N899AT
Service difficulty reports · 143
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 = 'N899AT' 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 = 'N899AT' 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 DALA2026102105789Pseu · failedPERFORMED A GO AROUND AND THEN DECLARED AN EMERGENCY DUE TO A PSEU FAILURE. REPLACED PSEU AND LANDING GEAR POSITION INDICATOR PER AMM 32-61. OPS CHECK GOOD. (9383024) (AIRCRAFT GROUNDED).SDR DALA2026101405658Piston · faultedABORTED TAKE OFF, APPROX 10KTS DUE TO NLG GRINDING NOISE. R & R LEFT CENTER DEFLECTOR SUPPORT IAW AMM 32-22, REMOVED AND INSTALLED NLG PISTON IAW AMM 32-21. (9540698) (AIRCRAFT GROUNDED).SDR DALA2026101405654Tire · damagedLANDING GEAR HAD A RUBBING NOISE ON EXTENSION & RETRACTION, FOUND BOTH TIRES WITH FLAT SPOTS. R & R BOTH NLG TIRES IAW AMM 32-41. (9540696) (AIRCRAFT GROUNDED).SDR DALA2026080704573Hydraulic System · overtempATO- APPROX 15KTS DUE TO RT HYDRAULIC TEMP HIGH MESSAGE. BLED AND SERVICED HYDRAULIC SYSTEMS AND PERFORMED ENGINE RUN PER B717 AMM 12-13. SUBSEQUENTLY REPLACED RT HYDRAULIC SYSTEM BLEED VALVE PER B717 AMM 29-12. OPS AND LEAK CHECK GOOD. (9204346) (AIRCRAFT GSDR DALA2026042902733Tire · failedATB/TIRE- THE CREW PERFORMED AN AIR TURN BACK DUE TO A BLOWN TIRE ON ROTATION WITH ASSOCIATED LEFT ENGINE VIBRATIONS. REPLACED #1- AND #2-WHEEL ASSY. FLAP AND ENGINE REPAIR IN PROGRESS. (8687069) (AIRCRAFT GROUNDED)SDR DALA2025081105961Reservoir · leakingCREW DIVERTED TO ORD AFTER RECEIVING A LT SYSTEM HYDRAULIC QUANTITY LOW MESSAGE WITH QUANTITY DEPLETING. FOUND LEFT HYD LEAKING AT HYD RESERVOIR BLEED VALVE DRAIN HOSE CONNECTION. REPLACED RESERVOIR. LEAK CHECK NORMAL.(7712608)SDR DALA2025061604512Thermocouple · faultedSHIP 9557 -ATB- PERFORMED AN AIR TURN BACK TO ATL DUE TO RIGHT ENGINE SYSTEM FAIL MESSAGE JUST AFTER TAKEOFF. CORRECTIVE ACTION: DURING INSPECTION OF RIGHT ENGINE TGT THERMOCOUPLE PROBES, FOUND TCC COOLING TUBE LINE BLOWN OUT AND MISSING HARDWARE. REPLACED COOSDR DALA2025060604345Transformer · failedSHIP 9557 STRONG ELECTRICAL ODOR ON FINAL RIGHT S THE GEAR WENT DOWN AND FLAPS WENT TO 18 DEGREES. R/R TRANSFORMERS TI-5 AND T1-6.(T1-5 SMELLED BURNT) PER B717 SWPM 20-20-03. RT NOSE LDG AND TAXI LIGHT CKS OK. C/B FUNCTION NORMAL. REF B717 WDM 34-41-01 (72629SDR DALA2024091809142Windshield · arcedENROUTE F/O WINDSHIELD WAS ARCING. FOLLOWED BY A "LEVEL 1 WSHLD HEAT FAIL" MESSAGE. RAN QRH CHECK LED US TO "WINDSHIELD CRACKED OR ARCING" CHECKLIST ON PAGE 3.13. PULLED CB Z-24. LOOKS LIKE A HAIRLINE CRACK ON OUTER PANE - UPPER PORTION OF WINDSHIELD. MAINTENASDR DALA2024080507764Battery Pack · no testBOTH AFT EMERGENCY DOORS "EMERGENCY EXIT IDENTIFIER" LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK POWER SUPPLY B5-119 PER B717 AMM 33-51-03. OPERATIONAL TEST WAS GOOD. (LP #5908832)SDR DALA2024070806854Battery Pack · no testTHE AFT LEFT AND AFT RIGHT OVERWING EXIT LIGHTS (LOWER) ARE INOPERATIVE. DISCONNECTED R5-4255A FOR T/S. RE-CONNECTED R5-4255A AND REPLACED BATTERY POWER SUPPLY AND BATTERY ASSEMBLY B5-119 PER B717 AMM 33-51. ALL CHECKS ARE GOOD.SDR DALA2024050104834Computer · faultedBOTH FCC FAULTING BOTH REDUNDANT STOP SWITCHES ON DESCENT MULTIPLE FLIGHTS. VERIFY CONDITION AND SECURITY OF REDUNDANT RUDDER LIMITER RETURN SPRINGS. FOUND RUDDER LIMITER PUH ROD BINDING. REMOVED ROD AND REPLACED BOTH BEARINGS REF P.S. 900-9-1 #06. INSTALLRD RSDR DALA2024051605257Trunnion · corrodedLT MLG UPPER STRUT O/B ATTACH LUG HAS CORROSION ON THE AFT FACE. MARKED. SUMMARY SEE NRC 004-0003:3211-4001/015 00016: C/W ERA 615978-14 REV ORIGINAL. VERIFIED PRI AND ERA MATCH. (LP #0209458)SDR DALA2024022102375Trunnion · corrodedLT MLG - TRAPEZOIDAL FITTING BUSHING PITTED ON AFT SIDE. MARKED IN RED. SUMMARY SEE NRC 004-0003:3211-4001/014 00015: REPLACED BUSHING PER OHM 57-40-1. (LP #0206822)SDR DALA2024031403326Trunnion · corrodedTRUNNION MOUNT ATTACH AFT FITTING AFT LUG AFT BUSHING HAS CORROSION. (MARKED) REF NR 013 VISIT ID P682670620231227 AND REPAIRED PER B717 SRM 51-10-04. (LP #0205683)SDR DALA2023121810337Unknown · unknownEMERGENCY EXIT SIGNS AT LOCATION 601 ARE INOPERATIVE. THE INTERIOR EMERGECY EXIT LIGHTS ARE FLASHING IN FLIGHT. MAINTENANCE REPLACED B5-235 POWER SUPPLY AND BATTERY IAW B717 AMM 33-51. OPERATIONAL TESTS WERE GOOD. (LP #0112909)SDR DALA2023120710008Unknown · unknownTHE EMERGENCY EXIT LIGHTS BY L1 DOOR ABOVE F/A JUMPSEAT ARE INOPERATIVE. MAINTENANCE DROPPED THE O2 MASK DOOR BELOW LIGHT FOR BETTER ACCESS. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM IAW B717 AMM 33-51. TWO OUT OF THREE LIGHT ASSEMBLYS FROM PSDR DALA2023070405379Unknown · unknownCORROSION ON FLOOR PANELS 121HF, 181KF, 181HF, 181UF, 121DF, 121FF, 121NF, 181AF (PART 2), 181FF, 181AF (PART 3), 181CF, 121TF, 181JF, 181DF, 121SF, 121JF, 121CF, 121PF, 121QF, 121MF, 121UF, 121VF, 121SF, 181AF (PART 1), 181EF (PART 1), 181EF (PART 2), AND 181SDR DALA2023061604900Unknown · unknownCORROSION ON R1 DOOR SERVICE LOWER DOOR JAMB STA Y=168 TO STA Y=200. IN REFERENCE NRC 0428. PTAS. SUMMARY OF NRC 00531: CORROSION LEVEL 2, R1 DOOR SERVICE LOWER DOOR JAMB STA Y=168 TO STA Y=200 WAS REPAIRED PER PRI 609065-14 REV 2 AND ER/A 609065-14 REV ORIGINSDR DALA2023061504879Unknown · unknownCORROSION ON DOOR JAMB AFT LOWER SECTION STA =950 TO STA=992. SUMMARY OF NRC 00071: CORROSION LEVEL 2. DOOR JAMB AFT LOWER SECTION STA=950 TO STA=992 WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #2816939)SDR DALA2023061404850Unknown · unknownCORROSION ON FLOOR SUPPORT BTW STA Y=120 AND Y=148 X=-50 AT COCKPIT. SUMMARY OF NRC 00440: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=120 TO Y=148 X=-50 AT COCKPIT WAS REPLACED PER B717-200 SRM 51-41-08-0G. (LP #2814601)SDR DALA2023061304795Unknown · unknownCRACKED MEMBRANE BTW STA Y=172 AND Y=187 APROX AND X54 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00577: MEMBRANE BTW STA Y=172 AND Y=200 APROX AND X54 AT CABIN FLOOR STRUCTURE WAS REPLACED PER DRAWING 9936534-5 REV BW AND PER B717-200 SRM 51-41-05-0G AND 51-41-SDR DALA2023061504876Unknown · unknownCORROSION ON FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1). SUMMARY OF NRC 00409: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1) WERE REPLACED PER DWG 9936534 REV BW AND PER B717-2SDR DALA2023061304791Unknown · unknownCORRODED OUT OF LIMITS IN REF TO NRC 339: CORROSION ON FLOOR SUPPORT BTW STA 200 AND -X=46 TO -X=57 AT PAX CAB. SUMMARY OF NRC 00584: NEW FLOOR SUPPORT BTW STA 200 AND -X=46 TO -X=57 WAS INSTALLED, ADJUSTED, AND DRILLED PER B717-200 SRM 51-40-08- 0G GENERAL ANSDR DALA2023061304789Unknown · unknownCORROSION ON WEB FROM STA Y 155 TO 200 AND FROM X 20 TO X-60 AT R1 DOOR LOWER DOOR JAMB. IN REF NRC 00531. SUMMARY OF NRC 00549: CORROSION LEVEL 2. WEB FROM STA Y 155 TO 200 AND FROM X 20 TO X-60 AT WAS REPLACED PER B717-200 SRM 51-41 -02-0G AND 51-41-05-0G. (SDR DALA2023060804667Unknown · unknownCORROSION ON WEB FROM STA 218 TO 237, X -55 TO 44:5 AT W1 IN REF NRC 531. CPAX. SUMMARY OF NRC 00546: CORROSION LEVEL 2. WEB FROM STA 218 TO 237, X -55 TO 44:5 AT W1 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 226 AND SRM 51-41-02-0G. (LSDR DALA2023060804664Unknown · unknownERODED MATERIAL ON FUSELAGE SKIN BTW STA 992 AND LONGERON 25R APPROX (DOOR CUTOUT). SUMMARY OF NRC 00214: FUSELAGE SKIN BTW STA 992 AND LONGERON 25R APPROX (DOOR CUTOUT) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12 PAR 6 OPTION 1, FIGURE 20SDR DALA2023060704644Unknown · unknownCRACK FRAME OF LH AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7 LH. SUMMARY OF NRC 00231: FRAME OF LH AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7 LH WAS REPAIRED PER PRI 608989-14 REV. 0 AND ER/A 608989-14 REV ORIGSDR DALA2023060704643Unknown · unknownCORROSION ON WEB PRODUCTION DOUBLER FROM STA 157 TO 178 AT R1 DOOR LOWER JAMB. W1. SUMMARY OF NRC 00550: CORROSION LEVEL 2. WEB PRODUCTION DOUBLER FROM STA 157 TO 178 AT R1 DOOR LOWER JAMB W1 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2803SDR DALA2023060204425Unknown · unknownDELAMINATION AND BROKEN COMPOSITE MATERIAL AND SHEET ON FWD CARGO FLOOR PANEL 121CF AND 121NF (C1). SUMMARY OF NRC 00376: FWD CARGO FLOOR PANEL 121CF AND 121NF WERE MANUFACTURED PER ERA 544901-14 REV A PAR 6. AND FIGURE 5 AND ERA 591778-14TR REV ORIGINAL SECTISDR DALA2023060104390Unknown · unknownCRACK ON FRAME STA 1037 BTW LONG-16 LH TO LONG-17 AT PAX CABIN. SUMMARY OF NRC 00534: FRAME STA 1037 BTW LONG-16 LH TO LONG-17 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4, REPAIR 4. (LP #2794265)SDR DALA2023053004259Unknown · unknownCORROSION ON PREVIOUS DOUBLER REPAIR OF LH CUSP WEB BTW STA Y=446 TO Y=465 AND STA Y=484 TO Y=503 AT PAX CABIN. SUMMARY OF NRC 00459: CORROSION LEVEL 2. PREVIOUS DOUBLER REPAIR OF LH CUSP WEB BTW STA Y=446 TO Y=465 AND STA Y=484 TO Y=503 AT PAX CABIN WERE REPLSDR DALA2023053004258Unknown · unknownCORROSION ON LH CUSP MEMBRANE (WEB) UPPER FACE BTW STA 863 TO 865 AT PAX CABIN. SUMMARY OF NRC 00545: CORROSION LEVEL 2. CUSP MEMBRANE (WEB) UPPER FACE BTW STA 863 TO 865 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2790489SDR DALA2023053004257Unknown · unknownCORROSION ON PREVIOUS DOUBLERS REPAIR OF RH CUSP WEB BTW STA Y=446 TO Y=503, STA Y=541 TO Y=560, AND Y=598 TO Y=617 AT PAX CABIN. SUMMARY OF NRC 00460: CORROSION LEVEL 2. PREVIOUS DOUBLERS REPAIR OF RH CUSP WEB BTW STA Y=446 TO Y=503, STA Y=541 TO Y=560, AND YSDR DALA2023053004256Unknown · unknownCORROSION ON SEAL RETAINER (2 EA) ON THE LOWER CUTOUT AREA AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00079: CORROSION LEVEL 2. SEAL RETAINERS (2 EA) ON THE LOWER CUTOUT AREA AT FWD CARGO COMPARTMENT DOOR WERE FABRICATED PER DWG #PL 5910141 REV FE AND REPLASDR DALA2023053104382Unknown · unknownCORROSION ON RH CUSP MEMBRANE (WEB) UPPER/ LOWER SURFACE FROM STA 200 TO 218 AT PAX CABIN. SUMMARY OF NRC 00564. CORROSION LEVEL 2: RH CUSP MEMBRANE (WEB) FROM STA 200 TO 218 AT PAX CABIN WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2 ITEM 32. (LP #2787SDR DALA2023053004255Unknown · unknownCORROSION ON LOWER HALF OF SETTLEMENT AREA ON RUDDER DRIVE TORQUE (FUSELAGE STRUCTURE). SUMMARY OF NRC 00373: PLATE ASSY, BEARING SUPPORT WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2787763)SDR DALA2023053004253Unknown · unknownCRACK INNER PAN AFT FRAME, BEAM #1 END AT FWD CARGO DOOR C1. SUMMARY OF NRC 000168: INNER PAN AFT FRAME, BEAM #1 END AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1, FIGURE 201. (LP #2787424)SDR DALA2023053004251Unknown · unknownCRACK ON CUTOUT DOOR STRUCTURE FWD SIDE ON LOWER CORNER, BTW BEAMS 1-2 AT FWD CARGO DOOR. SUMMARY OF NRC 00076: CUTOUT DOOR STRUCTURE FWD SIDE ON LOWER CORNER, BTW BEAMS 1-2 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 4, REPAIR 4. (LPSDR DALA2023053004250Unknown · unknownCORROSION ON FLOOR SUPPORT STA Y=256 X-22 TO X10 CPAX (W1). SUMMARY OF NRC 406: FLOOR SUPPORT STA Y=256 X-22 TO X10 CPAX WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2785801)SDR DALA2023052604193Unknown · unknownCORROSION OUT OF LIMITS ON LH OTBD SEAT TRACK BTW STA 357 TO 358, 427 TO 428, AND 462 TO 463. PER B717-200 SRM 53-20-52-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PARAGRAPH 4. A. FIGURE 101 AND DWG S00482. SUMMARY OF NRC 00530: CORROSION LEVEL 2. LH OTBD SEAT TRACK BTWSDR DALA2023052604192Unknown · unknownBROKEN PAN ON FWD CARGO DOOR AFT SIDE BTW 1-2 BEAMS. SUMMARY OF NRC 00091: PAN OF FWD CARGO DOOR AFT SIDE BTW 1-2 BEAMS WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 4, REPAIR 4. (LP #2783956)SDR DALA2018091005511Frame · crackedDURING RT OVERWING FRAME INSPECTION, FOUND FRAME AT STA 696 CRACKED. RT OVERWING FRAME AT STA 696 REPLACED ON CARD 5310-01436-03B.SDR DALA2018091005510Frame · crackedUPPER RADIUS OF THE FRAME TAB AT STA Y=696.00 RT OVERWING FRAME HAS CRACK INDICATION. INSTALLED INTERCOSTALS 11R, 12R, 10R, 15R, 16R, 17R, AND 18R REF DWG 9919671. REPAIRED ON WORK CARD 5310-01436-03B.SDR DALA2018091005509Pan · corrodedFWD CARGO DOOR CUT-OUT INNER PAN HAS AREAS OF CORROSION. REPAIRED IN REF TO SRM 53-20-15-2R PROC 6.SDR DALA201805173102Skin · damagedFOUND DAMAGE ON THE LT INBD FLAP TRAILING EDGE WEDGE. PERFORMED A TEMP REPAIR IAW ER/A 568347-14.SDR DALA2017100207191Lens · missingCABIN STANDBY LIGHT AT SEAT 15 ABC MISSING THE LENS. REPLACED THE OVERHEAD EMERGENCY LIGHT ASSY IAW AMM 33-51. PERFORMED AN OPS TEST IAW AMM 33-51. OPS TESTED OK.SDR DALA2016100807114Skin · crackedSKIN CRACKED BS 1152 BETWEEN STRINGERS 2 & 3R. REPAIRED THE SKIN IAW ER/A 549622-14 REV O.SDR DALA2016100707101Skin · crackedFUSELAGE SKIN CRACKED BS 1152 BETWEEN STR 3L & 4L AT FORMER I/B FASTENER. HFEC VERIFIED IAW NDTSPM ETHF PROCEDURE 1, 06-10-01 .001. FABRICATED DOUBLER AND FILLER. REPAIRED IAW SRM 53-02-01 FIG 202.SDR DALA2016100707100Frame · corrodedFOUND CORROSION AT BS 1022 AT LONGERON 29R TO 29L AFT CARGO. BLENDED AREAS OF CORROSION ON AFT SIDE OF FRAME 1022 FROM STR 29R TO 29L IAW B717 SRM 53-00-00 FIG 103. MINIMUM OF .033 REMAINING OF ORIGINAL .050 AT STR30, FOUND TO BE OUT OF LIMITS IAW B717 SRM 53
Back to N899AT