Boeing 717-200

Service difficulty reports · 18,756

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '717200'
  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 DALA2024030402931Beam · crackedCRACK ON BEAM #1 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00138: BEAM #1 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 7, REPAIR 7, FIGURE 201. (LP #0225315)Mar 1, 2024 · N935AT · Boeing 717200 · Fuselage Main, 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 DALA2024031103220Skin · damagedFUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER HAS A LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN RH WINDOW BELT AT STA 446-465, WINDOW 12 LOWER FWD CORNER PER ERA 596251-14AD REV A SECTION III TIME LIMITED REPAIR. REPETITIVELY INSPECT THEFeb 29, 2024 · N982AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024022902795Web · corrodedCORROSION ON MEMBRANE STA Y=178 AND BTW X=-2 AND X=-26 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 0551: CORROSION LEVEL 2. MEMBRANE STA Y=178 AND BTW X=-2 AND X=-26 AT PASSENGER COMPARTMENT (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP #02225Feb 28, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022902794Cusp Web · corrodedCORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN. SUMMARY OF NRC 0395: CORROSION LEVEL 2. CORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN WAS REMOVED B717-200 SRM 51-10-04-0G PAR 26 C (1). (UT) THICKNESS MEASUREMENT WAS AFeb 28, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022902793Doubler · crackedCRACK ON HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC: 00120. HANDLE DOUBLER STA Y=396 AT FWD CARGO COMPARMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 52-30-01-2R PROCEDURE 1 REPAIR 1. (LP #0222418)Feb 28, 2024 · N982AT · Boeing 717200 · Cargo/Baggage DoorsSDR 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 DALA2024022802765Frame · crackedCRACK ON FRAME STA Y1037 OVER LONG 17 RH AT CPAX. SUMMARY OF NRC 00409: FRAME STA 1037 OVER LONG 17 RH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0221351)Feb 27, 2024 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024022802764Strip · corrodedCORROSION ON STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 FWD CARGO COMPARTMENT. SUMMARY OF NRC 00625: CORROSION LEVEL 2. STRIP BESIDE RH TIE TRACK BTW STA 332 TO 370 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-08-0G. (LP #0221234)Feb 27, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022802763Cusp Web · crackedCRACK ON CUSP WEB (LOWER AREA) BTW STA 1017 TO STA 1020 AND X=45 AT CPAX. SUMMARY OF NRC 00589: CUSP WEB (LOWER AREA) BTW STA 1017 TO STA 1020 AND X=45 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PRCEDURE 4 REPAIR 4. (LP #0221152)Feb 27, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA20240228010Line · failedL HYDRACLIC QUANTITY LOSS. REMOVED AND REPLACED HYDRAULIC LINES TO "ANTISKID CONTROL VALVE" PER AMM 32-45-11.PER PILOT SHUT-OFF LH SYSTEM PUMPS AT 5QTS.LEAK CHECK AND OPS CHECK PENDING(02/26/24 25002) PRESSURIZATION ON BOTH HYD SYTEM AND CHECK GOOD ,NO LEAK Feb 26, 2024 · N485HA · Boeing 717200 · Hydraulic System, MainSDR DALA2024022602642Door Frame · corrodedEXFOLIATION CORROSION AT AFT CARGO LWR DOOR JAMB FROM STA Y=954 TO Y=996. SUMMARY OF NRC 00020: CORROSION LEVEL 2. AFT CARGO LWR DOOR JAMB FROM STA Y=954 TO Y=996 WAS REPLACED PER B717 SRM 53-20-15-2R REPAIR 7, 51-41-02-0G, AND 51-41-04-0G. (LP #0218389)Feb 25, 2024 · N963AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024022602641Beam · crackedCRACK ON BEAM #2 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00139: BEAM #2 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP #0218077)Feb 25, 2024 · N935AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024022602640Longeron · corrodedCORROSION AT STA 130 APROX AND L30 COMPARTMENT E&E. SUMMARY OF NRC 00225: CORROSION LEVEL 2. LONGERON 30 STA Y=110 TO Y=130 WAS REPLACED PER DWG 5411401 REV DT AND B717-200 SRM 51-41-02-0G. (LP #0217998)Feb 25, 2024 · N963AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024022702692Control Valve · malfunctionedSHIP 9565 -ATB/DE- THE CREW PERFORMED AN AIR TURNBACK AND DECLARED AN EMERGENCY WITH ATC DUE TO A SLAT DISAGREE. THE AIRCRAFT REQUIRED SIGNIFICANT AILERON CORRECTION FOR WINGS LEVEL ATTITUDE. THE QRH WAS COMPLIED WITH, AND THE RESULT WAS A NORMAL SLAT EXTENSIOFeb 24, 2024 · N934AT · Boeing 717200 · Leading Edge Slat Control SystemSDR DALA2024022602643Battery Pack · inoperativeTHE FWD OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5424766)Feb 24, 2024 · N607AT · Boeing 717200 · Emergency LightingSDR DALA2024022602639Cusp Web · crackedCRACK ON LH CUSP WEB STA 716 AND X44/60 AT CAB PAX. SUMMARY OF NRC 00399: CUSP WEB STA 716 AND X44/60 AT CAB PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 (FIG.221). (LP #0216965)Feb 24, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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 StructureSDR DALA2024052105396Pan · unknownPD: PAN ISSUES / CA: REPAIRED PER CMM 52-30-2 OEM REV 35 DATED 11/01/2021 WITH DELTA SUPPLEMENTAL INFORMATION REV 6 DATED 11/08/2021, B717 SRM 52-00-00 REL 65.00, 52-00-01-2R-2 REPAIR 2, 52-30-02-2R-8 FIG 205, 51-20-10-0G, AND 51-20-10-0G.Feb 23, 2024 · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024052105408Pan · crackedPD: OUTER PAN CRACKED AT AFT LOWER STOP. / CA: REPAIRED PER SRM 52-30-02-2R-1 REV 65.Feb 23, 2024 · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022602635Seat Track · corrodedCORROSION ON SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN. SUMMARY OF NRC 00580: CORROSION LEVEL 2. SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN WAS REPAIRED PER B717-200 53-20-52-2R PROCEDURE 5. (LP #0215602)Feb 23, 2024 · N935AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR HALA20240223009Power Supply · inoperativeMULTIPLE CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY (B5-231, B5-119, B5-259 & B5-227) PER AMM 33-51-03. OPS CHECK GOOD. OK FOR SVCFeb 22, 2024 · N479HA · Boeing 717200 · Emergency LightingSDR DALA2024022202463Door Frame · corrodedCORROSION AFT PREVIOUS REPAIR DOUBLER ON FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00195: CORROSION LEVEL 2. NEW DOUBLER ON FWD CARGO COMPARTMENT DOOR JAMB WAS FABRICATED PER B717 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6 AND REPLACED PER SRM 51-41-02-0G AND Feb 22, 2024 · N977AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024022202462Frame · crackedCRACK ON FRAME STA Y1037 OVER LONG 17 LH AT CPAX. SUMMARY OF NRC 00408: FRAME STA Y1037 OVER LONG 17 LH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. PERFORM AN GVI ON FRAME STA Y=1037 OVER LONG 17 LH AT CPAX EVERY "C" CHECK PER B717 SRM 53-20Feb 22, 2024 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024022202461Floorbeam · corrodedCORROSION ON ANGLE OF FLOOR STRUCTURE STA Y=1053 X=20 AT CABIN PAX. SUMMARY OF NRC 00374: CORROSION LEVEL 2. ANGLE OF FLOOR STRUCTURE STA Y=1053 X=20 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0212052)Feb 21, 2024 · N963AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024051605257Trunnion · corrodedLT MLG UPPER STRUT O/B ATTACH LUG HAS CORROSION ON THE AFT FACE. MARKED. SUMMARY SEE NRC 004-0003:3211-4001/015 00016: C/W ERA 615978-14 REV ORIGINAL. VERIFIED PRI AND ERA MATCH. (LP #0209458)Feb 20, 2024 · N899AT · Boeing 717200 · Fuselage, Landing Gear Attach FittingsSDR DALA2024022002327Doubler · corrodedCORROSION ON FWD PREVIOUS REPAIR DOUBLER ON AFT CARGO COMPARTMENT DOOR JAMB PAN. SUMMARY OF NRC 00137: CORROSION LEVEL 2. FWD PREVIOUS REPAIR DOUBLERS ON AFT CARGO COMPARTMENT DOOR JAMB PAN WERE REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. PERFORM GFeb 20, 2024 · N977AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024022002326Frame · crackedCRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA. (FUS) SUMMARY OF NRC 0549: CRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. PERFORM AN EXTERNAL GVIFeb 20, 2024 · N963AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024022002325Frame · crackedA.D. CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00265: CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH WAS REPAIRED PER AMDFeb 20, 2024 · N977AT · Boeing 717200 · Fuselage Main, FrameSDR 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 DALA2024022102375Trunnion · corrodedLT MLG - TRAPEZOIDAL FITTING BUSHING PITTED ON AFT SIDE. MARKED IN RED. SUMMARY SEE NRC 004-0003:3211-4001/014 00015: REPLACED BUSHING PER OHM 57-40-1. (LP #0206822)Feb 18, 2024 · N899AT · Boeing 717200 · Fuselage, Landing Gear Attach FittingsSDR DALA2024022002328Battery Pack · inoperativeTHE OVERWING EMERGENCY LIGHTS STAY ON. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY REF B717 AMM 33-51. BATTERY WAS CHARGED UP. OPERATIONAL CHECK IS GOOD. (LP #5478322)Feb 18, 2024 · N951AT · Boeing 717200 · Emergency LightingSDR DALA2024031403326Trunnion · corrodedTRUNNION MOUNT ATTACH AFT FITTING AFT LUG AFT BUSHING HAS CORROSION. (MARKED) REF NR 013 VISIT ID P682670620231227 AND REPAIRED PER B717 SRM 51-10-04. (LP #0205683)Feb 17, 2024 · N899AT · Boeing 717200 · Fuselage, Landing Gear Attach FittingsSDR DALA2024022002323Cusp Web · crackedCRACK WAS FOUND AT CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00678: CUSP MEMBRANE (LWR SKIN) BTW STA Y=218 AND X=60 APPROX WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 FIG.215. (LP #0206279)Feb 17, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024022002322Floor Support · crackedCRACK ON FLOOR SUPPORT STA 636 X=0 AND Z=-2 AT FWD CC. SUMMARY OF NRC 00309: FLOOR SUPPORT (INTERCOSTAL) STA 636 X=0 AND Z=-2 AT FWD CARGO WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #0205320)Feb 17, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024021602272Cusp Web · crackedCRACK ON RH CUSP WEB (LOWER SURFACE) STA Y=672 X=- 57 AT PASSENGER CABIN. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=672 X=- 57 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND AFTER TFeb 16, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024021602271Cusp Web · crackedCRACK ON RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00518: RH CUSP WEB STA Y=245 X=-60 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ALONG THE CUT OUT EDGES, NO CRACKS WERE FOUND PERFeb 16, 2024 · N982AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024021602270Doubler · corrodedCORROSION ON RH PREVIOUS REPAIR DOUBLERS STA Y=451-464 AND Y=479 (LOWER SURFACE) X=-60 AT PASSENGER CABIN. SUMMARY OF NRC 00524: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER STA Y=451-464 AND Y=479 (LOWER SURFACE) X=- 60 AT PASSENGER CABIN WAS REPLACED PER B717-Feb 16, 2024 · N982AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024021502204Battery · inoperativeTHE TAIL CONE AREA EMERGENCY LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY ASSEMBLY B5-260 BAD. BATTERY ASSEMBLY B5-260 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #5412733)Feb 15, 2024 · N995AT · Boeing 717200 · Emergency LightingSDR DALA2024021502205Display · inoperativeSHIP 9577 -MISC/DE- THE FLIGHT CREW REPORTED ELECTRICAL ISSUES, VIA FAILURE, FCP BLANKING, NAV DISPLAY BLANKING, FLIGHT DIRECTORS NOT WORKING, AND ALL ARE CAUSING UNRELIABLE PRIMARY NAVIGATION. THE QRH WAS COMPLIED WITH AND THE SITUATION STABILIZED ONCE THE EMFeb 14, 2024 · N921AT · Boeing 717200 · Central ComputersSDR 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 DALA2024021301998Power Supply · inoperativeTHE FORWARD OVERWING LOWER EXIT EMERGENCY LIGHTS ON THE LEFT AND RIGHT SIDES ARE INOPERATIVE. MAINTENANCE REPLACED B5-118 BATTERY EMERGENCY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK IS NOW NORMAL AND ALL PANELS ARE CLOSED. (LP #5003415)Feb 13, 2024 · N961AT · Boeing 717200 · Emergency LightingSDR DALA2024021201856Battery Pack · inoperativeDOOR 1L & 1R EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT STA B5-118 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9376629)Feb 12, 2024 · N893AT · Boeing 717200 · Emergency Lighting
Back to Boeing 717-200