N128UP
Service difficulty reports · 214
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 = 'N128UP' 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.
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 = 'N128UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA2026020329998Engine · bird ingestionSUSPECTED BIRD STRIKE DURING TAKE OFF. ENG #2 N1 VIBRATION REACHED 7.5 DURING CLIMBOUT. REPLACED FAN BLADES ON #2 ENG ACCOMPLISHED ENG RUN OPS CK NORMAL.SDR IPXA2026013029998Engine · vibrationAIR TURN BACK. SUSPECTED BIRD STRIKE DURING TAKE OFF. ENG NR 2 N1 VIBRATION REACHED 7.5 DURING CLIMBOUT, C/W BIRDSTRIKE INSPECTION FOR ENGINE IAW AMM 05-51-19/0001 AND 72-00-00/601 PARA. 21. SEE T3F18E0086DCU AND T3F18E0086CV5 FOR FINDINGS.SDR IPXA2025030910596Limiter · faulted*EMERGENCY DECLARED* SLAT SYS#1 &SLAT SYS #2 FAULT FLAPS OPERATED NORMAL LANDED 0 SLATS 40 FLAPS INSTALLED NEW TORQUE LIMITER PER AMM 27-84-12/401. OP€™S CHECK€™S GOOD.SDR IPXA2024040117865Shear Plate · crackedCRACK FOUND AT FWD SIDE OF FRAME 65 STR 42 ON INTERCOSTAL. INSTALLED SHEAR PLATE AT FWD SIDE OF FRAME 65 STR 42 IAW A300 SRM 51-40-21 PARAGRAPH 6 AND 7.SDR IPXA2024040221180Rib · crackedZONE 513 LT WING, FWD WING ROOT STA71/RIB2 LEADING EDGE RIB HAS A CRACK. INSTALLED REINFORCED ANGLE P/N: A5724199320200 AT FWD WING ROOT RH RIB 2. IAW SRM 51-40-21.SDR IPXA2024041502252Frame · damagedHOLES A & S HAVE DAMAGE INDICATIONS. HOLES B, F, AND P HAVE CRACK INDICATIONS ON FR 47 LH HORIZONTAL JUNCTION. COMPLIED WITH UPS EO: EO-90000-REQ1 AND VT MAE FINAL EA 300-5710-27-A3547 REV.SDR IPXA2024041102178Skin · crackedHOLES C AND E HAVE DAMAGE INDICATIONS. HOLE B HAS A CRACK AT 5'OCLOCK POSTION FACING FWD ON RH FR47 HORIZONTAL JUNCTION. REVIEWEDSDR IPXA2024040178433Floor Panel · crackedMCD FLOOR PANEL 251VJ IS DAMAGED. FABBED PANEL 251VJ FROM 5024N40000SS-G,BATCH #40552-B PER SREO -40552-REQ001 (APPX B).SDR IPXA2024040177288Floor Panel · crackedMCD FLOOR PANEL 251ZF IS DAMAGED. FABBED PANEL 251ZF FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).SDR IPXA2024040177370Floor Panel · crackedMCD FLOOR PANEL 242KN IS DAMAGED. FABBED PANEL 242KN FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).SDR IPXA2024040169755Floor Panel · crackedMCD FLOOR PANEL 232LF IS DAMAGED FABBED PANEL 232LF FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).SDR IPXA2024040169921Floor Panel · crackedMCDFLOOR PANEL 221E IS DAMAGED FABBED PANEL 221EG FROM 5024N400001SS-G ,BATCH #4055277 PER SREO-40552-REQ001 ((APPX B)SDR IPXA2024040846502Frame · damagedDAMAGE FOUND ON BOTTOM HOLE ON FR 40 RH LOWER JUNCTION FASTENERS. COMPLIED WITH UPS EO-89994-REQ1 AND VTMAE FINAL EA 300-5710-27-A3542 REV-.SDR IPXA2024033025126Floor Panel · crackedMCD FLOOR PANEL 231MJ IS DAMAGED. FABBED PANEL 231MJ FROM 5024N400001SS-G, BATCH # 4055277 PER SREO-40552-REQ001 (APPX B).SDR IPXA2024040121999Floor Panel · crackedMCD FLOOR PANEL 241AQ IS DAMAGED FABBED PANEL 241AQ FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).SDR IPXA2024040125736Floor Panel · crackedMCD FLOOR PANEL 232QH IS DAMAGED FABBED PANEL 232QH FROM 5024N400001SS-G BATCH#4055277 PER SREO-40552-REQ001 (APPX B).SDR IPXA2024032525309Panel · crackedR/H WING ROOT UNDER PANEL 613AB, SKIN IS CRACKED BY NUTPLATE. INSTALLED DOUBLER AT R/H WING ROOT UNDER PANEL 613AB, IAW SRM 53-15-53 AND SRM 51-40-21. APPLIED TOP COAT AT EXTERNAL DOUBLER AT R/H WING ROOT UNDER PANEL 613AB. IAW SRM 51-23-10.SDR IPXA2024040102721Floor Panel · damagedMAJOR REPAIR MCD FLOOR PANEL 261KF HAS (1EA) BROKEN INSERT. FABBED PANEL 261KF FROM 5024N400001SS-G BATCH # 4055277. PER SREO- 40552-REQ001(APPX B).SDR IPXA2024032064596Floor Support · corrodedFAULT: FLOOR STRUCTURE IN FRONT OF LAV HAS CORROSION ON TOP OF BEAM, BENEATH PANEL 221TF. DOT 60-047 INSTALLED FLOOR BEAM SUPPORT IAW SRM 51-40-21-001SDR IPXA2024040157286Fitting · cracked*** SUPPLEMENTAL SDR *** FAULT: CRACK FOUND AT 10 O'CLOCK POSITION FACING AFT AT FR40 LOWER JUNCTION RH SIDE. APPLIED PROTECTION SURFACE ON FASTENERS HEAD IAW SRM 51-23-10. (8 OZ PAINT CUP #02-012-176) AND APPLIED CIC IAW EO: M-5100-2780-L ON STIFFENER AT FR 4SDR IPXA2024032057068Support Bracket · crackedAFT CARGO BULKHEAD FRAME 54 HAS A CRACKED FLOOR SUPPORT BRACKET L/H SIDE. DOT 60-043 INSTALLED BRACKET SUPPORT IAW SRM 51-40-21-001 .SDR IPXA2024040826401Frame · damagedTOP HOLE RH SIDE ON FR17 HAS DAMAGE THROUGHOUT HOLE. INSTALLED SHACKLE AT FR 17 RH, IAW SRM 51-40-21.SDR IPXA2024032231515Crossbeam · corrodedFAULT: AFT CARGO AT FR65, FLOOR BEAM HAS CORROSION. (EXFOLIATION) DOT 60-045 INSTALLED T-PROFILE AND ANGLES REPAIR IAW SRM 51-10-15 PARAGRAPH 11. INSTALLED FILLER BEAM IAW SRM 51-40-21.SDR IPXA2024041663795Frame Splice · damagedMAJOR REPAIR, HOLES A,B,E,F,L,M & N ALL HAVE DAMAGE ON FRAME 47 LH SPLICE FITTING. AREAS MARKED IN RED. VERIFIED INSTALLATION OF FRAME SPLICE AT FR47 FROM S24 TO S26. COMPLIED WITH UPS EO-89765-REQ1 AND VTMAE FINAL EA 300-5315-27-A3531 REV 1SDR IPXA2023100613615Skin · damagedSTAND IMPACTED AIRCRAFT CREATING HOLE APPROX 4' BEHIND R/H MLG DOOR REMOVED DAMAGE IAW SRM 51-27-00. REPAIRED SKIN IAW EO-88377-REQ1. CW EOSDR IPXA2022122089173Apu · inoperativeINSPECTION TYPE:NA*EMERGENCY DECLARED* *DIVERSION* *LANDED WITHOUT FURTHER INCIDENT* AT FL360 (WITH GEN 2 DEFERRED)WE LOST APU AND APU GENERATOR,ATTEMTED APU RESTART WITHOUT SUCCESS. DIVERTED DUE TO ONE OPERATING GENERATOR.PERFROMED BITE CHK ON ECB, LOW OIL PRSDR IPXA2022081985397Indicator · inoperativeINSPECTION TYPE:N/A**ATB** - IMMEDIATELY AFTER TAKE OFF, HOT BRAKE MESSAGE AND LIGHT IN FAN SWITCH. LEFT TRUCK BRAKE TEMP WERE ALL HIGH WITH #5 AND #6 THE HIGHEST. #6 INDICATED 335^ GEAR WAS EXTENDED TO COOL BRAKES WITH VERY LITTLE EFFECT. THE LEFT TRUCK WHEESDR IPXA2022020478646None · noneINSPECTION TYPE:NA**SUPPLEMENTAL SDR** AIR TURN BACK DUE TO LOWER FWD CARGO DOOR OPEN INDICATION JUST AFTER TAKEOFF. BOTH ECAM AND SYSTEM PAGE CONFIRMED DOOR OPEN CABIN ALT COULD NOT BE VERIFIED DUE TO PHASE OF FLIGHT. DEFERRED CARGO DOOR INDICATION PER MEL 52SDR IPXA2021083173352Web · crackedINSPECTION TYPE:CAFTER PERFORMING ROTO PROBE INSP. PER NTM 57-10-29 FOUND A CRACK INDICATION AT CWB CENTER WEB SPAR REINFORMENT FR 44 LH CUT OUT DOUBLER BOTTOM HOLE AFT LAYER AT 12 O'CLOCK I/B BOTTOM HOLE FWD LAYER.REAMED HOLE TO .262 PER SRM 51-40-40.SDR IPXA2021083173351Web · crackedINSPECTION TYPE:CAFTER PERFORMING ROTO PROBE INSP. PER NTM 57-10-29 FOUND A CRACK INDICATION AT CWB CENTER WEB SPAR REINFORMENT FR 44 LH CUT OUT DOUBLER BOTTOM HOLE AFT LAYER AT 6 O'CLOCK O/B BOTTOM HOLE FWD LAYER.REAMED HOLE TO .262 PER SRM 51-40-40.SDR IPXA2021083173350Spar · crackedINSPECTION TYPE:CAFTER PERFORMING ROTO PROBE INSP. PER NTM 57-10-29 FOUND A CRACK INDICATION AT CWB CENTER WEB SPAR REINFORMENT FR 44 RH CUT OUT DOUBLER O/B BOTTOM HOLE FWD AND AFT LAYER AT 9 O'CLOCK.REAMED HOLE TO .276 PER SRM 51-40-40.SDR IPXA2021082873240Shear Tie · crackedINSPECTION TYPE:A300RH FR44 FRAME FOOT FITTING HAS A CRACKACCOMPLISHED REPAIR PER EO A300-5310-46789-G APPENDIX KSDR IPXA2021082773198Bracket · crackedINSPECTION TYPE:CAFT CARGO COMP. AT FWD BULHEAD FR54 FOUND 2EA BRACKETS CRACKED.REMOVED AND REPLACED 2EA BRACKETS PER SRM 51-40-21.SDR IPXA2021082873241Shear Tie · crackedINSPECTION TYPE:A300LH FR44 FRAME FOOT FITTING HAS A SIGN OF CRACKACCOMPLISHED REPAIR PER EO A300-5310-46789-G APPENDIX JSDR IPXA2021082773197Bracket · crackedINSPECTION TYPE:CAFT CARGO COMP. AT FWD BULHEAD FR54 FOUND 2EA BRACKETS CRACKED.REMOVED AND REPLACED 2EA BRACKETS PER SRM 51-40-21.SDR IPXA2021012864998Switch · failedINSPECTION TYPE: NA ATB-NO EMERGENCY DECLARED-LANDING UNEVENTFUL. ON CLIMB ECAM LOWER FWD CARGO DOOR OPEN MESSAGE. ACCOMPLISHED AIR TURN BACK ON INSPECTION FOUND AFT DOOR SILL MICRO SWITCH 14WS COVERED IN ICE, CLEANED MICRO SWITCH. REMOVED ALL ICE DEBRIS C/SDR IPXA2020071767840Stiffener · crackedLEFT WING TE STIFFENER CRACKED OUTBOARD OF NR 6 SPOILER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-21 AND SRM 51-40-44.SDR IPXA2020072087908Floor Panel · canningINSPECTION TYPE:A300COCKPIT FLOOR PANEL CO-PILOTS SDE OB BETWEEN SEAT AND CB PANEL HAS PREVIOUS REPAIR OR CANNINGREPAIRED IAW SRM 51-77-12 PAR 2 (2) FIG 202 SHEET 3SDR IPXA2020072087910Panel · chafedPANEL 147BZ FLANGE CHAFED. REMOVED AND REPLACED THE PANEL.SDR IPXA2020071757882Support Bracket · crackedRIGHT WING NR 3 SPOILER OTBD HINGE SUPPORT BRACKET WAS CRACKED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-21.SDR IPXA2020050454937Hinge · brokenINSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** FWD PASSENGER/ CREW DOOR PANEL # Z831 UPPER HINGE BROKEN. DEFERRED PER REF NEF 25-70-52-10-02 AMC # M706114 ORDER PARTS REQ # 309055.REMOVED SUPPORT ARM LINING. REPLACED UPPER & LOWER HINGES TO FLAP LINING & REINSTALLESDR IPXA2019052642494Floor Panel · puncturedINSPECTION TYPE:12Y MAIN CABIN FLOOR PANEL 242DN HAS A PUNCTURE ON UPPER SKIN. REPAIRED PER UPS REO A300-5320-42721-F.SDR IPXA2019052442432Rib · crackedINSPECTION TYPE:12YR L/W I/B FLAP NOSE RIB #16 IS CRACKED. REMOVED AND REPLACED RIB PER DWG #A57960058-200.SDR IPXA2019051942259Floor Panel · crackedINSPECTION TYPE:124C CRACKED/DELAMINATEDFABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07/29/2010.SDR IPXA2019051942258Floor Panel · crackedINSPECTION TYPE:124C CRACKED/DELAMINATEDFABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07-29-2010.SDR IPXA2019051942257Floor Panel · crackedINSPECTION TYPE:124C CRACKED / DELAMINATEDFABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07/29/2010.SDR IPXA2019051942256Floor Panel · crackedINSPECTION TYPE:124C CRACKED / DELAMINATED FABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07-29-2010.SDR IPXA2019051942255Floor Panel · crackedINSPECTION TYPE:12C CRACKED/DELAMINATEDFABRICATED FLOOOR PANEL IAW EO A300-5320-16407-E REV DATE 07/29/2010.SDR IPXA2019051342057Seat Track · corrodedINSPECTION TYPE:12YR MAIN CABIN SEAT TRACK AT FR 79-80 -Y450 IS CORRODED. REPAIRED PER SRM 53-10-16.SDR IPXA2019051342056Seat Track · corrodedINSPECTION TYPE:12YR MAIN CABIN SEAT TRACK AT FR 79-80 Y1794 IS CORRODED. REPAIRED PER SRM 53-10-16.
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