N274UP
Service difficulty reports · 350
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 = 'N274UP' 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 = 'N274UP' 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 IPXA2025090125093Pressure Panel · corrodedMAJOR REPAIR. MAIN CABIN AT CENTER WING L/H TUNNEL AT THE PRESSURE PANEL HAS CORROSION. ATA 36-14 CENTER WING UPPER AFT SKIN CORROSION REPAIR BTWN XCW=101.850 AND XCW=110 AT REAR SPAR ACCOMPLISHED IN ACCORDANCE WITH UPS EO-94951-REQ1 REVISION 1 AND VT SAA EASDR IPXA2025081524093Pressure Panel · corrodedMAIN CABIN AT CENTER WING L/H TUNNEL AT THE PRESSURE PANEL HAS CORROSION. VERIFIED STEP 7 C/W IAW UPS RII GMM 04-02.SDR IPXA2025081560455Stringer · damagedMAJOR REPAIR, EXISTING REPAIRS IS TIME LIMITED RT WING UPPER STRINGER 6 AT XORS 980.80 REQUIRED PERM. REF EO # 87790-REQ 001. ACCOMPLISHED REPAIR IAW EO-87790-REQ001 REV2 AND VT-SAA EA 011-5700-01-B0550 REV IR.SDR IPXA2025062146821Duct · blownATB, IN CLIMB CABIN PRESS UNCONTROLLABLE. CABIN EXCEEDED 10,000 AT 13,000 MSL. RETURNED TO KSDF. R & R CPC-1 REF. AMM 21-31-04 FUNCTIONAL TEST & RTS TEST PASSED, NO FAULTS NOTED. R & R ACC-2 REF. AMM 21-62-01 RTS TEST PASSED. DURING OPS TEST, SENSOR READOUT OFSDR IPXA2024101038501Power Supply · no testEMER LT BAT 1 LO LVL ALERT ON F/O PREFLIGHT REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MD11 AMM 33-51-01. OPS CHECK GOOD. THIS CLEARS THE DEFERRAL. DMP REVERSED.SDR IPXA2024100938501Battery · faulted*SDR FILED OPEN* EMER LT BAT 1 LO LVL ALERT ON F/O PREFLIGHT REMOVED AND REPLACED EMERGENCY BATT IAW MM 33-51-01. NO HELP. DEFERRED EMERGENCY LIGHT SYSTEM IAW MEL 33-50-4. DMP ACCOMPLISHED. PLACARD INSTALLEDSDR IPXA2024100951875Structure · damagedBIRD STRIKE ON RH WING #4 SLAT. INSTALLED #4 SLAT IAW AMM 27-80-30-400-802 UP TO AND 5F(2)(C)2)D). WITNESSED TORQUES AND VERIFIED SECURITY OF MOUNTING HARDWARE PER GMM REQUIREMENTS 04-02. ACCOMPLISHED AMM 27-80-30-400-802 5 F (3) THRU END. AND 27-80-30-820-802SDR IPXA2024100751875Slat · damagedBIRD STRIKE ON RH WING #4 SLAT. INSPECTED ,A/C SIDE ONLY .OK TO INSTALL , AIRFRAME SIDE .SDR IPXA2024091618103Fire Detector · faultedINTERMITTENT FIRE DET APU FAULT ENROUTE PERFORMED BITE TEST OF THE FIRE DETECTION CONTROL UNIT IAW 26-11-02-700-801 AMM TEST OK.WORK PERFORMED BY CHARTER AMT PRODANOV, A&P 3839872, IAW GMM 03.47.01.05 CHARTER PROCEDURES.SDR IPXA2024091618200Fire Loop · faultedREF ITEM #1 NEED TO DEFFER APU FIRE DETECTION LOOP A REMOVED AND REPLACED APU FIRE DETECTION CONTROL UNIT PER AMM 26-12-04. OPS CK GOOD AT THIS TIMESDR IPXA2024090408239Power Unit · no testON F/O PREFLIGHT LVL 1 EMER POWER TEST FAIL. WITH L EMER AC OFF LIGHT ILL. '' L EMER AC". PER FIM 24-24-01-00 PERFORMED EMERG POWER TEST. ALL TESTS PASSED. NO DEFECTS NOTED AT THIS TIME. BATT VOLTAGE NORMAL. ELEC SYSTEM CHECKS GOOD.SDR IPXA2024050251161Battery · faultedDURING PREFLIGHT EMERGENCY POWER TEST FAILED. IRU 1 ON BAT ILLUMINATED. REMOVED AND REPLACED EPCU REF MM 24-08-01. R-T-S PASS REF MM 24-08-01. EMERGENCY POWER TEST PASSED SEVERAL TIMES WITH NO FAULTS NOTED. TESTED ALL IRU€™S REF MM 34-43-00-700-803, NO FAULTSDR IPXA2024050151161Electrical Sys · no testOPEN, DURING PREFLIGHT EMERGENCY POWER TEST FAILED. IRU 1 ON BAT ILLUMINATED. FOUND NR 2 DU RED X WHEN ON STAND BY POWER. T/S PER FIM 24-24-03-00 BLOCKS 1,2,7,8,16. INVERTER I1-1 HAS 28V IN WITH NO 115V OUTPUT.SDR IPXA2024042687620Electrical Sys · no testEMERGENCY PWR TEST FAIL REMOVED & REPLACED BOTH MAIN BATTERIES PER AMM 24-34-02 - BATTERY OPS CHECK NORMAL. PERFORMED TEST OF EMERGENCY POWER SYSTEM, TEST INITIALLY PASSED AND THEN BEGAN CONTINUOUSLY RUNNING THE EMERGENCY POWER TEST WITHOUT BEING PROMPTED BY ASDR IPXA2024042552154Light · no testDURING PREFLIGHT EMERGENCY POWER TEST FAIL OPERATIONALLY CHECKED SHIPS BATTERIES, OPS CHECK GOOD, RESET EPCU EMERGENCY POWER TEST GOOD. PER FIM 24-30-03-00SDR IPXA2024032928442Unknown · no testEMER PWR TEST FAIL ON PREFLIGHT TROUBLE SHOT IAW MD11 FIM 24-30-03-00, BATTERIES CHECK GOOD, PERFORMED OPS CHECK OF EPCU IAW MD11 AMM 24-08-01-741-801, OPS CHECK GOODSDR IPXA2024032511259None · noneEMERGENCY PWR TEST FAIL R&R'D EPCU NO HELP RE-INSTALLED ORIGINAL PER AMM 24-08-01. AFTER INSTALLATION OF ORIGINAL EPCU. EMERGENCY PWR TEST WAS SUCCUSSFULL PER PDC. SYS OK. PER FIM 24-30-03SDR IPXA2024030727140Power Unit · no testPREFLIGHT: LEVEL 1 EMERGENCY POWER TEST FAIL C/W TECH ALERT IAW SWPM 20-00-09 PARAGRAPH 3.B.(5). OPS CHECK GOOD.SDR IPXA2024030442563Metering Valve · faultedENG #3 LVL 0 ALERT AND FF (0) (FUEL OFF). VERIFIED TORQUE OF MAJOR MOUNTING HARDWARE OF #3 ENGINE FUEL METERING UNIT AS PER AMM 73-21-01 AS REQUIRED PER GMM 04-02 ATA 71-80; C/W REMAINDER OF INSTALLATION OF AMM 73-31-02 AND 73-21-01. OPS CHECK AND LEAK CHECKS SDR IPXA2024022777693Battery · no testEMERGENCY POWER TEST FAIL R/R BATT 1 AND BATT 2 REF AMM 24-34-00 OPS CHK GOODSDR IPXA2024011652124Door · inoperativeL1 DOOR WILL NOT OPERATE ELECTRICALLY. REPLACED L1 DOOR ACTUATOR PER AMM 52-11-01/401. TEST GOOD.SDR IPXA2024011019213Unknown · unknownFWD LOWER CARGO DOOR CUT OUT, AFT EDGE SKIN PREVIOUS BLENDOUT DAMAGE. BLENDED OUT DAMAGE TO PREVIOUS CUTOUT, NEW DIMENSIONS ARE 10.00 INCH VERTICAL X .350 DEEP. APPLIED PRIMER AND PAINT AS REQ. REF. SRM 53-00-15-2R-8 REPAIR 8 AND AMM 51-22-00.SDR IPXA2024010819213Unknown · unknownFWD LOWER CARGO DOOR CUT OUT, AFT EDGE SKIN PREVIOUS BLENDOUT DAMAGE.SDR IPXA2023113038884Unknown · unknown*** SUPPLEMENTAL SDR *** L1 DOOR AFT LOWERING CABLE FOUND BROKEN ** OII 2 ** INSTALLED L1 DOOR AFT LOWERING CABLE PER MM 52-11-03. THIS CLEARS DEFERRAL, PLACARD REMOVED.SDR IPXA2023113032565Unknown · unknownL1 DOOR INOP WILL NOT OPEN FOUND BROKEN AFT LOWERING CABLE L1 DOOR DEFERRAL TRANSFERRED TO BAR CODE T3F18E003EFTT FOR DEFERRAL. INSTALLED L1 DOOR AFT LOWERING CABLE PER MM 52-11-03. THIS CLEARS DEFERRAL, PLACARD REMOVED.SDR IPXA2023120138884Unknown · unknown*SDR FILED OPEN* L1 DOOR AFT LOWERING CABLE FOUND BROKEN ** OII 2 ** DEFERRED PER MEL 52-10-3-1-2-1-2SDR IPXA2023120132565Unknown · unknown*SDR FILED OPEN* L1 DOOR INOP WILL NOT OPEN FOUND BROKEN AFT LOWERING CABLE L1 DOOR DEFERRAL TRANSFERRED TO BAR CODE T3F18E003EFTT FOR DEFERRAL.SDR IPXA2023112058316Unknown · unknownEMER PWR TST FAIL FOLLOWED FIM 24-30-03-00 AND PERFORMED THE OPS TEST OF THE BATTERIES IAW AMM 24-34-02. TEST OK.SDR IPXA2023101700187Unknown · unknownEMERGENCY LIGHT TEST LEVEL 1 ALERT DISPLAYED €ŒEMERGENCY LT BAT 1 LO€? REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY PER AMM 33-51-01-400-802. OPS CHECK GOODSDR IPXA2023091594162Door Latch · inoperativeINSPECTION TYPE:NATHE LATCH THAT HOLDS COCKPIT DOOR OPEN IS MISSING SPRING AND IT WILL NOT HOLD DOOR OPENLATCH/DOOR RSTRAINT ASSY R&R'D REF AMM 20-50-02SDR IPXA2023081693926Support Bracket · crackedINSPECTION TYPE:3CL/H WING O/B FLAP I/B HINGE FOUND O/B SUPPORT BRACKET CRACKED AT STA XORS=538 .REMOVED, REPLACED CRACKED SUPPORT BRACKET AT THE L/H WING O/B FLAP I/B HINGE AT STA XORX=538 IAW SRM 51-31-01 AND AMM 20-50-02. (MINOR)SDR IPXA2023080793830Floor Panel · corrodedINSPECTION TYPE:1C3CFLOOR PANEL HAS CORROSION UNDER RCB WALL Y= 475 TO -Y=500BLENDED AREA FOUND TO BE OUT OF LIMIT IAW SRM 51-21-01 , REPLACED FLOOR PANEL IAW SRM 51-31-01. MINORSDR IPXA2023080793828Floor Panel · corrodedINSPECTION TYPE:1C3CFLOOR PANEL HAS CORROSION UNDER RCB WALL AT STA X=25BLENDED AREA FOUND TO BE OUT OF LIMITS IAW DM-11 SRM 51-21-01,REPLACED FLOOR PANEL IAW SRM 51-31-01. MINORSDR IPXA2023080793821Stiffener · crackedINSPECTION TYPE:1C3CL/H MLG W/W LWR AFT O/B WALL 1EA STIFFENER HAS A CRACKREMOVED AND REPLACED STIFFENER IAW SRM 51-31-01,51-35-01 AND 51-33-01, CIC APPLIED PER E.O. M-5100-2780-M. MINORSDR IPXA2023081693924Bracket · gougedINSPECTION TYPE:3CNLG RETRACT ACTUATOR A/C SIDE BRACKET ANTI-ROTATION LUG IS GOUGED AT STA Y=596, X=3.0 .REPAIRED BRACKET ASSY. AT THE NLG RETRACT ACTUATOR A/C SIDE AT STA Y=596, X=3.0 IAW VTSAA EA 011-5310-01-B0068 I/R, UPS EO MD11-5310-87842-A DATED 08/14/23SDR IPXA2023081793948Stringer · crackedINSPECTION TYPE:3C*** MAJOR REPAIR *** R/H WING FUEL TANK AT THE UPPER STRINGER #6 HAS A CRACKED BETWEEN STA XORS=981, XORS=1013 .REPAIRED CRACKED UPPER STRINGER #6 AT THE R/H WING FUEL TANK AT STA XORS=981, XORS=1013 IAW VTSAA EA 011-5710-01-B0051 I/R, UPS EOSDR IPXA2023081693922Door Frame · gougedINSPECTION TYPE:3C*** MAJOR REPAIR *** MAIN CARGO DOOR FOUND FWD LOWER DOOR FRAME GOUGED AND CRACKED STA Y=624.625 .REPAIRED CRACKED LOWER FWD DOOR FRAME AT THE MAIN CARGO DOOR AT STA Y=624.625 IAW VTSAA EA 011-5230-01-B0045 I/R, UPS EO MD11-5230-87782-A DATEDSDR IPXA2023081293882Skin · corrodedINSPECTION TYPE:C3*** MAJOR REPAIR *** MAIN CABIN AFTER FLOOR PANEL REMOVAL FOUND CORROSION AT THE CENTER WING SKIN AT STRINGER #15 L/H TUNNEL BETWEEN STA XCW=97,XCW=103.REPAIRED CORRODED SKIN AT THE CENTER WING UPPER SKIN AREA AT STRINGER #15 L/H TUNNEL BETWESDR IPXA2023081093872Tee Angle · corrodedINSPECTION TYPE:3CR/H WING I/B FLAP LOWER SURFACE SKIN BULGING O/B OF VANE SPRING CARTRIDGE.REMOVED, FABRICATED AND REPLACED TEE ANGEL AT THE R/H WING I/B FLAP LOWER SURFACE O/B OF VANE SPRING CARTRIDGE IAW DWG ARC2493 AND SRM 51-31-01 (MINOR)SDR IPXA2023080393790Unknown · crackedINSPECTION TYPE:3CCENTER WING LOWER AUX L/H STRINGER 52 SPLICES REPAIR C AND Z HAS A CRACKED AT STA XCW=64.REMOVED, FABRICATED AND REPLACED CRACKED SPLICES REPAIR AT THE CENTER WING LOWER AUX L/H STRINGER 52 IAW SRM 57-10-03 FIG 201 REPAIR 1. (MAJOR)SDR IPXA2023081693923Unknown · crackedINSPECTION TYPE:3C*** MAJOR REPAIR *** RCB WALL INSIDE #2 INSPECTION HOLE R/H SIDE HAS A CRACKED GOING FROM NUT-PLATE TO NUT-PLATE AT STA Y=489.12 AND X=73.340.REPAIRED CRACKED RCB WALL INSIDE #2 INSPECTION HOLE AT STA Y=489.12 AND X=73.340 IAW VTSAA EA 011-53SDR IPXA2023081093871Stiffener · crackedINSPECTION TYPE:3CAFT CARGO COMP. AT STA 1841 FLOOR BEAM AREA AT LONGERON 47R HAS A STIFFENER WITH A CRACKED.REMOVED, FABRICATED AND REPLACED STIFFENER AT THE AFT CARGO COMP. STA 1841 FLOOR BEAM AREA AT LONGERON 47R IAW DWG AGA7170 AND SRM 51-33-01. (MINOR)SDR IPXA2023072893754Bracket · crackedINSPECTION TYPE:3CCAC COMP. HAS A CRACKED BRACKET AT THE RADIO RACK LOCATED AT UPPER FWD I/B SIDE OF RADIO RACK.REMOVED, FABRICATED AND REPLACED BRACKET AT THE CAC COMP. UPPER FWD I/B SIDE OF RADIO RACK IAW SRM 51-33-01 AND DWG AAN7180. (MINOR)SDR IPXA2023081593918Skin · corrodedINSPECTION TYPE:3C*** MAJOR REPAIR *** MAIN CABIN AFTER REMOVAL OF FLOOR PANEL ON CENTER WING AREA FOUND CORROSION ON L/H TUNNEL AT STA 1239, XCW= 101.8 AND XCW= 108.REPAIRED CORRODED AREA AT THE CENTER WING L/H TUNNEL AT STA XCW=101.8 AND XCW=108 IAW VTSAA EASDR IPXA2023081493899Skin · corrodedINSPECTION TYPE:4CMAIN CABIN AFTER REMOVAL OF FLOOR PANEL CENTER WING AREA FOUND CORROSION AT STRINGER #8 BETWEEN STA XCW=101.8, XCW=108.REPAIRED CORRODED SKIN AREA AT THE CENTER WING ON MAIN CABIN AT STRINGER #8 BETWEEN STA XCW=101.8, XCW=108 IAW VTSAA EA 01SDR IPXA2023071193647Strap · missingINSPECTION TYPE:NAAIRCRAFT MISSING A RED SAFETY STRAP AT R1.INSTALLED SAFETY STRAP REF 25 60 01SDR IPXA2023052493307Test Switch · inoperativeINSPECTION TYPE:NAL1 DOOR SLIDE PRESS TO TEST SWITCH LIGHT INOP. SWITCH DEFERRED PER MEL 25-61-2. DMP C/W. PLACARD INSTALLEDR/R PTT BATTERIES. OPS CHECK GOOD. REF AMM 25-61-04-710-801. THIS CLEARS M808848. PLACARD REMOVEDSDR IPXA2023041192832Door · inoperativeAFTER BLOCK OUT LEV 1 CARGO DOOR TEST FAIL. PERFORMED MANUAL TEST PER QRH. DOOR TEST OK. RESULTED IN CREW DEFERRAL OF AUTO TEST FUNCTION. CARGO DOOR TEST AUTOMATIC MODE MEL/CDL : 52-30-7 AUTHORIZED BY 0559165 PLACARD INSTALLED D.I. LOG UPDATEDR/R MSC PER AMM 3SDR IPXA2023040592613Door · inoperativeFLIGHT CREW REPORTS L1 DOOR INOP. DEFERRED L1 DOOR IAW MD11 MEL 52-10-3-1-2-1-2. ITEM TRANSFERRED TO DI CONTROL# M 806416. PLACARD INSTALLED. NO DMP.R/R L1 DOOR LOCK PIN RELEASE SOLENOID IAW AMM 52-10-06. OPS CHECK GOOD. THIS CLEARS M806416SDR IPXA2023033192474Lever · bentINSPECTION TYPE:NAENTERING AIRCRAFT THRU R1 EMERGENCY SLIDE LEVER BENT FOWARD OUT OF POSITION BLOCKING ABILITY TO ARM DOOR.OPERATED R1 DOOR PER AMM 52-30-00. HANDLE IN PROPER DETENTED POSITION AND FUNCTIONAL. NO FAULTS NOTED. OK FOR SERVICE.
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