# Service difficulty reports: N880UP, cancelled Jul 19, 2011

A list on [N880UP, cancelled Jul 19, 2011](https://openairdocs.org/deregistered/N880UP-2011-07-19.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 7 · 301 reports

- [SDR UPS09854460](https://openairdocs.org/sdr/UPS09854460.md): Control Valve · defective · Jan 28, 2009 · N880UP · Doug DC873F · Cabin Cooling System
  > INSPECTION TYPE:N/A BTB - WHEN STARTING NR 2 ENGINE ON PUSHBACK, DUCT OVERHEAT LIGHT ILLUMINATED, FOLLOWED BY PACK TRIP LIGHT ILLUMINATING, FOLLOWED BY SMOKE IN THE COCKPIT. SUPPLY DUCT LEAKING AT CLAMP IN FWD ACC. DEFERRED LT PACK PER MEL 21-38-1. DMP C/W
- [SDR UPS09854420](https://openairdocs.org/sdr/UPS09854420.md): Actuator · failed · Jan 23, 2009 · N880UP · Doug DC873F · Stabilizer Control System
  > EMERGENCY DECLARED. PITCH TRIM FAILED IN EXTENDED POSITION IN FLIGHT. R&R PTC ACTUATOR PER MM 27-30-07-2
- [SDR UPS08853829](https://openairdocs.org/sdr/UPS08853829.md): Doubler · cracked · Oct 27, 2008 · N880UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SP COMPLY WITH ATTACHED WAN NR 1421616 REGARDING CRACK ON L24L. NDT'D NEW CRACKS AND STOP DRILLED, INSTALLED REPAIR DOUBLER AND TAPERED SHIMS IAW SRM, EA 008-10-01-A1544, 51-1-20D, 51-1-8, UPS EO M-5100-27 80-E.
- [SDR UPS08853848](https://openairdocs.org/sdr/UPS08853848.md): Battery Pack · unserviceable · Oct 20, 2008 · N880UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS UNSERVICEABLE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY IAW AMM 33-50-01-02 AND FOUND SERVICEABLE.
- [SDR UPS08852601](https://openairdocs.org/sdr/UPS08852601.md): Panel · corroded · Jun 27, 2008 · N880UP · Doug DC873F · Wing, Plate/Skin
  > LT WING PANEL CORROSION. REMOVED DAMAGED SKIN. ACCOMPLISHED STEPS 1-6 OF EO DC8-5720-29785 APPENDIX A. ACCOMPLISHED REPAIR STEPS 1-9 OF EO DC8-5720-29785-A.
- [SDR UPS08852000](https://openairdocs.org/sdr/UPS08852000.md): Battery Pack · discharged · Apr 10, 2008 · N880UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTING SYSTEM INOP. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECKED AS PER DC8 MM 33-50-01-2. OPS CHECK GOOD.
- [SDR UPS08851766](https://openairdocs.org/sdr/UPS08851766.md): Battery Pack · inoperative · Mar 9, 2008 · N880UP · Doug DC873F · Emergency Lighting
  > ON PREFLT, FOUND EMERGENCY EXIT LTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK PER UPS AMM 33-50.
- [SDR UPS08851672](https://openairdocs.org/sdr/UPS08851672.md): Latch · broken · Feb 14, 2008 · N880UP · Doug DC873F · Escape Slide
  > INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE HAS BROKEN LATCH. SLIDE INOP FOR CREW ENTRY DOOR. DEFERRED CREW ENTRY DOOR SLIDE PER MEL 52-7-4. SLIDE IS SECURED IN SUITCASE. REMOVED SLIDE COVER AND ROUTED TO SHEET METAL. REMOVED AND REPLACED LATCH REF DCI SRM
- [SDR UPS08851544](https://openairdocs.org/sdr/UPS08851544.md): Structure · missing · Jan 22, 2008 · N880UP · Doug DC873F · Wing, Plate/Skin
  > APPROX 3/8 BY 1 INCH PIECE OF SHEETMETAL MISSING ON T/E OF WING. LOCATED ON LT WING INBD OF NR 3 SPOILER PANEL. ACCOMPLISHED EO DC8-5730-28460A.
- [SDR UPS08851524](https://openairdocs.org/sdr/UPS08851524.md): Skin · chafed · Jan 21, 2008 · N880UP · Doug DC873F · Spoilers
  > LEFT WING INBOARD LATERAL CONTROL SPOILER LOWER SURFACE IS CHAFFED ALONG T/E. INSTALLED NEW SPOILER ASSEMBLY IAW DC8 AMM 27-61-01-2, PARAGRAPH 3B STEPS 1 THROUGH 6.
- [SDR UPS07851086](https://openairdocs.org/sdr/UPS07851086.md): Fan · frozen · Nov 2, 2007 · N880UP · Doug DC873F · Air Distribution Fan
  > DIVERSION, CREW SMELLED SMOKE IN CABIN. DISCHARGE HAND EXTINGUISHER IN LAV, CREW REPORTED LAV PUMP WAS TURNING. PARKED FOR FAA EVALUATION. FOUND RECIRCULATING FAN FROZE UP. REMOVED AND REPLACED IAW AMM 21-1-01-2. OPS CHECK GOOD. INSPECTED SURROUNDING ARE
- [SDR UPS07850682](https://openairdocs.org/sdr/UPS07850682.md): Battery · discharged · Sep 19, 2007 · N880UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT FAILED PREFLIGHT TEST. REPLACED BATTERY AND RELAY UNIT W/REF M/M 33-50-01-2, OPS TEST GOOD.
- [SDR UPS07850689](https://openairdocs.org/sdr/UPS07850689.md): Battery · discharged · Sep 18, 2007 · N880UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT FAILED PREFLIGHT TEST. REPLACED BATTERY AND RELAY UNIT W/REF M 33-50-01-2, OPS TEST GOOD.
- [SDR UPS07849879](https://openairdocs.org/sdr/UPS07849879.md): Engine · flamed out · Jun 4, 2007 · N880UP · Doug DC873F · Engine (Turbine/Turboprop)
  > INSPECTION TYPE:N/A ATB - NR 4 ENGINE FLAMEOUT CLIMBING THROUGH 30,000FT. NOTICED FUEL PUMP IN OFF POSITION. RAN ENGINE FLAMEOUT CHECK LIST AND ENGINE RESTARTED. ALL INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. PERFORMED NEG PRESSURE CHECK ON NR 4 ENG. FUE
- [SDR UPS07849855](https://openairdocs.org/sdr/UPS07849855.md): Skin · corroded · May 20, 2007 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 EXFOLIATED CORROSION UNDER L33R AT STA 1620. REPAIRED SKIN AND FINGER DOUBLER AT STA 1620 L33R IAW SAA EA 008- 5330-00-A0885, UPS RAA DC8-53-20632, AND FAA FORM 8100-9.
- [SDR UPS07849821](https://openairdocs.org/sdr/UPS07849821.md): Fitting · cracked · May 10, 2007 · N880UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C3 END FITTING CRACKED AT STA 1690 L34R, 2.5 INCHES AT BARREL NUT HOLE. REMOVED CRACKED END FITTING AT STA 1690 L34R IAW SRM 51-01-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 1690 L34R IAW SRM 51-03-02, AND SRM 51-01-20D.
- [SDR UPS07849789](https://openairdocs.org/sdr/UPS07849789.md): Frame · gouged · May 2, 2007 · N880UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C3 A-PIT, BELT FRAME GOUGED AT STA 240 L31R. TRIMMED OUT DAMAGED AREA AT STA 240 L31R IAW E0 DC8-5310-11728-B, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DC8-5310-11728-B.
- [SDR UPS07849835](https://openairdocs.org/sdr/UPS07849835.md): Longeron · cracked · Apr 29, 2007 · N880UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 L33R SPLICE BETWEEN STA 1640-1660 CRACKED. REMOVED AND REPLACED LONGERON SECTION FROM STA 1640-1660 L33R IAW SRM 51-01-20D, 51-1-21, AND 51-3-2.
- [SDR UPS07849820](https://openairdocs.org/sdr/UPS07849820.md): Skin · canning · Apr 28, 2007 · N880UP · Doug DC873F · Elevator, Plate/Skin
  > INSPECTION TYPE:C3 L/ELEVATOR UPPER SKIN ON INBD SIDE HAS DINGS AND SKIN HAS OIL CANNING. CUT OUT DAMAGED SKIN ON L/ELEVATOR AT STA XE 57.5 IAW SRM 55-02-01-0, FABRICATED, BONDED FINGER DOUBLER, AND INSTALLED REPLACEMENT SKIN ON L/ELEVATOR AT STA XE 57.5 IAW
- [SDR UPS07849822](https://openairdocs.org/sdr/UPS07849822.md): Pressure Panel · misrepaired · Apr 27, 2007 · N880UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C3 VISUAL INSP OF PRESSURE WEB AT STA 863 RBL 42-48, FOUND DOUBLER TO BE TAPERED ON ENDS, WITH NO TAPERED SHIMS INSTALLED, REF: EO DC8- 5310-22195-B. INSTALLED CORRECT REPAIR AT STA 863 RBL 42-48 IAW SAA EA 008-5310- 01-A0841, UPS EO DC8-5310-
- [SDR UPS07849782](https://openairdocs.org/sdr/UPS07849782.md): Skin · cracked · Apr 26, 2007 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 FS 1690 L32L HAS A 1 INCH CRACK AND EXISTING REPAIR DOUBLER AT L30L SRM REPAIR WILL NOT BE INCOMPLIANCE WITH EO DC8-5330-20248. CUT OUT DAMAGED AREA AT STA 1690 L32L IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLERS,
- [SDR UPS07849748](https://openairdocs.org/sdr/UPS07849748.md): Doubler · cracked · Apr 26, 2007 · N880UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 CRACK ON INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE UPPER SURFACE I/B EDGE OF SLOT DOOR. REMOVED INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT WING LEADING EDGE
- [SDR UPS07849742](https://openairdocs.org/sdr/UPS07849742.md): Rib · cracked · Apr 26, 2007 · N880UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB CRACKED AT XFS 484. STOP DRILLED CRACK IAW SRM 57-02-00. FABRICATED AND INSTALLED 2 DOUBLERS IAW SRM 57-02-00, 51-1-21, AND 51-1-20D.
- [SDR UPS07849741](https://openairdocs.org/sdr/UPS07849741.md): Rib · cracked · Apr 26, 2007 · N880UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LEFT WING CENTER RIB CRACKED AT XFS 409. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-00 51-1-21, AND 51-1-20D.
- [SDR UPS07849823](https://openairdocs.org/sdr/UPS07849823.md): Skin · misrepaired · Apr 25, 2007 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 L28R AT FS 1746 HAS 2 EA EXISTING REPAIR DOUBLERS UPPER AND LWR OF L28R, NOT IN COMPLIANCE WITH EO DC8-5330-20248 NOR DWG SRO8530032. REPAIRED FUSELAGE TAIL SECTION SKINS AT STA 1746, L28R - L30R IAW SAA EA 008-5330-01-A0854, UPS EO DC8-533
- [SDR UPS07849750](https://openairdocs.org/sdr/UPS07849750.md): Fitting · corroded · Apr 25, 2007 · N880UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C3 MAIN CABIN, CORROSION ON BELTFRAME END FITTING, STA 220 L21R. REMOVED AND REPLACED BELTFRAME FITTING AT STA 220 L21R IAW SRM 51-1-20D, AND SRM 51-3-0.
- [SDR UPS07849806](https://openairdocs.org/sdr/UPS07849806.md): Longeron · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 L24L 12 INCHES AFT OF BARREL NUT STA 869 CRACKED: VIEWED FROM TOP OF WING. STOP DRILLED CRACKED L24L AT STA 869 IAW SRM 53-2-2 VIEW G. STOP DRILLS TERMINATE CRACKS PER HFEC NDTS 06-10-01.001. FABRICATED AND INSTALLED -3, -5 DOUBLERS, -7,
- [SDR UPS07849788](https://openairdocs.org/sdr/UPS07849788.md): Bulkhead · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C3 AFT PRESS BULKHEAD CRACKED AT STA 1766 L10L, LBL 25 AND LBL 35. CUT OUT DAMAGED AREA AT STA 1766 LBL 25 AND LBL 35 IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED REPAIR FILLERS, AND DOUBLERS AT STA 1766 LBL 25 AND LBL 35 IAW SRM 53-2-5 F
- [SDR UPS07849786](https://openairdocs.org/sdr/UPS07849786.md): Bulkhead · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C3 AFT PRESS BULKHEAD CRACKED 2 AREAS AT STA 1766 L10R, RBL 25 AND RBL 35. CUT OUT DAMAGED AREA AT ST 1766 L10R, RBL 25 AND RBL 35 IAW SRM 53-02-05 FIG 14A. FABRICATED & INSTALLED REPAIR DOUBLERS, & FILLERS AT STA 1766 L10R IAW SRM 53-02-05 F
- [SDR UPS07849739](https://openairdocs.org/sdr/UPS07849739.md): Attach Angle · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO L16L ATTACH ANGLE CRACKED AT STA 1766. REMOVED ATTACH ANGLE AT STA 1766 L16L IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERCOSTAL CLIP AT STA 1766 L16L IAW DWG NR 5773844, AND SRM'S 51-1-20D, 51-3-2.
- [SDR UPS07849738](https://openairdocs.org/sdr/UPS07849738.md): Rib · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT STA XFS 609. NDT VERIFIED CRACK TERMINATES AT FASTNER HOLE IAW NDSPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR ANGLE AT L/WING L/E RIB STA XFS 609 IAW SRM 57-03-03 FIG 6.
- [SDR UPS07849737](https://openairdocs.org/sdr/UPS07849737.md): Rib · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT XFS 591. NDT VERIFIED CRACK ENDS AT FASTENER HOLE IAW NDSPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR ANGLE AT LT WING OUTBD L/E STA XFS 591 IAW SRM 57-03-03 FIG 6.
- [SDR UPS07849722](https://openairdocs.org/sdr/UPS07849722.md): Rib · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LT WING OB LE RIB CRACKED AT XFS 804. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00, 51-01-21 AND 51-1-20D.
- [SDR UPS07849721](https://openairdocs.org/sdr/UPS07849721.md): Rib · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LT WING OB LE CRACKED AT XFS 876. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-02-00, 51-1-21 AND 51-1-20D.
- [SDR UPS07849720](https://openairdocs.org/sdr/UPS07849720.md): Rib · cracked · Apr 24, 2007 · N880UP · Doug DC873F · Wing, Rib/Bulkhead
  > C3 LT WING OB LE RIB CRACKED AT XFS 798. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-07-00, 57-02-00, 51-1-21 AND 51-1-20D.
- [SDR UPS07849831](https://openairdocs.org/sdr/UPS07849831.md): Skin · canning · Apr 23, 2007 · N880UP · Doug DC873F · Rudder, Plate/Skin
  > INSPECTION TYPE:C3 LEFT RUDDER SKIN OIL CANNING AT STA ZR 185. REPAIRED LEFT RUDDER SKIN AT STA ZR 185 IAW SAA EA 008-2720-01-A0856 DAC DWG 5655077 REV-S, AND FAA FORM 8100-9.
- [SDR UPS07849828](https://openairdocs.org/sdr/UPS07849828.md): Skin · gouged · Apr 23, 2007 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN GOUGED AT STA 140 L22L. REPAIRED FUSELAGE SKIN AT STA 140 L22L IAW SAA EA 008-5330-01-A0849 UPS EO DC8-5330-26786-A, DOUGLAS DWG SRO8530027.
- [SDR UPS07849808](https://openairdocs.org/sdr/UPS07849808.md): Skin · corroded · Apr 23, 2007 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CORRODED AT FS 310 L2R. CUT OUT DAMAGED AREA AT STA 310 L2R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 310 L2R IAW SRM 53-02-01 FIG 7.
- [SDR UPS07849809](https://openairdocs.org/sdr/UPS07849809.md): Skin · gouged · Apr 21, 2007 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 FUSELAGE EXTERIOR EXISTING REPAIR DOUBLER HAS DEEP GOUGE AND FASTENER HEADS MISSING AT STA 520 L31R. REMOVED DAMAGED DOUBLER AND CUT OUT AREA AT STA 520 L31R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS AT STA 520
- [SDR UPS07849781](https://openairdocs.org/sdr/UPS07849781.md): Skin · misrepaired · Apr 20, 2007 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 REMOVE STEEL DOUBLER FROM THE C-4 (D-PIT) UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 21. REMOVED AND REPLACED DOUBLER AT C-4 (D-PIT) UPPER FWD CORNER IAW SRM 53-02-00 FIG 21, AND SRM TR 53-140, & 53-188, THIS REPAIR REQUIRES AN MPI WITH
- [SDR UPS07849192](https://openairdocs.org/sdr/UPS07849192.md): Battery Pack · inoperative · Feb 11, 2007 · N880UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A ON EMERGENCY EXIT LIGHTS TEST, NO LIGHTS WOULD OPERATE. STANDBY INSTRUMENTS OK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER PACK ASSY & SYS. OPS CHECKED NORMAL IAW MM 33-50-01-2.
- [SDR UPS07849158](https://openairdocs.org/sdr/UPS07849158.md): Battery Pack · inoperative · Feb 8, 2007 · N880UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK IAW 33-50-01-2.
- [SDR UPS06848401](https://openairdocs.org/sdr/UPS06848401.md): Battery Pack · no test · Nov 1, 2006 · N880UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.
- [SDR UPS06847595](https://openairdocs.org/sdr/UPS06847595.md): Light · inoperative · Aug 4, 2006 · N880UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:NA EMERGENCY EXIT/DISARM LIGHT INOP. RELAMPED, OPS CHECKED GOOD.
- [SDR UPS06846787](https://openairdocs.org/sdr/UPS06846787.md): Fan · malfunctioned · May 4, 2006 · N880UP · Doug DC873F · Air Distribution Fan
  > SMOKY ODOR NOTICED AT TOP OF DESCENT. SMOKE APPEARED WHEN DESCENDING THROUGH 18000'. AFTER FUMES EVACUATION PROCEDURE SMOKE DISSIPATED. SMELL RECURRED AT ABOUT 5000'. COCKPIT AND GALLEY AREA SMELL OF SMOKE AFTER SHUTDOWN. DEFERRED M324868. REMOVED AND RE
- [SDR UPS06845930](https://openairdocs.org/sdr/UPS06845930.md): Battery Pack · no test · Jan 10, 2006 · N880UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER DC8 MM 33-50-00. OPS CK GOOD.
- [SDR UPS05844559](https://openairdocs.org/sdr/UPS05844559.md): Case · leaking · May 28, 2005 · N880UP · Doug DC873F · Hydraulic System, Main
  > INSPECTION TYPE:N/A EMERGENCY DECLARED, NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER DUE INSPECTION DUE TO LOSS OF HYDRAULIC PRESSURE. LANDED UNEVENTFUL AND TOWED TO RAMP TWO. REMOVED AND REPLACED NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER IAW MM 29-1 0-15-2, FILTER
- [SDR UPS05844507](https://openairdocs.org/sdr/UPS05844507.md): Skin · corroded · May 16, 2005 · N880UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C1, FOUND CORROSION AT AFT MANUFACTURING SPLICE 6 O`CLOCK. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7, 53-5-3 FIG 1, 51-1-20D, AND 51-1-21.
- [SDR UPS05844508](https://openairdocs.org/sdr/UPS05844508.md): Pressure Panel · corroded · Apr 28, 2005 · N880UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C1 CORROSION ON RT W/W CEILING AT STA 863 RBL 42 AND 48 UNDER LONGERONS, ON WEB, AND DOUBLER IN MAIN CABIN IS BULGED. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW SAA SK 880-7620 56 AND EO DC-8-5310-22195-A.
- [SDR UPS05844505](https://openairdocs.org/sdr/UPS05844505.md): Fitting · corroded · Apr 25, 2005 · N880UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 LONGERON SPLICE FITTING HAS HEAVY CORROSION AT STA 1270 L35R. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.

Next page: https://openairdocs.org/deregistered/N880UP-2011-07-19/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 = 'N880UP' AND deregistration_id = 'N880UP-2011-07-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N880UP-2011-07-19/reports

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