N120UP

Service difficulty reports · 202

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 IPXA2026092263257Contact · inoperativeSLIDE RELEASE WARNING LIGHT DOES NOT ILLUMINATE DURING TEST, REPLACED CONTACTS IAW ESPM 20-48-25-01. REMOVED AND REPLACED SLIDE RELEASE WARNING LIGHT IAW AMM 52-73-11. OPS CK GOOD.Sep 22, 2026 · N120UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026083158089Limit Switch · faultedAIR TURN BACK, DURING CLIMB THE ESCAPE SLIDE WARNING LIGHT AND ALARM ACTIVATED PASSING THRU 10,000FT. LEVELED OF AT 27,000 FT THEN DESCEND BACK FOR LANDING AND IT CEASED PASSING THRU 14,500 FT. REPLACED EMERGENCY ESCAPE SLIDE SYSTEM LIMIT SWITCHES IAW AMM 52-Aug 27, 2026 · N120UP · Airbus A300F4622R · Escape SlideSDR IPXA2026042054544Light · inoperativeLAV EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB OPS CK GOOD REF 33-51-21-02 OK FOR SERVICEApr 17, 2026 · N120UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025041754051Fairing · damagedAGING ACFT INSP-300-STR- FUSELAGE SKIN UNDER LEFT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE. DOT AA001.FOUND CHAFE DAMAGE THRU CHAFE PLATE 100% MATERIAL LOSS, REMOVED CHAFE PLATE AS REQUIRED IAW SRM 53-19-12 PARA 5.VERIFIED CHAFE DAMAGE THRU CHAFEMar 25, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2025041754643Fairing · damagedAGING ACFT INSP-300-STR- FUSELAGE SKIN UNDER RIGHT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE.FOUND CHAFFE DAMAGE TO BE OUT OF LIMITS 100% MATERIAL LOSS. REMOVED CHAFFE PLATE IAW-A300 SRM-53-19-12.PRIMED INTERIOR SIDE IAW-A300-SRM-51-75-10.INSTALLEDMar 25, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2025032554643Skin · chafedFUSELAGE SKIN UNDER RIGHT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE. [Mar 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025032554051Skin · chafedFUSELAGE SKIN UNDER LEFT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE.Mar 25, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer, Plate/SkinSDR IPXA2025042095015Skin · corrodedCONDITION EXIST ON RH WING UPPER SURFACE THAT NEEDS TO BE EVALUATED AT BETWEEN RIB 8 TO RIB10, (SPECIAL ATTENTION AT RIB9).REMOVED PAINT ON RH WING UPPER SURFACE BETWEEN RIB 8 TO RIB 10 AREA BY CHEMICAL METHOD USING PAINT STRIPPER P/N: E3000, BATCH: 4342177, IMar 22, 2025 · N120UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2025031998250Adapter · corrodedSEAT ADAPTER AT Y0 RH AT FR 38.2 CORRODED. DOT# 110-401 JP-110.REMOVED CLS ADAPTER AT Y 0 R/H AT FR38.2 IAW A300-600 SRM 51-40-21.INSTALLED ROBBED PART CLS ADAPTER P/N:B53774136200 AT Y0 R/H AT FR38.2 IAW A300-600 SRM 51-40-21. MATERIAL USED SEALANT P/N:04-0Mar 17, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025031095741Roller · excess playAPG-830-CREW DOOR 2 EACH ROLLER ASSYS HAVE EXCESSIVE PLAY DOT# 110-182 JP-110.REMOVED AND REPLACED ROLLER ASSY 2EA IN CREW DOOR IAW AMM 20-21-12.VERIFIED REPLACEMENT OF ROLLER ASSY 2EA IN CREW DOOR IAW AMM 20-21-12.Mar 6, 2025 · N120UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025030795741Roller · excess playCREW DOOR 2 EACH ROLLER ASSYS HAVE EXCESSIVE PLAY. OPE NMar 6, 2025 · N120UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025032115716Web · crackedWEB AT FR 69 IS CRACKED FROM -Y300 TO -Y950 AT MANY LOCATIONS DOT# 110-171 JP-110.REMOVED WEB AT FR 69 , FROM Y300 TO Y950 AND REMOVED RIVET L/H WEB FOR ACCESS IAW A300 SRM 51-40-21.INSTALLED RIVET L/H WEB AT FR 69 IAW A300 SRM 51-40-21.PERFORMED CUTOUT OF DAMar 1, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025031314196Structure · corrodedSDR FILED OPEN, RH WING KRUEGER FLAP NOTED IG CORROSION. INSTALLED RH WING KRUEGER FLAP IAW AMM 27-87-11-0401.Mar 1, 2025 · N120UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2025040185553Fairing · chafedFAULT-AGING ACFT INSP-300-STR- FUSELAGE SKIN UNDER LEFT LOWER HORIZ STAB FAIRING HAS CHAFE DAMAGE AT AFT SIDE. DOT AA001. VERIFIED INSTALLATION OF LOWER STAB FARING CHAFE PLATE ON LEFT HAND SIDE USING SEALSNT PS870C24 BATCH # 0004366606 AND FAY SEALED WITH 5-Feb 27, 2025 · N120UP · Airbus A300F4622R · Horizontal Stabilizer StructureSDR IPXA2025031962725Seat Track · corrodedMAIN DECK COMPARTMENT-FLOOR PNL 251LM INSIDE LOWER FR60- C TRACK PLATE HAS CORROSION DOT43-059. ACCOMPLISHED STEP 11, EA#:300-5317-27-A3822, PRELIMINARY 2. "INSTALL CLS ADAPTER PER AIRBUS DRAWING A53275515". USING EXISTING FASTENERS(HI-LOK). COLLAR P/N: NSAFeb 26, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025031960736Adapter · corrodedMAIN DECK SEAT TRACK ADAPTER AT FR34, Y0 LEFT EXFOLIATED.. DOT# 110-305 JP-110. ACCOMPLISHED STEP 11, EA #:300-5314-27-A3812, PRELIMINARY 2. "INSTALL CLS ADAPTER PER AIRBUS DRAWING B53774150". ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH UPS EO-92964-REQ1 AFeb 26, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025031964328Adapter · corrodedMAIN DECK COMPARMENT, FLOOR SUPPORT STRUCTURE, CLS AT PANEL 251LG CORRODED. DOT 28-13. ACCOMPLISHED STEP 3, EA#:300-5316-27-A3814, PRELIMINARY 1." FABRICATE A REPLACEMENT CLS ADAPTER (P/N:A53275451200) PER AIRBUS DRAWING A53275451 FROM MAXIMUM 2.00 INCH THICKFeb 26, 2025 · N120UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025040844111Frame · crackedCRACK FOUND ON HOLE "A" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ERIFIED INSTALLATION OF HAREWARE PER EA 300-5710-27-A3809.COMPLIED WITH EA 300-5710-27-A3809 STEP 31. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -.Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025031940161Floor Support · corrodedMAIN DECK FLOOR SUPPORT FR11-FR115A, Y1456 CORRODED AT MANY LOCATIONS. DOT# 110-107 JP-110. INSTALLED FLOOR SUPPORT Y1456 LOCATED AT FR11 TO FR19 IAW A300-600F SRM 53-12-15-001-1, SRM 51-40-21-001, DRAWING A53613033210 JH 11000495.Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025031940305Floor Support · corrodedMAIN DECK FLOOR SUPPORT CORRODED BETWEEN FR12-FR14, Y1959 DOT# 110-108 JP-110. REMOVE AND REPLACE 1 EACH Y1959 FLOOR SUPPORT (P/N: A53613033212) PER AIRBUS DRAWING A53613033212 REQUIREMENTS AND A300-600F SRM 53-12-15-001-1.Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025032044146Fitting · crackedCRACK FOUND ON HOLE "Q" ON FR47 LH HORIZONTAL JUNCTION. ACCOMPLISHED THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -.Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025032044127Fitting · crackedCRACK FOUND ON HOLE "P" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -.Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025032044111Frame · crackedCRACK FOUND ON HOLE "A" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -. CFeb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025031939728Floor Support · corrodedMAIN DECK FLOOR SUPPORT AT FR11-FR15A, Y953 CORRODED AT MANY LOCATIONS. DOT# 110-106 JP-110. INSTALLED FLOOR SUPPORT Y 953 LOCATED AT FR11 TO FR15A IAW A300-600 SRM 51-40-21-001 AND DRAWING A53613033210.Feb 25, 2025 · N120UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025022799560Attach Plate · damagedFAULT-STR-ZONE 400-#1 ENG PYLON PNL475AL FWD I/B UPPER PLATE HOLE ENLONGATED DOT 43-047. INSTALLED NEW ATTACH FAIRING, IAW A300-600 SRM 51-40-21. USED MATERIAL: SOLID RIVET P/N MS20426AD5-5 BATCH 0004361891. REVIEWEDFeb 22, 2025 · N120UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2025022599592Plate · crackedFAULT-STR-ZONE 400-#1 ENG PYLON PNL475AL FWD I/B UPPER PLATE HOLE CRACKED DOT 43-048. INSTALLED NEW ATTACH FAIRING, IAW A300-600 SRM 51-40-21. USED MATERIAL: SOLID RIVET P/N MS20426AD5-5 BATCH 0004361891. REVIEWEDFeb 22, 2025 · N120UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2025040172383Floor Panel · damaged**SUPPLEMENTAL SDR** FAULT-COMP-FUSELAGE TAIL COMPARTMENT FLOOR PANEL BTW FR 84-85 LH SIDE DELAMINATED-DOT 139/34-MR/139. INSTALLED FUSELAGE TAIL COMPARTMENT FLOOR PANEL BTW FR 84-85 LH SIDE I.A.W A300-600 AMM 20-21-12/001. REVIEWEDFeb 21, 2025 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025032472383Floor Panel · delaminatedMAJOR REPAIR, FUSELAGE TAIL COMPARTMENT FLOOR PANEL BTW FR 84-85 LH SIDE DELAMINATED. CERTIFICATION COMPLETEDFeb 21, 2025 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025031385283Rib · damagedDAMAGE INDICATION FOUND INSIDE 2ND LAYER OF FRAME 40 TO CENTER WING JOINT UPPER SKIN LEVEL TENSION BOLT (TOP HOLE) R/H SIDE. ACOMPLISHED REPAIR IN ACCORDANCE WITH UPS EO-93055-REQ1 AND VT-MAE EA 300-5710-27-A3843, REV. -.Feb 21, 2025 · N120UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2025030786437Rib · crackedTHE L/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (3EA) AT RIB LOCATION 26 AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3811, REV.-.Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025030686391Rib · crackedTHE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 27 FWD SIDE. INSTALL REPAIR DOUBLER GIVEN.COMPLIED WITH STEP 17 OF EA 300-5750-27-A3811. ACCOMPLISH REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3811, REV. -.Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025030786389Rib · crackedTHE L/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 27 AFT SIDE. INSTALL REPAIR DOUBLER GIVEN.COMPLIED WITH STEP 17 OF EA 300-5750-27-A3811. ACCOMPLISH REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A3811, REV. -.Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025030586446Rib · cracked*SDR FILED OPEN* FAULT: THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 12 AFT SIDE. COMPLIED WITH STEP 17 OF EA 300-5750-27-A3813 PRELIMINARY 1.Feb 21, 2025 · N120UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025031161633Bracket · crackedE&E BAY FRAME 10 RH WEB BRACKET BROKEN. FABRICATED NEW BRACKET USING MATERIAL 2024-T3 .063C, BATCH 0004324652, IAW GMM 09-08, PARAGRAPH 09.08.01.04 AND LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED NEW BRACKET IAW SRM 51-40-21.Feb 20, 2025 · N120UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2025020104401Warning Light · inoperativeEVAC SLIDE WARNING LIGHT INOP CLEANED CONNECTOR AT POWER SUPPLY, OPERATIONAL CHECK REF 52-73-11/401. OPERATES NORMALLY. OSD: 2/3/2025Jan 31, 2025 · N120UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2024091670995Windshield · cracked2:30 INTO FLT@FL340,CAPTS WINDSCREEN OUTER PANE CRACKED LEFT TO RIGHT AT -48 REPLACED L/H WINDSHIELD IAW AMM 56-11-11-0401 OPS CK GOOD.Sep 13, 2024 · N120UP · Airbus A300F4622R · Flight Compartment WindowsSDR IPXA2024071037812Clamp · looseATB, EMD, PACK #2 ADVISORY FOR HIGH INLET TEMP. NOT ABLE TO CONTROL OR REDUCE TEMP. FOLLOWING TSM 21-61-00 FOUND LARGE BLEED LEAK AT LOOSE CLAMP ON COMPRESSOR BYPASS DUCT ASSY - REPOSITIONED AND TORQUED CLAMP (34H40-400) IAW A300 AMM 21-51-25/401. LEAK CHECK Jul 10, 2024 · N120UP · Airbus A300F4622R · Engine Bleed Air SystemSDR IPXA2023100962149Unknown · unknownWHILE WORKING WATER INTRUSION DEFERRAL BARCODE T3F18E002SM1Q FOUND FLOOR PANEL 231KJ DAMAGED. MARKED WITH GREEN TAPE.***SM EVAL REQ*** TEMPORARY REPAIR IAW EO-88400-REQ1 DEFERRAL REQUESTED. OPENOct 7, 2023 · N120UP · Airbus A300F4622R · Passenger Compartment EquipmentSDR IPXA2023092943606Unknown · unknownOPEN CEILING DAMAGE CENTER COVER PLATE PUNCTURED AND HONEYCOMB DAMAGED AT DOOR POSITION. REF M# 812723 POS AFT CARGO CEILING DOOR ENTRY. REMOVED & REPLACED MM-25-55-10.Sep 26, 2023 · N120UP · Airbus A300F4622R · Passenger Compartment EquipmentSDR IPXA2022082785670Bracket · crackedINSPECTION TYPE:1CLH WING FIXED T/E UPPER FAIRING SUPPORT STRUCTURE CRACKED LOCATED ON RIB 10.REMOVED, FABRICATED AND REPLACED PER SRM 51-40-21 AND SRM 57-51-11.Aug 27, 2022 · N120UP · Airbus A300* · Trailing Edge FlapsSDR IPXA2022082985728None · crackedINSPECTION TYPE:SEG#2 ENG PYLON ARC WEB REAR AT BUTTERFLY PANELS HAS CRACKS.WELD REPAIR PER SRM 54-50-00Aug 22, 2022 · N120UP · Airbus A300* · Nacelle/Pylon StructureSDR IPXA2022083085765Angle · crackedINSPECTION TYPE:SEGLH KRUEGER FLAP WELL WEB SUPPORT O/B OF THE ACTUATOR IS CRACKED.REMOVED AND REPLACED PER SRM 51-40-21Aug 21, 2022 · N120UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2022082985719None · crackedINSPECTION TYPE:SEGENG 2 FAIRING 485AL AFT SKIN I/B SIDE WITH 2EA CRACKS.WELD REPAIR PER EO A300-5450-21297-LAug 21, 2022 · N120UP · Airbus A300* · Nacelle/Pylon StructureSDR IPXA2022082985720Precooler · crackedINSPECTION TYPE:SEGENG 1 PRECOOLER PANEL 413BL HAS SEVERAL CRACKS.WELD REPAIR PER SRM 54-52-51Aug 20, 2022 · N120UP · Airbus A300* · Nacelle/Pylon StructureSDR IPXA2022083185792None · crackedINSPECTION TYPE:SEGCLIP CRACKED FOR SUPPORT AT FR 17 E&E COMPARTMENT.REMOVED AND REPLACED PER SRM 51-40-21Aug 19, 2022 · N120UP · Airbus A300* · Emergency ExitsSDR IPXA2022082985721Precooler · crackedINSPECTION TYPE:SEGENG 2 PRECOOLER PANEL 423BL HAS SEVERAL CRACKSWELD REPAIR PER SRM 54-52-51Aug 19, 2022 · N120UP · Airbus A300* · Nacelle/Pylon StructureSDR IPXA2022041181064None · dentedINSPECTION TYPE:N/ADENT WITH GOUGE IN AFT BULK CARGO DOOR FORWARD LOWER EDGEREPAIRED AFT BULK CARGO DOOR FORWARD LOWER EDGE IAW E.O A300-5230-83401Apr 11, 2022 · N120UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA2020121763540Door · stuckINSPECTION TYPE: N/A CAPT OPENED MAIN ENTRY DOOR WITH SLIDE LEVER ARMED. THE SLIDE WAS IMMEDIATELY DISARMED AND DID NOT INFLATE BUT THE DOOR WAS STUCK AND WOULD NOT OPEN OR CLOSE. DEPRESSURIZED FWD DOOR DAMPER & EMERGENCY OPERATIONS CYL DEF MAIN CABIN DOOR, Dec 16, 2020 · N120UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2020050354879Bearing · damagedINSPECTION TYPE:C, AIRCRAFT PITCH BEGAN FEELING HEAVY IN CLIMB. GOT PROGRESSIVE WORSE. APPROCH FLIGHT CONTROLS BEGAN EXTREMLY HEAVY. REMOVED AND REPLACED UPPER BEARING LH #5 RIB BELLCRANK IAW AMM 20-21-12-0001 AND IPC27-31-07-17A ITEM NR 200.May 2, 2020 · N120UP · Airbus A300F4622R · Elevator StructureSDR IPXA2020042954774Bearing · failedEMERGENCY DECLARED, AIRCRAFT PITCH BEGAN FEELING HEAVY IN CLIMB, GOT PROGRESSIVELY WORSE APPROACH FLIGHT CONTROLS BEGAN EXTREMELY HEAVY. UPON SAFE TAXI THE EMERGENCY WAS CANCELLED; NO EQUIP USED. REMOVED AND REPLACED UPPER BEARING ON LT NR 5 RIB BELLCRANK, Apr 28, 2020 · N120UP · Airbus A300F4622R · Elevator Control System
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