N1511A
Service difficulty reports · 333
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 = 'N1511A' 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 = 'N1511A' 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 UIEA2026061100458Tamper Strip · tornELT NEXT TO L1 DOOR HAS TAMPER TAPE TORN. R & R PORTABLE ELT BY L1 DOOR IAW AMM 25-63-03 & AIPC 25-64-54-01B. OPS CHKD OK.SDR UIEA2026042200238Outflow Valve · faultedCABIN ALTITUDE EICAS MSG WARNING. PERFORMED EMERGENCY DESCENT TO 10,000 FT @ FL330, DIFF PSI 60-7.0, CABIN ALT 10000-11000 FT. NOTED OUTFLOW VALVE WAS APPROX HALF OPEN, NO CHANGE W/ AUTO 2 OR AUTO 1, WAS A SLOW RATE DECOMPRESSION.(<P>PERFORMED BITE TEST OF CABSDR UIEA2026032300105Escape Reel · inoperative1 EACH ESCAPE HARNESS INOPERATIVE ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} ESCAPE HARNESSES ) NR 2 ESCAPE HARNESS IS TRANSFER TO DMI 249625 PER MEL 25-61-01-02 CAT C DUE DATE 31MAR26. PLACARDS INSTALLED. MX ACTIONS C/W. INSTALLED SDR UIEA2025122701361Not Reported · not reportedREJECTED TAKEOFF DUE TO NON-MECHANICAL CONDITION. SPEED WAS APPROXIMIATELY 30 KNOTS.AND BRAKE TEMPS NORMAL.. PERFORMED HIGH STOP INSPECTION IAW AMM 05-51-14, NO DISCREPANCIES NOTED AT THIS TIME.SDR UIEA2025121401344Controller · faultedAT TOP OF DESCENT, CREW ALTITUDE EICAS MSG. CABIN ALT WENT TO 11,000 FT AFTER DESCENT TO 8000 FT, CABIN PRESS DIFF WAS 0.(<P>FOLLOWED FIM FOR CABIN ALTITUDE BITE CHECK PER FIM 21-31-00. FOUND CABIN ALT CONTROLLER 2 FAULT LOW FLOW. THEN FOLLOWED AMM 36-23-00 AISDR UIEA2025102501279Bottle · no test#2 FIRE CARGO BOTTLE WON'T TEST(<P>PERFORMED ALL WIRING CHECKS FROM THE SQUIB TEST PANEL TO EACH SQUIB FOR BOTTLES 1, 2, & 2A PER WDM 26-23-12, FOUND PIN 14 ON D866 AND PIN 14 ON D864 HAD NO GROUND FOR TEST CIRCUIT. FOUND APU/CGO FIRE CONTROL PANEL REPLACED. LSDR UIEA2025093001247Door Frame · crackedCRACK (1 EA) IS DETECTED AT L1 FWD ENTRY DOOR AFT LWR CORNER DURING OPEN HOLE HFEC INSPECTION IAW EO 6753A937(<P>REPAIRED WITH 2 EA OF FILLER AND 3 EA OF DOUBLER AS PER SRM 53-10-01-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025093001248Fitting · crackedFUSELAGE SECTION 48 BODY STATION 1809.5 BULK HEAD LH TENSTION FITTING CRACK(<P>REAMED FASTENER HOLE TO A DIAMETER OF 0.3120" AS PER SRM 51-40-05 & SP1-TLS-25-0031-038. PERFORMED OPEN HOLE HFEC INSPECTION PER NDTM 51-00-16 PART 6, RESULT NORMAL. R/R FASTENER PESDR UIEA2025093001249Skin · damagedREQUIRED TO PERFORM SURFACE HFEC INSPECTION AT REPAIRED AREA (REF EO 6755A032)(<P>ACCOMPLISHED SURFACE HFEC INSPECTION AT RH HORIZONTAL STAB. REPAIRED AREA PER NDTM 51-00-19 PART 6, RESULT NORMAL. INSPECTED THE BLIND RIVETS LOCATED AT THE HORIZONTAL STAB RH UPSDR UIEA2025093001250Door · crackedCRACKS (2 EA) ARE DETECTED AT R1 FWD ENTRY DOOR AFT LWR CORNER DURING OPEN HOLE HFEC INSPECTION IAW EO 6753A937(<P>REPAIRED WITH 2 EA OF REPAIR FILLER & 3 EA OF DOUBLER AS PER SRM 53-10-01-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025071600960Oxygen Mask · no testRH PAX OXYGEN MASK WILL NOT TEST. R/R RH PAX O2 MASK IAW AMM 35-11-51. OPS CHK GOOD AT THIS TIME. NO LEAKS NOTED AT THIS TIME.SDR UIEA2025071600961Oxygen System · no discrepancyPAX OXYGEN SYSTEM SUSPECT LEAK. SERVICED PAX O2 TO 1760 PSI PER AMM 12-15-08 & GMM 3.25.2 & 3.25.3. AFTER SITTING FOR 3 DAYS, NO LEAKS DETECTED. NO FURTHER DEFECTS NOTED.SDR UIEA2025071600962Seal · brokenPORTABLE ELT SEAL BROKEN. INSPECTED TAMPER TAPE ON PORTABLE ELT IAW AMM 25-05-03. FOUND SMALL WEAR MARK BUT SEAL IS INTACT AND NOT BROKEN. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR UIEA2025052800701Seal · missingF/O EVAS MISSING SEAL. R & R THE TAMPER SEAL IAW AMM 25-60-99. NO FURTHER DEFECTS NOTED.SDR UIEA2025040900449Bottle · low pressureSUPERNUMERARY PAX O2 LOW.(<P>R/R PAX O2 CYLINDER IAW AMM 12-15-08. LEAK CHECK GOOD.</P>)SDR UIEA2024111501090Pump · faultedCTR L FUEL PUMP EICAS MSG IN CRUISE WITH 22000 LBS OF FUEL IN THE CTR TANK, FOUND C/B POPPED(<P>R/R LH FUEL CENTER OVERRIDE PUMP IAW AMM 28-22-05. OPS & LEAK CHK GOOD. DMI 220641 CLOSED</P>)SDR UIEA2024081900837Escape Reel · unsecureESCAPE REELS ARE LOOSE(<P>RESECURED ESCAPE REELS IAW AMM 25-61-05/401. OPS CHECK GOOD</P>)SDR UIEA2024062000560Elt · inoperativeENTRY WAY ELT AT L1 INOP ( EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS )(<P>TRANSFERRED TO DMI 211008 IAW MEL 25-63-10-01 CAT D DUE DATE 18OCT24. MCC NOTIFIED.REMOVED AND REPLACED PORTABLE ELT IAW AMM 25-63-03, THIS CLEARS DMI 211088, PLACARDS REMOSDR UIEA2024062000559Elt · inoperativeCOCKPIT ELT INOP ( EMERGENCY LOCATOR TRANSMITTER (ELT), SURVIVAL TYPE ELTS )(<P>REMOVED AND REPLACED LAV PORTABLE ELT IAW AMM 25-63-03. OPS CHECKS GOOD. THIS CLEARS MDDR 211017. MCC NOTIFIED. PLACARDS REMOVED.</P>)SDR UIEA2024051800392Hook And Loop · wornFO'S EVAS HOOK AND LOOP STRIP ON GLARESHIELD IS WORN OUT(<P>RE-SECURED FO'S EVAS GLARESHIELD VELCRO IAW B767 AMM 25-60-99. NO OTHER DEFECTS NOTED.SDR UIEA2024041900297Doubler · damagedONE CRACK INDICATION FOUND ON NOSE WHEEL WELL IN SRM 3 PLATE RADIUS ON RBL 25 VERTICAL CHORD AT WL 173 0.400 LONG(<P>DAMAGED DOUBLER WAS REPLACED PER EO6753A027. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400307Skin · dentedRH WING OUTBOARD FLAP INNER SURFACE FWD SECOND BAY STA 622 APPROX WITH TWO DENTS(<P>DENTS (2 EA) ON RH WING OUTBOARD FLAP INNER SKIN PANEL WERE REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400308Skin · dentedRH WING OUTBOARD FLAP INNER SURFACE FWD SECOND BAY STA 636 WITH DENT(<P>DENT ON RH WING OUTBOARD FLAP INNER SKIN LOWER PANEL AT OTEF 101.73 WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400309Skin · debondedLH HORIZONTAL STAB FIXED LE, DISBONDED PREVIOUS REPAIR ON LOWER SKIN AT L.STA 366.377(<P>DISBOND ON LH HORIZONTAL STABILIZER LOWER SKIN WAS REPAIRED PER SRM 51-70-10-2R-0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400310Skin · delaminatedLH WING, SLAT #4 SURFACE INNERSIDE AREA UPPER INSIDE CORNER WITH DELAMINATION.(<P>DELAMINATIONS (2 EA) ON LH WING SLAT #4 T/E WEDGE WERE REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024042400311Skin · delaminatedDELAMINATED UPPER CORNER OF SLAT 9 AT RH WING(<P>DELAMINATION ON RH WING SLAT# 9 T/E WEDGE UPPER SKIN INBD CORNER WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400312Skin · delaminatedDELAMINATED UPPER CORNER (UPPER SURFACE) OF SLAT 12 AT RH WING(<P>DELAMINATION ON RH WING SLAT #12 T/E WEDGE UPPER SURFACE WAS REPAIRED PER SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042400315Skin · delaminatedLH WING, INBOARD FLAP SURFACE INNER SIDE AREA AFT FLAP OUTSIDE CORNER WITH DELAMINATION(<P>DELAMINATION ON LH WING INBOARD AFT FLAP LOWER SURFACE WAS REPAIRED PER SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024042500316Skin · corrodedRH WING, TOP SURFACE,BTW WB 289.45 AND WBL 97.9566, DURING REMOVAL OF ACCESS SPOILER HINGE PANEL, CORROSION WAS FOUND ON THE SPOILER BEAM(<P>CORROSION RH WING TRAILING EDGE STRUCTURE INBOARD SPOILER SUPPORT BEAM UPPER CHORDS WERE REPAIRED PER SRM 57-51-02-2R-2SDR UIEA2024042600317Beam · corrodedCORROSION ON RH WING TRAILING EDGE STRUCTURE SPOILER BEAM UPPER CHORDS BETWEEN WBL 154.54 / 294.02(<P>CORROSION DAMAGES ON RH WING TRAILING EDGE STRUCTURE SPOILER BEAM UPPER CHORDS WERE BLEND OUT, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS PER SRM 57-51-02-1ASDR UIEA2023112080961Blade · damagedBIRDSTRIKE ON RH ENG. FOUND FANBLADES #32 & 34 DAMAGED(<P>R/R FAN BLADES #32, 34, 13 AND 15 IAW AMM 72-31-02. C/W ENG TEST #8. ALL VIBE INDICATIONS WITHIN LIMITS.</P>)SDR UIEA2023091500834Battery Pack · unknownAISLE EMERGENCY LIGHING INOP. R/R EMERGENCY BATTERY PACK IAW AMM 33-51-07. OPS CHECKS GOOD. DMI 193326 CLOSED</P>)SDR UIEA2023060300555Escape Reel · unknown1 EA INTERTIA REEL INOP. SUPPORT BRACKET BROKEN . INERTIAL REEL REMOVED FROM ACFT(<P>TRANSFERRED TO DMI 186721 IAW MEL 25-61-01-01 CAT C DUE DATE 13JUN23. MX ACTIONS C/W. INERTIAL REEL REMOVED FROM ACFT. 6 INERTIAL REELS REMAIN SERVICEABLE. INSTALLED DESCENT SDR UIEA2022122801220Lamp · inoperativeEMERGENCY LIGHT ON RIGHT SIDE CEILING INOP. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00.SDR UIEA2022121101211Skin · dented#10 SLAT HAS SEVERAL DEEP DENTS ON TOP OF THE SLAT.(<P>REPAIRED #10 SLAT IAW SRM 51-70-10-2R-2 REPAIR 2</P>)SDR UIEA2022090600939None · noneLH WING, ON L9 AND RIB 1 WITH LEAK OF FUEL(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV 136</P>)SDR UIEA2022090900943None · noneENGINE LH PERFORM TSM, PRV ( NOT CLOSED )(<P>ENGINE LH, TSM WAS PERFORMED. PRV, PRVC AND HPC WERE REPLACED AND TESTED OK IAW AMM 36-00-32-405-001 REV 136</P>)SDR UIEA2022090900944None · noneEVIDENCE OF HYDRAULIC LEAK, INBOARD PCA LEFT ELEVATOR(<P>ELEVATOR ACT ASSY POWER WAS REPLACED & OPS CHECK GOOD IAW AMM 27-31-05-424-027 REV 136</P>)SDR UIEA2022090900945None · noneRH WING CENTER SECTION, LOWER SURFACE, SPLICE STRINGER L-6 AND BBL97.42 WITH LEAK FUEL(<P>FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013 PARAGRAPH 2</P>)SDR UIEA2022090900946None · noneRH WING LOWER SURFACE, AT L-10 BETWEEN WS 197 AND WS 228 WITH FUEL LEAK(<P>FUEL LEAK WAS REPAIRED PER <SPAN> </SPAN><SPAN>AMM 28-11-00-308-013 PARAGRAPH 2</SPAN></P>)SDR UIEA2022090900947None · noneRH WING LOWER SURFACE, AT L-10 BETWEEN WS 284 AND WS 344 WITH FUEL LEAK(<P>FUEL LEAK WAS REPAIRED PER <SPAN> </SPAN><SPAN>AMM 28-11-00-308-013 PARAGRAPH 2</SPAN></P>)SDR UIEA2022090900948None · noneRH WING LOWER SURFACE, AT L-10 AND WS 486 WITH FUEL LEAK(<P>FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013</P>)SDR UIEA2022090900949None · noneLOG BOOK PAGE 1524770: ATC FAULT WITH LH XPONDER SELECTED(<P>FIM TASK 34-53 FAULT TREE 805 WAS PERFORMED. TEST WAS SATISFACTORY</P>)SDR UIEA2022090900950Rod End Bearing · noneLH ELEVATOR, INBOARD POWER CONTROL ACTUATOR , INPUT ROD END BEARING DAMAGED(<P>INBOARD POWER CONTROL ACTUATOR INPUT ROD END BEARING WAS REPLACED <SPAN>AMM 27-31-07-424-016 REV 136</SPAN></P>)SDR UIEA2022090900951None · noneRIGHT ELEVATOR ACTUATOR INPUT ROD, RIGHT CENTER OUT OF LIMITS (COLLAPSING DIRECTIONS 65.5LBS/0.845")(<P>RIGHT ELEVATOR ACTUATOR INPUT ROD WAS REPLACED 27-31-07-424-016 REV136. OPS CHECK GOOD</P>)SDR UIEA2022090900952None · noneRH FUEL LEAK BETWEEN WSTA 197.4/226.3 AT STGR L-15(<P>FUEL LEAK WAS REPAIRED AMM 28-11-00-308-013 REV 136.</P>)SDR UIEA2022090900953None · noneRH FUEL LEAK BETWEEN WSTA 375.8/404.4 AT STGR L-6(<P>FUEL LEAK WAS REPAIRED <SPAN>AMM 28-11-00-308-013 REV 136</SPAN></P>)SDR UIEA2022062800674Truck · smokeAFTER 400 YARDS OF TAXI ANOTHER AIRCRAFT REPORTED SMOKE COMING FROM BOTH LANDING GEAR TRUCKS. ARFF REPORTED NO HEAT READING. RTB(<P>PERFORMED GVI OF LT/RT MAIN LANDING GEAR ALONG WITH WHEELS AND BRAKES NO DEFECTS FOUND. PERFORMED ANTI SKID BITE TEST IAW B767 ASDR UIEA2022012700078None · noneCAPTS O2 MASK NOT WORKING PROPERLY.(<P>SWAPPED CAPTAINS O2 MASK WITH # 1 SUPERNUMARY O2 MASK IAW AMM 35-11-51. CAPT MASK OPS GOOD. # 1 SUPERNUMARY O2 MASK TRANSFERRED TO MDDR 160411 IAW MEL 36-11-03-02A, CAT C, DUE DATE 06FEB22.</P> / <P>CVG MX- 29JAN. LP 15SDR UIEA2022012500076Shutoff Valve · leakingAIR RETURN, HYDRAULIC QUANTITY DROPPING DURING FLIGHT. .86 DROPPED TO .72 HYD QTY IN FLIGHT. .96 QTY HYD ON TAXI OUT.(<P>FOUND HYRAULIC LEAK @ RUDDER & ELEVATOR SHUT OFF VALVE (V 101). REMOVED AND REPLACED L EMPENNAGE SHUTOFF VALVE IAW AMM 267-3001 27-23.01. O
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