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 = '777F' 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 = '777F' 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 UIEA2025042100552Lamp · inoperativeL1 DOOR EXTERIOR EMERGENCY LIGHT INOP.(<P>R&R LAMP IAW AMM 33-51-04/201. OPS CHK OK PER AMM 33-51-00/501.</P>)SDR UIEA2025041900550Seal · missingCREW REPORTED FIRST AID KIT MISSING SEAL AND ITEMS. REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-64-50. NO FURTHER DEFECTS NOTED.SDR FDEA202504080581Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 3 IN AWAY TO AFT EDGE AND 213 IN TO IB EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 247 AS PER B777 SRM 57-53-01-2R- 2 AND SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-T0382953 P1. THIS IS A MAJOR REPAIRSDR FDEA202504070586Hydraulic Line · leakingLOST ALL CENTER HYDRAULIC FLUID SHORTLY AFTER AIRBORNE. EICAS MSSG HYD PRESS SYS C APPEARED AFTER RAISING LANDING GEAR HANDLE. REMOVED AND REPLACED ELEVATOR RETURN LINE P/N # 272W8290-82 REF B777 AMM 20-11-10-2, SERVICED CENTER HYD SYSTEM REF B777 AMM SDR KCSA2025032410Circuit Card · unserviceable100240750 - DETECT FIRE ENGINE LEFT (BOTH FIRE LOOP #1 AND #2). PERFORMED GENERAL VISUAL INSPECTION OF LEFT-HAND ENGINE, FIRE LOOP 1 AND LOOP 2 IAW B777-200 WDM 26-11-11. NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED LEFT-HAND ENGINE FIRE DETECTION CARDSDR UIEA2025031900361Smoke Detector · false activationSMOKE CREW REST F/D EICAS MESSAGE.(<P>CREW RESET SMOKE DETECTOR C/B RESET AND OPERATIONAL CHECK SATISFACTORY IAW AMM 26-14-10.</P>)SDR FDEA202503130389Skin · dentedFOUND RHW T/E I/B AFT FLAP LOWER SURFACE DENT AT THE CROSS ITEF 250 AND T/E 2 INCHES. REPAIRED RHW T/E I/B AFT FLAP LOWER SURFACE DENT AT THE CROSS ITEF 250 AND T/E 2 INCHES AS PER B777 SRM 57-53-01-2R-1. SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-T0382576 P1.SDR FDEA202503130387Fan · failedEQUIP COOLING FAN R ON SHUTDOWN. REMOVED AND REPLACED FWD EQUIPMENT COOLING FAN R.OPS CHECK GOOD.SDR FDEA202503040329Autothrottle Sys · malfunctionedAFTER STARTING ENGINES AND CALLING FOR THE AFTER START CHECKLIST AND COMPLETING FLOW, I HEARD AUTO THROTTLE SERVO S AND NOTICED UNCOMMANDED THROTTLE ADVANCEMENT. I RETARDED THROTTLES AT ABOUT 30% N1 AND DISCONNECTED. THRUST FMA WAS THR REF. TURNED FLT DSDR FDEA202503040326Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 231RF P/N:152W8301-67 FOUND CRACKED AT STA 1014 LBL 84. MAIN DECK CARGO FLOOR PANEL 231RF P/N:152W8301-67 CRACKED AT STA 1014 LBL 84. DAMAGE SIZE: L=2.9" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 REV SDR FDEA202503040320Lamp · inoperativeCEILING EMERGENCY LIGHT IN SUPERNUMERARY AREA IS INOPERATIVE. R/R'D CEILING EMERGENCY LIGHTL LAMP IN SUPERNUMERARY AREA AND CHECKED NORMAL IAW AMM 33-51-03-2.SDR FDEA202502180247Power Supply · failedEMERGENCY OVERHEAD LIGHT INOP IN SUPERNUMERARY CABIN - OVER DOOR L1. REMOVED AND REPLACED LH EMERGENCY LIGHT POWER SUPPLY REF. AMM 33-51-06-2. ALL LIGHTS TEST GOOD. A/C OK FOR SERVICE.SDR UIEA2025012700109Seal · brokenCAPT SIDE EVAS RED SEAL FOUND BROKEN.(<P>TRANSFER TO DMI 224765 PER MEL 25-64-04 CAT D. PLACARD INSTALLED. </P> / <P>25JAN25 - ORD - 1904731 - ITEM 5 - REPLACED CAPTAIN EVAS RED SEAL PER ATLAS TASK CARD C-25-099-17-01. THIS CLEARS DMI 224765. PLACARDS REMOVED<SDR FDEA202501130060Lamp · failedDEBRIEF WITH CREW ENERGENCY LIGHT NEAR GALLEY DOES NOT ILLUMINATE WITH PERFLIGHT EMER LIGHT/TEST LIGHT CHECK. AMM: 33-50-00-2 PER AMM 33-50-00-2, RELAMP ENERGENCY LIGHT ,OPS NORMAL,A/C OK TO SVC.SDR FDEA202501110059Lamp · failedEMERGENCY DOME LIGHT OUT IN COCKPIT. AMM: 33-51-07-2 RELAMPED AND OPS CHECKED NORMAL IAW AMM 33-51-07-2.SDR FDEA202501110058Lamp · inoperativeEMERGENCY DOME LIGHT OUT IN COCKPIT. AMM: 33-51-07-2 RELAMPED AND OPS CHECKED NORMAL IAW AMM 33-51-07-2.SDR FDEA202501100057Door · stuckL1 DOOR STUCK IN CLOSED POSITION. OPENED AND CLOSED L1 DOOR FROM INSIDE AND OUTSIDE OVER 20 TIMES WITH NO ISSUES, INCLUDING ARMING AND DISARMING. THE DOOR OPENS/CLOSES SMOOTHLY EVERY TIME, OPS CHECKS GOOD. FOUND NOTHING ABNORMAL ON GVI OF LATCH MECHANISMS OSDR FDEA202501100054Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 249 AND T/E 11 INCHS. REPAIRED RH WING T/E O/B FLAP LOWER SURFACE DENT AT OTEF STA 249 AS PER B777 SRM 57- 53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.2 AND EA: G-5750-T0381784 P1. TSDR UIEA2024123001193Battery · inoperativeL1 DOOR/SLIDE INOP EVAS BATTERY PACK INOP(<P>R/R EPAS PACK BATTERY FOR L1 DOOR IAW AMM 52-11-20 -00-805-002 & 52-11-20-400-805. OPS CHK GOOD</P>)SDR FDEA202412281848Amu · burnedINTERPHONE SERVICE BREAKER N P11 C23631 FOUND POPPED AFTER POWER SURGE/DROPPED OFFLINE. FOUND BOTH P11 C23631 INTERPHONE SERVICE BREAKER B24 POPPED AND P320 PANEL INTPH- GRD C13 CIRCUIT BREAKER POPPED. NO FAULTS LOGGED IN MATT EXSITING FAULTS OR EXTESDR FDEA202412271847Power Supply · failedRH EMER EXIT LIGHTS POWER SUPPLY CANNED. AMM: 33-51-06-2 REMOVED/REPLACED POWER SUPPLY. OPS CHECK NORMALSDR FDEA202412201822Tire · wornON TAKE OFF RECEIVED #3 TIRE LOW PRESSURE ALERT. ACCOMPLISHED LOW TIRE CHECKLIST AND DID A 30 FLAP NO AUTO BRAKES LANDING FOUND #3 TIRE PUNCTURE IN TREAD WITH NO FINDINGS. NO VISIBLE DAMAGE EITHER ON TIRES. CARRIED OUT INSPECTION OF MAIN & AFT INBOARD RIGSDR KCSA2024122031Cover · brokenLOGPAGE - 100214767 L1 DOOR AFT EXIT LIGHT COVER BROKEN. TRANSFERRED TO DMI 100214768 IAW B777 MEL 33-51-1, CAT C, DUE DATE 12-30-24. NO (M) PROCEDURES. PLACARDS INSTALLED. LOGPAGE - 100214782 REFRENCE DMI 100214768 L1 DOOR AFT EXIT LIGHT COVER BROKEN. REMOVEDSDR UIEA2024120901170Life Vest · missingPRIOR TO DEPARTURE, SUPERNUMARY SEAT 4 LIFE VEST MISSING.(<P>INSTALLED NEW LIFEVEST INTO SEAT 4 (SUPERNUMARY) POS IAW AMM 25-62-01 & AIPC 25-62-01. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024120501167Life Vest · missingON PREFLIGHT, 2 LIFE VESTS MISSING FROM COCKPIT(<P>ADDED TWO LIFE VESTS TO COCKPIT PER AMM 25-62-01. NO FURTHER DEFECTS NOTED. DMI 221886 CLOSED.</P>)SDR FDEA202411131676Efb · burnedF/O EFB IS HOT AND SCREEN IS WARPING AWAY FROM DEVICE. F/O EFB REMOVED FROM A/C AS PER AMM 46_11_96_4_0. FLT CREW DISCONNECTED F/O EFB AND PLACED IT INTO FIRE BAG. CDG MX REMOVED THE EFB FROM A/C.SDR FDEA202410191551Autothrottle Sys · malfunctionedAFTER ENGINE START AND TAXI. RELEASED THE BRAKES AND ADVANCED THE THROTTLES. AUTO THROTTLES CAME ON AND ADVANCED. PULLED THROTTLES BACK AND THEY ADVANCED AGAIN. DISCONNECTED AUTO THROTTLES, CYCLED AT/ARM SWITCHES OFF THEN ON. AUTO THROTTLES PERFORMED NORMSDR FDEA202410081446Floor Panel · damagedWHEN ACCOMPLISH EA G-5321-T0377185 REV B, FOUND THE PANEL STILL CAN BE REPAIRED, PLEASE EVALUATE TO REVISTE THE EA. REPAIRED MAIN DECK CARGO FLOOR PANEL AT APPROX STA 1736/LBL49.5 AS PER B777 SRM 53- 00-50 REPAIR 4 REV 47.0 AND EA:G-5321-T0377185C P4 TITLSDR FDEA202410061429Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 4.5 IN TO AFT EDGE AND 211.5 IN TO OB. DENT LOACTION RH OB FLAP OTEF STA 316. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 316 AS PER B777 SRM 57-53-01- 2R-2 AND SRM 51-70-04-2R-14 REV 47.0 AND EA:G-5750-SDR FDEA202409211360Fan · failedDURING PREFLIGHT AN ELECTRICAL SMELL WAS NOTICED OUT OF OVERHEAD PANEL AIR VENTS. REMOVED AND REPLACED RIGHT RECIRCULATION FAN PER BOEING AMM 21-25-07-4.SDR FDEA202408301198Window · crackedPOST-FLT INSP, L1 DOOR ESCAPE SLIDE BUSTLE PRESSURE GAUGE VIEWPORT WINDOW CRACKED. THE PART FINALLY SHOWED UP. REMOVED AND REPLACED L1 DOOR EMERGENCY ESCAPE SLIDE BUSTLE PRESSURE VIEWPORT LENS ASSY, REF AMM: 25-66-06-4.SDR UIEA2024082700847Oil Filter · warning messageENG OIL FILTER L STATUS.(<P>PERFORMED FIM TASK 79-21 TASK 819. PERFORMED PROCEDURE E (1A), (1B), (1C) & (1D).</P> / <P>PERFORMED ENGINE FLUSH PER AMM 12-22-01. REPLACED LH ENG OIL FILTER PER AMM 79-21-07 & IPC 79-21-03-03. PERFORMED ENGINE RUN PER AMM TASK 71-SDR FDEA202408031080Window · overheatedRIGHT SIDE AFT WINDOW IS VERY HOT TO THE TOUCH AND APPEARS TO HAVE SOME CHARRING AND DELAMINATION IN THE MIDDLE OF THE WINDOW ALONG THE BOTTOM EDGE. COMPLIED WITH PART 3 OF E.A. # : G-5610-T0380167 REMOVED AND REPLACED R3 WINDOW, OPS CHECKS GOOD.SDR UIEA2024073100764Medical Unit · abnormalAED MIISSING EMERGENCY AIRWAY. R & R AED IAW DWG 777F-25-EEL PER AMM 25-64-53. OPS CHECK NORMAL ON LCD. THIS CLEARS MDDR 213839 PLACARD REMOVED.SDR UIEA2024060700501Battery Pack · no testA/C FLASHLIGHT ON CAPTAIN' S SIDE DOES NOT TEST.(<P>CAPT FLASHLIGHT BATTERY REPLACED IAW AMM 25-60-00. FOUND TEST GOOD. </P> / <P>P/N OFF P2-07-0021-002 S/N NSN </P> / <P>P/N ON P2-07-0021-002 S/N NSN </P>)SDR KCSA2024042714Fire Warning · illuminatedSTATUS MESSAGES: OVERHEAT CIRCUIT R2. TRANSFERRED TO DMI #100122850 IAW B777 MEL REFERENCE 26-11-2. CATEGORY C. DUE 5-7-24. PLACARDS INSTALLED. STATUS MESSAGE: FIRE LOOP 2 ENGINE RIGHT. TRANSFERRED TO DMI #100122851 IAW B777 MEL REFERENCE 26-11-1-1. CATEGORY CSDR KCSA2024042715Fire Loop · false indicationOVERHEAT CIRCUIT 2R. PERFORMED TROUBLESHOOTING PER KA B777 FIM 26-11 TASK 811. FAULT WAS INTERMITTENT MESSAGE. CLEARS, NO DEFECTS NOTED AT THIS TIME. FIRE LOOP 2 ENGINE RIGHT. PERFORMED TROUBLESHOOTING PER KA B777 FIM 26-11 TASK 811. FAULT WAS INTERMITTENT. MESDR KCSA2024042513Detection Sys · false activationOVERHEAT CIRCUIT R2 STATUS MESSAGE. NO ACTIVE STATUS OR EXISTING FAULTS. PERFORMED ENGINE FIRE DETECTION OPERATIONAL TEST IAW B777 AMM 26-11-00. ALL CHECKS GOOD. FIRE LOOP 2 ENGINE RIGHT. NO ACTIVE STATUS OR EXISTING FAULTS. PERFORMED ENGINE FIRE DETECTION OPESDR UIEA2024041100270Flashlight · no testCAPT'S FLASHLIGHT WILL NOT TEST ( FLASHLIGHT HOLDER ASSEMBLIES (INCLUDING FLASHLIGHT)(<P>TRANSFER TO DMI 206439 PER MEL 25-64-02 CAT C, DUE 20APR24.</P> / <P>LP 1815370 - M4 - HKG - CAPT FLASHLIGHT REPLACED AND TEST OK IAW AMM 25-64-01. THIS CLOSES MDDR 206439SDR UIEA2024041200271Flashlight · inoperativeCAPT FLASHLIGHT DOES NOT FLASH GREEN ON THE TEST MODE. R 7 R CAPT FLASHLIGHT IAW AMM 25-64-01. OPS CHECK NORMAL.SDR FDEA202403270381Module · inoperativeRECEIVED MULTIPLE EICAS ALERTS CLIMBING TO FL330. NO AUTOLAND, WNDSHEAR SYS, EEC MODE L, EEC MODE R. RAN ECL CHECKLISTS FOR EEC MODE LT & RT. ACFT CONTINUED TO CLIMB THRU MCP SELECTED ALT ON ATTEMPING LEVEL OFF. ATC SHOWED 200 FT LOW WHEN MCP SELECTED ALTITUSDR FDEA202403260372Pitot Head · failedAUTO PILOT DISCONNECTED AFTER LEVELING FL340. ALTIMETERS LEFT AND RIGHT INDICATED 400' HIGH. MULTIPLE EICAS : "AIRSPEED UNRELIABLE" " ENG EEC MODE R" "ENG EEC MODE L" " GND PROX WARN". ATC READOUT SHOWED 300' LOW WHEN WE RETURNED TO FL 340'. EICAS BUTTON DESDR FDEA202402210205Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 57, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 57, SHEET 2 OF 5 SECTION CUT B-B ARROW ORIENTATION IS CLARISDR FDEA202402210204Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 53, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE GAP 0.60 MIN IS TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURESDR FDEA202402210203Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 51, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE "0.60 - 0.30 TYPICAL GAP" SHOWN SEEMS TOO BIG. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 51, SSDR FDEA202402210202Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 49, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 49, SHEET 2 OF 3 SECTION CUT B-B ARROW ORIENTATION IS CLARISDR FDEA202402210201Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART7, FOUND FIGURE 47, SHEET 2 OF 4, THE SECTION CUT D-D ARROW NOT MATCH THE VIEW D-D ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART7, FIGURE 47, SHEET 2 OF 4 SECTION CUT D-D ARROW ORIENTATION IS CLARISDR FDEA202402210200Longeron · misoverhauledWHILE ACCOMPLISHING EO E G-5710-E0366409 D PART7,(LEFT HAND LONGERON MODIFICATION) FOUND FIGURE 44, SHEET 2 OF 2, VIEW A, CIRCLE STEP 2, THE PRINTED QUANTITY 48 LOCATIONS IS NOT IN ACCORDANCE WITH THE FIGURE AND AIRCRAFT QUANTITY. DISCREPANCY IN EO E G-5SDR FDEA202402210199Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 120, SHEET 2 OF 5, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 120, SHEET 2 OF 5, SECTION CUT B-B ARROW ORIENTATION IS CLSDR FDEA202402210198Unknown · misoverhauledWHILE CARRY OUT EO E G-5710-E0366409 D PART8, FOUND FIGURE 116, SHEET 2 OF 3, THE SECTION CUT B-B ARROW NOT MATCH THE VIEW B-B ORIENTATION SHOWN AND THE 0.60 MIN GAP TOO WIDE TO LOCATE THE REPAIR ANGLE. DISCREPANCY IN EO E G-5710-E0366409 D PART8, FIGURE 1
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