# Service difficulty reports: N705UP, cancelled Mar 30, 2010

A list on [N705UP, cancelled Mar 30, 2010](https://openairdocs.org/deregistered/N705UP-2010-03-30.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 4 · 188 reports

- [SDR UPS07851215](https://openairdocs.org/sdr/UPS07851215.md): Battery Pack · discharged · Nov 26, 2007 · N705UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, SYSTEM OPS CHECKS GOOD PER MM 33-50-01-2.
- [SDR UPS07850983](https://openairdocs.org/sdr/UPS07850983.md): Engine · flamed out · Oct 23, 2007 · N705UP · Doug DC871F · Engine (Turbine/Turboprop)
  > NNNDURING CRUISE FLT W/ENG ANTI-ICE ON (TAT -1), NR 4 ENGINE FLAMED OUT. ENG INDICATIONS WERE NORMAL. RESTART ACCOMPLISHED. ENG OPERATED NORMALLY FOR REMAINDER OF FLT. PERFORMED NR 4 ENG FLAME OUT T/S CHART PER AMM 71-00-00-1 FIG 139. INSPECTED CHIP DETEC
- [SDR UPS07850131](https://openairdocs.org/sdr/UPS07850131.md): Bulkhead · cracked · Jun 29, 2007 · N705UP · Doug DC871F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C3 MAIN CABIN AFT PRESS BULKHEAD CRACKED 2 INCHES LONG AT STA 1766 BETWEEN L10L AND L11L, LBL 30. CUT OUT DAMAGED AREA OF PRESS BULKHEAD STA 1766 L10L AND L11L IAW SRM 53-02-05 FIG 14A. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER,
- [SDR UPS07850212](https://openairdocs.org/sdr/UPS07850212.md): Floorbeam · cracked · Jun 26, 2007 · N705UP · Doug DC871F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C3 CRACKED FLOORBEAM SUPPORT FITTING FS 340 RBL 60 A-PIT DOOR UPPER CUTOUT L21 CUSP AREA. REMOVED AND REPLACED FLOORBEAM SUPPORT FITTING AT STA 340 RBL 60 IAW SRM 51-01-20D, DWG 9754022, AND SRM 51-3-2.
- [SDR UPS07850168](https://openairdocs.org/sdr/UPS07850168.md): Doubler · cracked · Jun 23, 2007 · N705UP · Doug DC871F · Leading Edge Devices
  > INSPECTION TYPE:C3 LT/WING OUTBOARD L/E INNER DOUBLER CRACKED AT STA XFS 597. REMOVED CRACKED INNER DOUBLER AT LT/WING OUTBOARD L/E AT STA XFS 597. FABRICATED AND INSTALLED REPAIR DOUBLER AT LT/WING OUTBOARD L/E STA XFS 597 IAW SRM 51-1-21, 51-1-4, AND DWG 5
- [SDR UPS07850123](https://openairdocs.org/sdr/UPS07850123.md): Door Frame · damaged · Jun 23, 2007 · N705UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C3 DOUBLE DRILLED HOLES IN WEB AT LWR AFT CORNER OF L2 DOOR JAMB STA 1667. TRIMMED OUT DAMAGED AREA OF WEB AND FRAME SEGMENT OF L2 DOOR LWR AFT CORNER DOOR JAMB IAW DWG DC8-53A-011. FABRICATED AND INSTALLED "J" ANGLE DOUBLER AT L2 DOOR LWR AF
- [SDR UPS07850088](https://openairdocs.org/sdr/UPS07850088.md): Doubler · cracked · Jun 23, 2007 · N705UP · Doug DC871F · Wing Main, Frame Structure
  > INSPECTION TYPE:C3 L/WING OUTBD L/E UPPER INNER DOUBLER CRACKED AT STA XW 761. REMOVED INNER DOUBLER ON L/WING OUTBD L/E AT STA XW 761 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON L/WING OUTBD L/E AT STA XW 761 IAW SRM 51-3-2, AND SRM 51-1-8.
- [SDR UPS07850053](https://openairdocs.org/sdr/UPS07850053.md): Rib · cracked · Jun 23, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE AT STA XFS 641 IS CRACKED. STOP DRILLED CRACK AT STA XFS 641 L/WING LEADING EDGE IAW SRM 57-2- 0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LEADING EDGE STA XFS 641 IAW SRM 57-03-01 FIG 006.
- [SDR UPS07850052](https://openairdocs.org/sdr/UPS07850052.md): Rib · cracked · Jun 23, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE RIB CRACKED AT STA XFS 672. STOP DRILLED CRACK AT STA XFS 672 L/WING LEADING EDGE IAW SRM 57-2- 0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 672 L/WING LEADING EDGE IAW SRM 57-03-01 FIG 006.
- [SDR UPS07850051](https://openairdocs.org/sdr/UPS07850051.md): Rib · cracked · Jun 23, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 L/WING OUTBD LEADING EDGE UPPER RIB CRACKED AT XFS 678. STOP DRILLED CRACK AT STA XFS 678 L/WING LEADING EDGE IAW SRM 57-02-00-0 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 678 L/WING LEADING EDGE IAW SRM 57-03-01-0 FIG 006
- [SDR UPS07850050](https://openairdocs.org/sdr/UPS07850050.md): Rib · cracked · Jun 23, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > C3 L/WING LEADING EDGE OUTBD LWR RIB CRACKED AT STA XFS 772. STOP DRILLED CRACK ON RIB AT STA XFS 772 L/WING LEADING EDGE IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 772 L/WING LEADING EDGE IAW SRM 57-03-01-0 FIG 007.
- [SDR UPS07850195](https://openairdocs.org/sdr/UPS07850195.md): Rib · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 697. STOP DRILLED CRACK AT XFS 697 RIGHT WING IAW SRM 51-1-21. INSTALLED DOUBLER IAW SRM 57-03-01 AND 57-02-00.
- [SDR UPS07850097](https://openairdocs.org/sdr/UPS07850097.md): Fitting · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 LONGERON END FITTING AT STA 1770 L10R IS CRACKED. REMOVED CRACKED END FITTING AT STA 1770 L10R IAW SRM 51-1-21. LOCATED, DRILLED-UP, AND INSTALLED LONGERON END FITTING AT STA 1770 L10R IAW SRM 51-1-20D.
- [SDR UPS07850096](https://openairdocs.org/sdr/UPS07850096.md): Doubler · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Leading Edge Devices
  > INSPECTION TYPE:C3 R/WING CENTER L/E INNER DOUBLER CRACKED AT DRAIN HOLE AT STA XFS 334. REMOVED CRACKED INNER DOUBLER AT R/WING STA XFS 334 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT R/WING L/E STA XFS 334 IAW SRM 57-03-01-0 FIG 004.
- [SDR UPS07850081](https://openairdocs.org/sdr/UPS07850081.md): Doubler · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing Main, Frame Structure
  > INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER AND LWR INNER DOUBLER CRACKED AT STA XW 761. REMOVED CRACKED DOUBLERS AT R/WIND L/E STA XW 761 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLERS AT R/WING L/E STA XW 761 IAW SRM 51-01-20D, AND DWG 5769545.
- [SDR UPS07850080](https://openairdocs.org/sdr/UPS07850080.md): Channel · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C3 R/WING CENTER L/E OUTBD T CHANNEL IS CRACKED. STOP DRILLED CRACKED T CHANNEL AT R/WING STA X 501 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE ON T CHANNEL IAW SRM 57-02-00 FIG 002.
- [SDR UPS07850079](https://openairdocs.org/sdr/UPS07850079.md): Rib · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 360. STOPPED DRILLED CRACKED RIB AT R/WING L/E STA XFS 360 IAW SRM 57-03 -03-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING STA XFS360 IAW SRM 57-03-03-0 FIG 2.
- [SDR UPS07850078](https://openairdocs.org/sdr/UPS07850078.md): Rib · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 R/WING CENTER L/E UPPER RIB CRACKED AT STA XFS 461 STOPPED DRILLED CRACK RIB AT STA XFS 461 IAW SRM 57-03-03-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 461 IAW SRM 57-03-0 3-0 FIG 7.
- [SDR UPS07850077](https://openairdocs.org/sdr/UPS07850077.md): Rib · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 L/WING OUTBD L/E LWR RIB CRACKED AT STA XFS 734. STOPPED DRILLED CRACKED RIB AT L/WING LE STA XFS 734 IAW SRM 57-02- 0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LE STA XFS 734 IAW SRM 57-03-03-0 FIG 7.
- [SDR UPS07850076](https://openairdocs.org/sdr/UPS07850076.md): Rib · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 816. STOPPED DRILLED CRACK AT R/WING L/E STA XFS 816 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING L/E STA XFS 816 IAW SRM 57-03-03-0 FIG 7, AND SRM 57-02-00-0 FIG 2.
- [SDR UPS07850075](https://openairdocs.org/sdr/UPS07850075.md): Rib · cracked · Jun 22, 2007 · N705UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 R/WING OUTBD L/E UPPER RIB CRACKED AT XFS 734. STOP DRILLED CRACK ON R/WING UPPER OUTBD L/E AT STA XFS 734 IAW SRM 57-03-03-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA XFS 734 R/WING L/E IAW SRM 57-03-03-0 FIG 7.
- [SDR UPS07850211](https://openairdocs.org/sdr/UPS07850211.md): Floorbeam · cracked · Jun 21, 2007 · N705UP · Doug DC871F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C3 INTERCOSTAL CORRODED AROUND AND UNDER NUT PLATE AT FS 50 AND RBL 30. REPAIRED INTERCOSTAL AND FLOORBEAM AT STA 55 RBL 10 TO RBL 28 IAW SAA EA 008-5310-01-A0946, UPS RAA DC8-53-20638, AND FAA FORM 8100-9.
- [SDR UPS07850149](https://openairdocs.org/sdr/UPS07850149.md): Cusp Web · cracked · Jun 21, 2007 · N705UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 L21L UPPER CUSP BETWEEN STA 1160-1140 CRACKED. CUT OUT CRACKED CUSP SEGMENT AT STA 1130-1160 L21L IAW SRM 53-02-05 FIG 15A. FABRICATED AND INSTALLED REPAIR CUSP SEGMENT, DOUBLERS AND FILLERS AT STA 1130-1160 L21L IAW SRM 53-02-05 FIG 15A.
- [SDR UPS07850095](https://openairdocs.org/sdr/UPS07850095.md): Skin · cracked · Jun 19, 2007 · N705UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CRACKED AT STA 1742 L17L. CUT OUT DAMAGED AREA OF FUSELAGE SKIN AT STA 1742 L17L IAW SRM 53-02-01-0 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLERS AT STA 1742 L17L IAW SRM 53-03-02-0 FIG
- [SDR UPS07850082](https://openairdocs.org/sdr/UPS07850082.md): Skin · cracked · Jun 19, 2007 · N705UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 R/WING INBD L/E (AUX TANK) INBD LWR CORNER CRACKED. CUT OUT DAMAGED AREA ON R/WING L/E AUX TANK IAW SRM 57-02-00 FIG 6. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/WING INDB L/E AUX TANK IAW SRM 57-03-00 FIG 3, AND SRM 51-01-26.
- [SDR UPS07850234](https://openairdocs.org/sdr/UPS07850234.md): Skin · cracked · Jun 18, 2007 · N705UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 LEFT WING UPPER FRONT SPAR SKIN CRACKED 2 INCHES LONG AT XRS -36.000. REPAIRED LEFT WING UPPER FRONT SPAR SKIN AT STA XRS -36.000 IAW SAA EA 008-5730-01-A0937, UPS EO DC8-5730-27267-A, AND FAA FORM 8100-9.
- [SDR UPS07850129](https://openairdocs.org/sdr/UPS07850129.md): Skin · dented · Jun 17, 2007 · N705UP · Doug DC871F · Elevator, Plate/Skin
  > INSPECTION TYPE:C3 LEFT ELEVATOR LWR INBOARD SKIN HAS DEEP DENT. CUT OUT DAMAGED AREA ON L/ELEV INBOARD SKIN IAW SRM 55-02-01 FIG 010, FABRICATED AND INSTALLED REPAIR DOUBLER ON L/ELEV INBOARD LWR SKIN IAW SRM 55-02-01 FIG 010.
- [SDR UPS07850124](https://openairdocs.org/sdr/UPS07850124.md): Skin · canning · Jun 17, 2007 · N705UP · Doug DC871F · Elevator, Plate/Skin
  > INSPECTION TYPE:C3 L/ELEVATOR UPPER MIDDLE SKIN HAS OIL CANNING ON O/B SIDE. CUT OUT DAMAGED SKIN SECTION FROM L/ELEVATOR, UPPER MIDDLE STA 219 - 234 IAW SRM 55-02-01 FIG 008. FABRICATED AND INSTALLED SKIN SEGMENT ON L/ELEVATOR STA 219 - 234.5 IAW DWG 565497
- [SDR UPS07849967](https://openairdocs.org/sdr/UPS07849967.md): Window · dirty · Jun 13, 2007 · N705UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A ESCAPE SLIDE VIEWING WINDOW INOP. REMOVED COVER FROM SLIDE. CLEANED WINDOW, SECURED SLIDE TO DOOR & VERIFIED PROPER CYLINDER PRESSURE, REF MM 25-60-01-2.
- [SDR UPS07849724](https://openairdocs.org/sdr/UPS07849724.md): Battery Pack · weak · Apr 30, 2007 · N705UP · Doug DC871F · Emergency Lighting
  > DURING PDC, FOUND EMERGENCY LIGHTING DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. OPS CHECK GOOD.
- [SDR UPS07849499](https://openairdocs.org/sdr/UPS07849499.md): Indicator · dislodged · Mar 14, 2007 · N705UP · Doug DC871F · Escape Slide
  > DOOR SLIDE PRESS INDICATOR SLIDE OUT OF SIGHT. CANNOT READ. REPACKED/REPOSITIONED SLIDE INDICATOR, NOW IN VIEW.
- [SDR UPS06848800](https://openairdocs.org/sdr/UPS06848800.md): Light · inoperative · Dec 23, 2006 · N705UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A CENTER LIGHT UNDER GLARESHIELD FOR EMERGENCY LIGHT ARM INOP. ACCOMPLISHED OPERATIONAL TEST, NO DISCREPANCY NOTED IAW MM 33-50-01.
- [SDR UPS06847708](https://openairdocs.org/sdr/UPS06847708.md): Gauge · out of position · Aug 15, 2006 · N705UP · Doug DC871F · Escape Slide
  > FOUND ESCAPE SLIDE PRESSURE GAUGE NOT IN VIEW. REPOSITIONED SLIDE PACK. OK FOR SERVICE.
- [SDR UPS06847184](https://openairdocs.org/sdr/UPS06847184.md): Coalescer Bag · dirty · Jun 22, 2006 · N705UP · Doug DC871F · Humidity Control System
  > INSPECTION TYPE:N/A STRONG BURNING ODOR WHEN LEFT PACK OPERATED WITH MIX VALVE IN FULL COLD POSITION. REMOVED AND CLEANED LT PACK COALESCER BAG IAW MM 21-55-03-2. RAN PACK WITH NO ODOR NOTED. A/C OK TO CONTINUE.
- [SDR UPS06845928](https://openairdocs.org/sdr/UPS06845928.md): Smoke Goggles · scratched · Jan 9, 2006 · N705UP · Doug DC871F · Emergency Equipment
  > F/O SMOKE GOGGLES SCRATCHED. REPLACED F/O SMOKE GOGGLES. OPS NORMAL.
- [SDR UPS06845925](https://openairdocs.org/sdr/UPS06845925.md): Skin · corroded · Jan 7, 2006 · N705UP · Doug DC871F · Fuselage Main, Plate/Skin
  > FUSELAGE HAS A BULGED AREA 25" FWD OF PIT 31 LWR FWD CORNER MARKED AND ADVISED BY MX. GAINED ACCESS TO THE BACKSIDE OF AREA NO CORROSION OR DEFECTS FOUND AT THIS TIME AS PER SRM 51-1-0. OK FOR SERVICE, AREA FOUND TO BE FREE AND SMOOTH.
- [SDR UPS05844805](https://openairdocs.org/sdr/UPS05844805.md): Intercostal · corroded · Jun 25, 2005 · N705UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-2, INTERCOSTAL AT STA 980 HAS CORROSION. CORROSION OUT OF LIMITS PER SRM 53-2-0. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-21, AND SRM 51-1-20D.
- [SDR UPS05844803](https://openairdocs.org/sdr/UPS05844803.md): Longeron · cracked · Jun 20, 2005 · N705UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C-2, LONGERON 24L CRACKED ON O/B FLANGE. REMOVED AND REPLACED LONGERON 24L IAW SRM 51-3-2, 51-1-8, AND 51-1-20D.
- [SDR UPS05844771](https://openairdocs.org/sdr/UPS05844771.md): Fitting · cracked · Jun 8, 2005 · N705UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C-2. BANANA FITTING CRACKED AT STA 340 L33R. REMOVED AND REPLACED BANANA FITTING AT STA 340 L33R IAW SRM 51-1-20D.
- [SDR UPS05844770](https://openairdocs.org/sdr/UPS05844770.md): Frame · corroded · Jun 8, 2005 · N705UP · Doug DC871F · Fuselage Main, Frame
  > INSPECTION TYPE:C-2. MAIN CARGO STA 1700 RBL 24 SEVERE CORROSION AT TOP OF FRAME ON UNDERSIDE AND CONTINUES OUTBD TO RBL48. CUT OUT DAMAGED AREA PER SRM 51-2-1 FIG 1, SHEET 7. FABRICATED REPAIR REPAIR DOUBLER AND REPAIR ANGLES IAW SRM 51-1-21 FIG 1, AND INS
- [SDR UPS05844767](https://openairdocs.org/sdr/UPS05844767.md): Seat Track · corroded · Jun 8, 2005 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C-2. HEAVY CORROSION IN SEAT TRACK ALONG RBL 59 STA 375-420. REMOVED AND FABRICATED SEAT TRACK PER DWG S2400463. INSTALLED FABBED SEAT TRACK AT STA 375-420 PER SRM 53-2-3.
- [SDR UPS05844766](https://openairdocs.org/sdr/UPS05844766.md): Fitting · corroded · Jun 8, 2005 · N705UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C-2. A-PIT AT STA 320 L33R, BATH TUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED BATH TUB FITTING AT A-PIT STA 320 L33R IAW SRM 53-2-0 FIG 1F, 51-1-20D, AND 51-1-21.
- [SDR UPS05844763](https://openairdocs.org/sdr/UPS05844763.md): Seat Track · corroded · Jun 8, 2005 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > C2 SEAT TRACK HEAVILY CORRODED AT STA 420 LBL 25. REMOVED AND REPLACED SEAT TRACK AT STA 360-560 LBL 25 IAW SRM 51-3-0, 51-3-2, 53B-003-501.
- [SDR UPS05844761](https://openairdocs.org/sdr/UPS05844761.md): Seat Track · corroded · Jun 8, 2005 · N705UP · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS HEAVY CORROSION, STA 1480 RBL 50. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1460-1580 RBL 50 IAW SRM 51-3-0.
- [SDR UPS05844935](https://openairdocs.org/sdr/UPS05844935.md): Fitting · cracked · Jun 7, 2005 · N705UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C2, B-PIT BETWEEN STA 460-440 L28R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IN B-PIT AT STA 460-440, L28R IAW SRM 51-1-21D AND SRM 51-1-21
- [SDR UPS05844772](https://openairdocs.org/sdr/UPS05844772.md): Skin · damaged · Jun 7, 2005 · N705UP · Doug DC871F · Rudder, Plate/Skin
  > INSPECTION TYPE:C-2. UPPER PORTION OF RUDDER ON RT SIDE JUST ABOVE LOGO, OIL CANNING OF SKIN. REMOVED AND REPLACED SKIN ON RT SIDE OF RUDDER JUST ABOVE LOGO IAW DC8 DWG 5655077 AND SRM 51-1-8, AND 51-1-21A. NO WEIGHT AND BALANCE DUE TO 1FOR 1 SKIN CHANGE.
- [SDR UPS05844768](https://openairdocs.org/sdr/UPS05844768.md): Floor Support · cracked · Jun 7, 2005 · N705UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-2. MAIN CABIN STA 759 LBL24 UNDER SEAT TRACK. SEAT TRACK FLOOR SUPPORT FITTING CRACKED. REMOVED AND REPLACED SUPPORT FITTING AT STA 759 LBL24 IAW 51-1-20D, AND 51-3-0.
- [SDR UPS05844769](https://openairdocs.org/sdr/UPS05844769.md): Fitting · corroded · Jun 5, 2005 · N705UP · Doug DC871F · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE C-2, CORNER FITTING CRACKED AND HEAVILY CORRODED, RT W/W STA 980 CEILING O/B CORNER NEXT TO L24R. REMOVED FITTING IAW SRM 51-1-20D. FABRICATED DOUBLER, REPAIR ANGLE AND FILLERS IAW SRM 53-02-00-0, INSTALLED DOUBLER REPAIR ANGLE AND FILLERS IA
- [SDR UPS05844765](https://openairdocs.org/sdr/UPS05844765.md): Skin · cracked · Jun 5, 2005 · N705UP · Doug DC871F · Elevator, Plate/Skin
  > INSPECTION TYPE:C-2. LT ELEVATOR CONTROL TAB SKIN AND DOUBLER CRACKED AT INBD EYEBOLT ACCESS HOLE LWR SKIN. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB ASSY PER TASK CARD 3016 STEP 13.
- [SDR UPS05844762](https://openairdocs.org/sdr/UPS05844762.md): Rib · cracked · Jun 5, 2005 · N705UP · Doug DC871F · Horizontal Stabilizer, Spar/Rib
  > LT HORIZ STAB L/E 2ND INBD LWR RIB REPAIR HAS DOUBLER AND TRIPLER CRACKED. REMOVED, FABRICATED, AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 55-2-0, 51-1-21, AND SRM 55-2-0 FIG 2.

Next page: https://openairdocs.org/deregistered/N705UP-2010-03-30/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 = 'N705UP' AND deregistration_id = 'N705UP-2010-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N705UP-2010-03-30/reports

---
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