Boeing 717-200

Service difficulty reports · 18,756

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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 HALA20240212007Bungee · faulted"WHEN LNDG GEAR EXTENDED NOSE GEAR UNSAFE LT. MANUAL GEAR EXTESION PERFORMED. REMOVED LANDING GEAR CONTROL VALVE PER AMM 32-31-01. NEED TO INSTALL REF AMM 32-31-01. (TV 23201) 02/09/2024. INSTALLED LG CONTROL VALVE UP TO STEP 3H PER AMM 32-31-01.. CONTINED INSFeb 9, 2024 · N490HA · Boeing 717200 · Nose/Tail Landing GearSDR 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 DALA2024020801688Sign · damagedTHE FORWARD EMERGENCY EXIT SIGN IS DAMAGED. MAINTENANCE REINSTALLED AND SECURED THE FORWARD EMERGENCY EXIT SIGN. OK FOR SERVICE. (LP #0191155)Feb 7, 2024 · N921AT · Boeing 717200 · Emergency LightingSDR 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 DALA2024020801685Cover · misalignedDURING SERVICE CHECK, THE CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH C/B A11 PULLED. MAINTENANCE FOUND F/A PANEL SWITCH COVER MISALIGNED, CAUSING SWITCH TO NOT GO TO OFF POSITION FULLY. ADJUSTED SWITCH COVER AND OPERATIONAL CHECK WAS GOOD PER B717 AMM 33Feb 7, 2024 · N959AT · Boeing 717200 · Emergency LightingSDR DALA2024031203226Spar · crackedCRACK ON REAR SPAR APPROX XRS 145 AT LH WING. ERA 615453-14 AD REV ORIG SECTION I AND SECTION II ACCOMPLISHED ON NRC 7628 IN TOMX. NEEDS SECTION III ACCOMPLISHED XFRD TO NR #1 ATG WO PO51540620240205. (LP #5518464)Feb 6, 2024 · N985AT · Boeing 717200 · Wing SparSDR 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 HALA20240207006Battery · inoperativeEMER LT. NOT STAY ON. REMOVED AND REPLACED 13 EA CABIN EMERGENCY EXIT LIGHT BATTERIES PER AMM 33-51-03/401. OPS TEST GOOD. OK FOR SVC.Feb 6, 2024 · N486HA · Boeing 717200 · Emergency LightingSDR DALA2024020601580Skin · bentBENT ON EDGE EXTERNAL SKIN AFT UPPER, AFT LOWER, AND BEAM #4 AT SERVICE DOOR L1. SUMMARY OF NRC 00069: EXTERNAL SKIN ON AFT UPPER EDGE AND EDGE OF EXTERNAL SKIN AT BEAM #4 WAS CONFORMED PER B717 SRM-51-20-09-0G. AFT LOWER EDGE OF EXTERNAL SKIN AT SERVICE DOOR Feb 6, 2024 · N997AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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 DALA2024020601578Spar · crackedCRACK ON REAR SPAR LOWER SECTION LH WING AT XRS=214.000. SUMMARY OF NRC 00651: REAR SPAR LOWER SECTION LH WING AT XRS=214.000 WAS REPAIRED PER ERA 615443-14AD REV ORIGINAL. SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615443 ADDED FOR AC 9523. (LP #0188635)Feb 5, 2024 · N964AT · Boeing 717200 · Wing SparSDR DALA2024020601581Holder · shortedSHIP 9518 -SMKE- THE FLIGHT CREW REPORTED VISIBLE SMOKE FROM THE CAPTAIN SIDE CLIPBOARD LIGHT. THE SMOKE STOPPED AFTER ABOUT 10 SECONDS. THE QRH WAS COMPLIED WITH AND THE CREW CONTACTED MAINTENANCE TO PULL THE CIRCUIT BREAKERS. THE FLIGHT CONTINUED TO THE SCHEFeb 4, 2024 · N959AT · Boeing 717200 · Light System WiringSDR 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 DALA2024020601573Pan · crackedCRACKED PAN AND FITTING ON BEAM #4 FWD STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00156: FITTING REPLACED PER B717-200 SRM 51-41-03-0G, 51-41-01-0G, AND 51-41-05-0G. PAN BEAM #4 FWD STOP FITTING AREA AT AFT CARGO DOOR WAS REPAIRED PER PRI 614439-14 REFeb 3, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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 DALA2024020301512Web · crackedCRACK MEMBRANE ON UPPER SURFACE OF CENTER WING STA Y=715 AND -X=44 UNDER RH MIDDLE SEAT TRACK AT WING BOX AREA. SUMMARY OF NRC 00357: MEMBRANE ON UPPER SURFACE OF CENTER WING STA Y=715 AND -X=44 UNDER RH MIDDLE SEAT TRACK AT WING BOX AREA WAS REPAIRED PER PRI Feb 2, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020301511Pan · crackedCRACKED PAN AND FITTING ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR. SUMMARY OF NRC 00154: FITTING WAS FABRICATED PER DWG 3914025 REV C AND PAN ON BEAM #4 AFT STOP FITTING AREA AT AFT CARGO DOOR WAS REPAIRED PER PRI 614439-14 REV 6 AND ERA 614439-14 REVFeb 2, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020301510Frame · crackedCRACK ON MAIN FRAME BTW LONGERON 7 STA Y=1022 AT CPAX. SUMMARY OF NRC 00355: MAIN FRAME BTW LONGERON 7 STA Y=1022 AT CPAX WAS REPAIRED PER ERA 614511-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-614511 ADDED FOR AC 9562. (LP #0184100)Feb 2, 2024 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024020301508Skin · corrodedCORROSION ON INNER SKIN BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00166: CORROSION LEVEL 2. INTERNAL SKIN DOUBLER BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT WAS REPAIRED PER ERA 614961-1Feb 1, 2024 · N997AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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 DALA2024020301506Door Frame · corrodedCORROSION ON DOOR JAMB STA 951 TO STA 994 AT AFT CARGO COMPARTMENT. C2. SUMMARY OF NRC 00071: CORROSION LEVEL 2. PREVIOUS REPAIR SECTION OF DOOR JAMB STA 951 TO STA 994 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LFeb 1, 2024 · N997AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024020101448Longeron · corrodedCORROSION ON LOWER SURFACE LONGERON END STA 360 L26R AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00172: CORROSION LEVEL 2. CLIP LONGERON END STA 360 L26R AT FWD COMPARTMENT (C1) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0181288)Feb 1, 2024 · N997AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024020101447Frame · crackedCRACK ON FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00146: FRAME FORMER STA 1133 AND LONGERON 2LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 1 EXAMPLE A. (LP #0181239)Feb 1, 2024 · N964AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024020101446Angle · corrodedCORROSION WAS FOUND ON LH UPPER CUSP ANGLE (LOWER SKIN) BTW STA Y=200 TO Y=226 FROM X=56 TO X=60 AT PAX CABIN. SUMMARY OF NRC 00571: CORROSION LEVEL 2. LH UPPER CUSP ANGLE (LOWER SKIN) BTW STA Y=200 TO Y=226 FROM X=56 TO X=60 AT PAX CABIN WAS REPAIRED PER B717Feb 1, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020301505Web · crackedCRACKS ON INTERNAL STRUCTURE (WEB) BTW STA Y=1053, -X14 Y53, AND X14 Y53 AT EMERGENCY EXIT DOOR. SUMMARY OF NRC 00255: INTERNAL STRUCTURE (WEB) BTW STA Y=1053, -X14 Y53, AND X14 Y53 AT EMERGENCY EXIT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G PROCEDURE GENJan 31, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020101445Cusp Web · crackedCRACK ON CUSP MEMBRANE ON STA 655 WAS FOUND IN REFERENCE TO CARD 5310-01436-03B STEP 3. SUMMARY OF NRC 00568: CUSP MEMBRANE ON STA 655 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 AND INSTALL CUSP MEMBRANE MUST BE INSTALLED PER CARD 5310-01436-04B STEP 1Jan 31, 2024 · N939AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024020101444Frame · crackedA.D. CRACK OF 0.500 IN ON UPPER RADIUS OF THE FRAME TAB OVERWING FRAME AT STA Y=674.000 LH (REF. CARD 5310-01436-04B). SUMMARY OF NRC 00253: FRAME TAB OVERWING FRAME AT STA Y=674.000 LH WAS REPLACED CARD 5310-01436-03A. ASSOCIATED AA 5310-01436 ADDED FOR AC 95Jan 31, 2024 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024020101443Pan · crackedCRACK ON INTERNAL PAN ON UPPER FWD CORNER AT AFT CARGO DOOR. SUMMARY OF NRC 00087: INTERNAL PAN ON UPPER FWD CORNER AT AFT CARGO DOOR WAS REPAIRED PER ERA 615204-14 REV ORIGINAL SECTION I: REPAIR AND PRI 615204-14 REV 2. ASSOCIATED ERA 14-615204 ADDED FOR AC 9Jan 31, 2024 · N986AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024013101413Battery · inoperativeMAINTENANCE FOUND THE L-1 ENTRY EMERGENCY EXIT SIGN TO BE INOPERATIVE. THE POWER SUPPLY FOR THE EMERGENCY LIGHT BATTERY WAS REPLACED IAW B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4369370)Jan 31, 2024 · N717JL · Boeing 717200 · Emergency LightingSDR DALA2024013101412Angle · corrodedCORROSION ON FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00168: CORROSION LEVEL 2. FWD LOWER ANGLE OF DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7. (LP #0179772)Jan 31, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024121611733Repair · unknownERA 615468-14 SECTION I REPAIR REQUIRES DTE WITHIN 12 MONTHS OF AIRCRAFT RETURN TO SERVICE. ADDED FOR AC 9526. REDEFERRED LOG TO QC, ESTAB MON INSP. ER/A 615468-14 REV A, DTE STAGE 2 AND 3 ACCOMPLISHED ON 11DEC24. ER/A SECTION II FOLLOW-ON INSPECTIONS ARE REQUJan 30, 2024 · N967AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024013001358Cargo Track · corrodedCORROSION ON FLOOR TRACK LH STA Y=889, AFT CARGO WAS REMOVED AND REMAINDER TRACK IS OUT OF LIMITS. SUMMARY OF NRC 00648: CORROSION LEVEL 2. FLOOR TRACK LH STA Y=889, AFT CARGO WAS REPAIRED B717-200 SRM 53-20-52-2R PROCEDURE 4 FIG 201. (LP #0178275)Jan 29, 2024 · N964AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024013001357Skin · corrodedCORROSION ON INNER SKIN NEXT TO HINGE AT FORWARD AIR STAIRWELL DOOR. SUMMARY OF NRC 00127: STAIRWELL DOOR WAS REPLACED PER BOEING 717-200 AMM 52-63-01. (LP #0177811)Jan 29, 2024 · N986AT · Boeing 717200 · Entrance StairsSDR DALA2024013001356Pan · crackedCRACK ON INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD SIDE OF FWD CARGO DOOR. SUMMARY OF NRC 00239: INNER PAN, SETTLEMENT AREA OF STOP FITTING #2 AT FWD SIDE OF FWD CARGO DOOR WERE REPAIRED PER PRI 614520-14 REV 5 AND ERA 614520-14 REV ORIGINAL SECTIONJan 29, 2024 · N964AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024020101442Skin · crackedCRACK AT FWD UPPER CORNER OF R1 DOOR ON FUSELAGE SKIN. REMOVED PAINT AND FASTENER FOR FURTHER EVALUATION PER B717 SRM 51-22-01 AND SRM 51-40-02-06. VERIFIED CRACK PER BHEC AND HFEC INSPECTION, NDTSPM PART 06-10-01.003 AND PART 06-10-01.001. TWO CRACKS MARKED AJan 28, 2024 · N967AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024012901231Longeron Splice · corrodedCORROSION ON LONGERON SPLICE 24L BTW STA Y=889 AND STA Y=908 IN REFERENCE TO NRC 00644. SUMMARY OF NRC 00650: CORROSION LEVEL 2. SPLICE ON LONGERON 24L BTW STA Y=889 AND STA Y=908 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0176297)Jan 28, 2024 · N964AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024012901230Frame · crackedCRACK ON UNDER THE FASTENER OF THE FRAME TAB OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-04C). A.D. A.A. SUMMARY OF NRC 00306: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER CARD 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9562. (LP Jan 28, 2024 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024012901229Doubler · corrodedCORROSION ON DOUBLER STA=908 BTW LONGERON 29LH TO 29RH AT CARGO COMPARTMENT. SUMMARY OF NRC 00535: CORROSION LEVEL 2. DOUBLER STA=908 BTW LONGERON 29LH TO 29RH AT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 FIG 201 AND 51-41-05-0G. Jan 28, 2024 · N986AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024012901228Intercostal · corrodedCORROSION ON INTERCOSTAL OVER STRG 29R AND 28R BTW STA Y=927 TO 946 AT AFT CARGO CPMPARMENT. SUMMARY OF NRC 00271: CORROSION LEVEL 2. INTERCOSTALS OVER STRG 29R AND 28R BTW STA Y=927 TO 946 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-02-0G ANJan 28, 2024 · N985AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024012901232Battery Pack · inoperativeFOUND THE FORWARD ENTRANCE EXIT PATHWAY SIGN GOING INTO COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. LIGHT OPERATION NOW CHECKS GOOD IAW B717 AMM 33-51-18. (LP #5448489)Jan 27, 2024 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2024012901227Cusp Web · corrodedCORROSION ON LH CUSP WEB UPPER AND LOWER BTW STA Y=200 TO Y=294 FROM X=53 TO X=60 AT PAX CAB. SUMMARY OF NRC 00361: CORROSION LEVEL 2. LH CUSP WEB UPPER AND LOWER BTW STA Y=200 TO Y=294 FROM X=53 TO X=60 AT PAX CAB WAS FABRICATED AND REPLACED PER DWG 9936535-3Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024012901226Web · corrodedCORROSION ON WEB (UPPER SURFACE) BTW STA 160-200 AND X=44.5 TO X=55 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB (UPPER SURFACE) BTW STA 160-200 AND X=44.5 TO X=55 AT PAX CABIN FLOOR STRUCTURE WAS FABRICATED AND REPLACED PER B717 Jan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024012901225Floor Support · corrodedCORROSION ON FLOOR SUPPORT (1 EA) (UPPER/ LOWER SURFACE) BTW STA 186-195 ON X=52.5 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00408: CORROSION LEVEL 2. FLOOR SUPPORT (1 EA) (UPPER/LOWER SURFACE) BTW STA 186-195 ON X=52.5 AT PAX CABIN FLOOR STRUCTURE WAS REPLJan 27, 2024 · N964AT · Boeing 717200 · Fuselage Miscellaneous Structure
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