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 IXXA07SMN239SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER HEAT INTERCHARGER COMPARTMENT LOWER AFT JAMB CORNER CRACKED AT STATION FS 12.000 LONGERON 27 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED ARENov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN238SVane · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING EXTERNAL VANE WITH ELONGATED HOLES AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DNov 10, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN237SVane · elongatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INTERNAL VANE WITH ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER AND INTERNAL DOUBLER. Nov 10, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN236SFrame · damagedDURING ROUTINE C CHECK INSPECTION, AT F/S STATION 240 LEFT FRAME HAS DOUBLE DRILLED HOLE BETWEEN LONGERON 29 LEFT AND LONGERON 30 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PLUGGED MISDRILLED HOLE WITH RIVET. PERFORMED NDT INSPECTION. NO CRACK, NNov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, FrameSDR IXXA07SMN235SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FS 1518 LONGERON 32.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER. CLEANED, TREATEDNov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN234SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 97.000 LONGERON 34.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NET INSPECTION. NO CRACK NOR CORROSION FOUND. FABRICATED EXTERNAL AND INTERNANov 10, 2007 · N604BX · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA07SMN232SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND INBOARD FLAP UPPER PLATING HAS A IMPROPER REPAIR AT STATION XW 71.000 AND STATION XW 91.000.REMOVED FASTNER AS NEEDED TO PERFORM REPAIR.REMOVED EXISTING REPAIR.FABRICATED NEW SKIN AND INTERNAL DOUBLRE. CLEANEDNov 10, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN231SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PLATING HAS IMPROPER REPAIR AND DENT BETWEEN STATION XW 104.000 AND XW 115.000. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CNov 10, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN230SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOIND LEFT HAND WING INBOARD FLAP HAS A DENT ON UPPER PANEL PLATING BETWEEN STATION XW 115.000 AND STATION XW 122.000.REMOVED FASTNERS AS NEEDED. REMOVED DAMAGEDAREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED REPAIR Nov 10, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR IXXA07SMN229SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP UPPER PLATING HAD IMPROPER REPAIR AT STATION XF 213.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTNov 9, 2007 · N604BX · Doug DC873F · Trailing Edge FlapsSDR DHL2007801523Skin · crackedLT RUDDER SKIN CRACKED 5" AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM AL 2024T3 0.016" IAW SRNov 9, 2007 · N801DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2007801522Skin · deformedRT RUDDER SKIN DEFORMED AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM IAW SRM 55-6-1 FIG 1 PG 2Nov 9, 2007 · N801DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2007801532Skin · damagedRUDDER TIP SKIN BROKEN AT STA ZR 335.250 (DAMAGE CAUSED BY SEMAN). REMOVED BROKEN TIP IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TIP IAW SRM 51-1-21A. REFER TO JC EC-00592-001 (WO 2624) FOR FABRICATION AND NR 101137 FONov 9, 2007 · N801DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2007801520Skin · wornNR 1 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 150.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION. FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLICNov 8, 2007 · N801DH · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR DHL2007801521Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SKIN WORN AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLICE (STEEL TYPNov 8, 2007 · N801DH · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR DHL2007801529Fitting · crackedMAIN CARGO COMPT SERVICE DOOR JAMB FITTING CRACKED 1" AT STA 1118.528 L11R. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1.Nov 8, 2007 · N801DH · Doug DC873F · Service DoorsSDR DHL2007801512Skin · delaminatedRT WING ACCESS DOOR NR 577B INTERNAL SKIN DELAMINATED (STA XA 650.000 - 670.000). REMOVED AND REPLACED DOOR ASSY IAW SRM 51-3-0, SRM 51-3-1.Nov 7, 2007 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007801524Support · crackedNR 7 LT AILERON HINGE SUPPORT CRACKED. REMOVED AND REPLACED NR 7 LT AIL HINGE SUPPORT IAW MM 20-16-0 PG 201-207, OHM 27-2-3A. REFER TO NR 130478 FOR OPS CHECK AND NR 130141 FOR LT OUTBD AIL REMOVAL/REINSTALLATION.Nov 7, 2007 · N801DH · Doug DC873F · AileronsSDR DHL2007801510Skin · delaminatedLT WING UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XW 0 - 33.000). REMOVED AND REPLACED LT WING UPPER PANEL ASSY IAW SRM 51-3-0, SRM 51-3-1.Nov 6, 2007 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007801513Fitting · crackedLT WING CTR L/E UPPER INTERNAL SPLICE FITTING CRACKED 3" AT STA XOLDI 6.2246. REMOVED SPLICE FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-21, SRM 51-1-20DNov 6, 2007 · N801DH · Doug DC873F · Wing, Attach FittingsSDR DHL2007801515Skin · damagedINSPECT REPAIR AT FUSELAGE STA 490 L-23R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACCOMPLISHED AT AIR CANADA AUG 94. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 2. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21.Nov 6, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07851100Battery · weakEMERGENCY EXIT LIGHTS ARE VERY DIM AND FLIGHT DECK LIGHT GOES OUT IN APPROX 2 MINUTES. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW DC8 AMM 33-50-01-2. OPS TEST NORMAL.Nov 6, 2007 · N802UP · Doug DC873F · Emergency LightingSDR DHL2007801511Skin · delaminatedNR 3 RT FLAP VANE LWR SKIN DELAMINATED (STA XF 160.000 - 213.000). REMOVED AND REINSTALLED NR 3 RT FLAP VANE (REPAIRED CONDITION) IAW MM 27-51-14 PG 201-202. REFER TO NR 130478 FOR OPS CHECK.Nov 5, 2007 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2007801508Skin · delaminatedLT MLG MID DOOR EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED LT MLG MID DOOR IAW MM 32-12-1 PG 401. REFER TO JC BZ5A32376 FOR OPS CHECK.Nov 5, 2007 · N801DH · Doug DC873F · Landing Gear DoorsSDR DHL2007801525Skin · damagedINSPECT REPAIR AT FUSELAGE 40 LONGERON 28L PER INSTRUCTIONS REQUIREMENTS OF SRM 53-2-1 CLASS II TYPE REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13 SHEET 3,5. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-20D. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 Nov 5, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007801516Skin · damagedINSPECT REPAIR AT FUSELAGE STA 160 LONGERON 31R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACCOMPLISHED AUG 94. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 5. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51Nov 5, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07851088Indicator · out of positionESCAPE SLIDE PRESSURE IND SLIDE DOWN BELOW VIEWING WINDOW. REPOSITIONED ESCAPE SLIDE.Nov 4, 2007 · N814UP · Doug DC873F · Escape SlideSDR DHL2007801518Fitting · crackedNR 4 ALT TANK FITTING CRACKED 0.500" AT STA XRS 408.000 S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00590-001, DOUGLAS DWG 5644972. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALNov 2, 2007 · N801DH · Doug DC873F · Wing, Attach FittingsSDR UPS07851086Fan · frozenDIVERSION, CREW SMELLED SMOKE IN CABIN. DISCHARGE HAND EXTINGUISHER IN LAV, CREW REPORTED LAV PUMP WAS TURNING. PARKED FOR FAA EVALUATION. FOUND RECIRCULATING FAN FROZE UP. REMOVED AND REPLACED IAW AMM 21-1-01-2. OPS CHECK GOOD. INSPECTED SURROUNDING ARENov 2, 2007 · N880UP · Doug DC873F · Air Distribution FanSDR UPS07851089Battery Pack · inoperativeEMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. CKS OK IAW MM 33-50-01-2.Nov 2, 2007 · N851UP · Doug DC873F · Emergency LightingSDR UPS07851099Fitting · crackedINSPECTION TYPE:C2 FITTING AT STA 1230 L33R IS CRACKED. REMOVED AND REPLACED END FITTING AT STA 1230 L33R IAW SRM 51-01-20D AND SRM 51-01-24.Oct 30, 2007 · N813UP · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2007801509Skin · crackedFUSELAGE AFT SVC DOOR CRACKED 0.750" STA 1620.000 L-20R TO L-21R AT LWR FWD JAMB CORNER (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD200-20-08 S/B DC8-53-075, DRAWING DOUGLAS SR08530021. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 AND SRM 51-1-20D. CUT OUOct 29, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2007801507Skin · crackedRT AFT FUSELAGE EXTERNAL SKIN CRACKED 2" STA 1749.000 L-15R TO L-16R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 4. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER INTERNAL FINGER DOUBLER ANDOct 29, 2007 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07851077Tab · puncturedINSPECTION TYPE:N/A LEFT ELEVATOR INBOARD CONTROL TAB HAS A .3125 INCH PUNCTURE ON BOTTOM OF TAB. TRANS TO NRC 107944. CHECKED LEFT I/B ELEVATOR AREA ON AIRCRAFT SIDE FOR HARDWARE/ATTACH FITTING. NO DISCREPANCY FOUND. OK TO INSTALL ELEVATOR CONTROL TAB. IOct 28, 2007 · N812UP · Doug DC873F · Elevator, Tab StructureSDR UPS07851090Doubler · crackedINSPECTION TYPE:C1 AFTER REMOVAL OF EXTERIOR RT CV WINDOW RETAINER FOUND INTERNAL DOUBLER CRACKED AT UPPER FWD CORNER STA -72. REPAIRED RT CV WINDOW INTERNAL DOUBLER AT STA -72 IAW SAA EA NR 008- 5600-01-A1197, UPS RAA NR DC8-53-20669, AND FAA FORM 8100-9.Oct 27, 2007 · N867UP · Doug DC873F · Fuselage Main, StructureSDR DHL2007801504Doubler · crackedLT WING L/E LWR INTERNAL DOUBLER CRACKED 1" STA XFS 335.250. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1-21. FABRICATED NEW DOUBLER (AL7075T6 0.090") IAW SRM 57-3-3 FIG 5. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAOct 26, 2007 · N801DH · Doug DC873F · Wing, Plate/SkinSDR IXXA070054OWarning System · malfunctionedDURING CLIMB-OUT FROM KDFW TO KIAH, AFTER GEAR RETRACTION THE CREW NOTICED DOOR NOT LATCH LIGHT STAYED ON UNTIL THE CREW RECYCLED THE GEARS AND LIGHT WENT OUT. CREW LANDED AT KIAH WITHOUT INCIDENT. MAINTENANCE INSPECTED MAIN LANDING GEAR DOOR TARGET AND STRIOct 26, 2007 · N603AL · Doug DC873F · Landing Gear Position and WarningSDR UPS07851058Slide · unsecureESCAPE SLIDE CAME LOOSE. RESECURED ESCAPE SLIDE TO FWD ENTRY DOOR B DC8 25-60.Oct 26, 2007 · N806UP · Doug DC873F · Escape SlideSDR UPS07851013Housing · openESCAPE SLIDE HOUSING IS PARTIALLY OPEN. SECURED ESCAPE SLIDE HOUSING PER MM 25-60-01-2.Oct 26, 2007 · N874UP · Doug DC873F · Escape SlideSDR UPS07851118Mount · elongatedINSPECTION TYPE:C2 RIGHT MAIN GEAR DOOR SWITCH MOUNT HOLES ELONGATED. FABBED AND INSTALLED DOUBLER ON RIGHT MAIN GEAR DOOR SWITCH MOUNT IAW DWG 5653490 AND SRM 51-0-20-D, 51-1-8.Oct 24, 2007 · N813UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07851117Web · crackedINSPECTION TYPE:C2 LT HORIZONTAL STAB AFT WEB ACCESS HOLES HAVE CRACKS AT FASTENER HOLE ON NR 5, 9, 10, AND 12. STOP DRILLED ALL CRACKS, FABBED DOUBLERS, AND INSTALLED DOUBLERS IAW DC8 SRM 55-03-00, 51-1-8, AND 55-02-00.Oct 24, 2007 · N813UP · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07851101Skin · crackedINSPECTION TYPE:C2 RT HORIZ STAB AFT SPAR WEB ACCESS HOLES HAVE CRACKS AT FASTNER HOLE SKIN ON NR 2, 3, 6, 7, 8, 9, 11, AND 12. STOP DRILLED ALL CRACKS AT ACCESS HOLES IN RT HORIZ STAB STA XH 28.843-149.00. FABRICATED AND INSTALLED 12 EA DOUBLERS ON RT HORIZOct 24, 2007 · N813UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL2007801506Skin · misrepairedLT WING NR 1 STUB WING EXTERNAL PART SHOWS REPAIR NOT IAW SRM 57-2-1A AT STA XFS 533-375. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.080") AND INTEROct 22, 2007 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2007801503Structure · crackedRT INNER WING OUTBD EXTENDED L/E SLOT PLATING CRACKED 1.500" STA XFS 207.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 38 PG 2, TR NR 57-85 DATED 11-22-00. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 Oct 18, 2007 · N801DH · Doug DC873F · Leading Edge DevicesSDR DHL2007801505Structure · corrodedRT INNER WING OUTBD EXTENDED L/E SLOT PLATING CORRODED, STA XILD 42. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38 PG 2, TR NR 57-85 DATED 11-22-00. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57Oct 17, 2007 · N801DH · Doug DC873F · Leading Edge DevicesSDR IXXA070053OEadi · failedDURING TAKEOFF ROLL PRIOR TO 80 KIAS, FIRST OFFICER'S EADI WENT BLANK WITH FLAGS IN VIEW, BAR WITH ATT IN VIEW, GA .AND INST 2 FLAG. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS AT KIAH WITH OUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NUMBER 2 INSTRUMEOct 17, 2007 · N605AL · Doug DC873F · Attitude Gyro and Indicating SystemSDR DHL2007801500Frame · crackedRT WING CENTRAL L/E FORMER SHOWS 1" CRACK AT STA XFS 341.500. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER FROM AL7075T6 0.032 INCH IAW SRM 57-2-0 PG 9 AND 10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51Oct 16, 2007 · N801DH · Doug DC873F · Leading Edge DevicesSDR UPS07850988Seat Track · crackedINSPECTION TYPE:C1 CRACK AND HEAVY CORROSION ON SEAT TRACK AT STA 1360 LBL 59. CUT OUT DAMAGED SEAT TRACK AT STA 1290-1370 IAW SRM 51-3-0. INSTALLED REPAIR SEAT TRACK SECTION AT STA 1290-1370 LBL 59 IAW SRM 53-07-03 FIG 3D.Oct 16, 2007 · N867UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07851095Window Frame · corrodedINSPECTION TYPE:C2 WINDOW FRAME AT STA -67 L11L CAPT SIDE HAS EXFOLOIATED CORROSION. REPAIRED CAPT LT AFT WINDOW FRAME AT STA -67 L11L IAW SAA EA NR 008- 5310-01-A1194, UPS RAA NR DC8-53-20665, AND BAC SERV ID 1-659403655.Oct 15, 2007 · N813UP · Doug DC873F · Fuselage Main, StructureSDR UPS07851094Fitting · crackedINSPECTION TYPE:C2 INSIDE 60 HOLE LONGERON END FITTING CRACKED AT STA 1766 L19R. REMOVED AND REPLACED LONGERON END FITTING AT STA 1766 L19R IAW SRM 51-1-21, AND SRM 51-1-20D.Oct 15, 2007 · N813UP · Doug DC873F · Fuselage Main, Structure
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