N778FD
Service difficulty reports · 82
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 = 'N778FD' 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 = 'N778FD' 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 FDEA202505220793Gust Lock · failedLEFT ENTRY DOOR GUST LOCK WILL NOT RELEASE TO ALLOW THE DOOR TO CLOSE. REPLACED SPLIT COLLAR ON L1 DOOR. OPS CHECK GOOD. OK TO CONTINUE SERVICE.SDR FDEA202403280398Frame · crackedCRACK INDICATION NOTED ON FRAME WEB INBD OF S-26R STA 1560 AT 12 O'CLOCK ON FASTENER HOLE. CRACK MARKED IN RED. REPAIRED BY EA F-5310-T0378490 PT1 TITLE: FUSELAGE - MAINFRAME - CRACK FOUND ON FRAME STA 1560 AT S-27R. MAJOR REPAIRSDR FDEA202403270382Floorboard · damagedZONE 220 COURIER FLOORBOARD 222AF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222AF ON VT MAE TRAVELER T24/1738846 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIRSDR FDEA202403250369Floorboard · delaminatedMAIN DECK FLOOR PANEL 251MWF LOWER SURFACE DELAMINATED AND TORN. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VT MAE TRAVELER T24/1741743 IAW DWG SRZ-25-005 REVISION "R". MAJOR REPAIRSDR FDEA202403250368Floorboard · damagedMAIN CARGO COMPT ZONE 230 FLOORBOARD PANEL 231MFF DAMAGED. FABRICATED ZONE 230 FLOORBOARD 231MFF ON VT MAE TRAVELER T24/1740237 IAW DWG SRZ- 25-005 REVISION "R". MAJOR REPAIRSDR FDEA202403250367Floorboard · damagedZONE 220 COURIER FLOORBOARD 221MBF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 221MBF ON VT MAE TRAVELER T24/1738845 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIRSDR FDEA202403250366Floorboard · damagedZONE 220 COURIER FLOORBOARD 222BF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222BF ON VT MAE TRAVELER T24/1738847 IAW DWG SRZ-25-005 REVISION "R" . MAJOR REPAIRSDR FDEA202403160299Floor Panel · damagedZONE 220 COURIER FLOORBOARD 221BF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 221BF ON VT MAE TRAVELER T24/1738844 REVISION "R" MAJOR REPAIR.SDR FDEA202403160298Floor Panel · damagedZONE 220 COURIER FLOORBOARD 221AF DAMAGED. FABRICATED ZONE 220 FLOORBOARD 221AF ON VT MAE TRAVELER T24/1738843 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR.SDR FDEA202403160297Floor Panel · damagedZONE 220 CURIER FLOORBOARD 222MDF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222MDF ON VT MAE TRAVELER T24/1738850 IAW DWG SRZ-25-005 REVISION "R" MAJOR REPAIR.SDR FDEA202403160296Floor Panel · damagedZONE 220 COURIER FLOORBOARD 222MAF DAMAGED. FABRICATED ZONE 220 COURIER FLOORBOARD 222MAF ON VT MAE TRAVELER T24/1738849 REVISION "R" IAW DWG SRZ-25-005. MAJOR REPAIRSDR FDEA202307121206Ball Screw · failedTE FLAP DISAGREE WHEN GOING TO FLAPS 25. COMPLETED QRH 9.1.17 LANDED FLAPS 20 ***EMERGENCY DECLARED*** ENT BY:5190314 RPT BY:5190314 R/I 12JUL23 22:37 MEM U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 7820924 CPN: 2717624 POSSDR FDEA202305050813Transmission · unknownTE FLAP DISAGREE EICAS WHEN FLAPS 20 SELECTED AT APPROX 170 KIAS, FLAP INDICATION SHOWED BETWEEN 15 AND 20. COMPLETED QRH 9.1.17 AND LANDED USING FLAPS 20.EMERGENCY DECLARED. ***EMERGENCY DECLARED***. TROUBLESHOT IN REF TO FIM 27-51 FAULT TREE 808 WITH NSDR FDEA202304250759Gust Lock · damagedMDIS 778 52-10 6283 23APR23 MEM FACT U L1 GUST LOCK BROKEN. FACT 25APR23 17:35 GSO U AMM: 52-11-08-8 REPLACED L1 DOOR HOLD OPEN LOCK COLLAR IAW B757 AMM. INSTALLED PART: ALLIANCE AEROSPACE ENGINEERING SPLIT LOCK COLLAR P/N 10-N6008-1 S/N SDR FDEA202304200726Unknown · unknownEMERGENCY DECLARED FOR TE FLAP DISAGREE. FLAP EXTENSION NORMAL TO 15 DEGREES. AT APPROX 175 KNOTS WE SELECTED FLAPS 20. THE FLAP INDICATOR MOVED TO APPROX 17 DEGREES AND STOPPED. TE FLAP DISAG EICAS MESSAGE WAS DISPLAYED. RAN QRH PROCEDURE AND LANDED WISDR FDEA202203280722Flap · unknownPREVIOUS COMPSITE MAJOR REPAIR RW O/B FLAP, UPPER SURFACE, APPROX. 52" FROM THE I/B END AND 5.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERDORMED PERMANENT REPAIR IAW B757 SSDR FDEA202203280720None · noneMAIN CABIN SEAT TRACK SCALLOP IS GOUGED LBL0 AT APPROX STA 1013 ACCOMPLISHED FEDEX EA# F-5310-T0367542 : FUSELAGE - MAINFRAME - SEAT TRACK STA 1013, BL 0, SPLICE REPAIRSDR FDEA202203280719None · noneFLOOR PANEL REQ REWORK IAW FEDEX EA F-5310-T0367574 REWORKED FLOOR PANEL IAW FEDWX EA F-5310-T0367574 FUSELAGE - MAIN FRAME- DECK PLATE, STA 1708, BL 0, CORROSIONSDR FDEA202203280718None · noneAFT CABIN SHEAR WEB CORRODED AT FASTENER HOLES BS 1684 - BS 1720 BL 0 ACCOMPLISHED FEDEX EA # F-5310-T036757P1: FUSELAGE- MAINFRAME - DECK PLATE STA 1708 BL 0 CORROSIONSDR FDEA202203260698Skin Panel · unknownDURING AGING A/C INSPECTION, PERFORMED TAP TEST AND FOUND EXISTING REPAIR TO BE DISBANDED ON LEFT HORIZONTAL STAB LOWER SURFACE AT APPROX. STAB STA 214 AND 4' FROM FRONT SPAR. REMOVED PREVIOUS REPAIR AND PERFORMED PERMANENT REPAIR ON L/H HORIZONTAL STAB LOWSDR FDEA202203250694Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR RW O/B FLAP UPPER SURFACE APPROX 53" FROM I/B END AND 9.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERFOMED PERMANENT REPAIR IAW B757 SRM: SDR FDEA202203250693Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR R/W O/B FLAP UPPER SURFACE APPROX 95" FROM I/B END AND 7.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND PERFORMED PERMANENT REPAIR IAW B757 SRMSDR FDEA202203250690Rudder · unknownPREVIOUS COMPOSITE MAJOR REPAIR ON THE L/H SIDE OF RUDDER APPROX 20" FROM T/E AND 36" FROM BOTTOM. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND ACCOMPLISHED PERMANENT REPAIR TO L.H LOWERSDR FDEA202203250689Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 36" FROM I/B END AND 10" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-SDR FDEA202203250688Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 83" FROM I/B END AND 8" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-01SDR FDEA202203250687Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR. L/W O/B FLAP UPPER SURFACE APPROX 98" FROM I/B END AND 6.5" FROM T/E. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIRS IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53SDR FDEA202203250686Flap · unknownPREVIOUS COMPOSITE MAJOR REPAIR, L/W O/B FLAP UPPER SURFACE APPROX 42" FROM I/B END AND 5.5" FROM T/E; REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. REMOVED PREVIOUS REPAIR AND APPLIED NEW REPAIR IAW B757 SRM 57-53-SDR FDEA202203250685Web · damagedMAIN CARGO DOOR LOWER INNER WEB HAS DAMAGE FROM STA 580-590 REMOVED, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-49309 REV DSDR FDEA202203250684Web · damagedMAIN CARGO DOOR INNER WEB HAS DAMAGE FRO STA 500-520 REMOVED FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-49309 REV DSDR FDEA202203240681Support · crackedEMPENNAGE INTERIOR CROWN AREA APU INLET DUCT SUPPORT BRACKET CRACKED AT BS 1862 LOCATED & DRILLED NEW -1 SUPPORT BRACKET IAW BAC DWG 353N1043 REV A, ALODINED NEW -1 SUPPORT BRACKET IAW B757 SRM 51-20-01, PRIMED NEW -1 SUPPORT BRACKET IAW B757 SRM 51-20-01,SDR FDEA202203240680Stiffener · misalignedMAIN CABIN STIFFENER P/N 146N5376-7 REQUIRES TO BE FABRICATED PER PROD DWGS. FABRICATED MAIN CABIN STIFFENER, P/N 146N5376-7 IAW BAC DWG 146N5376 REV-SDR FDEA202203240679None · noneMAIN CARGO DOOR INNER ACCESS PANEL HAS SCRATCHES AT APPROX STA 592 REMOVED, FABRICATED AND INSTALLED NEW ACCESS PANEL IAW BOEING DWG 65-49309 REV DSDR FDEA202203230662None · unknownEXISTING COMPOSITE REPAIR ON L HORIZONTAL STAB. LWR SURFACE AT APPROX. STAB STA 214 AND 4" FROM FRONT SPAR EXISTING COMPOSITE REPAIR ON L HORIZONTAL STAB. LWR SURFACE AT APPROX. STAB STA 214 AND 4" FROM FRONT SPAR IS LOCATED ON A PRIMARY STRUCTURE PER B757SDR FDEA202203230661Flap · unknownEXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, UPPER SURFACE, APPROX. 30" FROM INBD END AND 2.5" FROM T/E EXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, UPPER SURFACE, APPROX. 30" FROM INBD END AND 2.5" FROM T/E IS LOCATED ON A PRIMARY STRUCTURE PER B757-2SDR FDEA202203230659Flap · unknownEXISTING COMPOSITE REPAIR ON R/WING OTBD FLAP, LWR SURFACE T/E, APPROX 12" FROM INBD END AND 5" FROM T/E. EXISTING COMPOSITE REPAIR, R/WING OTBD FLAP, LWR SURFACE T/E, APPROX 12" FROM INBD END AND 5" FROM T/E., IS LOCATED ON A PRIMARY STRUCTURE PER B757-20SDR FDEA202203230656Doubler · chafedR/W O/B FLAP L/E HAS A WORN AREA ON REPAIR DOUBLER 11IN I/B FROM O/B EDGE REPAIRED PER FEDEX EA # F-5750-T0322968 ASDR FDEA202203220645Floorboard · delaminatedMAIN CABIN STA 640/680 RBL 35 FLOOR PANEL TOP SURFACE DAMAGED. FABRICATED NEW PANEL 11862181-92 MAIN CABIN FLOOR PANEL IAW FED B757 SRZ 25-005 AND SRM 53-00-50-1A FIG 101 TABLE 1.SDR FDEA202203220644Floorboard · delaminatedMAIN CABIN STA 680/720 RBL 35 FLOOR PANEL TOP SURFACE DAMAGED. FABRICATED NEW PANEL 11862182-5 FLOOR PANEL IAW FED EX B757 SRZ-25-005 AND B757 SRM 53-00-50-1A FIG 101 TABLE 1.SDR FDEA202203220638None · noneEXTERIOR FUSELAGE SKIN HAS AN OUTWARDLY PROTUDING DENT AT STA 1602 BETWEEN S16R AND S17R ACCOMPLISHED B757-2 SRM 53-00-51-2R REPAIR 29 - FIG 201 - SHEET 129 - CATEGORY B REPAIRSDR FDEA202203190596Spoiler · dentedLEFT WING #4 SPOILER I/B SIDE UPPER SURFACE IS DENTED REPAIRED LEFT WING #4 SPOILER UPPER SKIN DENT IAW B757 SRM: 57-70-01-2R REP 1 AND SRM 51-70-05.SDR FDEA202203170563Seal · cracked#2 ENGINE O/B CORE COWL PYLON SKIRT SPRING SEAL IS CRACKED. REMOVE AND REPLACED CRACKED SPRING SEAL PER BAC DWG 311N3570 REV GSDR FDEA202202090266Hose · rupturedUPON LOWERING THE LANDING GEAR WE RECEIVED "L HYD PRESS" FOLLOWED BY "L HYD QTY" EICAS MESSAGES. HYD QTY WAS "0.00" ALONG WITH HYD PRESS "0". WE HAD ASSOCIATED "L YAW DAMPER" AND "RUDDER RATIO" MESSAGES. PERFORMED A GO AROUND, LEFT GEAR DOWN AND FLAPS 20.SDR FDEA202003170581Beam · crackedFWD CARGO STA 580 STUB BEAM IS CRACKED. LBL45.5 CUT OUT DAMAGED FLANGE ON FLOOR STUB BEAM STA 580 IAW FEDEX DWG SR57-53-004 REV -. FABRICATED, LOCATED, DRILLED AND INSTALLED ANGLE AND FILLER IAW FEDEX DWG SR57-53- 004 REV -. REF FEDEX EA F-5310-T0352978 P1SDR FDEA202002140337Filter · defectiveAFTER LANDING TOWARD END OF ROLLOUT, GOT FIRE EICAS MESSAGE AND FIRE MASTER WARNING INDICACTIONS. NO OTHER FIRE INDICATIONS. AS WE PULLED OFF RWY COCKPIT FILLED UP WITH SMOKE. FIRE INDICATION CLEARED. SHUT DOWN JET, RAN QRH FOR EMERG EVAC, AND EXITED LT SIDE VSDR FDEA2018081762048Warning Message · false activationREJECTED TAKEOFF, DUE TO A LT ENG BLEED OFF MESSAGE. DURING TAXI BACK, CREW PERFORMED SYSTEM TESTED IAW MM 36-11-00-5. COULD NOT DUPLICATE. OPS CHECKED OKAY. NO HISTORY IN PAST 30 DAYS.SDR FDEA201804020829Frame · puncturedBS 231 FRAME IS PUNCTURED. CUT OUT DAMAGED SECTION OF THE FRAME IAW SRM 53-00-07-2R, REP 7. REPAIRED IAW SRM 53-00-07-2R, REP 7, FIG 202.SDR FDEA201704261271Slide · low pressureL1 DOOR ESCAPE SLIDE PRESSURE BELOW GREEN BAND. REMOVED AND REPLACED THE L1 DOOR SLIDE IAW AMM 25-66-01-6, SLIDE AND ARMING SYSTEM OPS CHECKED NORMAL IAW AMM 25-66-01-4SDR FDEA201704251257Reservoir · low pressureL1 DOOR ESCAPE SLIDE PRESSURE BELOW GREEN BAND. REMOVED AND REPLACED THE SLIDE, SLIDE AND ARMING SYSTEM OPS CHECKED NORMAL IAW AMM 25-66-01-4.SDR FDEA201603130912Repair · debondedEXISTING REPAIR WING, THERE IS A REPAIR AT LT SIDE OUTER WING, UPPER INTER SPAR SKIN AT WS 790. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1 ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A5 PT 1 SDR FDEA201603090874Skin · delaminatedRIGHT INBD TE MAIN FLAP, UPPER OTBD ACCESS PANEL, UPPER SURFACE FOUND WITH MULTIPLE DENT MARKS & MULTIPLE DELAMINATED AREA. DAMAGED AREAS REMOVED, CLEANED & DRIED USING 150 DEG F PROCESS IAW SRM 57-53-01-2R DETAIL 1 REV 116 & SRM 57-70-10-2R REV 116. REPAIR
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