Boeing 717-200

Service difficulty reports · 18,771

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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 DALA2016012100479Floor Panel · damagedMAIN CABIN FLOOR PANEL, NR 222YF HAS 2 EA DAMAGED COVERS AND 2 EA DAMAGED STIFFENERS, LT AND RT SIDES. REPLACED MAIN CABIN FLOOR PANEL 222YF STIFFENERS, 2 EA AND COVERS 2 EA IAW SRM 51-41-08 AND DWG 9936639, REV P.Jan 20, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016102607662Doubler · corrodedLOWER FUSELAGE ANTENNA INTERNAL DOUBLER IS CORRODED AT FS 212 BETWEEN L229L & LONGERON 30 IN E&E COMPARTMENT. APPLIED TOP COAT ON AREA IAW AMM 51-10-00 701. REMOVED CORROSION FROM INTERNAL DOUBLER STA 212 BETWEEN 629L & L30L IAW SRM 51-10-04. NO LIMITS IN SJan 19, 2016 · N989DN · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016012100482Shear Tie · crackedAFT FUSELAGE BS 1022 BULKHEAD FWD FACE SHEAR TIE IS CRACKED BETWEEN LONGERON 6L AND L7L, MARKED. REMOVED SHEAR TIE AT AFT FUSELAGE FS 1022 BETWEEN LONG 6L TO L7L IAW SRM 51-40-02, LOCATED, DRILLED, AND DEBURRED NEW SHEAR TIE IAW SRM 51-40-08. INSTALLED NEW SJan 19, 2016 · N989DN · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016011900476Handle · dirtyCREW DISCOVERED THAT THE 1L DOOR WAS STUCK CLOSED AND THEY WERE UNABLE TO OPEN IT. THE DOOR HANDLE WAS CLEANED IAW PS 900-1, NR 6. MAINTENANCE OPERATED THE DOOR SEVERAL TIMES AND FOUND ALL OPERATIONS WERE NORMAL.Jan 19, 2016 · N946AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016012000474Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING BATTERY PACK WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jan 19, 2016 · N983AT · Boeing 717200 · Emergency LightingSDR DALA2016012000473Former · crackedAFT ACCESSORY COMPARTMENT BS 1116 BELOW LONG 15L FORMER CRACKED. REMOVED FORMER BS 1116, BELOW LONGERON 15L IAW SRM 51-41-02 LOCATED, DRILLED, AND DEBARRED NEW FORMER IAW SRM 51-40-08 AND DWG 5913596, REV AN. INSTALLED NEW FORMER BS 1116 BELOW LONGERON 15L IJan 19, 2016 · N989DN · Boeing 717200 · Fuselage Main, FrameSDR DALA2016012000472Support · chafedRUDDER L/E PANEL 370GL CENTER MOUNTING SUPPORT IS CHAFED, MARKED. REMOVED DAMAGED SUPPORT AT RUDDER L/E IAW SRM 51-41-02 LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-08 AND DWG 9971306, REV, INSTALLED NEW SUPPORT ON L/E OF RUDDER IAW SRM 51-41-02.Jan 19, 2016 · N989DN · Boeing 717200 · Rudder StructureSDR DALA2016011900475Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jan 17, 2016 · N948AT · Boeing 717200 · Emergency LightingSDR DALA2016012300584Former · crackedLEFT KEEL BEAM FORMER BS 674 CRACKED ON OTBD END. INSTALLED NEW FORMER IAW SRM 51-41-02, 51-41-05 AND DWG 9923453, REV C, REV A. REPLACED KEEL BEAM FORMER BS 674 IAW SRM 51-41-02 AND 51-41-05 COMPLIED WITH ER/A 542797-14, REV O FOR ALL OTHER WORK REQUIRED. AJan 16, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016102607661Panel · corrodedLT KEEL BEAM PANEL BETWEEN STA 715-747 LONG 30 TO OB SIDE OF CONT KEEL EDGE CORRODED. INSTALLED FASTENERS LT KEEL BEAM STA 715-747 IAW SRM 51-41-02. REMOVED CORROSION LT KEEL BEAM STA 715-747 LONG 30 TO OB SIDE OF CANTED KEEL EDGE IAW SRM 51-10-04 C/W NDT UTJan 15, 2016 · N989DN · Boeing 717200 · Fuselage Main, KeelSDR DALA2016011600425Angle · damagedUPPER ANGLE FOUND TO BE DAMAGED INSIDE OF CENTER TANK, FWD OF ACCESS PANEL 141AL CUTOUT BS 676, LBL 22. REPLACED UPPER ANGLE IAW SRM 51-41-05 AND DWG 9919346, REV. W.Jan 15, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011600424Cusp Web · corrodedMAIN CABIN CORRODED ON CUSP WEB CORRODED BETWEEN BS 908 TO 946 RT SIDE. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IN TWO LOCATIONS, BS 908-927 AND BS 927-946. CUT OUT DAMAGED AREAS AND INSTALLED REPAIR TO ENCOMPASS BOTH AREAS IAW SRM 53-00-55, REPAIR 4.Jan 15, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102607660Keelbeam · corrodedLT KEEL BEAM BARREL, BETWEEN STA 715-696 LONG 30 TO OB SIDE OF CANT KEEL EDGE CORRODED. TOPCOATED LT KEEL BEAM BARREL IAW SRM 51-10-04. REMOVED CORROSION LT KEEL BEAM STA 696-715 LONG 30 TO OB SIDE OF CANTED KEEL EDGE IAW SRM 51-10-04. C/W NDT UT INSPECTIONJan 14, 2016 · N989DN · Boeing 717200 · Fuselage Main, KeelSDR DALA2016011800431Pan · corrodedALC DOOR FRAME CORRODED AT LOWER END IN THRESHOLD AREA. REF ORNRC 63165-0800-0014. INSTALLED NEW DOOR PAN IAW SRM 53-20-15.Jan 14, 2016 · N953AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016011400009Tire · damagedRIGHT INBD TIRE TREADING CAME OFF DURING LANDING ROLL OUT. R & R NR 3 MAIN WHEEL TIRE IAW AMM 32-41-01-000-803 & AMM 32-41-01-400-802. ACCOMPLISHED CHECK ON NR 3 MAIN WHEEL TIRE IAW GMM VOL 1, CH 3 1-D AMM 32-42. ACFT OK FOR SERVICE, TIRE PRESSURE OFF 180 PJan 14, 2016 · N485HA · Boeing 717200 · TireSDR DALA2016011500333Floor Support · brokenFLIGHT COMPARTMENT FLOOR SUPPORT ANGLE IS BROKEN AT APPROXIMATELY BS 150, RBL 52. REPLACED FLIGHT COMPARTMENT FLOOR SUPPORT ANGLE APPROXIMATELY RBL 52, STA 150 IAW SRM 51-41-02 AND DWG 9936533, REV CM.Jan 14, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500326Floor Support · crackedMAIN CABIN FLOOR PANEL 222AFF LOWER HAT CHANNEL CRACKED. REPLACED FLOOR PANEL 222AFF LOWER HAT CHANNEL IN MAIN CABIN IAW SRM 51-20-05, DWG 9952521, REV BB, AND PROCESS STANDARD 1.07-100, REV NEW.Jan 14, 2016 · N988DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500325Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN BS 200-265, RBL 24 CORRODED. FOUND TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS IAW SRM 53-20-52, ALLOWABLE DAMAGE 1 AND DWG S00483, REV A. REPLACED SEAT TRACK SECTION IAW SRM 51-41-01.Jan 14, 2016 · N988DN · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016011400273Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES AND AT THE L2 DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Jan 14, 2016 · N947AT · Boeing 717200 · Emergency LightingSDR DALA2016102710191Door Frame · corrodedAFT CARGO, LOWER ENTRY JAMB CORRODED. REMOVED CORROSION PER SRM 53-00-15 FIG. 101. FABRICATED AND INSTALLED NEW SPLICE PLATES PER DWG 5910158. REINSTALLED THRESHOLD AND SEALED PER 51-41-01.Jan 13, 2016 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016012200580Floor Panel · damagedMAIN CABIN FLOOR PANEL 221 AF IS DAMAGED. MAIN CABIN FLOOR PANEL 221AF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50. ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 221AF DIM 36" X 11" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936544, REJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011900471Floor Panel · puncturedMAIN CABIN FLOOR PANEL NR 222ZF HAS A PUNCTURE APPROXIMATELY BS 730, RBL 46. CUTOUT DAMAGED AREA ON MAIN CABIN FLOOR PANEL NR 222ZF, DIM 1.8" X 1.2", FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS, DOUBLER DIM. 4" X 5" IAW SRM 53-20-50, REPAIR 2.Jan 13, 2016 · N988DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011600430Floor Support · corrodedAFT CARGO - SIDE PLATE FLOOR SUPPORT CORRODED AT BS 994, S 28L MARKED. REMOVED CORROSION AFT CARGO SIDE PLATE FLOOR SUPPORT BS 994 S28L, EVALUATED AREA FOUND ORIGINAL MATERIAL .063, MATERIAL REMOVED .015, MATERIAL REMAINING .048 AND IS FOUND TO BE BEYOND LIMIJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011600429Shear Tie · corrodedUPON REMOVAL OF RT KEEL BEAM BARREL FORMER BS 674 FOUND SEVERAL AREAS OF CORROSION ON THE FORMER SHEAR CLIP. REMOVED SHEAR CLIP FROM RT KEELBEAM FORMER BS 674 IAW SRM 51-41-02 FROM SHEAR CLIP AND EVALUATED AREA FOUND ORIGINAL MATERIAL .062", MATERIAL LOSS .0Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016011600427Floorboard · delaminatedMAIN CABIN FLOORBOARD NR 211ATF IS DELAMINATED. FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50, REPAIR 3 AND DWG DWG 9936539, REV AB.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500360Floor Panel · damagedMAIN CABIN FLOOR PANEL 221BF IS DAMAGED. MAIN CABIN FLOOR PANEL 221BF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221 BF DIM 40" X 36" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936545, REV M.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500359Floorboard · delaminatedMAIN CABIN FLOORBOARD 221LF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221LF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221LF DIM 21" X 56" IAW SRM 53-20-50, REPAIR 3. DWG 9936553, REV: C.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500358Floorboard · delaminatedMAIN CABIN FLOORBOARD 211ANF IS DELAMINATED. MAIN CABIN FLOOR PANEL 211 AND FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 211ANF DIM 22" X 29" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936539 REVJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500357Floorboard · delaminatedMAIN CABIN FLOORBOARD 222AEF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222 AEF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222AEF DIM 21" X 41" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936640, REJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500356Floor Panel · damagedMAIN CABIN FLOOR PANEL 221EF IS DAMAGED. MAIN CABIN FLOOR PANEL NR 221EF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221EF DIM 40" X 9" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936549, REV KJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500355Floorboard · delaminatedMAIN CABIN FLOORBOARD, 211ALF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211ALF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 211ALF DIM 40" X 29" IAW SRM 53-20-50, REPAIR 3 AND DWG 993Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500354Floorboard · delaminatedMAIN CABIN FLOORBOARD NR 222GF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 222GF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222GF DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688 Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500353Floorboard · delaminatedMAIN CABIN FLOORBOARD 222ACF IS DELAMINATED. MAIN CABIN FLOOR 222ACF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 222ACF DIM 21" X 41" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936640, REVJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500352Floorboard · delaminatedMAIN CABIN FLOORBOARD 222LF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222LF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 222LF DIM 21" X 76" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500351Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221CF IS DAMAGED. MAIN CABIN FLOOR PANEL 221CF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE. FABRICATED NEW FLOOR PANEL NR 221CF DIM 40" X 12" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936546, REV C.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500341Floor Panel · damagedMAIN CABIN FLOOR PANEL 221DF IS DAMAGED. MAIN CABIN FLOOR PANEL 221DF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 221DF DIM 20" X 36" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, REJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500340Floorboard · delaminatedMAIN CABIN FLOORBOARD NR 222AVF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 222AVF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222AVF DIM 42" X 65" IAW SRM 53-20-50, REPAIR 3 AND DWG 993658Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500339Floor Panel · damagedMAIN CABIN FLOOR PANEL 221FF IS DAMAGED. MAIN CABIN FLOOR PANEL 221FF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 20" X 36" IAW SRM 53-20-50 REPAIR 3 AND DWG 9936585, REV: W.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500338Floorboard · delaminatedMAIN CABIN FLOORBOARD NR 211ASF. IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 222ASF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 211, ASF DIM 11" X 15" IAW SRM 53-20-50, REPAIR 3 AND DWG 9Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500337Floorboard · delaminatedMAIN CABIN FLOORBOARD 211 ARF IS DELAMINATED. MAIN CABIN FLOOR PANEL NR 211 ARF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 211ARF DIM 11" X 15" IAW SRM 53-20-50. REPAIR 3 AND DWG 99Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500336Floorboard · delaminatedMAIN CABIN FLOORBOARD 221 IS DELAMINATED. MAIN CABIN FLOOR PANEL 221KF FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 221KF, DIM 36" X 56" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936552, REV: KJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011500335Floorboard · delaminatedMAIN CABIN FLOORBOARD 222FF IS DELAMINATED. MAIN CABIN FLOORBOARD FOUND TO BE 60 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED A NEW FLOORBOARD IAW SRM 53-20-50. REPAIR 3 AND DWG 9936583, REV: E.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500334Floorboard · delaminatedMAIN CABIN FLOORBOARD 222APF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222APF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222APF DIM 21" X 76" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936585, REJan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500332Floorboard · delaminatedMAIN CABIN FLOORBOARD 222RF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222RF FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL NR 222RF DIM 21" X 76" IAW SRM 53-20-50. REPAIR 3 AND DWG 9936585, Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500331Floor Panel · damagedMAIN CABIN FLOOR PANEL 221JF IS DAMAGED. MAIN CABIN FLOOR PANEL NR 221JF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL DIM 60" X 8" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936551, REV: AN.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500330Floorboard · delaminatedMAIN CABIN FLOORBOARD 223DF IS DELAMINATED. MAIN CABIN FLOOR PANEL 223DF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 223DF DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688, REV: Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500329Floorboard · delaminatedMAIN CABIN FLOORBOARD 222DF IS DELAMINATED. MAIN CABIN FLOOR PANEL 222DF FOUND TO BE 30 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOOR PANEL 222DF DIM 21" X 19" IAW SRM 53-20-50, REPAIR 3 AND DWG 9936688, REV: Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500328Floorboard · delaminatedMAIN CABIN FLOORBOARD 221WF IS DELAMINATED. MAIN CABIN FLOOR PANEL 221WF FOUND TO BE 40 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50, ALLOWABLE DAMAGE 1. FABRICATED FLOOR PANEL 221 WF DIM 21" X 76" IAW SRM 53-20-50, REPAIR 3 AND 9936585, REV: G.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011500327Floor Panel · puncturedAFT CABIN FLOOR PANEL UPPER SKIN IS PUNCTURED AT FS 986 BETWEEN RBL 44 AND RBL 54. REPAIRED AFT CABIN FLOOR PANEL UPPER SKIN AT FS 986, RBL 44-54 IAW SRM 53-20-50, REPAIR 2 AND DWG 9956320, REV: G.Jan 13, 2016 · N989DN · Boeing 717200 · Fuselage Floor PanelSDR DALA2016011400272Former · crackedLEFT KEELBEAM BARREL BS 696-OTBD END OF FORMER CRACKED. DISPLACED BARREL WEB LT KEELBEAM AT BS 696 IAW SRM 51-41-02 AND SRM 51-41-05 TO FOM. REMOVED FORMER IAW SRM 51-41-02 AND SRM 51-41-05. LOCATED, DRILLED, DEBURRED NEW FORMER IAW SRM 51-40-08 AND DWG 9923Jan 13, 2016 · N988DN · Boeing 717200 · Fuselage Main, Frame
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