# Service difficulty reports: N807UP, cancelled Sep 13, 2010

A list on [N807UP, cancelled Sep 13, 2010](https://openairdocs.org/deregistered/N807UP-2010-09-13.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 UPS08854052](https://openairdocs.org/sdr/UPS08854052.md): Skin · corroded · Nov 28, 2008 · N807UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A AREA OF CORROSION CAUSING RIVET HEADS TO DEFORM ON A/C SKIN LOWER CENTERLINE LOCATED NEAR VHF BLADE ANTENNA. INSTALLED INTERIM REPAIR DOUBLER REF NRC 224311 REF E/O DC8-5330-3135 3-A FOR REPEAT INSP AND PERM REPAIR REQUIREMENTS. THIS IS A
- [SDR UPS08853915](https://openairdocs.org/sdr/UPS08853915.md): Door · out of rig · Nov 13, 2008 · N807UP · Doug DC873F · Passenger/Crew Doors
  > INSPECTION TYPE:N/A L1 DOOR EXTREMELY HARD TO OPEN OR CLOSE. RERIGGED L-1 DOOR. OPS CHECK NORMAL.
- [SDR UPS08853700](https://openairdocs.org/sdr/UPS08853700.md): Battery · discharged · Oct 20, 2008 · N807UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A DURING EMERGENCY LIGHT CHECK, EMERGENCY STANDBY LIGHTS FAILED TO ILLUMINATE. REMOVED & REPLACED EMERGENCY LIGHT BATTERY / RELAY ASSY PER MM 33-50 -01-2. OPS CHECK GOOD.
- [SDR UPS08852736](https://openairdocs.org/sdr/UPS08852736.md): Frame · cracked · Jul 11, 2008 · N807UP · Doug DC873F · Fuselage Main, Structure
  > PITS 32 AND 34 CARGO DOOR INNER CRACKS. ISSUED DEFERRAL D380080 IAW EO DC8-5230-29933-A. DAMAGE CONSISTS OF 2.0" LONG CRACK LOCATED ON THE INSIDE RADIUS OF FRAME. VERIFIED ENDS OF CRACK IAW NDT MANUAL 06-10-01 MARKED ENDS. MEASURED CRACK TO BE 2.0" LONG.
- [SDR UPS08851759](https://openairdocs.org/sdr/UPS08851759.md): Door Frame · dented · Mar 4, 2008 · N807UP · Doug DC873F · Fuselage Main, Structure
  > MAIN ENTRY DOOR HAD DENT WITH CREASE JUST OUTBD OF BAYONET FITTING DENT MEASURES 1.25 LENGTH BY.750 WIDE AND.150 DEEP. CON'T ON ECA FORM 011317: FABRICATED DOUBLER. COLD WORKED AREA TO PROPER LIMITS OF.0 08 IAW UPS EO DC8-5310-28745-A, APPX PARA 3. AC
- [SDR UPS08851697](https://openairdocs.org/sdr/UPS08851697.md): Engine · flamed out · Feb 21, 2008 · N807UP · Doug DC873F · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:N/A NR 3 ENGINE FLAMEOUT AT CRUISE. FLT LVL 360, SPEED MACH.81, FUEL NORMAL AND BALANCED. ATTEMPTED RESTART AT FL 300 UNSUCCESSFUL. ATTEMPTED 2ND RESTART AT 16000 FT SUCCESSFUL. ENG OPERATED NORMALLY REMAINDER OF FLT. EMERGENCY WAS DECLAR
- [SDR UPS08851569](https://openairdocs.org/sdr/UPS08851569.md): Hose · chafed · Jan 29, 2008 · N807UP · Doug DC873F · Hydraulic System, Main
  > THE CREW EXPERIENCED A HYDRAULIC LEAK. AFTER RUNNING THE CHECKLIST, DECLARED AN EMERGENCY AND CONTINUED TO PHL. AFTER APPROX 20 MIN IN CRUISE, LOST HYD QTY DOWN TO AUX AT THE "X" AND AIL CTRL MANUAL AND RUDDER CTRL MANUAL LTS ILLUM. RAN LOSS OF HYD FLUID/PR
- [SDR UPS07851280](https://openairdocs.org/sdr/UPS07851280.md): Inertia Reel · sticks · Dec 8, 2007 · N807UP · Doug DC873F · Flight Compartment Equipment
  > CAPTAIN'S LEFT SHOULDER HARNESS INERTIAL REEL IS STICKY. REMOVED AND REPLACED CAPTAIN'S INERTIA REEL. OPS CHECK GOOD.
- [SDR UPS07850686](https://openairdocs.org/sdr/UPS07850686.md): Battery · discharged · Sep 17, 2007 · N807UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER 33-50-01-2, DC8 AMM. LIGHTS OP'S OK.
- [SDR UPS07850620](https://openairdocs.org/sdr/UPS07850620.md): Control Panel · inoperative · Sep 6, 2007 · N807UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A F/E PANEL EMERGENCY CONTROL LIGHT PANEL HAS 4 OR 6 LIGHTS INOP. DEF 358150 ASSIGNED. *SDR FILED OPEN* DEFERRED F/E EMERGENCY ELECT CONTROL LIGHTING PANEL REF MEL 33-1 PART REQ A 847094.
- [SDR UPS07850380](https://openairdocs.org/sdr/UPS07850380.md): Skin · gouged · Jul 14, 2007 · N807UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN HAS DEEP GOUGE AND DENT AT STA 160 L21L TO L22L. REPAIR EXTERIOR SKIN IAW SAA EA 008-5330-01-A0966, UPS RAA DC8-53-2064 3.
- [SDR UPS07850225](https://openairdocs.org/sdr/UPS07850225.md): Door Frame · cracked · Jul 14, 2007 · N807UP · Doug DC873F · Passenger/Crew Doors
  > INSPECTION TYPE:C2 L-1 DOOR FRAME SEGMENT CRACKED IN BAYONETTE AREA. STOP DRILLED CRACK IN FRAME SEGMENT AT L-1 DOOR IAW SRM 52-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON L-1 DOOR FRAME SEGMENT IAW SRM 52-02-02 FIG 007.
- [SDR UPS07850227](https://openairdocs.org/sdr/UPS07850227.md): Fitting · cracked · Jul 11, 2007 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 STA 1180 L27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED BANANA FITTING AT STA 1180 L27L IAW SRM 51-01-20D, AND SRM 51-3-2.
- [SDR UPS07850216](https://openairdocs.org/sdr/UPS07850216.md): Longeron · cracked · Jul 10, 2007 · N807UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L34R. REMOVED END FITTING AT STA 1140 L34R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT END FITTING AT STA 1140 L34R IAW SRM 51-1-20D, AND DWG 475814.
- [SDR UPS07850191](https://openairdocs.org/sdr/UPS07850191.md): Fitting · cracked · Jul 10, 2007 · N807UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT STA 1140 L35L. REMOVED L35L END FITTING AT STA 1140 IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED L35L END FITTING AT STA 1140 IAW SRM 51-3-2, AND SRM 51-1-20D.
- [SDR UPS07850185](https://openairdocs.org/sdr/UPS07850185.md): Fitting · cracked · Jul 10, 2007 · N807UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L33R. REMOVED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-3-2, AND SRM 51-1-20D.
- [SDR UPS07850192](https://openairdocs.org/sdr/UPS07850192.md): Skin · corroded · Jul 8, 2007 · N807UP · Doug DC873F · Rudder, Plate/Skin
  > INSPECTION TYPE:C2 LEFT SIDE OF RUDDER SKIN ZR 251 HAS CORROSION. REMOVED SKIN PANEL ON LEFT SIDE OF RUDDER STA ZR 251 IAW SRM 51-1-21. FABRICATED AND INSTALLED LEFT RUDDER SKIN PANEL AT STA ZR 251 IAW SRM 51-3-2, SRM 51-1-9A, AND DWG 5655077.
- [SDR UPS07850178](https://openairdocs.org/sdr/UPS07850178.md): Skin · canning · Jul 8, 2007 · N807UP · Doug DC873F · Rudder, Plate/Skin
  > INSPECTION TYPE:C2 RIGHT SIDE OF RUDDER SKIN ZR 271 HAS OIL CANNING. REMOVED SKIN PANEL ON RT/SIDE OF RUDDER AT ZR 271 IAW SRM 51-1-21. FABRICATED AND INSTALLED RUDDER SKIN PANEL ON RT/SIDE OF RUDDER STA ZR 271 IAW SRM 51-1-21, AND DWG 56555077.
- [SDR UPS07850184](https://openairdocs.org/sdr/UPS07850184.md): Floorbeam · corroded · Jul 7, 2007 · N807UP · Doug DC873F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C2 HEAVY CORROSION ON TOP OF FLOORBEAM IN C-PIT TUNNEL AT STA 1300 LBL 51. REMOVED CORROSION FROM FLOORBEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-00. FABRICATED AND INSTALLED REPAIR ANGLES AT STA 1300 LBL 51 FLOORBEAM IAW SRM 53-2-0 FIG 1B.
- [SDR UPS07850166](https://openairdocs.org/sdr/UPS07850166.md): Skin · dented · Jul 5, 2007 · N807UP · Doug DC873F · Landing Gear Doors
  > INSPECTION TYPE:C2 DENTS ON NLG RT/STRUT DOOR EXTERIOR SKIN. CUT OUT DAMAGED AREA ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 004.
- [SDR UPS07850172](https://openairdocs.org/sdr/UPS07850172.md): Skin · cracked · Jul 3, 2007 · N807UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 CRACK ON EXTERIOR FUSE SKIN AT STA 1740 L19R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN AT STA 1740 L19R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 1740 L19R IAW SRM 53-02-01 FIG 7.
- [SDR UPS07849886](https://openairdocs.org/sdr/UPS07849886.md): Slide · loose · Jun 6, 2007 · N807UP · Doug DC873F · Escape Slide
  > INSPECTION TYPE:N/A CABIN ESCAPE SLIDE WILL NOT STOW. INSTALLED RETAINING PIN IN SLIDE PER AMM 25-60-01-2.
- [SDR UPS07849749](https://openairdocs.org/sdr/UPS07849749.md): Slide · missing · May 3, 2007 · N807UP · Doug DC873F · Escape Slide
  > INSPECTION TYPE:N/A ESCAPE SLIDE NOT IN DOOR. INSTALLED ESCAPE SLIDE ON DOOR IAW MM 25-60-01-2.
- [SDR UPS07849501](https://openairdocs.org/sdr/UPS07849501.md): Bulb · burned out · Mar 15, 2007 · N807UP · Doug DC873F · Emergency Lighting
  > PILOTS OVERHEAD PANEL EMERGENCY LIGHTS DISARMED LIGHT INOP. FOUND BULB BURNED OUT. REPLACED BULB, CHECKS OK.
- [SDR UPS06848791](https://openairdocs.org/sdr/UPS06848791.md): Slide · unwanted deploy · Dec 20, 2006 · N807UP · Doug DC873F · Escape Slide
  > INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE DEPLOYED INADVERTENTLY. DEFERRAL M340403 ASSIGNED. CLEARED MEL 52-7-4 M340403. INSPECTED AND REINSTALLED ORIGINAL DOOR SLIDE IAW AMM 25-60-01 & CHECKS OK.
- [SDR UPS06848527](https://openairdocs.org/sdr/UPS06848527.md): Battery · discharged · Nov 8, 2006 · N807UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LTS INOP. REMOVED ADN REPLACED EMERGENCY EXIT BATT/RELAY PACK IAW MM 33-50-01-2. OPS CK GOOD.
- [SDR UPS06847468](https://openairdocs.org/sdr/UPS06847468.md): Odor · detected · Jul 28, 2006 · N807UP · Doug DC873F · Air Distribution System
  > ELECTRICAL ODOR ON F/O'S SIDE OF COCKPIT TROUBLESHOOTING IN PROGRESS COULD NOT SMELL ANY TYPE OF ELECTRICAL ODOR WHEN OPERATING ALL FOUR ENGINES.
- [SDR UPS05845146](https://openairdocs.org/sdr/UPS05845146.md): Fitting · cracked · Jul 29, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > WHILE WORKING N/R 859104 FOUND LONG 31L END FITTING CRACKED. REMOVED AND REPLACED LONG END FITTING AT STA 106 IAW SRM 51-3-0 51-1-21, AND SRM 51-1-20D.
- [SDR UPS05845112](https://openairdocs.org/sdr/UPS05845112.md): Frame · cracked · Jul 29, 2005 · N807UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE:C1 WHILE ACCOMPLISHMENT OF MCD FWD HINGE REPLACEMENT AFTER REMOVAL OF THE ACTUATOR CLOSE OUT PNL FOUND A 1" CRACK ON THE FWD UPPER MAIN FRAME CRACK ON "Z" FRAME STOPPED AT EXISTING HOLE NDT HFEC CRACK TERMINATES AT EXISTING HOLE IAW NDTSPM06-10
- [SDR UPS05845003](https://openairdocs.org/sdr/UPS05845003.md): Fitting · corroded · Jul 23, 2005 · N807UP · Doug DC873F · Fuselage Miscellaneous Structure
  > A/C COMPT LONGERON END FITTING CORRODED AROUND FASTENER HOLE AT STA 70 L32R. REMOVED AND REPLACED LONG END FITTING AT STA 70 L32R IAW SRM 57-1-20D, AND 51-3-2.
- [SDR UPS05844997](https://openairdocs.org/sdr/UPS05844997.md): Finger Doubler · corroded · Jul 22, 2005 · N807UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C1, SKIN SPLICE AT FS 1350 INTERIOR FINGER DOUBLER HAS PITTED CORROSION FROM L31R TO L31L. REMOVED FINGER DOUBLER AT FS 1350 IAW SRM 51-1-21 AND 51-1-20D. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 1350 L31L TO 31R IAW SRM 51-1-21.
- [SDR UPS05845188](https://openairdocs.org/sdr/UPS05845188.md): Hinge Pin · worn · Jul 20, 2005 · N807UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE:C1 REMOVE MAIN CARGO DOOR HINGE TO ACCOMPLISH FWD HINGE REPLACEMENT, CRACKED, FOUND DURING DOUBLER REMOVAL. REMOVED MAIN CARGO DOOR AND HINGE, MAG PARTICAL, HFEC AND FPI INSPECT IONS ACCOMPLISHED, NO CRACKS NOTED. REINSTALLED HINGE, REPLACED
- [SDR UPS05845121](https://openairdocs.org/sdr/UPS05845121.md): Skin · corroded · Jul 16, 2005 · N807UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE TO FOM FOR NDT INSPECTION TO COMPLY WITH EO DC8-5330-20206 FOUND CORROSION ON FUSELAGE SKIN FS 1395 TO 1445 L34R-L32R. REMOVED AND REPLACED FUSELAGE SKIN AT STA 1395-1445 L34R-L32R IAW SRM 51-1-21, 51-1-20D
- [SDR UPS05844965](https://openairdocs.org/sdr/UPS05844965.md): Longeron · corroded · Jul 16, 2005 · N807UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1 AFTER REMOVAL OF INTERCOSTAL ON N/R 858794 FS 1473 L34R FOUND CORROSION AT LONGERON UNDER STRAP REMOVED LONGERON 34R STA 1350 TO 1490 IAW DC8 SRM 53-2-2 FABRICATED AND INSTALLED LONGERON 34R AT STA 1350-1490 IAW DRWG 3646937
- [SDR UPS05845183](https://openairdocs.org/sdr/UPS05845183.md): Skin · cracked · Jul 14, 2005 · N807UP · Doug DC873F · Fuselage Main, Plate/Skin
  > REPLACE SKIN PANEL AT STA 70 TO -21.92 LONG 31R-L31L. REMOVED AND REPLACED FWD BELLY SKIN AT STA -21.92 TO STA LONG 31L TO LONG 31R IAW EO DC8-5330-8942-D.
- [SDR UPS05845182](https://openairdocs.org/sdr/UPS05845182.md): Plate · cracked · Jul 13, 2005 · N807UP · Doug DC873F · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR LWR AFT CORNER, THE DOOR JAMB CORNER INTERNAL SUPPORT PLATE IS CRACKED. REMOVED FILLET IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT FILLET AT THE MAIN CARGO DOOR LWR AFT DOOR JAMB INTERNAL SUPPORT PLATE IAW DWG 5772786 AND SRM 51-3-0
- [SDR UPS05845120](https://openairdocs.org/sdr/UPS05845120.md): Fitting · cracked · Jul 13, 2005 · N807UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 LONG 31R SPLICE FITTING CRACKED FROM 1040-1060. REMOVED AND REPLACED LONG SPLICE FITTING IAW SRM 53-1-0 AND 51-1-20 AT STA 1040-1060 LONG 31R.
- [SDR UPS05845115](https://openairdocs.org/sdr/UPS05845115.md): Fitting · cracked · Jul 13, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 BATHTUB FITTING CRACKED AT C-PIT DOOR JAMB STA 1200 L33R-L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 53-2-0 AND SRM 53-2-0 FIG 02G.
- [SDR UPS05845046](https://openairdocs.org/sdr/UPS05845046.md): Floorbeam · cracked · Jul 13, 2005 · N807UP · Doug DC873F · Fuselage Main, Floor Beam
  > F/S 960 LBL 60 FLOORBEAM AT LIGHTING HOLE ON VERT FLANGE AT CENTER OF HOLE HAS A 5" CRACK GOING AT HORIZ ANGLE. STOP DRILLED CRACKED FLOORBEAM, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SAA SK 807-858978 AND UPS EODC8-53-20486.
- [SDR UPS05844966](https://openairdocs.org/sdr/UPS05844966.md): Fitting · cracked · Jul 13, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 SPLICE FITTING CRACKED AT STA 610, L35L REMOVED CRACKED SPLICE FITTING AT STA 610, LONG 35L IAW SRM 51-1-20D. FABRICATED REPLACEMENT FITTING AND INSTALLED FITTING IAW DRWG 3750330
- [SDR UPS05845145](https://openairdocs.org/sdr/UPS05845145.md): Fitting · corroded · Jul 12, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > A-PIT CENTER TORQUE BOX BATHTUB FITTING AT FS 360 BETWEEN TORQUE BOX FRAME AND LONGERON34R HAS CORROSION. REMOVED CORROSION FROM BATH TUB FITTING AT STA 360 LONG 34R AND FOUND OUT OF LIMITS IAW SRM 51-1-8. REPLACED BATHTUB FITTING AT STA 360, 34R IAW 53-02-0
- [SDR UPS05844995](https://openairdocs.org/sdr/UPS05844995.md): Longeron · cracked · Jul 12, 2005 · N807UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FS 1488 LONG 32L CRACKED ON BACKSIDE OF SPLICE END. REMOVED LONG 32L AND SPLICE END FITTING AT FS 1488 IAW SRM 51-1-21, FABRICATED LONG 32L AND SPLICE END FITTING IAW SRM 53-02-02 FIG 010 AND INSTALLED LONG 32L AND SPLICE END FITTING IAW SRM 51-1-21.
- [SDR UPS05844949](https://openairdocs.org/sdr/UPS05844949.md): Fitting · corroded · Jul 12, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, EXFOILIATED CORROSION ON VERTICAL L-FITTING FWD BULKHEAD RT NOSE TUNNEL. REMOVED VERTICAL L-FITTING, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21, DWG 4642086,S-2506104 AND 51-1-20D.
- [SDR UPS05845125](https://openairdocs.org/sdr/UPS05845125.md): Structure · elongated · Jul 11, 2005 · N807UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C1, D-PIT DOOR AFT WEB HAS SEVERAL ELONGATED HOLES AND LITE CORROSION AROUND FASTENER. REMOVED DAMAGED WEB IAW SRM 51-1-21, FABRICATED DOOR JAMB SKIN AND WEB IAW DWG 5616674 AND SRM 51-1-21 AND INSTALLED JAMB SKIN AND WEB IAW DWG 5616674 AND
- [SDR UPS05845123](https://openairdocs.org/sdr/UPS05845123.md): Fitting · cracked · Jul 11, 2005 · N807UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:C1 60 COMPT L17L AT 1770 HAS 6 INCH CRACK AT END FITTING. REMOVED FITTING AND SUPPORT FROM STA 1770 L17L IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONGERON END SPLICE FITTING AT STA 1170 1793 IAW DWG S-1616757 AND SRM 51-1-8.
- [SDR UPS05845122](https://openairdocs.org/sdr/UPS05845122.md): Intercostal · corroded · Jul 11, 2005 · N807UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 D-PIT FS 1473 LONG 34R LWR RETURN FLANGE ON INTERCOSTAL IN LONGERON HAS HEAVY EXFOLIATION 4.00". REMOVED INTERCOSTAL ATTACH ANGLE AT STA 1473 LONG 34R IAW SRM 51-1-20D. FABRICATED AND INSTALLED INTERCOSTAL ATTACH ANGLE AT STA 1473 LONG 34R
- [SDR UPS05845111](https://openairdocs.org/sdr/UPS05845111.md): Fitting · cracked · Jul 11, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C1, LONGERON END FITTING CRACKED AT STA 690 L4L. REMOVED CRACKED END FITTING AT STA 690 L4L IAW SRM 53-2-2. REPLACED END FITTING AT STA 690 L4L IAW SRM 51-1-20 AND 51-3-0.
- [SDR UPS05845050](https://openairdocs.org/sdr/UPS05845050.md): Fitting · cracked · Jul 11, 2005 · N807UP · Doug DC873F · Fuselage Main, Attach Fittings
  > LONGERON END FITTING CRACKED AT STA 902 L7L. REMOVED AND REPLACED LONGERON END FITTING IAW 51-1-20D, 51-1-21 AND 51-3-0.
- [SDR UPS05845005](https://openairdocs.org/sdr/UPS05845005.md): Fitting · corroded · Jul 11, 2005 · N807UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE: C1, MAIN CARGO DOOR JAMB AFT LATCH SPOOL FITTING FWD ANGLE HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED MCD LATCH SPOOL FITTING IAW 51-3-0, 51-3-2, 51-1-21, AND 51-3-1.
- [SDR UPS05845006](https://openairdocs.org/sdr/UPS05845006.md): Finger Doubler · corroded · Jul 11, 2005 · N807UP · Doug DC873F · Fuselage Main, Structure
  > FINGER DOUBLER BLOWN OUT IN COCKPIT SUBFLOOR AT STA -67 TO -81. REMOVED FINGER DOUBLER AT STA -67 TO -81. FABRICATED FINGER DOUBLER AND INSTALLED IAW SRM 53-3-1, AND 51-1-21, 51-1-20D.

Next page: https://openairdocs.org/deregistered/N807UP-2010-09-13/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 = 'N807UP' AND deregistration_id = 'N807UP-2010-09-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N807UP-2010-09-13/reports

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