment LightingSDR RRXA9600012Clamp · missingKAUS - FLT 107 - AFTER TAKEOFF FROM KAUS NR 2 ENGINE FIRE WARNING SOUNDED. THE FLIGHT CREW SHUTDOWN NR 2 ENGINE AND RETURNED TO KAUS. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND A CLAMP OFF AT THE HIGH STAGE BLEED VALVE ELBOW DUCT. MAINTENANCEMar 26, 1996 · N997CF · Doug DC862F · Compressor Bleed ControlSDR IXXA9637Uplatch · lack of lubeON DEPARTURE OUT OF RODN, THE GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. THE LANDING GEAR WAS CYCLED, AND THE WARNING LIGHT EXTINGUISHED. IN RJTY, MAINTENANCE CLEANED THE MLG DOOR UPLATCH SWITCHES, CLEANED AND LUBRICATED THE MLG DOOR UPLATCH ROLLERS IAW THE Mar 18, 1996 · N41CX · Doug DC862F · Landing Gear Door Retract SectionSDR IXXA9617Frame · damagedDURING THE C-CHECK INSPECTION, FOUND A MISDRILLED HOLE IN FRAME AT FS 460R. THIS HOLE WAS REPAIRED PER ATI E.O. 53-DC8-222, AND ATI DRAWING SKA95253-4, REV: IR, DATED 1-6-96 AND IS APPROVED BY FAA FORM 8110-3. (X)Feb 7, 1996 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA9616Frame · damagedDURING THE C-CHECK INSPECTION, FOUND A MISDRILLED HOLE IN FRAME AT FS 740R. THIS HOLE WAS REPAIRED PER ATI E.O. 53-DC8-221 AND ATI DRAWING SKA95253-3, REV: IR, DATED 1-16-96 WHICH WAS APPROVED ON FAA FORM 8110-3. (X)Feb 7, 1996 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA9615Frame · damagedDURING THE C-CHECK INSPECTION, THE FRAME AT FS 500, LONGERON L35R WAS FOUND DAMAGED. A REPAIR WAS ACCOMPLISHED PER ATI DRAWING SKA95253-7, REV: IR, DATED 1-20-96 AND WAS APPROVED BY FAA FORM 8110-3. (X)Feb 7, 1996 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA9614Fitting · corrodedDURING THE C-CHECK INSPECTION, EXFOLIATED CORROSION WAS FOUND AT FS 490 TO FS 500 LOCATED IN THE FWD LOWER CARGO BILGE, LONGERON 33L-34L INSIDE THE TORQUE BOX TO SKIN ATTACH ANGLES. INSTALLED NEW FITTING AT FS 492 AND LONGERONS 33L-34L IAW DACO SRM 51-1-8 ANDFeb 7, 1996 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA9613Angle · crackedDURING THE C-CHECK INSPECTION, THE VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS FOUND CORRODED AND CRACKED ON THE LT FROM FORWARD OF THE FRONT SPAR TO CENTER SPAR. A REPAIR WAS PERFORMED PER ATI E.O. 53-DC8-223, AND DRAWING SKA95253-5, REV: A, DATED 1-23-96. Feb 7, 1996 · N41CX · Doug DC862F · Vertical Stabilizer, Attach FittingsSDR IXXA9612Door Frame · corrodedDURING THE C-CHECK INSPECTION, CORROSION WAS FOUND AT THE RT JET ESCAPE DOOR LOCATED ON THE FWD LOWER CORNER. A REPAIR WAS PERFORMED PER ATI E.O. 53-DC8-224, AND DRAWING SKA95253-6, REV: IR, DATED 1-6-96. (X)Feb 7, 1996 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA9611Seat Track · damagedDURING THE C-CHECK INPSECTION, A SEAT TRACK AT FS 440 WAS FOUND DAMAGED. A REPAIR WAS PERFORMED TO THE TRACK BY THE INSTALLATION OF A PLUG PER ATI E.O. 53-DC8-220, AND DRAWING SKA95253-1, REV: IR, SHEETS 1 AND 2, DATED 1-4-96. THIS REPAIR WAS APPROVED BY FAFeb 7, 1996 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA9610Seat Track · damagedDURING THE C-CHECK INSPECTION, A SEAT TRACK AT FS 530 WAS FOUND DAMAGED. A REPAIR WAS PERFORMED TO THE TRACK BY THE INSTALLATION OF A PLUG PER ATI E.O. 53-DC8-219, AND DRAWING SKA95253-2, REV: IR, SHEETS 1 AND 2, DATED 1-4-96. THIS REPAIR WAS APPROVED BY FAAFeb 7, 1996 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR EIAA9570Latch Light · illuminatedDOORS NOT LATCHED INDICATION ILLUMINATED AFTER GEAR RETRACTION. AFTER UPLATCH CHECK, LIGHT OUT AND ALL INDICATIONS NORMAL. TEST DOOR CLOSED SWITCH MECHANISM. NO DEFECTS NOTED. OPS NORMAL IAW DC8 MM 32-12-1. (M)Dec 22, 1995 · N817EV · Doug DC862F · Landing Gear Position and WarningSDR CKSA95039Fitting · corrodedKOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5570-0551 AREA, FORWARD LOWER CARGO BILGE, FORWARD PIT STA 492-STA 500 AT 32L-31L, CORROSION ON SKIN AND ANGLE. LEVEL 2 TASK NR 74816. CLEANED AND REMOVED CORROSION AS REQUIRED IAW SRM 51-1-8. Nov 28, 1995 · N3931A · Doug DC862F · Fuselage Miscellaneous StructureSDR 95ZZZM763Oil System · failedAIR TURNBACK AFTER APPROXIMATELY 15 MINUTES IN FLIGHT FROM JFK TO SDQ. SHUTDOWN NR 3 ENGINE DUE TO LOSS OF OIL QUANTITY. AIRCRAFT RETURNED TO JFK WHERE MAINTENANCE REPORTED INTERNAL FAILURE OF THE ENGINE OIL SYSTEM. THREE-ENGINE FERRIED AIRCRAFT TO MIAMI FONov 26, 1995 · N791AL · Doug DC862F · Turbine Engine Oil SystemSDR IXXA199578Brakes · out of adjustCUF/WRI - DURING FLIGHT BETWEEN CUF AND WRI, CREW REPORTED BURNING RUBBER ODOR IN AIRCRAFT. MAINTENANCE ADJUSTED THE NOSE WHEEL BRAKE PADS, WHICH CAUSED THE RUBBER ODOR, AND CLIMINATED A PNEUMATIC LEAK AT NR 2 CABIN COMPRESSOR DUCT. THE AIRCRAFT WAS RETURNEDSep 22, 1995 · N41CX · Doug DC862F · Landing Gear Brake SystemSDR ARWA090651Skin · crackedDURING C-CHECK, FOUND R/W UPPER SURFACE LEADING EDGE CRACKED AT XFS 315. CUT OUT DAMAGED AREA FABRICATED 7075-T6 .063 FILLER AND 7075T6-071 DOUBLER AND INSTALLED IAW SRM 57-2-1. (M)Sep 6, 1995 · N791AL · Doug DC862F · Fuselage Main, Plate/SkinSDR RRXA95005Bulkhead Doubler · corrodedCORROSION ON FRAME AND BULKHEAD AT Y= 680 TO 683 BETWEEN LONGERONS L35L TO L35R. REMOVED FRAME SECTION, SPLICE AND DOUBLERS. FABRICATED AND INSTALLED REPAIR ANGLES TO FRAME AND REPAIR DOUBLER TO BULKHEAD IAW COTNEY ENGINEERING ORDER SKA 95148-3 AND SRM 51-1-Aug 30, 1995 · N997CF · Doug DC862F · Fuselage Main, BulkheadSDR RRXA95004Skin · corrodedCORROSION ON SKIN AND SURROUNDING WINDOW PLUG LAND ON LT AFT TYPE 1 EXIT. REMOVED CORROSION BEYOND LIMITS. FABRICATED AND INSTALLED A REPAIR DOUBLER TO WINDOW PLUG LAND AND SKIN IAW COTNEY ENGINEERING ORDER SKA 95148-2.Aug 30, 1995 · N997CF · Doug DC862F · Fuselage Main, Plate/SkinSDR AR082251Skin · corrodedDURING C-CHECK INSPECTION, FOUND RT HORIZONTAL STABILIZER UPPER TIP WITH EXFOLIATION (LEVEL 2) CORROSION. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-1. SEALED REPAIR IAW SRM 51-20-0. (X)Aug 22, 1995 · N791AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR ARWA061754Floor Web · crackedDURING C-CHECK, FOUND 'A' PIT FLOOR WEB CRACKED. STOP DRILLED SMALL CRACK IAW WITH SRM 53-2-0. ARROW AIR WORKORDER NR 950007-5153 (0396). (M)Jun 17, 1995 · N791AL · Doug DC862F · Fuselage Floor PanelSDR ARWA061753Circumferential · crackedDUIRNG C-CHECK, FOUND MAIN CABIN CIRCUMFERENTIAL CRACKED AT FS 410 BETWEEN L7R AND L8R. CUT OUT DAMAGED AREA, AND FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0. ARROW AIR WORK ORDER NR 950007-5146 (0378). (M)Jun 17, 1995 · N791AL · Doug DC862F · Fuselage Main, FrameSDR ARWA061752Blkhd Beam · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD AFT SIDE THIRD HORIZONTAL BEAM FROM BOTTOM CRACKED AT BL ZERO. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-20D AND 53-20-0. ARROW AIR WORK ORDER NR 950007-6006 (0106). (M)Jun 17, 1995 · N791AL · Doug DC862F · Fuselage Main, BulkheadSDR 95ZZZX3172Plank · crackedKDAY/KMEM - FLT 040 - DURING SERVICE CHECK, MAINTENANCE FOUND THE NR 1 PYLON INTERMEDIATE SIDE PLANK CRACKED AT STA YN 226. THE AIRCRAFT WAS FERRIED TO KMCN TO FACILITATE PERMANENT REPAIRS. SD - ZANTOP MAINTENANCE REMOVED SIDE PLANK TO FACILITATE REPAIR. REJun 9, 1995 · N997CF · Doug DC862F · Nacelle/Pylon, Plate/SkinSDR 95ZZZM101Plank · crackedFLT 040 - KDAY-KMEM - DURING SERVICE CHECK, MAINTENANCE FOUND THE NR 1 PYLON INTERMEDIATE SIDE PLANK CRACKED AT STATION YN 226. THE AIRCRAFT WAS FERRIED TO KMCN TO FACILITATE PERMANENT REPAIRS.Jun 2, 1995 · N997CF · Doug DC862F · Nacelle/Pylon, Plate/SkinSDR 95ZZZX2493Floor Support · crackedAFT LOWER CARGO COMPARTMENT, FS 1100 AND STR 32L AND STR 35L. FRAME ATTACH FLOOR SUPPORT IS CRACKED AT 2 PLACES. W.O. 95007, CTL NR 5161, NR 0412. REMOVED FLOOR SUPPORT, WELDED CRACKS PER D.P.S. 10225 AND REINSTALLED FLOOR SUPPORT IAW SRM 51-1-20D AND SRM 5Mar 16, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR AWRA0927953Side Brace · corrodedDURING C-CHECK INSPECTION, FOUND LEFT MLG SIDE BRACE LUGS ON STRUT WITH INTERNAL PITTING. CLEANED LUGS, FABRICATED BUSHINGS IAW OHM 32-1-1B. INSTALLED SIDE BRACE BUSINGS IAW OHM 13-1-6. REINSTALLED SIDE BRACE ASSEMBLY IAW MM 32-11-5. (M)Mar 15, 1995 · N791AL · Doug DC862F · Main Landing GearSDR ARWA0927956Bushing · pittedDURING C-CHECK INSPECTION, FOUND LEFT MLG SIDE BRACE LUGS ON STRUT HAD INTERNAL PITTING. REMOVED SIDE BRACE AND ROUTED TO SHOP FOR OVERHAUL. RE-BRUSHED STRUT PER MM 32-1-8, PAGE 402E. REINSTALLED SERVICEABLE SIDE BRACE PER MM 32-11-3. OPS NORMAL IAW MM 32-Mar 15, 1995 · N791AL · Doug DC862F · Main Landing GearSDR ARWA0927955Crank · corrodedDURING C-CHECK INSPECTION, FOUND RUDDER TAB CONTROL CRANK WITH LEVEL 2 CORROSION. CORROSION REMOVED. REPLACED RUDDER CONTROL CRANK IAW MM 27-21-2. RIGGED TAB PER MM 27-13-3. OPS CHECK NORMAL. (M)Mar 15, 1995 · N791AL · Doug DC862F · Rudder Control SystemSDR ARWA031551Skin · crackedDURING C-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD LEADING END HAS (CORNER) PANEL CHAFFING AND CRACKED. REMOVED PANEL AND FABRICATED REPLACEMENT IAW SRM 53-1-0. INSTALLED PANEL SRM 53-1-0 AND 51-1-20. (M)Mar 15, 1995 · N791AL · Doug DC862F · Trailing Edge FlapsSDR AR031451Skin · crackDURING C-CHECK, FOUND LT LOWER WING L/E LOOSE, FASTENERS AT APPROXIMATELY XFS 240.000; FOUND SMALL CRACK AT FASTENER HOLE. THE DAMAGED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED TO RESTORE THE LOST STRENGTH PER E.O. NR 9502274 AND SRM 51-1-8. (X)Mar 14, 1995 · N791AL · Doug DC862F · Wing, Plate/SkinSDR ARWA031357Panel · corrosionDURING C-CHECK, FOUND VERTICAL STABILIZER TOP LEADING EDGE LEFT SIDE LEVEL 2 CORROSION. REMOVED CORROSION, FOUND BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-1 FIG 4. (M)Mar 13, 1995 · N791AL · Doug DC862F · Vertical Stabilizer, Plate/SkinSDR ARWA031356Bracket · crackedDURING C-CHECK, FOUND NR 1 PYLON LEFT SIDE CENTER COWL SUPPORT FITTING SUPPORT BRACKETS ARE CRACKED. REMOVED AND REPLACED SUPPORT BRACKETS AS PER SRM 54-2-1. (M)Mar 13, 1995 · N791AL · Doug DC862F · Nacelle/Pylon StructureSDR ARWA031355Angle · crackedDURING C-CHECK, FOUND MAIN CARGO DOOR LATCH SUPPORT ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-1-21, 51-3-0 AND 53-2-0. (M)Mar 13, 1995 · N791AL · Doug DC862F · Cargo/Baggage DoorsSDR ARWA031352Support · crackedDURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT FS 1120 L35-32L FRAME ATTACH FLOOR SUPPORT CRACKED AT TWO PLACES. REMOVED FLOOR SUPPORT, WELDED CRACKS PER DPS 102.25 AND REINSTALLED FLOOR SUPPORT IAW SRM 51-1-20D AND 51-1-21. ARROW AIR WORK ORDER NR 950007Mar 13, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR ARWA031351L/E Skin · crackedDURING C-CHECK, FOUND RIGHT WING LEADING EDGE BETWEEN NR 3 AND NR 4 ENGINES AT APPROXIMATE MID SECTION LOWER RIB SUPPORT PLATE WITH 2 CRACKS EMINATING FROM FASTENER HOLES. REMOVED AND FABRICATED REPLACEMENT PANEL PREPPED AND INSTALLED IAW SRM 57-2-1 PG 155/15Mar 13, 1995 · N791AL · Doug DC862F · Wing, Plate/SkinSDR 95ZZZX2495Cargo Track · corrodedAFT LOWER CARGO COMPARTMENT, LT TRACK, HAS LEVEL II CORROSION AT FS 1080 - FS 1120, W.O. NR 950007, C/N 5163. REMOVED DAMAGED AREAS, TREATED, PRIMED AND INSTALLED NEW SECTION OF TRACKS PER SRM 53-2-3, AND SRM 51-1-21D.Mar 13, 1995 · N791AL · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA199519Engine · bird stikeON DEPARTURE OUT OF DIEGO GARCIA, A SEA BIRD WAS OBSERVED TO ENTER THE NR 1 ENGINE, CAUSING SUBSTANTIAL FOREIGN OBJECT DAMAGE TO THE ENGINE GAS PATH. INGESTION OF THE SEA BIRD ALSO CAUSED DAMAGE TO THE NOSE COWL, BULLET, AND FAN DUCTS. THE AIRCRAFT RETURNED Mar 6, 1995 · N41CX · Doug DC862F · Engine (Turbine/Turboprop)SDR ARWA022854Intercostal · corrodedDURING C-CHECK, FOUND FORWARD ACCESS COMP VERT STIFFENER AT L-28L AND FS 208.00 HAS LEVEL 2 CORROSION. CUT OFF CORROSION SECTION OF STIFFENER, FABRICATED NEW SECTION OF STIFFENER FROM .071 7075-T6 AS PER SRM 53-1-0 AND SRM 52-2-0. (M)Feb 28, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR ARWA022852Web · crackedDURING C-CHECK, FOUND FORWARD FUSELAGE STRUCTURE JUST BELOW RADOME SUPPORT RODS, CRACKED LEFT AND RIGHT SIDE. ROUTED OUT CRACKED MATERIAL BLENDED, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0. (M)Feb 28, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR ARWA022851Fitting · brokenDURING C-CHECK, FOUND 'B' BELLY LOWER DOOR FRAME SECOND FROM ATT 'T' BOLT BRACKET BROKEN IN HALF. REMOVED FITTINGS, FOUND AREA CORRODED REMOVED CORROSION AND TREATED AND PRIMED IAW SRM 51-1-8. REINSTALLED FITTING IAW SRM 51-3-0. RESEALED AREA WITH PRC 1422 Feb 28, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR AR022853Panel · corrodedRIGHT WING OUTBOARD SLOT MIDDLE PANEL HAS LEVEL 2 CORROSION, REF CPCP 027 115R 0551. FOUND AREA BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER IAW EO 9503061. (X)Feb 28, 1995 · N791AL · Doug DC862F · Trailing Edge Flaps
Back to Douglas DC-8-62F