N401UP
Service difficulty reports · 299
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 = 'N401UP' 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 = 'N401UP' 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 IPXA2026102139239Smoke Goggles · deterioratedSECOND OBSERVERS SMOKE GOGGLES HAVE DETERIORATED FOAM SEAL. REMOVED AND REPLACED SECOND OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00.SDR IPXA2026102039239Smoke Goggles · deterioratedSECOND OBSERVERS SMOKE GOGGLES HAVE DETERIORATED FOAM SEAL. REMOVED AND REPLACED SECOND OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00.SDR IPXA2026092926582Evas Unit · inoperativeFOUND CAPT EVAS BAD. REMOVED AND REPLACED CAPT EVAS IAW AMM25-69.SDR IPXA2026092526582Evas Unit · failedFOUND CAPT EVAS BADSDR IPXA2026042783998Module · inoperativeEMERGENCY LIGHTS UNARMED WARNING LIGHT INOPERATIVE. REMOVED AND REPLACED MODULE AND LENS CAP FOR EMERGENCY LIGHT UNARMED LIGHT IAW AMM 33-13.SDR IPXA2025020571335Angle · corrodedAPU DOOR SURROUND BETWEEN FS 1790 - FS 1810 STR 6R ANGLE HAS SURFACE CORROSION ALL NUTPLATES ARE CORRODED WITH SCREW SHANKS STILL INSIDE. INSTALLED ANGLE LOWER DOOR STR 6 RH PER B757 SRM 51-40-02. REVIEWED.SDR IPXA2025020471181Angle · corrodedAPU DOOR SURROUND PN 148N3152-2 BETWEEN FS 1790 - 1810 STR 3R ANGLE HAS INTERGRANULAR CORROSION. INSTALLED ANGLE UPPER STR 3 RH SIDE PER B757 SRM 51-40-02. AUDIT COMPLETE.SDR IPXA2025020495767Strap · corrodedCLEAN CORROSION OFF OF STRAP AT FS 1825 S3R - S6R. ACCOMPLISH REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-80-15-2R-1, DETAIL I ON FIGURE 202 (SHEET 2).SDR IPXA2025012994882Door Frame · corrodedSEVERE CORROSION FOUND ON APU AIR INLET DOOR FRAME. INSTALLED NEW STRAP IAW B757-200, SRM 51-40-02. REVIEWEDSDR IPXA2025013155554Bracket · crackedNR 1 ENG PYLON NAC STA.149.5 FRAME I/B HAS ELONGATED HOLES AND 0,5 CRACK. EA-62. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INSTALLED NEW BRACKET ON FRAME ANGLE OF PYLON #1. IAW SRM 51-40-02-0G.SDR IPXA2025013142659Skin · crackedRH WING, FIXED L/E UPPER SKIN, UNDER SLAT #7 O/B, HAS 2,5 IN CRACK AFT PREVIOUS . EA-62. VERIFIED FINAL EA # 757-5741-27-A3772 REV WAS RECEIVED ACCOMPLISHED WITHOUT DEVIATIONS AND EO-92568-REQ1 WAS ACCOMPLISHED WITHOUT DEVIATIONS. OSD: 2/4/2025SDR IPXA2025020543514Tee Angle · corrodedFAULT-STR-ZONE 100. LH MID WING TO BODY STRUCTURE, T-CHORD AT STA 1080-1200, LBL 60 HAS CORROSION. DOT 28-01. INSTALLED NEW T-CHORD AT STA 1080-1200, LBL 60 IAW B757-200 SRM 51-40-02. REVIEWED.SDR IPXA2025020543758Tee Angle · corrodedRH WING TO BODY STRUCTURE, T-CHORD AT STA 1260, RBL 10 HAS LIGHT CORROSION. DOT 28-05. NEW T-CHORD IT IS FOUND TO BE INSTALLED IAW B757-200 SRM 51-40-02-0G-0.SDR IPXA2025020444461Bracket · crackedFS 900 LBL12 BRACKET THAT ATTACHES TO INTERCOSTAL TO 900 T-CHORD IS CRACKED INSTALLED NEW BRACKET ON STR FS 900 LBL12 IAW SRM 51-40-02.SDR IPXA2025020444699Tee Angle · corrodedFS 1037-1060 RBL 65 T-CHORD IS EXFOLIATED ON NUTPLATE EDGE. INSTALLED T-CHORD IAW B757-200, SRM 51-40-02 ON STR FS 1037-1060 RBL 65. PERFORMED CPCP STEPSSDR IPXA2025020443836Tee Angle · corroded.LH WING TO BODY STRUCTURE, T-CHORD AT STA 1020-1040, LBL 30 HAS LIGHT CORROSION. DOT 28-08. INSTALLED 8 NUTPLATE AND T-CHORD AT STA 1020-1040, LBL 30 IAW B757-200, SRM 51-40-02.SDR IPXA2025020443736Attach Bracket · crackedFS1180 LBL 13 ON BOTTOM OF FUSELAGE SKIN WTB STR ATTACH BRACKET HAS CRACK IB SIDE OF RADIUS. INSTALLED BRACKET AT FS 1180 LBL 13 OUTER FUSELAGE SKIN TO WTB STR IAW B757-200, SRM 51-40-02.SDR IPXA2025020444064Tee Fitting · corrodedFAULT-STR-ZONE 100. RH WING TO BODY STRUCTURE, T-CHORD AT STA 900-920, RBL 60 HAS CORROSION. DOT 28-10. INSTALLED T-CHORD AT STA 900-920 RBL 60 IAW B757 SRM51-40-02 HL P/N BACB30NX6K2 BACH #4244109 COLLAR P/N BACC30BL6 BACH # 4207142. REVIEWEDSDR IPXA2025020443668Tee Fitting · corrodedLH WING TO BODY STRUCTURE, T-CHORD AT STA 1040-1060, LBL 57 HAS LIGHT CORROSION . DOT 28-04. INSTALLED T-CHORD AT STA 1040-1060, LBL 57 LH WING TO BODY STRUCTURE, IAW B757-200, SRM 51-40-02.SDR IPXA2025013043970Tee Fitting · corrodedLH WING TO BODY STRUCTURE, T-CHORD AT STA 1020-1040, LBL 50 HAS 10 NUTPLATES CORRODED. DOT 28-09. INSTALLED T-CHORD AT STA 1020-1040, LBL 50 IAW B757-200, SRM 51-40-02. OSD: 1/31/2025SDR IPXA2025020443088Bracket · crackedFS 1180 RBL 13 OUTER FUSELAGE SKIN TO WTB STR BRACKET HAS CRACK ON IB RADIUS. INSTALLED BRACKET AT FS 1180 RBL 13 OUTER FUSELAGE SKIN TO WTB STR IAW B757-200, SRM 51-40-02.SDR IPXA2025020343798Tee Fitting · corrodedLOWER FUSELAGE STRUCTURE, T-CHORD AT STA 1020-1040, LBL 0, HAS CORROSION. VERIFIED INSTALLATION OF NEW T-CHORD AT STA 1020-1040 RBL 0. P/N BACB30NX8K12, BATCH 0004260079, QUANTITY 1EA. COLLAR P/N HL79-8, BATCH 0004088263, QUANTITY 1EA. RIVETS P/N MS20470AD6-6SDR IPXA2025020431025Skin · dentedR/H WING, #8 SLAT, UPPER SKIN WITH 8 DENTS (RED CIRCLE). DOT 73-004. RH SLAT#8 P/N 114N4004-172SP SERIAL:A2-0388 , INSTALLED IAW AMM TASK 27-81-02-424-021.SDR IPXA2025012012393Skin · damagedFUSELAJE ZONE 200 HAS EVIDENCE LIGHTNING STRIKE BETWEEN STA. 1320 TO 1440 (S11-S26). ACCOMPLISH REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-00-01-2R, REPAIR 28 PER SRM 53-60-01-2R-0.SDR IPXA2025013059623Skin · dentedFUSELAGE BETWEEN STA.1896.20 AND STA 1918.9 LEFT UPPER SIDE SKIN HAS DENT (NOT MAPPED). DOT 62-06. EA-62.ACCOMPLISH PERMANENT REPAIR PER 757-200PF SRM REV 121 CHAPTER 51-70-10-2R-4 FIGURE 201 SHEET 1 (REPAIRS TO LARGE DAMAGE) PER SRM 53-80-01-2R. OSD: 2/4/202SDR IPXA2025020765831Cam · gouged*SUPPLEMENTAL SDR* FAULT: STR Z837 - CREW ENTRY DOOR, UPPER AND LOWER LATCH CAM HAVE GOUGES. DOT 62-08. EA-62. VERIFIED SREO-14721-REQ001 REV1 WAS ACCOMPLISHED. REVIEWEDSDR IPXA2025020465996Angle · crackedNR 2 ENG STRAP AT NAC STA. 149.5 HAS CRACK AT HI-LOCK.DOT 69-003. EL-69. INSTALLED FRAME ANGLE IAW SRM 51-40-02-0G. AUDIT COMPLETE.SDR IPXA2025020465427Bracket · crackedFAULT:STR-Z400 #1 ENG PYLON HYD LINE BRACKET DAMAGED AT STRAP.NAC STA 149.5. DOT 69-001. EL-69. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INSTALLED NEW BRACKET ON FRAME ANGLE OF PYLON #1. IAW SRM 51-40-02-0G.SDR IPXA2025010865831Cam · gouged*SDR FILED OPEN* FAULT: STR Z837 - CREW ENTRY DOOR, UPPER AND LOWER LATCH CAM HAVE GOUGES. DOT 62-08. EA-62. APPROVED.SDR IPXA2025011351200Panel · crackedRT WING #8 SLAT OUTBD TRACK GAP PANEL IS CRACKED. DOT 8-010. RH SLAT#8 P/N 114N4004-172SP SERIAL:A2-0388 , INSTALLED IAW AMM TASK 27-81-02-424-021.SDR IPXA2024112636647Window · arcedR FWD WINDOW STARTED TO ARC. CHECK LIST SAID TO CONTINUE. WINDOW WAS NOT DEFORMED, AIR LEAK NOT OBSERVED. FL370. REMOVED AND REPLACED R1 WINDSHIELD REF MM 56-11-00-424-015. FINAL TORQUES COMPLETED. OPS CHECKS, INCLUDING WINDOW HEAT & WIPERS, PASSED, REF AMM 56SDR IPXA2024112236647Window · arcedRT FWD WINDOW STARTED TO ARC. CHECK LIST SAID TO CONTINUE. WINDOW WAS NOT DEFORMED, AIR LEAK NOT OBSERVED. FL370 REMOVED AND REPLACED R1 WINDSHIELD REF MM 56-11-00-424-015, UP TO AND INCLUDING STEP 3.E.(13).(A), FIRST TORQUE COMPLETED AT 11:45 AM LOCAL SDF TIMSDR IPXA2023030791651Flap · noneINSPECTION TYPE:N/A*A/C WAS OOS* *ATB* *EMER DECL* TE FLAPS DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS UP AT APPROX 1500 FT.REPL TORQ TUBE FOR RT INBD FLP OUTB TRNSMISSN PN 251N4281-21 AMM 27-51-25-201. AFT COUPLING FND DISCON CAUSING DAMAGE TO TUBE. FLP DAMASDR IPXA2023021190887Frame · noneINSPECTION TYPE:SEG1*MAJOR REPAIR* EXISTING REPAIR FOUND AT AFT CARGO COMPT FRAME STA 1360, S-26L.ACCOMPLISHED REPAIR PER UPS EO# B757-5310-85613-A AND EA# 757-5360-27-A3128 REV-SDR IPXA2023021190870Frame · noneINSPECTION TYPE:SEG1*MAJOR REPAIR* EXISTING REPAIR FOUND FRAME 1320, STR 25R TO 26R.ACCOMPLISHED REPAIR IAW UPS EO B757-5310-85615-ASDR IPXA2022062283383Battery Pack · inoperativeEMERGENCY LIGHTS INOP. EMERGENCY LIGHTS INOP.R/R BATTERY PACK PER AMM 33-51-07 OPS CHECK GOOD.SDR IPXA2021032067038Tee Fitting · corrodedINSPECTION TYPE:SEG4RH WTB FAIRING STRUCTURE TEE CHORD AT STA 1180-1186 RBL 30.75REMOVED AND REPLACED TEE CHORD IAW SRM 51-40-02-OGSDR IPXA2021032067037Tee Fitting · corrodedINSPECTION TYPE:SEG4RH WTB FAIRING STRUCTURE TEE CHORD AT STA 1180 RBL 20-30 HAS SEVERE CORROSIONREMOVED AND REPLACED TEE CHORD IAW SRM 51-40-02SDR IPXA2021032067033Stringer · corrodedINSPECTION TYPE:SEG4S-29L AT STA 1664 IS CORRODED AND REQUIRES REPAIRREPAIR AREA IAW SRM 53-00-03-2R-1SDR IPXA2021032067032Frame · dentedINSPECTION TYPE:SEG4FRAME LIP AT STA 660 STR24 RT LIP IS DELAMINATEDREPAIRED IAW SRM 53-00-07-2R-5 DETAIL IISDR IPXA2019122750421Evas Unit · looseCAPTAIN`S EVAS UNIT WAS LOOSE & NOT SECURED TO THE MANUAL BIN. REMOVED THE EVAS SYSTEM AND BRACKET DUE TO RIVETS PULLED THROUGH. PREPARED & INSTALLED THE ANCHOR PLATE & EVAS UNIT IAW EO B757-2560-45127-H, APPENDIX F, AND DRAWING 6307-5. REINSTALLED SERVICABLSDR IPXA2019122645354Engine · surgesATB - LT ENG SURGE AT 1300FT. TAKE OFF THRUST.RAN BOTH ENGINES AT EPR SETTING OF THE DAY AND PERFORMED FIM TASK 73-21-00-815-813-P00, NO DEFECTS NOTED, OK FOR SERVICE.SDR IPXA2019031239983Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 232XDF REQUIRES FAB. FABBED PANEL 232XDF FROM 5024N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.SDR IPXA2019031139952Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 232XEF REQUIRES FAB. FABBED PANEL 232 XEF FROM 2024N0000155-G,BATCH # 3441868 PER SREO B757=5320-9692-K.SDR IPXA2019031139951Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XBF REQUIRES FAB. FABBED PANEL 231XBF FROM 5024N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.SDR IPXA2019031139950Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XCF REQUIRES FAB. FABBED PANEL 231XCF FROM 504N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.SDR IPXA2019031139946Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XDF REQUIRES FAB. FABBED PANEL 231XDF FROM 5024N0000155-G,BATCH# 3441868 PER SREO B757-5320-9692-K.SDR IPXA2019031139945Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XEF REQUIRES FAB. FABBED PANEL 231XEF FROM 5024N0000155-G, BATCH# 3441868 PER SREO B757-5320-9692-K.SDR IPXA2019031139943Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XEF REQUIRES FAB. FABBED PANEL 231XEF FROM 5024N0000155-G, BATCH # 3441868 PER SREO B757-5320-9692-K.SDR IPXA2019031139942Floor Panel · damagedINSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 231XGF REQUIRES FAB. FABBED PANEL 231XGF FROM 50240000155-G, BATCH# 3441868 PER SREO B757-5320-9692.
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