# Service difficulty reports: N805UP, cancelled May 6, 2010

A list on [N805UP, cancelled May 6, 2010](https://openairdocs.org/deregistered/N805UP-2010-05-06.md).

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

Page 1 of 5 · 246 reports

- [SDR UPS08853860](https://openairdocs.org/sdr/UPS08853860.md): Door Seal · obstructed · Nov 5, 2008 · N805UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION 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 CARGO
- [SDR UPS08853469](https://openairdocs.org/sdr/UPS08853469.md): Skin · cracked · Oct 4, 2008 · N805UP · Doug DC873F · Fuselage Main, Plate/Skin
  > CRACK 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 DC8
- [SDR UPS08852235](https://openairdocs.org/sdr/UPS08852235.md): Engine · flamed out · May 13, 2008 · N805UP · Doug DC873F · Engine (Turbine/Turboprop)
  > INSPECTION 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 MOTO
- [SDR UPS08852164](https://openairdocs.org/sdr/UPS08852164.md): Door · binding · May 3, 2008 · N805UP · Doug DC873F · Emergency Exits
  > LT OVERWING EMERGENCY EXIT DOOR BINDING. LUBRICATED SEAL AND ALL MOVING PARTS IAW MM 12-80-00. OPS CHECK GOOD.
- [SDR UPS08851764](https://openairdocs.org/sdr/UPS08851764.md): Packing · unknown · Mar 6, 2008 · N805UP · Doug DC873F · Engine Starter
  > IFSD - 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
- [SDR UPS08851718](https://openairdocs.org/sdr/UPS08851718.md): Bottle · low pressure · Feb 26, 2008 · N805UP · Doug DC873F · Escape Slide
  > ESCAPE SLIDE PRESSURE OUT OF GREEN BAND. DEFERRED PER MEL 52-7-4. REMOVED AND REPLACED EVACUATION SLIDE ASSY PER AMM 25-60-01-2.
- [SDR UPS08851577](https://openairdocs.org/sdr/UPS08851577.md): Skin · cracked · Jan 26, 2008 · N805UP · Doug DC873F · Passenger/Crew Doors
  > SKIN 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.
- [SDR UPS07850685](https://openairdocs.org/sdr/UPS07850685.md): Slide · out of position · Sep 18, 2007 · N805UP · Doug DC873F · Escape Slide
  > INSPECTION 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.
- [SDR UPS07850163](https://openairdocs.org/sdr/UPS07850163.md): Slide · out of position · Jul 11, 2007 · N805UP · Doug DC873F · Escape Slide
  > INSPECTION TYPE:N/A RESTOW ESCAPE SLIDE. RESTOWED ESCAPE SLIDE IAW MM 25-60-01-2.
- [SDR UPS07849751](https://openairdocs.org/sdr/UPS07849751.md): Skin · misrepaired · May 1, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION 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 EO
- [SDR UPS07849744](https://openairdocs.org/sdr/UPS07849744.md): Cusp Web · cracked · Apr 7, 2007 · N805UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS07849626](https://openairdocs.org/sdr/UPS07849626.md): Floorbeam · cracked · Apr 2, 2007 · N805UP · Doug DC873F · Fuselage Main, Floor Beam
  > INSPECTION 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.
- [SDR UPS07849618](https://openairdocs.org/sdr/UPS07849618.md): Rib · cracked · Mar 31, 2007 · N805UP · Doug DC873F · Rudder, Spar/Rib
  > INSPECTION 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.
- [SDR UPS07849617](https://openairdocs.org/sdr/UPS07849617.md): Rib · cracked · Mar 31, 2007 · N805UP · Doug DC873F · Rudder, Spar/Rib
  > INSPECTION 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.
- [SDR UPS07849611](https://openairdocs.org/sdr/UPS07849611.md): Attach Angle · cracked · Mar 31, 2007 · N805UP · Doug DC873F · Vertical Stabilizer, Attach Fittings
  > INSPECTION 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
- [SDR UPS07849639](https://openairdocs.org/sdr/UPS07849639.md): Skin · corroded · Mar 30, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION 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, AND
- [SDR UPS07849631](https://openairdocs.org/sdr/UPS07849631.md): Skin · cracked · Mar 30, 2007 · N805UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION 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 INSTALLED
- [SDR UPS07849725](https://openairdocs.org/sdr/UPS07849725.md): Fitting · cracked · Mar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION 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 IA
- [SDR UPS07849628](https://openairdocs.org/sdr/UPS07849628.md): Longeron · cracked · Mar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION 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.
- [SDR UPS07849619](https://openairdocs.org/sdr/UPS07849619.md): Bulkhead · corroded · Mar 29, 2007 · N805UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION 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.
- [SDR UPS07849585](https://openairdocs.org/sdr/UPS07849585.md): Frame · cracked · Mar 28, 2007 · N805UP · Doug DC873F · Horizontal Stabilizer, Spar/Rib
  > INSPECTION 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.
- [SDR UPS07849584](https://openairdocs.org/sdr/UPS07849584.md): Frame · cracked · Mar 28, 2007 · N805UP · Doug DC873F · Horizontal Stabilizer, Spar/Rib
  > INSPECTION 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.
- [SDR UPS07849635](https://openairdocs.org/sdr/UPS07849635.md): Door Frame · damaged · Mar 24, 2007 · N805UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION 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 FI
- [SDR UPS07849627](https://openairdocs.org/sdr/UPS07849627.md): Door Frame · damaged · Mar 24, 2007 · N805UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION 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.
- [SDR UPS06848810](https://openairdocs.org/sdr/UPS06848810.md): Skin · gouged · Dec 28, 2006 · N805UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR UPS06846909](https://openairdocs.org/sdr/UPS06846909.md): Light · inoperative · May 11, 2006 · N805UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A ON SHUTDOWN EMERGENCY EXIT LIGHTS DISARM CHECK FAIL TO GIVE PROPER INDICATION. LIGHT SHOULD ILLUMINATE. RELAMPED, OPS CHECKS GOOD.
- [SDR UPS06846753](https://openairdocs.org/sdr/UPS06846753.md): Smoke Goggles · scratched · Apr 25, 2006 · N805UP · Doug DC873F · Emergency Equipment
  > F/O'S SMOKE GOGGLES SCRATCHED AND FOGGY. REPLACED CAPTAIN'S SMOKE GOGGLES PER 25-60-05-2.
- [SDR UPS06846270](https://openairdocs.org/sdr/UPS06846270.md): Battery Pack · discharged · Feb 23, 2006 · N805UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A ON PREFLIGHT FOUND EMERGENCY EXIT LIGHTS OVER ENTRY DOOR & IN COMPANION WAY OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKS OK.
- [SDR UPS05844379](https://openairdocs.org/sdr/UPS05844379.md): Wire · pulled · Apr 26, 2005 · N805UP · Doug DC873F · Light System Wiring
  > NO 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.
- [SDR UPS05844119](https://openairdocs.org/sdr/UPS05844119.md): Fitting · cracked · Feb 24, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 LONGERON 10L END FITTING CRACKED AT STA 1770. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D.
- [SDR UPS05844117](https://openairdocs.org/sdr/UPS05844117.md): Doubler · cracked · Feb 23, 2005 · N805UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION 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.
- [SDR UPS05844159](https://openairdocs.org/sdr/UPS05844159.md): Seat Track · corroded · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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 SECTION
- [SDR UPS05844120](https://openairdocs.org/sdr/UPS05844120.md): Seat Track · worn · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION 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 FLOO
- [SDR UPS05844116](https://openairdocs.org/sdr/UPS05844116.md): Skin · cracked · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION 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 S
- [SDR UPS05844021](https://openairdocs.org/sdr/UPS05844021.md): Finger Doubler · corroded · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION 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-.050
- [SDR UPS05844019](https://openairdocs.org/sdr/UPS05844019.md): Fitting · cracked · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, FITTING CRACKED UNDER FLOORBEAM, STA 700 RBL 24 MAIN CABIN. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D.
- [SDR UPS05844016](https://openairdocs.org/sdr/UPS05844016.md): Attach Angle · cracked · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage, Wing Attach Fittings
  > INSPECTION 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 TC
- [SDR UPS05844014](https://openairdocs.org/sdr/UPS05844014.md): Fitting · cracked · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION 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.
- [SDR UPS05844012](https://openairdocs.org/sdr/UPS05844012.md): Fitting · cracked · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C1, BATH-TUB FITTING CRACKED ON LONG 4R, STA 902. REMOVED AND REPLACED FITTING REF SRM 51-1-20D.
- [SDR UPS05844011](https://openairdocs.org/sdr/UPS05844011.md): Support Fitting · cracked · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION 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.
- [SDR UPS05844009](https://openairdocs.org/sdr/UPS05844009.md): Floor Support · cracked · Feb 22, 2005 · N805UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION 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.
- [SDR UPS05844158](https://openairdocs.org/sdr/UPS05844158.md): Longeron · cracked · Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION 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.
- [SDR UPS05844121](https://openairdocs.org/sdr/UPS05844121.md): Angle · cracked · Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION 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.
- [SDR UPS05844113](https://openairdocs.org/sdr/UPS05844113.md): Fitting · cracked · Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION 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.
- [SDR UPS05844022](https://openairdocs.org/sdr/UPS05844022.md): Clip · cracked · Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION 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.
- [SDR UPS05844020](https://openairdocs.org/sdr/UPS05844020.md): Fitting · cracked · Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION 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.
- [SDR UPS05844010](https://openairdocs.org/sdr/UPS05844010.md): Fitting · cracked · Feb 21, 2005 · N805UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, LONGERON 3R END FITTING CRACKED IN MAIN CABIN, STA 902-920. REMOVED & REPLACED FITTING REF SRM 51-1-20D.
- [SDR UPS05844015](https://openairdocs.org/sdr/UPS05844015.md): Pressure Blkhd · cracked · Feb 20, 2005 · N805UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION 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
- [SDR UPS05844115](https://openairdocs.org/sdr/UPS05844115.md): Longeron · cracked · Feb 19, 2005 · N805UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION 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). INSTALLE
- [SDR UPS05844114](https://openairdocs.org/sdr/UPS05844114.md): Longeron · cracked · Feb 19, 2005 · N805UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION 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 REPA

Next page: https://openairdocs.org/deregistered/N805UP-2010-05-06/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N805UP-2010-05-06/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.