# Service difficulty reports: N808UP, cancelled Sep 13, 2010

A list on [N808UP, cancelled Sep 13, 2010](https://openairdocs.org/deregistered/N808UP-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 · 273 reports

- [SDR UPS08853318](https://openairdocs.org/sdr/UPS08853318.md): Slide · unwanted deploy · Sep 11, 2008 · N808UP · Doug DC873F · Escape Slide
  > INSPECTION TYPE:N/A JUMP SEATER OPENED DOOR WITH RAFT ATTACHED. REPACKED EMERGENCY DOOR SLIDE AND SECURED. CHECK OK.
- [SDR UPS08852364](https://openairdocs.org/sdr/UPS08852364.md): Light · malfunctioned · May 26, 2008 · N808UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. EMERGENCY LIGHT SYSTEM OPS CKS GOOD PER MM 33-50-02-2.
- [SDR UPS08852233](https://openairdocs.org/sdr/UPS08852233.md): Skin · damaged · May 9, 2008 · N808UP · Doug DC873F · Fuselage Main, Plate/Skin
  > A/C IS OOS DUE TO FUSELAGE DAMAGE CAUSED BY OTHER CARRIER'S BAGGAGE CART. REPAIRED PER UPS EO DC8-5330-29309-A.
- [SDR UPS08851957](https://openairdocs.org/sdr/UPS08851957.md): Battery Pack · discharged · Apr 2, 2008 · N808UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK.
- [SDR UPS08851952](https://openairdocs.org/sdr/UPS08851952.md): Bracket · broken · Apr 1, 2008 · N808UP · Doug DC873F · Escape Slide
  > FWD LT CREW ENTRY DOOR BOTTOM BRACKET ON SLIDE CASE IS BROKEN CASE SLIDE WILL NOT CLOSE AND SECURE. DEFERRED PER MEL 34-7-4, M 372532. INSTALLED, INSTALLED EMER EVAC SLIDE PACK IAW 25-60-01-2. THIS CLEARS M-372532.
- [SDR UPS08851861](https://openairdocs.org/sdr/UPS08851861.md): Outflow Valve · malfunctioned · Mar 14, 2008 · N808UP · Doug DC873F · Pressure Regulator/Outflow Valve
  > CLIMBING THRU FL250 CABIN PRSR/ALT WARNING HORN SOUNDED. CABIN ATL WAS 13000 FT AND CLIMBING AT 4000 FPM. LOCKED OUTFLOW VLV CLOSED AND TURNED BOTH PACKS TO MAX. NO OTHER LIGHTS OR INDICATIONS. WENT BACK TO AUTO AND WORKED OK. BOTH PACKS WERE AT MINIMUM A
- [SDR UPS08851387](https://openairdocs.org/sdr/UPS08851387.md): Battery Pack · discharged · Jan 6, 2008 · N808UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01-2. CHECKS GOOD.
- [SDR UPS07851222](https://openairdocs.org/sdr/UPS07851222.md): Escape Rope · out of position · Nov 27, 2007 · N808UP · Doug DC873F · Emergency Equipment
  > CAPTAIN'S ESCAPE ROPE COVER FELL OFF, ROPE UNCOILED. REPACKED AND STOWED ESCAPE TAPE AND REINSTALLED AND RESECURED ACCESS DOOR ON CAPTAIN'S ESCAPE ROPE, REF MM 25-60-02-2.
- [SDR UPS07850673](https://openairdocs.org/sdr/UPS07850673.md): Lamp · inoperative · Sep 15, 2007 · N808UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT DISARM. REPLACED LAMP FOR "DISARM" LIGHT. OPERATION CHECK GOOD PER DC8 AMM 33-50-00.
- [SDR UPS07850671](https://openairdocs.org/sdr/UPS07850671.md): Battery Pack · inoperative · Sep 15, 2007 · N808UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WON'T CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-50-00-4.
- [SDR UPS07849870](https://openairdocs.org/sdr/UPS07849870.md): Stringer · cracked · May 17, 2007 · N808UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 CRACK ON FWD STRINGER END FITTING AT XRS 204 FROM STRINGER S-62 - S-63. REMOVED END FITTING AT STA XRS 204 S-62 - S-63 IAW SRM 51-03-02, FABRICATED AND INSTALLED END FITTING AT STA XRS 204 STRINGER S-62 TO STRINGER S-63 IAW DWG 5615767 AND
- [SDR UPS07849889](https://openairdocs.org/sdr/UPS07849889.md): Door Frame · cracked · May 15, 2007 · N808UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:C2 HFEC AND VISUAL INSPECTION DETECTED A.125 INCH CRACK ON THE C-2 DOOR LWR FWD DOOR JAMB CORNER. REPAIRED C-2 DOOR LWR FWD DOOR JAMB CORNER IAW SRM 53-02-00-0 FIG 22, AND SRM TR 53-187.
- [SDR UPS07849836](https://openairdocs.org/sdr/UPS07849836.md): Floorbeam · corroded · May 14, 2007 · N808UP · Doug DC873F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C2 FLOORBEAM STA 1300 RBL 12 HAS EXFOLIATION CORROSION BETWEEN FLOORBEAM AND FLOORBOARD. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER. IAW SRM 51-1-8, 53-7-3 FIG 10, 51-2-1 FIG 1 SHT 7, TR 51-130 NOTE 19.
- [SDR UPS07849854](https://openairdocs.org/sdr/UPS07849854.md): Stiffener · corroded · May 13, 2007 · N808UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 STIFFENER IN RT WHEEL WELL STA 857 HAS EXFOLIATION CORROSION. REMOVED STIFFENER AT STA 857 RT WHEEL WELL IAW SRM 51-1-21. FABRICATE AND INSTALLED STIFFENER AT STA 857 RT WHEEL WELL IAW DWG 5613917-19 AND SRM 51-1-20D.
- [SDR UPS07849912](https://openairdocs.org/sdr/UPS07849912.md): Skin · cracked · May 9, 2007 · N808UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 BULGING SKIN ON EXTERIOR OF SKIN AT STA 290 L21L AFT OF MAIN CARGO DOOR. REPAIRED FUSELAGE SKIN AT STA 290 L21L AFT OF MAIN CARGO DOOR IAW SAA EA 008-5330-01-A0883, UPS EO DC8-5330-26921-A, AND FAA FORM 8100-9.
- [SDR UPS07849888](https://openairdocs.org/sdr/UPS07849888.md): Attach Angle · cracked · May 8, 2007 · N808UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 CENTER WING EXTERIOR FUSELAGE -L- ANGLE CRACKED AT ST 857.125 RBL 65. REMOVED CRACKED -L- ANGLE AT STA 857.125 RBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR -L- ANGLE AT STA 857.125 RBL 65 IAW DWG 5649893, AND SRM 51-01-20D.
- [SDR UPS06848468](https://openairdocs.org/sdr/UPS06848468.md): Lamp · inoperative · Nov 4, 2006 · N808UP · Doug DC873F · Emergency Lighting
  > FOUND 1 DOOR EMERGENCY LIGHT INOP. RELAMPED. OPS CK OK.
- [SDR UPS06847552](https://openairdocs.org/sdr/UPS06847552.md): Slide · unwanted deploy · Aug 1, 2006 · N808UP · Doug DC873F · Escape Slide
  > MAIN CARGO DOOR EXIT SLIDE FELL OUT OF HOLDER, BROKEN CLIP ON COVER EMERG ESCAPE SLIDE INOP. SLIDE REMOVED FROM DOOR AND DEFERRED IAW MEL 52-07-4 AND ASSIGNED DEFERRAL NR M330482. REPLACED DMGD CLIP ON ESCAPE SLIDE COVER PER SMR 51-01-21. RE- INSTALLED SLIDE
- [SDR UPS06847128](https://openairdocs.org/sdr/UPS06847128.md): Battery Pack · no test · Jun 13, 2006 · N808UP · Doug DC873F · Emergency Lighting
  > EMERG EXIT LIGHTS WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK PER AMM. OPS CK NORMAL, P/N ON 5708458-503, S/N FTL010.
- [SDR UPS05845845](https://openairdocs.org/sdr/UPS05845845.md): Fire Warning · illuminated · Nov 29, 2005 · N808UP · Doug DC873F · Fire Detection
  > LOWER CARGO FIRE AMBER MX LIGHT CAME ON AFTER 4 HOURS OF FLIGHT (5 AND 11). PERFORMED ADJUSTMENT AND TEST PER DC-8 M/M 26-18-00-5, NO FAULTS FOUND IN MEMORY OR SIGNAL STRENGTH.
- [SDR UPS05845377](https://openairdocs.org/sdr/UPS05845377.md): Battery Pack · failed · Sep 9, 2005 · N808UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A DURING ROUTINE MX, EMERGENCY LIGHTING WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK ASSY IAW AMM 33-50-01-2, EMERGENCY LIGHTING OPS CHECKS NORMAL.
- [SDR UPS05844578](https://openairdocs.org/sdr/UPS05844578.md): Longeron · corroded · May 12, 2005 · N808UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSP TYPE: C3, D PIT INTERGRANULAR CORROSION ON L34R STA 1412. REMOVED AND REPLACED LONGERON 34R STA 1390-1460 IAW SRM 51-1-21D.
- [SDR UPS05844487](https://openairdocs.org/sdr/UPS05844487.md): Longeron · cracked · May 6, 2005 · N808UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C3, LONGERON 14L CRACKED AT STA 1746. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-2-2 FIG 11 AND 51-1-20D.
- [SDR UPS05844472](https://openairdocs.org/sdr/UPS05844472.md): Longeron · cracked · May 6, 2005 · N808UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C3 LONGERON CRACKED 1/4 INCH LONG AT STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED STRAPS 2 EA IAW DC-8 SRM 53-02-02, 51-1-8, 53-2-2 FIG 10 AND 51-1-20D.
- [SDR UPS05844490](https://openairdocs.org/sdr/UPS05844490.md): Rib · cracked · May 5, 2005 · N808UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C3, LEFT L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21 AND 51-1-20D.
- [SDR UPS05844489](https://openairdocs.org/sdr/UPS05844489.md): Rib · cracked · May 5, 2005 · N808UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C3, LT WING L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21, 51-1-20D AND DWG 5769471.
- [SDR UPS05844485](https://openairdocs.org/sdr/UPS05844485.md): Rib · cracked · May 5, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LT WING L/E AT XFS 385.000 LWR RIB CRACKED 2 INCHES LONG MIDDLE OF RIB. FABRICATED AND INSTALLED RIB FORMER AND 2 EA REPAIR ANGLES IAW DWG 5769603, SRM 51-3-2, 57-2-1 AND 51-3-2.
- [SDR UPS05844479](https://openairdocs.org/sdr/UPS05844479.md): Rib · cracked · May 5, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED XFS 316.000. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-21, 51-1-20D AND 51-1-15.
- [SDR UPS05844498](https://openairdocs.org/sdr/UPS05844498.md): Rib · cracked · May 4, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB CRACKED AT STA XFS 438. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR ANGLE DOUBLERS IAW SRM 53-02-00 FIG 001B, 51-1-21.
- [SDR UPS05844497](https://openairdocs.org/sdr/UPS05844497.md): Rib · cracked · May 4, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 408. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D AND DWG 5770375.
- [SDR UPS05844496](https://openairdocs.org/sdr/UPS05844496.md): Rib · cracked · May 4, 2005 · N808UP · Doug DC873F · Wing, Longeron/Stringer
  > INSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED AT XFS 391. STOP DRILLED CRACK, FABBED AND INSTALLED 2 EA DOUBLERS IAW SRM 57-2-0 FIG 2, 57-2-0, 51-1-20D, 51-1-8 AND DWG 5770087.
- [SDR UPS05844491](https://openairdocs.org/sdr/UPS05844491.md): Rib · cracked · May 4, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 385.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS 2 EA IAW SRM 57-2-0 FIG 018, 51-1-20D, 51-1-15 AND DWG 5770087.
- [SDR UPS05844486](https://openairdocs.org/sdr/UPS05844486.md): Skin · cracked · May 4, 2005 · N808UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE: C3, LT WING L/E UPPER SKIN FASTENER HOLES CRACKED.125 INCH LONG AT XFS 450. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 57-2-1-0 AND 51-3-2.
- [SDR UPS05844470](https://openairdocs.org/sdr/UPS05844470.md): Skin · damaged · May 4, 2005 · N808UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 LT WING L/E AT XFS 454, LWR SURFACE FASTENER HOLES ARE ELONGATED. REMOVE DAMAGE AND INSTALLED DOUBLER AND FILLER IAW EO DC-8 5720- 7767-A AND SRM 51-1-21.
- [SDR UPS05844494](https://openairdocs.org/sdr/UPS05844494.md): Rib · cracked · May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 828.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B, 57-2-0 FIG 2B, AND DWG'S 5769470-45, 576947U.
- [SDR UPS05844488](https://openairdocs.org/sdr/UPS05844488.md): Rib · cracked · May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 822.500.5 INCH LONG. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2 -0, 57-2-0 FIG 2, 51-1-20D, 51-1-21 AND DWG 5769470.
- [SDR UPS05844484](https://openairdocs.org/sdr/UPS05844484.md): Rib · cracked · May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED.25 INCH LONG AT XFS 809. STOP DRILLED CRACK AND FABRICATED INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.
- [SDR UPS05844471](https://openairdocs.org/sdr/UPS05844471.md): Rib · cracked · May 3, 2005 · N808UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 LT WING L/E UPPER RIB CRACKED 1/4 INCH LONG AT XFS779. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-2-0 FIG 2, DWG 5769470-29 AND SRM 51-1-20D,51-1-21 AND 51-1-15.
- [SDR UPS05844577](https://openairdocs.org/sdr/UPS05844577.md): Doubler · corroded · May 2, 2005 · N808UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSP TYPE: C3, A/C BAY L30R AT APPROX STA 38 TO STA 58 DOME NUTS UNDER LONGERON HAVE CORROSION OUT OF LIMITS AT ATTACH INTERNAL DOUBLER. R & R INTERNAL DOUBLER AT STA 38-58 L31R AND 2 EA LONGERONS AT STA 8 TO 70 L27R AND L30R IAW SRM 51-1-21 AND 51-1-20D.
- [SDR UPS05844469](https://openairdocs.org/sdr/UPS05844469.md): Splice · cracked · May 2, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 "D" PIT BETWEEN STA 1340-1360 L30R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-21 AND 51-1-20D.
- [SDR UPS05844685](https://openairdocs.org/sdr/UPS05844685.md): Frame · corroded · May 1, 2005 · N808UP · Doug DC873F · Fuselage Main, Frame
  > STA 1160 SEVERE CORROSION ON BASE OF FRAME AT L33L. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-1-20D, 51-1-20 D, DWG 3755842 AND SK808-785521.
- [SDR UPS05844483](https://openairdocs.org/sdr/UPS05844483.md): Fitting · cracked · May 1, 2005 · N808UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C3, LWR CUSP AT STA 153 RT CUSP TO FRAME FITTING AT TORQUE BOX IS CRACKED BOTH UPPER AND LWR OF CUSP, LENGTH OF FITTING. REMOVED AND REPLACED FRAME FITTING IAW SRM 51-1-21 AND 51-1-20D.
- [SDR UPS05844475](https://openairdocs.org/sdr/UPS05844475.md): Web · cracked · Apr 30, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous Structure
  > RT MLG AFT WEB CRACKED AT GEAR CUTOUT LWR CORNER OLD REPAIR CRACKED IN RADIUS. REMOVED WEB, FAB REPLACEMENT WEB AND INSTALLED IAW SRM51-1-21, 51-1-21D, SAA FAB TRAVLER NR 0001 AND 21-1-21A.
- [SDR UPS05844687](https://openairdocs.org/sdr/UPS05844687.md): Pressure Panel · cracked · Apr 29, 2005 · N808UP · Doug DC873F · Fuselage Main, Bulkhead
  > RT MLG WW FWD BULKHEAD LOWER SECTION FASTENERS HAVE MILD CORROSION IN SEVERAL PLACES RUNNING INBD TO OTBD AT SPLICE. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW SRM 53-2-0. HFEC INSP DETECTED 3 CRACKS. FABRICATED AND INSTALLED 3 EA. REPAIR ANGLES AND 1
- [SDR UPS05844474](https://openairdocs.org/sdr/UPS05844474.md): Fitting · cracked · Apr 29, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 C-1 CARGO FITTING CRACKED AT FS 280 L32R. FOUND ON X-RAY OF DOOR CORNER EO DC8-5330-20206-B. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-2.
- [SDR UPS05844686](https://openairdocs.org/sdr/UPS05844686.md): Web · cracked · Apr 28, 2005 · N808UP · Doug DC873F · Fuselage Miscellaneous Structure
  > LT FWD UPPER AC BAY AT APPROX STA 8 WEB IS CRACKED APPROX 4 INCH LONG IN 2 PLACES. FABRICATED AND INSTALLED 2 DOUBLERS AND REPAIR WEB IAW SRM 53-03-03-0, 53-02-00-0 FIG 001D, 53-2-0 FIG 1D 51-1-21,51-1-20D AND 51-1-21A.
- [SDR UPS05844477](https://openairdocs.org/sdr/UPS05844477.md): Skin · cracked · Apr 27, 2005 · N808UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 L16L HAS CRACK APROX 3/4 INCH LONG. REMOVED EXISTING DOUBLER AND FINGER DOUBLER AND FABRICATED EXTERNAL DOUBLER AND INSTALLED EXISTING FINGER DOUBLER, EXTERNAL DOUBLER AND FILLER IAW DC-8 SRM 51-1-21, 51-1-20
- [SDR UPS05844476](https://openairdocs.org/sdr/UPS05844476.md): Skin · cracked · Apr 27, 2005 · N808UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 RT L16 HAS CRACK APROX. 1/2 INCH LENGTH. CUT OUT DAMAGE AND INSTALLED DOUBLER, FINGER DOUBLER FILLER AND EXTERNAL DOUBLER IAW SRM 53-02-01-0 FIG 007.
- [SDR UPS05843872](https://openairdocs.org/sdr/UPS05843872.md): Windshield · cracked · Feb 10, 2005 · N808UP · Doug DC873F · Flight Compartment Windows
  > CAPTAIN'S LT SIDE WINDSHIELD CRACKED. BACK TO BLOCK. REMOVED AND REPLACED LT SIDE WINDSHIELD, WINDSHIELD HEAT CONTROLLER, LOWER POWER RELAY AND HIGH POWER RELAY IAW DC8 AMM 56-10-02-2, OPS CHECK GOOD.
- [SDR UPS04841891](https://openairdocs.org/sdr/UPS04841891.md): Regulator · leaking · Feb 12, 2004 · N808UP · Doug DC873F · Crew Oxygen System
  > F/O OXYGEN REGULATOR LEAKING. REMOVED AND REPLACED 02 BOTTLE IAW MM 12-70-01-3, NO LEAKS NOTED.

Next page: https://openairdocs.org/deregistered/N808UP-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 = 'N808UP' AND deregistration_id = 'N808UP-2010-09-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N808UP-2010-09-13/reports

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