Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = '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 DHL2000801138Intercostal · deformedMAIN CARGO COMPT INTERCOSTAL DEFORMED BETWEEN STA 280.000 AND 300.000. REMOVED DEFORMED INTERCOSTAL PER SRM 51-1-21. FABRICATED INTERCOSTAL PER SRM 53-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED INTERCOSTAL PER SRM 53-2-3.May 27, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000801136Fitting · crackedMAIN CARGO COMPT FITTING CRACKED 1 INCH AT STA 104.00. REMOVED AND REPLACED FITTING PER SRM 51-1-20.May 27, 2000 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2000801135Skin · wornRIGHT WING O/B FLAP T/E UPPER SKIN WORN BETWEEN XRS 171.000 AND 177.000. REMOVED T/E PER SRM 51-1-21. FABRICATED T/E PER SRM 57-2-1. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW T/E PER SRM 51-1-21.May 27, 2000 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2000801134Skin · deformedRIGHT O/B TRAILING EDGE FLAP DEFORMED BETWEEN XRS 210.000 AND 215.000. REMOVED DAMAGED TRAILING EDGE PER SRM 51-1-21. FABRICATED T/E PER SRM 57-2-3. TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW TRAILING EDGE PER SRM 51-1-21.May 27, 2000 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2000801128Fitting · crackedRIGHT WING FITTING UPPER PART CRACKED 2 INCHES AT STA XRS 421.000. REMOVED CRACKED FITTING PER SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA PER SRM 51-1-8B. INSTALLED NEW FITTING PER SRM 51-1-20D.May 27, 2000 · N801DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2000801127Angle · crackedRT WING I/B FLAP LOWER INTERNAL ANGLE CRACKED .5 INCH AT XW 132.0. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED REINFORCING ANGLE PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PER SRM 57-2-0.May 26, 2000 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080103CSupport Bracket · crackedFWD CARGO COMPT LINNING SUPPORT CRACKED 1 1/2 INCH STA L-27R - L28R.STOP DRILLED PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 53-2-5.May 26, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080102CSupport Bracket · crackedFWD CARGO COMPT LINING SUPPORT CRACKED 1 1/2 IN AND 1/2 INCH STA 220.000 L-28R-L-29R. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED PER SRM 53-2-5.FABRICATED DOUBLER PER SRM 53-2-5.PRIMED PER SRM 51-1-8.INSTALLED DOUBLER PER SRM 51-1-21.May 26, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080601Engine · failedENGINE FAILURE NR 2 AFTER TAKEOFF AT 5,000 FEET CLIMBING. REPLACED NR 2 ENGINE PER DHL DC-8 TASK M/M 71-00-01 AND 71-00-02, OPS CHECK NORMAL.May 26, 2000 · N806DH · Doug DC873F · Engine (Turbine/Turboprop)SDR RRXA003450Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER 'A' BIN CROSSSLIDE DOOR BILGE AREA AT FS 280-360, X54-X30, Z-34 TO -50 AND L27L TO L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.May 25, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2000801143Web · crackedFUSELAGE LOWER EXTERIOR WEB LIGHTENING HOLE SHOWS 1 INCH CRACK AT FS 810.000. STOP DRILLED CRACK PER SRM 53-2-0. FABRICATED DOUBLER PER SRM 53-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 53-2-0.May 25, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080104CSupport Bracket · crackedFWD CARGO COMPT LINING SUPPORT CRACKED 3/4 INCH AT STA.160.00 L-34L TO L35 LT. REMOVED FASTNERS PER SRM 51-1-21. STOP DRILLED CRACK PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-1-21.May 25, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832706Angle · corrodedINSPECTION TYPE:C2, ''Z'' ANGLE CORRODED AND MISDRILLED AND HAS LOOSE RIVETS BETWEEN STA 25 AND 8 AND 10 RBL. REMOVED DAMAGED ''Z'' ANGLE, FABBED NEW ''Z'' ANGLE IAW DC8 DWG 54616573 & REO G07339. INSTALLED IAW DC8 SRM 51-1-20D.May 25, 2000 · N894UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080502Actuator · failedAIRCRAFT OSCILATING AROUND VERT AXIS DURING FLT, BEGAN DURING ACCELERATION ACCOMPANIED BY LOUD NOISE (WIND). FOUND RIGHT I/B FLAP ACTUATOR BROKEN. REMOVED AND REPLACED FLAP ACTUATOR PER DC-8 M/M 27-51-10. LEAK CHECK AND OPS CHECK OK PER M/M 27-51-10.May 25, 2000 · N805DH · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA003459Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE BOTTOM OF FUSELAGE WHERE NR 2 ADF ANTENNA IS MOUNTED AT FS 136 TO 160 AND L35L TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.May 24, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003458Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATC TRANSPONDER ANTENNA PLATE AND RING AT FS370.5 TO 379.5 AND L35.8L TO 35.8R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PARTS ANDMay 24, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003457Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BOTTOM SIDE OF FUSELAGE WHERE NR 1 ADF ANTENNA MOUNTS AT FS X360 TO 380, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTMay 24, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2000801107Rib · crackedLEFT WING LEADING EDGE RIB CRACKED .5 INCH. STOP DRILLED CRACK PER SRM 57-2-0 PG 12. FABRICATED DOUBLER (ALCLADE 2024.T3.0.50) PER SRM 57-2-0 PG 12. CLEANED, TREATED AND PRIMED PER SRM 51-1-8 B PG 1 & 2. INSTALLED DOUBLER PER SRM 57-2-0 PG 12.May 24, 2000 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR RRXA003456Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT THE AFT LWR BAG BIN AT CROSSSLIDE BILGE AREA AT STA 1214 TO 1220, X6 TO -6 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WIMay 23, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003455Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT PIT INTERCOSTAL STR 31L O/B FACE BETWEEN STA'S 1340-1360 , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WITHIN LIMITS.May 23, 2000 · N796FT · Doug DC873F · Fuselage Main, StructureSDR RRXA003454Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT PIT LOWER CAP OF FRAME FWD AT FS 1020-1040 AND STR 35R-35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DCMay 23, 2000 · N796FT · Doug DC873F · Fuselage Main, FrameSDR DHL2000801111Rib · crackedLEFT WING LEADING EDGE RIB CRACKED .25 INCH AT STA XFS 631.000. STOP DRILLED PER SRM 57-2-0. FABRICATED DOUBLER PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 57-2-0.May 23, 2000 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2000801109Rib · crackedLEFT WING LEADING EDGE RIB CRACKED .25 INCH AT STA XFS 608.000. STOP DRILLED PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 57-2-0.May 23, 2000 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2000801106Rib · crackedLT WING LEADING EDGE RIB CRACKED 3/4 INCH, STA XFS 603. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER WITH ALCLADE 2024-T3 0.050 PER SRM 57-2-0.CLEANED TREATED AND PRIMED PER SRM 51-1-8B PAGE 1&2.INSTALLED DOUBLER ON INBD AREA PER SRM 57-2-0May 23, 2000 · N801DH · Doug DC873F · Leading Edge DevicesSDR RRXA003453Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER PORTION OF FLOOR BEAM AT STA 920, X-48 TO -53 AND Z-4 TO -7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED.May 22, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2000801144Seat Track · wornF/E SEAT TRACK WORN (AFT). REMOVED WORN TRACK PER SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA PER SRM 51-1-8B. INSTALLED NEW SEAT TRACK PER SRM 51-3-0.May 22, 2000 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832726Skin · crackedINSPECTION TYPE:C2, C-PIT DOOR LOWER CENTER SKIN CRACKED AND PEELED BACK. REMOVED DAMAGED AREA, FLATTENED OUT BEND. FABRICATED DOUBLER, ALODINED AND PRIMED THE SKIN AND THE DOUBLER, APPLIED SEALANT AND INSTALLED THE DOUBLER USING HI-LOK''S AND A CHERRY MAX.May 22, 2000 · N894UP · Doug DC873F · Cargo/Baggage DoorsSDR RRXA003416Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON STRINGER AND PNEUMATIC DUCT SUPPORT AT STA 25 TO 35, STR 25R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. MATERIAL LOSS WAS WITHIN LIMITS IAW DC-8 SRM 53-2-0May 21, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS00832725Skin · corrodedINSPECTION TYPE:C2, RT FUSELAGE EXTERNAL SKIN AT STA 902 HAS INTERGRANULAR CORROSION BELOW CUSP LINE ADJACENT TO SKIN SPLICE. BLENDED OUT AREA IAW REO-G07351. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. INSTALLED FAST IAW DAC DWG 5750554 & DC8 SRM 51-1-20D & 5May 21, 2000 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2000801117Cargo Track · wornMAIN CARGO COMPT 1 LT TRACK LUGS WORN AT STA 680.0. CUT OUT DAMAGED AREA PER SRM 53-2-3. FABRICATED CHANNEL AND PLUG PER SRM 53-2-3. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED CHANNEL AND PLUG PER SRM 53-2-3.May 20, 2000 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003449Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INNER SKIN AT STA 30 AND STR 27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. MATERIAL LOSS WITHIN LIMITS. (CORRMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003448Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LWR SIDE OF FLOOR AT STA 25-55 AND LBL 51, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-3-0.May 19, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR RRXA003447Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD AND AFT END OF STRINGER REPAIR AT STA 35-55 AND STR 26R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003446Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD UPPER FLANGE OF FLOOR BEAM AND LOWER SIDE OF FLOOR AT STA 45-55 AND LBL15-30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. MATERIAL LOSS WIMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003445Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD UPPER FLANGE OF FLOOR BEAM AND LOWER SIDE OF FLOOR AT STA 55-57 AND LBL10 TO RBL10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003444Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER 25R AND PNEUMATIC DUCT SUPPORT AT STA 25 TO 35 AND STR 25R, DAMAGE EXCEEDEDN LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WITHIN LIMITS.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003443Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER 31R AT STA 660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WITHIN LIMITS.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003442Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AT FS 655-657 AND BETWEEN L27R-28R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE FOUND TO BE WITHIN LIMITS.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003440Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BOTTOM O/B ANGLE INSIDE VERTICAL STAB BELOW ANTENNA COUPLER AT FS Z306.670, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. CORROSION DAMAGE WITHIMay 19, 2000 · N796FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003439Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT THE ANTENNA MOUNT AFT OF ACCESSORY COMPT DOOR AT FS 666.250 TO 678.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003438Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE #1 DME ANTENNA PLATE AND RING AT STA 76-85 AND L35.6R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. DAMAGE FOUND TMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003437Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BOTTOM SIDE OF FUSELAGE AT NR 1 DME ANTENNA MOUNT AFT OF NLG JACK POINTAT STA 80-85 AND L35.6R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. COMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003436Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LWR SIDE OF FLOOR AT STA 35 TO 40 AND RBL 35 TO 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SMay 19, 2000 · N796FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003441Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING BELOW NR 4 FLIGHT SPOILER WEB AT STA XRS 140-162, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SMay 18, 2000 · N796FT · Doug DC873F · Wing, Plate/SkinSDR DHL200080301Engine · failedAT FLT LEVEL 390 AT LEVEL OFF, NR 3 ENG FAILED, LESS THAN 2 MINS LATER NR 4 ENG FAILED. ALL ENG PARAMETERS PRIOR TO ENG FAIL WERE NORMAL. ENG''S RESTARTED BELOW F/L 220 AND PERFORMED NORMALLY. REMOVED AND REPLACED FUEL FILTERS ON ENG 3 AND 4 AS PRECAUTION, May 18, 2000 · N803DH · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS00832709Seat Track · corrodedINSPECTION TYPE:C2, SEAT TRACK ''I'' CORRODED ON BOTTOM SIDE, STA 1380 - 1540. REMOVED SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. FABRICATED AND INSTALLED NEW SEAT TRACK AT STA 1380 - 1540 WITH TWO SPLICES PER UPS EO REF DC8 5320-5167 AND DC8 May 14, 2000 · N894UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000296Harness · corrodedNR 1 ENGINE INFLIGHT SHUT DOWN DUE TO ERRATIC -OFF SCALE EGT INDICATION FOR BOTH ANALOG AND DIGITAL EGT READOUT. TESTED NR 1 EGT SYSTEM IAW M/M 77-20-4, FOUND ALL TO BE WITHIN LIMITS. USED WHEATSTONE BRIDGE (TT1000A) TEST BOX TO VERIFY EGT GAUGE AND EGT HARNMay 14, 2000 · N961R · Doug DC873F · Engine EGT/TIT Indicating SystemSDR UPS00832752Fitting · crackedINSPECTION TYPE:C123, STA 1120 FRAME TO CUSP FITTING IS CRACKED AT LONG 21L. REMOVED AND REPLACED FITTING IAW DWG 9755584 AND SRM 51-1-20D.May 13, 2000 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832723Seat Track · corrodedINSPECTION TYPE:C2, SEAT TRACK B AT STA 1060 - 1330 HAS CORROSION UNDER O/B FLANGE. REMOVED CORROSION IAW DC8 SRM 53-2-0, FOUND OUT OF LIMITS. REMOVED DAMAGED SECTION OF TRACK, LOCATED AND DRILLED NEW SECTION IAW DC8 SRM 51-1-24. FABBED SPLICES IAW UPS EO 5May 13, 2000 · N894UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832703Door Frame · crackedINSPECTION TYPE:C2, AFT PIT C-3 DOOR AFT FRAME SECTION CRACKED. REMOVED SEAL RETAINER FOR FOM, FABRICATED REPAIR ANGLES IAW DC8 SRM 52- 2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES IAW DC8 SRM 52-2-0, INSTALLED HIGH-SHEAR FASTENERS IAMay 13, 2000 · N894UP · Doug DC873F · Fuselage Main, Structure
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