N819UP, cancelled Mar 24, 2011

Service difficulty reports · 205

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS08854213Rod · brokenF/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.Dec 17, 2008 · N819UP · Doug DC873F · BrakeSDR UPS08853383Doubler · damagedINSPECTION 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 DOUBLESep 20, 2008 · N819UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS08853382Doubler · damagedINSPECTION 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-Sep 20, 2008 · N819UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07851177Slide · dislodgedINSPECTION 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/RNov 15, 2007 · N819UP · Doug DC873F · Escape SlideSDR UPS07850551Light · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2 AND CHECKS GOOD PER SAME.Aug 29, 2007 · N819UP · Doug DC873F · Emergency LightingSDR UPS07850350Battery · dischargedINSPECTION 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.Jul 24, 2007 · N819UP · Doug DC873F · Emergency LightingSDR UPS07849803Skin · crackedINSPECTION 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. REApr 20, 2007 · N819UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07849763Bracket · crackedINSPECTION 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.Apr 17, 2007 · N819UP · Doug DC873F · Wing SparSDR UPS07849683Finger Doubler · corrodedINSPECTION 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 SApr 15, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07849681Finger Doubler · corrodedINSPECTION 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, AApr 15, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07849761Fitting · crackedINSPECTION 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.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07849729Attach Fitting · crackedINSPECTION 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.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849728Attach Fitting · crackedINSPECTION 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.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849727Attach Fitting · crackedINSPECTION 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.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849713Fitting · corrodedINSPECTION 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.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849685Fitting · crackedINSPECTION 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.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07849671Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 822 L22L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849670Fitting · gougedINSPECTION 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.Apr 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07849765Door Frame · misrepairedINSPECTION 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.Apr 12, 2007 · N819UP · Doug DC873F · Fuselage Main, StructureSDR UPS07849684Channel · crackedINSPECTION 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 SRApr 12, 2007 · N819UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS07849826Skin · crackedINSPECTION 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.Apr 11, 2007 · N819UP · Doug DC873F · Wing, Plate/SkinSDR UPS07849791Spar Cap · crackedINSPECTION 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.Apr 11, 2007 · N819UP · Doug DC873F · Wing SparSDR UPS07849790Angle · crackedINSPECTION 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 FApr 11, 2007 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS07849745Skin · corrodedINSPECTION 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.Apr 10, 2007 · N819UP · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR UPS07849586Release Mech · contaminatedINSPECTION 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.Apr 3, 2007 · N819UP · Doug DC873F · Landing Gear DoorsSDR UPS07849680Attach Fitting · crackedINSPECTION 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.Jan 14, 2007 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS06848712Battery Pack · dischargedEMERGENCY LIGHT VERY DIM. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND UNIT IAW MM 33-50-01-2-4. OPS CHECK GOOD.Nov 15, 2006 · N819UP · Doug DC873F · Emergency LightingSDR UPS06848345Window · stickingCAPTAIN SIDE WINDOW HARD TO SLIDE. CLEARED DEBRIS FROM WINDOW TRACK. OPERATES AS REQUIRED, REF DC8 MM 56-10-00-0.Oct 20, 2006 · N819UP · Doug DC873F · Flight Compartment WindowsSDR UPS06847986Line · leakingLOST 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 HSep 13, 2006 · N819UP · Doug DC873F · Hydraulic System, MainSDR UPS06847948Window · obstructedCAPTAIN'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.Sep 6, 2006 · N819UP · Doug DC873F · Flight Compartment WindowsSDR UPS05845844Light · malfunctionedEMERGENCY 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.Nov 30, 2005 · N819UP · Doug DC873F · Emergency LightingSDR UPS05844301Spar · crackedINSPECTION 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 DCApr 11, 2005 · N819UP · Doug DC873F · Wing SparSDR UPS05844289Skin · crackedINSPECTION 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.Apr 10, 2005 · N819UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05844261Fitting · crackedINSPECTION 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.Mar 30, 2005 · N819UP · Doug DC873F · Wing, Attach FittingsSDR UPS05844267Stringer · crackedC2 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.Mar 25, 2005 · N819UP · Doug DC873F · Wing, Longeron/StringerSDR UPS05844299Support Fitting · crackedINSPECTION 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.Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844268Fitting · crackedC2 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.Mar 24, 2005 · N819UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS05844256Fitting · corrodedINSPECTION 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.Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844246Longeron · crackedINSPECTION 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.Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS05844245Fitting · crackedINSPECTION 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.Mar 24, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844259Fitting · crackedINSPECTION 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.Mar 22, 2005 · N819UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS05844298Fitting · crackedINSPECTION 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.Mar 21, 2005 · N819UP · Doug DC873F · Wing, Control Surface Attach FittingsSDR UPS05844258Rib · crackedC2 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.Mar 21, 2005 · N819UP · Doug DC873F · Vertical Stabilizer, Spar/RibSDR UPS05844251Rib · crackedINSPECTION 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.Mar 21, 2005 · N819UP · Doug DC873F · Vertical Stabilizer, Spar/RibSDR UPS05844243Fitting · crackedINSPECTION 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.Mar 21, 2005 · N819UP · Doug DC873F · Wing, Attach FittingsSDR UPS05844293Rib · damagedINSPECTION 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.Mar 20, 2005 · N819UP · Doug DC873F · Trailing Edge FlapsSDR UPS05844291Spar · crackedINSPECTION 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 SRMar 20, 2005 · N819UP · Doug DC873F · Wing SparSDR UPS05844269Channel · corrodedC2 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.Mar 20, 2005 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS05844260Rib · crackedINSPECTION 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.Mar 20, 2005 · N819UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS05844265Longeron · crackedINSPECTION 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.Mar 19, 2005 · N819UP · Doug DC873F · Fuselage Main, Longeron/Stringer
Back to N819UP, cancelled Mar 24, 2011