N572UP
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 = 'N572UP' 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 = 'N572UP' 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 IPXA2026080575871Battery · inoperativeFOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOP. IAW SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK AISLE EMERGENCY LIGHT SYSTEM CHECK , FOUND THE EMERGENCY LIGHT BATTERY M5168 FUNCTION FAIL. IAW AMM 33-51-04-902-001-001, REV.117. REPLACED THE EMERGENCY LIGHSDR IPXA2026080575748Battery · inoperativeFOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. I.A.W SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK EMERGENCY EXIT SIGN LIGHT SYSTEM CHECK , FOUND THE EMERGENCY LIGHT BATTERY M5169 FUNCTION FAIL. I.A.W AMM 33-51-04-902-001-001 REV.117 REPLACED THE EMERGENSDR IPXA2026080375748Light · inoperativeFOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. (REPLACE)SDR IPXA2026080375871Light · inoperativeFOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOPERATIVE. (REPLACE)SDR IPXA2026070878270Flap · crackedFOUND RT WING OUTBD AFT FLAP INBD SIDE BOTTOM SURFACE CRACK. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES AROUND HEATED AREA ,PER 747 NDT MANUAL PART 1 51-01-01 REV:183 RESULT:NO DEFECT WAS FOUND. IAW AMM 51-24-11-477-083, REV 116, REPAINT PEEL OFF SDR IPXA2026071560216Skin · crackedCRACKED SKIN, NR 4 PYLON R/H FAIRING DOOR L/E AREA. I.A.W.AMM 54-62-03-404-005 REV117 INSTALLED NO.4 PYLON R/H FAIRING DOOR.SDR IPXA2026070759188Cowling · dentedDENTED SKIN, NR 2 ENG NOSE COWL INLET AT 10 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 12.8" FROM AFT EDGE, 51.7" FROM LWR EDGE, AT 10 O'CLOCK ON THE ACOUSTIC PNL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CSDR IPXA2026070724623Seal · brokenBROKEN MOLDING SEAL, LT WING NR 11 KRUEGER FLAP INBD SIDE MOLDING. CHECKED OK.SDR IPXA2026070921962Web · corrodedCORRODED UPPER DECK FLOOR PNL WEB AT BS 480 - 520, LBL 10 - RBL 40 CORRODED. INSTALLED A NEW WEB IAW SRM 51-40-02-0G, REV 107.SDR IPXA2026070724617Seal · brokenBROKEN MOLDING SEAL, LT WING NR 6 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIRSDR IPXA2026070624604Seal · brokenBROKEN MOLDING SEAL, LT WING NR 3 VC FLAP INBD SIDE, IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR.SDR IPXA2026070624589Seal · brokenBROKEN MOLDING SEAL, LT WING NR 2 VC FLAP INBD SIDE. REMOVED THE RAIN EROSION SHIELDS AND CLEANED. APPLY THE SEALANT TO REPAIR AREA.SDR IPXA2026070324858Skin · damagedABRADED SKIN, UPPER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR, PANEL 521BB, IAW AMM 52-49-09-402-003, REV 116. INSTALLED REFUELING PANEL 521BB. CONDITION CHECKED NORMAL.SDR IPXA2026070420634Fairing · debondedDEBONDED PANEL, AFT WING TO BODY FAIRING PANEL 193CL EXTERNAL SURFACE. IAW AMM 20-51-01-912-008 REV.116 INSTALL PANEL 193CL. CONDITION CHECK NORMAL.SDR IPXA2026070524776Skin · crackedCRACKED SKIN, RT WING T/E NEAR INBD AILERON PANEL 673AB. IAW SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.107 PERFORM REPAIR AS BELOW STEP: REMOVE THE DAMAGE MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA (L:0.38", W:0.28", 11" FROM INBD EDGE,AT PNL AFT EDSDR IPXA2026070324807Skin · crackedCRACKED SKIN, RT WING T/E NEAR INBD AILERON 673CB. IAW AMM 20-51-01-912-008 REV. 116 INSTALLED THE ACCESS PANEL 673CB. CONDITION CHECKED NORMAL.SDR IPXA2026070624831Skin · crackedCRACKED SKIN, LOWER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR CUTOUT, ILES 845. IAW AMM 52-49-09-402-003, REV. 116. INSTALLED REFUELING PANEL NO. 521CB. 2. CONDITION CHECK NORMAL. ATTACHMENT ARE UPLOADED.SDR IPXA2026073009895Web · crackedSURFACE & HOLE CRACK INDICATION , DURING PFM SB 747-57A2357 FND SURFACE & HOLE CRACK . ACCOMPLISHED REPAIR IAW EO-98227-REQ1, REV 1, & EGAT EI F2026A57M-1427, REV 4.SDR IPXA2026072111084Panel · debondedDEBONDED PANEL, VERTICAL STABILIZER LOWER PANEL 322BL. REPAIR DISBOND ON PANEL ASSY OF VST FWD TORQUE BOX BETWEEN STA 2365 AND STA 2413 I.A.W. EGAT EI F2026A55M-1378 REV.1 AND UPS EO-98179-REQ1 REV.1 2. CONDITION CHECK IS SATISFACTORY.SDR IPXA2026072111043Panel · debondedDISBONDED PANEL , VERTICAL STABILIZER LOWER PANEL 322CL. REPAIR DISBOND DAMAGE ON LH FWD LWR VST FORWARD TORQUE BOX PANEL BETWEEN STA 2285 AND 2365 AND BETWEEN FIN WL10 AND 25 I.A.W. EGAT EI NO. F2026A55M-1379 REV. 1 AND UPS EO-98180-REQ1 REV. 2SDR IPXA2026070697892Seal · brokenBROKEN MOLDING SEAL, L/H WING NR 4 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12 REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED.APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.SDR IPXA2026070697902Seal · brokenBROKEN MOLDING SEAL, LT WING NR 5 VC FLAP INBD SIDE. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12, REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED, APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.SDR IPXA2026072186856Seal · damagedFOUND NR 1 ENTRY DOOR LOWER SEAL DAMAGED. IAW AMM 52-09-00-308-001, REV.116. REPLACED NR 1 ENTRY DOOR LOWER SEAL. CONDITION CHECK NORMAL.SDR IPXA2026071085535Skin · brokenCRACKED SKIN, RT WING L/E NR 23 V.C FLAP INBD LWR. ACCOMPLISHED JOB IAW EO-97981-REQ1, REV1 AND EGAT EI F2026A57M-1340. ACCOMPLISHED JOB I.A.W UPS EO-97981-REQ1 REV2 AND EGAT EI NO. F2026A57M-1340, REV.0 AND REV.1.SDR IPXA2026062986856Seal · damagedFOUND NO.1 ENTRY DOOR LOWER SEAL DAMAGEDSDR IPXA2026073003261Stiffener · wornMAJOR REPAIR, SUPPORT ROD INSIDE FUELING PANEL STATION AFT ATTACH BOLT HOLE IS ELONGATED AND ATTACH ANGLE IS WORN. ACCOMPLISH THE REPAIR IAW EO-97627-REQ2 REV1 AND EGAT EI F2026A57M-1357, REVISION 1. REFER TO DAMAGE REPORT FOR THE ORIGINAL MATERIAL & THICKSDR IPXA2026060120516Fuel Sys · out of balanceAFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG2 PUMPS. REMOVED AND REPLACED MAIN 2 AFT BOOST PUMP REF AMM 28-22-SDR IPXA2026051220516Transfer Sys · malfunctionedAFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG 2 PUMPS DEFERRED IAW EO-97441.SDR IPXA2026041322009Window · crackedAT FL 370 FWD WINDOW LEFT CRACKED. R & R L1 WINDOW IAW AMM 56-11-01/401. REPLACED WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01/401. OPS CHKD WINDSHIED HEATER SYS AND WIPER IAW AMM 30-41-00/501 & 30-42-00/501, CHKD NORMAL, AIRCRAFT OK FOR SERVICE.SDR IPXA2026041022009Window · crackedAT FL 370, FWD WINDOW LEFT CRACKEDSDR IPXA2026012682273Start Valve · faultedAIR TURN BACK, NR 3 STARTER CUTOUT EICAS MESSAGE IN CLIMB, CONTINUED THROUGH FLIGHT. QRH PROCEDURE FOLLOWED. R & R NR 3 ENG START VALVE IAW AMM 80-11-02/401 & OPS CHECKED NORMAL.SDR IPXA2025012496294Skin · damagedDAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND FOR CORRECTIVE ACTION PLEASE SEE REF: EO-92470-REQ1 (SECTION 48 FUSELAGE SKIN PANEL DENT, GOUGE, AND CRACK DAMAGE FORWARD OF STA 2598; BETWEEN STR 38R AND 46R - CATEGORY B REPAIR) COMPLIED WITH EO-92470SDR IPXA202501096294Structure · damagedDAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND DIRECT AFTER LANDING WE FOUND DAMAGE TO THE TAIL AREA OF THE AIRPLANE. BEFORE GROUND HANDLING TOUCHED THE AIRPLANE AT CGN. WE FOUND FOLLOWING DAMAGES BELOW THE TAIL STAND MOUNT:ONE TIME WE HAD A DENT ANDSDR IPXA2024122341321Bulb · inoperativeEMERGENCY LIGHT IN CEILING PANEL ABOVE L-1 DOOR FWD BULB INOP. RE-LAMPED FWD BULB IN EMERGENCY CEILING LIGHT ABOVE L1 DOOR PER AMM 33-51-07. OPS CHECK GOOD PER AMM 33-51-00.SDR IPXA2024101703256Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL APPROX. STA 1140 L TO APPROX STA 1220L CRACKED ALONG ENTIRE OUTBID LENGTH MARKED WITH TAPE. INSTALLED NEW FLOOR PANEL IAW AMM 53-21-02, RII €ŒOK TO INSTALL€? GIVEN ON BARCODE T3F18E005CL38.SDR IPXA2024070771367Skin · dentedDENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE.REMOVED THE DAMAGED SKIN,MEASURE THE CUTOUT (DIA:0.8", 10.75" FROM OUTBD EDGE I.A.W. 747-400F SRM 57-53-01-2R-1.PERFORMED NDT/ET FOR CUTOUT AREA I.A.W. 747 NTM PART6 51-00-00 PROCEDURE 23 REV:176 RESULT:NO CRSDR IPXA20240701367Skin · dentedDENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE. (REPAIR) PERFORMED NDT/UT REWORKED AREA AND PLUS 8" AROUND HEATED AREA, I.A.W. 747 NDT MANUAL PART 1 51-01-01 AND 747 NDT MANUAL PART 1 51-04-00 REV.176 , RESULT: NO DEFECT FOUND. OPENSDR IPXA2024070258057Shear Tie · crackedL/H FRONT SPAR THE SHEAR TIE AT LBL 75.92, STA 1000. REMOVED HARNESS FOR SM REWORK UNDER FLOOR PANEL IAW SWPM 20-10-12SDR IPXA2024070258045Fitting · crackedR/H FRONT SPAR THE INERCOSTAL LUG FITTING AT RBL 11.33 STA 1000 REMOVED BOTS AT STA 1000. CKD NORMAL. REMOVED TUBE. CKD NORMAL IAW IPC 57-14-01-01A.SDR IPXA2024070257995Fitting · crackedL/H FRONT SPAR THE INTERCOSTAL LUG FITTING AT LBL 11.30, STA 1000.REMOVED AND REINSTALLED THE BOLTS AND TUBE AT STA 1000. CONDITIONS WERE NORMAL IAW AMM 20-11-28-964-010SDR IPXA2024070518937Stringer · crackedSTRINGER, L/H WING NO.7 V/C FLAP (REPLACE) INSTALL NEW PART IAW SRM 51-40-02-0G REV.101 AND BOEING DWG NO: 65B15170 SH 2 REV:H. IAW AMM 27-81-02-404-010, REV110, STEP A~5(E), INSTALL NO.7 VARIABLE CAMBER FLAP IAW AMM 27-81-02-404-010 REV.110 STEP E(6) TO E(33)SDR IPXA2024041455734Skin · dentedNUMBER 14 INBOARD MOST RIGHT WING KRUGER FLAP HAS 2 DENTS VERIFIED CORRECT CLEARANCES AND OPS CHECK OF THE #14 KRUEGER FLAP IAW AMM 27-81-01. ALL CHECKS GOOD AT THIS TIME.SDR IPXA2024081812684Skin · crackedHFEC REINSPECT REVEALED CRACK INDICATION AND NEW DAMAGED IDENTIFIED VISUALLY (T3F18E001Y856 CLOSED IN ERROR) FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01-2R. MATERIAL ID FOR FILLER IS .100" 2024-T3 PO.#SP2586586, AND FOR DOUBLER .125" 2024 T-3 PO.#SP2SDR IPXA2023062831080Structure · puncturedLH I/B AFT FLAP HAS A PUNCTURE APPROX 26.75€? FROM TRAILING EDGE & 63€? FROM I/B EDGE. MARKED WITH TAPE.***SM36/LMX4/HGR*** ACCOMPLISHED STEPS 1-14 OF EO-87186-REQ3 PERMANENT REPAIR. THIS CLEARS DEFERRAL MOC 2500762.SDR IPXA2022122046355Gust Lock · brokenL1 CREW ENTRANCE DOOR LATCH TO HOLD OPEN IS BROKEN CLEANED AND CHECKED HOLD OPEN MECHANISM IAW AMM 52-11-00-201 REV. 106.01. FOUND SATISSDR IPXA2022081179940Light · inoperative**SUPPLEMENTAL SDR**FAULT FOUND THE MAIN DECK L1 DOOR AREA EMERGENCY LIGHT INOP (REPLACE) TASK COMPLETED IAW AMM 33-51-01 REV39.00SDR IPXA2022080419083Panel · brokenFAULT - BROKEN - LEFT WING OUTBOARD FORE FLAP ACCESS PANEL WBL 754 (REPAIR) TASK COMPLETEDSDR IPXA2022080100360Panel · corrodedFAULT - CORROSION - SUPPORT, RH AIR CONDITION COMPARTMENT ACCESS DOOR, MIDDLE SUPPORT. (REPLACE) TASK COMPLETEDSDR IPXA2022032580472Floor Panel · damagedINSPECTION TYPE:N/AMAIN DECK FLOOR PANEL POS 9L HAS DAMAED UPEPR FACE SHEETFABRICATE REPLACEMENT FLOOR PANEL PER EO B747-5320-42648-ASDR IPXA2022032580471Floor Panel · delaminatedINSPECTION TYPE:N/AUPPER FACE SHEET OF FLOOR PANEL POS 9L DELAMINATEDFABRICATE NEW FLOOR PANEL PER EO B747-5320-42648-A
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