N884FD
Service difficulty reports · 32
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N884FD' AND registry_match = 'registration' 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 n_number = 'N884FD' AND registry_match = 'registration' 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 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 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 FDEA202509231776Spring · damagedWHILE CLOSING DOOR 1L, AN INTERIOR SPRING BROKEN. REMOVED AND REPLACED 2 EACH SPRINGS ON VENT DOOR ASSY IAW AMM 52-11-04-4-0.SDR FDEA202411231725Module · inoperativeREF MTSI 33-50/4453, EMERGENCY LIGHT SW ON OVHD PANEL FOUND TO BE INTERMITTENT INOP. R/RED WINDOW HEAT/EMER LIGHTS MODULE, INSTALLATION TEST PASSED. EMERGENCY LIGHT TESTED NORMAL. WORK PERFORMED PER REF AMM 30-41-02-4, AMM 33-51-00-5SDR FDEA202411191687Light · malfunctionedEMERGENCY LIGHTS WOULD NOT SHUTOFF ON ENGINE SHUTDOWN CHECKLIST PERFORMED ENG SHUTDOWN CHKL RESET. EMER LT OPTION TURN GREEN, CHKL BACK TO NORMAL. A/C OK FOR SVC.SDR FDEA202403200317Power Cable · chafedFO EFB POWER CORD AT MAGNETIC PLUG HAD ELECTRICAL SPARKS AND ARCING IN FLIGHT. DISCONNECTED POWER CORD FROM EFB. DO NOT RECONNECT THE OLD CORD. F/O EFB POWER CORD REMOVED AND REPLACED AS PER AMM 46-11-96-4, TEST OK. A/C OK FOR SERVICE.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 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 FDEA202104090855Skin · crackedFUSELAGE LEFT HAND BILGE AREA AT STATION 1685 AREA FOUND WITH EXISTING BLENDOUT . FUSELAGE LEFT HAND BILGE AREA AT STATION 1685 AREA STRINGER-47 LEFT EXISTING BLENDOUT HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTED FOUND CRACK APPROXIMATELY 1/8 INCH PER B77SDR FDEA202104010805Floor Support · crackedBULK CARGO - FLOOR PANEL STRINGER AT RBL 41.5 FOUND 02 EA CRACKS AT STA 1937 AND STA 1958 AS MARKED. BULK CARGO FLOOR PANEL STRINGER AT RBL 41.5 AT STA 1937 AND STA 1958 02EA CRACKED REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STA 1926 -SDR FDEA202103300798Doubler · misalignedWHILE ACCOMPLISHING LH E.O.#G-5310-E0332629 K P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR S-35L NEAR MILLED EDGE. COMPLIED WITH E.A.# G-5310-T0360894 P1 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202103300797Doubler · misalignedWHILE ACCOMPLISHING RH E.O.#G-5310-E0332629 K P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.# G-5310-T0360894 P2, DEVIATION TO SB 777-53- 0087 REV 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202103290793Fitting · crackedDURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E-G-5310-E0332629 K P5 ON REMOVED FASTENER HOLES AND FOUND 01 EA CRACK INDICTION ON LHS VERTICAL FLANGE OF THE FRONT LOWER SPAR CHORD AT BS 1035 APPROX LBL 81.30 LOWER O/B HOLE AS MARKED. WING CSDR FDEA202103290792Fitting · crackedDURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E-G-5310-E0332629 K P6 ON REMOVED FASTENER HOLES AND FOUND 01 EA CRACK INDICATION ON RHS VERTICAL FLANGE OF THE FRONT LOWER SPAR CHORD AT BS 1035 APPROX RBL 81.30 LOWER O/B HOLE AS MARKED. WING SDR FDEA201908211991Lamp · inoperativePOST-FLT INSP, ONE OVERHEAD SUPRNMRY EMERGENCY LIGHT INOPERATIVE DURING A LIGHTS TEST. REPLACED THE LAMP, IAW AMM: 33-51-04-2. LIGHT TESTED SATIS, OK FOR SERVICE.SDR FDEA201705041358Latch · damagedPREFLIGHT MX CHECK, FOUND THE L1 DOOR EMERGENCY ESCAPE SLIDE COVER SHROUD FWD LATCH DEFORMED AND NOT RETAINING SHROUD ASSY. REMOVED AND REPLACED L1 DOOR BUSTLE FORWARD LATCH IAW CMM 25-66-06, REINSTALLED BUSTLE IAW MM 25-66-06-4.SDR FDEA201702220625Lamp · inoperativeDURING A POST FLIGHT INSPECTION, ONE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-50-00-2. LIGHTS TESTED GOOD, OK FOR SERVICE.SDR FDEA201601210273Skin · puncturedFORWARD LOWER FUSELAGE SKIN AT STATION 630, BETWEEN STRINGER 34R - 35R, FOUND A 2" PUNCTURE HOLE. REPAIR IDENTIFIED AS MAJOR REPAIR BY ENGINEERING. EA G-5330-T0322852A WAS COMPLIED WITH.SDR FDEA201506101753Bulb · inoperativeONE OVERHEAD EMERGENCY EXIT LIGHT DID NOT ILLUMINATE DURING CABIN INSPECTION. R & R THE OVERHEAD EMERGENCY EXIT LIGHT & OPS CHECKED NORMAL IAW AMM 33-51-03-2.SDR FDEA201501130144Light · inoperativePOST FLIGHT CHECK FOUND 1 SUP AREA EMER LT INOPERATIVE. RELAMPED IAW AMM 33-51-03-2. EMER LIGHTS TESTED NORMAL. ITEM OK FOR SERVICE.SDR FDEA201407041627Battery Pack · dischargedON POST FLIGHT CHECK FOUND L1 DOOR EMER ASSIST BATTERY PACK GREEN TEST LIGHT NOT FLASHING. R & R L1 DOOR ASSIST BATTERY PACK TEST LIGHT 9V BACK UP BATTERIES TWO EACH IAW AMM 52-11-20-4-2. OPERATIONS CHECKED NORMAL, ITEM OK FOR SERVICE.SDR FDEA201405110984Slide · deployedDOOR L1 SLIDE DEPLOYED. REMOVED L1 DOOR MOUNTED SCAPE SYS IAW MM 25-66-00-2. RESTORED DOOR MOUNTED ESCAPE SLIDE SYS AFTER SLIDE DEPLOYMENT. 2 SLIDE SAFETY PINS, BOTTLE & GIRT REMOVED IAW AMM 25-66-00-2.SDR FDEA201307231644Tire · leakingTIRE PRESSURE EICAS MESSAGE. NR 3 MLG TIRE PRESSURE 180 PSI DECREASED TO 160 PSI. REMAINED AT 160 PSI AFTER LANDING. VERIFIED NR 3 TIRE PRESSURE IS LOW. R & R NR 3 WHEEL ASSY IAW MM 32-45-01-4. ACFT OK TO CONTINUE.SDR FDEA201306151305Autopilot Sys · malfunctionedACFT WENT INTO AN UNCOMMANDED RIGHT TURN. NOTICED IT HAD GONE INTO HDG MODE AND THE HDG WAS APPROX 112 DEGREES (VS. 030) F/O DISCONNECTED AUTOPILOT AND BANKS 30 LEFT TO REJOIN COURSE. INTERROGATED MAT AND FOUND MAINT MESSAGE 22-11635 NOT ACTIVE. FIM 34-3SDR FDEA201211224125Interface Unit · inoperativeAPPROX 2.5 HRS INTO FLIGHT, RECIEVED HYD QTY LOW R CAUTION MESSAGE. OBSERVED CONTINUOUS DROP IN RIGHT HYD QTY THROUGHOUT REMAINDER OF FLIGHT, DIVERTED. R & R RT HYD INTERFACE MODULE. OPS CHECKED GOOD IAW MM 29-11-50-4. R & R RT HYD RESERVOIR QUANTITY TRANSSDR FDEA201203281167Computer · malfunctionedFLIGHT PLAN WAS LOADED VIA UPLINK. FLIGHT PLAN WAS CHECKED IN CAPTAINS PREFIGHT ON PLAN PAGE FOR PROPER SEQUENCING AND VERIFIED WITH F/O THROUGH CFM PROCEDURES. WHEN ACFT WAS AT FL340 APPROACHING N45/W160, WHEN ACFT SEQUENCE POINT, NEXT POINT WAS N43/W150, ASDR FDEA201110074382Battery · inoperativeFOUND R1 DOOR EPAS POWER GREEN LIGHT DOES NOT COMES ON. REPLACED EPAS POWER PACK BACKUP BATT AND CHECK OK IAW MM52-11-20-4-2, 52-11-20-5-2. ACFT OK FOR SERVICE. FINAL CLOSED.SDR FDEA201103150981Light · inoperativeR-1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR EMERGENCY EXIT LIGHT.
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