N977AT

Service difficulty reports · 159

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2026052803223Skin · crackedCRACK ON FUSELAGE SKIN BTW STA. Y=1037 & LONG 14R AT RH PYLON. REPAIRED PER ER/A 634213-14 (1607725) (AIRCRAFT GROUNDED)May 23, 2026 · N977AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052803222Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA 1087 LONG 14 RH. REPAIRED PER PRI 634296-14 (1606252) (AIRCRAFT GROUNDED)May 22, 2026 · N977AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052803218Vane · debondedONE 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)May 20, 2026 · N977AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2026051903066Skin · not reportedERA 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)May 13, 2026 · N977AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2026051703029Door Frame · corrodedCORROSION 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. (159051May 12, 2026 · N977AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025082206253Not Reported · not reportedER/A 628422-14AD REVISION ORIGINAL. REPAIR AT LT SIDE OF VERTICAL STAB SPAR AT ZFS=52.267. (1144341)Aug 15, 2025 · N977AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025081806154Skin · crackedSHIP 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)Aug 15, 2025 · N977AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2025060704355Fitting · damagedAIRCRAFT 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 62367Jun 5, 2025 · N977AT · Boeing 717200 · Wing Main, Frame StructureSDR DALA2025060604342Spar · damagedSHIP 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)May 30, 2025 · N977AT · Boeing 717200 · Wing SparSDR DALA2025052704025Skin · damagedSHIP 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)May 23, 2025 · N977AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025052704026Spar Cap · crackedSHIP 9541 B717-200 / RH WING / REAR SPAR / LOWER CAP / XRS=164 / CRACK. CORRECTIVE ACTION: ASSOCIATED ER/A 00-623681 C/W. (0980036)May 22, 2025 · N977AT · Boeing 717200 · Wing SparSDR DALA2025050103359Spar Web · damagedLEFT 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)Apr 30, 2025 · N977AT · Boeing 717200 · Wing SparSDR DALA2025050103358Skin · damagedLEFT 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 #0941448Apr 30, 2025 · N977AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025011300272Spar Cap · cracked-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 TRANSFERJan 10, 2025 · N977AT · Boeing 717200 · Wing SparSDR DALA2024112711257Spar · cracked-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 Nov 26, 2024 · N977AT · Boeing 717200 · Wing SparSDR DALA2024103010502None · none-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)Oct 29, 2024 · N977AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024103010501Fuel Cell · leaking-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)Oct 29, 2024 · N977AT · Boeing 717200 · Fuel StorageSDR DALA2024103010500Fuel Cell · leaking-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 615810-14Oct 29, 2024 · N977AT · Boeing 717200 · Fuel StorageSDR DALA2024112111101Spar · cracked-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 Oct 28, 2024 · N977AT · Boeing 717200 · Wing SparSDR DALA2024092309315Lens · missingTHE 1AB EMERGENCY LIGHT LENSE IS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT COVER AT 1AB AS REQUIRED. OK FOR SERVICE. (LP #0569847)Sep 22, 2024 · N977AT · Boeing 717200 · Emergency LightingSDR DALA2024071207052Battery Pack · no testDURING 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)Jul 11, 2024 · N977AT · Boeing 717200 · Emergency LightingSDR DALA2024042204628Lanyard · missingSLIDE 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 HApr 16, 2024 · N977AT · Boeing 717200 · Escape SlideSDR DALA2024040804183Door Frame · damagedCRACK 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)Apr 6, 2024 · N977AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024040804182Beam · damagedCRACK 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, PROCEApr 5, 2024 · N977AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024040504134Spar · crackedCRACK 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 PRIORApr 4, 2024 · N977AT · Boeing 717200 · Wing SparSDR DALA2024032703840Pan · crackedCRACK 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)Mar 26, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024032503737Skin · debondedTWO 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 595913-14Mar 24, 2024 · N977AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024032303704Pan · crackedCRACK 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)Mar 23, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024032103592Window Frame · crackedCRACK 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 WIMar 21, 2024 · N977AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024032103579Cusp Web · corrodedCORROSION 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)Mar 18, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024032103574Floor Support · corrodedCORROSION 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)Mar 15, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024031503377Angle · corrodedCORROSION 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 51Mar 15, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024031403327Seat Track · corrodedCORROSION 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,Mar 13, 2024 · N977AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024031303280Cusp Web · corrodedCORROSION 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 #024Mar 13, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024030803181Pan · crackedCRACK 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)Mar 7, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024030703128Web · corrodedCORROSION 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)Mar 7, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024030703127Cusp Web · corrodedAWR, 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. ASSOCMar 7, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024030703125Longeron · corrodedCORROSION 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-Mar 6, 2024 · N977AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024030603061Frame · crackedCRACK 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)Mar 5, 2024 · N977AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024030503006Floor Support · corrodedCORROSION 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)Mar 4, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024030402937Cusp Web · corrodedCORROSION 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 PROCEDUMar 2, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024030402935Doubler · corrodedCORROSION 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 AFMar 1, 2024 · N977AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024030402932Web · corrodedCORROSION 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)Mar 1, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024030402930Bulkhead Web · corrodedCORROSION 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 Mar 1, 2024 · N977AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2024022802768Frame · crackedAD. 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 5310-01436-03Feb 28, 2024 · N977AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024022802767Floor Support · corrodedCORROSION 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 #0Feb 28, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022802766Frame · crackedAD. 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 5310-01436-0Feb 28, 2024 · N977AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024022602638Floor Support · corrodedCORROSION 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)Feb 24, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022602637Floor Support · corrodedCORROSION 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)Feb 24, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022602636Cusp Web · mechanic errorMISDRILLED 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)Feb 24, 2024 · N977AT · Boeing 717200 · Fuselage Miscellaneous Structure
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