N706UP, cancelled Mar 30, 2010

Service difficulty reports · 179

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 = 'N706UP' AND deregistration_id = 'N706UP-2010-03-30'
  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 UPS06848022Slide · inoperativeMAIN CABIN EXIT SLIDE/SLIDE INOP, LOW PRESSURE. REMOVED AND REPLACED SLIDE ASSY PER 25-60-01-2. CLEARED, PLACARD REMOVED AND BOTH COURIER SEATS REACTIVATED.Sep 21, 2006 · N706UP · Doug DC871F · Escape SlideSDR UPS06846679Door Frame · crackedINSPECTION TYPE:C3 VISUAL AND HFEC INSP DETECTED A CRACK APPROX .125" ON THE L-2 DOOR UPPER FWD DOOR JAMB CORNER EXTENDING FROM FASTENER. CUT OUT DAMAGE AT L-2 DOOR UPPER FWD DOOR JAMB CORNER IAW SRM 53-02-00 FIG 18. FABRICATED AND INSTALLED FILLER, DOUBLER,Mar 29, 2006 · N706UP · Doug DC871F · Fuselage Main, StructureSDR UPS06846711Fairing · corrodedINSPECTION TYPE:C3 LT STA 98 CANOE CORRODED UNDER BOTH FLAP TRACKS. REMOVED LT STA 98 FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION BY MACHINING IAW SB 27-164. FABRICATED AND INSTALLED SHIMS IAW SB 27-164. INSTALLED FLAP CANOE AT STA 98 LT IAW DC8- MM Mar 24, 2006 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS06846718Stringer Clip · crackedINSPECTION TYPE:C2 CRACKED STRINGER CLIP ON OTBD SKATE ANGLE C/S-STRINGER 62 NR 4 MAIN TANK. REMOVED CRACKED CLIP AT OTBD SKATE ANGLE C/S STRINGER 62 NR 4 MAIN TANK IAW SRM 51-01-20D. FABRICATED AND INSTALLED CLIP ON O/B SKATE ANGLE C/S STRINGER 62 34 MAIN TMar 23, 2006 · N706UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846598Longeron · crackedFOUND LONGERON SPLICE L36 STA 1260-1280 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1260-1280 L36 IAW SRM 51-1-20D, AND 51-1-8.Mar 23, 2006 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06846719Fitting · crackedINSPECTION TYPE:C3 STA 98 FLAP ACTUATOR REAR SPAR FITTING O/B LUG FOR SUPPORT LINK ARM IS BROKEN. FABRICATED AND INSTALLED NEW FITTING FROM 7050-T7451 PER AMS 4050 PLATE IAW UPS ENG FILE # DC8-57-20160, SAA EA#008-2760-01- A0133 REV A, DOUGLAS PSAMSL DWG 7981Mar 21, 2006 · N706UP · Doug DC871F · Wing, Attach FittingsSDR UPS06846709Fairing · corrodedINSPECTION TYPE:C3 FLAP STA 98FH, CORROSION FOUND ON CANOE UNDER FLAP TRACKS. REMOVED STA 98 RH FLAP CANOE IAW DC8-MM 27-51-12. REMOVED CORROSION FROM FLAP CANOE IAW SB 27-164. FABRICATED AND INSTALLED SHIMS IAW SB 27-164. INSTALLED FLAP CANOE AT STA 98 RTMar 21, 2006 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS06846680Splice · corrodedA-PIT TORQUE BOX STA 280-270 LONGERON 34L-35L FITTING HAS CORROSION. REMOVED BATH TUB FITTING AT STA 280, AND REMOVED LONGERON SPLICE FITTING AT STA 270-280 L35L IAW SRM 51-1-20, AND SRM 53-2-2 FIG 10 LOCATED AND DRILLED AND INSTALLED NEW LONGERON SPLICE FITTMar 21, 2006 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06846597Longeron · crackedINSPECTION TYPE:C3 LONGERON 15R IS CRACKED WHERE VERTICAL STAB ATTACHES STA 1740. REMOVED CRACKED LONGERON SECTION AT STA 1730-1750 15R IAW SRM 51-01-21-0 AND SRM 53-02-02-0. FABRICATED AND INSTALLLED LONGERON SPLICE SECTION AT STA 1730-1750 L15R IAW SRM 53-Mar 20, 2006 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06846518Rib · crackedINSPECTION TYPE:C3 LT CENTER LE XRS 323 RIB IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-0, 57-3-1 AND 51-01-20D.Mar 18, 2006 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06846059Windshield · crackedOUTER PANE WINDSHIELD ON F/O'S SIDE CRACKED. REMOVED AND REPLACED RT WINDSHIELD PER MM 56-10-02-2, OPS AND LK CKS OK.Jan 27, 2006 · N706UP · Doug DC871F · Flight Compartment WindowsSDR UPS05845646Engine · flamed outNR 4 ENGINE FLAMED OUT IN CRUISE FLIGHT. T/S PER MM 71-00-00-1 FIG 139 SHT 1&2. REPLACED FUEL FILTER ELEMENT, RAN ENG WITH FEED & BOOST PUMP OFF, FUEL PRESS WITHIN LIMITS. ENG OPS NORMAL.Oct 26, 2005 · N706UP · Doug DC871F · Powerplant SystemSDR UPS04843616A/C Pack · odorON TOP OF DESCENT STRONG DIESEL FUEL JET FUEL ODOR WAS PRESENT AND SMELLED. ODOR WAS VERY STRONG. PRESSURIZED A/C, RAN BOTH PACKS FOR 30 MIN. NO ODOR NOTED. INSPECTED A/C FOR SPILLED FLUIDS IN CARGO AREA AND LOWER PITS. NONE FOUND. A/C OK FOR SERVICE.Dec 20, 2004 · N706UP · Doug DC871F · Cabin Cooling SystemSDR UPS04843555Battery Pack · dischargedEMER LIGHTS STAY ON FOR LESS THAN A SECOND. REMOVED AND REPLACED EMER LIGHTS BATT PACK. OPS CK GOOD.Nov 29, 2004 · N706UP · Doug DC871F · Emergency LightingSDR UPS04843333Lamp · inoperativeINSPECTION TYPE:N/A 3 EA LIGHTS FOR EMERGENCY LIGHTING AT ENTRY DOOR INOP. RELAMPED LIGHTS. OPS CHECKS GOOD.Oct 9, 2004 · N706UP · Doug DC871F · Emergency LightingSDR UPS04842661Link · brokenNR 4 BRAKE COMPENSATING LINK BROKE AND BRAKE SPUN. REMOVED AND REPLACED COMPENSATING LINK IAW MM 32-42-04-4, 32-33-00-2 ATTACHED LINK TO MLG 29046. SECURED LINK TO BRAKE IAW M/M 32-42-01-4 AND 32-33-002Jul 7, 2004 · N706UP · Doug DC871F · BrakeSDR UPS04842061Fitting · crackedINSPECTION TYPE:C2 STATION 270 BETWEEN LONG 35L-36 BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D.Mar 6, 2004 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04842063Longeron · crackedINSPECTION TYPE:C2 STATION 257 LONGERON 34R I/B SIDE IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 230-290, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10.Mar 5, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04842062Longeron · crackedINSPECTION TYPE:C2 STATION 257 LONG 36 RIGHT IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 250-290, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10.Mar 5, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04842035Floor Support · corrodedINSPECTION TYPE: C2, FLOOR SUPPORT IS CORRODED BEYOND LIMITS BETWEEN STATION 1702 -1723 AT LBL 19. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND SRM 51-1-20D, 51-1-21 AND 51-3-0.Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04842034Skin · crackedINSPECTION TYPE: C2, REMOVE EXTERNAL DOUBLER AT STATION 1722 LONGERON 17R-18R IAW EO DC8-5330-17288-A APPROX C AND REPAIR IAW SRM 53-2-1 FIG 7. REMOVED EXISTING DOUBLER, CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLMar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04842031Support Fitting · crackedINSPECTION TYPE: C2, STATION 780 FLOORBEAM SUPPORT FITTING IS CRACKED AT XC46R. REMOVED AND REPLACED FITTING IAW DWG 3641126 AND SRM 51-1-20D, 51-3-0.Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04842029Longeron · crackedINSPECTION TYPE:C2 STATION 1753 LONG 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION, INSTALLED STRAPS AND SPLICE FITTING IAW SRM 53-2-2 FIG 10.Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04842014Doubler · corrodedINSPECTION TYPE: C2, AFT SIDE STATION 1540 LONGERON 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17D, 51-1-20D, 51-1-21.Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04842013Longeron · crackedINSPECTION TYPE: C2, STA 1733 LONG 14L IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10.Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04842010Shear Tie · crackedINSPECTION TYPE:C2 STATION 1600 SHEAR TIE IS CRACKED BETWEEN LONGERONS 28L-29L. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 2A.Mar 3, 2004 · N706UP · Doug DC871F · Fuselage Main, StructureSDR UPS04842033Frame · corrodedINSPECTION TYPE: C2, STATION 1300 FRAME IS CORRODED BEYOND LIMITS ON LOWER FLANGE AT LONG 36. CUT OUT DAMAGED FRAME SECTION, FABRICATED, INSTALLED 2 SPLICES, ANGLES AND REPLACEMENT FRAME SECTION IAW SRM 53-2-0 FIG 2.Mar 2, 2004 · N706UP · Doug DC871F · Fuselage Main, FrameSDR UPS04842030Skin · crackedINSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STATION 1730 LONG 8L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.Mar 2, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04842017Skin · crackedINSPECTION TYPE: C2, RUDDER EXTERIOR SKIN IS CRACKED AT RT UPPER SIDE. REMOVED AND REPLACED RUDDER IAW MM 27-21-01.Mar 2, 2004 · N706UP · Doug DC871F · Rudder, Plate/SkinSDR UPS04842011Skin · corrodedINSPECTION TYPE: C2, RIGHT HORIZONTAL STAB L/E SKIN HAS INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4.Mar 2, 2004 · N706UP · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR UPS04842009Fitting · crackedINSPECTION TYPE: C2, LONGERON 31L SPLICE FITTING IS CRACKED BETWEEN STA 1260-1280. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D, 53-1-0.Mar 2, 2004 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04842067Skin · corrodedINSPECTION TYPE:C2 LOWER FUSELAGE SKIN IS BULGED AT STA 275 LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, INTERNAL DOUBLER FILLER AND SKIN FILLER IAW SAA SK 706-550 AND DC8-5330-20148-A.Feb 28, 2004 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04841751Relief Valve · stuckDURING CRUISE NOTICED HYDRAULICS DECREASING. FOLLOWED POM PROCEDURE AND DEPRESSURIZED AND ISOLATED THE SYSTEM. FOUND BOGIE UNLOCK CYLINDER RELIEF VALVE ON LEFT MAIN FEAR STUCK OPEN. REPLACED RELIEF VALVE POF 32-53-02. NO LEAKS DETECTED. HYD WAS SERVICED.Jan 16, 2004 · N706UP · Doug DC871F · Landing Gear Steering SystemSDR UPS03841456Skin · corrodedFOUND EXTENSIVE CORROSION AT STATION 1746 SEVERAL RIVETS PULLED THROUGH SKIN. SKIN IS CRACKED AT L36 AND STA 1746. REMOVED FASTENERS IN CORRODED AREA FOUND L36 AFT OF STA 1746. REMOVED 9 X 6 SECTION OF SKIN REF SRM 53-02-011 NR 39550, REF ECA 56908 LOG PAGEOct 17, 2003 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS03841223Fitting · crackedLT INBOARD FLAP HINGE CRACKED (MARKED) LT WING STA 98. DEFERRED PER FERRY PERMIT 9020. REMOVED STA 98 BASED FTG & ATTACHING STRUCTURE. LOCATED & DRILLED NEW 5751182-505 BASE FTG IAW DAC DWG 5751172. INSTALLED BASE FTG IAW DAC DWG 5751172. INSTALLED CLOSURSep 15, 2003 · N706UP · Doug DC871F · Trailing Edge FlapsSDR UPS03840376Smoke Detector · inoperativeNR 3 SMOKE DETECTOR DOES NOT TEST. RELAMPED, OPS CHECK GOOD.Mar 27, 2003 · N706UP · Doug DC871F · Smoke DetectionSDR UPS02837958Odor · detectedINSPECTION TYPE:N/A ODOR IN COCKPIT FROM A/C UNIT. RAN BOTH PACKS WITH GROUND CART AND OFF ENGINE BLEEDS, COULD NOT DUPLICATE ODOR. OK FOR CONTINUED SERVICE.Mar 30, 2002 · N706UP · Doug DC871F · Air Distribution SystemSDR UPS02837935Fitting · corrodedINSPECTION TYPE:C1 STA 70 FWD SIDE LONG 31R UPPER FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4614397, AND SRM 51-1-20D, 51-1-21.Mar 11, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837932Doubler · corrodedINSPECTION TYPE:C1 STA 25 TO 60 INTERNAL DOUBLER IS CORRODED BEYOND LIMITS BETWEEN LONG 26R TO 31R. REMOVED AND REPLACED DOUBLER IAW DWG 5649028, AND SRM 51-1-20D, 51- 1-21.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837908Longeron · corrodedINSPECTION TYPE:C1 STA 1650 LONG 35L LONGERON AND END FITTINGS ARE CORRODED BEYOND LIMITS. REMOVED END FITTINGS, AND LONG 35L BETWEEN STA 1650-1680, FABRICATED AND REPLACED LONGERON SECTION AND END FITTINGS IAW DWG 3647110, AND SRM 51-1-20D, 51-3-0.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02837897Fitting · crackedINSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D, 51-1-20D.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837896Fitting · crackedINSPECTION TYPE:C1 STA 1200 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 51-1-20D, 53-2-0 FIG 2D.Mar 8, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837911Fitting · crackedINSPECTION TYPE:C1 STA 960 T-FITTING BETWEEN MAIN LANDING GEAR DOORS IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5616306, AND SRM 51-1-20D.Mar 7, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837914Skin · crackedINSPECTION TYPE:C1 LT MID GALLEY DOOR LOWER FWD CORNER CUTOUT SKIN IS CRACKED AT STA 1306 BETWEEN LONG 20L AND 21L. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15A.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837904Skin · crackedINSPECTION TYPE:C1 L2 DOOR JAMB LOWER FWD CORNER SKIN IS CRACKED BETWEEN LONG 20L AND 21L STA 1620. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 18.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837900Skin · crackedINSPECTION TYPE:C1 L-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM 53 -2-0 FIG 15 AND SRO8530021, AND SKIN IS CRACKED AT STA 60 BETWEEN LONG 20L AND 21L. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLERMar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837899Skin · crackedINSPECTION TYPE:C1 REPAIR AT STA 1440, UPPER AFT CORNER D-PIT DOOR IS A CATEGORY D PER EO DC8-5330-12800, AND SKIN IS CRACKED AT LONG 22R APPROX. REMOVED EXISTING REPAIR, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS. AT CUTOUT, FABRICATED AND INSTALLED DOUBLEMar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02837895Fitting · corrodedINSPECTION TYPE:C1 MAIN CARGO DOOR JAMB NR 7 LATCH SPOOL FITTING HAS LOWER JAMB FITTINGS FWD AND AFT OF LATCH SPOOL FITTING HAVE INTERGRANULAR CORROSION AT STA 280 LONG 21L. REMOVED AND REPLACED FITTINGS IAW DWG 4773295 AND SRM 51-3-0, 51-1-20D.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02837878Door Frame · crackedINSPECTION TYPE:C1 L1 DOOR UPPER FWD PAN IS CRACKED IN CORNER, STA 25 LONG 10L. CUT OUT CRACK, NDT VERIFIED NO CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1D.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, StructureSDR UPS02837873Skin · crackedINSPECTION TYPE:C1 REPAIR AT STA 280 FWD LOWER CORNER OF A PIT DOOR CUTOUT IS A CATEGORY D PER EO DC8-5330-12800 AND SKIN IS CRACKED BETWEEN LONG 31R AND 32R. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-2-0 FIG 22.Mar 6, 2002 · N706UP · Doug DC871F · Fuselage Main, Plate/Skin
Back to N706UP, cancelled Mar 30, 2010