N393UP
Service difficulty reports · 52
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 = 'N393UP' 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 = 'N393UP' 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 IPXA2026102020598Sign · inoperativeDURING PSM FOUND EMERGENCY EXIT SIGN NEXT TO ENTRY DOOR NOT ILLUMINATING FIM 33-51 FT 805 REV. 149 FOLLOWED, PRESSED TEST BUTTON ON BATTERY PACK, NO LIGHTS ILLUMINATING. BATTERY PACK REPLACED IAW AMM 33-51-07/201 REV, 149 AND EMERGENCY LIGHTS TESTED SATISFACTOSDR IPXA2026101920598Battery Pack · inoperativeDURING PSM FOUND EMERGENCY EXIT SIGN NEXT TO ENTRY DOOR NOT ILLUMINATING FIM 33-51 FT 805 REV. 149 FOLLOWED, PRESSED TEST BUTTON ON BATTERY PACK, NO LIGHTS ILLUMINATING. BATTERY PACK REPLACED IAW AMM 33-51-07/201 REV, 149 AND EMERGENCY LIGHTS TESTED SATISFACTOSDR IPXA2026091744608Housing · cracked***MAJOR REPAIR*** FAULT - FOUND FUEL LEAK AT NO.2 SLAT OUTBD MAIN TRACK HOUSING DRAIN HOLE. ACCOMPLISHED THE REPAIR I.A.W UPS EO-98615-REQ1 REV1 AND BOEING DWG NO. 112T2001 SH 21 REV: D.SDR IPXA2026082995025Blowout Door · chafedCHAFED SKIN OF NR 1 ENG RT THRUST REVERSER LOWER BLOWOUT DOOR INNER L/E AREA. INSTALLED NEW BLOWOUT DOOR IAW SRM 51-40-02-0G, REV 132, & AIPC 78-31-51-03, REV 40, IPC 78-32-22, REV 96, & AMM 78-31-19-402-008, REV 149.SDR IPXA2026082995720Former · crackedCRACKED FORMER , RT WING OTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 456. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 132, DWG 114T2202, SH 1, REV D, AND SREO-57209-REQ001, REV 2.SDR IPXA2026082994280Longeron · chafedCHAFED LONGERON, NR 1 ENG LT CORE COWL AFT LWR AREA. INSTALL A NEW LONGERON IAW SRM 51-40-02-0G, REV 132, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026082995671Former · crackedCRACKED FORMER , RT WING OTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 499. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 132, & DWG 114T2511, SH 1, REV D, SREO-50900-REQ001, REV 2.SDR IPXA2026091681129Panel · wornWORN - HOLE, RT WING NR 8 SLAT INBD SIDE LWR CLOSURE DOOR. (REPAIR). IAW SRM 57-43-01-2R-3 REFER TO SRM 51-70-08-0G-0 REV. 132 PERFORM REPAIR AS BELOW STEP:1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE SIZE AND LOCATION ( L : 0.3", W : 0.2"SDR IPXA2026090377741Skin · debondedDEBONDED SKIN, INBD EDGE UPPER FACE OF LT WING T/E OTBD FLAP T/E SKIN , WBL 355. IAW SREO-70175-REQ001, REV 1, REMOVED THE CRACK AND CLEANED. MEASURE THE DAMAGE AREA L : 0.5", W : 0.01", 7" FROM TRAILING EDGE, AT INBD EDGE. BONDED THE REPAIR PLIES WITH RESDR IPXA2026082877723Skin · dentedDENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT DAMAGE AND CLEANED, MEASURE CUT OUT DIA 0.8", FROM FWD EDGE 27.5", AT 6 O'CLOCK ON INNER BARREL OF NR 2 ENG INLET COWL. BONDED THE SPACER WITH FILM ADHESIVE CURED AT 250 F FOR 2 HRS & FILLEDSDR IPXA2026082877089Skin · debondedDEBONDED LOWER SKIN OF LT WING T/E OTBD FLAP T/E SKIN, WBL 366. IAW SRM 57-53-01-2R-1 REF SRM 51-70-07-0G-0, REV 132. PERFORMED A REPAIR IAW STEP 1. REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION(DIA:1", 33.5" FROM INBD EDGE,SDR IPXA2026082877721Skin · debondedDEBONDED LOWER SKIN OF LT WING T/E OTBD FLAP T/E SKIN WBL 380. IAW SRM 57-53-01-2R-1, REF SRM 51-70-07-0G-0, REV 132. PERFORMED A REPAIR IAW STEP 1. REMOVED THE DEBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:6",W:1", 11" FROM INBD ESDR IPXA2026082577721Skin · debondedDISBOND - SKIN , LOWER SKIN OF L/H WING T/E OUTBD FLAP T/E SKIN WBL 380 (REPAIR) CORRECT THE TYPO IN STEP 1 : 1.I.A.W. 767-300 SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.132 PERFORM REPAIR AS BELOW STEP: 1. REMOVE THE DISBOND MATERIALS AND CLEAN. 1.2 MEASDR IPXA2026082577089Skin · debondedDISBOND - SKIN , LOWER OF L/H WING T/E OUTBD FLAP T/E SKIN , WBL 366 (REPAIR) CORRECT THE TYPO IN STEP 1 : 1.I.A.W. 767-300 SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.132 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DISBOND MATERIALS AND CLEAN. 1.2 MEASUSDR IPXA2026082577741Skin · debondedDISBOND - SKIN , INBD EDGE UPPER FACE OF L/H WING T/E OUTBD FLAP T/E SKIN , WBL 355 (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 6" AROUND HEATED AREA ,PER 767 NDT MANUAL PART 1 51-01-01 REV:144 RESULT: NO DEFECT WAS FOUNDSDR IPXA2026082961141Former · crackedCRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 648.6. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 132, DWG 114T2513, SH 1, REV D, & SREO-50900-REQ001, REV 2.SDR IPXA2026082634262Seat Track · crackedFOUND FIRST OFFICER SEAT TRACK ASSY CRACK AT FORWARD INBOARD. IAW AMM 25-11-01-822-095-001, REV 149. REPLACED THE SEAT TRACK.SDR IPXA2026080873740Pad · damagedCOMPOSITE AREA SURROUNDING RT WING FIXED LEADING EDGE MOST OTBD BEARING PAD IS CRACKED & CHIPPED AWAY. IAW AMM 51-21-10-307-020, REV 149, REPAINTED REWORK AREA. CONDITION CHECKED NORMAL.SDR IPXA2026062535966Latch · inoperativeMAIN ENTRY DOOR LATCH UNABLE TO LOCK. PERFORMED OPERATIONAL TEST OF CREW ENTRY DOOR REF AMM 52-11-00. OPS CHECKED GOOD. DOOR CLOSES AND LOCKS AS INTENDEDSDR IPXA2026083005141Seal Depressor · damagedRAMP REPORTED DAMAGE TO MCD AFT SEAL DEPRESSOR. INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-40-02-0G, REV 132 AND IAI DWG 368-53-00-95301, ISSUE AV.SDR IPXA2026052858550Skin · damagedMAJOR REPAIR, OVERSIZE RIVET HOLES, IN SLAT INSERT FITTING AND SLAT LEADING EDGE RIB ATTACH FASTENERS NR 9 SLAT ALL STEPS OF EO-96917-REQ7 C/W.SDR IPXA2025100720177Gearbox · stuckWHILE EXTENDING FLAPS FROM UP TO 1, RECEIVED LE FLAP ASYM EICAS MSG AND LEADINGEDGE DISCRETE LIGHT. INSTALLED INBOARD AND OUTBOARD ROTARY ACTUATORS AND OFFSET GEARBOX IAW. AMM 27-81-20 PB 201 REV. 146. AFTER INSTALLATION OF LEADING EDGE SLAT #8, #9 AND #10 ANSDR IPXA2025031292106Knob · out of adjustCREW REPORTS THAT THE TILT KNOB POSITION DID NOT MATCH WITH THE INDICATION ON THE NAV DISPLAY. TILT KNOB ADJUSTED IAW AMM 34-43-02 PB401 REV.144. AND TESTED IAW AMM 34-43-00 PB501 REV.144. FOUND SATIS.SDR IPXA2024120432892Idg · failedATB L GEN OFF DURING TAKEOFF ROLL. RAN CHECKLIST, RESULTED IN MOMENTARY GEN OPERATION BEFORE FAILING AGAIN. ATB REPLACED JAW AMM 24-22-02 PB 401 SATISSDR IPXA2024082938616None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDRSDR IPXA2024081938616Drain · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPENSDR IPXA2024082516569Floor Panel · damagedMAJOR REPAIR, DAMAGE FOUND M/D FLOOR PNL DAMAGE P/N:371-53-13-C4218-103 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-13-C4218-103SDR IPXA2024082516559Floor Panel · damagedMAJOR REPAIR, DAMAGE - FOUND M/D FLOOR PNL DAMAGE P/N:371-53-15-C6405-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 371-53-15-C6405-101.SDR IPXA2024082516575Floor Panel · damagedMAJOR REPAIR, DAMAGE , FOUND M/D FLOOR PNL DAMAGE P/N: 368-53-00-95626-101 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-00-95626-101SDR IPXA2024082996283Pump · cracked*** SUPPLEMENTAL SDR *** FAULT - CRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV 143 REPLACE THE R/H WING AUX FUEL PUMP PNLNO.631AB. 2.CONDITION CHECK NORMAL. 3.IPC VERIFIED AND SERVICEABLE TASDR IPXA2024082993754Handle · brokenFOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE 1. I.A.W AIPC 52-11-25-13-144 REV.28 TO REMOVE FWD ENTRY DOOR HANDLE. 2. I.A.W AIPC 52-11-25-13-144 REV.28 TO INSTALL NEW FWD ENTRY DOOR HANDLE. 3. I.A.W AMM TASK 52-11-00-715-128 REV.143 TO DO OPERATIONAL TESTSDR IPXA2024081693754Bearing · brokenFOUND THE BEARING BROKEN AT FWD ENTRY DOOR HANDLE OK TO WORKSDR IPXA2024081696283Access Panel · crackedCRACK - PNL, L/H WING INSPAR LOWER SKIN AUX FUEL PUMP PNL, PNL NO. 631AB (REPLACE)SDR IPXA2024090674434Skin · dentedSKIN DENTED, RT FUSELAGE TAIL SECTION BS 1915.1 - 1923.5. MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.4" DEPTH(Y)=0.006" AND A/Y = 66 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126SDR IPXA2024090674300Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-36R (EVALUATE) MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.6" DEPTH(Y)=0.007" AND A/Y = 85 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126SDR IPXA2024082977067Skin · cracked*** SUPPLEMENTAL SDR *** FAULT - CRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR) INSTALLED L/H WING LEADING EDGE UPPER FIX PANEL I.A.W SRM 51-40-02-0G REV.126 AND BOEING DWG 114T2230 SH1 REV.D AND 114T2510 SH1 REV.E AND 114T21SDR IPXA2024082977129Skin · crackedCRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL , NEAR INBD TRACK (REPAIR) INSTALLED LEFT WING NO.3 SLAT CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.126SDR IPXA2024082976940Skin · crackedCRACK - SKIN, LOWER FACE OF L/H WING NO.6 SLAT MID LINK LOWER DOOR (REPAIR) 1.I.A.W AMM 57-41-59-404-009 REV 143 INSTALLED THE LEFT WING NO.6 SLAT MIDDLE LINK DOOR, AND PERFORMED THE DOOR ADJUSTMENT WAS SATISFIED. 2.CONDITION CHECK NORMAL.SDR IPXA2024082975427Skin · dented*** SUPPLEMENTAL SDR *** FAULT - DENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) 1. MEASURED THE DENT DIMENSION LENGTH=0.8" WIDTH(A)=0.5" DEPTH(Y)=0.005" AND A/Y = 100 FOUND TO BE IN LIMIT PER SRM 52-40-01-1A-6 FIGURE 101 DETAIL IV REV.126 2. SUBSDR IPXA2024082577039Floor Panel · dentedMAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1197+132~1329, LBL11~RBL11, P/N:368-53-16-94477-127 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-94SDR IPXA2024082577009Floor Panel · dentedMAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT STA 1121.1~1197, LBL 11 ~ RBL 11, P/N:368-53-16-94477-109 (REPAIR) I.A.W IAI SUPPLEMENT AMM 53-01-01-404-013 REV.55 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. PART NUMBER: 368-53-16-SDR IPXA2024081577129Skin · dentedCRACK - SKIN, LOWER FACE OF L/H WING NO.3 SLAT LOWER CLOSURE PNL , NEAR INBD TRACK (REPAIR)SDR IPXA2024081577067Skin · dentedCRACK - SKIN, UPPER FACE OF L/H WING OUTBD FIXED L/E UPPER SKIN, OSS 567 (REPAIR)SDR IPXA2024081574422Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1788 S-38R~S-39R (EVALUATE) OK TO WORKSDR IPXA2024081574300Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-38R ~ S39R (EVALUATE) OK TO WORKSDR IPXA2024081574434Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1915.1 - 1923.5 (EVALUATE) OK TO WORKSDR IPXA2024081575427Skin · dentedDENT - SKIN, R/H APU DOOR SKIN STA 1846 - 1856 (EVALUATE) OK TO WORKSDR IPXA2024052987755A/C Pack · odorSTRONG ACRID OIL SMELL WITH PACKS ON WHILE USING BLEED AIR FROM APU ALSO NOTICED FILM ON INSIDE OF WINDOW AND CAUSED EYE IRRITATION AFTER LONG APU RUN WITH BOTH PACKS ON, THE SMOKE SMELL DISAPPEARED. OPS TEST PERFROMED IAW AMM 21-00-21-102-030, REV: 142.SDR IPXA2024032194772Valve · warning message*DIVERSION* R ENG PRV STATUS MESSAGE ON TAKEOFF #2 ENG PRV MANUAL WRENCHING ACCOMPLISHED AND VERIFIED TO BE HARD TO WRENCH AND WITH STUCK POSITION IN THE MIDDLE. THEREFORE #2 ENG PRV REPLACED AS PER AMM 36-11-18/401 REV.141 OPS AND LEAK TEST FOUND SATIS.SDR IPXA2023111611610Adc · faultedATB, IN FLIGHT ALT DISAGREE? EICAS MESSAGE DISPLAYED. 1ST OFFICER AIR DATA DETERMINED TO BE AT FAULT, ALT AIR DATA SELECTED PERFORMED T/S ON PITOT & STATIC SYS AS PREVIOUS TESTS SHOWED AN ALTITUDE DIFFRENCE OF 100 FEET BETWEEN CAPT AND F/O SIDE. CHECKED ALL CO
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