# Service difficulty reports: N977AT

A list on [N977AT](https://openairdocs.org/aircraft/N977AT.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 · 159 reports

- [SDR DALA2026052803223](https://openairdocs.org/sdr/DALA2026052803223.md): Skin · cracked · May 23, 2026 · N977AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BTW STA. Y=1037 & LONG 14R AT RH PYLON. REPAIRED PER ER/A 634213-14 (1607725) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803222](https://openairdocs.org/sdr/DALA2026052803222.md): Skin · cracked · May 22, 2026 · N977AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL FUSELAGE SKIN STA 1087 LONG 14 RH. REPAIRED PER PRI 634296-14 (1606252) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803218](https://openairdocs.org/sdr/DALA2026052803218.md): Vane · debonded · May 20, 2026 · N977AT · Boeing 717200 · Trailing Edge Flaps
  > ONE DISBONDED AREA OF 1.000IN ( LENGTH) X 1.000IN (WIDTH) WAS FOUND ON FLAP VANE, ON UPPER SURFACE AT RIGHT WING. REPAIRED PER PRI 634257-14 REV 2 AND ER/A NO.634257-14 (1604178) (AIRCRAFT GROUNDED)
- [SDR DALA2026051903066](https://openairdocs.org/sdr/DALA2026051903066.md): Skin · not reported · May 13, 2026 · N977AT · Boeing 717200 · Standard Practices/Structures
  > ERA 634294-14 ISSUED FOR FUSELAGE SKIN REPAIR AT STA 1076, L14L, FOLLOW ON INSPECTIONS ARE REQUIRED. ACCOMPLISH ERA 634294-14 SECTION II INSPECTIONS (1600062) (AIRCRAFT GROUNDED)
- [SDR DALA2026051703029](https://openairdocs.org/sdr/DALA2026051703029.md): Door Frame · corroded · May 12, 2026 · N977AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON PREVIOUS REPAIR ON DOOR JAMB STA Y= 994 BTW LONG 26R AND LONG 27R AT AFT CARGO COMPARTMENT. PREVIOUS REPAIR ON DOOR JAMB STA Y= 994 BTW LONG 26R AND LONG 27R AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 53-20-15-2R PROCEDURE 7 REPAIR.7. (159051
- [SDR DALA2025082206253](https://openairdocs.org/sdr/DALA2025082206253.md): Not Reported · not reported · Aug 15, 2025 · N977AT · Boeing 717200 · Standard Practices/Structures
  > ER/A 628422-14AD REVISION ORIGINAL. REPAIR AT LT SIDE OF VERTICAL STAB SPAR AT ZFS=52.267. (1144341)
- [SDR DALA2025081806154](https://openairdocs.org/sdr/DALA2025081806154.md): Skin · cracked · Aug 15, 2025 · N977AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > SHIP 9541 C/W ERA 628422-14AD REV ORIG VERTICAL STABILIZER LHS & RHS LEADING EDGE SKIN ZFS52.267 FASTENER HOLES CRACKED. CORRECTIVE ACTION: C/W PRI 628422-14AD. (1145072)
- [SDR DALA2025060704355](https://openairdocs.org/sdr/DALA2025060704355.md): Fitting · damaged · Jun 5, 2025 · N977AT · Boeing 717200 · Wing Main, Frame Structure
  > AIRCRAFT 9541, LEFT WING LOWER SURFACE BRACE FITTING AT STA XRS 164 HOLE HAS DAMAGE (1EA) LABLED C1. CORRECTIVE ACTION: LEFT WING LOWER SERFACE BRACE FITTING STA XR5164, REAMED HOLE C1.416 IAW ER/A 623679-14 AD REV 0 PRI REV 4 PERFORMED BHEC INSP IAW ERS 62367
- [SDR DALA2025060604342](https://openairdocs.org/sdr/DALA2025060604342.md): Spar · damaged · May 30, 2025 · N977AT · Boeing 717200 · Wing Spar
  > SHIP 9451 LH WING AFT SPAR FLAP TRACK MOUNT REQUIRES REMOVAL OF 8 BUSHINGS TO FOM SPAR REPAIR. CORRECTIVE ACTION: REPAIRED PER 623679-14AD REV 0 (0996171)
- [SDR DALA2025052704025](https://openairdocs.org/sdr/DALA2025052704025.md): Skin · damaged · May 23, 2025 · N977AT · Boeing 717200 · Wing, Plate/Skin
  > SHIP 9541 LEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137. CORRECTIVE ACTION: DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD (0982505)
- [SDR DALA2025052704026](https://openairdocs.org/sdr/DALA2025052704026.md): Spar Cap · cracked · May 22, 2025 · N977AT · Boeing 717200 · Wing Spar
  > SHIP 9541 B717-200 / RH WING / REAR SPAR / LOWER CAP / XRS=164 / CRACK. CORRECTIVE ACTION: ASSOCIATED ER/A 00-623681 C/W. (0980036)
- [SDR DALA2025050103359](https://openairdocs.org/sdr/DALA2025050103359.md): Spar Web · damaged · Apr 30, 2025 · N977AT · Boeing 717200 · Wing Spar
  > LEFT WING AFT SPAR WEB O/B LOWER HOLE HAS DAMAGE (1 EA), LABELED AS B1. NO DAMAGE FOUND IAW DELTA ER/A 623679-14AD REV 0, PRI REV 7 SECTION 4 STEP #1 AND TABLE 2. ASSOCIATED ER/A 14-623679 ADDED FOR AC 9541. (LP #0941455)
- [SDR DALA2025050103358](https://openairdocs.org/sdr/DALA2025050103358.md): Skin · damaged · Apr 30, 2025 · N977AT · Boeing 717200 · Wing, Plate/Skin
  > LEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137 (7 EA) MARKED AS A1 THRU A7. DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD REV 0 PRI REV 7 SECTION IV STEP # 5, #6, AND #7. ASSOCIATED ER/A 14-623679 ADDED FOR AC 9541. (LP #0941448
- [SDR DALA2025011300272](https://openairdocs.org/sdr/DALA2025011300272.md): Spar Cap · cracked · Jan 10, 2025 · N977AT · Boeing 717200 · Wing Spar
  > -AD- CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT REF FC5720-01103. CRACK IS LOCATED INBD OF XRS 164 AT RIVET HEAD 1/2 INCH ABOVE LWR RADIUS. DISCREPANCY TRANSFER
- [SDR DALA2024112711257](https://openairdocs.org/sdr/DALA2024112711257.md): Spar · cracked · Nov 26, 2024 · N977AT · Boeing 717200 · Wing Spar
  > -AD- WORKING PRI 615810-14AD REV 0. LH WING SPAR CRACK FUEL LEAK. ACCOMPLISHED PRI 615810-14AD REVISION D, REV 3. VERIFIED ERA 615810-14AD REV D SECTION VI TIME LIMITED REPAIR III MATCHES COMPLETED PRI 615810-14AD REV 0, 1, 2, AND 3. ASSOCIATED ER/A 14-615810
- [SDR DALA2024103010502](https://openairdocs.org/sdr/DALA2024103010502.md): None · none · Oct 29, 2024 · N977AT · Boeing 717200 · Standard Practices/Structures
  > -AD- WORKING PRI 615810AD REV 3. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS ARE C/W AND MATCH PRI 621847-14AD REV 0, 1, 2, AND PRI 615810-14AD REV 3. (LP #0634418)
- [SDR DALA2024103010501](https://openairdocs.org/sdr/DALA2024103010501.md): Fuel Cell · leaking · Oct 29, 2024 · N977AT · Boeing 717200 · Fuel Storage
  > -AD- L/H WING REAR SPAR LOWER CAP LEAKING FUEL. C/W PRI 621847-14AD REV 2. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS MATCH PRI 621847-14AD REV 0, 1, 2, AND PRI 615810 REV 3. (LP #0634404)
- [SDR DALA2024103010500](https://openairdocs.org/sdr/DALA2024103010500.md): Fuel Cell · leaking · Oct 29, 2024 · N977AT · Boeing 717200 · Fuel Storage
  > -AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING REAR SPAR LOWER CAP. CONTACT LIAISON ENG. REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT, AA#FC5720-01103. LEAK IDENTIFIED ORIGINATED FROM FASTENER. C/W PRI 621847-14AD REV ORIGINAL THRU REV 2. C/W PRI 615810-14
- [SDR DALA2024112111101](https://openairdocs.org/sdr/DALA2024112111101.md): Spar · cracked · Oct 28, 2024 · N977AT · Boeing 717200 · Wing Spar
  > -AD- LH WING REAR SPAR XRS 164 CRACKED. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) REQUIRED FOR CONTINUED SERVICE BEYOND 06NOV2024 (AD EFFECTIVE DATE). A NEW FAA FORM 8100-9 AND AMOC APPROVAL TO AD 2024-21-01 IS REQUIRED FOR CONTINUED SERVICE BEYOND
- [SDR DALA2024092309315](https://openairdocs.org/sdr/DALA2024092309315.md): Lens · missing · Sep 22, 2024 · N977AT · Boeing 717200 · Emergency Lighting
  > THE 1AB EMERGENCY LIGHT LENSE IS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT COVER AT 1AB AS REQUIRED. OK FOR SERVICE. (LP #0569847)
- [SDR DALA2024071207052](https://openairdocs.org/sdr/DALA2024071207052.md): Battery Pack · no test · Jul 11, 2024 · N977AT · Boeing 717200 · Emergency Lighting
  > DURING THE SERVICE CHECK, THE TAIL SIDE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK (B5-260) DEFECTIVE. THE BATTERY PACK WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW GOOD. (LP #5916991)
- [SDR DALA2024042204628](https://openairdocs.org/sdr/DALA2024042204628.md): Lanyard · missing · Apr 16, 2024 · N977AT · Boeing 717200 · Escape Slide
  > SLIDE DISARMING PIN ATTACHING LANYARD MISSING. LATCH MECHANISM MISSING TO SECURELY ARM TAILCONE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. WILL REQUIRE NEW LOWER CATCH ASSY AND ATTACHING H
- [SDR DALA2024040804183](https://openairdocs.org/sdr/DALA2024040804183.md): Door Frame · damaged · Apr 6, 2024 · N977AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK DOOR ON FRAME DOOR ANGLE BTW STA 195 (AFT UPPER CORNER) AT FWD SERVICE DOOR R1. SUMMARY OF NRC 00075: ANGLE WAS FABRICATED PER DOUGLAS AIRCRAFT COMPANY DRAWING: 9911579 REV: L AND REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0279803)
- [SDR DALA2024040804182](https://openairdocs.org/sdr/DALA2024040804182.md): Beam · damaged · Apr 5, 2024 · N977AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK BEYOND STOPDRILL, (PREVIOUS REPAIR) ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00071: 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, PROCE
- [SDR DALA2024040504134](https://openairdocs.org/sdr/DALA2024040504134.md): Spar · cracked · Apr 4, 2024 · N977AT · Boeing 717200 · Wing Spar
  > CRACK ON REAR SPAR XRS 150 AT LH WING. SUMMARY OF NRC 0054: REAR SPAR XRS 150 AT LH WING WAS REPAIRED PER ERA 615810-14 REV ORIGINAL SECTION I: TEMPORARY REPAIR. TIME CONTROLLED ITEMS, SEC II ACCOMPLISH SECTION II: INITIAL HFEC SURFACE INSPECTION AND DVI PRIOR
- [SDR DALA2024032703840](https://openairdocs.org/sdr/DALA2024032703840.md): Pan · cracked · Mar 26, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK PAN ON AFT EDGE AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00154: FWD CARGO COMPARMENT DOOR WAS REPAIRED PER ERA 559551-14 REV A. SECTION II. ASSOCIATED ER/A 14-559551 ADDED FOR AC 9541. (LP #0263823)
- [SDR DALA2024032503737](https://openairdocs.org/sdr/DALA2024032503737.md): Skin · debonded · Mar 24, 2024 · N977AT · Boeing 717200 · Trailing Edge Flaps
  > TWO DISBONDS FOUND ON LH AFT MOVABLE FLAP VANE LOWER SKIN: 1) LENGTH=1.700IN, WIDTH=1.500IN AND 2) LENGTH=2.100IN, WIDTH= 1.000IN (IN REF MON/9541/0138992 JOB # 005-0001). SUMMARY OF NRC 00037: LH AFT MOVABLE FLAP VANE LOWER SKIN WAS REPAIRED PER ERA 595913-14
- [SDR DALA2024032303704](https://openairdocs.org/sdr/DALA2024032303704.md): Pan · cracked · Mar 23, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00155: PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0257725)
- [SDR DALA2024032103592](https://openairdocs.org/sdr/DALA2024032103592.md): Window Frame · cracked · Mar 21, 2024 · N977AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW, AT COCKPIT. SUMMARY OF NRC 00439: UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW AT COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. BRACKET OF UPPER AFT CORNER CUTOUT OF LH SLIDING WI
- [SDR DALA2024032103579](https://openairdocs.org/sdr/DALA2024032103579.md): Cusp Web · corroded · Mar 18, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP ANGLE BTW STA Y=148 TO Y=218. SUMMARY OF NRC 00438: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA Y=148 TO Y=218 WAS REPAIRED PER ERA 616020-14 REV ORIGINAL. SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616020 ADDED FOR AC 9541. (LP #0251319)
- [SDR DALA2024032103574](https://openairdocs.org/sdr/DALA2024032103574.md): Floor Support · corroded · Mar 15, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BTW STA Y=160-200 X=6, X=0 AND X=-6. SUMMARY OF NRC 00620: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=160-200 X=6, X=0 AND X=-6 WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0246907)
- [SDR DALA2024031503377](https://openairdocs.org/sdr/DALA2024031503377.md): Angle · corroded · Mar 15, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FRAME CLIP STA Y=1087 AND LONGERON 18R AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00101: CORROSION LEVEL 2. FRAME CLIP STA Y=1087 AND LONGERON 18R AT AFT ACCESORY COMPARTMENT WAS FABRICATED PER B717 DWG S2931622 REV B AND REPLACED PER B717 SRM 51
- [SDR DALA2024031403327](https://openairdocs.org/sdr/DALA2024031403327.md): Seat Track · corroded · Mar 13, 2024 · N977AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BTW Y=200 TO STA Y=256, COORDINATE X=-44 (RH SIDE). SUMMARY OF NRC 00696: CORROSION LEVEL 2. SEAT TRACK BTW Y=200 TO STA Y=341, COORDINATE X=-44 (RH SIDE) WAS FABRICATED PER DRAWING #5930547 REV CW AND REPLACED PER B717 SRM 51-41-01-0G,
- [SDR DALA2024031303280](https://openairdocs.org/sdr/DALA2024031303280.md): Cusp Web · corroded · Mar 13, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB LOWER SURFACES BTW STA 446 TO STA 465 AND STA 494 TO STA 500. SUMMARY OF NRC 00669: CORROSION LEVEL 2. RH CUSP WEBS BTW STA 446 TO STA 465 AND STA 494 TO STA 500 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #024
- [SDR DALA2024030803181](https://openairdocs.org/sdr/DALA2024030803181.md): Pan · cracked · Mar 7, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON DOOR PAN AFT UPPER CORNER AT FWD PASSENGER DOOR. SUMMARY OF NRC 00119: DOOR PAN AFT UPPER CORNER AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #0234310)
- [SDR DALA2024030703128](https://openairdocs.org/sdr/DALA2024030703128.md): Web · corroded · Mar 7, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BTW STA Y=200/205 AND STA X=54 AT C PAX (W1) WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00719: CORROSION LEVEL 2. WEB BTW STA Y=200/205 AND STA X=54 AT C PAX WAS REPAIRED PER B717 SRM 51-70-10-2R REPAIR 2. (LP #0233534)
- [SDR DALA2024030703127](https://openairdocs.org/sdr/DALA2024030703127.md): Cusp Web · corroded · Mar 7, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AWR, AA, AD IN REF TO AMDS 5310-01436-03B STEP 3: AFTER RH CUSP WEB REMOVAL, SEVERAL CRACKS AND CORROSION WERE FOUND ON RIGHT CUSP WEB FROM STA Y 655 TO 715. SUMMARY OF NRC 00700: RH CUSP WEB FROM STA Y 655 TO 715 WAS REPAIRED PER B717 SRM 53-00-55-2R-4. ASSOC
- [SDR DALA2024030703125](https://openairdocs.org/sdr/DALA2024030703125.md): Longeron · corroded · Mar 6, 2024 · N977AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND OUT OF LIMITS AT LONGERON ENDS 28LH AND 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00713: CORROSION LEVEL 2. LONGERON ENDS 28LH AND 28RH WERE DRILLED AND ADJUSTED PER B717 SRM 51-40-08-0G AND REPLACED UNDER NRC 00464 AND PER B717 SRM 51-
- [SDR DALA2024030603061](https://openairdocs.org/sdr/DALA2024030603061.md): Frame · cracked · Mar 5, 2024 · N977AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA=1037 LONGERON 17LH SIDE AT PAX CABIN. SUMMARY OF NRC 00411: FRAME STA=1037 LONGERON 17LH SIDE AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R AND 51-41-05-0G. (LP #0231352)
- [SDR DALA2024030503006](https://openairdocs.org/sdr/DALA2024030503006.md): Floor Support · corroded · Mar 4, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPOORT BTW STA Y=200 TO 218 X-54 AT PAX CABIN. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=200 TO 218 X-54 WAS FABRICATED PER DWG 5952262 REV L AND REPLACED UNDER NRC 00438. (LP #0230263)
- [SDR DALA2024030402937](https://openairdocs.org/sdr/DALA2024030402937.md): Cusp Web · corroded · Mar 2, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB REPAIR DOUBLER BTW STA 484 TO 494 PAX CABIN. SUMMARY OF NRC 00484: CORROSION LEVEL 2. RH CUSP WEB REPAIR DOUBLER AND RING DOUBLER BTW STA 484 TO 494 PAX CABIN WERE REPLACED PER B717 SRM 51-41-05-0G, 51-40-02-0G, AND 53-00-55-2R PROCEDU
- [SDR DALA2024030402935](https://openairdocs.org/sdr/DALA2024030402935.md): Doubler · corroded · Mar 1, 2024 · N977AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON PRODUCTION DOUBLER ATTACHED TO FWD FACE STA 1053 BTW LONGERON 29L AND 29R AT AFT PRESSURE BULKHEAD (LOWER AREA) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00570: CORROSION LEVEL 2. DOUBLER ATTACHED TO FWD FACE STA 1053 BTW LONGERON 29L AND 29R AT AF
- [SDR DALA2024030402932](https://openairdocs.org/sdr/DALA2024030402932.md): Web · corroded · Mar 1, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON MEMBRANE STA Y=196 X=54.5 AT PAX CABIN. SUMMARY OF NRC 00618: CORROSION LEVEL 2. MEMBRANE STA Y=196 X=54.5 AT PAX CABIN WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0225652)
- [SDR DALA2024030402930](https://openairdocs.org/sdr/DALA2024030402930.md): Bulkhead Web · corroded · Mar 1, 2024 · N977AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON FWD LOWER FACE OF AFT PRESSURE BULKHEAD STA Y=1053 BTW L26L AND L26R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00462: CORROSION LEVEL 1. CORROSION ON FWD LOWER FACE OF AFT PRESSURE BULKHEAD STA Y=1053 BTW L26L AND L26R AT AFT CARGO COMPARTMENT WAS
- [SDR DALA2024022802768](https://openairdocs.org/sdr/DALA2024022802768.md): Frame · cracked · Feb 28, 2024 · N977AT · Boeing 717200 · Fuselage Main, Frame
  > AD. CRACK OF 0.734 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 RH. (IN REF CARD 5310-01436-04D, JOB #079-0004, STEP 7). SUMMARY OF NRC 00293: OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER AMDS 5310-01436-03
- [SDR DALA2024022802767](https://openairdocs.org/sdr/DALA2024022802767.md): Floor Support · corroded · Feb 28, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA Y=164, Y=190, AND Y=200 X=54.5 AT PAX CABIN. SUMMARY OF NRC 00616: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=164, Y=190, AND Y=200 X=54.5 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #0
- [SDR DALA2024022802766](https://openairdocs.org/sdr/DALA2024022802766.md): Frame · cracked · Feb 28, 2024 · N977AT · Boeing 717200 · Fuselage Main, Frame
  > AD. CRACK OF 0.359 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #079-0004, STEP 10). SUMMARY OF NRC 00294: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER AMDS 5310-01436-0
- [SDR DALA2024022602638](https://openairdocs.org/sdr/DALA2024022602638.md): Floor Support · corroded · Feb 24, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BTW STA Y=1017-1040 X=44.5 AT PAX CABIN. SUMMARY OF NRC 00604: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1017-1040 X=44.5 AT PAX CABIN WAS FABRICATED PER DWG 9981474 REV.L AND REPLACED PER B717 SRM 51-41-05-0G. (LP #0216570)
- [SDR DALA2024022602637](https://openairdocs.org/sdr/DALA2024022602637.md): Floor Support · corroded · Feb 24, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BTW STA Y=1027-1054 X=-54 AT PAX CABIN. SUMMARY OF NRC 00609: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1027-1054 X=-54 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0216555)
- [SDR DALA2024022602636](https://openairdocs.org/sdr/DALA2024022602636.md): Cusp Web · mechanic error · Feb 24, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > MISDRILLED ON CUSP WEB BTW STA Y=674 AT LH CABIN PAX. SUMMARY OF NRC 00426: CUSP WEB BTW STA Y=674 AT LH CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0216550)

Next page: https://openairdocs.org/aircraft/N977AT/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 = 'N977AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N977AT/reports

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