N146UP
Service difficulty reports · 317
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 = 'N146UP' 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 = 'N146UP' 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 IPXA2026101946534Fitting · crackedFRAME 12A LT FITTING. 2 EA CRACK NOTED IN ZONE "A" (0.100") & (0.205") AND 1 EA CRACK NOTED IN ZONE "B" (0.130"). REPLACE THE DISCREPANT FITTING PRIOR TO FURTHER FLIGHT IAW EO-23539-REQ003. VERIFIED REMOVAL OF AIR CONDITION DUCTS TWO FR 12A LT. IAW SRM 51-40-SDR IPXA2026101633178Seat Track · corrodedAFTER DOG BONE REMOVAL ON TASK CARD T3F18E009MXK9 WERE FOUND SEVERAL SPOTS WITH CORROSION AT SEAT TRACK Y2462 (UNDER CHANNEL DRAIN) BETWEEN FR38 & FR38.2 REPAIR IAW: SRM REV 43 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201. THIS IS A CATEGORY A REPAIR AND NO FUSDR IPXA2026101934070Skin · crackedPANEL 485AL FWD OUTER ARA, RH SKIN IS CRACKED.SDR IPXA2026101834137Plate · damagedPANEL 485AL FWD INNER AREA, LH UPPER LONGERON HAS WEAR DAMAGE WITH MATERIAL LOSS. REPLACED FAIRING ATTACH PLATE ON PANEL 485AL FWD INNER AREA, LT UPPER, IAW SRM 54-55-51, AND 51-40-21.SDR IPXA2026092119481Handle · gougedCREW DOOR, EXTERNAL HANDLE HAS A GOUGE.SDR IPXA2026102149392Floor Panel · damagedFLOOR PANEL 147AF HAS A PUNCTURE/ DOT.130.066 INSPECTED AND VERIFIED FLOOR PANEL 147AF IS FABRICATED I.A.W SREO-16407-REQ001. FLOOR PANEL MATERIAL P/N 4417A400001CC-10 B/N 00441768507 QTY 1. GLUE P/N 04-001-0012 B/N 000446927 QTY 1KIT. EDGE FEELER P/N EC3515B/SDR IPXA2026102245620Fan Cowl · corrodedNR 1 ENG.I/B FAN COWL INNER EDGE SEAL FAN COWL HAS SURFACE CORROSIONS AND DEEP WEAR. VERIFIED REMOVAL OF RUB STRIP (INNER SEAL) ON THE #1 ENG.I/B FAN COWL IAW A300 SRM 51-40-21.SDR IPXA2026092949047Access Panel · brokenMAJOR REPAIR, ACESS PANEL 143DF HAS BROKEN AND DELAMINATED FIBER/ DOT.130.065SDR IPXA2026100338118Roller Track · corrodedFWD CARGO COMPARTMENT, FLOOR STRUCTURE FR 20 TO 25 RT AT -Y140, BALL MAT TRACK BASE OTBD AREA HAS SEVEN SPOTS OF CORROSION. THE SPOTS OF CORROSION BENEATH BALL MATS AT -Y140 BTW FR 20 & FR 25 HAVE BEEN IDENTIFIED & BLENDED OUT IAW SRM 53-10-15-101, FIG 103, ASDR IPXA2026100338127Roller Track · corrodedFWD CARGO FLOOR STRUCTURE, BALL MAT BASE HAS SEVERAL SPOTS OF CORROSION AT Y140 (LT) BETWEEN FR 20 & FR 25. BLEND OUT COMPLETED IAW A300-600 SRM 51-74-10/201, ALL SPOTS FOUND WITHIN LIMITS IAW SRM 53-10-15.SDR IPXA2026100437064Roller Track · corrodedFWD CARGO FLOOR STRUCTURE, BALL MAT BASE HAS SEVERAL SPOTS OF CORROSION AT Y140 (LT) BETWEEN FR 20 & FR 25. BLEND OUT COMPLETED IAW A300-600 SRM 51-74-10/201, ALL SPOTS FOUND WITHIN LIMITS IAW SRM 53-10-15.SDR IPXA2026100619943Floor Panel · damagedMAIN DECK FLOOR PANEL 231NJ HAS AN INSERT DAMAGED, DOT 78-13. FLOOR PANEL 231NJ IS FABRICATED IAW SREO-16407-REQ001.SDR IPXA2026101619802Seat Track · corrodedMDC RH SIDE, SEAT TRACK AT FR30 BETWEEN CROSSBEAM -Y2462 WITH CORROSION. VERIFIED ACCOMPLISHED SEAT TRACK SPLICE REPAIR AT FR27 TO FR33 -Y2462 IAW SRM 53-10-16-201, PARAGRAPH 4.C. <BR>FROM STEP 1 TO STEP 5, FIGURE 201, SRM 51-27-11-001 AND SRM 51-40-21-001.SDR IPXA2026092919935Floor Panel · damagedMAIN DECK FLOOR PANEL 232NJ DAMAGED.SDR IPXA2026092919943Floor Panel · damagedMAIN DECK FLOOR PANEL 231NJ HAS AN INSERT DAMAGED,SDR IPXA2026092919442Floor Panel · damaged-MAIN DECK FLOOR PANEL 231KJ HAS A CORNER DAMAGED.SDR IPXA2026092919354Floor Panel · damagedMAIN DECK FLOOR PANEL 232SG HAS ONE CORNER DAMAGED.SDR IPXA2026102206792Adapter · corrodedMAIN DECK FLOOR STRUCTURE, FR 61 Y0 RH CLS HAS CORROSION. INSTALLED OF CLS ADAPTER ON MDC FR61 Y0. R/H IAW SRM 51-41-21-001.SDR IPXA2026102206731Adapter · corrodedMAIN DECK FLOOR STRUCTURE, FR 65 RH BETWEEN -Y1456 AND -Y1959, CLS HAS CORROSION. VERIFIED INSTALLATION OF CLS ADAPTER ON MDC FR65 R/H -Y1456 AND -Y1959 IAW SRM 51-41-21-001.SDR IPXA2026092993314Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 261BH BROKE IN THE MIDDLE.SDR IPXA2026100251661Crossbeam · corrodedAFT CARGO COMPT. FRAME 54, Y953 - Y1959. CEILING SUPPORT WAS CORRODED. REMOVAL OF CORROSION FROM CEILING SUPPORT AT FR54 CROSSBEAM Y953 TO Y1959. IAW A300 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A300 SRM 51-73-11.SDR IPXA2026100252048Crossbeam · corrodedAFT CARGO BAY CEILING SUPPORT AT FR 56 - 57.2, BTWN Y 450 - Y953 WAS CORRODED. REMOVAL OF CORROSION FROM CEILING SUPPORT AT FR 56 TO FR 57.2 BETWEEN Y450 TO Y953 IAW A300 SRM 51-74-10.FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW A300 SRM 51-73-11.SDR IPXA2026100252060Crossbeam · corrodedAFT CARGO BAY, FR 57, Y0 - Y953, CEILING SUPPORT WAS CORRODED. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR57, Y0 TO Y953. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL LOSS IS .002 REMAINING MATERIAL IS .061 T98828.FOUND TO BE NEGLIGIBLSDR IPXA2026100653507Crossbeam · corrodedAFT CARGO BAY AT FR 62 BTWN Y 0 - Y 1959, CEILING SUPPORT HAS CORROSION. VERIFIED REMOVAL OF CORROSION FROM CEILING AT SUPPORT PANEL FR62, Y0 TO Y1959. IAW SRM 51-74-10.FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW SRM 51-73-11.SDR IPXA2026091951476Bracket · crackedAFT CARGO STR. FR 54 / Y-953 TOP BULKHEAD ATTACH L-SHAPE BRACKET HAS A CRACK. INSTALLED NEW BRACKET AT Z100 AFT CARGO FR 54 / Y-953 TOP BULKHEAD, IAW SRM 51-40-21.SDR IPXA2026101940236Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y953. REMOVAL OF CORROSION FROM CEILING SUPPORT PANEL FR57, -Y450 TO -Y95 FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW SRM 51-73-11.3. IAW A300 SRM 51-74-10.SDR IPXA2026101940166Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT BETWEEN FR56/FR57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y963. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR56/FR57 -Y450 TO -Y953. IAW A300 SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL LOSS ISDR IPXA2026102042390Crossbeam · corrodedFWD CARGO FR 34, BETWEEN -Y140 AND -Y805 CEILING SUPPORT HAS CORROSION. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 34, BETWEEN -Y140 AND -Y805. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063 MATERIAL LOSS IS .003 REMAING MATERIAL IR .060.FOSDR IPXA2026101940470Crossbeam · corrodedAFT CARGO COMPARTMENT, CEALING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959 HAS A SCREW HOLES WITH CORROSION. REMOVED CORROSION FROM CEILING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL SDR IPXA2026101941134Crossbeam · corrodedAFT CARGO COMPARTMENT, ANGLE SUPPORT OF SMOKE DETECTOR BOX AT FR62 CROSSBEAM Y0 WITH CORROSION. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR62, IAW A300 SRM 51-74-10. ORIGINAL MATERIAL THICKNESS IS .063- MATERIAL LOSS IS .001 REMAINING MATERIAL IS .062 TSDR IPXA2026101840963Crossbeam · crackedAFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 CROSSBEAM Y0 ANGLE SUPORT WITH CRACKED INSTALLED NEW ANGLE SUPPORT, AFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 Y0, IAW SRM 51-40-21.SDR IPXA2026101841001Support Angle · crackedAFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 CROSSBEAM Y963 ANGLE SUPORT WITH CRACK. INSTALLED NEW ANGLE SUPPORT, AFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 Y953, IAW SRM 51-40-21. REVIEWEDSDR IPXA2026101840973Support Angle · crackedAFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 CROSSBEAM Y1963 ANGLE SUPORT WITH CRACK. INSTALLED NEW ANGLE SUPPORT AT Z100, AFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 Y1959, IAW SRM 51-40-21.SDR IPXA2026100240470Crossbeam · corrodedAFT CARGO COMPARTMENT, CEALING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959 HAS A SCREW HOLES WITH CORROSION DOT 31-037 VERIFIED CIC APPLIED IAW EO-2780-REQ001<BR>JOB COMPLETE.SDR IPXA2026100240122Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 57 WITH SPOTS OF CORROSION FROM CROSSBEAM Y450 TO -Y450. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. SURFACE PROTECTION RESTORED IAW SRM 51-21-10, AND SRM 51-75-10.SDR IPXA2026100240236Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y953.SDR IPXA2026100240166Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT BTWN FR 56 - 57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y963.SDR IPXA2026100240462Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 54.2 AT CROSSBEAM -Y1959 HAD A SCREW HOLE WITH CORROSION. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. AFTER REWORK FOUND WITHIN LIMITS IAW SRM 51-73-11, NEGLIGIBLE DAMAGE, TREATED, PRIMED AND TOPCSDR IPXA2026100240510Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 57.1 AT CROSSBEAM -Y1959 HAD A SCREW HOLE CORRODED. REMOVED CORROSION FROM CEILING SUPPORT AT CEILING SUPPORT. RESTORED SURFACE PROTECTION IAW SRM 51-21-10, AND SRM 51-75-10.SDR IPXA2026100240360Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 58 WITH SPOTS OF CORROSION AT CROSSBEAM -Y450 TO -Y963.SDR IPXA2026100241134Support Angle · corrodedAFT CARGO COMPARTMENT, SUPPORT ANGLE OF SMOKE DETECTOR BOX AT FR 62, CROSSBEAM Y0 CORRODED. RESTORED SURFACE PROTECTION ON THE AFT CARGO BAY, SUPPORT ANGLE AT FR 62 CROSSBEAM Y0 IAW SRM 51-21-10 AND SRM 51-75-10.SDR IPXA2026100241943Support · corrodedFWD CARGO FR 38.2, BTWN Y805 AND -Y805 CEILING,LINING SUPPORT HAD FIVE SPOTS OF CORROSION. INSPECTED APPLIED ALODINE AND PRIMER IAW SRM 51-21-10-001, AND APPLIED PAINT IAW SRM 51-75-10-201.SDR IPXA2026100242382Crossbeam · corrodedFWD CARGO FR 38.1, BTWN Y805 AND Y1407, CEILING SUPPORT BRACKET WAS CORRODED. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. APPLIED ALODINE AND PRIMER IAW SRM 51-21-10-001 AND APPLIED PAINT IAW SRM 51-75-10-201. NO FURTHER ACTION REQUIRED.SDR IPXA2026100242390Crossbeam · corrodedFWD CARGO FR 34, BTWN -Y140 AND -Y805, CEILING SUPPORT WAS CORRODED.SDR IPXA2026100242469Crossbeam · corrodedFWD CARGO FR 34, BTWN Y140 - Y805, CEILING SUPPORT WAS CORRODED. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 34, BETWEEN Y140 AND Y805. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063 MATERIAL LOSS IS .003 REMAING MATERIAL IR .060.FOUND TO BESDR IPXA2026100240158Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 54.2 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y953 TO -Y1959, CEILING SUPPORT REMOVED AT FR 54.2 FROM CROSSBEAM -Y953 TO -Y1959 AFT CARGO COMPARTMENT IAW IAW A300-600 SRM 51-40-21.SDR IPXA2026100240574Crossbeam · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR58 FROM CROSSBEAM -Y450 TO -Y953 HAS A SPOTS WITH CORROSION, PROFILE CROSS T26/1880702 AND LOCATED AND DRILLED PROFILE CROSS IAW SRM 51-40-44-001.SDR IPXA2026100217405Stiffener · crackedLH WING, FLAP KRUEGER HAS A CRACK UNDERNEATH TEFLON ROLLER BASE , STIFFENER REMOVED AT LH WING, FLAP KRUEGER UNDERNEATH TEFLON ROLLER BASE IAW A300-600 SRM 51-40-21SDR IPXA2026100217425Bracket · crackedLH WING, FIXED LEADING EDGE, INSIDE FLAP KRUEGER COMPARTMENT I/B SIDE HAS A BRACKET WITH CRACK (DOT 64-018)SDR IPXA2026081072086Lamp · inoperativeEMERGENCY EXIT LIGHT HAS 2 EA LAMPS INOP. RELAMPED 2 EA EMER EXIT LIGHT LAMPS W/REF TO MM 33-51-13 PB 0401. OPS CK GOOD.
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