N289UP
Service difficulty reports · 333
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 = 'N289UP' 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.
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 = 'N289UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS07M50747Structure · corrodedINSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LT 15 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM SURFACE REMN BLEND OUT DEPTH 0.050" DEEP. BORE REAMED TO 1.067" DIA, REMN BLEND OUT DEPTH 0.SDR UPS07M50745Structure · corrodedINSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LEFT NR 21 FOUND WITH CORROSION. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM SURFACE CLEANED. BORE REAMED TO 1.067" DIA & FOUND REMN BLEND OUT 0.037" DEEP, EXCSDR UPS07M50744Structure · corrodedINSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE LEFT NR 18 FOUND WITH CORROSION. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE THRU BOTTOM 0.0 60". BORE REAMED TO 1.067" DIA & REMN BLEND OUT 0.020" DEEP FOUND EXCEED SDR UPS07M50715Longeron · corrodedINSPECTION TYPE:C CENTER CARGO PIT ON L48 FOUND CORROSION STA 1531.0 AS MARKED. CORR LONGERON CUTOFF PER SRM 53-10-00 VI R38. HFEC INSP C/O PER DAC NDTSP M R13 PART06-10-01-001, NO CRACK FOUND. REPAIR LONGERON & SPLICE FAB SRM 53-10-00 VI R38 & EN1501-07. SDR UPS07M50675Longeron · corrodedINSPECTION TYPE:C CENTER CARGO AT STATION 1658 TO STATION 1786 (BILGE AREA) LONGERON 52 STRINGER FOUND CORRODED AS MARKED. ATTACH STA 1658-1879 LONG 52 SKIN FASTENERS & INNER AREA PARTS REMOVED PER SRM 51-31-01 VII R38. CORRODED LONG REMOVED PER SRM 53-10-00SDR UPS07M50748Structure · corrodedINSPECTION TYPE:C HORIZONTAL STAB CONSTANT SECTION BARREL NUT BORE RT NR 9 FOUND WITH CORROSION. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM REMN BLEND OUT 0.025" DEEP. BORE REAMED TO 0.988" DIA. REMN BLEND OUT 0.050" DEEP, EXCEEDSDR UPS07M50693Structure · corrodedINSPECTION TYPE:C HORZ STAB CONSTANT SECTION BARREL NUT BORE RIGHT NR 15 FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM SURFACE REMN BLEND OUT 0.065" DEEP. BORE REAMED TO 1.067 INCH DIA, REMN BLEND OUT 0.050 INCH DEEP, FOUND ESDR UPS07M50438Cable Guard · chafedINSPECTION TYPE:C LEFT WING - L/E PANEL NR 527AB U-BRACKET GUARD FOUND CHAFING AS MARKED. LEFT WING - L/E PANEL NR 527AB U-BRACKET GUARD CHAFE MARK REMOVED. ORG THK 0.0 63" MATL REMAIN 0.040" MATL REMOVED 0.023". FOUND EXCEED LIMIT SRM 51-00-01F IGAVIR38. SDR UPS07M50836Structure · corrodedINSPECTION TYPE:C HORIZONTAL STAB LEFT 01 BARREL NUT BORE FOUND CORRODED. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM REMN BLEND OUT 0.030" DEEP & BORE REAMED TO 1.549" DIA, REMN BLEND OUT 0.050" DEEP, EXCEED LIMIT. BARREL NUT BORESDR UPS07M50746Structure · corrodedINSPECTION TYPE:C HORIZONTAL STAB RIGHT NR 36 BARREL NUT BORE FOUND CORRODED. CORR AT BARREL NUT BORE REMOVED PER SRM 51-21-01 VII R38. BORE BOTTOM REMN BLEND OUT 0.160" DEEP & BORE REAMED TO 2.572" DIA, BOTTOM MACHINED DOWN 0.070" DEEP. BARREL NUT BORE, BLSDR UPS07M50349Structure · crackedINSPECTION TYPE:C RIGHT WING - WING T/E INBOARD ISLANDS UPPER SURFACE FOUND CRACK ON FWD SIDE APPROX AT XORS 444 AS MARKED. HFEC INSP C/O DAC NDTSPM R13P6 06-10-01.001 & 05 EA CRACKS END CON- FIRMED. FASTENERS AT AFFECTED AREA REMOVED FOR ACCESS SRM 51-31-01SDR UPS07M50447Skin · crackedINSPECTION TYPE:C RIGHT WING L/E CORRUGATED SKIN FOUND CRACKED AT 04 EA PLACES AROUND RIVETS AT 14 INCHES O/B OF REFUEL PANEL I/B EDGE AS MARKED. CRACKED AREA TRIM OUT PER SRM TEMP REV 57-10-00 FIG 25B R38. HFEC INSP C/O PER DAC NDT SPM REV13 PART6 06-10-01.SDR UPS07M50439Cable Guard · chafedINSPECTION TYPE:C RIGHT WING - L/E PANEL NR 627AB CABLE GUARD U-CHANNEL FOUND CHAFED AS MARKED. RIGHT WING - L/E PANEL NR 627AB CABLE GUARD U-CHANNEL CHAFE MARK REMOVED. ORG THK 0.063" MATL REMAIN 0.033" MATL REMOVED 0.030". FOUND EXCEED LIMIT SRM 57-00-01 SDR UPS07M50467Rib · crackedINSPECTION TYPE:C RIGHT WING FIXED WING L/E INTERIOR AREA APPROX STA XOS 667 FOUND RIB CRACKED. CRACKED RIB REMOVED (REF C/N: MD072549, STEP FOR WORK DETAILS). NEW RIB FAB PER DWG ARB2930-20. RIB HEAT - TREATED PER DPS 7.00-1 & HARDNESS VALUE HRB 81.7 PER DSDR UPS07M50815Hinge · corrodedINSPECTION TYPE:C LEFT O/B FLAP I/B HINGE (FLAP MOUNTED) PIVOT LUG I/B BORE & SPOT FACES FOUND CORROSION AS MARKED. CORROSION REMVD FROM AFFECTED AREAS & FOUND EXCEED LIMITS PER CMM57-52-0 4 PG 621-622 R58. ORG DIA 1.139" THK 0.497" FINAL DIA 1.189" THK 0.49SDR UPS07M50562Hinge · corrodedINSPECTION TYPE:C RT O/B FLAP I/B HINGE (WING MOUNTED) LOWER ATTACHMENT LUG I/B FOUND BORE AND SPOT FACES CORROSION AS MARKED. BORE AND SPOTFACE CORROSION REMOVED, EXCEED LIMIT CMM 57-44-08 PG 602-607 R58 ORG DIA 0.644" THK 0.460" FINAL DIA 0.707" THK 0.441" SDR UPS07M50561Hinge · corrodedINSPECTION TYPE:C RT O/B FLAP I/B HINGE (WING MOUNTED) LOWER ATTACHMENT LUG O/B FOUND BORE AND SPOT FACES CORROSION AS MARKED. BORE AND SPOTFACE CORROSION REMOVED, EXCEED LIMIT CMM 57-44-08 PG 602-607 R58. ORG DIA 0.644" THK 0.461" FINAL DIA 0.706" THK 0.435"SDR UPS07M50387Shear Web · corrodedINSPECTION TYPE:C CABIN - CORROSION ON UPPER & LWR SURFACE OF SHEAR WEB AT STA 1966 - 1976 L27 LT. UPPER & LWR SURFACE OF SHEAR WEB CORROSION REMOVED MAT'L ORG THK 0.040" REMV 0.018" REMAIN 0.022" FOUND EXCEED LIMIT PER SRM 53-00-01VI FIG 1A R38. CORROSION SSDR UPS07M50386Shear Web · corrodedINSPECTION TYPE:C CABIN - CORROSION ON UPPER & LWR SURFACE OF SHEAR WEB AT STA 1966 - 1996 L27 RT. SHEAR WEB CORROSION REMOVED PER SRM 53-00-01VI FIG 1AR38. WEB ORG THK 0.040" REMV 0.012" REMAIN 0.028" FOUND EXCEED LIMIT. NEW SHEAR WEB AGA7145-5 AND AGA71SDR UPS07M50863Skin · crackedINSPECTION TYPE:C RIGHT WING L/E LOWER ACCESS AT SLAT TRACK NR 10 TO 21 INCHES I/B, FOUND L/E UPPER CORRUGATED SKIN CRACKED AT 3EA PLACES AS MARKED. HFEC INSP C/O ON CRACK AREA & CRACK END MARKED OUT APPROX. 0.25". FASTENERS AT CRACK AREA REMOVED & CRACK ARESDR UPS07M50449Skin · crackedINSPECTION TYPE:C RIGHT WING L/E LOWER ACCESS WELL AREA FOUND CRACKED 6 INCHES LONG ON UPPER SKIN REINFORCED STRAP AT 6 INCHES O/B OF SLAT TRACK NR 10 AS MARKED. CRACKED STRAP AT AFFECTED AREA REMOVED PER SRM 51-31-01 VII R38. NEW STRAP FAB PER DWG ARB3954-6SDR UPS07M50448Skin · crackedINSPECTION TYPE:C RIGHT WING L/E LOWER ACCESS WELL AREA FOUND CRACKED 5 INCHES LONG ON UPPER SKIN REINFORCED STRAP AT 13 INCHES O/B OF SLAT TRACK NR 12 AS MARKED. CRACKED REINFORCED STRAP AT AFFECTED AREA (APPROX XOS 789), REMOVED PER SRM 51-31-01 VII R38. NSDR UPS07M50355Skin · canningINSPECTION TYPE:C LEFT I/B FLAP UPPER SURFACE FOUND OIL CANNING AT 4.75 INCHES FROM O/B END AND 33.75 INCHES FROM T/E AS MARKED. DAMAGES / AFFECTED AREA TRIM OUT SRM 57-10-00 FIG 34 VI R38. REWORKED AREA REPROTECTED SRM 51-21-01VII R38. HFEC INSP C/O NDTSPMSDR UPS07M50354Skin · dentedINSPECTION TYPE:C LEFT I/B FLAP LOWER SURFACE FOUND WITH SEVERAL SMALL DENTS AT 63 INCHES FROM O/B END AS MARKED. LEFT WING I/B FLAP LWR O/B SEGMENT LWR SKIN REMOVED PER SRM 51-35-01VII R38. NEW SKIN FAB PER BOEING DWG ARC2443, USE MATL 2024T3-0.040". HOLESSDR UPS07M50353Skin · dentedINSPECTION TYPE:C LEFT I/B FLAP LOWER SURFACE FOUND WITH SEVERAL DENTS AT 64 INCHES FROM I/B END AS MARKED. LEFT WING I/B FLAP LOWER I/B SEGMENT LOWER SKIN REMOVED SRM 51-35-01VII R38. NEW SKIN FAB BOEING DWG ARC2736, USE MATL 2024T3-0.040". HOLES PICK UP PSDR UPS07M50440Seat Track · corrodedINSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK AT STA 1966 X=107. AFFECTED AREA CORROSION REMOVED & REPROTECTED SRM 51-21-01VII R38. CROWN AREA ORG THK 0.145" MATL REMAIN 0.045" MATL REMV 0.100". FLANGE AREA ORG THK 0.080" MATL REMAIN 0.048" MATL REMV 0.SDR UPS07M50348Structure · crackedINSPECTION TYPE:C RIGHT WING - WING T/E INBOARD ISLANDS UPPER SURFACE FOUND CRACK ON FWD SIDE APPROX AT XORS 455 AS MARKED. HFEC INSP C/O DAC NDTSPM REV13 06-10-01.001 & FOUND CRACK OF .375 INCH. FASTENERS AT AFFECTED AREA REMOVED FOR ACCESS SRM 51-31-01VII SDR UPS07M50729Seat Track · corrodedINSPECTION TYPE:C CORROSION ON SEAT TRACK CROWN, CHANNEL & FLANGE FROM STA 839-939 X=-75. CABIN SEAT TRACK X=-75, STA 839-939, CROWN CHANNEL & FLANGE AREA CORR RMVD & AREA REPROTECTED SRM 51-21-01 VII R38. FLANGE ORG THK 0.080" MAT'L REMND 0.042". MATL RMVSDR UPS07M50719Skin · damagedINSPECTION TYPE:C FUSELAGE SKIN AROUND FORWARD CARGO DOOR OPENING AT LOWER AFT CORNER HAS DAMAGE (MATERIAL MISSING). DAMAGED AREA TRIMMED OFF PER EN 1486-07. HFEC INSP C/O AS PER DAC NDTSPM R13 06-10-01.001 ON TRIMMED OFF AREA & FOUND NO CRACK. REPAIR INNERSDR UPS07M50718Cover · crackedINSPECTION TYPE:C TAIL PYLON COVER BEHIND THE EXHAUST NOZZLE CRACKED (6 INCHES), STOPPED DRILLED, NUMEROUS RIVETS PULLED THRU IN LT AND RT SIDE, NEEDS REPLACEMENT. FPI C/O PER DAC NDTSPM R13 PT8 & MARKED OUT CRACK END. CRACK END STOP DRILLED PER EN 1438-07. SDR UPS07M50648Trunnion · crackedINSPECTION TYPE:C NLG WHEEL WELL, NLG LEFT TRUNNION FITTING FOUND CRACK WITH STOP DRILL. NLG W/W LEFT TRUNNION FITTING CRACK WITH STOP DRILL AREA TRIM OUT PER SRM 53-40-00 FIG 23 VI R40. HFEC INSPECT C/O DAC NDTSPM R13 PART06-10-01-0 1 ON TRIM OUT AREA FOUNDSDR UPS07M50629Skin · gougedINSPECTION TYPE:C RIGHT WING IN THE AREA OF THE LAST SLAT, HAS DEEP GOUGES, HARD CONTACT WITH OUTER/LAST SLAT. AFFECTED AREA DEEP GOUGES REMOVED & SMOOTHED. ORG THK 0.060" MATL REMAINN 0.024" MATL REMOVED 0.036" FOUND EXCEED LIMIT SRM 57-00-01 FIG 3 VI R38. SDR UPS07M50199Seat Track · corrodedINSPECTION TYPE:C CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 815-865 X=-8. CABIN SEAT TRACK X=-8 STA 815-865 CORROSION REMOVED & REPROTECTED SRM 512101VIIR38 . CHNNL ORG THK 0.100" MATL REMN 0.075" MATL REMV 0.025". EXCEEDS LIMIT. CORRODED SEAT TRACK CUTO
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