N805UP, cancelled May 6, 2010

Service difficulty reports · 246

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N805UP' AND deregistration_id = 'N805UP-2010-05-06'
  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 UPS08853860Door Seal · obstructedINSPECTION TYPE:N/A ON CLIMB WITH CABIN PRESSURE DIFFERENTIAL BETWEEN 1.5 - 3.5 PSI THERE WAS A LOUD AIR LEAK FROM CABIN DOOR AREA. NOISE LEVEL WAS SUCH THAT COCKPIT COMMUNICATIONS WERE LIMITED. ACCOMPLISHED AIR TURNBACK. REMOVED LOOSE SEALANT AT MAIN CARGONov 5, 2008 · N805UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS08853469Skin · crackedCRACK IN SKIN STA 25 STRINGER 33. CORROSION FOUND. REMOVED FASTENERS & MADE 3" C/O IN SKIN AT STA 25 L34-33R PER SRM 51-01-08-0. REMOVED CORROSION PER SRM 51-01-08. REPAIR COMPLETED REF NRC 225282 & 225283. PERMANENT REPAIR AT OR BEFORE NEXT C-CHECK PER DC8Oct 4, 2008 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08852235Engine · flamed outINSPECTION TYPE:N/A CLIMBING THROUGH FL360 THE NR 4 ENGINE FLAMED OUT. DESCENDED TO FL220 AFTER ACCOMPLISHING THE IN FLIGHT ENGINE FLAMEOUT CHECKLIST TO ATTEMPT A RESTART. FOLLOWED THE IN FLIGHT ENGINE START CHECKLIST AND ATTEMPTED 1 RESTART. AFTER DRY MOTOMay 13, 2008 · N805UP · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS08852164Door · bindingLT OVERWING EMERGENCY EXIT DOOR BINDING. LUBRICATED SEAL AND ALL MOVING PARTS IAW MM 12-80-00. OPS CHECK GOOD.May 3, 2008 · N805UP · Doug DC873F · Emergency ExitsSDR UPS08851764Packing · unknownIFSD - LOSS OF OIL QTY OIL QTY JUST ABOVE ZERO, OIL PRESSURE FLUCTUATING AT 40 PSI DURING ENGINE SHUTDOWN NR 2 ENG WINDMILLING SHUTDOWN AT 15 PSI PRESS FOR ONE HOUR. REMOVED AND REPLACED STARTER REDUCER PLUG PACKING IAW DC8 IPC 80-10-00/30 ITEM 150. SERVICE Mar 6, 2008 · N805UP · Doug DC873F · Engine StarterSDR UPS08851718Bottle · low pressureESCAPE SLIDE PRESSURE OUT OF GREEN BAND. DEFERRED PER MEL 52-7-4. REMOVED AND REPLACED EVACUATION SLIDE ASSY PER AMM 25-60-01-2.Feb 26, 2008 · N805UP · Doug DC873F · Escape SlideSDR UPS08851577Skin · crackedSKIN CRACK AT UPPER EDGE NEAR AFT CURVE OF L1 DOOR APPROX 1/2 INCH LINEAR, PARALLEL TO T/E OF DOOR. PERFORMED INTERIM REPAIR IAW UPS EO NR DC8-5210-28486-A PARAGRAPH 6A. PERM REPAIR OR PART REPLACEMENT WITHIN 25 FLIGHT CYLES. D367801 ASSIGNED BY AMC.Jan 26, 2008 · N805UP · Doug DC873F · Passenger/Crew DoorsSDR UPS07850685Slide · out of positionINSPECTION TYPE:N/A SLIDE CAME OUT OF COVER WHEN RT GIRT BAR WAS TAKEN OUT OF LOCK DETENT. RESECURED FWD ENTRY DOOR SLIDE/CONTAINER - SLIDE CHECKS OK IAW DC8 AMM 25-60-01-2. A/C OK FOR SERVICE.Sep 18, 2007 · N805UP · Doug DC873F · Escape SlideSDR UPS07850163Slide · out of positionINSPECTION TYPE:N/A RESTOW ESCAPE SLIDE. RESTOWED ESCAPE SLIDE IAW MM 25-60-01-2.Jul 11, 2007 · N805UP · Doug DC873F · Escape SlideSDR UPS07849751Skin · misrepairedINSPECTION TYPE:C2 INSPECTION FOUND PREVIOUS LWR CORNER REPAIR AT STA 1220 THE CUTOUT WAS TO CLOSE TO EDGE AND EXTENDS DOUBLER BEYOND NORMAL LENGTH. REMOVED AND REPLACED RIVETS WITH HI-LOKS AT C-3 DOOR LWR AFT CORNER IAW SAA EA 008-5330-01-A0809 REV-A, UPS EOMay 1, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849744Cusp Web · crackedINSPECTION TYPE:C2, 6 INCH CRACK ON CUSP AT FS 1220 RIGHT SIDE FLOORBEAM FITTING L21R. REPAIRED CUSP AT STA 1133 - 1248 L21R IAW SAA EA008-5330-01-A0815, UPS RAA DC8-53-20622, SRM TR 53-180, AND FAA FORM 8100-9.Apr 7, 2007 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07849626Floorbeam · crackedINSPECTION TYPE:C2 MAIN CARGO FLOORBEAM AT STA 280 RBL 24 CRACKED FROM EXFOLIATION CORROSION. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 280 RBL 24 IAW SRM 51-2-1 PG 8 FIG 1. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM TR 51-130 FIG 1 SHEET 1.Apr 2, 2007 · N805UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07849618Rib · crackedINSPECTION TYPE:C2 12TH RIB FROM BOTTOM OF RUDDER ON L/E IS CRACKED. STOP DRILLED CRACK ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0 FIG 2 SHEET 2.Mar 31, 2007 · N805UP · Doug DC873F · Rudder, Spar/RibSDR UPS07849617Rib · crackedINSPECTION TYPE:C2 18TH RIB FROM BOTTOM OF RUDDER ON L/E CRACKED. STOP DRILLED CRACK ON 18TH RIB FROM BOTTOM OF L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 18TH RIB IAW SRM 55-06-00 FIG 028.Mar 31, 2007 · N805UP · Doug DC873F · Rudder, Spar/RibSDR UPS07849611Attach Angle · crackedINSPECTION TYPE:C2 ATTACH ANGLE FOR VERT FIN L/E TO FUSELAGE BENT AND CRACKED RIGHT SIDE FS 1690. REMOVED ATTACH ANGLE FOR VERT FIN TO FUSELAGE AT STA 1690 IAW SRM 51-3-0. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER AT FS 1690 VERT FIN L/E TO FUSELAGE Mar 31, 2007 · N805UP · Doug DC873F · Vertical Stabilizer, Attach FittingsSDR UPS07849639Skin · corrodedINSPECTION TYPE:C2 AFTER REMOVAL OF C-2 (B-PIT) SCUFF PLATE FOUND CORROSION ON FUSELAGE SKIN. REMOVED CORROSION AND FOUND SKIN TO BE OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. PROCURED AND INSTALLED REPLACEMENT SKIN FROM STA 450-610 L31L-L31R IAW SRM 51-1-20D, ANDMar 30, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849631Skin · crackedINSPECTION TYPE:C2 HFEC INSP DETECTED A CRACK ON THE C-4 (D-PIT) LWR AFT DOOR JAMB CORNER STARTING AT FASTENER GOING FWD TO EDGE OF DOOR CUTOUT. CUT OUT DAMAGED AREA AT D-PIT LWR AFT DOOR JAMB CORNER (STA 1440) IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLEDMar 30, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849725Fitting · crackedINSPECTION TYPE:C2 C-PIT, AT UPPER CORNER OF CROSS SLIDE DOOR CUTOUT, FITTING HAS 4.5" CRACK STA 1200 RBL 65. REMOVED CRACK FITTING AT STA 1200 RBL 65 C-PIT DOOR CUT OUT IAW SRM 51-1-20D. INSTALLED REPLACEMENT FITTING AT STA 1200 RBL 65 C-PIT DOOR CUT OUT IAMar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849628Longeron · crackedINSPECTION TYPE:C2 AIR CONDITIONING COMPT LONGERON CORRODED AT STA 45 L30R AND 5 INCH LONG CRACK STA 65. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21 AND 51-1-20D.Mar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849619Bulkhead · corrodedINSPECTION TYPE:C2 A/C COMPT FWD BULKHEAD CORRODED AT STA 8 BL 0. REMOVED CORRODED WEB AND CHANNEL AT STA 8 BL 0 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR WEB, AND CHANNEL AT STA 8 BL 0 IAW SRM 51-09-00 FIG 068A, AND EO DC8-5350-7876.Mar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS07849585Frame · crackedINSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS 44 CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-02-00-0, 51-1-20D AND DWG 5644310.Mar 28, 2007 · N805UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS07849584Frame · crackedINSPECTION TYPE:C2 RT HORIZONTAL STAB LEADING EDGE LWR FORMER STA XFS32 CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 5 5-02-00-0, 51-1-20D AND DWG 5644310.Mar 28, 2007 · N805UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS07849635Door Frame · damagedINSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-2 (B-PIT) DOOR JAMB UPPER FWD CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 20. REMOVED STEEL DOUBLER FROM B-PIT DOOR JAMB UPPER FWD CORNER IAW SRM 51-01-21A. FABRICATED AND INSTALLED CORRECT TRIPLER, DOUBLER, AND FIMar 24, 2007 · N805UP · Doug DC873F · Fuselage Main, StructureSDR UPS07849627Door Frame · damagedINSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM C-3(C-PIT) DOOR JAMB LWR FWD CORNER AND REPAIR PER DC8 SRM 53-2-0, FIG 22 AND/OR DWG SRO8530019. REPAIRED DOOR CORNER IAW SAA EA 008-5310-01-A0755.Mar 24, 2007 · N805UP · Doug DC873F · Fuselage Main, StructureSDR UPS06848810Skin · gougedINSPECTION TYPE:SV TRANSFERRED FROM LOG PAGE 683072/1; REF DMI D-340854: SKIN GOUGES AT BS 120 BETWEEN L16L - L17L. REPAIRED FUSELAGE SKIN AT STA 120, L16L - 17L IAW SAA SK 008-5302- 01-A0556, UPS RAA DC8-53-20603, BAC SRID 1-264826789, AND FAA FORM 8100-9.Dec 28, 2006 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS06846909Light · inoperativeINSPECTION TYPE:N/A ON SHUTDOWN EMERGENCY EXIT LIGHTS DISARM CHECK FAIL TO GIVE PROPER INDICATION. LIGHT SHOULD ILLUMINATE. RELAMPED, OPS CHECKS GOOD.May 11, 2006 · N805UP · Doug DC873F · Emergency LightingSDR UPS06846753Smoke Goggles · scratchedF/O'S SMOKE GOGGLES SCRATCHED AND FOGGY. REPLACED CAPTAIN'S SMOKE GOGGLES PER 25-60-05-2.Apr 25, 2006 · N805UP · Doug DC873F · Emergency EquipmentSDR UPS06846270Battery Pack · dischargedINSPECTION TYPE:N/A ON PREFLIGHT FOUND EMERGENCY EXIT LIGHTS OVER ENTRY DOOR & IN COMPANION WAY OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKS OK.Feb 23, 2006 · N805UP · Doug DC873F · Emergency LightingSDR UPS05844379Wire · pulledNO EMERGENCY LIGHTS ON TEST. EMERGENCY BATTERY PACK REPLACED, BUT EMERGENCY LIGHTS WOULD NOT TURN OFF WHEN DISARMED. FOUND WIRE PULLED OUT OF SOCKET NR 8 ON P1-1345. REPLACED SOCKET PER MM 20-50-01-8 AND WDM 33-50-01 PG 5. TEST GOOD PER MM 33-50-01-2.Apr 26, 2005 · N805UP · Doug DC873F · Light System WiringSDR UPS05844119Fitting · crackedINSPECTION TYPE:C1 LONGERON 10L END FITTING CRACKED AT STA 1770. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D.Feb 24, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844117Doubler · crackedINSPECTION TYPE:C1 INTERNAL DOUBLER CRACKED AT STA 1880 BETWEEN SKIN AND LONG 34R. CORRODED FROM 1861-1890. REMOVED DOUBLER FROM STA 1770-1890. FAB REPLACEMENT DOUBLER FROM SHT7075T6 -.025. INSTALLED DOUBLER REF DWG 5649328, SRM 51-1-21, 51-1-8, 51-1-20D.Feb 23, 2005 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05844159Seat Track · corrodedINSPECTION TYPE: C1, AFT CARGO BS 1420 LT CUSP, APROX LBL 60 ON FWD SIDE OF FRAME, SEVERE CORROSION UNDER & AROUND NUTCLIPS APPROX .5 INCH DIA SEAT TRACK. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3. REMOVED AND REPLACED SEAT TRACK SECTIONFeb 22, 2005 · N805UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05844120Seat Track · wornINSPECTION TYPE:C1 MAIN CABIN SEAT TRACK SCALLOPS WORN BEYOND LIMITS STA 1360-1380, LBL 24. REMOVED FLOORBOARDS TO FOM. REMOVED SEAT TRACK FROM 1300-1460. FAB RPLACEMENT SEAT TRACK FROM S2772660 EXTRUSION. INSTALLED SEAT TRACK, NEW SPLICE FITTING, AND FLOOFeb 22, 2005 · N805UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05844116Skin · crackedINSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT RT PRIMARY HEAT EXCHANGER CUTOUT AT LOWER AFT CORNER. CRACK APPROX 1 INCH LONG. CUT OUT DAMAGED SKIN, NDT VERIFIED. FAB DOUBLER AT FILLER FROM SHT2024 T3-.100. INSTALLED CONICAL WASHERS AND ALL REPAIR PARTS REF SFeb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS05844021Finger Doubler · corrodedINSPECTION TYPE: C1, FINGER DOUBLER CRACKED & HAS SHEARED RIVET HEADS IN MAIN CABIN SUBFLOOR, STA 875 LBL 5. REMOVED FINGER DOUBLER & FOUND IT HEAVILY CORRODED ON UNDERSIDE. NO CORROSION NOTED ON PRESSURE WEB. FAB REPLACEMENT FINGER DOUBLER FROM 2024T3-.050Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, StructureSDR UPS05844019Fitting · crackedINSPECTION TYPE: C1, FITTING CRACKED UNDER FLOORBEAM, STA 700 RBL 24 MAIN CABIN. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D.Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844016Attach Angle · crackedINSPECTION TYPE: C1, SPAR-TO-WING ATTACH ANGLE CRACKED IN MAIN CABIN SUBFLOOR, STA 798 RBL 55. FAB REPLACEMENT ANGLE REF DWG3643112 ON SAA SERVICE ORDER 7034920. REMOVED & REPLACED ANGLE REF SRM 51-1-20D, 51-3-2, 51-1-24, 51-1-20D. FUEL LEAK CHECK C/W ON TCFeb 22, 2005 · N805UP · Doug DC873F · Fuselage, Wing Attach FittingsSDR UPS05844014Fitting · crackedINSPECTION TYPE: C1, LONGERON FITTING CRACKED IN MAIN CABIN STA 902-910 LONG 4L. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20B, 51-1-21, 51-1-20D.Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844012Fitting · crackedINSPECTION TYPE: C1, BATH-TUB FITTING CRACKED ON LONG 4R, STA 902. REMOVED AND REPLACED FITTING REF SRM 51-1-20D.Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, StructureSDR UPS05844011Support Fitting · crackedINSPECTION TYPE: C1, MAIN CABIN FLOORBEAM FITTING CRACKED AT STA 702 LBL 25 (SUBFLOOR). REMOVED & REPLACED FITTING REF SRM 51-1-20D, 51-1-8, 51-1-11.Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844009Floor Support · crackedINSPECTION TYPE: C1, MAIN CABIN AFT PRESSURE BULKHEAD VERTICAL STIFFENER TO FLOORBEAM ATTACH FITTING CRACKED, SUBFLOOR LBL 25. FABRICATED REPLACEMENT FITTING REF DWG 5773275 ON SAA TRAVELER 0001. REMOVED & REPLACED FITTING REF SRM 51-1-8, 51-1-20D.Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844158Longeron · crackedINSPECTION TYPE:C1, COMPT 60 L17R HAS 3 INCH CRACK AND LONGERON END FITTING HAS .5 INCH CRACK 1770. REMOVED AND REPLACED L17R AND END FITTING AT STATION 1770 IAW 51-1-8, 51-1-20D, 53-2-2 AND 51-1-21.Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844121Angle · crackedINSPECTION TYPE:C1 ANGLE CRACKED INSIDE L1 DOOR JAMB AT STA 35. NDT VERIFIED CRACK TERMINATED AT FASTENER HOLE. FAB REPAIR DOUBLER FROM SHT2027T3-.063. TREAT, PRIME, INSTALL REPAIR REF SRM 51-1-21, 51-1-8, 51-3-0, 53-2-0 FIG 1B, 51-1-21A, DWG 5597646.Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, StructureSDR UPS05844113Fitting · crackedINSPECTION TYPE:C1 LONGERON 11L SPLICE FITTING CRACKED STA 660-680. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-3-2, NDTSPM06-10-01.Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844022Clip · crackedINSPECTION TYPE: C1, TIE ANGLE CRACKED ON FWD SIDE OF AFT PRESSURE BULKHEAD TO LONG 6R. REMOVED CRACKED ANGLE. FAB REPLACEMENT ANGLE FROM SHT7075/0-.080 AND HEAT TREATED TO T6 ON SAA SERVICE ORDER 7034928. INSTALLED ANGLE REF DWG 5773844, SRM 51-1-21, DPS7.Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844020Fitting · crackedINSPECTION TYPE: C1, ATTACH FITTING CRACKED ON LONG 11R STA 680. FAB REPLACEMENT FITTING FROM 7075 T6 PLATE ON SAA SERVICE ORDER 7034927. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-21.Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844010Fitting · crackedINSPECTION TYPE: C1, LONGERON 3R END FITTING CRACKED IN MAIN CABIN, STA 902-920. REMOVED & REPLACED FITTING REF SRM 51-1-20D.Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844015Pressure Blkhd · crackedINSPECTION TYPE: C1, AFT PRESSURE BULKHEAD CRACKED AT LBL 35 NEAR LONG 11L. REMOVED EXISTING REPAIR AT SITE. CUT OUT DAMAGE. NDT VERIFIED. FAB-27 DOUBLER (SHT7075T6-.063), -25 DOUBLER (7075T6-.032), -9 FILLERS (7075T6-.050). TREAT, PRIME & INSTALL REPAIR Feb 20, 2005 · N805UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS05844115Longeron · crackedINSPECTION TYPE:C1 LONGERON 14R CRACKED UNDER CANTED FRAME AT STA 1756. REMOVED LONG SECTION, END FITTING, CLIP. FAB REPLACEMENT LONG SECTION (S1616757 EXTRUSION), 2 STRAPS (SHT7075T6-.080), SPLICE FITTING ON SVC ORDER 7034949 (S2645716 EXTRUSION). INSTALLEFeb 19, 2005 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844114Longeron · crackedINSPECTION TYPE:C1 LONGERON 15R CRACKED UNDER CANTED FRAME AT STA 1734 REMOVED LONG FROM 1725-1766, END FITTING, CLIP AT STA 1752. FAB REPLACEMENT LONG SECTIONS (S1616757 EXTRUSION), 2 SPLICE FITTINGS ON SERVICE ORDER 7034948 (S2645716 EXTRUSION), 4 REPAFeb 19, 2005 · N805UP · Doug DC873F · Fuselage Main, Longeron/Stringer
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