Douglas DC-8-73F

Service difficulty reports · 15,471

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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"

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SDR UPS06847597Skin · crackedINSPECTION TYPE:C1 LT UPPER WING SKIN CRACKED 1/2" LONG AT STA XCW 69.5 REAR SPAR UPPER SKIN. FABRICATED AND INSTALLED REPAIR -3 FILLER AND -5/-7 DOUBLERS LT UPPER WING SKIN AT XCW 69.5 IAW SRM 57-02-01-0, SAA EA 008-5710- A0314 DTD 2 AUG2006 AND UPS EO DC8 5Jun 29, 2006 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS06847548Skin · damagedINSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM C-4 (D PIT) LWR CORNER AND REPAIRED IAW SRM 53-2-0 FIG 21 AND/OR DWG SRO8530019. REPAIRED SKIN CUT OUT IAW SAA EA 008-5330-01-A0288 AND UPS EO DC8- 5330-24691-A.Jun 28, 2006 · N894UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006804003Engine · malfunctionedDURING CLIMBOUT OF FL340 NR 4 ENG FLAME-OUT. ALL ENG PARAMETERS NORMAL AT TIME OF FLAME-OUT. UNABLE TO RELIGHT AT FL340. DESCENDED FL280 - RELIGHT SUCCESSFUL - ENG PARAMETERS NORMAL - ENG NR 4 FUNCTIONING. PER CFM M/M 71-00-00 CHECKED CHIP DETECTORS ON NR Jun 25, 2006 · N804DH · Doug DC873F · Engine (Turbine/Turboprop)SDR DHL2006809002Uplock Switch · dirtyDURING GEAR UPLATCH CHECK, GEAR UNLOCK LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. CONTINUED FLIGHT WITH GEAR HANDLE UP. LUBED LEFT AND RIGHT UPLOCK ACTUATOR, CLEANED UPLOCK SWITCHES, PERFORMED A/C JACKING AND PERFORMED 3 GEAR SWINGS IAW 32-31-3. OPS Jun 24, 2006 · N809DH · Doug DC873F · Landing Gear Position and WarningSDR UPS06847168Closeout Panel · crackedINSPECTION TYPE:N/A LEFT MLG CLOSEOUT PANEL AFT OF MAIN GEAR DOOR TANG CUTOUT IS CRACKED. REPAIRED CLOSEOUT PANEL IAW DC8 SRM CAPT 51-00. INSTALLED NEW Z-CHANNEL IAW DC8 SRM 51-1-21.Jun 20, 2006 · N868UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006806002Warning Switch · malfunctionedLEFT AUX GEAR DOOR WARNING LIGHT ON IN FLIGHT. REPLACED LEFT AUX GEAR DOOR WARNING SWITCH IAW DC8 MM 32-60-0, OPS CHECK NORMAL. P/N H20-24B.Jun 20, 2006 · N806DH · Doug DC873F · Landing Gear Position and WarningSDR UPS06847260Longeron · crackedINSPECTION TYPE:C2 C-PIT LONGERON 35R STA 1260-1280 CRACKED ON IB SIDE. REMOVED AND REPLACED LONGERON CHANNEL. IAW SRM 51-3-0 AND 51-1-20D.Jun 19, 2006 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS06847361Fitting · crackedINSPECTION TYPE:C2 BATH-TUB FITTING CRACKED AT STA 1180 BETWEEN L34R TO L35R. REMOVE BATHTUB FITTING. FABRICATED SPLICES AND INSTALLED BATHTUB AND SPLICES IAW SRM 51-01-20D, 53-2-0 FIG 2G.Jun 16, 2006 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847150Skin · damagedINSPECTION TYPE:N/A EO DC8-5330-24525 - A FUSELAGE SKIN DAMAGE REPAIRS AT STA 1420 LONGERON 29L AND STA 1460 LONGERON 29L. COMPLIED WITH EO DC8-5330-24525-A APPENDIX A AND APPENDIX B REPEAT INSPECTIONS DUE AT C-CHECK PERMANENT REPAIR DUE WITH IN 6000 FLT CYCLJun 16, 2006 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847279Seat Track · gougedFOUND GOUGE ON SEAT TRACK AT FS 900 RBL 46 IN MAIN CARGO COMPT. CUT OUT DAMAGED SEAT TRACK FROM FS 820-900 RBL 46 IAW SRM 53-2-3, FABRICATED AND INSTALLED SEAT TRACK SPLICE FROM FS 820-900 IAW SRM 53-02-03 FIG 13 AND UPS EO DC8-5320-8309-D.Jun 15, 2006 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847158Seat Track · gougedINSPECTION TYPE:C2 SEAT TRACK GOUGED AT FS 880 RBL 46 IN MAIN CARGO DECK. CUT OUT DAMAGED SEAT TRACK AT STA 880 RBL 46 IAW SRM 53-02-03 FIG 006D. DRILLED UP AND INSTALLED SEAT TRACK PLUG AT STA 880 RBL 46 IAW SRM 51-3-0.Jun 15, 2006 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847156Seat Track · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON SEAT TRACK AT STA 1290 LBL 60, MAIN CARGO DECK CUTOUT DAMAGED SEAT TRACK AT STA 1290 LBL 60 IAW SRM 53-02-03 FIG 006. LOCATED, DRILLED UP HOLES IN SEAT TRACK PLUG REPAIR IAW SRM 51-3-2. INSTALLED SEAT TRACK PLUG AT STA 1Jun 15, 2006 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847130Smoke Barrier · tornTEAR IN BOTTOM RIGHT CORNER OF SMOKE CURTAIN. BOTTOM OF SMOKE CURTAIN NOT ATTACHED TO FLOOR. REPAIR SMOKE CURTAIN IAW EO DC8-2550-1872B.Jun 14, 2006 · N811UP · Doug DC873F · Emergency EquipmentSDR UPS06847128Battery Pack · no testEMERG EXIT LIGHTS WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK PER AMM. OPS CK NORMAL, P/N ON 5708458-503, S/N FTL010.Jun 13, 2006 · N808UP · Doug DC873F · Emergency LightingSDR UPS06847163Seat Track · corrodedINSPECTION TYPE:C2 MAIN CABIN SEAT TRACK AT STA 465 LBL 60 HAS EXFOLIATION CORROSION. CUT OUT DAMAGED SEAT TRACK AT STA 460-600 LBL 60 IAW SRM 53-2-0 FIG 12. LOCATED, DRILLED UP AND INSTALLED REPLACEMENT SEAT TRACK AT STA 460-600 LBL 60 IAW SRM 51-1-21 AND SJun 12, 2006 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847162Seat Track · gougedINSPECTION TYPE:C2 CABIN SEAT TRACK AT STA 240 RBL 44 IS GOUGED AND SCALLOPS ARE DAMAGED. CUT OUT DAMAGED SEAT TRACK IAW EO DC8-5340-7779 AT STA 240 RBL 44 INSTALLED SEAT TRACK PLUG AT STA 240 RBL 44 IAW SRM 51-3-0, AND EO DC8-5340-7779.Jun 12, 2006 · N803UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06847117Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC8 AMM 33-50-01-2, OPS NORMAL S/N ON 368.Jun 12, 2006 · N867UP · Doug DC873F · Emergency LightingSDR UPS06847097Skin · damagedINSPECTION TYPE:N/A CREASE LEFT FUSELAGE AT STA 1340 THRU 1400. A/C FERRIED TO HEAVY MX VENDOR FOR REPAIR. RMVD DMG. PER SRM 53-02-01-0, FIG.7;VERIFIED DMG RMVD; COMPLETED REPAIR BY INSTALLING DOUBLER PER SRM 53-02-01-0,FIG 7; PRIMED & PAINTED REPAIR DOUBLERJun 9, 2006 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847092Smoke Goggles · crackedINSPECTION TYPE:N/A, F/O SMOKE GOGGLES HAVE SMALL CRACK IN LENS. REMOVED AND REPLACED F/O SMOKE GOGGLES.Jun 9, 2006 · N801UP · Doug DC873F · Emergency EquipmentSDR UPS06847598Skin · crackedINSPECTION TYPE:C1 RT UPPER WING SKIN CRACKED 1.5" LONG AT STA XCW 69.5 REAR SPAR SPAR UPPER SKIN. FABRICATED AND INSTALLED REPAIR -4 FILLER,-8 TRIPLER, AND -6 DOUBLER RT WING UPPER SKIN AT XCW 69.5 IAW SRM 57-02-01-0,SAA EA 008-5710-01-A0314 DTD 02 AUG 2006,Jun 8, 2006 · N894UP · Doug DC873F · Wing, Plate/SkinSDR UPS06847129Splice · crackedINSPECTION TYPE:C1 FS 1360 L23R SPLICE FITTING IS CRACKED AT AFT END. REMOVED CRACKED SPLICE FITTING AT STA 1360 L23R IAW SRM 51-3-0 AND SRM 51-1-20D, FABRICATED AND INSTALLED SPLICE FITTING AT STA 1360 L23R IAW SRM 51-1-20D AND DWG 3755118.Jun 6, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847048Structure · cutINSPECTION TYPE:N/A 1 INCH CUT IN FLOOR PIT 33 STA 1020 L. PERFORMED INTERIM REPAIR REF EO DC8-5320-8724A APPENDIX A.Jun 3, 2006 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847002Floor Panel · damagedINSPECTION TYPE:N/A PHL LOAD SUP REPORTS HOLE IN PIT 33 FLOOR, APPROX 3 INCHES IN LENGTH LOC'D 24 INCHES AFT OF DOOR & SLIGHTLY LEFT OF CENTER. C/W DC8 LOWER CARGO COMPARTMENT PIT NR 33 FLOOR PANEL PERMANENT REPAIR PER EO DC8-5320-87224-A APPENDIX C. THIS CLMay 31, 2006 · N811UP · Doug DC873F · Fuselage Floor PanelSDR DHL2006873528Door Frame · crackedAFT PASSENGER DOOR JAMB AFT UPPER CORNER 0.750 INCH CRACK (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIMay 30, 2006 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR DHL2006873514Vane · corrodedLT WING INBD VANE SLOT CORRODED STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-19-2006, DWG AST060506 DATED 05-11-06. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS, CUT OUT DAMAGED SECTION IAW DWG AST060506. PERFORMED NDT INMay 29, 2006 · N873SJ · Doug DC873F · Leading Edge DevicesSDR DHL2006873519Vane · damagedRT INBD VANE SLOT L/E UPPER PART HOLES ELONGATED STA XILD 7095 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-19-06, DWG AST060505 DATED 05-11-06. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION. PERFORMED NDT INSP, NO CRACKMay 29, 2006 · N873SJ · Doug DC873F · Leading Edge DevicesSDR DHL2006873516Structure · damagedRIGHT OUTBOARD VANE SLOT L/E HAS AN INTERIM REPAIR AT STA XOLDO 67.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001 (NO CRACK OR CORROSION FOUND). FABRICATED EMay 29, 2006 · N873SJ · Doug DC873F · Leading Edge DevicesSDR DHL2006873526Skin · wornLT OUTBOARD FLAP UPPER SKIN WORN STA XF 345.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-19-06, DWG AST060510 DATED 05-13-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWG AST060510. PERFORMED NDTMay 29, 2006 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR DHL2006873527Skin · damagedRT OUTBOARD VANE SLOT L/E HAS INTERIM REPAIR AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DWG AST060503. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRMay 29, 2006 · N873SJ · Doug DC873F · Leading Edge DevicesSDR DHL2006873518Doubler · crackedLWR FUS EXTERIOR INTERNAL DOUBLER HAS A BREAKAGE AND 2 CRACKS OF 0.750" ON IT, BETWEEN STA 156.000 AND -165.000, NEAR DOOR 12 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-26-06, DWG W90-53-R21 REV IR DATED 05-11-06. REMOVED EXISTING INMay 28, 2006 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006873520Skin · crackedNR 13 DOOR EXTERNAL SKIN CRACKED 0.500 INCH (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 52-8-1 FIG 1 SHEET 1. REMOVED DAMAGED PLATING IAW SRM 52-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T6 0.050") IAW SRM 52-8-1 FIG 1 SHEET 1 ITEM -E-. CLEANED, TMay 27, 2006 · N873SJ · Doug DC873F · Service DoorsSDR UPS06847084Spar Cap · crackedINSPECTION TYPE:SP 3 MAIN-CRACK ONE HALF INCH CENTER SPAR AFT SURFACE AT XRS26. REPAIRED CENTER SPAR CAP IAW SAA EA 008-5710-01-A0218, UPS RAA DC8-57-20169.May 27, 2006 · N868UP · Doug DC873F · Wing SparSDR UPS06847066Fitting · crackedINSPECTION TYPE:C1 BATH TUB FITTING AT STA 1690 L32L IS CRACKED. REMOVED AND REPLACED BATH TUB FITTING AT STA 1690 L32L IAW SRM 51-1-20D, AND DWG 4641326.May 26, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06847065Fitting · crackedINSPECTION TYPE:C1 STA 1690 L31R BATH TUB FITTING IS CRACKED. REMOVED BATH TUB FITTING AT STA 1690 L31R IAW SRM 51-1-20D DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1690 L31R IAW SRM 51-1-24, AND SRM 51-1-20DMay 26, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006873530Rib · crackedNR 4 RIGHT STUB WING RIB 4 INCH CRACK STA XOLDO 67.750 (MAJOR REPAIR). REMOVED CRACKED RIB IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO JC EA5May 25, 2006 · N873SJ · Doug DC873F · Wing, Rib/BulkheadSDR DHL2006873511Doubler · crackedLWR FUS EXTERIOR MODIFICATION DOUBLER (ACS) ON HEAT EXCHANGER AFT UPPER CORNER AT STA -12.000 L-24L CRACKED 0.600". PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-23-06, DWG W90-53-R22 REV IR DATED 05-11-06. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DMay 24, 2006 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006873522Door Frame · crackedD-CARGO DOOR JAMB FWD LWR CORNER 0.500 INCH CRACK STA 1400.000 L-32R (MAJOR REPAIR) AND CORROSION DAMAGE ON LWR FUS SKIN. PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG 17A, DWG DACO 5779936. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRMMay 23, 2006 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR DHL2006873521Skin · damagedINSPECT SKIN REPAIR ON FWD FUSELAGE FWD OF LWR LEFT MAIN CARGO DOOR (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 4, BOEING MSG 1-187877162-6 DATED 05-09-06. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTIMay 23, 2006 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06847009Hinge Fitting · crackedINSPECTION TYPE:C1 DURING REMOVAL OF L-1 DOOR UPPER DOOR HINGE FITTING ASSY CRACKED. REMOVED AND REPLACED L-1 DOOR UPPER HINGE FITTING ASSY IAW SRM 51-1-2 0D, AND 51-3-0.May 23, 2006 · N818UP · Doug DC873F · Passenger/Crew DoorsSDR DHL2006873512Door Frame · crackedFWD SVC DOOR JAMB AFT LWR CORNER 0.250" CRACK. PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG NR`S SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.May 23, 2006 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR DHL2006873524Doubler · wornLEFT OUTBOARD FLAP UPPER SKIN DOUBLER WORN STA XF 225.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4 TR 57-94 DATED 10-01-02. REMOVED EXISTING PLATING WITH WORN REPAIR DOUBLER IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW PLAMay 22, 2006 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR DHL2006873523Skin · damagedLEFT OUTBOARD VANE SLOT HAS INTERIM REPAIR AT STA XOLDI 6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-18-06, EO AST060501 DATED 05-06-06. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PMay 22, 2006 · N873SJ · Doug DC873F · Leading Edge DevicesSDR UPS06847062Fitting · corrodedINSPECTION TYPE:C1 C PIT STA 1228 BETWEEN L35R-36 BATH TUB FITTING CORRODED OUT OF LIMITS REMOVED BATH TUB FITTING AT STA 1228 BETWEEN L35R-36 IAW SRM 51-1-20D LOCATED AND DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1228 L35R-36 IAW SRM 51-1-20D, May 20, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006873510Skin · corrodedLT INBD FLAP UPPER SKIN CORRODED (STA XW 104.000 - 115.000), MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1May 20, 2006 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR UPS06847063Fitting · corrodedINSPECTION TYPE:C1 C PIT STA 1220 BETWEEN L35R-36 BATH TUB FITTING INSIDE TORQUE BOX HAS EXFOLIATION CORROSION. REMOVED BATH TUB FITTING AT STA 1220 L35R-36 IAW SRM 51-1-20D DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1220 L35R-36 IAW SRM 51-1-20D, AMay 19, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006873509Skin · damagedLT OTBD STUB WING LWR SURFACE HAS INTERIM REPAIR ON IT. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1. REMOVED EXISTING REPAIR DOUBLERS IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.080") AND INTERNAL REPAIR DOUBLER (AL7075"0"May 17, 2006 · N873SJ · Doug DC873F · Wing, Plate/SkinSDR DHL2006873506Skin · damagedRT OTBD FLAP EXTERNAL SKIN (UPPER) HAS AN INTERIM REPAIR AT STA XF 417.000. PERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-188745980-2 DATED 05-10-06. REMOVED PLATING WITH INTERIM REPAIR ON IT IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3May 17, 2006 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR DHL2006873505Skin · wornLT OTBD FLAP UPPER SKIN WORN, STA XF 415.000. PERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-188745980-2 DATED 05-10-06. REMOVED WORN PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.032") IAW BOEING MESSAGE 1-188745980-2. CLEANED,May 17, 2006 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR UPS06846982Skin · gougedINSPECTION TYPE:C1 PANEL LANDING AT ACCESS PNL 506C HAS DEEP GOUGE NR 3 MAIN TANK. TRIMMED OUT DAMAGED AREA OF LANDING IAW SRM 57-02-01 FIG 036. FABRICATED INSTALLED REPAIR FILLER, EXTERIOR DOUBLER, INTERIOR FILLER AND DOUBLER IAW SRM 57-02-01 FIG 036, 51-01May 16, 2006 · N818UP · Doug DC873F · Wing, Plate/SkinSDR UPS06846939Fitting · crackedINSPECTION TYPE:C1 POSSIBLE CRACK ON STRINGER END FITTING AT STRINGER 59 BETWEEN XW408 AND XRS463 NR 1 ALT. REMOVED AND REPLACED FITTING AT STRINGER 59 BETWEEN XW408 AND XRS463 IAW SRM 51-1-20D AND 51-1-23.May 16, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/Stringer
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