N134UP

Service difficulty reports · 355

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 = 'N134UP' 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 IPXA11166951Floor Support · bentINSPECTION TYPE:10YR, MAIN CABIN OVER WING FLOOR SUPPORT AT FRE 49 IS BENT BETWEEN -Y450 AND -Y953. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR SUPPORT AT FR 49 BETWEEN -Y450 AND -Y953 IAW EO A300-5310-42765-A AND STA-SA EA 300-5310-01-A3129, REV IR DATED 05/20/1May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA11166911Floor Support · bentINSPECTION TYPE:10YR, MAIN CABIN FLOOR SUPPORT AT FR 50 IS BENT BETWEEN -Y450 AND -Y953. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR SUPPORT AT FR 50 BETWEEEN -Y450 AND -Y953 IAW EO A300-5310-42765-A AND STA-SA EA 300-5310-01-A3129 REV I/R DATED 05/20/11.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA11166910Floor Support · bentINSPECTION TYPE:10YR MAIN CABIN FLOOR SUPPORT AT FR 48 TO FR 49 IS BENT BETWEEN -Y450 AND -Y950. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR SUPPORT AT FR 48 TO FR 49 -Y450 AND -Y950 IAW EO A300-5310-42765-A, STA-SA, EA 300-5310-01-A3129, REV I/R 05/20/11.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA11166899Floor Panel · crackedINSPECTION TYPE:10Y, MDCC FLOOR PANEL 241MN CRACKED. REPAIRED MDCC FLOOR PANEL 241MN IAW EO A300-5320-42721-A.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166894Floor Panel · crackedINSPECTION TYPE:10Y, FWD CARGO COMPARTMENT FLOOR PANEL 132SG CRACKED AND DELAMINATED. FABRICATED FLOOR PANEL 132SG IAW EO A300-5320-16407-E.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166888Floorboard · crackedINSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 131AH IS CRACKED AT LOWER SURFACE. FABRICATED FWD CARGO FLOORBOARD NR 131AH IAW EO A300-5320-16407-E.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166887Floorboard · puncturedINSPECTION TYPE:10YR, AFT CARGO COMPARTMENT FLOORBOARD NR 152VF IS PUNCTURED AT UPPER SURFACE. FABRICATED AFT CARGO FLOORBOARD NR 152VF IAW EO A300-5320-16407-E, APPENDIX C.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166883Floorboard · crackedINSPECTION TYPE:10YR MAIN CABIN FLOORBOARD NR 261DM IS CRACKED. FABRICATED MAIN CABIN FLOORBOARD NR 261DM IAW EO A300-5320-40552-A.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166868Floorboard · crackedINSPECTION TYPE:10YR, MAIN DECK COURIER COMPARTMENT FLOORBOARD, NR221VF UNDERSURFACE IS CRACKED. REPAIRED COURIER COMPARTMENT FLOORBOARD NR221VF IAW EO A300-5320-42721-A PARA 6A.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166827Floorboard · crackedINSPECTION TYPE:10YR MAIN CABIN FLOORBOARD NR 241YH IS CRACKED AT LOWER SURFACE. FABRICATED MAIN CABIN FLOORBOARD NR 241YH IAW EO A300-5320-40552-A, APPENDIX B.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166802Floor Panel · brokenINSPECTION TYPE:10YR, FLOOR PANEL 262GH IS BROKEN AT EDGE. FABRICATED NEW FLOOR PANEL 262GH IAW EO A300-5320-40552-A.May 11, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA11166889Floorboard · crackedINSPECTION TYPE:10YR, FWD CARGO FLOORBOARD NR 132MG IS CRACKED AT LOWER SURFACE. FABRICATED FWD CARGO FLOORBOARD NR 132MG IAW EO A300-5320-16407-E, APPENDIX C.May 10, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1164732Skin · gougedFUSELAGE GOUGE FR54.3 BETWEEN STR 40 AND 41 RT REPAIRED IAW EO A300-5330-32996-D.Feb 13, 2011 · N134UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA1164731Frame · gougedGOUGE TO FUSELAGE FRAME 42.5, STR 40 R. REPAIRED IAW EO A300-5330-32996-D.Feb 13, 2011 · N134UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA11166801Floor Panel · crackedINSPECTION TYPE:10YR, FLOOR PANEL 252LM IS CRACKED. FABRICATED NEW FLOOR PANEL 252LM IAW EO A300-5320-40552-A.Feb 12, 2011 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA0163593Light · inoperativeLAVATORY AUXILIARY LIGHT IS INOP. RELAMPED LAVATORY AUXILIARY LIGHT ASSY IAW AMM 33-24-00-00. OPS CHECK GOOD IAW AMM 33-51-00-05. OK FOR SERVICE.Nov 9, 2010 · N134UP · Airbus A300F4622R · Emergency LightingSDR IPXA10158445Skin · misrepairedINSPECTION TYPE:4/C, REPAIR SURVEY SEQ NR 134-F1-02 DOES NOT CORRELATE WITH ANY SRM REPAIR , REPAIR DOUBLER FR20A, STRG. 28 ON FWD LOWER CARGO DOOR CUTOUT. REPAIRED IAW EO NR A300-5330-36578-A AND EA300-5330-01-A2154, REV. IR.Jan 30, 2010 · N134UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA10158446Skin · gougedINSPECTION TYPE:4/C, REPAIR SURVEY SEQ. NR 134-W4-01, RT WING INBD FLAP UPPER SKIN REPAIR DOUBLER GOUGED. REPAIRED IAW EO NR A300-5750-36605-A AND EA NR300-5750-01-A2156 IR.Jan 29, 2010 · N134UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10158421Skin · gougedINSPECTION TYPE:4/C, REPAIR SURVEY SEQ NR 134-W4-02, RT WING CTR FLAP UPPER SKIN REPAIR DOUBLER GOUGED. REPAIRED IAW SRM 57-50-00, PARA. 4E, FIG. 205, PG. 217-220 RE F RCD 385657.Jan 29, 2010 · N134UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10158450Skin · chafedINSPECTION TYPE:4/C, LT WING INBD FLAP UPPER SKIN CHAFED. CTR OF FLAP APPROX 18 IN FWD OF RIB STRIP. REPAIRED IAW SRM 57-50-00, FIG. 205.Jan 28, 2010 · N134UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10158422Floor Panel · misrepairedINSPECTION TYPE:4/C, PREVIOUS DAMAGE REPAIR TO BULK CARGO FLOORBOARD 161JF 7IN. FWD OF REAR WALL RBL 14 NOT IAW SRM FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX. D.Jan 28, 2010 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158420Floor Panel · misrepairedINSPECTION TYPE:4/C, PREVIOUS DAMAGE REPAIR ON MCD RT FLOORPANEL 252XG NOT PER SRM, FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX.B.Jan 28, 2010 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158404Floor Panel · misrepairedINSPECTION TYPE:4/C, PREVIOUS DAMAGE REPAIR TO BULK CARGO FLOORBOARD 162HF 22" FWD OF REAR WALL SHELF RBL 35 NOT IAW SRM. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. D.Jan 28, 2010 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA10158393Floor Panel · damagedINSPECTION TYPE:4/C, PREVIOUS DAMAGE REPAIR TO BULK CARGO FLOORBOARD 161GF 46" FWS OF REAR WALL SHELF RBL 32 NOT IAW SRM. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX. D.Jan 28, 2010 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158392Floor Panel · damagedINSPECTION TYPE:4/C, PREVIOUS DAMAGE REPAIR TO BULK CARGO FLOORBOARD 161HF LT OTBD REPAIR NOT IAW SRM. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX. D.Jan 28, 2010 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09157922Control Unit · inoperativeDECELERATING THROUGH APPROXIMATELY 8 KNOTS GROUNDSPEED, WHILE MAINTAINING SIGNIFICANT PRESSURE ON THE BRAKE PEDALS, THE BRAKES RELEASED COMPLETELY AND SYMMETRICALLY. INCREASED PEDAL PRESSURE SIGNIFICANTLY, AND ACFT CAME TO A STOP. REMOVED AND REPLACED BRAKE Nov 11, 2009 · N134UP · Airbus A300F4622R · Landing Gear Brake SystemSDR IPXA09157917Jackscrew · unknownINSPECTION TYPE:AS-E ECAM WARNING MSG SLATS SYS 1&2 FAULT WITH ACCOMPANYING SLAT FAULT LIGHTS ON SYS 1&2 ILLUMINATED ON OVERHEAD PANEL SLATS RECYCLED AS PER PROCEDURE, NO CHANGE, FLAP ONLY LANDING ACCOMPLISHED. FOUND LT SLAT TORQUE LIMITER TRIPPED (TSM 27-80-Nov 10, 2009 · N134UP · Airbus A300F4622R · Leading Edge Slat Control SystemSDR IPXA10163073Warning Light · malfunctionedON TEST FOUND BUZZER WARNING LIGHT ON ENTRY DOOR INOP. UNABLE TO DUPLICATE, SYS TEST NORMAL IAW MM 52-73-00-05Oct 9, 2009 · N134UP · Airbus A300F4622R · Door Warning SystemSDR IPXA09157579Skin · damagedINSPECTION TYPE:N/A FUSELAGE SKIN DAMAGE P/N A53613402200 SKIN DAMAGED BETWEEN STR 31R & 33R AND BETWEEN FRAME 17R-18R APPROX 8 INCHES LONG 0.3 INCH WIDE. REPAIRED PER EO A300-5330-35159.Oct 6, 2009 · N134UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR UPS09154289Windshield · crackedINSPECTION TYPE:NA, F/O'S WINDSHIELD CRACKED BEYOND AMM LIMITS. ***SDR FILED OPEN***Jan 6, 2009 · N134UP · Airbus A300F4622R · Flight Compartment WindowsSDR UPS08153569Fire Loop · malfunctionedON CLIMBOUT MID, MAIN DET LOOP B FAULT ILLUMINATED ON ECAM. ALTITUDE WAS 10,500. LEVELED 11,000 FT AS CARGO SMOKE LAND ASAP ILLUMINATED ON ECAM. ACCOMPLISHED ECAM PROCEDURE WHILE RETURNING TO BIL. PERFORMED MAIN CARGO COMPARTMENT SMOKE DETECTION TEST PER MOct 10, 2008 · N134UP · Airbus A300F4622R · Smoke DetectionSDR UPS08151715Slide · unsecureFOUND L1 DOOR EMERGENCY EVACUATION SLIDE NOT SECURE IN SLIDE ASSY DOOR MOUNTS, DOOR REMOVED. DEFERRED MAIN CABIN SLIDE PER MEL 52-11-01-3 M-369937 ASSIGNED. INSTALLED NEW SLIDE PER MM 25-61-21-4.Feb 25, 2008 · N134UP · Airbus A300F4622R · Escape SlideSDR UPS07150062Floor Panel · damagedAS REPORTED BY UNLOAD CREW, HOLE IN THE FLOOR OF A/B SECTION, MARKED WITH A RED STICKY. HOLE 1.5" 34" FROM FWD OF BULK PIT, 4' IN FROM FWD DOOR FRAME. DEFERRED IAW SRM 53-10-20 FIG 110. PERMANENT REPAIR IN 359 FLIGHT HOURS.Jun 26, 2007 · N134UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS07148868Light · inoperativeEMERGENCY EXIT LIGHT DISARMED LIGHT IS NOT ON WITH THE SWITCH IN THE DISARMED POSITION. THE EMERGENCY EXIT LIGHTS ARE ON IN THE COCKPIT. CYCLED SWITCH ON, THEN TO DISARM. EMERGENCY EXIT LIGHTS SHUTOFF. EMERGENCY EXIT LIGHT SWITCH OPERATES AS REQUIRED. OK Jan 13, 2007 · N134UP · Airbus A300F4622R · Emergency LightingSDR UPS06147666Control Lever · inoperativeONE MINUTE AFTER T/O PER MEL, GEAR LEVER POS UP. LANDING GEAR DID NOT RETRACT. ECAM L/G RET FAULT COMPLIED WITH. L/G ATTEMPT AT 4000' 220 KIAS L/G DID NOT UNLOCK, THREE GREEN, DOORS OPEN. FOUND PDEU FAULTING CODE 03 AND 04. REMOVED AND REPLACED PDPU PER 3Aug 13, 2006 · N134UP · Airbus A300F4622R · Landing Gear SelectorSDR UPS06146861Rib · crackedINSPECTION TYPE:5YR LT WING KRUEGER FLAP AREA RIB 2 IS CRACKED/CHAFED THRU. FABRICATED AND INSTALLED REPAIR IAW UPS ENGINEERING FILE NUMBER A300-57-20019 AND SAA EA 300-5741-01-A0184.May 6, 2006 · N134UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR UPS06146848Floor Support · crackedINSPECTION TYPE:5YR MAIN CABIN FLOORBOARD BRACE CRACKED AT STA 49 RBL 40. REMOVED & REPLACED MAIN CABIN FLOORBOARD BRACE PER A300 SRM 51-40-00.Apr 29, 2006 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146869Intercostal · crackedINSPECTION TYPE:5YR RIGHT T/E AT NR 4 MOVEABLE FLAP TRACK FAIRING I/B & O/B INTERCOSTALS CRACKED. REMOVED & REPLACED INTERCOSTALS PER A300 SRM 51-40-00 & 51-40-21.Apr 28, 2006 · N134UP · Airbus A300F4622R · Trailing Edge FlapsSDR UPS06146859Rib · crackedFOUND LT WING KRUEGER FLAP WELL RIB CRACKED. REMOVED AND REPLACED RIB PER A300 SRM 51-40-21 AND 51-40-00.Apr 28, 2006 · N134UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR UPS06146870Bracket · crackedINSPECTION TYPE:5YR AFT CARGO FWD BULKHEAD LEFT I/B SUPPORT BRACKET CRACKED. REMOVED & REPLACED SUPPORT BRACKET PER A300 SRM 51-40-00 & 51-40-21.Apr 27, 2006 · N134UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR UPS06146849Shear Plate · crackedINSPECTION TYPE:5YR SHEAR PLATE CRACKED AT FR 79/80 RBL 60 IN MAIN DECK CARGO COMPARTMENT. REMOVED & REPLACED SHEAR PLATE PER A300 SRM 51-40-21.Apr 27, 2006 · N134UP · Airbus A300F4622R · Fuselage Main, StructureSDR UPS06146820Bracket · crackedFOUND AFT CARGO FWD BULKHEAD LT OTBD SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-00.Apr 27, 2006 · N134UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR UPS06146818Bracket · crackedFOUND AFT CARGO FWD BULKHEAD SUPPORT BRACKET CENTER CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-00.Apr 27, 2006 · N134UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR UPS06146817Shear Plate · crackedFOUND SHEAR PLATE CRACKED AT FS 79/80 LBL 60 IN MAIN DECK CARGO COMPARTMENT. REMOVED AND REPLACED SHEAR PLATE PER SRM 51-40-21.Apr 27, 2006 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146816Angle · crackedNR 2 ENG PYLON INBD MEMBER SECTION ANGLE AT RIB 18 IS CRACKED. REMOVED AND REPLACED NR 2 PYLON INBD MEMBER SECTION ANGLE PER SRM 51-40-21.Apr 27, 2006 · N134UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR UPS06146815Angle · crackedNR 2 ENG PYLON OTBD MEMBER SECTION ANGLE AT RIB 18 IS CRACKED. REMOVED AND REPLACED NR 2 PYLON OTBD MEMBER SECTION ANGLE PER SRM 51-40-21.Apr 27, 2006 · N134UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR UPS06146474Oxygen Mask · failed3RD JUMPSEAT POS 02 MASK FAILS LEAK CK. REPLACED 02 MASK ASSY AT 3RD JUMPSEAT POSITION AS PER A300 M/M 32-12 -51-4. OPS CHKS GOOD.Mar 21, 2006 · N134UP · Airbus A300F4622R · Passenger Oxygen SystemSDR UPS05145802Diaphragm · malfunctionedSLIDE ALMOST DEPLOYED. DEFERRED MAIN ENTRY DOOR PER MEL 52-11-01-3. M314029 PLACARD INSTALLED AS MAIN CABIN DOOR SLIDE INOP. REMOVED AND REPLACED FWD DOOR DAMPER PERCUSSION MECHANISM DIAPHRAM PER AMM 52-10-14-3. PLACARD REMOVED.Nov 16, 2005 · N134UP · Airbus A300F4622R · Emergency ExitsSDR UPS05145244Slide · deployedSLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED DOOR SLIDE PER MM 25-61-21. OPS CK OK.Aug 21, 2005 · N134UP · Airbus A300F4622R · Escape SlideSDR UPS05144126Regulator · inoperativeINSPECTION TYPE:N/A ALL FOUR 02 BOTTLES FOUND EMPTY ON WALKAROUND. REMOVED AND REPLACED NR 3, 02 BOTTLE PRESSURE REGULATOR IAW AMM 35-11-31-4, LEAK CHECKS GOOD.Mar 15, 2005 · N134UP · Airbus A300B4622R · Crew Oxygen System
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