N988AT
Service difficulty reports · 177
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 = 'N988AT' 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 = 'N988AT' 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 DALA2026092405330Oxygen Mask · no testCAPTAIN`S OXYGEN MASK DOES NOT TEST PROPERLY, R & R OBSERVER SEAT CREW O2 MASK BOX IAW AMM 35-13-09. (9110692) (AIRCRAFT GROUNDED).SDR DALA2026061003517Skin · crackedCRACK ON FUSELAGE SKIN BTW STA Y=1037 & LONG 14R AT AFT FUSELAGE AREA. FUSELAGE SKIN BTW STA Y=1037 & LONG 14R AT AFT FUSELAGE AREA WAS REPAIRED PER PRI 634847-14 REV. 2 AND ER/A 634847-14 REV. ORIGINAL SECTION 1. (LP 1638764 - AIRCRAFT WAS GROUNDED)SDR DALA2026060903483Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA 1087 RT LONG 14R. EXTERNAL FUSELAGE SKIN STA 1087 RT LONG 14R WAS REPAIRED PER PRI 634855-14 REV. 1 AND ER/A 634855-14 REV. ORIGINAL. (LP 1637170 - AIRCRAFT WAS GROUNDED)SDR DALA2026060903480Skin · crackedAIRCRAFT 9521, CRACK ON EXTERNAL FUSELAGE SKIN STA 1076 RH BTW LONG 14RH. EXTERNAL FUSELAGE SKIN STA 1076 RH BTW LONG 14RH WAS REPAIRED PER PRI 634869-14 REV 0 AND ERA 634869-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP 1634693 - AIRCRAFT WAS GROUNDED)SDR DALA2026061103542Vane · dentedDENTS ON UPPER SURFACE OF AFT MOVABLE VANE AT RH WING. UPPER SURFACE OF AFT MOVABLE VANE AT RH WING WERE REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL, B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND ADJUSTMENT UNDER AMDS 2750-4008. (LP 1632855 -SDR DALA2026060903435Door Frame · corrodedCORROSION ON ANGLE DOOR JAM BTW BS 370 TO 389 APROX AT FWD CARGO COMPARMENT. REPAIRED IAW SRM 51-40-02 (1625046) (AIRCRAFT GROUNDED).SDR DALA2026051703033Battery Pack · faultedSHIP 9521 EMERGENCY LIGHTS FORWARD OF NACELLES ARE ILLUMINATED WHEN SHIPS POWER IS COMPLETELY POWERED DOWN. REPLACED BATTERY PACK INSIDE B5-125. ALL OPS NORMAL. (8664178) (AIRCRAFT GROUNDED)SDR DALA2026042302607Relay · faultedWHEN SECURING AC FOR THE NIGHT, WHEN TURNING COCKPIT EMERGENCY SWITCH TO "OFF" OUTSIDE WING EMERGENCY LIGHTS STAY "ON". REMOVED AND REPLACED RELAY R2-273 IAW B717 AMM 33-51. (8664106) (AIRCRAFT GROUNDED)SDR DALA2026011600379Transceiver · faultedATB- PERFORMED AN AIR TURN BACK DUE TO A WEATHER RADAR. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER AND PERFORMED OPERATIONAL TEST. AIRCRAFT RETURNED TO SERVICE.(7949802)SDR DALA2024112511166Bolt · shearedSHIP 9521 -ATB/GEAR/DE- THE FLIGHT CREW PERFORMED AN AIR TURN BACK TO CLT DUE TO A "RIGHT MAIN LANDING GEAR UNSAFE" MESSAGE WITH AN ASSOCIATED "RIGHT GEAR DOOR OPEN" MESSAGE. THE ALTERNATE GEAR EXTENSION LEVER WAS PULLED. AN EMERGENCY WAS DECLARED WITH ATC. COSDR DALA2024052205412Fuel Tank · corroded-AD- CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-32 AT LH MLG WHEEL WELL (AREA UNDER MLG CABLE FITTING). SUMMARY OF NRC 00775: CORROSION LEVEL 1. CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-SDR DALA2024050104835Skin · corrodedCORROSION ON SETTLEMENT AREA OF RUB STRIP FUSELAGE SKIN BTW STA Y=870 RH TO 896.5 RH AND LONGERON 27RH FUSELAGE. SUMMARY OF NRC 00737: CORROSION LEVEL 2. FUSELAGE SKIN BTW STA Y=870RH TO 896.5RH AND LONGERON 27RH WAS REPAIRED PER B717 SRM 53-20-70-2R PROCEDURESDR DALA2024042604729Frame · corrodedCORROSION AT FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT. SUMMARY OF NRC 00298: CORROSION LEVEL 2. FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3. PERFORM VISUAL INSPECTION INITIAL 25,SDR DALA2024042504693Floor Support · corrodedCORROSION ON FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00626: CORROSION LEVEL 2. FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE WERE FABRICATED PER B717 DWG 99SDR DALA2024042504692Window Frame · crackedCRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION ESDR DALA2024042504691Window Frame · crackedCRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION ESDR DALA2024042404674Cusp Web · corrodedCORROSION ON RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00525: CORROSION LEVEL 2. RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-SDR DALA2024042304668Longeron · crackedCRACK ON LONGERON 2LH FROM STA 1133 OF AFTER ACCESSORIES. SUMMARY OF NRC 00389: LONGERON 2LH STA 1121 TO STA 1136 WAS REPAIRED PER B717-200 SRM 53-00-05-2R-2 REPAIR 2. (LP #0307355)SDR DALA2024042304667Cusp Web · crackedCRACK ON RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-PROCEDURE 4. REPAIR 4. (LP #0306797)SDR DALA2024042304664Frame · cracked-A.D.- CRACK OF 0.250IN LENGTH WAS FOUND ON UPPER RADIUS OF THE FRAME TAB ON THE LH OVERWING FRAME STA Y=696, IN REF CARD 5310-01436-04B JOB #063-0002 STEP: 10. SUMMARY OF NRC 00522: FRAME TAB ON THE LH OVERWING FRAME STA Y=696 WAS REPLACED PER B717-200 SRM 51SDR DALA2024042204625Pan · crackedCRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160. SUMMARY OF NRC 00191: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDER 3 REPAIR 3. (LP #0305244)SDR DALA2024042204624Pan · crackedCRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200. SUMMARY OF NRC 00193: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0305238)SDR DALA2024042204622Beam · crackedCRACK ON BEAM #1 OF L1 DOOR STA Y=200. SUMMARY OF NRC 00194: BEAM #1 OF L1 DOOR STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0302430)SDR DALA2024041904570Cusp Web · corrodedCORROSION ON LH CUSP WEB, OUT OF LIMITS PER B717 SRM 53-00-55-1A-1 ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00701: CORROSION LEVEL 2. RING DOUBLER ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS FABRICATED AND REPLACESDR DALA2024041904569Cusp Web · crackedCRACK (3 EA) ON LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX. SUMMARY OF NRC 00717: LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 205. (LP #0300923)SDR DALA2024041904568Door Frame · corrodedCORROSION ON DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00700: CORROSION LEVEL 2. DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-SDR DALA2024041904565Door Frame · corrodedCORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00070: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0300206)SDR DALA2024041804534Pan · crackedCRACK ON PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00320: PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0298813)SDR DALA2024041504427Cusp Web · crackedCRACK ON RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00526: RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 1. (LP #0292417)SDR DALA2024041504425Web · crackedCRACKED WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00580: WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0290917)SDR DALA2024041504422Angle · corrodedCORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00072: CORROSION LEVEL 2. FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 FIG 201. (LSDR DALA2024041204362Cusp Web · corrodedCRACK ON LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00596: LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP SDR DALA2023112809763Unknown · unknownAT L1 DOOR CLOSURE PRIOR TO PUSH-BACK, GATE AGENT NOTICED DAMAGE TO BOTTOM FWD EDGE OF L1 DOOR. DAMAGE IS APROX 5" LONG. EDGE ROLLED BACK APROX 3/8". REMOVED DAMAGE PER SRM 52-10-01-2R-1. PERFORMED HFFC PER B717 NDT SPM PART 6-10-01.001. NO CRACKS FOUND QC 209SDR DALA2023060904692Unknown · unknownRAMP REPORTED DAMAGE TO AFT CARGO DOOR CUTOUT. FOUND DAMAGE TO PREVIOUS REPAIR SPLICE ONLY. REMOVED SPLICE TO PREPARE FOR REPLACEMENT. NO OPEN HOLE REQUIRED. INSTALLED REPAIR PER B717 SRM 53-20-15-2R PROC 4 PERMENANT REPAIR. (LP #4798350)SDR DALA2023050303434Unknown · unknownSHIP 9521 -ATB/GEAR- THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT TO DTW FOLLOWING THE FAILURE OF THE NOSE LANDING GEAR TO RETRACT. CORRECTIVE ACTION: MAINTENANCE ADJUSTED NOSE LANDING GEAR RETRACT ACTUATOR. (LP #4110406)SDR DALA2023042703290Unknown · unknownFOUND TWO FORWARD UPPER RIGHT OVERWING CABIN EXIT LIGHTS AND ONE CEILING AISLE LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED TWO EMERGENCY LIGHT POWER SUPPLY BATTERIES PER B717 AMM 33-51-03 PAGEBLOCK 401. OPERATIONAL CHECK WAS GOOD. (LP #9428982)SDR DALA2023022201325None · none"FAA APPROVAL PENDING" FOR ERA 605849-14 REV ORIG. FUSELAGE SKIN / STA 1002-1022 / L-24-L-26 / GROUND DAMAGE SECTION I PERMANENT REPAIR INSTRUCTIONS. SUMMARY SEE NRC 003-0001:0514-2001/005 00005: COMPLIED WITH ER/A PRI 605849-14 REV A PRI REV 0 REPAIR INSTRUCTSDR DALA2023021501178None · noneCOMPLY WITH FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L-26 PER ER/A 605849-14 REV ORIG. C/W ER/A 605849-14 REV ORIG. PERMANENT REPAIR AND ER/A 605849-14 REV A. RII C/W. ASSOCIATED ER/A 14-605849 ADDED FOR AC 9521. (LP #4025639)SDR DALA2023021401137Unknown · unknownC/W ERA 605849-14 REV ORIG, FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L26. SUMMARY NRC 003-0001:0514-2001/001 00001: COMPLIED WITH ER/A PRI 605849-14 REV "0","1","2","3". ALL REPAIR INSTRUCTION STEPS, ENSURE FINALE ER/A 605849-14 REV. ORIG. SSDR DALA2023021401135Unknown · unknownLONGERON 24R CORRODED FROM STA 1000-1035. SUMMARY NRC 003-0001:0514-2001/002 00002: REPLACED LONGERON REF DAC DWG 5911424. (LP #2625262)SDR DALA2023011200229Lens · missingTHE 1R DOOR EXIT SIGN LENSE WAS MISSING ON PREFLIGHT. MAINTENANCE INSTALLED THE 1R DOOR EXIT SIGN LENSE REF B717 IPC 33-51. (LP #9884344)SDR DALA2023010500070Fire Warning · false activationSHIP 9521 -DIV/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO BNA FOLLOWING A "FIRE" WARNING INDICATION ON THE #2 ENGINE WITH ANTI-ICE ON. THE QRH WAS COMPLIED WITH, AN EMERGENCY WAS DECLARED WITH ATC, AND THE SUBSEQUENT OVERWEIGHT LANDING WAS UNEVENTFUL. CFR DISDR DALA2022120207723Transmitter · faultedDECLARED EMERGENCY DUE TO AN INTERMITTENT FLAP DISAGREE INDICATION. STARTING AT 12000 FT, PFD SPORADICALLY SHOWED FLAPS 0 & PICTURE OF UNDERWING ON CONFIG PAGE. CREW REPORTED NO ADVERSE FEEL. CONTINUED THROUGH 25000 FT UNTIL THE FLAPS DISAG ON EICAS WITH SSDR DALA2022111707400Cable · frayedTHE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS FRAYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52-01 AND SDR DALA2022091206031None · noneCAPTAIN WINDSHIELD ARCING ON DESCENT. MCC FCP DEFERRED. FLIGHT CREW PLACARD VALIDATION IS ACCOMPLISHED AT CHA PER MEL 30-41-01B. REPLACED CAPTAIN WINDSHIELD PER B717 AMM 56-11. MEL AND PLACARD REMOVED. (LP #2402013)SDR DALA2022090405924None · noneAIRCRAFT 9521, DURING SVC CHK FOUND BATTERY 7 (685R) FOR EMERGENCY LIGHTS DRAINED. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY ASSEMBLY AT LOCATION 7 (685R). (LP9115548)SDR DALA2022040802422Tailpipe · pluggedSHIP 9521 - THE FLIGHT CREW RETURNED THE AIRCRAFT BACK TO ATL AND LANDED WITHOUT FURTHER INCIDENT AFTER THE #2 ENGINE EXPERIENCED A COMPRESSOR STALL DURING CLIMB OUT. AT FL230, A LOUD REPORT WAS HEARD, FOLLOWED BY STRONG VIBRATIONS (9.9 UNITS) FROM THE ENGINE,SDR DALA2022040602328Lanyard · out of positionGIRT BAR LANYARD WAS FOUND TO BE NOT ATTACHED TO PASSENGER DOOR. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THE LANYARD WAS NOT LOOPED AROUND THE GIRT BAR. PLACED THE GIRT BAR SDR DALA2021120907587None · noneSHIP 9521 - THE CREW DECLARED AN EMERGENCY DURING THE APPROACH FOR LANDING IN ATL DUE TO THE LOSS OF LEFT HYDRAULIC SYSTEM FLUID QUANTITY. CORRECTIVE ACTION: MAINTENANCE FOUND THE SOURCE OF THE LEAK AND REPLACED THE DAMAGED SECTION OF A HYDRAULIC LINE NEAR THESDR DALA2021102806675None · noneR1 DOOR SLIDE PINS PULLED OUT WHEN DOOR WAS OPENED FROM THE OUTSIDE. THE SLIDE DID NOT DEPLOY AS DESIGNED. THIS IS A FAILURE OF PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE R-1 DOOR SLIDE BOTTLE PIN WAS INSTALLE
Back to N988AT