N934FD
Service difficulty reports · 539
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 = 'N934FD' 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 = 'N934FD' 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 FDEA202609091291Flap System · faultedTE FLAP DISAGREE WHEN GOING FROM FLAPS 20 TO 25. RAN QRH. DECLARED EMERGENCY ***EMERGENCY DECLARED*** CARRIED OUT FIM TASK 27-51 808 ON TRAILING EDGE FLAP SYSTEM. NO DEFECTS NOTED OK FOR CONTINUED SERVICE.SDR FDEA202608201185Engine · damagedON CLIMB AT ABOUT 18000 FT RIGHT ENGINE EGT WENT INTO YELLOW RANGE. ENTERED HOLDING TO RUN ENGINE LIMIT OR SURGE OR STALL QRH. ENGINE WAS UNRESPONSIVE TO POWER SETTINGS AT TIMES. AFTER CYCLING BLEED PER QRH ENGINE WAS WITHIN NORMAL RANGES. UPON DIVERSION TOSDR FDEA202606160765Not Reported · not reportedWRI 57-40-5108 FACTED IN ERROR. EA: F-5740-T0387288 P1. CREATED WRI 5740-5115 FOR SDR OF WRI 5740-5108 BEING FACTED IN ERROR. REF MAJOR REPAIR E.A. F-5740-T0387288 P1.SDR FDEA202601280090Battery · failedON SERVICE CHECK, NOTED CENTER GALLEY EXIT SIGN & R1 DOOR EXIT SIGN, & R1 DOOR SLIDE LIGHT NOT ILLUMINATING ON TEST. R & R FWD GALLEY EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-07-2.CENTER GALLEY EXIT LIGHT R1 DOOR EXIT LIGHT & R1 DOOR SLIDE LIGHT OPSDR FDEA202506271069Stringer · corrodedDOT 80-059 AFT CARGO COMPARTMENT STR 27R/H JUST AFT OF F/S 1300 @ DOME NUT STRINGER EXFOLIATED. CORROSION FOUND TO BE OUT LIMITS IAW SRM 53-00-03 FIG 101 ACCOMPLISHED WITH 02 E/A STRINGER REPAIR BETWEEN BS 1260 TO BS1280 STR 27 R/H AND BS 1320 STR 27 R/H ISDR FDEA202506271068Strap · corrodedDOT 86-117 AFT CARGO STA 1420, STABILIZER STRAP IN CEILING AT RBL 45, CORRODED. REMOVED STABILIZER STRAP IN CEILING AT RBL 45 AND PEFORMED REPAIR IAW SRM 53-00-51-2R, FABRICATED STRAP ON VTMAE TRAVELER # T25/1820128 IAW SRM 53-00-51-2R, MAJOR REPAIR.SDR FDEA202506251047Skin · corrodedDOT 86-84 RH WING IB MAIN FLAP, CORROSION ON UPPER SURFACE EDGE, AT OB JUNCTION OF AFT FLAP. REMOVED, REPAIRED AND REINSTALLED RH WING MAIN FLAP UPPER SURFACE EDGE (WEDGE) AT O/B JUNCTION AT AFT FLAP IAW SRM 51-40-02, SRM 51-70-10-2R REPAIR 4 & SRM 57-53-0SDR FDEA202506241038Seat Track · corrodedUNDER CABIN FLOOR PNL. 242MAF, AROUND MANY SCREWHOLES HAVE SURFACE CORROSION, ON FLOOR STRUCTURE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED AND REPLACED SEAT TRACK FLANGE RBL 24.5 STA. 900-1080 AND FABRICATED SEAT TRACK FLANSDR FDEA202506211022Floor Panel · brokenAFT CABIN FLOOR PANEL 251 MWF IS BROKEN AND MISSING CORRECT INSERT. FABRICATED MAIN CABIN FLOOR PANEL 251 MWF ON VTMAE TRAVELER T25/1818647 PER DWG 11864182, MAJOR REPAIR.SDR FDEA202506211021Floor Panel · damagedMAIN CABIN FLOOR PANEL 252 MWF IS BROKEN AND HAS ALL WRONG INSERTS NOT FLUSH WITH THE PANEL ARE INSTALLED ALL THE WAY THROUGH THE PANEL, NEEDS THE VERY SHALLOW INSERTS PER THE BUILD PRINT FOR THE PANEL. DOT 4-139. FABRICATED MAIN CABIN FLOOR PANEL 252 MWF SDR FDEA202506211020Floorboard · damagedMAIN CABIN FLOORBOARD 251MVF IS BROKEN. FABRICATED MAIN CABIN FLOORBOARD 251MVF ON VTMAE TRAVELER T25/1818699 PER DWG 11864182, MAJOR REPAIR.SDR FDEA202506191011Seat Track · corrodedCORR. FOUND ON SEAT TRACK LBL 45 FROM 1180 TO 1280 REMOVED, FABRICATED NEW & INSTALLED MAIN CABIN SEAT TRACK FROM STA 1180-1280 LBL 45 PER DWG BAC 1520-792 & SRM 51-40-02, PART MARKED IAW GMM 7-1-1001, MAJOR REPAIRSDR FDEA202506191008Strap · damagedBROKEN FLANGE STRAP UNDER CABIN FLOOR PNL #222 MDF B STA 396 DOT# 204-16 REMOVED & REPLACED STRAP UNDER FLOOR PANEL #222 MDF AT STA 396 IAW SRM 53-10-51-2R- 1, PARTMARK PER GMM 7-1-1001, STRAP FABRICATED ON VTMAE TRAVELER #T25/1818344 MAJOR REPAIR.SDR FDEA202506191007Seat Track · corrodedMAIN CABIN SEAT TRACK AT STA 1189 RBL 58.2 HAS CORROSION AT FASTENER HOLES. DOT 4-142 REMOVED AND REPLACED NEW SEAT TRACK PER DWG BAC1520-792, BATCH #0004393834 FROM BS 920 TO BS 1200 RBL 58.2, TREATED AND PRIMED IAW DWG# BAC1520-792 AND SRM 51-40-02, PARTSDR FDEA202506191006Crossbeam · corrodedDOT 86-160 STA 1060-1100, LBL 0-24 CORROSION AROUND SCREWHOLES. CROSSBEAM AT BS 1060-1100, BL0-LBL24 CORROSION BEYOND ALLOWABLE LIMITS, REMOVED DAMAGE CROSSBEAM AND REPLACED WITH FABRICATED CROSSBEAM IAW DWG #144N5005, SRM 53-40-51 DETAIL 1 AND SRM 51-40-0SDR FDEA202506130929Seat Track · corrodedDOT 86-158 FLOOR TRACK AT LBL24, STA 1057, CORROSION ON LH FLANGE AT SCREWHOLE. REMOVED AND REPLACED FLOOR TRACK AT LBL 24 STA 1057 IAW SRM 51-40-02 & DWG 111N5202, PARTMARKED PER GMM 7-1-1001, MAJOR REPAIRSDR FDEA202506110921Repair · corrodedDOT 80-065 AFT CARGO COMPARTMENT CEILING STRUCTURE. FLOOR BEAM LOWER FLANGE. F/S 1560 APPROX 10 INCHES FROM R/H SIDEWALL BEAM CORRODED REMOVED DAMAGES AT AFT CARGO LWR FLANGE F/S IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-1A. REPAIRED FLOSDR FDEA202506100886Strap · corrodedDOT 86-118 AFT CARGO STA 1420, STABILIZER STRAP IN CEILING AT RBL 24, CRRODED. REMOVED AND REPLACED STABILIZER IN CEILING STRAP IAW SRM 51-40-02, FABRICATED ON VTMAE TRAVELER T25/1811436 IAW SRM 53-11-51-2R RBL 24 STA 1360-1440, PART MARK PER GMM 7-0-1001,SDR FDEA202506100885Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION A STA 1180 TO 1200 RBL 45, DOT 4-141 REMOVED, FABRICATED & INSTALLED NEW MAIN CABIN SEAT TRACK PER DWG BAC 1520-792 STA 1120-STA 1200 RBL 45, P.M. IAW GMM 7-0-1001, MAJOR REPAIR.SDR FDEA202501080035Bulb · inoperativeSLIDE LIGHT WOULD NOT ILLUMINATE WHEN RIGHT ENTRY DOOR WAS ARMED. REPLACED R1 DOOR SLIDE LIGHT BULBS, READY FOR SERVICE.SDR FDEA202401160079Probe · failedDURING CLIMB OUT AFTER TURNING OFF ENGINE ANTI-ICE THE LEFT ENGINE APPEARED TO NOT PRODUCE THE SAME POWER AS THE RIGHT ENGINE. 7 DEGREES RIGHT RUDDER REQUIRED. EGT WAS NEAR LIMIT WITH ALL OTHER ENGINE INDICATIONS MUCH LESS THAN THE RIGHT. EMERGENCY DECSDR FDEA202309081563Power Supply · failedL1 DOOR EMERGENCY LIGHT ABOVE DOOR AND SLIDE LIGHT FAILED TO ILLUMINATE DURING TEST. REMOVED AND REPLACED L1 DOOR POWER SUPPLY AS REQUIRED OPS CKS NORMAL OK FOR SERVICE.SDR FDEA202307181233Cylinder · failedL FWD ENT DOOR ARMED FLAG DID NOT FUNCTION. UPON OPENING DOOR THE SLIDE PARTIALLY DEPLOYED. FOUND L1 DOOR OPEN WITH SLIDE HANGING OUT OF DOOR AND ATTACHED TO GIRT BAR, SLIDE WAS NOT DEPLOYED. L1 DOOR ASSIST BOTTLE IS EMPTY. RELEASED FOR SERVICE PESDR FDEA202306301130Unknown · corrodedMAIN CABIN - SEAT TRACK AT STA565 TO 575 LBL24 HAS CORROSION BY FLOOR PANELS HOLES CORROSION ON MAIN SEAT STA 565 TO STA 575 LBL 24 FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A. REMOVED SEAT TRACK FROM STA 440-680 LBL24 IAW B757 SRM 53-00-52-2R, REMOSDR FDEA202306281124Skin · wornL.WING O/B FWD FLAP I/B L/E REINFORCING DOUBLER IS WORN. REPAIRED L/E SKIN ON L.WING O/B MAIN FLAP PER B757 SRM 57-53-01-2R, REPAIR 5SDR FDEA202306261109Attach Angle · corrodedL.WING L/E #3 SLAT IS CORRODED ON THE LOWER ATTACH ANGLE FOR COVE SKIN.. REMOVED AND REPLACE #3 SLAT ASSY ON FEDEX N/R N00374 AND HAECO N/R 22374. PER B757 AMM 27-81-02-4.SDR FDEA202306241092Slat · dentedLH WING #5 SLAT LOWER SURFACE OF T/E WEDGE IS DENTED JUST O/B OF I/B AUX TRACK REPAIRED LH WING #5 SLAT LOWER SKIN BY REMOVING DAMAGE AREA AND BONDING FILLER AND DOUBLER REPAIR IAW B757 SRM 57-43-02-2R AND 51-70-10-2R AND FEDEX EA# F-5750-T0374880-P1 - WINSDR FDEA202306211070Panel · crackedLEFT WING FIXED LEADING EDGE SKIN UPPER SURFACE CRACKED IN TWO EACH AREAS AT INBD END OF #3 SLAT. REPAIRED L/H WING FIXED LEADING EDGE SKIN UPPER SURFACE IS CRACKED IN 2 EACH LOACTIONS AT INBD END OF #3 SLAT IAW FED EX B757 SRM 57-41-01-0I, 57-41-01-2R REPSDR FDEA202306181055Slat · dentedLH #5 SLAT, INNER SKIN IS DENTED JUST OUTBD OF INBD AUX TRACK. REPAIRED L/W #5 SLAT COVE PANEL SKIN DENTED AND PUNCTURED IAW B757 SRM 57-43-01-2R REPAIR 3SDR FDEA202306171045Skin · burnedEXTERIOR FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT STA 1547 BETWEEN S23R & S24R EVALUATED LIGHTNING STRIKE @ STA 1547 BETWEEN S23R & S24R MATL LOSS .010 MATL REMAINING .030 ORIGINAL MATL .040 FOUND TO BE OUT OF LIMITS PER BAC DWG 146N3430 REV - & B757 SRSDR FDEA202306141035Flap · delaminatedRIGHT WING I/B FWD FLAP I/B END UPPER SKIN DISBONDED. ACCOMPLISHED PERMANENT REPAIR OF DISBONDED UPPER SKIN ON R/W INBD FLAP BONDED PART 113N2324 IAW B757 57-53-01-2R FIG 201 DETAIL 3 AND SRM 51-70-10-2R-0G.SDR FDEA202306141034Door · crackedRMLG BODY DOOR IS CRACKED AT THE FWD INBD CORNER OF THE DOOR TANG. REPAIRED RMLG DOOR FWD INBD CORNER OF THE DOOR TANG IAW B757 SRM 52-80-02-2R FIG 201 SHEET 6, SRM51-70-06-0G FIG 1 SHEET 1 AND BOEING DWG 149N6003 #DL PSDL REV -.SDR FDEA202306141033Panel · damagedMAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL24 TO LBL45. REMOVED AND REPLACED FLOOR PANEL AT STA 560 - 680 LBL 24 - LBL45 IAW B757 AMM 53-01-01-4 AND FEDEX DWG SRZ-25-005 REV RSDR FDEA202306141032Panel · damagedMAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL 0 TO LBL 24. REMOVED AND REPLACED FLOOR PANEL AT STA 560-680 LBL 0 - LBL 24 IAW B757 AMM 53-01-01-4 AND FEDEX DWG SRZ-25-005 REV R.SDR FDEA202209212353Case · corroded#2 ENGINE LPC CASE HAS EVIDENCE OF CORROSION UNDER THE KEVLAR CONTAINMENT RING OUTER SLEEVE AT THE REAR EDGE FROM APPROX 7:00 POSITION TO THE APPROX 12:00 POSITION 0000280794 : SHAEFFER, DAVID C - 21-SEP-2022 22:07 EVALUATED CORROSION AND REPAIRED TEFLON SSDR FDEA202208252049Girt Bar · unsecureFOUND L1 DOOR GIRT BAR LAYING ON CREW STAIRS. FACT 24AUG22 18:26 BNA REINSTALLED L1 DOOR GIRT BAR ASSY. PER AMM 25-66-10-2, ALL OPS CKS GOOD PER AMMSDR FDEA202202020179Oil System · overservicedSUSPECTED FUME EVENT. STRONG DIRTY SOCK SMELL DESCENDING THROUGH 10,000 FT. WHICH LASTED APPROXIMATELY 3 MINUTES. REMOVED HEPA FILTER PERFOMED GVI IT WAS CLEAN AND NO SIGNS OF OIL OR CONTAMINATION. REINSTAILLED HEPA FILTER AFTER VISUAL INSPECTION IAW SDR FDEA2022020320179Unknown · fumesSUSPECTED FUME EVENT. STRONG DIRTY SOCK SMELL DESCENDING THROUGH 10,000 FT. WHICH LASTED APPROXIMATELY 3 MINUTES.SDR FDEA202109162317Annunciator · failedPDIS 934 32-60 1456 16SEP21 MEM OPEN U ON FINAL 36R KMEM AT 1300 AGL 150 KIAS WITH GEAR LEVER - DOWN RIGHT MAIN NO INDICATION, LEFT MAIN AND NOSE GEAR- DOWN/ GREEN. RAN QRH USED ALT GEAR EXTENSION. ALL 3 GEAR- DOWN/ GREEN. LANDED WITHOUT INCSDR FDEA202107271877Dome Nut · corrodedDAMAGED AND CORRODED DOME NUT PLATES UNDER FLOOR PANEL 242MGF REMOVED DAMAGED CROWN SUPPORT IAW SRM 51-40-02, FABED NEW CROWN SUPPORT IAW BOEING DWG 111N5207 AND SRM 51-10-02, INSTALLED NEW CROWN SUPPORT IAW BOEING DWG 111N5201 AND SRM 51-40-02 STA. 900-10SDR FDEA202107151790Floor Panel · damagedZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VTMAE TRAVELER # T21/1560980 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.SDR FDEA202107151789Floor Panel · damagedZONE 220 FLOOR BOARD 221BF IS BROKEN. FABRICATED ZONE 220 FLOOR BOARD 221BF ON VTMAE TRAVELER # T21/1561021 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.SDR FDEA202107151788Floor Panel · damagedZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VTMAE TRAVELER # T21/1560977 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.SDR FDEA202107141775Floorboard · delaminatedZONE 200 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER # T21/1560978 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR.SDR FDEA202107141776Floorboard · delaminatedZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELERE # T21/1560979 IAW DWG SRZ-25- 005 REV R. MAJOR REPAIRSDR FDEA202103300801Adc · failedDECLARED EMERGENCY WITH ATC. LIGHTNING STRIKE, UNRELIABLE AIRSPEED ON CAPT/LEFT SIDE. RAN UNRELIABLE AIRSPEED QRH. LANDED FLAPS 20 REF20.RECEIVED MULTIPLE RANDOM EICAS MSGS ASSOCIATED WITH UNRELIABLE AIRSPEED AND NOT ASSOCIATED WITH URELIABLE AIRSPEED. SDR FDEA202102030299Girt Bar · damagedGIRT BAR NEEDED REPAIR. PIECE FELL OFF DURING CLOSURE ON L1 DOOR. RMV & INSTALL NEW L1 DOOR GIRT BAR IF PLACE REF B757 AMM 25-66-10-2. STILL REQ 52-11-25 25-5 NO. 1 PASS DR GIRT BAR MECHANISM-ADJ/TEST DUR ADJ OF GIRT BAR FND PLAY IN BOTH THE FWD & AFT SDR FDEA202102030275Girt Bar · no testL-1 DOOR FAILED STEP 3 OF E.O. F-5220-7-5000 REV NO. B PS PT3 REF 757 AMM 52-11-20-5, WHILE PERFORMING STEP 3. E.(2), WHEN OUTSIDE HANDLE IS EXTENDED (WITH MODE SDR FDEA202010302721Control Unit · wornEXCESSIVE ELEVATOR PLAY, FIRST FEW INCHES OF ELEVATOR YOLK INPUT, A DEAD SPOT WAS NOTED, WHERE THERE WAS VERY LITTLE RESISTANCE OR FEEL. VERY NOTEABLE DURING TO AND LANDING PHASE. PERF CAT I AUTOLAND AS FUNCTION CHECK AND OPERATIONS CHECKED GOOD. REMOVED ASDR FDEA201907031471Floorbeam · crackedCRACK STA. 580 FLOORBEAM LBL 45.50 UPPER CHORD AFT FLANGE. DOT 88-42 COMPLIED WITH EA # : F-5310-T0347950 P1 TITLE: FUSELAGE- MAINFRAME- STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.
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