Boeing 717-200

Service difficulty reports · 18,771

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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 DALA2016011400271Web · crackedRT SIDE KEELBEAM BARREL BS 696 OTBD END OF FORMER CRACKED. DISPLACED BARREL WEB FOR FOM , R & R RT SIDE KEELBEAM BARREL FORMER, BS 696 IAW SRM 51-41-02, 51-40-05 AND DWG 9923453, REV A , AB, C REINSTALLED IAW SRM 51-41-02 AND 51-41-05.Jan 13, 2016 · N988DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016011300247Skin · debondedLEFT ALTERNATE STATIC PORT INTERNAL DOUBLER DISBONDED FROM SKIN. REPLACED INTERNAL DOUBLER AND BONDED TO SKIN IAW DWG 5911412. REPLACED INTERNAL DOUBLER AND BONDED TO SKIN IAW DWG 5911412.Jan 13, 2016 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016011300244Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT, OVERHEAD AT ROW 17, AND THE EXIT SIGNS AT THE AFT OVERWING HATCH WERE ALL INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WERE GJan 13, 2016 · N948AT · Boeing 717200 · Emergency LightingSDR DALA2017072305663Skin · damagedDURING C CHECK, MAINTENANCE REPORTED DAMAGE TO THE UPPER EDGE OF THE LOWER FIXED LEADING EDGE PANEL COMMON TO THE ZFS=52 SPLICE STRAP. ON THE PANEL, ALL FASTENER LOCATIONS WERE BADLY OVERSIZED AND SKIN WASHERS HAD WORN INTO THE SURFACE ON THE LT UPPER AND LOWJan 12, 2016 · N995AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016012700650Cusp Web · corrodedCORROSION ON CUSP WEB, BS 208-218, LBL 56 JUST INSIDE L1 DOOR. REF ORNRC 63165-0200-0220, PERFORMED INSPECTION WEB REPAIR AT BS 208-218, LBL 56 IAW SRM 51-70-10, REPAIR 2.Jan 12, 2016 · N953AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500349Shear Tie · crackedAFT FUSELAGE BS 1022, BULKHEAD FWD FACE SHEAR TIE IS CRACKED BETWEEN LONGERON 7 & 8R. REPLACEDTHE SHEAR TIE IAW SRM 51-41-02 AND 51-41-05, DWG 9912243, REV HF.Jan 12, 2016 · N989DN · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016011500347Support · corrodedAFT CARGO COMPT; SIDE PLATE ON FRAME, SUPPORT CORRODED, BS 946 STRINGERS 27 - 28L. REMOVED CORROSION AFT CARGO FRAME SUPPORT BS 946 S28L TO S27L. EVALUATED DAMAGE FOUND ORIGINAL MATERIAL .063" MAT LOSS .020" REMAINING MAT .043" AND IS FOUND TO BE BEYOND SERVIJan 12, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500346Support · corrodedAFT CARGO BAY SIDE PLATE ON FRAME, SUPPORT CORRODED, BS 946 STRINGERS 27 - 28L. REMOVED CORROSION AFT CARGO FRAME SUPPORT BS 946, S28L TO S27L. EVALUATED DAMAGE FOUND ORIG MAT .063", MAT LOSS .020", REMAINING MATERIAL .043" AND IS FOUND TO BE BEYOND SERVICEABJan 12, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500345Former · crackedRT KEEL BEAM BARREL, BS 696 OTBD END OF FORMER CRACKED. REPLACED RT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG NR 9923453, REV A AND C.Jan 12, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016011500343Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT BS 197-207, LBL 58 JUST INSIDE L1 DOOR. REF ORNRC 63165-0200-0217. REPLACED FLOOR SUPPORT AT BS 197-207, LBL SB JUST INSIDE L-1 DOOR IAW SRM 57-41-02, FIG 211.Jan 12, 2016 · N953AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500342Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 218, LBL 48 JUST INSIDE L1 DOOR. REF ORNRC 63165-0200-0219. REPLACED FLOOR SUPPORT WITH NEW SUPPORT BS 218, LBL 48 IAW SRM 51-41-02, FIG 201.Jan 12, 2016 · N953AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016011200006Smoke Detector · activatedAFT CARGO SMOKE ALERT ILLUMINATED INFLT. BOTH BOTTLES DISCHARGED, LOWER CARGO COMP FIRE SUPPRESSION SYS. R & R CARGO COMPARTMENT FIRE EXTINGUISHER CONTAINER 1 AND 2 IAW AMM 26-22-01. PERFORMED CARGO FIRE EXT ADJUSTMENT/TEST NO FAULTS DEFECTS NOTED, OK FOR SJan 12, 2016 · N479HA · Boeing 717200 · Smoke DetectionSDR DALA2016011300246Longeron · corrodedAFT CARGO LONGERON 30 CORRODED AT BS 954. BLENDED CORROSION ON LONGERON 30 AT BS 954 ORIGINAL MATERIAL THICKNESS .125, .063 REMAINING AT DEEPEST POINT. INSTALLED REPAIR IAW SRM 53-00-05, REPAIR 3. WIP: BLENDED CORROSION ON LONGERON 30 AT BS 954 ORIGINAL MATEJan 12, 2016 · N929AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016011200245Door Frame · corrodedFWD CARGO, LOWER ENTRY JAMB CORRODED. REPLACED FWD CARGO LOWER ENTRY DOOR JAM IAW SRM 53-20-15, REPAIR NR 6, ACCESS RESTORED.Jan 12, 2016 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016012100481Fuel Tank · corrodedTHE UPPER LT EXTERNAL SURFACE OF THE CENTER WING FUEL TANK HAS AREAS OF CORROSION FROM BS 696 TO 737, LBL 30 TO FUSELAGE SKIN. AREAS MARKED. REF 63165-0100-0187. BLENDED AND REMOVED CORROSION ON UPPER SKIN IAW SRM 57-10-01. MATERIAL REMOVED .010 IN SKIN IS WIJan 11, 2016 · N953AT · Boeing 717200 · Fuel StorageSDR DALA2016011200196Support Angle · corrodedWING TO BS 813, LONGERON 30 CLIP SUPPORT CORRODED. CORROSION DAMAGE ON WING TO BODY CLIP BS 813, BL 0 FOUND TO BE OUT OF LIMITS, ORIG THICKNESS .156", MATERIAL LOSS .056", MAT REMAINING .100", DIM. 1" X 2" IAW SRM 53-00-00 AND DWG S2914624, REV A. REPLACED CJan 11, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011200195Former · crackedRIGHT SIDE KEEL BEAM BARREL BS 679, OTBD END OF FORMER CRACKED. REPLACED RT KEEL BEAM BARREL BS 679 FORMER IAW SRM 51-41-02 AND DWG 9923453, REV A AND REV C. ACCOMPLISHED A REPAIR TO FORMER TO ACCOMMODATE FLANGE SHORTNESS ISSUE IAW ER/A'S 536322-14, REV 0 ANDJan 11, 2016 · N988DN · Boeing 717200 · Fuselage Main, FrameSDR DALA2016011200194Former · crackedLEFT KEEL BEAM BARREL BS 679 OTBD END OF FORMER CRACKED. REPLACED FORMER AS LT KEEL BEAM BARREL BS 679 IAW SRM 51-41-02 AND DWG 9923453, REV C AND REV A. ACCOMPLISHED A REPAIR TO FORMER TO ACCOMMODATE FLANGE SHORTNESS ISSUE IAW ER/A 536323-14, REV 0 AND REV Jan 11, 2016 · N988DN · Boeing 717200 · Fuselage Main, FrameSDR DALA2016011200193Support Frame · corrodedRT WING TO BODY FAIRING SUPPORT FRAME BS 851 HAS CORROSION UNDER NUT CLIPS. CORROSION DAMAGE ON RT WING TO BODY FAIRING SUPPORT FRAME BS 851 FOUND OUT OF LIMITS, ORIG THICKNESS .050", MATERIAL LOSS .036", MATERIAL REMAINING .014" DIM 12" X 1" IAW SRM 53-00-00 Jan 11, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011100197Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jan 10, 2016 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2016011100192Floor Panel · crackedCOCKPIT FLOOR PANEL 211AKF CRACKED. CUT OUT DAMAGED AREA OF COCKPIT FLOOR PANEL 211AKF DIM 2.5" X 1.5" AND INSTALLED A REPAIR IAW SRM 53-10-50 AND 53-10-50, REPAIR 1. DOUBLER DIM. 3.6" X 2.0" CRACK DIM. 1.0".Jan 10, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011100191Cap · crackedLEFT ELEVATOR OTBD END, T/E END CAP CRACKED. REPLACED LT ELEVATOR OTBD END T/E END CAP IAW SRM 51-41-02 AND DWG 5910412, REV DS CRACK DIM .750".Jan 10, 2016 · N988DN · Boeing 717200 · Elevator StructureSDR DALA2016011100190Skin · delaminatedRUDDER UPPER AFT END DELAMINATED. REPAIRED RUDDER UPPER AFT END DIM 4" X 4" IAW SRM 55-00-01, REPAIR 2.Jan 10, 2016 · N988DN · Boeing 717200 · Rudder, Plate/SkinSDR DALA2016011100177Seat Track · damagedMAIN CABIN SEAT TRACK HAS SCRATCHES AND GOUGES BETWEEN BS 899- BS 1022, RBL 24. SEAT TRACK SECTION BS 899-1022, RBL 24 FOUND TO BE OUT OF LIMITS DUE TO SCALLOP DAMAGE, ORIGINAL THICKNESS .460", MATERAL LOSS .060", MATERIAL REMAINING .400" IAW SRM 53-20-53 ANDJan 10, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102607664Fitting · not reportedGIRT BAR FITTING MOUNT. SEE NR FOR ADDITIONAL INFORMATION 027-0015:5310-2005/004 00112. REPLACED FITTINGS PER DWG 3936190.Jan 9, 2016 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500350Former · crackedRT KEELBEAM BARREL BS 715 OTBD END OF FORMER CRACKED. REPLACED RT KEELBEAM FORMER IAW SRM 51-41-02 AND 51-41-05.Jan 8, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016011400269Stringer Splice · corrodedBS 958-974 S30 SPLICE IS CORRODED. MARKED, REF ORNRC 63165-0100-0037, REPLACED SPLICE IAW SRM 51-41-05.Jan 8, 2016 · N953AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016010900189Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222AEF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222AEF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 41" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV. D.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900188Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222DF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688, REV H.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900187Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 211ANF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 22" X 28" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936651, REV U.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900186Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222ACF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222ACF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 21" X 41" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV D.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900185Floor Panel · delaminatedMAIN CABIN FLOOR PANEL NR 222ABF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 22" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REV D.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900184Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221AF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221AF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 36" X 11" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936544, REV G.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900183Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221EF IS DELAMINATED. MAIN CABIN FLOOR PANEL FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 40" X 9" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936549, REV K.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900182Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 211AQF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211AQF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 11" X 9" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936537, REV AG.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900181Floor Panel · delaminatedMAIN CABIN FLOOR PANEL NR 222FF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222FF FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 21" X 38" IAW SRM 53-20-50, REPAIR 3 AND DWG NR 9936583 REV E.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900180Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222AAF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222AAF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 22" IAW SRM 53-20-50, REPAIR 3 AND DWG NR 9936640, REV Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900179Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 22GF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222GF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 21" X 19" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936688, REV H.Jan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010900178Floor Panel · delaminatedMAIN CABIN FLOOR PANEL NR 211ARF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ARF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 15" X 9" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936537, RJan 8, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500348Shear Tie · crackedFS 1022 BULKHEAD TO SKIN AFT SHEAR TIE IS CRACKED BETWEEN LONGERON 13R AND L14R MARKED. REPLACED FS 1022 BULKHEAD TO SKIN AFT ATTACHING SHEAR TIE BETWEEN LONGERON 13R AND 14R IAW SRM 51-41-05 AND DWG 9912243, REV JS.Jan 7, 2016 · N989DN · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016011500344Support Bracket · crackedRT KEELBEAM BARREL, BS 715 SUPPORT BRACKET ASSY CRACKED. REPLACED RT KEELBEAM SUPPORT BRACKET BS 715 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923454, REV F.Jan 7, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011400270Stringer Splice · corrodedBS 927- 946, S30 & SPLICE IS CORRODED. REPLACED THE STRINGER SPLICE IAW SRM 51-41-05.Jan 7, 2016 · N953AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016010800098Floor Support · corrodedMAIN CABIN BETWEEN BS 149-200, LBL 8 FLOOR SUPPORT CORRODED. REMOVED CORROSION FROM MAIN CABIN FLOOR SUPPORT BS 149-200, LBL 8, WITH 100 PERCENT MATERIAL LOSS ORIGINAL MATERIAL .125". R & R WITH NEW FLOOR SUPPORT IAW SRM 51-41-05, 51-41-02, AND DWG 9936534, Jan 7, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA1621279570Skin · crackedFUSELAGE SKIN BS 1087 AND L-14R. CRACK REPAIR.Jan 6, 2016 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016011600428Cusp Web · corrodedCORROSION ON RT SIDE CUSP WEB AND CLIPS BS 389 - 427. REMOVED CORROSION IAW SRM 53-00-55, PG 101. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR IAW SRM 53-00-55, REPAIR NR 4.Jan 6, 2016 · N953AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016010700092Floor Support · corrodedMAIN CABIN FLOOR SUPPORT CORRODED, BS 145, RBL 44. CORROSION DAMAGE ON FLOOR SUPPORT IN THE MAIN CABIN BS 145, RBL 44 FOUND TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS, ORIGINAL THICKNESS .070". DIM.1" X 3" IAW SRM 53-00-00 AND DWG S2929169, REV. B. Jan 6, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016010600091Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED BETWEEN BS 589-899, RBL 54. THE SEAT TRACK WAS FOUND OUT LIMITS DUE TO SCALLOP DAMAGE. REPLACED THE SEAT TRACK IAW SRM 51-41-01 AND AMM 53-22-01.Jan 5, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016010500090Floor Panel · delaminatedMAIN CABIN FLOOR PANEL NR 221BF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 221BF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM. 40" X 36" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936545, REVJan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010500089Floor Panel · delaminatedMAIN CABIN FLOOR PANEL NR 221JF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221JF FOUND TO BE 30PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL IAW SRM 53-20-50, REPAIR 3 AND DWG 9936551, REV AN.Jan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016010500088Floor Panel · delaminatedMAIN CABIN FLOOR PANEL NR 221DF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 221DF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 36" X 20" IAW SRM 53-20-50, REPAIR 3 AND DWG NR 9936547, RJan 4, 2016 · N988DN · Boeing 717200 · Fuselage Floor Panel
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