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"

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SDR DALA2016070705144Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB STA Y 546, IN REF CARD 24, ZONE 200. CARD 81, ZONE 200, RT CUSP WEB, STA Y:546 WAS REPAIRED IAW SRM 53-00-55, FIG 216. HFEC INSPECTION WAS ACCOMPLISHED ON RT CUSP WEB STA Y 546, NO CRACKS WERE FOUND AFTER CUTOUT IAW NDT SPMJul 6, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070605109Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 3-14 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jul 6, 2016 · N946AT · Boeing 717200 · Emergency LightingSDR DALA2016070705148Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 13 RT AND 14 RT, STA Y=1074 TO Y=1078, CARD 9, ZONE 200. AREA WAS REPAIRED IAW ER/A 547824-14, REV ORIGINAL. PERFORM EXTERNAL GVI AN REPAIR EVERY 3,000 FLIGHT CYCLCES IAW ER/A 547824-14, REV ORIGINAL SEC II ANJul 5, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016070705147Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 14 RT, STA Y=1086, CARD 10, ZONE 200. AREA WAS REPAIRED IAW ER/A 547824-14, REV ORIGINAL. PERFORM EXTERNAL GVI ON REPAIR EVERY 3,000 FLIGHT CYCLES IAW ER/A 547824-14, REV ORIGINAL, SEC II AND FOLLOW UP WITH LOGJul 5, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016070605108Beam · crackedCRACKS ON BEAM 1 FWD AND AFT EDGE AT FWD ENTRY DOOR. BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201 AND FIG 202 TYPE A. CRACKS OF .650" AND .850".Jul 5, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016070605107Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINKS FUEL TANK ACCESS PLATE NR 520DT. CORROSION ON SETTLEMENT AND COUNTERSINK AREA WAS REMOVED. FUEL ACCESS PLATE NR 520DT AND FOUND OUT OF LIMITS 3 ADJACENT HOLES 0.715", 0.710", 0.710". THEREFORE WAS REPLACED IAW SRM 51-Jul 5, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016070605106Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE, COUNTERSINK, SETTLEMENT AREA, 141AL. CORROSION ON FUEL ACCESS PLATE 141AL, COUNTERSINK AND SETTLEMENT AREA WAS REMOVED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .665", .665", .665". THEREFORE WAS REPLACED IAW SRM 51-10-04 Jul 5, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016070505077Fitting · crackedCRACK ON CLIP BEAM 1 AFT SIDE AT FWD LT OVERWING EMERGENCY EXIT. CLIP WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 9957735.Jul 4, 2016 · N958AT · Boeing 717200 · Emergency ExitsSDR DALA2016070705146Seat Track · corrodedRIGHT SEAT TRACK CORRODED BEYOND LIMITS AT STA 896-902, RBL 22. REPLACED RT SEAT TRACK AT STA 898-1022, RBL 22 IAW SRM 51-41-05, PG 17, STEP 8 AND SRM 51-41-01, STEP 6.Jul 3, 2016 · N960AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2016070300267Pump · faultyHYDRAULIC PRESSURE LOW LIGHT ILLUMINATED AT 19000 FT AFTER LEVEL OFF. RE-PRESSURE DID NOT WORK. R & R NR 1 EDP IAW AMM TASK 29-11-01-000-801. OPS AND LEAK CHECK GOOD.Jul 3, 2016 · N477HA · Boeing 717200 · Hydraulic Pump (Electric/Engine), MainSDR DALA2016070405076Pan · crackedCRACK ON UPPER FWD RING PAN STA Y=756, RT AT PAX CABIN, CARD 29, ZONE 201. UPPER FWD RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L=0.523" HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS FOUND AT TIME OF INSPECTION.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016070405075Pan · crackedCRACK ON UPPER AFT RING PAN STA Y=832 LH AT PAX, CABIN. UPPER AFT RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L =0.510". HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016070405074Pan · crackedCRACK ON LOWER FWD RING PAN STA Y=636 LT AT PAX CABIN, CARD 28, ZONE 201. LOWER RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK L=0.480", HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016070405073Pan · crackedCRACK ON UPPER AFT RING PAN STA Y=851 RT AT PAX CABIN, SM, CARD 25, ZONE 201. UPPER AFT RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. L= 0.420", HFEC WAS PERFORMED ON TRIMMED OUT AREA AND NO CRACKS FOUND AT TIME OF INSPECTION.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016070405072Pan · crackedCRACK ON LOWER FWD T-RING PAN STA Y=655 LT AT PAX CABIN, CARD 27, ZONE 201. LOWER FWD RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. HFEC WAS PERFORMED ON TRIMMED AREA AND NO CRACKS WERE FOUND AT TIME OF INSPECTION, CRACK L=0.450".Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016070405071Pan · crackedCRACK ON LOWER FWD RING PAN, STA Y=636 RT AT PASSENGER CABIN. SM, CARD 30, ZONE 201. LOWER FWD RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. LONG CRACK L= 0.510" HFEC PERFORMED TRIMMED AREA AND NO CRACKS FOUND AT TIME OF INSPECTION.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016070405070Support · corrodedCORROSION ON TEE SUPPORT X=57 FROM STA 203 TO 219, W1, SM, CARD 44, ZONE 200. CORROSION ON TEE SUPPORT X= 57 FROM STA Y=203 TO Y=219 DUE EXCESSIVE DAMAGE WAS REPLACED IAW DWG 9936535, REV CS, SRM 51-41-02, 51-41-05, 51-41-08, 51-30-08.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070405069Angle · crackedCRACKED ANGLE TIP STA Y=120, X=-53, Z=0 AT COCKPIT STRUCTURE. RT SIDE. CARD 27, ZONE 210. ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, 51-41-08, 51-20-09, 51-40-08, 51-10-04, PAR 14, 21, AND DWG 9911559, REV A.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070405068Cusp Web · crackedCRACKED LT CUSP WEB STA, Y=225, X=59 AT PAX CABIN. DAMAGE WAS REMOVED AND CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 216.Jul 3, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070305067Fairing · crackedCRACK ON INBD GEARED TAB PUSH-ROD FAIRING AT RT ELEVATOR SURFACE. CARD 18, ZONE 340. FAIRING WAS STOP DRILLED IAW SRM 51-00-00, FIG 201, SHEET 2 OF 2 AND REPAIRED IAW SRM 55-00-00 FIG 201 SHEET 2 OF 2 DIMENTION CRACK 0.958".Jul 2, 2016 · N958AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2016070305066Floor Support · crackedCRACKED FLOOR SUPPORT ON STA Y=655 X=15 AT PASSENGER CABIN, SM, CARD 71, ZONE 200. NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-41-05, 53-20-51, FIG 1 ID 2, 51-40-08, 51-40-03, PAR 17, AND 51-10-04, PAR 15/21, 37.Jul 2, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071105256Shear Tie · corrodedSHEAR TIE CORRODED BS 1002 BETWEEN LONGERON 29-30L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-02 AND 51-41-05.Jul 1, 2016 · N960AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016070205065Bracket · crackedCRACKED BRACKET TO ATTACH ACTUATOR EYEBOLT WITH ATTACH POINT EYEBOLT, STA XE=49 AT RT HORIZONTAL STABILIZER, CARD 7, ZONE 340. SUMMARY BRACKET WAS REPLACED IAW AMM 27-33-01 AND CMM 27-30-2.Jul 1, 2016 · N958AT · Boeing 717200 · Elevator Miscellaneous StructureSDR DALA2016070205064Web · corrodedCORROSION ON WEB X=-56, RT STA Y=1053 AT PAX CABIN. SM, CARD 60, ZONE 200. DUE EXCESIVE CORROSION, WEB WAS REPLACED IAW DWG NR 9981474, REV L TREATED, PAINTED, AND INSTALLED SRM 51-10-04 PAR 21 & 15; 51-22-01; 51-41-02.Jul 1, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070205063Floor Support · corrodedFLOOR SUPPORT AT STA 200, RBL 10-43 IS CORRODED AT MARKED LOCATIONS IN SIDE CHANNEL. FABRICATED NEW FLOOR SUPPORT IAW SRM 51-40-08 & DWG 9936534. PART BEYOND LIMIT IAW SRM 53-00-00, PG 105 FIG 103. FLOOR SUPPORTS TO BE INSTALLED ON NON-ROUTINE 69007-200-00Jul 1, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070205062Floor Support · corrodedFLOOR SUPPORT AT STA 160, RBL 46-52 IS CORRODED AT MARKED LOCATIONS. FABRICATED NEW FLOOR SUPPORT IAW DWG 9936534 AND SRM 51-40 08, BEYOND LIMIT IAW SRM 53-00-00, PG 105, FIG 103. FLOOR SUPPORTS WILL BE INSTALLED ON 69007-0200-0089. JOB COMPLETE.Jul 1, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070205061Floor Support · corrodedFLOOR SUPPORT AT STA 160-200, RBL 43 IS CORRODED AT MARKED LOCATIONS. FABRICATED NEW FLOOR SUPPORT IAW DWG 9936534 & SRM 51-40-08, BEYOND LIMITS IAW SRM 53-00-00, PG 105, FIG 103. JOB COMPLETE. FLOOR SUPPORTS TO BE INSTALLED ON 69007-0200-0049.Jul 1, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070205060Floor Support · corrodedFLOOR SUPPORT AT STA 180, RBL 43 IS CORRODED AT MARKED LOCATIONS. FABRICATED NEW FLOOR SUPPORT IAW DWG 9936534 AND SRM 51-40-08, BEYOND LIMITS IAW SRM 53-00-00, PG 105, FIG 103. FLOOR SUPPORTS TO BE INSTALLED ON NON-ROUTINE 69007-200-0049.Jul 1, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070205059Floor Support · corrodedSEVERAL CORROSION POINTS ON FLOOR SUPPORT X-44 FROM STA 160 TO 200, W1, SM, CARD 33, ZONE 200. FLOOR SUPPORT X-44 WAS REPLACED IAW SRM 53-10-51 AND SRM 51-41-02, DUE TO EXCESSIVE DAMAGE.Jul 1, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071105255Cusp Web · crackedCUSP WEB CRACKED FROM LIGHTING HOLE OTBD SEAT TRACK BS 661. REMOVED AND REPLACED THE CUSP WEB IAW SRM 53-00-55.Jun 30, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016070105058Shear Tie · crackedCRACKED SHEAR TIE AT BULKHEAD STA 1022 BETWEEN LONGERON 13LT AND 14LT. REPLACED CRACKED FORMER, SHEAR TIE AT FS 1022 BETWEEN LONGERON 13L AND 14L WITH FORMER, SHEAR TIE IAW SRM 51-41-05 AND 51-41-02. APPLIED LOG DECAL IAW DPS 900-5-1, NR 04.Jun 30, 2016 · N960AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR HALA2016063000265Duct · disconnectedF/A REPORTED AFT DOOR HOT TO FEEL. FOUND LEFT PACK DISHCHARGE ELBOW DUCT DISSCONECTED. REATTACHED DUCT RAN PACK, NO LEAK NOTED OK TO CONTINUE SECURITY CHECK GOOD, PACK OP'S CHECK GOOD NO FAULTS NOTED.Jun 30, 2016 · N480HA · Boeing 717200 · Air Distribution SystemSDR DALA2016103107965Seat Track · wornCAPTAIN`S AND FIRST OFFICER'S SEAT TRACKS ARE WORN ON EDGES AND LOWER SURFACE OF T FLANGE. REMOVED WORN AREA FROM CAPTAIN`S SEAT TRACK AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00. FOUND FO SEAT TRACK TO BE CORRODED BEYOND LIMITS AND REPLACED IAW SRM 51-41-Jun 28, 2016 · N920AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016062804986Battery Pack · dischargedDURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 15-19 OF THE CABIN AND THE AFT TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jun 28, 2016 · N939AT · Boeing 717200 · Emergency LightingSDR DALA2016FA0000311Wedge · damagedDURING NON-ROUTINE LINE UNSCHEDULED INSPECTION OF RT SPOILER AFT WEDGE FOUND DAMAGED.Jun 28, 2016 · N924AT · Boeing 717200 · SpoilersSDR DALA2016062804985Cusp Web · corrodedSERVICE DOOR CUTOUT CUSP ANGLE IS CORRODED. REPLACED CUSP ANGLE AT SERVICE DOOR CUTOUT IAW SRM 53-00-55, REPAIR 3. FABRICATED REPAIR DOUBLER.Jun 27, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016062804965Cusp Web · corrodedCUSP MEMBRANE CORRODED AT STA 160-STA 200 AND CRACKED AT STA 133-STA 138 ON RT SIDE. REPAIRED CORRODED CUSP MEMBRANE AT STA 160-STA 200 AND DOUBLER. REPAIRED CRACKED CUSP MEMBRANE AT STA 133-STA 138 IAW ER/A 547484-14 ALSO PRI REV 2, 547484. ASSOCIATED ER/AJun 27, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016062804964Skin · crackedLEFT FUSELAGE SKIN CRACKED APPROXIMATELY .125" AROUND FASTENER HEAD AT STA 1095 JUST ABOVE LONGERON 14L. VERIFIED BY EDDY CURRENT. REPAIR 4H FUSELAGE SKIN CRACK IAW ER/A 545686-14, REV ORIGINAL. ASSOCIATED ER/A 54-568614 ADDED FOR AC 9578.Jun 27, 2016 · N920AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062804963Skin · crackedRIGHT FUSELAGE SKIN CRACKED AT FASTENER HEAD AND BETWEEN 2 FASTENERS, STA 1095 JUST ABOVE LONGERON 14R. VERIFIED BY EDDY CURRENT. REPAIRED RT FUSELAGE SKIN CRACK IAW ER/A 545686-14, REV ORIGINAL. ASSOCIATED ER/A 54-568614 ADDED FOR AC 9578.Jun 27, 2016 · N920AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062804962Cusp Web · crackedLEFT CUSP WEB CRACKED AROUND 3 RIVETS, STA 589, LBL 44.5, VIEWED FROM TOP WITH MIRRIOR. REPAIRED CRACKS AROUND 3 RIVETS AT STA 589, LBL 44.5 IAW SRM 53-00-55, REPAIR 4, FROM 7075-T6 .032 AND 7075-T6 .020 FILLER.Jun 27, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016062600252Smoke Detector · inoperativeCARGO SMOKE TEST DID NOT TEST AT ALL. OPS CHECKED CARGO SMOKE TEST IAW AMM TASK 26-13-01-710-801. FAULT MESSAGE, CARGO SMOKE FWD, APPEARED. TROUBLESHOT IAW FIM TASK 26-13, TASK 803. R & R NR 8 SMOKE DETECTOR IN FWD CARGO IAW AMM 26-13-01. ALL TESTS PASSEDJun 26, 2016 · N483HA · Boeing 717200 · Smoke DetectionSDR DALA2016071905401Intercostal · crackedFORWARD CARGO FUSELAGE STA 636, BL0 AFT ANGLE ON INTERCOSTAL IS CRACKED, MARKED. REMOVED CRACKED END OF INTERCOSTAL AT STA 636, BLO. FABRICATED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLE IAW DWG 9936580, REV B2 AND SRM 51-70-11, REP 1, FIG 201.Jun 25, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016062504914Frame · corrodedFRAME CORRODED STA 832 AT LONGERON 30. FRAME AT STA 832, L30, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS IAW SRM 53-20-07, REPAIR 3. HEAT TREAT REPAIR PARTS 7075-T6 IAW CWO 68433-0018. INSTALLED REPAIR IAW SRM 53-20-07, REPAIR 3Jun 24, 2016 · N920AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016103107963Frame · corrodedFRAME CORRODED BS 870 AT LONGERON 30. BLENDED IAW SRM 53-00-00 AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-20-07 REPAIR 3.Jun 23, 2016 · N920AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016062404913Skin · damagedFUSELAGE SKIN DAMAGE BETWEEN STA 1095 AND STA 1116, L-21L AND L-23L REF EMPOWER NR 35, RII ENTRY, REF NR 35 REPAIRS MADE IAW ER/A 547473-14, REV A. ASSOCIATED ER/A 14-547473 ADDED FOR AC 9562.Jun 23, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404889Repair · crackedNR 2 PYLON REPAIR CRACKED AND CHERRY LOCK BACKED OUT AT FORWARD LATCH, MARKED. REMOVED FWD LATCH ASSY FROM NR 2 PYLON APRON FOR FOM AND REMOVED CRACKED REPAIR. FABRICATED, ALODINED, PRIMED, AND INSTALLED NEW REPAIR DOUBLER. RE-INSTALLED LATCH ASSY IAW SRM 5Jun 22, 2016 · N920AT · Boeing 717200 · Nacelle/Pylon Miscellaneous StructureSDR DALA2016062304866Support Fitting · chafedSUPPORT FITTING FOR PANEL 630HB IS HEAVILY CHAFED IN 2 PLACES, MARKED. PART REMOVED ON JIB CARD 2040-0049. PART FOUND TO BE OUT OF LIMITS IAW SRM 57-00-00, FIG 103. MATCH DRILLED NEW PART IAW SRM 51-40-08 AND INSTALLED NUTPLATES IAW SRM 51-40-02, PAR 4. PAJun 22, 2016 · N920AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2016062304865Skin · dentedFUSELAGE DENT ON LT SIDE, STA 1087 AT L-20L. CW ER/A 547473-14, REV A, FINAL ER/A MATCHES ALL PRI REVISIONS.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062304863Skin · damagedDAMAGE TO EMPENNAGE SKIN STA 1178-1144 FROM LONGERON 3R-9R MULTIPLE LOCATIONS. REPAIRED SKIN IAW ER/A 547582-14, REV ORIGINAL ER/A MATCHES ALL PRIS.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062304862Skin Panel · damagedVERTICAL STABILIZER, RT L/E LOWER MAIN SKIN PANELS DENTED AND GOUGED. REPAIRED SKIN IAW ER/A 547396-14, REV ORIGINAL, ER/A MATCHES ALL PRIS.Jun 22, 2016 · N939AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
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