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 RRXA991106Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 33 RIGHT END TIE FITTING IN FWD ACCESSORY BAY AT STA 8.00. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW FAA APPROVJun 2, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991105Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE, NR 1 LT FLAP WEDGE LOWER SKIN. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCJun 2, 1999 · N606AL · Doug DC873F · Trailing Edge FlapsSDR RRXA991104Flange · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, NR 2 STUB WING, 9.75 LEFT WING NR 2 STUB WING I/B FLANGE. 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 TENNESSJun 2, 1999 · N606AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA991103Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT UPPER CUSP FRAME 560 AT STA 560 ATTACH ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ATTACH ANGLE IAW DC8 SRM 51-1-21 AND 51-1-8. Jun 2, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991102Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 36 BETWEEN STA 1726 AND STA 1745. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR SPLICE IAW DC8 SRM 53-2-1 AND 51-1-21. (CORROSION DAMAJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991101Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, AREA UNDER PANEL 69 LT ELEV INSIDE THROUGHOUT AREA BETWEEN XE 32.937 TO XE 50.000 FWD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED CORROSION IAW FAA APPROVED TJun 2, 1999 · N606AL · Doug DC873F · Elevator, Plate/SkinSDR RRXA991100Skin · wornDURING A MAINTENANCE VISIT FOUND SCREWS MISSING, RIGHT WING, L/E DOUBLER O/B END OF O/B SLOT, MISSING, LOOSE, AND PULLING THROUGH. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991099Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACE AT XFS 193.675. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 57-2-1 AND INSTALLED IAW DC8 SRM 5Jun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991098Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKS, RIGHT WING, L/E JUST FWD O/B SLOT AT STA XFS 503.789 AND STA XFS 491.193. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. CRACKS ACCEPTABLE AS IS PER FAA APPROVED TENNESSEE TECH SERVICES DER ENGINEERING SKETCH NR EO-99-085 WITHJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991097Skin · crackedDURING A MAINTENANCE VISIT FOUND CORROSION AND CRACKS, RIGHT WING, O/B L/E I/B SEGMENT UPPER SURFACE BETWEEN STA XFS 566.250 TO XFS 603.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLEJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991096Skin · crackedDURING A MAINTENANCE VISIT FOUND CORROSION AND CRACKS, RIGHT WING, I/B L/E O/B SEGMENT LOWER SURFACE AT XFS 878.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND FILLER IAW DC8 SRM 57-2-1 ANDJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991093Skin · crackedDURING A MAINTENANCE VISIT FOUND A .25 INCH CRACK, RIGHT WING, EXTENDING FROM SCREW HOLE RIGHT WING O/B L/E I/B SEGMENT O/B EDGE AT STA XFS 710. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991092Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, O/B L/E O/B SEGMENT I/B EDGE AT STA XFS 710. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 57-2-1 AND INSTALLED IAW DJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991091Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN XFS 7.50 AND XFS 26.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 5Jun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991090Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, I/B L/E UPPER SURFACE AT SCREW HOLES BETWEEN XFS 7.50 TO XFS 26.250.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLEJun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991088Skin · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION, RUDDER TUB DELAMINATED LT SIDE AFT OF LOWER HINGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED RUDDER TAB IAW DC8 M/M 27-21-1.Jun 2, 1999 · N606AL · Doug DC873F · Rudder, Plate/SkinSDR RRXA991087Skin · chaffedDURING A MAINTENANCE VISIT FOUND PANEL 86 RUBBING ON FUSELAGE LT SIDE OF LOWER RUDDER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED OUT IAW DC8 SRM 51-1-8, LIMITS ACCEPTABLE PER FAA APPROVED TENNESSEE TECHJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991086Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, O/B L/E O/B SEGMENT LOWER SURFACE AT XFS 878.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW DC8 SRM 51-1-21.Jun 2, 1999 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991085Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LAV SERVICE DOOR FROM HINGE AT STA 80, LONGERON 24 RIGHT, FUSELAGE SKIN UNDER HINGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FAJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991084Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, BOTTOM OF FUSELAGE BEACON ANTENNA FROM BASE AND AROUND SKIN BETWEEN STA 680 AND STA 702. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER ANDJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991083Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM SKIN AT STA 717, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE TECH SERVICES DERJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991082Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTTOM FUSELAGE SKIN AT STA 702, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TENNESSEE TECH SEJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991081Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 360, AFT SIDE ABOVE LONGERONS 31 RIGHT AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IJun 2, 1999 · N606AL · Doug DC873F · Fuselage Main, FrameSDR RRXA991598Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TOP OF WHEEL WELL (MAIN CABIN) AND POPPED RIVET HEADS BETWEEN STA 857 AND STA 878, BETWEEN LEFT BL 64 AND LEFT BL 68 AT WL 9 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW Jun 1, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991383Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, SCREW HOLE LEFT WING I/B L/E UPPER SURFACE AT XFS 38.750 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IJun 1, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991016O Ring · leakingDURING CLIMB-OUT, NR 1 ENG OIL QUANTITY DROPPED TO 4 QTS. OIL PRESS FLUCTUATE AT 30-35 PSI, OIL TEMP 80DEG C. PULLED NR 1 THROTTLE TO IDLE, OIL QUANTITY CONTINUED TO 3QTS AND STEADY. DUMPED FUEL TO MAX LANDING WEIGHT AND RETURNED TO KFLL. UPON INSPECTION FMay 31, 1999 · N603AL · Doug DC873F · Engine Oil Storage (Airframe Furnished)SDR UPS99829691Jamb · damagedINSPECTION TYPE:N/A, LEFT MAIN GEAR DOOR CUTOUT AT REAR SIDE INNER CORNER HAS CURLED SHEET METAL AND A .5 INCH LONG TEAR. *S/D* REPAIRED AREA IAW SRM 51-1-20 AND SRM 53-4 -1.May 28, 1999 · N852UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991127Float Box · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, LEFT WING, NR 1 ALT FLOAT BOX 2.5 CRACK IN WELD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED FLOAT BOX, WELDED CRACK SECTION IAW FAA APPROVED TENNESSEE TECH SERVIMay 28, 1999 · N606AL · Doug DC873F · Fuel StorageSDR RRXA991015O Ring · leakingNR 4 ENG OIL QTY WENT TO ZERO IN FLT, OIL PRESSURE FLUCTUATED FROM 13 TO 20 PSI. SHUT DOWN ENGINE FOR PRECAUTION. WINDMILLING OIL AT 4PS. REMOVED AND REPLACED O-RING ON CAP. SERVICED OIL, 13 QUARTS. NR 4 ENG OPS CHECKS GOOD PER CFM MM 71-00.May 27, 1999 · N831AL · Doug DC873F · Engine Oil Storage (Airframe Furnished)SDR RRXA991014Connector · contaminatedNR 1 AND NR 2 FMS BECAME UNRELIABLE AFTER APPROX 2HRS INTO FLIGHT. NR 1 AND NR 2 FMS INOP, PLACARDED AS SUCH PER MEL 34-37-, CAT D, DMI NR'S NR 1 D7575041-1853 AND NR 2 D7575042-1854, DUE 24 SEP 99 PLACARDS INSTALLED. NR 1 FMS, CLEANED CANNON PLUG ON DADC. OMay 27, 1999 · N796FT · Doug DC873F · Flight Management Computing Hardware SystemSDR RRXA991615Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN BETWEEN STA 35 AND STA 80 AND LONGERON 32 RIGHT, CORROSION BULGE WITH PULLING FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CORROSION IAWMay 26, 1999 · N604AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991614Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BOTH INTER-COSTALS AT STA 1540 DOOR FRAME RIGHT SIDE, BETWEEN BL 16 RIGHT AND BL 32 RIGHT, AND BETWEEN WL 20 RIGHT AND WL 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DMay 26, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991013Seal · leakingLOST HYD FLUID DOWN TO STAND PIPE. FOUND O-RING SEAL LEAKING AT T FITTING ON RUDDER ACCUMULATOR. REMOVED AND REPLACED SEAL, SERVICED HYD SYST. OPS CK GOOD, NO LEAKS NOTED.May 26, 1999 · N796FT · Doug DC873F · Hydraulic Quantity IndicatorSDR RRXA99802Mechanism · lack of lubeAFTER T/O MAIN CARGO DOORS FAILED UPLATCH CK RAN CHECKLIST WITH NO HELP RETURN TO DAY AS PER OPS AND MX CONTROL. PERFORMED OP CK OF MLG DOOR FLT LOCKS, LUBED FLT LOCK, MLG DOOR UPLATCH CK OPS CKS NORMAL AT THIS TIME COULD NOT DUPLICATE ON GROUND NO LEAKS OR DMay 25, 1999 · N961R · Doug DC873F · Landing Gear Door Retract SectionSDR RRXA991012Gps · malfunctionedNR 2 GPS UNRELIABLE. REMOVED AND CLEANED CONTACTS ON NCU AND PERFORMED GROUND CK ON FLT SYST MANAGEMENT.May 25, 1999 · N796FT · Doug DC873F · Global Positioning SystemSDR DHL9980204CFitting · crackedC-CHECK NON-ROUTINE ENG NR 4 RT AT 12 O'CLOCK FWD CORE COWL CLOSE TO PRECOOLER SCOOP AREA HAD CRACK DAMAGE ON SURFACE. THRUST REVERSER RT HALF NR 4 ENG IAW MM. FACILITY S/M WORK REMOVED CRACKED FITTING FROM FWD CORE COWL IAW DC-8 SRM 51-1-21 PAR 5, 51-3-0 PARMay 25, 1999 · N802DH · Doug DC873F · Engine Cowling SystemSDR RRXA991602Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT PRESSURE BULKHEAD AT STA 1766, LONGERON 21 LEFT, HORIZONTAL STIFFENER FLOOR SUPPORT TEES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALMay 24, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991624Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, AFT FUSELAGE, TAIL CONE AROUND ACCESS PANEL 62 INTERIOR FRAME BETWEEN STA 1890 AND STA 1916, AND BETWEEN LONGERONS 34 RIGHT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IMay 23, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA991603Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT CABIN RIGHT FLOOR PANEL SUPPORT BETWEEN STA 1766 AND STA 1745 RIGHT AT NUT PLATES BOTTOM SIDE BL 20 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRMay 23, 1999 · N604AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA991597Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ON FINGER DOUBLER ANGLE BETWEEN STA 960 AND STA 980 -43 LBL, AT WL 10 RIGHT, BELOW NR 2 SEAT TRACK, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLMay 23, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829779Longeron · corrodedINSPECTION TYPE:C1, FWD PIT FS 600 L36 CORRODED. FABBED SPLICE SHIMS IAW TIMCO REO-06533, ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8, INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D AND TIMCO REO-06533.May 22, 1999 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991613Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERIOR AT STA 1690, AFT OF PRODUCTION SPLICE AT LONGERON 31 RIGHT FITTING CRACKED AND CORROSION EXFOLIATION INSIDE FITTING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRMay 22, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991623Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WHEEL WELL ANGLE FITTING TOP OF W/W AT STA 980, BL 46 LEFT AND WL 10 RIGHT, BELOW SEAT TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALMay 21, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991612Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, CENTER L/E UPPER SURFACE (SKIN) AT SCREW HOLE AT XFS 400.00 AT FRONT SPAR ATTACHMENT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILMay 21, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991609Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, RIGHT, O/B L/E SECTION UPPER SURFACE (SKIN) AT XFS 585.000 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IMay 21, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR RRXA991600Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBOARD TIE ENDS, 5 EACH, AT STA 980, BETWEEN LONGERONS 21 LEFT AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED May 21, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980251CSkin · delaminatedC-CHECK, FLAP VANE NR 3 DELAMINATED LEFT WING DOT 38255. REMOVED I/W NR 3 VANE IAW DC-8 27-51-14 ROUTE TO STORES TO BE SENT OUT FOR REPAIR. INSTALLED I/H NR 3 FLAP VANE IAW DC-8 MM 27-51-14 PG 201. PENDING RIG & OPS CHK ACCOMP. RIG & OPS CHK NORMAL IAW DC-May 21, 1999 · N802DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980211CFrame · crackedC-CHECK, UPPER CARGO COMPT AT STA 1600 CIRCUMFERENTIAL FRAME AT CUSP LINE WAS CRACKED RT SIDE. CUT OUT CRACKED SECTION OF FRAME AT FS 1580 RT M CARGO CABIN IAW DC-8 SRM 53-2-0 FIG 2. FABRICATED NEW SECTION OF FRAME: 6 X 2.5 AND 2 SPLICES 10 X 2.5 IAW MHA ENMay 21, 1999 · N802DH · Doug DC873F · Fuselage Main, FrameSDR UPS99829655Slide · misinstalledINSPECTION TYPE:N/A, EMERGENCY SLIDE WOULD NOT CONNECT TO LATCHES, PACKED INCORRECTLY. REPACKED ESCAPE SLIDE, OPS CHECK GOOD.May 20, 1999 · N852UP · Doug DC873F · Emergency EquipmentSDR RRXA991611Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CENTER FLOORBEAM AT AFT PRESSURE BULKHEAD FRAME ATTACHED FASTENERS LOOSE BOTH SIDES ATTACH ANGLE AND CORROSION EMANATING FROM FASTENERS AT STA 1766 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMay 20, 1999 · N604AL · Doug DC873F · Fuselage Main, Floor Beam
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