N260UP

Service difficulty reports · 329

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 = 'N260UP' 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 UPS07M50381Structure · corrodedINSPECTION TYPE:C CABIN T-CHORD AT STA 2007 LBL 53 FOUND CORRODED AS MARKED. CABIN T-CHORD REMOVED STA 2007 LBL 53 CORROSION REMOVED & FOUND OUT OF LIMIT PER SRM 53-40-00 V1 R38. NEW T-CHORD FAB PER SRM 53-40-00 V1 R38 & DWG NJC6040. HOLES P/UP ON FAB T-CHOMay 29, 2007 · N260UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M50376Channel · corrodedINSPECTION TYPE:C AFT CARGO STA 1960, LONGERON R43 LONGERON CHANNEL STIFFENER FOUND WITH CORROSION AS MARKED. NEW CHANNEL FAB AS PER DOC DWG NGA6313 MATL USED:7075-0-0.071. CHANNEL HEAT TREATED PER DPS7.00-1 & HARDNESS VALUES 86.9 PER DPS 1.05-3. NEW CHANNEMay 29, 2007 · N260UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M50231Longeron · corrodedINSPECTION TYPE:C AFT CARGO STA 1960 LONGERON R40 FOUND WITH CORROSION AS MARKED. AFT CARGO STA 1950 TO 1960 LONG R40 REMOVED & TRIMMED OFF PER SRM 53-10-01 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R.13 06-10-01.001 & FOUND NO CRACK EVIDENT. REP LONG & May 29, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50230Longeron Splice · corrodedINSPECTION TYPE:C AFT CARGO STA 1853-1871 LONGERON R48 FOUND LONGERON SPLICE WITH CORROSION AS MARKED. NEW SPLICE FAB PER DOC DWG: AGA7438. FPI CARRIED OUT IAW BOEING DPS 4.707 & FOUND NO CRACK EVIDENT. NEW SPLICE FASTENER HOLES PICK UP PER SRM 51-31-01 V2May 29, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50365Skin Panel · crackedINSPECTION TYPE:C RIGHT FIXED L/E LWR COMPT THRU ACCESS 619CB (REFUEL PANEL) UPPER SKIN DOUBLER SUSPECTED CRACK AT STA XORS 537. RIGHT WING REFUELING/DEFUELING ADAPTOR O/B REMOVED PER AMM28-21-08R.55. DAMAGE AREA TRIM OFF & REPAIR ANGLES FAB PER ADV EN1375-0May 25, 2007 · N260UP · Doug MD11F · Wing, Plate/SkinSDR UPS07M50284Skin · crackedINSPECTION TYPE:C LT FIXED LE LWR COMPT UPPER SKIN DOUBLER SUSPECTED CRACK AT STA XORS 535. HFEC INSP CARRIED OUT PER DAC NDTSPM R.13 PART 06-10-01-001 FOUND CRACK AS MARKED. REPAIR ANGLES FAB AND CRACK AREA TRIM OFF PER EN1375-07. REPAIR ANGLES HEAT TREATEMay 25, 2007 · N260UP · Doug MD11 · Wing, Plate/SkinSDR UPS07M50229Structure · crackedINSPECTION TYPE:C RIGHT FIXED L/E STRUCTURE FOUND CRACKS ON UPPER DOOR CUTOUT AREA NR 3 SLAT TELESCOPIC DUCT VICINITY. DAMAGE AREA TRIM OFF PER ADV EN1356-07. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR PARTS FAB, HOMay 25, 2007 · N260UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS07M50228Bracket · corrodedINSPECTION TYPE:C CTR CARGO BETWEEN STA 1541-1561 BETWEEN LONGERON L42 & L43 PARTITION BRACKET FOUND WITH CORROSION AS MARKED. CORROSION REMOVED PER SRM 51-21-01 V1 R38. MATL TK:0.063" TK RMV:0.036" THK REM:0.027" FOUND EXCEEDED LIMIT PER SRM 53-00-01 V2 FIGMay 23, 2007 · N260UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M50302Longeron · corrodedINSPECTION TYPE:C CTR CARGO THRU STATION 1661, LONGERON R48 FOUND WITH CORROSION AS MARKED. CORROSION REMOVED FOUND EXCEEDS PER SRM 53-00-01V.1R.38. REPAIR ANGLES FAB AND FASTENER HOLES PICK UP PER EN1355-07. REP ANGLES 02EA AND REWORK AREA REPROTECTED AND May 21, 2007 · N260UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M50222Longeron · corrodedINSPECTION TYPE:C CTR CARGO STA 5-110 THRU 5-119 LONGERON R46 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-110 THRU 5-119 DAMAGED LONG TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REP May 21, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50221Longeron · corrodedINSPECTION TYPE:C CTR CARGO STA 5-113, LONGERON R43 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-99 TO 5-119 DAMAGED LONG TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REP LONG & SPLICEMay 21, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50220Longeron · corrodedINSPECTION TYPE:C CTR CARGO STA 1701 LONGERON L43 FOUND WITH CORROSION AS MARKED. LONG STA 1091-1751 REMOVED & TRIMMED OFF PER SRM 53-10-01 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 FOUND NO CRACK EVIDENT. REPAIR LONG & SPLICE FAB & FASTENER HOLES PIMay 21, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50219Longeron · corrodedINSPECTION TYPE:C CTR CARGO STA 1561 LONGERON R43 FOUND WITH CORROSION AS MARKED. DAMAGED LONG REMOVED & TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR SPLICE FAB PER SRM 53-10-00 V1May 21, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50459Seat Track · corrodedINSPECTION TYPE:C CABIN - SEAT TRACK AT STA 1965 LBL 107 FOUND CORRODED. CORRODED EXISTING TRACK TRIMMED OFF FR STA 1831-2007 PER SRM 53-70-00 V1 FIG 7R.38. HFEC INSP C/OUT PRT DAC NDTSPM R.13 06-10-01.001 FOUND NO CRACK EVIDENT. SEAT TRACK SPLICE HAT, SPLIMay 18, 2007 · N260UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M50217Longeron · corrodedINSPECTION TYPE:C CTR CARGO STA 5-113 LONGERON L43 FOUND WITH CORROSION AS MARKED. DAMAGED LONG L43 TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC CARRIED OUT PER DAC NDTSPM R13 FOUND NO CRACK EVIDENT. REPAIR LONG & SPLICE FAB AND FASTENER HOLES PICK UP PER SRM May 18, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50208Longeron · corrodedINSPECTION TYPE:C CTR CARGO STA 5-113 THRU 1541 LONGERON L47 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-113 THRU 1551 DAMAGED LONG TRIMMED OFF PER SRM 53-10-00 V1 R38. HFEC CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 ON TRIMMED OFF AREA & FOUND NO CRACKMay 18, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50202Longeron · corrodedINSPECTION TYPE:C CTR CARGO STA 5-113 THRU 1541, LONGERON L48 FOUND WITH CORROSION AS MARKED. CTR CARGO STA 5-119 L48 SPLICE REMOVED PER SRM 51-33-01 V2 R38. DAMAGED LONGERON STA 5-113 THRU 1551 TRIMMED PER SRM 53-10-00 V1 FIG 2 R38, STA 5-119 L48 SPLICE & SMay 18, 2007 · N260UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS07M50094Seat Track · corrodedINSPECTION TYPE:C CABIN-SEAT TRACK BETWEEN STA889-919 RBL=107 FOUND CORRODED. REMOVAL C/OUT ON SEAT TRACK AREA TO EXECUTE REPAIR AS NECESSARY. REPAIRED S/TRACK SPLICE HAT AND SPLICE PLATE FAB PER SRM 53-70-00.V2.R 38. PICKED UP HOLES FOR FAB PARTS PER SRM 5May 18, 2007 · N260UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M50421Skin · corrodedINSPECTION TYPE:C CTR CARGO UNDERFLOOR SPACE STA 5-11 LONGERON R51, SKIN & ATTACHMENTS FOUND WITH CORROSION AS MARKED. CORROSION THROUGH SKIN TRIMMED OUT AS PER EN1397-07. HFEC INS C/OUT PER DAC NDTSPM R.13 06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR I/O DBMay 17, 2007 · N260UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS07M50364Skin · damagedINSPECTION TYPE:C RIGHT WING I/B FLAP LOWER SURFACE I/B SEGMENT SKIN TO REPLACE DUE TO BADLY PITTED. RIGHT WING I/B FLAP LOWER SURFACE I/B SEGMENT LOWER SKIN REMOVED PER SRM 51-31-01 V2 R38. NEW SKIN FAB PER BOEING DRAWING ARC2736 REV B. NEW SKIN HOLES PICKMay 17, 2007 · N260UP · Doug MD11F · Trailing Edge FlapsSDR UPS07M50207Skin · damagedINSPECTION TYPE:C LEFT WING I/B FLAP LOWER SURFACE I/B SEGMENT SKIN TO BE REPLACED. NEW SKIN FAB PER BOEING DWG ARC2736 R.B. NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V2 R38. NEW SKIN PROTECTED PER SRM 51-21-01 V2 R38. NEW SKIN INSTALLED PER SRM 51-31-01 VMay 17, 2007 · N260UP · Doug MD11F · Wing, Plate/SkinSDR UPS07M50201Skin · damagedINSPECTION TYPE:C RIGHT WING - I/B FLAP LWR SURFACE O/B SEGMENT SKIN TO BE REPLACED. SKIN REMOVED PER SRM 51-31-01 V2R38. NEW SKIN FAB USING MATL 2024T3-0. 040" TK PER DWGARB2444. NEW SKIN HOLES DRILLED & REPROTECTED PER SRM 51-21-01V2R38. OK TO INSTALL NEMay 17, 2007 · N260UP · Doug MD11F · Wing, Plate/SkinSDR UPS07M50200Skin · damagedINSPECTION TYPE:C LEFT WING - I/B FLAP, LWR SURFACE O/B SEGMENT SKIN TO BE REPLACED. SKIN REMOVED PER SRM 51-31-01V2R38. NEW SKIN FAB PER SRM 51-31-01V2R3 8. NEW SKIN HOLE P/UP PER 51-31-01V2R38. NEW SKIN PROTECTED PER SRM 51- 31-01V2R38. NEW SKIN PAINTEDMay 17, 2007 · N260UP · Doug MD11F · Wing, Plate/SkinSDR UPS07M50399Skin · corrodedINSPECTION TYPE:C RT EXTERIOR FUSELAGE SKIN FOUND WITH CORROSION AT SEVERAL AREAS ADJACENT TO FWD SIDE OF APU EXHAUST DOOR AS MARKED (UPPER PORTION). RT EXTERIOR FX SKIN FWD SIDE OF APU EXHAUST DOOR UPPER PORTION DAMAGED SKIN TRIMMED OUT PER EN1416-07 & PARTSMay 15, 2007 · N260UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS07M50366Skin · crackedINSPECTION TYPE:C EXISTING REPAIR FOUND ON RIGHT DROOP ASSY UPPER SURFACE O/B SIDE AS MARKED. EXISTING REPAIR REMOVED AS PER SRM 51-31-01 V2 R38. REPAIR DOUBLER FABRICATED PER EN1349-07. HFEC INS CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND CRACK APPROMay 15, 2007 · N260UP · Doug MD11F · Leading Edge DevicesSDR UPS07M50204Rib · crackedINSPECTION TYPE:C RIGHT SLAT TRACK 16 STRUCTURE I/B RIB CRACKED. CRACKED RIB 16 AT RIGHT WING REMOVED PER SRM 51-31-01 V2 R38. ATTACHMENT HOLES XFERRED ONTO NEW RIB PER DOUGLAS DWG ARB2873. FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R38. REWORKED AREA REMay 14, 2007 · N260UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS07M50203Rib · crackedINSPECTION TYPE:C LEFT SLAT TRACK 16 STRUCTURE I/B RIB CRACKED. CRACKED RIB 16 AT LEFT WING REMOVED PER SRM 51-31-01 V2. ATTACHMENT HOLES T XFERRED ONTO NEW RIB PER DOUGLAS DWG ARB2873. FASTENER HOLES PICKED UP PER SRM 51-31-01 V2 R38. REWORKED AREA REPROTMay 14, 2007 · N260UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS07M50400Stop Fitting · crackedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP STOP FITTING FOUND CRACK (VANE TRACK NR 4 FROM I/B VICINITY) LEFT WING O/B TRAILING EDGE FLAP ASSY REMOVED PER AMM27-50-30R.55. LEFT WING O/B FLAP I/B & O/B CARRIAGE ROLLERS ASSY REMOVED PER CMM 57-52-04 R.58.May 11, 2007 · N260UP · Doug MD11F · Trailing Edge FlapsSDR UPS07M50384Stop Fitting · crackedINSPECTION TYPE:C RIGHT O/B TRAILING EDGE FLAP STOP FITTING SUSPECTED CRACK (VANE TRACK NR 4 FROM I/B). RIGHT WING O/B TRAILING EDGE FLAP ASSY REMOVED PER AMM27-50-30 R55. HFEC INSP C/OUT PER DA DACNDTSPM R.13 PART 06-10-01-001 ON STOP FITTING FOUND CRACK. May 11, 2007 · N260UP · Doug MD11F · Trailing Edge Flaps
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