# Service difficulty reports: N927AT

A list on [N927AT](https://openairdocs.org/aircraft/N927AT.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 · 218 reports

- [SDR DALA2026091105082](https://openairdocs.org/sdr/DALA2026091105082.md): Apu · odor · Sep 10, 2026 · N927AT · Boeing 717200 · Airborne Auxiliary Power Unit (APU) System
  > BOARDING THE ACFT W/APU ON THERE IS A VERY STRONG DIRTY SOCK SMELL IN ALL AREAS OF THE COCKPIT AND CABIN, CORRECTIVE ACTION: R/R APU IAW W/C 4900-9901. (9518000) (AIRCRAFT GROUNDED).
- [SDR DALA2026090905049](https://openairdocs.org/sdr/DALA2026090905049.md): Vane · damaged · Sep 9, 2026 · N927AT · Boeing 717200 · Trailing Edge Flaps
  > EVIDENCE OF RUBBING ON AFT SIDE OF RIGHT MAIN LANDING GEAR AND LEADING EDGE OF FLAP, R&R RT FWD MOVEABLE VANE REF AMDS WC 2750-4010. (9488696) (AIRCRAFT GROUNDED).
- [SDR DALA2026082404795](https://openairdocs.org/sdr/DALA2026082404795.md): Coalescer Bag · odor · Aug 23, 2026 · N927AT · Boeing 717200 · Humidity Control System
  > SLIGHT DIRTY SOCK SMELL AFTER LONG IDLE DESCENT. R & R COALESCER BAGS IAW AMM 21-54-08. (9488641) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903842](https://openairdocs.org/sdr/DALA2026062903842.md): Elec Connector · damaged · Jun 28, 2026 · N927AT · Boeing 717200 · Light System Wiring
  > R1 EMERGENCY LIGHT INOP. REPINNED CONNECTOR PERB717 AMM 20-30. (9221037) (AIRCRAFT GROUNDED).
- [SDR DALA2026042202564](https://openairdocs.org/sdr/DALA2026042202564.md): Engine · failed · Apr 19, 2026 · N927AT · Boeing 717200 · APU Core Engine
  > SMKE/FUME - PRIOR TO PUSH, CREW REPORTED WHITE HAZY SMOKE AND AN OIL SMELL IN THE CABIN FOLLOWED BY A HARD CLUNK AND AN APU AUTO SHUTDOWN. RAMP REPORTED FLAMES IN APU EXHAUST. FOUND APU CHIP DETECTOR FULL OF METAL AND SUSPECTED APU INTERNAL FAILURE. APU REPL
- [SDR DALA2026012200496](https://openairdocs.org/sdr/DALA2026012200496.md): Fadec · faulted · Jan 17, 2026 · N927AT · Boeing 717200 · Fuel Controlling System
  > FLIGHT CREW DIVERTED TO ATL DUE TO RIGHT ENGINE FADEC ALTERNATE MODE CAUSING FLIGHT TO BE REMOVED FROM CAT 1/2/3 AND RVSM. REMOVED AND REPLACED RIGHT ENGINE P20/T20 PROBE AND EEC.(7905400)
- [SDR DALA2025111808427](https://openairdocs.org/sdr/DALA2025111808427.md): Engine · surges · Nov 14, 2025 · N927AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > ATB- RETURNED TO MSP DUE TO LEFT ENGINE SURGING. REDUCED THRUST AND SURGING STOPPED. REPLACED LEFT ENGINE. OPS CHECK NORMAL. (8225854).
- [SDR DALA2025091606815](https://openairdocs.org/sdr/DALA2025091606815.md): Compressor · damaged · Sep 11, 2025 · N927AT · Boeing 717200 · Turbine Engine Compressor Section
  > ATB TO ATL DUE TO NR 1 ENGINE COMPRESSOR STALL ON CLIMB OUT. BORESCOPED LT ENGINE AND FOUND MULTIPLE BLADES IN HPC DAMAGED. REPLACED ENGINE.(7723471)
- [SDR DALA2025081105984](https://openairdocs.org/sdr/DALA2025081105984.md): Power Supply · faulted · Aug 3, 2025 · N927AT · Boeing 717200 · Emergency Lighting
  > SHIP 9572 EMERGENCY LIGHT EXTERIOR DON'T TURN ON. CORECTIVE ACTION: OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-06. TEST OK.(6377081)
- [SDR DALA2025080205796](https://openairdocs.org/sdr/DALA2025080205796.md): Fuel Cell · corroded · Jul 28, 2025 · N927AT · Boeing 717200 · Fuel Storage
  > CORROSION ON CENTER FUEL TANK UPPER SKIN AFT FLANGE STA 747 X=-55 TO X=-59. REPAIRED PER PRI 626998-14.
- [SDR DALA2025072905675](https://openairdocs.org/sdr/DALA2025072905675.md): Skin · cracked · Jul 25, 2025 · N927AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9572 INITIAL INSPECTION: CRACK ON EXTERNAL FUSELAGE SKIN STA 1076 BTW. CORRECTIVE ACTION: EXTERNAL FUSELAGE SKIN STA 1076 BTW LONG 13-14 LH WAS REPAIRED PER REPAIR ERA PRI 626436-14AD (1105456)
- [SDR DALA2025072405582](https://openairdocs.org/sdr/DALA2025072405582.md): Hinge · corroded · Jul 23, 2025 · N927AT · Boeing 717200 · Leading Edge Devices
  > SHIP 9572 AFTER MIDLE FLAP HINGE, CORROSION ON HINGE FITTING HOLES AT LH FLAP. ALSO SCRATCHES HINGE BOLTS (3EA). CORRECTIVE ACTION: HINGE FITTING HOLES AT LH FLAP WERE REPAIRED PER PRI 626829-14 (1101699)
- [SDR DALA2025072405581](https://openairdocs.org/sdr/DALA2025072405581.md): Skin · corroded · Jul 22, 2025 · N927AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9572 IN REF NRC 00308, CORROSION ON CENTER WING UPPER SKIN BTW STA Y= 715/720 X = -60 AT WING BOX. CORRECTIVE ACTION: CORROSION ON CENTER WING UPPER SKIN BTW STA Y= 715/720 X = -60 AT WING BOX WAS REPAIRED PER ERA 626657- 14 AD REV ORIGINAL SECTION I: PER
- [SDR DALA2025071805420](https://openairdocs.org/sdr/DALA2025071805420.md): Pan · cracked · Jul 18, 2025 · N927AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING AN AFT LOWER CARGO DOOR INSPECTION PER WC 5231-2004, SEVEN (7 QTY) CRACKS WERE FOUND AFFECTING THE AFT CARGO DOOR INNER PAN AFT EDGE AT STOPS #1, # 3 & 5. ADDITIONALLY, A GOUGE WAS FOUND BETWEEN STOP FITTINGS
- [SDR DALA2025071705384](https://openairdocs.org/sdr/DALA2025071705384.md): Pan · cracked · Jul 17, 2025 · N927AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A FORWARD LOWER CARGO DOOR INSPECTION PER WC 5231-2005, FIVE (5 QTY) CRACKS WERE FOUND AFFECTING THE FWD CARGO DOOR AT LOWER INNER AND OUTER PAN BETWEEN STA Y=389 AND Y=408 AS FOLLOWS: TWO (2 QTY) CRACKS AT IN
- [SDR DALA2025071705383](https://openairdocs.org/sdr/DALA2025071705383.md): Pan · cracked · Jul 17, 2025 · N927AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING AN AFT LOWER CARGO DOOR INSPECTION PER WC 5231-2004, THREE (3 QTY) CRACKS WERE FOUND AFFECTING THE AFT CARGO DOOR INNER PAN FWD EDGE AT STOP #2. ADDITIONALLY, AN EXISTING REPAIR WAS FOUND INSTALLED AT THE FWD
- [SDR DALA2025071105224](https://openairdocs.org/sdr/DALA2025071105224.md): Pan · cracked · Jul 11, 2025 · N927AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A FORWARD LOWER CARGO DOOR INSPECTION PER WC. 5231-2005, THREE (3 QTY) CRACKS WERE FOUND AFFECTING THE FWD CARGO DOOR INNER & OUTER PANS AT THE AFT EDGE BETWEEN STOPS 1 & 2. ADDITIONALLY, AFTER REMOVAL OF THE
- [SDR DALA2025070805068](https://openairdocs.org/sdr/DALA2025070805068.md): Not Reported · not reported · Jun 30, 2025 · N927AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9572 DTA ER/A 626436-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 30-JUN-25. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. CORRECTIVE ACTION: C/W ER/A 00-626436. (1061415)
- [SDR DALA2025070104875](https://openairdocs.org/sdr/DALA2025070104875.md): Hinge Fitting · corroded · Jun 30, 2025 · N927AT · Boeing 717200 · Leading Edge Devices
  > SHIP 9572 DURING HCK AT QRO, CORROSION WAS NOTED ON THE LH INBD T/R FWD FLAP HINGE FITTING, XW 251. CORRECTIVE ACTION: ER/A REVISION REQUIRED TO INCORPORATE DTE IS REQUIRED WITHIN 24 MONTHS FROM 24JUN2025. IF ER/A REVISION IS NOT ACCOMPLISHED BY 23JUN2027, REM
- [SDR DALA2025063004851](https://openairdocs.org/sdr/DALA2025063004851.md): Skin · corroded · Jun 26, 2025 · N927AT · Boeing 717200 · Wing, Plate/Skin
  > SHIP 9572 CORROSION ON WING UPPER TRAILING EDGE SKIN APROX. BTW XRS=353 - XRS=383 AT LH WING. CORRECTIVE ACTION: CORROSION LEVEL 2. AREA ON WING UPPER TRAILING EDGE SKIN APROX. BTW XRS=353 - XRS=383 AT LH WING WAS REPAIRED PER ERA 626626-14 REV ORIGINAL (10478
- [SDR DALA2025062604789](https://openairdocs.org/sdr/DALA2025062604789.md): Cargo Track · corroded · Jun 25, 2025 · N927AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 9572 CORROSION OUT LIMITS,IN REF TO NRC 00250:CORROSION ON TIE TRACKS THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LH STA Y=896- 1022. CORRECTIVE ACTION: DAMAGED AREA WERE AJUSTED AND DRILLED PER DAL DWG S2922357 REV. - AND REPLACED PER B717-200 SRM 51-41-0
- [SDR DALA2025062604788](https://openairdocs.org/sdr/DALA2025062604788.md): Tab · delaminated · Jun 25, 2025 · N927AT · Boeing 717200 · Elevator, Spar/Rib
  > SHIP 9572 DELAMINATED CONTROL TAB OF RH ELEVATOR. CORRECTIVE ACTION: CONTROL TAB OF RH ELEVATOR WAS REPAIRED PER PRI 626667-14 REV. 2. AND ER/A 626667-14 REV ORIGINAL. (1044468)
- [SDR DALA2025062504752](https://openairdocs.org/sdr/DALA2025062504752.md): None · none · Jun 17, 2025 · N927AT · Boeing 717200 · Standard Practices/Structures
  > DTA ER/A 626583-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. CORRECTIVE ACTION: C.W ERA 626583.
- [SDR DALA2025061704574](https://openairdocs.org/sdr/DALA2025061704574.md): Beam · cracked · Jun 17, 2025 · N927AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK BEYONDS STOP DRILL ON BEAM NBR 1 AFT EDGE OF PASSENGER ENTRANCE DOOR. STOP DRILL ON BEAM NBR 1 AFT EDGE OF PASSENGER ENTRANCE DOOR WAS PERFORMED AND NOT ADDITIONAL ACTIONS WERE NECESARY BECAUSE AREA WAS FOUND REPAIRED, AND THE STOP DRILL PERFORMED IS W
- [SDR DALA2025061604510](https://openairdocs.org/sdr/DALA2025061604510.md): Skin · cracked · Jun 15, 2025 · N927AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9572, CRACK ON EXTERNAL FUSELAGE SKIN STA 1037 AND 1152 BTW LONG 13-RH-14RH. CORRECTIVE ACTION: TRIMMED SKIN, DOUBLER TO REMOVE CRACKS, AND PREFORMED HFEC PROCEDURE. FABRICATED SKIN FILLERS, SHIMS, AND DOUBLERS. INSTALLED REPAIR PARTS PER ER/A 626434-
- [SDR DALA2025061104459](https://openairdocs.org/sdr/DALA2025061104459.md): Seat Track · corroded · Jun 11, 2025 · N927AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9572, CORROSION WAS FOUND OUT LIMITS ON SEAT TRACKS STA Y=906-1015 X=-56 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACKS STA Y=906-1015 X=-56 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 1
- [SDR DALA2025061104456](https://openairdocs.org/sdr/DALA2025061104456.md): Seat Track · corroded · Jun 9, 2025 · N927AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9572, CORROSION ON RH OUTB SEAT TRACK (X-56) ON STA Y465 TO STA 484 AT PAX CABIN. WITH AN ORIGINAL THICKNES; ON CROWN= 0.115"; BOTTOM= 0.100"; AND MINIMUM REMAINING THICKNESS ON CROWN= 0.080" BOTTOM= 0.055. CORRECTIVE ACTION: RH OUTB SEAT TRACK (X-56)
- [SDR DALA2025061104463](https://openairdocs.org/sdr/DALA2025061104463.md): Skin · cracked · Jun 5, 2025 · N927AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9572, DURING HCK AT QRO, WHILE PERFORMING A LOWER FUSELAGE INCLUDING RADOME AND LOWER WING FILLETS INSPECTION PER WC 0593-2009, ONE DENT WITH TWO CRACKS WAS FOUND AFFECTING THE FUSELAGE SKIN AT STA 69.55 AND L-20R. CORRECTIVE ACTION: THIS ER/A AUTHORI
- [SDR DALA2025060704352](https://openairdocs.org/sdr/DALA2025060704352.md): Floor Support · corroded · Jun 2, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9572, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT (2EA) FROM STA Y=160 TO 200 X=7 AND X= - 7. ALSO, CORROSION ON FLOOR SUPPORT STA Y=145 TO 147 X= -29, STA 148 X= - 32 TO - 44. CORECTIVE ACTION: FLOOR SUPPORT (2EA) FROM STA Y= 160 TO 200 X=7 AND X=
- [SDR DALA2025060704350](https://openairdocs.org/sdr/DALA2025060704350.md): Seat Track · corroded · Jun 2, 2025 · N927AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 9572, CORROSION ON RH MID SEAT TRACK (X=-44) ON STA Y= 200-218 AT PAX CABIN WITH AN ORIGINAL THICKNESS ON CROWN=0.115IN BOTTOM= 0.100IN AND MINIMUM REMAINING THICKNESS ON CROWN= 0.079IN BOTTOM= 0.052IN THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53
- [SDR DALA2025060604339](https://openairdocs.org/sdr/DALA2025060604339.md): Membrane · corroded · May 30, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 CORROSION OUT OF LIMIT ON MEMBRANE, STA Y 160 TO 197 BTW X=44 TO X= 54; STA Y 200 BTW X= 52 & X=54 AT FLOOR STRUCTURE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-02 (0995815)
- [SDR DALA2025060604338](https://openairdocs.org/sdr/DALA2025060604338.md): Cusp Web · cracked · May 30, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 INITIAL INSPECTION: CRACK ON CUSP WEB STA Y=657 X=57 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4 (0995798)
- [SDR DALA2025060604334](https://openairdocs.org/sdr/DALA2025060604334.md): Web · corroded · May 29, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 IN REF NRC 00391 AFTER REMOVAL SEAT TRACK, CORROSION WAS FOUND ON DIAPHRAGM STA Y=200 TO 220 APROX X:-44 AT CABIN PAX. CORRECTIVE ACTION: REPAIRED PER PER B717 -200 SRM 51-70-10-2R PROCEDURE 1, REPAIR 1. (0993688)
- [SDR DALA2025060604333](https://openairdocs.org/sdr/DALA2025060604333.md): Web · cracked · May 28, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 INITIAL INSPECTION:CRACK ON MEMBRANE STA Y=258 X=-44 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4. (0990756)
- [SDR DALA2025060604332](https://openairdocs.org/sdr/DALA2025060604332.md): Floor Support · corroded · May 28, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 CORROSION OUT LIMITS, IN REF TO NRC 00467: CORROSION ON FLOOR SUPPORT FROM STA 1022 TO Y=1059 X=44, AT AFT FLOOR STRUCTURE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-01-0G. (0990577)
- [SDR DALA2025060604330](https://openairdocs.org/sdr/DALA2025060604330.md): Web · cracked · May 27, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 CRACK ON MEMBRANE STA Y=813 X=45 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4. (0990285)
- [SDR DALA2025060604325](https://openairdocs.org/sdr/DALA2025060604325.md): Cusp Web · cracked · May 26, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 CRACK ON MEMBRANE STA Y=715 X=44 AT LH PASSENGER CABIN (CPAX). REPAIRED PER B717-200 SRM 53-00-55-2R-4 (09881240988124)
- [SDR DALA2025060604323](https://openairdocs.org/sdr/DALA2025060604323.md): Floor Support · corroded · May 26, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 DUE TO CORROSION REMOVAL ON FLOOR SUPPORT STA Y=200, X=10, WAS MEASURE WITH ORIGINAL THICKNESS: 0.070IN MINIMUM REMAINING THICKNESS 0.042 IN THEREFORE IT IS AREA OUT LIMITS. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-02 (0986603)
- [SDR DALA2025052704030](https://openairdocs.org/sdr/DALA2025052704030.md): Web · cracked · May 22, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 CRACK ON MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00 -55-2R PROCEDURE 4 REP.4. (0980496)
- [SDR DALA2025052704023](https://openairdocs.org/sdr/DALA2025052704023.md): Web · cracked · May 20, 2025 · N927AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9572 INITIAL INSPECTION:CRACK ON MEMBRANE STA Y =692 X=-44 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55. (0976468)
- [SDR DALA2025052203939](https://openairdocs.org/sdr/DALA2025052203939.md): Torque Tube · corroded · May 20, 2025 · N927AT · Boeing 717200 · Rudder Control System
  > SHIP 9572 ON REF AMDS 2027-2004 CORROSION ON SPLINE AND BORE OF RUDDER DRIVE TORQUE TUBE P/N 5912802-13, ALSO CORROSION ON WASHER LOWER BRG P/N 2913035-1 OF RUDDER CONTROL AFT FUSELAGE // EMPENNAGE. CORRECTIVE ACTION: RUDDER TORQUE TUBE WAS REPLACED BY SERVICE
- [SDR DALA2025050503410](https://openairdocs.org/sdr/DALA2025050503410.md): Spar · cracked · May 2, 2025 · N927AT · Boeing 717200 · Wing Spar
  > -AD- LH WING SPAR CRACK. LEFT WING SPAR REPARED PER ERA 621363-14AD REV ORG. FINAL ERA REV ORG HAS BEEN RECEIVED AND MATCHES PRI REV. 21. ASSOCIATED ER/A 14-621363 ADDED FOR AC 9572. (LP #6377060)
- [SDR DALA2025051403731](https://openairdocs.org/sdr/DALA2025051403731.md): None · none · May 1, 2025 · N927AT · Boeing 717200 · Standard Practices/Structures
  > -AD- PER ERA 621363-14 AD REV 0 STAGE VIII STEP 9, PRIOR TO ACCESS CLOSE-UP, PERFORM A GENERAL VISUAL INSPECTION OF THE AREA FOR CLEANLINESS, AS DEFINED IN TOPP 40-10-10. A) ENSURE ALL TOOLS, RAGS, SHAVINGS, DEBRIS, ETC. HAVE BEEN REMOVED. B) PAY PARTICULAR AT
- [SDR DALA2025051403725](https://openairdocs.org/sdr/DALA2025051403725.md): None · none · May 1, 2025 · N927AT · Boeing 717200 · Standard Practices/Structures
  > -AD- PER ERA 621441-14AD REV ORIG STEP 25, PERFORM GVI OF RH WING AREA BEFORE ACCESS CLOSE UP. STEP 25 OF ERA 621441-14AD REV O WAS COMPLIED WITH ON NRC 11 DURING OK TO CLOSE FUEL PANELS. GVI OF RH WING ACCESS AREA WAS COMPLIED WITH ON NON ROUTINE 11, DURING O
- [SDR DALA2025051403724](https://openairdocs.org/sdr/DALA2025051403724.md): Spar · cracked · May 1, 2025 · N927AT · Boeing 717200 · Wing Spar
  > -AD- DUE TO CRACK INDICATION, COMPLY WITH RH WING SPAR REPAIR PER ERA 621441-14AD REV ORIG. SPAR REPAIRED PER PRI 621441-14AD REVS 0 THRU 8. COMPARED PRI 621441-14 REVS 0 THRU 8 WITH ERA 621441-14 REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 621441-14 REV ORIG
- [SDR DALA2025051403723](https://openairdocs.org/sdr/DALA2025051403723.md): Hinge Fitting · worn · May 1, 2025 · N927AT · Boeing 717200 · Trailing Edge Flaps
  > -AD- LH WING, OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. COMPLIED WITH ERA 623200-14AD REV ORG. REPAIRED LH WING OUBOARD FLAP HINGE POINT AC SIDE PER ERA 623200-14AD REV ORIG. REWORKED AND BUSHED LH WING OUTBOARD FLAP HINGE POINT, INBOARD FITTING PER
- [SDR DALA2025043003312](https://openairdocs.org/sdr/DALA2025043003312.md): Hinge Fitting · worn · Apr 25, 2025 · N927AT · Boeing 717200 · Trailing Edge Flaps
  > LH WING OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. MACHINED IB AND OB LUGS TO REMOVE DAMAGE. OB LUG BORE FINAL SIZE IS.533. IB LUG FINAL SIZE IS.594. INNER FACE OF IB LUG SPOTFACED.880 DIAMETER WITH.060 RADIUS TO A DEPTH OF.076. REMAINING LUG THI
- [SDR DALA2024100209620](https://openairdocs.org/sdr/DALA2024100209620.md): Spar Cap · cracked · Sep 30, 2024 · N927AT · Boeing 717200 · Wing Spar
  > CRACK IN LH WING REAR SPAR LOWER CAP RADIUS. REFERENCE AA NUMBER FC 5720-01103. CRACK LOCATION IS XRS 156.950. SUMMARY NRC 010-0001:5720-01103-01A/001 00001 COMPLIED WITH PRI 621210-14 REV 0 AND REV 1 AND ENSURED IT MATCHES ERA 621210-14 REV ORIG SECTION 1 STE
- [SDR DALA2024041204357](https://openairdocs.org/sdr/DALA2024041204357.md): Door Frame · corroded · Apr 10, 2024 · N927AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00091: CORROSION LEVEL 2. AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7, 51-41-05-0G, AND 51-41-02-0G. (LP #0287200)
- [SDR DALA2022123008503](https://openairdocs.org/sdr/DALA2022123008503.md): Battery Pack · inoperative · Dec 29, 2022 · N927AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS ON THE GALLEY OVERHEAD, AT SEATS 1-14, AND AT SEATS 24-29 ARE INOPERATIVE. MAINTENANCE FOUND BAD BATTERY PACKS AND BATTERY RACKS AT B5- 259, B5-227, AND B5-120. ALL WERE REPLACED PER AMM 33-51. OPERATIONAL CHECKS WERE GOOD. OK FOR SERVICE

Next page: https://openairdocs.org/aircraft/N927AT/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 = 'N927AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N927AT/reports

---
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.