Boeing 727-225

Service difficulty reports · 4,226

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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 = '727225'
  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 C8GA20090158Bracket · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT WING NR 7 SLAT OTBD SLAT ACTUATOR BRACKET AT WS 629 IS CRACKED. REMOVED DAMAGED STIFFENER, FABRICATED NEW STIFFENER FROM BAC 1503-100145 DIM. 9.2 INCH AND FILLER FROM 7075-T6 .125 INCH DIM 4.5 INCH X Jun 8, 2009 · N801EA · Boeing 727225 · Leading Edge DevicesSDR C8GA20090157Skin · dentedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT ELEVATOR UPPER SURFACE SKIN HAS A DENT AT ES 25, 5 INCH AFT OF SKIN PANEL L/E. DAMAGED AREA WAS REMOVED DIM 1.375 INCH X .750 INCH FABRICATED REPAIR DOUBLER FROM 2024 T3 .032 INCH DIM. 3 INCHES X 2.37Jun 8, 2009 · N801EA · Boeing 727225 · Elevator, Plate/SkinSDR C8GA20090156Skin · dentedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LT ELEVATOR UPPER SURFACE SKIN HAS A SHARP DENT AT ES 25 AND 8 INCH AFT OF SKIN PANEL L/E. DAMAGED AREA WAS REMOVED DIM 3.425 INCH X 2. FABRICATED REPAIR DOUBLER FROM 2024 T3 .032 INCH DIM 3.7 X 5.3 INCH Jun 8, 2009 · N801EA · Boeing 727225 · Elevator, Plate/SkinSDR C8GA20090155Floorbeam · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 17L FLOORBEAM SPLICE IS CRACKED AT STA 620. REMOVED SPLICE PLATE, FABRICATED NEW SPLICE PLATE FROM 2024 T3 .125 INCH DIM. 18 INCH X 9 INCH AND INSTALLED. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVJun 8, 2009 · N801EA · Boeing 727225 · Fuselage Main, Floor BeamSDR C8GA20090154Intercostal · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE INTERCOSTAL LOCATED AT STR 28L BS. 700-720 HAS CORROSION AT BASE. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW FROM 7075 T6 .040 INCH DIM 8.5 INCH X 18.5 INCH AND INSTALLED. NO OTHER DEFECTS NOTED. ACFTJun 8, 2009 · N801EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR C8GA20090153Skin · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LT OTBD FOREFLAP IS CRACKED AT INBD ATTACK CUTOUT. STOP DRILLED CRACK, PERFORMED HFEC INSP FOR CRACK CONTAINMENT NO FURTHER CRACKS. FABRICATED REPAIR DOUBLER FROM 2024 T3 .063 INCH DIM 6.5 INCH X 7 INCHJun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090152Support · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 17L AT STA 700 IS CRACKED AT WEB SUPPORT. REMOVED DAMAGED "T" ANGLE DIM 19 INCHES FABRICATED STR REPAIR FROM BAC1506-1133 7075 T6 DIM 19 INCHES, FABRICATED FWD SPLICE UPPER SECTION FROM 7075 T6 .040 INCHJun 8, 2009 · N801EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR C8GA20090149Hinge · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE L1 DOOR HINGES HAVE OVER SIZED FASTENER HOLES IN THE UPPER AND LOWER HINGES. HOLES WERE OVER SIZED AND PREVENTIVE MODIFICATION COMPLIED WITH SB 727-53A0198. NO OTHER DEFECTS WERE NOTED. AIJun 8, 2009 · N801EA · Boeing 727225 · Fuselage, Door HingeSDR C8GA20090148Web · wornWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE VERTICAL STAB LOWER RUDDER SEAL TO SEAL RUB STRIP IS WORN AT STA. 190.00. DAMAGED WEBS WERE REMOVED, FABRICATED NEW WEB FROM 2024 T3 .032" DIM 15 X 14.5 INCH . INSTALLED NEW WEB AND FABRICJun 8, 2009 · N801EA · Boeing 727225 · Elevator StructureSDR C8GA20090147Support Channel · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE SUPPORT CHANNEL INSIDE THE RT ELEVATOR LOWER PANEL 9406 IS CRACKED. CRACKED SUPPORT WAS REMOVED AND NEW SUPPORT WAS FABRICATED FROM 2024 T3 .032" DIM 2" X 18.25" INSTALLED CHANNEL, NO OTHEJun 8, 2009 · N801EA · Boeing 727225 · Elevator StructureSDR C8GA20090146Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LEFT WING O/B AILERON T/E WEDGE IS DELAMINATED AT THE I/B END. DAMAGED AREA WAS REMOVED DIM 7" X 8". FABRICATED FILLER DIM. 7" X 8" FROM 2024 T3 .012", FABRICATED DOUBLER FROM 2024 T3 .012Jun 8, 2009 · N801EA · Boeing 727225 · AileronsSDR C8GA20090145Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LEFT WING I/B FOREFLAP UPPER GUIDE PLATE ON TOP IS CRACKED. DAMAGED CHAFE STRIP WAS REMOVED, FABRICATED CHAFE STRIP DIA 3" X 11" FROM 301 1/4 HD .016". INSTALLED BONDED REPAIR, NO OTHER DEJun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090144Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING I/B MID FLAP UPPER TRAILING EDGE DELAMINATED IN TWO AREAS. DAMAGED AREAS WERE REMOVED APPROX 4" X 3", FABRICATED FILLER FROM 2024 T3 .016" DIM. 4" X 3" AND DOUBLER FROM 2024 T3 Jun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090143Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING I/B AFT FLAP UPPER EDGE IS DENTED. REMOVED DAMAGE DIM 3/16" X 1.5", APPLIED POTTING COMPOUND, FABRICATED DOUBLER 5" DIA. FROM 2024 T 3 .016" AND INSTALLED HOT BOND REPAIR.Jun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090142Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 12 SPOILER PANEL IS DELAMINATED ON THE I/B UPPER SURFACE. DAMAGED AREA WAS REMOVED, FILLER WAS FABRICATED FROM 2024 T3 .025" DIM 2" X 2", DOUBLER FABRICATED FROM 2024 T3 .025" DIM 5" X Jun 8, 2009 · N801EA · Boeing 727225 · SpoilersSDR C8GA20090141Skin · dented"SUPPLEMENTAL INFORMATION" WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING I/B AFT FLAP O/B UPPER EDGE DENTED. DAMAGED AREA WAS REMOVED 1" DIA, FABRICATED DOUBLER 5" DIA FROM 2024 T3 .016. INSTALLED REPAIR, NO OTHER DEFECTS NJun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090140Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING O/B AFT FLAP IS CRACKED AT THE NR 2 TRACK CUTOUT. DAMAGED AREA WAS REMOVED DIM 1" X 1". FABRICATED REPAIR DOUBLER FROM 2024-0 HEAT TREATED TO T4 .050" DIM 8" X 17". INSTALLED REJun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090139ASkin · dented"SUPPLEMENTAL INFORMATION" WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING O/B AILERON IS DENTED ON THE UPPER T/E WEDGE. DAMAGED AREA WAS REMOVED, FABRICATED DOUBLER FROM 2024 T3 .012" DIM 4" DIA. INSTALLED HOT BOND REPAIR. NOJun 8, 2009 · N801EA · Boeing 727225 · AileronsSDR C8GA20090138Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING NR 7 SLAT I/B TRACK CUTOUT IS CRACKED. STOP DRILLED CRACK, PERFORMED HFEC AND VERIFIED CRACK CONTAINMENT. FABRICATED DOUBLER FROM 2024 T 3 .063" DIM 6" X 6.5" AND INSTALLED REPAJun 8, 2009 · N801EA · Boeing 727225 · Leading Edge DevicesSDR C8GA20090137Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE UPPER FUSELAGE LT SIDE EXTERIOR SKIN AT STA. 720 BETWEEN STR S-4 & S-5 HAS EVIDENCE OF LIGHTING STRIKE. THE LIGHTING BURN WAS DRILLED, HFEC PERFORMED WITH NO DEFECTS NOTED. INSTALLED FASTENJun 8, 2009 · N801EA · Boeing 727225 · Fuselage Main, Plate/SkinSDR C8GA20090136ASkin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING O/B AFT FLAP IS CRACKED AT NR 2 TRACK CUTOUT. CUT OUT DAMAGED AREA DIM 1" X 1". FABRICATED REPAIR DOUBLER FROM 2024 -0 .050". HEAT TREATED TO T4, INSTALLED REPAIR DIM 6" X 5". NJun 8, 2009 · N801EA · Boeing 727225 · Trailing Edge FlapsSDR C8GA20090133ASkin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE UPPER FUSELAGE L/H SIDE EXTERIOR SKIN AT STATION 720 BETWEEN STRINGERS S-4 & S-5 HAS EVIDENCE OF LIGHTING STRIKE. REMOVED DAMAGED AREA, PERFORMED HFEC, AND INSTALLED FASTENER. NO OTHER DEFJun 8, 2009 · N801EA · Boeing 727225 · Fuselage Main, Plate/SkinSDR CA090611007Windshield · failed(CAN) ACFT ENROUTE, IN CRUISE AT FL 380 CAPTAIN`S FRONT WINDSHIELD SHATTERED. ACFT DIVERTED, LANDED WITHOUT INCIDENT. MX DETERMINED OUTER PANE FAILED, WINDOW REPLACED.Jun 3, 2009 · Boeing 727225 · Flight Compartment WindowsSDR C8GA20090075Pump · faultyFLT 720 FROM TOL TO ATL, DURING CLIMB-OUT THE NR 2 ENGINE FUEL FLOW BECAME ERRATIC, THE N1 AND N2 STARTED WINDING DOWN FOLLOWED BY COMPRESSOR STALL. THE NR 2 ENGINE WAS SHUT DOWN, EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT IMay 13, 2009 · N815EA · Boeing 727225 · Engine Fuel PumpSDR DHLA2009743DH665Stringer · corrodedLOWER FUSELAGE FROM BS 1183 TO BS 1193 S-26L WITH CORROSION. REPLACED S-26L SECTION FROM BS 1185 TO BS 1213.25 IAW SRM 51-10-1 PARA 7A.Feb 10, 2009 · N743DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHLA2009743DH618Frame · corrodedLOWER FUSELAGE E/E COMPARTMENT AT BS 460 BETWEEN S-23L AND S-24L FRAME WITH CORROSION. REPAIRED FRAME SECTION SHEAR TIE AT BS 460 BETWEEN S-23L AND S-24L IAW B727 SRM 53-10-4 FIG 13 AND REPLACED SHEAR TIE P/N 69-13293-3 IAW B727 SRM 51-10-1 PARA 7A.Jan 19, 2009 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR DHLA2009743543Seat Track · corrodedCABIN SEAT TRACK CORRODED, BS 950 +9 INCH TO BS 1135, RBL 45. REMOVED, FABRICATED NEW, AND INSTALLED SEAT TRACK SECTION PER B727 SRM 53-10-5 FIG 7 AND 51-10-1.Jan 19, 2009 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHLA2009743544Floorbeam · corrodedCABIN FLOORBEAM AT BS 950F CORRODED ON UPPER FLANGE AT RBL 11. ACCOMPLISHED FLOORBEAM REPAIR PER SRM 53-10-8 FIG 8.Jan 18, 2009 · N743DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHLA2009743542Floorbeam · damagedCABIN FLOORBEAM AT BS 660 HAS DOUBLE DRILLED HOLES AT RBL 62.5. REPAIRED FLOORBEAM AS REQUIRED IN EO COO-2-53-470-08 DATED 12/17/08. REF FAA FORM 8110-3 DATED 12/24/08 AND ASTAR EVA B253-00205 FOR REPAIR APPROVAL.Jan 18, 2009 · N743DH · Boeing 727225 · Fuselage Main, Floor BeamSDR CA090119014Drum · frozenON APPROACH INTO YYZ WHEN FLAPS 30 WAS SELECTED NEEDLES REMAINED IN FLAPS 25 POSITION BAND. "TO LOW FLAPS" AURAL WARNING SOUNDED. MISSED APPROACH WAS EXECUTED. RECTIFICATION TROUBLESHOOTING CARRIED OUT AS PER MM 27-51-000-5. UNABLE TO FAULT. SUSPECT FROZEN DJan 16, 2009 · Boeing 727225 · Trailing Edge Flap Control SystemSDR CA090116003Switch · worn(CAN) ESSENTIAL POWER WAS LOST AT ROTATION DURING TAKE-OFF. SECOND OFFICER WAS UNABLE TO ESTABLISH ESSENTIAL POWER WHEN CYCLED FROM GENERATOR 3, TO GEN 1, TO GEN 2. STANDBY POWER WAS SELECTED. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT OFJan 15, 2009 · Boeing 727225 · AC Power Distribution SystemSDR DHLA2009743541Angle · crackedLT INBD MID FLAP LOWER T/E PANEL ATTACH ANGLE CRACKED AT WBL 106. REPAIRED ANGLE BY SPLICING IN A NEW SECTION PER SRM 51-40-4 FIG 1.Jan 6, 2009 · N743DH · Boeing 727225 · Trailing Edge FlapsSDR DHLA2009743529Strap · corrodedFLOORBEAM STABALIZER STRAP CORRODED, BS 1010 TO BS 1130 AT RBL 25. REMOVED, FABRICATED, AND INSTALLED NEW STABALIZER STRAP IAW SRM 51-10-1 AND 51-30-2.Jan 6, 2009 · N743DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHLA2009743DH557Frame · damagedUPPER FUSELAGE MAIN CARGO CABIN BS 420 BTWN S-16R AND S-17R FUSELAGE FRAME WITH DOUBLE HOLE. REPAIRED FRAME SECTION AT BS 420 BTWN S-15R AND S-17R IAW B727 SRM 51-40-3 FIG 1.Jan 5, 2009 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR DHLA2009743535Frame · damagedFUSELAGE FRAME HAS DOUBLE DRILLED HOLES AT BS 560, STR 14R TO 17R. REMOVED FRAME SECTION. FABRICATED, AND INSTALLED FRAME SECTION PER SRM 53-10-2 FIG 2, 51-30-2, AND 51-10-1.Dec 29, 2008 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR DHLA2009743533Skin · dentedFUSELAGE SKIN DENTED AT BS 950F +14 INCH, BETWEEN STR 28R AND 29R. ACCOMPLISHED DOUBLER REPAIR TO FUSE SKIN PER SRM 53-30-3 FIG 1.Dec 29, 2008 · N743DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHLA2009743531Skin · dentedSKIN DENTED AT BS 1000, BETWEEN STR 28R AND 30. ACCOMPLISHED SKIN REPAIR AS REQUIRED IAW SRM 53-30-1 FIG 1.Dec 29, 2008 · N745DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR FDEA200812235263Indicator · failedNUMBER 2 FUEL GAUGE INDICATED ZERO DURING CRUISE THEN PASSING THROUGH APPROX 12000 FT GAUGE STARTED TO COME UP TO READ FUEL QUANTITY. SUMPED NR 3 TANK. NO WATER FOUND. NO FAULT CODES ON INDICATOR. CLEANED CANNON PLUG ON NR 3 VTO ON FWD SPAR. R&RD NR 3 FUEL Dec 23, 2008 · N469FE · Boeing 727225 · Fuel Indicating SystemSDR DHLA7432009648Attach Fitting · crackedLT WING NR 7 SPOILER ACTUATOR SUPPORT FITTING CRACKED. REPLACED NR 7 SPOILER ACTUATOR SUPPORT FITTING IAW B727 SRM 51-10-1 PARA 7. INSTALLED RIVETS, LOCK FASTENERS, BOLTS IAW B727 SRM 51-30-2 PARA 4B, PARA 7D AND PARA 9B.Dec 22, 2008 · N743DH · Boeing 727225 · Wing, Attach FittingsSDR DHLA2009743548Frame · dentedBS 1030 FRAME DENTED AT STR 26L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 51-40-3 FIG 1.Dec 22, 2008 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR CA081222003Hose · failed(CAN) ON DEPARTURE FROM YVR, WHEN GEAR SELECTED UP, HYDRAULIC `A` SYSTEM FAILED. HYDRAULIC QUANTITY INDICATION 0, HYDRAULIC PRESSURE INDICATION 0. CREW EXTENDED GEAR IN ACCORDANCE WITH FLIGHT MANUAL PROCEDURES. THE AIRCRAFT RETURNED TO YVR, STOPPED ON THE RDec 19, 2008 · Boeing 727225 · Hydraulic System, MainSDR DHLA2008743DH669Floorbeam · damagedUPPER FUSELAGE MAIN CARGO CABIN AT BS 1148 LBL 62 FLOORBEAM UPPER FLANGE WITH DOUBLE HOLE. REPAIRED FLOORBEAM SECTION AT BS 1148 BTWN LBL 22 AND LBL 70 IAW COOPESA EO COO-2-53-502-08 DTD 12/24/08 DOCUMENTED ON FAA FORM 8110-3.Dec 18, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHLA2009743DH655Floorbeam · damagedUPPER FUSELAGE MAIN CARGO CABIN AT BS 1148 RBL 62 FLOORBEAM UPPER FLANGE WITH DOUBLE HOLE. REPAIRED FLOORBEAM SECTION AT BS 1148 BTWN RBL 52 AND RBL 62 IAW EO COO-2-53-502-08 DTD 12/24/08 DOCUMENTED ON FAA FORM 8110-3.Dec 18, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor BeamSDR FDEA200812175187Controller · malfunctionedCABIN PRESSURIZATION CONTROLLER WOULD NOT MAINTAIN CABIN ALTITUDE. CONSTANT CLIMB OF 1500 FT/MIN SETTING OFF CABIN ALT WARNING HORN AT 10000 AND CLIMBING TO 14000 WHILE LEVEL AT FL 250. PERFORMED DECAY CHECK OF ACFT IN REF TO JRH AND DECAY PASSED, SO AS A PRDec 17, 2008 · N467FE · Boeing 727225 · Cabin Pressure ControllerSDR FDEA200812125134Support Bracket · crackedLT WING L/E SLAT ACTUATOR SUPPORT BRACKET CRACKED INBD SIDE AT NR 1 SLAT. REMOVED AND REPLACED NR 1 SLAT STA 390.9 RIB, WEB, AND DOUBLER IAW EA 7-5750-126863.Dec 12, 2008 · N469FE · Boeing 727225 · Wing Miscellaneous StructureSDR FDEA200812115121Bracket · crackedRT WING NR 7 SLAT ACTUATOR MOUNTING BRACKETS BOTH INBD AND OTBD ON WING SIDE ARE CRACKED AT WS 635. REMOVED AND REPLACED INBD AND OTBD NR 7 SLAT ACTUATOR MOUNTING BRACKETS AND STEEL DOUBLERS IAW FEDEX EA 7-5750-126869, WINGS, RT NR 7 SLAT STA 281.4 AND 288.6 Dec 11, 2008 · N469FE · Boeing 727225 · Wing, Attach FittingsSDR DHLA2009743DH570Web · corrodedUPPER FUSELAGE MAIN CARGO CABIN FROM BS 1130 TO BS 1183 BETWEEN LBL 25 AND LBL62 FLOOR WEB WITH DOUBLE HOLES AND CORROSION. REMOVED CORROSION FROM BS 1130 TO BS 1154.75 BETWEEN LBL 25 AND LBL 31 AND FROM BS 1154.75 TO BS 1183 BTWN LBL 25 AND LBL 62 FOUND WITHDec 10, 2008 · N743DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHLA2009743DH569Web · corrodedUPPER FUSELAGE MAIN CARGO CABIN FROM BS 1130 TO BS 1183 BETWEEN RBL 25 AND RBL 62 FLOOR WEB WITH CORROSION. REMOVED CORROSION AND FOUND WITHIN LIMITS AT BS 1130 TO BS 1183 BETWEEN RBL 25 AND RBL 52.5 AND FROM BS 1152.5 TO BS 1183 BETWEEN RBL 52.5 AND RBL62 IADec 10, 2008 · N743DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA200812095117Support · crackedLT WING NR 1 SLAT ACTUATOR RIB SUPPORT INBD SIDE IS CRACKED REPAIRED BY ACCOMPLISHING EA 7-5750-126863 WINGS - LT NR 1 SLAT STA 390.9 ACTUATOR SUPPORT RIB. REPAIR OF DOUBLER CRACKS PER SB 727-57-0130.Dec 9, 2008 · N469FE · Boeing 727225 · Wing Miscellaneous StructureSDR FDEA200812095116Skin · damagedINNER AFT EDGE OF MCD CUTOUT HAS NUMEROUS AREAS DAMAGED BY GILL LINER FASTENERS. REPAIRED BY ACCOMPLISHING EA 7-5310-126861 "FUSELAGE - AD 98-11-03 R1 - SSI 6.19A - P-F MOD MCD CUTOUT LOWER CORNER INNER SKIN, REPAIR OF GOUGE MARKS AT BS 620 S16L - EO 7-5100Dec 9, 2008 · N469FE · Boeing 727225 · Fuselage Main, Plate/Skin
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