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 UPS03840078Fitting · corrodedINSPECTION TYPE: C-2, AFT PIT DOOR SLIDE AREA STA 1210 BETWEEN LONG 31R-32R END FITTING CORRODED. REMOVED EXISTING FITTINGS, LOCATED, DRILLED AND DEBURRED NEW FITTINGS P/N 3754930-1N, 5894282-501, & 5894282-502 IAW DC8 SRM 51-3-2 AND INSTALLED FITTINGS IAW DJan 16, 2003 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003804525Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 628.758. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED AJan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804524Frame · crackedLT OUTER WING L/E FORMER UPPER PART HAS 1 IN CRACK AT STA XFS 778.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 5Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804523Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 616.250 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804522Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 641.250. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGJan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804521Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 622.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLEDJan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804520Frame · crackedLT OUTER WING L/E FORMER UPPER PART HAS A 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804519Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN STA XFS 653.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLJan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804516Frame · crackedLT WING I/B L/E FORMER CRACKED 1 IN AT XFS 610.000 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804515Frame · crackedLT OUTER WING L/E FORMER LOWER PART WITH 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804513Frame · crackedLT OUTER WING L/E FORMER UPPER PART WITH A 1 IN CRACK AT STA XFS 785.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804512Frame · crackedLT OUTER WING L/E FORMER UPPER PART WITH 1 IN CRACK AT STA XFS 760.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804509Frame · crackedLT OUTER WING L/E FORMER UPPER PART CRACKED 1 IN AT STA XFS. 722.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804507Frame · crackedLT OUTER WING L/E FORMER UPPER PART HAS A 1 INCH CRACK AT STA XFS 772.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024 T3 AL 0.032) PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804501Frame · crackedLT OUTER WING L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 766.500. REMOVED FASTENERS PER SRC2 PG 1. STOP DRILLED CRACK PER SRM 57-20 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-Jan 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR IXXA0300005OSwitch · failedAFTER DEPARTURE FROM BFI DURING GEAR RETRACTION CREW NOTED RIGHT HAND MAIN LANDING GEAR DOOR WARNING LIGHT ILLUMINATED. DURING GEAR RECYCLE IT WAS ADDITIONALLY NOTED THAT THE RIGHT HAND MAIN LANDING GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. UPON COMPLETJan 15, 2003 · N606AL · Doug DC873F · Main Landing GearSDR UPS03840074Frame · corrodedINSPECTION TYPE: C-2, FWD CARGO PIT FUSELAGE FRAME LOWER FLANGE CORRODED STA 500 L34L-L35R. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-4-1. FABRICATED -5 & -7 REPAIR PARTS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FJan 14, 2003 · N868UP · Doug DC873F · Fuselage Main, StructureSDR UPS03840013Battery Pack · dischargedEMERGENCY LIGHTS INOP ON PREFLIGHT. C/BS OUT AND SWITCH IN OFF POSITION AFTER WEEKEND. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK OK.Jan 13, 2003 · N803UP · Doug DC873F · Emergency LightingSDR DHL2003804505Frame · crackedRT WING CENTER L/E FORMER UPPER PART CRACKED 1 INCH AT XFS 483.750. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024.T3AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51Jan 12, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804504Frame · crackedLT WING CTR L/E FORMER PART WITH 2 INCH CRACK AT STA XFS 521.250. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED DOUBLER ANGLE (2024.T3 AL 0.063) PER SRM PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10.Jan 10, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003801001Switch1) DOORS NOT LATCHED LIGHT ILLUMINATED. LEFT DOOR UNSAFE LIGHT ILLUMINATED. PERFORMED "GEAR OR DOOR NOT LATCHED LIGHT ILLUMINATED" ABNORMAL PROCEDURE LIGHTS REMAINED ILLUMINATED.2) REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR SWITCH. OPS CHECKED GOOD PERJan 10, 2003 · N801DH · Doug DC873F · Landing Gear Position and WarningSDR DHL2003807002Door Seal1) IN CRUISE AT FL370 A SUDDEN POP AND THE SOUND OF RUSHING AIR WAS HEARD. THE CABIN BEGAN A SLOW CLIMB OF 100 FPM. WE DESCENDED TO FL290 AND THE CABIN PRESSURE STABILIZED AND THE SOUND OF LEAKING AIR STOPPED.2) FOUND SECTION OF LINE FWD CARGO DOOR SEAL NOT Jan 10, 2003 · N807DH · Doug DC873F · Cabin Pressure Control SystemSDR DHL2003807001Windshield1) F/O'S WINDSHIELD EMITS FREQUENT, BUT INTERMITTENT ELECTRICAL DISCHARGES ON THE INTERIOR OF WINDSHIELD. THIS ARCING CAN BE SEEN MOSTLY AT THE TOP AND BOTTOM OF WINDSHIELD WHERE IT MEETS THE WINDOW FRAME.2) REF. ITEM 3P THIS LOG PAGE (#312079) FOR CORRECTIVJan 10, 2003 · N807DH · Doug DC873F · Flight Compartment WindowsSDR DHL2003806002Windshield · crackedFIRST OFFICER WINDSHIELD CRACKED AT DEPARTURE TIME. DEFERRING F/O'S WINDSHIELD PER GMM 3.5 CAT I; IAW DC-8 M/M TEMP. REMOVED AND REPLACED FO'S WINDSHIELD IAW DC-8 M/M 56-10-2. OPERATIONAL CHECK SERVICEABLE. THIS CLEARS DMI #11530E. REF. DMI #11531 (DUJan 9, 2003 · N806DH · Doug DC873F · Flight Compartment WindowsSDR UPS03840079Seat Track · corrodedINSPECTION TYPE: C-2, SEAT TRACK FOUND CORRODED AT STA 1580 TRACK -H- UNDER SIDE. REMOVED DAMAGED SEAT TRACK, REPLACED PER DC8 SRM 53-2-3 AND 51-3-0.Jan 7, 2003 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840020Seat Track · corrodedINSPECTION TYPE:C-2 SEAT TRACK -D- FROM STA 1020 TO 1060 CORRODED ON UNDERSIDE AT CLIP NUTS. REMOVED DAMAGED TRACK, REPLACED WITH NEW TRACK AND UPS SPLICES.Jan 7, 2003 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806514Cargo Track · wornMAIN CARGO COMPT NR 1 FLOOR TRACK LUG WORN AT STA 290.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED PLUG AND CHANNEL IAW SRM 51-3-0 PG 1, SRM 53-2-3 PG 17.Jan 6, 2003 · N806DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004806518Rib · crackedLEFT WING OUTBOARD L/E FORMER UPPER PART CRACKED 0.500, STA XFS 772.500. PERFORMED STOP HOLE ON CRACK END IAW SRM 57-2-0 PG 9,10. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9,10. Jan 4, 2003 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003805001Lamp1) DURING PREFLIGHT #12 SMOKE DETECTOR DOES NOT PRESS TO TEST.2) ITEM TRANSFERRED TO DMI LOG PER 26-6-1 DMI #11487 PLACARD INSTALLED.3) DMI #11487 DURING PREFLIGHT #12 SMOKE DETECTOR DOES NOT PRESS TO TEST.4) REMOVED AND REPLACED LAMPS TO #12 SMOKE DETECTOJan 4, 2003 · N805DH · Doug DC873F · Smoke DetectionSDR UPS03840004Longeron · crackedINSPECTION TYPE: C2, AT STA 1540 STR 24L CRACK INSIDE OF HAT SECTION OF STRINGER AFT PIT. REMOVED DAMAGED SECTION OF LONG IAW DC8 SRM 53-2-2,TR 53-153. FAB NEW SECTION OF LONG FROM EXT S141597 IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, DRIJan 3, 2003 · N868UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA0300002OSocket · looseDURING CLIMB FROM DFW CREW NOTED LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED. THE GEAR WAS CYCLED AND AN UPLATCH CHECK PERFORMED. THE UPLATCH CHECK INDICATED THE GEAR SAFELY STOWED BUT LIGHT REMAINED ILLUMINATED. CREW CONTINUED TO LRD FOR AN UNEVENTFUL Jan 3, 2003 · N606AL · Doug DC873F · Landing Gear Position and WarningSDR UPS03839998Regulator · bypassing2ND OBSERVER O2 REGULATOR BY-PASSING AIR IN FLIGHT, LOST O2 EMERGENCY SYSTEM. FOUND FIRST OBSERVERS SUPPLY LINE TO REGULATOR LEAKING AT FITTING, DAMAGED. THIS FITTING WAS DAMAGED AT TEE FITTING BEHIND 2ND OBSERVERS REGULATOR. REMOVED AND REPLACED SUPPLY HOSJan 3, 2003 · N806UP · Doug DC873F · Crew Oxygen SystemSDR DHL2003804001Smoke Detector · will not testNR 4 SMOKE DETECTOR DOES NOT TEST. ITEM TRANSFERRED TO DMI LOG PER 26-6-1. DMI 11469, PLACARD INSTALLED.Jan 3, 2003 · N804DH · Doug DC873F · Smoke DetectionSDR UPS03839996Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS TEST INOP. REPLACED EMERGENCY LIGHTS BATTERY AND RELAY PACK PER MM 33-50-01.Jan 2, 2003 · N813UP · Doug DC873F · Emergency LightingSDR DHL2003806001Control Panel · sparksON THE TAXI WAY JUST PRIOR TO T/O A/C EXPERIENCED SPARKS AND SMOKE FROM OVERHEAD PANEL. EXECUTED EMERGENCY PROCEDURE AND RETURNED TO BLOCKS.Jan 2, 2003 · N806DH · Doug DC873F · Electrical Power System WiringSDR UPS03840087Seat Track · gougedINSPECTION TYPE: C-2, MAIN CABIN SEAT TRACK -E- GOUGED AT FS 220. REMOVED DAMAGE SEAT TRACK, REPLACED WITH NEW TRACK AND UPS SPLICES IAW UPS EO DC8-5320-5167-C & DC8 SRM 53-2-3.Dec 31, 2002 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840086Seat Track · wornINSPECTION TYPE: C-2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK -D- STA 1219 SCOLLOPS WORN. REMOVED AND REPLACED TRACK SECTION AND SPLICED PER UPS EO DC8-5320-5 167-C.Dec 31, 2002 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840077Angle · corrodedINSPECTION TYPE: C-2, AFT FUSELAGE SECTION STA 1690 PRODUCTION RING IS CORRODED BETWEEN L2 6L-L28L. REMOVED AND REPLACED SPLICES AND RING ANGLE SECTION AT L26R, L26L, L34L, & L28R DUE TO CRACKED AND CORRODED IAW DC8 SRM 53-2-5 FIG 8C-1 SHT 1, 51-1-20D, & DACDec 31, 2002 · N868UP · Doug DC873F · Fuselage Main, StructureSDR UPS03840075Seat Track · wornINSPECTION TYPE: C-2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK -E- STA 596 WORN. REMOVED AND REPLACED TRACK SECTION IAW DC8 EO-5320-5167-C.Dec 31, 2002 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840001Seat Track · wornINSPECTION TYPE: C2, MAIN CABIN BEAR TRAP LOCATION SEAT TRACK F STA 774 HAS WORN SCALLOPS. BLENDED SCALLOP AND FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGE AREA IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PLUG AND CHANNDec 31, 2002 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0200158OSwitch · looseON APPROACH TO SAN CREW NOTICED NOSE LANDING GEAR "GREEN" INDICATING LIGHTS NOT ILLUMINATED. CREW FOLLOWED COMPANY PROCEDURE AND RETURNED TO SAN FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THE NOSE GEAR PROXIMITY SWITCH CONNECTOR HAD BECOME INSECURE. MAINTEDec 31, 2002 · N605AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA02001158OConnector · looseON APPROACH TO SAN CREW NOTICED NOSE LANDING GEAR GREEN INDICATING LIGHTS NOT ILLUMINATED. CREW FOLLOWED COMPANY PROCEDURE AND RETURNED TO SAN FOR AN UNEVENTFUL LANDING. INSPECTION REVEALED THE NOSE GEAR PROXIMITY SWITCH CONNECTOR HAD BECOME INSECURE. MAINTDec 31, 2002 · N605AL · Doug DC873F · Landing Gear Position and WarningSDR UPS03840082Panel · crackedINSPECTION TYPE: C-2, R2 AFT SERVICE DOOR HAS CRACK INDICATION AT LOWER AFT CORNER FOUND BY RADIOGRAPHIC INSPECTION. REMOVED AND ROUTED OUT CRACK IN DOOR PAN. FABBED REPAIR IAW DC8 SRM 53-2-0 AND DAC DWG 5772789. REINSTALLED DOOR PAN STOPS, AND GUIDES IAW Dec 30, 2002 · N868UP · Doug DC873F · Service DoorsSDR UPS03840003Seat Track · wornINSPECTION TYPE: C2, SEAT TRACK WORN FS 710 LBL 50 DOT EO314. BLENDED AREA AND FOUND OUT OF LIMITS AT FS 685 AND 690. ROUTED OUT DAMAGE IAW DC8 SRM 53-2-3. ALODINED, PRIMED AND INSTALLED PLUG IAW DC8 SRM 53-2-3.Dec 30, 2002 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840002Seat Track · gougedINSPECTION TYPE: C2, MAIN CABIN SEAT TRACK G GOUGED AT FS 280. DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGE SCOLLOPS IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LOCATED PART IAW DC8 SRM 53-2-3. INSTALLED PART IAW DDec 30, 2002 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840084Fitting · corrodedINSPECTION TYPE: C-2, ALC STA 1400 L33R FITTING UNDER TORQUE BOX WEB CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.Dec 29, 2002 · N868UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS03840073Frame · gougedINSPECTION TYPE: C-2, INT CABIN CANTED FRAME AFT OF 1710 FRAME DEEP CHAFE ON TRIPLER LONG 29L. INSTALLED DOUBLER ON FRAME IAW UPS DWG DC8-53A-011 AND EO DC8-5310-1 1728-A.Dec 29, 2002 · N868UP · Doug DC873F · Fuselage Main, FrameSDR UPS03840017Fitting · corrodedINSPECTION TYPE: C2, ALL STA 1400 L30R FITTING UNDER TORQUE BOX WEB CORRODED. REMOVEED CORRODED FITTING IAW DC8 SRM 51-1-21. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.Dec 29, 2002 · N868UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS03840085Seat Track · corrodedINSPECTION TYPE: C-2, AFT PIT SEAT TRACK CORRODED AROUND CLIPNUTS. NUT PLATES IN SEVERAL ARE AS STA 980 TO 1260. REMOVED DAMAGE SEAT TRACK. INSTALLED NEW TRACK AND UPS SPLICE PARTS IAW DC8 SRM 51-3-0.Dec 28, 2002 · N868UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840081Skin · corrodedINSPECTION TYPE: C-2, LOWER EXTERIOR FUSELAGE AT STA 1690 BOTTOM AREA SKIN SIGN OF BULGING. CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0, REMOVED DAMAGED SKIN, FABBED NEW SKIN SECTION IAW DGIS DWG 5649329. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED NEW Dec 28, 2002 · N868UP · Doug DC873F · Fuselage Main, Plate/Skin
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