# Service difficulty reports: N818UP, cancelled Dec 27, 2010

A list on [N818UP, cancelled Dec 27, 2010](https://openairdocs.org/deregistered/N818UP-2010-12-27.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 · 266 reports

- [SDR UPS08852110](https://openairdocs.org/sdr/UPS08852110.md): Battery Pack · discharged · Apr 29, 2008 · N818UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTING DIM. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK ASSY IAW AMM 33-50-01-2-4. OPS CHECK NORMAL.
- [SDR UPS08851983](https://openairdocs.org/sdr/UPS08851983.md): Thrust Reverser · malfunctioned · Apr 9, 2008 · N818UP · Doug DC873F · Engine Thrust Reverser
  > DURING DESCENT NR 2 THRUST REVERSER W/NOT STOW IN FWD THRUST INDICATION BLINKED ON AND OFF. DEFERRED NR 2 ENGINE T/R, IN FWD THRUST POSITION. PLACARD INSTALLED. T/S PER MM 78-00-00-1 FIG 190 SHEETS 1-3. NO DEFECTS NOTED. THIS CLEARS M373174. PLACARD REMOVED
- [SDR UPS08851963](https://openairdocs.org/sdr/UPS08851963.md): Battery · inoperative · Apr 2, 2008 · N818UP · Doug DC873F · Emergency Lighting
  > PREFLIGHT, EMERGENCY INSTRUMENT LIGHTS DID NOT ILLUMINATE AND C/P DOME LIGHT SAME. DISARM CHECKS OK. REMOVED AND REPLACED BATTERY AND RELAY UNIT IAW MM 33-50-01-2. SYSTEM OK FOR CONTINUED SERVICE.
- [SDR UPS08851545](https://openairdocs.org/sdr/UPS08851545.md): Light · inoperative · Jan 23, 2008 · N818UP · Doug DC873F · Emergency Lighting
  > ON SHUTDOWN CHECKLIST, EMERGENCY EXIT LIGHTS DOES NOT ILLUMINATE. IN DISARM POSITION LIGHT WILL NOT PRESS TO TEST. RELAMPED EMERGENCY EXIT INDICATION LIGHT PER STD PRACTICES. OPS CHECKS NORMAL.
- [SDR UPS07850405](https://openairdocs.org/sdr/UPS07850405.md): Battery · discharged · Aug 7, 2007 · N818UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY UNIT PER MM 33-50-01-2. OPS CHECK GOOD.
- [SDR UPS07849983](https://openairdocs.org/sdr/UPS07849983.md): Slide · misinstalled · Jun 17, 2007 · N818UP · Doug DC873F · Escape Slide
  > MAIN EXIT ESCAPE SLIDE IS IMPROPERLY LOCATED INSIDE HOUSING. PRESSURE CANNOT BE READ. REMOVED AND REPLACED MAIN EXIT ESCAPE SLIDE CONTAINER IAW MM 25-60-01-2. PRESSURE INDICATOR VISIBLE THROUGH WINDOW.
- [SDR UPS07849982](https://openairdocs.org/sdr/UPS07849982.md): Fastener · faulty · Jun 16, 2007 · N818UP · Doug DC873F · Emergency Equipment
  > INSPECTION TYPE:N/A CAPTAINS ESCAPE ROPE FELL OUT OF STOW LOCATION. CHECK FOR PROPER STOWAGE. REPLACED FASTENER FOR DOOR CLIP. REINSTALLED ROPE AND DOOR. OPS CHECK NORMAL.
- [SDR UPS06847324](https://openairdocs.org/sdr/UPS06847324.md): Battery Pack · discharged · Jul 13, 2006 · N818UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.
- [SDR UPS06847129](https://openairdocs.org/sdr/UPS06847129.md): Splice · cracked · Jun 6, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 FS 1360 L23R SPLICE FITTING IS CRACKED AT AFT END. REMOVED CRACKED SPLICE FITTING AT STA 1360 L23R IAW SRM 51-3-0 AND SRM 51-1-20D, FABRICATED AND INSTALLED SPLICE FITTING AT STA 1360 L23R IAW SRM 51-1-20D AND DWG 3755118.
- [SDR UPS06847066](https://openairdocs.org/sdr/UPS06847066.md): Fitting · cracked · May 26, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 BATH TUB FITTING AT STA 1690 L32L IS CRACKED. REMOVED AND REPLACED BATH TUB FITTING AT STA 1690 L32L IAW SRM 51-1-20D, AND DWG 4641326.
- [SDR UPS06847065](https://openairdocs.org/sdr/UPS06847065.md): Fitting · cracked · May 26, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 STA 1690 L31R BATH TUB FITTING IS CRACKED. REMOVED BATH TUB FITTING AT STA 1690 L31R IAW SRM 51-1-20D DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1690 L31R IAW SRM 51-1-24, AND SRM 51-1-20D
- [SDR UPS06847009](https://openairdocs.org/sdr/UPS06847009.md): Hinge Fitting · cracked · May 23, 2006 · N818UP · Doug DC873F · Passenger/Crew Doors
  > INSPECTION TYPE:C1 DURING REMOVAL OF L-1 DOOR UPPER DOOR HINGE FITTING ASSY CRACKED. REMOVED AND REPLACED L-1 DOOR UPPER HINGE FITTING ASSY IAW SRM 51-1-2 0D, AND 51-3-0.
- [SDR UPS06847062](https://openairdocs.org/sdr/UPS06847062.md): Fitting · corroded · May 20, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 C PIT STA 1228 BETWEEN L35R-36 BATH TUB FITTING CORRODED OUT OF LIMITS REMOVED BATH TUB FITTING AT STA 1228 BETWEEN L35R-36 IAW SRM 51-1-20D LOCATED AND DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1228 L35R-36 IAW SRM 51-1-20D,
- [SDR UPS06847063](https://openairdocs.org/sdr/UPS06847063.md): Fitting · corroded · May 19, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 C PIT STA 1220 BETWEEN L35R-36 BATH TUB FITTING INSIDE TORQUE BOX HAS EXFOLIATION CORROSION. REMOVED BATH TUB FITTING AT STA 1220 L35R-36 IAW SRM 51-1-20D DRILLED UP AND INSTALLED NEW BATH TUB FITTING AT STA 1220 L35R-36 IAW SRM 51-1-20D, A
- [SDR UPS06846982](https://openairdocs.org/sdr/UPS06846982.md): Skin · gouged · May 16, 2006 · N818UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:C1 PANEL LANDING AT ACCESS PNL 506C HAS DEEP GOUGE NR 3 MAIN TANK. TRIMMED OUT DAMAGED AREA OF LANDING IAW SRM 57-02-01 FIG 036. FABRICATED INSTALLED REPAIR FILLER, EXTERIOR DOUBLER, INTERIOR FILLER AND DOUBLER IAW SRM 57-02-01 FIG 036, 51-01
- [SDR UPS06846939](https://openairdocs.org/sdr/UPS06846939.md): Fitting · cracked · May 16, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1 POSSIBLE CRACK ON STRINGER END FITTING AT STRINGER 59 BETWEEN XW408 AND XRS463 NR 1 ALT. REMOVED AND REPLACED FITTING AT STRINGER 59 BETWEEN XW408 AND XRS463 IAW SRM 51-1-20D AND 51-1-23.
- [SDR UPS06847093](https://openairdocs.org/sdr/UPS06847093.md): Frame · cracked · May 13, 2006 · N818UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C1 D-PIT STA 1340 BETWEEN L30R-31R FRAME CRACKED AND CORRODED. CUT OUT DAMAGED AREA STA 1340 FRAME BETWEEN L30R-L31R IAW 51-1-21D, FABRICATED AND INSTALLED REPAIR SPLICES AND FRAME SEGMENT AT STA 1340 BETWEEN L30R-L31R IAW SRM 53-02-00 FIG 2,
- [SDR UPS06847064](https://openairdocs.org/sdr/UPS06847064.md): Fitting · cracked · May 13, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 CRACK IN FITTING AT LT AFT OVERWING DOOR JAMB, UPPER AFT CORNER STA 824 L14L. REMOVED FITTING AT STA 824 L14L IAW SRM 51-3-0, AND 51-1-20D FABRICATED AND INSTALLED FITTING AT STA 824 L14R IAW DWG 4751643, AND SRM 51-3-2, AND SRM 51-1-20D.
- [SDR UPS06846987](https://openairdocs.org/sdr/UPS06846987.md): Fitting · cracked · May 13, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 3EA FITTINGS IN C-PIT DOOR TORQUE BOX CRACKED AT STA 1180-1200. REMOVED 3EA CRACKED TORQUE BOX FITTINGS IAW SRM 51-1-20D, INSTALLED NEW 3EA FITTINGS AT STA 1180-1200 C-PIT TORQUE BOX IAW SRM 51-1-24, 51-1-20D.
- [SDR UPS06846981](https://openairdocs.org/sdr/UPS06846981.md): Longeron · cracked · May 13, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1 60 HOLE LONGERON 17L HAS PREVIOUS REPAIR, HOWEVER CRACK HAS EXTENDED PAST STOP DRILL. REMOVED DAMAGED L17L AT STA 1776 IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON 17L AT STA 1766 IAW SRM 53-02-02-0, 51-3-02, AND SRM 51-1-20D.
- [SDR UPS06847127](https://openairdocs.org/sdr/UPS06847127.md): Cusp Web · corroded · May 12, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > RT FWD TYPE 1 DOOR LWR DOOR JAMB CUSP IS CORRODED. REMOVED CUSP AT STA 370-470 L21R IAW SRM 53-2-5 FIG 15, MILLED AND INSTALLED REPAIR CUSP AT STA 370 - 470 L21R IAW SRM 53-2-5 FIG 15.
- [SDR UPS06847011](https://openairdocs.org/sdr/UPS06847011.md): Seat Track · corroded · May 12, 2006 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK HEAVY CORROSION AT STA 70 LBL 24. REMOVED DAMAGED SEAT TRACK FROM STA 45-130 LBL 24 IAW SRM 51-03-00, FABRICATED AND INSTALLED SEAT TRACK SPLICE FROM STA 45-130 IAW SRM 53-02-03-0 FIG 014, SRM 51-3-0, AND DWG S-2440463
- [SDR UPS06847125](https://openairdocs.org/sdr/UPS06847125.md): Fitting · cracked · May 11, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > LEFT W/W TRAP FITTING CRACKED ALONG STA 902 FWD SIDE AT TOP VERTICAL BOLT THRU L24L. REMOVED AND REPLACED LEFT WHEEL WELL TRAP FITTING IAW SRM 51-1-20D, SRM 51-3-2, AND DC-8 AMM 51-03-01-0.
- [SDR UPS06847118](https://openairdocs.org/sdr/UPS06847118.md): Fitting · cracked · May 11, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FOUND A/C COMPT RT SIDE L33R END FITTING CRACKED AT FS 8.00. REMOVED AND REPLACED END FITTING ON LONGERON END FITTING L33R IAW SRM 51-1-21, 51-01-27 AND 51-1-8.
- [SDR UPS06847096](https://openairdocs.org/sdr/UPS06847096.md): Cusp Web · cracked · May 11, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 A-PIT LEFT STA 325 LWR CUSP HAS VISIBLE CRACK IN RADIUS. CUT OUT SECTION OF CUSP AT STA 325 - 275 L21L IAW SRM 53-02-05-0. FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, -15 & -9 FRAME SPLICE DRILLED UP LEFT CUSP AND INSTALLED IAW SRM 53-04-
- [SDR UPS06847043](https://openairdocs.org/sdr/UPS06847043.md): Spar Cap · cracked · May 11, 2006 · N818UP · Doug DC873F · Wing Spar
  > INSPECTION TYPE:C1 WING CTR LOWER SPAR CAP CRACKED, LEFT W/W LBL 9-19 AND LBL 37-44. STOP DRILLED CRACKS AT WING LWR CTR SPAR CAP LBL 9-19 AND LBL 37-44. FABRICATED AND INSTALLED REPAIR PARTS AT WING CTR SPAR CAP LBL 9-19 AND LBL 37-44 IAW SRO8570009 REV A C
- [SDR UPS06847126](https://openairdocs.org/sdr/UPS06847126.md): Cusp Web · corroded · May 10, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > FUS CUSP CORRODED AT FS 1310 AND 1340 RT FWD AND AFT SIDES OF T-1 DOOR. REMOVED CUSP AT STA 1310-1380 RT FUSELAGE IAW 51-1-21, AND SRM 51-3-0, MILLED AND INSTALLED CUSP SPLICE REPAIR AT STA 1310-1380 IAW SRM 52-2-0 FIG 15.
- [SDR UPS06846986](https://openairdocs.org/sdr/UPS06846986.md): Fitting · cracked · May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C1 FRAME FITTING CRACKED AT FS 832, RT SIDE 19 INCHES ABOVE FLOOR PLANE. REMOVED FITTING AT STA 832 IAW SRM 51-1-20D, FABRICATED AND INSTALLED FRAME FITTING AT FS 832 IAW SRM 51-1-20D, AND DWG 3779874.
- [SDR UPS06846984](https://openairdocs.org/sdr/UPS06846984.md): Attach Fitting · cracked · May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C1 FRAME ATTACH FITTING CRACKED AT STA 1180 L17R. REMOVED CRACKED FITTING AT FRAME STA 1180 L17R IAW SRM 51-1-20D, DRILLED REPLACEMENT FITTING AND INSTALLED AT STA 1180 L17R IAW SRM 51-1-20D.
- [SDR UPS06846983](https://openairdocs.org/sdr/UPS06846983.md): Fitting · cracked · May 10, 2006 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 FITTING CRACKED AT STA 670 L11R. REMOVED CRACKED FITTING AT STA 670 L11R IAW SRM 51-3-0, FABRICATED AND INSTALLED FITTING AT STA 670 L11R IAW DWG 5750540, SRM 51-3-2 AND SRM 51-1-20D.
- [SDR UPS06846952](https://openairdocs.org/sdr/UPS06846952.md): Fitting · cracked · May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 LONGERON/FRAME TIE FITTING CRACKED AT FS 860 19" ABOVE FLOOR PLANK RT SIDE. REMOVED FRAME TIE FITTING AT FS 860 IAW SRM 51-1-20D. FABRICATED AND INSTALLED FRAME FITTING AT FS 860 IAW DWG 4750422, AND SRM 51-1-20D, AND SRM 51-1-8.
- [SDR UPS06846951](https://openairdocs.org/sdr/UPS06846951.md): Fitting · cracked · May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 LONGERON TO FRAME FITTING CRACKED AT FS 855 19" ABOVE FLOOR PLANK RT SIDE. REMOVED CRACKED FITTING AT FS 855 IAW SRM 51-1-20D. FABRICATED AND INSTALLED FITTING AT FS 855 19" ABOVE FLOOR PLANK IAW DWG 3779498 AND SRM 51-1-20D, AND SRM 51-1-
- [SDR UPS06846936](https://openairdocs.org/sdr/UPS06846936.md): Fitting · cracked · May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 LONGERON/FRAME TIE FITTING CRACKED AT FS 860 (RT SIDE 17" ABOVE FLOOR PANEL). REMOVED, FAB`D AND REPLACED LONGERON FITTING IAW SRM 51-1-21 AND 51-1-20D.
- [SDR UPS06846865](https://openairdocs.org/sdr/UPS06846865.md): Fitting · cracked · May 10, 2006 · N818UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 670 L6L. REMOVED END FITTING AT STA 670 L6L IAW SRM 51-1-20D, DRILLED UP AND INSTALLED END FITTING AT STA 670 L6L IAW SRM 51-03-02, AND SRM 51-1-20D.
- [SDR UPS06846866](https://openairdocs.org/sdr/UPS06846866.md): Door Frame · cracked · May 8, 2006 · N818UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:C1 HFEC AND VISUAL INSP DETECTED A.250 INCH CRACK ON THE D-PIT UPPER FWD DOOR JAMB CORNER. CUT OUT DAMAGED AREA ON C-PIT UPPER FWD DOOR JAMB CORNER IAW SRM 53-02-00 FIG 021, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER AT THE C-PIT UP
- [SDR UPS06846985](https://openairdocs.org/sdr/UPS06846985.md): Skin · dented · Apr 21, 2006 · N818UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 COMPLY WITH MPI 17970 REGARDING PERM REPAIR TO DENT AFT OF LWR FWD PIT DOOR OPENING IAW ATTACHED WAN 1096454 AND MPI SUMMARY REPORT PAGE 1. REPAIRED DENT ON SKIN AFT SIDE OF -A- PIT DOOR CORNER IAW SAA EA 008-5320-01-A0189, DOUGLAS DWG 975
- [SDR UPS06846447](https://openairdocs.org/sdr/UPS06846447.md): Battery Pack · inoperative · Mar 15, 2006 · N818UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS DO NOT WORK. REMOVED AND REPLACED EMERG EXIT LIGHTS BATTERY PACK. OPS CHECK GOOD REF MM CH 33-50-01-2.
- [SDR UPS06846191](https://openairdocs.org/sdr/UPS06846191.md): Battery Pack · inoperative · Feb 15, 2006 · N818UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERG LIGHT BATTERY PACK. OPS CK GOOD.
- [SDR UPS05845353](https://openairdocs.org/sdr/UPS05845353.md): Motor · overheated · Sep 2, 2005 · N818UP · Doug DC873F · Waste Disposal System
  > LAV FLUSH MOTOR OVERHEATED CAUSING SMOKE IN CABIN. REMOVED AND REPLACED LAV TIMER AND FLUSH MOTOR PER MM 20-10-03, 20-16-00-2. OPS CK NORMAL PER MM 38-30-00-1. NO LEAKS NOTED.
- [SDR UPS05844880](https://openairdocs.org/sdr/UPS05844880.md): Control Valve · closed · Jul 13, 2005 · N818UP · Doug DC873F · Cabin Cooling System
  > BTB DUE TO SMOKE IN COCKPIT DURING PUSHBACK. SUSPECT LEFT PACK OPEN DUE TO DMI ON LEFT PACK. LEFT PACK SWITCH WAS IN THE OFF POSITION. FOUND LEFT PACK FLOW CONTROL VLV OPEN CLOSE VLV PER MEL ITEM 7 STEP 1 OPS CK LEFT AND RIGHT PACKS ON GROUND LEFT PACK IS C
- [SDR UPS04843492](https://openairdocs.org/sdr/UPS04843492.md): Window · inoperative · Nov 13, 2004 · N818UP · Doug DC873F · Flight Compartment Windows
  > CAPTAIN SLIDING WINDOW WILL NOT OPEN. LUBED UPPER CATCH ON SLIDING WINDOW. OP CHECKS GOOD. WINDOW OPENS EASILY.
- [SDR UPS04843472](https://openairdocs.org/sdr/UPS04843472.md): Window · stuck · Nov 10, 2004 · N818UP · Doug DC873F · Flight Compartment Windows
  > INSPECTION TYPE:N/A CAPT'S L2 WINDOW WILL NOT OPEN. UPPER WINDOW FRAME LOCK BAR STUCK WOULD NOT RELEASE. CLEANED & LUBRICATED MECHANISM. OPS CHECK NORMAL IAW MM 56-10-03-5.
- [SDR UPS04842655](https://openairdocs.org/sdr/UPS04842655.md): Window · stiff · Jul 7, 2004 · N818UP · Doug DC873F · Flight Compartment Windows
  > INSPECTION TYPE:N/A CAPTAINS CLEARVIEW WINDOW HARD TO OPEN. OPENED AND CLOSED CAPTAIN'S SLIDING WINDOW THROUGH CYCLES. WINDOW OPENS AND CLOSES NORMALLY. NO DEFECTS NOTED. OK FOR CONTINUOUS SERVICE.
- [SDR UPS04842480](https://openairdocs.org/sdr/UPS04842480.md): Longeron · corroded · May 23, 2004 · N818UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C-2, FWD BAG PIT, L28L CORROSION BETWEEN FS 320 & 340. REMOVED CORR FROM L28L SIDE OF VERTICAL LEG AT FS 325, 330 & 335. ORIG THICKNESS VERTICAL LEG.063 IAW DAC DWG 9754913 MAT'L REMOVED.015, AMT REMAINING.048. OUT OF LIMITS. FAB -31 REP
- [SDR UPS04842542](https://openairdocs.org/sdr/UPS04842542.md): Skin · corroded · May 14, 2004 · N818UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C-2, MARKER BEACON MOUNT AREA HAS HEAVY CORROSION (SKIN). BLEND CORROSION FOUND OUT OF LIMITS. REMOVED LT LOWER STRESS PANEL MAT ID 7075-T6, -.071, PO 434977.6 FOR DOUBLER IAW REO GO 9816. FAB REPAIR DOUBLERS IAW REO GO9816. ALODINED & PRI
- [SDR UPS04842541](https://openairdocs.org/sdr/UPS04842541.md): Seat Track · corroded · May 13, 2004 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C-2, MAIN CABIN FS AT 995 SEAT TRACK -E- HAS CORROSION BETWEEN LUGS. REMOVED CORROSON FOUND TO BE OUT OF LIMITS. REMOVED FLOORBOARD 1000 TO 1060. CUT SEAT TRACK FROM STA 830 TO 1100 IAW EO DC8 5320517C DWG DC8 53B 003. MAT ID SEAT TRACK 277
- [SDR UPS04842449](https://openairdocs.org/sdr/UPS04842449.md): Seat Track · corroded · May 13, 2004 · N818UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C-2 MAIN CABIN FS AT 995 SEAT TRACK "E" HAS CORROSION BETWEEN LUGS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT SEAT TRACK EO DC8-5320-5167C DWG DC8-53B-003. LOCATED, DRILL AND DEBURRED SEAT TRACK PLUS 2 SPLICE FITTING SEAT TRACK. ALODINE
- [SDR UPS04842444](https://openairdocs.org/sdr/UPS04842444.md): Skin · dented · May 13, 2004 · N818UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C-2 JUST BELOW LOWER CUTOUT OF MAIN CARGO DOOR, FUSELAGE SKIN HAS TWO DENTS. REMOVED FASTENER IN SKIN FS 200-220, RMVD DAMAGE SECTION OF SKIN AT FS 210 MATERIAL ID FOR DOUBLER REPAIR EXTERNAL DOUBLER 7075-T6.080 PO 43557 21 FILLER 2024-T-3,071
- [SDR UPS04842479](https://openairdocs.org/sdr/UPS04842479.md): Longeron · corroded · May 12, 2004 · N818UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE: C-2, CORROSION ON FUSELAGE SKIN AND AROUND FASTENER HOLES FS 300-320 L29L. REMOVED CORROSION AND FOUND OUT OF LIMITS ORIG THICKNESS.063 THINNEST SPOT.034 720 IAW DC8 SRM 51-1-8 AND 53-2-0. FAB, ALODINED, PRIMED AND INSTALLED 31 REPAIR ANGL
- [SDR UPS04842450](https://openairdocs.org/sdr/UPS04842450.md): Frame · corroded · May 12, 2004 · N818UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C-2 CORROSION ON FRAME AT FS 180 L35L-35R. REMOVED CORROSION, FOUND BLENDOUT BEYOND ALLOWABLE LIMITS IAW SRM 53-2-0 FIG 1F. FAB -9 DOUBLER, -11 FILLER IAW EO 11728-B AND UPS DWG 53A-011A. INSTALLED PARTS IAW EO AND DWG. ALODINED AND PRIMED IAW

Next page: https://openairdocs.org/deregistered/N818UP-2010-12-27/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 = 'N818UP' AND deregistration_id = 'N818UP-2010-12-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N818UP-2010-12-27/reports

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