N294UP

Service difficulty reports · 369

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 = 'N294UP' 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 UPS08M51973Skin · chafedINSPECTION TYPE:C RIGHT I/B AILERON FOUND CHAFE MARKS ALONG L/E LOWER SKIN I/B SIDE. CHAFED SKIN REMOVED PER SRM 51-35-01V.2R.40. HOLES ON NEW SKIN PICKED UP PER SRM 51-31-01 V.2 R.40. NEW SKIN INSTALLED AS PER SRM 51-35-01 V.2 R.40.Jan 27, 2008 · N294UP · Doug MD11 · AileronsSDR UPS08M52148Intercostal · crackedINSPECTION TYPE:C CABIN AT STA 1215, ADJACENT LONGERON 27 RT TOP INTERCOSTAL STIFFENER FOUND CRACKED AT FWD EDGE. NEW INTERCOSTAL STIFFENER FABRICATED USING MATL 60-17778X7075T6511 PER EN1069-08. FPI C/OUT IAW BOEING DPS 4.707 REV.AW FOUND NO CRACK EVIDENT. Jan 25, 2008 · N294UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS08M52138Seat Track · corrodedINSPECTION TYPE:C CABIN-MAIN DECK SEAT TRACK AT BS 840-BS 859 X=+27.5 (LT) FOUND CORROSION AS MARKED. CORRODED SEAT TRACK FRAME EXISTING SECTION REMOVED PER SRM 51-33-01 V.2R.40. HFEC INSP C/OUT IAW DACNDTSPM R.13 PART06.10.01.001 FOUND NO CRACK EVIDENT. REJan 25, 2008 · N294UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52137Seat Track · corrodedINSPECTION TYPE:C CABIN, MAIN DECK SEAT TRACK AT BS 840-BS859 X=-7.5 (RT) FOUND CORROSION AS MARKED CORRODED SECTION TRIMMED OFF PER SRM 53-70-00 V.1FIG.R.40. HFEC INSP C/OUT IAW DAC NDTSPM 06-10-01.001R.13 FOUND NO CRACK EVIDENT. REPAIR SPLICES AND PLATES FJan 25, 2008 · N294UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M51972Spar · crackedINSPECTION TYPE:C LEFT WING FIXED WING FRONT SPAR ENCLOSURE APPROX STA XORS 506 UPPER SKIN FOUND CRACKED. CRACKED AREA TRIMMED OFF AS PER SRM 57-10-00 FIG.27V.1R.40. HFEC C/OUT IAW DA CNDTSPM R.13 PART 06-10-01.001, FOUND NO CRACK EVIDENT. REP ANGLES FAB USJan 25, 2008 · N294UP · Doug MD11F · Wing SparSDR UPS08M52108Fairing · damagedINSPECTION TYPE:C ENG NR 2 EXHAUST FAIRING RT SIDE WITH EXISTING PATCH REPAIR. FPI C/OUT ON EXISTING REPAIR IAW DACNDTSPM R.13 PART08 FOUND NO CRACK EVIDENT ON FAIRING SKIN & REPAIR DOUBLER. NEW REPAIR DOUBLER FAB USING 2219-0 0.071" PER EN 1123-08&MD11-54-2Jan 24, 2008 · N294UP · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR UPS08M52058Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER O/B BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT O/B BORE & SPOTFACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG 602-607R.60. FPI C/Jan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52057Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING HINGE MOUNTED SIDE ATTACHMENT UPPER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT UPR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57-44-08 PG 613-615R.6Jan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52056Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER I/B BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT I/B BORE & SPOT FACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG602-607R.60. FPI CJan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52054Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE SIDE ATTACHMENT LOWER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT LWR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57-44-08 PG 613-615R.6Jan 21, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52107Stringer · crackedINSPECTION TYPE:C LEFT WING UPPER STRINGER END S9 SUSPECT AS MARKED, THRU ACCESS 38AB. HFEC INSP C/OUT PER DACNDTSPM R.13 PART06.10.01.001&CRACK APPROX 12" FOUND. STR 9 CRACKED AREA TRIMMED OFF PER SRM 57-20-00 FIG 10V.1&EN1055-0 8. NEW STR & 03EA REP PARTSJan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52106Stringer · crackedINSPECTION TYPE:C LEFT WING UPPER STRINGER END S11 SUSPECT CRACK AS MARKED, THRU ACCESS 536AB. HFEC INSP C/OUT PER DACNDTSPM R.13 PART06-10.01.001 & CRACK APPROX 11" FOUND CRACK AT STR 11 LT WING TRIMMED OFF PER SRM 57-20-00 FIG 10V.1&EN1056-08 NEW STR 11 & 0Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52105Stringer · crackedINSPECTION TYPE:C RIGHT WING UPPER STRINGER END S-12 SUSPECT CRACK AS MARKED, THRU ACCESS 635BT. HFEC INSP C/OUT PER DAC NDTSPM R.13PART06.10.01.001 & CRACK APPROX 11" FOUND AS MARKED. CRACK AT STR 12 TRIMMED OFF PER SRM 57-20-00 FIG 10V.1 & EN1064-08. NEW Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52104Stringer · crackedINSPECTION TYPE:C RT WING UPPER STRINGER END NR S9 SUSPECT CRACK AS MARKED, THRU ACCESS NR 638AB. HFEC INSP CARRIED OUT PER DACNDT SPM R.13 PART06.10.01.001 AND CRACK APPROX 9 INCH FOUND AS MARKED. CRACK AT RHW STR NR 9 SLOTTED OUT PER SRM 57-20-00 FIG 10V.1Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52103Stringer · crackedINSPECTION TYPE:C RT WING UPPER STRINGER END NR S10 SUSPECT CRACK AS MARKED, THRU ACCESS NR 636CB. HFEC INSP CARRIED OUT PER DAC NDT SPM R.13 PART06.10.01.001 AND CRACK APPROX 11 INCHES FOUND AS MARKED. CRACK AT RHW STR NR 10 SLOTTED OUT PER SRM 57-20-00 FIGJan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52102Stringer · crackedINSPECTION TYPE:C LT WING UPPER STRINGER END NR S12 SUSPECT CRACK AS MARKED THRU ACCESS NR 535BT. HFEC INSP CARRIED OUT PER DAC NDT SPM R.13 PART 06.10.01.00 AND CRACK APPROX 7 INCHES FOUND. CRACK AT LHW STR NR 12 SLOTTED OUT PER SRM 57-20-00 FIG 10 V.1R.35.Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52101Stringer · crackedINSPECTION TYPE:C RT WING UPPER STRINGER END S11 SUSPECT CRACK AS MARKED THRU ACCESS NR 636AB. HFEC INSP C/OUT PER DAC NDTSPM R.13 PART06.10.01.001 AT UPPER STRINGER END NR S11 AND CRACK APPROX 9 INCH FOUND. CRACK AT RHW STR NR 11 SLOTTED PER SRM 57- 200-00 Jan 20, 2008 · N294UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52151Structure · bentINSPECTION TYPE:C EVALUATE CENTER CARGO DOOR C2 LOWER EDGE BENT BACK TO ORIGINAL CONTOUR PER DELTA ERA 36046-1-14. CORNER DOUBLER FAB FR MATL 7075-0-0.063" PER DWG ADA3774 AND REPAIR ANGLE FAB FR MATL 7075-0-0.080" PER EN1085-08. CORNER DOUBLER AND REPAIR ANJan 17, 2008 · N294UP · Doug MD11 · Cargo/Baggage DoorsSDR UPS08M52011Structure · damagedINSPECTION TYPE:C LT WING OUTBOARD FIXED L/E AT NR 8 SLAT 13 INCHES LONG GROOVE WORN FROM CONTACT WITH SEAL RETAINER, OUT OF LIMITS. GROOVE MARK REWORKED PER SRM 51-21-01V.2R35 ORIG THK:0.040", MAT`L REMVD :0.007", MATL REM:0.033" FOUND EXCEED LIMIT PER SRM 5Jan 15, 2008 · N294UP · Doug MD11 · Wing Main, Frame Structure
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