# Service difficulty reports: N936AT

A list on [N936AT](https://openairdocs.org/aircraft/N936AT.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 · 206 reports

- [SDR DALA2026082404796](https://openairdocs.org/sdr/DALA2026082404796.md): Oxygen Mask · unsecure · Aug 21, 2026 · N936AT · Boeing 717200 · Passenger Oxygen System
  > FWD FA JS OXYGEN MASK FELL, SECURED MASKS & STOWAGE BOX IAW AMM 35-13. (6787282) (AIRCRAFT GROUNDED).
- [SDR DALA2026080404491](https://openairdocs.org/sdr/DALA2026080404491.md): Aoa · failed · Aug 1, 2026 · N936AT · Boeing 717200 · Stall Warning System
  > ATO- APPROX 30KTS DUE TO STICK PUSHER FAIL AND DISARM SPOILERS ANNUNCIATION WITH ASSOCIATED MASTER CAUTION. REPLACED NR 2 AOA SENSOR. ALL OPS CHECK GOOD. (6787252) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026071304125](https://openairdocs.org/sdr/DALA2026071304125.md): Structure · corroded · Jul 10, 2026 · N936AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON INTERNAL STRUCTURE OF BOLT HOLES AND BARREL NUT HOLES 30. INTERNAL STRUCTURE OF BOLT HOLES AND BARREL NUT HOLES 30, 32, AND 34 OF RH SIDE AT HORIZONTAL STAB WERE REPAIRED PER ER/A 635300-14AD. (1693000) (AIRCRAFT GROUNDED)
- [SDR DALA2026071004048](https://openairdocs.org/sdr/DALA2026071004048.md): Web · cracked · Jul 10, 2026 · N936AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON AFT CABIN BULKHEAD DOOR WEB AND X= 12 L/H AT CPAX, R & R CABIN BULKHEAD DOOR PER B717-200 SRM 51-41-02-0G, B717-200 SRM 51- 41-01-0G, B717-200 SRM 51-41-05-0G AND B717- 200 SRM 51-20-09-0G, B717-200 SRM 51-10-04-0G, B717-200 SRM 51-40- 04-0G. (16914
- [SDR DALA2026070904034](https://openairdocs.org/sdr/DALA2026070904034.md): Skin · cracked · Jul 9, 2026 · N936AT · Boeing 717200 · Landing Gear Doors
  > CRACKS ON INTERNAL SKIN BTW STA Y= 760/770 AND BTW STA X= -45/-60 APPROX AT RT MLG DOOR, COMPLIED WITH ER/A 634942-14. (1689728) (AIRCRAFT GROUNDED).
- [SDR DALA2026070603939](https://openairdocs.org/sdr/DALA2026070603939.md): Support Bracket · worn · Jul 5, 2026 · N936AT · Boeing 717200 · Aerodynamic Fairings
  > WORN SPRING SUPPORT BRACKET & PULLEY BRACKET OF RELEASE MECHANISM AT TAIL CONE. SPRING SUPPORT BRACKET, SPRING RELEASE MECHANISM & PULLEY BRACKET OF RELEASE MECHANISM AT TAIL CONE WERE REPLACED IAW AMM 20-50-01 AND SRM 51-41-01-0G. (1682506)(AIRCRAFT GROUNDED)
- [SDR DALA2026070703971](https://openairdocs.org/sdr/DALA2026070703971.md): Spar Cap · corroded · Jul 3, 2026 · N936AT · Boeing 717200 · Horizontal Stabilizer, Spar/Rib
  > CORROSION, LT HORIZONTAL STAB UPPER & LOWER AFT PANEL, UPPER CENTER PANEL, REAR SPAR LWR CAP BARREL NUT HOLES 10, 14, 29, 31, 32, 33. REPAIRED IAW ER/A 635147-14. (1684969) (AIRCRAFT GROUNDED)
- [SDR DALA2026070603941](https://openairdocs.org/sdr/DALA2026070603941.md): Spar Cap · corroded · Jul 1, 2026 · N936AT · Boeing 717200 · Horizontal Stabilizer, Spar/Rib
  > CORROSION RT HORIZONTAL STAB LOWER AFT PANEL, LOWER REAR SPAR CAP BARREL NUT HOLES 30, 32, 34. REPAIRED IAW ER/A 635300-14AD. (1679290)(AIRCRAFT GROUNDED)
- [SDR DALA2026062503777](https://openairdocs.org/sdr/DALA2026062503777.md): Skin · corroded · Jun 25, 2026 · N936AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON UPPER WING SKIN BTW XRS=449 TO XRS=455 AND 12 FROM TRAILING EDGE AT RT WING. REPAIRED PER ER/A 634809-14. (1664981) (AIRCRAFT GROUNDED)
- [SDR DALA2026062303738](https://openairdocs.org/sdr/DALA2026062303738.md): Cusp Web · corroded · Jun 23, 2026 · N936AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON CUSP WEB UPPER SIDE BTW X=-56 AND BS 304-310, BS 456-463, BS 570-577, STA 797-811 AND STA 944. CORROSION LEVEL 2, CUSP WEB UPPER SIDE BTW X=-56 AND BS 304-310, BS 456-463, BS 570-577, BS 797-811 AND 944 WERE REPAIRED IAW SRM 53-00-5
- [SDR DALA2026062303737](https://openairdocs.org/sdr/DALA2026062303737.md): Diaphragm · corroded · Jun 22, 2026 · N936AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON DIAPHRAGM BTW STA Y=190, AND X46.5 TO X56 STA Y=196.5, AT CPAX (LH SIDE). CORROSION LEVEL 2 DIAPHRAGM BTW STA Y=160 TO STA Y=200 AND X=46.5 TO X=56, AT CPAX (LH) WAS REPLACED PER DWG 9936534-289 REV. BW AND PER B717-200 SRM 51-41-02
- [SDR DALA2026061903680](https://openairdocs.org/sdr/DALA2026061903680.md): Cusp Web · cracked · Jun 19, 2026 · N936AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW X=-44 AND STA 674, STA 717 ALSO IN X=-56 AND STA 1014 AT CPAX. CUSP WEB BTW X=-44 AND STA 674, CUSP WEB BTW X=-56 AND STA 1014 WERE REPAIRED IAW SRM 53-00-55-2R-4 PAR. 5 FIG. 215, NO CRACKS WERE FOUND AT STA 717 PER NDTSPM PART 6, 06-10
- [SDR DALA2026061903676](https://openairdocs.org/sdr/DALA2026061903676.md): Skin · out of limits · Jun 17, 2026 · N936AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > HOLES OUT OF LIMITS ON LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267, LT AND RT SIDE) AT VERTICAL STABILIZER REMOVABLE LEADING EDGE. LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267, LT AND RT SIDE) AT VERTICAL STABILIZER REMOVABLE LEADING EDGE WAS REPAIRED PER
- [SDR DALA2026061603615](https://openairdocs.org/sdr/DALA2026061603615.md): Cusp Web · cracked · Jun 15, 2026 · N936AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9563, INITIAL INSPECTION: CRACK ON LH CUSP WEB BTW X54 STA Y=499, X56.5 STA Y= 631, X46 AND STA Y=675 AT CPAX. LT CUSP WEB BTW X54 STA Y=499, X56.5 STA Y=631, X46 AND STA Y=675 AT CPAX WERE REPAIRED IAW SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG. 221
- [SDR DALA2026061103543](https://openairdocs.org/sdr/DALA2026061103543.md): Longeron · cracked · Jun 6, 2026 · N936AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERONS L7R, L8R, AND L17R STA Y=1022 AND -X=56 AT CPAX. LONGERON L8R WAS CUT OUT ON STA Y=1012 TO STA Y= 1053 AND -X=56 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-05-2R. REPAIR 2, LONGERON L7R. CRACKS NO WERE FOUND. PER DC-MD/BOEING NDTSPM PART
- [SDR DALA2025111908460](https://openairdocs.org/sdr/DALA2025111908460.md): Landing Gear · malfunctioned · Nov 18, 2025 · N936AT · Boeing 717200 · Landing Gear Retraction/Extension System
  > LANDING GEAR DID NOT DEPLOY ALL RED INDICATIONS NO FAULT MESSAGES DISPLAYED. AFTER GO AROUND GEAR DEPLOYED NORMAL ON 2ND ATTEMPT. GEAR HANDLE FULL DOWN HYD PRESS NML, NML DOOR INDICATIONS NO FAULTS ON PSEU BITE IAW B717 FIM 32-60. (8154976)
- [SDR DALA2025090906666](https://openairdocs.org/sdr/DALA2025090906666.md): Access Panel · damaged · Sep 5, 2025 · N936AT · Boeing 717200 · Wing, Plate/Skin
  > IN REF NRC 124 AFTER CLEAN ELONGATED HOLE FOUND ON FUEL ACCESS PLATE 520 JB. FUEL ACCESS PLATE 520JB WAS REPAIRED PER ER/A 628967-14AD (1183419)
- [SDR DALA2025081806156](https://openairdocs.org/sdr/DALA2025081806156.md): Battery · no test · Aug 12, 2025 · N936AT · Boeing 717200 · Emergency Lighting
  > SHIP 9563 AFT BULKHEAD EMERGENCY EXIT LIGHT FLICKERING. CORRECTIVE ACTION: REMOVED AND REPLACED EMERG BATT ASSY B5-260.PER B717 AMM 33-51 AND BATT PER B717B AMM 33-51 OPS CHK OK. (6671296)
- [SDR DALA2025081105990](https://openairdocs.org/sdr/DALA2025081105990.md): None · none · Jun 21, 2025 · N936AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9563 LOGPAGE CREATED TRACKING SECTION II INSPECTIONS TO ER/A 610356- 14AD. CORECTIVE ACTION: C/W ER/A 571712-14AD. (1037974)
- [SDR DALA2025052704029](https://openairdocs.org/sdr/DALA2025052704029.md): Generator · failed · May 19, 2025 · N936AT · Boeing 717200 · AC Generator-Alternator
  > ABORTED TAKE-OFF DUE TO A LEFT ENGINE GENERATOR FAILURE MESSAGE: REPLACED GROND RELAY AND AUX POWER RELAY. TEST GOOD.
- [SDR DALA2025033102355](https://openairdocs.org/sdr/DALA2025033102355.md): Power Supply · inoperative · Mar 30, 2025 · N936AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN ABOVE FWD F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE B5-235 EMERGENCY BATTERY POWER SUPPLY/CHARGER REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7237017)
- [SDR DALA2024110510647](https://openairdocs.org/sdr/DALA2024110510647.md): Battery Pack · inoperative · Nov 5, 2024 · N936AT · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN TAIL COMPARTMENT TO BE INOPERATIVE. DETERMINED THAT THE BATTERY PACK B5-116 WAS BAD. BATTERY PACK WAS REPLACED REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6585244)
- [SDR DALA2023082406885](https://openairdocs.org/sdr/DALA2023082406885.md): Unknown · unknown · Aug 23, 2023 · N936AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED FRAME) AT PYLON OF RH ENGINE. SUMMARY OF NRC 00066; UPPER EXTERNAL SKIN PROTECTION STA Y=1200 (CANTED FRAME) AT PYLON OF RH ENGINE WAS REPAIRED PER B717-200 SRM 54-00-00-2R PROCEDURE 1 REPAIR 1. (LP #2
- [SDR DALA2023072105930](https://openairdocs.org/sdr/DALA2023072105930.md): Unknown · unknown · Jul 20, 2023 · N936AT · Boeing 717200 · Emergency Lighting
  > THE CABIN OVERWING EMERGENCY EXIT LIGHTS B5-121/P9 AND B5-121/P11 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-121 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #4711630)
- [SDR DALA2023071305677](https://openairdocs.org/sdr/DALA2023071305677.md): Unknown · unknown · Jul 12, 2023 · N936AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > WHILE PERFORMING AA 5530-01048 AND AD 2018-10-08, FOUND 3 CRACK INDICATIONS ON LT. LOWER FIXED LEADING EDGE SKIN (MARKED). COMPLIED WITH ER/A 610352-14AD REV ORIGINAL PRI REV 0. COMPLIED WITH PRI 610352-14AD PRI REV 1, ER/A 610352-14 REV. ORIGINAL MATCHES PRI
- [SDR DALA2023071205667](https://openairdocs.org/sdr/DALA2023071205667.md): Unknown · unknown · Jul 12, 2023 · N936AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > FOUND ONE CRACK INDICATION ON RH VERTICAL STAB WHILE PERFORMING AA5530-01048 AND AD 2018-10-08 (MARKED). ONE CRACK INDICATION RH VERTICAL STAB IN SPAR AND WHILE REINSPECTING AREA IN QUESTION WHILE PERFORMING AA5530-01048 AND AD2018-10-08. COMPLIED WITH ER/A 61
- [SDR DALA2023071205666](https://openairdocs.org/sdr/DALA2023071205666.md): Unknown · unknown · Jul 12, 2023 · N936AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > R/H VERTICAL STAB, WHILE ACCOMPLISHING INSPECTION PER WORK CARD 5530-0148-02 FAA AD 2018, FOUND A CRACK INDICATION TO ONE HOLE OF THE FRONT SPAR CAP. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 0. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 1. CO
- [SDR DALA2023071305676](https://openairdocs.org/sdr/DALA2023071305676.md): Unknown · unknown · Jul 11, 2023 · N936AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > FOUR CRACK INDICATIONS ON LH VERTICAL STAB WHILE PERFORMING AA5530- 01048 AND AD 2018-10-08 (MARKED). REINSPECTED AREA FOUND 3 CRACK INDICATIONS IN LOWER SPAR CAP WHILE PERFORMING AA5530-01048 AND AD 2018-10-08. THE ABOVE 3 CRACK INDICATIONS ARE ON LT LOWER SK
- [SDR DALA2022092106229](https://openairdocs.org/sdr/DALA2022092106229.md): None · none · Sep 20, 2022 · N936AT · Boeing 717200 · Escape Slide
  > THE J HOOK FOR THE GIRT BAR TO SLIDE WAS DISCONNCTED AT DOOR 1R. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE RESECURED GIRT BAR PER B717 AMM 25-61 R1 DOOR. (LP #9063162)
- [SDR DALA2022020800814](https://openairdocs.org/sdr/DALA2022020800814.md): None · none · Feb 5, 2022 · N936AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON AFT CARGO DOOR JAMB LOWER AREA (CCT). SUMMARY OF NRC #00013: AFT CARGO DOOR JAMB LOWER AREA WAS REPAIRED PER B717 SRM 53-20-15-2R, REPAIR 7. (LP #2111475)
- [SDR DALA2022020800813](https://openairdocs.org/sdr/DALA2022020800813.md): None · none · Feb 5, 2022 · N936AT · Boeing 717200 · Fuselage Floor Panel
  > NICK ON FWD CARGO DOOR JAMB LOWER AREA, BTW STA 389-393 (CCD). SUMMARY OF NRC 00017: FWD CARGO DOOR JAMB LOWER AREA, BTW STA 389-393 WAS REPAIRED PER B717 SRM 53-20-15-2R REP. 6. (LP #2110946)
- [SDR DALA2022020800811](https://openairdocs.org/sdr/DALA2022020800811.md): None · none · Feb 4, 2022 · N936AT · Boeing 717200 · Aerodynamic Fairings
  > THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS TORN OUT OF LIMITS. 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 5
- [SDR DALA2021122308001](https://openairdocs.org/sdr/DALA2021122308001.md): None · none · Dec 22, 2021 · N936AT · Boeing 717200 · Fire Detection
  > SHIP 9563 -DIV/INFLT SHUTDN- TO MSY DUE TO RIGHT ENGINE FIRE WARNING. CREW PULLED FIRE HANDLE AND DISCHARGED BOTH BOTTLES. CORRECTIVE ACTION: MAINTENANCE REPLACED NUMBER 1 AND 2 FIRE BOTTLES PER B717 AMM 26-21 AND REPLACED RIGHT ENGINE FDCU PER B717 AMM 26-11.
- [SDR DALA2021080904512](https://openairdocs.org/sdr/DALA2021080904512.md): Battery Pack · discharged · Aug 7, 2021 · N936AT · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND THAT THE B5235 EMERGENCY BATTERY PACK WAS DEAD. THE B5235 EMERGENCY BATTERY PACK WAS REPLACED. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. (LP #7930220)
- [SDR DALA2021062503447](https://openairdocs.org/sdr/DALA2021062503447.md): Battery Pack · no test · Jun 25, 2021 · N936AT · Boeing 717200 · Emergency Lighting
  > THE OVERWING EMERGENCY EVACUATION LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK B5-125 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7803975)
- [SDR DALA2020112303835](https://openairdocs.org/sdr/DALA2020112303835.md): Battery Pack · inoperative · Nov 22, 2020 · N936AT · Boeing 717200 · Emergency Lighting
  > THE LOWER EXIT SIGNS AT DOORS 1L AND 1R NOT WORKING. MAINTENANCE FOUND THE BATTERY 35-118 TO BE INOPERATIVE. THE BATTERY WAS REPLACED, PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE.
- [SDR DALA2019062903951](https://openairdocs.org/sdr/DALA2019062903951.md): Skin · nicked · Jun 29, 2019 · N936AT · Boeing 717200 · Wing, Plate/Skin
  > NICKS AT LT WING LOWER SKIN, LOWER SURFACE AROUND FUEL ACCESS PLATES, #520EB, 520LB, AND 520MB. NRC 00603: NICKS AROUND FUEL ACCESS PLATES #520EB AND 520LB WERE REPAIRED PER ETI- 17-19-105 REV. 1 AND ER/A 579383-14 REV. ORIG SECTION I. NICK ON FUEL ACCESS PLAT
- [SDR DALA2019070304029](https://openairdocs.org/sdr/DALA2019070304029.md): Skin · dented · Jun 28, 2019 · N936AT · Boeing 717200 · Aileron Tabs
  > INITIAL INSPECTION, DENT ON AILERON CONTROL TAB UPPER FACE AT RT WING. AILERON CONTROL TAB RT P/N 5910047-410 S/N 518 WAS REMOVED PER AMM 27-10-02 AILERON CONTROL TAB P/N 5910047-502 S/N NSN1 WAS INSTALLED PER AMM 27-10-02. TAB, AILERON, C OFF 09-5750-9-0002 0
- [SDR DALA2019062903950](https://openairdocs.org/sdr/DALA2019062903950.md): Pin · missing · Jun 28, 2019 · N936AT · Boeing 717200 · Aerodynamic Fairings
  > DURING INSTALLATION OF TAILCONE SLIDE, PIN P/N MS20392-2C9 WAS NOT FOUND IN REFERENCE TO 5352-4002 STEP 6 ( CPAX). NRC 0721: NEW PIN FOR THE TAILCONE SLIDE WAS INSTALLED PER AMM 25-61-02-400-801 STEP D 1 (I). (LP #1146033)
- [SDR DALA2019062903939](https://openairdocs.org/sdr/DALA2019062903939.md): Skin · nicked · Jun 28, 2019 · N936AT · Boeing 717200 · Trailing Edge Flaps
  > NICKS ON AFT MOVABLE FLAP VANE LOWER SURFACE AT RT WING (AD). NRC 00236: NICKS ON AFT MOVABLE FLAP VANE LOWER SURFACE AT RT WING WERE REPAIRED PER SRM 57-53-01-2R-1 AND 51-70-02-0G. (LP #1145757)
- [SDR DALA2019062803912](https://openairdocs.org/sdr/DALA2019062803912.md): Frame · corroded · Jun 27, 2019 · N936AT · Boeing 717200 · Fuselage Main, Frame
  > EXFOLEATED FRAME ON STA Y=1022 BTW LONG 23 LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00303: CORROSION LEVEL 2, FRAME ON STA Y=1022 BTW LONG 23 LH AND 27RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3, 51-41-02-0G, AND 51-41-05-0G
- [SDR DALA2019062703886](https://openairdocs.org/sdr/DALA2019062703886.md): Stiffener · corroded · Jun 26, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON STIFFENER STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT. NRC 00322: CORROSION LEVEL 2, STIFFENER STA Y=1053 AND LONG 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG #9915561 REV. CG. (LP #1143074)
- [SDR DALA2019062703884](https://openairdocs.org/sdr/DALA2019062703884.md): Frame · corroded · Jun 26, 2019 · N936AT · Boeing 717200 · Fuselage Main, Frame
  > EXFOLEATED FRAME ON STA Y=1022 BTW LONG 23LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00303: CORROSION LEVEL 2, FRAME ON STA Y=1022 BTW LONG 23LH AND 27RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3, 51-41-02-0G, AND 51-41-05-0G E
- [SDR DALA2019062703883](https://openairdocs.org/sdr/DALA2019062703883.md): Frame · corroded · Jun 26, 2019 · N936AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=1002 BTW LONG 24LH TO LONG 29LH AT AFT CARGO COMPARTMENT. NRC 00267: CORROSION LEVEL 2, FRAME STA Y=1002 BTW LONG 24LH TO LONG 29LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, 53-20-07-2R REPAIR 3 P
- [SDR DALA2019062703877](https://openairdocs.org/sdr/DALA2019062703877.md): Intercostal · corroded · Jun 26, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > EXFOLATION ON INTERCOSTAL STA Y=1037 AND LONG 30 AT AFT CARGO COMPARTMENT. NRC 00315: CORROSION LEVEL 2, INTERCOSTAL WAS REPLACED PER B717-200 SRM 53-20-51-0I 7 ITEM 12 AND 51-41-02-0G. (LP #1142061)
- [SDR DALA2019062703876](https://openairdocs.org/sdr/DALA2019062703876.md): Retainer · cracked · Jun 26, 2019 · N936AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK AT AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS FOUND (CPIL). NRC 00654: AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R. (LP #1142006)
- [SDR DALA2019062603864](https://openairdocs.org/sdr/DALA2019062603864.md): Longeron · corroded · Jun 25, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > LONGERON 30 CORROED BS 1022. THE LONGERON WAS REPLACED IAW SRM 53-20-05 PROCEDURE 3 ITEM 9, 51- 41-02-OG, AND 51-41-05-OG.
- [SDR DALA2019062603860](https://openairdocs.org/sdr/DALA2019062603860.md): Longeron · corroded · Jun 25, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION BTW LONGERON 25L, BS 1002 - 1037 AT CARGO COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2 AND SRM 51-40-08-0G.
- [SDR DALA2019062603859](https://openairdocs.org/sdr/DALA2019062603859.md): Skin · cracked · Jun 25, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK AT FUSELAGE SKIN BS 1076 BETWEEN LONGERON 13 & 14R. THE SKIN WAS REPAIRED PER ETI-17-19-075 REV 5 AND ER/A 579256-14 REV. ORIG.
- [SDR DALA2019062603858](https://openairdocs.org/sdr/DALA2019062603858.md): Skin · damaged · Jun 25, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DAMAGE ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT. REWORKED AREA ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT WAS REPAIRED PER PERMANET REPAIR IAW SRM 53-02-01- 2R FIG. 202 (SHEET 13).

Next page: https://openairdocs.org/aircraft/N936AT/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 = 'N936AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N936AT/reports

---
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