N220FE, cancelled Mar 19, 2013
Service difficulty reports · 124
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 = 'N220FE' AND deregistration_id = 'N220FE-2013-03-19' 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 = 'N220FE' AND deregistration_id = 'N220FE-2013-03-19' 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 FDEA201006232116Engine · stalledNR 2 ENGINE COMPRESSOR STALL/SURGE AT LEVEL OFF - FL340 EPR WAS OBSERVED TO GO DOWN TO 1.6 EPR WITH ENGINE VIBRATION NOISE ASSOCIATED WITH COMPRESSOR STALL. AIRTURN BACK. R & R NR 2 ENGINE AS PER WORK CARD 70T0002 AND TESTED PER WORK CARD 70T0301-02. ALLSDR FDEA201003050653Seat Track · corrodedUPON REMOVAL OF FLOORBOARD TO ACCESS MLG SIDE STRUT AFT BRG, FOUND SEAT TRACK CORRODED AT STA 950, 12 REMOVED DAMAGED SEAT TRACK SECTION FROM BS 950+ 10 TO BS 950B+10 LBL 24, FABRICATED NEW SEAT TRACK SECTION AND SPLICES, INSTALLED NEW SEAT TRACK SECTION ANDSDR FDEA200810294619Fan · failedSLIGHT ELECTRICAL ODOR WAS DETECTED APPROACHING DESTINATION. TURNED OFF GASPER FAN. ODOR WAS STILL DETECTED AND BECOMING STRONGER. DONNED OXYGEN MASKS RAN QRH SMOKE, FUMES, ODORS CHECKLIST. DECLARED ATC EMERGENCY LANDED AT RWY 9 WITH FIRE TRUCKS IN TOW. SDR 08FDEA04619Gasper Fan · malfunctionedAT FL 350 A SLIGHT ELECTRICAL ODOR WAS DETECTED APPROACHING MEMPHIS. TURNED OFF GASPER FAN. ODOR WAS STILL DETECTED AND BECOMING STRONGER. DONNED OXYGEN MASKS RAN QRH SMOKE, FUMES, ODORS CHECKLIST. DECLARED ATC EMERGENCY AND LANDED. AT GATE SHUTDOWN ACFT SDR 08FDEA02133Beam · corrodedKEEL BEAM END TOP ATTACH ANGLE ON BACK OF BULKHEAD AT FS 740 HAS CORROSION ON TOP SIDE OF ANGLE AT RBL 4, ABOVE CONTROL CABLE PULLEY WHEELS. REMOVED AND REPLACED ANGLE REF SRM 51-30-02. FABRICATED REPLACEMENT ANGLE ON N/R N00726. FLAP PEENED, ALODINED, PRISDR 08FDEA02132Beam · corrodedDELTA BEAM INTERIOR RT LOWER CHORD AT BS 747 - 749, RBL 5, IS CORRODED ON INNER SURFACE AT AND AROUND SPLICE. BLENDED CORROSION AT LOWER, FWD CHORD. FOUND TO BE OUT OF LIMITS, REF DWG 69-47111. REPLACED CHORD REF DWG 65-47111. THIS IS CLASSIFIED AS A MAJORSDR 08FDEA02129Beam · corrodedCORROSION INSIDE DELTA BEAM STA740, LBL 3, WL 148 CUT AWAY LWR WEB SECTION OF DELTA BOX TO FOM. REMOVED CORROSION FROM DELTA BEAM STA 740, LBL 3, WL 148. VERIFIED MATERIAL LOSS BY NDT, AND FOUND TO BE OUT OF LIMITS REF DWG 65-23555. REPLACED INTERCOSTAL REFSDR 08FDEA02127Frame · corrodedCORROSION ON TOP OF WING TO BODY FAIRING FRAME WORK AT TWO FWD ADF ANTENNA LEAD POSITION CLAMP ATTACH AT FS 730F, RBL 10, INBOARD OF RT RAM AIR DUCT REMOVED PANELS REF SRM 51-30-2, REMOVED CORROSION REF SRM 53-10-01. FOUND TO BE OUT OF LIMITS REF SRM 51-20-01SDR 08FDEA02074Bulkhead · corrodedFWD PANEL RACK: BULKHEAD BS 720 FWD PIT FRAME CORROSION AROUND NUT PLATES (MKD) FABRICATED NEW FRAME ANGLE REF DAD DWG 65-82623. TREATED PRIMED RES AMM 51-20-021-7 PG 1-7 51-20-031-7 PG 1-7. MARKED PART REF FEDEX GMM 7-0-1001. THIS IS CLASSIFIED AS AMINOR RSDR 08FDEA02073Beam · corrodedRT A/C EQUIP BAY PANEL 3455 HAS CORROSION UNDER FWD HINGE PLATE ON FRAME REMOVED PNL NR 3453, 3358, 3465. SPLICED IN NEW BEAM ASSY P/N NR 65-58502-90. FABRICATED 4. REPAIR ANGLES, TREATED AND PRIMED AND INSTALLED. RE-INSTALLED A/C PANELS. REF SRM 51-30-0SDR 08FDEA02072Mount · corrodedCORROSION ON CARGO TIE DOWN MOUNT ON BOTTOM INBOARD FWD CORNER AT FS 720, LBL 22, WL 156. REMOVED AND REPLACED DAMAGED FITTING, REF SRM 51-30-02 PG 1-3. FITTING FOUND TO BE OUT F LIMITS, REF BOEING DWG 65-57848 ITEM NR 1, ORIG THK IS .110 INCH, MAT LOSS IS SDR 08FDEA02071Panel · delaminatedRT A/C BAY PANEL 3456 R DELAMINATED REMOVED AND REPLACED PANEL 3456R WITH SERVICEABLE PANEL REF SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02020Door Frame · crackedREF SNRM N00174 JPF ITEM NR 1. MAIN DECK, 1L DOOR FRAME IS CRACKED UNDER REMOVED STOP FITTING, AT BOTTOM CROSS BEAM AFT END. REMOVED DAMAGED MATERIAL REF SRM 51-40-02. VERIFIED CRACK REMOVED REF. 727 NDT MAN. PT. 6 51.00-00 FIG 23. NO DEFECTS FOUND. INSSDR 08FDEA02015Skin · crackedNOSE LANDING GEAR RIGHT FWD DOOR, CRACK AT AFT END EDGE SKIN AT O/B STOP ANGLE SUPPORT REPAIRED, R NLG DOOR REF 51-40-3, 51-30-5, 51-10-02, AND MM 32-22-001-4 . PERFORMED ADJUSTMENT AND TEST OF DOOR REF MM 32-22-001-5. OPS CHECK GOOD. THIS IS CLASSIFIED AS SDR 08FDEA02014Floorbeam · corrodedAFT CABIN, AT BS 1130 FLOORBEAM LOWER FLANGE, UPPER SURFACE CORRODED, BETWEEN LBL 22 AND LBL 35. REMOVED LOWER LT EXISTING T-CAP REPAIR, REF SRM 51-30-2. FABRICATED NEW T-CAP AND SPLICE ANGLES AND STRAP, REF SRM 53-10-8 FIG 10. INSTALLED REPAIR PARTS, REF SSDR 08FDEA01999Frame · corrodedAFT PIT BILGE BODY FRAME UPPER FLG IS BUCKLED/CORRODED BS 1050, STR 26L-28L, WL 148 (MKD). REMOVED CORROSION ON AFT PIT BILGE BODY FRAME UPPER FLG STA 1050 STR 26L 28L WL148. ORIGINAL THICKNESS IS .063 REMAINING MATERIAL IS .061, .002 REMOVED FOUND TO BE INSDR 08FDEA01998Seat Track · corrodedMAIN DECK FLOOR, SEAT TRACK EXTRUSION IS CORRODED, BS 850 - 870, LBL 45, WL 208. REMOVED AND REPLACED TRACK WITH NEW TRACK. FABRICATED FROM BAC 1520-1466 EXTRUSION REF SRM 51-30-2 PG 2, SRM 51-10-2 PG -3, GMM7-0-1001, AMM 51-20-014. THIS IS CLASSIFIED AS A SDR 08FDEA01996Cover · crackedC-2 PIT RT THRESHOLD COVER AT STA 950E IS CRACKED AT BOLT HOLE WITH LIGHT CORROSION ON BOTTOM SIDE OF PANEL TRANSFERRED HOLES, INSTALLED NUTPLATES, TREATED, PRIMED AND PAINTED NEW PANEL. REF; SRM 51-30-2 PG 1 - 3, FX 727 200 MM 51-20-151-7, AND FX727-200 MSDR 08FDEA01995Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED STA 1148 - 1170, RBL 45 WL 208 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, ORIGINAL THICKNESS .070 INCH, MATERIAL LOSS OF .030", REMAINING MATERIAL .040". REMOVED SEAT TRACK, REF SRM 53-10-1 PAGE 16 DET 5. SEAT TRACK FABRICSDR 08FDEA01994Shear Tie · chafedAFT PIT BILGE BODY FRAME SHEAR TIE ASSY HAS DISBONDED LEVELING COMPOUND/CORROSION BS 1130 AFT, STR 29R - 30, WL 148. BLENDED CORROSION ON SHEAR TIE, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PIECE. REF SRM 51-30-02 AND DWG NR 69-20813. THIS ISDR 08FDEA01993Seal · dirtyLOWER FWD CARGO COMPARTMENT DOOR, UPPER AFT CORNER CRACKED FABRICATED PER BOEING DWG 65-57146 CARGO DOOR AFT UPPER CORNER REF SRM 51-30-2. INSTALLED NEW SEAL DEPRESSOR CORNER REF 51-30-2, RESTORED LEVELING COMPOUND TO AREA. REF AMM 51-40-000-0. THIS IS CLASSDR 08FDEA01992Channel · damagedFWD PIT STA 620 ABOVE STR 27L " U " CHANNEL SUPPORT ON FWD SIDE OF FRAME HAS 2 MISDRILLED HOLES AT LBL 26. REMOVED DAMAGE, FABRICATED 2 REPAIR ANGLES, HEAT TREATED TO T-6 CONDITION. FABRICATED FILLER. ALODINED AND PRIMED ALL REPAIR PARTS, INSTALLED REPAIR PSDR 08FDEA01991Angle · corrodedC-2 PIT Z - ANGLE FROM STA 960 TO 1036, RT SIDE, HAS SEVERAL LOOSE/MISSING NUT PLATES WITH AREAS OF LIGHT CORROSION ON PANEL REMOVED CORROSION, ORIGINAL THICKNESS, .062 INCH, REMOVED .037 INCH, REMAINING THICKNESS .025 INCH. OUT OF LIMITS. VERIFIED NEW PARTSDR 08FDEA01990Seal · damagedLOWER NR 2 CARGO DOOR S/N BNW 506, AFT LWR CORNER, OF SEAL DEPRESSOR HAS NICKS. NR 2 CARGO DOOR SEAL DEPRESSOR, AFT CORNER FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT CORNER SEAL DEPRESSOR PN NR 65-59948-502, REF 51-40-02 AND DWG 65-60234 THIS IS CLASDR 08FDEA01989Stringer Clip · corrodedAFT PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 950F FWD, STR 29 R, O/B WL 139. REMOVED AND REPLACED STRINGER CLIP/CHANNEL REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA01988Frame · damagedAFT PIT BILGE BODY FRAME UPPER FLG IS BUCKLED, BS 1070, STR 25R - 27R DAMAGE ON FRAME FLANGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 1-3 DETAIL 4 NOTE 5. REMOVED DAMAGE, NDT VERIFIED DAMAGE REMOVAL. VERIFIED MATERIAL FOR REPAIR DOUBLER, 7075 - O - .06SDR 08FDEA01987Angle · corrodedCORROSION ON SKIN ATTACH ANGLE IN C-1 PIT, FS 700, BL 0, WL 148 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPLACEMENT ANGLE FROM 7075- T6, .040' REF BOEING DWG 69-14871 AND PRINT NR 65-15938. REMOVED OLD ANGLE REF SRM 51-10-2 AND MM 51-30SDR 08FDEA01986Stringer Clip · damagedFWD PIT BILGE BODY FRAME STRINGER CLIP IS MISDRILLED BS 720, STR 26L. INSTALLED STRINGER CLIP AT STA STA 720, STR 26L REF SRM 51-30-02.SDR 08FDEA01985Seat Track · corrodedAFT CABIN, LBL 25 , SEAT TRACK IB AND OB UPPER FLANGES CORRODED ON LOWER SURFACE AT 1130. REMOVED AND REPLACED SEAT TRACK AT STA 1130, LBL 25, FOUND OLD SEAT TRACK OUT OF LIMITS. FABRICATED NEW AND INSTALLED REF BOEING DWG. 65-19606.SDR 08FDEA01951Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM COMPOSITE REPAIR BS 1176 - 1183, RBL 18-27, WL 208 REMOVED OLD DITCHING PAN. FABRICATED NEW DITCHING PAN OUT OF 6061-O, HEAT TREATED TO T-6, DRILLED TRIMMED, TREATED PRIMED AND INSTALLED. REF BAC DSDR 08FDEA01950Door · crackedNOSE LANDING GEAR LEFT DOOR, CRACK AT AFT END EDGE SKIN AT B-STOP ANGLE SUPPORT REMOVED DAMAGE, NDT FOR CRACKS REMOVAL, FABRICATED FILLER AND DOUBLER REPAIR PARTS. INSTALLED FILLER AND DOUBLER REF SRM 51-30-2 PG 1, SRM 51-40-3 PG 1-3, SRM 52-80-1 ITEM 3, SRM SDR 08FDEA01946Fairing · crackedNR 4 T/E FLAP TRACK FWD FAIRING, HAS CRACK AT FWD END CUTOUT REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, NDT CHECKED FAIRING AND FOUND CRACK TO BE TERMINATED. MADE ADDITIONAL CUT FINALE CUT. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED. INSTALLEDSDR 08FDEA01945Pan · crackedDITCHING PAN FWD ATTACH ANGLE BS 1166, RBL 38 - 47, IS CRACKED AT RBL 45 - 4. REMOVED DAMAGED PART (ANGLE) FABRICATED NEW, TREATED AND PRIMED AND INSTALLED IAW SRM 51-10-02 PG 1, 51-30-02, PG 1 AND DWG 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01944Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED BS 1176 - 1183, LBL 27 - 37, WL 208 REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 27 - 37, WL 208 REF BOEING DWG 65-29548 AND SRM 51-30-2 AND 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01943Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED BS 1176 - 1183, LBL 27 - 37, WL 208. REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 27 - 37, WL 208 REF BOEING DWG 65-29548 AND SRM 51-30-2 AND 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01941Doubler · crackedNR 3 ENG LOWER COWL, I/B SIDE EDGE, 3RD LATCH CUTOUT FROM FWD END, LOWER CUTOUT AREA, DOUBLER CRACKED OUT. REMOVED AND REPLACED DOUBLER, REF SRM 51-30-2 PG 2, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01940Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM / DISBONDED. COMPOSITE REPAIR, BS 1176 - 1183, RBL 27-37, WL 208. REMOVED CRACKED DITCHING PAN. FABRICATED NEW DITCHING PAN, HEAT TREATED TO T-6 CONDITION, TREATED AND PRIMED, AND INSTALLED. REFSDR 08FDEA01939Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM COMPOSITE REPAIR BS 1176-1183, RBL 37-47 WL 208 (MKD). FABRICATED NEW DITCHING PAN, HEAT TREATED, ALODINED AND PRIMED, INSTALLED IAW SRM 51-10-2, PG 1, 51-30-2, PG 1, 51-30-5 PG 1. BOEING DWD: 65SDR 08FDEA01933Angle · corrodedAFT PIT BS 950E BULKHEAD RIGHT FWD BLOW OUT PANEL FRAME HAS CORROSION AROUND NUTPLATES. REMOVED DAMAGED Z-ANGLE, REPLACED WITH FABRICATED Z-ANGLE. INSTALLED ON BULKHEAD PANEL STA 950E IAW DWG 65-57172 AND SRM 51-40-02. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01930Floor Panel · corrodedC-2 PIT FLOOR PANELS NR 3 HAS CORROSION ALONG ONE SIDE EDGE FABRICATED NEW C-2 NR 3 PIT FLOOR PANEL REF DRAWING 65-67245 AND SRM 51-30-05 PG 13-21. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01928Frame · corrodedAFT PIT BILGE BODY FRAME UPPER FLG IS CORRODED BS 103, STR 26R - 28R, WL 147 REMOVED .007 INCH FROM ORIGINAL MATERIAL OF .063 INCHES WITH .056 INCH REMAINING AND FOUND FRAME TO BE OUT OF LIMITS. HEAT TREATED, DRILLED TREATED, PRIMED AND PAINTED, REPAIR DOUBLESDR 08FDEA01917Pan · crackedAFT MAIN DECK FLOOR DITCHING PAN ASSY HAS 2 CRACKS AND A MISSING FASTENER COLLER, BS 1176 - 1183,LBL 18 - 27, WL 208. REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 18 - 27 REF BOEING DWG 65-29548 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01910Skin · corrodedCORROSION ON AFT SKIN IN C-1 PIT AT FS 683 LBL 11, WL 148 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIINAL "T" IS .045" REMAINING 'T' IS .024. MATERIAL LOSS OF .021 REF SRM 53-30-1 FIG 1. FABRICATED DOUBLER AND FILLER, TREATED AND PRIMED, INSTALLED DSDR 08FDEA01907Rib · crackedLT HORIZ STAB TRAILING EDGE ELEVATOR HINGE SUPPORT RIB CRACKED 2 AREAS AT ELEVATOR STA 99.79 AFT INBOARD SIDE. REPAIRED LT HORIZONTAL TRAILING EDGE HINGE SUPPORT RIB AT STA 99.79 REF SRM 55-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA01923Angle · crackedLEFT WING INBD LE CAVITY NR 2 FLAP ACTUATOR AFT MOUNT, UPPER CORNER ANGLE IS CRACKED REMOVED AND REPLACED WEB REF SRM 51-30-2. OPS CHECKED ACCOMPLISHED ON W/C 70C003-00 THIS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01921Angle · corrodedFWD PANEL RACK, FWD PIT FRAME BS 720 CORROSION AROUND NUTPLATES REMOVED CORROSION IAW SRM 51-10-6, ORIGINAL "T'' .040 INCH, MAT. REMOVED IS .012. MAT REMAINING .028 INCH IS OUT OF LIMITS IAW SRM 53-1031. FABRICATED NEW LINER SUPPORT ANGLE FROM 7075-0 .050SDR 08FDEA01915Pan · crackedAFT MAIN DECK FLOOR DITCHING PANS PAN ASSY IS CRACKED BS 1176 - 1183, LBL 37-47, WL 208. REMOVED DITCHING PAN, FABRICATED, HEAT TREATED TO T-6 CONDITION, ALODINED AND PRIMED AND INSTALLED NEW PAN, REF SRM 51-30-2 PG 1, CWG 65-29549, MM 51-30-05 PG1, SRM 51-10SDR 08FDEA01906Structure · crackedFWD LAV SINK CABINET WASTE DISPOSAL FIBERGLASS SHOOT IS CRACKED. REPAIRED LAV SINK CABINET WASTE DISPOSAL CHUTE REF SRM 51-40-9 PAR 7, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01905Stringer · corrodedCORROSION ON I/B SIDE OF STR 28L AT FS 661, LBL6, WL 149 REPAIRED STRINGER AT 292 AT FS 661 LBL 6, WL 149. REF SRM 53-10-3, PG 3 -4, FIG 1, DETAIL 1, THIS IS CLASSIFIED AS MAJOR REPAIR.SDR 08FDEA01904Frame · damagedAFT PIT, BILGE BODY FRAME, HAS A DRILL START ON UPPER FLANGE AND CORRODED WEB BS 1143, FWD AND AFT SIDE, STR 26R - 27R, WL 153 - 156 LEVEL 1 CORROSION BLENDED AREA, FLAP PEENED AREA, APPLIED ALODINE AND PRIMER TO AREA APPLIED CORROSION INHIBITOR TO AREA, REF E
Back to N220FE, cancelled Mar 19, 2013