N220CY
Service difficulty reports · 78
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 = 'N220CY' 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 = 'N220CY' 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 ABXA2021331046Beam · corrodedDURING C-CHECK NWW FWD FACE 'AFT LOCK LINK BEAM AT WL 147 CORRODED ON TOP RIGHT SIDE LUG BACK UO FITTING. FOUND TO BE OUT OF LIMITS, BEAM WAS REPLACED IAW B767-300 SRM 53-10-14SDR ABXA2021329039Stiffener · corrodedWHILE IN C-CHECK RH STA.966 STIFFENER WAS FOUND TO BE CORRODED. A NEW STRINGER SPLICE WAS FABRICATED AND INSTALLED.SDR ABXA2021327051Skin · crackedDURING AIRCRAFT CURRENT C-CHECK AT AIRBORNE (TPA), MAINTENANCE DISCOVERED A CRACK IN FUSELAGE SKIN (P/N 143T3262-4) AT STA 782 BETWEEN STRINGERS 37R AND 38R. THE CRACK WAS REMOVED BY TRIMMING OUT (2.3” X 2.75”), SEE (FIGURE 1, SHEET 2). THE SKIN IS FABRICATED SDR ABXA2021226052Support Angle · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE MAIN CABIN FLOOR PANEL SUPPORT ANGLE (P/N 368-53-16-94490-201) AT STA 1605, LBL 64. THE CORROSION WAS REMOVED BY BLENDING PER SRM 51-10-02 AND EXCEEDING 10% NOMINAL MATERIAL LOSS. THSDR ABXA2021325050Failsafe · corrodedDURING C-CHECK, FOUND CORROSION ON FAIL SAFE STRAP LOWER SURFACE AT STA505 AROUND FASTENER HOLE AND SHEARED BOLT AT STA494 AT RBL44. REMOVED CORROSION AND EVALUATED AREA AT FWD. CARGO DOOR SILL FAIL SAFE STRAP LOWER SURFACE. ORIGINAL MATERIAL .200", MATERIAL RSDR ABXA2021322047Seat Track · corrodedDURING C-CHECK,MAIN CABIN SEAT TRACK HAS CORROSION AT STA 1487-1518 AT RBL 75. REMOVED CORROSION, EVALUATED AREA FOUND TO BE OUT LIMITS IAW B767-300 SRM 53-00-52. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW B767-300 SRM 51-40-02, SRM 51-40-05 AND IAI'S SRMSDR ABXA2021322045Seat Track · corrodedCORROSION ON CABIN SEAT TRACK STA 1605 AND LBL 54.REMOVED CORROSION AREA ON CABIN SEAT TRACK 1605 AND LBL54, ORIG. MAT .080", MAT LOSS .024", MAT REMAINING .056". FOUND TO BE OUT OF LIMITS IAW B767-300 SRM 53-00-02 DETAIL VII. FABRICATE, LOCATED AND DRILLED NESDR ABXA2021319040Failsafe · corrodedWHILE IN C-CHECK FAILSAFE STRAP AT LT STA955 REQUIRED REPAIR. REPAIR WAS COMPLETED IAW AMES EO 47207ORD03SDR ABXA2021318044Stringer · crackedDURING C-CHECK FWD CARGO COMPARTMENT, STRINGER 32R HAS DAMAGE ON UPPER FLANGE RADIUS AND END OF FLANGE AT STA413.REMOVED DAMAGE AND EVALUATED FWD. CARGO COMPARTMENT, STRINGER 32R AT STA. 413. FOUND TO BE OUT OF LIMITS IAW B767-300, SRM 53-00-03 NOTE A CRACKSSDR ABXA2021317038Pin · wornWHILE IN C-CHECK,MDCD LATCH CAM PINS 4, 10 AND 12 FAIL DIAMETER MEASUREMENT CHECKS. REMOVED AND REPLACED MDCD LATCH CAM PINS 4, 10, AND 12 IAW B767-300 AMM SUPPLEMENT 52-32-00. ADJUSTMENT CHECK GOOD, NO ADJUSTMENT NEEDED.SDR ABXA2021316049Floor Support · corrodedDURING C CHECH, INTERCOSTAL FOUND CORRODED AT FS 1263-1285 RBL 21.5 OUT OF LIMITS, REPLACED IAW B767-300 SRM 51-21.SDR ABXA2021316048Web · corrodedDURING C CHECK, AFT CARGO DECK WEB HAS MULTIPLE AREAS OF CORROSION STA"S 1263-1280 AND RBL30 - RBL44. REMOVED CORROSION FROM AFT PIT DECK WEB IAW B767-300 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .071", REMOVED .071", REMAINING .000". OUT OF LIMITS IAW B767-3SDR ABXA2021316043Skin · corrodedWHILE IN C-CHECK, RIGHT WING UPPER SKIN AT WING TO BODY FAIRING, SKIN BELOW FWD OVERWING HATCH HAS CORROSION. CORROSION REPAIRED IAW ABX REA-5725-64113-00SDR ABXA2021316042Skin · corrodedWHILE IN C- CHECK LH UPPER WING WAS FOUND TO BE EXFOLIATED. REPAIRED IAW ABX-REA-5725-64112-00. REQUIRES REPETITIVE INSPECTION NOT TO EXCEED 48 MONTHS.SDR ABXA2021216011Display · inoperativeLWR EICAS DISPAY INOP IN LEFT POSITION. AIR TURN BACK PERFORMED. AICRAFT GROUNDED BY MAINTENANCE. REMOVED AND REPLACED THE RIGHT EICAS COMP, THE BOTTOM EICAS DSIP. SWITCH MODULE AND THE EICAS SIGNAL CONSOLIDATION CARD IAW AMM 31-41-01, 31-41-04, AND 31-41-07 SDR ABXA2021012001Isolation Valve · intermittentEICAS MESSAGE RT BLEED ISO VALVE. BACK TO BLOCK, AIRCRAFT GROUNDED. DEFERRED, REMOVED/REPLACED RT BLEED ISO VALVE, IAW AMM 36-11-04. ACCOMPLISHED REACTIVATION PROCEDURES. REFERENCE CLEARING ACTION FOR DI 19878 ON L/P 38224-01/2. VERIFIED P/N 2780539-105 SSDR ABXA20200803224Pressure Switch · deterioratedRT ENGINE OIL PRESS DISCRETE LIGHT + EICAS MESSAGE WERE ILLUMINATED AFTER ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED. REMOVED AND REPLACED LOW OIL PRESSURE SWITC,H AS PER B767 AMM 79-33-01. LEAK CHECK + OPERATIONS CHECK GOOD. AIRCRAFT REMAINS ETOPS 18SDR ABXA20200803177Circuit Breaker · not closedAFTER PUSH BACK FROM GATE, PRIOR TO ENGINE START LEFT AND RIGHT EEC EICAS MESSAGE DISPLAYED. AIRCRAFT PULLED BACK IN TO GATE AND WAS GROUNDED. MAINTENANCE FOUND BREAKERS ON P-6 PANEL NOT SET. RESET ALL BREAKERS, EEC INOP LIGHTS EXTINGUISHED WITH IRU'S ALIGNSDR ABXA20200803158Bearing · corrodedRIGHT MLG AFT TRUNNION BEARING HAS CORROSION. AIRCRAFT WAS GROUNDED WHILE IN MAINTENANCE FOR MLG CHANGE.SDR ABXA20190410007Splice Plate · damagedDAMAGE ON RIGHT WING LEADING EDGE LOWER SPLICE PLATE AT LEADING EDGE STATIONS 568 AND 982. THE SPLICE PLATE WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA20170515062Skin · corrodedCORROSION ON RIGHT SKIN COVERED BY SATCOM ANTENNA BETWEEN FUSELAGE BS 1087 AND 1122. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20170515061Skin · corrodedCORROSION ON LEFT SKIN COVERED BY SATCOM ANTENNA BETWEEN BS 1087 AND 1122. SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA20150708079Unknown · malfunctionedUN-COMMANDED RAPID ROLLBACK OF BOTH ENGS TO THE IDLE POSITION, OCCURRED DURING CRUISE FLIGHT. THE AUTO THROTTLE ARM SWITCH WAS ON. THE ENG & WING ANTI-ICE SWITCHES WERE IN AUTO. THE THRUST LEVERS FOLLOWED ENGS TO IDLE POSITION. THE CREW THEN DISCONNECTED TSDR ABXA20131120656Angle · crackedANGLE BRACKET FROM TOP OF FRONT SPAR TO INBD LE STRUCTURE ABOVE SLAT PDU CRACKED. R & R ANGLE BRACKET ON LE FRONT SPAR. INSTALLED TWO PA FASTENERS ON SPAR THROUGH FUEL TANK, LEAK CHECKED FASTENERS. REINSTALLED ACCESS PANELS IAW SRM 51-40-02, AMM 28-11-00 & SDR ABXA20131120655Angle · crackedNUMBER 7 SLAT STA LES 155.00 UPPER AT SPAR INTERCOSTAL ANGLE CRACKED. FABRICATED BRACKET FROM 2024-0-.080 PO 0036528 IAW DRAWING 114T1305. SDR INFORMATION, CRACKED 1/4 INCH, LOC RT WING LES 155.0, PART 114T1342-106, PART NAME ANGLE, SN NSN. ACFT WAS GNDED.SDR ABXA20131105657Stringer · dentedFORWARD LOWER CARGO STRINGER 30L IS DENTED AT BS 506. REMOVED DAMAGED SECTION OF STRINGER. REMOVED STRINGER CLIPS & SKARTIES IN REPAIR AREA. REPAIRED STRINGER IAW REA-B653-60773-MR & SRM 53-00-03 FIG 201 REPAIR 2. REINSTALLED REMOVED COMPONENTS IN REPAIR ASDR ABXA20130522437Printed Ckt Board · faultySTATUS MESSAGE AFTER DISPATCH: RT ENG FIRE LP1 RT ENG FIRE LP1 DISPLAYED. RT ENGINE FIRE/OVERHEAT SYS FAILED ON APPROACH. ACCOMPLISHED FIRE/OVERHEAT SYS NON NORMAL IAW QRH. R & R AFLOTS CARD 10274. OPS CHECK GOOD IAW AMM 26-10-01. PART EFFECTIVITY VERIFIESDR ABXR2012070900055Skin · dentedBULK CARGO DOOR DENTED AT LOWER FWD CORNER. REPAIRED IAW SRM.
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