N153UP

Service difficulty reports · 237

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 = 'N153UP' 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 IPXA3178568Seat Track · corrodedINSPECTION TYPE:10YR, SEAT TRACK BET FR79 AND FR80/82 AT -Y794.3 IS CORRODED. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.May 13, 2013 · N153UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA3178567Seat Track · corrodedINSPECTION TYPE:10YR, SEAT TRACK BETWEEN FR79 AND FR80/82 AT -Y450 IS CORRODED. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.May 13, 2013 · N153UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA3178566Seat Track · corrodedINSPECTION TYPE:10YR, SEAT TRACK BETWEEN FR79 AND 80/82 AT Y0 IS CORRODED. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201, REV 23.May 13, 2013 · N153UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA13178710Skin · chafedINSPECTION TYPE:10YR, RT OTBD FLAP BULLNOSE SKIN IS CHAFED BETWEEN RIB 1 AND 3. ACCOMPLISHED REPAIR ON RT OTBD FLAP BULLNOSE SKIN BETWEEN RIB 1 AND RIB 3 IAW EO A300-5750-50830-A, PARA 6A.May 11, 2013 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA3178843Skin · chafedINSPECTION TYPE:10YR, RT INBD FLAP UPPER SKIN IS CHAFED BETWEEN RIB 11 AND 12 STGR 2.1 TO 2.4. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN IAW EO A300-5750-51067-A.May 10, 2013 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA3178831Skin · gougedINSPECTION TYPE:10YR, RT INBD FLAP UPPER SKIN IS GOUGED BETWEEN RIB 5 AND 7 STGR 2.2 AND STGR 2.3. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN IAW EO A300-5750-50868-A, PARA 6A.May 10, 2013 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA3178748Skin · chafedINSPECTION TYPE:10YR, RT MID FLAP UPPER SURFACE IS CHAFED BETWEEN RIB 20 AND 21 STGR 2.6 AND STGR 2.7. REPAIRED RT CENTER FLAP UPPER SKIN BETWEEN RIB 20 AND 21 STGR 2.6 AND STGR 2.7 IAW SRM 57-50-00, PARA 4E, FIG 205 AND EO A300-5750-35931-C, APPENDIX A.May 10, 2013 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2174088Floor Panel · damagedMAIN CARGO DECK POS 9R/10R OTBD FLOOR PANEL DAMAGED. REPAIRED IAW EO B757-5320-42721-B & SRM 53-10-20.Jun 25, 2012 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1165867Floor Panel · damagedR & R BULK CARGO FLOOR PANEL 161GF IAW WAN 1740685. FABRICATED NEW BULK CARGO FLOOR PANEL 161GF IAW EO A300-5320-16407-E, APPENDIX A/D.Apr 4, 2011 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1164916Slat System · inoperativeSLATS 1/2 ON APPROACH. CYCLED HANDLE. FLAPS 40 SLATS STAYED AT 0. EMERGENCY DECLARED NRC336455, SUPPLEMENTAL SDR. C/W ALERT T149038 AND WAN 1726288. ACCOMPLISH BOW TS2560/998. PERFORM SFCC BITE CHECK IAW AMM 27-51-05. BITE TEST GOOD.Feb 23, 2011 · N153UP · Airbus A300F4622R · Leading Edge Slat Control SystemSDR IPXA11164916Flap System · malfunctionedSLATS 1/2 ON APPROACH. CYCLED HANDLE. FLAPS 40 SLATS STAYED AT 0. EMERGENCY DECLARED.Feb 23, 2011 · N153UP · Airbus A300F4622R · Trailing Edge Flap Control SystemSDR IPXA1164700Floor Panel · damagedINSPECTION TYPE:3C, CABIN COMPARTMENT FLOOR PANEL 241QN 1EA SCREW MOUNTING HOLE ENLONGATED. FABRICATED MAIN DECK COMPARTMENT FLOOR PANEL 241QN REF A300-5320-16407-E, APPROX A AND C.Jan 31, 2011 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1164723Skin · misrepairedINSPECTION TYPE:3C,, REPAIR DOES NOT CORRELATE TO SRM. LT WING CENTER FLAP, RIB 15 TO 17, STGR1.1 TO 1.2. ENLARGED SKIN CUT OUT, FABRICATED AND INSTALLED REPLACEMENT REPAIR AT LT WING CTR FLAP NOSE SKIN BETWEEN RIB 15 TO 17 AND STGR 1.1 TO 1.2 REF STA, SA, EAJan 29, 2011 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA1164722Structure · gougedINSPECTION TYPE:3C, RT WING OTBD FLAP INBD BULLNOSE IS GOUGED. REMOVED RT WING OTBD FLAP INBD BULLNOSE REPAIR. CUT-OUT DAMAGED AREA AND FABRICATED & INSTALLED REPLACEMENT REPAIR REF SRM 57-50-00, PAGE BLOCK 201, PARA 4H, FIG 208.Jan 29, 2011 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA1164721Structure · gougedINSPECTION TYPE:3C, LT WING OTBD FLAP L/E BULLNOSE HAS GOUGE. CUT OUT DAMAGE ON LT WING OTBD FLAP L/E INBD BULLNOSE AND FABRICATED REPAIR REF STA, SA, EA 300-5750-01-A2884 AND EO A300-5750-41 388-A.Jan 29, 2011 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA1164702Floor Panel · damagedINSPECTION TYPE:3C, REPAIR RECORD VALIDATION SURVEY, REPAIR OF MAIN CARGO COMPARTMENT RT FLOORBOARD NR262DM BOTTOM SIDE AT TIE-DOWN CUT OUT. FABRICATED MAIN DECK COMPARTMENT FLOOR PANEL NR262DM REF A300-5320-16407-E, APPX A/B.Jan 27, 2011 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159073Jackscrew · bindingDIVERSION - FLAP 1 AND 2 SYS FAULT. FLAPS STUCK AT 20 ON T/O. AT 3500 FT CYCLED FLAPS IAW ECAM NO HELP. ESTIMATED FLAP OVERSPEED OF 10 KNOTS DURING LEVEL OFF ESTIMATED DURATION OF OVERSPEED 5 SEC. FOUND NR 5 JACKSCREW SUPPORT ASSY BINDING. R & R NR 5 JACKSCApr 1, 2010 · N153UP · Airbus A300F4622R · Trailing Edge Flap Control SystemSDR UPS08153043Floor Panel · puncturedINSPECTION TYPE:5 YR, MAIN CARGO COMPT FLOOR PNL APPROX FR26 IN AFT CABIN HAS PUNCTURE. REPAIRED MAIN CABIN FLOOR PNL, NR 252WJ REF SRM 53-10-20 TABLE 201 PARA 8A.Aug 5, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152980Floor Panel · crackedINSPECTION TYPE:5 YR, MAIN CABIN FLOOR PNL NR 262BM IS CRACKED ON THE AFT END. REPAIRED MAIN CABIN FLOOR PNL NR 262BM IAW SRM 53-10-20 TABLE 201 PARA 8A.Jul 24, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08153051Floor Panel · delaminatedINSPECTION TYPE-5YR, MAIN CARGO COMPT FLOOR PNL 231GH AT FR27 LT SIDE, FOUND DELAMINATED. REPAIRED MAIN CARGO COMPT FLOOR PNL 231GH AT FR27 LT SIDE REF SRM 53-10-20 TABLE 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152982Floor Panel · delaminatedINSPECTION TYPE:5 YR, MAIN CARGO COMPT FLOOR PNL NR 231QJ AT FR 26 LT SIDE FOUND DELAMINATED. REPAIRED MAIN CABIN FLOOR PNL NR 231QJ AT FR 26 LT SIDE IAW A300-600 SRM 53-10-20 TABLE 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152979Floor Panel · crackedINSPECTION TYPE-5, YR MAIN CARGO COMPT RT FLOORBOARD NR 262DM CRACKED BOTTOM SIDE AT TIE- DOWN CUT OUT. REPAIRED MAIN CABIN FLOORBOARD NR 262DM IAW SRM 53-10-20 FIG 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152977Floor Panel · brokenINSPECTION TYPE:5 YR, MAIN CABIN COMPT, FLOOR PANEL 252BN AT FR. 72 FOUND BROKEN. REPAIRED MAIN CABIN FLOOR PANEL 252BN AT FR 72 IAW SRM 53- 10-20 FIG 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152909Floorboard · crackedINSPECTION TYPE-5 YR MAIN CARGO COMPARTMENT FLOORBOARD NR 242UK CRACKED AT TOP SURFACE AND BOTTOM T/E AT FR. 38.2. REPAIRED MAIN CARGO COMPARTMENT FLOORBOARD NR 242UK AT FR.38.2 REF. A-300-600 SRM 53-10-20 TABLE 201 PARA 8A.Jul 23, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152981Floor Panel · crackedINSPECTION TYPE:5 YR, MAIN CABIN FLOOR PNL NR 231SG IS CRACKED AT THE FWD END. REPAIRED MAIN CABIN FLOOR PNL NR 231SG IAW SRM 53-10-20 TABLE 201 PARA 8A.Jul 22, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152978Floor Panel · crackedINSPECTION TYPE: 5 YR, MAIN CABIN FLOOR PANEL NR 252BN IS CRACKED AT FWD END. REPAIRED MAIN CABIN FLOOR PANEL NR 252BN FWD CRACK IAW SRM 53- 10-20 FIG 201 PARA 8.Jul 22, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152975Skin · chafedINSPECTION TYPE:5 YR, RT WING OB FLAP L/E IB CHAFED. REPAIRED RT WING OB FLAP L/E IB SIDE REF A-300-600 SRM 57-50-0 0 FIG 208.Jul 22, 2008 · N153UP · Airbus A300F4622R · Trailing Edge FlapsSDR UPS08152913Shear Plate · crackedINSPECTION TYPE:5 YR MAIN CARGO COMPARTMENT LT FR 79 FLOOR LEVEL SHEAR PLATE CRACKED FWD OF AFT PRESSURE BULKHEAD. REPLACED MAIN CARGO COMPARTMENT LT FR 79 FLOOR LEVEL SHEAR PLATE REF. A-300-600 SRM 51-40-21.Jul 22, 2008 · N153UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR UPS08152908Shear Plate · crackedINSPECTION TYPE-5 YR, MAIN CARGO COMPARTMENT RT FR 79 FLOOR LEVEL SHEAR PLATE CRACKED FWD OF AFT PRESSURE BULKHEAD. REPLACED RT FR79 FLOOR LEVEL SHEAR PLATE REF. A300-600 SRM 51-40-21.Jul 22, 2008 · N153UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS08152907Floor Panel · crackedINSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL Z261BH IS CRACKED. REPAIRED MAIN CABIN FLOOR PANEL Z261BH REF. A-300-600 SRM 53-10-20 TABLE 201 PARA 8A.Jul 22, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152906Floor Panel · gougedINSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL NR Z251XJ HAS SEVERAL GOUGES. REPAIRED CABIN FLOOR PANEL NR Z251XJ REF. A-300-600 SRM 53-10-20 TABLE 2 01 PARA. 8A.Jul 22, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08152905Floorboard · gougedINSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL NR Z251BN HAS SEVERAL GOUGES. REPAIRED MAIN CABIN FLOORBOARD NR Z251BN REF. A-300-600 SRM 53-10-20 TABLE 201 PARA. 8A.Jul 22, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08153044Floor Panel · damagedINSPECTION TYPE:5 YR, MAIN CARGO DECK POS P4R, FLOOR INTERIM REPAIR. REPAIRED MAIN CABIN FLOOR PNL NR 241LH REF SRM 53-10-20, TABLE 201, PARA 8A.Jul 17, 2008 · N153UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS06147943Switch · defectiveEMERGENCY EXIT LIGHTS DO NOT DISARM WHILE IN DISARM POSITION. ITEM DEFERRED IAW MEL 33-51-02; D332943. REMOVED AND REPLACED EMERGENCY EXIT LIGHT DISARM SWITCH IAW ESPM 20-45-21; TESTED ALL SWITCHES ON PANEL, FOUND SATIS. THIS CLOSES DEF D332943. S/N OFF N/Sep 6, 2006 · N153UP · Airbus A300F4622R · Emergency LightingSDR UPS06146940Water Separator · odorAT HIGH POWER SETTING ON TAKEOFF AND LANDING A HOT INSULATION SMELL CAME THROUGH THE AIR CONDITIONING SYSTEM AT HIGH ALTITUDE. EVERYTHING WAS FINE. ALL INSTRUMENTS WERE NORMAL. REPLACED LEFT AND RIGHT WATER SEPARATOR COALESCERS PER MM 21-51-16. RAN LEFT ANMay 23, 2006 · N153UP · Airbus A300F4622R · Humidity Control SystemSDR UPS06146768Lamp · inoperativeENTRY DOOR EXIT LIGHTS INOP, ALL BULBS. RELAMPED OPS CKS OK.Apr 30, 2006 · N153UP · Airbus A300F4622R · Emergency LightingSDR UPS05143870Slide · reads lowEMERGENCY ESCAPE SLIDE PRESSURE SHOWS IN THE RED M296931 ASSIGNED. INSPECTED L1 ESCAPE SLIDE AND FOUND PRESSURE WITHIN LIMITS PER MM 25-61-21-4 OK FOR SVD, PLACARD REMOVED.Feb 10, 2005 · N153UP · Airbus A300F4622R · Escape Slide
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