Boeing 777-FS2
Service difficulty reports · 695
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '777FS2' 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 aircraft_model_key = '777FS2' 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 FDEA2020070671373Relay · failedAT 6000' ON DESCENT WITH AUTOPILOT ENGAGED GOT SEVERAL EICAS INDICATIONS ON NOTICEABLE "THUMP" EICAS AND STATUS MSG INCLUDED : ALT CALLOUTS, TERR POSS, SATCOM, NO LAND 3 STATUS PAGE SATCOM SYSTEM, AFDC-L, NO LAND 3 PACK L AND CAPT FSS LIGHT CAME ON FOR 2 SECOSDR FDEA2020063071373Unknown · malfunctionedAT 6000' ON DESCENT WITH AUTOPILOT ENGAGED GOT SEVERAL EICAS INDICATIONS ON NOTICEABLE "THUMP" EICAS AND STATUS MSG INCLUDED: ALT CALLOUTS, TERR POSS, SATCOM, NO LAND 3 STATUS PAGE SATCOM SYSTEM, AFDC-L, NO LAND 3 PACK L AND CAPT FSS LIGHT CAME ON FOR 2 SECONDSDR FDEA202006261367Spar · crackedDURING ULTRASONIC INSPECTION ON THE VERTICAL FLANGE OF THE SPAR CHORD AND HIGH FREQENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES AT RIGHT HAND SIDE UNDERWING LONGERON LOWER WING, BUTT STATION 1035, VERTICAL FLANGE OF THE SPAR CHSDR FDEA202006261366Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 01 EACH CRACKS ON THE SKIN APPROXIMATE 0.7" AT STATION 1030 BETWEENSDR FDEA202006261365Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 01 EACH CRACKS ON THE SKIN APPROXIMATE 0.6" AT STATION 1030 BETWEESDR FDEA202006191279Longeron · crackedCRACK INDICATION FOUND DURING ULTRASONIC INSPECTION ON LEFT HAND SIDE UNDERWING LONGERON FITTING AT BODY STATION 1035. COMPLIANCE WITH EO G-5310-E0332629 G (P5). TITLE: FUSELAGE - MAINFRAME - INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATSDR FDEA202006191278Longeron · crackedCRACK INDICATION FOUND DURING ULTRASONIC INSPECTION ON RIGHT HAND SIDE UNDERWING LONGERON FITTING AT BODY STATION 1035. COMPLIANCE WITH EO G-5310-E0332629 G (P6). TITLE: FUSELAGE - MAINFRAME - INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STASDR FDEA2020061091156Skin · puncturedLT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS722. LEFT HAND WING NR 5 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 717 TO WING STATION 722. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354457 PART1. TITLE : WINGS- FLIGHSDR FDEA2020062571140Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 1.5Ï¿½ AT STATION 10SDR FDEA2020062571139Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 0.5Ï¿½ AT STATION 1SDR FDEA2020060871140Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 1.5 AT STATION 1027 STRISDR FDEA2020060871139Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN. FOUND 03 EACH CRACKS ON THE SKIN APPROXIMATELY 0.5 AT STATION 1027 STRINSDR FDEA202006051132Skin · puncturedLT WING NR 5 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS 717. LEFT HAND WING NR 5 SPOILER UPPER SURFACE AT WING STATION 717 TO WING STATION 722. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354457 PART1. TITLE : WING - FLIGHT SURFACES LT WSDR FDEA202006051131Skin · puncturedLT WING NR 3 SPOILER UPPER SURFACE FOUND PUNCTURE DAMAGE AT WS907. LEFT HAND WING NR 3 SPOILER UPPER SURFACE PUNCTURE DAMAGE AT WING STATION 907. REPAIRED AND SMOOTHENED AS PER SRM 51-70-04 AND EA G-5750-T0354459 PART 1 TITLE : WINGS - FLIGHT SURFACES - LT WINSDR FDEA2020062641124Spar · crackedDURING ULTRASONIC INSPECTION ON THE VERTICAL FLANGE OF THE SPAR CHORD AND HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES AT RIGHT HAND SIDE UNDERWING LONGERON LOWER WING BODY STATION 1035. VERTICAL FLANGE OF THE SPAR CHSDR FDEA2020060541124Longeron · crackedHIGH FREQUENCY EDDY CURRENT, OPEN HOLE INSPECTION CARRIED OUT ON. REMOVED FASTENER HOLES AT RIGHT HAND SIDE UNDERWING LONGERON LOWER WING BASE STATION 1035. VERTICAL FLANGE OF THE SPAR CHORD AND FOUND 01 EA LOWEST OUTBOARD HOLE WITH CRACK INDICATION.SDR FDEA202005291077Longeron · crackedULTRASONIC INSPECTION OF THE RIGHT HAND UNDERWING LONGERON FOUND CRACK AT BASE STATION 1035. COMPLIANCE WITH E.O. # G-5310-E0332629 E P6. TITEL: FUSELAGE Ï¿½ MAINFRAME INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035. SERVICE BSDR FDEA202005291076Longeron · crackedULTRASONIC INSPECTION OF THE LEFT HAND UNDERWING LONGERON FOUND CRACKED AT BS 1035. COMPLIANCE WITH E.O. # G-5310-E0332629 E P5. TITEL: FUSELAGE Ï¿½ MAINFRAME Ï¿½ INSPECTION AND MODIFICATION OF THE UNDERWING LONGERON AT BODY STATION 1035, SERVICE BULLETISDR FDEA202005221030Skin · crackedDURING ACCOMPLISHMENT OF MEDIUM FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND WING SLAT NR 5 OUTER SKIN FOUND 01 EACH CRACK. INDICATION AT FASTENER HOLE AT STATION OSCS 713 APPROXIMATELY 0.2" IN LENGTH. LEFT HAND WING SLAT NR 5 OUTER SKIN REPAIRED AS PER SRM SDR FDEA2020052211028Pseu · looseNUMEROUS STATUS MESSAGES RELATED TO EICAS CAUTION AUTOSPEED BRAKES. PSEU 2, PSEU 1, GEAR CONTROL...AND MANY MORE. ALL CAME ON WHEN CAUTION CAME UP. FOUND PSEU #1 LOOSE IN THE RACK, RESET PSEU #1 IN IT'S RACK REF B777 M.M. 32-08-01-4, VERIFIED #2 PSEU ISSDR FDEA2020052230881Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAN HAND UNDERWING LONGERON AND FUSELAGE SKIN, FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.1" AND 0.9' AT STASDR FDEA2020050430881Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHR HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.1" AND 0.9' AT STATION 1033 STRINGSDR FDEA2020050430880Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING LONGERON AND FUSELAGE SKIN FOUND 03 EACH CRACKS WHICH APPROXIMATELY 1.0" AT STATION 1028 SRINGSDR FDEA202004300852Structure · crackedDURING ACCOMPLISHMENT OF HIGH FFEQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON LEFT FRONT LOWER CHORD 04 EACH FASTENER HOLES AT STATION 1035 LEFT BUTT LINE 82 AND FOUND WITH CRACK INDICATION AT LOWER ROW OUTBOARD HOLE AS MARKED.SDR FDEA202004300851Spar · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON RIGHT HAND FRONT LOWER SPAR CHORD 04 EACH FASTENER HOLES AT STATION 1035 RIGHT BUTT LINE 82 FOUND WITH CRACK INDICATION AT LOWER ROW OUTBORAD HOLE AS MARKED.SDR FDEA202004270801Longeron · crackedULTRASONIC INSPECTION CARRIED OUT AND FOUND THE LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 WITH CRACK INDICATION.SDR FDEA202004270800Longeron · crackedULTRASONIC INSPECTION CARRIED OUT AND FOUND THE RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 WITH CRACK INDICATION.SDR FDEA202004130738Floor Support · wornLOWER BULK CARGO COMPARTMENT STATION 1926 RIGHT BUTT LINE 41 STRINGER FOUND SEVERAL HOLES AS MARKED. LOWER BULK CARGO COMPARTMENT STATION 1926 RIGHT BUTT LINE 41 FLOOR STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2. REPAIR CLASSIFIED AS SDR FDEA2020031750566Tire · failedPDIS 878 32-42 1892 15MAR20 LGG FACT U LOGPAGES:3025092 TIRE #10 PRESSURE LOW. INDICATION IN AMBER STATUS PAGE HAS TIRE PRESS MESSAGE. PRESSURE 162 AND DROPPING. TIRE #9 PRESSURE IS ALSO IN AMBER WITH PRESSURE AT 208. R/I 15MAR20 13:18 SDR FDEA202002210365Switch · malfunctionedDURING PREFLIGHT EMER LIGHTS EICAS REMAINED ILLUMINATED AFTER SWITCH TO GUARDED POSITION. CYCLED EMERGENCY LIGHTS SWITCH PER B777 FIM ATA 33-51-00-2. OK FOR SERVICE.SDR FDEA2020012180176Contactor · burnedHYD ELEC PUMP ELCU HAS DAMAGE. INSATLLED ELCU (M29303) FOR ACMP C-1 IAW MM 24-51-05-4. OPS TESTED NORMAL IAW MM 24-51-05-4.SDR FDEA202001020002Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON FUSELAGE SKIN OF LEFT HAND UNDERWING LONGERON FOUND 02 EACH CRACKS INDICATION AT STATION 1024 AND STATION 1035 STRINGER 37 LEFT. APPROXIMATELY 2.0" IN LENGTH EACH, AS MARKED. FUSELAGE SKIN LEFT HAND UNDERWING LONGESDR FDEA201912233282Skin · crackedHFEC SURFACE INSPECTION CARRIED OUT ON THE RIGHT HAND SIDE OF THE FUSELAGE SKIN COMMON TO THE UNDERWING LONGERON WITHIN A 2 INCHES RADIUS OF THE FASTENER HOLES FOUND CRACK APPROXIMATE 1/2" AT STATION 1027 STRINGER 37 RIGHT. FUSELAGE SKIN UNDERWING LONGERON WISDR FDEA2019122313285Tire · wornRECEIVED EICAS MESSAGE OF TIRE PRESS. PRESSURE ON NR 7 INDICATED 180 PSI AND DURING FLIGHT CONTINUED DOWN TO 113 PSI. EMERGENCY WAS DECLARED AND TIRE REMAINED IN TACT DURING LANDING & SUBSEQUENT TAXI IN INITIAL INDICATION AT APPROXIMATELY 2 HOURS 30 MINUTES ISDR FDEA2019122093263Floor Support · crackedBULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1980.5 RBL 40 FOUND CRACKED. REFER SNRM N00384 FOR WORK DETAIL CARRIED OUT AT BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER SECTION REPAIR (STATION 1980.5 RBL 40 ) FROM STATION 1925 TO STATION SDR FDEA2019122093262Floor Support · crackedBULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER STATION 1937 RBL 16 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER STATION 1937 RBL 16 SECTION STRINGER REPAIR CARRIED OUT AT BULK CARGO COMPARTMENT AT STATION 1928 AND STATION 1967 RBL 16 AS PER SRMSDR FDEA2019122093261Floor Support · crackedBULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1931 RBL 40 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER AT STATION 1931 RBL 40 SECTION STRINGER REPAIR CARRIED OUT AT BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT AREA AT STATIONSDR FDEA201912193260Floor Support · crackedBULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1958 RBL 49.8 FOUND CRACKED. BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRINGER STATION 1958 RBL 49.8 SECTION STRINGER REPAIR CARRIED OUT AT BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT AREA AT STATISDR FDEA201912173255Structure · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON RIGHT HAND UNDERWING LONGERON AT BODY STATION 1035, FOUND CRACK INDICATION ON FRONT SPAR LOWER CHORD, LOWER ROW OUTBOARD FASTENER HOLE AND MIDDLE FASTENER HOLE. RIGHT HAND UNDERWING SDR FDEA201912173254Longeron · crackedULTRASONIC INSPECTION CARRIED OUT ON LEFT HAND UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOUND AT 01EACH FORWARD INBOARD FASTENER HOLE AND 02EACH AFT FASTENER HOLES. LEFT HAND UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOUSDR FDEA201912173253Longeron · crackedULTRASONIC INSPECTION CARRIED OUT ON THE RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND CRACK INDICATION FOUND AT 02EACH FORWARD FASTENER HOLES AND 01EACH AFT OUTBOARD FASTENER HOLE. RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 AND CRASDR FDEA2019121753248Line · leakingPDIS 856 29-02 9464 15DEC19 LGG FACT U LOGPAGES:3029639 HYD QTY LOW C EICAS MESSAGE FOLLOWED BY RESERVE BRAKES / STRG MESSAGE. ISLN VALVES CLOSED AT .40 LEAK STOPPED AT .36. PART 15DEC19 16:38 MC1 U IDENTIFIED PARTS MPN: AE717930-1 SDR FDEA2019121313221Switch · out of positionPDIS 861 25-60 8026 11DEC19 CGN FACT U EMERG LIGHTS SWITCH COVER TURNS OFF SWITCH WHEN CLOSED. CGN U FOUND PULLING MECHANISM OF SWITCH GUARD MOVED OF THE SWITCH. RE-ALLIGNED THE SWITCH POSITION AND MECHANISM (MOVING NUTS TO LET THE SWITCH SHSDR FDEA2019120433163Tire · leakingPDIS 887 32-42 6858 03DEC19 MEM OPEN U LOGPAGES:3182122 TIRE PRESS EICAS ON DEPARTURE FROM ZSPD, TIRE #12 PRESSURE IS LOW AND DECREASING. REMOVED AND REPLACED #12 MLG TIRE C/W 777AMM32-45-01-4. FIRE TRUCKS PRESENT ON TAXI INSDR FDEA201911223047Pcu · leakingON CLIMBOUT RECEIVED "HYD QTY LOW R" EICAS, FOLLOWED BY "HYD PRESS PRI R" EICAS AND THEN "HYD PRESS SYS R" EICAS, COMPLIED WITH ALL NON-NORMAL CHECKLISTS. CHECKED FOUND RT ENGINE EDP HYD LEAK, ALSO FOUND HYD LEAK FROM NR 6 SPOILER PCA. CHECK THE RT EDP AND ACMSDR FDEA2019111532949Valve · failedPDIS 866 32-44 0191 13NOV19 MEM LOGPAGES:2941013 ANTISKID ALERT CAME ON AGAIN AFTER LANDIING AFTER PARKING BRAKE WAS SET THTE RELEASE. ANTISKID MALFUNCTION FROM THIS FLIGHT AND PERVIOUS FLIGHT MAY BE DUE TO PARKING BRAKE USE. POSSIBLE SWITCHSDR FDEA2019111532940None · nonePDIS 857 05-50 9138 13NOV19 SEA OPEN U LOGPAGES:3182688 FLEW INTO A VERY THIN, RAGGED VOLCANIC ASH CLOUD @ FL340 AT APPROX 2350Z NOTICED A SMALL, BUT STEADY EGT CLIMB AT A FIXED N1. EGT MAXED OUT AT 710 DEGREES BEFORE MAEUVERING OUT OF CLOUD.SDR FDEA2019111522925Warning Message · false activationPDIS 866 32-44 0188 12NOV19 MEM AFTER BLOCK OUT ANTI-SKID ALERT. DID EICAS SNAPSHOT ERASING PROCEDURE WITH THE ERASE SELECTION MENU PER M/M 31_61_00_2_0. DID ANTI-SKID/AUTOBRAKE SYSTEM CHECK PER M/M 32-42-00-5. ALL PASSED. OK FOR SERVICE.SDR FDEA201910312793Slide Raft · jammedPDIS 856 52-10 9353 31OCT19 LAX OPEN U LOGPAGES:2986641 F/O STATES L1 DOOR IS VERY DIFFICULT TO ARM. HAD TO SELECT IT TO ARM MORE THAN ONCE FOR THE DEPARTURE. R/I 31OCT19 02:10 LAX U REASON CODE : REMOVAL FROM A/C ONLY **NO INSTALLATIONSDR FDEA2019102422725Floor Support · crackedBULK CARGO COMPARTMENT FLOOR STRINGER AT STATION 1936 RBL 49.8 FOUND CRACKED.
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