# Service difficulty reports: N819UP, cancelled Mar 24, 2011

A list on [N819UP, cancelled Mar 24, 2011](https://openairdocs.org/deregistered/N819UP-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 5 · 205 reports

- [SDR UPS08854213](https://openairdocs.org/sdr/UPS08854213.md): Rod · broken · Dec 17, 2008 · N819UP · Doug DC873F · Brake
  > F/O MADE UNEVENTFUL LANDING WITH NORMAL BRAKING. EXITED RUNWAY & HAD NO BRAKES AT 55 KTS. NOSE WHEEL STEERING WORKED, BUT HAD TO USE EMERGENCY AIR BRAKES. R&R NOSE STEERING CABLE GUIDE, REF MM 29-10-0.
- [SDR UPS08853383](https://openairdocs.org/sdr/UPS08853383.md): Doubler · damaged · Sep 20, 2008 · N819UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A REPAIR DOUBLER AT FUSELAGE FRAME 50 AND STRINGER 24L REQUIRED REPLACEM MENT D385232. REMOVED DOUBLER, ACCOMPLISHED STEPS APPENDIX-A (1) THRU (6). PER PRELIMINARY EO DC8-5330-30623-A. DAMAGE REMOVAL VERIFIED OK TO INSTALL FABRICATED DOUBLE
- [SDR UPS08853382](https://openairdocs.org/sdr/UPS08853382.md): Doubler · damaged · Sep 20, 2008 · N819UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A DOUBLER AT FUSELAGE STATION 902, LT SIDE OF FUSELAGE REQUIRES REPLACEMENT. REMOVED EXISTING DOUBLER AND SHIM PER SRM 51-1-00, C/W EO DC8-5330-3 9 UP TO STEP 6. INSTALLED 28 1/4" HI-LOKS IN REPAIR DOUBLER PER PRELIMINARY EO DC8 5330-30619-
- [SDR UPS07851177](https://openairdocs.org/sdr/UPS07851177.md): Slide · dislodged · Nov 15, 2007 · N819UP · Doug DC873F · Escape Slide
  > INSPECTION TYPE:N/A THE MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE NEEDS TO BE ADJUSTED IN THE HOLDING CASE AS IT APPEARS TO BE SLIDING OUT AND IT IS DIFFICULT TO READ SLIDE PRESSURE. REPOSITIONED MAIN ENTRY DOOR EVACUATION SLIDE IN CONTAINER AND RE-INSTALLED W/R
- [SDR UPS07850551](https://openairdocs.org/sdr/UPS07850551.md): Light · inoperative · Aug 29, 2007 · N819UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2 AND CHECKS GOOD PER SAME.
- [SDR UPS07850350](https://openairdocs.org/sdr/UPS07850350.md): Battery · discharged · Jul 24, 2007 · N819UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A ON PREFLIGHT AIRCRAFT FAILED EMERGENCY EXIT LIGHTS CHECK. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY & RELAY PACK IAW DC8 MM 33-50-1-2. OPS CHECKS NORMAL.
- [SDR UPS07849803](https://openairdocs.org/sdr/UPS07849803.md): Skin · cracked · Apr 20, 2007 · N819UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE C-4 (D-PIT) UPPER FWD DOOR JAMB CORNER. CRACK RUNS FROM FASTENER HOLE TO EDGE OF CUTOUT. REMOVED EXISTING DOUBLER. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER. RE
- [SDR UPS07849763](https://openairdocs.org/sdr/UPS07849763.md): Bracket · cracked · Apr 17, 2007 · N819UP · Doug DC873F · Wing Spar
  > INSPECTION TYPE:C1 LOWER FRONT SPAR CAP BRACKET IS CRACKED IN 2 PLACES BETWEEN XRS 463-428 NR 1 ALT. REMOVED, FABRICATED AND INSTALLED BRACKET IN NR 1 ALT TANK IAW SRM 51-01-20D, 51-03-02, AND DWG 76335150001.
- [SDR UPS07849683](https://openairdocs.org/sdr/UPS07849683.md): Finger Doubler · corroded · Apr 15, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 CORROSION AND POSSIBLE STRESS CRACK ON FINGER DOUBLER COCKPIT SUB FLOOR FS -25 TO 8 RBL 22. REMOVED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -25 TO 8 RBL 22 IAW DWG5612298, AND S
- [SDR UPS07849681](https://openairdocs.org/sdr/UPS07849681.md): Finger Doubler · corroded · Apr 15, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 SEVERAL AREAS OF CORROSION AND POSSIBLE CRACK IN FINGER DOUBLER COCKPIT SUBFLOOR FS -60, RBL 22. REMOVED CORRODED FINGER DOUBLER AT STA -60 RBL 22 IAW SRM 51-1-21. FABRICATED AND INSTALLED FINGER DOUBLER AT STA -60 RBL22 IAW DWG 5612298, A
- [SDR UPS07849761](https://openairdocs.org/sdr/UPS07849761.md): Fitting · cracked · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 855 L10R. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D, 51-1-21, AND 51-3-0.
- [SDR UPS07849729](https://openairdocs.org/sdr/UPS07849729.md): Attach Fitting · cracked · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 756 L13L. REMOVED END FITTING AT STA 756 L13L IAW SRM 51-1-20D. LOCATED, DRILLED UP AND INSTALLED REPLACEMENT FITTING AT STA 756 L13L IAW SRM 51-3-2, AND SRM 51-1-20D.
- [SDR UPS07849728](https://openairdocs.org/sdr/UPS07849728.md): Attach Fitting · cracked · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 697 L18L. REMOVED CRACKED END FITTING AT STA 697 L18L IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 697 L18L IAW SRM 51-3-1, AND SRM 51-1-20D.
- [SDR UPS07849727](https://openairdocs.org/sdr/UPS07849727.md): Attach Fitting · cracked · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 901 L19R. REMOVED CRACKED FITTING AT STA 901 L19R IAW SRM 51-1-20D. LOCATED DRILLED UP, AND INSTALLED REPLACEMENT FITTING AT STA 901 L19R IAW SRM 51-3-2, AND SRM 51-1-20D.
- [SDR UPS07849713](https://openairdocs.org/sdr/UPS07849713.md): Fitting · corroded · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 BOOT FITTING CORRODED AT STA 759 L22R. REMOVED CORRODED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-20D. PROCURED, LOCATED, DRILLED UP, AND INSTALLED BOOT FITTING AT STA 759 L22R IAW SRM 51-1-21, AND SRM 51-1-20D.
- [SDR UPS07849685](https://openairdocs.org/sdr/UPS07849685.md): Fitting · cracked · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 T-BOLT BACKUP FITTING CRACKED IN C-PIT TORQUE BOX, STA 1177 L33R UPPER AND LWR FLANGES. REMOVED DAMAGED FITTING AT STA 1177 L33R IAW SRM 51-1-20D. LOCATED DRILLED UP AND INSTALLED FITTING AT STA 1177 L33R IAW SRM 51-3-2 AND SRM 51-01-20D.
- [SDR UPS07849671](https://openairdocs.org/sdr/UPS07849671.md): Fitting · cracked · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 822 L22L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
- [SDR UPS07849670](https://openairdocs.org/sdr/UPS07849670.md): Fitting · gouged · Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 LOWER FWD T-BOLT FITTING GOUGED AT C-PIT DOOR JAM. REMOVED AND REPLACED LWR FWD T-BOLT FITTING IAW SRM 51-3-2.
- [SDR UPS07849765](https://openairdocs.org/sdr/UPS07849765.md): Door Frame · misrepaired · Apr 12, 2007 · N819UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:C1 L1 DOOR CUTOUT HAS RIVET WITH NO ED AT LWR HINGE CUTOUT. REMOVED, FABRICATED, AND INSTALLED L1 DOOR JAMB FRAME IAW SRM 51-1-21, 0D, 51-03-02,51-1-8,51-01-14, AND 51-3-0.
- [SDR UPS07849684](https://openairdocs.org/sdr/UPS07849684.md): Channel · cracked · Apr 12, 2007 · N819UP · Doug DC873F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C1 T-CHANNEL CRACKED UPPER SURFACE AT XRS 204 BETWEEN STRINGERS 60 AND 59. STOPPED DRILLED CRACK AT XRS 204 BETWEEN STRINGERS 59 & 60 IN NR 4 MAIN TANK IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0, AND SR
- [SDR UPS07849826](https://openairdocs.org/sdr/UPS07849826.md): Skin · cracked · Apr 11, 2007 · N819UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:C1 LEFT WING UPPER REAR SPAR SKIN CRACKED 5 INCHES AT STA XCW 69. REPAIRED LEFT WING UPPER AFT SPAR AT STA XCW 69.5 IAW SAA EA 008- 5710-01-A0835, UPS EO DC8-5730-26787-A, AND FAA FORM 8100-9.
- [SDR UPS07849791](https://openairdocs.org/sdr/UPS07849791.md): Spar Cap · cracked · Apr 11, 2007 · N819UP · Doug DC873F · Wing Spar
  > INSPECTION TYPE:C1 CRACK ON LWR CENTER SPAR CAP FLANGE NEAR XRS 172 NR 2 MAIN TANK. REPAIRED WING CENTER LWR CAP AND WEB AT STA XRS 168 NR 2 MAIN TANK IAW SAA EA 008-5710-01-A0808, UPS EO DC8-5710-26734-A, SRO8570015, AND FAA FORM 8100-9.
- [SDR UPS07849790](https://openairdocs.org/sdr/UPS07849790.md): Angle · cracked · Apr 11, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 CENTER SECTION EXTERIOR L-ANGLE CRACKED THRU STOP DRILLED HOLE AT STA 855 LBL 65. REMOVED CRACKED L-ANGLE AT STA 855 LBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR FILLER, AND ANGLE DOUBLER AT STA 855 LBL 65 IAW SRM 53-02-00 F
- [SDR UPS07849745](https://openairdocs.org/sdr/UPS07849745.md): Skin · corroded · Apr 10, 2007 · N819UP · Doug DC873F · Vertical Stabilizer, Plate/Skin
  > INSPECTION TYPE:C1 EVIDENCE OF CORROSION UNDER VERT STAB SKIN, RIGHT SIDE LARGE AREA OF PILLOWED SKIN WITH SEVERAL FAILED RIVETS. EXTERIOR ZR252-296 ALONG REAR SPAR. REMOVED AND REPLACED RIGHT VERT STAB SKIN IAW SRM 51-1-21, 51-1-20D, AND 51-3-0.
- [SDR UPS07849586](https://openairdocs.org/sdr/UPS07849586.md): Release Mech · contaminated · Apr 3, 2007 · N819UP · Doug DC873F · Landing Gear Doors
  > INSPECTION TYPE:N/A DIVERSION - LEFT NOSE GEAR DOOR OPEN IN FLIGHT. FOUND LEFT NOSE GEAR DOOR RELEASE TRIGGER JAMMED WITH DEBRIS. CLEANED TRIGGER IAW MM 32-20-00-01. GEAR DOOR LATCHES NORMALLY, A/C OK FOR SERVICE.
- [SDR UPS07849680](https://openairdocs.org/sdr/UPS07849680.md): Attach Fitting · cracked · Jan 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 787 L13R. REMOVED FITTING AT STA 787 L13R IAW SRM 51-1-20D. FABRICATED AND INSTALLED LONGERON END FITTING AT STA 787 L13R IAW SRM 51-01-21-0, NAD SRM 51-1-20D.
- [SDR UPS06848712](https://openairdocs.org/sdr/UPS06848712.md): Battery Pack · discharged · Nov 15, 2006 · N819UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHT VERY DIM. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND UNIT IAW MM 33-50-01-2-4. OPS CHECK GOOD.
- [SDR UPS06848345](https://openairdocs.org/sdr/UPS06848345.md): Window · sticking · Oct 20, 2006 · N819UP · Doug DC873F · Flight Compartment Windows
  > CAPTAIN SIDE WINDOW HARD TO SLIDE. CLEARED DEBRIS FROM WINDOW TRACK. OPERATES AS REQUIRED, REF DC8 MM 56-10-00-0.
- [SDR UPS06847986](https://openairdocs.org/sdr/UPS06847986.md): Line · leaking · Sep 13, 2006 · N819UP · Doug DC873F · Hydraulic System, Main
  > LOST HYD FLUID - DROPPED TO AUX - FOLLOWED BY MAIN SYSTEM PRESS FLUCTU ATIONS + - 1500 - 2000 PSI. DIVERT TO RICKENBACKER AFB (THIS INFO DIRE CTLY OFF LOGPAGE AS NOTED BY FLIGHT CREW). FOUND INBOARD HYD FLEX HOSE FROM NOSE GEAR RETRACT CYLINDER LEAKING. R/R H
- [SDR UPS06847948](https://openairdocs.org/sdr/UPS06847948.md): Window · obstructed · Sep 6, 2006 · N819UP · Doug DC873F · Flight Compartment Windows
  > CAPTAIN'S EMERGENCY WINDOW WILL NOT FULLY OPEN. REMOVED TRIM ON L3 WINDOW AND DEFERRED PER GMM 3-6-10. WINDOW OPERATES NORMALLY. OK TO CONTINUE D332951.
- [SDR UPS05845844](https://openairdocs.org/sdr/UPS05845844.md): Light · malfunctioned · Nov 30, 2005 · N819UP · Doug DC873F · Emergency Lighting
  > EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT, BREAKER POPPED, BREAKER RESET LIGHTS OPERATING NORMAL. OPS CK NORMAL ON GROUND PER MM 33-50-00, OK TO CONTINUE SERVICE.
- [SDR UPS05844301](https://openairdocs.org/sdr/UPS05844301.md): Spar · cracked · Apr 11, 2005 · N819UP · Doug DC873F · Wing Spar
  > INSPECTION TYPE: C2, FOUND POSSIBLE CRACK JUST I/B OF XCW 46 ON LOWER FRONT SPAR CAP VERTICAL ANGLE INSIDE RT CTR FUEL TANK. NDT VERIFIED CRACK APPROX 3 INCH LONG PER NDTSPM 06=10-01.001. CRACK RUNS FROM FASTENER HOLE TO FASTENER HOLE. REPAIRED CRACK IAW DC
- [SDR UPS05844289](https://openairdocs.org/sdr/UPS05844289.md): Skin · cracked · Apr 10, 2005 · N819UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE:C2 C-PIT DOOR UPPER AFT CORNER HAS CRACK IN FIRST FASTENER HOLE ABOVE FITTING ATTACH LIP UNDER INTERIOR SKIN. REPAIRED C-PIT DOOR IAW DC-8 SRM 52-2-0 FIG 2.
- [SDR UPS05844261](https://openairdocs.org/sdr/UPS05844261.md): Fitting · cracked · Mar 30, 2005 · N819UP · Doug DC873F · Wing, Attach Fittings
  > INSPECTION TYPE: C2, STRINGER END FITTING FWD INSIDE ACCESS PANEL 505E NR 3 MAIN CRACKED AT STRINGER 51. REMOVED AND REPLACED STRINGER 51 END FITTING IAW DC-8 SRM 51-1-20D.
- [SDR UPS05844267](https://openairdocs.org/sdr/UPS05844267.md): Stringer · cracked · Mar 25, 2005 · N819UP · Doug DC873F · Wing, Longeron/Stringer
  > C2 FOUND STRINGER CRACKED INSIDE FUEL PANEL 506B NR 2 MAIN STRINGER 71. REMOVED CRACKED SECTION OF STRINGER; FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER IAW DC-8 SRM 57-2-2 FIG 3D AND E AND 51-1-20D.
- [SDR UPS05844299](https://openairdocs.org/sdr/UPS05844299.md): Support Fitting · cracked · Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C2, 62 COMPARTMENT FITTING FOR "POGO STICK" CRACKED AT FWD RT ATTACH BOLT STA 1875. REMOVED AND REPLACED FITTING FOR "POGO STICK" IAW DC-8 SRM 51-1-21, 51 -3-0, AND 51-3-2.
- [SDR UPS05844268](https://openairdocs.org/sdr/UPS05844268.md): Fitting · cracked · Mar 24, 2005 · N819UP · Doug DC873F · Cargo/Baggage Doors
  > C2 CRACKED CORNER FITTING IN C-PIT DOOR UPPER AFT CORNER. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-21A, AND 51-1- 20D.
- [SDR UPS05844256](https://openairdocs.org/sdr/UPS05844256.md): Fitting · corroded · Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C2, AFT CARGO DOOR -C- LOWER DOOR JAMB CUTOUT AFT REAR LOWER CORNER CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-1-0, 51-3-2, 51-1-20D, 51-1- 21, & 51-3-0.
- [SDR UPS05844246](https://openairdocs.org/sdr/UPS05844246.md): Longeron · cracked · Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C2, 60 COMPT, 6 INCHES CRACK IN L-17L STA 1770. REMOVED LONGERON 17L IAW DC-8 SRM 51-1-21. FABRICATED LONGERON IAW DC- 8 SRM 53-5-3 AND SRM 51-3-2. INSTALLED REPLACEMENT LONGERON IAW DC-8 SRM 51-1-20D.
- [SDR UPS05844245](https://openairdocs.org/sdr/UPS05844245.md): Fitting · cracked · Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C2, AFT CARGO PIT STA 1200 LONGERON 34R BATHTUB FITTING CRACKED IN FWD AND AFT CORNERS. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-0 FIG 26 AND SRM 51-1-20D.
- [SDR UPS05844259](https://openairdocs.org/sdr/UPS05844259.md): Fitting · cracked · Mar 22, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2 "A" PIT CARGO DOOR ENTRANCE L33R FWD CORNER BOTTOM BANANA FITTING HAS.400 INCH LONG CRACK. ROMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D & 51-1-21.
- [SDR UPS05844298](https://openairdocs.org/sdr/UPS05844298.md): Fitting · cracked · Mar 21, 2005 · N819UP · Doug DC873F · Wing, Control Surface Attach Fittings
  > INSPECTION TYPE:C2 RIGHT FLAP STA 3 SUPPORT FITTING HAS APPROX 6.125 INCH CRACK ON BOTTOM OF FITTING. REMOVED AND REPLACED RIGHT FLAP STA 3 SUPPORT FITTING IAW DC-8 SRM 51-3-0, 51-1-21, AND 51-1-20D.
- [SDR UPS05844258](https://openairdocs.org/sdr/UPS05844258.md): Rib · cracked · Mar 21, 2005 · N819UP · Doug DC873F · Vertical Stabilizer, Spar/Rib
  > C2 VER. FIN L/E HAS CRACKED RIB 3/4 INCH AT ACCESS PNL 51I. STOP DRILLED CRACK IAW DC-8 SRM 55-02-00. REPAIRED RIB IAW 55-02-00, 51 -1-20D, AND 51-3-0.
- [SDR UPS05844251](https://openairdocs.org/sdr/UPS05844251.md): Rib · cracked · Mar 21, 2005 · N819UP · Doug DC873F · Vertical Stabilizer, Spar/Rib
  > INSPECTION TYPE: C2, VERTICAL FIN L/E HAS CRACKED RIB.75 INCH AT ACCESS PNL 51F. REPAIRED VERTICAL FIN RIB IAW DC-8 SRM 55-02-00 FIG 002 AND SRM 51-1-20D.
- [SDR UPS05844243](https://openairdocs.org/sdr/UPS05844243.md): Fitting · cracked · Mar 21, 2005 · N819UP · Doug DC873F · Wing, Attach Fittings
  > INSPECTION TYPE:C2 RT WING FLAP WELL STA 230 UPPER AREA HAS CRACKED WEB TO INTERCOSTAL ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING IAW DC-8 SRM 51-1-21D.
- [SDR UPS05844293](https://openairdocs.org/sdr/UPS05844293.md): Rib · damaged · Mar 20, 2005 · N819UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:C2 RIGHT STA 3 AFT LINK TO FLAP HINGE BOLT FROZEN & NUT PLATE BROKEN. REMOVED DAMAGED RIB, REMOVED AND REPLACED NUT PLATE, AND FABRICATED & INSTALLED REPLACEMENT RIB PER EO DC8-5750-16293-A AND DWG DC8-57-009.
- [SDR UPS05844291](https://openairdocs.org/sdr/UPS05844291.md): Spar · cracked · Mar 20, 2005 · N819UP · Doug DC873F · Wing Spar
  > INSPECTION TYPE:C2 POSSIBLE CRACK BETWEEN VERTICAL FASTENERS ON RT WING REAR SPAR LOWER T-CAP RIGHT W/W STA 857 RBL 28-32. NDT DETECTED A 4 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK PER DWG SRO8570009. REPAIRED REAR SPAR LOWER T-CAP PER DWG SR
- [SDR UPS05844269](https://openairdocs.org/sdr/UPS05844269.md): Channel · corroded · Mar 20, 2005 · N819UP · Doug DC873F · Fuselage Miscellaneous Structure
  > C2 CEILING RIB CORRODED WITH CORROSION UNDER RADIUS FILLER RT W/W ABOVE FLAP BUSS DIRECTION CHANGE PULLEYS STA 930 RBL 58. REMOVED AND REPLACED HAT CHANNEL, STIFFENER, AND U-CHANNEL IAW DWG 5 645332, SRM TR 51-130, AND SRM 51-1-21 AND 51-2-1 FIG 1.
- [SDR UPS05844260](https://openairdocs.org/sdr/UPS05844260.md): Rib · cracked · Mar 20, 2005 · N819UP · Doug DC873F · Horizontal Stabilizer, Spar/Rib
  > INSPECTION TYPE: C2, CRACKED LOWER RIB ON L/H HORIZONTAL LEADING EDGE 40 INCHES FROM IB END. STOPDRILLED CRACK IAW DC-8 SRM 55-2-0 FIG.2. REPAIRED CRACKED RIB IAW DC-8 SRM 55-3-1 FIG. 3, 55-2-0 FIG. 2, & 51-1-20D.
- [SDR UPS05844265](https://openairdocs.org/sdr/UPS05844265.md): Longeron · cracked · Mar 19, 2005 · N819UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C2, LONGERON 15R IS CRACKED AT F/S 1730 & F/S 1750 AT CANTED FRAMES. REMOVED AND REPLACED LONGERON SECTION IAW DC-8 SRM53-2-2 FIG. 10, 51-1 -21, & 51-1-20D.

Next page: https://openairdocs.org/deregistered/N819UP-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 = 'N819UP' AND deregistration_id = 'N819UP-2011-03-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N819UP-2011-03-24/reports

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