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 RRXA991717Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-2 BETWEEN Y=1330 TO Y=1500 AND X=30. 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 APPROVJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991716Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=1300 TO Y=1580. 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 ENGJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991710Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=960 TO Y=1000. 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 ENGJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991706Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=813 TO Y=990. 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 ENGINJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991705Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=760 TO Y=1000 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 APPROVEDJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991704Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=584 TO Y=600. 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 ENGINEERIJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991703Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-2 BETWEEN Y=580 TO Y=435 AND X=24. 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 Jul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991697Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E BETWEEN Y=95 TO Y=110 AND BETWEEN X=-27 TO 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 IAWJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRAX991706Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=880 TO Y=900. 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 ENGINJul 1, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR UPS99830184Fitting · crackedINSPECTION TYPE:C123, THE RT STA 410 FLAP UP STOP FITTING IS CRACKED. REMOVED AND REPLACED STOP FITTING IAW SRM 51-3-0.Jun 30, 1999 · N874UP · Doug DC873F · Trailing Edge FlapsSDR UPS99830159Fitting · crackedINSPECTION TYPE:C2, MAIN CARGO DOOR FTG CRACKED UPPER FWD CORNER NEAR ACTUATOR. INSTALLED NEW FITTING, ACTUATOR SUPPORT AND CORNER FITTING IAW UPS DC8 SRM 51-1-21 & 51-3-0, UPS DCI M/M 52-36-03 & 52-36-01.Jun 30, 1999 · N809UP · Doug DC873F · Cargo/Baggage DoorsSDR RRXA991487Skin · damagedDURING A MAINTENANCE VISIT FOUND LEFT WING OUTBOARD SLOT LEADING EDGE I/B EDGE HAS SCREWS PULLING THROUGH SKIN AND MISSING. 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 Jun 30, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991485Skin · crackDURING A MAINTENANCE VISIT FOUND CRACKS, SKIN, LEFT WING O/B LEADING EDGE I/B SECTIONS LOWER SURFACE AT STA XFS 591.250, 1 TO 4 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLJun 30, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR UPS99830183Skin · corrodedINSPECTION TYPE:C123, RT WING L/E LWR SKIN, AT THE L/E, STA XW 761.75 HAS INTERGRANNULAR CORROSION AROUND 2 SCREWS. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5720-4087B.Jun 29, 1999 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830182Skin · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 422.75 IS CRACKED AT A FASTENER. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087B.Jun 29, 1999 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830181Rib · crackedINSPECTION TYPE:C123, RT WING OTBD SLOT, UPPER OTBD CLOSURE RIB AT XW 453 IS CRACKED AT THE AFT END. REMOVED AND REPLACED RIB IAW SRM 51-1-20D AND 51-3-0.Jun 29, 1999 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830180Skin · crackedINSPECTION TYPE:C123 RT WING L/E UPPER SKIN AT XFS 330, AT THE SPAR, HAS INTERGRANNULAR CORROSION AND IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.Jun 29, 1999 · N874UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830179Skin · crackedINSPECTION TYPE:C123, RT WING L/E UPPER SKIN AT XW 257.5, 33 FWD OF THE SPAR, IS CRACKED BETWEEN 2 FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1.Jun 29, 1999 · N874UP · Doug DC873F · Wing, Plate/SkinSDR RRXA991732Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 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 APPROVJun 29, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991731Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 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 29, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991714Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 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 APPROVJun 29, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991702Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL AT Y=435 BETWEEN X=16 TO X=24. 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 ENJun 29, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991503Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, SEVERAL RIVET HEADS POPPED ON DOUBLER BETWEEN STA -52 TO STA -12, 20 RIGHT CENTER COCKPIT PRESSURE DECK AFT OF F/E TABLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABJun 29, 1999 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991486Skin · gougedDURING A MAINTENANCE VISIT, FOUND TWO SMALL GOUGES, LEFT WING CENTER LEADING EDGE LOWER SURFACE AT STA XS 478.897 AND STA XS 484.895 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALJun 28, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR RRXA991396Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD LAV SVC PANEL WELL AREA, ALSO RUSTED DOME NUTS BETWEEN STA 260 AND STA 280, AND BETWEEN LONGERONS 24 RIGHT AND LONGERON 26 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAWJun 28, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991506Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RT WING, OUTBOARD LEADING EDGE O/B SECTION LWR. SURFACE I/B END, CORROSION CRACK AT STA XFS 710.000 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEDJun 26, 1999 · N791FT · Doug DC873F · Wing, Plate/SkinSDR UPS99829975Doubler · damagedINSPECTION TYPE:C-1, PERMANENT REPAIR TO AIRSTART CUTOUT (D161352) INCIDENT NR R598473 DATE OF OCCURANCE 10/22/98 ORIGINAL INCIDENT. AIRCART PULLED AWAY FROM AIRCRAFT WITH CART STILL CONNECTED. ACCOMPLISHED REPAIR IAW UPS EO DC8-5330-0793 AND UPS DC8 SRM 53-Jun 25, 1999 · N807UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991423Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING O/B L/E I/B SECTION HAS CRACK AT DRIPLESS DRAIN AT STA 597.500. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REINSTALLED RIVET ACCEPTABLE TO RETURN TO SERVICE IAW FAA APPJun 25, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991394Stiffener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT CABIN BETWEEN STA 1745 AND STA 1766 FLOOR SUPPORT CHANNEL CROSS OVER STIFFENER HAS CORROSION EXFOLIATION EMANATING FROM FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAJun 25, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991387Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, LEADING EDGE CENTER SECTION I/B EDGE BETWEEN STA 291.5 TO 297.500, 15 TO 21 INCHES FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED Jun 25, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829954Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD.Jun 24, 1999 · N811UP · Doug DC873F · Emergency LightingSDR UPS99829953Battery Pack · deadEMERGENCY LIGHTS INOP. FOUND EMERGENCY LIGHT SWITCH LEFT ON TURNED SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, OPS CHECK GOOD.Jun 24, 1999 · N811UP · Doug DC873F · Emergency LightingSDR RRXA991700Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 AT Y=360 BETWEEN X=16 TO X=24. 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 DJun 24, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991695Angle · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO DOOR, SEAL ATTACHMENT ANGLE BETWEEN Y=213 TO Y=240. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ATTACHMENT ANGLE AND INSTALLED Jun 24, 1999 · N791FT · Doug DC873F · Cargo/Baggage DoorsSDR RRXA991694Angle · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO DOOR, SEAL ATTACHMENT ANGLE BETWEEN SPOOLS 2 AND 3 AND BETWEEN Y=160 TO Y=180. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ATTAJun 24, 1999 · N791FT · Doug DC873F · Cargo/Baggage DoorsSDR RRXA991418Plenum · crackedDURING A MAINTENANCE VISIT, FOUND RT FWD PLENUM ASSY PRIMARY HEAT EXCHANGER HAS SEVERAL CRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOPPED DRILLED CRACKS, WELDED IAW FAA APPROVED TENNESSEE TECHNICAL SERVIJun 24, 1999 · N604AL · Doug DC873F · Cabin Cooling SystemSDR RRXA991419Door Panel · crackedDURING A MAINTENANCE VISIT, FOUND AFT LOWER CARGO COMPT STA 1540 AFT BULKHEAD DOOR BENT AND CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOOR IAW FAA APPROVED TENNESSEE TECHNICJun 22, 1999 · N604AL · Doug DC873F · Accessory Compartment DoorsSDR RRXA991401Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BLISTER AND CRACK IN FINGER DOUBLER B PIT AT STA 506.000, LONGERON 30 RIGHT LOWER LEG, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CORROSION, CUT OUT DAJun 22, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829979Web · crackedINSPECTION TYPE:C-1, RUDDER STIFFENER INSIDE L/E AT STA ZR 110 IS CRACKED. FABRICATED AND INSTALLED NEW STIFFENER (WEB) IAW DAC DWG 5656229, DC 8 SRM 51-1-20D & 51-1-21.Jun 21, 1999 · N807UP · Doug DC873F · Rudder StructureSDR UPS99829899Battery Pack · dischargedINSPECTION TYPE:PDC, AIRCRAFT EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01, OP CK GOOD.Jun 21, 1999 · N851UP · Doug DC873F · Emergency LightingSDR RRXA991750Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO VERTICAL STABILIZER FRONT SPAR ATTACHMENT ANGLE AT Y=1766 AND X=24. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW Jun 21, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991410Skin · chafedDURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN RIGHT WING CENTER L/E STA 520.168, 30 TO 36 INCHES 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 REPLACEMENT DOJun 21, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829977Web · crackedINSPECTION TYPE:C-1, SUPPORT WEB BENEATH 2ND RUDDER DAMPENER CRACKED IN SEVERAL PLACES STA ZR155. REMOVED AND FABBED NEW 5656229-11 WEB IAW DAC DWG 5656229. REINSTALLED RIB, WEB AND SIDE SKIN IAW DC8 SRM 51-1-21 & 51-1-20D. REINSTALLED L/E SECTION IAW DC8 SJun 20, 1999 · N807UP · Doug DC873F · Rudder StructureSDR RRXA991620Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LEFT O/B AILERON I/B LWR ACCESS PANEL TOP PLATE AT XA 659. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW DC8 SRM 51-3-3. Jun 19, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991095Bulkhead · leakingAT APPROXIMATELY FLT LEVEL 230 CABIN PRESS WENT TO 10,000 FT, LEVEL OFF A FLT 220 TO MAINTAIN CABIN PRESSURIZATION. AIRCRAFT FERRIED TO EDDF FOR REPAIR. AFT PRESURE BULKHEAD REPAIRED PER BOEING ROD SKETCH 99-06-22-001, REF : EWA M/A NR AM-5312-01:00 AND WORKJun 19, 1999 · N870TV · Doug DC873F · Fuselage Main, BulkheadSDR UPS99829978Fitting · crackedINSPECTION TYPE:C-1, STRINGER-51 NR 2 MAIN O/B AT WS 74.00 REAR SPAR HAS FWD FITTING CRACKED. REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D.Jun 18, 1999 · N807UP · Doug DC873F · Wing Miscellaneous StructureSDR RRXA991384Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, POPPED RIVET AND BULGE IN EXTERNAL SKIN, LONGERON FITTING END CORRODED INSIDE FWD ACCESSORY COMPARTMENT AT STA 8, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW Jun 18, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991686Bulkhead · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BULKHEAD MOUNT AT Y=1360 BETWEEN LONGERONS 34 LEFT TO 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED MOUNT, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW MOUNT IAW DCJun 17, 1999 · N791FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA991484Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEFT, APPROX 3-1/2 CRACK BETWEEN BL 35.0 RIGHT AND BL 35.750 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DCJun 17, 1999 · N791FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA991482Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 RIGHT AND LONGERON 11 RIGHT, APPROX 3.75 INCH CRACK BETWEEN BL 33.50 LEFT AND BL 37.00 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAWJun 17, 1999 · N791FT · Doug DC873F · Fuselage Main, Bulkhead
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