# Service difficulty reports: N949AT

A list on [N949AT](https://openairdocs.org/aircraft/N949AT.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 · 238 reports

- [SDR DALA2026031001638](https://openairdocs.org/sdr/DALA2026031001638.md): Skin · damaged · Mar 4, 2026 · N949AT · Boeing 717200 · Wing, Plate/Skin
  > SHIP 9500 ELONGATED HOLE (1EA) AND TOOL MARKS (1EA) ON INNER/OUTER SKIN FROM FUEL ACCESS PANEL 620JB AT RH WING. CORRECTIVE ACTION: REPAIRED PER PRI 632126-14 (1479482)
- [SDR DALA2026031001637](https://openairdocs.org/sdr/DALA2026031001637.md): Doubler · cracked · Mar 4, 2026 · N949AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON INTERNAL PRODUCTION DOUBLER INSIDE OF AFT ACCESSORY COMPARMET IN LONGERON 3 RH,CANTED STA Y= 1178.225 APPROX. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-30-08-2R-9 PROCEDURE 9 REPAIR 9 (1478843)
- [SDR DALA2026030501523](https://openairdocs.org/sdr/DALA2026030501523.md): Longeron · cracked · Mar 4, 2026 · N949AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 2L, BS 1133 IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW SRM 53-00-05 -2R-2. (1478132)
- [SDR DALA2026030501521](https://openairdocs.org/sdr/DALA2026030501521.md): Fuel Tank · cracked · Mar 1, 2026 · N949AT · Boeing 717200 · Fuel Storage
  > CRACKED WEB, FUEL TANK, X=56 APROX BS 696 AT LH CENTRAL FUEL TANK.: WEB FUEL TANK X=56 APROX STA Y =696 AT LH CENTRAL FUEL TANK WAS REPAIRED PER ERA 631718-14AD (1474080)
- [SDR DALA2026030501520](https://openairdocs.org/sdr/DALA2026030501520.md): Frame · cracked · Mar 1, 2026 · N949AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME BS 1133, LONGERON 2 RT, AFT ACCESSORY COMPARTMENT. THE FRAME WAS REPAIRED IAW ERA 631717-14 REV. (1474071)
- [SDR DALA2026030201419](https://openairdocs.org/sdr/DALA2026030201419.md): Diaphragm · cracked · Feb 26, 2026 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9500 CRACKS ON DIAPHRAGM BTW STA Y=160 TO STA Y= 170 X=8 TO X=9 AT PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER B717- 200 SRM 53-00-00 (1468333)
- [SDR DALA2026030201418](https://openairdocs.org/sdr/DALA2026030201418.md): Skin · corroded · Feb 24, 2026 · N949AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN STA 737 X: -15 TO -30 APROX AT FUSELAGE. REPAIR INSTRUCTIONS AND PRI 631685-14 (1466288)
- [SDR DALA2026030201416](https://openairdocs.org/sdr/DALA2026030201416.md): Skin · cracked · Feb 24, 2026 · N949AT · Boeing 717200 · Rudder, Plate/Skin
  > SHIP 9500 BENT, ALSO CRACK ON RUDDER SKIN AT LH LOWER EDGE XR -5.000 CANT. CORRECTIVE ACTION: REPAIRED PER PRI 631766-14 (1466225)
- [SDR DALA2026022501336](https://openairdocs.org/sdr/DALA2026022501336.md): Cusp Web · cracked · Feb 23, 2026 · N949AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON RH CUSP WEB AT Y=940 AND Y= 665 X=-53 TO X=-56 ALSO Y=716 X= -44. DAMAGED AREA REPAIRED PER B717-200 SRM 53-00-55 (1464546)
- [SDR DALA2026022501335](https://openairdocs.org/sdr/DALA2026022501335.md): Seat Track · damaged · Feb 23, 2026 · N949AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AFTER THICKNESS MEASUREMENT WAS ACCOMPLISHED ON RH SEAT TRACK X= -22.0 (BTW Y=250 TO Y=260. DAMAGED AREA REPAIRED PER SRM 53-20-52 (1464489)
- [SDR DALA2026022501334](https://openairdocs.org/sdr/DALA2026022501334.md): Cusp Web · cracked · Feb 23, 2026 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9500 CORROSION ON RH CUSP WEB BTW Y=237 TO Y= 257, BTW Y= 450 TO Y= 455, BTW Y= 484 TO Y= 491, BTW Y= 794 TO Y= 802, BTW Y= 860 TO Y= 865 BTW Y=938 TO Y= 942. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B717 SRM 53-00-55 (1464374)
- [SDR DALA2026022501333](https://openairdocs.org/sdr/DALA2026022501333.md): Cusp Web · cracked · Feb 21, 2026 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB PREVIOUS REPAIR DOUBLER BTW STA 446 TO 456 X=-60 CABIN FLOOR STRUCTURE. DAMAGED AREA REPAIRED PER SRM 53-00-55 (1462080)
- [SDR DALA2026022501332](https://openairdocs.org/sdr/DALA2026022501332.md): Cusp Web · cracked · Feb 21, 2026 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION TYPE EXFOLATION AND CRACKED RH CUSP WEBS X=-56 BTW STA 234 TO 248. DAMAGED AREA REPAIRED PER SRM 53-00-55 (1462073)
- [SDR DALA2026022501331](https://openairdocs.org/sdr/DALA2026022501331.md): Seat Track · corroded · Feb 21, 2026 · N949AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BTW STA Y= 200 TO STA Y= 304 X= -22 APPROX CORROSION. DAMAGED AREA REPAIRED IAW SRM 51-70-10 (1460872)
- [SDR DALA2026021901202](https://openairdocs.org/sdr/DALA2026021901202.md): Web · cracked · Feb 19, 2026 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9500, CRACK ON WEB WAS FOUND FROM STA 465 TO STA 475, AFTER REMOVAL OF RT OUTB SEAT TRACK. CRACK ON WEB STA 465 TO STA 475 OF RH OUTB SEAT TRACK WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP 1457705)
- [SDR DALA2026021901199](https://openairdocs.org/sdr/DALA2026021901199.md): Cusp Web · cracked · Feb 15, 2026 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9500, CRACK LT ON CUSP WEB BS 852, BTW Y=655 TO Y=700 AT PAX CABIN. REPLACED IAW SRM 51-41-05-0G, AND SRM 51-41-02-0G PAR 4. (LP 1452693)
- [SDR DALA2026021901198](https://openairdocs.org/sdr/DALA2026021901198.md): Cusp Web · damaged · Feb 15, 2026 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFTER THICKNES MEASUREMENT ON LT CUSP WEB BTW BS 332 - 351, BS 446 - 465, BS 522 - 579, BS 813 - 832, BS 889 - 908, & BS 908 - 927. REWORKED AREAS ARE OUT OF LIMITS IAW SRM 53-00-55-1A, PARA 4A, FIG 101. REPAIRED IAW SRM 53-00-55-2R, PROCEDURE 4, & LT CUSP
- [SDR DALA2026021801120](https://openairdocs.org/sdr/DALA2026021801120.md): Longeron · cracked · Feb 13, 2026 · N949AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK, LONGERONS 5R, 6R, & 8R, BS 1022. REPAIRED IAW SRM 53-00-05-2R. (1449808).
- [SDR DALA2026021801115](https://openairdocs.org/sdr/DALA2026021801115.md): Skin · cracked · Feb 10, 2026 · N949AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE EXTERNAL SKIN, BS 1076, BTW LONGERONS 13-14R. REPAIRED IAW ER/A 631539-14 (1445437).
- [SDR DALA2026021801114](https://openairdocs.org/sdr/DALA2026021801114.md): Doubler · worn · Feb 10, 2026 · N949AT · Boeing 717200 · Fuselage Main, Structure
  > WORN PRODUCTION DOUBLER, RT SIDE ON FLIGHT ATTENDANT SEAT STOWAGE AREA, AFT CABIN PRESSURE BULKHEAD. REPAIRED IAW ER/A 14-631800. (1445027).
- [SDR DALA2026020900910](https://openairdocs.org/sdr/DALA2026020900910.md): Door Frame · punctured · Feb 8, 2026 · N949AT · Boeing 717200 · Fuselage Main, Structure
  > PUNCTURED BULKHEAD DOOR JAM AT LOWER SECTION AT Y= 1053, X= 7 APPROX AFT ACCESSORY BAY. REPAIRED IAW SRM 51-70-10. (1442140)
- [SDR DALA2026020900909](https://openairdocs.org/sdr/DALA2026020900909.md): Longeron · cracked · Feb 8, 2026 · N949AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERONS NR 5L & 6L AT Y= 1022. LONGERONS NR 5L & 6L INSIDE HAT SECTION IN THE PAX CABIN WERE REPAIRED IAW SRM 53-00-05. (1442139)
- [SDR DALA2026020200755](https://openairdocs.org/sdr/DALA2026020200755.md): Frame Angle · cracked · Jan 30, 2026 · N949AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME ANGLES (2 EACH) BS 1022 AND LONGERON 7 RT & LT SIDES AT PASSENGER CABIN. PERMANENT REPAIR IAW PRI 631537-14, REV 1, ERA 631536-14. (1426473)
- [SDR DALA2026020200754](https://openairdocs.org/sdr/DALA2026020200754.md): Frame · cracked · Jan 28, 2026 · N949AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME BS 1037 AND LONGERON 17LT AT PASSENGER CABIN. FRAME BTWN WAS REPAIRED IAW SRM 53-20-07-2R, PROCEDURE 4, REPAIR 4. (1424411)
- [SDR DALA2026012700603](https://openairdocs.org/sdr/DALA2026012700603.md): Frame · cracked · Jan 25, 2026 · N949AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME BTW BS 1037, L17R, THE FRAME WAS REPAIRED IAW SRM 53-20-07. (1419213)
- [SDR DALA2026012700600](https://openairdocs.org/sdr/DALA2026012700600.md): Skin · cracked · Jan 24, 2026 · N949AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED LEFT FUSELAGE EXTERNAL SKIN BS 1087 BTW LONGERONS 13 - 14L. REPAIRED IAW ER/A 631513-14 REV. (1416717)
- [SDR DALA2026012200492](https://openairdocs.org/sdr/DALA2026012200492.md): Skin · cracked · Jan 16, 2026 · N949AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK INTERNAL SKIN ON TOP FWD EDGE AT FWD ENTRY DOOR. INTERNAL SKIN ON TOP FWD EDGE AT FWD ENTRY DOOR WAS REPAIRED PER B717-200 S.R.M. 52-10-02 (1404734)
- [SDR DALA2025081105988](https://openairdocs.org/sdr/DALA2025081105988.md): Cover · unsecure · Aug 6, 2025 · N949AT · Boeing 717200 · Battery/Charger System
  > SHIP 9500 ROW 19C & 19D EMERGENCY BATTERY COVER LOOSE. CORECTIVE ACTION: RE-SECURED AS REQUIRED (7813580)
- [SDR DALA2025081105987](https://openairdocs.org/sdr/DALA2025081105987.md): Apu · odor · Aug 6, 2025 · N949AT · Boeing 717200 · Airborne Auxiliary Power Unit (APU) System
  > SHIP 9500 DIRTY SOCKS SMELL WITH APU AIR ON WHEN TAKING OVER THE AIRPLANE. CORECTIVE ACTION: R/R APU REF B717 AMM 49-10 (7813574)
- [SDR DALA2025100807329](https://openairdocs.org/sdr/DALA2025100807329.md): Skin · damaged · Jun 30, 2025 · N949AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR AND DOOR FRAME: FUSELAGE SKIN DOOR CUTOUT AREA AFT EDGE DAMAGED. C/W AFT CARGO CORROSION ERA 627055-14 REV A. (1055785)
- [SDR DALA2025070104880](https://openairdocs.org/sdr/DALA2025070104880.md): Web · corroded · Jun 30, 2025 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > SHIP 9500 AFT CARGO DOOR THRESHOLD WEB CORRODED SEVERAL LOCATIONS AT UPPER AND LOWER SURFACES. CORRECTIVE ACTION: REMOVED AND REPLACED WEB PER B717 DWG 5910158 (1055786)
- [SDR DALA2025070104876](https://openairdocs.org/sdr/DALA2025070104876.md): Not Entered · no discrepancy · Jun 30, 2025 · N949AT · Boeing 717200 · Standard Practices/Structures
  > 9500 REPETITIVE INSP PER SECT II. OF ERA 627055-14 REV A. CORRECTIVE ACTION: ACCOMPLISH SECTION II: REPETITIVE INSPECTIONS EVERY EIGHT THOUSAND (8,000) FLIGHT CYCLES FROM ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR PER ER/A 627055-14 REV A. (1055040)
- [SDR DALA2025061104462](https://openairdocs.org/sdr/DALA2025061104462.md): Skin · bent · Jun 8, 2025 · N949AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9500, FWD CARGO DOOR AND DOOR FRAME: DOOR SKIN BENT ALONG LOWER EDGE. CORRECTIVE ACTION: REPAIRED PER B717 SRM 52-00-01-2R-8. (LP 1011857)
- [SDR DALA2025060604329](https://openairdocs.org/sdr/DALA2025060604329.md): Spar Cap · cracked · May 27, 2025 · N949AT · Boeing 717200 · Wing Spar
  > SHIP 9500 LH WING REAR SPAR LOWER CAP CRACK. REPAIRED PER ERA 623615-14AD REV 0 (0990246)
- [SDR DALA2025060604324](https://openairdocs.org/sdr/DALA2025060604324.md): Repair · not reported · May 25, 2025 · N949AT · Boeing 717200 · Wing Structure
  > SHIP 9500 EXISTING REPAIR FOUND PER ERA 623617-14AD REV ORIG. CORRECTIVE ACTION: REPAIRED PER 623617-14AD (0986223)
- [SDR DALA2025020500872](https://openairdocs.org/sdr/DALA2025020500872.md): Spar Cap · cracked · Jan 2, 2025 · N949AT · Boeing 717200 · Wing Spar
  > -AD- LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK. CRACK INDICATION IN HOLE THAT IS 2 HOLES IB OF EXISTING CRACK, XRS 164. REF PRI 621050-14 REV 1 STEP 11 AND FIGURE 3. SUMMARY SEE NRC 006-0001:10-0557-8-8910/002 00039: REFERENCED PRI 621050-14 ALL REVISIONS
- [SDR DALA2025020500871](https://openairdocs.org/sdr/DALA2025020500871.md): Spar · cracked · Jan 2, 2025 · N949AT · Boeing 717200 · Wing Spar
  > -AD- VISIBLE CRACK FOUND ON LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK, OB OF THE TE RIB CLIP BETWEEN XRS 150.450 AND XRS 164.000. SUMMARY SEE NRC 006-0001:10-0557-8-8910/001 00017: COMPLIED WITH PRI 621050-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV
- [SDR DALA2025020500870](https://openairdocs.org/sdr/DALA2025020500870.md): None · none · Jan 2, 2025 · N949AT · Boeing 717200 · Standard Practices/Structures
  > -AD- WHILE IN MAINTENANCE, AA WORK CARD 5720-01103-01B RH WING XRS 164, REAR SPAR AND LWR SKIN INSPECTION WAS COMPLETED WITH NO FINDINGS. DAL BELIEVES ADDITIONAL INSPECTIONS BEYOND THE SCOPE OF AA WC 5720-01103-01B ARE NECESSARY TO VERIFY NO DAMAGE IS PRESENT
- [SDR DALA2024081408115](https://openairdocs.org/sdr/DALA2024081408115.md): Battery Pack · inoperative · Aug 14, 2024 · N949AT · Boeing 717200 · Emergency Lighting
  > FOUND L & R FWD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. ALSO FOUND L & R FWD SERVICE DOOR EXIT EMERGENCY LIGHTS INOPERATIVE. PER B717 WDM 33-51-14, ALL LIGHTS ASSOCIATED WITH BATTERY PACK B5-118. REPLACED EMERGENCY LIGHT BATTERY PACK B5-118 IAW B717
- [SDR DALA2024072907542](https://openairdocs.org/sdr/DALA2024072907542.md): Battery Pack · inoperative · Jul 27, 2024 · N949AT · Boeing 717200 · Emergency Lighting
  > CEILING PANEL 6,7,8, AND MID CABIN OVERHEAD EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED #5 EMERGENCY BATTERY PACK PER B717 FRMFIM 33-50. OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (LP #6057526)
- [SDR DALA2024062606519](https://openairdocs.org/sdr/DALA2024062606519.md): Battery Pack · inoperative · Jun 26, 2024 · N949AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHT IN CEILING PANELS FROM ROW 2 TO ROW 11 ARE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY BATTERY #5 B5-227 TO BE INOPERATIVE PER B717 FRMFIM 33-50. THE #5 EMERGENCY BATTERY WAS REPLACED PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. NO FURTHER D
- [SDR DALA2024062106298](https://openairdocs.org/sdr/DALA2024062106298.md): Floor Panel · gouged · Apr 10, 2024 · N949AT · Boeing 717200 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL HAS GOUGE AND UPPER SURFACE CRACKED. REPAIRED FLOOR PANEL 121NF FWD CARGO IAW B717-200, SRM 53-20-50-2R, ACCOMPLISH PERMANENT REPAIR WITHIN 500 FLIGHT HOURS PARTS REQUIRED 9936599-501 PANEL OR MATERIAL S00096. REDEFERRED LOG TO QC, ESTAB
- [SDR DALA2023101608459](https://openairdocs.org/sdr/DALA2023101608459.md): Unknown · unknown · Oct 15, 2023 · N949AT · Boeing 717200 · Turbine Engine Compressor Section
  > SHIP 9500 -ATB- THE AIRCRAFT WAS RETURNED TO ATL FOLLOWING COMPRESSOR SURGES IN THE #1 ENGINE. THE PILOT DECLARED AN EMERGENCY WITH ATC AND THE LANDING & TAXI TO THE GATE WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 ENGINE (ESN 13197) AND THE
- [SDR DALA2023091907688](https://openairdocs.org/sdr/DALA2023091907688.md): Unknown · unknown · Sep 17, 2023 · N949AT · Boeing 717200 · Escape Slide
  > FOUND TAIL SLIDE CONTAINER OPEN AND SLIDE UNPACKED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REPLACED TAILCONE SLIDE PER B717 W/C 2561-9006. ALL RII STEPS ACCOMPLISHED PER W/C 2561-9006. (LP #
- [SDR DALA2023031702019](https://openairdocs.org/sdr/DALA2023031702019.md): Unknown · unknown · Mar 15, 2023 · N949AT · Boeing 717200 · Landing Gear Brake System
  > SHIP 9500 -ATB- THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT MYR DUE THE #2 BRAKE OVER TEMPERATURE WARNING ILLUMINATING. QRH PROCEDURES FAILED TO LOWER THE TEMPERATURE INDICATION. THE LANDING WAS UNEVENTFUL AND THE AIRCRAFT BRAKING WAS NORMAL. CORR
- [SDR DALA2023031401856](https://openairdocs.org/sdr/DALA2023031401856.md): Unknown · unknown · Mar 13, 2023 · N949AT · Boeing 717200 · Emergency Lighting
  > THE FORWRD EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY BATTERY POWER SUPPLY B5-118 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4076686)
- [SDR DALA2023031401854](https://openairdocs.org/sdr/DALA2023031401854.md): Unknown · unknown · Mar 13, 2023 · N949AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHT OVER THE CATWALK IS INOPERATIVE. MAINTENACE REPLACED THE POWER SUPPLY B5-116 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #4076685)
- [SDR DALA2022122708379](https://openairdocs.org/sdr/DALA2022122708379.md): Skin · dented · Dec 26, 2022 · N949AT · Boeing 717200 · Trailing Edge Flaps
  > SEVERAL DENTS ON LOWER SKIN OF RT WING FLAP FIXED VANE, THE SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1, AND SRM 51-70-02-0G.
- [SDR DALA2022122808451](https://openairdocs.org/sdr/DALA2022122808451.md): Vane · damaged · Dec 24, 2022 · N949AT · Boeing 717200 · Trailing Edge Flaps
  > DURING TAP-TEST INSPECTION OF DENTS AT RHS FWD MOVABLE VANE, A DISBONDED AREA OF 4.750 IN LENGTH AND 2.000 IN WIDTH WAS FOUND ON THE RUB STRIP. RT FWD MOVABLE VANE WAS REPAIRED IAW SRM 51-70-02-0G PAR. 15, 17A, AND SRM 57-53-01-2R-1 PAR. 4 D.
- [SDR DALA2022122208294](https://openairdocs.org/sdr/DALA2022122208294.md): Support Rib · worn · Dec 21, 2022 · N949AT · Boeing 717200 · Wing, Rib/Bulkhead
  > WORN INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 APPROX AT RH WING. AD. SUMMARY OF NRC 00166: INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 APPROX AT RH WING WAS REPAIRED PER ER/A 604521-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR AND PRI 6045

Next page: https://openairdocs.org/aircraft/N949AT/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 = 'N949AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N949AT/reports

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