N122UP

Service difficulty reports · 274

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 = 'N122UP' 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 IPXA2024020801203Floor Panel · crackedFWD CARGO FLOOR PANEL 132DE CRACKED DOT 146-161 FABBED PNL 132DE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWEDJan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024020804243Floor Panel · crackedAFT CARGO FLOOR PNL 151SF CRACKED DOT 146-181 FABBED PNL 151SF FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWEDJan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024022287857Angle · damagedDAMAGE ON HOLE E NEAR TOP OF THE HOLE ON LH FRAME 47 HORIZONTAL JUNCTIONAREA OF THE CWB LOWER ANGLE FITTING. ACCOMPLISH EO-89300-REQ1 AND EO 300-5710-27-A3498 REV. -. REVIEWEDJan 16, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024021287243Panel · damagedVERTICAL STABILIZER L/E PANEL322 AL EXTERNAL MIDDLE CTR COMPOSITE DAMAGED . 89-168 PANEL WAS DOCUMENTED FOR REMOVAL ON TWO NRC'S. PANEL WILL BE REINSTALLED ON NRC T#F18E003S5ZL / 6100408536.Jan 16, 2024 · N122UP · Airbus A300F4622R · Vertical Stabilizer, Plate/SkinSDR IPXA2024021287366Panel · damagedVERTICAL STABILIZER LE PANEL 322AL , 322BL ,ALLUMINIUM BONDED COVER AT LE HAS APPEAR TO HAVE DENTS AT SEVERAL PLACECS . 89-171 INSTALLED VERTICAL STAB LEADING EDGE PANELS 322AL, 322BL, IAW A300 AMM 53-32-11/401 VERIFIED.Jan 16, 2024 · N122UP · Airbus A300F4622R · Vertical Stabilizer, Plate/SkinSDR IPXA2024011787857Frame · damaged*** SDR FILED OPEN *** FAULT: DAMAGE ON HOLE E NEAR TOP OF THE HOLE ON LH FRAME 47 HORIZONTAL JUNCTIONAREA OF THE CWB LOWER ANGLE FITTING.Jan 16, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024011787243Panel · damaged*** SDR FILED OPEN *** FAULT - VERTICAL STABILIZER L/E PANEL322 AL EXTERNAL MIDDLE CTR COMPOSITE DAMAGED . 89-168Jan 16, 2024 · N122UP · Airbus A300F4622R · Vertical Stabilizer, Plate/SkinSDR IPXA2024011787366Panel · dented*** SDR FILED OPEN *** FAULT - VERTICAL STABILIZER LE PANEL 322AL , 322BL ,ALLUMINIUM BONDED COVER AT LE HAS APPEAR TO HAVE DENTS AT SEVERAL PLACECS . 89-171Jan 16, 2024 · N122UP · Airbus A300F4622R · Vertical Stabilizer, Plate/SkinSDR IPXA2024020642707Floor Panel · cracked-CARGO MAIN DECK, FLOOR PANEL 221EG HAS DELAMINATION 1. FABRICATED PANEL 221EG FROM 5024N40000155-G BATCH# 4055277 PER SREO-A300-5320-16407-EJan 15, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024013042960Angle · crackedACCESS PANEL 672AB ANGLE CONDUCTOR CRAKED DOT 146-120 REMOVED AND REPLACED ANGLE CONDUCTOR. IAW A300-600 SRM 51-40-21.Jan 15, 2024 · N122UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2024013142969Angle · crackedFAULT-ACCESS PANEL 672LB ANGLE CONDUCTOR CRACKED DOT 146-121 REMOVED AND REPLACED ANGLE CONDUCTOR. IAW A300-600 SRM 51-40-21.Jan 15, 2024 · N122UP · Airbus A300F4622R · Wing StructureSDR IPXA2024013102960Angle · crackedFAULT-ACCESS PANEL 672AB ANGLE CONDUCTOR CRAKED DOT 146-120 VERIFIED FABRICATEDJan 15, 2024 · N122UP · Airbus A300F4622R · Wing StructureSDR IPXA2024013042917Angle · crackedFAULT-ACCESS PANEL 672GB ANGLE CONDUCTOR CRACKED DOT 146-119 REMOVED AND REPLACED ANGLE CONDUCTOR IAW SRM 51-40-21Jan 15, 2024 · N122UP · Airbus A300F4622R · Wing StructureSDR IPXA2024013042671Angle · crackedACCESS PANEL 672CB ANGLE CONDUCTOR CRACKED DOT 146-111 REMOVED AND REPLACED ANGLE CONDUCTOR IAW SRM 51-40-21Jan 15, 2024 · N122UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2024012342212Seat Track · corrodedSEAT TRACK AT FRAME 80 RBL -450 IS EXFOLIATED INSTALLED 1EA. SEAT TRACK REPAIR SECTION AND 2 EA. SPLICE ANGLES AT FRAME 78.10 TO 80 AT -Y450 IAW SRM 51-10-16 REPAIR 201 AND SRM 51-40-23 (P/N HL10VF8-5 AND HL10VF6-5) REVIEWEDJan 15, 2024 · N122UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024013031634Frame · damagedCRACK FOUND IN FASTENER HOLE ON LEFT WING FRAME 40 LOWER RADIUS. ROTO PERFORMED ON LEFT WING FRAME 40 LOWER RADIUS FASTENER HOLE. DAMAGE STILL PRESENT IN HOLE, IAW 51-10-01. T96525 T91779. ROTO PERFORMED ON LH FRAME 40 LOWER RADIUS FASTENER HOLE. NO DEFECTS FOJan 14, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024013031632Frame · damagedL/H FRAME 40 LOWER JUNCTION FASTENERS HAVE TWO HOLES WITH DAMAGE/CRACK INDICATIONS. MIDDLE HOLE (DAMAGE) BOTTOM HOLE (CRACK). ROTO PERFORMED ON LH FRAME 40 LOWER JUNCTION. MIDDLE HOLE IS FREE OF DEFECTS. BOTTOM HOLE STILL WITH DAMAGE, IAW 51-10-01. T96525 T917Jan 14, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024013031689Frame · damagedR/H FRAME 40 LOWER JUNCTION HAS TWO FASTENER HOLES WITH DAMAGE. (TOP HOLE AND BOTTOM HOLES) ROTO PERFORMED ON RH FRAME 40 LOWER FASTENER HOLES. BOTTOM HOLE IS GOOD, TOP HOLE HAS DAMAGE. IAW 51-10-01. T96525 T91779. PER E0-61305-JIC0004-REV 1 TOP HOLE NOT TO BEJan 14, 2024 · N122UP · Airbus A300F4622R · Wing SparSDR IPXA2024013031680Frame · damagedDAMAGE FOUND IN MIDDLE HOLE ON RIGHT WING FRAME 40 LOWER JUNCTION. ROTO PERFORMED ON RIGHT WING MIDDLE HOLE FASTENER FRAME 40 LOWER JUNCTION. DAMAGE STILL PRESENT IN HOLE, IAW 51-10-01. T96525 T91779. ROTO PERFORMED ON FRAME 40 LOWER JUNCTION RH MIDDLE HOLE. NJan 14, 2024 · N122UP · Airbus A300F4622R · Wing SparSDR IPXA2024013131634Frame · damaged*** SDR FILED OPEN *** FAULT: CRACK FOUND IN FASTENER HOLE ON LEFT WING FRAME 40 LOWER RADIUS. VERIFIEDJan 14, 2024 · N122UP · Airbus A300F4622R · Wing SparSDR IPXA2024013131632Frame · damaged*** SDR FILED OPEN *** FAULT: L/H FRAME 40 LOWER JUNCTION FASTENERS HAVE TWO HOLES WITH DAMAGE/CRACK INDICATIONS. MIDDLE HOLE (DAMAGE) BOTTOM HOLE (CRACK). STEP #7 VERIFIEDJan 14, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024020822908Bracket · corrodedCARGO MAIN DECK FLOOR, SKIN UNDER PANEL 231VG HAS CORROSION.DOT119-013 INSTALLED THRUST BRACKET IAW A300-600 SRM 51-40-21 CIC APPLIED IAW EO NO: M-5100-2780-L REVIEWEDJan 13, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024021522802Adapter · corrodedCARGO MAIN DECK FLOOR , SKIN UNDER FLOOR PANELS 231MJ-231LG-231RG-231WG-231BH HAS CORROSION BETWEEN FR16A AND FR31.DOT119-011. REMOVED CORROSION AT MCD UNDER FLOOR PANELS 231MJ, 231LG, 231RG, 231WG AND 231BH BETWEEN FR16A TO FR31. IAW A300-600 SRM 51-74-10. MJan 13, 2024 · N122UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024020822614Hinge · damaged44 DAMAGE HOLES ON PIANO HINGE FITTINGS. INSTALLED HINGES AT 3 LOCATIONS IAW SRM 51-40-21 AND IPC 52-36-12-14Jan 13, 2024 · N122UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2024020922908Bracket · corroded*SDR FILED OPEN* FAULT-CARGO MAIN DECK FLOOR, SKIN UNDER PANEL 231VG HAS CORROSION.DOT119-013 AUDIT COMPLETEDJan 13, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2024020622887Floor Panel · puncturedCARGO MAIN DECK, FLOOR PANEL 231VG HAS PUNCTURE.DOT119-012 1. FABRICATED PANEL 231VG FROM 5024N4D000155-G BATCH# 4055277 PER SREO A300-5320-40552-B.Jan 13, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024020123653Adapter · corrodedRH MAIN DECK SEAT TRACK ADAPTER WITH SURFACE CORROSION AT FR31 AND Y0 DOT 146-077 INSTALLED SEAT TRACK ADAPTER AT FR 31, Y O. P/N EN6114V4-15, BATCH # 0004191764. P/N HL70-8, BATCH # 0004212587. IAW SRM 51-40-21.Jan 13, 2024 · N122UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024013026774Access Door · damagedTAIL APU RH ACCESS DOOR SKIN BENT AND CRACKED AFT END DOT 146-080APPLIED TREAT AND PRIME IN AREA CUT, DOUBLER AND FILLER. IAW A300-600 SRM 51-21-10. INSTALLED DOUBLER AND FILLER. IAW A300-600 SRM 52-41-11, FIGURE 202 AND SRM 51-40-21Jan 13, 2024 · N122UP · Airbus A300F4622R · Auxiliary Power Unit (APU) DoorsSDR IPXA2024013011834Frame · damagedMIDDLE HOLE ON FRAME 40 LH UPPER TENSION BOLTS HAS DAMAGE AT THE BACK OF THE HOLE. CLEANED HOLE IAW-SRM-51-40-44. ROTO PERFORMED ON FRAME 40 L/H UPPER TENSION MIDDLE HOLE. NO DEFECTS FOUND IAW 51-10-01 T96525 T91779Jan 12, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024013011803Frame · damagedTOP HOLE ON FRAME 40 RH UPPER TENSION BOLT HAS DAMAGE AT THE BACK OF THE HOLE. ROTO PERFORMED ON FRAME 40 RH UPPER TOP HOLE WITH DAMAGE. NO DEFECTS FOUND IAW 51-10-01. T96525 T91779. WOR COMPLETED ON EO MXP-571039-01-1-138-JICJan 12, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024020115612Adapter · corrodedRH MAIN DECK SEAT TRACK ADAPTER WITH SURFACE CORROSION AT FR38.1 AND Y0 DOT 146-074 ACCOMPLISH PERMANENT REPAIR PER UPS EO-89244-REQ1. REVIEWEDJan 12, 2024 · N122UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA202401311834Frame · damaged*** SDR FILED OPEN *** FAULT: MIDDLE HOLE ON FRAME 40 LH UPPER TENSION BOLTS HAS DAMAGE AT THE BACK OF THE HOLE. VERIFIEDJan 12, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA202401311803Frame · damaged*** SDR FILED OPEN *** FAULT: TOP HOLE ON FRAME 40 RH UPPER TENSION BOLT HAS DAMAGE AT THE BACK OF THE HOLE. VERIFIEDJan 12, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024012380670Stiffener · crackedLOWER FR 91 TO 92 SECTION C68 LOWER RIB SIDEWALL BETWEEN C67 AND C68 CRACKED ON TOP AT MIDDLE SECTION DOT 101- 120 INSTALLED WEB STIFFENER IAW A300-600 SRM 51-40-21 REVIEWEDJan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024021092062Skin · crackedTHE R/H CENTER FLAP HAS 1 EA CRACK AT RIB 27 AFT SIDE ON STR 2.1. ACCOMPLISH PERMANENT REPAIR PER EA 300-5750-27-A3483 REV. - AND EO-89185-REQ1.Jan 11, 2024 · N122UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024021295267Door · crackedLT WING #1 SLAT INBD SLAT DRIVE RETRACTABLE DOOR IS CRACK. PERFORMED SURFACE HFEC INSP OF THE L/H WING #1 SLAT INBD DRIVE RETRACTABLE DOOR IAW A300 NTM PART 6 51-10-08. THE SURFACE AREA OF THE DOOR IS CRACK / DEFECT FREE AT THIS TIME. NDT COMPLETE. INSP ONLY. Jan 11, 2024 · N122UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024020195540Web · bentFUS STRUCTURE FR86 TO FR87 LH WEB ( INTERCOSTAL) BENT DOT 146-052 REPAIRED INTERNAL STRUCTURE FR 86 TO FR 87 INTERCOSTAL BENT IAW E.O.: M-5100-41097-C. APPLIED C.I.C. AT FUS. LH INTERNAL STRUCTURE FR86 TO FR87 INTERCOSTAL I.A.W. E.O. M-5100-278-L.Jan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024020181248Floor Support · corrodedR/H FWD CARGO FLOOR RBL 0 STA.2029/FR31 - STA.2082/FR32 HAS CORROSION. DOT 33-003 CLEANED AREA FWD CARGO DOOR FLOOR BOTTOM RBL-0, FR31- FR32. AFTER EVALUATION IN THE AREA NOT DAMAGE FOUND IAW SRM 51-78-00.Jan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024012395489Plate · cracked*** SUPPLEMENTAL SDR *** AFT CARGO DOOR CUTOUT PLATE CRACKED (AFT ZONE ) DOT 041 INSTALLED NEW CUTOUT PLATE P/N: F5347537320600 AND NEW SUPPORT ASSY P/N: F5397134701000 AT AFT. CARGO DOOR (AFT. ZONE) I.A.W. A300-600 S.R.M. 51-40-21.Jan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024011295489Unknown · unknown*SDR FILED OPEN* AFT CARGO DOOR CUTOUT PLATE CRACKED (AFT ZONE ) DOT 041 APPROVEDJan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2024011295540Unknown · unknown*SDR FILED OPEN* FAULT-FUS STRUCTURE FR86 TO FR87 LH WEB ( INTERCOSTAL) BENT DOT 146-052 APPROVEDJan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024011295267Unknown · unknown*SDR FILED OPEN* FAULT:AA014 -LT WING #1 SLAT INBD SLAT DRIVE RETRACTABLE DOOR IS CRACK. APPROVEDJan 11, 2024 · N122UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024011180670Unknown · unknown*SDR FILED OPEN* FAULT: LOWER FR 91 TO 92 SECTION C68 LOWER RIB SIDEWALL BETWEEN C67 AND C68 CRACKED ON TOP AT MIDDLE SECTION DOT 101- 120Jan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024011181248Unknown · unknown*SDR FILED OPEN* FAULT: R/H FWD CARGO FLOOR RBL 0 STA.2029/FR31 - STA.2082/FR32 HAS CORROSION. DOT 33-003Jan 11, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024020875857Sleeve · debondedENG#2 T/R O/B SLEEVE FWD, EDGE DISBONDING. DOT 641/11 INSTALLED 02 TRANSLATING SLEEVE EDGE PROTECTOR ON ENGINE #2 T/R, O/B, IAW SRM 51-40-21.Jan 10, 2024 · N122UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2024013176121Bracket · crackedFAULT: UNDER FLIGHT DECK IN AVIONICS BAY, R/H CORNER ABOVE O2 BOTTLES, CORNER BRACKET TO DECK SUPPORT IS CRACKED. DOT 60-001 INSTALLED NEW BRACKET USING FASTENER P/N: HL18PB5-3, BATCH NO: 0004146161 IAW SRM 51-40-21Jan 10, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024013175620Angle · dentedFAULT, ENG#2 T/R I/B FWD BOTTOM IN THE CORNER, DENT DOT 641/07 INSTALLED ANGLE AT #2 ENG. T/R I/B FWD FRAME. IAW A300-600 PW4000 SRM 54-04-01.Jan 10, 2024 · N122UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2024021346432Frame Splice · damagedFR 47 RH SPLICE FITTING HAS 2 HOLES DAMAGED AT THE BACK OF HOLE. AREAS MARKED IN RED. ROTO PERFORMED ON FRAME 47 RH SPLICE FITTINGS. BOTH HOLES A & E ARE FREE OF DEFECTS, IAW 51-10-01. T96525 T91779. T96515 T91779. FASTENERS WILL BE INSTALLED ON THE EO-18288-JJan 9, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024021246511Frame · damaged4 DAMAGED HOLES (2 L/H) (2 R/H) AT SPLICING AT FRAME 17 AND MAIN DECK FLOOR BEAM ATTACHMENT. AREAS MARKED IN RED. ROTO PERFORMED ON FRAME 17 HOLES. ALL HOLES ARE FREE OF DEFECTS, IAW 51-10-01. T96525 T91779Jan 9, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024011046432Unknown · unknownFR 47 RH SPLICE FITTING HAS 2 HOLES DAMAGED AT THE BACK OF HOLE. AREAS MARKED IN RED. ROTO PERFORMED ON FRAME 47 RH SPLICE FITTINGS. BOTH HOLES A & E ARE FREE OF DEFECTS, IAW 51-10-01. T96525 T91779. T96515 T91779Jan 9, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, Structure
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