N788FD
Service difficulty reports · 60
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 = 'N788FD' 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 = 'N788FD' 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 FDEA202608041082Battery · failedBETWEEN 16-18000 FT GOT LT, RT, & CENTER IRS DC FAILED. TRIED STARTING APU TO VERIFY HOT BATTERY BUS STILL WORKING. WHEN APU REACHED SPEED GOT EICAS APU FUEL VALVE & RT FUEL SPAR VALVE. MAIN BATTERY CHARGER MSG ILLUMINATED. BTWN IRU FAILS & EICAS MGS NOTICESDR FDEA202510242090Skin · dentedRH HORIZONTAL STAB FRONT SPAR UPPER SURFACE DENT STA 159.248 APPROX FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 159.248 OUT OF LIMITS DIM A= 1.500" Y=0.054" A/Y=27.77 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I, NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4SDR FDEA202510242089Skin · dentedRH HORIZONTAL STAB FRONT SPAR UPPER SURFACE HAS A DENT (STA 86.600) FOUND DENT AT UPPER SKIN RH HORIZONTAL STA 86.600, OUT OF LIMITS DIM A=1.500", Y=0.069", A/Y=21.73 AND REPAIRED IAW B757 SRM 55-10-01-1A TABLE I NOTE I AND IAW B757 SRM 51-70-10- 2R REP 4SDR FDEA202510232076Skin · corrodedAFT POTABLE WATER SERVICE DOOR PAN POSSIBLE CORROSION STA 1681 TO STA1701 BTW STRINGERS 26R TO STR 29R COMPLIED WITH FEDEX EA F-5330-T0385436 P1 TITLE: FUSELAGE-PLATES AND SKINS-AFT LAV PAN CUT OUT SKIN CORROSION REPAIR. MAJOR REPAIR.SDR FDEA202504250652Reservoir · emptyL1 DOOR EMERGENCY POWER ASSIST RESERVOIR GAUGE SHOWS EMPTY. REMOVED AND REPLACE DTHE L1 DOOR EMERGENCY POWER RESERVOIR IN REF TO AMM 52-11-30-4. A/C OK FOR SERVICE.SDR FDEA202312101929Frame · crackedCRACK FOUND AT FRAME 1640 RIGHT HAND SIDE COMPLIED WITH ALL STEPS 1-16 OF E.A. TF-5310-T0377033 P1 AND COMPLETED "FUSELAGE- MAINFRAME-STA 1640 FRAME, SPLICE REPAIR BETWEEN STRINGER I-9F AND S-20R-EO F-5310- E0367020 A CRACK INDICATION REPAIR-PARTIAL FRAME RESDR FDEA202312051917Floorboard · damagedZONE 220 COURIER FLOORBOARD 221BF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 221BF ON VTMAE TRAVELER #T23/1718651 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202312051915Floorboard · damagedZONE 220 COURIER FLOORBOARD 221MBF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221MBF ON VTMAE TRAVELER # T23/1718650 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIRSDR FDEA202312051914Floorboard · damagedZONE 220 FLOORBOARD 221AF DAMAGED FABRICATED ZONE 220 FLOORBOARD 221AF ON VTMAE TRAVELER # T23/1718653 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIRSDR FDEA202312051913Floorboard · damagedZONE 220 COURIER FLOORBOARD 222AF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222AF ON VTMAE TRAVELER # T23/1718647 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202312051912Floorboard · damagedZONE 220 FLOORBOARD 222MAF DAMAGED FABRICATED ZONE 220 FLOORBOARD 222MAF ON VTMAE TRAVELER # T23/1718633 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIRSDR FDEA202312051911Floorboard · damagedZONE 220 COURIER FLOORBOARD 222BF DAMAGED FABRICATED ZONE 220 COURIER FLOORBOARD 222BF ON VTMAE TRAVELER # T23/1718643 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202311051828Battery · failedL/H SLIDE LIGHT DOES NOT TURN ON. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK FOR L/H SLIDE LIGHT, REF. AMM 33-51-07-2. L/H SLIDE LIGHT OPS CHECK NORMAL, REF. SAME. OK TO CONTINUE.SDR FDEA202311031825Unknown · unknownPDIS 788 26-12 6589 03NOV23 BHM FACT U DESCENDING THROUGH 12000 MSL RECEIVED MAIN CARGO FIRE EICAS MESSAGE AND INDICATIONS. INDICATIONS WENT AWAY WHILE RUNNING QRH. AFTER LANDING RECEIVED EQUIPT OVERHEAT. EMERGENCY DECLARED. ***EMERGENCY DECLSDR FDEA202206031370Light · inoperativeRT DOOR SLIDE EMERGENCY LIGHT INOP. FACT 04JUN22 18:56 GJT REF WRI 25-60/5466. REMOVED AND REPLACED R1 DOOR AND SLIDE EMERGENCY LIGHT BATTERY HOLDER ASSY AND SDR FDEA202206031371Light · inoperativeRT ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOP REMOVED AND REPLACED R1 DOOR AND SLIDE EMERGENCY LIGHT BATTERY HOLDER ASSY AND BATTERY CHARGER PER AMM 33-51-07-2. SYSTEM OPS NORM.SDR FDEA202112103081None · noneSTRINGER SPLICE AT STA 1464 , STR29L , REQUIRES REPLACEMENT ACCOMPLISHED FEDEX EA# F-5310-T0365675-P1 ;FUSELAGE -,MAIN FRAME - STRINGER ,STA 1430-1460 , S29L,SPLICE REPAIR AND STA1460 - STA1489 STRINGER AND STRINGER SPLICE REPAIR IAW B757-200 SRM 53-00-0SDR FDEA202112103080Frame · corrodedAFT CARGO LOWER FRAME CORRODED AT STA 1460 BL0 TO RBL 4.5 ACCOMPLISHED FEDEX EA # F-5310-T0365644-P1 , FUSELAGE MAIN FRAME , S28L TO S28R SPLICE REPAIRSDR FDEA202111302954Bracket · crackedEMPENNAGE INTERIOR ABOVE CENTER SECTIONAPU INLET DUCT LOWER SUPPORT BRACKET CRACKED AT BS1864 REMOVED BRACKET , INSTALLED SERVICEABLE BRACKET IAW B757 SRM 51-40-02-0GSDR FDEA202111292948Bracket · crackedSUPPORT BRACKET AT STA 1864 FOR APU INLET DUCT ,CRACKED REMOVED AND REPLACED BRACKET PER BOEING DWG # 353N1043 REV A AND BOEING DWG # 353N1001 REV FSDR FDEA202111292947Fitting · damagedR/H ELEVATOR TIP FITTING HAS ELONGATED HOLES UNDER STATIC WICK BASE REPAIRED PER FEDEX EA #F-5520-T0365567-P1SDR FDEA202111242931Panel · delaminatedR/W I/B L/E PANEL 611KT HAS COMPOSITE DAMAGE ON THE INNER SURFACE@ CORNER REPAIRED PER FEDEX EA # F-5730-T0365459-P1SDR FDEA202111232926Slat · delaminated#6 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED SLAT PER B757 AMM 27-81-01-4SDR FDEA202111222918Door · unknownR2 DOOR UPPER HINGE CUT OUT REPAIR HAS INCORRECT AND MISSING FASTENERS INSTALLED IAW B757 SRM 52-10-02-2R REMOVED AND REPLACED FASTENERS FOR R2 DOOR UPPER HINGE CUT OUT REPAIR IAW B757-200 SRM 52- 10-02-2R, FIG 201, REPAIR 1, DETAIL IIISDR FDEA202111202910None · none#7 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED #7 SLAT IAW B757 AMM 27-81-02-4 OPS CHECK GOOD.SDR FDEA202111202909None · none#8 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED AND REPLACED #8 SLAT AND OPS TEST IAWB757 AMM 27-81-02-4SDR FDEA202111202908None · none#4 SLAT SHOWS SKIN TO CORE DISBONDING REMOVED AND REPLACED #4 SLAT AND OPS TEST PER B757 AMM 27-81-02-4SDR FDEA202111192904Frame · gougedEMPENNAGE INTERIOR BELOW CENTER SECTION BILGE AREA FRAME HAS A GOUGE AT BS 1844 RBL 5 REPAIRED PER B757 SRM 51-70-11-OGSDR FDEA202111182891None · corrodedR/H ELEVATOR TIP UPPER AND LOWER PLATES ARE CORRODED FABRICATED NEW PLATES PER BOEING DWG # 183N2007 REV ASDR FDEA202111112824None · cracked#1 ENG I/B SIDE CORE COWL SPRING SEAL IS CRACKED APPROX 12"AFT OF THE FWD EDGE REMOVED AND REPLACED PER BOEING DWG # 311N3570 REV YSDR FDEA202111092802None · noneMAIN CABIN RH SIDE AT THE R4 DOOR ENTRANCE STA 1660 UPPER SURFACE OF THE DOOR SILL WEB IS CORRODED REMOVED DAMAGE FROM UPPER SURFACE OF DOOR SILL WEB, STA 1660 RBL 52, ORIGINAL MATERIAL .071, MAT REMOVED .O07", MATERIAL REMAINING .064" , FOUND TO BE WITHINSDR FDEA202111092801Deflector · cracked#1 ENG I/B CORE COWL LOWER LONGERON FWD EDGE SUBSTRUCTURE IS CRACKED REMOVED AND REPLACED DEFLECTOR PER BAC DWG # 314N3210 REV H AND B757 SRM 51-40-02-0GSDR FDEA202002140341Lamp · inoperativeL1 DOOR EXTERIOR EMER EXIT LIGHT INOP RELAMPED L1 DOOR EXT EMER EXIT LIGHT (SLIDE LIGHT) USING LAMP P/N 767 LIGHT CHECKS GOOD. REF B757 AMM 33-51-06-2-1. OK FOR SERVICESDR FDEA2019122083258Strap · dentedMAIN EQUIPMENT CENTER CEILING AREA,, MAIN FLOOR STRUCTURE ATTACH STABILIZER STRAP HAS A CRACK AT FASTENER HOLE ABOUT 1.5" LONG, BS.480 RBL. 24.75 CUT DAMAGED AT STABILIZER STRAP IAW B757 SRM 51-10-02-0G AND SRM 53-00-51-2R FIG 201 DETAILV REP 12, FABSDR FDEA201912133241Stringer Splice · corrodedLOWER FUSELAGE SKIN BULGE AT BS 1464 STR29L APPROX. SUSPECT OF CORROSION EVALUATED AREA AT LWR FUSE SKIN FOUND STR SPLICE CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW STRINGER SPLICE AS PER SRM 51-40-02-0G, 51-10-02-0G AND DWG 146N3820 REV CSDR FDEA2019121323230Angle · corrodedUPON REMOVAL OF APU INTAKE DUCT FOUND ANGLE CORRODED APPROX STA 1787 TO 1800 RBL6. FOUND ANGLE AT APU INTAKE DUCT TO BE 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-80-15. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG 148N3152 REV -.SDR FDEA2019100312380Solenoid Valve · leakingRIGHT HYD QTY EICAS MESSAGE INFLIGHT. COMPLIED WITH QRH. FOUND LEAK AT RT SYSTEM APCS ELECTROHYDRAULIC SOLENOID VALVE WHERE IT MATES TO THE SOLENOID. REMOVED AND REPLACED METAL GASKET ON SOLENOID VALVE IAW MM 22-12-02-2. PERFORMED OPS AND LEAK CHECKS. OPSSDR FDEA2018122103564Liner · out of adjustPDIS 788 25-60 2763 20DEC18 MEM FACT U LOGPAGES:2992755 R FWD DOOR ARMED PANEL DOSN'T EXTEND FACT 20DEC18 06:30 MEM U ADJUSTED R-1 DOOR LINING- DOOR ARMED PANEL(KNUCKLE KNOCKER) OPS CHKS GOOD- REF: B757 M/M 52-11-02-4SDR FDEA201804231094Socket · shortedRIGHT EXTERIOR EMERGENCY LIGHT FOR R1 DOOR INOPERATIVE. REMOVED LIGHT SOCKET AND REFLECTOR FROM OUTSIDE OF AIRCRAFT AS PER SB 33-0012 IAW AMM 33-51-06-2-1. TROUBLESHOT IAW WDM 33-51-12, PG 902. FOUND GOOD POWER AND GROUND AT LIGHT ASSY L30. FOUND THAT TSDR FDEA201707151969Power Supply · bentRIGHT EXTERNAL EMERGENCY SLIDE LIGHT FAILED AN OPS TEST. REPLACED THE POWER SUPPLY IAW MM 33-51-07-2, OPS CHECKED OK.SDR FDEA201602260691Torque Tube · looseAFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 1 TO FLAPS 0, HAD EICAS MESSAGE, LE FLAP ASYM, & AMBER LIGHT LE. RETURNED TO LAND IAW QRH FAULT CODE FRM 27 90 24 00. INSTALLED TORQUE TUBE COUPLER AND OPS CHECKED LEADING EDGE SLAT SYSTEM IN REF 27-81-00-5 ANSDR FDEA201512073929Skin · chafedPANEL 655AR EXTERNAL SKIN HAS CHAFED. REPAIRED IAW EA F5750-T0320958. MAJOR REPAIR.SDR FDEA201511253777Skin · dentedREWORK OF NR N00207, VERTICAL STAB LT SIDE AUXILIARY PANEL HAS DENT, 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM, DUE TO PER NOTED SRM. A VISUAL & NDT INSPECTION OF DAMAGED AREA FOR DISBONDS, DELAMINATION, IS REQUIRED PRIOR TO APPLYING REPAIR. THIS WAS NOT DOCSDR FDEA201511233763Flap · crackedDURING SURVEILLANCE CHECK, A CRACK WAS NOTED, APPROX 1/2", ON LT WING INBD MAIN FLAP, MID TE. REPAIRED CRACK ON LT WING INBD MAIN FLAP, MID TE, LOCATED AT TE, 111.5" OTBD OF MF STATION 74.0. PN 113N2003-47H, SN 000539, FINAL REPAIR 7.5" X 3.25". COMPLIED WISDR FDEA201511173669Skin Panel · delaminatedVERTICAL STAB RT SIDE, AUXILIARY PANEL HAS DELAMINATION, 26" FROM AUXILIARY SPAR & 120" FROM BOTTOM. REMOVED DAMAGED PANEL ASSEMBLY & INSTALLED NEW PANEL ASSEMBLY PN 175N2001-4, IAW SRM 51-40-02 & WG 175N2001, SHEET 1 AT RT SIDE VERTICAL STAB. MAJOR REPAIR.SDR FDEA201511103547Skin · corrodedAFTER PREPARING THE REPAIR AREA ON THE VERTICAL STAB AUXILIARY PANEL DENT, FOUND A DISBONDED AREA OF APPROX 13" X 13" DUE TO CORROSION ON THE INNER SKIN. THIS DISBONDED AREA IS APPROX 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM. REPAIRED LT VERTICAL STAB AUXILSDR FDEA201510193278Skin · dentedFUSELAGE EXTERIOR SKIN HAS DENT WITH ASSOCIATED SCRATCH, BELOW STRINGER 24R & FWD OF BS 1768. NOTED DURING EVALUATION OF NR N00049, ACCOMPLISHED EA F-5330-T0320261. FUSELAGE SKIN CREASE, GOUGE & DEEP SCRATCH DAMAGES, BETWEEN BS 1763 & BS 1773, STRINGER 24R TSDR FDEA201510133188Skin · dentedFUSELAGE EXT SKIN DENT BETWEEN STATION 1380 - 1400, JUST BELOW AFT CARGO DOOR CUT OUT. ACCOMPLISHED EA F-5330-T0320147. FUSELAGE SKIN REPAIR BETWEEN BS 1380 - 1400 & NR 2 CARGO DOORWAY LOWER MAIN SILL & STRINGER 29R. THIS IS A CAT B REPAIR, MAJOR REPAIR.SDR FDEA201510093154Skin · corrodedPITTING CORROSION RUNNING UP UNDER LAP SEAM AT STRINGER 19L, BS 753 - 780. ACCOMPLISHED EA F-5330-T0320609. CATEGORY B REPAIR, MAJOR REPAIR.SDR FDEA201510073109Skin · puncturedLEFT WING INBD FLAP EXTERNAL UPPER SKIN HAS PUNCTURE AT 3 LOCATIONS. REPAIRED LT WING AT 3 LOCATIONS IAW SRM 51-70-06-0G. REF EA F-5750-T0320431 ISSUED FOR TRACKING. CATEGORY A REPAIR MAJOR REPAIR.
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