Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  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 UPS97825254Angle · corrodedINSPECTION TYPE:C/CK, STA 1690 LONGERON 21 RIGHT LOWER FRAME TO CUSP ANGLE HAS CORROSION. REMOVED ANGLE AT CUSP STA 1690 IAW DC8 SRM 51 3 0. DRILLED NEW ANGLE IAW DC8 SRM 51-1-24. INSTALLED NEW ANGLE IAW DC8 SRM 51-3-0.Nov 7, 1997 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA97310Engine · failedNR 3 ENGINE HAD A VIBRATION. PRECAUTIONARY SHUT DOWN, 0 - OIL QUANTITY. FOUND OIL RESIDUE AND METAL FRAGMENTS IN TAILPIPE AREA OF NR 3 ENG. PREPARED A/C FOR ONE ENG INOPERATIVE FERRY FLT IAW EWA FORM MEO 30.Nov 7, 1997 · N8079U · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS97825320Longeron · corrodedINSPECTION TYPE-C, STA 140 L20R END OF LONGERON CRACKED. FABRICATED SPLICE IAW DC8 SRM 53-4-1. DRILLED SPLICE IAW DC8 SRM 53-2-2. ALODINED, PRIMED, INSTALLED SPLICE IAW DC8 SRM 51-1-8, 53-2-2 AND 51-1-20D.Nov 6, 1997 · N702UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS97825307Longeron · crackedINSPECTION TYPE-C, STA 140L 20R END OF LONGERON IS CRACKED. REPAIRED L20R END FITTING IAW DC8 SRM 53-2-2.Nov 6, 1997 · N702UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS97824963Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS VERY DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKS GOOD.Nov 6, 1997 · N730UP · Doug DC871F · Emergency LightingSDR UPS97824906Window · out of adjINSPECTION TYPE-N/A, 1ST OFFICERS CLEARVIEW WINDOW VERY HARD TO OPEN. ADJUSTED F/O'S CLEARVIEW WINDOW PER MM CH 56-10-03 ADJ/TEST.Nov 4, 1997 · N707UP · Doug DC871F · Flight Compartment WindowsSDR UPS97825076Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS DID NOT FUNCTION DURING (ILLEGIBLE) CHECK. REPLACED EMERGENCY LIGHTING BATTERY PACK, OPS CKS GOOD.Nov 3, 1997 · N707UP · Doug DC871F · Emergency LightingSDR UPS97824831Panel · corrosionINSPECTION TYPE-C, FOUND CORROSION ON LEFT WING LEADING EDGE ACCESS PANEL 520E, XFS 114-137.5. REMOVED AND REPLACED ACCESS PANEL 520E IAW DC8 SRM 51-3-0.Oct 31, 1997 · N797UP · Doug DC871F · Wing, Plate/SkinSDR UPS97824843Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, CHECKS GOOD MM 33-50-0.Oct 30, 1997 · N772UP · Doug DC871F · Emergency LightingSDR UPS97824813Battery Pack · dischargedINSPECTION TYPE:DAL EMG EVAC LIGHTS INOP. FOUND ON DAILY INSPECTION. REMOVED AND REPLACED BATTERY PACK.Oct 30, 1997 · N772UP · Doug DC871F · Emergency LightingSDR UPS97825308Fitting · crackedINSPECTION TYPE-C, FS 1600 BEAM END FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-2 AND 51-1-20D.Oct 29, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825288Floorbeam · corrodedINSPECTION TYPE-C/CK, FUSELAGE STATION 1660 FLOORBEAM IS CORRODED. REMOVED CORRODED SECTION OF BEAM IAW REO 03846, FABBED REPAIR ANGLE IAW REO 03846. INSTALLED, ALODINED AND PRIMED IAW REO 03846 AND DC8 SRM 51-3-0 AND 51-1-20D AND 51-1-8.Oct 29, 1997 · N702UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS97825283Fitting · crackedINSPECTION TYPE-C/CK, AFT FUSELAGE STATION 1600 BEAM END FITTING CRACKED. REMOVED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D.Oct 29, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825260Floorbeam · corrodedINSPECTION TYPE:C/CK, FS 1660 FLOORBEAM IS CORRODED. REMOVED CORRODED SECTION OF BEAM IAW REO 03846. FABBED REPAIR ANGLE IAW REO 03846 INSTALLED ALODINED AND PRIMED IAW REO 03846 DC8 SRM 51-3-0 AND 51-1-20D AND 51-1-8.Oct 29, 1997 · N702UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS97825255Fitting · crackedINSPECTION TYPE:C/CK, AFT FUSELAGE STATION 1600 BEAM END FITTING CRACKED. REMOVED FITTING DRILLED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D.Oct 29, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9700159Pin · shearedEN ROUTE DFW TO TOL UPON GEAR RETRACTION, THE LEFT MAIN GEAR DOWN AND LOCK LIGHT REMAINED ILLUMINATED. THE CREW RECYCLED THE LANDING GEAR AND THE INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL WITH THE LANDING GEAR IN THE DOWN AND LOCKED POSITIONOct 28, 1997 · N820BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR SRAA971011Wire · brokenDURING PREFLIGHT, NR 9 AND NR 10 SMOKE DETECTOR, WOULD NOT TEST. INSPECTED AND FOUND WIRE BROKEN DURING LOADING. NR 9 SMOKE DETECTOR REPAIRED, OPS CHECK GOOD IAW DC8 MM CH 26.Oct 27, 1997 · N872SJ · Doug DC871F · Smoke DetectionSDR UPS97825319Angle · corrodedINSPECTION TYPE-C, R1 DOOR JAMB CUSP ANGLE CORRODED. REMOVED CORR ANGLE,TRIMMED AND DRILLED NEW ONE IAW DC8 SRM 51-1-24 AND DAC DWG 5615700. ALODINED, PRIMED, INSTALLED IAW DC8 SRM 51-1-8, 51-1-21 AND 51-1-20D AND 51-3-0.Oct 26, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825317Jamb · corrodedINSPECTION TYPE-C, R-1 DOOR JAMB, LOWER FWD AND AFT PANS CORRODED. REMOVED PANS, FABBED -3 AND -5 SEGMENTS IAW DAC DWG NR 5615700. ALODINED PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D.Oct 26, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824836Skin · corrodedINSPECTION TYPE-C, FOUND CORROSION ON BOTTOM OF FUSELAGE SKIN FWD OF DOOR G2 AT STA 1890. REMOVED CORROSION, CUT OUT CORRODED AREA, FABRICATED FILLER AND REPAIR DOUBLER, DRILLED TREATED PRIMED AND INSTALLED IAW DC8 SRM 53-2-0 FIG 1, 51-1-8, 51-1-21.Oct 23, 1997 · N797UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97824772Slide · damagedINSPECTION TYPE-N/A, EMERGENCY ESCAPE SLIDE GIRT BAR HAS BEEN PULLED OUT TO FAR FROM STORAGE AREA AND NEEDS TO BE REPLACED. EMERGENCY SLIDE DEFERRED PER MMOC CONTR NR D-140201. SLIDE REMOVED AND STOWED IN THE BELLY COMPARTMENT 32. COURIER SEATS TAPED REF EOOct 23, 1997 · N701UP · Doug DC871F · Escape SlideSDR IXXA9700153Seat Track · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND SEAT TRACK TO BE CRACKED IN MAIN CARGO COMPARTMENT BETWEEN FUSELAGE STATIONS 240 AND 247, BUTT LINE X-25. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED TRACK, FABRICATION AND INSTALLATION OF NEW SEAT TRACK PLUG IN ACCORDANCEOct 21, 1997 · N829BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA9700152Longeron · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON LONGERON 33 RIGHT, BETWEEN FUSELAGE STATIONS 10 TO 70. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION OF LONGERON SECTION IN ACCORDANCE WITH DER APPROVED DRAWING 853-396-97 AND ENGINEERING OROct 21, 1997 · N829BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA9700151Doubler · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL FINGER DOUBLER BETWEEN FUSELAGE STATIONS 10 TO 70, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW FINGER DOUBLER IN ACCORDANCE WITH DOUOct 21, 1997 · N829BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9700150Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL PLATING AT FUSELAGE STATION 25.5, BETWEEN LONGERONS 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNAL REOct 21, 1997 · N829BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97824988Skin · damagedINSPECTION TYPE-C, FOUND FASTENER ROW LOOSE AND PULLED THROUGH SKIN AT RT WING LEADING EDGE ABOVE NR 4 PYLON APPROX XS 493 TO 503. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW REA 97762 AND DACO ROD SKETCH 97-10-29-003.Oct 20, 1997 · N797UP · Doug DC871F · Wing, Plate/SkinSDR UPS97824840Clip · corrodedINSPECTION TYPE-C, FOUND CORROSION ON SUPPORT CLIP ON PRESS BULKHEAD STA 8 TO 13, X 38 LT, -Z37. FABRICATED, DRILLED, TREATED AND INSTALLED NEW CLIP IAW DC8 SRM 53-2-0, PAGE 1, PAR 3, 51-1-20D AND 51-1-8.Oct 19, 1997 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97824839Skin · corrosionINSPECTION TYPE-C, FOUND CORROSION ON FUSELAGE SKIN AROUND FASTENER IN LONGERON 35 LEFT AT Y=680. REMOVED CORROSION .003 BEYOND DC8 SRM LIMIT. REMOVAL FOUND ACCEPTABLE PER (A) BCAG FAX MISC-A099/RRR, ATA:8-53-02-03 (B) AEROCORP MACON INC FAX FILE 102197-2/RSOct 19, 1997 · N797UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97824838Skin · crackedINSPECTION TYPE-C, FOUND 2 INCH CRACK AT ATTACH HOLES ON UPPER SURFACE OF LEFT WING CENTER LEADING EDGE AT XFS 285. FABRICATED REPAIR DOUBLER, DRILLED, TREATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0, FIG 2A SHEET 1, 51-1-21, 51-3-0 AND 51-1-8.Oct 17, 1997 · N797UP · Doug DC871F · Wing, Plate/SkinSDR UPS97824837Skin · crackedINSPECTION TYPE-C, FOUND CRACK AT SCREW HOLE ON UPPER SURFACE OF LEFT WING LEADING EDGE AT XOLD 6.2. CUT OUT CRACKED AREA, FABRICATED REPAIR DOUBLER, DRILLED, TREATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D AND 57-2-0 PAGE 10A.Oct 17, 1997 · N797UP · Doug DC871F · Wing, Plate/SkinSDR UPS97824835Lid · crackedINSPECTION TYPE-C, FOUND NR 2 MAIN TANK ACCESS LID 506C HAS CORROSION CRACK AT ATTACH HOLE STA XRS 5. REMOVED CORROSION/CRACK, FABRICATED REPAIR DOUBLER, DRILLED,TRATED, PRIMED AND INSTALLED IAW DC8 SRM 57-2-1 FIG 43, 51-1-8, 51-1-21.Oct 17, 1997 · N797UP · Doug DC871F · Wing, Plate/SkinSDR UPS97825298Shear Tie · crackedINSPECTION TYPE-C, BOTTOM FUSELAGE APPROX STA 710, RT KEEL AREA, SHEAR TIE CRACKED. FABBED SHEAR TIE IAW DC8 SRM 53-2-0 AND 51-1-4. HEAT TREAT IAW DC8 SRM 51-1-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D.Oct 15, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825266Shear Tie · crackedINSPECTION TYPE:C, BOTTOM FUSELAGE APPROX STA 710, RT KEEL AREA, SHEAR TIE CRACKED. FABBED SHEAR TIE IAW DC8 SRM 53-2-0 AND 51-1-4. HEAT TREAT IAW DC8 SRM 51-1-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SR M 51-1-20D.Oct 15, 1997 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825285Web · corrodedINSPECTION TYPE-C/CK, FLOOR WEB CORRODED AT FUSELAGE STATION 70 AFT OF FWD ACCY COMPT AFT BULKHEAD AT FLOOR LINE TOP OF RIGHT HAND FWD LOWER CARGO COMPT STRUT. REMOVED CORROSION IAW DC8 SRM 51-1-8, FABRICATED REPAIR DOUBLER AND FILLER IAW REO 03853 IR. INSTAOct 9, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825257Floor Web · corrodedINSPECTION TYPE:C/CK, FLOOR WEB CORRODED AT FS 70 AFT OF FWD ACCY COMPT AFT BULKHEAD AT FLOOR LINE TOP OF RIGHT FWD LOWER CARGO COMPT STRUT. REMOVED CORROSION IAW DC8 SRM 51-1-8 FABRICATED REPAIR DOUBLER AND FILLER IAW REO 03853 IR INSTALLED IAW REO 03853 IOct 9, 1997 · N702UP · Doug DC871F · Fuselage Floor PanelSDR UPS97825297Fitting · crackedINSPECTION TYPE-C, FS 300, L28L, HAS CRACKED Z-FITTING. REPLACED Z-FITTING, FABBED REPAIR ANGLES IAW DC8 SRM 53-2-0, LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, INSTALLED IAW DC8 SRM 51-1-20D.Oct 8, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825265Fitting · crackedINSPECTION TYPE:C, FS 300, L28L HAS CRACKED Z FITTING. REPLACED Z FITTING. FABBED REPAIR ANGLES IAW DC8-SRM 53-2-0, LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1- 8, AND INSTALLED IAW DC8 SRM 51-1-20D.Oct 8, 1997 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97825195Fitting · crackedINSPECTION TYPE-C/CK, FS 300 LONGERON 28 LEFT HAND HAS CRACKED Z-FITTING. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-24, FABBED REPAIR ANGLES IAW DC8 SRM 53-2-0, INSTALLED REPAIR ANGLES IAW DC8 SRM 51-1-24, INSTALLED FITTING AND ANGLES IAW DC8 SRM 51-1-20D.Oct 8, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9700145Connector · deterioratedEN ROUTE LAX TO TOL, THE NR 4 ENGINE FIRE WARNING SOUNDED AND ILLUMINATED. THE CREW ACCOMPLISHED AN ENGINE SHUTDOWN IN ACCORDANCE WITH COMPANY PROCEDURES. THE FLIGHT CONTINUED TO TOL WITH AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE ENGINE COMPARTMENT WIRINOct 8, 1997 · N825BX · Doug DC871F · Fire DetectionSDR UPS97825322Track · damagedINSPECTION TYPE-C, STA 500 TRACK E DAMAGED. INSTALLED REPAIR BUSHING PER REO 03816.Oct 6, 1997 · N702UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97825299Fitting · crackedINSPECTION TYPE-C, CORNER FITTING CRACKED INSIDE NR 3 ALT TANK AT STA 74, LOWER FRONT SPAR. FITTING FABBED AND TREATED ON TIMCO OPS. 50043. INSTALLED FITTING IAW DC8 SRM 51-1-20D. LK CKECK TO BE PERFORMED ON TC NR 1000-03.Oct 6, 1997 · N702UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS97825286Frame · corrodedINSPECTION TYPE-C/CK, CORROSION ON FWD LOWER FLANGE OF FRAME FUSELAGE STATION 1140 BETWEEN LONGERON 33 RIGHT TO 33 LEFT. REMOVED CORROSION OUT OF LIMITS, RECEIVED REO 03814. REMOVED CAP, FABRICATED NEW CAPS AND GUSSETS IAW TIMCO REO 03814. ALODINED AND PRIMOct 6, 1997 · N702UP · Doug DC871F · Fuselage Main, FrameSDR UPS97825263Fitting · crackedINSPECTION TYPE:C CORNER FITTING CRACKED INSIDE NR 3 ALT TANK AT STA 74, LOWER FRONT SPAR. FITTING FABBED AND TREATED ON TIMCO OPS 50043. INSTALLED FITTING IAW DC8 SRM 51-1-20D LK CHECK TO BE PERFORMED ON TC NR 1000-03.Oct 6, 1997 · N718UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS97825258Frame · corrodedINSPECTION TYPE:C/CK, CORROSION ON FWD LOWER FLANGE OF FRAME FS 1140 BETWEEN LONGERON 33 RT TO 33 LEFT 6. REMOVED CORROSION OUT OF LIMITS RECEIVED REO 03814. REMOVED CAP FABRICATED NEW CAPS AND GUSSETS IAW TIMCO REO 03814 ALODINED NEW CAP AND GUSSET IAW DCOct 6, 1997 · N702UP · Doug DC871F · Fuselage Main, FrameSDR UPS97825191Skin · corrodedINSPECTION TYPE-C/CK, EMPENNAGE SKIN CORRODED JUST FWD OF TAIL SKID. REMOVED AND REPLACED LONGERON 36 STA 1690 TO 1790 IAW DC8 SRM 81-3-0, HOLES ON LONGERON TO BE PICKED UP AND DRILLED ON UPS NR 75 1718 INCLUDE SKIN INSTALLTION.Oct 6, 1997 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97824937Seat Track · brokenINSPECTION TYPE-C/CK, MAIN CARGO STATION 510 TRACK D FLOOR TRACK PIECE BROKEN. REMOVED BROKEN SECTION STA 420 TO 650, FABBED NEW SECTION AND INSTALLED IAW UPS EO DC8 5320 5167C AND DC8 SRM 51-1-8 AND 53-2-3.Oct 5, 1997 · N702UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS97824624Skin · corrodedINSPECTION TYPE-N/A, VISIBLE CORROSION NOTICED LEFT OF CENTER ACCESSORY ACCESS TRANSCRIBED TO SV PACKAGE NON-ROUTINE 724751, TEMPORARY REPAIR INSTALLED IAW UPS EO DC8-5330-9765A. THIS ITEM TO BE MPI'D ON L/P 871216 ITEM NR 3.Oct 5, 1997 · N715UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9700158Pan · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON RIGHT AFT SERVICE DOOR PAN, LOWER AFT CORNER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRAWING 852-386-97 AND ENGINEEROct 5, 1997 · N829BX · Doug DC871F · Service DoorsSDR UPS97825192Fitting · crackedINSPECTION TYPE-C/CK, CRACK IN STRINGER ATTACH FITTING XRS 600 SECOND STRINGER AFT OF C-SPAR. REMOVED CRACK STRINGER END FITTING NEW FITTING FABBED ON TIMCO PRINTED OPERATION 50016, DRILLED AND INSTALLED FITTING IAW DC8 SRM 51-3-2 AND 51-1-20D AND 51-3-0, ALOOct 4, 1997 · N702UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS97824942Fitting · corrodedINSPECTION TYPE-C/CK, FUSELAGE STATION 280 L29L HAS CORRODED Z-FITTING. REMOVED CORRODED Z-FITTING CUT NEW FITTING IAW DC8 SRM 53-2-0 FIG 2 D FABRICATED SPLICES IAW DC8 SRM 53-2-0 FIG 2D LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMEOct 4, 1997 · N702UP · Doug DC871F · Fuselage Miscellaneous Structure
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