N938AT
Service difficulty reports · 150
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 = 'N938AT' 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 = 'N938AT' 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 DALA2026100705545Flap · damagedFOUND DAMAGE ON LEFT TRAILING EDGE FLAP, INSTALLED PERMANENT REPAIR PER B717 SRM 57-00-01-02A. (9483579) (AIRCRAFT GROUNDED).SDR DALA2026071404143Display · faultedDIVERTED TO BWI DUE TO SYSTEM DISPLAY CONTROL PANEL FAULTS. REPLACED EFIS DISPLAY SELECT PANEL IAW AMM 31-62-01. OPS CHKD GOOD. (8290442) (AIRCRAFT GROUNDED)SDR DALA2026070803992Lamp · inoperativeCOCKPIT EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-11. (8290423) (AIRCRAFT GROUNDED).SDR DALA2026012200495Unknown · vibrationDIVERTED TO SYR DUE TO AIRFRAME VIBRATIONS IN FLIGHT. PERFORMED AIRFRAME VIBRATION INSPECTION PER AMM. PERFORMED IDLE ENGINE RUN WITH BOTH VIBRATION INDICATIONS WITHIN LIMITS. OPS CHECKS NORMAL.(7787876)SDR DALA2026012200494Battery Pack · inoperativeNUMEROUSE EMERGENCY CEILING LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK B5-231 AND OPS CHECKED GOOD IAW BN717 AMM 33-21. (8406044)SDR DALA2025111808426Module · inoperativeDIVERTED TO MSN DUE TO FUEL QUANTITY INOPERATIVE. REPLACED ELECTRONIC MODULE. OPS CHECK NORMAL.(1301584)SDR DALA2025070805069Valve · bindingSHIP 9561 -ATB- DUE TO CLT DUE TO SMOKE IN THE CABIN COMING FROM FWD GALLEY AREA. SMOKE DISSIPATED AND EMERGENCY WAS DECLARED. CORRECTIVE ACTION: FOUND BUFFER AIR VALVE BINDING. REPLACED SAME. OPS CHECKS GOOD.SDR DALA2025043003320Battery Pack · inoperativeEMERGENCY LIGHTS (3 EA) LOCATED AT CEILING PANEL IN FRONT OF FWD LAVATORY, EXIT SIGN AT TOP OF COW 1 AND ABOVE THE SERVICE DOOR DOES NOT OPERATE. THE POWER ASSEMBLY BATTERY PACK WAS REPLACED PER B717-200 AMM 33-51-04. TEST OK. (LP #6915838)SDR DALA2025042403189Skin · wornWEAR ON SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR. WORN SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR WAS REPAIRED PER PRI 625059-14 REV 7 AND ER/A 625059-14 REV ORIGINAL SECTION I: PERMANENT REPAIR.SDR DALA2025041602959Doubler · crackedCRACK FOUND ON INTERNAL DOUBLER AT STA Y=1178 CANT LONGERON 17RH AT AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00686: INTERNAL CAP DOUBLER AT STA Y=1178 CANT LONGERON 17RH AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 RESDR DALA2025041202832Longeron · crackedCRACK WAS FOUND BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE. SUMMARY OF NRC 00660: CRACK BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE WAS REPAIRED PER ERA 625404-14 REV ORIGINAL SECTION 1: PERMANENT REPAIR. ASSOCIATED ER/A 14-625404 ADDED FOR AC 956SDR DALA2025041202830Access Panel · corrodedCORROSION OUT OF LIMITS ON COUNTERSINKS OF ACCESS PANELS: 520CB (3 HOLES), 520DB (4 HOLES), 520FT (6 HOLES), 620GB (3 HOLES), 620FT (2 HOLES), AND 620DT (3 HOLES) PER B717-200 SRM 57-10-01-2R PROCEDURE 2. SUMMARY OF NRC 00631: CORROSION LEVEL 2. ACCESS PANELS:SDR DALA2025040802704Cargo Track · corrodedDUE TO CORRISION REWORK, (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON SIDE TIE TRACK BTW L27L TO L28L AND STA=900 LH TO STA=1022 LH AFT CARGO COMPARTMENT. WITH AN ORIGINAL THICKNESS OF 0.060IN, AND MINIMUN REMAINING THICKNESS OF 0.027IN. THE AREA REWORKED ISSDR DALA2025040802702Frame · corrodedCORROSION ON FRAME STA Y=870 L29L TO L29R. ORIGINAL THICKNESS IS 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.029IN THEREFORE AREA IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A PAR 4C (2) FIG 103. SUMMARY OF NRC 00663: CORROSION LEVEL 2. FRAME STA Y=870 L29L TSDR DALA2025040802700Skin · corrodedCORROSION ON BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE (CENTER SECTION). (EHV). SUMMARY OF NRC 00383: CORROSION LEVEL 2. BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE WAS REPAIRED PER PRI 624982-14 REV 1 & ER/A 624SDR DALA2025040802698Pan · corrodedCORROSION AROUND DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/28R. SUMMARY OF NRC 00305: CORROSION LEVEL 2. DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/28R WAS REPLACED AND INSTALLED PER B717 SRM 53-20-15-2R-7 REPAIR 7. (LP #0896016)SDR DALA2025040402565Frame · crackedCRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00149: CRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20 -07-2R PROCEDURE 3 REPAIR 3. PERFORM VISUAL INITIAL INSDR DALA2025040402564Longeron · corrodedCORROSION OUT LIMITS, IN REFERENCE TO NRC 00163: CORROSION ON LONGERON BTW STA Y=956 TO STA Y=964 L30 AT AFT CARGO COMPARTMENT WITH ORIGINAL THICKNESS IS 0.125IN AND MINIMUM REMAINING THICKNESS IS 0.055IN, THEREFORE AREA IS OUT OF LIMITS PER B717-200 SRM 53-00SDR DALA2025040302495Angle · corrodedCORROSION ON ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00300: CORROSION LEVEL 2. ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLESDR DALA2025040302493Strap · crackedCRACKED STRAP STA Y 1178 CANT UPPER CHORD, PROJECTION LONG 2 RH AT AFT ACCESORY COMPARTMENT. INITIAL INSPECTION: PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK PER TOPP MANUAL 30-10-70 PAR I PAGE 14. LOG PAGE FOR CRACKED STRAP STA Y 1178 CANT UPPER CHORD, PRSDR DALA2025033102352Skin · crackedCRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00035: CRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 624820-14 REV 3 AND ER/A 624820-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GVI EVERY 24 MONTSDR DALA2025033102350Skin · crackedCRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L. SUMMARY OF NRC 00444: CRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L WAS REPAIRED PER PRI 625028-14 REV 1 AND ER/A 625028-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GENERAL VISSDR DALA2025032402191Skin · dentedDENT ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE. SUMMARY OF NRC 00554: AREA DAMAGE WAS REPAIRED ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP #0873498)SDR DALA2025032402189Pan · crackedCRACKED PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2. SUMMARY OF NRC 00096: PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2 WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8 FIGURE 202, 51-41-02-0G PROCEDURE GENERAL, AND 51-41-05-0G. (LSDR DALA2025032402188Beam · crackedCRACK ON BEAM #8 AFT SIDE AT PASSENGER DOOR. SUMMARY OF NRC 00083: BEAM #8 AFT SIDE AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 14 PAR 6. (LP #0871639)SDR DALA2025032402187Pan · crackedA CRACK WAS FOUND ON THE #2 INNER PAN AT AFT EDGE OF THE FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00598: INNER PAN ON AFT EDGE BEAM #2 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R-3 PROCEDURE 3 REPAIR 3. (LP #0871599)SDR DALA2025032402186Door Frame · crackedCRACK ON BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00290: BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0871550)SDR DALA2025032102134Frame · crackedCRACK OF 0.093 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #090-0004, STEP 10). SUMMARY OF NRC 00281: FRAME TAB ON THE OVERWING FRAME AT STA Y= 696.000 RH WAS REPAIRED PER CARSDR DALA2025032102132Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PASSENGER. SUMMARY OF NRC 00338: CRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53- 00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 203. (LP #0868343)SDR DALA2025032002096Frame · crackedCRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN. SUMMARY OF NRC 00360: CRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN WAS REPAIRED PER B717-200 53-20-07-2R REPAIR 4. (LP #0866910)SDR DALA2025032002094Cusp Web · damagedELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER. SUMMARY OF NRC 00339: ELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REP 4. (LP #0866724)SDR DALA2025031902063Cusp Web · crackedCRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER. SUMMARY OF NRC 00330: CRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4, PAR 5, FIG 223, AND FIG 226. (LP #0864855)SDR DALA2025031702029Frame · crackedCRACK ON FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN. SUMMARY OF NRC 00361: FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0861190)SDR DALA2025031702025Longeron · crackedCRACK ON INTERNAL AREA OF LONGERON 7R, 8R, 5R, STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00363: LONGERON 8R, 5R, STA Y=1022 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 AND LONGERON 7R NO DAMAGE WAS FOUND PER DC-MD/BOEING NDTSPM PSDR DALA2025031702022Seat Track · corrodedCORROSION ON RH SEAT TRACK STA Y=236-238 -X=22 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00398: CORROSION LEVEL 2. CORROSION ON RH SEAT TRACK STA Y=236-238 -X=22 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-20-52-2R. PROC 1, REPAIR 1. (LP #SDR DALA2025031401969Longeron · crackedCRACK ON INTERNAL AREA OF LONGERON 5L STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00432: CRACK ON INTERNAL AREA OF LONGERON 5L STA Y=1022 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0856135)SDR DALA2024042604730Cover · missingTHE CABIN CEILING EMERGENCY STANDBY LIGHT LENS COVER IS MISSING AT SEAT ROW 3. MAINTENANCE FORWARDED IT TO NEF 33-21-02. CABIN LIGHT LENS MISSING SEAT ROW 3. (LP #0309494)SDR DALA2024010500149Unknown · unknownTHE EMERGENCY LIGHTS FROM ROW 1 TO ROW 13 CEILING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT B5-227 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5006827)SDR DALA2023102008641Unknown · unknownTHE LOWER EMERGENCY LIGHTS ARE INOPERATIVE AT THE AFT EMERGENCY EXIT. MAINTENANCE REPLACED THE BATTERY (B5-119) PER B717 AMM 33-51-04. ALL EMERGENCY LIGHT OPERATIONAL CHECKS ARE GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4620011)SDR DALA2023062305084Unknown · unknownON A SERVICE CHECK, THE SIDE PAX DOOR EMERGENCY EXIT LIGHT AND SERVICE DOOR SIDE EMERGENCY EXIT LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY B5-118 AND THE BATTERY ASSEMBLY IAW B717 AMM 33-51. (LP #4798653)SDR DALA2023052004046Unknown · unknownMAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE CABIN AT STA 715-737R TO BE INOPERATIVE. THE EMERGENCY LIGHTS BATTERY SUPPLY (B5-230) WAS REPLACED. OPERATIONAL CHECK WAS GOOD. (LP #4774723)SDR DALA2022090405925None · noneAIRCRAFT 9561, EXIT LOCATOR SIGN FWD/AFT FACING DOES NOT ILLUMINATE. LIGHTED SIGN IS LOCATED ON CEILING OF CABIN BETWEEN OVER-WING EMERGENCY EXITS. CORECTIVE ACTION: REPLACED EMERGENCY LIGHTS BATTERY ASSY (LP 9147282)SDR DALA2022041202525None · noneEMERGENCY LIGHTS AT LOWER AFT OVERWING DOOR ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7883681)SDR DALA2022010300010None · noneHIDDEN DAMAGE DURING THE DOUBLER REMOVE PROCESS. WEB DAMAGE WAS FOUND ON LEFT HAND SIDE, LOCATED ON INTECECTION STA 674 AND STGR 18LH. SUMMARY OF NRC 00175: WEB ON STA 674 LH WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #2071146)SDR DALA2021112407218None · noneTHERE ARE MULTIPLE CABIN EMERGENCY ESCAPE LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-121 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #8141196)SDR DALA2020111303714Battery Pack · inoperativeDURING A SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT CEILING PANELS 11, 12, AND 13 WERE INOPERATIVE. THE BATTERY PACK, B5-231, WAS REPLACED, PER B717 WDM 33-51-12. OPERATIONAL CHECK WAS SATISFACTORY. THE AIRCRAFT IS OK FOR SERVICE.SDR DALA2020031301823Pump · malfunctionedACCORDING TO THE AOS REPORT, EMERGENCY DECLARED - HYD R TEMP HI MESSAGE AFTER T/O. R&R RT ENG EDP PER B717 AMM 29-11. OPS AND LEAK CHK OK. ODI PAPERWORK C/W. PUMP, HYD, ENG 95-2911-9-0001 S/N 00019. (LP6906554)SDR 2020F00283Skin · delaminatedNON ROUTINE CHECK, UPPER AND LOWER SKINS OF THE RT WING SPOILER WAS DELAMINATED.SDR DALA2024012401104Skin · dentedDENT INSPECTION RHS AFT MOVABLE VANE, UPPER SKIN - QTY 6. #5) APPROX 25" FROM O/B EDGE & 4.5" FROM T/E. 5) DENT DIMENSIONS WIDTH 1.3" X DEPTH 0.024" APPROX 25" FROM O/B EDGE & 4.5" FROM T/E. IAW B717 SRM 57-53-01 AD 1 ACCOMPLISH DVI AND TAP TEST FOR POSSIBLE DSDR DALA2019121807399Skin · corrodedFUSELAGE SKIN CORRODED INTERNALLY AT CUTOUT FOR DRAIN MAST IN FLOOR OF E/E COMPARTMENT. EXTERNAL FILLET SEALER AROUND MAST SHOWS CORROSION PROTRUSION ALSO. NRC 001-0223:2570-2002/002 00076: (CORROSION LEVEL 2), REPLACED DOUBLER REF BOEING DWG #9923686. (LP #14
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