N435FE, cancelled Feb 3, 2024
Service difficulty reports · 94
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 = 'N435FE' AND deregistration_id = 'N435FE-2024-02-03' 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 = 'N435FE' AND deregistration_id = 'N435FE-2024-02-03' 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 FDEA201309042115Selector Valve · failedON LANDING, NOSE TILLER COULD NOT BE MOVED. DIFFERENTIAL BRAKING USED TO CLEAR RWY. TROUBLESHOT IAW TSM 32-51-00 FIG 103 TO STEP 4. NOSE GEAR DOORS WILL NOT RAISE. SUSPECT LANDING GEAR SELECTOR VALVE. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-3SDR FDEA201210313788Jackscrew · failedDURING DESCENT AT MEM TO 36R, SLATS WOULD NOT EXTEND AT 210 KTS. EXECUTED QRH PROCEDURES, DECLARED EMERGENCY AND REMAINDER OF APPROACH AND LANDING NORMAL. CREW LEFT SLAT/FLAP HANDLE IN 30/40 POSITION TO ASSIST MX PROCEDURES. REMOVED REPLACED RIGHT WING NR SDR FDEA201108193388Panel · corrodedRT ELEVATOR, L/E PANEL 345DT, OTBD LANDING HAS 1 EA CORRODED FASTNER HOLE, 2EA MISDRILLED HOLES, AND CORROSION ON THE WEB ATTACHMENT STRAP. REMOVED LEVEL 1 CORROSION AT RT ELEVATOR L/E PANEL FASTNER HOLE AND WEB ATTACHMENT STRAP IAW SRM 51-74-10, PAGE 204. FSDR FDEA201108183365Skin · gougedRT WING FIX L/E IS GOUGED APPROX 6" LONG BETWEEN SLAT TRACK 5 AND 6, FROM CONTACT WITH NR 2 SLAT LOWER SKIN FASTENERS. SMOOTHED AND BLENDED AREA IAW SRM 51-75-10 AT RT WING FIX L/E SLAT TRACK 5 AND 6. NDT FOR CRACK AND LIMITS, NO LIMIT REMAINING THICKNESS.SDR FDEA201108183356Skin · gougedRT HORIZONTAL STAB L/E PANEL 341AB, EXTERNAL SKIN SCRATCHED AND GOUGED, ENTIRE LENGTH OF INBD EDGE. BLENDED OUT AREAS (4EA) ON RT HORIZONTAL STAB L/E PANEL 341AB EXTERNAL SKIN IAW SRM 51-73-10; CHECKED LIMITS FOUND AREAS (3EA) WITHIN LIMITS, 1 AREA OUT OF LSDR FDEA201108173303Attach Fitting · corrodedLT WING RIB 5 FWD LUG BORE DIAMETER HAS CORROSION THAT HAS EXCEEDED MAX ALLOWABLE REWORK DIMENSIONS "4.8405 IN". REMOVED LEVEL 1 CORROSION FROM LT WING RIB 5 BY OVERSIZING THE BORE AND SPOT FACING THE AFT LUG FACE, NDT INSPECTED (NIL FINDING) INCLUDED ACID SDR FDEA201108163289Adapter · crackedCLEVIS ADAPTER AT FR 46 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX.2" LONG AT FWD & AFT FLANGE. R & R CLEVIS ADAPTER AT FR 46, BETWEEN TRACKS 2R AND 3R IAW SRM 51-72-10, PG. 1-3.SDR FDEA201108153280Channel · bentINNER FUSELAGE "U" CHANNEL IS BENT STR 33L BETWEEN FR 83 TO FR 84. R & R CHANNEL AT STR 33L BETWEEN FR 83 TO FR 84 IAW SRM 51-40-21. PARAGRAPH 7.SDR FDEA201108143274Intercostal · bentINTERCOSTAL AND UPPER ANGLE ARE BENT STR 33R. INNER FUSELAGE BETWEEN FRAME 85 AND FRAME 86. REMOVED AND FAB AND INSTALLED INTERCOSTAL ANGLE ON FR 85 TO 86 RT STRINGER 33R, REF SRM 51-40-21, PG7 REPROTECTED AREA IAW SRM 51-75-10.SDR FDEA201108113220Skin · gougedUPPER AFT AREA OF AFT CARGO DOOR CUTOUT, EXT SURFACE, HAS MULTIPLE SCRATCHES EXTENDING 10" AFT OF CUTOUT (FR63) BETWEEN STRINGERS 27R & 28R. SMOOTHED AND BLENDED 10" SQ IN AFT CARGO DOOR CUTOUT EXT SURFACE FR63, STR 27 & 28 IAW SRM 51-73-10. MAP AREA FOR NSDR FDEA201108113219Panel · crackedRT HORIZ L/E PANEL 341AB, INTERNAL STIFFENER CRACKED AT AFT END, FROM FASTENER TO EDGE OF PART, .3125" LONG, UPPER AFT CORNER OF PANEL. REMOVED FASTENERS HORZ L/E PANEL 341AB STOP-DRILLED CRACK ON INTERNAL STIFFENER, NDT FOR CRACKS. NO CRACKS WERE FOUND, FABRSDR FDEA201108113200Frame · corrodedAFT CARGO DOOR AFT EDGE SEAL LANDING STRIP GOUGED AT MULTIPLE PLACES ON FUSELAGE CUTOUT FR 63A R & R 3EA AFT CARGO DOOR AFT EDGE SEAL LANDINGS IAW SRM 51-72-10. UPON FURTHER EVALUATION, FOUND CORROSION AT FR 63A, STR 28R TO 29R, REMOVED CORROSION IAW SRM SDR FDEA201108083139Access Door · crackedAPU RT ACCESS DOOR 316AR AFT MATING FLANGE ON TAILCONE ASSY DEFORMED BELOW LATCH RECEPTACLE, MEASURED 4 IN LENGTH. REMOVED MATING FLANGE IAW SRM 51-40-21. INSTALLED NEW MATING FLANGE IAW SRM 51-40-21 AT AFT APU DOORS AFT MATING FLANGE.SDR FDEA201108083138Tray · corrodedAFT CARGO COMPARTMENT LT FWD PDU TRAY FLANGE IS BENT BETWEEN FR55 AND 56 AND NR 2L AND NR 3L TRACK ROLLERS. R & R PDU TRAY IAW SRM 51-40-21, DUE TO CORROSION FOUND OUT OF LIMITS IAW SRM 51-74-10 CORRODED AREA MEASURES 6.00L X 5.00 W X .012. MATERIAL LOSSSDR FDEA201108083133Hinge · crackedBOTTOM EXT FUSE EXT ELECTRICAL POWER PLUG ACCESS DOOR INNER DOUBLER CRACKED .2" IN LENGTH. REMOVED ELECTRICAL POWER PLUG ACCESS DOOR, R & R DAMAGED INNER DOUBLER, AND RE-INSTALLED ELECTRICAL POWER PLUG ACCESS DOOR IAW SRM 51-40-21, PARA 5 AND 6.SDR FDEA201108073130Retainer · crackedRT WING NR1 SPOILER T/E RETAINER STRAP IS CRACKED APPROX 1" LONG INBD END. R & R RETAINER STRIP IAW CMM 57-71-11.SDR FDEA201108073132Access Panel · crackedRT WING L/E ACCESS PANEL NR 624EB CUT OUT LANDING IS CRACKED APPROX 1" LONG. R & R CUT OUT LANDING FOR ACCESS PANEL 624EB IAW SRM 51-40-01, PAR 6 & 7 AND SRM 51-40-44 PG1-16, SRM 51-40-21 PARA 6&7. APPLIED ALODINE, PRIMED AND PAINTED IAW SRM 51-75-10.SDR FDEA201108063117Adapter · crackedCLEVIS ADAPTER AT FR 45 BETWEEN SEAT TRACK 2 & 3 RT IS CRACKED APPROX 1" LONG AT FWD FLANGE. R & R CLEVIS ADAPTER IN MDCC AT FR 45 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT IAW SRM51-40-21. FLOORBOARD LOCATED AND DRILLED IAW SRM 51-40-44. HOLES TREATED AND PROSDR FDEA201108053112Support Bracket · crackedNR1 ENGINE THRUST REVERSER TRANSLATING COWL UPPER GUIDE SUPPORT SLIDER BRACKET CRACKED. REMOVED NR 1 ENG O/B TRANSLATING SLEEVE IAW A310-200 AMM 78-32-11-04. REMOVED CRACKED UPPER COWL GUIDE SUPPORT BRACKET IAW SRM 54-40-21 AND SRM 54-04-01 PG.11. FABRICATESDR FDEA201108033081Stringer · crackedRT SIDE STRINGER 9R BETWEEN FR 98 TO 100 HAS 2 PIECES BROKEN OFF. R & R STRINGER 9R FROM FR 95 TO 102 IAW SRM 51-72-10, PARA 5A & 6A. FABRICATED NEW STRINGER IAW DWG 19A53989507. REPROTECTED IAW SRM 51-21-10, 51-23-10, & 51-75-10.SDR FDEA201108033083Intercostal · bentINNER FUSELAGE INTERCOSTAL IS BENT STR 33L BETWEEN FR85 TO FR84. REMOVED INTERCOSTAL STR 33L BETWEEN FR85 TO FR84 IAW SRM51-40-21, PARA 6, B/S FABRICATED STIFFENER AND WEB IAW DWG A53986749.LOCATED AND DRILLED AND INSTALLED STIFFENER AND WEB ,FR85 TO FR84, STSDR FDEA201108013058Intercostal · bentINTERCOSTAL IS BENT STR 35R INNER FUSELAGE BETWEEN FR86 TO FR87. REMOVED DAMAGED INTERCOSTAL, REPLACED WITH NEW INTERCOSTAL AND STRIP AT STR 35R BETWEEN FR 86 AND FR87 IAW SRM51-75-10 AND SRM51-21-10.SDR FDEA201107313046Structure · gougedRT WING SPOILER NR 7 LOWER T/E IS GOUGED APPROX .500" WIDE. R & R T/E OF RT WING NR 7 SPOILER IAW SRM 51-72-10.SDR FDEA201107303040Seat Track · damagedFLOOR TRACK L3 HAS DAMAGED RECEPTICLES LOCATED BETWEEN FLOORBEAM 61 AND 60. REMOVED DAMAGED SECTION FROM BETWEEN FRAMES 58 AND FRAMES 62 AND INSTALLED SPLICE REPAIR IAW SRM 53-10-16, FIG 208 SHEET 1. RESTORED PROTECTIVE COATINGS IAW SRM 51-75-10 AND 51-21-10SDR FDEA201107303038Mount Bracket · crackedAFT UPPER PYLON RIB 21, 3 INCH CRACK AT WING TO PYLON MOUNT BRACKET. R & R TEE PICK-UP ANGLE IAW SRM 51-72-10, PGS 1-3 AND SRM 51-40-21, PGS 31-36.SDR FDEA201107303037Access Panel · crackedLT EXTERNAL PACK AREA INBD LANDING FOR PANEL 143FL HAS .250. CRACK REMOVED LANDING FOR PANEL 143FL, INSTALLED NUTPLATES ON NEW LANDING IAW SRM 51-40-21. INSTALLED NEW LANDING ON LT EXTERNAL PACK AREA FOR PANEL 143FL IAW SRM 51-40-21.SDR FDEA201107293031Seal · wornPANEL 475CL FWD FINGER SEAL IS WORN APPROX 20 PERCENT ACROSS THE RT SIDE. REMOVED SEAL , FABRICATED NEW SEAL IAW SRM 51-40-44. INSTALLED NEW SEAL IAW SRM 51-40-21.SDR FDEA201107293021Bracket · bentFR 33, STGR 15L, 2 EA ISOLATOR BRACKET BENT. REMOVED 2 EA BRACKETS IAW SRM 51-40-21. FABBED 2 EA BRACKETS IAW DWG A53771078. ALODINED BRACKETS IAW SRM 51-21-10. PRIMED AND TOPCOATED IAW SRM 51-21-10, PARTMARKED IAW GMM 7-0-1001. INSTALLED 2 EA BRAKETS SDR FDEA201107293020Frame · corrodedAFT PRESSURE BULKHEAD LWR FWD SIDE CIRCUMFERENCE STRAP CORRODED 2 INCHES LENGTH X 3 INCHES WIDTH BETWEEN STGR 44L AND 46L. REMOVED AND REAPPLIED SEALANT ON AFT PRESS BULKHEAD FWD SIDE IAW SRM 51-74-10 PB 201, R & R ANGLE ANGLE SUPPORT IAW SRM 51-40-21; FABRSDR FDEA201107293019Intercostal · bentINTERCOSTAL IS BENT STR 33R INNER FUSELAGE BETWEEN FR'S 86 AND 87 FABRICATED. REPLACEMENT INTERCOSTAL, LOCATED, DRILLED, INSTALLED AND REPROTECTED IAW SRM 51-40-44, DWG A539-86751 AND 51-42-11, PG 7-22 AND 51-75-10.SDR FDEA201107252942Roller Tray · corrodedINSIDE AFT CARGO COMPT AT THE BOTTOM SURFACE OF 2R ROLLER TRACK, CORROSION 2.5" X 3" AT 10" FWD OF FR62. AFTER REMOVAL OF BALL MATS FOUND 1EA AREA ON ROLLER TRAY TO BE LEVEL 1, OUT OF LIMITS IAW SRM 53-10-15, FIG 102, BEYOND REPAIR, R & R ROLLER TRAY IAW AT FSDR FDEA201107252941Seat Track · crackedCLS ADAPTER AT FS 43 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX 1 INCH LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2 & 3 IAW SRM 51-40-21.SDR FDEA201107252937Adapter · crackedCLS ADAPTER AT FS 42 BETWEEN SEAT TRACK 2R AND 3R IS CRACKED APPROX 1.5" LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR42 BETWEEN SEAT TRACKS 2 AND 3RT IAW SRM 51-40-21.SDR FDEA201107252931Stringer Splice · corrodedSTRINGER 26R SPLICE AT FRAME 54 HAS A 1 SQ IN AREA OF CORROSION, AFT SIDE OF FRAME. REMOVED CORROSION AT SPLICE PLATE AND FOUND LEVEL 1 CORROSION TO BE OUT OF LIMITS IAW SRM 51-73-10. R & R SPLICE IAW SRM 51-72-10.SDR FDEA201107242925Strap · corrodedRUDDER L/E ATTACH LANDING , RT SIDE , INTERNAL STRAP CORRODED, 2SQ IN , 6 INCHES ABOVE NR1 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10, PAR 5, FABRICATED NUT PLATE STRAP IAW DWG A554-71556, ALODINED IAW SRM 51-21-10 PG 6. PRIMED IAW SRM 51-75-10, SDR FDEA201107242929Rib · crackedLT PYLON AT RIB 22 UPPER AFT SIDE HAS A 2 IN LONG CRACK. R & R TEE PICKUP ON LT NR1 PYLON AT RIB 22 IAW SRM 51-72-10.SDR FDEA201107242924Strap · corrodedRUDDER L/E ATTACH LANDING, RT SIDE INTERNAL STRAP CORRODED 2SQ IN, 8" ABOVE NR4 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10: FABRICATED PLATE IAW DWG A554-71556, ALODINED NUT PLATE STRAP IAW SRM 51-21-10 PAR.6, PRIMED IAW A310-200 SRM 51-75-10 PSDR FDEA201107242923Bracket · crackedFR26, STR 15 LT ISOLATOR BRACKET BROKEN IAW AMM 25-50-00-06. R & R ISOLATOR BRACKET AT FR 26 STR 15 LT IAW SRM 51-72-10 & 51-40-21, PARA 6.SDR FDEA201107222908Floorboard · damagedAFT CARGO FLOORBOARD 152EF MISSING EDGE FILLER DEFCT MEASURES 2 SQ INCHES. FABRICATED REPLACEMENT FLOORBOARD 152EF IAW DWG SR2 25-005, REV J.SDR FDEA201107222907Floor Panel · crackedFLOOR PANEL 252GF HAS 1EA 12" CRACK FABRICATED REPLACEMENT FLOOR PANEL 262GF IAW DWG SR2 25-005, REV J.SDR FDEA201107222906Floorboard · damagedFLOORBOARD 251GF HAS PUNCTURE. FABRICATED REPLACEMENT FLOORBOARD 251GF IAW DWG SRZ-25-005, REV J.SDR FDEA201107222905Floor Panel · crackedFLOOR PANEL 251WH HAS 12 IN CRACK FABRICATED REPLACEMENT PANEL 251WH IAW DWG SRZ-25-005, REV J.SDR FDEA201107222904Floor Panel · contaminatedFLOOR PANEL 147BF IS OIL SOAKED. FABRICATED REPLACEMENT PANEL 147BF IAW DWG SRZ-25-005, REV J.SDR FDEA201107222902Floor Panel · damagedAVIONICS COMPT FLOOR PANEL 121JF HAS 1 EA CORNER BROKEN AND 1 EA CORNER PLIES WORN THRU. FABRICATED REPLACEMENT FLOOR PANEL 121JF IAW DWG SRZ-25-005, REV J.SDR FDEA201107212888Spar · corrodedLEFT HORIZONTAL STAB UPPER REAR SPAR TOP FLANGE BOTTOM SIDE CORRODED AT 4EA NUTPLATE HOLES LOCATED 6 TO 18 INCHES OTBD OF FUSELAGE BETWEEN RIBS 3 AND 5 MEASURED 8 SQ INCHES. REMOVED CORROSION IAW A SRM 51-74-10, FOUND TO BE OUT OF LIMITS IAW SRM 55-10-00 COSDR FDEA201107192817Floorbeam · crackedFWD CARGO MAIN DECK FLOORBEAM AT FRAME 34 CRACKED AT STIFFENER, BETWEEN SEAT TRACKS 2 & 3 RT SIDE. CUTOUT DAMAGE AT FLOORBEAM IN FWD CARGO COMPARTMENT SUPPORT FR 34 RT SIDE IAW SRM 53-10-15. NDT IAW NTM 51-10-08 SHOW NO CRACK INDICATION AFTER CUTOUT OF DAMAGSDR FDEA201107192816Skin · crackedAPU EXHAUST DOOR 317AL RT LOWER LATCH CUTOUT SKIN HAS A .10 INCH CRACK. ROUTED OUT CRACK, NDT FOUND NO CRACKS, REPROTECTED AREA IAW SRM 52-41-18, PAGE 203 AND SRM 51-75-10. FABRICATED DOUBLER, DRILLED AND INSTALLED IAW SRM 52-41-18, FIG 201, PAGES 207-208.SDR FDEA201107192798Clevis · bentMDCC AT FS 54.1 BETWEEN SEAT TRACKS 2 & 3 RT CLEVIS ADAPTER FWD FLANGE IS BENT IN 2 EA PLACES. R & R ADAPTER AT FR 54.1 MDCC BETWEEN TRACKS 2 & 3 ON RT SIDE IAW SRM 51-72-10 PARA 5A & 6A . LOCATED, DRILLED & DEBURRED NEW ADAPTER IAW SRM 51-40-44, PG 1-16.SDR FDEA201107192793Clevis · crackedMDCC AT FS 54.1 AT SEAT TRACK 3RT CLEVIS ADAPTER MOUNT FITTING CRACK APPROX 2" LONG. R & R CLEVIS IN MDCC AT FR 54.1 ON RT NR 3 TRACK IAW SRM 51-72-10 PARA 5A & 6A. LOCATED, DRILLED & DEBURRED NEW CLEVIS IAW SRM 51-40-44, PG 16.SDR FDEA201107182783Floor Panel · crackedFLOOR PANEL 147 AF HAS A 1" INCH CRACK AND IS OIL SOAKED. FABRICATED REPLACEMENT FLOOR PANEL 147 AF USING DWG SRZ 25-005, REV J.
Back to N435FE, cancelled Feb 3, 2024