# Service difficulty reports: N703UP, cancelled Mar 30, 2010

A list on [N703UP, cancelled Mar 30, 2010](https://openairdocs.org/deregistered/N703UP-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 8 · 368 reports

- [SDR UPS07851332](https://openairdocs.org/sdr/UPS07851332.md): Battery Pack · malfunctioned · Dec 26, 2007 · N703UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01-2, SN OFF 356 SN ON UP12384.
- [SDR UPS07851330](https://openairdocs.org/sdr/UPS07851330.md): Battery · inoperative · Dec 26, 2007 · N703UP · Doug DC871F · Emergency Lighting
  > ON PRE-FLIGHT, FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT ASSY IAW AMM 33-50-01-2.
- [SDR UPS07850475](https://openairdocs.org/sdr/UPS07850475.md): Slide · out of position · Aug 17, 2007 · N703UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A EMERGENCY EXIT SLIDE AT CREW ENTRY DOOR IS PARTIALLY OUT OF PACK. SECURED EVAC SLIDE AS PER AMM 25-60-01. NO DEFECTS NOTED.
- [SDR UPS07850409](https://openairdocs.org/sdr/UPS07850409.md): Brake · fire · Aug 7, 2007 · N703UP · Doug DC871F · Brake
  > INSPECTION TYPE:N/A NR 8 BRAKE ON FIRE AT BLOCK IN. REMOVED AND REPLACED NR 8 BRAKE ASSY. INSPECTED AREA AND FOUND NO FURTHER DAMAGE. REPLACED WHEEL AND TIRE ASSY PER MM 32-40-01-2 DUE TO HEAT DISTRESS TO WHEEL. BRAKE ASSY INSTALLED PER MM 32-42-01-4. OK
- [SDR UPS07850160](https://openairdocs.org/sdr/UPS07850160.md): Light · inoperative · Jul 11, 2007 · N703UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT DISARM LIGHT ON OVERHEAD PANEL IS INOP. RELAMPED EMERGENCY EXIT DISARM LIGHT ON OVERHEAD PANEL PER MM 33-13-00-2.
- [SDR UPS07850152](https://openairdocs.org/sdr/UPS07850152.md): Case · separated · Jul 11, 2007 · N703UP · Doug DC871F · Emergency Equipment
  > INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE CASE IS SEPARATED. CLOSED SLIDE COVER AND RE-INSTALLED PIN PER MM 25-60-01-2.
- [SDR UPS07850089](https://openairdocs.org/sdr/UPS07850089.md): Battery Pack · no test · Jun 28, 2007 · N703UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHT FAILS TO TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 33-50-01-2-4. OPS CHECK OK.
- [SDR UPS07849226](https://openairdocs.org/sdr/UPS07849226.md): O-Ring · leaking · Feb 21, 2007 · N703UP · Doug DC871F · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:N/A EMERGENCY DECLARED - AT TOP OF DESCENT FLUID DROPPED TO AUX POSITION PERFORMED LOSS OF FLUID ON PRESSURE CHECKLIST. AS PER QRH LANDING & TAXI IN NORMAL. FLUID INDICATION NEVER DROPPED BELOW AUX POSITION. FOUND LEFT MLG BOGIE SWIVEL UNLOC
- [SDR UPS06848466](https://openairdocs.org/sdr/UPS06848466.md): Lamp · inoperative · Nov 3, 2006 · N703UP · Doug DC871F · Emergency Lighting
  > ENTRY AREA EMERGENCY OVERHEAD LIGHT INOP. RELAMPED THE ENTRY AREA OVERHEAD LIGHT. OPS CKS NORMAL.
- [SDR UPS06848465](https://openairdocs.org/sdr/UPS06848465.md): Light · inoperative · Nov 3, 2006 · N703UP · Doug DC871F · Emergency Lighting
  > EMERGENCY LIGHTS OVER ENTRY DOOR INOP. RELAMPED THE OVERHEAD ENTRY DOOR LIGHT ASSY. OPS CKS NORMAL.
- [SDR UPS06848324](https://openairdocs.org/sdr/UPS06848324.md): Line · failed · Oct 25, 2006 · N703UP · Doug DC871F · Hydraulic System, Main
  > LOSS OF HYDRAULICS ON TAXI IN. HYDRAULIC LEAK RT WHEEL WELL. HYDRAULIC LINE TO THE RIGHT GEAR OVERCENTER LINK ACTUATOR FAILED. FOUND PRESSURE LINE TO R/H GEAR BUNGEE CYLINDER LEAKING. REPLACED LINE WITH TEMP LINE IAW 32-32903-2. REPOSITIONED LINES AND LK CK
- [SDR UPS06846643](https://openairdocs.org/sdr/UPS06846643.md): Battery · discharged · Apr 4, 2006 · N703UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY DEAD R&R EMERGENCY EXIT LIGHT BATTERY PACK W/R/T M/M 33-50-01-2 OPS CK GOOD.
- [SDR UPS06846442](https://openairdocs.org/sdr/UPS06846442.md): Repair · misinstalled · Feb 28, 2006 · N703UP · Doug DC871F · Fuselage Main, Plate/Skin
  > C-2 DOOR JAMB UPPER AFT CORNER REPAIR DOES NOT MEET REQUIREMENTS OF SRM 53-2-0, AND DWG SRO 8530019. REMOVED EXISTING DOUBLER ON C-2 DOOR JAMB UPPER AFT CORNER IAW SRM 53-2-0 FIG 20, FABRICATED AND INSTALLED FILLERS DOUBLER AND TRIPLER IAW SRM53-02-00 FIG 20
- [SDR UPS06846401](https://openairdocs.org/sdr/UPS06846401.md): Door Frame · gouged · Feb 24, 2006 · N703UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C1 D-PIT AFT LOWER DOOR SURROUND FRAME FITTING HAS DEEP GOUGE. REMOVED AND REPLACED FRAME FITTING IAW SRM 51-3-0.
- [SDR UPS06846438](https://openairdocs.org/sdr/UPS06846438.md): Spar Cap · cracked · Feb 23, 2006 · N703UP · Doug DC871F · Wing Spar
  > RT WW LWR SPAR CAP CRACKED 1/2" LONG AT STA 857.125. STOP DRILLED CRACK AT AT RT WW LWR SPAR CAP IAW SRO 8570009 INSTALLED -47 PLUG IN WING SKIN, FABRICATED AND INSTALLED REPAIR ANGLES, AND -66 SPACER IAW SRO 8570009, AND SRM 51-1-20D AT STA 857.125 RT WW LWR
- [SDR UPS06846437](https://openairdocs.org/sdr/UPS06846437.md): Attach Fitting · cracked · Feb 23, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 LONGERON ATTACH FITTING CRACKED AT STA 1240 L33R. REMOVED AND REPLACED LONGERON ATTACH FITTING AT STA 1240 L33R IAW SRM 51-1-20D, AND SRM 51-1-8.
- [SDR UPS06846435](https://openairdocs.org/sdr/UPS06846435.md): Frame · gouged · Feb 23, 2006 · N703UP · Doug DC871F · Fuselage Main, Frame
  > C-PIT STA 1140 FRAME UPPER FLANGE ABOVE LONGERON 34R HAS DEEP, LONG DRILL WALK. REMOVED AND REPLACED FRAME UPPER CAP IAW SRM 20-15-00-2,51-3-2 AND 51 -1-20D.
- [SDR UPS06846439](https://openairdocs.org/sdr/UPS06846439.md): Bulkhead · corroded · Feb 22, 2006 · N703UP · Doug DC871F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C1 IN 60 HOLE CORROSION ON WEB UNDER L-ANGLE OF BULKHEAD JUST AFT OF HOLE ENTRANCE. REMOVED CORRODED WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR WEB AND ANGLE AT STA 1788 IAW SRM 53-02-00-0, 53-05-03-0, AND S
- [SDR UPS06846405](https://openairdocs.org/sdr/UPS06846405.md): Fitting · corroded · Feb 22, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 IN 60 HOLE, FRAME FITTING ON FIRST LATERAL FRAME SUPPORT RT CENTER ABOVE ENTRANCE HAS BAD CORROSION AROUND FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D AND DWG 3753645.
- [SDR UPS06846404](https://openairdocs.org/sdr/UPS06846404.md): Support Channel · broken · Feb 22, 2006 · N703UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 STA 360 L34L FLOOR SUPPORT CHANNEL BROKEN. REMOVED, FABRICATED AND INSTALLED SUPPORT CHANNEL IAW SRM 51-1-21 AND DWG 9759429.
- [SDR UPS06846338](https://openairdocs.org/sdr/UPS06846338.md): Web · cracked · Feb 22, 2006 · N703UP · Doug DC871F · Fuselage Miscellaneous Structure
  > FOUND PIT SLIDING CARGO DOOR TORQUE BOX UPPER WEB CRACKED STA 1220 L33L. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-02-00, AND 51-1-21.
- [SDR UPS06846407](https://openairdocs.org/sdr/UPS06846407.md): Finger Doubler · corroded · Feb 21, 2006 · N703UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 AFTER SKIN REMOVAL FOUND FINGER DOUBLER CORRODED OUT OF LIMITS AND CRACKED STA 1350 - 1390 L31R. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-04-01-0, 51-1-20D.
- [SDR UPS06846406](https://openairdocs.org/sdr/UPS06846406.md): Shear Tie · corroded · Feb 21, 2006 · N703UP · Doug DC871F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORROSION OUT OF LIMITS AND CRACKED AT STA 1400 BETWEEN L35R- L36. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 51-1-21, 51-1-20D, 53-02-33.
- [SDR UPS06846398](https://openairdocs.org/sdr/UPS06846398.md): Shear Tie · cracked · Feb 21, 2006 · N703UP · Doug DC871F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 BETWEEN L31L-L32L. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-04-01 FIG 51, 51-1-20D AND 51-1-21.
- [SDR UPS06846397](https://openairdocs.org/sdr/UPS06846397.md): Shear Tie · cracked · Feb 21, 2006 · N703UP · Doug DC871F · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:C1 AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1440 BETWEEN L33R-L34R. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW 53-04-01 FIG 51, 51-1-20D AND 51-1-21.
- [SDR UPS06846358](https://openairdocs.org/sdr/UPS06846358.md): Shear Tie · corroded · Feb 21, 2006 · N703UP · Doug DC871F · Fuselage Internal Mounting Structure
  > AFTER SKIN REMOVAL FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 L35R-L36. REMOVED SHEAR TIE AT STA 1380 L35R-L36 IAW SRM 51-1-21. FABRICATED AND INSTALLED SHEAR TIE AT STA 1380 L35R-L36 IAW SRM 53-02-00-0, 51-1-8, SRM 51-1-21, 51-1-20D.
- [SDR UPS06846357](https://openairdocs.org/sdr/UPS06846357.md): Shear Tie · corroded · Feb 21, 2006 · N703UP · Doug DC871F · Fuselage Internal Mounting Structure
  > AFTER REMOVAL OF SKIN FOUND SHEAR TIE CORRODED OUT OF LIMITS AND CRACKED AT STA 1380 L34L AND L35L. REMOVED SHEAR TIE AT FS 1380 L34L-L35L IAW SRM 51-01-20D. FABRICATED AND INSTALLED SHEAR TIES AT STA 1380 L34L-L35L IAW SRM 53-02-00-0, 51-1-8, AND SRM 51-1-2
- [SDR UPS06846332](https://openairdocs.org/sdr/UPS06846332.md): Keelbeam · cracked · Feb 21, 2006 · N703UP · Doug DC871F · Fuselage Main, Keel
  > FITTING CRACKED ON RT CORNER IN RADIUS OF KEEL BEAM STA 960. REMOVED AND REPLACED L ANGLE AT STA 960 RT IAW SRM 51-1-2OD, 51-1-15 AND SRM 51-3-0.
- [SDR UPS06846436](https://openairdocs.org/sdr/UPS06846436.md): Floorbeam · corroded · Feb 20, 2006 · N703UP · Doug DC871F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C1 IN A/C COMPT CEILING, FLOORBEAM STA 50 BETWEEN RBL 10-25 HAS CORROSION. REMOVED CORRODED UPPER FLANGE OF FLOORBEAM AT STA 50 RBL 10 -25 IAW SRM 51-1-8, AND SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR FLANGE, REPAIR ANGLE AND REPAIR
- [SDR UPS06846402](https://openairdocs.org/sdr/UPS06846402.md): Attach Fitting · corroded · Feb 20, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 FRAME ATTACH FITTING HEAVY CORRODED AT STA 834.500 L22R. REMOVED AND REPLACED FRAME ATTACH FITTING IAW SRM 51-1-20D.
- [SDR UPS06846340](https://openairdocs.org/sdr/UPS06846340.md): Fitting · cracked · Feb 20, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND FRAME ATTACH FITTING CRACKED AT STA 822.500 L22L AFT SIDE. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 53-1-0 AND 51-3-2.
- [SDR UPS06846335](https://openairdocs.org/sdr/UPS06846335.md): Longeron · cracked · Feb 20, 2006 · N703UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > FOUND POSSIBLE CRACK ON LONG 32L AT FS 1440. REMOVED DAMAGED LONGERON FROM STA 1350-1490, FABRICATE AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 51-1-20D, 51-3-2 AND DWG 3645897.
- [SDR UPS06846444](https://openairdocs.org/sdr/UPS06846444.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND FITTING CRACKED AT STA 700 L13R FWD SIDE. REMOVED CRACKED FITTING AT STA 700 L13R IAW SRM 51-1-20D. FABRICATED AND INSTALLED FITTING AT STA 700 L13R IAW DWG 3779978, AND SRM 51-1-20D.
- [SDR UPS06846403](https://openairdocs.org/sdr/UPS06846403.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 1160 L19R AFT SIDE. REMOVE AND REPLACE FITTING IAW SRM 51-1-20D.
- [SDR UPS06846395](https://openairdocs.org/sdr/UPS06846395.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 FITTING CRACKED AT STA 834.500 L22R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
- [SDR UPS06846355](https://openairdocs.org/sdr/UPS06846355.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND LONGERON END FITTING CRACKED AT STA 902.125 L4L. REMOVED AND REPLACED END FITTING AT STA 902.125 L4L IAW SRM 51-1-20D, 51-3-0 AND SRM 51-1-21.
- [SDR UPS06846354](https://openairdocs.org/sdr/UPS06846354.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND FITTING CRACKED AT STA 820 L18L. REMOVED AND REPLACED END FITTING AT STA 820 L18L IAW SRM 51-1-20D, 51-03-02-0 AND SRM 51-01-08-0.
- [SDR UPS06846339](https://openairdocs.org/sdr/UPS06846339.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND ATTACH FITTING CRACKED AT STA 1150 L18R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D.
- [SDR UPS06846334](https://openairdocs.org/sdr/UPS06846334.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND LONGERON END FITTING CRACKED AT STA.857.125 L9L. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21 AND 51-1-20D.
- [SDR UPS06846331](https://openairdocs.org/sdr/UPS06846331.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND LONGERON END FITTING CRACKED AT STA 680 L5R. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L5R IAW SRM 51-01-21, 51-03-02-0 AND SRM 51-01-20D.
- [SDR UPS06846330](https://openairdocs.org/sdr/UPS06846330.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND LONGERON END FITTING AT STA 902.125 L8R IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 902.125 L8R IAW SRM 51-1-21, 51-1-20D, AND SRM 51-3-0.
- [SDR UPS06846329](https://openairdocs.org/sdr/UPS06846329.md): Fitting · cracked · Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > LONGERON END FITTING CRACKED AT STA 857.125 L7L. REMOVED AND REPLACED LONGERON END FITTING AT STA 857.125 L7L IAW 51-3-2 AND SRM 51-1-20D.
- [SDR UPS06846440](https://openairdocs.org/sdr/UPS06846440.md): Skin · corroded · Feb 17, 2006 · N703UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE FOUND LWR SKIN CORRODED IN SEVERAL AREAS BEYOND LIMITS. REMOVED AND REPLACED LWR BELLY SKIN AT STA 1350-1450 L31L TO L32R IAW SRM 51-01-20D, 51-01-21, AND DWG 5615572
- [SDR UPS06846333](https://openairdocs.org/sdr/UPS06846333.md): Skin · cracked · Feb 14, 2006 · N703UP · Doug DC871F · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CRACKED 1" LONG AT STA 1746 L17L. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7, 51-1-21 AND 51-1-20D.
- [SDR UPS06846353](https://openairdocs.org/sdr/UPS06846353.md): Fitting · cracked · Jan 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach Fittings
  > FOUND STA 1180 L20R FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 1180 L20R IAW SRM 51-1-20D, 51-3-2 AND 51-1-8.
- [SDR UPS05845558](https://openairdocs.org/sdr/UPS05845558.md): Battery Pack · weak · Oct 6, 2005 · N703UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-50-01-2.
- [SDR UPS05845520](https://openairdocs.org/sdr/UPS05845520.md): Indicator · inoperative · Sep 27, 2005 · N703UP · Doug DC871F · Pitot/Static System
  > ALL 3 (CAPT'S, FO'S & ALTERANTE) AIRSPEED INDICATIONS ARE UNRELIABLE. AIR TURN BACK - EMERGENCY DECLARED. REPLACED STANDBY ALT/AIRSPEED INDICATOR PER MM 34-11-02-4. R&R AUXILIARY PITOT STATIC DRAIN. SYSTEM OPS CKS NORMAL IAW AMM 34-12-00-5.
- [SDR UPS05845402](https://openairdocs.org/sdr/UPS05845402.md): Adc · failed · Sep 12, 2005 · N703UP · Doug DC871F · Air Data Computer
  > INSPECTION TYPE:N/A ATB - AFTER T/O LOST NR 1 ADC, PULLED C/B COULD NOT RESTORE, XFRD TO NR 2 ADC ON CAPT SIDE. ATB DUE TO SLIGHT ELEC BURNING SMELL. REMOVED AND REPLACED AIR DATA COMP IAW MM 34-11-01-4 AND NR 1 ADC SELECT XFR RELAY IAW MM 20-50-16-2. CHECK
- [SDR UPS04841952](https://openairdocs.org/sdr/UPS04841952.md): Intercostal · cracked · Feb 17, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C3, STATION 25 CUSP WEB/INTERCOSTAL IS CRACKED AT LONG 21L. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.
- [SDR UPS04841951](https://openairdocs.org/sdr/UPS04841951.md): Bearing · corroded · Feb 12, 2004 · N703UP · Doug DC871F · Horizontal Stabilizer Structure
  > INSPECTION TYPE: C3, LEFT HORIZONTAL STAB HINGE BEARING WILL NOT ACCEPT GREASE. DISASSEMBLED HINGE. FOUND STAB BEARING BORE CORRODED. REPAIRED PER SAA SK 703-677 AND UPS EO DC8-5510-19991-A.

Next page: https://openairdocs.org/deregistered/N703UP-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 = 'N703UP' AND deregistration_id = 'N703UP-2010-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N703UP-2010-03-30/reports

---
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