N998AT

Service difficulty reports · 212

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 = 'N998AT' 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.

SDR DALA2026100505510Skin · damagedFUSELAGE SKIN FS 294-351 S-28R TO S-27L DAMAGED. REPAIRED PER ER/A 590835-14. (1845326) AIRCRAFT WAS GROUNDED.Oct 2, 2026 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026092505347Skin · dentedFOUND DENT AFFECTING THE FUSELAGE SKIN BETWEEN STA 237 TO 256 AND L-15 -16R, COMPLIED WITH ER/A 624583-14. (1829579) (AIRCRAFT GROUNDED).Sep 24, 2026 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026090404999Unknown · odorCREW REPORTED A BURNING ELECTRICAL ODOR, INSPECTED ALL COFFEE MAKERS AND OVENS FOR RESIDUAL DEBRIS. NO DEBRIS NOTED; ALSO RAN COFFEE MAKERS AND OVENS, NO ODOR TO REPORT. PERFORMED MAINTENANCE TAXI WITH BOTH ENGINES; NO ELECTRICAL BURNING ODOR NOTICED WITH GENSep 4, 2026 · N998AT · Boeing 717200 · Air Distribution SystemSDR DALA2026080604551Electrical Sys · faultedATO- APPROX 60KTS DUE TO ELECTRICAL FAULT AND STICK PUSHER FAIL ANNUNCIATION. PERFORMED ENGINE RUN WITH BOTH ENGINES AT ALL POWER SETTINGS NO FAULTS NOTED. RT GENERATOR CAME ONLINE AND POWER WAS STABLE WITH NO FLICKERING, REF. AMM 71-00 UNABLE TO DUPLICATE FAug 5, 2026 · N998AT · Boeing 717200 · Electrical Power SystemSDR DALA2026060903442Unknown · noiseDIV- CREW REPORTED A BEEPING NOISE FROM FIRST CLASS TO EMERGENCY EXIT UNDER FLOOR AREA. (FOSR) EMERGENCY DECLARED WITH ATC. INSPECT AIRCRAFT COULD NOT DUPLICATE, PERFORMED LAV SMOKE DETECTOR TEST, ALL NORMAL AIRCRAFT RETURNED TO SERVICE. (8834624) (AIRCRAFT May 30, 2026 · N998AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2026042902734Ecu · failedAPU AUTO SHUTDOWN PROCESS BEGAN. RAN THE QRH WITH NO FIRE VISIBLE. APU WAS SHUT DOWN. THERE WAS AN ELECTRICAL SMELL IN THE AFT CABIN. R/R APU ECU REF B717 AMM 49-61 (8304376) (AIRCRAFT GROUNDED)Apr 26, 2026 · N998AT · Boeing 717200 · APU Start/Ignition SystemSDR DALA2026021801126Valve · odorDIRTY SOCK ODOR. REPLACED 35 DEGREE VALVE & MUFFLER IAW AMM 21-54. (8499820).Feb 10, 2026 · N998AT · Boeing 717200 · Air Distribution SystemSDR DALA2026020900917Unknown · odorDIRTY SOCK ODOR DURING DESCENT AT 14,000 FT, ANTI-ICE WAS ON CABIN DID NOT NOTICE THE ODOR, STRONG ODOR IN COCKPIT. FOUND AN OIL/FUEL LIKE MIX TO COME OUT. INSPECTED THE START OF THE APU BLEED DUCT FOR ANY FLUIDS, NO FLUIDS FOUND, ALL FURTHER FINDINGS ANFeb 1, 2026 · N998AT · Boeing 717200 · Air Distribution SystemSDR DALA2026010500070Engine · fireREJECTED TAKEOFF AT 140 KNOTS DUE TO A LEFT ENGINE FIRE INDICATION. FOUND LEFT ENGINE INNER CORE PANELS DAMAGED AND BLOWN OUT. ALSO NOTED DAMAGED FIRE DETECTOR SENSOR, NO EVIDENCE OF FIRE. DUE TO DAMAGE FOUND, ENGINE CHANGE REQUIRED.(7793260)Jan 2, 2026 · N998AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR DALA2025101707598Idg · faultedSHIP 9547-MISC/DE- ON DESCENT THE CREW RECEIVED A "RT GEN OFF" MESSAGE WITH THE APU ON MEL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED ALL RTS TESTS.(7586116)Oct 14, 2025 · N998AT · Boeing 717200 · AC Generator-AlternatorSDR DALA2025101707599Oil System · leakingSHIP 9547 OIL FUMES PRESAENT IN COCKPIT AND FORWARS GALLEY WITH APU RUNNING AND LEFT PACK IN AUTO. COCKPIT SMELLED OF FRESH OIL & GALLEY SMELLED OF BURNED POPCORN. CORRECTIVE ACTION: CLEAN AND BURN OUT THE PNEMATIC HIGH PRSSEURE DUCTING PER B717 AMM 21-51. OPEOct 12, 2025 · N998AT · Boeing 717200 · APU Oil SystemSDR DALA2025051503782Power Supply · inoperativeFOUND EMERGENCY LIGHTS TO BE INOPERATIVE FOR THE TAILCONE HANDLE RELEASE AND WALKWAY. MAINTENANCE REPLACED B5-260 EMERGENCY LIGHTS BATTERY POWER SUPPLY AND BATTERY IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7027929)May 15, 2025 · N998AT · Boeing 717200 · Emergency LightingSDR DALA2025042103073Pan · crackedCRACK ON UPPER PAN. ALSO FWD EDGE PAN ON BEAM #2 CRACKED AT LH FWD EMERGENCY EXIT. SUMMARY OF NRC-00781: UPPER PAN AND ALSO FWD EDGE PAN CRACKS ON BEAM #2 AT LH FWD EMERGENCY EXIT WERE REPAIRED PER B717-200 SRM 52-20-02-2R PROCEDURE 1 REPAIR 1. (LP #0919966)Apr 18, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025042103072Skin · damagedWORN AND BENT ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1. ALSO LOOSE RIVETS ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1 (LOWER REAR AREA). SUMMARY OF NRC 00238: REPAIR DOUBLER OF PASSENGER ENTRANCE DOOR SKIN L1 (LOWER REAR AREA) WAS FABRICApr 18, 2025 · N998AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2025041602960Pan · crackedCRACK ON INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC-00139: INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 623951-14 REV ORIGINAL. ASSOCIATED ER/A 14-623951 ADDED FOR AC Apr 16, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025041202833Cargo Track · corrodedCORROSION ALONG OF LH TRACK BTW STA=1022-890, STA=898-851 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0255: CORROSION LEVEL 2. LH TRACK BTW STA=1022-890, STA=898-851 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-40-04-0G, 51-41-01-0G, AND 51-41-05-0G.Apr 12, 2025 · N998AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025040902760Repair · misinstalledFASTENER DISCREPANT INSTALLATION ON PREVIOUS FUSELAGE SKIN REPAIR, ALSO THERE ARE LIGHTNING STRIKES AT TWO LOCATIONS ADJACENT TO REPAIR FASTENERS AT AFT LH ALTERNATE STATIC PORT AREA BTW STA Y=256-362 AND BTW LONG 26LH-27RH. SUMMARY OF NRC 00664: FASTENER DISCApr 9, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025040902758Longeron · corrodedCORROSION ON LONGERON 30 STA=994-946, STA=927-908 AFT CARGO COMPARTMENT. SUMMARY OF NRC 0256: CORROSION LEVEL 2. LONGERON 30 STA=994-946, STA=927-908 AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PARAGRAPH 8 AND 51-41-02-0G PARAGRAPH 4. (LP #Apr 8, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025040802699Vane · dentedDENTS ON AFT MOVABLE VANE (LOWER SURFACE) AT LH WING. SUMMARY OF NRC 00468: AFT MOVABLE VANE (LOWER SURFACE) AT LH WING WAS REPAIRED PER ER/A 624886-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI REV 2. ASSOCIATED ER/A 14-624886 ADDED FOR AC 9547. (LP #08Apr 4, 2025 · N998AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025040802697Support · crackedCRACKED ON SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00740: SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 FIG 201. (LP #0895966)Apr 4, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025040302494Retainer · crackedCRACK WAS FOUND ON RETAINER OF LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00878: CRACK ON RETAINER OF LH SLIDING WINDOW CUTOUT WAS REPAIRED PER ER/A 624944-14 REV ORIG SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624944 ADDED FOR AC 9547. (LP #0891407)Apr 2, 2025 · N998AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025033102354Repair · crackedCRACKED PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH. SUMMARY OF NRC 00334: PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH, WERE REPLACED PER B717-200 SRM 5Mar 29, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025033102351Pan · crackedCRACKED INNER PAN OVER BEAM #4 AFT EDGE, AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00171: INNER PAN OVER BEAM #4 AFT EDGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 623968-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623968-14 REV 2. ASSOCIATEMar 28, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025033102348Skin · dentedPERFORM REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP. SUMMARY OF NRC 00637: SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP WAS REPAIRED PER ER/A 624583-14AD REV ORIGINAL SECTMar 27, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025033102346Longeron · crackedCRACK LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00456: LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. (LP #087885Mar 26, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025032502209Longeron · corrodedCORROSION ON END-LONGERON BTW STA 1002 LONGERON 27RH AT AFT CARGO COMPARTMENT. SUMMARY OF THE NRC 00284: CORROSION LEVEL 2. END-LONGERON BTW STA 1002 LONGERON 27RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (UT) THICKNESS MEASURED WAS Mar 24, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025032402190Support · corrodedCORROSION ON INNER STRUCTURE OF RUDDER YOKE BEARING SUPPORT HOUSING. SUMMARY OF NRC 00770: CORROSION LEVEL 2. AREA ON INNER STRUCTURE OF RUDDER YOKE BEARING SUPPORT HOUSING WAS REPAIRED PER ER/A 619864-14TR REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED EMar 23, 2025 · N998AT · Boeing 717200 · Rudder StructureSDR DALA2025032402184Access Panel · corrodedCORROSION ON CONTACT AREA OF FUEL ACCESS PLATE 620QB. ALSO, CORROSION ON FASTENER HOLES OF PLATE 620JB AT RH WING. SUMMARY OF NRC 00604: CORROSION LEVEL 2. ACCESS PLATE 620JB WAS REPLACED AND VERIFIED FOR A NEW ACCESS PLATE PER B717-200 AIPC 57-23-01-01 ITEM 2Mar 21, 2025 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025032402183Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PLATES 620GB, 620HB, 620CB, 620FT, 620DB, AND ARB0872-535 AT RH WING WAS FOUND. SUMMARY OF NRC 00602: CORROSION LEVEL 2. FUEL ACCESS DOORS 620FT AND 620DB WERE REPAIRED PER B717-200 SRM 57-10-01-2R PROCEDURE 2. FUEL ACCEMar 21, 2025 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025032102133Barrel Nut · corrodedCORROSION ON HORIZONTAL STAB BARREL NUTS RH SIDE #13 AND #27. SUMMARY OF NRC 00800: LEVEL CORROSION 2. BARREL NUTS HORIZONTAL STAB RH SIDE #13 AND 27 WERE REPAIRED PER PRI 624606-14 REV 1 & ER/A 624606-14 REV ORIG. SECTION I: PERMANENT REPAIR APPROVAL IS LIMITMar 20, 2025 · N998AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2025031902066Floor Support · corrodedCORROSION ON FLOOR SUPPORTS BTW STA Y=210 TO STA Y=218 X=-11, Y=180 TO STA Y=190 X=-56, STA Y=190 TO STA Y=198 X=54, STA Y=197 X=22 TO X=42 AND STA Y=180 X=-22 TO X=-42, STA X=7RH BTW Y=148-200, IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A PROCEDURE ALLOWABLEMar 19, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031902062Pan · crackedCRACK ON INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00532: INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #0864707)Mar 18, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031401970Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID PASSENGER CABIN. SUMMARY OF NRC 00649: CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID CABIN PASSENGER WAS REPAIRED PER B-717-200 SRM 53-00-55-2R REP 4, PAR 5, FIG 212. (LP #0856963)Mar 14, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031201904Frame · crackedCRACK AT FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00638: FRAME 1037 CROSSING WITH L17L INTERNAL STRUCTURE FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0853086)Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025031201902Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH WAS REPAIRED PER B717-200 SRM 53-10-01-2R, PROCEDURE 10, REPAIR 10, FIGURE 2Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025031201901Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH WAS REPAIRED PER B717-200 SRM 53-10-01-2R, PROCEDURE 10, REPAIR 10, FIGURE 2Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025031101891Pan · crackedCRACKS ON INNER PAN AT BEAM 5 (AFT EDGE) AND BEAM 3 (FWD EDGE) AT FWD CARGO DOOR WERE FOUND. SUMMARY OF NRC 00501: INNER PAN AT BEAM 5 (AFT EDGE) AND BEAM 3 (FWD EDGE) AT FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 7 REPAIR 7, 52-30-02-Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031101889Frame · crackedCRACK AT FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE. SUMMARY OF NRC 00644: FRAME STA 1037 AND L17R INTERNAL STRUCTURE OF FUSELAGE WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0851423)Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025031101892Skin · corroded-AD- CORROSION ON AFT EDGE LOWER SKIN OF WING BOX STA Y=747 X=15-25 RH AT RH MLG W/W AREA. SUMMARY OF NRC 00670: CORROSION LEVEL 1. CORROSION ON AFT EDGE LOWER SKIN OF WING BOX STA Y=747 X=15-25 RH AT RH MLG WAS REPAIRED PER ER/A 624679-14AD REV ORIGINAL SECTIMar 10, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025031101887Longeron · crackedCRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00652: CRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL STRUCTURE FUSELAGE WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201 AND (ET) Mar 10, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025031001821Longeron · crackedCRACK AT LONGERON 6R STA 1022 INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00794: CRACK AT LONGERON 6R STA 1022 INTERNAL STRUCTURE FUSELAGE WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0847702)Mar 8, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025031001820Cusp Web · corrodedCORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=660-665, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, PER B717-200 SRM 53-00-55-1A-1 PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR. 4. A. FIG 101. SUMMARY OF NRC 00Mar 8, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025030601745Cusp Web · corrodedCORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=777-780, PER B717 SRM 51-10-02-0G PAR 8.F.(1). SUMMARY OF NRC 00832: CORROSION LEVEL 2. RH CUSP WEB STA Y=777-780 WAS REPAIRED PER B717-200 SRM 53-00-55-2R, PROCEDURE 4, REPAIR 4. (LP Mar 6, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025030501714Cusp Web · corrodedCORROSION OUT OF LIMITS, IN REF TO NRC 0642. CORROSION ON RH CUSP WEB STA Y=262-270, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, PER B717-200 SRM 53-00-55-1A-1 PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4. A. FIG 101. SUMMARY OF NRC 008Mar 5, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025030501713Cusp Web · corrodedCORROSION OUT OF LIMITS, IN REF TO NRC 0642: CORROSION ON RH CUSP WEB STA Y=389, ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, PER B717-200 SRM 53-00-55-1A-1 PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR. 4. A. FIG. 101. SUMMARY OF NRC 00830Mar 5, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025030501712Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=717 -X=44 RH SIDE AT MID PASSENGER CABIN. SUMMARY OF NRC 00650: CUSP WEB BTW STA Y=717 -X=44 RH SIDE AT MID PASSENGER CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 221. (LP #0841317)Mar 5, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025021801195Skin · dentedPERFORM PERMANENT REPAIR DUE TO DENT ON EXTERNAL SKIN OF AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE. SUMMARY OF NRC 00299: EXTERNAL SKIN OF AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE WAS REPAIRED PER B717-200 SRM 52-00-01-02R PROCEDURE 8 REPAIR 8 FIGURFeb 16, 2025 · N998AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2025030601774Access Door · missing-PDA- THE LEFT ELEVATOR LEFT CENTER HINGE NUT ACCESS LOWER DOOR IS MISSING. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED. FWD TO CDL 55-25-01, PLACARD INSTALLED. SUMMARY NRC 00528: NUTS OF ELEVATOR HINGE ACCESS DOORS WERE INSTALLED PER B717 AMM 20-50-01. (LP #Dec 3, 2024 · N998AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2024071607170Stringer Splice · damagedSTR 26L PRODUCTION SPLICE AREA, 1EA FASTENER SHOWS INDICATION WITH VISIBLE DAMAGE TO THE BACKSIDE OF THE STRINGER HOLE-LOCATED FIVE HOLES AFT OF PRODUCTION CUT LINE (MARKED) REF PRI 610260-14 REV 2 STEP 7. SUMMARY SEE NRC 004-0001:10-0653-8-7621/004 00009: COMJul 14, 2024 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024071607169Skin · dentedC/W ER/A 610260-14 REV B FUSELAGE SKIN DENTS. SUMMARY SEE NRC 004-0001:10-0653-8-7621/002 00006: COMPLIED WITH ER/A 610260-14 REV B. PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS. ENSURED ALL ER/A 610260-14 REV B. PRI REV "0", "Jul 14, 2024 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
Back to N998AT