N164UP

Service difficulty reports · 137

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 = 'N164UP' 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 IPXA2019092047018Fitting · crackedINSPECTION TYPE:12YR LT WING FR 40 FITTING FASTENER HOLE IS CRACKED AT 7 O'CLOCK POS APPROX 0.250" IN LENGTH, DEPTH GREATER THAN .020". REPAIRED CRACKED LT WING FR 40 FITTING FASTENER HOLE IAW EO A300-5710-64579-C APPENDIX D. (MINOR)Aug 28, 2019 · N164UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2019091846968Seat Track · corrodedINSPECTION TYPE:12YR MAIN CABIN SEAT TRACK HAS CORROSION AT Y=0 FR 80/82. REPAIRED CORRODED MAIN CABIN SEAT TRACK AT Y=0 & FR 80/82 IAW SRM 53-10-16 PAR 4, FIG 201B. (MAJOR)Aug 28, 2019 · N164UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2019091146633Shear Plate · crackedINSPECTION TYPE:12YR MAIN CABIN SHEAR PLATE IS CRACKED AT RT FR 79 FLOOR LEVEL. REMOVED AND REPLACED CRACKED MAIN CABIN SHEAR PLATE AT RT FR 79 FLOOR LEVEL IAW SRM 51-40-21. (MINOR)Aug 28, 2019 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019091146632Support Bracket · crackedINSPECTION TYPE:12YR AFT CARGO FWD BULKHEAD UPPER VERTICAL WALL SUPPORT BRACKET IS CRACKED AT FR 54 APPROX LBL 28. REMOVED AND REPLACED CRACKED AFT CARGO FWD BULKHEAD UPPER VERTICAL WALL SUPPORT BRACKET AT FR 54 APPROX LBL 28 IAW SRM 51-40-21. (MINOR)Aug 28, 2019 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019091146631Intercostal · crackedINSPECTION TYPE:12YR FWD CARGO INTERCOSTAL WEB IS CRACKED BELOW FLOOR AT FR 21 LT SIDE.REMOVED AND REPLACED CRACKED FWD CARGO INTERCOSTAL WEB BELOW FLOOR AT LT FR 21 IAW SRM 51-40-21. (MINOR)Aug 28, 2019 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019091146630Shear Web · crackedINSPECTION TYPE:12YR MAIN CABIN RH SHEAR WEB BETWEEN FR 76 & 77 IS CRACKED AT FLOOR LEVEL. REMOVED AND REPLACED CRACKED MAIN CABIN SHEAR WEB AT FLOOR LEVEL BETWEEN FR 76 & 77 IAW SRM 51-40-21. (MINOR)Aug 27, 2019 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2019090646416Floor Panel · brokenINSPECTION TYPE:12Y FWD LOWER CARGO FLOOR PANEL #132QG IS BROKEN. REMOVED, FABRICATED AND REPLACED FLOOR PANEL #132QG IAW EO A300-5320-16407-E APPX. C. (MAJOR)Aug 27, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019090646415Floor Panel · brokenINSPECTION TYPE:12Y FWD LOWER FLOOR PANEL #131MG IS BROKEN. REMOVED, FABRICATED AND REPLACED FLOOR PANEL #131MG IAW EO A300-5320-16407-E APPX. C. (MAJOR)Aug 27, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019091846953Stiffener · crackedINSPECTION TYPE:12YR #1 PYLON AFT DRAIN LINE COVER FAIRING HAS O/B PLATE (STIFFENER) CRACKED. REPAIRED CRACKED #1 PYLON AFT DRAIN LINE COVER FAIRING O/B PLATE (STIFFENER) IAW EA 300-5451-01-A7887 REV IR AND EO A300-5450-73859-A. (MINOR)Aug 26, 2019 · N164UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2019091146635Web · crackedINSPECTION TYPE:12YR #1 PYLON PRECOOLER LOUVER PANEL 413BL WEB IS CRACKED IN 2 PLACES AT CORNERS OF SEAL RETAINER. REPAIRED CRACKED #1 PYLON PRECOOLER LOUVER PANEL 413BL WEB AT CORNERS OF SEAL RETAINER IAW SRM 54-52-51 FIG 204. (MINOR)Aug 26, 2019 · N164UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2019091146628Plate · crackedINSPECTION TYPE:12YR #1 PYLON O/B FISH PLATE IS CRACKED. REMOVED AND REPLACED CRACKED #1 PYLON O/B FISH PLATE IAW SRM 51-40-21. (MINOR)Aug 26, 2019 · N164UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2019091146626Plate · crackedINSPECTION TYPE:12YR #1 PYLON I/B FISH PLATE IS CRACKED. REMOVED AND REPLACED CRACKED #1 PYLON I/B FISH PLATE IAW SRM 51-40-21. (MINOR)Aug 26, 2019 · N164UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2019091146625Web · crackedINSPECTION TYPE:12YR #1 PYLON RIB 8A WEB IS CRACKED AT TOP RT SIDE AFT OF PRECOOLER. REPAIRED CRACKED #1 PYLON RIB 8A WEB AT TOP RT SIDE AFT OF PRECOOLER IAW EO A300-5450-51643-A APPENDIX B. (MINOR)Aug 26, 2019 · N164UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2019091146623Web · crackedINSPECTION TYPE:12YR #1 PYLON AFT LOWER WEB IS CRACKED AT DRAIN LINE BULKHEAD FITTING. REMOVED AND REPLACED CRACKED #1 PYLON AFT LOWER WEB AT DRAIN LINE BULKHEAD FITTING IAW SRM 51-40-21. (MINOR)Aug 26, 2019 · N164UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2019090446333Floor Panel · brokenINSPECTION TYPE:12YR MAIN CARGO COMPARTMENT FLOOR PANEL 232BH HAS PIECES BROKEN OUT. FABRICATED REPLACEMENT DAMAGED MAIN CARGO COMPARTMENT FLOOR PANEL 232BH IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)Aug 26, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2019091146634Rib · wornINSPECTION TYPE:12YR LT WING FIXED T/E VERTICAL STIFFENER RIB IS WORN AT O/B FWD END OF SHROUD PANEL 572LB. REMOVED AND REPLACED WORN LT WING FIXED T/E VERTICAL STIFFENER RIB AT O/B FWD END OF SHROUD PANEL 572LB IAW SRM 51-40-21. (MINOR)Aug 25, 2019 · N164UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2019092147031Skin · chafedINSPECTION TYPE:12YR LT WING #1 SLAT LOWER T/E SKIN IS CHAFED ABOVE PYLON. REPAIRED CHAFED LT WING #1 SLAT LOWER T/E SKIN 24" FROM O/B END ABOVE PYLON IAW EA 300-5750-01-A7886 REV IR AND EO A300-5750-73995-A. (MAJOR)Aug 23, 2019 · N164UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2019091446741Shroud · gougedINSPECTION TYPE:12YR RT WING O/B FIXED L/E SHROUD IS GOUGED. REMOVED AND REPLACED GOUGED RT WING O/B FIXED L/E SHROUD IAW SRM 51-40-21. (MINOR)Aug 23, 2019 · N164UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2019091446753Angle · crackedINSPECTION TYPE:12YR LT WING FIXED L/E RIB HAS A ROW OF LOOSE/MISSING RIVETS AND ANGLE IS CRACKED O/B OF KRUEGER FLAP. REMOVED AND REPLACED CRACKED LT WING FIXED L/E RIB ANGLE AND LOOSE/MISSING RIVETS O/B OF KRUEGER FLAP IAW SRM 51-40-21. (MINOR)Aug 23, 2019 · N164UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2019091446752Angle · crackedINSPECTION TYPE:12YR LT WING FIXED L/E "L" BRACKET (ANGLE) IS CRACKED O/B OF KRUEGER FLAP. REMOVED AND REPLACED CRACKED LT WING FIXED L/E "L" BRACKET (ANGLE) O/B OF KRUEDER FLAP IAW SRM 51-40-21. (MINOR)Aug 23, 2019 · N164UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2019091846952Hinge Fitting · chafedINSPECTION TYPE:12YR #2 ENGINE RT FAN COWL AFT HINGE FITTING IS CHAFED. REPAIRED CHAFED #2 ENGINE RT FAN COWL AFT HINGE FITTING IAW EA 300-7110-01-A7891 REV IR AND EO A300-7110-73917-A. (MINOR) LP 181477/2.Aug 22, 2019 · N164UP · Airbus A300F4622R · Engine Cowling SystemSDR IPXA2019091446751Hinge Fitting · chafedINSPECTION TYPE:12YR #1 ENGINE I/B FAN COWL AFT HINGE FITTING IS CHAFED. REPAIRED CHAFED #1 ENGINE I/B FAN COWL AFT HINGE FITTING IAW EA 300-7110-01-A7889 REV IR AND EO A300-7110-73916-A. (MINOR)Aug 22, 2019 · N164UP · Airbus A300F4622R · Engine Cowling SystemSDR IPXA2018121096720Eec · inoperativeDURING DESCENT, AND LEVELING AT 5000 FT, 250 KTS. FIRST ENG ANO LOW OIL PRESSURE WARNING CAME ON ECAM AND RED WARNING LIGHT. RECHECKED, ECAM THEN ENG, 1 FAIL CAME ON. ENGINE ONE WAS AT IDLE AND WOULD NOT RESPOND. STARTED ENGINE FAIL ECAM PROCEEDURE. ACCOMPDec 9, 2018 · N164UP · Airbus A300F4622R · Fuel Controlling SystemSDR IPXA2018031827553Skin · dentedFUSELAGE SKIN DENTED AND GOUGED, FRAMES 85 TO 86 STRINGERS 42 - 43L. REPAIRED IAW EO 5330-67752-B.Mar 17, 2018 · N164UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2018020826356Lamp · inoperativeLAVATORY MIRROR LIGHT INOPERATIVE REPLACED THE LAMPS IAW 33-51-21-04-01.Feb 7, 2018 · N164UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2017062318539Bracket · damagedINSPECTION TYPE: EVAS CONTAINER ON PILOT SIDE NOT SECURLY FASTENED. FOUND A DAMAGED MOUNTING BRACKET. THE EVAS WAS REMOVED. REINSTALLED EVAS MOUNT AND CASE IAW A300-2560-45128 STEP 21.Jun 23, 2017 · N164UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2017042516469Skin · dentedINSPECTION TYPE: C1, RIGHT WING INBD FLAP LOWER SURFACE IS DENTED IN SEVERAL PLACES. REPAIRED THE FLAP SKIN IAW EO A300-5750-64016-A.Apr 15, 2017 · N164UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2017042516465Skin · crackedINSPECTION TYPE: C1, RT WING PANEL LANDING AT PANEL 613AB IS CRACKED AT THE CORNER, CRACK IS OUT OF SRM LIMITS. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW SRM 53-15-63.Apr 15, 2017 · N164UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2017042516477Fairing · crackedINSPECTION TYPE: 1C, NR 1 PYLON FAIRING 475AL HAS A PARTIAL STOP DRILLED CRACK IN THE OTBD MID SECTION. ACCOMPLISHED A REPAIR TO THE PYLON FAIRING IAW SREO 300-5450-32659, APPENDIX A.Apr 15, 2017 · N164UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2017042416403Angle · crackedINSPECTION TYPE: 1C, LEFT TWING FIXED LE FLANGE CRACKED ON INSIDE RADIUS AT INBD LE ADJACENT TO THE KRUEGER FLAP. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-21.Apr 15, 2017 · N164UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2017042216367Skin · crackedINSPECTION TYPE:C-1, LT WING ACCESS PANEL LANDING AT 513AB IS CRACKED AT THE CORNER. CRACK OUT OF LIMITS IAW SRM. STOP DRILLED THE CRACK AND INSTALLED SKIN DOUBLER IAW SRM 53-15-63.Apr 15, 2017 · N164UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2017041616156Support Angle · crackedINSPECTION TYPE: 1C, AFT CARGO FWD BULKHEAD WALL SUPPORT ANGLE CRACKED AT FRAME 54, RBL 47. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-21.Apr 15, 2017 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2017041616154Stiffener · crackedINSPECTION TYPE: 1C, AFT CARGO BAY FWD BULKHEAD SUPPORT STIFFENER CRACKED AT FRAME 54, RBL 75. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-21.Apr 15, 2017 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2017032315433Lever · obstructedESCAPE SLIDE ARMING LEVER DOES NOT FULLY MOVE TO THE RIGHT WHEN ARMING, HOWEVER ON EACM DOOR SPAGE SHOWS ARMED. FOUND DEBRIS BLOCKING FULL ENGAGEMENT OF ESCAPE SLIDE ARMING LEVER. REMOVED DEBRIS ESCAPE SLIDE ARMING LEVER WORKS NORMAL IAW MM 52-10-00Mar 23, 2017 · N164UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2017020313646Cover · unsecurePROTECTIVE PLASTIC COVER OVER ARM/DISARM LEVER ON CREW ENTERY DOOR DOES NOT CLOSE FULLY.FOUND EMERGENCY SLIDE WARNING LIGHT NOT SECURED. REINSTALLED LIGHT IAW MM 52-73-11. DISARM LEVER COVER OPENS FULLY.Feb 2, 2017 · N164UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2017013013437Power Supply · inoperativeEVACUATION SLIDE OR SLIDE RAFT RELEASE WARNING SYSTEM LIGHT. R & R AUTOMOMOUS POWER SUPPLY AND BOTH BATTERIES IAW MM 52-7318 OPS CHK NORMAL IAW MM 52-73-00-0501.Jan 28, 2017 · N164UP · Airbus A300F4622R · Escape SlideSDR IPXA2017010212309Light · inoperativeLAVATORY MIRROR LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM33-51-21-401.Dec 31, 2016 · N164UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2015031186932Angle · crackedINSPECTION TYPE:C12, EACH ANGLE AT FR79 RT AND LT HAVE 90 DAY LEAD TIME. EXTRUSION HAS 120 DAY LEAD TIME, NEED TO FABRICATE TO AN ALTERNATE EXTRUSION. FABRICATION IAW EA A300-5310-5310-56895-A.Mar 11, 2015 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2015031186931Angle · crackedINSPECTION TYPE:C12 EA, ANGLES AT FR79 RT AND LT HAVE 90 DAY LEAD TIME. EXTRUSION HAS 120 DAY LEAD TIME NEED TO FABRICATE TO AN ALTERNATE EXTRUSION, FABRICATION IAW EA A300-5310-5310-56895-A.Mar 11, 2015 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2015031186930Angle · crackedINSPECTION TYPE:C12 EA ANGLES AT FR79 RT AND LT HAVE 90 DAY LEAD TIME. EXTRUSION HAS 120 DAY LEAD TIME NEED TO FABRICATE TO AN ALTERNATE EXTRUSION FAB IAW EO A300-5310-5310-56895-A.Mar 11, 2015 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2015030486656Skin · puncturedINSPECTION TYPE:10Y, LEFT WING INBD FLAP HAD TEMPORARY REPAIR IAW EOA 300-5750-56307-B. PERMANENT REPAIR ACCOMPLISHED IAW EO A300-5750-56856-B.Mar 3, 2015 · N164UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2015031086896Floorboard · puncturedINSPECTION TYPE:10Y, MAIN CABIN FLOORBOARD 232LF HAS A PUNCTURE. FABRICATED NEW FLOORBOARD IAW EO A300-5320-16407-E.Feb 26, 2015 · N164UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2015031086889Angle · crackedINSPECTION TYPE:10Y, 2 EA ANGLES AT FR 79 RT AND LT HAVE 90 DAY LEAD TIME. EXTRUSION HAS 120 DAY LEAD TIME. NEED TO FABRICATE TO AN ALTERNATE EXTRUSION, FABRICATE IAW EO A300-5310-56895-A.Feb 17, 2015 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2015031086895Seat Track · corrodedINSPECTION TYPE:10Y, SEAT TRACK CORRODED AND CRACKED, REPAIRED IAW SRM 53-10-16, FIG 201, P 207/208.Feb 9, 2015 · N164UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2015022486411Floor Panel · crackedINSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 231WG BROKEN/CRACKED. FABRICATED NEW FLOORBOARD IAW EO A300-5320-40552-B.Feb 9, 2015 · N164UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2015022486410Floor Panel · damagedINSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 232LF BROKEN/CRACKED. FABRICATED NEW PANEL IAW EO A300-5320-40552-B.Feb 9, 2015 · N164UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2015031086891Floorbeam · crackedINSPECTION TYPE:10Y, MAIN CABIN CROSSBEAM LT FRAME 79 CRACKED AT CUSP AREA REPAIRED IAW EO A300-5310-56642-P2.Feb 7, 2015 · N164UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2015030586668Frame · crackedINSPECTION TYPE:10YR, MAIN CABIN CROSS BEAM AT RT FRAME 79 CRACKED AT CUSP AREA. REPAIRED IAW: EO A300-5310-56642-P2.Feb 5, 2015 · N164UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA201409084209Light · malfunctionedDURING PREFLIGHT, EMERGENCY EXIT LIGHTS ILLUMINATED WITH EMERGENCY EXIT LIGHT SWITCH IN ARM POSITION. COMPLIED WITH ADJ/TEST REF AMM 33-51-00-501.Sep 4, 2014 · N164UP · Airbus A300F4622R · Emergency LightingSDR IPXA2014012200548Cylinder · deactivatedIN PAX CREW DOOR EMERGENCY OPERATION, CYLINDER DISARMED AND SAFETY PIN INSTALLED. REMOVED SAFETY PIN AND REARMED DOOR EMERGENCY OPERATION CYLINDER, AMM CH 52-10-00-301.Jan 17, 2014 · N164UP · Airbus A300F4622R · Emergency Equipment
Back to N164UP