N963AT
Service difficulty reports · 196
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 = 'N963AT' 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 = 'N963AT' 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 DALA2026051903063Hinge Fitting · corrodedCORROSION ON UPPER HOLES (2EAS) OF RH OUTBOARD WING FLAP HINGE FITTING ALSO CORROSION AND WEAR ON AFT OUTBOARD HINGE POINT (OUT FACE)OF SAME HINGE. RT OUTBOARD WING FLAP HINGE FITTING WAS REPAIRED PER CMM 27-50-5, PRI 634038-14 REV 6. & ER/A 634038-14 REV. (SDR DALA2026051202974Spar Web · crackedDURING TEST FLIGHT SPOILER ACTUATOR, CRACKED REAR SPAR WEB STA XRS=295-324 AT LT WING. REPAIRED PRI 633829-14 REV 8 AND ER/A 633829-14 (1589343) (AIRCRAFT GROUNDED)SDR DALA2026051202973Skin · crackedCRACKED FUSELAGE SKIN BS 1076 AND LONG 15L. REPAIR AND PRI 633842-14 (1588945) (AIRCRAFT GROUNDED)SDR DALA2026042902723Angle · crackedCRACK ON ANGLE ADJACENT TO FUSELAGE SKIN ON STA Y=1178 CANT AND LONG 17 LH SIDE. REPAIRED PER PRI 633860-14 (1561136) (AIRCRAFT GROUNDED)SDR DALA2026031001643Valve · bindingSHIP 9522 CREW REPORTS STRONG DIRTY SOCK SMELL IN BACK OF AIRCRAFT. CORRECTIVE ACTION: FOUND #2 ENG SOURCE R/R #2 ENG BUFFER AIR VALVE FOUND IT BINDING & STIFF IN REF B717 AMM 75-22. CKS GOOD. (1485009)SDR DALA2025082206255Latch · faultedATB, PERFORMED AN AIR TURN BACK DUE TO A RIGHT MAIN LANDING GEAR UNSAFE LIGHT. REPLACED RT GEAR DOOR LATCH. OPS CHECK NORMAL.(7841530).SDR DALA2024040103936Pan · crackedCRACKS ON INNER PAN (3 EA) NEAR BEAMS #5 & #3 FWD SIDE. ALSO NEAR BEAM #2 AFT SIDE AT FWD CARGO DOOR. ER/A 554100-14 REV. A SECTION I WAS ACCOMPLISHED. SUMMARY OF NRC 00097: FWD AND AFT INNER PAN BETWEEN BEAMS #1 AND BEAM #4 AT FWD CARGO DOOR WAS REPAIRED PER SDR DALA2024040103935Hinge · obstructedINTERFERENCE BTW HEAD BOLT AND FWD OUTB FLAP HINGE AT RH WING. SUMMARY OF NRC 00808: FWD OUTB FLAP HINGE AT RH WING WAS REPAIRED PER ERA 616905-14 REV ORIGINAL SECTION I. ASSOCIATED ER/A 14-616905 ADDED FOR AC 9522. (LP #0268113)SDR DALA2024032503738Bulkhead Web · crackedCRACK ON WEB LH AND RH SIDE, (PROJECTION OF UPPER HINGE) AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. SUMMARY OF NRC 00558: WEB AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. ALSO AFT CABIN SDR DALA2024032303705Web · corrodedCORROSION ON WEB BTW Y=200 TO Y=208 X=56. SUMMARY OF NRC 00734: CORROSION LEVEL 2. CORROSION ON WEB BTW Y=200 TO Y=208 X=56 WAS REPAIRED PER PRI 616504-14 REV. 1 AND ERA 616504-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616504 ADDED FOR AC SDR DALA2024050805017Aileron · unknown-AD- PERFORM BALANCE PROCEDURE ON AILERON LH. SUMMARY OF NRC 00770: AILERON LH BALANCE PROCEDURE WAS PERFORMED PER B717-200 SRM 51-60-01-0G, ALSO AILERON LH WAS REMOVED / INSTALLED PER B717-200 AMM 27-10-01. ADJUSTMENT / TEST OK; AILERON CONTROL TAB L/H WAS RESDR DALA2024032203633Skin · corrodedCORROSION ON INTERNAL SKIN AND CUT OUT OF FWD AIR STAIRWELL DOOR. SUMMARY OF NRC 00109: FWD AIR STAIRWELL DOOR WAS REPLACED PER B717-200 AMM 52-63-01. (LP #0255910)SDR DALA2024032203631Frame · crackedCRACK ON FRAME STA Y=1037 BTW LONG 14 RH AND 15 RH AT CABIN PAX. SUMMARY OF NRC 00386: FRAME STA Y=1037 BTW LONG 14 RH AND 15 RH AT CABIN PAX WAS REPAIRED PER ERA 616076-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 616076-14 REV 3. (LP #0255676)SDR DALA2024032103584Longeron · corrodedCORROSION ON LONGERON END 25RH AT AFT CARGO COMPARTMENT C-2. SUMMARY OF NRC 00686: CORROSION LEVEL 2. LONGERON END 25RH AT AFT CARGO COMPARTMENT C-2 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0252387)SDR DALA2024032103573Cusp Web · corrodedCORROSION AT CUSP ANGLE WAS FOUND ON STA Y=200 AND X=54 - 60. SUMMARY OF NRC 00713: CUSP ANGLE WAS ON STA Y=200 AND X=54 - 60 REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 3 REPAIR 3. (LP #0246718)SDR DALA2024031403330Skin · wornWORN FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB). SUMMARY OF NRC 00013: FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10. PERFORM VISUAL INSPECTION SDR DALA2024031303282Skin · wornWORN FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB). SUMMARY OF NRC 00013: FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10. (LP #0242390)SDR DALA2024031203223Floor Support · corrodedCORROSION OUT OF LIMITS AT FLOOR SUPPORT BTW STA Y=1022 AND STA Y=1060, ON X=44. SUMMARY OF NRC 00696: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1022 AND STA Y=1060, ON X=44 WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0239946)SDR DALA2024031103216Skin · dentedSEVERAL DENTS BTW 1 THRU 3 BEAMS AT AFT CARGO DOOR SKIN AND ALSO WORN SKIN AT AFT LWR DOOR SKIN CORNER. SUMMARY OF NRC 00016: OUTER SKIN AT AFT CARGO COMPARTMENT DOOR WAS FABRICATED AND REPLACED PER DWG 5910157 REV CW AND B717-200 SRM 51-41-02-0G. (LP #0237570SDR DALA2024031103215Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y986 TO STA Y1000 X=-60 AT CPAX. STRUCTURE WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.020IN. REMAINING THICKNESS IS 0.005IN THEREFORE REWORKED AREA IS OUT OF LIMITS. SUMMARY OF NRC 00697: CORROSION LEVEL 2. CUSP WEB BTW STA Y986SDR DALA2024031103214Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y408 AND X=- 60 AT CPAX. SUMMARY OF NRC 00569: CORROSION LEVEL 2. CUSP WEB BTW STA Y408 AND X=-60 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0235862)SDR DALA2024030803182Intercostal · corrodedCORROSION ON INTERCOSTAL BTW STA 636 TO 653 AND BTW LONGERONS 27-L TO 28-L AT FWD CC. SUMMARY OF NRC 00316: CORROSION LEVEL 2. INTERCOSTAL ON BTW STA 636 TO 653 AND BTW LONGERONS 27-L TO 28-L AT FWD CC WAS REPLACED PER B717 SRM 51-40-02-0G. (LP #0234436)SDR DALA2024030603064Web · corrodedCORROSION WAS FOUND AT DIAPHRAGM BEETWEN STA Y=198 AND X=54 (PASSENGER DOOR ENTRANCE). SUMMARY OF NRC 00616: CORROSION LEVEL 2. DIAPHRAGM BEETWEN STA Y=198 AND X=54 (PASSENGER DOOR ENTRANCE) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PAR 4 SDR DALA2024030503010Intercostal · crackedCRACK ON INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR. SUMMARY OF NRC 00059: INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR WAS FABRICATED AND REPLACED PER DWG 9955763 REV L, B717-200 SRM 51-41-01-0G AND 51-41-02-0G. (LP #0229988)SDR DALA2024030603063Skin · crackedCRACK ON INTERNAL SKIN NEAR TO BEAM #3 FWD EDGE WAS FOUND AT FWD CARGO DOOR. SUMMARY OF NRC 00745: INTERNAL SKIN NEAR TO BEAM #3 FWD EDGE AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3, FIGURE 201. (LP #0231760)SDR DALA2024030503004Tab · dentedSEVERAL DENTS ON RH SIDE OF RUDDER CONTROL TAB. SUMMARY OF NRC 00081: SEVERAL DENTS ON RH SIDE OF RUDDER CONTROL TAB WERE MEASURED AND FOUND WITH NO DISBONDS AND ARE WITHIN LIMITS PER B717-200 SRM 55-41-01-1A PROCEDURE I ALLOWABLE DAMAGE I PAR 3,A,(4),(C), ANDSDR DALA2024030402939Cusp Web · corrodedCRACK CUSP WEB RH LOWER AREA STA 696 CPAX. SUMMARY OF NRC 0547: CUSP WEB RH ON STA 655 TO STA 715 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, 51-41-02-0G, AND 51-41-05-0G. PERFORM A GVI EVERY "C" CHECK PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, PAR 6. SDR DALA2024030402936Floor Support · corrodedCORROSION ON FLOOR SUPPORT ON STA Y=200 BTW X=-44 AND X=-55 AT PAX COMPARTMENT. (W1). SUMMARY OF NRC 00553: CORROSION LEVEL 2. DUE TO EXCESS CORROSION (EXFOLIATION), FLOOR SUPPORT ON STA Y=200 BTW X=-44 AND X=-55 AT PAX COMPARTMENT (W1) WAS REPLACED PER DWG 99SDR DALA2024030402933Web · corrodedCORROSION ON MEMBRANE STA Y=201 BTW X=11 TO X=-44 AT PAX COMPARTMENT. (W1). CORROSION LEVEL 2. MEMBRANE STA Y=201 BTW X=11 TO X=-44 AT PAX COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R, PROCEDURE 2 REPAIR 2. (LP #0225731)SDR DALA2024022902795Web · corrodedCORROSION ON MEMBRANE STA Y=178 AND BTW X=-2 AND X=-26 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 0551: CORROSION LEVEL 2. MEMBRANE STA Y=178 AND BTW X=-2 AND X=-26 AT PASSENGER COMPARTMENT (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP #02225SDR DALA2024022902794Cusp Web · corrodedCORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN. SUMMARY OF NRC 0395: CORROSION LEVEL 2. CORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN WAS REMOVED B717-200 SRM 51-10-04-0G PAR 26 C (1). (UT) THICKNESS MEASUREMENT WAS ASDR DALA2024022802763Cusp Web · crackedCRACK ON CUSP WEB (LOWER AREA) BTW STA 1017 TO STA 1020 AND X=45 AT CPAX. SUMMARY OF NRC 00589: CUSP WEB (LOWER AREA) BTW STA 1017 TO STA 1020 AND X=45 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PRCEDURE 4 REPAIR 4. (LP #0221152)SDR DALA2024022602642Door Frame · corrodedEXFOLIATION CORROSION AT AFT CARGO LWR DOOR JAMB FROM STA Y=954 TO Y=996. SUMMARY OF NRC 00020: CORROSION LEVEL 2. AFT CARGO LWR DOOR JAMB FROM STA Y=954 TO Y=996 WAS REPLACED PER B717 SRM 53-20-15-2R REPAIR 7, 51-41-02-0G, AND 51-41-04-0G. (LP #0218389)SDR DALA2024022602640Longeron · corrodedCORROSION AT STA 130 APROX AND L30 COMPARTMENT E&E. SUMMARY OF NRC 00225: CORROSION LEVEL 2. LONGERON 30 STA Y=110 TO Y=130 WAS REPLACED PER DWG 5411401 REV DT AND B717-200 SRM 51-41-02-0G. (LP #0217998)SDR DALA2024022202461Floorbeam · corrodedCORROSION ON ANGLE OF FLOOR STRUCTURE STA Y=1053 X=20 AT CABIN PAX. SUMMARY OF NRC 00374: CORROSION LEVEL 2. ANGLE OF FLOOR STRUCTURE STA Y=1053 X=20 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0212052)SDR DALA2024022002326Frame · crackedCRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA. (FUS) SUMMARY OF NRC 0549: CRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. PERFORM AN EXTERNAL GVISDR DALA2024022002322Floor Support · crackedCRACK ON FLOOR SUPPORT STA 636 X=0 AND Z=-2 AT FWD CC. SUMMARY OF NRC 00309: FLOOR SUPPORT (INTERCOSTAL) STA 636 X=0 AND Z=-2 AT FWD CARGO WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #0205320)SDR DALA2023080406303Unknown · unknownTHE CENTER AISLE OVERHEAD RED EXIT SIGN IS BROKEN AND MISSING THE BACK HALF OF THE SIGN. MAINTENANCE REPLACED THE SIGNAGE. OPERATIONAL CHECK OF THE SIGN WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #4398332)SDR DALA2023060204427Unknown · unknownSHIP 9522 -MISC/DE- DURING APPROACH FOR LANDING, THE "BUS DC R OFF" INDICATION ILLUMINATED. WHICH WAS FOLLOWED BY 15 OTHER DISCREPANCY INDICATIONS. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED EMERGENCY DUE TO THE IMPENDING NO FLAP AND NO SLAT LANDING. A HOSDR DALA2022081605533None · noneSHIP 9522 -HYD/GEAR- THE AIRCRAFT EXPERIENCED A BIRD STRIKE WHICH DAMAGED HYDRAULIC LINES AND DUE TO THAT DAMAGE, LOSS FLUID OUT OF THE RIGHT HYDRAULIC SYSTEM. AN ALTERNATE GEAR EXTENSION WAS REQUIRED TO LOWER THE LANDING GEAR. AN EMERGENCY WAS DECLARED FOR THSDR DALA2022052403549Light · unserviceableTHE EVACUATION EXTERIOR EMERGENCY LIGHTS ON BOTH SIDES ARE INOPERATIVE. TRANSFER TO MEL 33-51-02A. NEEDS BATTERY. REPLACED OVERWING EMERGENCY LIGHT AND POWER SUPPLY BATTERY PER B717 AMM 33-51-06. NO HELP. REPLACED OVERWING EMERGENCY LIGHT POWER RELAY R2-273 PESDR DALA2022052403548Skin · crackedCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1022 BTW LONG 13RH-14 RH (FUS). SUMMARY OF NRC 00029: FUSELAGE SKIN STA Y=1022 WAS REPAIRED PER PRI 599215-14 REV. 2 AND ER/A 599215-14 REV ORIGINAL SECTION I: PERMANENET REPAIR. ACCOMPLISH REPETITIVE INSPECTION WITHIN EVSDR DALA2022052003455Frame · corrodedCORROSION ON FRAME CLIP STA Y=927 BTW LONG 27LH TO 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00191: CORROSION LEVEL 2, FRAME CLIP STA Y=927 BTW LONG 27LH TO 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G, SRM 51-41-05-0G. (LP #2242428)SDR DALA2022052003454Track · corrodedCORROSION ON RH TIE TRACK BTW STA Y=896-954 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00098: CORROSION LEVEL 2, TIE TRACK WAS REPLACED PER B717 SRM 51-41-01-0G BECAUSE IT IS OUT OF LIMITS PER B717 SRM-53-20-52-1A-2 PAR 4 FIG 101 AND B717 DC-MD/BOEING NDT MANUALSDR DALA2022052003457Battery Pack · inoperativeER/A 599216-14, FUSELAGE SKIN AT Y=1076 AND Y=1087, L-13R TO L-14R HAS CRACKS. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. ACCOMPLISH ER/A 599216-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 24 MONTH INTERVAL AFTER 17MAY22. ASSOCIATED ER/A 1SDR DALA2022051903434None · noneCRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND Y=1087 BTW LONG 13RH-14RH (FUS). SUMMARY OF NRC 00030: EXTERNAL FUSELAGE SKIN STA Y=1076 AND Y=1087 BTW LONG 13RH-14RH WAS REPAIRED PER ER/A 599216-14 REV. ORIGINAL SECTION L: PERMANENT REPAIR AND PRI 599216-14 RSDR DALA2022051803423None · noneCORROSION ON FRAME CLIP STA Y=908 BTW LONG 28LH TO 28 RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00190: LEVEL CORROSION 2, FRAME CLIP STA Y=908 BTW LONG 28LH TO 28 RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2239592)SDR DALA2022051703372Skin · debondedDISBOND (0.700 IN LENGTH X 0.700 IN WIDTH) ON RHS I/B FIXED VANE, UPPER SKIN 60.5 IN FROM I/B END AND 5.5 IN FROM T/E. SUMMARY OF NRC 00317: INBOARD FIXED VANE, UPPER SKIN AT RH WING WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE OF SDR DALA2022051703371Skin · debondedIN REF NRC 00116: ONE DISBOND WAS FOUND ON DENT STA XV1=143 OF 1.500 IN X 1.100 IN LENGTH / WIDTH ON INBOARD FIXED VANE UPPER SKIN AT LH WING. SUMMARY OF NRC 00311: INBOARD FIXED VANE UPPER SKIN AT LH WING WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GSDR DALA2022051603339None · noneCRACK ON BEAM #1 STA=160 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00089: BEAM #1, STA=160 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B-717 SRM 52-10-02-2R REPAIR 7. (LP #2237275)
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