# Service difficulty reports: N802UP, cancelled Jul 2, 2010

A list on [N802UP, cancelled Jul 2, 2010](https://openairdocs.org/deregistered/N802UP-2010-07-02.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 6 · 268 reports

- [SDR UPS09854304](https://openairdocs.org/sdr/UPS09854304.md): Girt Bar · broken · Jan 7, 2009 · N802UP · Doug DC873F · Emergency Equipment
  > EMERGENCY ESCAPE SLIDE INOP, GIRT BAR CLIP BROKEN. REPLACED FWD GIRT BAR CLIP IAW DPS 1.07-2.
- [SDR UPS09854279](https://openairdocs.org/sdr/UPS09854279.md): Latch · broken · Jan 3, 2009 · N802UP · Doug DC873F · Escape Slide
  > ESCAPE SLIDE CONTAINER CLOSURE CLIP BROKEN CONTAINER WILL NOT STAY CLOSED. M391960, DEFERRED IAW MEL 52-7-4. REMOVED SLIDE AND SECURED ENCLOSURE PLACARD INSTALLED. OPEN
- [SDR UPS08854080](https://openairdocs.org/sdr/UPS08854080.md): Engine · flamed out · Dec 2, 2008 · N802UP · Doug DC873F · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT. ENGINE RELIT ON IT'S OWN. PERFORMED FIRST FOUR STEPS OF DC-8 M/M 71-00-00-1 FIG 139 UP TO INSPECT FUEL FILTER. FILTER KIT ON ORDER. REPLACED NR 3 FUEL FILTER PER AMM 73-10-02-4. LEAK CHECK OK. ACCOMPLISHED STEP
- [SDR UPS08852457](https://openairdocs.org/sdr/UPS08852457.md): Floorboard · damaged · Jun 8, 2008 · N802UP · Doug DC873F · Fuselage Floor Panel
  > INSPECTION TYPE:C2 FLOORBOARD F81 HAS ONE EACH SCREW HOLE BROKEN OUT. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-3 FIG 10, 51-1-8, 51-1-21, 51-1-16.
- [SDR UPS08852570](https://openairdocs.org/sdr/UPS08852570.md): Support Angle · chafed · Jun 5, 2008 · N802UP · Doug DC873F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C2 RT WING INBD SLOT VANE HAS A DEEP CHAFING MARK AT SUPPORT ANGLE AT OTBD SIDE. REMOVED AND REPLACED SUPPORT ANGLE IAW AMM, 51-1-24, 27-80-00.
- [SDR UPS08852572](https://openairdocs.org/sdr/UPS08852572.md): Intercostal · cracked · Jun 4, 2008 · N802UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 INTERCOSTAL CRACKED AT STA -84 L21L BELOW SUB-FLOOR. REMOVED AND REPLACED INTERCOSTAL IAW, SRM, 51-1-20D,51-1-8, 51-1-21
- [SDR UPS08852432](https://openairdocs.org/sdr/UPS08852432.md): Skin · gouged · May 31, 2008 · N802UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE:C2 C-PIT CROSS SLIDE DOOR INTERIOR SKIN IS GOUGED, FWD LWR AREA. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-21, 52-2-0 FIG 2.
- [SDR UPS08852567](https://openairdocs.org/sdr/UPS08852567.md): Attach Fitting · corroded · May 30, 2008 · N802UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 C PIT STA 1230 L27L ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED LONGERON ATTACH FITTING IAW DC8 SRM 51-01-20D.
- [SDR UPS08852566](https://openairdocs.org/sdr/UPS08852566.md): Fitting · cracked · May 30, 2008 · N802UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 D PIT STA 1360 L35L SPLICE FITTING CRACKED AND CORRODED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-03-01 AND 51-01-20D.
- [SDR UPS08852733](https://openairdocs.org/sdr/UPS08852733.md): Attach Angle · cracked · May 29, 2008 · N802UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE-C2 POSSIBLE CRACK IN RADIUS OF INTERCOSTAL ATTACH ANGLE, AT BOTTOM J-BEAM, AFT SIDE OF APB, 60 COMPT RT BS 1771. REMOVED INTERCOSTAL ATTACH ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANGLE. IAW DWG 5773844 AND SRM 51-1-21,51-3-00 AND 51-1-2
- [SDR UPS08852414](https://openairdocs.org/sdr/UPS08852414.md): Shear Tie · cracked · May 29, 2008 · N802UP · Doug DC873F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:C2 LARGE SHEAR TIE CRACKED IN RADIUS, 60 COMARTMENT CEILING, STA 1800 L4R. STOP DRILLED, FABBED AND INSTALLED REPAIR ANGLE IAW, SRM 51-1-21, 53-2 -0, 51-1-8, 53-5-03, 51-1-20D.
- [SDR UPS08852438](https://openairdocs.org/sdr/UPS08852438.md): Fitting · corroded · May 29, 2008 · N802UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 END FITTING BLOWN OUT, L30L, STA 1759 DIFFICULT ACCESS. REMOVED AND REPLACED CORRODED FITTING IAW SRM 51-1-21, 51-1-8, 51-1-24, 51-3-0.
- [SDR UPS08852577](https://openairdocs.org/sdr/UPS08852577.md): Attach Fitting · corroded · May 28, 2008 · N802UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 AFT ACCESSORY COMPT STA 1580, L21L FLOORBEAM ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED END FITTING IAW SRM, 51-1-8, 51-1-20D, 51-3-1.
- [SDR UPS08852603](https://openairdocs.org/sdr/UPS08852603.md): Frame · corroded · May 28, 2008 · N802UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C2 FLIGHT DECK STA -52 RT SIDE FRAME HAS CORROSION BY SUBFLOOR AREA. REPAIRED FLT DECK FRAME AT STA -52 AND SUBFLOOR AREA IAW EA 008- 5310-01-A1403.
- [SDR UPS08852427](https://openairdocs.org/sdr/UPS08852427.md): Skin · gouged · May 28, 2008 · N802UP · Doug DC873F · Elevator, Plate/Skin
  > INSPECTION TYPE:C2 RIGHT ELEVATOR UPPER SKIN IS DENTED AND GOUGED, FWD OF GEARED TAB. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-0, 55 51-1-8, 53-1-8, 55-2-0 FIG 10.
- [SDR UPS08852571](https://openairdocs.org/sdr/UPS08852571.md): Longeron · cracked · May 28, 2008 · N802UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 MAIN CABIN, L-15L CRACKED AT CANT FRAME STA 1746. REMOVED, FABBED AND INSTALLED LONGERON SLICE IAW SRM, 51-1-8, 53-2-2 FIG 10, 53-5-1 FIG 7, 51-1-20D.
- [SDR UPS08852568](https://openairdocs.org/sdr/UPS08852568.md): Skin · corroded · May 28, 2008 · N802UP · Doug DC873F · Rudder, Plate/Skin
  > INSPECTION TYPE:C2 RUDDER RT SIDE EXTERIOR SKIN HAS CORROSION, POPPED RIVETS AND BEADED SKIN IS SEPARATED. REMOVED AND REPLACED 2 RUDDER SKINS IAW DC8 SRM 51-1-21, 51-1-21A, AND51-01-22.
- [SDR UPS08852565](https://openairdocs.org/sdr/UPS08852565.md): Seat Track · worn · May 27, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK STA 1460, 0BL 2 EACH HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK PLUG IAW SRM, 51-3-00.
- [SDR UPS08852564](https://openairdocs.org/sdr/UPS08852564.md): Seat Track · worn · May 27, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C2 COPILOT REAR LT AND RT SEAT TRACKS SHOWS ELONGATION. REMOVED AND REPLACED SEAT TRACKS IAW SRM, 51-1-20D, 51-3-1, 51-1-24 AN D 25-11-1.
- [SDR UPS08852578](https://openairdocs.org/sdr/UPS08852578.md): Hinge Fitting · gouged · May 25, 2008 · N802UP · Doug DC873F · Spoilers
  > INSPECTION TYPE:C2 LEFT WING NR 1 SPOILER HINGE FITTING GOUGED NEAR STA XW38. REMOVED AND REPLACED HINGE FITTING IAW SRM, 51-1-8, 51-3-0, 51-3-2.
- [SDR UPS08852444](https://openairdocs.org/sdr/UPS08852444.md): Structure · damaged · May 25, 2008 · N802UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 MAIN CABIN, FLOORBOARD TIEDOWN BULGED AND FASTENERS PULLING STA 350 LBL 35. REMOVED, DAMAGED RECEPTICLE, FABBED AND INSTALLED REPAIR DOUBLER ON FLOOR PANEL, INSTALLED NEW RECEPTICLE IAW SRM 51-1-8, 53-2-3 FIG 1F, 51-1 -21A, 51-1-11.
- [SDR UPS08852536](https://openairdocs.org/sdr/UPS08852536.md): Floorboard · cracked · May 25, 2008 · N802UP · Doug DC873F · Fuselage Floor Panel
  > INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD CRACKED, STA 45 RBL 47. FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 53-2-00, 53-2-3, 510108, 51-1-26, 51-1-21.
- [SDR UPS08852606](https://openairdocs.org/sdr/UPS08852606.md): Fitting · cracked · May 24, 2008 · N802UP · Doug DC873F · Main Landing Gear
  > INSPECTION TYPE:C2 RIGHT WHEEL WELL AT UPPER FWD BULKHEAD, HYDRAULIC MANIFOLD PULLEY BRACKET IS CRACKED. REMOVED CRACKED FITTING, REPAIRED AND RE-INSTALLED FITTING IAW SRM 20-16-0, 51-1-8, DPS 4.706, DPS9.18.
- [SDR UPS08852433](https://openairdocs.org/sdr/UPS08852433.md): Seat Track · damaged · May 24, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C2 COCKPIT, SECOND OBSERVER SEAT TRACKS SHOW ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-3-0, 51-1-2, 51-1-8.
- [SDR UPS08852462](https://openairdocs.org/sdr/UPS08852462.md): Seat Track · worn · May 24, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C2 COCKPIT SECOND OBSERVER SEAT TRACKS SHOWS ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-8, 51-3-0, 51-1-24.
- [SDR UPS08852535](https://openairdocs.org/sdr/UPS08852535.md): Seat Track · worn · May 24, 2008 · N802UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C2 PILOT REAR LT AND RT SEAT TRACKS SHOW ELONGATIONS REMOVED AND REPLACED 2 EACH SEAT TRACKS IAW SRM, 51-1-20D, 51-1-24.
- [SDR UPS08852463](https://openairdocs.org/sdr/UPS08852463.md): Frame · chafed · May 23, 2008 · N802UP · Doug DC873F · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION TYPE:C2 NR 2 PYLON UPPER PANEL FRAME, WORN BEYOND LIMITS, DEEP CHAFED DAMAGE BETWEEN PANELS 293A/B AND 294A/B. FABBED AND INSTALLED NEW PANEL FRAME IAW SRM, 51-1-8, 51-1-20D, 51-1-2 1, 54-3-3 FIG 7.
- [SDR UPS08852461](https://openairdocs.org/sdr/UPS08852461.md): Fitting · cracked · May 22, 2008 · N802UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 MAIN CARGO COMP STA 980, L22R ATTACHING FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20, 51-1-20D, 51-1-8.
- [SDR UPS08852579](https://openairdocs.org/sdr/UPS08852579.md): Flap · damaged · May 21, 2008 · N802UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:C2 INTERIM REPAIR TO RT INBOARD FLAP AT TRAILING EDGE XM-75. REMOVED INTERIM REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-21A, 51-1-8, 51-1-9A.
- [SDR UPS08852022](https://openairdocs.org/sdr/UPS08852022.md): Bulb · inoperative · Apr 13, 2008 · N802UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT THE C1 DOOR HAS 2 BULBS OUT. REMOVED AND REPLACED 2 BULBS FOR THE EMERGENCY EXIT LIGHTING AS NEEDED.
- [SDR UPS08851978](https://openairdocs.org/sdr/UPS08851978.md): Limiter · inoperative · Apr 8, 2008 · N802UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS DISARM LIGHT WAS NOT ILLUMINATED. FOUND BATTERY BUS 30 AMP CURRENT LIMITER BAD. REPLACED SAME AND PERFORMED EMERGENCY LIGHT TEST IAW DC8 AMM 33-50-01-2. SYS OPS CKS NORMAL.
- [SDR UPS08851880](https://openairdocs.org/sdr/UPS08851880.md): Door · cracked · Mar 16, 2008 · N802UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE:N/A PIT 32 DOOR CRACKED. ACCOMPLISHED HFEC INSPECTION PER EO DC8-5230-28827 PAR 6 A2. ACCOMPLISHED STOP DRILL PER EO DC8-5230-28827 PAR 6 A3-A4. NEEDS HFEC. ALSO REMOVED MOUNT BOLTS & 2 EA RIVETS FOR ACCESS. PERFORMED EDDY CURRENT ON STOP
- [SDR UPS08851552](https://openairdocs.org/sdr/UPS08851552.md): Light · inoperative · Jan 24, 2008 · N802UP · Doug DC873F · Emergency Lighting
  > GLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD.
- [SDR UPS07851217](https://openairdocs.org/sdr/UPS07851217.md): Engine · flamed out · Nov 27, 2007 · N802UP · Doug DC873F · Engine (Turbine/Turboprop)
  > NR 3 ENGINE FLAME OUT. INFLIGHT RESTART ACCOMPLISHED AFTER DESCENT TO FL220. NORMAL ENGINE INDICATIONS AFTER RESTART. A/C IS CURRENTLY OUT OF SERVICE. PERFORMED DC8 MM71-00-00-1, FIG 139 AS REQUIRED. REF LP 887083/1,2,3 LOG PAGE 887084 ITEM 1,2,3. NR 3 EN
- [SDR UPS07851100](https://openairdocs.org/sdr/UPS07851100.md): Battery · weak · Nov 6, 2007 · N802UP · Doug DC873F · Emergency Lighting
  > EMERGENCY 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.
- [SDR UPS07850639](https://openairdocs.org/sdr/UPS07850639.md): Door · loose · Sep 11, 2007 · N802UP · Doug DC873F · Emergency Equipment
  > INSPECTION TYPE:N/A CAPT ESCAPE ROPE DOOR LOOSE, ROPE FELL OUT. ROLLED, INSTALLED ESCAPE ROPE. RESECURED ESCAPE ROPE DOOR, OK TO CONTINUE.
- [SDR UPS07849225](https://openairdocs.org/sdr/UPS07849225.md): Light · faulty · Feb 20, 2007 · N802UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT DISARM. RELAMPED DISARM INDICATION LIGHT. OPS CHECK OK.
- [SDR UPS07849215](https://openairdocs.org/sdr/UPS07849215.md): Switch · stiff · Feb 18, 2007 · N802UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH HARD TO MOVE TO DISARM CHECK POSITION. REPLACED EMERGENCY EXIT LIGHT SWITCH PER IPC 33-50-00-003. OPS CHECK OK PER AMM 33-50-00-0.
- [SDR UPS06848716](https://openairdocs.org/sdr/UPS06848716.md): Packing · worn · Nov 23, 2006 · N802UP · Doug DC873F · Engine Fuel Distribution
  > INSPECTION TYPE:N/A FLIGHT LEVEL 370.79 MACH AT CRUISE ENGINE 3 FLAMED OUT AND WITH IGNITION ON RESTARTED ALL INDICATIONS NORMAL. PERFORMED AMM 71-00-00-1 UP TO ENG RUN. SUBSEQUENT STEPS OF THE ENGINE FLAMEOUT TROUBLESHOOTING TREE ARE NOT REQUIRED DUE TO R/
- [SDR UPS06848567](https://openairdocs.org/sdr/UPS06848567.md): Bar · defective · Nov 9, 2006 · N802UP · Doug DC873F · Flight Compartment Windows
  > CAPTAIN'S CLEARVIEW WINDOW STUCK CLOSED. REMOVED AND REPLACED CAPT'S SLIDING WINDOW UPPER LOCK BAR W/REF TO DC8 AMM 56-10-03-5 CAPTAIN'S CLEARVIEW WINDOW OPS NORMAL.
- [SDR UPS06848515](https://openairdocs.org/sdr/UPS06848515.md): Window · jammed · Nov 3, 2006 · N802UP · Doug DC873F · Flight Compartment Windows
  > CAPT CLEARVIEW WINDOW WILL NOT OPEN. FOUND WINDOW TRIM ON AFT OF SLIDING WINDOW JAMMING WINDOW MOTION. REMOVED WINDOW TRIM FROM AFT OF WINDOW. WINDOW OPS CK NORMAL.
- [SDR UPS06847940](https://openairdocs.org/sdr/UPS06847940.md): Fitting · cracked · Aug 23, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 END FITTING FOR STRINGER 51 OUTBOARD OF XRS 74 NR 2 MAIN TANK. REMOVED STRINGER END FITTING 51 AT STA XRS 74 NR 2 MAIN TANK IAW SRM 51-3-0. LOCATED, DRILLED UP AND INSTALLED END FITTING ON STRINGER 51 AT STA 74 NR 2 MAIN TANK IAW SRM 51-1-
- [SDR UPS06847787](https://openairdocs.org/sdr/UPS06847787.md): Rib · cracked · Aug 22, 2006 · N802UP · Doug DC873F · Leading Edge Devices
  > INSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACKED RIB AT LT L/E STA XFS 460 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT LT L/E RIB STA XFS 460 IAW SRM 57-02-00 FIG 002.
- [SDR UPS06847995](https://openairdocs.org/sdr/UPS06847995.md): Longeron · corroded · Aug 18, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-C3 AFTER REMOVED FUSELAGE BELLY SKIN FROM FS -22 TO 70 L31L-L31R, FOUND LONGERON HAS HEAVY CORROSION AT STA 55 TO 70 L36. FABRICATED AND INSTALLED LONGERON AND END FITTING. IAW SRM 51-3-2 AND 51-1-20D.
- [SDR UPS06847892](https://openairdocs.org/sdr/UPS06847892.md): Attach Angle · corroded · Aug 18, 2006 · N802UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C3 STA 857 RBL 53 UPPER HORIZONTAL ATTACH ANGLE, CENTER FUEL TANK, FWD BULKHEAD HAS EXFOLIATED CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR WEB ANGLE RAT WHEEL WELL, FWD BULKHEAD (CENTER FUEL TANK), STA 857 RBL 53 IAW DRAWING NR 5644011,
- [SDR UPS06847894](https://openairdocs.org/sdr/UPS06847894.md): Longeron · corroded · Aug 17, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-C3 STA.1766 LONGERON 28R CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF LONGERON 28R FROM STA 1752 TO 1766 IAW SRM 53-02-02-0 FIG 10 AND SRM 51-01-21-0. FABRICATED LONGERON SECTION AND REPAIR STRAPS IAW SRM 53-05-03-0, AND SRM 53-02-02-0 FI
- [SDR UPS06847893](https://openairdocs.org/sdr/UPS06847893.md): Fitting · cracked · Aug 17, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-C3 STA 1766 LONGERON 28R END FITTING CORRODED. END FITTING FOUND TO BE CORRODED AND CRACKED. REMOVED AND REPLACED STA 1766 LONGERON 28R END FITTING IAW SRM 51-1-20D, AND SRM 51-03-02 -0.
- [SDR UPS06847891](https://openairdocs.org/sdr/UPS06847891.md): Fitting · cracked · Aug 17, 2006 · N802UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE-C3 STA 1760 LONGERON 14R END FITTING CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 1760 LONGERON 14R IAW SRM 51-01-21, SRM 51-03-00, AND SRM 51-01-20D.
- [SDR UPS06847768](https://openairdocs.org/sdr/UPS06847768.md): Rib · cracked · Aug 17, 2006 · N802UP · Doug DC873F · Leading Edge Devices
  > INSPECTION TYPE:C3 LEFT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-3-3, 57-02-00, 51-1-21 AND 51-1-20D.
- [SDR UPS06847871](https://openairdocs.org/sdr/UPS06847871.md): Skin · corroded · Aug 16, 2006 · N802UP · Doug DC873F · Fuselage Main, Plate/Skin
  > FOUND CORROSION BETWEEN SKIN AND DOUBLER AT L36 STA 1180, EXTERIOR BULGED. CUT OUT DAMAGED AREA AT STA 1180 L36 IAW SAA EA 008-5320-01-A0381. FABRICATED AND INSTALLED REPAIR PARTS AT STA 1180 L36 IAW SAA EA NR 008-5320-01-A0381, UPS RAA DC8-53-20581, DOUGLAS

Next page: https://openairdocs.org/deregistered/N802UP-2010-07-02/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 = 'N802UP' AND deregistration_id = 'N802UP-2010-07-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N802UP-2010-07-02/reports

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