N933AT

Service difficulty reports · 176

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 = 'N933AT' 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 DALA2026102305843Skin · crackedFOUND A CRACK INDICATION COMMON TO ONE (1) HOLE ON THE LEADING EDGE SKIN ON THE RHS OF THE VERTICAL STABILIZER, COMPLIED WITH ER/A 613198-14. (1879346) (AIRCRAFT GROUNDED).Oct 22, 2026 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2026102305842Skin · crackedFOUND CRACK ON VERTICAL STABILIZER RHS LEADING EDGE SKIN, COMPLIED WITH ER/A 613198-14. (1879339) (AIRCRAFT GROUNDED).Oct 22, 2026 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2026050502823Spar Cap · not reportedAMOC REQUIRED FOR ERA 583922-14AD REV B. AD 2018-10-08, VERTICAL STAB RH SPAR CAP. REPAIRED PER ER/A 00-583922. (1571590) (AIRCRAFT GROUNDED)Apr 29, 2026 · N933AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2026033002080Cap · crackedCRACKED CAP BS 1178, & LONG 17L, AFT ACCESORY COMPARTMENT. REPAIRED IAW PRI 632618-14. (1514424)Mar 27, 2026 · N933AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2026020900911Clamp · leakingSMOKE AND ODOR IN CABIN, NO PASSENGERS ABOARD, ONLY CREW AND MTC. FOUND EXTERNAL LEAK AT TEE CLAMP BETWEEN GEARBOX AND INLET COMPRESSOR. OPENED PLENUM FOUND INLET CONTAMINATED WITH OIL. CLEANED CONTAMINATION FROM INLET PLENUM, R & R COALESCER BAGS IAW AMM Feb 8, 2026 · N933AT · Boeing 717200 · APU Oil SystemSDR DALA2025101407522Sensor · faultedON THE GROUND ON APU POWER WHEN RT PACK TURNED ON, DID NOT COME ON. SMELLED SMOKE & THEN GOT PACK R FLO DISAG. TURNED SWITCH OFF AND SMELL WENT AWAY. R & R RT AIRFLOW SENSOR REF AMM 21-52. OPS CHK NML NO FAULTS, GOOD AIRFLOW. MEL/PLAC REMOVED. REVERSED M PROct 3, 2025 · N933AT · Boeing 717200 · Cabin Cooling SystemSDR DALA2025082206252Not Reported · no discrepancyWORKING REP CK RH MLG DOOR KEEL BEAM . C/W REP CK PER ER/A 621720-14 (9858048)Aug 16, 2025 · N933AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025081806155Strut · dischargedATB/GEAR- RETURNED ATL DUE TO PSEU FAIL MESSAGE WITH LANDING GEAR INDICATION INCORRECT. GEAR HANDLE UP AND INDICATION SHOWS DOWN. FAULT CLEARED WITH CORRECT INDICATION. RETURNED ATL PRECAUTIONARY. SERVICED NLG STRUT. REPLACED GEAR INDICATION BULBS. OPS NORMALAug 13, 2025 · N933AT · Boeing 717200 · Nose/Tail Landing Gear Strut/AxleSDR DALA2025040802706Defog System · faultedWHEN COCKPIT CREW TURNED ON THE WINSHIELD ANTI-FOG SWITCH, WHILE AT CRUISE, A SHOWER OF SPARKS SHOT OUT OF THE UPPER EDGE OF FIRST OFFICER'S FORWARD FACING WINDOW. THE CREW PULLED CIRCUIT BREAKER X26 10592. MAINTENANCE PERFORMED A VISUAL INSPECTION OF FIRST OFMar 29, 2025 · N933AT · Boeing 717200 · Windshield/Door Rain/Ice RemovalSDR DALA2025021001047Lens · missingTHE FIRST EMERGENCY LIGHT ON CATWALK IN EMPENNAGE IS MISSING THE LENS COVER. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (LP #0803705)Feb 9, 2025 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2024041504429Lens · missingEMERGENCY LENS COVER AT 17CDE MISSING. MAINTENANCE INSTALLED NEW EMERGENCY LENS COVER AT 17CDE PER B717 AMM 33-51. (LP #5874313)Apr 13, 2024 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2024041004264Union · leakingAN EMERGENCY WAS DECLARED WITH ATC DUE TO THE RIGHT HYDRAULIC FLUID QUANTITY DECREASING. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOWN TEE ASSEMBLY. OPERATIONAL AND LEAK CHECKS WERE BOTH GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5300792)Apr 10, 2024 · N933AT · Boeing 717200 · Hydraulic System, MainSDR DALA2024030703129Skin · damagedBOTTOM FWD CORNER OF AFT CARGO DOOR SKIN DAMAGED. REMOVED CARGO (AFT CARGO) PER B717 AMM 52-31. CUT OUT DAMAGE PER B717 SRM 52-00-01-2R. PERFORMED HFEC INSP OF CUT OUT REPAIR AREA PER B717 SRM 52-00-01-2R. NO CRACK INDICATION NOTED. COMPLETED REPAIR PER B717 SMar 2, 2024 · N933AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024022002324Skin · corrodedA.D. RUST IN BARREL NUT AND CORROSION IN BARREL NUT HOLE (HSTAB SKIN) WAS FOUND IN NUT #11 AT RH HSTAB UPPER SIDE, IN REFERENCE NRC 438. SUMMARY OF NRC 00727: HORIZONTAL STABILIZER RH UPPER BARREL NUT HOLE #11 AND LOWER BARREL NUT HOLE #29 WERE REPAIRED PER PRFeb 20, 2024 · N933AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2024021502203Angle · crackedCRACK ANGLE STA 710-715 X=-43 AT CENTER TANK WING UPPER SURFACE AT PAX CABIN (WINGBOX AREA). SUMMARY OF NRC 00320: ANGLE STA 710-715 X=-43 AT CENTER TANK WING UPPER SURFACE AT PAXCABIN WAS REPAIRED PER PRI 615191-14 REV 4 AND ERA 615191-14 REV ORIGINAL, SECTIOFeb 14, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024021502202Beam · crackedCRACKS ON BEAM #1 FWD AND AFT EDGE (INTERNAL STRUCTURE) AT PASSENGER DOOR (L1). SUMMARY OF NRC 00083: BEAM #1 FWD AND AFT EDGE (INTERNAL STRUCTURE) AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7. (LP #0201880)Feb 14, 2024 · N933AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024021402123Unknown · damagedELONGATED HOLES ON AREA TO ATTACH ANCHOR NUT ON SETTLEMENT AREAS OF ACCESS 370CR AT RUDDER LOWER AREA. SUMMARY OF NRC 00455: AREA TO ATTACH ANCHOR NUT ON SETTLEMENT AREAS OF ACCESS 370CR AT RUDDER LOWER AREA WAS REPAIRED PER ERA 615547-14, REV ORIGINAL. MAINTEFeb 14, 2024 · N933AT · Boeing 717200 · Rudder StructureSDR DALA2024021402122Pan · wornWEAR ON EXTERNAL PAN UPPER FWD/AFT CORNERS AT AFT CARGO DOOR. SUMMARY OF NRC 00116: EXTERNAL PAN UPPER FWD CORNER AT AFT CARGO DOOR WAS BLENDED OUT AND MEASURED AS FOLLOW: ORIGINAL THICKNESS OF 0.050" REMAINING THICKNESS.0.048" THEREFORE IT IS WITHIN THE ALLOWFeb 14, 2024 · N933AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024021201855Skin · dentedDENTS ON RH FWD MOVABLE FLAP. SUMMARY OF NRC 00381: DENTS (10 LOCATIONS) ON RH FWD MOVABLE FLAP, #2, #3, #5, #6, #8, #9, & # 10 WERE EVALUATED AND FOUND TO BE WITHIN LIMTS PER B717-200 SRM 57-53-01-1A-1 PAR 3 A (1)(2)(4). DENT #1: O/B=18 IN, T/E=6.700 IN, L=1.Feb 9, 2024 · N933AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024020901764Frame · crackedCRACK ON RH FRAME STA 1037 LONG 14RH AT PAX CABIN. SUMMARY OF NRC 00296: CRACK ON RH FRAME STA 1037 LONG 14RH AT PAX CABIN WAS REPAIRED PER PRI 614871-14 REV 2 AND ERA 614871-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-614871 ADDED FOR AC 9Feb 9, 2024 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024020901763Cap · crackedCRACK ON CAP STA 1022 AND LONG 1. SUMMARY OF NRC 00351: CAP STA 1022 AND LONG 1 WAS REPAIRED PER PRI 615124-14 REV 0 AND ERA 615124-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615124 ADDED FOR AC 9566. (LP #0192767)Feb 8, 2024 · N933AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024020801687Skin · crackedCRACKS (2 EA) ON FUSELAGE SKIN BTW STA Y=1076 AND STA Y=1087 BTW LONG 13R AND LONG 14R AT AFT FUSELAGE. SUMMARY OF NRC 0514: CRACKS (2 EA) ON FUSELAGE SKIN BTW STA Y=1076 AND STA Y=1087 BTW LONG 13R AND LONG 14R AT AFT FUSELAGE. WERE REPAIRED PER PRI 614977-14Feb 8, 2024 · N933AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024020801686Skin · crackedCRACK ON FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00513: FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT AFT FUSELAGE WAS REPAIRED PER PRI 614985-14 REV 3 AND ERA 614985-14 REV ORIGINAL SECTION I: PERMANENTFeb 7, 2024 · N933AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024020801684Frame · crackedCRACK ON CANTED FRAME INTERNAL STRUCTURE Y=1200 REF STGR 17 APROX. SUMMARY OF NRC 00257: CANTED FRAME INTERNAL STRUCTURE Y=1200 REF STGR 17 APROX WAS REPAIRED PER PRI 614980-14 REV 1 AND ERA 614980-14 REV ORIGINAL.Feb 6, 2024 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024020601579Frame · crackedCRACK ON FRAMES 2 EA, STA Y=660 AND 675 OUTBOARD EDGE LH SIDE OF KEEL BEAM AREA. SUMMARY OF NRC 0807: FRAME STA=660 AND FRAME STA=675 OUTBOARD EDGE LH SIDE OF KEEL BEAM AREA WERE REPAIRED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND 51-70-11-2R PROC 1 REPAIRFeb 6, 2024 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024020601577Pan · crackedCRACK ON INTERNAL PAN FWD EDGE ON BEAM #1 AT FWD CARGO DOOR. SUMMARY OF NRC 00103: INTERNAL PAN FWD EDGE ON BEAM #1 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0187095)Feb 4, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020601576Doubler · crackedCRACK ON INTERNAL DOUBLER AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO DOOR. SUMMARY OF NRC 00104: INTERNAL DOUBLER (WEB) AFT EDGE BTW BEAM #1 AND #2 AT FWD CARGO DOOR WAS FABRICATED AND REPLACED PER BOEING DWG 9957664 REV "N", B717-200 SRM 51-41-01-0G, 51-41-02-0Feb 4, 2024 · N933AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024022102376Drag Brace · corrodedCORROSION ON DRAG BRACE BORE (LH TAPER PIN HOLE) AND CORROSION ON LH / RH (2 EA) TAPER PIN AT NLG. DRAG BRACE WAS REMOVED PER B717-200 AMM 32-22-05 000-802. SUMMARY OF NRC 00250: NLG DRAG BRACE ASSY WAS REPLACED PER B717-200 AMM 32-22-05. OPERATIONAL TEST OK. Feb 3, 2024 · N933AT · Boeing 717200 · Nose/Tail Landing GearSDR DALA2024020601575Pan · crackedCRACK ON LOWER EDGE OF EXTERNAL PAN AT FWD CARGO DOOR WAS FOUND IN REF NRC 00098. SUMMARY OF NRC 00788P: LOWER EDGE OF EXTERNAL PAN AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0185876)Feb 3, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020601574Frame · crackedCRACK ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME STA 696 RH AT PAX CABIN. SUMMARY OF NRC 00462: CRACKED FRAME TAB OF THE OVERWING FRAME STA 696 RH AT PAX CABIN WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND 51-41-02-0G IN REFERENCE CARD 5310-01436-Feb 3, 2024 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024020601572Intercostal · crackedCRACK ON INTERCOSTAL BTW BEAMS 4 AND 5 STA Y=180 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00087: INTERCOSTAL BTW BEAMS 4 AND 5 STA Y=180 AT PASSENGER DOOR (L1) WAS FABRICATED AND REPLACED PER DWG 9955763 REV K, B717-200 SRM 51-41-01-0G AND 51-41- 02-0G. (LP #018Feb 3, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020301507Beam · crackedCRACK BEAM NBR 6 (MID SECTION) ON PASSENGER DOOR (L1). SUMMARY OF NRC 00174: BEAM NBR 6 (MID SECTION) ON PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 51-70-11-2R, PROCEDURE 1, REPAIR 1. (LP #0182665)Feb 1, 2024 · N933AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024012901219Fitting · crackedCRACK ON VERTICAL FITTING ON AFT PRESSURE BULKHEAD STA 1053 LONGERON #1 (ABOVE DOOR CUT OUT) AT PAX CABIN. SUMMARY OF NRC 00522: SPRING OF THE ARM ASSEMBLY WAS REMOVED AND INSTALLED PER B717-200 AMM 53-52-02-020-801 AND 53-52-02- 420-801, VERTICAL FITTING ON AJan 25, 2024 · N933AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2024012601171Cusp Web · corrodedCORROSION ON DOUBLER OF LH CUSP WEB UPPER BTW STA Y=389 TO Y=408 AT PAX CAB. SUMMARY OF NRC 00477: CORROSION LEVEL 2. DOUBLER OF REPAIR ON LH CUSP WEB UPPER BTW STA Y=389 TO Y=408 AT PAX CAB WAS REPLACED PER B-717-200 SRM 53-00-55-2R. (LP #0171752)Jan 25, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024012501107Cusp Web · corrodedCORROSION ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=660 APROX AT PAX CABIN. SUMMARY OF NRC 00510: CORROSION LEVEL 2. AREA ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=660 APROX AT PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-55-2R. (LP #0170434)Jan 25, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024012501106Frame · crackedCRACK ON LH FRAME STA 1037 LONG 17LH AT PAX CABIN. SUMMARY OF NRC 00294: LH FRAME STA 1037 LONG 17LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R. (LP #0170333)Jan 25, 2024 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024011900806Cusp Web · crackedCRACKS ON CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN. SUMMARY OF NRC 00376: CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 51-41-02-0G AND 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0160778)Jan 18, 2024 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024010900328Unknown · unknownCORROSION ON REPAIR PLUG ON OUTB SEAT TRACK X=56 LH IN STA Y= 547 AND 610 (2 EA). SUMMARY OF NRC 00604: CORROSION LEVEL 2. PLUG ON OUTB SEAT TRACK X=56 LH IN STA Y=547 AND 610 (2 EA) WERE REPLACED PER B-717-200 SRM 51-41-01-0G AND 53-20-52-2R-1 REPAIR 1. (LP #Jan 8, 2024 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024010500203Unknown · unknown-AD- A SKIN LAYER CRACK WAS FOUND ON THE LEADING-EDGE SKIN ON THE RHS OF THE VERTICAL STABILIZER OF A B717-200. THE CRACK WAS REPAIRED PER ER/A 613198-14. THIS ER/A REQUIRES FOLLOW ON INSPECTION. UPDATED MONITOR LOG THRESHOLD TO ACCOUNT FOR TIME FLOWN SINCE SENov 23, 2023 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023112009531Unknown · unknownALL TAIL COMPARTMENT EMERGENCY PATHWAY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-260 & B5-116 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4368053)Nov 18, 2023 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2023103008882Unknown · unknownFOUR (4) CRACK INDICATIONS NOTED ON RT VERT STAB (MARKED) REF STEP 12 OF AMDS CARD 5530-01048-02 (AD2018-10-08). AFTER SEPERATION OF LAYERS PER AMDS 5530-01048-02, BHEC INSP SHOWS UPPER 3 HOLES OK AND LOWER MARKED HOLE HAS CRACK IN SKIN LAYER ONLY (QC 4031). COct 30, 2023 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023112809766Unknown · unknownAD RELATED. DTE ERA 613198-14 REV ORIGINAL. ERA ISSUED FOR VERT STAB FRONT SPAR REPAIR AT ZFS=43.000, RHS. DAMAGE TOLERANCE EVALUATION REQUIRED ADDL TIME RLTD MON #0078171. DAMAGE TOLERANCE EVALUATION REQUIRED. DTE LOG #0040724 NO LONGER LIMITED TO 30 DAYS. EROct 29, 2023 · N933AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2023021401130Unknown · unknownAFT LOWER CARGO COMPARTMENT LINERS METAL TRANSITION STRIP BENT UP. MCC FCP DEFERRAL TO MEL 25-50-01, FLIGHT CREW PLACARD INSTALLED. LOWER COMPARTMENT LINERS BINS 3-4. INSTALLED SIDEWALL PANELS PUSHED OUT. FOUND PNL 181HF BENT UP AND WILL NEED REPLACED REF IPC Feb 6, 2023 · N933AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023011200228Light · inoperativeTHE EXTERIOR EMERGENCY LIGHTS WERE ON IN THE ARM POSITION AT WAKE UP. MAINTENANCE REPLACED THE EMERGENCY LIGHTS RACK PER B717 AMM 33-51. OPERATIONAL CHECK IS OK. (LP #9624134)Jan 11, 2023 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2022120607806Slide · failedCATERING ATTEMPTED TO OPEN 1L WITHOUT VISUAL CONFIRMATION FROM LEAD FA, AFTER JET WAY PULLED AND DOORS ARMED. THE RAFT FELL AND DID NOT INFLATE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE SLDec 4, 2022 · N933AT · Boeing 717200 · Escape SlideSDR DALA2022102606954Battery · inoperativeDURING THE SERVICE CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHTS TO NOT BE TESTING PROPERLY. THE OVERWING EMERGENCY EVACUATION BATTERY WAS REPLACED PER B717 AMM 33-51. (LP #9586900)Oct 22, 2022 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2022082205657None · noneON WALKAROUND FOUND MISSING PANEL ON UNDERSIDE OF LEFT HAND ELEVATOR. MAINTENANCE INSTALLED A NEW PANEL PER AMM 06-33 B717. (LP #9236464)Aug 19, 2022 · N933AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2022051003226Frame · corrodedCORROSION ON FRAME CHANNEL STA Y=889 BTW LONG 29LH AND 29 RH AT AFT CARGO COMPARTMENT IN REF NRC 00107. SUMMARY OF NRC 00214: CORROSION LEVEL 2, FRAME WAS REPAIRED PER B717 SRM 53-20-07-2R, REPAIR 3. PERFORM A VISUAL INSPECTION, INITIAL AT 25,000 FH AND REPETIMay 8, 2022 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2022050603162Skin Panel · crackedCRACKED UPPER SKIN PANEL TRAILING EDGE STA XRS 111.500 AT LH WING (LW). SUMMARY OF NRC 00030: CRACKED UPPER SKIN PANEL TRAILING EDGE STA XRS 111.500 AT LH WING WAS REPAIRED PER. PRI 599039-14 REV. 0 AND ER/A 599039-14, REV. ORIGINAL, SECTION I: PERMANENT REPAIMay 5, 2022 · N933AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2022050503142Channel · corrodedCORROSION ON FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT. SUMMARY OF NRC 00113: CORROSION LEVEL 2, FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT, WAS REPAIRED PER B717-200 SRM 53-20-07-2R, REPAIR 3. (LP #2223147)May 4, 2022 · N933AT · Boeing 717200 · Fuselage Main, Frame
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