N399DA
Service difficulty reports · 97
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 = 'N399DA' 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 = 'N399DA' 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 DALA2026082404799Cover · missingCREW REPORTS OVERWING EXIT DOOR HANDLE MISSING. REINSTALLED COVER IAW AMM 52-22. (8621846) AIRCRAFT WAS GROUNDEDSDR DALA2026081804722Sign · detachedEMERGENCY EXIT SIGN (AFT, OVERHEAD) KNOCKED OFF IN BOARDING PROCESS. RESECURED SIGNS PER B737 AMM 33-51. (8621818) AIRCRAFT WAS GROUNDEDSDR DALA2026070703973Battery Pack · no testDURING SERVICE CHECK FOUND SEATS 19-22 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER M1671 PER B737 AMM 33-51. CHECKS GOOD AFTER. (8091671) AIRCRAFT WAS GROUNDEDSDR DALA2025112508588Battery Pack · inoperativeEMERGENCY LIGHTS ROW 11-15 NOT ILLUMINATING. R & R BATTERY PACK (M1676) REF B737 AMM 33-51. OPS CHK GOOD.SDR DALA2025111008219Shutoff Valve · bypassingDECLARED EMERGENCY AND DIVERTED TO ONT DUE TO FLT CONTROL 'B' LOW PRESSURE LIGHT ILLUMINATED. FOUND SYSTEM 'B' FLIGHT CONTROL SHUTOFF VALVE BYPASSING. REPLACED SAME. OPS CHECK GOOD.SDR DALA2025091806864Case · bird ingestionRETURNED TO MIA DUE TO RIGHT ENGINE BIRD STRIKE AFTER TAKEOFF. MAINTENANCE FOUND MULTIPLE FAN BLADES AND FAN CASE DAMAGED. FAN CASE DAMAGE EXCEEDS B737AMM LIMIT. ENGINE CHANGE ON LOG PAGE 1199194.SDR DALA2025021301121Seat · loose(LOG 6912038) DURING CHECK, FOUND SEAT 15DEF ROW SEAT ASSY LOOSE FROM TRACK. TIGHTENED LOOSE SEAT ASSY HARDWARE PER B737 AMM 25-22. OK FOR SVC.SDR DALA2024100409691Light · inoperative(LOG 6101623) LT AFT VERTICAL EMERGENCY EXIT DOOR SIGN LIGHT INOP. INSTALLED AFT LEFT EXITS DOOR LIGHT ASSY PER B737 AMM 33-51.OPS CHK GOOD.SDR DALA2024071007007Trim Panel · corroded(LOG 0438104) CORROSION ON TRIM UNDER OF THE DOOR ACCESS A423 AT GALLEY 4. TRIM UNDER OF THE DOOR ACCESS A423 AND A417 AT GALLEY 4 WERE FABRICATED AND INSTALLED PER ER/A NO. 619100-14.SDR DALA2024071007006Floorbeam · corroded(LOG 0438541) CORROSION OUT OF LIMITS ON FLOOR SUPPORTS BTW STA 727A LBL 13.84 AND RBL 12.5 AND STA 727I RBL 8.1 AND 3.0. FLOOR SUPPORT STA 727A LBL 13.84 AND RBL 12.5 WERE REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 3 REPAIR 3 AND FLOOR SUPPORT ON STA. 72SDR DALA2024071007005Skin · gouged(LOG 0437697) GOUGE SKIN FROM STA. 727D TO 727E AND BTW S-1L TO S-2L AT INTERNAL FUSELAGE SKIN.FUSELAGE SKIN FROM STA. 727D TO 727E AND BTW S-1L TO S-2L WAS REPAIRED PER ER/A 619002-14AD REV. A SECTION I PERMANENT REPAIR AND FASTENER ON UPPER SKIN FROM STA. 72SDR DALA2024070906959Skin · gouged(LOG 0436172) WHILE ACCOMPLISHING INSPECTION WORK CARD 2330-2048 FOR THE AREA COMMON TO THE DOUBLERS INSTALLED BY THE VIASAT IFE/C RADOME, THE SKIN WAS FOUND GOUGED AT THE FWD TWO ROWS OF THE DOUBLER INSTALLED BETWEEN FS727D AND FS727E AND STRINGERS S-1 AND S-SDR DALA2024070906942Plate · corroded(LOG 0432574) CORROSION ON SIDE PLATE LH/RH SIDE STA 727 TO 887 AT AFT CARGO COMPARTMENT. SIDE PLATE LH AND RH SIDE BTW STA 727 TO 887 AT AFT CARGO COMPARTMENT WERE REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024070506794Web · corroded(LOG 0429660) CORROSION ON WEB AT AREA TO INSTALL SCUFF PLATE OF AFT CARGO COMPARTMENT. SCUFF PLATE OF AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024070506791Floor Support · corroded(LOG 0427486) CORROSION ON FLOOR ANGLE SILL BTW. STA 947.5 TO 995 AND LBL.51 ALSO CORROSION ON FLOOR ANGLE SILL BTW. STA 967 TO 986.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR ANGLE SILL BTW. STA 947.5 TO 995 AND LBL.51, AND FLOOR ANGLE SILL BTW. STSDR DALA2024070506789Floorbeam · corroded(LOG 0427216) CORROSION ON FLOOR BEAM UPPER SURFACE AND FASTENERS HOLES STA 985.5 AND LBL.45 TO RBL.45 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR BEAM STA.986.5 WAS REPAIRED PER B737-800 SRM 53-70-51-2R REPAIR 4.SDR DALA2024070506788Floorbeam · corrodedFLOOR ANGLE: 1EA ( STA. 991 AND RBL.34 TO RBL.45) ( OUT OF LIMITS ) AT PASSENGER CABIN. FLOOR ANGLE STA. 991 AND RBL.34 TO RBL.45 AT PASSENGER CABIN WAS REPLACED PER DWG 147A5700 REV.C AND B737-800 SRM 51-40-02-0G.SDR DALA2024070506787Floorbeam · corroded(LOG 0427149) CORROSION ON FLOOR BEAM BELOW LAVATORY ATTACH FITTING BTW STA. 947.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR BEAM BELOW LAVATORY ATTACH FITTING BTW STA. 947.5 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER B737-800 SRSDR DALA2024070506782Frame · crackedCRACK (0.100IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 907 BTW S-8L & S-9L. FUSELAGE FRAME STA 907 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-03A.SDR DALA2024070506779Support · corrodedCORROSION ON LOWER SILL AT FWD CARGO COMPARTMENT. LOWER SILL AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024070506768Strap · corroded(LOG 0423713) CORROSION ON STABILIZER STRAP (2 EAS) BTW STA 312 AND 344 LBL 12 AT W1. STABILIZER STRAP (2 EAS) BTW STA 312 AND 344 LBL 12 WERE REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024070506766Floorbeam · corroded(LOG 0423548) CORROSION OUT LIMITS ON FLOOR " T" SUPPORT 1EA (BTW. STA.947.5 AND RBL.26.5 TO RBL.49) AT PASSENGER CABIN FLOOR STRUCTURE. PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024070206713Floor Support · corroded(LOG 0422146) CORROSION ON FLOOR SUPPORT BTW. STA.947.5 TO 967 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE. REPAIR FLOOR SUPPORT BTW. STA 947.5 TO 967 AND RBL.51 AT PASSENGER CABIN FLOOR STRUCTURE PER B737-800 SRM 51-40-02-0G.SDR DALA2024070106619Frame · cracked(LOG 0416127) CRACK (0.200IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827 BTW S-8R & S-9R. FUSELAGE FRAME STA 827 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024070106618Frame · cracked(LOG 0416124) CRACK (0.380IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B BTW S-8R & S-9R. FUSELAGE FRAME STA 727B BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024070106617Frame · cracked(LOG 0416116) CRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8R & S-9R. FUSELAGE FRAME STA 500C BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024070106616Frame · cracked(LOG 0415526) CRACK (0.480IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B BTW S-8L & S-9L. FUSELAGE FRAME STA 727B BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024070106615Frame · cracked(LOG 0415377) CRACK (0.280IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727D BTW S-8L & S-9L. FUSELAGE FRAME STA 727D BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024070106614Frame · cracked(LOG 0415367) CRACK (0.120 IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8L & S-9L. FUSELAGE FRAME STA 500A BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024070106613Frame · cracked(LOG 0415333) CRACK (0.520IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L AND CRACK (0.200IN LENGTH) ON FUSELAGE FRAME AT OUTBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L.SDR DALA2024062706557Frame · crackedCRACK (0.680IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R. FUSELAGE FRAME STA 380 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.SDR DALA2024062706556Frame · crackedCRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8L & S-9L. FUSELAGE FRAME STA 500C BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.SDR DALA2024062706555Frame · crackedCRACK (1.000IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 440 BTW S-8L & S-9L. FUSELAGE FRAME STA 440 BTW S-8L & S-9L WAS REPAIRED UNDER CARD(AMDS) 2526-01236-02A.SDR DALA2024062706554Plate · corrodedCORROSION OUT LIMITS ON LH SIDEPLATE FROM STA 500E TO STA 500I AT FWD CARGO COMPARTMENT. SIDE PLATE FROM STA BETWEEN 500 D AND 500 E TO STA 500 I AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 53-00-53-2R.SDR DALA2024062706543Seat Track · corrodedCORROSION OUT LIMITS ON SEAT TRACK STA 520 RBL 25 AT FLOOR STRUCTURE. SEAT TRACK STA 520 RBL 25 AT FLOOR STRUCTURE WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024062106306Beam · corroded(LOG 0404892) CORROSION ON BEAM STA 294 RBL 10 AT W1. BEAM STA 294 RBL 10 AT W1 WAS REPAIRED PER B737-800 SRM 53-10-51-2R.SDR DALA2024062106305Strap · corroded(LOG 0404888) CORROSION ON STABILIZER STRAP BTW STA 312 AND 328 RBL 10 AT W1. STABILIZER STRAP BTW STA 312 AND 328 RBL 10 AT W1 WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024012901304Battery Pack · inoperative(LOG 5081756) FOUND UPPER AND LOWER EXIT LIGHTS AT AFT LEFT DOOR INOP. REMOVED AND REPLACED BATTERY PACK M1673 IAW B737 AMM 33-51.SDR DALA2023051503800Battery Pack · inoperative(LOG 5519314) DURING INSPECTION FOUND SEVERAL AFT CABIN SEAT ROWS EMERGENCY AISLE LIGHTS INOP. R/R BATTERY PACK M1672 REF B737 AMM 33-51. OPS OK.SDR DALA2023041603007Unknown · unknown(LOG 4030192) DURING INSPECTION FOUND ROW 16 SEATS FED ISLE ILLUMINATION EMERGENCY LIGHT INOP. FOUND CONNECTOR UNDER SEAT DISCONNECTED . RECONNECTED AND PERFORMED OPERATIONAL TEST PER B737 AMM 33-51. CHECKS SATISFACTORY.SDR DALA2022102406844Light · inoperative(LOG 9443576) DURING INSPECTION FOUND 17F VERTICLE EXIT LIGHT INOP. REPLACED LIGHT ASSY PN BR9476-G-145-01 REF B737 IPC 33-51-01-06C ITEM 545, REF B737 AMM 33-51-01-201.SDR DALA2022091506145None · none(LOG 2406863) DURING INSPECTION FOUND EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:33D. RESECURED EMERGENCY SEAT MOUNTED LIGHTING AT LOCATION 33D PER B737 AMM 33-14. CHKS OK.SDR DALA2021101106217Transmitter · inoperativeSHIP 3729 -DE- DUE TO FLAPS WOULD NOT EXTEND ON APPROACH. PERFORMED FSEU BITE CHECK FAULT 27-53256 (FLAP 7 SKEW) REPORTED. REPLACED #7 FLAP SKEW SENSOR. REPLACED RIGHT FLAP POSITION TRANSMITTER PRECAUTIONARY DUE TO AHM REPORT. OPS CHECKS GOOD.SDR DALA2021072004081Light · inoperative(LOG 1877386) DURING INSPECTION FOUND EMERGENCY AREA LIGHT (OVERHEAD BIN) AT SEAT ROW 28FED INOP. REMOVED AND REPLACED EMERGENCY AREA LIGHT (OVERHEAD BIN) AT SEAT ROW 28FED IAW B737 AMM 33-51-03-960-802 OPS CHECK GOOD.SDR DALA2021072004080Wire · damaged(LOG 1877385) DURING INSPECTION FOUND EMERGENCY SEAT PATH LIGHTING INOP RH SIDE BETWEEN STA 663 TO STATION 927. REPAIRED EEPL WIRING AT SEAT 28FED AND 33FED, REPLACED FUSES AT POWER SUPPLY M1671, AND PERFORMED OPS CHECK OF THE EEPLS PER B737 AMM 33-51-06, B737SDR DALA201811206706Connector · disconnected(LOG 4855139) EMERGENCY CEILING AREA LIGHTS AT 1AB AND 10ABC INOP DURING WORKCARD 3350-7390 EMERGENCY LIGHT CHECK. TROUBLESHOT SYSTEM FOUND CANNON PLUG D11088 AND D11344 CAP AND STOWED. RECONNECTED PLUGS OPS CHECK GOOD PER WORKCARD 3350-7390.SDR DALA2018090705481Structure · damagedDURING INSPECTION FOUND ELONGATED HOLES ON J22 JUNCTION BOX ASSEMBLY. ELONGATED HOLES ON J22 JUNCTION BOX ASSEMBLY WAS REPAIR PER ETI-37-18-497, REV ORIG AND ERA 571331-14AD REV ORIG.SDR DALA2018090705480Frame · dentedDURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727J FUSELAGE FRAME FREE FLANGE IS DENTED, STR 25R. FRAME STR 23-24RH WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-496 REV 1 AND ER/A 571308-14 REV ORIG.SDR DALA2018090605461Frame · dentedDURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727G FUSELAGE FRAME FREE FLANGE IS DENTED BTW STR 24L. FRAME STR 24L WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-491 REV 2 AND ER/A 571309-14 REV ORIG.SDR DALA2018090605460Frame · dentedDURING INSPECTION FOUND AFT CARGO COMPARTMENT STA 727G FUSELAGE FRAME FREE FLANGE IS DENTED BTW STR 25L. FRAME STR 25L WAS ACCOMPLISHED SECTION I AS PERMANENT REPAIR PER ETI-37-18-491 REV 2 AND ER/A 571309-14 REV ORIG.
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