N120UP

Service difficulty reports · 203

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 = 'N120UP' 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 IPXA12173594Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231WG IS PUNCTURED AND CRACKED ON LWR SURFACE. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.May 14, 2012 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12173593Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231QH LWR SKIN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.May 14, 2012 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2171100Skin · gougedRT WING NR 1 SLAT INBD END OF OUTER SKIN INTERIM BLEND REPAIR. REPAIRED IAW EO A300-5750-45278-B.Jan 16, 2012 · N120UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA1168818Skin · damagedFUSELAGE SKIN DAMAGED AT FRAME 85, STRINGERS 44L - 45L. REPAIRED IAW EO A300-5330-43720-B.Aug 22, 2011 · N120UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA0163859Module · inoperativeLANDING GEAR WOULD NOT RETRACT. ECAM MESSAGE LANDING GEAR RETRACT INOP. SWITCHED FROM SYS 2 TO SYS 1. NO HELP. HANDLE WOULD NOT MOVE FROM MIDDLE POSITION. C/W FIM 32-30-00 BLOCK 1, 2 AND 5. FOUND BAD LEVER MODULE ASSY. TSM 32-30-00 C/W TESTS/OPS CK C/W REFDec 15, 2010 · N120UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA10163810Slide · unwanted deployCREW INADVERTENTLY DEPLOYED DOOR SLIDE. DOOR SLIDE REMOVED AND DEF 441338 ASSIGNED. SUPPLEMENTAL ETOPS REPORT, INSTALLED SERVICEABLE SLIDE, GIRTBAR, SLIDERS AND COVER IAW AMM 25-61-21-04. OK FOR SERVICE. STICKER REMOVED. M441338 CLEARED.Dec 9, 2010 · N120UP · Airbus A300F4622R · Escape SlideSDR IPXA10159912Control Unit · inoperativeAFTER T/O L/G WOULD NOT RETRACT. TRIED BOTH POS DET 1&2 L/G LEVER WOULD NOT MOVE PAST OFF POSITION. DIVERTED, IAW FLT CONTROL. FAILURE CODE "65" DETECTED ON PROXIMITY DETECTOR PROCESSING UNIT WHILE PERFORMING T/S IAW FIM 32-30-00. PG. 105 FIG 108. R & R PRMay 18, 2010 · N120UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA10159502Power Supply · inoperativeSW 25WL WILL NOT ILLUMINATE DURING TEST REF PS-1 STEP 18. REPLACED POWER SUPPLY UNIT IAW AMM 33-51-14-04. OPS GOOD.Apr 24, 2010 · N120UP · Airbus A300F4622R · Emergency LightingSDR IPXA10159046Floor Panel · damagedINSPECTION TYPE:10YR, BULK CARGO FLOOR PANEL 161HF HAS SEVERAL DENTS AND PUNCTURES. FABRICATED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX D.Mar 18, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158923Floor Panel · crackedINSPECTION TYPE:10YR, MCD FLOOR PANEL 242LJ IS CRACKED. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 18, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158999Floor Panel · damagedINSP TYPE:10YR, MAIN CABIN NR 231KJ FLOORBOARD IS PUNCTURED AT UPPER SKIN. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX. B.Mar 17, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158922Floor Panel · crackedINSP TYPE:10YR, MCD FLOOR PANEL 222DG IS CRACKED. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 17, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158919Floor Panel · delaminatedINSPECTION TYPE:10YR, MCD FLOOR PANEL 232JF IS DELAMED. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 17, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158916Floor Panel · brokenINSPECTION TYPE:10YR, MCD FLOOR PANEL 232XG IS BROKEN. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 17, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158914Floor Panel · brokenINSPECTION TYPE:10YR, MCD FLOOR PANEL 232XG IS BROKEN. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203, SHEET 2.Mar 17, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158913Floor Panel · crackedINSPECTION TYPE: 10YR MAIN CABIN NR 231SG FLOORBOARD CRACKED AT FWD RT CORNER. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 17, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159045Floor Panel · crackedINSPECTION TYPE: 10YR, FLOOR PANEL 242JF IS CRACKED AT FABRICATED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX B.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159042Floor Panel · crackedINSPECTION TYPE:10YR, FLOOR PANEL 241 LJ IS CRACKED FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX.B.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158921Floor Panel · crackedINSP TYPE:10YR, MAIN DECK COMP FLOOR PANEL 251UJ HAS A CRACK. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158920Floorboard · crackedINSPECTION TYPE:10YR FLOORBOARD 251YJ IS CRACKED REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158918Floor Panel · delaminatedINSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241HN IS DELAMINATED AT INNER AFT CORNER. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158917Floor Panel · crackedINSPECTION TYPE:10YR, MCD FLOOR PANEL 251FM IS CRACKED. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159024Floorboard · delaminatedINSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251ZG IS DELAM AT LWR SURFACE FABBED FLOOR PANEL IAW SRM 53-10-20, PARA. 8B, FIG. 203, SHEE T 1.Mar 11, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159044Floorboard · delaminatedINSPECTION TYPE:10YR FLOORBOARD 242TN AT MAIN CABIN IS DELAMED FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX. B.Mar 10, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159043Floor Panel · damagedINSPECTION TYPE:10YR, BULK CARGO COMP FLOOR PANEL 162HF CORNER OF PANEL IS CRUSHED FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. D.Mar 2, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158208Connector · dirtyL1 ENTRY DOOR EVAC SLIDE WARNING LIGHT INOP. DEFERRED IAW MEL 52-73-01-1. M417463 ASSIGNED. CLEANED CONNECTOR AND RESET AUTONOMOUS POWER SUPPLY UNIT. ESCAPE SLIDE WARNING SYS NORMAL IAW TSM 52-73 FIG 103. THIS CLEARS M417463.Jan 18, 2010 · N120UP · Airbus A300F4622R · Equipment/Furnishings WiringSDR IPXA09157718Floorboard · damagedFLOOR BOARD DAMAGE. FAB'D NEW PNL IAW EO B757-5320-9692-G.Oct 18, 2009 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09155582Skin · gougedINSPECTION TYPE:4C, RT WING INBD FLAP UPPER SKIN GOUGED 7 PLACES APPROX 18 TO 24 INCHES ABOVE RUB STRIP. CUTOUT DAMAGED AREA OF SKIN PER A300 SRM 57-50-00. PERFORMED HFEC . FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00.Apr 8, 2009 · N120UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA09155568Floor Panel · crackedINSPECTION TYPE:4C BULK CARGO COMP FLOOR PANEL 161GF IS CRACKED AT UPPER SKIN AT FR 67 LB L6. FABRICATED NEW FLOOR PANEL IAW EO NR A300-5320-16407-C, APPX D.Apr 6, 2009 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09155567Floor Panel · delaminatedINSPECTION TYPE:4C BULK CARGO FLOOR PANEL NR 161JF IS DELAMINATED IN 2 PLACES. FABRICATED NEW FLOOR PANEL IAW EO NR A300-5320-16407-C APPX D.Apr 6, 2009 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09155573Angle · crackedINSPECTION TYPE:4C NR 1 ENGINE INBD T/R LWR CIRCUMFERENTIAL CLOSURE IS CRACKED AT RADIUS. FABRICATED AND INSTALLED REPAIR ANGLE IAW EO A300-7830-33132-A, AND SAA EA 300-7830-01-A1703.Apr 5, 2009 · N120UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA09155572Support · crackedINSPECTION TYPE:4C NR 2 ENGINE OTBD T/R TRANSLATING SLEEVE AT 6:00 POSITION HAS CRACKED ANGLE SUPPORT OF LOWER LONGERON. FABRICATED AND INSTALLED REPAIR ANGLE IAW EO NR A300-7839-33132-A AND SAA EA3 300-7830-01-A1704.Apr 5, 2009 · N120UP · Airbus A300F4622R · Engine Thrust ReverserSDR UPS09154466Switch · faultyINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT "DISARM" DOES NOT ILLUMINATE WHEN EMERGENCY EXIT LIGHT SWITCH IS DISARMED. BULBS TEST OKAY. FOUND SWITCH 22WL (EMERGENCY LIGHT CONTROL) INTERMITTENT. SWAPPED SWITCH 22WL WITH 12WZ (402VU, EGPWS), 22WL TEST OK PER MM Jan 29, 2009 · N120UP · Airbus A300F4622R · Emergency LightingSDR UPS08152910Sign · inoperativeCREW ENTRY DOOR TOP EXIT SIGN (LIGHT) BOTTOM LIGHTS INOP. RELAMPED CREW DOOR EXIT SIGN BOTTOM LAMPS IAW AMM 35-51-13-04. OPS CHECK GOOD.Jul 29, 2008 · N120UP · Airbus A300F4622R · Emergency LightingSDR UPS08151586Slide · dislodgedDOOR WAS OPEN BEFORE SLIDE DISARMED, SLIDE DID NOT DEPLOY BUT FELL OUT ON STAIRS. DEFERRAL M367928. INSTALLED MAIN ENTRY DOOR ESCAPE SLIDE REF 25-61-21-04. PLACARD REMOVED.Jan 28, 2008 · N120UP · Airbus A300F4622R · Escape SlideSDR UPS07151323Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER T/O, LDG WT 301K#. ONLY SYS 1 UTILIZED. PERFORMED PDCU BITE TEST PER AMM 32-00-00-05. NO FAULTS FOUND. PERFORMED TEST OF 2GA USING SIMULATED TEST BOX PER AMM 32-31-11-04 ON BOTH SYS 1 AND 2. OPS CK GOOD. LDG GEAR POSIDec 24, 2007 · N120UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR UPS07148887Handle · stiffCABIN DOOR EVA SLIDE DISARM HANDLE VERY HARD TO MOVE. DEFERRED MAIN CABIN DOOR SLIDE IAW MEL 52-11-01-3. ACCOMPLISHED DMP 52-11-01-3. SLIDE NEEDS NOT BE REMOVED. DMI OPENED.Jan 18, 2007 · N120UP · Airbus A300B4622R · Escape SlideSDR UPS07148847Arming Lever · bindingEMERGENCY SLIDE ARMING LEVER BINDS AND DOES NOT MOVE WHEN DISARMING. AFTER NUMEROUS ATTEMPTS TO UNLOCK LEVER FINALLY DISARMED. DEFERRED #M341771. CHECKED ESCAPE SLIDE RELEASE MECHANISM IAW MM 52-10-30-06. NO DAMAGE OR ADJUSTMENT OUT OF LIMITS FOUND. OPS CJan 10, 2007 · N120UP · Airbus A300F4622R · Escape SlideSDR UPS07148834Lever · bindingMAIN ENTRANCE DOOR (CREW DOOR) SLIDE ARMING LEVER BINDS WHEN UNLOCKING, SEVERAL ATTEMPTS TO UNLOCK WERE NEEDED TO DISARM THE SLIDE. PERFORMED LUBRICATION ON THE SLIDE ARM/DISARM MECHANISM.Jan 4, 2007 · N120UP · Airbus A300F4622R · Escape SlideSDR UPS07148858Arming Lever · jammedCABIN DOOR SLIDE ARMING HANDLE JAMMING WHEN DISARMING. CHECKED DOOR SLIDE ARMING SYSTEM IAW MM 25-61-04. FOUND NO ABNORMALS.Jan 2, 2007 · N120UP · Airbus A300F4622R · Escape SlideSDR UPS07148857Handle · jammedCABIN MAIN ENTRY DOOR DIS-ARM HANDLE IS JAMMING WHEN DIS-ARMING SLIDE. MAIN ENTRY DOOR SLIDE RAIL LOCKS CLEANED, DRIED, AND LUBRICATED. TESTED SEVERAL TIMES SATISFACTORY.Jan 2, 2007 · N120UP · Airbus A300F4622R · Passenger/Crew DoorsSDR UPS06148807Isolation Valve · stuckINSPECTION TYPE:N/A ATB - EMERGENCY DECLARED - MAIN CARGO DECK SMOKE WARNING MSG WAS DISPLAYED ON ECAM WHILE DESCENDING. ALSO RECEIVED AN AVIONICS SMOKE WARNING ECAM MSG. INSPECTED AIR COND BAY COMPONENTS, DUCTING, VALVES & DUCTING IN FWD CARGO BAY FLOOR, VLDec 29, 2006 · N120UP · Airbus A300F4622R · Air Distribution SystemSDR UPS06146271Connector · dirtyINSPECTION TYPE:N/A CREW ENTRY DOOR ESCAPE SLIDE WARNING LIGHT INOP. CLEANED CONNECTOR 70WN -A ON ASPSU. OPS CHECKED GOOD IAW MM 52-73-18.Feb 23, 2006 · N120UP · Airbus A300F4622R · Escape SlideSDR UPS06146181Oxygen Mask · no testFO'S 02 MASK W/N TEST. RESEATED FO'S 02 MASK CONNECTOR. OPS NORMAL IAW MM 35-12-51-5.Feb 15, 2006 · N120UP · Airbus A300F4622R · Crew Oxygen SystemSDR UPS05145730Access Panel · crackedACCESS PANEL REMOVED IN RIGHT KRUEGER FLAP BOX AREA. INSTALLED ACCESS PANEL IN RIGHT KRUEGER FLAP BOX AREA PER 57000.Nov 7, 2005 · N120UP · Airbus A300F4622R · Leading Edge DevicesSDR UPS05144708Light · inoperativeEMERGENCY EXIT LIGHT JUST OUTSIDE CABIN ENTRY INOPERATIVE. RESET SOCKET AND OPS CHECKED PER AMM 33-51-00-0. OPS CHECK. THIS CLEARS M304232. PLACARD REMOVED.Jun 15, 2005 · N120UP · Airbus A300F4622R · Emergency LightingSDR UPS05144675Floorbeam · crackedMAIN CABIN RT FLOORBOARD SUPPORT BRACE CRACKED STA 51 RBL 24. REMOVED AND REPLACED FLOORBOARD SUPPORT BRACE (CROSSBEAM) IAW A300 SRM 51-40-00, AIRBUS STANDARDS MANUAL ANSA 2814 AND DWG 15-A53813309.May 24, 2005 · N120UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR UPS05144551Light · inoperativeINSPECTION TYPE:N/A SEVERAL LAMPS INOP IN EMERGENCY LIGHT ABOVE L1 DOOR. RELAMPED, CHECKS OK.May 7, 2005 · N120UP · Airbus A300B4622R · Emergency LightingSDR UPS04142689Brake · inoperativeINSPECTION TYPE:N/A ON LANDING & TAXI IN NO LEFT BRAKE ON EITHER SIDE OF COCKPIT. REMOVED AND REPLACED NORMAL BRAKE MASTER VALVE LT PER MM 32-42-19-4 R/R 774905 PERFORM FUNCTIONAL TEST OR MAXIMUM PRESS DELIVERED TO BRACES IAW MM 32-42-00-5 PARA 3 (3), SYS CKSJul 9, 2004 · N120UP · Airbus A300F4622R · BrakeSDR UPS04142613Skin · chafedINSPECTION TYPE: C, LEFT WING INBOARD DAMAGED INTERIM REPAIR MADE IAW EO A300-5750-19043-A 1500 FLT CYCLE LIMIT (D263708). REPAIRED I/B FLAP WITH PERMANENT REPAIR IAW A300-600 SRM 57-50-00.Jun 15, 2004 · N120UP · Airbus A300F4622R · Trailing Edge Flaps
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