Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR UPS99830705Intercostal · crackedINSPECTION TYPE:C1 INTERCOSTAL AT FS 280, LONGERON 11R IS BENT, CRACKED AND CORRODED. REMOVED DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL IAW DAC DWG 3704510. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D.Sep 6, 1999 · N836UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830704Fitting · corrodedINSPECTION TYPE:C1 RT LONGERON 24 FITTING AT STA 879 HAS CORROSION FWD AND AFT (REMOVED FITTING AND FOUND 2 CRACKS). REMOVED FITTING, REMOVED CORROSION. REPAIRED CRACKS ON LONG 24 WITH REPAIR ANGLES IAW DC8 SRM 53-2-2 FIG 5.Sep 6, 1999 · N836UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830699Skin · punctureINSPECTION TYPE:C1 PUNCTURE, UNDERSIDE NR 1 SPOILER, DOT E972. MATERIAL ID FILLER AND DOUBLER 7075-T-6.016 PO NR 271715, FABBED FILLER AND DOUBLER IAW SRM 51-1-9A. BONDED FILLER AND DOUBLER IAW DC8 SRM 51-1- 9A. REINSTALLED SPOILER IAW DC8 MM 27-61-01.Sep 6, 1999 · N836UP · Doug DC873F · SpoilersSDR UPS99830670Skin · dentedINSPECTION TYPE:C1, RT I/B FLAP LOWER SKIN HAS 2 DENTS STA XRS 74 AND XRS 172. REMOVED DAMAGE FROM FLAP, FABBED AND INSTALLED DOUBLERS IAW DC8 SRM 57 2-1 & 51-1-21.Sep 6, 1999 · N836UP · Doug DC873F · Trailing Edge FlapsSDR RRXA991685Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FORWARD PRESSURE PANEL BETWEEN Y=-52 TO Y=-12 AND Z=-8. 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 APPROVEDSep 6, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830773Seat Track · gougedINSPECTION TYPE:C1, STA 781 SEAT TRACK G GOUGED. BLENDED SCALLOPS AT DAMAGED AREA PER DC8 SRM 51-1-8. FOUND OUT OF LIMITS. CUT DAMAGED AREA AT G SEAT TRACK FROM STA 770 TO 810 PER UPS SRM ADDENDUM DC8-5320-8309. REPLACED DAMAGED SEAT TRACK IAW UPS DC8 SRM Sep 5, 1999 · N836UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99830744Frame · damagedINSPECTION TYPE:C1, STA 1580 LONG, L19L TO L14L HAD DRILL DAMAGE. CLEANED UP DAMAGED AREA AND REPAIRED FRAME IAW TIMCO DWG DC8 53-0229, REO 06737 AND UPS COVER SHEET DC8 53-2711.Sep 5, 1999 · N836UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830743Frame · corrodedINSPECTION TYPE:C1, MAIN CABIN STA 1480 L3R TO L4R FRAME FWD FACE CORRODED. REMOVED CORROSION, FRAME FOUND TO BE OUT OF LIMITS. FABBED SPLICES IAW DC8 SRM 53-2-0, HEAT TREAT FOR T-6 CONDITION. GEN AND REC'D RFTS NR 836UP-24-20191 W/REO 06760, MAT ID S253771Sep 5, 1999 · N836UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830742Seat Track · gougedINSPECTION TYPE:C1, STA 160 SEAT TRACK F SCALLOPS GOUGED IN TRACK OUT OF LIMITS. REMOVED DAMAGED TRACK, FABBED AND INSTALLED REPLACEMENT SECTION IAW DC8 SRM 53-2-3.Sep 5, 1999 · N836UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99830741Web · double drilledINSPECTION TYPE:C1, MISDRILLED HOLE FS 160 FWD LOWER CORNER OF TORQUE BOX AND FWD PART O F FWD RT SERVICE DOOR, DOTS E761, E764, E768. FABBED WEB AND REPAIR ANGLE IAW DAC DWG 561570D & FDC8 SRM 53-2-0 FIG 1B. HEAT TREATED ANGLE IAW TPS 1003 REV A. INSTALLEDSep 5, 1999 · N836UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830717Fitting · crackedINSPECTION TYPE:C1, FLOORBEAM LWR TIE FITTING IS CRACKED AT STA 759, LBL 48. REPAIRED AREA IAW 8110-3 APPROVED DH SK 852-726.Sep 5, 1999 · N852UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830707Frame · damagedINSPECTION TYPE:C1 STA 1580 R/S 26 ABOVE CUSP FRAME AND GUSSETT HAS DRILL DAMAGE. REMOVED DAMAGED GUSSETT AND FASTENER IAW DC8 SRM 51-21-1. REMOVED DAMAGE FROM FRAME IAW REO 06735. FABBED AND INSTALLED NEW GUSSET AND REPAIR ANGLE IAW DAC DWG 9751061, REO 06Sep 5, 1999 · N836UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830706Frame · damagedINSPECTION TYPE:C1 STA 1600 19 ABOVE CUSP, FRAME AS DRILL DAMAGE IN RADIUS OF FLANGE GEN RFTS N836UP-03-20183 ON 9-7-99, REC'D RFTS 9-8-99. MATERIAL VERIF ICATION 7075-0.071 PO NR 296823, FABBED FILLER AND SPLICES IAW DC8 SRM 53 -2-0; LOCATED, DRILLED AND TRISep 5, 1999 · N836UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830684Seat Track · corrodedINSPECTION TYPE:C1, STA 1270 SEAT TRACK G HAS CORROSION DOWN CENTER. FABRICATED SPLICE CHANNEL IAW DC8 5320-8309 APP-B. DRILLED AND LOCATED SEAT TRACK SPLICES AND SEAT TRACK IAW DC8 SRM 51-1-24. INSTALLED SEAT TRACK SPLICES & SEAT TRACK IAW DC8 SRM 51-3-0.Sep 5, 1999 · N836UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99830669Seat Track · gougedINSPECTION TYPE:C1, STA 600 SEAT TRACK F SCALLOPS GOUGED BLENDED DAMAGED IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED OUT OF LIMITS SECTION STA 570-610 IAW DC8 SRM UPS ADDENDUM DC8-53B-003.Sep 5, 1999 · N836UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99830668Beam · crackedINSPECTION TYPE:C1, RT AFT DOOR HAS CRACKED FRAME AT UPPER FWD CORNER. OPENED INNER WEB AND REMOVED CRACKED DOOR BEAM. FABRICATED NEW DOOR BEAM (P/N 5772639-21) IAW DC8 SRM 51-1-21, INSTALLED IAW DC8 SRM 51-1-2 0D, 51-1-21 AND REINSTALLED INNER WEB IAW DC8 SSep 5, 1999 · N836UP · Doug DC873F · Service DoorsSDR UPS99830667Frame · gougedINSPECTION TYPE:C1, FRAME FACE GOUGED IN RADIUS AT STA 1660 LONG 4L. TRIMMED OUT DAMAGE AND REPAIRED IAW REO-06735.Sep 5, 1999 · N836UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830569Switch · inopINSPECTION TYPE:N/A, ATB-LOUD HOWLING NOISE IN THE COCKPIT COMING FROM THE NOSE AREA IMPEDING COMMUNICATIONS. FOUND LEFT FAN INLET DOOR REMAINS OPEN IN FLIGHT. REPAIRED GROUND AT S3-8012. ALSO, REMOVED AND REPLACED R2-25, DOOR NOW CLOSES WITH GROUND TO FLIGSep 5, 1999 · N808UP · Doug DC873F · Cabin Temperature Control SystemSDR RRXA991683Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, UPPER SURFACE SKIN BETWEEN XFS=20 TO XFS=38.750. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLESep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991511Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FINGER DOUBLER AT LONGERON 31 LEFT BETWEEN STA 440 AND STA 460 LT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TENNESSEESep 5, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991507Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, SCREWS PULLING THROUGH SKIN LEFT WING INBOARD LEADING EDGE UPPER BETWEEN STA XFS 20 AND STA XFS 38.750 AT FRONT SPAR. CORROSION FOUND IN SCREW HOLES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREASep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991488Skin · damagedDURING A MAINTENANCE VISIT, FOUND FASTENERS LOOSE RIGHT WING O/B SLOT L/E O/B END AT STA XS 491.193. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAA APPROVED TENNESSEE TECSep 5, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR UPS99830576Battery · dischargedINSPECTION TYPE:N/A, DURING BISE CHECK THE EMERGENCY EXIT LIGHT DO NOT ILLUMINATE. REMOVED AND REPLACED EMER EXIT LIGHTS BATTERY, OPS CHECK NORMAL.Sep 4, 1999 · N814UP · Doug DC873F · Emergency LightingSDR 99T64R448EWAFlange · gougedFOUND DURING D-CHECK, FLANGE ON AFT SIDE OF OUTBOARD W/W AT WING AT WING STATION XRS 90.0 GOUGE APPROX .25 INCH IN DIAMETER. (M)Sep 3, 1999 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA991495Skin · crackedDURING A MAINTENANCE VISIT FOUND 4 CRACK EXTENDING FROM RIVET RT WING UPPER SURFACE AT STA 69.5 AT REAR SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 57-2-1 AND FAA APPROVED TENNESSep 3, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR DHL9980669CSkn · crackedAT C CHECK, LOWER EXT FUSELAGE STA 800 RIGHT SIDE AREA AROUND RIVET IS CRACKED. CUT OUT DAMAGED SECTION AREA OF SKIN. FABRICATED NEW SKIN AND INSTALLED PER SRM 53-3-0. N/R 835.Sep 3, 1999 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991502Insert · strippedDURING A MAINTENANCE VISIT, FOUND NUMEROUS TRAY TIE DOWN INSERTS STRIPPED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED DYNA SYSTEM THREAD INSERTS P/N: 021-1-8200 IN PLACE OF P/N: 3755486-1 IAW FAA APPROVSep 2, 1999 · N791FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980668CFloor · puncturedAT C CHECK, CENTER FLOOR STA 1240-1260 HAS HOLES IN MIDDLE OF PANEL. FABRIACATED DOUBLERS TWO 3 BY 3 FT AND TWO 1 BY 1 PER SRM 53-2-0. N/R 802.Sep 1, 1999 · N806DH · Doug DC873F · Fuselage Floor PanelSDR DHL9980667CSkin · crackedAT C CHECK, RT WING T/E SECTION I/B AREA APPROX STA XW 33 WEB HAS CRACK. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER PER SRM 51-1-8 AND INSTALLED PER SRM 57-2-0, 7 BY 2 N/R 773.Sep 1, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980636CFloor · crackedAT C CHECK, C3 CARGO COMPT FLOOR FROM STA 1140-1160 CENTER HAS CRACK AROUND GOUGE ON LWR SIDE. TRIMMED CRACKED AREA OF FLOOR BOARD, FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. INSTALLED DOUBLER IAW DC8 SRM 51-1-21, PG 1. N/R CARD NR 0810.Sep 1, 1999 · N806DH · Doug DC873F · Fuselage Floor PanelSDR RRXA991501Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY RT O/B STA 340. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 57-51-12 AND IAW FAA APPROVED TAug 31, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA991500Support · damagedDURING A MAINTENANCE VISIT REMOVE AND REPLACE FLAP LINK SUPPORT ASSY RT MID STA 219. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINK SUPPORT IAW DC8 M/M 27-51-12 AND IAW FAA APPROVED TENAug 31, 1999 · N791FT · Doug DC873F · Trailing Edge Flap ActuatorSDR DHL9980666CIntercostal · crackedAT C CHECK, BELOW FLOOR PANEL AT COCKPIT, INTERCOSTAL PANEL AT CENTER LINE REAR UPPER FLANGE CRACKED. STOP DRILLED END OF CRACK, FABRICATED ANGLE PER SRM 53-2-0 AND INSTALLED 7 BY 3.5, N/R 693.Aug 31, 1999 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980642CDoubler · crackedAT C CHECK, MAIN CARGO DOOR CUTOUT LWR AREA EXISTING DOUBLER REPAIR IS CRACKED AT STA 170.00. REMOVED DAMAGED EXISTING DOUBLER, FABRICATED REPAIR DOUBLER AND INSTALLED IAW E/O NR 999090303. N/R CARD NR 0684.Aug 31, 1999 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980625CStrip · brokenAT C CHECK, LT WING UPPER EXTERIOR SURFACE CTR SPAR TRIM ANGLE BROKEN XRS 50. REMOVED DAMAGED STRIP AND FABRICATED NEW METAL STRIP FROM SAME MATERIAL IAW DC8 SRM 51-1-4 PAR 3. INSTALLED STRIP IAW DC8 SRM 51-1-15, PAR 2. N/R CARD NR 0711.Aug 31, 1999 · N806DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980624CBracket · crackedAT C CHECK, AFT CARGO DOOR C4 SHOWS TWO SUPPORT BRACKETS CRACKED UPPER SECTOR OF DOOR. REMOVED AND REPLACED BRACKETS IAW DC8 SRM 51-30-0 PAR 1 AND 2. N/R CARD NR 0679.Aug 31, 1999 · N806DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL9980623CBase · crackedAT C CHECK, RADAR ANTENNA BASE ON BULKHEAD HAS CRACK AROUND HOLE. ROUNDED OUT HOLE, DID NOT REQUIRE REPAIR IAW DC8 SRM 53-2-0, PG 2, FIG 1F. N/R CARD NR 0675.Aug 31, 1999 · N806DH · Doug DC873F · Weather Radar SystemSDR UPS99830526Hinge Rod · out of adjustCREW ENTRY DOOR WILL NOT OPEN. LWR HINGE ASSY W/N RETRACT WHEN TURNING HANDLE TO OPEN DOOR, CANNOT BE OPENED UNLESS HINGE IS HELD UP. FWD ENTRY LOWER HINGE CONTROL ROD ASSY PER 52-11-01, OPS CK GOOD PER 52-11-01.Aug 30, 1999 · N852UP · Doug DC873F · Passenger/Crew DoorsSDR DHL9980622CPanel · crackedAT C CHECK, NR 1 RT SPOILER PANEL O/B FITTING IS CRACKED. REMOVED AND REPLACED SPOILER PANEL IAW DC8 MM 27-61-1, PG 201, OPS CKD IAW DC8 MM 27-60-0, PG 501. N/R CARD NR 0635.Aug 30, 1999 · N806DH · Doug DC873F · SpoilersSDR DHL9980665CSkin · crackedAT C CHECK, LEFT WING L/E LOWER SURFACE CRACKED AT RIVET HOLE XFS 291. STOP DRILLED ENDS OF CRACKS. INSTALLED REAPAIR DOUBLER PER EO 99090302, 18 BY 9 N/R 545.Aug 29, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980664CSkin · crackedAT C CHECK, LEFT WING L/E INTERIOR LOWER AREA CRACKED. STOP DRILLED ON WEB SECTON XFS ACCESS PANEL 519 C. FABRICATED REPAIR WEB AND INSTALLED PER SRM 51-1-21.3 BY 2.75, N/R 533.Aug 29, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980635CSkin · crackedAT C CHECK, LT WING L/E LOWER SURFACE CRACK AT RIVET HOLE MARKED DOT 32-59 XFS 291. FABRICATED AND INSTALLED REPAIR DOUBLER IAW E/O NR 99090302 N/R CARD NR 0545.Aug 29, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980621CSkin · damagedAT C CHECK, C3 DOOR SHOWS SKIN DAMAGED AT BOTTOM SIDE. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED NEW SECTION IAW DC8 SRM 52-2-0, INSTALLED SKIN SECTION IAW DC8 SRM 52-2-0 FIG 4, SRM 51-1-21, PAR 1 FIG 32. N/R CARD NR0547Aug 29, 1999 · N806DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL9980620CSkin · crackedAT C CHECK, LT WING L/E INTERIOR CRACK STOP DRILLED ON WEB SECTION MARKED DOT 32-60. FABRICATED DOUBLER IAW DC8 SRM 57-2-0, INSTALLED DOUBLER IAW DC8 SRM 51-1-21, PG 1. N/R CARD NR 0544.Aug 29, 1999 · N806DH · Doug DC873F · Wing, Plate/SkinSDR UPS99830506Skin · dentedINSPECTION TYPE:N/A, DENT IN NR 1 ENGINE OUTBOARD THRUST REVERSER AT 4 O'CLOCK POSITION REF D175215. INSTALLED REPAIR DOUBLER PER CFM MM 78-30-00.Aug 28, 1999 · N810UP · Doug DC873F · Engine Thrust ReverserSDR RRXA991719Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1500 TO Y=1540. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGAug 28, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991513Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT FINGER DOUBLERS ABOVE M/W/W BETWEEN STA 940 AND STA 980, 8 CENTER OF FLOOR PRESS PANEL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEAug 28, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991496Duct · damagedDURING A MAINTENANCE VISIT FOUND DUCT THAT GOES UNDER CONSTANT SECTION HAS HOLE (EO). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLIT SLEEVE AND WELDED OVER CUT OUT. NDT WELD. NO DEFECAug 28, 1999 · N791FT · Doug DC873F · Air Distribution SystemSDR RRXA991749Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-2 BETWEEN Y=1580 TO Y=1680. 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 ENGAug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991747Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-2 BETWEEN Y=1500 TO Y=1540 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 APPROVAug 27, 1999 · N791FT · Doug DC873F · Fuselage Floor Panel
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