N989DN, cancelled Mar 1, 2025

Service difficulty reports · 79

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 = 'N989DN' AND deregistration_id = 'N989DN-2025-03-01'
  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 DALA2019120407052Release Mech · out of positionTAILCONE RELEASE CAM MECHANISM IS CLOCKED INCORRECTLY. NRC 001-0310:5300-2004/015 00218: RECLOCKED CAM REF AMDS CARD 5352-4002 TAILCONE INSTALL. (LP #1377133)Nov 26, 2019 · N989DN · Boeing 717200 · Aerodynamic FairingsSDR DALA2019112836950Skin · corrodedCORROSION AFT CARGO THRESHOLD DOOR PAN AND LOWER SKIN DOOR CUT OUT. NRC 001-0371:5231-2002/002 00002: COMPLIED WITH ER/A 582992-14 REV O. (LP #1371567)Nov 22, 2019 · N989DN · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019111906760Pan · corrodedCORROSION WAS FOUND ON THE AFT CARGO DOOR JAMB PAN. MAINTENANCE REPLACED THE LOWER DOOR JAMB PAN SECTION REF B717 SRM 53-20-15-2R PROCEDURE 7. CORROSION LEVEL 1. (LP #1365811)Nov 18, 2019 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019101005821Lens · missingTHE AFT DOOR EMERGENCY EXIT LIGHT DIFFUSER COVER IS MISSING. MAINTENANCE LOCATED THE LENS AND RESECURED IT. SYSTEM IS NOW OK FOR SERVICE. (LP #6567004)Oct 10, 2019 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2019100105611Battery Pack · inoperativeTHE RH OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE RH OVERWING EMERGENCY EXIT LIGHT BATTERY IAW B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #6172176)Oct 1, 2019 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2019031901824Battery · dischargedTHE EMERGENCY LIGHTS AT ROWS 15-19 ARE INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE EMERGENCY LIGHT BATTERY POWER SUPPLY AND BATTERY PER AMM 33-51-03. (LP #5291341)Mar 19, 2019 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2018022001002Spar Cap · damagedVERTICAL STABILIZER LEFT FRONT SPAR CAP DAMAGED, BELOW ZFS 52.267. REPAIRED THE SPAR CAP IAW ERA 565658-14AD, REV ORIGINAL.Feb 19, 2018 · N989DN · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017060504514Frame · crackedFRAME 1225 CRACKED AT TAIL CONE ALIGNMENT PIN 7 O'CLOCK POSITION. REMOVED DAMAGED AREA REF 497316-14MA. MANUFACTURED DOUBLER AND DRILLED REF 497316-14MA. INSTALLED REPAIR PER RI 559273-14.Jun 4, 2017 · N989DN · Boeing 717200 · Fuselage Main, FrameSDR DALA2017052304108Light · contaminatedOVERWING AISLE OVERHEAD EMERGENCY EXIT SIGN PARTIALLY OBSCURED. REMOVED DEBRIS FROM INSIDE BOTH LENS, OPS CHECKED GOOD.May 23, 2017 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016073105683Connector · failedTHE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE FOUND A FAILED CONNECTOR IN THE WIRE HARNESS FOR THE OVERWING LIGHTS AND REPLJul 29, 2016 · N989DN · Boeing 717200 · Light System WiringSDR DALA2016073105681Power Supply · unknownTHE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY AT P1-119 AND THE FUNCTIONAL CHECK OF TJul 29, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016072705623Switch · intermittentTHE PILOT REPORTED THAT SOME OF THE EMERGENCY LIGHTS IN THE AIRCRAFT HAD ILLUMINATED UNCOMMANDED. MAINTENANCE REPLACED AN INTERMITTENT EMERGENCY LIGHT SWITCH S1-177 IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jul 27, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016072705588Light · malfunctionedTHE F/A REPORTED THAT THE EEPL AT THE LOWER SIDEWALL OVERWING AND THE TAIL EXIT LIGHTS HAD ILLUMINATED UNCOMMANDED DURING FLIGHT. MAINTENANCE CYCLED THE EEPL SWITCH IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jul 26, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016041103477Light · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE LT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.Apr 5, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016030401627Frame · crackedUPPER RADIUS BS 696 OF OVERWING FRAME TAB RT CRACKED. REPLACED FRAME AT RT BS 696 IAW SRM 51-41-02, 51-41-05, DWG SR95530013, REV: A, PN SA95530034-9.Mar 3, 2016 · N989DN · Boeing 717200 · Fuselage Main, FrameSDR DALA2016022201273Vane · puncturedRIGHT WING, INBD FLAP VANE, INBD END HAS A PUNCTURE HOLE. REMOVED DAMAGE ON RT WING INBD FLAP VANE INBD END IAW SRM 57-53-01 REPAIR NR 1. MATERIAL REMOVED .75" DIA CIRCLE. FABRICATED .75" FILLER FROM 7075-T6 BARE .016", FABRICATED 11.5" X 4.25" DOUBLER FROMFeb 21, 2016 · N989DN · Boeing 717200 · Trailing Edge FlapsSDR DALA2016102807812Cargo Track · corrodedFWD CARGO BAY. CARGO TRACK CORRODED AT BS 427 - 655. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE BEYOND LIMITS IAW SRM 53-20- 52. REPLACED THE CARGO TRACK IAW SRM 53-20-52 AND DWG 5965411 REV AW.Feb 20, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016021901246Longeron · damagedAFT CARGO COMPARTMENT CENTER LONGERON 30 HAS CHIPPED PAINT, POSSIBLE LIGHT CORROSION FRAME BS 908. REMOVED CORRODED IAW SRM 51-10-04 AT AFT CARGO BS 908, L30. EVALUATED AND FOUND ORIG .093" LOSS .040" REM .053" OUT OF LIMITS IAW SRM 53-00-00 REMOVED, FABRICAFeb 18, 2016 · N989DN · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016102707774Cargo Track · corrodedAFT CARGO BAY, CARGO TRACK CORRODED BS 813 TO 1028 S26L. REMOVED CORROSION IAW SRM 51-10-04. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 AND 51-30-07 AND DWG 5956331 REV BS. REPLACED FWD CARGO TRACK IAW DWG 5956331 REV BS & BE.Feb 17, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016021802609Duct · dentedAFT ACCESSORY COMPARTMENT, GROUND AC DUCT LOWER SIDE HAS DENT.Feb 17, 2016 · N989DN · Boeing 717200 · Air Distribution SystemSDR DALA2016021801685Slat Track · gougedRIGHT WING FIXED L/E INBD SIDE OF SLAT TRACK NR 2 HAS GOUGE ON DOUBLER. ASSOCIATED ER/A 14-542808 ADDED FOR AC 9589. REPLACED EXISTING REPAIR AT RT WING FIXED L/E INBD SIDE OF TRACK NR 2 SLAT IAW SRM 51-40-02 AND COMPLIED WITH ER/A 542808-14, REV: ORIGINAL. Feb 17, 2016 · N989DN · Boeing 717200 · Leading Edge DevicesSDR DALA2016021501050Cargo Track · corrodedAFT CARGO BAY CARGO TRACK AT BS 813 - 1028, CORRODED, REMOVED CORROSION IAW SRM 51-10-04 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, FIG 101 & 51-30-07, FIG 18. REPLACED THE CARGO TRACK IAW SRM 51-41-01, 51-41-02, AND DWG 59366 63, REV: W.Feb 1, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016031501960Seat Track · damagedMAIN CABIN SEAT TRACK HAS CORROSION, SCRATCHES AND GOUGES BETWEEN BS 237-589, RBL 22. REPLACED MAIN CABIN SEAT TRACK AT RBL 22, FS 237-589 IAW SRM 51-41-01. DAMAGE REMOVED IAW SRM 53-20-52. ORIGINAL MATERIAL 0.100", MATERIAL REMOVED 0.060", MATERIAL REMAININGJan 29, 2016 · N989DN · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016013001039Cusp Web · crackedMAIN CABIN CUSP WEB CRACKED AT LT BS 674 AND 696 BETWEEN LBL 44 -54. CUT OUT DAMAGE, FABRICATE AND INSTALLED CUSP WEB 7075-T6 .020, 2 EA SPLICES 7075-T6 .032 IAW SRM 51-41-02 AND 53-00-55, FIG 223.Jan 29, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016013000746Angle · crackedAFT ACCESSORY COMPARTMENT BS 1152 HAS CRACKED ANGLE L2R. REPLACED ANGLE IAW SRM 51-41-05 AND DWG 9911860, REV L.Jan 25, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102707768Floorbeam · corrodedBS 200 FLOORBEAM IS CORRODED BETWEEN RBL 44 & 52. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53- 00-00. THE FLOORBEAM WAS REPLACED IAW DWG 9936534 REV BW & SRM 51-41-02.Jan 24, 2016 · N989DN · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2016012400589Former · corrodedLEFT KEEL BEAM BARREL, BS 715, OTBD END CORRODED FORMER. REPLACED LT KEELBEAM FORMER BS 715 IAW SRM 51-41-05, DWG 9923454, REV: F. REMOVED CORROSION & EVALUAED DAMAGE ORIGINAL MATERIAL .063 REMAINING .000 AND IS OUT OF LIMITS IAW SRM 53-00-00.Jan 23, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016012500592Former · crackedLEFT KEELBEAM BARREL BS 696, OTBD END OF FORMER CRACKED. REPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.Jan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016012400591Longeron · crackedAFT ACCESSORY COMPARTMENT, BS 1133, LONG 2R CRACKED. REMOVED EWIS PROTECTION FROM WORK AREA IAW SWPM 20-10-10. CUTOUT DAMAGED AREA AT AFT ACCESSORY COMPARTMENT BS 1133, LONG 2R, DIM 15" IAW SRM 20-10-10, FABRICATED, LOCATED, AND DRILLED LONGERON SECTION FROMJan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016012400590Former · not reportedREPLACED LT KEELBEAM FORMER BS 696 IAW SRM 51-41-02 AND 51-41-05 AND DWG 9923453, REV C, REV A.Jan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016012400587Door Frame · crackedCRACKED DOOR LANDING AT FWD OTBD CORNER OF GROUND CONDITIONED AIR SUPPLY DOOR CUTOUT. REMOVED DOOR ASSY FOR CONDITIONED AIR GROUND CONNECTION IAW SRM 51-41-01. REMOVED DOOR LANDING IAW SRM 51-41-02. REMOVED AIR GROUND CONNECTION IAW SRM 51-41-02. FABRICATED Jan 22, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR DALA2016012400586Angle · corrodedFWD GALLEY SERVICE DOOR LOWER JAMB AREA, Z-ANGLE IS CORRODED FWD OF RBL 54 SEAT TRACK AT FS 202. REMOVED CORROSION FWD GALLEY GALLEY SERVICE DOOR LOWER JAMB AREA "Z" ANGLE FWD OF RBL 54, SEAT TRACK AT FS 202 IAW SRM 51-10-04. EVALUATED AREA AND FOUND ORIG MAJan 21, 2016 · N989DN · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016012400585Former · crackedAFT ACCESSORY COMP BS 1116 BELOW LONGERON 15R FORMER CRACKED. REPLACED FORMER BS 1116 BELOW LONGERON 15R IAW SRM 51-41-02.Jan 21, 2016 · N989DN · Boeing 717200 · Fuselage Main, StructureSDR 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 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 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 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 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 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 Panel
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