N786FD
Service difficulty reports · 41
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 = 'N786FD' 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 = 'N786FD' 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 FDEA202610011465Skin · noneC2 DOOR AFT LOWER CORNER FOUND EXISTING REPAIR. ACCOMPLISHED WITH EA# F-5330-T0388754 TITLE: FUSELAGE-PLATE AND SKIN-ALTERNATIVE INSPECTION TO REPAIR AT NO 2 CARGO DOOR CUT OUT AFT LOWER CORNER, STA 1410-1450, S- 25R TO S-28R. *THIS EA DEVIATES FROM EO F-5SDR FDEA202609191371Skin · dentedEVALUATE EXISTING REPAIR ON FUSELAGE SKIN AT SECTION 48 LH UPPER SIDE OF TAILCONE BETWEEN BS 1941 AND BS 1963.8 APPLIED PERMANENT REPAIR AT FUSELAGE SKIN SECTION 48 LT UPPER SIDE BTW BS 1941 AND 1963.8 IAW B757 SRM 53-80-01-2R, DETAIL, I, FIG 201, SHEET 1 ANDSDR FDEA202609191370Crease Beam · corrodedMAIN CARGO DECK CREASE BEAM INNER CHORD AT BS 880 RBL 64 FOUND EXFOLIATED.SDR FDEA202609181365Seat Track · corrodedMAIN CABIN SEAT TRACKS BTWN BS 1180 - 1200, RBL 58 HAD CORROSION. REMOVED & REPLACED THE SEAT TRACK BTWN BS 1180 - 1420, RBL 58.22 IAW DWG 657N3332, REV -, AND SRM 51-40-02-0G.SDR FDEA202609181364Seat Track · corrodedMAIN CABIN SEAT TRACKS BTW BS 1180 - 1200, RBL 45.5 HAD CORROSION. REMOVED & REPLACED THE SEAT TRACK BTWN BS 1180 - 1320, RBL 45.2 IAW DWG 146N5133, REV -, AND SRM 51-40-02-0G.SDR FDEA202609181363Seat Track · corrodedMAIN CABIN SEAT TRACKS BTW BS 980 - 1180, RBL 58 HAD CORROSION. REMOVED & REPLACED THE SEAT TRACK BTWN BS 900 - 1200, RBL 58.22 IAW DWG 657N3332, REV -, P.L 657N3332, REV C, & SRM 51-40-02-0G.SDR FDEA202609141336Elevator · no discrepancyEVALUATE EXISTING COMPOSITE REPAIR AT LH ELEVATOR UPPER SURFACE T/E, ON INBOARD AREA THIS ITEM HAS BEEN ACCOMPLISHED ON E.A.#: F-5520-T0388684, P1, TITLE: STABILIZER- ELEVATORS-LH ELEVATOR- EXISTING REPAIR- RSC TRACKING.SDR FDEA202509121697Lamp · failedR1 DOOR SLIDE LIGHT INOPERATIVE. AMM: 33-51-06-2-1 RELAMPED R1 DOOR SLIDE LIGHT, OP'S CHECKS GOOD. USED P/N 767 LIGHT BULB. AMM: 33-51-06-2-1 RELAMPED R1 DOOR SLIDE LIGHT, OP'S CHECKS GOOD.SDR FDEA202505300825Warning Message · false activationTRAILING EDGE FLAP DISAGREE DURING FLAP RETRACTION FROM 1 TO UP ON TAKEOFF. RAN CHECKLIST, FLAPS RETRACTED & LIGHTS WENT OUT. CONTINUED TO DAY & LANDED AT FLAPS 20 USING ALTERNATE EXTENSION. DECLARED AN EMERGENCY. C/W HIGH ENERGY STOP/HEAT DAMAGE CONDITIONSDR FDEA202303010357Skin · corrodedRIGHT WING PYLON UPPR FITTING #2 HOLE HAS CORROSION IN SKIN AT 3 O'CLOCK POSITION. 1) PERFORMED REPAIR OF SKIN ON R/H WING UPPER PYLON FITTING HOLE #2 IAW SRM 57-20- 01-2A REPAIR 8 & EA # F-5730-T0372934 A P1 WINGS - PLATES AND SKINS - RH WING, UPPER SKIN ASDR FDEA202303010356Beam · crackedFORWARD PIT STA 580 AT LBL 45.5 FLOOR BEAM UPPER CAP AFT FLANGE LWR SURFACE RADIUS IS CRACKED. REPAIRED STA 580 UPPER AFT FLANGE OF FLOOR BEAM SPLICE SEGMENT 657N4313-5 PER FEDEX DRAWING SR57-53-004. MAJOR REPAIR.SDR FDEA202209012135O-Ring · leakingR ENG OIL QUANTITY WENT TO 0 BY TOP OF CLIMB. PRESS WAS 180 INITIALLY. APPROXIMATELY 10 MINUTES LATER OIL PRESSURE BEGAN TO DECREASE, EVENTUALLY BEGAN TO FLUCTUATE SO WE DECLARED AN EMERGENCY AND DIVERTED TO MCI. OIL PRESSURE FURTHER DECREASED TO 90 PSISDR FDEA202103200733Frame Splice · crackedDURING ACCOMPLISHMENT OF ROTO PROBE AT BS 1640 S-14L PER EO 5310-E0344602 PT1. THE BOTTOM OUTBD FASTENER HOLE HAD A CRACK INDICATION IN THE FRAME. WORK ACCOMPLISHED ON EA F-5310-T0359979 TITLE: FUSELAGE - MAINFRAME - STA 1640 FRAME SPLICE REPAIR BETWEEN STSDR FDEA2020051870966Adc · faultyPDIS 786 34-14 4200 17MAY20 TYS FACT U LOGPAGES:3215525 REJECTED ON RUNWAY DUE TO NO AIRSPEED ON PILOT/LEFT SIDE. REJECTED AT 78 KTS FACT 17MAY20 12:59 TYS U REPLACED LH CADC AS PER 757 MM 34-12-01-4 AIR DATA COMPUTER - REMOVAL/INSTALLATISDR FDEA202001240214Charger · failedR1 DOOR EXTERIOR EMERGENCY LIGHT INOP. R1 INDOOR EMERGENCY LIGHT OPS NORMALLY. EMERGENCY BATTERY VOLTAGE GOOD, RELAMPED, NO HELP. NO POWER AT SOCKET. REF SSM 33-51-01 PG101 SH2, VERIFIED GOOD WIRING FROM BULB CONTACT AT L30 BACK TO CONNECTOR D66 AT EMERG LSDR FDEA201911263107Warning Message · false activationPDIS 786 36-11 3853 26NOV19 GSO OPEN U LOGPAGES:3166516 REJECTED T/O BECAUSE OF "LEFT ENG BLEED AIR" AT 80 KTS. CLEARED EICAS WITH QRH AND CHECK LIST. RAN LEFT AND RIGHT ENGINES TO 80 PERCENT N2 WITH BOTH ENGISDR FDEA201804211090Brake · damagedDURING WALKAROUND, FOUND THE NR 3 BRAKE BROKEN. REMOVED AND REPLACED THE NR 3 MAIN GEAR BRAKE ASSY IAW AMM 32-41-10-4. LEAK AND OPS CHECKED GOOD.SDR FDEA201504031147Inverter · failedDURING INITIAL PREFLIGHT, STANDBY INVERTER INDICATION SHOWED ON EICAS & WOULD NOT CLEAR. RAN FIM REF 24-33 FAULT TREE 802 FOUND STANDBY INVERTER SMOKING. INSPECTED IAW FIM 24-51-21-00 NO OTHER DAMAGE TO ANY COMPONENTS BESIDES INVERTER. R & R STANDBY INVERTESDR FDEA201412044062Slide · unserviceableR1 DOOR SLIDE PRESS BELOW LIMIT. RELEASED FOR SERVICE IAW MEL 52-11-01-B CATEGORY B. IDENTIFY L1 & R1 DOOR SLIDES INOPERATIVE OR MISSING. NO JUMP SEATERS ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT. R & R R1 DOOR SLIDE IAW 75 MM 25-66-01-4. OK TO CONTINUESDR FDEA201412024028Sensor · trippedRIGHT WING SLIDE DISPLAYED ON EICAS DURING APPROACH. DISAPPEARED AFTER LANDING. PRESSURIZATION WAS NORMAL. SMP CHECK TARGET ON RT WING SLIDE DOOR S10374 NO DEFECTS NOTED. CLEANED SAME, CHECKED PSEU FOUND SENSOR S10374 TRIPPED, RESET SAME. OPERATIONAL CHESDR FDEA201406061323Skin · damagedEXTERNAL LOWER SKIN BETWEEN BS 1306 - 1310, STRINGERS 29 - 30R HAD THREE NICKS WITH PREVIOUS BLEND. BLENDED IAW EA F-5330-T0308052.SDR FDEA201406041307Frame · puncturedMDC LT FRAME WEB AT STATION 395, BETWEEN STRINGER 11L TO 12L, HAS 2 AREAS WITH PUNCTURED HOLES. REPAIRED FRAME WEB AT STATION 395, BETWEEN STRINGER 11L TO 12L IAW EA F-5310-T0308591 PT 1. FUSELAGE MAINFRAME, FUSELAGE FRAME REPAIR STATION 395 BETWEEN STRINGERSDR FDEA201405231149Door Frame · crackedR2 DOOR FWD FRAME, UPPER HINGE CUT OUT EDGE NICKED. CRACK WAS FOUND OUT OF LIMITS IAW SRM 52-10-02, DETAIL IX, FIG. 101. LOCATED AND DRILLED AND INSTALLED REPAIR IAW SRM 52-10-02, FIG. 201, REPAIR 1. COMPLIED WITH EA F-5210-T0308334, PT. 1. MAJOR REPAISDR FDEA201405130993Spar · corrodedRT REAR SPAR AT IRSS 183 CORROSION NOTED. REPAIRED IAW EA F-5710-T0307459 P1.SDR FDEA201405130995Fitting · gougedIAW NR N00032 DURING OK TO INSTALL NR 1 PYLON FOUND MID SPAR FITTING INBD LUG BUSHING INNER BORE HAS DEEP SCORED MARKS, WING SIDE. REPAIRED IAW EA F-5740-T0307296 DATED APR 30,2014. TITLE, WINGS & ATTACH FITTINGS NR 1 ENG PYLON INBD WING MOUNTED SIDE LOAD SDR FDEA201405130994Frame Splice · corrodedAFT CARGO COMPARTMENT STATION 1540 STRINGER 24L FRAME SPLICE HAS CORROSION. REMOVED FRAME SPLICE STATION 1540 DUE TO ELONGATED HOLES, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET I. R & R FRAME SPLICE IAW SRM 51-40-05 & DWG 146N1042. REMOVED CORROSDR FDEA201405030932Frame Splice · corrodedHIDDEN DAMAGE FRAME SPLICE STA 1480 STRINGER 24L CORRODED. EVALUATED CORROSION IAW SRM 53-00-07 FIG 101 DETAIL 2, FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL IS .071 INCHES, MATERIAL REMOVED IS .021 INCHES & MATERIAL REMAINING IS .050 INCHES. FABRICATED SPSDR FDEA201405030931Frame Splice · corrodedHIDDEN DAMAGE FRAME SPLICE STA 1420, STRINGER 24L CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET 1. R & R FRAME SPLICE PN FX146N1012-3 IAW SRM 51-40-02 & DWG 146N1012 STA 1420, STRINGER 24L. MAJOR REPAIR.SDR FDEA201404230797Sill · corrodedAFT CARGO DOOR CUT OUT LOWER SILL CORRODED BS 1360 - 1460, STRINGER 27R.SDR FDEA201404140729Crease Beam · corrodedMAIN DECK CARGO LT CREASE BEAM OTBD ANGLE SPLICE HAS EDGE CORROSION AT BS 1462. SPLICE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 DETAIL III PG 103. REMOVED AND REPLACED SPLICE IAW SRM 51-40-02 AND DRAWING 146N5590. MAJOR REPAIR.SDR FDEA201404120718Floorbeam · corrodedFLOORBEAM AT FS 1661 BL 0 HAS CORROSION ON TOP CHORD. R & R CORRODED FLOORBEAM IAW SRM 51-40-02 & DWG 146N5110.SDR FDEA201404110717Shear Tie · crackedMDC RT FRAME SHEAR TIE INNER RADIUS, UPPER AREA AT STATION 1160 BETWEEN STRINGER 10R - 11R HAS A CRACK. REMOVED CRACKED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE PN FX144N1126-10 & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02. SHEAR TIE FABRICATED OSDR FDEA201404100704Web · corrodedMAIN DECK, BS 1380 - 1400 STRINGER 17R UPPER SURFACE WEB CORRODED. R & R WEB IAW SRM 51-40-02 & DWG 146N5590.SDR FDEA201404100705Rib · crackedRIGHT WING INBD FLAP INBD EDGE RIB IS CRACKED. FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01. REPAIRED IAW SRM 51-70-04 PAR 4G. MAJOR REPAIR.SDR FDEA201404020640Frame · misrepairedAFT CARGO, FRAME REPAIR AT BS 1440 S24L-27RFRAME MISINSTALLED. R & R FRAME IAW SRM 51-40-02 & DWG 146N1013.SDR FDEA201403290599Crease Beam · corrodedMAIN CARGO DECK BETWEEN BS 940 - 960, RT CREASE BEAM CORRODED. R & R IAW SRM 53-40-13, SRM 51-40-02, & DWG 144N5150.SDR FDEA201403220545Floor Support · damagedBS 377.7 - 395 RBL 24.75 FLOOR SUPPORT DOUBLE DRILLED. R & R FLOOR SUPPORT IAW DWG 141N5130 & SRM 51-40-02.SDR FDEA201403220544Floorbeam · corrodedFWD CABIN FLOORBEAM AT STATION 365 BL 0 - RBL 62 UPPER TEE HAS CORROSION. REPAIRED FLOORBEAM RBL 70 TO LBL 16 IAW SRM 53-00-51 REPAIR 8.SDR FDEA201403180520Floorbeam · corrodedMAIN DECK CARGO FLOORBEAM AT BS 377 HAS AREAS WITH NICKS, SCRATCHES & CORROSION. REPAIRED FLOORBEAM AT STATION 377 LBL 35 - 70 IAW SRM 53-00-51, FIG 201, DET II, SHEET NR 4, REPAIR NR 8. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DSDR FDEA201403110489Floorbeam · corrodedFLOORBEAM AT FS 1640 RBL-LBL 65, HAS AREAS OF CORROSION ON TOP TEE. REMOVED CORROSION ON FLOORBEAM. FOUND OUT OF LIMITS, REMOVED FLOORBEAM , FABRICATED NEW FLOORBEAM. INSTALLED FLOORBEAM IAW DWG 146N5136 & SRM 51-40-02. MAJOR REPAIR.SDR FDEA201403040443Floorbeam · corrodedMAIN DECK CARGO FLOORBEAM BS 333.45, BETWEEN LBL 45-58, UPPER TEE CORRODED. REMOVED CORROSION IAW SRM51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET6. R & R FLOORBEAM IAW SRM 51-40-02.
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