N160UP
Service difficulty reports · 181
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 = 'N160UP' 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 = 'N160UP' 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 IPXA2026080420489Controller · unserviceableAIR TURN BACK, ENG 1 BLEED LEAK RESULTING IN AIR TURN BACK FOUND LT WING MFA ILLUMINATED ON MX PANEL. INSPECTED WING PNEUMATIC JOINTS FROM PACK BAY OUT TO LT WING TIP. NO LEAKS NOTED IAW TSM 36-22-00/401. RAN NR 1 ENGINE, NO LEAK INDICATIONS. CHANGED NR 2 OVESDR IPXA2025031741931Door · damagedLIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 2€?AFT OF LE, 6€? OF OUTBD EDGE ADDRESSED AREA AS PER AMM 12-21-11.SDR IPXA2025031742006Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR. BLENDED AREA WITHIN ALLOWABLE LIMITS AND RESTORED FINISHED TO THE REQUIREMENTS OF SRM 53-10-12 REPAIR 6.SDR IPXA2025031741968Door · damagedLIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 1€?FWD OF AFT EDGE, 10€? FROM OUTBD EDGE. REPAIRED IAW SRM 53-10-12.SDR IPXA2025031741956Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING. PERFORMED A DVI AT STATION 2410 35 INCHES BELOW WING RIGHT HAND SIDE. AT ORANGE TAPE THERE WAS A BLACK SPECK ON FUSELAGE. WIPED ENTIRE AREA DOWN WITH ACETONE. NO LIGHTNING STRIKE NOTED ISDR IPXA2025031441931Skin · damagedLIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 2€?AFT OF LE, 6€? OF OUTBD EDGESDR IPXA2025031442006Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR.SDR IPXA2025031441968Skin · damagedLIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 1€?FWD OF AFT EDGE, 10€? FROM OUTBD EDGE.SDR IPXA2025031441956Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING.SDR IPXA2024102930903Adc · faultedECAM: NAV ADC FAULT 2 FAULT WAS INTERMITTENT EVERY 30 SECONDS / USE EMERGENCY CANCEL TO STOP AUDIO ALERT TROUBLESHOT PER TSM CH 34-10-00-101 FIGURE 103. PERFORMED BITE TEST OF ADC #2 BOX. NO FAULTS FOUND. PERFORMED BITE TEST OF ADC #2 SYSTEM PER AMM CH 34-10-0SDR IPXA2024081222135Hydraulic System · leaking**EMERGENCY DECLARED**ECAM GREEN HYD RES LO , FLUID QTY INDICATION LOSS OF FLUID. COMPLIED WITH ECAM / ARCH PROCEDURES SERVICED GREEN HYDRAULIC WITH 2 GALLONS REF AMM 12-12-29/0001SDR IPXA2024052191808Adapter · brokenFOUND BROKEN "CLS" ADAPTOR , RH FR19 BETWEEN MCD FLOOR PANELS 222DG AND 232EF REMOVED AND REPLACED CLS ADAPTER IN R/H FR 19 IAW A300 SRM 51-40-21 PARAGRAPH 7. P/N: B5377413820200 S/N: TAG 02036446. INSTALLED MCD FLOOR PANELS 222DE AND 232EF. IAW AMM 53-10-23-SDR IPXA2024052144309Support Angle · crackedFAULT -A300 OPEN Z200 - RH FR 37 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21 P/N HL11VF6-3 BATCH# 0004186230 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.SDR IPXA2024052144327Support Angle · crackedFAULT -A300 OPEN Z200 - RH FR 38.1 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED STIFFENER AT FRAME 38.1 R/H TO 38.2 R/H IAW SRM 51-40-21 P/N HL11VF6-3 BATCH #0004186230 P/N HL116-6 BATCH# 4279917 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.SDR IPXA2024052844359Support Angle · crackedRH FR 38.2 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED TREATED AND PRIMED NEW CUSP WEB IAW A300 SRM 51-21-10 PRIMER PN: 10P4-2NF BATCH: 8473297014 ALODINE1132 BATCH: 1445846. APPLIED TOPCOAT IAW A300 SRM 51-75-10-201 P/N ECL-G-101SDR IPXA2024052523679Cusp Web · brokenBROKEN CUSP WEB AT MCD LH FR 38.2 TREATED AND PRIMED NEW CUSP WEB IAW A300 SRM 51-21-10 PRIMER PN: 10P4-2NF BATCH: 8473297014 ALODINE1132 BATCH: 1445846. APPLIED TOPCOAT IAW A300 SRM 51-75-10-201 P/N ECL-G-101 BATCH: 4266626SDR IPXA2024052183546Floor Panel · damagedFWD CARGO FLOOR PANEL 131AH IS DAMAGED.SDR IPXA2024052183493Floor Panel · damaged- FWD CARGO FLOOR PANEL 131RG IS DAMAGED. COMPLETED SREO-16407-REQ002 ((APPX C). JOB IS NOW COMPLETE.SDR IPXA2024052183513Floorboard · brokenFWD CARGO FLOOR PANEL 131FE IS DAMAGED FABRICATED FWD CARGO FLOOR PANEL 131FE P/N B5327052700000 USING MATERIAL P/N 5024N400001SS-G BATCH:0004055277 I.A.W. SREO A300-5320-16407-E.SDR IPXA2024050283493Floor Panel · damagedFWD CARGO FLOOR PANEL 131RG IS DAMAGED APPROVED.SDR IPXA2024050283546Floor Panel · damagedFWD CARGO FLOOR PANEL 131AH IS DAMAGED REVIEWED.SDR IPXA2024050283513Floor Panel · damagedFWD CARGO FLOOR PANEL 131FE IS DAMAGED APPROVED.SDR IPXA2024061056443Repair · damagedRIGHT WING INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AT INNER FLAP IAW SRM 57-50-00-201. APPLIED TOP COAT AT REPAIR DOUBLER ON INNER FLAP IAW SRM 51-23-10-001. ACCOMPLISH A PERMANENT REPAIR PER SRM REV. 40, 57-50-00-201 PARAGRSDR IPXA2024050754126Floor Panel · crackedMAIN CARGO FLOOR PANEL 231LG HAS A CRACK UNDER PANEL.DOT 135/057 FABRICATED M.D.C. FLOOR PANEL 231LG PN: B5327073500000 USING MATERIAL PN:5024N400001SS-G BTCH: 0004055277 I.A.W. S.R.O.A300-5320-40552.SDR IPXA2024043056443Repair · damagedOPEN, RW INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER AND FILLED OUT MEASUREMENTSSDR IPXA2024042766820Floor Panel · brokenMAIN CARGO FLOOR PANEL 232WG FOUND TO BE CRACKED ON BOTTOM FABRICATED M.D.C. FLOOR PANEL 232WG PN: B5327074600400 USING MATERIAL PN:5024N400001SS-G BTCH: 0004055277 I.A.W. S.R.O.A300-5320-40552. INSTALLED FLOOR PANEL 232WG IAW A300 AMM 53-10-23-0401.SDR IPXA2024061087686Support Angle · corrodedFAULT - MXP-531535-01-1-151- AFT CARGO FR54 BLKHD RH UPPER ANGLE IS CORRODED DOT 5612-1 INSTALLED NEW AFT CARGO BLKH RIGHT UPPER ANGLE IAW SRM 51-40-21 REVIEWEDSDR IPXA2024042753612Support · corrodedAFT CARGO CEILING SUPPORT AT FR58 IS CORRODED. VERIFIED APPLICATION OF TOPCOAT ON CEILING SUPPORT AND OK TO INSTALL CEILING SUPPORT GIVEN INSP ONLY. INSTALLED CEILING SUPPORT IAW A300 SRM 51-40-21.SDR IPXA2024042753647Support · corrodedAFT CARGO CEILING SUPPORT AT FR54.2 IS CORRODED. TREATED AND PRIMED NEW CEILING SUPPPORTS (2EA) IAW SRM 51-21-10. INSTALLED 2EA CEILING SUPPORTS IAW SRM 51-40-21.SDR IPXA2024042753575Support · corrodedAFT CARGO CEILING SUPPORT AT FR57 IS CORRODED. TREATED AND PRIMED SUPPORTS IAW A300 SRM 51-21-10. INSTALLED 2EA CEILING SUPPORTS IAW SRM 51-40-21.SDR IPXA2024042753524Support · corrodedAFT CARGO CEILING SUPPORT AT FR62 IS CORRODED. TREATED AND PRIMED SUPPORT IAW SRM 51-21-10. INSTALLED CELING SUPPORT IAW SRM 51-40-21.SDR IPXA2024042937639Floor Panel · broken**SDR FILED OPEN** FAULT- MCD FLOOR PANEL 231WG IS BROKEN INSTALLED FLOOR PANEL 231WG IAW A300 AMM 53-10-23-0401.SDR IPXA2024042993716Angle · crackedACCESS AVIONICS AREA FRAME 10 Y-953 INTERCOASTAL HAS PREVIUOS REPAIR CRACKED 3 INCHS LONG IN THE CORNER NO DOT. INSTALLED 1EA. ANGLE P/N UPA53610270522 AND 1EA. WEB P/N UPA5361197720201 IAW SRM 51-40-21.SDR IPXA2024061071382Rib · crackedONE CRACK FOUND ON RIB FLANGE 17 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024051575400Shroud · gougedLEFT WINGTIP LE HAS A DENT FRONT INBD SIDE. APPLIED TREAT AND PRIMER IAW SRM 51-21-10 PARAGRAPH 2. INSTALLED NEW SHROUD ASSY IAW SRM 51-40-21, PARAGRAPH 13. INSTALLED STRIP IAW IAW SRM 51-40-21 PARAGRAPH 5. APPLIED TOP COAT IN AREA IAW SRM 51-75-10, PARAGRAPHSDR IPXA2024050271382Rib · cracked**SDR FILED OPEN** FAULT: 1 CRACK FOUND ON RIB FLANGE 17A RIGHT WING FLAP. VERIFIED STEP # 31 COMPLETED .SDR IPXA2024050271374Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 18 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024050271247Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 27 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024050271299Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 25 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024050271412Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 11 RIGHT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.SDR IPXA2024050271410Rib · crackedONE CRACK FOUND ON RIB FLANGE 12 RT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.SDR IPXA2024050271406Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 13 RT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024050271311Rib · crackedCRACK FOUND ON RIB FLANGE 19 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024050271279Rib · crackedONE CRACK FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024050271249Rib · crackedTWO CRACKS FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV-.SDR IPXA2024050271400Rib · crackedONE CRACK FOUND ON RIB FLANGE 15 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.SDR IPXA2024041371234Skin · crackedCRACK FOUND RIB FLANGE 27A LEFT FLAP TOP SKIN. ACCOMPLISH PERMANENT REPAIR PER EO-90102-REQ1 AND EA 300-5750-27-A3568 REV -.SDR IPXA2024052145562Cover Plate · crackedFAULT: CRACK FOUND ON FR40 R/W LOWER CORNER RADIUS AT 6 O'CLOCK POSITION FACING FORWARD. INSTALLEED REPAIR PARTS IAW DRAWING R53810798 REV C AND SRM 51-40-21 AND EO 64579-JIC004 REV 1. INSTALLED RIB AND INTERCOSTAL AT FR 40 L/E IAW SRM 51-40-21 AND EO 64579-JISDR IPXA2024052145527Cover Plate · crackedFAULT: MULTIPLE CRACKS FOUND ON F40 L/W LOWER RADIUS HOLE AROUND 9-11 O'CLOCK FACING FOWARD. INSTALLED REPAIR PARTS IAW DRAWING R53810798 REV C AND SRM 51-40-21 AND EO 64579-JIC003 REV 1. RE-INSTALLED RIB AND INTERCOSTAL AT FR 40 L/E IAW SRM 51-40-21 AND EO 64SDR IPXA2024042701079Skin · dented**SDR FILED OPEN**FAULT - LH OUTBOARD FLAP HAS DENT IN LEADING EDGE VERIFIED TOP COAT APPLICATION STEP 49.
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