Douglas DC-8-73F

Service difficulty reports · 15,471

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 = 'DC873F'
  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 RRXA000481Fitting · crackedDURING A MAINTENANCE VISIT FOUND LONGERON 31 LEFT SPLICE FITTING CRACKED BETWEEN STA 200 TO STA 220. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLICE FITTING IAW DC-8 SRM 51-1-20Dec 3, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R483EWAFitting · corrodedFOUND DURING D-CHECK, NR 3 FLAP CANOE T/E CHAFFED TRACK BOLT HOLES HAVE CORROSION EMANATING FROM THEM. REAMED HOLES TO REMOVE CORROSION. TREATED AND PRIMED. INSTALLED TWO NAS4653151-7-27 BOLTS AND ASSOCIATED HARDWARE PER EO NR 99-186 WITH APPROVED 8110-3 DADec 3, 1999 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR 99T64R544EWAFitting · damagedFOUND DURING D-CHECK, LT TRAPEZOIDAL FITTING HAS ELONGATED HOLE. REAMED HOLE. FABRICATED BUSHING AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/12/99. (M)Dec 3, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000199Fitting · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO NR 3 FLAP CANOE TRAILING EDGE TRACK BOLTS HOLES. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REAMED HOLES TO REMOVE CORROSION, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED TWO NAS4653151-7-27 BOLTS AND ASSOCIADec 3, 1999 · N605AL · Doug DC873F · Trailing Edge FlapsSDR RRXA000236Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 36 BETWEEN STA 720 TO STA 781, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER & DOUBLER IAW BOEING M-7200-99-10647 & M7200-Dec 2, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000194Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN BETWEEN STA. 781 TO STA. 742 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA Dec 2, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 99T64R740EWAKeelbeam · corrodedFOUND DURING D-CHECK, KEEL BEAM STATION 720 TO 781 HAS EXFOLIATED CORROSION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER AND INSTALLED PER BOEING M-7200-99-10647 AND M7200-99-10680 WITH APPROVED 8110-3 DATED 12/10/99. (M)Dec 2, 1999 · N605AL · Doug DC873F · Fuselage Main, KeelSDR 99T64R739EWASkin · corrodedFOUND DURING D-CHECK, LEFT FILLET SKIN CORROSION AT L35L BETWEEN STATION 781-742. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SPLICE PLATE AND REPLACEMENT SKIN AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/01/99. (M)Dec 2, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 99T64R738EWAAngle · corrodedFOUND DURING D-CHECK, ATTACH ANGLE IN FRONT OF WING LIGHT LENS CORRODED ON WING FILLET PANEL 262A RIGHT. BLENDED OUT CORROSION. FABRICATED DOUBLERS AND INSTALLED PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/19/99. (M)Dec 2, 1999 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR 99T64R547EWASkin · damagedFOUND DURING D-CHECK, RIGHT WING LEADING EDGE HAS 4 NUT PLATES MISSING TOP OF L/E STATION XFS 22.75 - 24 AND 103-104.25. INSTALLED NAS 1670-4L FASTENERS WET WITH PR 1422B.5 PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/24/99. (M)Dec 2, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000201Skin · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACH ANGLE IN FRONT OF RT WING LIGHT LENS COMMON TO FILLET PANEL 262 RIGHTHAND. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERDec 2, 1999 · N605AL · Doug DC873F · Wing, Plate/SkinSDR 20000609AP011Floorbeam · corrodedFOUND DURING D-CHECK, FLOORBEAM AT STATION 1580 BETWEEN NR 1 - NR 2 SEAT TRACKS HAS BLOWOUT OF CORROSION AT NUT PLATE. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20D. (M)Dec 1, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR 20000522AP011Brace · crackedFOUND DURING D-CHECK, CRACK IN FLOOR BRACE AT STATIN 1740 AT XCW 40 LEFT CABIN. REMOVED FLOOR BRACE IAW DC-8 SRM 51-1-4. FABRICATED L ANGLE BRACE. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-20, 51-1-8. (M)Dec 1, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000227Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1580 BETWEEN NR 1 AND NR 2 SEAT TRACK. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0, 51-1Dec 1, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR DHL99801003Line · leakingEXPERIENCED HYDRAULIC QUANTITY LOSS. FOUND PRESSURE LEAKING AT STBY HYDRAULIC PUMP. REMOVED AND REPLACED FLEX PRESSURE LINE, OPS AND LEAK CHECK GOOD.Dec 1, 1999 · N801DH · Doug DC873F · Hydraulic System, MainSDR RRXA000475Seat Track · damagedDURING A MAINTENANCE VISIT FOUND MAIN CABIN SEAT TRACK BETWEEN STA 120 TO STA 240 AND BL 69 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3.Nov 30, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 20000427AP006Seat Track · wornFOUND DURING D-CHECK, CABIN SEAT TRACK NR 1 XCW 69 LEFT STATION 120-240 WORN. REMOVED SEAT TRACK IAW DC-8 SRM 51-1-21. INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-1-21, 51-3-0, 51-1-8, 53-2-3. (M)Nov 30, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000283Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 1050 AND LONGERON 21 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4.Nov 29, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000609AP013Floorbeam · corrodedFOUND DURING D-CHECK, CABIN STATION 1680 FLOORBEAM BETWEEN SEAT TRACK 6-7 HAS EXFOLIATED CORROSION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FLOORBEAM EXTRUSION. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21, 51-1-4. (M)Nov 28, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000226Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1680 BETWEEN SEAT TRACK NR 6 & 7. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM EXTRUSION IAW DC-8 SRM 51-1-Nov 28, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991588Skin · corrodedON WALKAROUND, FOUND CORROSION HOLE ON LOWER BELLY AFT OF ADF ANTENNA LT SIDE. ACFT PREPARED FOR FERRY FLIGHT. THIS ACFT INSPECTED AND FOUND IT SAFE FOR THE FLIGHT INTENDED.Nov 28, 1999 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000248Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 1220 AND LONGERON 32 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE SHEETNov 27, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000613AP003Fitting · corrodedFOUND DURING D-CHECK, AFT LOWER CARGO COMPARTMENT STATION 1220 L32R END FITTING CORRODED. REMOVED FITTING IAW DC-8 SRM 51-1-20D. CUT NEW FITTING IAW DC8 SRM 53-2-0 F2 SHEET 2. TREATED, PRIMED AND INSTALLED FITTING IAW DC-8 SRM 51-1-8, 53-2-0. (M)Nov 27, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000281Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOASTAL BETWEEN STA 520 TO STA 560 AND LONGERON 33 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW INTERCOASTAL AND INSTALLED IAW DC-Nov 26, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000242Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1060 AND LONGERON 36, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FILLER & DOUBLER IAW FAA DER APPROVED ENGINEERING SNov 26, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR 20000613AP005Frame · corrodedFOUND DURING D-CHECK, C PIT STATION 1060 L36 CORROSION ON CIRCUMFERENTIAL FRAME. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED NEW FRAME AND DOUBLERS FOR SPLICE IAW DC-8 SRM 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D AND EO NR 99Nov 26, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000311Plate · crackedDURING A MAINTENANCE VISIT FOUND AFT LOWER CARGO DOOR EXTERNAL SKIN SCUFF PLATE CRACKED RIGHT SIDE STA 1240. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGNov 26, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R540EWAPlate · crackedFOUND DURING D-CHECK, RIGHT AFT PASSENGER DOOR SCUFF PLATE CRACKED IN CORNER AND BROKEN ON ENDS. STOP DRILLED CRACK. NDT CONFIRMED CRACK HAD BEEN STOPPED. WELDED CRACK PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11Nov 26, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99831154Battery Pack · dischargedINSPECTION TYPE:N/A, ON PREFLIGHT EMERGENCY LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CK GOOD.Nov 26, 1999 · N806UP · Doug DC873F · Emergency LightingSDR RRXA000317Attach Fitting · crackedDURING A MAINTENANCE VISIT FOUND FITTING CRACKED AT STA 1200 AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D.Nov 25, 1999 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA991587Switch · malfunctionedLM GEAR DOWN (GREEN) LIGHT WILL NOT ILLUMINATE GEAR WARNING (RED) LIGHTS NORMAL RECYCLED GEAR. NO HELP LIGHT CAME ON DURING FINAL APPROACH. REMOVED AND REPLACED LT MAIN LANDING GEAR SWITCH OP'S CHECK NORMAL ON GROUND AS PER MM 32-60-00.Nov 25, 1999 · N791FT · Doug DC873F · Landing Gear Position and WarningSDR UPS99831152Fuel Filter · contaminatedINSPECTION TYPE:N/A, NR 4 ENGINE FLAME-OUT FL350 1717Z OIL PRESS ZERO FLAME-OUT. INFLIGHT ENGINE START AND INFLIGHT ENGINE SHUTDOWN ACCOMPLISHED, MX CONTROL NOTIFIED. FL 310 RE-ATTEMPTED ENG START 1728Z OIL PRESS ZERO. ALL ENG PARAMETERS NORMAL, NO LIGHT OFNov 24, 1999 · N802UP · Doug DC873F · Aircraft Fuel Filter/StrainerSDR UPS99831147Gauge · inopREVERSER HYDRALIC PRESS GAUGE INDICATES ZERO WITH HYD S/O SWITCH OFF WITH SWITCH IN THE OPEN POSITION ABLE TO GET ALL 4 REVERSORS ON LANDING ROLL. REPLACED HYD PRESS GAUGE AND TRANSMITTERS. OPS CHECK OK, NO LEAKS.Nov 24, 1999 · N810UP · Doug DC873F · Hydraulic Indicating SystemSDR DHL99805002Strut · dischargedAFTER TAKEOFF, LANDING GEAR HANDLE JAMMED IN DOWN POSITION. COMPLETED ABNORMAL PROCEDURES RETURNED TO CVG. RESERVICED NOSE STRUT WITH HYDRAULIC FLUID AND NITROGEN. PERORMED GEAR SWING AND OPS CHECKED GOOD PER DC-8 M/M.Nov 24, 1999 · N805DH · Doug DC873F · Nose/Tail Landing Gear Strut/AxleSDR RRXA000254Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 70 AND LONGERON 31 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-4-1.Nov 23, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000249Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOASTAL BETWEEN STA 1380 TO STA 1400 AND XCW 48 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTION OF INTERCOASTAL IAW DNov 23, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000247Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO END FITTING AT STA 1220 BETWEEN LONGERONS 33 RIGHT TO 34 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53Nov 23, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000613AP006Intercostal · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPT STATION 1380-1400 INTERCOSTAL EXFOLIATED XCW 48 RT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SECTION OF INTERCOSTAL IAW DC-8 SRM 53-2-0. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M)Nov 23, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000613AP002Fitting · corrodedFOUND DURING D-CHECK, AFT LOWER CARGO COMPT STATION 1220 L33R-L34R END FITTING CORRODED. REMOVED FITTING IAW DC-8 SRM 51-1-20D, CUT NEW FITTING IAW DC-8 SRM 53-3-0, 53-20 F2C SHEET 1. TREATED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4, 51-1-20D. (M)Nov 23, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000312Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND AFT PRESSURE BULKHEAD CRACKED AT STA 1766 AND LONGERON 3 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKENov 23, 1999 · N605AL · Doug DC873F · Fuselage Main, BulkheadSDR T64R442EWABulkhead · crackedREAR PRESSURE BULKHEAD CIRCUMFERENTIAL FRAME TOP RIGHT SIDE HAS CRACK STATION 1766-L3R. NDT CONFIMRED END OF CRACK. CUT OUT CRACK SECTION. FABRICATED REPAIR ANGLES. TREATED AND PRIMED. INSTALLED REPAIR PER EO NR 99-186 WITH APPROVED 8110-3 DATED 9/24/99. Nov 23, 1999 · N605AL · Doug DC873F · Fuselage Main, BulkheadSDR 20000424AP020Fitting · corrodedFOUND DURING D-CHECK, A PIT FORWARD STATION 70 L31L END FITTING CORRODED. REMOVED FITTING. REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-24. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-21D, 53-4-1. (M)Nov 23, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000424AP019Fitting · corrodedFOUND DURING D-CHECK, A PIT FORWARD STATION 70 L31L END FITTING CORRODED. REMOVED FITTING. REPLACED FITTING IAW IAW DC-8 SRM 51-1-21, 51-1-24. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-21D, 53-4-1. (M)Nov 23, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000244Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1220 BETWEEN LONGERON 36 TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLEND-OUT DAMAGE TO A ACCEPTABLE LIMIT IAW FAA DER APPROVED ENGINNov 22, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000241Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 35 RIGHT BETWEEN STA 1150 TO STA 1160, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLEND-OUT CORROSION DAMAGE TO A ACCEPTABLE LIMIT IAW FAA DER APPROVEDNov 22, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000238Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN STA 1440 TO STA 1460 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW FAANov 22, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 99T64R686EWAFitting · wornFOUND DURING D-CHECK, EXTERIOR DRAIN FITTING WORN STATION 1270 L36. FABRICATED EXTERNAL DOUBLER AND INSTALLED DOUBLER AND DRAIN FITTING PER EO NR 99-186 WITH APPROVED 8110-3 DATED 11/19/99. (M)Nov 22, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 99T64R488EWASkin · corrodedFOUND DURING D-CHECK, AFT LOWER CARGO COMPARTMENT STATION 1440-1460, L31R FINGER DOUBLER HAS CORROSION. REMOVED CORROSION, CUT FINGER DOUBLER OFF. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/27/99Nov 22, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000309Fitting · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING FLAP STOP FITTING CRACKED AT XFS 410. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FLAP STOP FITTING IAW DC-8 SRM 51-3-0.Nov 22, 1999 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000298Rib · crackedDURING A MAINTENANCE VISIT FOUND LEFT WING, FLAP WELL, RIB CRACKED AT XRS 178. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA DER APPROVED ENGINEERING SKETCH EO 99-18Nov 22, 1999 · N605AL · Doug DC873F · Wing, Rib/Bulkhead
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