# Service difficulty reports: N988AT

A list on [N988AT](https://openairdocs.org/aircraft/N988AT.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 4 · 177 reports

- [SDR DALA2026092405330](https://openairdocs.org/sdr/DALA2026092405330.md): Oxygen Mask · no test · Sep 23, 2026 · N988AT · Boeing 717200 · Crew Oxygen System
  > CAPTAIN`S OXYGEN MASK DOES NOT TEST PROPERLY, R & R OBSERVER SEAT CREW O2 MASK BOX IAW AMM 35-13-09. (9110692) (AIRCRAFT GROUNDED).
- [SDR DALA2026061003517](https://openairdocs.org/sdr/DALA2026061003517.md): Skin · cracked · Jun 9, 2026 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BTW STA Y=1037 & LONG 14R AT AFT FUSELAGE AREA. FUSELAGE SKIN BTW STA Y=1037 & LONG 14R AT AFT FUSELAGE AREA WAS REPAIRED PER PRI 634847-14 REV. 2 AND ER/A 634847-14 REV. ORIGINAL SECTION 1. (LP 1638764 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060903483](https://openairdocs.org/sdr/DALA2026060903483.md): Skin · cracked · Jun 9, 2026 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN STA 1087 RT LONG 14R. EXTERNAL FUSELAGE SKIN STA 1087 RT LONG 14R WAS REPAIRED PER PRI 634855-14 REV. 1 AND ER/A 634855-14 REV. ORIGINAL. (LP 1637170 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060903480](https://openairdocs.org/sdr/DALA2026060903480.md): Skin · cracked · Jun 7, 2026 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9521, CRACK ON EXTERNAL FUSELAGE SKIN STA 1076 RH BTW LONG 14RH. EXTERNAL FUSELAGE SKIN STA 1076 RH BTW LONG 14RH WAS REPAIRED PER PRI 634869-14 REV 0 AND ERA 634869-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP 1634693 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026061103542](https://openairdocs.org/sdr/DALA2026061103542.md): Vane · dented · Jun 6, 2026 · N988AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS ON UPPER SURFACE OF AFT MOVABLE VANE AT RH WING. UPPER SURFACE OF AFT MOVABLE VANE AT RH WING WERE REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL, B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND ADJUSTMENT UNDER AMDS 2750-4008. (LP 1632855 -
- [SDR DALA2026060903435](https://openairdocs.org/sdr/DALA2026060903435.md): Door Frame · corroded · Jun 1, 2026 · N988AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON ANGLE DOOR JAM BTW BS 370 TO 389 APROX AT FWD CARGO COMPARMENT. REPAIRED IAW SRM 51-40-02 (1625046) (AIRCRAFT GROUNDED).
- [SDR DALA2026051703033](https://openairdocs.org/sdr/DALA2026051703033.md): Battery Pack · faulted · May 13, 2026 · N988AT · Boeing 717200 · Emergency Lighting
  > SHIP 9521 EMERGENCY LIGHTS FORWARD OF NACELLES ARE ILLUMINATED WHEN SHIPS POWER IS COMPLETELY POWERED DOWN. REPLACED BATTERY PACK INSIDE B5-125. ALL OPS NORMAL. (8664178) (AIRCRAFT GROUNDED)
- [SDR DALA2026042302607](https://openairdocs.org/sdr/DALA2026042302607.md): Relay · faulted · Apr 22, 2026 · N988AT · Boeing 717200 · Emergency Lighting
  > WHEN SECURING AC FOR THE NIGHT, WHEN TURNING COCKPIT EMERGENCY SWITCH TO "OFF" OUTSIDE WING EMERGENCY LIGHTS STAY "ON". REMOVED AND REPLACED RELAY R2-273 IAW B717 AMM 33-51. (8664106) (AIRCRAFT GROUNDED)
- [SDR DALA2026011600379](https://openairdocs.org/sdr/DALA2026011600379.md): Transceiver · faulted · Jan 9, 2026 · N988AT · Boeing 717200 · Weather Radar System
  > ATB- PERFORMED AN AIR TURN BACK DUE TO A WEATHER RADAR. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER AND PERFORMED OPERATIONAL TEST. AIRCRAFT RETURNED TO SERVICE.(7949802)
- [SDR DALA2024112511166](https://openairdocs.org/sdr/DALA2024112511166.md): Bolt · sheared · Nov 22, 2024 · N988AT · Boeing 717200 · Landing Gear Actuator
  > SHIP 9521 -ATB/GEAR/DE- THE FLIGHT CREW PERFORMED AN AIR TURN BACK TO CLT DUE TO A "RIGHT MAIN LANDING GEAR UNSAFE" MESSAGE WITH AN ASSOCIATED "RIGHT GEAR DOOR OPEN" MESSAGE. THE ALTERNATE GEAR EXTENSION LEVER WAS PULLED. AN EMERGENCY WAS DECLARED WITH ATC. CO
- [SDR DALA2024052205412](https://openairdocs.org/sdr/DALA2024052205412.md): Fuel Tank · corroded · May 20, 2024 · N988AT · Boeing 717200 · Fuel Storage
  > -AD- CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-32 AT LH MLG WHEEL WELL (AREA UNDER MLG CABLE FITTING). SUMMARY OF NRC 00775: CORROSION LEVEL 1. CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-
- [SDR DALA2024050104835](https://openairdocs.org/sdr/DALA2024050104835.md): Skin · corroded · Apr 30, 2024 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON SETTLEMENT AREA OF RUB STRIP FUSELAGE SKIN BTW STA Y=870 RH TO 896.5 RH AND LONGERON 27RH FUSELAGE. SUMMARY OF NRC 00737: CORROSION LEVEL 2. FUSELAGE SKIN BTW STA Y=870RH TO 896.5RH AND LONGERON 27RH WAS REPAIRED PER B717 SRM 53-20-70-2R PROCEDURE
- [SDR DALA2024042604729](https://openairdocs.org/sdr/DALA2024042604729.md): Frame · corroded · Apr 26, 2024 · N988AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION AT FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT. SUMMARY OF NRC 00298: CORROSION LEVEL 2. FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3. PERFORM VISUAL INSPECTION INITIAL 25,
- [SDR DALA2024042504693](https://openairdocs.org/sdr/DALA2024042504693.md): Floor Support · corroded · Apr 24, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00626: CORROSION LEVEL 2. FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE WERE FABRICATED PER B717 DWG 99
- [SDR DALA2024042504692](https://openairdocs.org/sdr/DALA2024042504692.md): Window Frame · cracked · Apr 24, 2024 · N988AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION E
- [SDR DALA2024042504691](https://openairdocs.org/sdr/DALA2024042504691.md): Window Frame · cracked · Apr 24, 2024 · N988AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION E
- [SDR DALA2024042404674](https://openairdocs.org/sdr/DALA2024042404674.md): Cusp Web · corroded · Apr 24, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00525: CORROSION LEVEL 2. RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-
- [SDR DALA2024042304668](https://openairdocs.org/sdr/DALA2024042304668.md): Longeron · cracked · Apr 22, 2024 · N988AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 2LH FROM STA 1133 OF AFTER ACCESSORIES. SUMMARY OF NRC 00389: LONGERON 2LH STA 1121 TO STA 1136 WAS REPAIRED PER B717-200 SRM 53-00-05-2R-2 REPAIR 2. (LP #0307355)
- [SDR DALA2024042304667](https://openairdocs.org/sdr/DALA2024042304667.md): Cusp Web · cracked · Apr 22, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-PROCEDURE 4. REPAIR 4. (LP #0306797)
- [SDR DALA2024042304664](https://openairdocs.org/sdr/DALA2024042304664.md): Frame · cracked · Apr 22, 2024 · N988AT · Boeing 717200 · Fuselage Main, Frame
  > -A.D.- CRACK OF 0.250IN LENGTH WAS FOUND ON UPPER RADIUS OF THE FRAME TAB ON THE LH OVERWING FRAME STA Y=696, IN REF CARD 5310-01436-04B JOB #063-0002 STEP: 10. SUMMARY OF NRC 00522: FRAME TAB ON THE LH OVERWING FRAME STA Y=696 WAS REPLACED PER B717-200 SRM 51
- [SDR DALA2024042204625](https://openairdocs.org/sdr/DALA2024042204625.md): Pan · cracked · Apr 21, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160. SUMMARY OF NRC 00191: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDER 3 REPAIR 3. (LP #0305244)
- [SDR DALA2024042204624](https://openairdocs.org/sdr/DALA2024042204624.md): Pan · cracked · Apr 21, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200. SUMMARY OF NRC 00193: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0305238)
- [SDR DALA2024042204622](https://openairdocs.org/sdr/DALA2024042204622.md): Beam · cracked · Apr 19, 2024 · N988AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM #1 OF L1 DOOR STA Y=200. SUMMARY OF NRC 00194: BEAM #1 OF L1 DOOR STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0302430)
- [SDR DALA2024041904570](https://openairdocs.org/sdr/DALA2024041904570.md): Cusp Web · corroded · Apr 19, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP WEB, OUT OF LIMITS PER B717 SRM 53-00-55-1A-1 ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00701: CORROSION LEVEL 2. RING DOUBLER ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS FABRICATED AND REPLACE
- [SDR DALA2024041904569](https://openairdocs.org/sdr/DALA2024041904569.md): Cusp Web · cracked · Apr 18, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK (3 EA) ON LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX. SUMMARY OF NRC 00717: LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 205. (LP #0300923)
- [SDR DALA2024041904568](https://openairdocs.org/sdr/DALA2024041904568.md): Door Frame · corroded · Apr 18, 2024 · N988AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00700: CORROSION LEVEL 2. DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-
- [SDR DALA2024041904565](https://openairdocs.org/sdr/DALA2024041904565.md): Door Frame · corroded · Apr 18, 2024 · N988AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00070: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0300206)
- [SDR DALA2024041804534](https://openairdocs.org/sdr/DALA2024041804534.md): Pan · cracked · Apr 17, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00320: PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0298813)
- [SDR DALA2024041504427](https://openairdocs.org/sdr/DALA2024041504427.md): Cusp Web · cracked · Apr 13, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00526: RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 1. (LP #0292417)
- [SDR DALA2024041504425](https://openairdocs.org/sdr/DALA2024041504425.md): Web · cracked · Apr 12, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00580: WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0290917)
- [SDR DALA2024041504422](https://openairdocs.org/sdr/DALA2024041504422.md): Angle · corroded · Apr 12, 2024 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00072: CORROSION LEVEL 2. FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 FIG 201. (L
- [SDR DALA2024041204362](https://openairdocs.org/sdr/DALA2024041204362.md): Cusp Web · corroded · Apr 12, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00596: LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP
- [SDR DALA2023112809763](https://openairdocs.org/sdr/DALA2023112809763.md): Unknown · unknown · Nov 26, 2023 · N988AT · Boeing 717200 · Passenger/Crew Doors
  > AT L1 DOOR CLOSURE PRIOR TO PUSH-BACK, GATE AGENT NOTICED DAMAGE TO BOTTOM FWD EDGE OF L1 DOOR. DAMAGE IS APROX 5" LONG. EDGE ROLLED BACK APROX 3/8". REMOVED DAMAGE PER SRM 52-10-01-2R-1. PERFORMED HFFC PER B717 NDT SPM PART 6-10-01.001. NO CRACKS FOUND QC 209
- [SDR DALA2023060904692](https://openairdocs.org/sdr/DALA2023060904692.md): Unknown · unknown · Jun 7, 2023 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > RAMP REPORTED DAMAGE TO AFT CARGO DOOR CUTOUT. FOUND DAMAGE TO PREVIOUS REPAIR SPLICE ONLY. REMOVED SPLICE TO PREPARE FOR REPLACEMENT. NO OPEN HOLE REQUIRED. INSTALLED REPAIR PER B717 SRM 53-20-15-2R PROC 4 PERMENANT REPAIR. (LP #4798350)
- [SDR DALA2023050303434](https://openairdocs.org/sdr/DALA2023050303434.md): Unknown · unknown · May 2, 2023 · N988AT · Boeing 717200 · Landing Gear Actuator
  > SHIP 9521 -ATB/GEAR- THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT TO DTW FOLLOWING THE FAILURE OF THE NOSE LANDING GEAR TO RETRACT. CORRECTIVE ACTION: MAINTENANCE ADJUSTED NOSE LANDING GEAR RETRACT ACTUATOR. (LP #4110406)
- [SDR DALA2023042703290](https://openairdocs.org/sdr/DALA2023042703290.md): Unknown · unknown · Apr 27, 2023 · N988AT · Boeing 717200 · Emergency Lighting
  > FOUND TWO FORWARD UPPER RIGHT OVERWING CABIN EXIT LIGHTS AND ONE CEILING AISLE LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED TWO EMERGENCY LIGHT POWER SUPPLY BATTERIES PER B717 AMM 33-51-03 PAGEBLOCK 401. OPERATIONAL CHECK WAS GOOD. (LP #9428982)
- [SDR DALA2023022201325](https://openairdocs.org/sdr/DALA2023022201325.md): None · none · Feb 14, 2023 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > "FAA APPROVAL PENDING" FOR ERA 605849-14 REV ORIG. FUSELAGE SKIN / STA 1002-1022 / L-24-L-26 / GROUND DAMAGE SECTION I PERMANENT REPAIR INSTRUCTIONS. SUMMARY SEE NRC 003-0001:0514-2001/005 00005: COMPLIED WITH ER/A PRI 605849-14 REV A PRI REV 0 REPAIR INSTRUCT
- [SDR DALA2023021501178](https://openairdocs.org/sdr/DALA2023021501178.md): None · none · Feb 12, 2023 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > COMPLY WITH FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L-26 PER ER/A 605849-14 REV ORIG. C/W ER/A 605849-14 REV ORIG. PERMANENT REPAIR AND ER/A 605849-14 REV A. RII C/W. ASSOCIATED ER/A 14-605849 ADDED FOR AC 9521. (LP #4025639)
- [SDR DALA2023021401137](https://openairdocs.org/sdr/DALA2023021401137.md): Unknown · unknown · Feb 12, 2023 · N988AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > C/W ERA 605849-14 REV ORIG, FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L26. SUMMARY NRC 003-0001:0514-2001/001 00001: COMPLIED WITH ER/A PRI 605849-14 REV "0","1","2","3". ALL REPAIR INSTRUCTION STEPS, ENSURE FINALE ER/A 605849-14 REV. ORIG. S
- [SDR DALA2023021401135](https://openairdocs.org/sdr/DALA2023021401135.md): Unknown · unknown · Feb 11, 2023 · N988AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > LONGERON 24R CORRODED FROM STA 1000-1035. SUMMARY NRC 003-0001:0514-2001/002 00002: REPLACED LONGERON REF DAC DWG 5911424. (LP #2625262)
- [SDR DALA2023011200229](https://openairdocs.org/sdr/DALA2023011200229.md): Lens · missing · Jan 11, 2023 · N988AT · Boeing 717200 · Emergency Lighting
  > THE 1R DOOR EXIT SIGN LENSE WAS MISSING ON PREFLIGHT. MAINTENANCE INSTALLED THE 1R DOOR EXIT SIGN LENSE REF B717 IPC 33-51. (LP #9884344)
- [SDR DALA2023010500070](https://openairdocs.org/sdr/DALA2023010500070.md): Fire Warning · false activation · Jan 4, 2023 · N988AT · Boeing 717200 · Fire Detection
  > SHIP 9521 -DIV/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO BNA FOLLOWING A "FIRE" WARNING INDICATION ON THE #2 ENGINE WITH ANTI-ICE ON. THE QRH WAS COMPLIED WITH, AN EMERGENCY WAS DECLARED WITH ATC, AND THE SUBSEQUENT OVERWEIGHT LANDING WAS UNEVENTFUL. CFR DI
- [SDR DALA2022120207723](https://openairdocs.org/sdr/DALA2022120207723.md): Transmitter · faulted · Dec 1, 2022 · N988AT · Boeing 717200 · Trailing Flap Position Indicating System
  > DECLARED EMERGENCY DUE TO AN INTERMITTENT FLAP DISAGREE INDICATION. STARTING AT 12000 FT, PFD SPORADICALLY SHOWED FLAPS 0 & PICTURE OF UNDERWING ON CONFIG PAGE. CREW REPORTED NO ADVERSE FEEL. CONTINUED THROUGH 25000 FT UNTIL THE FLAPS DISAG ON EICAS WITH S
- [SDR DALA2022111707400](https://openairdocs.org/sdr/DALA2022111707400.md): Cable · frayed · Nov 15, 2022 · N988AT · Boeing 717200 · Aerodynamic Fairings
  > THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS FRAYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52-01 AND
- [SDR DALA2022091206031](https://openairdocs.org/sdr/DALA2022091206031.md): None · none · Sep 9, 2022 · N988AT · Boeing 717200 · Windshield/Door Rain/Ice Removal
  > CAPTAIN WINDSHIELD ARCING ON DESCENT. MCC FCP DEFERRED. FLIGHT CREW PLACARD VALIDATION IS ACCOMPLISHED AT CHA PER MEL 30-41-01B. REPLACED CAPTAIN WINDSHIELD PER B717 AMM 56-11. MEL AND PLACARD REMOVED. (LP #2402013)
- [SDR DALA2022090405924](https://openairdocs.org/sdr/DALA2022090405924.md): None · none · Sep 3, 2022 · N988AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9521, DURING SVC CHK FOUND BATTERY 7 (685R) FOR EMERGENCY LIGHTS DRAINED. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY ASSEMBLY AT LOCATION 7 (685R). (LP9115548)
- [SDR DALA2022040802422](https://openairdocs.org/sdr/DALA2022040802422.md): Tailpipe · plugged · Apr 6, 2022 · N988AT · Boeing 717200 · Turbine Engine Compressor Section
  > SHIP 9521 - THE FLIGHT CREW RETURNED THE AIRCRAFT BACK TO ATL AND LANDED WITHOUT FURTHER INCIDENT AFTER THE #2 ENGINE EXPERIENCED A COMPRESSOR STALL DURING CLIMB OUT. AT FL230, A LOUD REPORT WAS HEARD, FOLLOWED BY STRONG VIBRATIONS (9.9 UNITS) FROM THE ENGINE,
- [SDR DALA2022040602328](https://openairdocs.org/sdr/DALA2022040602328.md): Lanyard · out of position · Mar 30, 2022 · N988AT · Boeing 717200 · Escape Slide
  > GIRT BAR LANYARD WAS FOUND TO BE NOT ATTACHED TO PASSENGER DOOR. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THE LANYARD WAS NOT LOOPED AROUND THE GIRT BAR. PLACED THE GIRT BAR
- [SDR DALA2021120907587](https://openairdocs.org/sdr/DALA2021120907587.md): None · none · Dec 8, 2021 · N988AT · Boeing 717200 · Engine Thrust Reverser
  > SHIP 9521 - THE CREW DECLARED AN EMERGENCY DURING THE APPROACH FOR LANDING IN ATL DUE TO THE LOSS OF LEFT HYDRAULIC SYSTEM FLUID QUANTITY. CORRECTIVE ACTION: MAINTENANCE FOUND THE SOURCE OF THE LEAK AND REPLACED THE DAMAGED SECTION OF A HYDRAULIC LINE NEAR THE
- [SDR DALA2021102806675](https://openairdocs.org/sdr/DALA2021102806675.md): None · none · Oct 27, 2021 · N988AT · Boeing 717200 · Escape Slide
  > R1 DOOR SLIDE PINS PULLED OUT WHEN DOOR WAS OPENED FROM THE OUTSIDE. THE SLIDE DID NOT DEPLOY AS DESIGNED. THIS IS A FAILURE OF PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE R-1 DOOR SLIDE BOTTLE PIN WAS INSTALLE

Next page: https://openairdocs.org/aircraft/N988AT/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 = 'N988AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N988AT/reports

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