N649DL
Service difficulty reports · 209
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 = 'N649DL' 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 = 'N649DL' 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 DALA2016042803540Floor Skin · corrodedFLOOR SKIN CORRODED STA 1715 BL 0. REMOVED CORROSION, BS 1715, BL-0 AFT DECK PLATE IAW SRM, FOUND OUT OF LIMITS. R & R FLOOR SKIN AFT DECK PLATE IAW SRM.SDR DALA2016042803539Seat Track · damagedMAIN CABIN SEAT TRACK HAS GOUGES AND SCRATCHES BETWEEN BS 630-780, LBL 22. REMOVED DAMAGE AND EVALUATED MAIN CABIN SEAT TRACK BETWEEN BS 630-780, LBL 22 MAXIMUM ALLOWABLE DAMAGE IS .060 DAMAGE FOUND TO BE .211 AND OUT OF LIMITS IAW SRM. REPLACED SEAT TRACK SDR DALA2016042803538Strap · chafedCABIN BS 690 AT RT STR 11 INT STRAP HAS DEEP AFT END CHAFED AT DOOR FRAME. REMOVED DAMAGE FROM CABIN BS 690 RT INSTALLATION STRAP IAW SRM AND IS OUT OF LIMITS IAW SRM. R & R STRAP IAW SRM & DWG.SDR DALA2016051404006Floorbeam · corrodedFLOORBEAM CORRODED BS 1640, RBL 52. FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED IAW SRM, INSTALLED T-CHORD AND REPAIR ANGLES IAW SRM 51-40-02 AND SRM & COMPLIED WITH ER/A 545017-14 REV:O.SDR DALA2016042703534Seal · damagedNR 1 ENGINE INBD FIRE SEAL PREVIOUS REPAIR CHAFE FWD OF FWD T/R HINGE. REMOVED DAMAGED DOUBLER REPAIR AND FILLER AT NR 1 ENGINE INBD FIRE SEAL FWD T/R HINGE IAW SRM. FABRICATED NEW DOUBLER REPAIR IAW EA 06-462518-14 INSTALLED REPAIR PART IAW EA 06-462512-14.SDR DALA2016042703532Floorbeam · corrodedFLOORBEAM CORRODED BS 1640, RBL 52. DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED PREVIOUS REPAIR IAW SRM AND CUT OUT DAMAGE IAW SRM. FABRICATED REPAIR AND INSTALLED IAW SRM.SDR DALA2016042703529Cusp Web · corrodedCUSP WEBS AFT OF BULKHEAD BS 996 AND RBL 60 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-40-02 AND DWG.SDR DALA2016042703525Floor Support · corrodedFLOOR SUPPORT CORRODED BS 1660-1680, LBL 54. FOUND TO BE 100 PERCENT MATERIAL LOSS AND OUT OF LIMITS IAW SRM. R & R THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG REV B ORIG.SDR DALA2016042703524Floorbeam · corrodedFLOOR ANGLE BLOWN OUT BS 1720, RBL 52. UPON FURTHER INVESTIGATION FOUND TEE FITTING TOTALLY EXFOLIATED. DAMAGE OUT OF LIMITS. REMOVED TEE FITTING IAW SRM 51-40-02. LOCATED AND DRILLED THE NEW TEE FITTING IAW SRM AND B DWG, REV F. INSTALLED THE NEW TEE FITSDR DALA2016042703523Seat Track · corrodedMAIN CABIN, SEVERAL AREA'S OF THE CROWN AND INSIDE TRACK HAVE WEAR MARK'S SCRATCHES AND CORROSION LBL 45, BS 377-440. BLENDED AREA AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW DWG REV 4.SDR DALA2016042703369Cusp Web · corrodedCUSP WEBS BETWEEN BS 1020 AND 1040 AND LBL 60 HAS CORROSION. R & R THE CUSP WEB IAW DWG 144N5140, REV A.SDR DALA2016042503365Cusp Web · corrodedPASSENGER CABIN LT CUSP UPPER WEB IS CORRODED AT FS 1178, LBL64. REMOVED CORROSION AND EVALUATED MAIN CABIN LT CUSP WEB AT BS 1178, LBL 64 ORIGINAL .063 LOSS .028 REMAINING .035 AND OUT OF ALLOWABLE LIMITS IAW SRM 51-10-02 AND 53-40-13. R & R CUSP WEB IAW SRMSDR DALA2016042303323Floor Support · corrodedFLOOR SUPPORT CORRODED BS 1660-1681, RBL 52. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMVOED AND INSTALLED FLOOR SUPPORT IAW SRM.SDR DALA2016042303322Fitting · corrodedFLOOR FITTING BS 1720, RBL 50 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW FITTING IAW SRM.SDR DALA2016041603004Floor Support · corrodedMAIN CABIN, CORROSION ON FLOOR SUPPORT AT L-1 DOORWAY, BETWEEN 345-365, LBL - 62. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM.SDR DALA2016052004078Skin · dentedMULTIPLE DENTS LOCATED BETWEEN FS 1380-1440, L29L. COMPLIED WITH ER/A 545021-14, REV: ORIGINAL AT FS 1380-1440 BETWEEN L29L & L29R.SDR DALA2016022301349Lamp · inoperativeL1, L2 AND R3 EXTERIOR EMERGENCY SLIDE LIGHTS INOPERATIVE. REPLACED THE LAMPS IAW MM TASK 33-51-06-962-001-001. OPS CHECK NORMAL IAW AMM SUBTASK 712-048-001.SDR DALA2016022301346Lens · looseL1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT LENS LOOSE. R & R L1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT LENS ASSY IAW SUBTASKS 032-003-001, 032-002-001, 432-038-001, 822-039-001, AND 432-040-001.SDR DALA2016020100804Stringer · corrodedCORROSION FOUND ON STRINGER 28R, BS 1600. REPAIRED IAW ER/A 52229 2-14. REPAIR APPROVAL LIMITED TO 12 MONTHS VALIDITY. DTE REQUIRED WIT HIN 12 MONTHS. DEFER TO M-CHECK VISIT FEB 2016. GVI WAS ACCOMPLISHED WITH NO DISCREPANCIES FOUND. OK TO MAINTENANCE FESDR DALA2014102905838Guard · damagedEMERGENY EXIT LIGHT SWITCH ON P11 GUARD INOPERATIVE. REPLACED GUARD AS REQUIRED, OPS NORMAL IAW AMM 33-51.SDR DALA2014102305725Skin · corrodedCORROSION WAS FOUND ON THE OVERWING ESCAPE HATCH CUTOUTS CUB STRAP AT BS 960 AND S15L, REPAIRED IAW ER/A 471189-14, REV B.SDR DALA2016041303684Skin · crackedA CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 1640, AT THE UPPER FWD CORNER OF THE OUTFLOW VALVE CUT OUT. ER/A 471888-14 AUTHORIZED REPAIR. COMPLIED WITH SECTION II OF ERA 471888C-14, REV C IAW NDTM PT 6, 53-00-06 AT BS 1640, STR 22-24L WITH NO DEFECTS NOTED.SDR DALA2014070703904Floor Support · unknownAFT FLOOR SUPPORT, LBL 7.55 BS 1500-1640. REPLACED AFT FLOOR SUPPORT IAW SRM.SDR DALA14002000649Battery Pack · inoperativeR4 DOOR, EMERGENCY POWER RESERVOIR FAILED INSPECTION. REPLACED EMERGENCY POWER RESERVOIR.SDR DALA1302210649Structure · damagedON WALK AROUND FOUND NR 1 ENG INBD FAN COWL. DELAMINATED ON INBD LOWER LEADING EDGE. APROX 3 IN X 3 IN DELAMINATION. REMOVED RT FAN COWL. WIP 644787. APPLIED PERMANENT REPAIR IAW SRM 51-70-17, PARA 4GT. REINSTALLED RT FAN COWLINGS.SDR DALA1017860649Unknown · odorFOUR HOURS INTO FLIGHT AND CRUISING AT FL 340, AN ELECTRICAL, CHEMICAL ODOR DEVELOPED IN THE COCKPIT. FLIGHT CREW DONNED O2 MASKS, DIVERTED, DECLARED EMERGENCY, AND LANDED UNEVENTFULLY. MX REPLACED THE L1 WINDOW, L1 WINDOW HEAT CONTROLLER, AND THE L1 WINDOW HSDR DL757081788Cusp Web · corrodedSTA 968 AT STR 17L CUSP WEB HAS AREA OF HEAVY CORROSION. REPLACE CUSP WEB.SDR DL757081787Skin · gougedPERM REPAIR ON ERA 384204-14 STA 420 BELOW STR 22R. REPAIR PER ERA.SDR DL757081786Skin · dentedAFT FUSE SKIN DENT RT STA 1763 S-27R TO S 28R. REPAIR PER SRM 53-00-01 FIG 201 REP 2.SDR DL757081785Skin · dentedLT FUSELAGE SKIN AT STA 600-640 BETWEEN S 16L TO 18L HAS SEVERAL DENTS AS MARKED. REPAIRED PER ERA 471873-14 REV O.SDR DL757081784Skin · dentedDURING HMV, FUSELAGE SKIN DENTS AND OIL CANNING WERE FOUND AT BETWEEN STA 1701 TO 1720 AND S-15L AND S-17L. THE DENTS WERE APPROVED AS IS AND THE OIL CANNING SKIN WAS CUT OUT AND REPAIRED PER BOEING REPAIR INSTRUCTIONS.SDR DL757081783Skin · crackedDURING HMV, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 1640 AT THE UPPER FWD CORNER OF THE OUTFLOW VALVE CUTOUT. THE DAMAGE WAS REPAIRED WITH A REPAIR DOUBLER PER BOEING REPAIR INSTRUCTIONS.SDR DL757081782Floorbeam · damagedDURING HMV, DAMAGE WAS FOUND ON AN UNDOCUMENTED REPAIR TO THE STA 760 FLOORBEAM WEB AND UPPER CHORD. THE UNAPPROVED REPAIR WAS REMOVED AND A NEW UPPER CHORD SPLICE WAS INSTALLED PER SRM AND BOEING REPAIR INSTRUCTIONS.SDR DL757081781Doubler · corrodedDURING HMV, CORROSION WAS FOUND ON THE OVERWING ESCAPE HATCH CUTOUT REINFORCING STRAP AT STA 960 AND S-15L. THE CORROSION WAS BLENDED AND A REPAIR DOUBLER WAS INSTALLED PER BOEING REPAIR INSTRUCTIONS.SDR DL757081780Spar · damagedFWD SPAR UPPER CHORD OVER SIZED HOLES FROM FACTORY. CLEANED HOLE NDT, INSTALLED OVERSIZED FASTENERS.SDR DL757081776Strap · corrodedDURING HMV, CORROSION WAS FOUND ON A REINFORCING STRAP AT THE OVERWING ESCAPE HATCH CUTOUT AT STA 960 ON THE LT SIDE. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED PER BOEING REPAIR INSTRUCTIONS.SDR DL757081765Skin · damagedDURING HMV AT SAA, A TOTAL OF SIX DENTS AND TWO GOUGES WERE FOUND IN THE EXTERNAL SKIN BETWEEN STA 600 AND 640 AND S-16L AND S-18L. THREE DENTS AND THE TWO GOUGES WERE FOUND TO BE ACCEPTABLE AFTER BLENDING AND TREATING AND THREE DENTS WERE TRIMMED OUT AND REPSDR DL757081746Frame · corrodedAFT CARGO PIT FRAME STA 1500 AT S25L. REPAIRED AS PER SRM 53-00-07 REPAIR 5 AT SAA ON NON-ROUTINE 81608560001.SDR DL757081743Frame · dentedAFT CARGO PIT FRAME STA 1500 AT S25L DENT. REPAIRED IAW SRM 53-00-07 REPAIR NR 5 AT SAA ON NON ROUTINE 81608560001.SDR DL757090124Skin · canningRT FUSELAGE SKIN 5 INCHES FORWARD OF STA 1480 AND 4 INCHES BELOW STR 16R DENT IS OIL CANNING. REPAIRED PER 53-00-01 DATA RETRIEVAL SUBMITTED.SDR DL75K050631Skin · damagedTHE FUSELAGE SKIN AT BS 686, STR 2R HAS A LIGHTNING STRIKE NEXT TO FASTENER. SKIN DAMAGE WAS REMOVED STRINGER WAS REINFORCED, AND A DOUBLER WAS INSTALLED ON THE SKIN PER ER/A 451161-14.SDR DL75K050324Line · leakingLT HYD SYS FAILURE. QUANITY DROPPED TO 1.6. GEAR AND FLAPS EXTENDED NORMALY. REPAIRED LEAK.SDR DL75K040253Piston · shearedLANDING GEAR OVERRIDE HANDLE MOVING IN FLT. FOUND RT TRUCK TILT ACUATOR PISTON BROKE. REPLACED ACTUATOR.SDR DL757021442Door Frame · corrodedCORROSION REPAIR, THE OUTER CHORD OF THE C1 DOOR CUTOUT LOWER SILL BEAM WAS FOUND CORRODED AND REQUIRED REPLACEMENT. TO FACILITATE THE REPLACEMENT, THE FS 620 FRAME WEB AND OUTER CHORD WERE CUT BETWEEN STRINGERS 25R-26R AND THE LOWER PORTIONS REMOVED. THE SISDR DL757021423Door Frame · corrodedCORROSION REPAIR, THE INNER CHORD OF THE FS 729 FRAME OF THE L2 DOOR OPENING WAS FOUND WITH CORROSION ON THE INBD FLANGE AT WL 212. THE CORROSION WAS REMOVED WITH A TRIMOUT TO THE FLANGE. THE TRIMOUT WAS REPAIRED WITH A REPAIR ANGLE PER THE B757 SRM AND ER/ASDR DL757020400Fitting · crackedDURING INSPECTION THE NR 1 PYLON STRUT ATTACH MIDSPAR FITTING INBOARD FITTING OUTBOARD LUG A CRACK INDICATION WAS NOTED. THE LUG WAS OVERSIZED TO REMOVE CRACK INDICATION. REPAIRED PER ER/A 389368-14, REV A.SDR DL757011943Wire Harness · brokenEMERGENCY PATH LIGHT AT 22DEF INOP. REPAIRED BROKEN WIRING HARNESS, CHECKS OK.SDR DL757011889Battery Pack · dischargedR3 EXIT LIGHT DOES NOT ILLUMINATE. REPLACED BATTERY PACK, OPS CK. GOODSDR DL757011833Power Supply · dischargedLAST EIGHT ROWS OF COACH CLASS EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY CHECKS OK.SDR DL757011690Engine · failedNR 2 ENG LOST OIL PRESS ON T/O ROLL. REPLACED ENGINE.
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