N133UP
Service difficulty reports · 246
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 = 'N133UP' 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 = 'N133UP' 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 IPXA2026090347689Fuel · leakingSTRONG ODOR OF JET FUEL ON THE FLIGHT DECK. IN AIR OR GROUND WITH PACKS ON WITH ENG OR APU AS BLEED SOURCE. CLEANED AREA OF THE FUEL LEAK, RAN APU FOR SEVERAL HOURS. VERIFIED NO FUEL SMELL FROM PACKS USING APU. REF MM 49-32-12-401.SDR IPXA2026090247689Unknown · odorSTRONG ODOR OF JET FUEL ON THE FLIGHT DECK. IN AIR OR GROUND WITH PACKS ON WITH ENG OR APU AS BLEED SOURCE.SDR IPXA2026071456799Cover · brokenSAFETY COVER FOR DOOR ARMING LEVER BROKEN & CRACKED, SHARP EDGES EXPOSED. REMOVED DAMAGED ENTRY DOOR SLIDE ARMING COVER. REPLACED ARMING COVER DOOR IAW AMM 52-10-13. OPS CHECKS GOOD.SDR IPXA2026060401733Valve · odorIN DECENT WITH NON IDLE POWER SETTING THE #1 AND #2 HP VALVES CYCLED WITH A HOT SMELL. #1 HP EVENTUALLY FAULTED AND RESET VIA THE CHECKLIST. THE CYCLING CONTINUED DURING DECENT. ON FINAL WITH #2 PACK. FOUND PNEUMATIC SYSTEM CONTROLLER 1 TO HAVE €ŒC CONTROLLESDR IPXA2025120329714Button · stuckON MAIN CABIN ENTERY DOOR. THE PUSH TO RELEASE BUTTON IS STUCK DOWN. DOOR WILL NOT LOCK OPEN. FREED UP PUSH TO RELEASE BUTTON AND OPS CHECK GOOD PER AMM 52-10-00-2.SDR IPXA2025111229656Computer · faultedEMERGENCY DECLARED, AUTO FUEL FAULT IN FLIGHT RAN QRH PROCEDURES AFTER EVALUATING FUEL QUANITY WE SAW OUTER FUEL @ 4700 REVIEWED FUEL IMBALANCE CHECK BALANCEED FUEL UPON LANDING OUTER FUEL TANK SHOWED 8200 LBS. T/S AUTO FUEL FEED FAULT PREFORMED AUTO FUSDR IPXA2025103116091Web · crackedNR 1 PYLON AFT MEMBER BETWEEN RIB 18 AND RIB 21 CRACKED. JP-110. REMOVED AND REPLACED AFT MEMBER (WEB) IAW A300-600 SRM 51-40-21.SDR IPXA2025103185179Bracket · brokenFLOOR PANEL 144FR AREA, AFT BRACKET BROKEN. SUPPORT FAIRING WAS INSTALLED IAW A300/600 SRM 51-40-21. REVIEWEDSDR IPXA2025103121028Floor Panel · damagedINSP MLG W/W PANEL 147BF DELAMINATED. VERIFIED FLOOR PANEL 147BF FABRICATED IAW SREO-16407-REQ002.SDR IPXA2025103104418Floor Panel · debondedFLOOR PANEL 131 BH EDGE IS DISBONDED. FLOOR PANEL 131BH FABRICATION IS COMPLETED IAW SERO-16407-REQ002((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).SDR IPXA2025103104517Floor Panel · damagedFLOOR PANEL 152 M CORNER HAS BROKEN COMPOSITE. FLOOR PANEL 152MG FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).SDR IPXA2025110188289Deflector · crackedFAULT - STR, Z500, PANEL RACK, LH WING, DEFLECTOR PANEL 572LB HAS GOUGE W/CRACK. DOT 103-1524. PROFILE WAS INSTALLED IAW A300/600 SRM 51-40-21 REVIEWEDSDR IPXA2025102102022Seat Track · damagedMAIN CABIN - ENLONGATED HOLE ON SEAT TRACK BTW FR79 AND FR80/82 -Y450. REMOVED SEAT TRACK BTW FR79 AND FR80/82 -Y450 IAW SRM 53-10-16 PG 207 FIGURE 201. INSTALLED NEW SEAT TRACK BTW FR79 AND FR80/82-Y450 IAW SRM 53-10-16 PAG.207, FIG. 20.SDR IPXA2025101675564Adapter · corroded***SUPPLEMENTAL SDR*** FAULT: STR - Z200 - MAIN CABIN - CLS ADAPTER WITH CRACK AT FR34 BTW -Y1959 & -Y2462. INSTALLED CLS ADAPTER IAW A300 SRM 51-40-21.SDR IPXA2025101475564Adapter · crackedMAIN CABIN, CLS ADAPTER WITH CRACK AT FR34 BTW -Y1959 & -Y2462 LOCATED AND DRILLED CLS ADAPTER. IAW A300 SRM 51-40-40. REQUEST OK TO INSTALL.SDR IPXA2025110459260Adapter · corrodedMAIN CABIN - SEAT TRACK ADAPTER SEGMENT CLS WITH CORROSION BTW FR20 AND FR27 BTW Y1580 & Y2244. INSTALLED NEW TRACK ADAPTER CLS SEGMENT IAW A300-600 SRM 51-40-21. REVIEWEDSDR IPXA2025110561418Adapter · corrodedMAIN CABIN - CLS ADAPTER WITH CORROSION AT FR 27 Y0 RH. INSTALED CLS ADAPTER I.A.W. A300-600 SRM 51-40-21 . REVIEWEDSDR IPXA2025102461494Adapter · corrodedMAIN CABIN - SEAT TRACK CLS ADAPTER WITH CORROSION AT FR 27 Y0 LT. INSTALLED CLS ADAPTER IAW SRM 51-40-21.SDR IPXA2025102356354Profile · damagedMAIN CABIN - Z-PROFILE CRACKED BTW FR73-FR74 -Y2127.6. REMOVED Z-PROFILE IN MAIN CABIN BTW FR73-FR74 -Y 2127.6 IAW AIRBUS A300-600 SRM 51-40-21. INSTALLED NEW Z-PROFILE AT FR73-FR74 -Y2127.6 IAW AIRBUS A300-600 SRM 51-40-21.SDR IPXA2025101658777Adapter · corrodedMAIN CABIN - CLS ADAPTER WITH CRACK AT FR37 BTW Y1580.5 & Y2127.5. INSTALLED CLS ADAPTER IAW A300 SRM 51-40-21.SDR IPXA2025102461059Hinge Fitting · corrodedFAULT - STR Z400 - ENG #2 O/B FAN COWL, AFT ATTACH SUPPORT DAMAGED. DOT 90-038. ++REPLACED FAN COWL HINGE AT STR Z400 - ENG #2 O/B FAN COWL, AFT ATTACH SUPPORT IAW A300-600 SRM 51-40-21SDR IPXA2025101655510Profile · crackedMAIN CABIN - T-PROFILE CRACKED AT FR80/82 -Y2127. REMOVED T-PROFILE IN MAIN CABIN AT FR80/82 -Y 2127. IAW SRM 51-40-21. INSTALLED. MAIN CABIN NEW T-PROFILE AT FR80/82-Y2127 IAW SRM 51-40-21 USED.SDR IPXA2025102355969Profile · damagedMAIN CABIN - Z-PROFILE CRACKED AT FR75 Y2127.6. REMOVED Z-PROFILE IN MAIN CABIN AT FR75 Y 2127.6 IAW SRM 51-40-21. INSTALLED NEW Z-PROFILE AT FR75 Y2127.6 IAW SRM 51-40-21.SDR IPXA2025102356317Web · damagedMAIN CABIN - WEB CRACKED BTW FR73-FR74 Y2127.6. REMOVED WEB IN MAIN CABIN BTW FR73-FR74 Y2127.6 IAW SRM 51-40-21. ++INSTALLED NEW WEB BTW FR73-FR74 Y2127.6. IAW SRM 51-40-21.SDR IPXA2025102356212Web · crackedMAIN CABIN - WEB CRACKED BTW FR73-FR74 -Y2127.6. REMOVED Z-PROFILE IN MAIN CABIN BTW FR73-FR74 -Y 2127.6 IAW SRM 51-40-21. INSTALLED NEW Z-PROFILE AT FR73-FR74 -Y2127.6 IAW SRM 51-40-21.SDR IPXA2025102261418Adapter · corrodedMAIN CABIN - CLS ADAPTER (SEAT TRACK) WITH CORROSION AT FR 27 Y0 RH VERIFIED INSTALLATION OF CLS ADAPTER IAW SRM 51-40-21. OPENSDR IPXA2025102261494Adapter · corrodedMAIN CABIN - CLS ADAPTER (SEAT TRACK) WITH CORROSION AT FR 27 Y0 LT VERIFIED INSTALLATION OF CLS ADAPTER IAW A300-600 SRM 51-40-21 (1 TUBE QTY). OPENSDR IPXA2025102158491Seat Track · corrodedMAIN CABIN - SEAT TRACK WITH CORROSION AT FR67 Y0. INSTALLED NEW SEAT TRACK BTW FR66-FR67 AND FR68-69 Y0 IAW AIRBUS A300-600 SRM 53-10-16 PAG.207, FIG. 20.SDR IPXA2025101555582Profile · crackedMAIN CABIN - T-PROFILE CRACKED AT FR80/82 Y2127. REMOVED T-PROFILE IN MAIN CABIN AT FR80/82 Y 2127. IAW SRM 51-40-21. INSTALLED. MAIN CABIN NEW T-PROFILE AT FR80/82 Y2127 IAW SRM 51-40-21 USED.SDR IPXA2025101458777Adapter · corrodedMAIN CABIN, CLS ADAPTER WITH CRACK AT FR37 BTW Y1580.5 & Y2127.5 LOCATED AND DRILLED CLS ADAPTER . IAW A300 SRM 51-40-40. REQUEST OK TO INSTALL.SDR IPXA2025101458725Adapter · corrodedADAPTER WITH CORROSION AT FR 38 BTW Y1580.5 & Y2127.5. INSTALLED CLS ADAPTER IAW A300 SRM 51-40-21.SDR IPXA2025102434573Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. ONE CRACK NOTED AT RIB 17. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.SDR IPXA2025102434841Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. TWO CRACKS NOTED AT RIB 27. ACCOMPLISH PERMANENT REPAIR IAW EA 300-5750-27-A4183, REV. -.SDR IPXA2025102434554Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1EA CRACK NOTED AT RIB 11. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.SDR IPXA2025102434561Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1EA CRACK NOTED AT RIB 18. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.SDR IPXA2025102434775Rib · crackedFAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 2EA CRACKS NOTED AT RIB 26. CIRCLED IN RED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -. REVIEWEDSDR IPXA2025102434779Rib · crackedFAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 2EA CRACKS NOTED AT RIB 25. CIRCLED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -. REVIEWEDSDR IPXA2025102838770Fitting · crackedCRACK FOUND AT OPEN HOLE OF LT WING FR 40 LOWER RADIUS, CRACK NOTED AT FIRST LAYER FWD LAYER, 6 O'CLOCK POSITION, CRACK DEPTH FROM FWD TO AFT AT 5MM. INSTALLED REINFORCING SKIN AND STIFFENER UNDER IAW SRM 51-40-21 .SDR IPXA2025101740226Floor Support · crackedCABIN FLOOR SIDE SUPPORT BETWEEN FR 38.1 AND FR38.2 LH, Y2462 CRACKED. JP-110. REMOVED SIDE FLOOR SUPPORT BTW FR38.1 AND FR38.2 LH IAW SRM 51-40-21. INSTALLED NEW SUPPORT BRACKET IAW SRM A300-600 51-40-21.SDR IPXA2025103099591Web · crackedNR 1 PYLON RIB 3 UPPER WEB CRACKED. JP-110. INSTALLED PYLON #1 SUPPORT OF THE PRESSURE RELIEF DOOR, IAW-A300-AMM 54-52-62/401 ITEM (4).SDR IPXA2025102298127Support · crackedCABIN FLOOR SIDE SUPPORT BETWEEN FR 38 AND FR38.1 LH, Y2462 CRACKED. REMOVAL FUNNEL FROM FRAME 34 TO FRAME 38 AND FROM FRAME 38 TO FRAME 38.2 IAW SRM 51-40-21 AND AIPC 25-58-04-85B. FLOOR SIDE SUPPORT WAS REMOVED FROM FR 38 TO FR 38.1 LH IAW A300-600 SRM 51-4SDR IPXA2025101498133Floor Support · crackedCABIN FLOOR SIDE SUPPORT BETWEEN FR 37 AND FR38 RH, -Y2462 CRACKED. JP-110. REMOVED SIDE SUPPORT BETWEEN FR 37 AND FR 38 RH -Y2462 IAW SRM 51-40-21. SIDE SUPPORT WAS INSTALLED IAW SRM 51-40-2.SDR IPXA2025102988759Web · crackedAFT CARGO COMPARTMENT WEB AT FR54, Y1959 CRACKED. REMOVED THE WEB AT FR54, Y1959 IAW SRM 51-40-21. INSTALLED NEW WEB ANGLE AT FR54 Y1959 LH SIDE.SDR IPXA2025102988782Angle · crackedAFT CARGO COMPARTMENT WEB AT FR54, Y953 LH CRACKED. REMOVED AFT CARGO COMPARTMENT WEB AT FR54, Y953 LT IAW SRM 51-40-21. INSTALLED NEW WEB ANGLE AT FR54 7953 LH SIDE.SDR IPXA2025101379065Angle · crackedAVIONICS COMPARTMNT FR9 ANGLE CRACKED AT Y950. FABRICATED AND DRILLED NEW ANGLE FITTING FROM 2024-T3 .063C", B/N:0004276732. IAW SRM 53-12-15 FIG.7ITEM #80 AND UPS GMM-09.08.01.03, FOLLOW #4. INSTALLED NEW ANGLE FITTING IAW SRM 51-40-21.SDR IPXA2025101379032Angle · crackedAVIONICS COMPARTMNT FR9 ANGLE CRACKED AT -Y950 JP-110. REMOVED WEB CRACKED RH SIDE IAW A300/600 SRM 51-40-21. INSTALLED NEW ANGLE FITTING IAW A300-600 SRM 51-40-21.SDR IPXA2024102271179Slide · unknownAFTER SHUTDOWN SLIDE DISARMS BUT WONT DISARM TO WHERE YOU CAN INSERT THE SAFETY PIN INSTALLED EMERGENCY EVACUATION SLIDE IAW MM 25-61-21SDR IPXA2023080293780Door · inoperativeINSPECTION TYPE:N/ACREW ENTRY DOOR GUST LOCK BUTTON STUCK DOWNLUBRICATED GUST LOCK BUTTON AND CHECKED DOOR OPERATION PER AMM 52 10 20. SOP CHECKS NORMAL AT THIS TIMESDR IPXA2023061793461Skin · gougedINSPECTION TYPE:C#2 ENGINE OB EXHAUST CONE AREA HAS A GOUGEREPAIRED AREA IAW PW SRM 54-40-00SDR IPXA2023060993406Fairing · crackedINSPECTION TYPE:C611AB OPENING HAS A CRACKREPAIRED AREA IAW SRM 53-15-63
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