N714CB, cancelled Oct 15, 2024
Service difficulty reports · 270
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 = 'N714CB' AND deregistration_id = 'N714CB-2024-10-15' 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 = 'N714CB' AND deregistration_id = 'N714CB-2024-10-15' 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 SWAA2021122154114Flap System · faultedON APPROACH SELECTED FLAPS 15 AND THEN 30. AT WHICH TIME WE NOTICED FLAP INDICATOR WAS AT 5. EXC. GO AROUND AND USED QRH ALT FLAP EXT PROCEDURES. PERFORMED FSEU BITE REF FIM 27-51 TASK 801; FAULT HISTORY SHOWED FAULTS 27-52261 AND 27-53280. CLEANED CONNECTORSSDR SWAA2021122053486Panel · elongatedSUPPLEMENTAL INFORMATION: AFT WING-TO-BODY FAIRING PANEL 194E HAS ELONGATED FASTENER HOLES. ; / [01] TRIMMED; DRILLED; AND PAINTED NEW PNL; [02] REMOVED & REPLACED PANEL PER AMM 53-51-21SDR SWAA2021122053205Panel · elongatedCENTER WHEEL WELL PANEL 193D FASTENER HOLES ELONGATED. ; / [01] TRIMMED; DRILLED AND PAINTED NEW PNL; [02] REMOVED &REPLACE PANEL PER AMM 53-51-21SDR SWAA2021092119554Handle · looseAFT ENTRY DOOR SLIDE HANDLE EXPOSED ; / [01] SECURED AFT ENTRY DOOR SLIDE HANDLE IAW AMM 25-66-01SDR SWAA2021092120453Handle · looseAFT ENTRY DOOR SLIDE HANDLE EXPOSED ; / [01] SECURED AFT ENTRY DOOR SLIDE HANDLE IAW AMM 25-66-01SDR SWAA2021061682904Light · inoperativeLH EMERGENCY EXIT SIDEWALL LIGHT INOP ; / OK TO CONTINUE PER MEL 33-2-03 SP1B; RR'D RH OVERWING EXIT SIDEWALL FUSE IAW AMM 33-51-01SDR SWAA2021042967409Light · inoperativeROW 12 DEF SIDEWALL LIGHT INOP ; ROW 12 DEF SIDEWALL LIGHT INOP /SDR SWAA2021040159266Lens · missingEMERGENCY AISLE LIGHT BEZEL/LENS MISSING AT 13DEF / CLEARED ON DMA 0718865 REPLACED MISSING EMERGENCY LIGHT LENS AT SEAT ROW 13DEF IAW AMM 33-51-03 CL NO 74301SDR SWAA2020112331793Linkage · brokenR1 DOOR SLIDE LINKAGE BROKEN. REPLACED LINKAGE, REF MT 725-61-06 AMM 25-66-01.SDR SWAA2021051204424Skate Angle · corroded#2 ENG FWD ENG STRUT FAIRING STRUCTURE INBD SKATE ANGLE HAS CORROSION AT APPROX NAC STA 252-256 UNDER PANEL 441DL. / REPAIRED PER EA 20-154-01219SDR SWAA2020080304426Battery Pack · no testEMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY FUNCTIONAL CHECK AT LOCATION M01669. R&R EMERGENCY LIGHTING BATTERY PACK AND POWER SUPPLY AS PER AMM 33-51-06.SDR SWAA2020072702817Battery Pack · inoperativeEXIT LIGHTS CONNECTED TO M1674 BATTERY PACK DO NOT COME ON / REMOVED AND REPLACED M1674 BATTERY PACK AND OPS CHECKED PER AMM 33-51-06-960-805 CHECKED GOODSDR SWAA2020072702351Housing · damagedAFT ENTRY WAY CENTER EMERGENCY EXIT LIGHT HOUSING IS DAMAGED. / REPLACED AFT ENTRY WAY CENTER EMERGENCY LIGHT HOUSING; OPS CHECK WAS GOOD IAW AMM 33-51-01-960-802. 57193U 23JUL20SDR SWAA2020072700652Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 679 RBL 5 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.SDR SWAA2020072700651Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 683 RBL 2;RBL 9 AT FASTENER HOLES. INBETWEEN STRINGER 1R AND 2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.SDR SWAA2020072700650Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 694;RBL 9 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND STR2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.SDR SWAA2020072700649Skin · corrodedUPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 701; RBL3 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / REPAIRED UPPER EXTERIOR FUSELAGE SKIN PER ATS ER 20-02895; REV IR; PER EA 20-153-01151; REV IR.SDR SWAA2020072797632Frame · corrodedBS 847 FRAME UPPER SURFACE CORRODED. LBL20; WL156. REPAIRED THE FRAME IAW ER20-02837, REV IR, AND EA 20-153-01157, REV IR.SDR SWAA2020072797627Bulkhead Web · corroded***CORROSION*** ON BS 259.5 BULKHEAD WEB WL 207 LBL 10 - RBL 2. / BS 259.5 WEB REPAIRED IAW EA # 20-153-01002 REV IR AND ER # 20-02836 REV IR.SDR SWAA2021080397612Floorbeam · crackedBREAK PANEL IS CRACKED STA 540; RBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 RBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05SDR SWAA2021080397611Floorbeam · crackedBREAK PANEL IS CRACKED STA 540; LBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 LBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05SDR SWAA2020072797614Structure · corroded***CORROSION*** ON AFT CHORD OF BS 259.5 BULKHEAD WL 207 LBL 10-RBL 6. / THE DAMAGE IS REPAIRED PER EA 20-153-01002 REV IR AND ER #20-02836 REV IR. REFER TO NRC U186702 FOR TRACKING.SDR SWAA2020072797613Structure · corrodedCORROSION ON FWD CHORD OF BS 259.5 BULKHEAD, WL 207, LBL 10 - RBL 3. REMOVED AND REPLACED CHORD IAW SRM 51-40-02-0G-0, DWG 141A5133, REV C, AND DWG 141A7430, REV B.SDR SWAA2020072797623Stiffener · corrodedCORROSION ON VERTICAL STIFFENER AT BS 225 RBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS225 RBL5 WL160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED VERTICAL STIFFNER AT BS225 RBL5 WL160 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0;SDR SWAA2020072797624Stiffener · corrodedCORROSION ON VERTICAL STIFFENER AT BS 225 LBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS 225, LBL 5, WL 160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED VERTICAL STIFFNER IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 141A7410.SDR SWAA2020072797602Stringer · corrodedFWD CARGO BAY STRINGER 23R HAS CORROSION AT END OF STRINGER BS536 WL164 RBL46 / REPAIRED STRINGER IN FWD CARGO BAY BS536. STR 23R WL164; RBL46 PER ER 20-02826 REV IR AND EA 20-153-01129 REV IR.SDR SWAA2021081997560Beam · crackedLT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE #1 PYLON IS CRACKED. / REMOVED AND REPLACED LT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE NO 1 PYLON IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-17 59779U 6JUL20SDR SWAA2021081797590Support · corrodedAFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS767 RBL23 WL156 / REMOVED CORROSION DAMAGED FLOOR TO SIDEWALL SUPPORT BS727-767 RBL23 WL156 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORSDR SWAA2021081797589Support · corrodedAFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS847 LBL23 WL156 / EVALUATED CORROSION ON ACB L/H FLOOR TO SIDEWALL SUPPORT; BS727 847; REMOVED .015' FROM ORIG .040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-SDR SWAA2021081797591Splice Strap · corrodedAFT CARGO BAY FLOOR SPLICE STRAP AT BS767+4 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / RECEIVED NEW ACB FLOOR SPLICE STRAP BS767+4 ON PO# 796202. NEW SPLICE STRAP TO BE INSTALLED ON CUST CARD# JPANEL-141-CLOSESDR SWAA2021081797592Splice Strap · corrodedAFT CARGO BAY FLOOR SPLICE STRAP AT BS887 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / EVALUATED CORROSION ON ACB FLOOR SPLICE STRAP; BS887; FOUND TO BE OUT OF LIMITS; DUE TO NO LIMITS IN SRM.51-10-02-0G-0. REMOVED DAMAGED SPLICE STRAP; LOCATED;SDR SWAA2021081597593Support · corrodedAFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO BS867 LBL10 TO WL156 HAS CORROSION / REMOVED AND REPLACED AFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO 867 LBL10 WL156 IAW SRM 51-40-05; SRM 51-40-02; AND AIPC 53-42-51-06.SDR SWAA2021081397594Web · corrodedAFT CARGO BAY WEB BETWEEN BS787 TO BS807 RBL6 WL150 HAS CORROSION / EVALUATED CORROSION ON WEB BETWEEN BS787-807; RBL6; FOUND TO BE OUT OF LIMITS; DUE TO NO LIMITS IN SRM. LOCATED; DRILLED; AND INSTALLED NEW WEB; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 1SDR SWAA2021072997552Bolt · brokenBROKEN NUTPLATE FOR MOUNT BOLT ON DORSAL FIN. / REMOVED AND REPLACED NUT PLATE FOR MOUNT BOLT ON DORSAL FIN IAW SRM 51-40-02-0G-0 AND IPC 55-32-11-02. DWG #174A0101. 59769U 1JUL20SDR SWAA2020072797574Seat Track · corrodedCORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS480 - BS520 LBL45 WL208. MARKED / REMOVED CORROSION AND SEAT TRACK WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. SEAT TRACK WAS FABBED AS PER ATS HFAB-100-307 AND REPLACED IAW SRM 51-40-02SDR SWAA2020072797575Seat Track · corrodedCORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS 480 - 520, RBL 45, WL 208. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G-0.SDR SWAA2020072797598Floor Panel · damagedCABIN FLOOR PANEL 231XF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW CABIN FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A, AND DWG 144A5810-7.SDR SWAA2020072797599Floor Panel · damagedCABIN FLOOR PANEL 241AF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A AND DWG 144A5810-8.SDR SWAA2020072797600Floor Panel · damagedCABIN FLOOR PANEL 241DF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0, PARA 1A, AND DWG 144A5810-9.SDR SWAA2020072797551Skin · corrodedCORROSION ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS 887- BS 996 STR 3L - STR 3R / REPAIRED DAMAGE ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS887-996; STR3L- STR3R PER ER# 20-02823 REV IR AND EA # 20-153-0SDR SWAA2020072703504Floor Skin · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR EA #1-A53-33179 REV IR.SDR SWAA2020012874817Fuse · inoperativeEMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOP. REMOVED AND REPLACED BATTERY PACK AND FUSES FOR EMERGENCY LIGHT POWER SUPPLY M01675 PER AMM 33-51-06.SDR SWAA2020012874775Battery Pack · inoperativeEMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND FUSES FOR EMERGENCY LIGHT POWER SUPPLY M01675 IAW AMM 33-51-06.SDR SWAA2019121739763Slide · out of positionL2 DOOR SLIDE LOOSE AND WAS HANGING ON DOOR. / REPOSITIONED SLIDE PER MT.SDR SWAA2019103138404Lamp · inoperativeR/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.SDR SWAA2019103138403Lamp · inoperativeL/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.SDR SWAA2019100237460Wire · brokenFORWARD LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE, AFT OF THE FORWARD ENTRY DOOR, RETAINING LANYARD. REPAIRED LIGHT PER AMM. R&R LENS RETAINER WIRE PER AMM.SDR SWAA2019100137431Oil System · low pressureINFLIGHT SHUTDOWN, DIVERTED, AND DECLARED AN EMERGENCY, OIL QUANTITY FOR THE NR 2 ENGINE DECREASED TO ZERO, FOLLOWED BY A LOW OIL PRESSURE LIGHT AND OIL PRESSURE DECREASING BELOW 13 PSI FOR 15 SECONDS. FLASHING YELLOW THEN RED. PERFORMED ENGINE SHUTDOSDR SWAA2019091036733Girt Bar · looseR1 DOOR GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.SDR SWAA2022031569917Bracket · crackedLEFT WING FIXED UPPER TRAILING EDGE PANEL CENTER INNER BRACKET CRACKED ABOVE NACELLE STRUT FAIRING / REMOVED AND REPLACED PER SRM 51-40-02.
Back to N714CB, cancelled Oct 15, 2024