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 FDEA202305090832Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242PF(PN:152W8652-6) AT STA1473.75/RBL83-84 FOUND CRACK. (OFF WING). MAIN DECK CARGO FLOOR PANEL 242PF (PN:152W8652-6) AT STA 1473.75/RBL 83-84 CRACK (OFF WING), DAMAGE SIZE:L=1" IN LOWER SKIN WITHIN LIMIT. EVALUATED THE DAMAGE SDR FDEA202305090831Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241UF(PN:152W8652-3) AT STA1446-1447/LBL73.75-75.75 FOUND CRACK.(OFF WING). MAIN DECK CARGO FLOOR PANEL 241UF(PN:152W8652-3) AT STA1446-1447/LBL73.75-75.75 CRACK (OFF WING),DAMAGE SIZE:L=2" IN LOWER SKIN WITHIN LIMIT. EVALUATEDSDR FDEA202305090830Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241QF(PN:152W8452-21) AT STA1358/LBL52-54.75 FOUND CRACK. (OFF WING). MAIN DECK CARGO FLOOR PANEL 241QF(PN:152W8452-21) AT STA1358/LBL52-54.75 CRACK (OFF WING). DAMAGE SIZE:L=2.75" IN LOWER SKIN WITHIN LIMIT. EVALUATED THE DAMAGSDR FDEA202305090829Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241PF(PN:152W8452-19) AT STA1309.5-1310/LBL20-22 FOUND CRACK(OFF WING). MAIN DECK CARGO FLOOR PANEL 241PF(PN:152W8452-19) AT STA1309.5-1310/LBL20-22 CRACK(OFF WING).DAMAGE SIZE:L=2.1" IN LOWER SKIN WITHIN LIMIT. EVALUATED AND SDR FDEA202304200719Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #242HF FOUND TORN AT STATION 1285 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 242 HF. AS PER B777 SRM 53-00-50-2R REPAIR 1.REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304200718Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #242JF FOUND TORN AT STATION 1285 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 242 JF.AS PER B777 SRM 53-00-50-2R REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304200717Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #214LF FOUND TORN AT STATION 1285 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 241 LF.AS PER B777 SRM 53-00-50-2R REPAIR 1.REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304200716Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #242EF FOUND TORN AT STATION 1235 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1235 FLOOR PANEL # 242 EF. AS PER B777 SRM 53-00-50-2R REPAIR 1.REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304200715Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL#242FF FOUND TORN AT STATION 1140 REPAIRED MAIN DECK CARGO COMPART MENT STATION 1140 FLOOR PANEL # 242FF. AS PER B777 SRM 53-00-50-2R REPAIR 1.REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304200713Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #241GF FOUND TORN AT STATION 1140 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1140 FLOOR PANEL # 241 GF.AS PER B777 SRM 53-00-50-2R REPAIR 1.REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304200711Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #241JF FOUND TORN AT STATION 1300. REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1300. FLOOR PANEL # 241 JF. AS PER B777 SRM 53-00-50-2R REPAIR 1.REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304190701Panel · tornCABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL#241KF FOUND TORN AT STATION 1285. REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 241 KF. AS PER B777 SRM 53-00-50-2R REPAIR 1.REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA202304190676Floor Panel · crackedMAIN DECK CARGO FLLOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL73.5-76 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL73.5-76 CRACK(OFF WING), CRACK SIZE L =2.5" IN LOWER SURFACE WITHIN LIMIT. EVALUATED AS PER B777 SRM 53-00- SDR FDEA202304180666Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8652-19) AT STA1393/LBL20-21.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1393/LBL20-21.5 CRACK(OFF WING), CRACK SIZE L =1.4" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER B777 SRM 53-00SDR FDEA202304180665Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8652-21) AT STA1363/LBL43.75-44.75 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1363/LBL43.75-44.75 CRACK(OFF WING), CRACK SIZE L =0.9" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER B777SDR FDEA202304180664Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1435.75/RBL76.25-77.25 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1435.75/RBL76.25-77.25 CRACK(OFF WING), CRACK SIZE L =0.9" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER SDR FDEA202304180663Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1292/LBL110-111 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1292/LBL110-111 CRACK(OFF WING), CRACK SIZE L =1.0" IN LOWER SURFACE WITHIN LIMIT, EVALUATED AS PER SRM 53-00- 50SDR FDEA202304180662Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT SVTA1272/RBL110-113 FOUND CRACK. CRACK SIZE L =3.0" IN LOWER SKIN WITHIN LIMIT. EVALUATED AS PER B777 SRM 53-00-50- 1A,REV 43.1. REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 43.1. REPAIR CLASSIFIESDR FDEA202303310534Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1475/RBL38.5-40 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1475/RBL38.5-40 CRACK.SIZE:L=1.6" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00SDR FDEA202303310533Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242PF(P/N:152W8652-6) AT STA1475/RBL27-29 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242PF (P/N:152W8652-6) AT STA1475/RBL27-29 CRACK.SIZE:L=1.8" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00-50-1SDR FDEA202303310532Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1430.5-1431/RBL45.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1430.5-1431/RBL45.5 CRACK.SIZE:L=1.4" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM SDR FDEA202303310531Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1391.25/LBL42.75-44.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241QF (P/N:152W8652-21) AT STA1391.25/LBL42.75-44.5 CRACK.SIZE:L=1.7" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PERSDR FDEA202303310530Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1415.5/LBL39-40 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1415.5/LBL39-40 CRACK.SIZE:L=1.5" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00-SDR FDEA202303310529Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1447.5/LBL43.5-44.25 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1447.5/LBL43.5-44.25 CRACK.SIZE:L=1.2" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777SDR FDEA202303300527Pdu · unknownEICAS FLAP DRIVE ALERT ON DEPARTURE AFTER SELECTING FLAPS UP. ECL PROCEDURES ACCOMPLISHED. RTB MEM. EMERGENCY DECLARED & CANCELED AFTER LANDING. EMERGENCY DECLARED. ALL WORK ACCOMPLISHED UNDER THE FOLLOWING WRI'S; 27-50/4918, 4919, 4920, 4921, 4925 & SDR FDEA202303300524Floor Panel · crackedREWORK:MAIN DECK CARGO FLOOR PANEL P/N:152W8750-2 FOUND CRACKED AT STA2020 BL0. EVALUATED MAIN DECK CARGO FLOOR.P/N:152W8750-2 AT STA 2020 BL0 AS.PER B777 SRM 53-00- 50-1A. ALLOWABLE DAMAGE 1, REV.43.1 FOUND UPPER TEAR L X W=2.1" X 0.5", OUT OF ALLOWABLE LISDR FDEA202303230496Flap · dentedLH OB FLAP LWR SURFACE FROM OB TO IB 162INCH CROSS TE TO LE 6INCH FOUND ONE DENT LH OB FLAP LWR SURFACE FROM OB TO IB 162INCH CROSS TE TO LE 6INCH DENT WITH DELAMINATION L X W=3.4" X 2.3", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2,SDR FDEA202303230495Flap · dentedLH OB FLAP LWR SURFACE FROM IB TO OB 177INCH CROSS TE TO LE 15.8INCH FOUND ONE DENT LH OB FLAP LWR SURFACE FROM IB TO OB 177INCH CROSS TE TO LE 15.8INCH DENT WITH DELAMINATION L X W=3.1" X 2.5", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMSDR FDEA202303190469Pdu · faultedFLAPS DRIVE EICAS AFTER TAKEOFF. REF TSI 27-80/4883, PUT THE AIR/GROUND SYSTEM IN THE AIR MODE. PERFORMED STEP 7, OPS FLAPS WHEN FSEU #2 IN CONTROL, ALL OPS SATISFIED. OPS FLAPS WHEN FSEU #1 IN CONTROL, MX MSG 27-20391 LATCHED WITH STATUS MSG FLAP/SLAT CONSDR FDEA202303150428Light · failedFLT CREW PRE-FLT CK REPORTED, L1 DOOR FWD EMER EXIT SIGN INDICATOR ALL OF LIGHTS INOP. ENT BY:3711964 RPT BY:3711964 R&R'D LIGHT ASSY PER MM 33-51-01-2. LIGHT F/C AND EMER LT TEST PASS. A/C OK FOR SVC. (P/N; 702409-1001) ENT BY:3711964 RPT BY:3711964SDR FDEA202303140421Wheel · failedFOUND #3 WHEEL WITH SKIDDING DAMAGE THAT CAUSED TIRE TO BURST. ACCOMPLISHED AMM 05-51-16-2 TIRE BURST INPECTION. NO FINDINGS. REMOVED AND REPLACED #3 MAIN WHEEL AND TIRE ASSEMBLY IAW AMM 32-45-01-4SDR FDEA202303070390Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241PF AT STA1309/LBL20-21 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241PF AT STA 1309/LBL20-21 CRACK L X W= 1.2" X 0.1" ,WITHIN LIMIT PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1, REV43.1, REPAIRED AS PER B777 SRM 53-00-50-2R REPASDR FDEA202303070389Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241UF AT STA1446/LBL75-76.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241UF AT STA 1446/LBL75-76.5 CRACK L X W= 1.5" X 0.1" ,WITHIN LIMIT PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1, REV43.1, REPAIRED AS PER B777 SRM 53-00-50-2RSDR FDEA202303070388Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QF AT STA1445.5/RBL73.5-76.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242QF AT STA 1445.5/RBL73.5-76.5 CRACK L X W= 3.0" X 0.1", WITHIN LIMIT PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1, REV43.1, REPAIRED AS PER B777 SRM 53-0SDR FDEA202303070387Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241QF AT STA1346.25-1347/LBL81-85 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241QF AT STA 1346.25-1347/LBL81-85 CRACK L X W= 4" X 0.1", WITHIN LIMIT PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1, REV43.1, REPAIRED AS PER B777 SRM 53SDR FDEA202303070386Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242PF AT STA1440/RBL22-24.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242PF AT STA 1440/RBL22-24.5 CRACK L X W= 2.5" X 0.1" ,WITHIN LIMIT PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1, REV43.1, REPAIRED AS PER B777 SRM 53-00-50-2RSDR FDEA202303070385Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242LF AT STA1309/RBL20-21 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242LF AT STA 1309/RBL20-21 CRACK L X W= 1.0" X 0.1" ,WITHIN LIMIT PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1, REV43.1, REPAIRED AS PER B777 SRM 53-00-50-2R REPSDR FDEA202303030374Unknown · unknownUPON ARRIVAL FOUND DENT ON RT BS 132.21 BETWEEN F/O WINDOW & RADOME. SRM 53-00-01-1A. DENT IS 5 IN FROM RADOME CUTOUT, MEASUREMENT FOUND WIDTH 3.5 INCH, LENGTH 6 INCH AND DEPTH 0.11 INCH. REF. FIG 102 DETAIL E. NDTM PT6 PERFORMED HFEC OF SKIN CUTOUT AND INTERSDR FDEA202302090239Unknown · unknownDURING INSPECTION OF APU OIL LEVEL FOR SERVICE CHECK, LIFT TRUCK FORWARD BARRIER HIT PANEL LOCATED IN FRONT OF 313AL DOOR DUE TO MALFUNCTION OF THIS LIFTRUCK. EA: G-5310-T0372876 P2 C/W WITH STEPSDR FDEA202302080230Flap · dentedLH OB FLAP LWR SURFACE FROM OB TO IB 98 INCH CROSS TE TO LE 8 INCH FOUND ONE DENT LH O/B FLAP LWR SURACE FROM O/B TO I/B 98 INCH CROSS T/E TO L/E 8 INCH DENT DAMAGE SIZE: L XW=1.7" X 1.5", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2,SDR FDEA202302080229Flap · damagedRH WING OB FLAP LEADING EDGE FOUND BROKEN AT OTEF STA 437. RH WING OB FLAP LEADING EDGE PUNCTURE DAMAGE SIZE L X W: 1.0" X 0.5", OUT OF ALLOWABLE LIMIT PER B777 SRM 57-53-01-1A ALLOWABLE DAMAGE 2, REV 43.1, REPAIRED AS PER WORK CARD TG-5750-T0372808 P1, TISDR FDEA202302071766Flap · damagedDUE BIRD STRIKE INSPECTION FOUND DAMAGE ON LH OUTBOARD FLAP BETWEEN INBOARD FAIRING AND FLAPERON. IT MEASURES 1"X 0,8" AND IT S LOCATED 2" FROM TRAILING EDGE. TERMINATING ACTION ACCOMPLISHED FOR SRM 57-53-01SDR FDEA202301200148Actuator · failedL/H ENGINE I/B FAN COWL OPEN ACTUATOR UPPER ROD END BROKEN. REMOVED L/H ENGINE INBOARD FAN COWL ACTUATOR REF AMM 71-12-01-4 R/I. INSTALLED NEW FAN COWL OPENING ACTUATOR ON #1 ENGINE, RH (INBOARD) SIDE REFERENCE BOEING 777 AMM 71-12-01-4. OPERATIONAL CHSDR FDEA202211232829Lamp · inoperativePRE-FLT MX INSP, GALLEY CTR OVRHD (1) EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.SDR FDEA202211092740Unknown · unknownSHUTDOWN L ENGINE IAW ECL FOR ENGINE OIL FILTER L. ENGINE SHUTDOWN AT 1825Z AT 3000 MSL.ESTIMATE ENGINE WAS SHUTDOWN A MAX OF 5 MIN IN FLIGHT. ***EMERGENCY DECLARED*** SYSTEM FLUSHED AND SERVICED PER AMM 79-00-00-200 804-H01, AMM 71-00-0-5-907-001-H01/POSDR FDEA202210072506Doubler · misrepairedDURING PERFORMING EO G-5710-E0365655 B P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N : 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE SDR FDEA2022101172505Doubler · misrepairedDURING PERFORMING EO G-5710-E0365655 B P7 STEP8.C.(5), FOUND 01EA ZLJ-8 COUNTERSUNK FASTENER AT STA 998 S35L TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNK HOLE.SDR FDEA202210032455Skin · dentedRHW T/E O/B FLAP MIDDLE LOWER SURFACE FOUND 1EA DENT AT 310" TO O/B CROSS 10" TO T/E. RHW T/E O/B FLAP MIDDLE LOWER SURFACE AT 310" TO O/B CROSS 10" TO T/E REPAIRED AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1,REV 41.0. THE B777 SRM 5SDR FDEA202210032454Skin · dentedLH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6" AREA FOUND DENTED. LH WING O/B FLAP LOWER SURFACE FROM O/B TO I/B 39" CROSS AFT TO FWD 6"AREA REPAIRED AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR1,REV 41.0. THE B777SDR FDEA202210022450Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL38.5-40 FOUND CRACK. REPAIRED MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1413/RBL38.5-40 CRACK AS PER B777 SRM 53-00-50-2R REPAIR 1, REV41.0. REPAIR CLASSIFIED AS MAJOR PER GM
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