# Service difficulty reports: N998AT

A list on [N998AT](https://openairdocs.org/aircraft/N998AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 212 reports

- [SDR DALA2026100505510](https://openairdocs.org/sdr/DALA2026100505510.md): Skin · damaged · Oct 2, 2026 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 294-351 S-28R TO S-27L DAMAGED. REPAIRED PER ER/A 590835-14. (1845326) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026092505347](https://openairdocs.org/sdr/DALA2026092505347.md): Skin · dented · Sep 24, 2026 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND DENT AFFECTING THE FUSELAGE SKIN BETWEEN STA 237 TO 256 AND L-15 -16R, COMPLIED WITH ER/A 624583-14. (1829579) (AIRCRAFT GROUNDED).
- [SDR DALA2026090404999](https://openairdocs.org/sdr/DALA2026090404999.md): Unknown · odor · Sep 4, 2026 · N998AT · Boeing 717200 · Air Distribution System
  > CREW 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 GEN
- [SDR DALA2026080604551](https://openairdocs.org/sdr/DALA2026080604551.md): Electrical Sys · faulted · Aug 5, 2026 · N998AT · Boeing 717200 · Electrical Power System
  > ATO- 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 F
- [SDR DALA2026060903442](https://openairdocs.org/sdr/DALA2026060903442.md): Unknown · noise · May 30, 2026 · N998AT · Boeing 717200 · Standard Practices/Structures
  > DIV- 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
- [SDR DALA2026042902734](https://openairdocs.org/sdr/DALA2026042902734.md): Ecu · failed · Apr 26, 2026 · N998AT · Boeing 717200 · APU Start/Ignition System
  > APU 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)
- [SDR DALA2026021801126](https://openairdocs.org/sdr/DALA2026021801126.md): Valve · odor · Feb 10, 2026 · N998AT · Boeing 717200 · Air Distribution System
  > DIRTY SOCK ODOR. REPLACED 35 DEGREE VALVE & MUFFLER IAW AMM 21-54. (8499820).
- [SDR DALA2026020900917](https://openairdocs.org/sdr/DALA2026020900917.md): Unknown · odor · Feb 1, 2026 · N998AT · Boeing 717200 · Air Distribution System
  > DIRTY 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 AN
- [SDR DALA2026010500070](https://openairdocs.org/sdr/DALA2026010500070.md): Engine · fire · Jan 2, 2026 · N998AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > REJECTED 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)
- [SDR DALA2025101707598](https://openairdocs.org/sdr/DALA2025101707598.md): Idg · faulted · Oct 14, 2025 · N998AT · Boeing 717200 · AC Generator-Alternator
  > SHIP 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)
- [SDR DALA2025101707599](https://openairdocs.org/sdr/DALA2025101707599.md): Oil System · leaking · Oct 12, 2025 · N998AT · Boeing 717200 · APU Oil System
  > SHIP 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. OPE
- [SDR DALA2025051503782](https://openairdocs.org/sdr/DALA2025051503782.md): Power Supply · inoperative · May 15, 2025 · N998AT · Boeing 717200 · Emergency Lighting
  > FOUND 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)
- [SDR DALA2025042103073](https://openairdocs.org/sdr/DALA2025042103073.md): Pan · cracked · Apr 18, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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)
- [SDR DALA2025042103072](https://openairdocs.org/sdr/DALA2025042103072.md): Skin · damaged · Apr 18, 2025 · N998AT · Boeing 717200 · Passenger/Crew Doors
  > WORN 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 FABRIC
- [SDR DALA2025041602960](https://openairdocs.org/sdr/DALA2025041602960.md): Pan · cracked · Apr 16, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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
- [SDR DALA2025041202833](https://openairdocs.org/sdr/DALA2025041202833.md): Cargo Track · corroded · Apr 12, 2025 · N998AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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.
- [SDR DALA2025040902760](https://openairdocs.org/sdr/DALA2025040902760.md): Repair · misinstalled · Apr 9, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FASTENER 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 DISC
- [SDR DALA2025040902758](https://openairdocs.org/sdr/DALA2025040902758.md): Longeron · corroded · Apr 8, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 #
- [SDR DALA2025040802699](https://openairdocs.org/sdr/DALA2025040802699.md): Vane · dented · Apr 4, 2025 · N998AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS 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 #08
- [SDR DALA2025040802697](https://openairdocs.org/sdr/DALA2025040802697.md): Support · cracked · Apr 4, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED 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)
- [SDR DALA2025040302494](https://openairdocs.org/sdr/DALA2025040302494.md): Retainer · cracked · Apr 2, 2025 · N998AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK 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)
- [SDR DALA2025033102354](https://openairdocs.org/sdr/DALA2025033102354.md): Repair · cracked · Mar 29, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED 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 5
- [SDR DALA2025033102351](https://openairdocs.org/sdr/DALA2025033102351.md): Pan · cracked · Mar 28, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED 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. ASSOCIATE
- [SDR DALA2025033102348](https://openairdocs.org/sdr/DALA2025033102348.md): Skin · dented · Mar 27, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > PERFORM 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 SECT
- [SDR DALA2025033102346](https://openairdocs.org/sdr/DALA2025033102346.md): Longeron · cracked · Mar 26, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK 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 #087885
- [SDR DALA2025032502209](https://openairdocs.org/sdr/DALA2025032502209.md): Longeron · corroded · Mar 24, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION 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
- [SDR DALA2025032402190](https://openairdocs.org/sdr/DALA2025032402190.md): Support · corroded · Mar 23, 2025 · N998AT · Boeing 717200 · Rudder Structure
  > CORROSION 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 E
- [SDR DALA2025032402184](https://openairdocs.org/sdr/DALA2025032402184.md): Access Panel · corroded · Mar 21, 2025 · N998AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION 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 2
- [SDR DALA2025032402183](https://openairdocs.org/sdr/DALA2025032402183.md): Access Panel · corroded · Mar 21, 2025 · N998AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION 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 ACCE
- [SDR DALA2025032102133](https://openairdocs.org/sdr/DALA2025032102133.md): Barrel Nut · corroded · Mar 20, 2025 · N998AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION 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 LIMIT
- [SDR DALA2025031902066](https://openairdocs.org/sdr/DALA2025031902066.md): Floor Support · corroded · Mar 19, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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 ALLOWABLE
- [SDR DALA2025031902062](https://openairdocs.org/sdr/DALA2025031902062.md): Pan · cracked · Mar 18, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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)
- [SDR DALA2025031401970](https://openairdocs.org/sdr/DALA2025031401970.md): Cusp Web · cracked · Mar 14, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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)
- [SDR DALA2025031201904](https://openairdocs.org/sdr/DALA2025031201904.md): Frame · cracked · Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK 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)
- [SDR DALA2025031201902](https://openairdocs.org/sdr/DALA2025031201902.md): Skin · dented · Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENT 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 2
- [SDR DALA2025031201901](https://openairdocs.org/sdr/DALA2025031201901.md): Skin · dented · Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENT 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 2
- [SDR DALA2025031101891](https://openairdocs.org/sdr/DALA2025031101891.md): Pan · cracked · Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS 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-
- [SDR DALA2025031101889](https://openairdocs.org/sdr/DALA2025031101889.md): Frame · cracked · Mar 11, 2025 · N998AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK 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)
- [SDR DALA2025031101892](https://openairdocs.org/sdr/DALA2025031101892.md): Skin · corroded · Mar 10, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > -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 SECTI
- [SDR DALA2025031101887](https://openairdocs.org/sdr/DALA2025031101887.md): Longeron · cracked · Mar 10, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKS 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)
- [SDR DALA2025031001821](https://openairdocs.org/sdr/DALA2025031001821.md): Longeron · cracked · Mar 8, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK 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)
- [SDR DALA2025031001820](https://openairdocs.org/sdr/DALA2025031001820.md): Cusp Web · corroded · Mar 8, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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 00
- [SDR DALA2025030601745](https://openairdocs.org/sdr/DALA2025030601745.md): Cusp Web · corroded · Mar 6, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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
- [SDR DALA2025030501714](https://openairdocs.org/sdr/DALA2025030501714.md): Cusp Web · corroded · Mar 5, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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 008
- [SDR DALA2025030501713](https://openairdocs.org/sdr/DALA2025030501713.md): Cusp Web · corroded · Mar 5, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION 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 00830
- [SDR DALA2025030501712](https://openairdocs.org/sdr/DALA2025030501712.md): Cusp Web · cracked · Mar 5, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK 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)
- [SDR DALA2025021801195](https://openairdocs.org/sdr/DALA2025021801195.md): Skin · dented · Feb 16, 2025 · N998AT · Boeing 717200 · Cargo/Baggage Doors
  > PERFORM 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 FIGUR
- [SDR DALA2025030601774](https://openairdocs.org/sdr/DALA2025030601774.md): Access Door · missing · Dec 3, 2024 · N998AT · Boeing 717200 · Elevator, Plate/Skin
  > -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 #
- [SDR DALA2024071607170](https://openairdocs.org/sdr/DALA2024071607170.md): Stringer Splice · damaged · Jul 14, 2024 · N998AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > STR 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: COM
- [SDR DALA2024071607169](https://openairdocs.org/sdr/DALA2024071607169.md): Skin · dented · Jul 14, 2024 · N998AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > C/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", "

Next page: https://openairdocs.org/aircraft/N998AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N998AT/reports

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