N329UP

Service difficulty reports · 129

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 = 'N329UP' AND registry_match = 'registration'
  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 IPXA10658538Skin · crackedINSPECTION TYPE:6C, LT WING - NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 46 JUST AT OSS572.5, ORIGINAL MATERIAL IS 7075T6-0063IN, CRACK LENGTH IS 0.07", DAMAGED CUTOUT SIZE IFeb 11, 2010 · N329UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658537Skin · crackedINSP TYPE:6C, LT WING - NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46, JUST AT OSS641.9, ORIGINAL MATERIAL IS 7075T6-0063IN, CRACK LENGTH IS 0.09", DAMAGED CUTOUT SIZE IS 8.8Feb 11, 2010 · N329UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658536Hinge Fitting · crackedINSPECTION TYPE:6C, LT WING - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. LT WING - INBD MAIN FLAP HINGE FTG, REPAIRED IAW SRM 57-53-02-2R1, FIG 201, REF 46, ORIGINAL MATERIAL IS 7075T73 FORGING, CRACK LENGTH AT INBD FLANGE IS 1", OTBD FLANGE IS 0.9", DAMFeb 11, 2010 · N329UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658535Hinge Fitting · crackedRT WING - INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG 2 201, REV 46 ORIGINAL MATERIAL IS 7075T73 FORGING, CRACK LENGTH INBD FLANGE IS 1.125" & OTBD FLANGE IS 1.25", DAMAGED CUTOUT SIZE Feb 11, 2010 · N329UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658514Skin · crackedINSP TYPE:C, LT WING - NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS723.9, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.12" DAMAGED CUTOUT SIZE IS 8.875" X 7.125" TFeb 11, 2010 · N329UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658513Skin · crackedINSP TYPE:C, LT WING - NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR3 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS792.5, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.13" DAMAGED CUTOUT SIZE IS 8.875" X 7.125" THFeb 11, 2010 · N329UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658512Skin · crackedINSPECTION TYPE:C RHW - NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RHW 9 SLAT INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV46 JUST AT OSS572.5, ORG MATL IS 7075T6-0063IN, CRACK LENGTH 0.08 INCH DAMAGED CUTOUT SIZE IS 8.875 INCH BY 7.37Feb 11, 2010 · N329UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658511Skin · crackedINSPECTION TYPE:C RHW - NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING NR 9 SLAT OTBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 46 JUST AT OSS641.9, ORG MATL IS 7075T6-0063IN, CRACK LENGTH IS 0.15 INCH, DAMAGED CUTOUT SIZE IS 8.875"Feb 11, 2010 · N329UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658505Stiffener · crackedINSPECTION TYPE:C MEC, CABIN FLOOR SUPPORT BEAM STA246 LBL40 FWD STIFFENER FOUND CRACKED MEC CABIN FLOOR SUPPORT STA 246 LBL40 INCH STIFFENER REPAIRED AS PER SRM 53-10-51-2R4 FIG 201 REV46, ORG MATL IS BAC1490-2793-7075T62, CRACK LENGTH IS 1 INCH, THIS REPAIR Feb 11, 2010 · N329UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09658017Cover · tornCREW ENTRY DOOR IS DIFFICULT TO OPEN. FOUND INGRESS/RE ENTRY ROPE COVER TORN FROM CHANNEL CAUSING DOOR TO BIND. ACCOMP EO B767-2520-35992. SECURED DOOR INGRESS ROPE COVER IAW EO DEFERRED FOR PERM REPAIR.Dec 15, 2009 · N329UP · Boeing 76734AF · Emergency EquipmentSDR IPXA09657984Escape Rope · tornESCAPE ROPE JAMMED IN L1 DOOR ROLLERS. MX PERFORMED TEMP REPAIR ON THE ROPE COVER PER AN EO D414512 ASSIGNED. L1 DOOR ESCAPE ROPE COVER REPLACED IAW MM 25-20-00-2.Dec 6, 2009 · N329UP · Boeing 76734AF · Emergency EquipmentSDR IPXA09656472Skin · dentedINSPECTION TYPE:N/A RIGHT TRAILING EDGE I/B AFT FLAP LOWER SKIN DENT. REPAIRED PER EO B767-5750-34041-A.Jun 28, 2009 · N329UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS09654637Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK POS 2R MOST O/B PANEL 40 INCHES AFT OF RED LINE AND APPROX 4 INCHES I/B OF O/B SEAT TRACK. GOUGED 2.1" LONG X 1" WIDE. REPAIRED PER EO B767-5320-31355-A.Feb 8, 2009 · N329UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS08652203Skin · chafedINSPECTION TYPE:C FX MEC DOOR EXTERIOR SURFACE FOUND CHAFING MARK. MEC DOOR SKIN REPAIRED AS PER SRM 52-40-01-2R5 FIG 201.Apr 30, 2008 · N329UP · Boeing 76734AF · Service DoorsSDR UPS08652190Stiffener · crackedINSPECTION TYPE:C CARGO MEC STA 246 LBL 50 INCH STIFFENER CRACK, CRACK LENGTH 3/8 INCH. MEC STA 246 LBL 50 INCH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-40-02 AND 51-10-02.Apr 30, 2008 · N329UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652189Angle · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1085 LBL 26" BELOW FLOOR VERTICAL WEB ATT ANGLE CRACK, CRACK LENGTH 3/4 INCH. AFT CARGO COMPT STA 1085 LBL 26 INCHES VERTICAL WEB ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Apr 29, 2008 · N329UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652188Angle · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1085 RBL 26" BELOW FLOOR VERTICAL WEB ATT ANGLE CRACK, CRACK LENGTH 3/4 INCH. AFT CARGO COMPT STA 1085 RBL 26 IINCHES VERTICAL WEB ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Apr 29, 2008 · N329UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652187Splice · crackedINSPECTION TYPE:C AFT OF BULK CARGO MAIN DECK FLOOR SUPPORT ATT SPLICE ANGLE CRACK, CRACK LENGTH 1.25 INCH. AFT OF BULK CARGO MAIN DECK FLOOR SUPPORT ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Apr 29, 2008 · N329UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652042Warning Light · illuminatedATB - CREW REPORTED DURING CLIMB THEY RECEIVED A LT DUCT EICAS MESSAGE. LIGHT EXTINGUISHED AFTER ENG BLEED AIR SUPPLY AND ISOLATION VALVE CLOSED. OPS CHECKS NORMAL PER FIM 26-18-00 FIG 104 SHEET 1.Apr 16, 2008 · N329UP · Boeing 76734AF · Central WarningSDR UPS07650935Pressure Valve · defectiveINSPECTION TYPE:ETOP DIVERSION - ON CLIMB AT FL 250, HAD A R ENGINE BLEED OVHT EICAS MSG & OVHT ON PANEL, LTV LIST COMPLETE, HAD 10 PSI OF PRESSURE ON R SIDE, R BLEED AIR SWITCH OFF. CYCLED BLEED AIR SWITCH WITH PWR REDUCTION & LIGHT STAYED ON 20 MINS STRAIGHOct 17, 2007 · N329UP · Boeing 76734AF · Pneumatic Distribution SystemSDR UPS07650848Seat Track · corrodedINSPECTION TYPE:C1 FUSELAGE UPPER LOBE, CORROSION ON I/B FLANGE OF SEAT TRACK AT NUT PLATE HOLE, BS 527, LBL 55, WL 200. BLENDED CORROSION, FABRICATED & INSTALLED REPAIR PARTS PER ER 07-3583.Sep 23, 2007 · N329UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR UPS07650593Transceiver · inoperativeINSPECTION TYPE:ETOP ATB - WX RADAR FAIL DISPLAYED ON HSI W/BOTH SYSTEMS SELECTED. WXR TEST DISPLAYS WXR FAIL WEAK R/T ON HSI. ATB ACCOMPLISHED DUE TO NO WX RADAR AND THUNDERSTORMS ON PLANNED FLIGHT ROUTE. T/S PER FIM 34-43-00. FOUND WXR TRANSCEIVER INOP RSep 3, 2007 · N329UP · Boeing 76734AF · Weather Radar SystemSDR UPS07650455Indicator · faultyINSPECTION TYPE:ETOP ALL 3 F/Q INDICATOR WINDOWS IN COCKPIT UNREADABLE. BUBBLES IN FUEL INDICATOR LEFT & RIGHT. *SUPPLEMENTAL SDR* REMOVED AND REPLACED FUEL QUANTITY INDICATOR PER MM 28-41-04-4. PERFORMED ADJ AND TEST IAW MM 28-41-00-5.Aug 17, 2007 · N329UP · Boeing 76734AF · Fuel Quantity IndicatorSDR UPS07650327Anti-Ice Valve · inoperativeINSPECTION TYPE:ETOP EICAS MESSAGE ANTI-ICE DISPLAYED AND ENGINE ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH SELECTED ON TO OFF. REMOVED AND REPLACED ANTI-ICE VALVE. OPS CHK WITH ENG RUNNING AND LEAK CHK DONE SATISFACTORY. NO LEAK REF B767 AMM 30-Jul 20, 2007 · N329UP · Boeing 76734AF · Air Intake Anti/De-Ice SystemSDR UPS06647396Bracket · crackedLT T/R LOCKOUT BRACKET CRACKED ON NR 1 ENG, 11 OCLOCK POSITION. REPAIRED IAW CMM 78-32-02 REPAIR 16.Jul 23, 2006 · N329UP · Boeing 76734AF · Engine Thrust ReverserSDR UPS06646375Window · inoperativeF/O'S (R2) EMERG EXIT WINDOW LATCHING HANDLE OUT OF RIG, WILL NOT MOVE TO FULLY AFT POS. REMOVED AND REPLACED R2 WINDOW PER MM 56-11-02, OPS CK GOOD.Mar 2, 2006 · N329UP · Boeing 76734AF · Flight Compartment WindowsSDR UPS04643615Unknown · fumesFUMES IN COCKPIT, NO SMOKE, NO EMERGENCY DECLARED. RAN BOTH ENGS FOR 35 MINS WITH BOTH DUCTS OPERATING WENT TO FULL HOT AND COLD. INSPECTED ENG INLETS RAN AIR INLETS & EXHAUSTS INSPECTED BOTH ACM'S ALSO USED APU AIR WENT FULL HOT & COLD. RAN ENG ABOVE IDLDec 21, 2004 · N329UP · Boeing 76734AF · Air Distribution SystemSDR UPS03640234Engine · stalledINSPECTION TYPE: ETOP, SUSPECTED COMPRESSOR STALL LT ENGINE. VIBRATION INCREASED TO 4.4, ALL OTHER PARAMETERS NORMAL. REPLACED LT ENGINE, OPS CHECK NORMAL IAW MAINT FUNCTION TC6002.Feb 24, 2003 · N329UP · Boeing 76734AF · Powerplant SystemSDR UPS01635181Compressor · stalledINSPECTION TYPE:ETOP PILOT REPORT - NR 1 ENG FLUX/COMP STALLS. LEFT ENGINE STALLED. STALL STOPPED AFTER THRUST REDUCED TO IDLE AS THRUST LEVER WAS ADVANCED, FLUCTUATIONS AGAIN OCCURRED. ENGINE LEFT AT IDLE. ENGINE BORESCOPE INSPECTION C/O IAW MM 72-00-00 PMar 4, 2001 · N329UP · Boeing 76734AF · Turbine Engine Compressor Section
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