N6714Q
Service difficulty reports · 149
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 = 'N6714Q' 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 = 'N6714Q' 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 DALA2021042702434Warning Message · false activationSHIP 6714- MISC/DE- DUE TO FUEL CONFIG EICAS MESSAGE. INITIAL CORRECTIVE ACTION: RAN MAIN TANK PUMPS FOR 15 MINUTES WITH NO TRANSFER NOTED. TRANSFERRED FUEL FROM CENTER TO RT & LT MAIN TANKS. QUANTITY REMAINED STABLE. OK FOR SERVICE. FOLLOW UP ACTION: REPLACEDSDR DALA2021040702055Collar · brokenSHIP 6714 R4 DOOR LOCK COLLAR BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED LOCK COLLAR AND CATCH PER B757 AMM 52-11. OPS CHECK GOOD. (4054986)SDR DALA2020041602266Lens · unknownSHIP 6714 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:652. CORRECTIVE ACTION: REMOVED AND REPLACED EXIT IDENTIFIER SIGN PER B757 AMM 33-51. OPS GOOD. (1549218)SDR DALA2020041302247Fitting · unsecureSHIP 6714 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: FND FWD SIDE OF GIRT BAR LOOSE. SECURED GIRT BAR FITTING TO GIRT BAR CKS GOOD REF B757 AMM 25-61. (6982624)SDR DALA2020021421149Battery · unsecureSHIP 6714 WHILE WKG JOB CARD 3351-7001 NUMEROUS EMERG INTERIOR LIGHTS IN THE AFT CABIN INOP. CORRECTIVE ACTION: SECURED BATTERY AT POWER SUPPLY RACK M737. RETEST EMERG LIGHT OPS CKS GOOD. (6488454)SDR DALA2019111306625Window · arced(AIRCRAFT 6714, L/P 6398764) F/O FRONT WINDOW ARCHING AND DELAMINATING THEN MULTIPLE CRACKS. COMPLIUED W/ QRH. CORRECTIVE ACTION: REPLACED 1R WINDOW PER B757 AMM 56-11. ALL THREE TORQUES APPLIED TO 1R WINDOW PER B757 AMM 56-11. SPEED TAPE OVER AERO SEAL AROUNDSDR DALA2019100435714Bottle · no test(AIRCRAFT 6714, L/P 1296282) DURING TEST OF EMERGENCY SCAPE SQUIB RH SIDE DOES NOT TURNED ON (TEST NOT PASS). SUMMARY OF NRC 0627: OFF-WING SLIDE PRESSURE BOTTLE WAS REMOVED PER B 757-200 AMM 25-65-02-004-010 AND INSTALLED SERVICEABLE OFF-WING SLIDE PRESSURE BSDR DALA2019100315668Access Panel · corrodedCORROSION ON FASTENERS COUNTERSINK NR 1 TO 10 ON THE LT WING UPPER SKIN AND LT ENGINE DRAG FITTING. CORROSION ON FASTENERS COUNTERSINK REPAIRED IAW ETI-57-19-102 REV 15, & ER/A 581720-14AD, SECTION I, PERMANENT REPAIR, REV. ORIG.SDR DALA2019100305667Shim · migratedMIGRATION ON SHIM ID #1A WAS NOTED ON MEASUREMENT ID# 2A, AT INBOARD DRAG FITTING PERCARD 5720-01100-0101A, STEP 17. CORRECTIVE ACTION: MIGRATION SHIMS WERE REPAIRED PER ER/A 581720-14AD REV ORIGSECTION 1 AS PERMANENT REPAIR AND ETI-57-19-102 REV 15.SDR DALA2019100393666Doubler · crackedCRACK ON INTERNAL DOUBLER AT LT PYLON, NAC. STA. 114.5 LT SIDE. THE DOUBLER WAS REPAIRED PER ER/A 581756-14 REV.ORG AND ETI-57-19-113REV. 6.SDR DALA2019100395665Failsafe · damagedA HOLE WAS FOUND WITH MORE THAN MAXIMUM DIAMETER ALLOWABLE, .286 OF .275, ON THE FAILSAFE AT THE AFT CARGO EQUIPMENT RACK. THE DIAMETER OF ADJACENT RIVET IS .269" WITH A SPACING OF 1 INCH REGARDING TO HOLE AFFECTED. OUT OF LIMITS, FRAME AT BS 1560 WAS RSDR DALA2019100295646Fitting · damagedDAMAGE FOUND ON LOWER SIDE AND HOLES 7 AND 8 OF LH PYLON FWD INBD DRAG FITTING AFTER REMOVAL. REPAIRED IAW ER/A 581720-14AD REV ORIG SECTION 1 AS PERMANENT REPAIR AND ETI-57-19-102 REV 15.SDR DALA2019100205639Skin · damagedDURING DETAILED VISUAL INSPECTION ON REMOVED FWD INBD DRAG FITTING, PERFORMED IAW ETI-57-19-111 REV 1 STEP 5 AND DAMAGE ON THREE HOLES ADJACENT TO PREVIOUS REAMED HOLES WERE FOUND. REPAIRED IAW ER/A 581720-14AD REV ORIG SECTION 1, PERMANENT REPAIR, AND ETI-SDR DALA2019100295638Shim · migratedMIGRATION ON SKIN PANEL SHIM 1B WAS NOTED ON MEASUREMENT 2F AT OUTBOARD DRAG FITTING IAW CARD 5720-01100-0101A, STEP 18. THE SHIMS WERE REPAIRED IAW ER/A 581720-14AD REV ORIG SECTION 1, PERMANENT REPAIR AND ETI-57-19-102 REV 15.SDR DALA2019100295636Skin · damagedDAMAGE FOUND ON THE WING UPPER SKIN, ADJACENT TO HOLES NR 2 AND 4 OF THE RT ENGINE DRAG FITTING. REPAIRED IAW ETI-57-19-099. REV.9 AND ER/A 581628-14AD REV.ORG.SDR DALA2019100192616Skin · damagedDAMAGE FOUND ON THE COUNTERSINK OF HOLES NUMBER 2, 4, 5 AND 7 AT UPPER SKIN RT ENG DRAG FITTING CLAMP. PERMANENT REPAIR WAS PERFORMED ON WING UPPER SKIN AND RT ENGINE DRAG FITTINGS PER ETI 57-19-099 REV. 9 AND ER/A 581628-14AD REV.ORG. SECTION I.SDR DALA2019100192615Shim · migratedMIGRATION ON SKIN PANEL SHIM ID # 1B WAS NOTED ON MEASUREMENT ID# 2D AT OUTBOARD DRAG FITTING OF THE RH WING, PER CARD. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00493, SHIMS WERE REPLACED PER ER/A 581628-14AD REV ORIG, AND ETI-57-19-099 REV 9.SDR DALA2019100197614Shim · migratedMIGRATION ON SKIN PANEL SHIM ID# 1A WAS NOTED ON MEASUREMENT ID# 2B AT INBOARD DRAG FITTING OF THE RH WING, PER CARD 5720-01100-0101B, STEP 17. (RH-MOT 2). CORRECTIVE ACTION: SUMMARY OF NRC S/N 00492, SHIMS WERE REPLACED PER ER/A 581628-14AD REV ORIG, AND ETI-SDR DALA2019100195613Skin · corrodedCORROSION ON FASTENERS COUNTERSINK NBR 1 TO 10 AT RH WING UPPER SKIN AND RH ENGINE DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NR 00443 PERMANENT REPAIR WAS PERFORMED ON WING UPPER SKIN AND RH ENGINE DRAG FITTINGS PER ETI 57-19-099 REV. 9 AND ER/A 581628-14AD SDR DALA2019092805585Skin · corrodedSHIP 6714 AWR, AD, A.A.: CORROSION ON FASTENER HOLE BORE NBR 2 AT RH WING UPPER SKIN AND RH ENGINE DRAG FTG. CORRECTIVE ACTION: SUMMARY OF NR 00442 PERMANENT REPAIR WAS PERFORMED ON WING UPPER SKIN AND RH ENGINE DRAG FITTINGS PER ETI 57-19-099 REV. 9 AND ER/A SDR DALA2019092505579Skin · debonded(AIRCRAFT 6714, L/P 1285570) 1 DISBOND WAS FOUND OF 20" X 19" ON L1 DOOR CUTOUT AT FWD UPPER CORNER IN REFERENCE WORK CARD 5331-01232-02G STEP 5.B.(2). CORRECTIVE ACTION: DISBOND AREA WAS BONDED AND REPAIR PERMANENT WAS PERFORMED PER ER/A 581555-14AD REV. ORG,SDR DALA2019092105486Skin · dented(AIRCRAFT 6714, L/P 1280728) DENT ON EXTERNAL FUSELAGE SKIN STA 1473 APPROX BTW S-27R (FUS). DENT ON EXTERNAL FUSELAGE SKIN STA 1473 APPROX BTW S-27R WAS REPAIRED PER ER/A 581527-14 REV ORIGINAL AND ETI-57-19-101 REV 2. MAINTENANCE REQUERIMENTS WERE VERIFIED ASDR DALA2019092105484Skin · dented(AIRCRAFT 6714, L/P 1280610) FROM MON 36, LOG 2167125: TWO ADJACENT DENTS CLOSE TO MON DENT LOG # 2167125 AND .800" CLOSE TO PREVIOUS DOUBLER REPAIR STA 619 TO 626 BTW ST 16L AND ST18L. FUS. SUMMARY OF NRC S/N 00515 LT FUSELAGE SKIN FROM STA 590 TO STA 660 BTWSDR DALA2019092105449Panel · corroded(AIRCRAFT 6714, L/P 1279781) CORROSION ON RT SIDE PANEL FROM STA 1440 TO 1530 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL: 2 RT SIDE PANEL FROM STA 1440 TO 1530 AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02 PAR 7.SDR DALA2019092005448Structure · corroded(AIRCRAFT 6714, L/P 1279282) AWR HIDDEN CORROSION: DURING REMOTION OF AFT CARGO LOWER SILL (SIDE PANEL), WAS FOUND CORROSION AT INNER CHORD (LOWER FACE) BTW STA 1380 TO 1440, IN REF TO NRC 00356. CORRECTIVE ACTION: SUMMARY OF NRC 456 INNER CHORD (LOWER FACE) BSDR DALA2019092005446Floorbeam · corroded(AIRCRAFT 6714, L/P 1279064) CORROSION OUT OF LIMIT ON FLOORBEAM STA 1640 BTW LBL 32 TO RBL 20 AT FLOOR STRUCTURE WET AREA. CORRECTIVE ACTION: CORROSION LEVEL 2. CORROSION ON FLOORBEAM STA 1640 BTW LBL 32 TO RBL 20 AT FLOOR STRUCTURE WET AREA WAS REPAIRED PER SDR DALA2019091805419Mechanism · out of adjust(AIRCRAFT 6714, L/P 1275787) REQUEST. DURING TEST EMERGENCY POWER ACTUATION CABLE, LOWER TORQUE TUBE ON 1 LH DOOR WAS FOUND 180 GRADE INVERTED IN REFERENCE AMDS 5211-3001-1L STEP 4. (PTAS). MODE SELECT LOCKOUT MECHANISM WAS ADJUSTED PER AMM 52-11-20-825-001. CSDR DALA2019091705397Repair · worn(AIRCRAFT 6714, L/P 1272819) INITIAL INSPECTION: WEAR ON PREVIOUS REPAIR TO NR1 PYLON STA 102 FAN COWL SUPPORT WEB RT SIDE. SUMMARY OF NRC 00437:PREVIOUS REPAIR ON NR 1 PYLON STA 102 WAS REPLACED PER EA: 06-462518-14 REV A.SDR DALA2019091405365Panel · corroded(AIRCRAFT 6714, L/P 1269612) AFTER CORROSION REMOVAL A CRACK WAS FOUND ON RT SIDE PANEL STA 1617 AT AFT CARGO COMPARTMENT. RT SIDE PANEL STA 1617 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-00-53 REP 2.SDR DALA2019091305338Structure · corroded(AIRCRAFT 6714, L/P 1267733) EXFOLIATION CORROSION ON FLOOR STRUCTURE, STA 436, LBL 67 AT PASSENGER CABIN (FWD WET AREA). SUMMARY: OF NRC. 00242 CORROSION LEVEL 2, FLOOR STRUCTURE, (CHORD) STA 436, LBL 67 AT PASSENGER CABIN WAS REPLACED PER SRM 51-40-02 PAR.SDR DALA2019091105306Floor Support · corroded(AIRCRAFT 6714, L/P 1265419) AWR CORROSION OUT OF LIMITS ON FLOOR STRINGERS STA 1460 TO STA 1480 RBL AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. OUT OF LIMITS ON FLOOR STRINGERS STA 1460 TO STA 1480 AT AFT CARGO COMPARTMENT WERE REPAIR PER SRM 53-00-53 REP 1.SDR DALA2019091105285Panel · corroded(AIRCRAFT 6714, L/P 1265182) INITIAL INSPECTION: CORROSION ON LT SIDE PANEL FROM STA 1310 TO 1410 AT AFT CARGO COMPARTMENT.(ACP 0600-155-01Z).(C2). CORRECTIVE ACTION: CORROSION LEVEL 2, LT SIDE PANEL FROM STA 1310 TO 1410 AT AFT CARGO COMPARTMENT WAS REPLACED SDR DALA2019091105284Panel · corroded(AIRCRAFT 6714, L/P 1265179) AWR, CORROSION OUT OF LIMITS ON LT SIDE PANEL STA 1551 AT AFT CARGO COMPARTMENT (REF NRC 00351) (C2). SUMMARY: IN REFERENCE NRC 00536, CORROSION LEVEL 2: SIDE PANEL STA 1551 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-00-53 RESDR DALA2019091105283Floor Support · corroded(AIRCRAFT 6714, L/P 1265166) INITIAL INSPECTION: CORROSION ON STRINGERS (FLOOR SUPPORTS) 6EAS STA 1510 RBL/LBL AT AFT CARGO COMPARTMENT. (ACP 0600-155/156-01Z). (C2). CORRECTIVE ACTION: CORROSION ON STRINGERS (FLOOR SUPPORTS) 6EAS STA 1510 RBL/LBL AT AFT CARGOSDR DALA2019090905270Panel · out of limits(AIRCRAFT 6714, L/P 1261563) LT SIDE PANEL OUT OF LIMITS FROM STA 605 TO STA 608 AT FWD CARGO COMPARTMEN. (C1), REASON FOR RE-WRITE, WRONG PROCESS ON WORK PERFORMED. LIMITS FROM STA 605 TO STA 608 AT FWD CARGO COMPARTMENT. (C1), REASON FOR RE-WRITE, WRONG PROCSDR DALA2019090905252Strap · cracked(AIRCRAFT 6714, L/P 1261677) INITIAL INSPECTION: CRACKED METALLIC STRAP ON MAIN DECK FLOOR STRUCTURE STA Y=1660 RBL=26 AT AFT OF AFT CARGO COMPARTMENT (CCT) (2020-2379). SUMMARY OF NRC 00381-METALLIC STRAP ON MAIN DECK FLOOR STRUCTURE STA Y=1660 RBL=26 WAS REPSDR DALA2019090805250Splice · corroded(AIRCRAFT 6714, L/P 1260631) AWR HIDDEN CORROSION: DURING REMOTION OF AFT CARGO LOWER SILL (SIDE PANEL), WAS FOUND CORROSION ON SPLICE UNION STA 1380 (1 EA) STA 1440 (1 EA), IN REF TO NRC 00356. SUMMARY: IN REFERENCE NRC 00461: SPLICE (2 EA) AT STA 1380 AND ATSDR DALA2019090805249Door Sill · corroded(AIRCRAFT 6714, L/P 1260619) INITIAL INSPECTION: CORROSION ON LOWER SILL FROM STA 1380 TO 1440 AT AFT CARGO COMPARTMENT. (ACP 0600-156-01Z).(C2). SUMMARY: IN REFERENCE NRC 00356; LOWER SILL FROM STA 1380 TO 1440 WAS REPLACED PER SRM 51-40-02 PAR 4 AND 7.SDR DALA2019090705222Strap · cracked(AIRCRAFT 6714, L/P 1258484) INITIAL INSPECTION: CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA 372, LBL 26. (FWD WET AREA). SUMMARY: IN REFERENCE NRC 00236: CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA 372, LBL 26 WAS REPAISDR DALA2019090405167Floor Support · corroded(AIRCRAFT 6714, L/P 1254174) AWR HIDDEN DAMAGE: CORROSION OUT LIMITS ON RT FLOOR SUPPORTS BTW STA 1661-1681 AND RBL 56 AT AFT WET AREA. IN REFERENCES NRC 00465 (2020-2441). AREA IS OUT OF LIMITS PER SRM 53-60-15 ALLOWABLE DAMAGE 1 FIG. 101 NOTE B DET. VI. EQUISDR DALA2019090305166Strap · cracked(AIRCRAFT 6714, L/P 1253425) INITIAL INSPECTION: CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA 375, LBL 46. (FWD WET AREA). SUMMARY: OF NRC 00237. CRACK ON METALLIC STRAP AT PASSENGER CABIN FLOOR STRUCTURE, STA. 375, LBL 46. WAS REPAIRED PER,SDR DALA2019090305142Floor Support · corroded(AIRCRAFT 6714, L/P 1253004) INITIAL INSPECTION: CORROSION ON LT FLOOR SUPPORTS BTW 1640-1681 AND LBL 56 AT AFT WET AREA. (AMDS 2020-2441). AREA ARE OUT OF LIMITS PER SRM 53-60-15 ALLOWABLE. LT FLOOR SUPPORTS (2EA) BTW 1640-1681 AND LBL 56 WERE REPLACED PER SRSDR DALA2019083105125Doubler · corrodedSHIP 6714 INITIAL INSPECTION. CORROSION ON PREVIOUS DOUBLER REPAIR ON WEB STA 1718 RBL 3 AT PASSENGER FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00395: DOUBLER WAS REPLACED PER SRM. (1248370)SDR DALA2019083105124Doubler · corrodedSHIP 6714 INITIAL INSPECTION. CORROSION ON PREVIOUS DOUBLER REPAIR ON WEB STA 1681 LBL 27 AT PASSENGER FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00394: DOUBLER WAS REPLACED PER SRM. (1248358)SDR DALA201906203678Sign · detachedEXIT SIGN CENTER AISLE ROW 20 DAMAGED. RESECURED EXIT SIGN AT ROW OPS CK GOOD.SDR DALA2019042542643Sensor · out of limitsSHIP 6714 R WING SLIDE WARNING LIGHT EICAS MSG ILLUMINATED ON FINAL TO RUNWAY. STAYED ON FOR 1 MINUTE THEN WENT OUT. CORRECTIVE ACTION: FOUND RIGHT OFF-WING SLIDE DOOR SENSOR (S10374) NEAR INDUCTANCE OUT-OF-LIMITS LOW (5.0 MH). ADJUSTED SENSOR TO GET 5.4 MH PESDR DALA2019041752494Lens · missingEXIT SIGN LEN MISSING R2 DOOR. REPLACED LEN PER B757 AMM 33-51. OK FOR SVC . (LP# 5828808)SDR DALA2019040902358Warning Message · false activationAFTER EXTENDING LNDG GEAR ON FINAL, GOT A "R SLIDE DOOR" EICAS MSG. IT EXTINGUISHED AS WE SELECTED LNDG FLAPS 25. INSPECTED RT OVERWING SLIDE ASSY AND DOORS. NO TROUBLE FOUND. COULD NOT GET MSG TO REAPPEAR. (5824586)SDR DALA2019032001857Plate · missingSHIP 6714 DURING GIRT BAR INSP /LUBE FOUND R4 DOOR ONE STOP FITTINGS BEARING PLATE MISSING. CORRECTIVE ACTION: INSTALLED BEARING PLATE IAW AMM 52-11. (5824508)SDR DALA2019031801803Warning System · false activationSHIP 6714 RIGHT WING SLIDE EICAS MSG. UPON GEAR EXTENSION FOR APPROXIMATELY:10. CORRECTIVE ACTION: NO FAULTS FOUND. VERIFIED OVER WING SLIDE SYS. (9550490)
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