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 UPS03841165Fitting · crackedINSPECTION TYPE: C2, LT HORIZONTAL STAB O/B TIP INTERNAL REAR SPAR ANGLE FITTING IS CRACKED AT XE 312.5 REMOVED,FABRICATED AND REPLACED FITTING I.A.W. DWG. 5640789 AND SRM 51-1-20D,51-3-0,AND DWG. 4651609Aug 26, 2003 · N809UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS03841158Skin · crackedINSPECTION TYPE: C2, RT WING L/E SKIN IS CRACKED AT LOWER SURFACE XFS 304. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX C.Aug 26, 2003 · N809UP · Doug DC873F · Leading Edge DevicesSDR DHL2003805579Skin · corrodedRIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING CORRODED, AROUND STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND Aug 25, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805577Skin · damagedLEFT WING OTBD FLAP UPPER PLATING HAS INTERIM REPAIR AROUND STA XF 225.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGAug 25, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805576Skin · damagedLEFT WING OTBD FLAP UPPER SKIN SHOWS INTERIM REPAIR AROUND XF 345.000 TO STA XF 354.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8Aug 25, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805572Frame · crackedFWD ACCY COMPT FRAME CRACKED 3.000 AT STA 55.000, L-25R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. TRIMMED OUT CRACKED FRAME SEGMENT IAW SRM 53-2-0 FIG 2. FABRICATED FRAME SEGMENAug 25, 2003 · N805DH · Doug DC873F · Fuselage Main, FrameSDR UPS03841244Skin · crackedINSPECTION TYPE: C2, WHILE ACCOMPLISHING WORK TASK AND REMOVAL OF SHUTTER BOX ON NR 687218. FOUND LOWER AFT SKIN CUT OUT CRACKED. C/W EO DC-8-5330-4732D, HFEC IAW NDBDM 06-10-01.0001, NO CRACKS AROUND CUT OUT,FABBED FILLER AND DOUBLER FROM 2024T3 .100 TREAAug 25, 2003 · N809UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841157Rib · crackedINSPECTION TYPE: C2, LEFT HORIZONTAL STAB. LE. RIB IS CRACKED AT XFS 47.5 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2Aug 25, 2003 · N809UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS03841204Skin · nickedINSPECTION TYPE: C2, DEEP NICKS ON FUSELAGE SKIN AT STATION 520 LONGERON 25R, BLENDED OUT NICKS, FOUND OUT OF LIMITS, NDT VERIFIED NO CRACKS AT BLENDOUT AREAS. FABRICATED AND INSTALLED REPAIR DOUBLERS AT B-PIT UPPER FORWARD DOOR CORNER I.A.W. SRM. 53-2-0Aug 25, 2003 · N809UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841202Skin · corrodedINSPECTION TYPE: C2, RT WING LE UPPER SURFACE HAS 6 CRACKED FASTENER HOLES BETWEEN XFS 597.5 TO XFS 628.75. BLENDED OUT CORRODED AREAS, CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLER AND FILLERS I.A.W SRM. 57-2-1 FIG. Aug 25, 2003 · N809UP · Doug DC873F · Wing, Plate/SkinSDR UPS03841198Fitting · crackedINSPECTION TYPE: C1, AFT ACCY COMPT. FS 1660 FLOORBEAM END FITTING AT RBL 48 IS CRACKED. HFEC IAW DC8 NDT SPM 06-10-01.001 NOTED TO BE CRACKED. RECEIVED, LOCATE D, AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLEAug 25, 2003 · N801UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03841163Rib · crackedINSPECTION TYPE: C2, RT HORIZONTAL STAB. LEADING EDGE RIB IS CRACKED AT XFS 116.25 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATED CRACK,FABRICATED AND INSTALLED REPAIR ANGLES I.A.W. SRM. 55-2-0 FIG. 2Aug 25, 2003 · N809UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS03841161Skin · lightning strikeINSPECTION TYPE: C2, 1 EA LIGHTNING STRIKE IS OUT OF LIMITS AT STA -95 4 INCHES ABOVE LONG 20L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.Aug 25, 2003 · N809UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03841160Rib · crackedINSPECTION TYPE: C2, RT WING L/E LOWER RIBS ARE CRACKED AT XFS 616.25 AND XFS 622.5. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Aug 25, 2003 · N809UP · Doug DC873F · Leading Edge DevicesSDR UPS03841159Rib · crackedINSPECTION TYPE: C2, RT WING L/E LOWER RIB IS CRACKED AT XFS 772.5. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Aug 25, 2003 · N809UP · Doug DC873F · Leading Edge DevicesSDR DHL2003805584Skin · corrodedRIGHT OUTER WING INBD EXTENDED L/E OUTER PLATING HAS CORROSION AROUND STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PAug 24, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805578Skin · damagedLWR AFT CARGO COMPT FWD DOOR PLATING SHOW INTERIM REPAIR BETWEEN STA 1200.000 AND 1260.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS THE EXISTING SEGMENT AND SPLICE REPAIR. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICAug 23, 2003 · N805DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL2003805581Skin · corrodedLEFT OUTER WING INBD EXTENDED L/E OUTER PLATING CORRODED AROUND STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA IAW DHL-EDT66-3, DHL-DWGT66-R03. PERFORMED NDT INSPECTIAug 23, 2003 · N805DH · Doug DC873F · Leading Edge DevicesSDR DHL2003805586Skin · corrodedRIGHT OUTER WING INBD EXTENDED L/E SHOWS CORROSION AND ELONGATED HOLES AROUND STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. CUT OUT CORRODED AREA. PERFORMED NDT INSPECTION. FABRICATED Aug 23, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR UPS03841139Acm · defectiveINSPECTION TYPE:N/A WILL NOT MAINTAIN PRESSURIZATION. EMERGENCY DELARED AND REQUESTED IMMEDIATE DESCENT PER EVENT REPORT. FOUND LEFT ACM TEMP UNCONTROLLABLE. R/R'D LEFT ACM PER 21-55-01-4 OPS CHECKS GOOD.Aug 21, 2003 · N868UP · Doug DC873F · Cabin Cooling SystemSDR DHL2003805585Skin · delaminatedLEFT WING FUSELAGE NR 706 UPPER FAIRING SKIN DELAMINATED, STA 912.000 - STA 980.000. REMOVED AND REPLACED LEFT WING TO FUSELAGE UPPER FAIRING NR 706 (STA 912.000 - 980.000) IAW SRM 51-3-0 PG 1.Aug 20, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805574Intercostal · crackedKEEL BEAM LWR SECTION INTERCOSTAL 0.500 CRACKED, STA 940.000. REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-20D PG 21. FABRICATED INTERCOSTAL IAW SRM 53-2-0 PG 1. HEAT TREATED IAW SRM 51-1-1 PG 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED INTERCOAug 20, 2003 · N805DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003805604Shaft · crackedRIGHT OTBD SLOT TORQUE TUBE CRANK CRACKED. REMOVED TORQUE TUBE IAW OHM 27-37-6 PG 2. REMOVED AND REPLACED CRANK ASSY IAW SRM 51-1-21 PG 1. REINSTALLED TORQUE TUBE ON RIGHT OTBD SLOT IAW OHM 27-37-6 PG 2, 3, 4. FOR OPS CHECK SEE N/R 1896.Aug 20, 2003 · N805DH · Doug DC873F · Leading Edge Slat Control SystemSDR IXXA0300056OEngine · fluctuatesDURING CLIMB FROM KTOL TO KBNA THE NR 3 ENGINE EGT BEGAN TO FLUCUATE BOTH ANALOG AND DIGITAL +/- 50 DEGREES C. CREW RETURNED AIRCRAFT TO KTOL AND FLUCUATION CONTINUED THROUGH DESCENT AND LANDING. AIRCRAFT LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS ON GOAug 20, 2003 · N603AL · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS03841174Seat Track · corrodedINSPECTION TYPE: C1, CORROSION AT FASTENER HOLES FOR SEAT TRACK/FLOORBEAM STA 781 LBL 50. REMOVED FASTERNERS IAW DC8 SRM 51-3-0. CUT SEAT TRACK STA 781 TO 845 LT IAW UPS EO DC8 5320-8309. FABBED SPLICE CHANNEL IAW UPS EO DC8- 5320-8309 LOCATED & DRILLED SEATAug 19, 2003 · N801UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03841125Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTING WILL NOT WORK. REMOVED & REPLACED EMERGENCY BATTERY PACK OPS CK GOOD PER MM 33-50-01-2 P/N ON AND OFF SAME 60-1223-5. S/N ON 219 & OFF FTL070.Aug 19, 2003 · N851UP · Doug DC873F · Emergency LightingSDR UPS03841124Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT TEST. R&R EMERGENCY LIGHT BATTERY PACK. P/N ON AND OFF 5708403, S/N ON FLS/ST/7021, S/N OFF CAW250.Aug 19, 2003 · N805UP · Doug DC873F · Emergency LightingSDR DHL2003805527Frame · crackedRIGHT WING OTBD STUB WING FRAME ANGLE DOUBLER CRACKED 2.000 AT STA XW 454.000. REMOVED ANGLE DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (7075-0.071) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. PERFORMED HEAug 18, 2003 · N805DH · Doug DC873F · Wing SparSDR DHL2003805528Frame · wornRIGHT WING OTBD STUB WING L/E FORMER WORN AT XW 454.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 17. INSTALLED ANGLEAug 18, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805603Seat Track · damagedFLIGHT COMPT CAPT'S LEFT AFT SEAT TRACK HOLES ELONGATED. FABRICATED STRAP IAW SRM 53-2- PG 3 OF 3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED STRAP ON FLIGHT COMPT CAPT'S LEFT AFT SEAT TRACK IAW SRM 53-2-3 PG 3 OF 3, SRM 51-1-21 PG 1.Aug 18, 2003 · N805DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003604790Warning System · faultyGPWS FAIL LIGHT ILLUMINATED. REPLACED GPWS MK II WITH GPWS/WS MKVII AND OPS CHECKED GOOD IAW J/C EA34450002-001-D.Aug 18, 2003 · N604AL · Doug DC873F · Ground Proximity SystemSDR DHL2003805514Skin · crackedLEFT WING T/E UPPER SKIN SURFACE 0.500 CRACKED, STA XW 31.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-15 PG 1, Aug 17, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003805532Fitting · crackedFWD CARGO COMPT FITTING ATTACHING CUSP EXTRUSION TO FLOORBEAM WITH TWO CRACKS OF 3.000 AND 1.000 AT STA 340.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACK FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRAug 16, 2003 · N805DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03841197Seat Track · corrodedINSPECTION TYPE: C1, CABIN SEAT TRACK CORRODED STA 822 RBL 48 REMOVED AND REPLACED SEAT TRACK IAW UPS EO DC8-5320-8309. MATERIAL VERIFICATION IS P/N 4755395-2400, NR 00633513, NR 00633514,NR 00633527, 00 633528, PO NR 0841577Aug 16, 2003 · N801UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003805513Frame · crackedLEFT WING CTR L/E FORMER CRACKED (STA XFS 335.250 - XFS 329.000). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. HEAT TREATED IAW SRM 51-1-1 PG 17. Aug 15, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805566Longeron · crackedAFT FUSELAGE SECTION L-17R AT STA 1770.000 CRACKED 3.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED CRACKED L-17R IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED Aug 14, 2003 · N805DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2003805564Longeron · crackedAFT FUSELAGE SECTION L-17L AT STA 1770.000 CRACKED 4.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED L-17L WITH CRACK IN IT IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-21 Aug 14, 2003 · N805DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2003805501Clip · crackedKEEL BEAM LWR SECTION CLIP 0.500 CRACKED, STA 960.000. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG 21. FABRICATED CLIP (EXTRUSION LS4031) IAW SRM 53-2-0 PG 2E, 2F. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CLIP ON KEEL BEAM, STA 960.000 IAW SAug 13, 2003 · N805DH · Doug DC873F · Fuselage Main, KeelSDR DHL2003805504Frame · crackedRIGHT WING CTR L/E FORMER CRACKED 4.000, AT STA XFS 341.500 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER IAW SRM 57-2-0 PG 9-10 (7075-T6 0.040). CLEANED, Aug 13, 2003 · N805DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805503Fitting · crackedRIGHT WING CTR L/E ZEE-PAN CRACKED 8.000 AT STA XS.520.000. REMOVED CRACKED ZEE-PAN FITTING IAW SRM 51-1-20 PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE-PAN FITTING IAW SRM 51-1-20D PG 9.Aug 13, 2003 · N805DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS03841195Floorbeam · corrodedINSPECTION TYPE: C1, MAIN CABIN FS 1620 FLOORBEAM UPPER FLANGE IS CORRODED AT LBL 40. REMOVED CORROSION IAW DC8 SRM 51-1-8. MATERIAL REMAINING .034 ORIG MATERIAL .125 FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR ANGLE AND FILLER IAW DC8 Aug 13, 2003 · N801UP · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2003805505Panel · delaminatedLEFT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XA 450.000 - XA 475.000). REMOVED UPPER PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL ON LT WING T/E, STA XA 450.000 - XA 475.000 IAW SRM 51-3-0 PG 1Aug 12, 2003 · N805DH · Doug DC873F · Wing, Plate/SkinSDR UPS03841194Longeron · crackedINSPECTION TYPE: C1, AFT FUSELAGE TAIL SECTION AT FS 1766-1780 L17L IS CRACKED. REMOVED L17LT TO FOM. LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.Aug 12, 2003 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841193Longeron · crackedINSPECTION TYPE:C1 AFT FUSELAGE TAIL SECTION AT FS 1766-1780 L17R IS CRACKED. REMOVED L17 RT TO FOM LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONGERON AND END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.Aug 12, 2003 · N801UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS03841085Battery Pack · dischargedINSPECTION TYPE:ASV EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, EMERGENCY LIGHTS OPS CHECK NORMAL.Aug 12, 2003 · N807UP · Doug DC873F · Emergency LightingSDR UPS03841076Oil Cap · unsecureINSPECTION TYPE:N/A NR 3 ENGINE SLOW TO RESPOND TO THROTTLE INPUT DURING BOOST TO START NR 2 ENGINE. APPROX 10 MIN INTO FLT OIL QTY DECREASED TO 4 QTS. ENGINE SHUTDOWN ACCOM AT 2 QTS, IAW CHECKLIST. WINDMILL TIME OF APPROX 40 MIN WITH 2-5 PSI. FOUND NR 3 Aug 12, 2003 · N805UP · Doug DC873F · Engine StarterSDR DHL2003805500Channel · crackedNOSE SECTION INTERIOR LEFT TUNNEL CHANNEL CRACKED 2.000, STA 17.000, L32L - L35L. REMOVED CRACKED CHANNEL IAW SRM 51-1-20C AND SRM 51-1-21 PG 1. FABRICATED CHANNEL IAW SRM 51-1-4 PG 1-5, SRM 53-3-3 FIG 2. PERFORMED HEAT TREATMENT TO CHANNEL IAW SRM 51-1-1 PAug 11, 2003 · N805DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003805571Skin · damagedLEFT WING OTBD FLAP LWR SKIN SHOWS INTERIM REPAIR, STA XF 333.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 AND SRM 57-7-1 FIG 4. REMOVED INTERIM REPAIR AND OLD PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 4. CLEAug 11, 2003 · N805DH · Doug DC873F · Trailing Edge FlapsSDR UPS03841192Fitting · crackedINSPECTION TYPE: C1, RT AFT TYPE 1 DOOR HAS A CRACKED FITTING BELOW THE MOST FORWARD LOWER DOOR STOP AT AFT FRAME OF THE FORWARD WEB SECTION REMOVED RT AFT TYPE 1 DOOR. REMOVED FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTINAug 11, 2003 · N801UP · Doug DC873F · Emergency ExitsSDR UPS03841191Fitting · corrodedINSPECTION TYPE: C1, RT FORWARD TYPE 1 DOOR HAS CORROSION INSIDE OF FASTENER HOLE AT AFT LOWER CORNER. REMOVED FITTING IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW DC8 SRM 51 -1-8. MATERIAL LOSS TO 0.00 FROM .185, FOUND BEYOND LIMITS IAW DC8 SRM 52 -2-0 AND DAug 11, 2003 · N801UP · Doug DC873F · Emergency Exits
Back to Douglas DC-8-73F