# Service difficulty reports: N930AT

A list on [N930AT](https://openairdocs.org/aircraft/N930AT.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 · 188 reports

- [SDR DALA2026062903840](https://openairdocs.org/sdr/DALA2026062903840.md): Door Frame · cracked · Jun 28, 2026 · N930AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION AND CRACK ON FWD CARGO DOOR JAMB LOWER SECTION AT FWD CARGO COMPARTMENT. FWD CARGO DOOR JAMB LOWER SECTION AND SPLICE ANGLES (4EAS) AT FWD CARGO DOOR JAMB LOWER SECTION WERE REPLACED PER B717-200 SRM 53-20-15-2R. (1670437) (AIRCRAFT GROUNDED).
- [SDR DALA2026062503778](https://openairdocs.org/sdr/DALA2026062503778.md): Lanyard · frayed · Jun 24, 2026 · N930AT · Boeing 717200 · Emergency Equipment
  > FRAYED LANYARD OF SLIDE DOOR LT. REPLACED IAW AIPC 25-61-01-01. (1663123) (AIRCRAFT GROUNDED)
- [SDR DALA2026051903065](https://openairdocs.org/sdr/DALA2026051903065.md): Not Reported · not reported · May 17, 2026 · N930AT · Boeing 717200 · Standard Practices/Structures
  > AD 2024-21-01 ER/A 634524-14AD. ASSOCIATED ER/A 14-634524 (1598852) (AIRCRAFT GROUNDED)
- [SDR DALA2026040102132](https://openairdocs.org/sdr/DALA2026040102132.md): Windshield · arced · Mar 31, 2026 · N930AT · Boeing 717200 · Flight Compartment Windows
  > CENTER WINDSHIELD ANTIICE FAIL DUE TO ARCING HEATER CRACK IN WINDSHIELD. REPLACED CENTER WINDSHIELD PER B717 AMM 56-11-01 LEAK CK OK A/C OK FOR SERVICE (8424138)
- [SDR DALA2025122309343](https://openairdocs.org/sdr/DALA2025122309343.md): Slide · dislodged · Dec 17, 2025 · N930AT · Boeing 717200 · Escape Slide
  > OPS REPORTS R1 DOOR SLIDE DISLODGED. DOOR SLIDE IAW AMM 25-61. ACFT OK FOR SERVICE. (8406508)
- [SDR DALA2025111208301](https://openairdocs.org/sdr/DALA2025111208301.md): Cable · out of adjust · Nov 11, 2025 · N930AT · Boeing 717200 · Landing Gear Position and Warning
  > ATB- RETURNED TO ATL DUE TO AIR/GROUND FAULTS. ADJUSTED GROUND SHIFT CABLE. OPS NORMAL.(7834142)
- [SDR DALA2025061104461](https://openairdocs.org/sdr/DALA2025061104461.md): Power Supply · inoperative · Jun 10, 2025 · N930AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9567, ON SVC CK FOUND AFT L/R OVER WING DOOR EMERGENCY BOTTOM LIGHT INOP. CORRECTIVE ACTION: REPLACED EMERGENGY BATT POWER SUPPLY IAW B717 AMM 33-51-03 OPS CK GOOD. (LP 6812167)
- [SDR DALA2025021201091](https://openairdocs.org/sdr/DALA2025021201091.md): Light · unknown · Feb 11, 2025 · N930AT · Boeing 717200 · Emergency Lighting
  > THE F/A REPORTED THAT THE EXIT ROW EMERGENCY LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE PERFORMED A TEST OF THE EMERGENCY LIGHT SYSTEM AND NO FAULTS WERE FOUND. ALSO, THERE IS NOT ANY HISTORY OF EMERGENCY LIGHTS MALFUNCTIONING IN THE LAST 30 DAYS. ALL CHECKS ARE
- [SDR DALA2025010300046](https://openairdocs.org/sdr/DALA2025010300046.md): Power Supply · faulted · Jan 2, 2025 · N930AT · Boeing 717200 · Emergency Lighting
  > FOUND ROW 21 EMERGENCY EXIT LIGHT B5-230/P9 TO BE INOPERATIVE. MAINTENANCE TRIED A NEW EMERGENCY LIGHT BATTERY. NO HELP, REINSTALLED ORIGINAL. REPLACED POWER SUPPLY B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6733147)
- [SDR DALA2024090408735](https://openairdocs.org/sdr/DALA2024090408735.md): Light · intermittent · Sep 4, 2024 · N930AT · Boeing 717200 · Emergency Lighting
  > WITH THE COCKPIT EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THE CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTANTLY DURING FLIGHT. MAINTENANCE TROUBLESHOT PER B717 FIM 33-50-00 810-801 AND FAULT WAS INTERMITANT. NO 60 DAY HISTORY. AIRCRAFT OK FOR SERVICE. (LP #5
- [SDR DALA2024071507164](https://openairdocs.org/sdr/DALA2024071507164.md): Angle · corroded · Jul 15, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP ANGLE INSIDE FWD SERVICE DOOR JAMB (R1) BTW STA Y=200 AND STA X=-55 AT PASSENGER CABIN. SUMMARY OF NRC 541: CORROSION LEVEL 2. CUSP ANGLE INSIDE FWD SERVICE DOOR JAMB (R1) BTW STA Y=200 AND STA X=-55 WAS REPAIRED PER PRI 618606-14 REV 5 AND E
- [SDR DALA2024071507161](https://openairdocs.org/sdr/DALA2024071507161.md): Pan · cracked · Jul 14, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS (3 EA) WERE FOUND ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR. SUMMARY OF NRC 00573: CRACKS (3 EA) ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR WERE REPAIRED PER ER/A 618437-14 REV ORIGINAL. ASSOCIATED ER/A 14-618437 ADDED FOR AC 9567. (LP #0446314)
- [SDR DALA2024071507156](https://openairdocs.org/sdr/DALA2024071507156.md): Skin · cracked · Jul 12, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK ON OPEN POSITION. ALSO FWD PREVIOUSLY REWORK DOES NOT MEET WITH RADII. SUMMARY OF NRC 175: EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK WAS REPAIRED PER PRI 618669-
- [SDR DALA2024070206725](https://openairdocs.org/sdr/DALA2024070206725.md): Skin · cracked · Jul 1, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9567, DURING HCK AT QRO, WHILE PERFORMING THE AFT FUSELAGE AND EMPENNAGE INSPECTION PER WC 5300-2019, A CRACK WAS FOUND AFFECTING THE FUSELAGE SKIN AT Y=1087 AND L-14R. AN EXISTING SKIN SPLICE REPAIR IS ADJACENT TO THE DAMAGE REPORTED. CORRECTIVE ACTI
- [SDR DALA2024062906603](https://openairdocs.org/sdr/DALA2024062906603.md): Seat Track · corroded · Jun 28, 2024 · N930AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9567, CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX WAS REPAIRED PER B717 SRM 53-20-52-2R
- [SDR DALA2024062906599](https://openairdocs.org/sdr/DALA2024062906599.md): Seat Track · corroded · Jun 27, 2024 · N930AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9567, CORROSION ON CENTER SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2. SECTION CENTER SEAT TRACK BTW STA= 200 TO STA= 256 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 53-20-52-2R
- [SDR DALA2024062906598](https://openairdocs.org/sdr/DALA2024062906598.md): Longeron · cracked · Jun 27, 2024 · N930AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 9567, INITIAL INSPECTION: CRACK ON LONGERON END L2R AND STA 1133 ALSO BRACKET SUPPORT LOWER SECTION CANTED BULKHEAD 1103 RH SIDE AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CRACK ON LONGERON END L2R AND STA 1133 WAS REPAIRED PER B717-200 SRM 53-00-05
- [SDR DALA2024062706576](https://openairdocs.org/sdr/DALA2024062706576.md): Angle · cracked · Jun 27, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9567, CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE. W1. CORRECTIVE ACTION: CORROSION LEVEL 2. CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE WAS
- [SDR DALA2024062706577](https://openairdocs.org/sdr/DALA2024062706577.md): Skin · damaged · Jun 25, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9567, FUSELAGE/SKIN/L1 DOOR GUST LATCH/CUTOUT/EDGE DAMAGE REPAIR. CORRECTIVE ACTION: ACCOMPLISH ER/A 618643-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. (LP 0413016)
- [SDR DALA2024062706572](https://openairdocs.org/sdr/DALA2024062706572.md): Skin · cracked · Jun 25, 2024 · N930AT · Boeing 717200 · Passenger/Crew Doors
  > AIRCRAFT 9567, CRACK ON DOOR SKIN ADJACENT TO EXTERNAL DOOR HANDLE HOUSING AT LEFT PASSENGER ENTRANCE DOOR. SUMMARY OF NRC SERIAL 00370: DUE TO SEVERAL DAMAGE ON FWD PASSENGER DOOR (L1) WILL BE REPLACED WITH SERVICEABLE DOOR; PER TRACKING PURPOSE ONLY; FWD PAS
- [SDR DALA2024062506488](https://openairdocs.org/sdr/DALA2024062506488.md): Longeron · corroded · Jun 24, 2024 · N930AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION OUT OF LIMIT ON LONGERON END STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT. C2. SUMMARYOF NRC 00857: CORROSION LEVEL 2. LONGERON END ON STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT C2 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8. (LP #0411089)
- [SDR DALA2024062406343](https://openairdocs.org/sdr/DALA2024062406343.md): Cusp Web · cracked · Jun 22, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS WERE FOUND ON MEMBRANE OF PASSENGER CABIN AT CUSP WEB BTW STA 218/237 AND BTW STA X=-56/-22. SUMMARY OF NRC 00678: CUSP WEB BTW STA 218/237 AND BTW STA X=-56 /-22 WAS REPAIRED PER B717 53-00-55-2R-4 CONFIGURATION 7015 FIG 210 PAR 40 AND 51-41-02-0G. (LP
- [SDR DALA2024062406339](https://openairdocs.org/sdr/DALA2024062406339.md): Frame · cracked · Jun 21, 2024 · N930AT · Boeing 717200 · Fuselage Main, Frame
  > A.D. CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=715.000 RH IN REFERENCE CARD 5310- 01436-01D JOB# 082-0004. (SM) SUMMARY OF NRC 00508: OVERWING FRAME AT STA Y=715 WAS REPLACED PER CARD 5310-01436-03B AND B717-200 SRM 51-41-
- [SDR DALA2024062106294](https://openairdocs.org/sdr/DALA2024062106294.md): Intercostal · cracked · Jun 20, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL WAS FOUND ON STA Y=636 X=0 AT PAX CABIN. SUMMARY OF NRC 00838: CRACK ON INTERCOSTAL ON STA Y=636 X=0 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #0403676)
- [SDR DALA2024062006268](https://openairdocs.org/sdr/DALA2024062006268.md): Beam · cracked · Jun 19, 2024 · N930AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00685: INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER B717-200 SRM 52-30- 02-2R PROCEDURE 1 REPAIR 1. (LP #0402498)
- [SDR DALA2024061806170](https://openairdocs.org/sdr/DALA2024061806170.md): Skin · cracked · Jun 17, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R. SUMMARY OF NRC 00226: CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R WAS REPAIRED PER B717-200 SRM 53-20-15- 2R PROCEDURE 12. PERFORM AN EXTERNAL GVI EVERY 8000 CYCLES TO T
- [SDR DALA2024061606112](https://openairdocs.org/sdr/DALA2024061606112.md): Floor Support · corroded · Jun 15, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE. IN REFERENCE NRC 00604. SUMMARY OF NRC 00789: CORROSION LEVEL 2. FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE WAS FABRICATED AND INSTALLED PER DWG 9936534 REV
- [SDR DALA2024061606110](https://openairdocs.org/sdr/DALA2024061606110.md): Cusp Web · cracked · Jun 14, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00610: CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN WERE REPAIRED PER B717- 200 SRM 53-00-55-2R-4. (LP #0393751)
- [SDR DALA2024061606109](https://openairdocs.org/sdr/DALA2024061606109.md): Pan · cracked · Jun 14, 2024 · N930AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE. SUMMARY OF NRC 00686: INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0393395)
- [SDR DALA2024061606108](https://openairdocs.org/sdr/DALA2024061606108.md): Frame · damaged · Jun 13, 2024 · N930AT · Boeing 717200 · Fuselage Main, Frame
  > TOOL MARKS ON OVERWING FRAME STA737 L-18R AT WING BOX. SUMMARY OF NRC 00533: OVERWING FRAME STA737 L-18R AT WING BOX WAS REPAIRED PER PRI 618675-14 REV.0 AND ERA 618675-14 REV. ORIGINAL ASSOCIATED ER/A 14-618675 ADDED FOR AC 9567. (LP #0392376)
- [SDR DALA2024061306056](https://openairdocs.org/sdr/DALA2024061306056.md): Cusp Web · corroded · Jun 13, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00791: CORROSION LEVEL 2, LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 216. (LP #0391165)
- [SDR DALA2023081606669](https://openairdocs.org/sdr/DALA2023081606669.md): Unknown · unknown · Aug 15, 2023 · N930AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS IN ROWS 15-19 ARE INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK B5-120 TO BE INOPERATIVE AND REPLACED THE BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #4952903)
- [SDR DALA2023051803951](https://openairdocs.org/sdr/DALA2023051803951.md): Unknown · unknown · May 15, 2023 · N930AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > SHIP 9567 -HYD/DE- THE FLIGHT CREW NOTICED A LOSS OF HYDRAULIC FLUID INDICATION WITH THE LEFT SYSTEM. THE QRH WAS COMPLIED WITH AND THE LEFT ENGINE DRIVEN HYDRAULIC PUMP WAS SHUTDOWN. AN EMERGENCY WAS DECLARED DUE TO THE LOSS OF THE LEFT SYSTEM HYDRAULICS WHIL
- [SDR DALA2022112907614](https://openairdocs.org/sdr/DALA2022112907614.md): Lens · detached · Nov 27, 2022 · N930AT · Boeing 717200 · Emergency Lighting
  > THE EXIT LENS COVER AT ROW 19 IS MISSING. MAINTENANCE REPLACED THE MISSING LENS COVER AT ROW 19. (LP #2513959)
- [SDR DALA2022032802027](https://openairdocs.org/sdr/DALA2022032802027.md): Longeron · damaged · Mar 25, 2022 · N930AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > SECOND DAMAGE AFTER CORROSION REMOVAL ON L29 LH BTW STA 900 TO STA 968 REMAINING THICKNESS IS OUT OF LIMITS. IN REFERENCE NRC 184. SUMMARY OF NRC 00252: CORROSION LEVEL 2, LONGERON 29LH BTW STA 900 TO STA 968 WAS REPAIRED PER B717-200 SRM 53-20-05-2R REPAIR 1,
- [SDR DALA2022032502000](https://openairdocs.org/sdr/DALA2022032502000.md): Frame Splice · corroded · Mar 25, 2022 · N930AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON REPAIR SPLICE FRAME STA 1022 BTW LONGS 30 TO 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: (CORROSION LEVEL 2) REPAIR SPLICE FRAME STA 1022 BTW LONGS 30 TO 26 LH AT AFT CARGO COMPARTMENT WAS REPLACE PER B717 SRM 53-20-07-2R. REPAIR 3. (LP
- [SDR DALA2022032401937](https://openairdocs.org/sdr/DALA2022032401937.md): Unknown · unknown · Mar 23, 2022 · N930AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICE OF STRINGER 30 STA=960 TO 975 AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00196: CORROSION LEVEL 2, SPLICE OF STRINGER 30 STA=960 TO 975 AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-00-05-2R, REPAIR 2. (LP #2168169)
- [SDR DALA2022032201862](https://openairdocs.org/sdr/DALA2022032201862.md): Not Reported · not reported · Mar 21, 2022 · N930AT · Boeing 717200 · Trailing Edge Flaps
  > SECONDARY DAMAGE AREAS WERE FOUND AT DENTS #8 & #10 ON INNER FACE OF REAR MOVABLE VANE AT LH WING. AREAS WERE FOUND DEBONDED (IN REF NRC 00060). SUMMARY OF NRC 00238: INNER FACE OF REAR MOVABLE VANE AT LH WING WAS REPAIRED PER B717 SRM 51-70-02-0G AND IN REFER
- [SDR DALA2022032101831](https://openairdocs.org/sdr/DALA2022032101831.md): Not Reported · not reported · Mar 20, 2022 · N930AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON DOOR JAMB BTW STA 950 TO 1000 OF AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00030: CORROSION LEVEL 2, DOOR JAMB OF AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R, REP. 7. (LP #2164034)
- [SDR DALA2019082004881](https://openairdocs.org/sdr/DALA2019082004881.md): Lens · missing · Aug 19, 2019 · N930AT · Boeing 717200 · Emergency Lighting
  > THE FORWARD FACING LENS FROM THE CENTER AISLE EMERGENCY EXIT SIGN AT THE OVERWING EXIT IS MISSING. MAINTENANCE INSTALLED THE CENTER AISLE FORWARD FACING LENS AT THE OVERWING EXITS PER B717 AMM 33-51. (LP #6167025)
- [SDR DALA2019010400049](https://openairdocs.org/sdr/DALA2019010400049.md): Skin · damaged · Jan 4, 2019 · N930AT · Boeing 717200 · Trailing Edge Flaps
  > THE LEFT HAND INBOARD FLAP LEADING EDGE WAS FOUND DAMAGED. NRC 010-0001:0514-2001/001 00011: REMOVED AFT VANE PER AMM 27-50-03. REMOVED NOSE ASSY AND ROUTED TO SHOP 383 FOR REPAIR WHICH WAS ACCOMPLISHED ON SHOP ORDER PA4968/ WORK ORDER 19567 AND INSTALLED ORIG
- [SDR DALA2018111206582](https://openairdocs.org/sdr/DALA2018111206582.md): Lens · missing · Nov 11, 2018 · N930AT · Boeing 717200 · Emergency Lighting
  > THE FIRST EMERGENCY LIGHT IN THE AFT ACCESSORY COMPARTMENT IS MISSING THE LENS COVER. MAINTENANCE HAS RE-INSTALLED THE COVER. LIGHT OPERATIONAL CHECK IS GOOD. (LP #5101298)
- [SDR DALA2018091805644](https://openairdocs.org/sdr/DALA2018091805644.md): Power Supply · inoperative · Sep 14, 2018 · N930AT · Boeing 717200 · Emergency Lighting
  > ON A SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERHEAD CEILING EMERGENCY LIGHTS TURNING ON AND THEN OFF. MAINTENANCE REPLACED THE FORWARD TWO EMERGENCY LIGHT POWER SUPPLIES PER AMM 33-51. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM
- [SDR DALA2017112008243](https://openairdocs.org/sdr/DALA2017112008243.md): Lens · missing · Nov 19, 2017 · N930AT · Boeing 717200 · Emergency Lighting
  > AFT EXIT DOOR CEILING LIGHT MISSING THE LENS. MAINTENANCE INSTALLED A NEW LENS.
- [SDR DALA201706301](https://openairdocs.org/sdr/DALA201706301.md): Skin · delaminated · Jun 30, 2017 · N930AT · Boeing 717200 · Spoilers
  > DURING UNSCHEDULE MAINTENANCE CHECK, THE LT OTBD SPOILER FOUND DELAMINATED.
- [SDR DALA2017042603394](https://openairdocs.org/sdr/DALA2017042603394.md): Floor Panel · cracked · Apr 25, 2017 · N930AT · Boeing 717200 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 223AF IS CORRODED IN SEVERAL AREAS AND CRACKED AT CORNER. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-20-50-01. STOP DRILLED THE CRACK IAW SRM 53-00-00-2R-1. INSTALLED REPAIR DOUBLER IAW SRM 53-00-00-2R-1 FIG 201.
- [SDR DALA2017042403350](https://openairdocs.org/sdr/DALA2017042403350.md): Pan · corroded · Apr 23, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON DOOR JAMB PAN AT LOWER CENTER DOOR STOP. BLENDED CORROSION ON ALC DOOR JAMB PAN AT LOWER CENTER DOOR STOP, REMOVED.020" OUT OF.050" ORIGINAL THICKNESS (MAX ALLOWABLE.010"), FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 TOOL TAG #2737, REPLACE
- [SDR DALA2017042303302](https://openairdocs.org/sdr/DALA2017042303302.md): Floor Support · corroded · Apr 21, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > UPPER CABIN FLOOR SUPPORTS BETWEEN STA 178 - 202 AT RBL 30-44 ARE CORRODED IN SEVERAL AREAS. REPLACE FLOOR SUPPORT RBL 30.00-44 PER SRM 51-41-02 & DRAWING 9936534.
- [SDR DALA2017042203299](https://openairdocs.org/sdr/DALA2017042203299.md): Cusp Web · corroded · Apr 21, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > RIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND UPPER AND LOWER SURFACES OF LIGHTENING HOLES. REPAIRED CUSP WEB AT STA 446 TO 465 IAW SRM 53-00-55-2R-4 SHEET 4.
- [SDR DALA2017042203298](https://openairdocs.org/sdr/DALA2017042203298.md): Cusp Web · corroded · Apr 21, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > RIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND AROUND LOWER SURFACE OF LIGHTENING HOLES AT STA 484 TO 503. BLENDED CORROSION ON CUSP WEB AT FS 484-503R OT.020 REMAINING.010 OUT OF LIMITS IAW SRM 53-00-55. REPAIRED CUSP WEB IAW SRM 53-00-55-2R-4 FIG 215

Next page: https://openairdocs.org/aircraft/N930AT/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 = 'N930AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N930AT/reports

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