# Service difficulty reports: N840UP, cancelled Mar 24, 2011

A list on [N840UP, cancelled Mar 24, 2011](https://openairdocs.org/deregistered/N840UP-2011-03-24.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 · 317 reports

- [SDR UPS08853073](https://openairdocs.org/sdr/UPS08853073.md): Bulb · broken · Aug 7, 2008 · N840UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:ASE EMERGENCY LIGHTS VERY DIM OVER ENTRY DOOR. RELAMPED EMERGENCY LIGHTS. FOUND BAD BULB. BASE PARTIALLY SEPARATED FROM LAMP. WORK DONE IAW MM 33-50-02-2. OPERATION CHECK GOOD AT THIS TIME.
- [SDR UPS08851779](https://openairdocs.org/sdr/UPS08851779.md): Battery Pack · discharged · Mar 8, 2008 · N840UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LT BATTERY PACK PER MM 33-50-01-2. OPS CHECK GOOD.
- [SDR UPS08851810](https://openairdocs.org/sdr/UPS08851810.md): Battery Pack · discharged · Mar 5, 2008 · N840UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS DO NOT TEST. REPLACED EMERGENCY BATTERY PACK AND RELAY ASSY. OPS CHECK GOOD, REF MM 33-50-01.
- [SDR UPS07851335](https://openairdocs.org/sdr/UPS07851335.md): Oil System · low pressure · Dec 21, 2007 · N840UP · Doug DC873F · Engine Oil Pressure
  > NR 4 ENGINE LOST PRESSURE, SHUT DOWN WITH 20 PSI N1 16 PERCENT, N2 9.4 PERCENT 5 QUARTS INDICATED 6000 FT/200 KTS. REMOVED AND REPLACED LINE SUPPLY OIL TO OIL PRESSURE TRANSMITTER IAW M/M 20-12-00-2. LEAK AND OPS CHECK GOOD IAW M/M 71-00-00.
- [SDR UPS07851319](https://openairdocs.org/sdr/UPS07851319.md): Line · leaking · Dec 21, 2007 · N840UP · Doug DC873F · Turbine Engine Oil System
  > NR 4 ENG LOW OIL PRESSURE AND QTY ON DESCENT INTO SDF. REMOVED AND REPLACED LINE SUPPLY OIL TO OIL PRESSURE TRANSMITTER IAW MM 20-12-00-2. LEAK AND OPS CHECK GOOD IAW MM 71-00-00.
- [SDR UPS07851227](https://openairdocs.org/sdr/UPS07851227.md): Battery Pack · inoperative · Nov 29, 2007 · N840UP · Doug DC873F · Emergency Lighting
  > AT CRUISE, THE DOME LIGHT AND PEANUT LIGHTS CAME ON BY THEMSELVES NO SWITCHES WERE THROWN, NO ABNORMAL INDICATIONS OF F/E PANEL WHEN WENT TO DC TIE WITH THE FREQ SELECTOR, THE LIGHTS WENT OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-
- [SDR UPS07849925](https://openairdocs.org/sdr/UPS07849925.md): Longeron · cracked · May 31, 2007 · N840UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1 L14L STA 1756 UPPER VERT FLANGE HAS A.25 INCH CRACK FROM ATTACH FASTENER HOLE. REMOVED DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON, AND SPLICE FITTING IAW SRM 51-1-21, 53-02-02 FIG 10, 51-1-8, 51-1-20D.
- [SDR UPS07849951](https://openairdocs.org/sdr/UPS07849951.md): Pressure Panel · corroded · May 30, 2007 · N840UP · Doug DC873F · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C1 RIGHT NLG TUNNEL INTERGRANULAR CORROSION AND GUSSET MISSING ON UPPER PRESSURE DECK (CEILING) STA -32 RBL 58. REMOVED FINGER DOUBLER AND CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW SRO 8530026, SRM 51-1-21, 51-20D AND APPROVED
- [SDR UPS07849881](https://openairdocs.org/sdr/UPS07849881.md): Floorbeam · corroded · May 26, 2007 · N840UP · Doug DC873F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C1 CORROSION ON FLOOR SUPPORT FITTING ON AFT VERTICAL BEAM, FS 1760 BL 0. REMOVED FLOOR SUPPORT FITTING AT STA 1760 BL 0 IAW SRM 51-03-00-0. FABRICATED AND INSTALLED FLOOR SUPPORT FITTING AT STA 1760 BL 0 IAW DWG 5773846, AND SRM 51-1-20D.
- [SDR UPS07849883](https://openairdocs.org/sdr/UPS07849883.md): Fitting · cracked · May 25, 2007 · N840UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 FITTING CRACKED AT STA 834 L18L. REMOVED END FITTING AT STA 834 L18L IAW SRM 51-01-20D. FABRICATED AND INSTALLED END FITTING AT STA 834 L18L IAW DWG 3779874, AND SRM 51-1-20D.
- [SDR UPS07849882](https://openairdocs.org/sdr/UPS07849882.md): Fitting · cracked · May 25, 2007 · N840UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 FITTING CRACKED AT STA 857 L19L AFT. REMOVED FITTING AT STA 857 L19L IAW SRM 51-01-20D. FABRICATED AND INSTALLED END FITTING AT STA 857 L19L IAW DWG 4750422, AND SRM 51-1-20D.
- [SDR UPS07849981](https://openairdocs.org/sdr/UPS07849981.md): Skin · corroded · May 22, 2007 · N840UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 FUSELAGE SKIN CORRODED AT FS 60 BETWEEN L34R AND L35R. REMOVED AND REPLACED FUSELAGE SKIN FROM STA - 21.92 - STA 70 L31L TO L31R IAW UPS EO DC8-5330-8942-D.
- [SDR UPS07849875](https://openairdocs.org/sdr/UPS07849875.md): Skin · cracked · May 22, 2007 · N840UP · Doug DC873F · Landing Gear Doors
  > INSPECTION TYPE:C1 LEFT NLG DOOR SKIN IS CRACKED ON OUTBOARD SIDE. CUT OUT DAMAGED SKIN ON LT NLG DOOR IAW SRM 52-02-03. FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER ON LEFT NLG DOOR IAW SRM 52-02-0 FIG 2, AND 51-1-21.
- [SDR UPS06848705](https://openairdocs.org/sdr/UPS06848705.md): Battery Pack · inoperative · Nov 17, 2006 · N840UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CHECKED OK. P/N ON 5708458-503, S/N ON 10389.
- [SDR UPS06847979](https://openairdocs.org/sdr/UPS06847979.md): Wire · shorted · Sep 12, 2006 · N840UP · Doug DC873F · Ice/Rain Protection System Wiring
  > INSPECTION TYPE: PFLT, CREW PREFLT - SMOKE IN COCKPIT. F/O'S SLIDING WINDOW ANTI-FOG WIRES SHORTED TO GROUND AT WINDOW FLEX CONDUIT AND C/B FAILED IN THE POWER CLOSED POS. WIRES & C/B REPLACED, SEE NRC 271362 - 271369 FOR DETAILS OF REPAIRS & CKS. ALL CHECKS G
- [SDR UPS06847150](https://openairdocs.org/sdr/UPS06847150.md): Skin · damaged · Jun 16, 2006 · N840UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A EO DC8-5330-24525 - A FUSELAGE SKIN DAMAGE REPAIRS AT STA 1420 LONGERON 29L AND STA 1460 LONGERON 29L. COMPLIED WITH EO DC8-5330-24525-A APPENDIX A AND APPENDIX B REPEAT INSPECTIONS DUE AT C-CHECK PERMANENT REPAIR DUE WITH IN 6000 FLT CYCL
- [SDR UPS06847097](https://openairdocs.org/sdr/UPS06847097.md): Skin · damaged · Jun 9, 2006 · N840UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A CREASE LEFT FUSELAGE AT STA 1340 THRU 1400. A/C FERRIED TO HEAVY MX VENDOR FOR REPAIR. RMVD DMG. PER SRM 53-02-01-0, FIG.7;VERIFIED DMG RMVD; COMPLETED REPAIR BY INSTALLING DOUBLER PER SRM 53-02-01-0,FIG 7; PRIMED & PAINTED REPAIR DOUBLER
- [SDR UPS06846530](https://openairdocs.org/sdr/UPS06846530.md): Battery Pack · inoperative · Mar 28, 2006 · N840UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY INOP. REPLACED BATTERY PACK.
- [SDR UPS05845687](https://openairdocs.org/sdr/UPS05845687.md): Unknown · corroded · Oct 27, 2005 · N840UP · Doug DC873F · Fuselage Structure (General)
  > FOUND CORROSION IN LT W/W. AIRCRAFT BEING FERRIED NR 9157 TO SAA FOR REPAIR. CUT OUT CORROSION FROM EXTERNAL SKIN, AND FAB'D AND INSTALLED REPAIR PARTS FOR SKIN REPAIR. ALL WORK PERFORMED IAW SAA SK 840-727258 & UPS EO DC8-53-20523.
- [SDR UPS05845296](https://openairdocs.org/sdr/UPS05845296.md): Window · jammed · Aug 31, 2005 · N840UP · Doug DC873F · Flight Compartment Windows
  > F/O'S SLIDING WINDOW JAMMED.
- [SDR UPS05845260](https://openairdocs.org/sdr/UPS05845260.md): Mechanism · stuck · Aug 23, 2005 · N840UP · Doug DC873F · Flight Compartment Windows
  > F/O'S EMERG (CLEAR VIEW, DV WINDOW) WILL NOT OPEN. CLEANED AND LUBED F/O'S WINDOW SLIDE MECH. OPS CK NORMAL.
- [SDR UPS05845201](https://openairdocs.org/sdr/UPS05845201.md): Battery Pack · inoperative · Jul 29, 2005 · N840UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:PNT EMERGENCY EXIT LIGHTS FAILED TEST REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL
- [SDR UPS05844760](https://openairdocs.org/sdr/UPS05844760.md): Battery Pack · discharged · Jun 30, 2005 · N840UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY INOP. REMOVED & REPLACED EMERGENCY LIGHTING BATTERY & RELAY ASSY & OPS CK GOOD IAW MM 33-50-01-2.
- [SDR UPS05844758](https://openairdocs.org/sdr/UPS05844758.md): Skin · gouged · Jun 3, 2005 · N840UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C-3. RT FS 70 L31R AND L32R, DEEP GOUGES ON EXTERIOR SKIN. REMOVED DAMAGED SKIN SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER IAW EO DC8-53-20473 AND SAA SK840-808375.
- [SDR UPS05844748](https://openairdocs.org/sdr/UPS05844748.md): Longeron · corroded · Jun 2, 2005 · N840UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > AFTER REMOVAL OF L33R END FITTING STA 8 FOUND L33R CORRODED OUT OF LIMITS STA 8. REF N/R 807385. REMOVED AND REPLACED LONGERON 33R STA 8 TO 70 IAW SRM 51-1-21, 1-1-21D AND 51-3-2.
- [SDR UPS05844700](https://openairdocs.org/sdr/UPS05844700.md): Rib · cracked · Jun 1, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > LT WING CENTER L/E AT XFS 335 RIB CRACKED ON L/E LOWER SURFACE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844743](https://openairdocs.org/sdr/UPS05844743.md): Frame · corroded · May 29, 2005 · N840UP · Doug DC873F · Fuselage Main, Frame
  > DEEP CORROSION AROUND SHEAR TIE FASTENER HEADS AFT SIDE OF FRAME, STA 1300 LONGERON 36. REMOVED CORROSION AND FOUND FRAME OUT OF LIMITS. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIG 2.
- [SDR UPS05844757](https://openairdocs.org/sdr/UPS05844757.md): Fitting · cracked · May 28, 2005 · N840UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-3. WING BOX BOOT FITTING CRACKED APPROX 5 IN LONG STA 759 BETWEEN L17L-L18L. CUT OUT CRACKS, FABRICATED AND INSTALLED REPAIR PARTS IAW SAASK 840-808203 AND EO DC853-20469.
- [SDR UPS05844705](https://openairdocs.org/sdr/UPS05844705.md): Longeron · cracked · May 27, 2005 · N840UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > CRACK APPROX 3 INCHES LONG ON LONGERON 35R AT FS 1270. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DC-8 SRM 51-1-20D AND DWG'S 3758593 AND 575 0322.
- [SDR UPS05844703](https://openairdocs.org/sdr/UPS05844703.md): Fitting · cracked · May 27, 2005 · N840UP · Doug DC873F · Fuselage Main, Structure
  > CRACKED FITTING ON TORQUE BOX AT CARGO DOOR AT FS 1160 BETWEEN L31 AND L32 R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.
- [SDR UPS05844698](https://openairdocs.org/sdr/UPS05844698.md): Splice · cracked · May 27, 2005 · N840UP · Doug DC873F · Fuselage Miscellaneous Structure
  > LONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L36. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.
- [SDR UPS05844759](https://openairdocs.org/sdr/UPS05844759.md): Panel · corroded · May 25, 2005 · N840UP · Doug DC873F · Fuselage Main, Bulkhead
  > HEAVY CORROSION ON LT WW CEILING STA 860 LBL 61. CUT OUT DAMAGE AND INSTALLED REPAIR PARTS IAW EO DC8-5310-22401-A AND SAA SK 840-807868.
- [SDR UPS05844755](https://openairdocs.org/sdr/UPS05844755.md): Skin · cracked · May 25, 2005 · N840UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C-3. EXTERNAL FUSELAGE L1 DOOR CUTOUT UPPER AFT CORNER, SKIN VISUALLY CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW EO DC8 5330-22342-A AND SAA SK 840-807798.
- [SDR UPS05844701](https://openairdocs.org/sdr/UPS05844701.md): Fuel Tank · damaged · May 25, 2005 · N840UP · Doug DC873F · Fuel Storage
  > RT AUX TANK UPPER SURFACE FASTENER HOLE ELONGATED AT XW 208. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-1 FIG 37, 51-1-26, 51-1-20D, AND 51-1-21.
- [SDR UPS05844697](https://openairdocs.org/sdr/UPS05844697.md): Rib · chafed · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > RT CENTER WING L/E RIB CHAFED THROUGH AROUND PNEUMATIC DUCT SUPPORT ROD CONNECTION AT XFS 513. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57 -2-0 FIG 2 AND 51-1-20D.
- [SDR UPS05844696](https://openairdocs.org/sdr/UPS05844696.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > RT CENTER WING L/E PNEUMATIC DUCT ATTACH POINT UPPER RIB CRACKED 3 INCH LONG AT XFS 304. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-15, AND 51-1-20D.
- [SDR UPS05844575](https://openairdocs.org/sdr/UPS05844575.md): Skin · damaged · May 25, 2005 · N840UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:C3 RIGHT WING CENTER L/E LWR SURFACE FASTENER HOLES ELONGATED AT XFS 527. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0, 51-1-11, AND 51-1-21.
- [SDR UPS05844574](https://openairdocs.org/sdr/UPS05844574.md): Splice · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C3 RIGHT WING CENTER L/E INTERNAL DOUBLER SPLICE CRACKED.5 INCH LONG AT XFS 42 9. REMOVED 2 EA CRACKED SPLICES, FABRICATED, AND INSTALLED 2 EA REPLACEMENT SPLICES IAW DC-8 SRM 51-1-20D, DWG 5769589-15 & -17.
- [SDR UPS05844573](https://openairdocs.org/sdr/UPS05844573.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB CRACKED AT XFS 454. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844572](https://openairdocs.org/sdr/UPS05844572.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE LWR RIB CRACKED AT XFS 623.500. CRACK TERMINATES AT FASTENER HOLE, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844570](https://openairdocs.org/sdr/UPS05844570.md): Doubler · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C3, RIGHT CTR WING L/E LWR INNER DOUBLER AROUND DRAIN HOLE CRACKED.5 INCH LONG AT XFS 335. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INNER DOUBLER IAW DC8 SRM 57-3-3 FIG 5 AND 51-1-21.
- [SDR UPS05844569](https://openairdocs.org/sdr/UPS05844569.md): Doubler · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C3, CENTER WING L/E UPPER INNER DOUBLER CRACKED.5 INCH LONG AT XFS 422. REMOVED INNER DOUBLER, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DC-8 SRM 51-1-21 AND DWG 5769891.
- [SDR UPS05844566](https://openairdocs.org/sdr/UPS05844566.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RIGHT CENTER WING L/E LWR RIB CRACKED AT XFS 304. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER & ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844565](https://openairdocs.org/sdr/UPS05844565.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3, RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 495. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844564](https://openairdocs.org/sdr/UPS05844564.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 416. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844560](https://openairdocs.org/sdr/UPS05844560.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RT CENTER WING L/E UPPER RIB CRACKED AT XFS 297. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844558](https://openairdocs.org/sdr/UPS05844558.md): Rib · cracked · May 25, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 291. CRACK TERMINATES AT FASTENER HOLE. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.
- [SDR UPS05844754](https://openairdocs.org/sdr/UPS05844754.md): Floor Support · corroded · May 24, 2005 · N840UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-3. MAIN CABIN SUB FLOOR STA 960 RBL 60 UNDER FLOORBEAM AREA CORRODED. CUT OUT DAMAGE ON SUBFLOOR STA 960 RBL60. REMOVED CORROSION ON FLOORBEAM. FABRICATED AND INSTALLED FILLER, 2 FINGER DOUBLERS, 2 DOUBLERS AND 1 SPLICE DOUBLER IAW EO DC
- [SDR UPS05844563](https://openairdocs.org/sdr/UPS05844563.md): Rib · cracked · May 24, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3, RIGHT OUTBOARD L/E LWR RIB CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-21.
- [SDR UPS05844557](https://openairdocs.org/sdr/UPS05844557.md): Rib · cracked · May 24, 2005 · N840UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 603.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-20D.

Next page: https://openairdocs.org/deregistered/N840UP-2011-03-24/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 = 'N840UP' AND deregistration_id = 'N840UP-2011-03-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N840UP-2011-03-24/reports

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