N528FE
Service difficulty reports · 229
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 = 'N528FE' 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 = 'N528FE' 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 FDEA2019110752883Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT LBL 18 SHOWING EXFOLIATTION AREA MARKED DOT 37 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGESDR FDEA2019110752882Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR AREA, STRUCTURE/AROUND FASTNERS NEAR STA 1225 AT CENTER- LINE SHOWING EXFOLIATTION AREA MARKED DOT 36 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- SSDR FDEA2019112243018Floor Panel · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1321 AT LBL 106 TUNNEL. STRUCTURE EXFOLIATED DOT 16 REMOVED CORROSION, ALODINED AND FR-PRIMED AREA PER SRM 51-21-01-0G. BLEND OUT AREA IS ACCEPTABLE TO USE AS IS REF E.A # T-1-5730-T0349941 P1. WING PLATES AND SKISDR FDEA2019102142701Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1321 AT RBL 106 TUNNEL STRUCTURE EXFOLIATED DOT 16 REWORKED AREA I.A.W. E.A # 1-5730-T0350534 WING-PLATES AND SKINS-CENTER WING UPPER SKIN PANEL RHS-REWORK.SDR FDEA2019101342689Fuel Tank · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1270 LBL 106 IN TUNNEL AREA STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 29 REMOVED CORROSION, ALODINED AND FR-PRIMED AREA. PER BOEING BLEND OUT AREA IS ACCEPTABLETO USE AS IS REF SRM 57-10-01SDR FDEA2019101392686Skin · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1260 LBL 106 IN TUNNEL AREA STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 28 REPAIRED PER E.A # T-1-5730-T0350159 TITTLED "WING-PLATES AND SKINS-CENTER TANK UPPER SKIN EXFOLIATION SEVERAL LOCATSDR FDEA2019110742890Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 FROM RBL 75 TO NEAR RBL95 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 23 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANSDR FDEA2019110742885Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA. 1225 RBL 62 STRUCTURE EXFOLIATED DOT 15 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110742881Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 LBL 32 SHOWING EXFOLIATION ON STRUCTURE/AROUND FASTNERS AREA MARKED DOT 26 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110742880Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 FROM RBL 25 TO NEAR RBL45 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 25 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANSDR FDEA2019110742879Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 FROM RBL 60 TO NEAR RBL 75 STRUCTURE/AROUND FASTNERS SHOWING EXFOLIATTION AREA MARKED DOT 24 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PASDR FDEA2019110742878Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 LBL 82 STRUCTURE EXFOLIATED DOT 20 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110742877Structure · corrodedUPPER CARGO COMPT. UNDER FLOOR NEAR STA 1225 LBL 47. STRUCTURE EXFOLIATED DOT 19 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110742876Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 RBL 12 STRUCTURE EXFOLIATED. SHOWING 2 EACH CLOSE TO EACH-OTHER DOT 18 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110742875Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 RBL 24. STRUCTURE EXFOLIATED DOT 17 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019110712874Structure · corrodedUPPER CARGO COMPT UNDER FLOOR NEAR STA 1225 RBL 70 STRUCTURE EXFOLIATED DOT 14 ALL WORK COMPLIED WITH ACCORDING TO E.A.# 1-5730-T0350197. TILLE: WING-PLATES AND SKINS- CENTER WING UPPER SKIN PANELS- STRINGER 15.SDR FDEA2019091732648Beam · crackedL/H O/B FLAP I/B HINGE O/B SIDE, FAIRING PANEL MOUNT STRUCTURE IS CRACKED. REPAIRED BEAM AT L/H FLAP HINGE O/B SIDE REF DOUGLAS DRAWING ARC0745, AND SRM 51- 31-01.SDR FDEA201909112240Seat Track · corrodedMAIN DECK SEAT TRACK HAS LIGHT GOUGE APPR AT STA 919 RBL 8. REPLACED DAMAGED SEAT TRACK SECTION AT STA 919TO STA 945 RBL-8 REF SRM 53-00-52 REPAIR 1 FIG 201.SDR FDEA2019110792869Skin · corrodedRH WING UPPER SURFACE - APPROX XORS 242 - STRINGER 18 - CORROSION AROUND FASTENER. 5121818. R/H WING UPPER SURFACE XORS 242, STR 18, REPAIRED PER SRM 57-00-01-1A, FIG 101, SHT 1, E.A 1-5730-T0349983 PT. 1, & DPS 4.50-143 .SDR FDEA2019100392409Skin · corrodedRH WING UPPER SURFACE, XORS 180, STRINGER 22R, HAD CORROSION AROUND FASTENER. REMOVED CORROSION IAW SRM 57-00-01-1A, SHEETS 6-8. AREA IS WITHIN LIMITS IAW SRM 57-00-01-1A, FIG 101, SHEET 1.SDR FDEA2019100392408Skin · corrodedRIGHT WING UPPER SURFACE, XORS 203, FOUND CORROSION AROUND FASTENER. REMOVED CORROSION IAW SRM 57-00-01-1A FIG 101 SHEET 1.SDR FDEA2019100392407Skin · corrodedRIGHT WING UPPER SURFACE, APPROX XORS 207, STRINGER 4 HAD CORROSION AROUND FASTENER. REMOVED CORROSION IAW SRM 57-00-01-1A, SHEETS 6-8, AREA IS WITHIN LIMITS IAW SRM 57-00-01-1A, FIG 101, SHEET 1.SDR FDEA201906281423Charger · malfunctionedLVL 1 " BATT CHARGER IONP" ON TAXI, FOUND BATT CHARGER CONNECTOR ON BATT CHARGER DIS-CONNECTED FROM BATT CHARGER...PERFORMED BATTERY CHARGER ADJ/TEST AND NOT FAULTS NOTED ALSO HAD APU RUNNING WITH LOAD APPLIED HAD NORMAL BATTERY CHARGING LIGHT COME ON ANDSDR FDEA201906281422Warning Message · illuminatedLVL 1 "BAT DISCHARGING" ALERT FL 380. DIVERTED.SDR FDEA201807021625Doubler · crackedFIXED WING LEADING EDGE UPPER INTERNAL BEADED DOUBLER PANEL HAS CRACK AT FASTENER HOLE NEAR WING STATION XOS 584.891.SDR FDEA201805221312Cylinder · leakingHYD ELEV 3 OFF AT 4.9 QUANTITY IN HYD SYSTEM 3. TURNED LT & RT HYD 3 PUMPS OFF. QUANTITY CONTINUED TO DECREASE. HYD 3 OFF ILLUMINATED AT 2.5, SELECTED HYD AUTO AND QUANTITY CONTINUED TO DECREASE. HYD 3 QUATITY AT .8 WHEN LANDING GEAR LOWERED NORMALLY. RESDR FDEA201711213296Roller Tray · corrodedCENTER CARGO BAY BS 1644 - 1654 CENTERLINE FLOOR TRAY IS CORRODED. REMOVED AND REPLACED THE DAMAGED SECTION OF THE ROLLER TRAY, IAW DWG NFJ6775 AND SRM 53-50-53. REPAIR 1, FIG 201, SHEET 3.SDR FDEA201711213294Roller Tray · corrodedCENTER CARGO BAY, AFT CTR ROLLER & LOCK FLOOR TRAY IS CORRODED. REMOVED AND REPLACED THE SECTION OF THE ROLLER TRAY IAW DWG NFJ 6775SDR FDEA201707262084Seat Track · damagedMAIN DECK SEAT TRACK IS DAMAGED BS 1451, RBL 8. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 3, FIG. 201, SHEETS 1 AND 2.SDR FDEA201707252028Access Panel · crackedRIGHT WING LOWER OUTER FUEL ACCESS DOOR ATTACH HOLES HAD CRACK INDICATIONS. REPAIRED IAW SRM 57-20-02-2R, PG 29.SDR FDEA201707252076Spar Cap · crackedNR 2 PYLON RT UPPER SPAR CAP FLANGE AT YID=408.5 HAS A CRACK IN THE OUTER RADIUS BETWEEN FWD EDGE AND THE FIRST FASTENER. REPAIRED IAW EA 1-5450-T0334610, PART 1.SDR FDEA201708152223Skin · crackedON TOP OF THE LEFT WING DROOPED LEADING EDGE, FOUND A SUSPECTED CRACK COMING FROM THE OUTBOARD MOST FASTNER HOLE. REPAIRED THE DROOPED L/E WITH DOUBLERS IAW SRM 57-40-01, REPAIR 5, FIG 201, SHEET 1-6.SDR FDEA201707192090Seat Track · corrodedMAIN DECK SEAT TRACK HAS MINOR SURFACE CORROSION AT BS 1441, LBL 8. REMOVED AND REPLACED THE SECTION OF SEAT TRACK FROM BS 1441 TO 1501 IAW SRM 53-00-52-2R, FIG 201, SHEETS 1-3.SDR FDEA201703240987Longeron · corrodedFOUND INTERNAL DOUBLER FOR ACCESS DOOR AT LONGERON 52L, BS 1711 CORRODED BEYOND LIMITS. REMOVED THE CORRODED DOUBLER IAW SRM 51-30-00. FABRACATED A NEW DOUBLER IAW DRAWING AGA7808. REPLACED THE CORRODED LONGERON AND CORRODED INTERNAL DOUBLER IAW SRM.SDR FDEA201703020724Warning Light · false activationL1 DOOR ALERT, DURING TAXI. SPRAY LUBED GIRT BAR & SWITCH AREA, CLEANED SWITCH, L1 DOOR CONNECTOR BACK SHELL, MOVED ROLLERS IAW SMP. OPERATED DOOR FIVE TIMES, DOOR SLIDE ARMED & DISARMED, L1 DOOR CLOSED LIGHT ON ECAM OUT IAW MM 52-11-02-2. OPS CHECKED NORSDR FDEA201609273379Brake Assy · failedDURING TAXI OUT, RECEIVED A TIRE DIFF TEMP ALERT. NR 3 & 4 TEMPS WERE 79 FOR NR 3 & 518 FOR NR 4. TAXIED TO PARKING, RECEIVED A LEVEL 2 TIRE PRESSURE LOW, FOLLOWED BY A TIRE FAIL. R & R THE NR 4 BRAKE IAW MM 32-43-20-04.SDR FDEA201607092334O-Ring · damagedNOTICED A SLOW LEAK IN HYD QTY NR 3 RESERVOIR ,WITH A LEVEL 1 "HYD 3 ELEV OFF" ALERT. CONFIGERED AND GEAR DOWN EARLY THE GTY CONTINUED TO DECREASE WITH EVENTUALLY GOING TO 0GALLIONS QTY AND LEVEL 2 "HYD 3 FAIL" ALERT. ALSO NR 1 HYD SYSTEM LEFT EDP APPEARSSDR FDEA201601020009Yoke · excess playTURNS TO THE RT, MORE PRONOUNCED AT SPEEDS LESS THAN 300 KTS, AN APPARENT PERCEIVED BIND IN THE YOKE. THEN LET’S GO & YOKE WILL THEN MOVE. ALSO NOTICED THIS WITH AUTOPILOT ENGAGED. PLAY IN THE YOKE, CAPTAINS SIDE. PERFORMED DETAILED VISUAL INSPECTION OF AISDR FDEA201509262962Coalescer Bag · dirtyDURING NR 1 ENG START, ODOR OF BURNT OIL FILLED THE COCKPIT. STRONG ODOR LASTED APPROX 90 SECONDS. ON DESCENT FOR LANDING, WHEN POWER REDUCED ODOR OF DIRTY SOCK OR MOLDY CHEESE BECAME STRONG IN COCKPIT. IAW MOCC COMPLIED WITH MTSI 21-50 1351. INSPECTED APUSDR FDEA201509242938Unknown · odorFUME EVENT ON ENG START. WHEN TRANSFER FROM ACFT TO APU AIR, EXPERIENCED STRONG ODOR OF DIRTY SOCK OR MOLDY CHEESE. WHEN STARTING ENG 1, EXPERIENCED STRONG PETROLEUM SMELL. CREW WILL SUBMIT FLIGHT SAFETY REPORT FOR FUME EVENT. DID APU RUN AS PER MD11 JRH. SDR FDEA201507282418Fuel Cell · corrodedCABIN UPPER CARGO COMPARTMENT, UNDERFLOOR AREA LEFT BS 1229, XCW = 37 CENTER WING TANK TOP SURFACE FOUND WITH CORROSION. REPAIRED IAW EA 1-5730-T0319232 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201507282417Fuel Cell · corrodedCABIN UPPER CARGO COMPARTMENT, UNDERFLOOR AREA RIGHT BS 1289, XCW = -109 CENTER WING TANK TOP SURFACE FOUND WITH CORROSION. REPAIRED IAW EA 1-5730-T0319232 P I. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.SDR FDEA201507282416Fuel Cell · corrodedCABIN UPPER CARGO COMPARTMENT, UNDERFLOOR AREA RIGHT BS 1309, XCW = -109, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION. REPAIRED IAW EA 1-5730-T0319232 P 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201507282415Fuel Cell · corrodedCABIN UPPER CARGO COMPARTMENT, UNDERFLOOR AREA BS 1234, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION. REPAIRED IAW EA 1-5730-T0319232 PART 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.SDR FDEA201507282414Fuel Cell · corrodedCABIN UPPER CARGO COMPARTMENT, UNDERFLOOR AREA RIGHT BS 1234, XCW = -95, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION. REPAIRED IAW EA 1-5730-T0319257 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201507282413Fuel Cell · corrodedCABIN UPPER CARGO COMPARTMENT UNDERFLOOR AREA, LEFT BS 1222, XCW = 17, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION. REPAIRED IAW EA 1-5730-T0319232 P 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201507272399Bracket · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0139125 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201507272398Bracket · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0319125 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201507272397Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE PIVOT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-02. REPAIRED IAW EA 1-5750-T0319124 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201507272396Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE PIVOT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0319124 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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