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 RRXA991388Finger Dougler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BLISTER AT FINGER DOUBLER AT STA 616 BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEWJun 17, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL99806002Computer · malfunctionedON TAKEOFF ROLL, STICK SHAKER CAME ON AND STAYED ON, REJECTED TAKEOFF. REMOVED AND REPLACED LIFT COMPUTER, LIFT TRANSDUCEER, STALL WARNING MOD TRANSFER RELAY.Jun 17, 1999 · N806DH · Doug DC873F · Stall Warning SystemSDR UPS99829853Battery Pack · dischargedINSPECTION TYPE:N/A, DURING CREW PREFLIGHT EMERGENCY EXIT LIGHTS FAILED TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. LIGHTS CHECK GOOD.Jun 16, 1999 · N806UP · Doug DC873F · Emergency LightingSDR RRXA991403Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK IN SKIN AT STA 55, LONGERON 34 RIGHT EXTERNAL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SEJun 16, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991395Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 31 LEFT AT STA 1220. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLATE DOUBLER IAW DC8 SRM 51-1-21 AND IAW FAA APPROVED TENNEJun 16, 1999 · N604AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991380Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN, BOTTOM OF FWD LAV SERVICE PANEL BETWEEN STA 75R AND STA 105R, AND BETWEEN LONGERONS 25 RIGHT AND LONGERON 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51Jun 16, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829970Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 2 MAIN O/B AT W/S 74.000 REAR SPAR HAS AFT FITTING CRACKED. REMOVED AND REPLACED END FITTING IAW DAC DAW 5613423 AND DC8 SRM 51-1-20 D.Jun 15, 1999 · N807UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829969Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN I/B AT W/S 74.000 REAR SPAR HAS FWD AND AFT FITTINGS CRACKED. REMOVED AND REPLACED FITTINGS W/SERVICABLE PART IAW DAC DWG 5613423 AND DC8 SRM 51-1-20D.Jun 15, 1999 · N807UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829968Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN IB AT FS 74 REAR SPAR HAS TWO CRACKED FITTINGS. REMOVED AND REPLACED END FITTING IAW UPS DC8 SRM 51-2-20D AND DWG 3704 841.Jun 15, 1999 · N807UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829960Fitting · crackedINSPECTION TYPE:C-1 LONGERON END FITTING CRACKED L10L AFT SIDE OF FRAME 902. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-21.Jun 15, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991746Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1680 AND X=56. 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 APPROVED Jun 15, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991739Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=1000 TO Y=1300 AND X=50. 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 APPROVEJun 15, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991692Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT BEAM HAT CHANNEL BETWEEN AT Y=1766 AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNELJun 15, 1999 · N791FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991691Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL BETWEEN Y=1745 TO Y=1766 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 NEW HAT Jun 15, 1999 · N791FT · Doug DC873F · Fuselage Main, FrameSDR RRXA991690Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL AT Y=1766 AND X=-10. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNEL IAW DC-8 SRM 51-3-Jun 15, 1999 · N791FT · Doug DC873F · Fuselage Main, FrameSDR RRXA991689Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL AT Y=1745 AND X=-10. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNEL IAW DC-8 SRM 51-3-Jun 15, 1999 · N791FT · Doug DC873F · Fuselage Main, FrameSDR RRXA991688Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM UPPER SURFACE AT Y=1700 BETWEEN LONGERONS 21 LEFT TO 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 53-2-0.Jun 15, 1999 · N791FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991745Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1680 AND X=-10. 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 APPROVEDJun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991744Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1620 AND X=50. 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 APPROVED Jun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991742Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-3 BETWEEN Y=1300 TO Y=1680 AND X=-20. 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 APPROVJun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991741Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 BETWEEN Y=1300 TO Y=1680 AND X=-10. 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 APPROVJun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991738Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=1000 TO Y=1300 AND X=30. 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 APPROVEJun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991737Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=1000 TO Y=1300 AND X=-30. 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 APPROVJun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991736Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL F BETWEEN Y=1000 TO Y=1300 AND X=-50. 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 APPROVEDJun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991709Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D AT Y=907 AND X=-15. 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 APPROVED DER ENGINEERINGJun 14, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991693Doubler · corrodedDURING FOUND CORROSION DAMAGE TO L-1 DOOR WINDOW EXTERNAL DOUBLER AT Y=160 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED DOUBLER, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW DC-8 SRM 51-1-20.Jun 14, 1999 · N791FT · Doug DC873F · Passenger/Crew DoorsSDR RRXA991424Frame · crackedDURING A MAINTENANCE VISIT, FOUND MAIN CARGO DOOR UPPER JAM 2 AREAS CRACKED OUT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICEJun 14, 1999 · N604AL · Doug DC873F · Fuselage Main, FrameSDR UPS99829967Fitting · crackedINSPECTION TYPE:C-1 SPLICE FITTING FS 1050 AT LONGERON 35 RT IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-3-2 AND 51-1-20D.Jun 13, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829966Intercostal · crackedINSPECTION TYPE:C-1 INTERCOSTAL CRACKED AT LONGERON 35L BETWEEN FS 1080-1100. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DAC DWG 9758507 AND DC8 SRM 51-1-20D.Jun 13, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829961Splice · crackedINSPECTION TYPE:C-1 STA 1700 LONG 24 LEFT FRAME SPLICE IS CRACKED. REMOVED FABRICATED AND INSTALLED FRAME SPLICE IAW DC8 SRM 51-1-20D, 53-5-3, DAC DWG 612142, 51-1-8 AND 51-1-20D.Jun 13, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991751Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERIOR SKIN PANEL AT Y=718 AND LONGERON 35 RIGHT. 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 APPROVED DERJun 12, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991701Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=409 TO Y=417 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 DOUBLER IAW DC-8 Jun 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR UPS99829963Floor · corrodedINSPECTION TYPE:C-1, CORROSION ON FLOOR PANEL AT RBL 35 AT FS 350. REMOVED CORROSION, FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-3 AND INSTALLED REPAIR.Jun 11, 1999 · N807UP · Doug DC873F · Fuselage Floor PanelSDR UPS99829965Frame · corrodedINSPECTION TYPE:C-1, CORROSION EMITTING FROM AROUND AND UNDER NUT PLATES ON BOTTOM SIDE OF FRAME FLANGE AT STA 100 BETWEEN LONG 34R TO 36. REMOVED CORRODED MATERIAL OUT OF LIMITS. REPAIRED WITH FILLER/DOUBLER REPAIR IAW DAC DWG 9753784, 53-2-0, 51-1-8, 51-1-Jun 10, 1999 · N807UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829800Girt Bar · inoperativeCREW ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT BAR INOP. REPOSITIONED GIRT BAR LOCKING CLIPS ON FLOOR, GIRT BAR LOCK CKS GOOD.Jun 10, 1999 · N805UP · Doug DC873F · Emergency EquipmentSDR RRXA991412Plate · chafedDURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN LEFT WING CENTER L/E LWR SURFACE STA XFS 304, 2 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAA AJun 10, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991411Skin · chafedDURING A MAINTENANCE VISIT, FOUND CRACK EMANATING FROM RIVET LT WING CENTER L/E STA XFS 304, 15 FWD OF FRONT SPAR ON LWR SURFACE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAJun 10, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991390Cargo Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 980 AND STA 1100 TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK IAW DC8 SRM 51-1Jun 10, 1999 · N604AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991389Cargo Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 1020 AND STA 1140, FLOOR TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK IAW DC8 Jun 10, 1999 · N604AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991379Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, AFT LOWER CARGO COMPARTMENT AT STA 1220, BL 45 RIGHT FLOOR STRUT DOUBLER NEXT TO FLOORBEAM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED DOUBLER IAW Jun 10, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829964Seat Track · corrodedINSPECTION TYPE:C-1, SEAT TRACK AT STA 870, BL O.O CORR DOT E560. REMOVED CORROSION IAW DC8 SRM 51-1-8 NOT WITHIN LIMITS IAW DC8 SRM 5 3-2-3. REMOVED DAMAGED SECTION OF TRACK STA 850-890 IAW DC8 SRM 53- 2-3. INSTALLED NEW TRACK SECTION IAW DC8 SRM 53-2-3.Jun 9, 1999 · N807UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829962Floor · corrodedINSPECTION TYPE:C-1 FLOOR PNL 58-880 ROW A IS CRACKED AT ATTACH HOLE, HAS 2 EACH GOUGES, NUMEROUS AREAS OF BARE METAL AND CORROSION, AND MISSING/DAMAGED NON- SKID. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0 FIG LF. INSTALLED NON-SKID TAPE AS NECESSARY IAW Jun 9, 1999 · N807UP · Doug DC873F · Fuselage Floor PanelSDR UPS99829957Floor Panel · corrodedINSPECTION TYPE:C-1 FLOORBOARD CORRODED ROW-C FS880-1000. REMOVED CORROSION IAW DC8 SRM 51-1-8, REPAIR CORRODED AREA IAW DC8 SRM 53-2-3. ALODINE AND PRIME IAW DC8 SRM 51-1-8, INSTALL REPAIR DOUBLER IAW DC8 SRM 51-1-21.Jun 9, 1999 · N807UP · Doug DC873F · Fuselage Floor PanelSDR UPS99829956Floorboard · corrodedINSPECTION TYPE:C-1 FLOOR PANEL FS 1470 LBL 35 HAS CORROSION BULGE AROUND INSERT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, FAB DOUBLER IAW DC8 SRM 53-2-3, INSTALL DOUBLER IAW DC8 SRM 51-1-8.Jun 9, 1999 · N807UP · Doug DC873F · Fuselage Floor PanelSDR UPS99829955Floorboard · corrodedINSPECTION TYPE:C-1 FLOORBOARD CORRODED AROUND INSERT FS 1420 LBL 10. REMOVED CORROSION IAW DC8 SRM 51-1-8, CUT OUT DAMAGE AND REPAIR IAW DC 8 SRM 53-2-3 ALODINE AND PRIME REPAIR DOUBLER IAW DC8 SRM 51-1-8. INSTALLED ALL REPAIR DOUBLER IAW DC8 SRM 51-1-21A.Jun 9, 1999 · N807UP · Doug DC873F · Fuselage Floor PanelSDR UPS99829928Floorbeam · corrodedINSPECTION TYPE:C-1, MAIN CABIN RT SIDE FS 1680 BL 24 THRU 34 FLOORBEAM T-CAP CORRODED ON UNDERSIDE OF NUT PLATE. FAB NEW ANGLE IAW DOUGLAS DWG 5892151, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-3-0.Jun 9, 1999 · N807UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99829890Doubler · crackedINSPECTION TYPE: C1, RT W/W INBOARD DOOR, AFT CORNER OF TONGUE REPAIR. DOUBLER GOUGED AND CRACKED. REPAIRED BY FABRICATION AND INSTALLATION OF DOUBLER IAW DC 8 SRM 52- 2-0 AND DC 8 SRM 51-1-21, 51-1-20A, 51-3-0. SEALED REPAIR IAW DC8 SRM 51-1-16.Jun 9, 1999 · N807UP · Doug DC873F · Landing Gear DoorsSDR RRXA991621Splice · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LWR FWD CARGO COMPT AT STA 616 AND LONGERON 31 RIGHT, SPLICE CRACKED AND HAS CORROSION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SJun 9, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991382Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT WING I/B L/E UPPER SURFACE AT STA XFS 54.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW FAA APPROVED TENNEJun 9, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829773Switch · failedINSPECTION TYPE:ASN, CABIN DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. ACARS SENSORS (MAIN CREW) CONFIRMED DOOR. AIRCRAFT MAINTAINED DIFFERENTIAL PRESSURIZATION. DOOR APPEARS CLOSED AND SECURE. REPLACED LEFT AFT SERVICE DOOR MICROSWITCH AND CHECKED PER 52-70.Jun 8, 1999 · N813UP · Doug DC873F · Door Warning System
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