Boeing 777-FS2
Service difficulty reports · 690
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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 FDEA202608221219Tire Tread · separatedCHECK FOUND NR 11 TIRE TREAD SEPARATION.SDR FDEA202608221218Power Supply · inoperativeDURING SERVICE CHECK, FOUND EXTERIOR RT EMERGENCY LIGHT NOT WORKING. RT EMERGENCY LIGHT POWER SUPPLY REPLACED IAW AMM 33-51-06-2. TESTED OK.SDR FDEA202607150925Skin · bulgedRIGHT WING NR 9 SLAT UPPER SURFACE 32IN FROM OTBD EDGE FOUND BULGE. NR 9 SLAT UPPER SURFACE 32 INCH FROM OB EDGE BULGE AREA REPAIRED IAW SRM 51-40-02-0G, SRM 57-43-01-2R REPAIR 16 FIG 202, SRM 51-40-05-0G, SRM 51-20-01-0G REV 53.0 AND EA G-5750-T0388015 P1.SDR FDEA202607120916Light Sys · malfunctionedCHECK FOUND WHEN THE OVERHEAD PANEL EMER LIGHTS SWITCH IN "ON" POSITION, THE EMERGENCY LIGHTS NOT ILLUMINATED. AMM: 33-51-00-5 RESET THE CB'S AND PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE CONTROL SWITCH ON THE OVERHEAD PANEL REF AMM33-51-00SDR FDEA202606090690Retainer · damagedFOUND RH WING SLAT NR 8 IB EDGE SEAL RETAINER UPPER SURFACE AFT SECOND FASTENER HOLE WORN. RH WING NO.8 SLAT IB EDGE OUTER SKIN FASTENER HOLE WORN AREA REPAIRED IAW SRM 57-43-01-2R REPAIR 6 FIGURE 203, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-20-01-0G, REV SDR FDEA202606090689Skin · damagedNO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE FOUND WORN. NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE WORN AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 6 FIGURE 203, SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 51-20-SDR FDEA202606060678Skin · crackedDURING PERFORM WORK CARD: E G-5710-E0376285 G P11 STEP 5.A.(2) THEN FOUND 01 EA CRACKED ON LT UPPER WING SKIN FASTENER NR 5. REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 53.0 AND SDR FDEA202606060677Skin · crackedDURING PERFORM WORK CARD:E G-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 01 EA CRACK ON RH UPPER WING SKIN FASTENER #5. REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 53.0 AND EA GSDR FDEA202606050674Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 02EA CRACKS ON RH UPPER WING SKIN COMMON TO FASTENER #5 AS MARKED.SDR FDEA202606050673Skin · damagedREQUEST A PERMANENT REPAIR ON AFT FUSELAGE SKIN STA 2319 TO STA 2344.5, S-48R TO S-49R.SDR FDEA202606040671Lamp · inoperativePOST-FLT INSP, L1 OVERHEAD EMERGENCY LT INOP. AMM: 33-51-04-2 RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.SDR FDEA202606010665Fire Bottle · failedAT 2335Z (APPROX 1:15 INTO THE FLIGHT), FL340, TAT -11, .838MACH, GOT BOTTLE DISCHARGE APU CAUTION WITH LIGHT APU BTL DSCG ON OVERHEAD AND BOTTLE APU ON STATUS PAGE. PERFORMED APU FIRE EXTINGUISHING BOTTLE PRESSURE SWITCH TEST PER ABOVE REF, TEST PASS, ANDSDR FDEA202605310656Skin · damagedREQUEST A PERMANENT REPAIR ON LT AFT FUSELAGE AT APPROXIMATELY STA 1895 TO 1958 AND S-40L TO S-43L. LT AFT FUSELAGE AT APPROXIMATELY BS 1895 TO 1958 AND S-40L TO S-43L. DAMAGED SKIN & STRINGER PERFORMED PERMANENT REPAIR IAW SRM51-10-02-0G. SRM51-20-01-0G. SDR FDEA202605300655Wire · detachedARMING WIRE ON EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL IS STRETCHED OUT AND NOT ARMING EMERGENCY LIGHTS NORMALLY WHEN THE WIRE FALLS OFF SWITCH. AMM: 33-51-00-710-803 REINSTALLED ARMING WIRE IN NORMAL POSITION, OP TEST WAS SUCCESSFUL,AS PER AMM 33-51-0SDR FDEA202605140595Skin · debondedLEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 AND SRM 51-70-04-2R-0 PARA 4N FIGURE SDR FDEA202605110586Switch · out of adjustEMERGENCY LIGHTS ADVISORY MESSAGE STILL APPEARS. AMM: 33-51-00-5 ADJUSTED SWITCH GAURD, OPS CHECK GOOD.SDR FDEA202605110585Warning Message · false activationEMERGENCY LIGHTS ADVISORY APPEARED ON PREFLIGHT. AMM: 33-51-00-5 EMERGENCY LIGHTS OPS CHECKS OK PER ABOVE REF, OK FOR SERVICESDR FDEA202605110581Skin · bulgedFOUND RT WING LE NR 11 SLAT EXTERNAL SURFACE A BULGE AT STA 873. BULGE REPAIRED AS PER B777 SRM57- 43-01-2R REPAIR 9 FIGURE 202 REV:51.0 AND EA G-5750-T0387321 P1. TITLE: WING-FLIGHT SURFACES-RH WING #11 SLAT OUTER SKIN BULGES AT NOSE BEAM AREA BETWEEN OSBSDR FDEA202605110580Skin · bulgedFOUND RT WING LE NR 9 SLAT EXTERNAL SURFACE A BULGE AT STA 564. BULGE REPAIRED AS PER B777 SRM57-43- 01-2R REPAIR 16 FIGURE 202 REV:53.0. AND EA G-5750-T0387322 P1. TITLE: WING - FLIGHT SURFACES-RH WING #9 SLAT OUTER SKIN BULGE AT NOSE RIB AT OSCS 564 - SRSDR FDEA202605100579Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP3.B & STEP5.A.(2) THEN FOUND 01EA CRACK ON THE RH UPPER WING SKIN FASTENER #5. RH UPPER WING SKIN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C,51-40-02-0G,51-40-SDR FDEA202605100578Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP3.B & STEP5.A.(2) FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER #5. H WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-50- 02-0G FINGURE 1,51-40-02-0G,51-10-01-0G,51-20SDR FDEA202605030534Skin · dentedFOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 127 INCHES AND T/E 10 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 127 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIGSDR FDEA202605030533Skin · dentedFOUND LEFT WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT THE CROSS OTEF 231 INCHES AND T/E 8 INCHES. REPAIRED LH WING T/E O/B FLAP I/B LOWER SURFACE 1EA DENT AT OTEF STA 231 AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4I FIGUSDR FDEA202604300524Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT RH WING UPPER WING SKIN COMMON TO FASTENER 5. RT WING UPPER SKIN 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50-02-0G, FIG 1, SRM 51-40-02-0G, FIG 12, SDR FDEA202604300523Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT LT WING UPPER WING SKIN COMMON TO FASTENER 5. LT WING UPPER SKIN NR 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50- 02-0G, FIGURE 1, SRM 51-40-02-0G FSDR FDEA202604240496Bulb · inoperativeR1 DOOR AFT EMERGENCY EXIT SIGN LIGHT INOP (1EA BULB). REPLACED THE BULB EMERGENCY EXIT LIGHT AT R1 DOOR IAW AMM 33-51-01-2.SDR FDEA202603200359Skin · dentedRIGHT WING OTBD FLAP LOWER SURFACE FROM OB TO IB 272 INCHES CROSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED RH WING OB FLAP LOWER SURFACE DENT AT OTEF STA 250 IAW SRM 57-53-01- 2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4G FIGURE 210 REV 51.0 AND ESDR FDEA202603170356Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK ON UPPER WING SKIN FASTENER NR 5. RH WING UPPER SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM 51-50-02-0G FIGURE 1, SRM 51-40-02-0G FIGURE 12, SRM 51-10-01-0G FSDR FDEA202603160354Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285G P11 STEP 3.B.(1)& STEP 5.A.(2) THEN FOUND 01EA CRACK ON UPPER WING SKIN FASTENER #5. LT WING UPPER SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM51-40-05-0G FIGURE 4 TABLE C, SRM51-40-02-0G FIGURE 12, SRM51-40-04-0G SDR FDEA202603050315Lamp · inoperativeDURING POSTFLIGHT, FOUND R1 DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED THE LAMPS, R1 DOOR SLIDE EMERGENCY EXTERIOR LIGHT 777 AMM. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA202603020314Slide · faultedUPON CLOSING THE AIRCRAFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L AND 13R. F/O OPENED THE DOOR TO SEE IF THE FAULTS WOULD RESET WITHOUT DISARMING DOOR 1L AND THE EVACUATION SLIDE DEPLOYED BUT DID NOT INFLATE.SDR FDEA202603020304Slide · unwanted deployUPON CLOSING THE ACFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L & 13R. F/O OPENED THE DOOR TO SEE IF THE FAULTS WOULD RESET WITHOUT DISARMING DOOR 1L & THE EVACUATION SLIDE DEPLOYED BUT DID NOT INFLATE. MAINTENANCSDR FDEA202602280291Safety Wire · wrong partLEFT SLIDE PACKBOARD RELEASE CABLE MECHANISM REQUIRES CAD COPPER SAFETY WIRE. REF FEA G-2560-F0386282 C P1. SAFETIED LT SLIDE PACKBOARD RELEASE CABLE MECHANISH WITH CAD COPPER BREAKAWAY WIRE.SDR FDEA202602230259Safety Wire · wrong partFOUND INCORRECT SAFETY WIRE ON L1 DOOR SLIDE. AMM: 25-66-01-4 REPLACED SAFETY WIRE WITH CAD COPPER.SDR FDEA202602200247Skin · dentedLH WING OB FLAP LOWER SURFACE FROM OB TO IB 97 INCHES CROSS TE TO LE 8 INCHES FOUND ONE DENT. REPAIRED LT WING OB FLAP LOWER SURFACE DENT AT OTEF STA 431 AS PER B777 SRM 57-53-01- 2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4 FIGURE 210 REV 51.0 AND EASDR FDEA202602180233Slide · damagedR1 DOOR SLIDE REQUIRES CORRECT BREAKAWAY WIRE TO BE INSTALLED ON PACKBOARD RELEASE CABLE. REF F.E.A. G2560-F0386294 C P1. INSTALLED CAD-PLATED COPPER BREAKAWAY WIRE MS20995CY16 ON R1 DOOR SLIDE SERIAL # M10771 PACKBOARD RELEASE CABLE PER F.E.A. WORK CARD INSDR FDEA202602160217Safety Wire · wrong partLEFT SLIDE ASSY. SN 3359, FOUND BREAK AWAY WIRE SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. RELEASED FOR SERVICE PER MEL : 52-11-01-02 CATEGORY : C EXPIRATION : 22FEB26 "MEL 52-11-01-02: DOOR _L1__ DOOR - INOP. IF SLID E/RAFT TO BE SDR FDEA202602160216Safety Wire · wrong partFOUND L1 DOOR SLIDE SAFETY WIRE NON-COMPATIBLE, NEEDS REPLACING. REPLACED SAFETY WIRE WITH PART NO. MS20995CY16 CAD PLATED COPPER. REF. AMM 25-66-01-4. AC OK FOR SERVICE.SDR FDEA202602160215Safety Wire · wrong partRH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A.# G-2560-F0386294 C PART 1) RH SLIDE - REPLACE THE BREAKAWAY WIRE SESDR FDEA202602160214Safety Wire · wrong partLH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOAR RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/3937 (FEA G-2560-F0386282 C P1). REMOVED AND REPLACED BREAKAWAY WIRE SECURING RELESDR FDEA202602150211Safety Wire · wrong partWRI TO REPLACE THE R1 DOOR SLIDE WIRE WITH MS20995CY16 WIRE. AMM: 25-66-01-4 REPLACED R1 DOOR SLIDE SHEAR WIRE WITH MS20995CY16 WIRE PER REF ABOVESDR FDEA202602150204Release Cable · wrong partRIGHT SLIDE PACKBOARD RELAEASE CABLE MECHANISM REQUIRES CAD PLATED COPPER BREAKAWAY WIRE. REF WRI 25-60/4116 FEA 2560-F0386282 C P1. SAFETIED RT SLIDE PACKBOARD RELEASE CABLE MECHANISM WITH CAD PLATED COPPER WIRE.SDR FDEA202602150203Slide · fomL1 DOOR SLIDE REMOVED FOR F.O.M. OF F.E.A. MOD TYPE F MOD NR G-2560-F0386282 REV NR C PS P1. INSTALLED L1 DOOR SLIDE OPS CHECKS GOOD IAW AMM 25-66-01-4, & AMM 25-66-01-4.SDR FDEA202602140194Safety Wire · wrong partSAFETY WIRE FOUND ON SLIDE WAS NOT THE CORRECT TYPE ACCORDING TO F.E.A.#:G-2560-F0386282 C PART: 1 (P1) REPLACED BREAKAWAY WIRE WITH CORRECT WIRE SPEC (MS20995CY16) THAT SECURES THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD. MPSDR FDEA202602140193Safety Wire · wrong partRIGHT SLIDE, REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A. G-2560-F0386294 C PART 1) CMM: 25-61-31 EA: 9-2560-T0386431 FEA: SDR FDEA202602130192Slide · miswiredR1 DOOR SLIDE HAS INCORRECT SAFETY WIRE ON PACKBOARD RELEASE CABLE. INSTALLED PROPER SAFETY WIRE ON R1 SLIDE PACKBOARD RELEASE CABLE IAW B777MM 25-66-01-4. A/C OK FOR SERVICE.SDR FDEA202602120183Wire · wrong partFOUND BREAKAWAY WIRE THAT SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. REMOVED LT DOOR SLIDE IAW MM 25-66-01-4. REMOVED STAINLESS SAFETY WIRE AND INSTALLED CORRECT WIRE IAW FEA G-2560-F0386282C. REINSTALLED DOOR SLIDE IAW 25-66-01-4. DOSDR FDEA202602090152Skin · crackedDURING WORK CARD: EG-5710-E0376285F P12 STEP3.B(1) & 5.A.(2), FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RIGHT WING UPPER SKIN NR 5 FASTENER HOLE REPAIRED IAW SRM 51-40-05-0G, FIGURE 4, TABLE C, SRM 51-40-02-0G, FIGURE 12, SRM 51-40-04-0G, FIGURE 2SDR FDEA202602090151Skin · crackedDURING WORK CARD: EG-5710-E0376285F P12 STEP4.B(2).(B), THEN FOUND ONE CRACK ON RT UPPER WING SKIN FASTENER #6 AS MARKED. RIGHT WING UPPER SKIN NR 6 FASTENER HOLE REPAIRED IAW SRM 51-40-05-0G, FIGURE 4, TABLE C , SRM 51-40-02-0G, FIGURE 12, SRM 51-40-04-0G, SDR FDEA202602090150Skin · crackedDURING WORK CARD: EG-5710-E0376285F P11 STEP4.B(2).(B), THEN FOUND ONE CRACK ON LT UPPER WING SKIN FASTENER NR 6. THE LEFT WING UPPER SKIN #6 FASTENER HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51- 20-07-0G FIGURE 2, SRM 51-50-02-0G FOGURE 1, SRM 51-40-02
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