N618FE
Service difficulty reports · 366
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 = 'N618FE' 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 = 'N618FE' 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 FDEA201611294286Door Frame · crackedR3 DOOR FRAME FWD UPPER WEB IS CRACKED ON THE AFT END, ACCOMPLISHED REPAIR ON R3 DOOR JAMB FWD UPPER WEB IAW EA 1-5310-T329909 P1.SDR FDEA201611264252Doubler · crackedRIGHT WING FIXED L/E BEADED DOUBLER AT XOS 648 - 703 HAS NUMEROUS CRACKS, REPAIRED IAW SRM 57-40-02-2R, FIG 203.SDR FDEA201611264250Doubler · crackedRIGHT WING FIXED L/E BEADED DOUBLER IS CRACKED AROUND FOUR FASTENERS BETWEEN XOS 62 5- 629. REPAIRED IAW SRM 57-40-02-2R, REP 15, FIG 203.SDR FDEA201611264249Doubler · crackedLEFT OTBD WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACKED AT XOS 587. REPAIRED IAW SRM 57-40-02-2R, FIG 203.SDR FDEA201611264248Doubler · crackedLEFT OTBD WING FIXED L/E COMPARTMENT BEADED DOUBLER CRACKED AT XOS 544. REPAIRED IAW SRM 57-40-02-2R, FIG 203.SDR FDEA201611234233Web · crackedMAIN CARGO BAY L3 DOOR FRAME LOWER TORSION BOX HASA WEB CRACKED, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-40-15-2R, FIG 201.SDR FDEA201605091518Hydraulic Line · leakingON TOUCH DOWN WHEN AUTO BRAKE ENGAGED, ACFT PULLED TO THE LT. MANUALLY DISCONNECTED AUTO BRAKE & MANUALLY BRAKED TO TURNOFF SPEED. UPON ARRIVAL AT GATE THE NR 8 BRAKE INDICATED A HYD LEAK. R & R HYD LINE FOR NR 8 BRAKE ASSEMBLY IAW AMM 20-40-01-2.SDR FDEA201601300400Switch · brokenPRIOR DEPARTURE, FOUND R1 EVAC SLIDE PTT SWITCH BROKEN. R1 DOOR OPERATES NORMAL. REPLACED PTT SWITCH IAW MM 25-61-04-4. ACFT OK FOR SERVICE.SDR FDEA201508052486Shutoff Valve · malfunctionedAT FL 320, 2 30 HRS INTO FLIGHT, RECEIVED LEVEL 1 ALERT. ENG 2 ANTI-ICE OFF. CONSULTED QRH, REFERENCING EXISTING MEL 30-22-02-03-A. WE WERE CONCERNED WITH POSSIBLE LIKELY DUCK LEAK. LANDED AT NEAREST SUITABLE AIRPORT. TROUBLE SHOT IAW FIM 30-22-07-00. RESDR FDEA201506292112Engine · failedCLIMBING TO FL 350 AT APPROX FL 250 AT CLIMB POWER, HAD A NR 3 ENG EVM COMPUTER AMBER BOX 5.0. ALL OTHER ENG PARAMETERS NORMAL., HAD AIRFRAME VIBRATION WITH THROTTLE OUT OF IDLE. CLIMB POWER N1 WAS 105. RAN QRH & CALLED MX, RECOMMENDED RTB. TURBINE FAILURESDR FDEA201506282110Charger · inoperativeEMERGENCY LIGHT TEST HAS, BATT 1 LO, ALERT. FAULT WAS AT POWER UP AFTER LAYOVER. AFTER 2 HOURS ALLOWED TO CHARGE, FAULT CONTINUES. R & R BATTERY & CHARGER PACK.SDR FDEA201505131504Handle · looseL1 DOOR ARMING HANDLE SAFETY BUTTON WILL NOT STAY IN THE SAFE POSITION. FOUND HARDWARE LOOSE ON ARMING HANDLE. SECURED HARDWARE, BUTTON NOW STAYS IN THE SAFE POSITION.SDR FDEA201502160535Sign · unsecureEXIT SIGN OVER DOOR R1 FELL OFF. SECURED DOOR R1 EXIT LIGHT COVER IAW AMM SMP. ACFT OK FOR SERVICE.SDR FDEA201412024023Hinge · wornMAIN DECK CARGO DOOR HINGE, DOOR SIDE, FOUND 8 EACH HINGE LOBES EXCEED WEAR LIMITS.SDR FDEA201412013988Support Angle · crackedLEFT WING NR 2 SLAT OTBD EDGE SUPPORT ANGLE FOUND CRACK AT STATION XDLE 328. ANGLE REMOVED IAW SRM 51-35-01, A NEW SUPPORT ANGLE WAS FABRICATED IAW DRAWING ARB1647 REVISION C, AND INSTALLED IAW SRM 51-35-01 AND EA 1-5750-T0313966 PART 1 STEP 5. REPAIR CLSDR FDEA201412013987Rib · crackedLEFT WING NR 2 SLAT RIB AT STATION XIS 342 FOUND CRACKED. RIB REMOVED IAW SRM 51-35-01, A NEW RIB FABRICATED IAW DRAWING ARB1629 AND INSTALLED IAW SRM 51-35-01 AND EA 1-5750-T0313966 PART 1 STEP 4. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201411303983Doubler · crackedRIGHT WING FIXED LE BEADED DOUBLER FOUND CRACK AT STATION XOS 613.SDR FDEA201411263898Wedge · delaminatedRIGHT WING OTBD FLAP TE WEDGE INBD EDGE FOUND DELAMINATION 6 INCHES X 12 INCHES.SDR FDEA201311122745Slat System · malfunctionedDURING SLAT EXTENSION, THE SLATS REMAINED RETRACTED. RAN QRH AND MADE A SLATS RET 28 FLAP LANDING. PERFORMED OPS CHECK OF SLATS REF AMM 27-80-01-5. OPS CHECKED GOOD.SDR FDEA201301250178Skin · damagedON BLOCK IN, VISUALLY FOUND TAIL STRIKE. MULTIPLE AREA OF DAMAGE TO TAIL SECTION BELLY SKIN AND STRUCTURE.SDR FDEA201210143613Battery · failedPREFLT CHECK FOUND LEVEL 1 "EMER LT BAT LO" R & R EMERGENCY EXIT LIGHTS BATTERY IAW MM 33-51-01-4,CARRIED OUT OPS TEST IAW MM 33-51-01-05.SDR FDEA201210023529Access Panel · corrodedRT WING T/E LOWER ACCESS PANEL NR 641JB CUT-OUT FORWARD TEE FITTING, FOUND CORROSION. TEE FITTING REPAIRED IAW EA 1-5710-163502. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201209303517Longeron · crackedBS 595, LONGERON 49 RT FASTENER HOLE COMMON TO RT NLG TRUNNION FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 50 AND SRM 51-33-01 REVISION 50. NEW LONGERON FABRICATED AND REWORKED AS PER DRAWING ACA3796 REVISION A. REPAIR CLASSIFIED AS MAJSDR FDEA201209283487Structure · corrodedOVERWING TANK PANEL BS 1234, "X" = 0, FOUND CORRODED. EXFOLIATION CORROSION REMOVED IAW SRM 51-21-01 REVISION 50. FOUND ACCEPTABLE AS PER EA 1-5730-163505, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209273470Access Panel · crackedRT WING L/E LOWER SURFACE ACCESS PANEL 619AB CUTOUT, FORWARD EDGE FOUND CRACKED AT STA XOS 608. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209273471Skin · crackedRT WING FIXED L/E LOWER SURFACE AT STATION XOS 775 (NR 12 SLAT TRACK LOWER CUTOUT) FOUND CRACKED. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209273469Access Panel · crackedLT WING - L/E LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBOARD CORNER AS PER SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 50. REPAIR CLASSIFIEDSDR FDEA201209263444Doubler · crackedRT WING REFUELING ACCESS DOOR COMPARTMENT UPPER BEADED DOUBLER CRACKED BETWEEN XOS 640 AND XOS 648. REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209263443Doubler · crackedRT WING LOWER FIXED L/E AT XOS 612 INBD REFUELING PANEL CUTOUT FWD CORNER, FOUND CRACKED.SRM 51-31-01 REVISION 50. NEW DOUBLER FABRICATED AS PER DRAWING ARB2933 REVISION AJ AND INSTALLED AS PER SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR FDEA201209253435Trunnion · crackedNLG WHEEL WELL, RT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209253434Trunnion · crackedNLG WHEEL WELL LT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50 AND REPAIR PARTS INSTALLED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6SDR FDEA201209253433Skin · chafedFORWARD CARGO DOOR FORWARD LOWER CUTOUT FOUND EDGE CHAFED. TRIMMED OUT AND REPAIR CARRY-OUT AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 50 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209253432Tee Fitting · corrodedLT WING T/E LOWER ACCESS PANEL 541JB CUTOUT FORWARD TEE FOUND CORRODED AT XW317. CUTOUT FORWARD AREA REMOVED AS PER SRM 51-31-01 REVISION 50 AND REPLACED WITH NEW TEE AS PER SRM 51-35-01 REVISION 50 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR SDR FDEA201205101787Bottle · low pressureDURING POST FLT CHECK, FOUND L1 DOOR PNEUMATIC PRESSURE LOW. SERVICED PASSENGER DOOR PNEUMATIC STORAGE BOTTLE. PRESSURE AND LEAK CHECKED GOOD.SDR FDEA201112125246Valve · failedR1 DOOR ESCAPE SLIDE PNEUMATIC ACCUMULATOR PRESSURE GAUGE READS BELOW GREEN BAND. SERVICED R1 DOOR PNEUMATIC STORAGE IAW MM 12-25-04-3-0. REF ITEM 52-10/7162 R & R R1 BOTTLE RECHARGE VALVE.SDR FDEA201106252422Reservoir · dischargedDURING TRANSIT CHECK, FOUND R1 DOOR PNEUMATIC STORAGE RESERVOIR PRESSURE BELOW GREEN BAND. SERVICED R1 DOOR IAW AMM 12-25-04-3, ACFT OK TO CONTINUE SERVICE. FINAL CLOSED.SDR FDEA201104011276Bottle · underservicedR1 DOOR ASSIST BOTTLE NEEDS SERVICE. SERVICED R1 DOOR ASSIST BOTTLE IAW MM 12-25-04-0. FINAL CLOSED.SDR FDEA201102020454Motor · leakingHYD 3 FAIL, HYD 3 QTY DECREASED TO 0 (ZERO). FUEL DUMPED AND EMERGENCY GEAR EXTENSION IAW JQH. R & R NR 3 UPPER AND LOWER HYD EDP IAW AMM 29-11-20-4. TURN OVER TO NEXT SHIFT FOR LEAK CHECK AND TEST. CHECK FOUND HYD LEAKED FROM THE CASING OF NR 3 HYD HORIZ SDR FDEA201011084285Frame · deformedMAIN DECK CARGO - FRAME AT STA 1721, LONGERON 12 LT FOUND DEFORMED. MAIN DECK CARGO STATION 1721 LONGERON 12LH FRAME AREA CARRIED OUT REPAIR AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 44. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 1SDR FDEA201011024229Fitting · crackedLWR VERTICAL STABILIZER FOUND RT SIDE BANJO FITTING FWD CRACK. REPAIR CARRIED OUT AS PER SRM 55-30-02 REPAIR 3 REVISION 44 AND EA 1-5530-143476: REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201011014202Skin · cracked10 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA XORS 713.6. REPAIR CARRIED OUT AT R/H WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= SDR FDEA201011014201Skin · cracked08 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA 713.6.SDR FDEA201011014200Longeron · crackedCTR CARGO COMPARTMENT RT TUNNEL STRUCTURE FOUND LONGERON L-29 CRACKED AT STA 1676. LONGERON AT STATION 1676 L-29RH CENTER CARGO COMPARTMENT TUNNEL TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-00-05 FIGURE 202 REVISION 44. THIS REPAIR IS CLASSIFIED AS MSDR FDEA201008163009Heat Exchanger · failedPASSING FL200, RECEIVED LEVEL 2 "ENG 1 OIL TEMP HI" FOLLOWED BY DECREASING OIL QUANTITY AND DECREASING PRESSURE. NR1 ENGINE WAS SHUTDOWN IAW CHECKLIST AFTER OIL QUANTITY REACHED ZERO. OIL TEMP PEAKED AT 167 DEG. AFTER SHUTDOWN NOTICED OIL QUANTITY INCREASINSDR FDEA200903110888Skin · corrodedMAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -70. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR FDEA200903110887Skin · corrodedMAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -54. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR FDEA200903110886Skin · corrodedMAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -56. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR FDEA200903110885Skin · corrodedMAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = -25. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR FDEA200903110884Skin · corrodedMAIN DECK UNDER FLOOR, CENTER WING UPPER SKIN SURFACE FOUND CORROSION AT STA 1229, X = 0. COMPLIED WITH E.A. 1-5710-127476. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR FDEA200903050848Skin · chafedFORWARD CARGO DOOR CUT-OUT AFT EDGE, APPROX STA 1009, LONGERON 39-R FOUND CHAFED SKIN ADA7030-1. CARRIED OUT REPAIR AS PER SRM 53-50-01 FIG. 17 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.
Back to N618FE