# Service difficulty reports: N974AT

A list on [N974AT](https://openairdocs.org/aircraft/N974AT.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 · 168 reports

- [SDR DALA2026101405657](https://openairdocs.org/sdr/DALA2026101405657.md): Display · no discrepancy · Oct 13, 2026 · N974AT · Boeing 717200 · Central Display
  > ABORTED TAKE OFF, APPROX 60KTS DUE TO DISPLAY AND STAB TRIM FAULT ANNUNCIATIONS. DISPLAY BLANKING WAS MOMENTARY, NO FAULTS OR ABNORMALITIES FOUND. OK TO CONTINUE IN SERVICE. (9030520) (AIRCRAFT GROUNDED).
- [SDR DALA2026033002084](https://openairdocs.org/sdr/DALA2026033002084.md): Lug · damaged · Mar 26, 2026 · N974AT · Boeing 717200 · Trailing Edge Flaps
  > ER/A 617866-14, RT WING T/E FLAP, FWD IDLER HINGE FITTING NR 3, INBD LUG DAMAGED HOLE, ASSOCIATED ER/A 14-617866. (1513485)
- [SDR DALA2026021801127](https://openairdocs.org/sdr/DALA2026021801127.md): Autothrottle Sys · faulted · Feb 10, 2026 · N974AT · Boeing 717200 · Auto Throttle System
  > ATO, LOW SPEED ABORTED TAKEOFF DUE TO AUTOTHROTTLES FAILED TO ENGAGE. MAINTENANCE PERFORMED FCC 1 & 2 AUTOTHROTTLE RTS. (1445239).
- [SDR DALA2026011600377](https://openairdocs.org/sdr/DALA2026011600377.md): Skin · cracked · Jan 14, 2026 · N974AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > REFERENCE ER/A 617297-14 - FUSELAGE / SKIN / STA 1037, L-14L / CRACKS. CORRECTIVE ACTION: REPAIRED PER ER/A 14-617297. (1401870)
- [SDR DALA2025110708137](https://openairdocs.org/sdr/DALA2025110708137.md): Light · inoperative · Oct 31, 2025 · N974AT · Boeing 717200 · Emergency Lighting
  > RT OVERWING EMERGENCY EXIT LIGHT NOT OPERATIONAL. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT PER B717 AMM 33-51. (8143300)
- [SDR DALA2025072405584](https://openairdocs.org/sdr/DALA2025072405584.md): Cylinder · faulted · Jul 22, 2025 · N974AT · Boeing 717200 · Leading Edge Slat Actuator
  > SHIP 9536-FCNT-THE CREW RECEIVED A SLAT DISAGREE MESSAGE ON APPROACH WITH ASSOCIATED ROLL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT INBOARD SLAT DRIVE CYLINDER.(7345922)
- [SDR DALA2025040802708](https://openairdocs.org/sdr/DALA2025040802708.md): Battery Pack · no test · Apr 7, 2025 · N974AT · Boeing 717200 · Emergency Lighting
  > THE R1 AND L1 SMALL EMERGENCY EXIT SIGNS ARE INOPERATIVE (LOWER). AFTER TROUBLESHOOTING MAINTENANCE FOUND THAT THE BATTERY PACK (B5-118) INSIDE THE OVERHEAD BIN ABOVE 2D WAS NOT CONNECTED. THE PLUG WAS RECONNECTED AND THE OPERATIONAL CHECK WAS GOOD IAW B717 AM
- [SDR DALA2025011500348](https://openairdocs.org/sdr/DALA2025011500348.md): Battery Pack · inoperative · Jan 14, 2025 · N974AT · Boeing 717200 · Emergency Lighting
  > MAINTENANCE FOUND ROW 19 LT & RT EMERGENCY EXIT SIGN LIGHTS WERE INOPERATIVE. THEY REPLACED THE EMERGENCY LIGHT BATTERY PACK LOC B5-121 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6776224)
- [SDR DALA2025021201088](https://openairdocs.org/sdr/DALA2025021201088.md): Fuel Sys · leaking · Jan 9, 2025 · N974AT · Boeing 717200 · Fuel Storage
  > FUEL LEAK FOUND DURING INSP OF LH WING AFT LOWER SKIN DOUBLER AT XRS 164. ACCOMPLISHED PRI 623309-14 REV O THROUGH 3 REMAINING FUEL SEE POST PRI'S WITHIN B717 AMM 28-11-00 GROUP A ALLOWANCE. FORWARD TO MON PER ER/A 623309-14 AD REV O REPETITIVE INSP REQ DAILY
- [SDR DALA2024123012069](https://openairdocs.org/sdr/DALA2024123012069.md): Wire · overtemp · Dec 25, 2024 · N974AT · Boeing 717200 · Electrical Power System Wiring
  > SHIP 9536 -DIV/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO DTW AND DECLARED AN EMERGENCY WITH ATC DUE TO BURNING SMELL IN THE CABIN AROUND ROW 17. AN OVERWEIGHT LANDING RESULTED BUT WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE PED POWER OUTLE
- [SDR DALA2024120911542](https://openairdocs.org/sdr/DALA2024120911542.md): Control Unit · faulted · Dec 5, 2024 · N974AT · Boeing 717200 · AC Generator-Alternator
  > SHIP 9536 -MISC/DE- FLIGHT CREW NOTED THE "LEFT GENERATOR OFF" MESSAGE WITH A POSSIBLE ELECTRICAL SMELL IN THE CABIN. THE PILOT DECLARED AN EMERGENCY WITH ATC AND WAS MET BY ARFF AFTER A NORMAL SAFE LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE EPCU, L
- [SDR DALA2024122411974](https://openairdocs.org/sdr/DALA2024122411974.md): Pump · failed · Dec 3, 2024 · N974AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > SHIP 9536 -MISC/DE- DECLARED AN EMERGENCY DUE TO LEFT HYDRAULIC PUMP FAIL MESSAGE AND LEFT GENERATOR OFF MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND THE LEFT IDG. ALL RETURN TO SERVICE TEST PASSED. (LP #0690281)
- [SDR DALA2024081408114](https://openairdocs.org/sdr/DALA2024081408114.md): Cover · detached · Aug 13, 2024 · N974AT · Boeing 717200 · Emergency Lighting
  > MISSING FWD ''EXIT'' PLACARD/SIGN. MAINTENANCE RE-INSTALLED EXIT SIGN COVER REF B717 AMM 33-51. (LP #6186440)
- [SDR DALA2024070306745](https://openairdocs.org/sdr/DALA2024070306745.md): Skin · cracked · Jul 2, 2024 · N974AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > WHILE IN ATL FOR SCHEDULED MAINTENANCE AND DURING ACCOMPLISHMENT OF WORKCARD 5530-01048-02, MAINTENANCE REPORTED CRACK INDICATIONS AT TWO EXISTING FASTENER LOCATIONS IN THE RH FRONT SPAR CAP LAYER FORWARD FLANGE. SUBJECT FASTENERS ARE IDENTIFIED AS HOLE 4 AND
- [SDR DALA2024062406340](https://openairdocs.org/sdr/DALA2024062406340.md): Hinge Fitting · damaged · Jun 21, 2024 · N974AT · Boeing 717200 · Trailing Edge Flaps
  > ELONGATED HOLE AND DAMAGED BOLT WAS FOUND AT RH FLAP HINGE #3. SUMMARY OF NRC 00776: ELONGATED HOLE AND DAMAGED BOLT AT RH FLAP HINGE #3 WAS REPAIRED PER PRI 617866-14 REV 1 & ER/A PRI 617866-14 REV ORIG. DTE REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM MAY 18
- [SDR DALA2024062006271](https://openairdocs.org/sdr/DALA2024062006271.md): Beam · damaged · Jun 20, 2024 · N974AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK BEYOND STOP DRILL ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00174: DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7 PAR. 6 FIGURE 2
- [SDR DALA2024061906215](https://openairdocs.org/sdr/DALA2024061906215.md): Window Frame · cracked · Jun 18, 2024 · N974AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON RETAINER AND FRAME AT LH SLIDING WINDOW A COCKPIT. SUMMARY OF NRC 00182: FRAME AT LH SLIDING WINDOW A COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1 AND RETAINER LH SLIDING WINDOW COCKPIT WAS REPLACED PER B717-200 SRM 51-41-02
- [SDR DALA2024061806169](https://openairdocs.org/sdr/DALA2024061806169.md): Skin · damaged · Jun 17, 2024 · N974AT · Boeing 717200 · Horizontal Stabilizer, Plate/Skin
  > CORROSION WAS FOUND ON VERTICAL AND HORIZONTAL UPPER HOLES LH #10, 11, AND LOWER HOLE #29, LOWER HOLES RH #29 AND 39 AT CENTER BOX OF HORIZONTAL STABILIZER. UPPER HOLES LH #10, 11, AND LOWER HOLE #29, LOWER HOLES RH #29 AND 39 AT CENTER BOX OF HORIZONTAL STABI
- [SDR DALA2024060505796](https://openairdocs.org/sdr/DALA2024060505796.md): Pan · cracked · Jun 4, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN BTW 5 AND STOP FITTINGS NBR 5 OF AFT CARGO DOOR. SUMMARY OF NRC 00781: INNER PAN ON BEAM 5 AT AFT CARGO DOOR WAS REPAIRED PER ERA 617933-14. REV ORIGINAL AND PRI 617933-14 REV 2 ASSOCIATED ER/A 14-617933 ADDED FOR AC 9536. (LP #0376682)
- [SDR DALA2024060505795](https://openairdocs.org/sdr/DALA2024060505795.md): Lug · corroded · Jun 4, 2024 · N974AT · Boeing 717200 · Elevator Structure
  > CORROSION ON FITTING LUGS OF ELEVATOR HINGE EYEBOLT STA XHS=50 AROUND BUSHINGS, WAS FOUND ON LH AND RH SIDE. SUMMARY OF NRC 00775: ELEVATOR HINGE EYEBOLT STA XHS=50 ON LH AND RH SIDE WERE REPAIRED PER ER/A 618032-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND
- [SDR DALA2024052205414](https://openairdocs.org/sdr/DALA2024052205414.md): Skin · dented · May 22, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN STA 205, 1" ABOVE LONGERON 17L WITH DIMENSIONS AS A FOLLOW D (WIDTH)=1.300, X (DEPTH)=0.110, D/X=11.81 IS OUT OF LIMITS PER B717 SRM 53-01-01-1A, PROCEDURE 3 ALLOWABLE DAMAGE 3 PAR 4. C CONDITION 1B. SUMMARY OF NRC 00388: PREVIOUS REPAIR
- [SDR DALA2024052205413](https://openairdocs.org/sdr/DALA2024052205413.md): Door Frame · damaged · May 21, 2024 · N974AT · Boeing 717200 · Fuselage Main, Structure
  > ELONGATED HOLE ON DOOR JAMB STA Y=427 AND LONGERON 25R. SUMMARY OF NRC 00173: DOOR JAMB STA Y=427 AND LONGERON 25R WAS REPAIRED PER PRI 617550-14 REV 3 AND ER/A 617550-14 REV 0, SECTION I: REPAIR. ASSOCIATED ER/A 14-617550 ADDED FOR AC 9536. (LP #0353594)
- [SDR DALA2024052105379](https://openairdocs.org/sdr/DALA2024052105379.md): Skin · cracked · May 20, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R. SUMMARY OF NRC 00164: FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECTIONS W
- [SDR DALA2024052105378](https://openairdocs.org/sdr/DALA2024052105378.md): Skin · cracked · May 20, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R. SUMMARY OF NRC 00165: FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECT
- [SDR DALA2024052005344](https://openairdocs.org/sdr/DALA2024052005344.md): Floorbeam · damaged · May 17, 2024 · N974AT · Boeing 717200 · Fuselage Main, Floor Beam
  > -AD- REWORK ON WEB BELOW FLOOR BEAM DOES NOT MEET WITH EDGE DISTANCE REQUIREMENTS AT STA 696 X=56 LH. SUMMARY OF NRC 00439: WEB BELOW FLOOR BEAM ON STA 696 X=56 LH WAS REPAIRED PER ER/A 617901-14AD REV ORIGINAL, SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS
- [SDR DALA2024052005343](https://openairdocs.org/sdr/DALA2024052005343.md): Frame · cracked · May 17, 2024 · N974AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON MAIN FRAME STA 1037 LONGERON 17L AND LONGERON 17R AT PAX CABIN. SUMMARY OF NRC 00459: MAIN FRAME STA 1037 LONGERON 17L WAS REPAIRED PER ER/A 617631-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND MAIN FRAME STA 1037 LONGERON 17R WAS REPAIRED PER B717
- [SDR DALA2024052005341](https://openairdocs.org/sdr/DALA2024052005341.md): Pan · cracked · May 17, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND ON PAN IN BEAM #2 AT FWD CARGO COMPARTMENT DOOR (FWD EDGE). SUMMARY OF NRC 00610: INNER PAN IN BEAM #2 AT FWD CARGO COMPARTMENT DOOR (FWD EDGE) WAS REPAIRED PER ER/A 617689-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617689-14 REV 2. AS
- [SDR DALA2024051705297](https://openairdocs.org/sdr/DALA2024051705297.md): Door Frame · corroded · May 17, 2024 · N974AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB BTW L24 AND L24 LOWER AREA AFT CARGO. SUMMARY OF NRC 00205: CORROSION LEVEL 2. DOOR JAMB AND REPAIR DOUBLERS (ANGLES) BTW L24 AND L24 LOWER AREA AFT CARGO WERE REPLACED PER B717 SRM 53-20-15-2R REP 7.
- [SDR DALA2024051705295](https://openairdocs.org/sdr/DALA2024051705295.md): Cargo Track · corroded · May 16, 2024 · N974AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS FOUND ON TIE TRACK LOCATED BETWEEN Y=1002 AND Y=1022 RH SIDE, CORROSION LEVEL 2. TIE TRACK LOCATED BETWEEN Y=1002 AND Y=1022 RH SIDE WAS REPLACED PER B717 SRM 51-41-01-0G. (LP #0345653)
- [SDR DALA2024051605251](https://openairdocs.org/sdr/DALA2024051605251.md): Door Frame · corroded · May 16, 2024 · N974AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB BTW STA Y=370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT. SUMMARY OF NRC 00172: CORROSION LEVEL 2. DOOR JAMB BTW STA Y =370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R-REP 6, PAR 6. (L
- [SDR DALA2024051605250](https://openairdocs.org/sdr/DALA2024051605250.md): Skin · cracked · May 16, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L. SUMMARY OF NRC 00162: FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L WAS REPAIRED PER ER/A 617297-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617297 ADDED FOR AC 9536. (LP #0
- [SDR DALA2024051605249](https://openairdocs.org/sdr/DALA2024051605249.md): Intercostal · cracked · May 15, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL X=0 BTW STA Y=832 AND Y=851 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00509: INTERCOSTAL X=0 BTW STA Y=832 AND Y=851 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 PAR. 4. (LP #0344606)
- [SDR DALA2024051605254](https://openairdocs.org/sdr/DALA2024051605254.md): Pin · out of position · May 15, 2024 · N974AT · Boeing 717200 · Aerodynamic Fairings
  > INCORRECT HRS POSITION OF TAILCONE RELEASE MECHANISM CAM PIN STA Y=1225 CANT AT AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00817: TAILCONE RELEASE MEC
- [SDR DALA2024051405174](https://openairdocs.org/sdr/DALA2024051405174.md): Longeron Splice · corroded · May 13, 2024 · N974AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LOWER SPLICE (BELOW CUSP WEB) BTW STA Y=908 AND Y=889 APPROX LONG 18RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00514: CORROSION LEVEL 2. SPLICE (BELOW CUSP WEB) BTW STA Y=908 AND Y=889 APPROX LONG 18RH AT AFT CARGO COMPARTMENT WAS REPLACED PER DW
- [SDR DALA2024051405173](https://openairdocs.org/sdr/DALA2024051405173.md): Skin · cracked · May 12, 2024 · N974AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > CRACK WAS FOUND OVER THE VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP. SUMMARY OF NRC 00469: CRACK ON VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP WAS REPAIRED (WELDED) PER ER/A 382101-14MA REV H. SECTION I: PERMANENT REPAIR. ASSOCIAT
- [SDR DALA2024050905043](https://openairdocs.org/sdr/DALA2024050905043.md): Lug · cracked · May 8, 2024 · N974AT · Boeing 717200 · Fuselage Main, Attach Fittings
  > CRACK ON OVERWING FRAME LUG STA Y=715.000, X=-54 RH AT PASSENGER CABIN FLOOR. OVERWING FRAME STA Y=715.000, X=-54 RH AT PASSENGER CABIN FLOOR WAS REPLACED PER AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9536.
- [SDR DALA2024050805024](https://openairdocs.org/sdr/DALA2024050805024.md): Cusp Web · corroded · May 8, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SURFACE OF CUSP WEB AT STA Y 940 AND -X56 IN PAX CABIN. SUMMARY OF NRC 00594: CORROSION LEVEL 2. CORROSION ON CUSP WEB AT STA Y 940 AND -X56 IN PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 209 CONFIGURATION-701
- [SDR DALA2024050805020](https://openairdocs.org/sdr/DALA2024050805020.md): Cusp Web · corroded · May 7, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB LOWER AND UPPER SIDE IN SECTION STA Y: 832 TO 845 X: 56, PAX CABIN. SUMMARY OF NRC 00784: CORROSION LEVEL 2. CORROSION ON CUSP WEB STA Y: 832 TO 845 X: 56, PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4, FIGURE 215. (LP #0331554
- [SDR DALA2024050805019](https://openairdocs.org/sdr/DALA2024050805019.md): Frame · cracked · May 7, 2024 · N974AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME CANTED KEEL BEAM AREA BTW STA Y 715, 674, AND 696 - L24R/26R AT LOWER FUSELAGE. SUMMARY OF NRC 00494: FRAMES CANTED KEEL BEAM AREA BTW STA Y 715, 674, AND 696 - L24R/26R AT LOWER FUSELAGE WERE REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR
- [SDR DALA2024050704973](https://openairdocs.org/sdr/DALA2024050704973.md): Cusp Web · corroded · May 6, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB LOWER AND UPPER SIDE STA Y=526 AND Y=571 APPROX X=58 LH SIDE AT PAX CABIN (CPAX). SUMMARY OF NRC 00728: CORROSION LEVEL 2. CUSP WEB STA Y=526 AND X=58 WAS MEASURED ON LIGHTENING HOLE AND MATERIAL REMOVAL IS 0.100IN THERFORE IS WITHIN LIMI
- [SDR DALA2024050704972](https://openairdocs.org/sdr/DALA2024050704972.md): Cusp Web · cracked · May 6, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LOWER SURFACE OD CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT PAX CABIN. SUMMARY OF NRC 00591: CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329495)
- [SDR DALA2024050704971](https://openairdocs.org/sdr/DALA2024050704971.md): Cusp Web · cracked · May 6, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > TWO CRACKS WERE FOUND ON RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X=45 TO -X=60 IN PAX CABIN. SUMMARY OF NRC 00534: RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X= 45 TO -X=60 IN CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329432)
- [SDR DALA2024050604956](https://openairdocs.org/sdr/DALA2024050604956.md): Cusp Web · cracked · May 3, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB STA Y=225 AND X=56 AT PAX CABIN. SUMMARY OF NRC 00567: CUSP WEB STA Y=225 AND X=56 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-PROCEDURE 4 FIG 216. (LP #0325208)
- [SDR DALA2024050604955](https://openairdocs.org/sdr/DALA2024050604955.md): Cusp Web · cracked · May 3, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB STA Y=657 AND Y=715 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00599: CUSP WEB STA Y=657 AND Y=715 LH SIDE AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0325055)
- [SDR DALA2024050304922](https://openairdocs.org/sdr/DALA2024050304922.md): Floorbeam · cracked · May 2, 2024 · N974AT · Boeing 717200 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM STA Y=737 BELOW X=54 RH/LH AT PASSENGER FLOOR CABIN. SUMMARY OF NRC 00438: FLOOR BEAM STA Y=737 BELOW X=54 RH/LH AT PASSENGER FLOOR CABIN WERE REPLACED PER B717 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #0323733)
- [SDR DALA2024050304921](https://openairdocs.org/sdr/DALA2024050304921.md): Floor Support · corroded · May 2, 2024 · N974AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=150-200 X=7 RH, STA Y=200 X=7LH TO 7RH, AND STA Y=160 X=5LH TO 5RH AT PASSENGER CABIN (W1). SUMMARY OF NRC 00700: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=150-200 X=7 RH, STA Y=200 X=7LH TO 7RH, AND STA Y=160 X=5LH TO 5RH AT PASS
- [SDR DALA2024050104838](https://openairdocs.org/sdr/DALA2024050104838.md): Cusp Web · corroded · Apr 30, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION CUSP WEB PREVIOUS REPAIR LOWER SIDE STA Y=471 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00598: CORROSION LEVEL 2. PREVIOUS REPAIR PART (RING DOUBLER) WAS REPLACED PER B717 SRM 53-00-55-2R-4 REPAIR 4, PAR. 5, FIGURE 216 AND 51-41-02-0G. (LP #0320091)
- [SDR DALA2024043004793](https://openairdocs.org/sdr/DALA2024043004793.md): Angle · damaged · Apr 27, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CLIP STA Y=1072 AND X=-16 LONGERON PROJECTION 18RH AT AFT EMERGENCY EXIT DOOR JAMB AREA. SUMMARY OF NRC 00381: CORROSION LEVEL 2. CLIP (GUSSET) STA Y=1072 AND X=-16 LONGERON PROJECTION 18RH AT AFT EMERGENCY EXIT DOOR JAMB AREA WAS REPLACED PER B71
- [SDR DALA2024043004790](https://openairdocs.org/sdr/DALA2024043004790.md): Release Cable · corroded · Apr 26, 2024 · N974AT · Boeing 717200 · Aerodynamic Fairings
  > RUSTED CABLES AND ALL PINS ON TAILCONE RELEASE CABLE AND PULLEY MECHANISMS. ALSO BROKEN STRANDS OF CABLE AT 10 HRS POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00180: CAB
- [SDR DALA2022113007648](https://openairdocs.org/sdr/DALA2022113007648.md): Skin · delaminated · Nov 30, 2022 · N974AT · Boeing 717200 · Wing, Plate/Skin
  > RIGHT WING, UPPER SKIN OF INBOARD SPOILER IS DELAMINATED IN SEVERAL AREAS. REPLACED RIGHT INBOARD PANEL IAW AMM 27-60-01.

Next page: https://openairdocs.org/aircraft/N974AT/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 = 'N974AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N974AT/reports

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