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 FDEA202402240211Lamp · failedPRE-FLT MX INSP, GALLEY OVRHD (1EA) EMERGENCY LT INOP. AMM: 33-50-00-2 RELAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.SDR FDEA202401260113Skin · dentedRH WING IB AFT FLAP UPR SURFACE FOUND DENT AT ITEF 340 AND 2.7 IN AWAY FROM AFT EDGE. EVALUATED RH WING IB AFT FLAP UPR SURFACE AT ITEF 340 AND 2.7 IN AWAY FROM AFT EDGE DENT WITH DISBOND DAMAGE SIZE LXW=5.1"X2.1" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57- SDR FDEA202401250110Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT OTEF 234 AND 5.4 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT OTEF 234 AND 5.4 IN AWAY FROM AFT EDGE WITH DISBOND DAMAGE SIZE LXW=4.25"X2.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-53-01SDR FDEA202401250109Skin · dentedLH WING OB FLAP LWR SURFACE FROM OB TO IB 233 INCHES CROSS TE TO LE 11 INCHES FOUND ONE DENT. EVALUATED LH WING OB FLAP LWR SURFACE FROM OB TO IB 233 INCHES CROSS TE TO LE 11 INCHES ONE DENT WITH DISBOND DAMAGE SIZE LXW=2.0"X1.0" OUT OF ALLOWABLE LIMIT ASSDR FDEA202401150077Unknown · unknownAIRBORNE RETURN DUE TO AIR CONTAMINATION OF AN UNKNOWN SUBSTANCE. NOTED SOOT ON BOTH SIDES OF FLIGHTR COMPARTMENT CAPTAIN AND FO SEATS ON FLAT AREAS NEAR TILLER AND WINDOW CONTROL. CLEANED UP SOOT AND R AND R'ED LOWER RECIRCUULATION AIR FILTERSREF AMM 2SDR FDEA202312261958Smoke Detector · failedMAIN DECK AND LWR AFT CARGO FIRE LIGHT ILLUMINATED DURING COCKPIT SETUP. MX WAS CALLED AND SYSTEM CHECKED OK. BOTH LIGHTS AGAIN ILLUMINATED AFTER CLOSING THE ENTRY DOORS PRIOR TO PUSH. REMOVED AND REPLACED CARGO SMOKE DETECTION CONTROLLER P/N 905701-SDR FDEA202312201949Blade · damagedAFTER AIRBORNE PASSING APPROXIMATELY 2500 FEET DURING THE CLIMB OUT, WE NOTICED VIBRATION BEGIN ON THE AIRCRAFT. IT CONTINUED TO WORSEN AND STABILIZED WITH THE RIGHT ENGINE EVM SHOWING 4.8 AT CLIMB THRUST WHICH WAS ABOUT 85%. REFERENCING THE APPROPRIATE SDR FDEA202312111932Light · failedEMERGENCY LIGHTING LITE IN SUPERNUMERARY IS INOPERATIVE. REMOVED & REPLACED LEFT CEILING INTERIOR EMER LT ASSY AND OPS CHECKED NORMAL.SDR FDEA202312051909Unknown · unknownEMERGENCY EXIT LIGHTS WILL NOT TEST WITH SUPERNUMERARY TEST BUTTON. HIGH RESITANCE ON PIN 8 CONNECTOR DM33093 CHECKING TO GROUND WITH BOTH POWER SUPPLY UNITS DISCONNECTED. DISCONNECTED CONNECTOR D2238P & WAS ABLE TO SUCCESFULLY TEST EMER LIGHTS FROM SUPERNSDR FDEA202311301900Battery · failedEMERGENCY LIGHTS IN SUPERNUMERARY ILLUMINATED ON SHORT FINAL TO LANDING. STAYED ON FOR ABOUT 10 SECONDS. COMPLIED WITH OPERATIONAL CHECKS AND FUNCTIONAL CHECKS PER AMM 33-51-00-5. ALL TESTS PASSED AND OBSERVED THE A/C FOR 20 MINUTES WITH NO DEFFECTS NOTEDSDR FDEA202311231886Lamp · failedRIGHT SLIDE/OVERWING LIGHT IS BURNED OUT AMM: 33_51_04_2 IPC: 33-51-11-01 ITEM 30 REMOVED AND REPLACED RIGHT SLIDE/OVERWING LIGHT REF AMM AMD IPC ABOVE WITH PN 767 FROM STOCK, OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202310311817Unknown · unknownUPON BLOCK IN, GROUND CREW OPENED FORWARD CARGO COMPARTMENT DOOR AND PLACED DISINSECTION CANISTER IN COMPARTMENT. WHEN THE DOOR WAS CLOSED, IT GENERATED A LOWER CARGO FIRE WARNING. FOLLOWED ECAS PROCEDURES. PRIOR TO DISCHARGE OF BOTTLE, WARNING DISAPPEARESDR FDEA202310181772Floor Panel · crackedREWORK:MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA 1660 RBL 1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 CRACKED AT STA 1660 RBL 1, SIZE:L=1.2" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1,REVSDR FDEA202310091733Flap · damagedLH IB AFT FLAP I/B LWR SURFACE FROM IB TO OB 65INCH CROSS LE TO TE 34INCH FOUND ONE BIRD STRIKE. EVALUATED LH IB AFT FLAP I/B LWR SURFACE FROM IB TO OB 65INCH CROSS LE TO TE 34INCH ONE BIRD STRIKE, DAMAGE SIZE L*W=1" *0.75" WITHIN REPAIR LIMIT AS PER B777SDR FDEA202310081728Flap · damagedLH OB FLAP LWR SURFACE FROM IB TO OB 52 INCH CROSS LE TO TE 67 INCH FOUND ONE BIRD STRIKE. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 52 INCH CROSS LE TO TE 67 INCH ONE BIRD STRIKE. DAMAGE SIZE L*W=1" *0.8" WITHIN REPAIR LIMIT AS PER B777 SRM 57-53-01-SDR FDEA202310061715Skin · dentedFUSELAGE SKIN INTERIM REPAIR FOR DENT, AT STA 132.21 BELOW F/O WINDOW. FUSELAGE SKIN AT STA 132.21 BELOW F/O WINDOW DENT AREA REPAIRED AS PER B777 SRM 51- 40-02,SRM 51-10-02,SRM 51-70-01,SRM 51-40-08,SRM 51-40-05,SRM 53-00-01 REPAIR 4 ,SRM 51-20-01 AND SRM SDR FDEA202309271662Power Supply · failedEMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN TESTED. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLIES ABOVE L1 DOOR AND R1 DOOR REF. AMM 33-51-06-2. ALL LIGHTS OPERATE NORMALLY PER ABOVE AMM REF. A/C OK FOR SERVICE.SDR FDEA202309211631Lamp · failedPOST-FLT INSP, SUPRNMRY EMERGENCY LT INOP IN GALLEY DIRECT OVERHEAD CEILING. AMM: 33-51-04-2 RE-LAMPED, REF B777 AMM: 33-51-04-2. LT'S TEST SATIS, ITEM OK FOR SVC.SDR FDEA202309091568Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8352-29 FOUND CRACKED AT STA1014 LBL86. EVALUATED AND MEASURED MAIN DECK CARGO FLOOR PANEL P/N:152W8352-29 CRACKED AT STA 1014 LBL86, DAMAGE SIZE: L=2.75", DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00- 50-1A ALLOSDR FDEA202309051545Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1706 RBL1 EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 AT STA 1706 RBL 1 CRACK SIZE L=3.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV 44.0.REPAIRED THE DASDR FDEA202309051544Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA1660 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 AT STA 1660 RBL 1 CRACK SIZE L=3.0" OUT OF ALLOWABLE LIMIT AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV 44.0.REPAIRED THE DSDR FDEA202308171453Skin · bentRH WING NO.10 SLAT OUTER SKIN FOUND BULGE AT WS 657-661 AND 19.5 IN AWAY FROM AFT EDEG. RH WING NO.10 SLAT OUTER SKIN BULGE AREA AT WS 657-661 AND 19.5 IN AWAY FROM AFT EDGE REPAIRED AS PER B777 SRM 57-43-01-2R-9, SRM 51-40-05, SRM51-20-01 REV 44.0 AND EA SDR FDEA202308161448Skin · dentedLH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE 4 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LOWER SURFACE FROM IB TO OB 15.5 INCH CROSS TE TO LE 4 INCH ONE DENT DAMAGE SIZE L X W=4"X2" WITH DISBOND WITHIN REPAIR LIMIT AS PER B777 SRM 57-53SDR FDEA202308151433Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH ONE DENT WITH DAMAGE SIZE L*W=3"*2.75" WITHIN REPAIR LIMIT AS PER B777 SRM 57-53-01-1A ALLOWSDR FDEA202308101393Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) AT STA1290/LBL105.5-107.5 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) CRACK, THE DAMAGE SIZE : L=2.2", OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DSDR FDEA202308101392Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) AT STA1269.5/RBL81-83.25 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) CRACK ,THE DAMAGE SIZE :L=2.3" , OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DSDR FDEA202308081373Skin · corrodedFOUND THE LOWER FUSELAGE SKIN CORROSION INSIDE BODY FAIRING 192JR AT BS 930 TO BS 940 AND S-49L TO S-49R. THE LOWER FUSELGE SKIN CORRODED AREA AT BS 930 TO BS 940 AND S-49L TO S-49R REMOVED & THE REWORKED AREA MEASURED THE ORIGINAL THICKNESS IS T=0.100", SDR FDEA202308011343Flap · delaminatedLH OB FLAP LWR SURFACE FROM IB TO OB 12 INCH CROSS TE TO LE 11.8 INCH FOUND ONE DENT EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 12 INCH CROSS TE TO LE 11.8 INCH ONE DENT WITH DELAMINATION DAMAGE SIZE LXW=1.8"X1.0" OUT OF ALLOWABLE LIMIT AS PER B777 SRSDR FDEA202307261296Door · damagedON PRE FLIGHT FOUND FUEL LEAKING FROM L/H WING PANEL 541CB CONTAINING MEASURING STICK #5 AMM: 28-44-01-4 TRANSFERRED FUEL MEASURING STICK AND BASE PLATE FROM REMOVED FUEL ACCESS DOOR (541CB) TO NEW ACCESS DOOR IAW AMM 28-44-01-4. INSPECTED FUEL MSDR FDEA202307051151Skin · wornFOUND FUSELAGE SKIN A ABRASION (DEPTH:0.016 IN) AT STA 1014, S36R-S37R, WHICH EXCEEDS 0.005 IN DEPTH. COMPLETED AS PER EA G-5710-T0375107 P2 STEP 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202306281117Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL P/N:152W8452-17 FOUND PUNCTURED AT STA 1288 LBL92. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8452-17 PUNCTURED AT STA 1288 LBL92, THE DAMAGE SIZE :DIA=1.1", DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABSDR FDEA202306281116Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8652-1 FOUND CRACKED AT STA 1434 LBL109. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8652-1 CRACKED AT STA 1434 LBL109, THE DAMAGE SIZE :LENGTH=1.9", DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLSDR FDEA202306281115Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N: 152W8452-21 FOUND CRACKED AT STA 1359 LBL45. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N: 152W8452-21 CRACKED AT STA 1359 LBL45. THE DAMAGE SIZE :LENGTH=1.8", DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50- 1A ALLOSDR FDEA202306151039Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1268.75/RBL112.75-115 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1268.75/RBL 112.75- 115 CRACK(OFF WING), THE CRACK SIZE:L=2.25", DAMAGE OUT OF ALLOWABLSDR FDEA202306151038Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1240-1241.5/LBL109 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1240-1241.5/LBL109 CRACK(OFF WING), THE CRACK SIZE:L=1.5", DAMAGE OUT OF ALLOWABLE LIMIT SDR FDEA202306101019Unknown · unknownAT TIME 2320Z CREW RECEIVED A SMOKE CREW REST F/D ADVISORY THAT LASTED 7-10 SECONDS. NO SMOKE SEEN OR SMELLED . ALL THREE SENSORS IN THE CREW REST INDICATE GREEN AS WELL AS THE LAV SENSOR. EICAS EVENT RCD PUSHED. AMM 26-14-10-5 PERFORMED OPS CHECK OF SDR FDEA202306091011Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL P/N:152W8402-7 FOUND PUNCTURED AT STA1224 LBL29. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8402-7 PUNCTURED AT STA1224 LBL29 DAMAGE SIZE LXW=1.8"X 1.5" WITHIN ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 RSDR FDEA202306070999Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 110INCH CROSS TE TO LE 6.2INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 110INCH CROSS TE TO LE 6.2INCH DENT DAMAGE SIZE LXW=3.1"X1.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-53-01-1A ALLOWABLE DASDR FDEA202306060997Unknown · unknownOVERHEAD EMERGENCY LIGHT BURNT OUT IN SUPERNUMERARY AREA REPLACED EMERGENCY BULB ON SUPERNUMERARY AREA PER AMM : 33-51-03-2SDR FDEA202305260943Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.5 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.5 A HOLE ,THE HOLE SIZE :LXW=2.0"X1.8" IN UPPER SURFACE ,WITHIN LIMIT AS PER B777 SRM 53-00- 5SDR FDEA202305260942Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 A HOLE ,THE HOLE SIZE :LXW=1.8"X1.6" IN UPPER SURFACE ,WITHIN LIMIT AS PER B777 SRM 53-00-50-1A SDR FDEA202305220916Unknown · unknownON CLIMB OUT OF ICN TIRE PRESS EICAS. RAN CHECKLIST AND GEAR SYNOPSIS SHOWED RIGHT NOSE GEAR TIRE PRESSURE AT 54 PSI. IT EVENTUALLY WENT TO 0. LANDED AT CAN AND MX TOWED AC TO THE GATE. EMERGENCY DECLARED. CHECK FOUND THE RIGHT NOSE PUNCTURED.REMOVED AND SDR FDEA202305220915Oven · failedPDIS 894 25-30 4173 22MAY23 ANC ACRID SMELL COMING FROM OVEN AREA. TURNED OVEN OFF AND NO MORE SMELL. NEEDS TROUBLESHOOTING. FACT 22MAY23 17:57 ANC REMOVED OVEN WITH THE STANK, REPLACED WITH NEW OVEN REF B777 AMM 25-32-52-4-2 OPS CHECK GSDR DALA2022120607829Unknown · unknownON CLIMB OUT OF ICN TIRE PRESS EICAS. RAN CHECKLIST AND GEAR SYNOPSIS SHOWED RIGHT NOSE GEAR TIRE PRESSURE AT 54 PSI. IT EVENTUALLY WENT TO 0. LANDED AT CAN AND MX TOWED AC TO THE GATE. EMERGENCY DECLARED. CHECK FOUND THE RIGHT NOSE PUNCTURED.REMOVED AND SDR FDEA202305160877Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA 1660 RBL1. EVALUATED THE MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 CRACKED AT STA 1660 RBL1.DAMAGE SIZE L=2.7", OUT OF ALLOWABLE LIMIT .AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV.43.SDR FDEA202305160876Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1780 RBL1. EVALUATED THE MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 CRACKED AT STA1780 RBL1 DAMAGE SIZE L=2.5", OUT OF ALLOWABLE LIMIT. AS PER B777 SRM53-00-50-1A ALLOWABLE DAMAGE 1 REV.4SDR FDEA202305160875Flap · dentedLH OB FLAP LWR SURFACE FROM OB TO IB 10INCH CROSS TE TO LE 2.25INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM OB TO IB 10INCH CROSS TE TO LE 2.25INCH DENT.DAMAGE SIZE LXW=1.8"X1. OUT OF ALLOWABLE LIMIT. AS PER B777 SRM 57-53-01-1A ALLOWABLE DASDR FDEA202305160874Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 3.8INCH CROSS TE TO LE 15.5INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 3.8INCH CROSS TE TO LE 15.5INCH ONE DENT DAMAGE SIZE LXW=2.6"X2.5" OUT OF ALLOWABLE LIMIT. AS PER B777 SRM 57-53-01-1A ALLOSDR FDEA202305160873Flap · delaminatedLH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7INCH FOUND DELAMINATION . EVALUATED LH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7INCH. DELAMINATION DAMAGE SIZE LXW=2"X1.5" OUT OF ALLOWABLE LIMIT. AS PER B777 SRM 57-53-01- 1ASDR FDEA202305090833Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QF(PN:152W8652-4) AT STA1451-1452.25/RBL44 FOUND CRACK.(OFF WING). MAIN DECK CARGO FLOOR PANEL 242QF (PN:152W8652-4) AT STA 1451-1452.25/RBL44 CRACK (OFF WING),DAMAGE SIZE:L=1.3" IN LOWER SKIN WITHIN LIMIT. EVALUATED THE DAM
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