N930AT

Service difficulty reports · 188

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 = 'N930AT' 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 DALA2026062903840Door Frame · crackedCORROSION AND CRACK ON FWD CARGO DOOR JAMB LOWER SECTION AT FWD CARGO COMPARTMENT. FWD CARGO DOOR JAMB LOWER SECTION AND SPLICE ANGLES (4EAS) AT FWD CARGO DOOR JAMB LOWER SECTION WERE REPLACED PER B717-200 SRM 53-20-15-2R. (1670437) (AIRCRAFT GROUNDED).Jun 28, 2026 · N930AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2026062503778Lanyard · frayedFRAYED LANYARD OF SLIDE DOOR LT. REPLACED IAW AIPC 25-61-01-01. (1663123) (AIRCRAFT GROUNDED)Jun 24, 2026 · N930AT · Boeing 717200 · Emergency EquipmentSDR DALA2026051903065Not Reported · not reportedAD 2024-21-01 ER/A 634524-14AD. ASSOCIATED ER/A 14-634524 (1598852) (AIRCRAFT GROUNDED)May 17, 2026 · N930AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2026040102132Windshield · arcedCENTER WINDSHIELD ANTIICE FAIL DUE TO ARCING HEATER CRACK IN WINDSHIELD. REPLACED CENTER WINDSHIELD PER B717 AMM 56-11-01 LEAK CK OK A/C OK FOR SERVICE (8424138)Mar 31, 2026 · N930AT · Boeing 717200 · Flight Compartment WindowsSDR DALA2025122309343Slide · dislodgedOPS REPORTS R1 DOOR SLIDE DISLODGED. DOOR SLIDE IAW AMM 25-61. ACFT OK FOR SERVICE. (8406508)Dec 17, 2025 · N930AT · Boeing 717200 · Escape SlideSDR DALA2025111208301Cable · out of adjustATB- RETURNED TO ATL DUE TO AIR/GROUND FAULTS. ADJUSTED GROUND SHIFT CABLE. OPS NORMAL.(7834142)Nov 11, 2025 · N930AT · Boeing 717200 · Landing Gear Position and WarningSDR DALA2025061104461Power Supply · inoperativeAIRCRAFT 9567, ON SVC CK FOUND AFT L/R OVER WING DOOR EMERGENCY BOTTOM LIGHT INOP. CORRECTIVE ACTION: REPLACED EMERGENGY BATT POWER SUPPLY IAW B717 AMM 33-51-03 OPS CK GOOD. (LP 6812167)Jun 10, 2025 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2025021201091Light · unknownTHE F/A REPORTED THAT THE EXIT ROW EMERGENCY LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE PERFORMED A TEST OF THE EMERGENCY LIGHT SYSTEM AND NO FAULTS WERE FOUND. ALSO, THERE IS NOT ANY HISTORY OF EMERGENCY LIGHTS MALFUNCTIONING IN THE LAST 30 DAYS. ALL CHECKS AREFeb 11, 2025 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2025010300046Power Supply · faultedFOUND ROW 21 EMERGENCY EXIT LIGHT B5-230/P9 TO BE INOPERATIVE. MAINTENANCE TRIED A NEW EMERGENCY LIGHT BATTERY. NO HELP, REINSTALLED ORIGINAL. REPLACED POWER SUPPLY B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6733147)Jan 2, 2025 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2024090408735Light · intermittentWITH THE COCKPIT EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THE CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTANTLY DURING FLIGHT. MAINTENANCE TROUBLESHOT PER B717 FIM 33-50-00 810-801 AND FAULT WAS INTERMITANT. NO 60 DAY HISTORY. AIRCRAFT OK FOR SERVICE. (LP #5Sep 4, 2024 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2024071507164Angle · corrodedCORROSION ON CUSP ANGLE INSIDE FWD SERVICE DOOR JAMB (R1) BTW STA Y=200 AND STA X=-55 AT PASSENGER CABIN. SUMMARY OF NRC 541: CORROSION LEVEL 2. CUSP ANGLE INSIDE FWD SERVICE DOOR JAMB (R1) BTW STA Y=200 AND STA X=-55 WAS REPAIRED PER PRI 618606-14 REV 5 AND EJul 15, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024071507161Pan · crackedCRACKS (3 EA) WERE FOUND ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR. SUMMARY OF NRC 00573: CRACKS (3 EA) ON AFT PAN ON BEAM #4 AT FWD CARGO DOOR WERE REPAIRED PER ER/A 618437-14 REV ORIGINAL. ASSOCIATED ER/A 14-618437 ADDED FOR AC 9567. (LP #0446314)Jul 14, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024071507156Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK ON OPEN POSITION. ALSO FWD PREVIOUSLY REWORK DOES NOT MEET WITH RADII. SUMMARY OF NRC 175: EXTERNAL FUSELAGE SKIN AROUND ATTACH POINT CUTOUT OF L1 DOOR HOOK WAS REPAIRED PER PRI 618669-Jul 12, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024070206725Skin · crackedAIRCRAFT 9567, DURING HCK AT QRO, WHILE PERFORMING THE AFT FUSELAGE AND EMPENNAGE INSPECTION PER WC 5300-2019, A CRACK WAS FOUND AFFECTING THE FUSELAGE SKIN AT Y=1087 AND L-14R. AN EXISTING SKIN SPLICE REPAIR IS ADJACENT TO THE DAMAGE REPORTED. CORRECTIVE ACTIJul 1, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024062906603Seat Track · corrodedAIRCRAFT 9567, CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX WAS REPAIRED PER B717 SRM 53-20-52-2RJun 28, 2024 · N930AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024062906599Seat Track · corrodedAIRCRAFT 9567, CORROSION ON CENTER SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2. SECTION CENTER SEAT TRACK BTW STA= 200 TO STA= 256 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 53-20-52-2R Jun 27, 2024 · N930AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024062906598Longeron · crackedAIRCRAFT 9567, INITIAL INSPECTION: CRACK ON LONGERON END L2R AND STA 1133 ALSO BRACKET SUPPORT LOWER SECTION CANTED BULKHEAD 1103 RH SIDE AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CRACK ON LONGERON END L2R AND STA 1133 WAS REPAIRED PER B717-200 SRM 53-00-05Jun 27, 2024 · N930AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024062706576Angle · crackedAIRCRAFT 9567, CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE. W1. CORRECTIVE ACTION: CORROSION LEVEL 2. CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE WAS Jun 27, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024062706577Skin · damagedAIRCRAFT 9567, FUSELAGE/SKIN/L1 DOOR GUST LATCH/CUTOUT/EDGE DAMAGE REPAIR. CORRECTIVE ACTION: ACCOMPLISH ER/A 618643-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. (LP 0413016)Jun 25, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024062706572Skin · crackedAIRCRAFT 9567, CRACK ON DOOR SKIN ADJACENT TO EXTERNAL DOOR HANDLE HOUSING AT LEFT PASSENGER ENTRANCE DOOR. SUMMARY OF NRC SERIAL 00370: DUE TO SEVERAL DAMAGE ON FWD PASSENGER DOOR (L1) WILL BE REPLACED WITH SERVICEABLE DOOR; PER TRACKING PURPOSE ONLY; FWD PASJun 25, 2024 · N930AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024062506488Longeron · corrodedCORROSION OUT OF LIMIT ON LONGERON END STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT. C2. SUMMARYOF NRC 00857: CORROSION LEVEL 2. LONGERON END ON STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT C2 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8. (LP #0411089)Jun 24, 2024 · N930AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024062406343Cusp Web · crackedCRACKS WERE FOUND ON MEMBRANE OF PASSENGER CABIN AT CUSP WEB BTW STA 218/237 AND BTW STA X=-56/-22. SUMMARY OF NRC 00678: CUSP WEB BTW STA 218/237 AND BTW STA X=-56 /-22 WAS REPAIRED PER B717 53-00-55-2R-4 CONFIGURATION 7015 FIG 210 PAR 40 AND 51-41-02-0G. (LPJun 22, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024062406339Frame · crackedA.D. CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=715.000 RH IN REFERENCE CARD 5310- 01436-01D JOB# 082-0004. (SM) SUMMARY OF NRC 00508: OVERWING FRAME AT STA Y=715 WAS REPLACED PER CARD 5310-01436-03B AND B717-200 SRM 51-41-Jun 21, 2024 · N930AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024062106294Intercostal · crackedCRACK ON INTERCOSTAL WAS FOUND ON STA Y=636 X=0 AT PAX CABIN. SUMMARY OF NRC 00838: CRACK ON INTERCOSTAL ON STA Y=636 X=0 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #0403676)Jun 20, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024062006268Beam · crackedCRACK ON INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00685: INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER B717-200 SRM 52-30- 02-2R PROCEDURE 1 REPAIR 1. (LP #0402498)Jun 19, 2024 · N930AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024061806170Skin · crackedCRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R. SUMMARY OF NRC 00226: CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R WAS REPAIRED PER B717-200 SRM 53-20-15- 2R PROCEDURE 12. PERFORM AN EXTERNAL GVI EVERY 8000 CYCLES TO TJun 17, 2024 · N930AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024061606112Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE. IN REFERENCE NRC 00604. SUMMARY OF NRC 00789: CORROSION LEVEL 2. FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE WAS FABRICATED AND INSTALLED PER DWG 9936534 REV Jun 15, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024061606110Cusp Web · crackedCRACKS CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00610: CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN WERE REPAIRED PER B717- 200 SRM 53-00-55-2R-4. (LP #0393751)Jun 14, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024061606109Pan · crackedCRACK ON INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE. SUMMARY OF NRC 00686: INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0393395)Jun 14, 2024 · N930AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024061606108Frame · damagedTOOL MARKS ON OVERWING FRAME STA737 L-18R AT WING BOX. SUMMARY OF NRC 00533: OVERWING FRAME STA737 L-18R AT WING BOX WAS REPAIRED PER PRI 618675-14 REV.0 AND ERA 618675-14 REV. ORIGINAL ASSOCIATED ER/A 14-618675 ADDED FOR AC 9567. (LP #0392376)Jun 13, 2024 · N930AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024061306056Cusp Web · corrodedCORROSION ON LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00791: CORROSION LEVEL 2, LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 216. (LP #0391165)Jun 13, 2024 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023081606669Unknown · unknownTHE EMERGENCY LIGHTS IN ROWS 15-19 ARE INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK B5-120 TO BE INOPERATIVE AND REPLACED THE BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #4952903)Aug 15, 2023 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2023051803951Unknown · unknownSHIP 9567 -HYD/DE- THE FLIGHT CREW NOTICED A LOSS OF HYDRAULIC FLUID INDICATION WITH THE LEFT SYSTEM. THE QRH WAS COMPLIED WITH AND THE LEFT ENGINE DRIVEN HYDRAULIC PUMP WAS SHUTDOWN. AN EMERGENCY WAS DECLARED DUE TO THE LOSS OF THE LEFT SYSTEM HYDRAULICS WHILMay 15, 2023 · N930AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), MainSDR DALA2022112907614Lens · detachedTHE EXIT LENS COVER AT ROW 19 IS MISSING. MAINTENANCE REPLACED THE MISSING LENS COVER AT ROW 19. (LP #2513959)Nov 27, 2022 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2022032802027Longeron · damagedSECOND DAMAGE AFTER CORROSION REMOVAL ON L29 LH BTW STA 900 TO STA 968 REMAINING THICKNESS IS OUT OF LIMITS. IN REFERENCE NRC 184. SUMMARY OF NRC 00252: CORROSION LEVEL 2, LONGERON 29LH BTW STA 900 TO STA 968 WAS REPAIRED PER B717-200 SRM 53-20-05-2R REPAIR 1,Mar 25, 2022 · N930AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022032502000Frame Splice · corrodedCORROSION ON REPAIR SPLICE FRAME STA 1022 BTW LONGS 30 TO 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: (CORROSION LEVEL 2) REPAIR SPLICE FRAME STA 1022 BTW LONGS 30 TO 26 LH AT AFT CARGO COMPARTMENT WAS REPLACE PER B717 SRM 53-20-07-2R. REPAIR 3. (LP Mar 25, 2022 · N930AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2022032401937Unknown · unknownCORROSION ON SPLICE OF STRINGER 30 STA=960 TO 975 AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00196: CORROSION LEVEL 2, SPLICE OF STRINGER 30 STA=960 TO 975 AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-00-05-2R, REPAIR 2. (LP #2168169)Mar 23, 2022 · N930AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022032201862Not Reported · not reportedSECONDARY DAMAGE AREAS WERE FOUND AT DENTS #8 & #10 ON INNER FACE OF REAR MOVABLE VANE AT LH WING. AREAS WERE FOUND DEBONDED (IN REF NRC 00060). SUMMARY OF NRC 00238: INNER FACE OF REAR MOVABLE VANE AT LH WING WAS REPAIRED PER B717 SRM 51-70-02-0G AND IN REFERMar 21, 2022 · N930AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2022032101831Not Reported · not reportedCORROSION ON DOOR JAMB BTW STA 950 TO 1000 OF AFT CARGO COMPARTMENT (SM). SUMMARY OF NRC 00030: CORROSION LEVEL 2, DOOR JAMB OF AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R, REP. 7. (LP #2164034)Mar 20, 2022 · N930AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019082004881Lens · missingTHE FORWARD FACING LENS FROM THE CENTER AISLE EMERGENCY EXIT SIGN AT THE OVERWING EXIT IS MISSING. MAINTENANCE INSTALLED THE CENTER AISLE FORWARD FACING LENS AT THE OVERWING EXITS PER B717 AMM 33-51. (LP #6167025)Aug 19, 2019 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2019010400049Skin · damagedTHE LEFT HAND INBOARD FLAP LEADING EDGE WAS FOUND DAMAGED. NRC 010-0001:0514-2001/001 00011: REMOVED AFT VANE PER AMM 27-50-03. REMOVED NOSE ASSY AND ROUTED TO SHOP 383 FOR REPAIR WHICH WAS ACCOMPLISHED ON SHOP ORDER PA4968/ WORK ORDER 19567 AND INSTALLED ORIGJan 4, 2019 · N930AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018111206582Lens · missingTHE FIRST EMERGENCY LIGHT IN THE AFT ACCESSORY COMPARTMENT IS MISSING THE LENS COVER. MAINTENANCE HAS RE-INSTALLED THE COVER. LIGHT OPERATIONAL CHECK IS GOOD. (LP #5101298)Nov 11, 2018 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2018091805644Power Supply · inoperativeON A SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERHEAD CEILING EMERGENCY LIGHTS TURNING ON AND THEN OFF. MAINTENANCE REPLACED THE FORWARD TWO EMERGENCY LIGHT POWER SUPPLIES PER AMM 33-51. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMMSep 14, 2018 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2017112008243Lens · missingAFT EXIT DOOR CEILING LIGHT MISSING THE LENS. MAINTENANCE INSTALLED A NEW LENS.Nov 19, 2017 · N930AT · Boeing 717200 · Emergency LightingSDR DALA201706301Skin · delaminatedDURING UNSCHEDULE MAINTENANCE CHECK, THE LT OTBD SPOILER FOUND DELAMINATED.Jun 30, 2017 · N930AT · Boeing 717200 · SpoilersSDR DALA2017042603394Floor Panel · crackedCABIN FLOOR PANEL 223AF IS CORRODED IN SEVERAL AREAS AND CRACKED AT CORNER. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-20-50-01. STOP DRILLED THE CRACK IAW SRM 53-00-00-2R-1. INSTALLED REPAIR DOUBLER IAW SRM 53-00-00-2R-1 FIG 201.Apr 25, 2017 · N930AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017042403350Pan · corrodedCORROSION ON DOOR JAMB PAN AT LOWER CENTER DOOR STOP. BLENDED CORROSION ON ALC DOOR JAMB PAN AT LOWER CENTER DOOR STOP, REMOVED .020" OUT OF .050" ORIGINAL THICKNESS (MAX ALLOWABLE .010"), FOUND TO BE OUT OF LIMITS IAW B717 SRM 53-00-00 TOOL TAG #2737, REPLACEApr 23, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017042303302Floor Support · corrodedUPPER CABIN FLOOR SUPPORTS BETWEEN STA 178 - 202 AT RBL 30-44 ARE CORRODED IN SEVERAL AREAS. REPLACE FLOOR SUPPORT RBL 30.00-44 PER SRM 51-41-02 & DRAWING 9936534.Apr 21, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017042203299Cusp Web · corrodedRIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND UPPER AND LOWER SURFACES OF LIGHTENING HOLES. REPAIRED CUSP WEB AT STA 446 TO 465 IAW SRM 53-00-55-2R-4 SHEET 4.Apr 21, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017042203298Cusp Web · corrodedRIGHT OUTBOARD CUSP HAS CORROSION AROUND RIVETS AND AROUND LOWER SURFACE OF LIGHTENING HOLES AT STA 484 TO 503. BLENDED CORROSION ON CUSP WEB AT FS 484-503R OT .020 REMAINING .010 OUT OF LIMITS IAW SRM 53-00-55. REPAIRED CUSP WEB IAW SRM 53-00-55-2R-4 FIG 215Apr 21, 2017 · N930AT · Boeing 717200 · Fuselage Miscellaneous Structure
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