# Service difficulty reports: N937AT

A list on [N937AT](https://openairdocs.org/aircraft/N937AT.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 · 240 reports

- [SDR DALA2026092905409](https://openairdocs.org/sdr/DALA2026092905409.md): Doubler · misinstalled · Sep 28, 2026 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND PCS DOUBLER AT WRONG LOCATION. REPAIRED PER ER/A 637058-14AD. (1837396) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026092805398](https://openairdocs.org/sdr/DALA2026092805398.md): Skin · not reported · Sep 26, 2026 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE CROWN Y503 - Y522, L-1 - L-3R EXISTING DOUBLER NEAR STC INSTALL AREA. REPAIRED PER ER/A 637058-14. (1833937) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026090204947](https://openairdocs.org/sdr/DALA2026090204947.md): Skin · damaged · Sep 1, 2026 · N937AT · Boeing 717200 · Cargo/Baggage Doors
  > FOUND DAMAGE AT AFT CARGO DOOR SKIN AFT EDGE. BLENDED MINOR SKIN EDGE DAMAGE FROM AFT CARGO AFT AREA SKIN IAW SRM 51-70-01-2R. (8313198) (AIRCRAFT GROUNDED).
- [SDR DALA2026090204946](https://openairdocs.org/sdr/DALA2026090204946.md): Skin · damaged · Sep 1, 2026 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > RAMP REPORTS DAMAGE ON SKIN EDGE OF AFT CARGO DOOR CUTOUT AFT FUSELAGE SKIN. BLENDED MINOR DAMAGE ON AFT CARGO AFT DOOR SIL IAW SRM 51- 70-01-2R. (8313197) (AIRCRAFT GROUNDED).
- [SDR DALA2026090204945](https://openairdocs.org/sdr/DALA2026090204945.md): Skin · damaged · Sep 1, 2026 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE ON SKIN EDGE OF AFT CARGO DOOR FWD FUSELAGE SKIN. BLENDED SURFACE IAW SRM 53-01-01-1A-1. (8313196) (AIRCRAFT GROUNDED).
- [SDR DALA2026061903681](https://openairdocs.org/sdr/DALA2026061903681.md): Tire · failed · Jun 19, 2026 · N937AT · Boeing 717200 · Tire
  > SHIP 9586-ATB- THE FLIGHT CREW REPORTED A SUSPECTED RT MAIN TIRE FAILURE ON TAKEOFF WITH AN ASSOCIATED GEAR UNSAFE LIGHT ILLUMINATED AND RETURNED FROM FLIGHT. REPLACED NR 3 AND 4 TIRE ASSEMBLIES, RIGHT MLG DOWNLOCK SENSOR HARNESS, AND RIGHT WING FLAP. (LP 887
- [SDR DALA2026060903441](https://openairdocs.org/sdr/DALA2026060903441.md): Oil System · leaking · Jun 4, 2026 · N937AT · Boeing 717200 · APU Oil System
  > DIRTY SOCK ODOR ON GROUND AT GATE FROM BOTH PACKS INDEPENDENTLY ON APU AIR. T/S PER FIM 49-50 FOUND OIL INSIDE THE APU PLENUM. R & R COELESSOR BAGS IAW AMM 21-54 OLD BAGS SMELLED LIKE OIL (8655364) (AIRCRAFT GROUNDED)
- [SDR DALA2026060203346](https://openairdocs.org/sdr/DALA2026060203346.md): Oil System · leaking · May 31, 2026 · N937AT · Boeing 717200 · APU Oil System
  > FLIGHT ATTENDANTS REPORTED A MUSTY OR MILDEW SMELL DURING FLIGHT IN THE MID-CABIN. FOUND APU COMPARTMENT CONTAMINATED WITH OIL. REPLACED APU PER AMDS W/C 4900-9901. (8655352) (AIRCRAFT GROUNDED)
- [SDR DALA2025122309341](https://openairdocs.org/sdr/DALA2025122309341.md): Hinge Fitting · corroded · Dec 20, 2025 · N937AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION FOUND ON BOLT SETTLEMENT AREA (INBRD SIDE) AT RT WING FLAP FWD HINGE NR 3. RT FLAP FWD HINGE WAS REPAIRED IAW PRI 631116-14 REV 2, AND ER/A 631116-14 (1361088)
- [SDR DALA2025122309340](https://openairdocs.org/sdr/DALA2025122309340.md): Strap · cracked · Dec 19, 2025 · N937AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKED ANGLE STRAP BTW CANTED BS 1178, L2R AT ROOT OF VERTICAL STABILIZER. REPAIRED IAW SRM 53-30-01-2R -1. (1358667)
- [SDR DALA2025122909451](https://openairdocs.org/sdr/DALA2025122909451.md): Not Reported · not reported · Dec 18, 2025 · N937AT · Boeing 717200 · Standard Practices/Structures
  > DTA ER/A 631116-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-631116 (1359292)
- [SDR DALA2025121709199](https://openairdocs.org/sdr/DALA2025121709199.md): Lanyard · frayed · Dec 16, 2025 · N937AT · Boeing 717200 · Emergency Equipment
  > FRAYED LANDYARD CABLE FROM L1 SLIDE DOOR. LANYARD CABLE FROM L1 SLIDE DOOR WAS REPLACED AND PART NUMBER WAS VERIFIED PER AIPC 25-61-01 AND INSTALLATION IS ACCOMPLISHED UNDER AMDS 5211-4002. (1354881)
- [SDR DALA2025040102422](https://openairdocs.org/sdr/DALA2025040102422.md): Structure · cracked · Mar 27, 2025 · N937AT · Boeing 717200 · Wing Structure
  > -AD- COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 623843-14AD DUE TO CRACK INDICATION FOUND DURING INSP. COMPLIED WITH PRI 623843-14AD REV 0,1,2, & 3. COMPARED PRI 623843-14AD REV 0,1,2, & 3 WITH ERA 623843-14AD REV ORIG AND ALL ITEMS MAT
- [SDR DALA2025033102349](https://openairdocs.org/sdr/DALA2025033102349.md): Spar · cracked · Mar 27, 2025 · N937AT · Boeing 717200 · Wing Spar
  > -AD- CRACK FOUND IN LWR AFT LEG OF LWR REAR SPAR JUST OB OF FLAP FITTING @ XRS170 DURING LT WING REAR SPAR INSP AMDS #5720-01103-01A. COMPLIED WITH PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7. COMPARED PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7 WITH ERA 623680-14AD R
- [SDR DALA2024060605813](https://openairdocs.org/sdr/DALA2024060605813.md): B-Nut · loose · Jun 6, 2024 · N937AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9586 -ATB/HYD/DE- THE CREW RETURNED THE AIRCRAFT BACK TO MSP AND DECLARED AN EMERGENCY WITH ATC DURING THE APPROACH DUE TO THE LOSS OF THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY. THE LANDING GEAR WAS EXTENDED USING THE ALTERNATE GEAR EXTENSION PROCEDURES.
- [SDR DALA2024060305737](https://openairdocs.org/sdr/DALA2024060305737.md): Jackscrew · corroded · Jun 2, 2024 · N937AT · Boeing 717200 · Flight Control System
  > -AD- FOUND CORROSION ON LOWER JACKSCREW THREADS APPROX 6"ABOVE LOWER STOP. SUMMARY SEE NRC 006-0001:2740-01114-05 /002 00007: REPLACED JACK SCREW PER AMDS 2740-01114-05. CLOSING REQUIREMENTS RII: INSPECTOR 00260220. (LP #0373180)
- [SDR DALA2024042204627](https://openairdocs.org/sdr/DALA2024042204627.md): Battery Pack · malfunctioned · Apr 20, 2024 · N937AT · Boeing 717200 · Emergency Lighting
  > THE TAIL EXIT LIGHT STAYS FLASHING WITH THE EMERGENCY POWER SWITCH ARMED. MAINTENANCE REPLACED THE BATTERY PACK AND CRADLE ASSEMBLY B5-260 PER B717 AMM 33-51. NOW OPERATES NORMALLY. (LP #5832652)
- [SDR DALA2024040103938](https://openairdocs.org/sdr/DALA2024040103938.md): Generator · failed · Mar 29, 2024 · N937AT · Boeing 717200 · AC Generator-Alternator
  > SHIP 9586 -DIV- THE FLIGHT WAS DIVERTED TO MCO FOLLOWING THE FAILURE OF THE RIGHT GENERATOR AFTER TAKEOFF, WHILE THE APU GENERATOR WAS ON MEL. THE CAPTAIN DECLARED AN EMERGENCY WITH ATC. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED ALL R
- [SDR DALA2023122410544](https://openairdocs.org/sdr/DALA2023122410544.md): Unknown · unknown · Dec 24, 2023 · N937AT · Boeing 717200 · Escape Slide
  > IMPROPERLY INSTALLATION OF LATCH AND MANUAL DEPLOYMENT HANDLE OF TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00756: LATCH AND MANUAL DEPLOYMENT HANDLE OF TAIL
- [SDR DALA2023122410542](https://openairdocs.org/sdr/DALA2023122410542.md): Unknown · unknown · Dec 23, 2023 · N937AT · Boeing 717200 · Emergency Exits
  > CRACKED PLATE ON EMERGENCY DOOR INTERNAL STRUCTURE (MIDDLE SECTION) Y=1053 X=10 AT PAX CABIN. SUMMARY OF NRC 00097: PLATE (WEB) ON EMERGENCY DOOR INTERNAL STRUCTURE (MIDDLE SECTION) Y=1053 X=10 AT PAX CABIN WAS REPAIRED PER B717 AMM 52-12-03 000-801, 52-12-03
- [SDR DALA2023121510287](https://openairdocs.org/sdr/DALA2023121510287.md): Unknown · unknown · Dec 13, 2023 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER SKIN ON STA Y 627 BTW LONG 28RH AND LONG 29RH BILGE AREA AT FWD COMPARTMENT. SUMMARY OF NRC 00072: CORROSION LEVEL 2. INNER SKIN ON STA Y 627 BTW LONG 28RH AND LONG 29RH BILGE AREA AT FWD COMPARTMENT WAS REPAIRED PER ERA 598923-14 REV. A AND
- [SDR DALA2023121310200](https://openairdocs.org/sdr/DALA2023121310200.md): Unknown · unknown · Dec 12, 2023 · N937AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON PREVIOUS REPAIR SPLICES ON DOOR JAMB STA Y=954 BTW STRINGER 26-27RH. SUMMARY OF NRC 00698: CORROSION LEVEL 2. PREVIOUS REPAIR SPLICES ON DOOR JAMB STA Y=954 BTW STRINGER 26-27RH SPLICES (2 EA) WERE FABRICATED AND INSTALLED PER B717 SRM 53-20-15-2R
- [SDR DALA2023121310199](https://openairdocs.org/sdr/DALA2023121310199.md): Unknown · unknown · Dec 11, 2023 · N937AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON SPLICE L30 BETWEEN Y=889 AND Y=908, AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2. SPLICE ON L30 BETWEEN Y=889 AND Y=908 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-05-0G PAR 10 AND 51-41-01-0G. (LP #01059
- [SDR DALA2023121110136](https://openairdocs.org/sdr/DALA2023121110136.md): Unknown · unknown · Dec 11, 2023 · N937AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH TRACK ABOVE R=28 BTW STA Y=427+13, Y=446+6 AT LOWER FWD CARGO COMPARTMENT. SUMMARY OF NRC 00068: CORROSION LEVEL 2. RH TRACK ABOVE R=28 BTW STA Y=427+13, Y=446+6 AT LOWER FWD CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 4 R
- [SDR DALA2023121110135](https://openairdocs.org/sdr/DALA2023121110135.md): Unknown · unknown · Dec 11, 2023 · N937AT · Boeing 717200 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM AND BEAM-WEB ATTACHED TO LH FRAME Y=674, X=57 AT PASSENGER CABIN. SUMMARY OF NRC 228: FLOOR BEAM WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. BEAM-WEB ATTACHED TO LH FRAME Y=674, X=57 AT PASSENGER CABIN WAS REPAIRED PER ER/A
- [SDR DALA2023120710007](https://openairdocs.org/sdr/DALA2023120710007.md): Unknown · unknown · Dec 7, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP ANGLE BTW STA Y 208 TO STA Y 164 SERVICE DOOR (R1) AT PAX CABIN. SUMMARY OF NRC 284: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y 208 TO STA Y 164 SERVICE DOOR (R1) AT PAX CABIN WAS REPAIRED PER ERA 613317-14 REV ORIG AND PRI 613317-14 REV 2. ASSO
- [SDR DALA2023120710006](https://openairdocs.org/sdr/DALA2023120710006.md): Unknown · unknown · Dec 6, 2023 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > BEND AND CRACK ON CUTOUT UPPER SIDE OF AIR STAIRWELL DOOR AT APPROX STA Y 160 AND BTW LONG 18LH AND LONG 19LH ON FUSELAGE. SUMMARY OF NRC 00126: CUTOUT UPPER SIDE OF AIR STAIRWELL DOOR AT APPROX STA Y 160 AND BTW LONG 18LH AND LONG 19LH ON FUSELAGE WAS REPAIRE
- [SDR DALA2023120609978](https://openairdocs.org/sdr/DALA2023120609978.md): Unknown · unknown · Dec 5, 2023 · N937AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SEAT TRACK X=-56 BTW STA Y=215-256 AT PAX CABIN. SUMMARY OF NRC 00494: CORROSION LEVEL 2. RH SEAT TRACK X=-56 BTW STA Y=215-256 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-01-0G, AND 53-20-52-2R REPAIR 5. (LP #0096562)
- [SDR DALA2023120609976](https://openairdocs.org/sdr/DALA2023120609976.md): Unknown · unknown · Dec 5, 2023 · N937AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SEAT TRACK X=-44 BTW STA Y=199-256 AT PAX CABIN. SUMMARY OF NRC 0495: CORROSION LEVEL 2. SEAT TRACK X=-44 BTW STA Y=199-256 WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-05-0G, AND PER DWG 5930547 REV CW. (LP #0095908)
- [SDR DALA2023120609975](https://openairdocs.org/sdr/DALA2023120609975.md): Unknown · unknown · Dec 5, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB X=-49 TO X=-60 BTW STA 389-408 AT PAX CABIN. SUMMARY OF NRC 00509: CORROSION LEVEL 2. CUSP WEB X=-49 TO X=-60 BTW STA 389-408 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0095789)
- [SDR DALA2023120409904](https://openairdocs.org/sdr/DALA2023120409904.md): Unknown · unknown · Dec 3, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SURFACE OF CUSP WEB STA Y 705 OVER X49 AND STA Y 676 AND X58 LH SIDE AT CPAX. SUMMARY OF NRC 00307: CORROSION LEVEL 2. CUSP WEB STA Y 655 TO 715 X58 LH SIDE AT CPAX WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0G AND REPAIR PER B71
- [SDR DALA2023120409903](https://openairdocs.org/sdr/DALA2023120409903.md): Unknown · unknown · Dec 2, 2023 · N937AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SEAT TRACK X=22 BTW STA Y=199-256 AT PAX CABIN. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK X=22 BTW Y=199-265 WAS REPLACED PER DWG 5930547 REV CZ AND B717-200 SRM 51-41-01-0G. (LP #0092293)
- [SDR DALA2023120409899](https://openairdocs.org/sdr/DALA2023120409899.md): Unknown · unknown · Dec 2, 2023 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L. SUMMARY OF NRC 00368: EXTERNAL FUSELAGE SKIN Y=1022 BETWEEN LONGERONS L-8L AND L-7L WAS REPAIRED PER ER/A 613350-14 REV ORIGINAL SECTION I: TEMPORARY REPAIR. TIME OF ACCOMPLISHMENT ACCOMPL
- [SDR DALA2023120109872](https://openairdocs.org/sdr/DALA2023120109872.md): Unknown · unknown · Nov 30, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEP STA Y 665, STA Y 674 OVER -X58 RH SIDE AT CPAX. SUMMARY OF NRC 0293: SECTION CUSP WEB STA Y 665, STA Y 674 OVER -X58 RH SIDE AT CPAX WAS REPAIRED PER B-717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #0089035)
- [SDR DALA2023112809759](https://openairdocs.org/sdr/DALA2023112809759.md): Unknown · unknown · Nov 27, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STA Y=1022 TO STAY=1037, LONGERON 30 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00543: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=1022 TO STAY=1037, LONGERON 30 AT AFT CARGO COMPARTMENT WAS FABRICATED PER DWG 9936718 REV N AND REP
- [SDR DALA2023112809758](https://openairdocs.org/sdr/DALA2023112809758.md): Unknown · unknown · Nov 27, 2023 · N937AT · Boeing 717200 · Escape Slide
  > CORROSION ON SLIDE LATCHES AT SERVICE DOOR (R1) IN PAX CABIN. SUMMARY OF NRC 00344: CORROSION LEVEL 2. LATCHES FOR SLIDE AT SERVICE DOOR (R1) IN PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0084409)
- [SDR DALA2023112809751](https://openairdocs.org/sdr/DALA2023112809751.md): Unknown · unknown · Nov 26, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE X=-56 RH Y=150/170 AT CABIN PASSENGER IN REF NRC 284. SUMMARY OF NRC 00518: CORROSION LEVEL 2. NEW ANGLE X=-56 RH Y=150/170 AT CABIN PASSENGER WAS FABRICATED AND REPLACED PER DWG 590085-19 REV DJ. (LP #0081789)
- [SDR DALA2023112709723](https://openairdocs.org/sdr/DALA2023112709723.md): Unknown · unknown · Nov 24, 2023 · N937AT · Boeing 717200 · Vertical Stabilizer
  > CORROSION ON VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN. SUMMARY OF NRC 00230: CORROSION LEVEL 2. VERTICAL WEB STA Y199 TO Y205 X 56.0 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G. (LP #0080112)
- [SDR DALA2023112709717](https://openairdocs.org/sdr/DALA2023112709717.md): Unknown · unknown · Nov 22, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB STA Y 715 AND X44 LH SIDE AT CPAX. SUMMARY OF NRC 00305: CUSP WEB STA Y 715 AND X44 LH SIDE AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, FIGURE 220. (LP #0077736)
- [SDR DALA2023112209649](https://openairdocs.org/sdr/DALA2023112209649.md): Unknown · unknown · Nov 21, 2023 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK AT STA 1086.5 AND LONGERON 13RH APROX ON EXTERIOR FUSELAGE. SUMMARY OF NRC 00014: CRACK AT STA 1086.5 AND LONGERON 13RH APROX WAS REPAIRED PER PRI 613146-14 REV 2 AND ER/A 613146-14 REV ORIGINAL, SECTION I. PERMANENT REPAIR.ACCOMPLISH SECTION II. REPETIT
- [SDR DALA2023111409350](https://openairdocs.org/sdr/DALA2023111409350.md): Unknown · unknown · Nov 13, 2023 · N937AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK UPPER CAP ON STA Y=1022 AND LONGERON 7 LH SIDE AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00188: UPPER CAP ON STA Y=1022 AND LONGERON 7LH SIDE AT PASSENGER CABIN WAS REPAIRED PER PRI 613311-14 REV 1 AND ERA 613311-14 REV ORIGINAL SECTION I: PERMANENT REPA
- [SDR DALA2023111309298](https://openairdocs.org/sdr/DALA2023111309298.md): Unknown · unknown · Nov 9, 2023 · N937AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON PREVIOUS REPAIR ON CUSP WEB RH SIDE ON STA Y 332 AND -X56 AT CPAX. SUMMARY OF NRC 00240: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON CUSP WEB RH SIDE ON STA Y 332 AND -X56 AT CPAX WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #005749
- [SDR DALA2023110409090](https://openairdocs.org/sdr/DALA2023110409090.md): Unknown · unknown · Nov 4, 2023 · N937AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAMS (3 EA) OVER BEAM #1 AFT EDGE AND BEAM #2 AFT/FWD EDGE AT FWD PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00128: CRACK ON BEAMS OVER BEAM #1 AFT EDGE WAS FOUND REPAIRED IN REFERENCE TO LOG 2214723 AND CRACKED BEAM #2 AFT/FWD EDGE AT FWD PASSENGE
- [SDR DALA2023071305679](https://openairdocs.org/sdr/DALA2023071305679.md): Unknown · unknown · Jul 12, 2023 · N937AT · Boeing 717200 · Emergency Lighting
  > AFT F/A READY LIGHT COVER MISSING. RESECURED AFT F/A EMERGENCY LIGHT LENS COVER PER B717 AMM 33-51. A/C OK FOR SVC. (LP #4984108)
- [SDR DALA2023051203750](https://openairdocs.org/sdr/DALA2023051203750.md): Unknown · unknown · May 12, 2023 · N937AT · Boeing 717200 · Emergency Lighting
  > SEVERAL CABIN EMERGENCY LIGHTS AND THE MID-CABIN EXIT IDENFIER LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD AND MID-CABIN BATTERY PACKS IAW B717 AMM 33-55. EMERGENCY LIGHT OPERATIONAL CHECK WAS NORMAL. (LP #9957867)
- [SDR DALA2023050903617](https://openairdocs.org/sdr/DALA2023050903617.md): Unknown · unknown · May 9, 2023 · N937AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS ARE INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THREE EMERGENCY LIGHT BATTERY PACKS PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #9957841)
- [SDR DALA2022092806347](https://openairdocs.org/sdr/DALA2022092806347.md): None · none · Sep 24, 2022 · N937AT · Boeing 717200 · Emergency Lighting
  > ON INTERIOR WALK-THROUGH, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED ONE BATTERY PACK ABOVER ROW 19, FOR THE OVERWING EMERGENCY EXIT LIGHTS PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. ALL EMERGENCY LIGHTS NOW OPERA
- [SDR DALA2022071304854](https://openairdocs.org/sdr/DALA2022071304854.md): None · none · Jul 10, 2022 · N937AT · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND THAT THE EMERGENCY LIGHT OVER THE AFT EMERGENCY EXIT WAS NOT WORKING, WHEN PREFORMING LIGHTS TEST. THE POWER SUPPLY ASSOCIATED WITH THE LIGHT WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #7301237)
- [SDR DALA2022050103043](https://openairdocs.org/sdr/DALA2022050103043.md): Skin · corroded · Apr 29, 2022 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > PROTUBERANCE PROVOKED BY CORROSION ON EXTERNAL FUSELAGE SKIN STA 650-655 BTW LONG 28LH TO 29LH. SUMMARY OF NRC 00226: LEVEL CORROSION 2, EXTERNAL FUSELAGE SKIN STA 650-655 BTW LONG 28LH TO 29LH WAS REPAIRED PER PRI 598923-14 REV. 2 AND ER/A 598923-14 SECTION I
- [SDR DALA2022051203283](https://openairdocs.org/sdr/DALA2022051203283.md): None · none · Apr 28, 2022 · N937AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND INTERNAL DOUBLER STA 630 TO 655, L-28R TO L-29L CORROSION & CRACKS. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. REVISED REPAIR LOCATION DESCRIPTION TO MATCH ER/A AS FOLLOWS; FUSELAGE SKIN AND INTERNAL DOUBLER STA 626 TO 661, L-2

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## 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 = 'N937AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N937AT/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.