N948AT
Service difficulty reports · 269
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 = 'N948AT' 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 = 'N948AT' 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 DALA2026063003868Light · detachedLIGHTING OVER EXIT ROW 18-21 LEFT SIDE OF ACFT HANGING LOW. SECURED CABIN LIGHT COVER AS REQUIRED IAW AMM 33-51. (8906374) (AIRCRAFT GROUNDED).SDR DALA2026061003518Lamp · inoperativeOVERHEAD EMERGENCY LIGHT AT 24C INOP. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 24C PER B717 AMM 33-51. OPS CHK NML. OK FOR SVC. (LP 868086 - AIRCRAFT WAS GROUNDED)SDR DALA2026060903439Sliding Window · out of rigATB- PERFORMED AN AIR TURN BACK DUE TO THE CAPTAIN'S SLIDING WINDOW PARTIALLY OPENED DURING TAKEOFF. MAINTENANCE ADJUSTED AND RIGGED THE CAPTAINS CLEARVIEW WINDOW. (8680962)(AIRCRAFT GROUNDED)SDR DALA2026040802227Apu · odorCREW REPORTS ON TAXI IN APU START HAD FUEL FUMES THROUGHOUT CABIN. REPLACED APU. (1528181) (AIRCRAFT GROUNDED)SDR DALA2026031701820Pcdu · faultedABORTED TAKEOFF DUE TO A RIGHT GENERATOR OFF MESSAGE. MAINTENANCE REPLACED THE RIGHT PCDU AND RIGHT GENERATOR RELAY. ALL ENGINE RUNS AND RETURN TO SERVICE TESTS PASSED.SDR DALA2026021801129Pseu · failedRECEIVED A PSEU FAIL MESSAGE WITH AN ABNORMAL SLAT EXTENSION INDICATION. MAINTENANCE REPLACED THE PSEU DUE TO AN INTERNAL FAILURE FAULT CODE AND PERFORMED ALL APPLICABLE RETURN TO SERVICE TESTS.(8153812).SDR DALA2025110708138Panel · not reportedFABRICATED PANEL STILL NEEDS LIGHT ASSY INSTALLED. INSTALLED AFT COMPARTMENT LT PER B717 AMM 33-51. OP CHECK NORMAL . OK FOR SVC. (7724261)SDR DALA2025103107966None · noneMONITOR LOG FOR ER/A 619015-14AD REV A SECTION II. COMPLY WITH SECTION II OF ER/A 619015-14AD (1275112)SDR DALA2025091606817Fairing · damagedDAMAGE NOTED RUDDER FAIRING PANEL 370CR. ER/A 629084-14 CREATED TRACKING TEMPORARY REPAIR ACCOMPLISHMENT. (1191759)SDR DALA2025091606816Access Panel · damagedENGINEERING CREATES LOGPAGE TRACKING DAMAGE TO RUDDER ACCESS PANEL PER ER/A 628805-14. ER/A 628805-14 LOGPAGE CREATED TRACKING TEMPORARY REPAIR TO RUDDER ACCESS PANEL. (1191716)SDR DALA2025090406563None · noneER/A 622181-14AD REV ORIGINAL REQUIRES STAGE 2 DTA APPROVAL. ER/A 622181-14AD REV ORIGINAL REQUIRES STAGE 2 DTA APPROVAL ON OR BEFORE 24 MONTHS FROM 26-AUG-2025. (1167637)SDR DALA2025090906669Pulley Bracket · damagedL/E CAVITY AFT OF LT #2 SLAT. REPLACED PULLEY BRACKET PER BOEING DWG 5920286 (1164395)SDR DALA2025063004853None · noneSHIP 9508 TRACKING FOR DTE FOR 24 MONTHS FROM DATE OF REPAIR APPROVAL. CORRECTIVE ACTION: C/W ERA ERA 626897-14 REV ORIGINAL. (1033207)SDR DALA2025050803560Door Sill · corrodedAFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. REPAIRED PER REF B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. AFT CARGO DOOR JAMB LOWER PAN CORROSION DAMAGE SPLICE REPAIR CHECKED AND REPLACED HI-SHEAR FASTENERS PER REF B717-200 SRM 51-41-04-0G ANSDR DALA2025042303171Door Sill · corrodedAFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. MARKED. SUMMARY SEE NRC 001-0319:5231-2002/001 00174: REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. AFT CARGO DOOR JAMB LOWER PAN, CORROSION DAMAGE SPLICE REPAIR. CHECKED AND REPLACED HISDR DALA2024062706578Skin · crackedAIRCRAFT 9508, WHILE ACCOMPLISHING HFEC INSPECTION PER WORK CARD 5530-01048-02 IN COMPLIANCE WITH FAA AD 2018-10-08, MTC FOUND THREE (3) FASTENER HOLES IN THE VERTICAL STABILIZER LEADING EDGE SKIN (P/N 5910189-15) BELOW ZFS 52.267 WITH CRACK INDICATIONS. THE DSDR DALA2024062606518Skin · crackedCRACK INDICATION NOTED WORKING STEP 12 OF CARD 5530-01048-02 (AD 2018-10-08) WHILE PERFORMING OPEN HOLE HFEC. RH STAB L/E CRACK INDICATION IN SKIN LAYER ONLY. COMPLIED WITH N/R CARD 001 AND ER/A 619015-14AD REV ORIGINAL SECTION I PERMANENT REPAIR.SDR DALA2023111309310Unknown · unknownTHE EMERGENCY EXIT COVER IS MISSING AT 1R DOOR. MAINTENANCE INSTALLED A NEW EMERGENCY EXIT LIGHT COVER AT 1R DOOR PER B717 AMM 33-51. AIRCRAFT IS NOW OK FOR SERVICE. (LP #4294606)SDR DALA2023070405368Unknown · unknownPUNCTURES (2 EA) ON CTR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00172: CTR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #2847265)SDR DALA2023070305312Unknown · unknownPUNCTURES (4 EA) ON INBR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00033: INBR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10SDR DALA2023070305311Unknown · unknownDENTS (2 EA) ON INBR FIXED GUIDE VANE LOWER SKIN AT RH WING. SUMMARY OF NRC 00178: DENTS (2 EA) WITH THE MEASUREMENTS OF: DENT1 "D DIAMETER=2.000 IN, X DEPTH=0.0450, RATIO=44.444". DENT2 "D DIAMETER=1.200 IN, X DEPTH=0.0150, RATIO=80". (ET) HFEC WAS ACCOMPLISHSDR DALA2023070305304Unknown · unknownDISBONDS (2 EA) WERE FOUND ON RH WING AFT MOVABLE VANE UPPER SKIN. SUMMARY OF NRC 00102: RH WING AFT MOVABLE VANE UPPER SKIN WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #2844542)SDR DALA2023063005261Unknown · unknownDISBONDS (2 EA) WERE FOUND ON RH WING AFT MOVABLE VANE LOWER SKIN. SUMMARY OF NRC 00103: REPAIR WAS PERFORMED ON RH WING AFT MOVABLE VANE LOWER SKIN PER B717-200 SRM 57-53-01-2R-1 PAR.4. (LP #2841425)SDR DALA2023063005260Unknown · unknownDISBONDS (2 EA) WERE FOUND ON LH WING INBD FIXED VANE LOWER SKIN. SUMMARY OF NRC 00104: REPAIR WAS PERFORMED ON LH WING INBD FIXED VANE LOWER SKIN PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP #2841415)SDR DALA2023062805187Unknown · unknownCORROSION ON LOWER SIDE PLATE AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00122: CORROSION LEVEL 2. LOWER SECTION OF JAMB PAN WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. (LP #2837667)SDR DALA2023063005264Unknown · unknownCORROSION ON FLOOR SUPPORT WAS FOUND. SUMMARY OF NRC 00156: CORROSION LEVEL 2. FLOOR SUPPORT WAS FABRICATED PER DWG 993634-7 REV BW AND WAS REPLACED PER B717- 200 SRM 51-41-02-0G PAR 7, 51-41-05-0G PAR 8, AND 51-41-08-0G PAR 7. (LP #2834091)SDR DALA2023062805180Unknown · unknownCORROSION ON ANGLE ON AFT LOWER SEAL DEPRESSOR AT FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00124: CORROSION LEVEL 2. ANGLE ON AFT LOWER SEAL DEPRESSOR AT FWD CARGO COMPARTMENT DOOR JAMB WAS FABRICATED PER DWG 5910142 REV DJ AND REPLACED PER B717 SRM 51-SDR DALA2023051703948Unknown · unknownTHE LEFT FIXED FOWARD POSITION LIGHT LENSE COVER AND ATTACHING HARDWARE WAS DISCOVERED MISSING. THE LEFT FWD POSITION LIGHT LENS WAS FORWRDED TO CDL 33-42-03. ALL 'M' PROCEDURES WERE COMPLIED WITH. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #9957992)SDR DALA2022080205280Lens · missingTHE THRESHOLD LIGHT LENS WAS MISSING ABOVE 29C. MAINTENANCE INSTALLED THE STANDBY LIGHT LENS COVER IN THE AFT CABIN REF B717 AMM 33-52. (LP #9299354)SDR DALA2022050603164Battery · inoperativeAFT UPPER OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-230 PER B717 AMM 33-51. (LP #8616540)SDR DALA2021041902264Battery Pack · inoperativeTHE COCKPIT OVERHEAD EMERGENCY FLOOD LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT STA 175 ABOVE R1 DOOR PER B717 AMM 33-51. (LP #7444921)SDR DALA2021022501094Lens · missingTHE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 1C. MAINTENANCE INSTALLED A NEW EMERGENCY LIGHT COVER FOR THE FORWARD CABIN. OPERATIONAL CHECK WAS GOOD. (LP 1737515)SDR DALA2020102003406Structure · damagedON WALKAROUND FOUND DAMAGE ON FWD CARGO DOOR BOTTOM FWD CORNER. MAINTENANCE REMOVED FWD CARGO DOOR FROM A/C TO FACILITATE REPAIR, PER B717 AMM 52-31-01 020-001. CUT OUT DAMAGED AREA AS REQUIRED, PER B717 SRM 52-00-01-2R-8. PERFOREMED DAMAGE CONTAINMENT HFECSDR DALA2020030501635Plate · missing#2 ENG, UPPER COWL, INBOARD SIDE, HAS PLATE MISSING . MAINTENANCE ACCOMPLISHED SECTION I TIME LIMITED REPAIR PER ER/A 585840-14 REV ORIGINAL. COMPLIED WITH THE PERMANENT REPAIR PER ER/A 585840-14 REV O SEC II. THIS CLOSES THE MONITOR. AIRCRAFT IS OK FOR SERVICSDR DALA2020022311344Plate · missingTHE #2 ENG UPPER COWL HAS A PLATE MISSING ON THE INBOARD SIDE. MAINTENANCE ACCOMPLISHED A TIME LIMITED REPAIR, PER ER/A 547093-14MA AND DEFERRED THE PERMANENT REPAIR TO MONITOR TO BE ACCOMPLISHED WITHIN 10 CALENDER DAYS OF SECT 1 ACCOMPLISHMENT. MONITOR,#2 ENGSDR DALA2020013000697Cover · missingTHE EMERGENCY EXIT LIGHT IS MISSING THE COVER. MAINTENANCE REPLACED THE EXIT COVER PER B717 AMM 52-22. OK FOR SERVICE.SDR DALA2020011300236Battery · dischargedTHE LT AND RT OVERWING EXIT IDENTIFIER SIGNS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY/ POWER PACK IAW AMM 33-51. OPERATIONAL CHECKS ARE NORMAL.SDR DALA2019112286839Connector · damagedDURING SERVICE CHECK MAINTENANCE FOUND THAT THE CEILING MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 24 LEFT IS INOPERATIVE. RELAMPED WAS NO HELP. NO POWER TO LIGHT ASSEMBLY. FWD TO MEL 53-51-01A. PLACARDS INSTALLED. 21NOV19 RDU: FOUND PLUG P1-6724 WIRES PULLED SDR DALA2019111806743Power Supply · inoperativeDURING SERVICE CHECK MAINTENANCE FOUND THAT THE LOWER EMERGENCY EXIT IDENTIFIERS WERE INOPERATIVE AT ROW 20. MAINTENANCE REPLACED POWER SUPPLY B5-119. OPERATIONAL CHECK IS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #6754276)SDR DALA2019071304237Window Frame · crackedCRACK ON FRAME OF CLEAR VIEW WINDOW RT, UPPER AFT CORNER. (CPIL). NRC 00528: REPAIR SECTION I WAS PERFORMED ON FRAME OF CLEAR VIEW WINDOW RT, UPPER AFT CORNER PER ER/A 579524-14 REV ORIGINAL AND ETI-17-19-110 REV. 9. NO LEAKS WERE FOUND PER AMM 21-30-00 780-80SDR DALA2019071304236Skin · corrodedSEVERAL CORROSION POINTS ON FUSELAGE SKIN BTW STA Y=794 TO Y=851 BTW LONG 26L TO 26R AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00420: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579SDR DALA2019071304235Splice · corrodedCORROSION ON SPLICE BTW LONG 26L TO 26R AT STA Y=815 AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00421: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579396 ADDED FOR AC 9508. (LP #1168SDR DALA2019071304234Window Frame · crackedCRACK ON FRAME OF CLEAR VIEW WINDOW LT, UPPER AFT CORNER. (CPIL). NRC 00527: CRACK WAS REPAIRED PER SRM 56-10-02-2R-1 REPAIR 1 FIG.201, PERFORM LEAK CHECK PRESSURIZATION PER AMM 21-30-00 780-801. NO LEAKS WERE FOUND. (LP #1168010)SDR DALA2019071104149Frame · crackedINITIAL INSPECTION: CRACK ON FRAME STA 1225 CANT BTW 3/4 O CLOCK POSITION AT AFT FUSELAGE. SUMMARY: OF NRC 00412 AREA WAS REPAIRED PER ER/A 579525-14 REV. ORIGINAL AND ETI-17-19-118 REV 2 ( PERMANENT REPAIR). (LP1164569)SDR DALA2019071004139Hinge · crackedINITIAL INSPECTION: CRACK ON INBD FLAP FAIRING HINGE AT STA. XRS =137. 750 AT LT WING. (AI). INB FLAP HINGE FAIRING WAS REPLACED SERVICEABLE PN: 5912150-509 PER DWG 5910134 AND AMM 20-50-01-911-801 TOOL USED P/N TE25AC S/N 1049 DUE DATE 21/AUG/19. (LP1163426)SDR DALA2019070904113Access Panel · corrodedPART RACKS: CORROSION ON COUNTERSUNK AREA ON FUEL ACCESS PLATES NR 520DT AND 520GB. CORROSION LEVEL 2. FUEL ACCESS PLATES NR 520DT AND 520GB WERE REPLACED AND VERIFIED PER IPC 57-22-01-01 ITEM 015 AND IPC 57-23-01-01 ITEM 345. (LP1161708)SDR DALA2019070904112Skin · crackedAWR IN REFERENCE MON 2071758 : A CRACK WAS FOUND ON DENT # 10 AT RT AFTER MOVABLE VANE LOWER SKIN (AD). SUMMARY OF THIS N.R.C. 00747": IN REFERENCE MON 2071758 CRACK IN DENT NO. 10 (LOCATION: 25" OF INBD EDGE AND 14" OF T/E) WAS REPAIRED AT LOWER SKIN AFT MOVASDR DALA2019070804078Release Cable · brokenINITIAL INSPECTION: BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE EMERGENCY RELEASE SYSTEM. BROKEN STRANDS ON CONTROL CABLE (LT MIDDLE) OF TAIL CONE EMERGENCY RELEASE SYSTEM WAS REPLACED PER AMM 53-52-01-830-802. OPERATIONAL TEST WAS PERFORMED PER ASDR DALA2019070804077Access Panel · corrodedPART RACKS: CORROCION ON COUNTERSINK AREA ON FUEL ACCESS PLATE NBR 620DT AND 620DB. CORROSION LEVEL 2. FUEL ACCESS PLATE NR 620DT AND 620DB WERE REPLACED PER SRM 57-10-01-2R REPAIR 2 PAR.5C CONDITION III TABLE 201, VERIFIED PER IPC 57-22-01-01 ITEM 020 AND IPCSDR DALA2019070804076Access Panel · damagedPART RACKS: ELONGATED HOLES ON FUEL ACCESS PLATES NBR 141AL AND 520CB. ACCESS PLATES NBR 141AL AND 520CB WERE REPLACED AND VERIFIED PER IPC 57-22-01-01 ITEM 015, IPC 57-23-01-01 ITEM 465J. (LP1160237)
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