N857FD
Service difficulty reports · 39
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 = 'N857FD' 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 = 'N857FD' 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 FDEA202608221219Tire Tread · separatedCHECK FOUND NR 11 TIRE TREAD SEPARATION.SDR 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 FDEA202601220080Skin · dentedFOUND RT WWING T/E OTBD FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHS. REPAIRED RHW T/E O/B FLAP LOWER SURFACE DENT 1EA AT THE CROSS OTEF 335 AND T/E 2 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 203 AND SRM 51-70-04-2R-1 REV 51.0 AND SDR FDEA202601220078Fitting · crackedFOUND RH WING NR 11 SLAT L/E UPPER SKIN 1 EA BULGE AT THE O/B MAIN TRACK FITTING AREA. RH WING NO.11 SLAT L/E UPPER SKIN BULGE AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 202 REV:51.0 AND EA G-5750-T0386209 P1. TITLE:WING-FLIGHT SURFACES-RH WING SDR FDEA202601210077Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285E P12 STEP 3.B.& STEP5 A.(2) THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RT WING UPPER SKIN FASTENER HOLE REPAIRED IAW SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0G, FIGURE 12, SRM 51-20-07-0G, FIGURE 1, SRSDR FDEA202601210076Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285F P12 STEP4. B. (2). (B). THEN FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 6. RT WING UPPER SKIN NR 6 CRACKED FASTENER HOLE REPAIRED IAW SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0G, FIGURE 12, SRM 51-20-07-0GSDR FDEA202601200074Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) DAMAGED AT STA 1450 LBL 2. MAIN DECK FLOOR PANEL 241SF (P/N 152W8601-7) CRACKED AT STA 1450 LBL 2 DAMAGE SIZE: L= 0.8" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGURE SDR FDEA202601200073Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL 241LF DAMAGED AT BS 1300, LBL 45. FLOOR PANEL 241LF DAMAGED: L= 1", DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51. REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51.SDR FDEA202601200072Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) DAMAGED AT STA 1400 LBL 45. MAIN DECK FLOOR PANEL 241QF (P/N 152W8402-21) CRACKED AT STA 1400 LBL 45 DAMAGE SIZE: L= 1.2" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMAGE 1 FIGUSDR FDEA202601200071Skin · damagedNUMBER 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS184 SCREW HOLE FOUND ELONGATE. NR 7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 ELONGATE SCREW HOLE REPAIRED IAW SRM 57-43-01-2R REPAIR 6, FIG 203, REV: 51.0 AND EA G-5750-T0386196 P1, MAJOR REPAIR ISDR FDEA202601200070Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285F P11 STEP3. B. (1). & STEP5 A. (2), THEN FOUND 02EA CRACKS ON LH UPPER WING SKIN FASTENER #5 AS MARKED. THE LEFT WING UPPER SKIN #5 FASTENER CRACKED HOLE REPAIRED IAW SRM 51-50- 02-0G, FIGURE 1, SRM 51-40-02-0G, FIGUSDR FDEA202503220473Power Supply · inoperativeDURING SERVICE CHECK, FOUND L/H SLIDE LIGHT INOP. PART 22MAR25 14:16 MC1 IDENTIFIED PARTS EMERGENCY LIGHTS. RELAMPED L/H SLIDE LIGHT PER AMM 33-51-04-2. NO HELP. REMOVED AND REPLACED L1 EMER LIGHTS POWER SUPPLY PER AMM 33-51-06-2, BUT PART BFS. SSDR FDEA202501210113Lamp · inoperativeCHECK FOUND ONE EMERGENCY AREA LIGHT IS INOP. RELAMPED THE EMERGENCY AREA LIGHT REF AMM 33-51-03-2, TEST NORMAL. A/C OK TO CONTINUE.SDR FDEA202501020002Lamp · failedLOWER RIGHT EXIT SIGN ON THE RIGHT SIDE OF ENTRY DOOR L1 HAS ONE BULB INOP. REPLACED LAMP PER AMM : 33-51-01-2. TEST PASSED.SDR 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 FDEA202010232615Structure · damagedWHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM N00526) FOUND 02 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATION 1035 RIGHT HAND BUTTLINE 88 AND RIGHT HAND BUTTLINE 90.5. RIGHT HAND WING CENTER SECTION FRSDR FDEA202010232614Structure · damagedWHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR. SNRM N00525 FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB STATION 1035 LEFT HAND BUTTLINE 88. LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EACSDR FDEA202010232613Structure · damagedWHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM N00526) FOUND 02 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 RIGHT HAND BUTTLINE 88 AND RIGHT HAND BUTTLINE 90.5. RIGHT HAND WING CENTER SECTION FRONT SPAR LOWSDR FDEA202010232611Structure · damagedWHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR, SNRM #N00525. FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 1035 LEFT HAND BUTTLINE 88. LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (01 EACH) EXISTINSDR FDEA202010152502Doubler · out of alignmentWHILE ACCOMPLISHING EO G-5310-E0332629 H PART 6 FOUND 3 EACH PILOT HOLES AT NEW FUSELAGE SKIN DOUBLER MISALIGNED WITH THE LONGERON FITTING BETWEEN BODY STATION 993 TO BODY STATION 1008 BETWEEN STRINGER 35 RIGHT TO STRINGER 36 RIGHT. DOUBLER WITH MISALIGNED HOSDR FDEA202010152501Doubler · out of alignmentWHILE ACCOMPLISHING EO G-5310-E0332629 H PART 6 FOUND NEW FUSELAGE SKIN DOUBLER PART NUMBER 143W2314Y406 PILOT HOLES MISALIGN WITH EXISTING FUSELAGE SKIN HOLES BETWEEN BODY STATION 993 TO BODY STATION 1008 BETWEEN STRINGER 35 RIGHT TO STRINGER 36 RIGHT. DOUSDR FDEA202010152500Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON RIGHT HAND SIDE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON AND THE FUSELAGE SKIN AND FOUND 1 EACH CRACK APPROXIMATELY 0.5 INCHES LENGTH, AS SDR FDEA202010152499Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND SIDE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON AND THE FUSELAGE SKIN AND FOUND 1 EACH CRACK APPROXIMATELY 0.75 INCHES LENGTH, AS MASDR FDEA202010152503Doubler · out of alignmentWHILE ACCOMPLISHING LEFT HAND EO G-5310-E0332629 H PART 5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35 LEFT NEAR MILLED EDGE. COMPLIED WITH EA G-5310-T0357565 P1. TITLE: FUSELAGE MAINFRAME-DEVIATION TO SB-777-53-0087 R1-LT AND RSDR FDEA202010152498Structure · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON RIGHT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING LONGERON LOWER WING BODY STATION 1035 APPROXIMATELY RIGHT HAND BUTTLINE 82AND FOUND 01 EACH LOWESTSDR FDEA202010152497Structure · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON LEFT HAND SIDE VERTICAL FLANGE OF THE SPAR CHORD AT UNDERWING LONGERON LOWER WING BODY STATION 1035 APPROXIMATELY LEFT HAND BUTTLINE 82 AND FOUND 01 EACH LOWEST SDR FDEA202010152504Doubler · out of alignmentWHILE ACCOMPLISHING RIGHT HAND EO G-5310-E0332629 H PART 6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35 RIGHT NEAR MILLED EDGE. COMPLIED WITH EA G-5310-T0357565 P2. TITLE: FUSELAGE MAINFRAME-DEVIATION TO SB-777-53-0087 R1-LT ANDSDR FDEA202010082435Floor Support · crackedLOWER BULK CARGO COMPARTMENT FLOOR STRINGER FOUND CRACK AT STATION 1958 RBL 41.5. LOWER BULK CARGO COMPARTMENT AT STATION 1958 RBL 41.5 CRACKED FLOOR STRINGER REPAIRED, AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2. REPAIR STRINGER 01 EACH AND REPAIR ANGLSDR FDEA2019111532940None · nonePDIS 857 05-50 9138 13NOV19 SEA OPEN U LOGPAGES:3182688 FLEW INTO A VERY THIN, RAGGED VOLCANIC ASH CLOUD @ FL340 AT APPROX 2350Z NOTICED A SMALL, BUT STEADY EGT CLIMB AT A FIXED N1. EGT MAXED OUT AT 710 DEGREES BEFORE MAEUVERING OUT OF CLOUD.SDR FDEA201705021333Lamp · inoperativeRT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP AND OPS CHECKED GOOD IAW AMM 33-51-00-5. ACFT OK FOR SERVICE.SDR FDEA201508182609Battery · damagedL1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH EPAS BATTERIES & TESTED OK IAW AMM 52-11-20.SDR FDEA201508182608Battery · damagedL1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH EPAS BATTERIES & TESTED OK IAW AMM 52-11-20.SDR FDEA201508182602Battery · damagedL1 DOOR EMER POWER ASSIST SYS STATUS LIGHT FOUND NOT BLINKING. FOUND LOWER EPAS BACKUP BATTERY SOCKET DEFORMED & NOT FULLY INSERTED INTO EPAS PACK. R & R BOTH EPAS BATTERIES & TESTED OK IAW AMM 52-11-20.SDR FDEA201307111543Unknown · odorON ENTERING COCKPIT, FAINT ODOR SIMILAR TO A BURNED ELECTRICAL WAS PRESENT. SWITCHED AIR CONDITION CART AIR TO APU AIR, ODOR STOPPED IAW FIM 21-00-00-2, CHECKED MEC COMP'T NORMAL. ACFT OK FOR SERVICE. FINAL CLOSED.SDR FDEA201307101520Bulb · inoperativeFOUND RT OVERWING SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED BULB IAW MM33-51-04-2. TEST PASSED.SDR FDEA201210213709Slide · failedMAIN CABIN DOOR SLIDE ACTIVATED. CAPT/FO, BOTH VERIFIED DOOR(S) WERE DISARMED BUT SLIDE ACTIVATED, DOOR SYNOPSIS INDICATED "M" ON BOTH DOORS. REMOVED LT DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-66-00 201, AND LT CREW DOOR CLOSED EASILY. INSTALLED LT ENTRY DOSDR FDEA201103130949Slide · unwanted deployL1 SLIDE DEPLOYED ON ARRIVAL. R&R L1 DOOR MOUNTED ESCAPE SLIDE PACK IAW AMM 25-66-01-4 AND R&R L1 EPAS RESERVOIR IAW AMM 52-11-22-4, ACFT OK FOR SERVICE.SDR FDEA201010124015Line · leakingHYD QTY LOW CTR (LOST ALL HYD FLUID IN CTR) SVC'D HYD FLUID TO CTR HYD SYS TO PROPER LEVEL IAW AMM 12-12-01-3-0, PERF CTR HYD SYS LEAKS FOUND. NO EXTERIOR LEAKS CAN BE FOUND. SUMP DRAINED LT FUEL TK & RT FUEL TK, FOUND HYD CONTAMINATED IN RT FUEL TK FUEL SAM
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