N136UP

Service difficulty reports · 276

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 = 'N136UP' 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 IPXA10161562Floor Panel · misrepairedINSPECTION TYPE:4C, AFT PIT FLOOR PANEL NR 151QF REQUIRES REPLACEMENT IAW EO A300-5320-16407-D. FABRICATED AFT CARGO FLOOR PANEL NR 151QF IAW EO A300-5320-16407-D, APPENDIX C.Jul 30, 2010 · N136UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10161561Floor Panel · misrepairedINSPECTION TYPE:4C, BULK CARGO FLOOR PANEL NR 162HF REQUIRES REPLACEMENT IAW EO A300-5320-16407-D. FABRICATED BULK CARGO FLOOR PANEL NR 162HF IAW EO A300-5320-16407-D APPENDIX D.Jul 30, 2010 · N136UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10161560Floorboard · misrepairedINSPECTION TYPE:4C, BULK CARGO COMPARTMENT FLOOR PANEL NR161HF REQUIRES REPLACEMENT IAW EO A300-A300-5320-16407-D. FABRICATED BULK CARGO FLOORBOARD NR 161HF IAW EO A300-5320-16407-D, APPENDIX D.Jul 30, 2010 · N136UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10161535Skin · gougedINSPECTION TYPE:4C, REPAIR SURVEY SEQUENCE NR 136-W4-01 EXISTING REPAIR DOUBLER GOUGED ON RT WING CTR FLAP UPPER SURFACE. ACCOMPLISHED REPAIR IAW SRM 57-50-00 PARA 4E, FIG 205.Jul 30, 2010 · N136UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10160900Skin · dentedRT AILERON BOTTOM SURFACE HAS DENT 2.200 X 3.100. REPAIRED DENT IAW SRM 57-61-114D, FIG 204 AND EO A300-5750-34868-C.Jul 4, 2010 · N136UP · Airbus A300F4622R · AileronsSDR IPXA10158523Switch · out of positionDIVERSION - ANNUNCIATOR LIGHT TEST ACTIVATED IN FLIGHT. CREW DECLARED EMERGENCY AND DIVERTED TO MIA. ON APPROACH CREW FOUND THE TEST SWITCH IN THE ON POSITION. C/W ANNUNCIATOR LIGHT DIMMING ADJ AND TEST AND ANNUNCIATOR LIGHT TEST IAW 33-161-00-5, 33-14-00-5Feb 16, 2010 · N136UP · Airbus A310200 · Indicating/Recording SystemSDR IPXA10158369Skin · dentedDENT 2 FT FWD AND LT OF TAIL STAND BALL. APPLIED SKIN DOUBLER IAW EO A300-5330-36482-A.Jan 31, 2010 · N136UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA09155397Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS / EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHTING PSU PER MM 33-51-14-04. OPS CHECK GOOD.Apr 5, 2009 · N136UP · Airbus A300F4622R · Emergency LightingSDR IPXA09155151Light · malfunctionedINSPECTION TYPE:N/A EXIT LIGHT DID NOT ILLUMINATE WHEN GEAR EXTENDED. DEFERRED. TESTED EMERGENCY LIGHTING SYSTEM. OPS CHECK GOOD REF AMM 33-51-00-5. CLEARS DEFERRAL M397423.Mar 24, 2009 · N136UP · Airbus A300F4622R · Emergency LightingSDR UPS08154245Floorboard · puncturedINSPECTION TYPE:N/A FLOORBOARD DAMAGED MAIN CARGO DECK POS 1 RT SIDE. FABRICATED NEW PANEL IAW EO A300-5320-16409-C.Dec 28, 2008 · N136UP · Airbus A300F4622R · Fuselage Floor PanelSDR UPS08151910Connector · dirtyINSPECTION TYPE:1C ESCAPE SLIDE RELEASE WARNING FAILED OP CHECK, EMERGENCY EXIT LIGHT INTERMITTENT. TROUBLESHOT TO PINS "C" AND "F", CLEANED CONNECTOR, PINS, OP CHECKED ESCAPE SLIDE RELEASE WARNING, OP CHECKED GOOD, EMERGENCY EXIT LIGHT ALSO CHECKS GOOD PER AMar 7, 2008 · N136UP · Airbus A300F4622R · Equipment/Furnishings WiringSDR UPS08151888Skin · dentedINSPECTION TYPE:3C TRANSFERRED FROM LOG PAGE 954176 ITEM 2. REF DMI D370413. SKIN DENTS FWD AND RIGHT OF TAIL STAND FITTING. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLER IAW A300-600 SRM 53-10-12 FIG 210.Mar 7, 2008 · N136UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR UPS06148098Light · no testSUPERNUMERARY EMERGENCY LIGHTS WON'T TEST PROPERLY. RELAMPED 3 LAMPS IN EXIT SIGN. SYSTEM OPS CKS GOOD.Sep 28, 2006 · N136UP · Airbus A300F4622R · Emergency LightingSDR UPS06147606Skin · dentedINSPECTION TYPE:5YR REF DMI D314583 FOUND DENT 5 INCHES LONG X .25 INCHES WIDE X .063 INCH DEEP AT SECTION 11/12, FRAME 18, STRINGER 32 AND FWD OF THE LWR AOA VANE RIGHT. CUT OUT DAMAGED SKIN AT FR 17/18 STR 30/32, FABRICATED REPAIR DOUBLER, FILLER AND INSTALJul 20, 2006 · N136UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR UPS06147123Lamp · inoperativeCREW DOOR EMERG EXIT SIGN LOWER LAMP INOP. RELAMPED, CKS OK AMM 33-50-00.Jun 13, 2006 · N136UP · Airbus A300F4622R · Emergency LightingSDR UPS06147008Light · malfunctionedINSPECTION TYPE:N/A EMERGENCY LIGHT ON FOR EXTENDED TIME. PERFORMED OPERATION TEST PER MM 33-51-14. OPS CHECK NORMAL.May 30, 2006 · N136UP · Airbus A300F4622R · Emergency LightingSDR UPS06146988Coalescer Bag · dirtyINSPECTION TYPE:N/A AFTER BLOCK OUT C/P FILLED WITH GREY SMOKE. CREW DONNED OXYGEN MASKS AVIONICS SMOKE AND MAIN CARGO DECK SMOKE WARNING RECEIVED. *S/D* PERFORMED MM 21-51-00-3 USED APU AIR FIRST AND HAD SMELL OF SKYDROL CYCLE THROUGH CHECK UNTIL SMELL WASMay 30, 2006 · N136UP · Airbus A300F4622R · Humidity Control SystemSDR UPS06147175Skin · ground damageINSPECTION TYPE:CK COMPLY WITH MAG GA 300-5318-27-A1438 AFT LOWER FUSELAGE SKIN REPAIR DU E TO CONTACT WITH GROUND EQUIPMENT COMPLY WITH EA VERIFIED EXISTING AND REINSPECTED FOR FURTHER DAMAGE PER EA 300-5318-24-1438.May 5, 2006 · N136UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR UPS06147174Skin · ground damageINSPECTION TYPE:CK COMPLY WITH MAG EA 300-5318-27-A1438 AFT LOWER FUSELAGE SKIN REPAIR. DUE TO CONTACT WITH GROUND EQUIPMENT. COMPLY WITH EA VERIFIED EXISTING AND REINSPECTED FOR FURTHER DAMAGE PER EA300-5318-27-1438May 5, 2006 · N136UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR UPS06147068Skin · ground damageINSPECTION TYPE:N/A REPAIR SKIN DAMAGE CAUSED BY GROUND EQUIPMENT REF EO A300-5310-24267-A. REPLACED SKIN AND REPAIRED DAMAGED FRAMES AND STRINGERS.May 1, 2006 · N136UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR UPS05145765Angle · crackedINSPECTION TYPE:1C RT WING KRUEGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED & REPLACED DOUBLER ON 2ND RIB FROM FUSELAGE PER SRM 51-40-21 & 51-40-00.Nov 8, 2005 · N136UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR UPS05145761Rib · crackedFOUND LEFT WING KRUGER FLAP BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE CRACKED. REMOVED AND REPLACED DOUBLER PER SRM 51-40-00.Nov 7, 2005 · N136UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR UPS05145760Crossbeam · crackedFOUND MAIN CARGO FS 50 RBL 20 FLOORBOARD BRACE CRACKED. REMOVED, FABRICATED AND REPLACED FLOORBOARD BRACE CROSSBEAM AT FS 50 RBL 20 PER DWG A53813379, SRM 51-40-00, SRM 53-15-15, SRM 51-20-10 AND SRM 51-23-10.Nov 7, 2005 · N136UP · Airbus A300F4622R · Fuselage Main, StructureSDR UPS05144510Smoke Barrier · tornINSPECTION TYPE:N/A CURTAIN BETWEEN AFT LOWER CARGO AND BULK CARGO IS TORN UPPER CENTER. REMOVED AND REPLACED CURTAIN WITH REF TO MM 25-56-11-2.May 23, 2005 · N136UP · Airbus A300B4622R · Emergency EquipmentSDR UPS04142327Light · inoperativeCREW ENTRY DOOR EVAC SLIDE RELEASE WARNING SYSTEM LIGHTS WILL NOT TEST. BUZZERS OK. CLEANED DEBRIS FROM SWITCH NOW OPS GOOD PER MM 52-73-00. THIS CLEARS M280249. LP 234452May 3, 2004 · N136UP · Airbus A300F4622R · Escape SlideSDR UPS03141228Light · inoperativeCREW DISCOVERED EVAC SLIDE LIGHT (WARNING LIGHT) INOPERATIVE. DEFERRED UNDER MEL 52-73-01 01 W/CONTROL NR M266526 PLACARD INSTALLED.Sep 15, 2003 · N136UP · Airbus A300F4622R · Escape Slide
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