N3758Y
Service difficulty reports · 146
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 = 'N3758Y' 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 = 'N3758Y' 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 DALA2026092105264Windshield · arcedLEFT FWD WINDOW HEAT DISPLAYED OVERHEAT CLIMBING THROUGH FL 260. QRH PROCEDURE DID NOT CLEAR. CAPTAIN ALSO WITNESSED ELECTRICAL ARCING ON POWER STRIP IN GLASS. R & R WHCU M321 PER B737 AMM 30-41. R/R #1 WINDOW PER B737 AMM 56-11. OPS CK LK CK GOOD. (9463784) SDR DALA2025061604525Stanchion · cracked(LOG 1018403) WHILE AT SEA, MTC DISCOVERED DAMAGE CONSISTING OF A CRACK RUNNING HORIZONTALLY ACROSS THE INSIDE OF THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-5) OF THE LH NO. 1 FLIGHT DECK WINDOW. REPAIRED PER ERA 623978-14.SDR DALA2025061604523Window Frame · cracked(LOG 1017247) CRACK ON WINDOW FRAME UPPER AFT CORNER AREA #1 RH WINDOW. WINDOW FRAME UPPER AFT CORNER AREA #1 RH WINDOW WAS REPAIRED ERA 619132-14ADTR REV. A.SDR DALA2025061204475Stringer Splice · corroded(LOG 1016117) CORROSION ON STRINGER SPLICE 24LH APPROX. BTW BS=328 TO 300 AT E/E COMPARTMENT. OUTER CHORD (STRINGER SPLICE) BWT STA 294.5 AND STA 325 AT S-23L AND S-24L WAS REPAIRED PER PRI 626655-14 REV.2 AND ER/A 626655-14 REV. ORIGINAL SECTION I: PERMANENT SDR DALA2025060904375Frame · corroded(LOG 1011352) CORROSION WAS FOUND ON FRAMES AT STA 325 AND STA 320 S-24L AT E/E COMPARTMENT. AFTER CLEANING AND FRAME (WEB) STA 320 BTW S-23L TO S-22L WAS REPLACE PER B737-800 SRM 51-40-02-0G.SDR DALA2025060904374Floor Support · corroded(LOG 1011324) SEVERAL AREAS OF CORROSION ON FLOOR SUPPORTS BTW STA 727H TO 827 BTW 25L/26R AT AFT CARGO COMPARMENT. STA 727H TO 727J WAS REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 3 REPAIR 3 AND PER B737-800 SRM 53-00-53-2R PROCEDURE 2 REPAIR 2.SDR DALA2025060604310Plate · corroded(LOG 1005483) CORROSION ON UPPER AN LOWER SURFACE OF SIDE PLATE RH BTW STA 727G TO 907 AT AFT CARGO COMPARMENT. SIDE PLATE BTW STA 727G TO 767 WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060604309Intercostal · corroded(LOG 1005426) CORROSION ON INTERCOSTAL (2 E/AS) 141A8131-32/ 141A8131-17, STRAP (1 E/A)141A8131-24, CLIPS (3 E/AS) ON INTERCOSTAL 141A8131-32, TEE (3E/AS) ON INTERCOSTAL 141A8131-17, BTW BS=325.3 TO 294 AT E/E. INTERCOSTAL (2 E/AS) 141A8131-32/ 141A8131-17,CLISDR DALA2025060504292Plate · corroded(LOG 1003194) CORROSION ON UPPER AN LOWER SURFACE OF SIDE PLATE RH BTW STA 727 TO 727G AT AFT CARGO COMPARMENT. SIDE PLATE RH BTW STA 727 TO 727G AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060504290Plate · corroded(LOG 1003164) CORROSION ON UPPER AN LOWER SURFACE OF SIDE PLATE LH BTW STA 727G TO 847 AT AFT CARGO COMPARMENT. SIDE PLATE LH BTW STA 727G TO 847 AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0GSDR DALA2025060504289Plate · corroded(LOG 1003151) CORROSION ON UPPER AN LOWER SURFACE OF SIDE PLATE LH BTW STA 727 TO 727G AT AFT CARGO COMPARMENT. SIDE PLATE LH BTW STA 727 TO 727G AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060204211Stringer Splice · corroded(LOG 0998309) CORROSION ON LOGITUDINAL LAP SPLICE BTW BS= 28 TO 312 STRINGER 30 AND 29LH AT E/E COMPARTMENT. LOGITUDINAL LAP SPLICE (INTERCOSTAL) BTW BS=328 TO 312 STRINGER 30 AND 29LH AT E/E COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060204210Access Panel · corroded(LOG 0998144) AFTER CLEANING FUEL TANK ACCESS DOORS, SEVERAL CORROSION WAS FOUND ON ACCESS #632HB, RH WING. FUEL TANK ACCESS DOORS #632HB ON RH WING WAS REPLACED PER B-737-800 IPC: 28-11-11-02 ITEM: -140 AND WILL BE INSTALL PER AMDS: 2820-0599.SDR DALA2025060204209Plate · corroded(LOG 0998075) CORROSION ON RH SIDEPLATE FROM STA 500 TO STA 500I FWD CARGO. RH SIDEPLATE FROM STA 500 TO STA 500I FWD CARGO WAS REPLACED PER DGW 143A8126 REV. B AND B737-800 SRM 51-40-02-0G.SDR DALA2025060204207Floor Support · corroded(LOG 0995823) CORROSION ON FLOOR SUPPORT (SHIELD) BTW STA 767 TO 794.3 BTW STRG 25R/26R AT AFT CARGO COMPARMENT. FLOOR SUPPORT (SHIELD) BTW STA 767 TO 794.3 BTW STRG 25R/26R AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025053004156Intercostal · corroded(LOG 0994513) CORROSION WAS FOUND INTERCOSTAL BELOW SIDE PLATE BETWEEN STA 500F AND 500G. INTERCOSTAL BELOW SIDE PLATE BETWEEN STA 500F AND 500G WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025053004152Seat Track · corroded(LOG 0991762) SEAT TRACK OUTBOARD LH SIDE IN STA 500 I + 18 TO 500 I +20 AT CAB. PAX. HAS CORROSION. ORIGINAL THICKNESS AND CROWN IS 0.530IN MINIMUM REMAINING THICKNESS IS 0.502 IN THEREFORE AREA REWORKED IS OUT OF LIMITS AT CPAX. SEAT TRACK OUTBOARD LBL 24.75SDR DALA2025052904132Doubler · corroded(LOG 0989278) CRACKS SEVERAL SECTIONS ON INNER DOUBLER AT EXTERNAL POWER PANEL. SECTIONS ON INNER DOUBLER AT EXTERNAL POWER PANEL WAS REPAIRED PER B737-800 SRM 53-10-15-2R REP. 5.SDR DALA2025052904131Floorbeam · corroded(LOG 0988528) CORROSION ON BEAM W2 STA 947 LBL 50 TO LBL 54 AT CPAX. BEAM W2 STA 947 LBL 50 TO LBL 54 WAS ALTERNATIVE 2 REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.SDR DALA2025052904130Intercostal · corroded(LOG 0988039) CORROSION ON INTERCOSTAL W2 STA 950 LBL 50 AT CPAX. INTERCOSTAL W2 STA 950 LBL 50 AT CPAX WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025052904126Floorbeam · corroded(LOG 0987657) CORROSION ON FLOORBEAM W2 STA 986 LBL 37 TO LBL 39 AT PAX CABIN. FLOORBEAM W2 STA 986 LBL 37 TO LBL 39 AT PAX CABIN WAS REPAIRED PER ER/A 464736-14MA REV.ASDR DALA2025052203963Frame · damaged(LOG 0976311) ACCOMPLISH AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER. ACCOMPLISHED AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02.SDR DALA2025052203962Frame · damaged(LOG 0976303) ACCOMPLISH AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER. ACCOMPLISHED AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02.SDR DALA2025051903824Floor Support · corroded(LOG 0968193) CORROSION ON FLOOR SUPPORT W2 STA 957 RBL 40 AT CPAX. FLOOR SUPPORT (INTERCOSTAL) WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025022401421Seat · unsecure(LOG 6743232) SEAT 33DEF ARE NOT ATTACHED AND LOOSE. OUTBOARD EDGE NOT ATTATCHED. INBOARD EDGE ATTATCHED. REINSTALLED 33DEF SEATROW PER B737 CMM 25-27-48.SDR DALA2025022001337Seat · unsecure(LOG 6743229) SEATS ROW 33DEF NOT SECURED IN FLOOR TRACK. RESECURED ROW 33 DEF SEAT ASSY TO SEAT TRACK PER B737 AMM 25-22.SDR DALA2025020400856Window · cracked(LOG 0789354) CAPT'S #1 WINDOW UPPER OUTBD CORNER CRACKED. REPAIRED PER ERA 623978-14.SDR DALA2025020300794Stanchion · cracked(LOG 0788678) WHILE AT SEA, MTC DISCOVERED DAMAGE CONSISTING OF A CRACK RUNNING HORIZONTALLY ACROSS THE INSIDE OF THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-5) OF THE LH NO. 1 FLIGHT DECK WINDOW. THE CRACK EXTENDS INTO THE VERTICAL SDR DALA2025012100489Transmitter · inoperativeSHIP 3758 -DIV- DIVERSION TO GEG FOR A LEFT ENGINE OIL FILTER BYPASS MESSAGE. CORRECTIVE ACTION: INSPECTED MCD AND SUPPLY POP OUT INDICATOR, ALL NORMAL. MEL 79-00-02 APPLIED. SEA MAINTENANCE INSPECTED FILTER, NO FINDINGS. REPLACED OIL CLOGGING TRANSMITTER.SDR DALA2024082708476Battery Pack · inoperative(LOG 6097603) DURING SERVICE CHECK FOUND A NUMBER OF EMERGENCY LIGHTS INOP. R/R EMERGENCY LIGHT BATTERY IAW B737 AMM 33-51. OPS CHECK GOOD.SDR DALA2024081408158Window Frame · crackedAIRCRAFT 3758, RIGHT #2 WINDOW FRAME DAMAGED DURING THE REPAIR TRIM OUT OF THE #3 WINDOW FRAME. CORRECTIVE ACTION: REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR PARTS PER ER/A 619933-14. (LP 0500284)SDR DALA2024081408157Window Frame · crackedAIRCRAFT 3758, SUPPORT R-3 WINDOW FRAME CRACKED. CORRECTIVE ACTION: REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER ER/A 619933-14. (LP 0500278, 6210954)SDR DALA2024080807915Window Frame · cracked(LOG 6210954) R3 WINDOW FRAME CRACKED. PERMANENT REPAIR TO BE COMPLETED PER ERA 619933-14.SDR DALA2024051605270Battery Pack · inoperative(LOG 4920867) ROW 19-22 EMERGENCY LIGHTS INOP. R/R BATTERY PACK ON POWER SUPPLY IAW B737 AMM 33-51.SDR DALA2024042504703Module · inoperativeSHIP 3758-DE- DECLARED AN EMERGENCY DUE TO AN ANTI-SKID FAIL MESSAGE IN FLIGHT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE AUTOBRAKE VALVE MODULE, AUTOBRAKE CONTROLLER AND THE #2 TRANSDUCER.SDR DALA2023112709713Unknown · unknown(LOG 9969490) RAMP AGENT FOUND FWD CARGO DOOR DENT LOCATION 7 INCH FROM AFT EDGE AND 5 INCH ABOVE DOOR HANDLE. INSPECTED PER B737 SRM 52-30-01-1A. FOUND DENT OUT OF ALLOWABLE DAMAGE LIMITS. PER SRM FWD TO MON FOR DVI FOR CORROSION AND CRACKS AFTER EACH 1500 FLSDR DALA2022111807425Light · faulty(LOG 9033366) DURING FLT. F/A'S NOTICED AN ODOR AT ROW 14, NO VISIBLE SMOKE, ELECTRICAL SMELL. TURNING OFF CEILING NIGHT LIGHTS CAUSED ODOR TO STOP. FOUND O/HEAD CEILING NIGHT LIGHT ABOVE ROW 17 DEF FLIKERING , UPON INSPECTION NOTICED A SLIGHT ELECTRICAL SMELLSDR DALA2022080905432None · none(LOG 2351968) AIRCRAFT SUSTAINED GSE IMPACT DAMAGE DURING LINE OPS IN SJD. SKIN DAMAGE INCURRED ABOVE AND BELOW S-25L JUST AFT OF FS 807. MAINTENANCE REPAIRED DAMAGE PER ERA 589965-14.SDR DALA2022080805399None · none(LOG 2350677) DURING INSPECTION FOUND LH HORIZONTAL STABILIZER LEADING SKIN BETWEEN LE STA 206.23 AND LE STA 221.23 WITH SEVERAL GOUGES. LH HORIZONTAL STABILIZER LEADING EDGE SKIN. LE STA 206.23 AND LE STA 221.28 WAS REPAIRED IAW B737-800 SRM 55-10-01-1A.SDR DALA2022072505096Battery Pack · inoperative(LOG 9297269) DURING INSPECTION FOUND EMERG LTS AT ROWS 21 THRU 25 INOP. REMOVED AND REPLACED BATTERY PACK MO1621 PER B737 AMM 33-51. OPS CK GOOD.SDR DALA2022071504904Battery Pack · inoperative(LOG 9297261) DURING INSPECTION FOUND FWD ENTRY DOOR EMERGENCY LIGHTS NOT ILLUMINATING. REPLACED FWD ENTRY DOOR EMERGENCY BATTERY PACK M1675 IAW B717 AMM 33-51-06. OPS CHK GOOD.SDR DALA2021081904830Trunnion · corroded(LOG 1915688) DURING INSPECTION FOUND NLG RH TRUNNION BUSHING I/B FACE HAS CORROSION AT 8 O CLOCK POSITION. C/W ERA 593425-14 REV O.SDR DALA2021081604703Bushing · corroded(LOG 1909923) DURING INSPECTION FOUND RH MLG FWD TRUNION OB LOWER HOLE BUSHING CORRODED IB AND OB SIDES. REPAIRED PER B737-800 SRM 57-20-90.SDR DALA2021081604702Bushing · corroded(LOG 1909922) DURING INSPECTION FOUND CORROSION FWD TRUNNION BUSHING-CORRODED IB AND OB. REPAIRED PER B737-800 SRM 57-20-90.SDR DALA2021081604700Bushing · corroded(LOG 1909918) DURING INSPECTION FOUND RMLG FWD TRUNNION I/B UPPER BUSHING CORRODED. REPAIRED PER B737-800 SRM 57-20-90.SDR DALA2021081604699Trunnion · corroded(LOG 1909916) DURING INSPECTION FOUND CORROSION LH MLG FWD TRUNNION IB UPPER HOLE ,BUSHING AND FACE. REPAIRED PER B737-800 SRM 57-20-90.SDR DALA2021081604698Bushing · corrodedDURING INSPECTION, FOUND LH MLG BUSHING CORRODED FWD TRUNION OB LOWER HOLE FACE AND BUSHING. REPAIRED PER B737-800 SRM 57-20-90.SDR DALA2021081604697Trunnion · corrodedDURING INSPECTION FOUND CORROSION LH MLG FWD TRUNION OB UPPER HOLE,BUSHING AND FACE,OB SIDE. REPAIRED PER B737-800 SRM 57-20-90.SDR DALA2021080304382Battery Pack · inoperative(LOG 7840565) DURING INSPECTION FOUND SEAT MOUNTED EMERG LIGHTS INOP. R/R M01674 BATTERY PACK PER B737 M/M 33-51-06 - TEST OK.SDR DALA2021050302501Sensor · inoperativeSHIP 3758 -ATB- RETURNED DUE TO TRAILING EDGE FLAP ASYMMETRY. CORRECTIVE ACTION: REPLACED #6 FLAP SKEW SENSOR. PERFORMED FLAP FUNCTIONAL TEST. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
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