N989AT
Service difficulty reports · 198
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 = 'N989AT' 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 = 'N989AT' 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 DALA2026090404996Fairing · puncturedPUNCTURE ON TIP FAIRNG OF RT HORIZONTAL STAB. COMPLIED WITH ER/A 636479-14. (1793989) (AIRCRAFT GROUNDED).SDR DALA2026082404793Door Frame · crackedCRACK ON FWD UPPER CORNER OF GALLEY SERVICE DOOR CUTOUT IN BS Y=174.0 AND 3.5 INCHES FROM LONG 11 RH AT EXTERNAL FUSELAGE, REPAIRED DOOR CUTOUT PER B717-200 SRM 53-10-01-2R. (1773337) (AIRCRAFT GROUNDED).SDR DALA2026082404791Frame · damagedELONGATED FRAME HOLE TO ATTACH AFT ROD OF LT AIR CONDITIONING PACK BS Y=1133 & LONG 9L AT AFT ACCESORY COMPARTMENT, REPAIRED FRAME HOLE IAW SRM 53-00-07-2R. (1772689) (AIRCRAFT GROUNDED).SDR DALA2026082404788Vane · dentedSEVERAL DENTS ON LOWER SURFACE FWD MOVABLE FLAP VANE AT RT WING, FWD MOVABLE FLAP VANE AT RH WING WAS REPAIRED IAW SRM 57-53-01-2R. (1769283) (AIRCRAFT GROUNDED).SDR DALA2026082404804Vane · crackedCRACK WAS FOUND ON AFT MOVABLE VANE IN FWD INBD FITTING AT RT WING, R & R AFT RT MOVABLE FLAP VANE UNDER AMDS 2000-2638. (1765421) (AIRCRFT GROUNDED).SDR DALA2026032201929Anti-Skid Sys · faultedDUE TO RIGHT ANTISKID FAIL ON APPROACH ATL. CORRECTIVE ACTION: FAULTED #3 WHEEL SPEED TRANSDUCER. REPLACED SAME NO HELP. FOUND CONNECTOR P1-3700 PIN 1 AT TRANSDUCER DISCONNECTED. RE-TERMINATED WIRE. OPS CHECK GOOD. (LP 8356405)SDR DALA2025061104460Battery Pack · inoperativeAIRCRAFT 9527, MULTIPLE EMERGENCY LIGHTS INOP THROUGHOUT CABIN. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT BATTERY PACKS B5-227 AND B5-230 PER B717 AMM 33-51. OPS CHECK GOOD. (LP 6564077)SDR DALA2024120211375Light Sys · inoperativeDURING SERVICE NOTED THAT THE LH AND RH AFT OVERWING AND RH FWD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY B5-119 REF B717 AMM 33-51. BOTH AFT OVER WING LIGHTS WORK BUT RH FWD STILL INOPERATIVE. FOUND GROUND LOOSE FOR L2-832. RESDR DALA2024120911532Duct · temp repairCRACK ON RIGHT ENG BYPASS DUCT NEAR PRECOOLER INLET WAS TEMPORARILY REPAIRED. RE-INSPECTION REQUIRED PER ER/A 620571-14 REV ORIGINAL. REFER TO LOG #0580374 FOR PRIOR INSPECTION. SECTION 4 INSPECTION MUST BE ACCOMPLISHED BETWEEN 220 AND 180 FLIGHT CYCLES PER ERSDR DALA2024091809140Hinge · excess playFREEPLAY WAS FOUND ON RH WING FLAP OUTBD HINGE AREA. SUMMARY OF NRC 00781: RH WING FLAP OUTBD HINGE WAS REPAIRED PER ER/A 620752-14 REV ORIGINAL AND PRI 620752-14 REV 2 AND WAS INSTALLED PER B717-200 AMM 27-55-03 400-801. ASSOCIATED ER/A 14-620752 ADDED FOR ACSDR DALA2024091809136Pan · crackedCRACK ON PAN FWD EDGE IN LOWER SIDE AT FWD CARGO COMPARTMENT DOOR. RE-WRITE REASON: TECHNICAL REFERENCE USED DOES NOT APPLY TO FWD CARGO COMPARTMENT. ALSO, AFTER DOUBLERS REMOVED CRACKS WERE FOUND ON PAN BTW BEAM 1 AND 2 AND ELONGATED HOLES ON INNER/OUTER PAN.SDR DALA2024091609051Pan · crackedCRACK ON AFT PAN WAS FOUND BTW BEAM 1 AND 2 AT AFT CARGO DOOR (REF NRC NBR 00640). SUMMARY OF NRC 00693: AFT INNER PAN BTW BEAM 1 AND 2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620224-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620224-14 REVSDR DALA2024091609047Shear Tie · crackedFABRICATED PARTS IN REFERENCE NRC 00592 AND PRI 620225-14 REV 0. MANUFACTURE SHEAR CLIP (AFT ACCESS). CRACK WAS FOUND ON SHEAR CLIP IN REFERENCE NRC 00592: FABRICATE SHEAR CLIP PER PRI 620225-14 REV 4 AND ER/A 620225-14 REV OROGINAL, SECTION I PERMANENT REPAIRSDR DALA2024091308982Skin · crackedCRACK ON SKIN, SHEAR CLIP, AND SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESORY COMPARTMENT (IN REFERENCE TO ERA 95-520358-14 REV ORIGINAL FIGURE 4). SUMMARY OF NRC 00592: SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESOSDR DALA2024091008881Frame · corrodedCORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00754: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #0542411)SDR DALA2026080404487Skin · corrodedCORROSION STABILIZERS RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL BARREL NUT HOLE #11. REPAIRED PER ERA 620136-14. (0541097) AIRCRAFT WAS GROUNDED.SDR DALA2024090608757Access Panel · corrodedCORROSION INSIDE HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX. SUMMARY OF NRC 00399: CORROSION LEVEL 2. HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX WAS REPAIRED PER ER/A 620168-14 REV ORIGINAL, SECTION 1: PERMANENSDR DALA2024090608756Barrel Nut · corrodedCORROSION IN BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER IN REF NRC 00400. SUMMARY OF NRC 00649: CORROSION LEVEL 2. BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER WAS REPAIRED PER PRI 620136-14 REV 3 & ER/A 620136-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSDR DALA2024090308637Cusp Web · crackedCRACK ON CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00516: CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN WERE FABRCATED AND REPAIRED PER DWG 9910151 REV CH, B717 SRM 51-70-10-2R SDR DALA2024090308636Former · crackedCRACK FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR. L1. SUMMARY OF NRC 00118: FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 3, REPAIR 3. (LP #0533710)SDR DALA2024090308635Pan · crackedCRACK ON AFT PAN INTERSECTION WITH BEAM #5, CRACK ON FWD PAN INTERSECTION WITH BEAM #3 , 3) CRACK ON FWD PAN INTERSECTION WITH BEAM #5 ON FWD CARGO DOOR. SUMMARY OF NRC 00132: AFT PAN INTERSECTION WITH BEAM #5, FWD PAN INTERSECTION WITH BEAM #3, AND FWD PAN INSDR DALA2024083008600Cap · crackedCRACK ON CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN. SUMMARY OF NRC 00554: CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN WAS REPAIRED PER ERA 620017-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620017-14 REV 1. ASSOCIATED ER/A 14-620017 ADDED FOR AC 9527SDR DALA2024090408731Intercostal · crackedCRACK ON INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT. SUMMARY OF NRC 00361: INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT WERE REPLACED PER B717-200 SRM 51- 41-02-0G AND 51-42-05-0G AND SPRINGS WERE REMOVED ASDR DALA2024083008598Longeron · crackedCRACK ON LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN. SUMMARY OF NRC 00553: LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2. (LP #0527480)SDR DALA2024083008593Beam · crackedCRACK BEAM #1 AFT EDGE AT L1 DOOR PTAS. SUMMARY OF NRC 00320: BEAM #1 AFT EDGE AT L1 DOOR PTAS WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0526246)SDR DALA2024082808521Seat Track · crackedAIRCRAFT 9527, AFTER SEAT TRACK X = -44 BTW STA Y = 646 TO Y = 775 REMOVAL, CRACK ON HOLES AT WEB BTW STA 648 AND STA 650. CORRECTIVE ACTION: WEB BTW STA 648 AND STA 650 WAS REPAIRED PER B717 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2. (LP 0524830)SDR DALA2024082508422Window Frame · crackedAIRCRAFT 9527, CRACK LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN. CPRRECTIVE ACTION: LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN WAS REPAIRED PER B717 SRM 56-10-02-2R-1. (LP 0519523)SDR DALA2024082408419Frame · crackedAIRCRAFT 9527, CRACKS ON FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN. CORRECTIVE ACTION: FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCESDR DALA2024082308414Cusp Web · crackedAIRCRAFT 9527, CRACK CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 AND SRM 51-41-02-0G. (LP 0516434)SDR DALA2024082308413Cusp Web · crackedAIRCRAFT 9527, CRACK ON CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX) REPAIRED PER B717-200 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2 FIG. 201. (LP 0516174)SDR DALA2024082308411Window Frame · crackedAIRCRAFT 9527, CRACK ON RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX. CORRECTIVE ACTION: RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX WERE REPAIRED PER B717-200 SRM 56-20-0SDR DALA2024082208364Cusp Web · crackedAIRCRAFT 9527, CRACK ON CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM. 53-00-55-2R PROCEDURE 4 FIG. 205. (LP 0514941)SDR DALA2024082208363Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. FIGURE 210. (LP 0514913)SDR DALA2024082208360Pan · crackedAIRCRAFT 9527, INITIAL INSPECTION: CRACK ON LH RING PAN (FWD/UPPER) STA Y= 484, (FWD/LOWER) STA Y=636, (AFT/UPPER) STA Y=851, (FWD/LOWER) STA Y= 851, (FWD/LOWER) STA Y=870, (FWD/LOWER) STA Y=908, (FWD/LOWER) STA Y=927, (FWD/UPPER/LOWER) STA Y= 946 AT CABIN PAXSDR DALA2024082208359Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 210. (LP 0514363)SDR DALA2024082208357Longeron · crackedAIRCRAFT 9527, CRACK ON LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT. CORRECTIVE ACTION: LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R. PROCEDURE 2. REPAIR 2 FIG. 201. (LP 0514325)SDR DALA2024082108332Structure · ground damageAIRCRAFT 9527, FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER. CORRECTIVE ACTION: PERMANENT REPAIR ON FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER WAS PERFORMED PER B717-200 SRM 53-20-15-2R, REPAIR 11, OPTION 1. PERFORMED VISUAL INSPECTION ON PERMASDR DALA2024082108330Web · crackedAIRCRAFT 9527, INITIAL INSPECTION: SEVERAL CRACKS BELOW INBD WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX. CORRECTIVE ACTION: WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX WAS REPAIRED PER B717-200 SRM 57-70-10-2R-2, PAR. 4 AND B717-200 SRM 51-41-02-0G.SDR DALA2024081908279Beam · crackedCRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR. PTAS. SUMMARY OF NRC 00321: CRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV ORIGINAL. ASSOCIATED ER/A 14-559578 ADDED FOR AC 9527. SDR DALA2024081608211Cusp Web · crackedCRACK ON CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00515: CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #0504361)SDR DALA2024081408111Longeron · crackedCRACK ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00552: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN, 1 CRACK WAS CONFIRMED ON LONG 6LH. PER DC-MD/BOEING NDTSSDR DALA2024080807886Beam · crackedCRACK WAS FOUND ON AFT BEAM 3 AT PAN. SUMMARY OF NRC 00254: PAN AFT SIDE BEAM 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3. (LP #0489872)SDR DALA2024072907549Hub Cap · missingSHIP 9527 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 65 KTS DUE TO RIGHT "ANTI-SKID FAIL" MESSAGE. CORRECTIVE ACTION: MAINTENANCE FOUND THE #4 MAIN GEAR HUBCAP AND CLAMP MISSING. THE HUBCAP AND CLAMP WERE REPLACED AND ALL ANTI-SKID RETURN TO SERVICE TESTS WESDR DALA2024071507165Spring · brokenSHIP 9527 -ATB/GEAR/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO A RIGHT MAIN LANDING GEAR "DOOR UP AND LATCHED UNSAFE" INDICATION. ATC DECLARED AN EMERGENCY FOR THIS EVENT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR UP AND LATCHED SENSOR SPRINSDR DALA2023102508761Unknown · unknownTHE CIRCUIT BEAKER Z26 WAS DISCOVERED OUT. FLIGHT CREW RESET IT ON DIRECTION OF MAINTENANCE. BREAKER VISIBLY SPARKED. BREAKER IS OUT AGAIN. MAINTENANCE FOUND WIRES CROSSED AT F/O SLIDING WINDOW. RETERMINATED WIRES AT SPLICE. BREAKER NOW OPERATES NORMALLY. WINDSDR DALA2023092807972Unknown · unknownCRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE. SUMMARY OF NRC 00077: CRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE WAS REPAIRED PER PRI 612145-14 REV 5 AND ER/A 612142-14AD REV ORIGINAL. SECTION I: PERMANENT SDR DALA2023092707955Unknown · unknownCRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME. (WINGBOX AREA). SUMMARY OF NRC 00118: CRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME WAS REPAIRED PER PRI 612213-14 REV 2 AND ER/A 612213-14 REV ORIGINAL SECTION SDR DALA2023092707954Unknown · unknownCRACK ON LH CUSP WEB STA Y=696 X=54 AT PAX CABIN. SUMMARY OF NRC 00135: CUSP WEB FROM STA Y=655 TO STA Y=715 X=54 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2988642)SDR DALA2023092707951Unknown · unknownCORROSION FOUND ON AFT CARGO LOWER DOOR JAMB BTW STA Y-954 TO Y-994 AND LONGERONS 27R AND 28R. SUMMARY OF NRC 0163: CORROSION LEVEL 2. LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 53-20-15-2R-7 REPAIR 7. (LP #2987631)SDR DALA2023092607924Unknown · unknownCRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14. SUMMARY OF NRC 00024: CRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14 WAS REPAIRED PER ER/A 612108-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612108-14 REV 2. REPETITIVE INSPECTION
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