N256AY, cancelled Feb 5, 2022
Service difficulty reports · 121
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 = 'N256AY' AND deregistration_id = 'N256AY-2022-02-05' 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 = 'N256AY' AND deregistration_id = 'N256AY-2022-02-05' 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 USAA2014122400005Pump · leakingENROUTE, RT ENGINE OIL PRESSURE DROPPED TO 13 PSI, WITH OIL QTY LOSS. SHUTDOWN THE RT ENGINE. LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 2 ENGINE LUBE PUMP DUE TO DAMAGED THREADS ON THE TGB INLET SCREEN. REPLACED THE SCAVENGE OIL FILTER. CHECKED THSDR USAA2014062300013Handle · looseFWD ENTRY DOOR WOULD NOT ARM & DIFFICULT TO CLOSE. MX FOUND L1 DOOR ARMING HANDLE LOOSE. SECURED HANDLE. PERFORMED SATISFACTORY OPERATIONAL TEST OF L1 DOOR OPENING & CLOSING FUNCTIONS & SLIDE ARMING & DISARMING FUNCTIONS. ACFT OK FOR SERVICE.SDR USAA2014042100004Power Supply · inoperativeCLT L1 & L2 DOOR EXIT & THRESHOLD LIGHTS WOULD NOT TEST. REPLACED M1208 POWER SUPPLY.SDR USAA2013122700003Control Panel · faultyFLT 751 ENROUTE, RECEIVED FWD EQ OVERHEAT MESSAGE FOLLOWED BY UNCONTROLLABLE CABIN AIR PRESSURE. DECLARED AN EMERGENCY & PERFORMED A RAPID DESCENT TO 10,000 FT. RETURNED TO DEPARTURE & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE CABIN PRESSURE SELECTOSDR USAA2013121200001Slide · unsecureC1 CHECK, RT OFF WING ESCAPE SLIDE ASSEMBLY UNLACED, SLIDE NOT SECURED. REPLACED RT ESCAPE SLIDE ASSEMBLY & INSTALLED IAW B767 AMM 25-65-05-424-056.SDR USAA2013112200005Aileron · delaminatedC1 CHECK DELAMINATION ON RT AILERON AT APPROXIMATELY 75 INCHES OTBD OF INBD END & 13.5 INCHES FWD OF AFT TE. REPLACED RT AILERON IAW JOB CARD 12L56027004.SDR USAA2013111400009Skin · delaminatedDURING C1 CHECK, DELAMINATION WAS FOUND ON RT OTBD AFT FLAP APPROX 85 INCHES OTBD FROM INBD END LOWER SURFACE & 13.5 INCHES FORWARD OF T/E. REPAIRED RT AFT FLAP IAW SRM 57-53-01-2R-1.SDR USAA2013111400008Skin · delaminatedDURING C1 CHECK, DELAMINATION FOUND ON RT AFT FLAP APPROX 14 INCHES FROM INBD END & 12 INCHES FROM T/E. REPAIRED RT AFT FLAP IAW SRM 51-70-10.SDR USAA2013110800007Stiffener · crackedDURING C1 CHECK, CRACK FOUND IN VERTICAL STIFFNER OF NOSE WHEEL WELL AT BS 287, WL 172, LBL 25. REPAIRED VERTICAL STIFFENER OF NOSE WHEEL WELL AT BS287, WL172, LBL25 IAW SRM 51-70-12 & EA 130449.SDR USAA2013091600008Sign · unsecureEXIT SIGN OVER F/A J/S AT 2L DOOR IS OFF. R & R 2L EXIT SIGN.SDR USAA2013091600006Cover · unsecureEXIT SIGN COVER 2L JUMPSEAT FELL OUT. COVER REINSTALLED; OPC SATISF.SDR USAA2013090900001Cable · shortedENROUTE, ACFT RT AFT GALLEY A-302, CIRCUIT BREAKER TRIPPED. TRIED ONE RESET, STARTED SMOKING. PULLED CIRCUIT BREAKER AND UNPLUGGED CART. R & R AFT GALLEY CART CABLE. OP'S CHECED GOOD. NO OTHER DEFECTS NOTED.SDR USAA2013072300001Cover · dislodgedEXIT SIGN OVERWING EXIT ACFT LT COVER FELL OFF DURING TAKEOFF ROLL STRIKING PASSENGER IN SEAT 12A. MX SECURED EXIT SIGN OVERWING AS REQUIRED.SDR USAA2013070300003Service Cart · faultyEN-ROUTE, THE GALLEY FOOD HEATING UNIT IN THE AFT GALLEY MELTED THE PLASTIC FOOD TRAYS AND EMITTED AN ODOR. THEY WERE NEW FOOD TRAYS. MX EXCHANGED ALL HEATING UNITS AND VISUALLY CHECKED ALL CORDS. NO DAMAGE FOUND.SDR USAA2013050600002Battery · dischargedPHL - FLASHLIGHT AT FWD F/A STATION BATTERY DEAD. REPLACED BATTERY.SDR USAA2013042300002Sign · missingPHL - EXIT SIGN IN CEILING A/C RT AFT OF 1ST CLASS MISSING. RE-SECURED SIGN.SDR USAA2013031900002Check Valve · failedFLT 1628 ENROUTE, NR 2 ENGINE FLAMED OUT DURING REVERSE SELECTION ON LANDING. THE FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REPLACED THE NR 2 ENGINE MEC AND FUEL PUMP, PERFORMED THE NR 2 ENGINE VSV ADJUSTMENT, AND CLEARED THE CDP AND CBP WATER SDR USAA2013030600010Slide Raft · malfunctionedDURING ESCAPE SLIDE/RAFT OPS CHECK, TWO FWD SLIDE/RAFTS FAILED TO INFLATE PROPERLY. SLIDE DID NOT UNFOLD. CENTER WEBBING ATTACH POINT (BELOW GIRT) DID NOT BREAK AWAY. MAINTENANCE MANUALLY CUT WEBBING TO UNFOLD SLIDE. MAINTENANCE REPLACED THE ESCAPE SLIDE/RSDR USAA2013012800001Reheater · contaminatedFLT 9465 TEST FLIGHT. FL 360, IN CRUISE. CABIN AND COCKPIT SMOKE NOTED. CREW DONNED O2 MASKS AND ENDED TEST FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK REHEATER DUE TO CONTAMINATION.SDR USAA2013012200005Power Unit · brokenC4 CHECK - AFT CRT LEFT FLASHLIGHT POWER UNIT HAS A BROKEN WIRE. REPLACED AFT CRT LEFT FLASHLIGHT POWER UNIT IAW DME CORPORATION CMM 25-60-02.SDR USAA2013012200004Sign · brokenC4 CHECK - L2 DOOR LINER EXIT SIGN "L333" HAS BROKEN LIGHT COVER. REPLACED L-2 DOOR LINER EXIT SIGN "L333" & OPS CHECKS GOOD IAW B767 AMM 33-51-022-029 & 33-51-01-402-030.SDR USAA2013011800010Light · brokenC4 CHECK - WORN & BROKEN FORWARD & AFT GALLEY MAT EMERGENCY PATH LIGHT REQUIRES REPLACEMENT. REPLACED FORWARD & AFT GALLEY MAT EMERGENCY PATH LIGHT IAW DRAWING 12P25D0301.SDR USAA2013011600005Light · crackedC4 CHECK - RIGHT CEILING PANEL 11 EMERGENCY LIGHT ASSY IS BROKEN. REPLACED RIGHT CEILING PANEL 11 EMERGENCY LIGHT ASSY (AISLE LIGHT). OPS CHECK GOOD IAW B767 AMM 33-51-05-002-016 & 33-51-05-402-024.SDR USAA2013011500004Flap · damagedC4 CHECK - FIBER DAMAGE ON RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DTEF265.88 TO DTEF267.88. REPAIRED RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DTEF265.88 TO DTEF267.88 IAW B767 SRM 51-70-06-0G, REPAIR A, FIG. 9.SDR USAA2013010300027Floorbeam · corrodedC4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT BS 303, LBL 13. REPAIRED FLOORBEAM AT BS 303, LBL 13 IAW B767 SRM 53-00-51-2R-1 FIG 201.SDR USAA2012122800018Floorbeam · corrodedC4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT BS 1518, LBL 30. REPAIRED FLOORBEAM AT BS 1518, LBL 30 IAW B767 SRM 53-00-51-2R-1 FIG 201.SDR USAA2013012500014Channel · crackedC4 CHECK - CRACK ON FLOOR SUPPORT CHANNEL BETWEEN BS 347 & BS 357, RBL 34. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 347 & BS 357, RBL 34 IAW B767 SRM 51-40-02-0G, PAR 7, FIG 8 & 12.SDR USAA2013011500005Floorbeam · corrodedC4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 347, RBL 46.25. REPAIRED FLOORBEAM T-CAP AT BS 347, RBL 46.25 IAW B767 SRM 53-00-51-2R-1, FIG 201.SDR USAA2013012500015Attach Fitting · crackedC4 CHECK - CRACK ON FRAME ATTACH CLIP AT BS 1562, S33L. REPLACED FRAME ATTACH CLIP AT BS 1562, S33L IAW BOEING DRAWING 216T1014.SDR USAA2013012500013Floor Support · crackedC4 CHECK - CRACK ON FLOOR SUPPORT WEB UPPER CHORD AT B S1412, LBL 40. REPLACED FLOOR SUPPORT WEB UPPER CHORD AT BS 1412, LBL 40 IAW B767 SRM 51-40-02-0G, PAR. 4, FIG 3 & 12.SDR USAA2012121800026Floorbeam · corrodedC4 CHECK - CORROSION ON FLOORBEAM REPAIR STRAP AT BS 347, RBL 68. REPLACED FLOORBEAM REPAIR STRAP AT BS 347, RBL 68 IAW B767 SRM 53-00-51-2R-2 FIG 201.SDR USAA2012121300006Placard · missingC4 CHECK - LEFT AND RIGHT OVERWING HATCHES MISSING PLACARD. INSTALLED LEFT AND RIGHT OUTER WING HATCHES MISSING PLACARD IAW B767 AMM 20-10-13-964-001.SDR USAA2013010300024Shear Web · crackedC4 CHECK - CRACK IN LEFT PYLON FORWARD SPAR UPPER SHEAR WEB AT NAC STA 227, LBL 5. REPAIRED LEFT PYLON FORWARD SPAR UPPER SHEAR WEB AT NAC STA 227, LBL 5 IAW EO 5403T119, PG III-9, STEP G & E.SDR USAA2013011500003Floor Support · damagedC4 CHECK - ELONGATED HOLES ON CABIN FLOOR STRUCTURE SUPPORT WEB AT BS 1412, LBL 40. REPLACED CABIN FLOOR STRUCTURE SUPPORT WEB AT BS 1412, LBL 40 IAW B767 SRM 51-40-02-0G, FIG 12.SDR USAA2012120700005Fastener · damagedC4 CHECK - RIGHT OFF WING SLIDE LATCH ACTUATOR HAS DAMAGED HARDWARE. REMOVED AND REPLACED HARDWARE IAW B767 AMM 20-11-00-427-003. USED TW 1111113012SDR USAA2012120700004Fastener · damagedC4 CHECK - RIGHT OFF WING SLIDE INTEGRATOR HAS DAMAGED HARDWARE. REMOVED AND REPLACED HARDWARE IAW B767 AMM 20-11-00-422-003. USED TW 1111113012.SDR USAA2012120600005Spring · weakC4 CHECK, L-2 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REMOVED AND REPLACED L-2 DOOR DEPLOYMENT BAR GAS SPRING IAW B767 AMM 25-66-03-004-053 AND 25-66-03-404-067.SDR USAA2012120600004Spring · weakC4 CHECK, L-1 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REMOVED AND REPLACED L-1 DOOR DEPLOYMENT BAR GAS SPRING IAW B767AMM 25-66-03-004-053 AND 25-66-03-404-067.SDR USAA2013011500010Skin · corrodedC4 CHECK - CORROSION FUSELAGE SKIN AT BS 959, LBL 94. REPAIRED FUSELAGE SKIN AT BS 959, LBL 94 IAW EA 131979.SDR USAA2013011500009Skin · corrodedC4 CHECK - CORROSION FUSELAGE SKIN AT BS 955, RBL 92. REPAIRED FUSELAGE SKIN AT BS 955, RBL 92 IAW EA 131979.SDR USAA2013010300025Frame · crackedC4 CHECK - CRACK IN LEFT PYLON FRAME AT NAC STA 285.30, WL 148.0, LBL 12. REPAIRED LEFT PYLON FRAME AT NAC STA 285.30, WL 148.0, LBL 12 IAW B767 SRM 51-40-02-0G FIG 12.SDR USAA2013012500016Structure · corrodedC4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CENTER WING UPPER SKIN AT BS 955, RBL 4. REPAIRED CENTER WING UPPER SKIN AT BS 955, RBL4 IAW EA 504597A.SDR USAA2013010800024Floorbeam · corrodedC4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 1480, LBL 44. REPAIRED FLOORBEAM AT BS 1480, LBL 44 IAW B767 SRM 53-00-51-2R-1 FIG 201.SDR USAA2013010300026Attach Angle · crackedC4 CHECK - CRACK ON CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS 1087 TO BS 1109, LBL 39. REPLACED CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS 1087 TO BS 1109, LBL 39 IAW B767 SRM 51-40-02-0G FIG 3.SDR USAA2013011500006Seat Track · corrodedC4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN BS 1263 TO BS 1285, RBL 88.5. REPLACED SEAT TRACK BETWEEN BS 1263 TO BS 1285, RBL 88.5 IAW B767 SRM 51-40-02-0G, FIG 16.SDR USAA2012121800023Structure · crackedC3 CHECK - CRACK ON CHORD AT BS 1382, RBL 39. REPLACED CHORD AT BS 1382, RBL 39 IAW B767 SRM 51-40-02-0G FIG 3.SDR USAA2012122100022Structure · crackedC4 CHECK - CRACKS ON CABIN FLOOR STRUCTURE SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS1241 TO BS 1262, RBL 39. REPLACED CABIN FLOOR STRUCTURE SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS 1241 TO BS 1262, RBL 39 IAW B767 SRM 51-40-02-0G FIG 3, 8, 12.SDR USAA2013012500012Floor Support · crackedC4 CHECK - CRACK ON FLOOR SUPPORT WEB UPPER CHORD BETWEEN BS 1087 TO BS 1109, RBL 39. REPLACED FLOOR SUPPORT WEB UPPER CHORD BETWEEN BS 1087 TO BS 1109, RBL 39 IAW B767 SRM 51-40-02-0G, FIGS 3, 8 & 12.SDR USAA2013011500008Failsafe · crackedC4 CHECK - CRACK ON RIGHT FUSELAGE FAIL SAFE STRAP AT BS 959, RBL 92. REPAIRED RIGHT FUSELAGE FAIL SAFE STRAP AT BS 959, RBL 92 IAW EA 131979.SDR USAA2013011500007Failsafe · crackedC4 CHECK - CRACK ON LEFT FUSELAGE FAIL SAFE STRAP AT BS 959, LBL92. REPAIRED LEFT FUSELAGE FAIL SAFE STRAP AT BS 959, LBL92 IAW EA 131979.
Back to N256AY, cancelled Feb 5, 2022