N781FD
Service difficulty reports · 67
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 = 'N781FD' 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 = 'N781FD' 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 FDEA202511172188Slide · low pressureR1 DOOR SLIDE PRESSURE BELOW GREEN BAND. REMOVED AND REPLACED R-1 DOOR ESCAPE SLIDE ASSY. IAW AMM 25-66-01-4 OK FOR SERVICE.SDR FDEA202502200254Warning Light · malfunctionedDURING POST FLIGHT FOUND RIGHT ENTRY DOOR DISARMED AND OPENED SLIDE LIGHT REMAINS ILLUMINATED. OPERATED R1 DOOR SLIDE ARMING LEVER SEVERAL TIMES. R1 DOOR SLIDE LIGHT OPERATED NORMAL PER MM. A/C OK FOR SERVICE.SDR FDEA202502150234Indication Sys · malfunctionedPER CREW RIGHT ENTRY DOOR DISARMED AND OPENED SLIDE LIGHT REMAINS ILLUMINATED. WORKED WRI IN CONJUCTION WITH TSI 52-10/6355 COMPLETING THE REQUIRED STEP ON TSI LUBE EMERGENCY MECHANISM OPS CHECK DOOR SEVERAL TIMES SLIDE LIGHT ARMED AND DISARMED AS DESCRIBED SDR FDEA202502070193Girt Bar · fodR-1 DOOR "SLIDE" LIGHT ABOVE R-1 DOOR STAYS ILLUMINATED WITH DOOR IN DISARM POSITION. FACT 08FEB25 03:10 ORD FOUND R1 DOOR GIRT BAR AND FLOOR FITTINGS WITH SOME DEBRIS, CLEANED PROX SENSOR AND FLOOR FITTING AND LUBRICATED ACCORDINGLY. REF. AMM 12-21-1SDR FDEA202412271844Battery Pack · no testTHROUGHOUT MAINTANENCE PREFLIGHT ROUTINE FOR LAYOVER'S FOUND EMERGENCY LIGHTS FORWARD TEST SYS 1, INOP. REMOVED AND REPLACED BATTERY PACK ASSY, PERFORMED SYS OPS CHECK, ALL CHECKS NORMAL, ALL IAW B757-200 AMM CH 33-51-07-2.SDR FDEA202412071779Wedge · damagedRH WING, MAIN FLAP TRAILING EDGE WEDGE AT THE OUTBD END OF THE EXTENSION HAS COMPOSITE DAMAGE AND DENT. REMOVED RH WING MAIN FLAP TRAILING EDGE WEDGE AT THE OUTBD IAW SRM 51-40-02. REPAIRED FLAP WEDGE IAW SRM 51-70-10-2R REPAIR 4. REINSTALLED RH WING MAIN SDR FDEA202412031770Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 252MTF HAS SEVERAL INSERTS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MTF ON VTMAE TRAVELER #T24/1787480 IAW DWG 11864182 REVISION D MAJOR REPAIR.SDR FDEA202412031771Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANELS 251MSF INSERTS TORN. FABRICATED ZONE 250 FLOORBOARD PANEL 251MSF ON VTMAE TRAVELER #T24/1787474 IAW DWG 11864182 REVISION D MAJOR REPAIRSDR FDEA202412031769Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 241MDF DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MDF ON VTMAE TRAVELER #T24/1787472 IAW DWG 11863182 REVISION C MAJOR REPAIRSDR FDEA202412031768Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 251MTF HAS SEVERAL INSERTS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MTF ON VTMAE TRAVELER #T24/1787475 IAW DWG 1186182 REVISION D MAJOR REPAIRSDR FDEA202412031767Shear Tie · corrodedDOT 139/41 AFT CARGO COMP. FRAME CLIP AND SKIN WITH CORROSION STA 1460 STRG 29L-29R. REWORK ON FRAMECLIP (SHEAR TIE) AND SKIN @ STA 1460 BTWN STR 29L TO 29R: NO CORROSION WAS FOUND ON FRAME AND SKIN. FOUND 2 EA SHEAR-TIES CORROSION OUT OF LIMIT IAW SRM 53-SDR FDEA202411271745Floor Panel · damagedFLOOR PANEL 222MAF HAS FIBER DAMAGED CRACKED AND PEELED DUE TO REMOVAL OF TAPE. FABRICATED ZONE 220 FLOOR PANEL 222MAF ON VTMAE TRAVELER # T24/1786765 IAW DWG 141N5370 REV. CY MAJOR REPAIRSDR FDEA202411271749Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 252MFF DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MFF ON VTMAE TRAVELER # T24/1787479 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202411271748Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 241MNF DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MNF ON VTMAE TRAVELER # T24/1787473 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202411271747Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 232MFF BROKEN FABRICATED ZONE 230 FLOORBOARD PANEL 232MFF ON VTMAE TRAVELER #T24/1787469 IAW DWG 11862181 REV L MAJOR REPAIRSDR FDEA202411271746Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 232MWF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MWF ON VTMAE TRAVELER # T24/1787471 IAW DWG 11862182 REV. H, MAJOR REPAIRSDR FDEA202305090860Skin · damagedJUST AFT OF THE PRESSURE BULKHEAD, STA 1845 RBL 10 SKIN IS PUNCTURED. REPAIRED FUSELAGE SKIN AT STA 1845 RBL 10 JUST AFT OF PRESSURE BULKHEAD IAW EA F-5330- T0373981. THIS IS A MAJOR REPAIRSDR FDEA202210072514Wedge · delaminated#6 SLAT REQUIRES REPLACEMENT DUE TO T/E WEDGE DELAMINATION FOUND ON FEDEX E.O F- 5750-E0336930-P6 REPAIRED #6 SLAT T/E WEDGE IAW FEDEX EA# F-5750-T0370813-P1 - WINGS - FLIGHT SURFACES - #6 SLAT, TRAILING EDGE WEDGE, ISS 193, DELAMINATIONSDR FDEA202210062499Angle · cracked**PARTS RACK ITEM** R/W FLAP FAIRIG 672HB HAS A BENT FORWARD R/H CLOSEOUT ANGLE REPAIRED R/W, I/B FLAP FAIRING 672HB FORWARD R/H CLOSEOUT ANGLE IAW FEDEX EA # F-5720-T0370931- P1, TITLED "WING - SECONDARY WING STRCT - RH INBD FLAO FAIRING, 672HB, INBD AND OUTSDR FDEA202210042463Floor Support · corrodedMAIN CABIN, FLOOR SUPPORT AT STA 1640 TO 1660, LBL 55 HAS CORROSION AROUND NUT PLATES. BLENDED CORRODED AREAS IAW B757 SRM 51-10-02-0G. ORIGINAL MATERIAL THICKNESS OF .071" IAW B757 SRM 53-60-13-0I, FIG. 1, DETAIL VII. REMOVED .003" FOR REMAINING THICKNESSSDR FDEA202210042461Fitting · noneACCOMPLISH FEDEX E.A. F-5310-T0357573-P2 REQUIRED, REPLACEMENT OF THE L4 DOOR LOWER HINGE SUPPORT FITTING P/N 146N8762-13. REMOVED AND REPLACED THE L-4 DOOR LOWER HINGE SUPPORT FITTING IAW BAC DWG 146N8739, REV. K AND FEDEX E.A. F-5310-T0357573-P2, TITLE: SDR FDEA202210012439Floor Panel · crackedMAIN CABIN, FLOOR PANEL 251MVF IS CRACKED AND HAS AREAS OF DISBOND ON LOWER SIDE REPAIRED FLOOR PANEL 251MVF IAW BAC D6-55191, REV. C, AND B757 SRM 53-00-50-2R, REPAIR 2, FIG. 201, SHEET 1 AND PARA. 4.A., AND VT MAE DWG 11864182, REV. ASDR FDEA202209302420Shear Web · corrodedMAIN CABIN, AFT FLOOR, SHEAR WEB HAS SEVERAL, AREAS OF CORROSION, STA 1681 TO 1720, LBL 56 TO RBL 56 REPAIRED THE AFT MAIN CABIN SHEAR WEB (DECK PLATE), STA 1681 TO 1720, LBL 56 TO RBL 56, IAW FEDEX E.A. F-5310-T0370865-P1, RELEASE DATE: 29 SEPTEMBER, 2022SDR FDEA202209302418None · noneFOUND EXISTING COMPOSITE REPAIR LOCATED ON R/WING OUTBOARD AFT FLAP, LOWER SURFACE. REPAIR INSTALLED ON REMOVABLE STRUCTURAL COMPONENT AND REQUIRES TRACKING OF COMPONENT, NOT EXISTING REPAIR. EXISTING COMPOSITE REPAIR LOCATED ON R/WING OUTBOARD AFT FLAP, SDR FDEA202209292396Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251MWF HAS AREA OF DISBON ON THE BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 251MWF IAW B757 SRM 53-00-50-1A REPAIR 2, BAC D6-55191 REV: CSDR FDEA202209292395Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 252MVF HAS AREAS OF DISBOND ON BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5SDR FDEA202209292394Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 252MVF HAS DELAMINATION ON TOP SIDE REPAIRED DELAMINATION ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5SDR FDEA202209292393Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 52MVF HAS AREAS OF DISBONDED ON THE BOTTOM SIDE REPAIRED DISBOND ON MAIN CABIN FLOOR PANEL 252MVF IAW B757 SRM 53-00-50-1A TABLE 2, BAC D6-55191 REV: C PARA 8.4.3, 8.4.6 FIG 14, 15, 2 TABLE 5SDR FDEA202209262371Plate · crackedRIGHT WING T/E REAR SPAR LOWER CORD WIGGLE PLATE CRACK AT WSTA330 APPROX STREAMER ATTACHED CRACKED WIGGLE PLATE AT WS 330 RIGHT WING T/E REAR SPAR LOWER CHORD WAS REMOVED AS REQ IAW FEDEX B757 SRM 51-40-02-0G AND REPLACED WITH NEW WIGGLE PLATE P/N 113N16SDR FDEA202203120485None · crackedDURING POST FLIGHT, FOUND THE LEFT OB TE FLAP SKIN CRACKED APPROX 3" THROUGH A RIVET. REF SRM 57-53-01-01 SHEET 8, LOWER AFT, MOST OB LOWER SKIN PAINTED FABRICATED DOUBLER ON LEFT OB TE FLAP REF. AMM 51-21-07.SDR FDEA202010222603Skin · crackedAIRCRAFT DAMAGED STA 1620 UNDER STR 17L DENT IS L=1.75" W=1". C/W EA NR F-5330-T0357572 P1 TITLE: FUSELAGE-PLATES AND SKIN-FUSELAGES SKIN REPAIR NEAR STA 1620 BETWEEN STRINGERS S-16L AND S-18L.SDR FDEA202010102459Frame · crackedLT BS 1640 FRAME LEWER INBOARD HOLE HAS (2) INDICATIONS OF CRACKS AT 3 O`CLOCK AND 9 O`CLOCK POSITIONS. C/W FEDEX EA NR F-5310-T 0357202 P1 TITLE: FUSELAGE-MAINFRAME-STA 1640 SPLICE REPAIR BETWEEN STRINGER I-9 F AND S-20L.SDR FDEA202010062423Strap · crackedCOURIER AREA STA 350 LBL 25 LOWER SUPPORT STRAP LOWER SURFACE IS CRACKED. REMOVED EXISTING STABILIZATION STRAP REPAIR BETWEEN STA 345 TO STA 377 LBL 25, IAW B757 SRM 51-40-02-OG. FABRICATED AND INSTALLED NEW STABILIZATION STRAP REPAIR AND FILLER SECTION, IAWSDR FDEA202010062422Strap · crackedUPON REMOVE LOWER STRAP (STABILIZATION) FOUND INTERCOSTAL PREVIOUS REPAIR CRACKED BETWEEN BS 350 TO BS 365.5 ON LBL 24.750. REMOVED INTERCOSTAL BETWEEN STA 350 TO STA 365.5 LBL 24.75, IAW B 757 SRM 51-40-02-OG. FABRICATED AND INSTALLED NEW INTERCOSTAL, IAW BSDR FDEA202010052420Floorbeam · damagedMAIN CABIN FLOOR PANEL SUPPORT HAS PULLED RIVETS THRU UPPER SHIM AT BS 1055 LBL 24.75 TO 45.5. REMOVED AND FABRICATED, INSTALLED NEW FLOOR SUPPORT (PLATE) AT STA 1055 BETWEEN LBL 24.75-LBL 45.5, IAW B 757 SRM 51-40-02-OG, 51-40-05-OG AND BOEING DWG 144N5070 RSDR FDEA202010052419Floorbeam · crackedMAIN DECK STA 900 BETWEEN LBL 24.75-LBL 44.5 FLOOR SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT (PLATE) STA 900 BETWEEN LBL 24.75-LBL 44.5, IAW B 757 SRM 51-40-02-OG, 51-40-05-OG AND BOEING DWG 144N5070 REV W AND REV B.SDR FDEA202010042414Crease Beam · corrodedMAIN DECK BETWEEN STA 1020-1040 RT CREASE BEAM CORRODED. REMOVED CORROSION AT CREASE BEAM STA 1020-1040 RT SIDE, IAW B 757 SRM 51-10-02-OG, ORIGINAL MAT .070", MINIMUN REMAINING .022". MAT LOSS .048" FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG SDR FDEA202010012384Frame · crackedHFEC SURFACE INDICATION OF DEFECT(CRACK)NOTED AND MARKED IN RED SHARPIE ON FUSELAGE MAIN FRAME 1640RIGHT HAND SIDE INNER CHORD FWD RETURN FLANGE RADIUS INLINE WITH STRINGER 14R. INDICATION RUNS FROM EDGE OF FLANGE UNDER STRAP TO SINGLE FASTENER ATTACHED SDR FDEA2019042650929Unknown · vibrationON APPROACH AT 150 FT A STRANGE /MODERATE ELEVATOR RYTHMIC VIBRATION, ALMOST NOT CONTROTABLE ACCURED, LASTED ALL THE WAY TO LANDING FLAP 25 137 KTS WIND 190 AT 12 GUST 18. PERFORMED BITE ON BOTH SAM COMPUTERS, NO FAULTS FOUND, PERFORMED A BITE CHECKS ALLSDR FDEA201903020527Fitting · obstructedAFTER LANDING FO NOTED LEFT DOOR SLIDE ARM LIGHT FLASHING INTERMITTANTLY. REF AMM 25-66-00 CLEANED DEBRIS FROM GIRT BAR FLOOR FITTINGS. OPERATIONAL CHECKS GOOD.SDR FDEA201809242668Door Frame · gougedLOWER FUSELAGE FWD ACCY COMPT ACCESS DOOR CUTOUT FWD FRAME, AND LATCH PLATE HAS GOUGES AT BS 231.25. EVALUATED DAMAGED AREA ON FRAME AT BS 231.25, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-2R AND EVALUATED LATCH PLATE AREA WITH NO DEFECT NOTED ONLY PAINT DAMSDR FDEA2018091872560Seat Track · crackedMAIN CABIN SEAT TRACK CROWN BETWEEN STA 500-550 RBL 24.75 CRACKED. EVALUATED DAMAGE AREA ON SEAT TRACK FROM STA 484 AND STA 546 TO BE FOUND OUT OF LIMITS IAW SRM 53-00-52-1A DETAIL II & III FIG 101. CUT-OUT DAMAGED AREA SEAT TRACK STA 470 TO STA 570 RBL 24.75 SDR FDEA201809112440Collar · defectiveL1 DOOR HOLD OPEN LOCK INOP. DOOR CLOSES NORMAL. REPLACED L1 DOOR HOLD-OPEN LOCK COLLAR PER AMM 52-11-08-8.SDR FDEA201612154470Warning Light · false activationDURING APPROACH, MOMENTARY LT WING SLIDE EICAS ALERT. OPS CHECKED DOOR IAW AMM 52-71-00-5. NO FAULTS NOTEDSDR FDEA201609093161Access Panel · damagedRIGHT WING, TANK DRY BAY ACCESS DOOR ASSY PANEL BROKEN, OTBD WS 258.5, PN 112N8003-2 COMPLIED WITH EA F-5720-T0326684, DATED SEPT 02,2016. FUEL SYSTEMS, CELLS, TANKS, VENTS, RT WING TANK ACCESS DOOR ASSY CAT-B, MAJOR REPAIR.SDR FDEA201609093160Spar · corrodedRIGHT WING REAR SPAR AT IRSS 183, CORROSION ON AFT SPAR, FOUND ON REMOVAL OF BONDING JUMPER REPLACEMENT, THE LOWER BONDING POINT. ACCOMPLISHED ON EA F-5710-T0326498, DATED AUG 02,2016. WINGS BASIC WING STRUCTURE, RT REAR SPAR WEB CORROSION AT IRSS 183, REF: FSDR FDEA201609063122Panel · delaminatedDELAMINATION ON VERTICAL STABILIZER, LEFT SIDE ADJACENT TO L/E PANEL 321CL. DELAMINATION ON VERTICAL STABILIZER PANEL, LT SIDE FOUND TO BE OUT OF LIMITS IAW SRM 55-30-01-1A, FIG 101, NOTE K AND SRM 51-70-10-2R. R & R PANEL 175N2001-3 WITH O/H PANEL 175N2001-SDR FDEA201608232957Shear Tie · corrodedAFT CARGO BS 1620, ONE SHEAR TIE CORRODED, STRINGER 29R. REMOVED THE CORROSION IAW SRM 51-10-02-0G, FOUND NO ALLOWABLE DAMAGE IN SRM. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, MAJOR REPAIR.SDR FDEA201608192942Stringer · corrodedMCD BS 438, STG CORRODED AT 5L. REPAIRED STR 5L, STA 410-440, IAW-SRM-53-00-53-2R, SHEET 6, DETAIL I, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-03-1A, FIG
101, SHEET 1, CAT-A, MAJOR REPAIR.SDR FDEA201608192941Aileron · damagedLT AILERON UPPER COAT INBD SIDE CHIPPED COMPOSITE. LT AILERON REPAIRED AS REQUIRED IAW-SRM-51-70-04 PARA. 5G, FIG 9, AILERON REBALANCE ACCOMPLISHED ON NR N00658, FOR WEIGHT ADDED AT REPAIR, DAMAGE LOCATION, WING STA 670.266-673.266, PN:113N7100-64, SN:32942
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