Boeing 727-2Q9

Service difficulty reports · 830

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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 = '7272Q9'
  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 DHL9774007CDoor · crackedAT C-CHECK, FORWARD CARGO DOOR FLANGE BENT BY UPPER LATCH ROLLER, BENT AND CRACKED BY LOWER ROLLER. STRAIGHTENED OUT BENT AFT FLANGE PER SRM 51-40-1 AND STOP DRILLED CRACK, HFEC STOP DRILL, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 3 BY 1.125.Jan 3, 1997 · N740DH · Boeing 7272Q9 · Cargo/Baggage DoorsSDR DHL9774002CClip · corrodedAT C-CHECK, FWD CARGO STRINGER AT STA 560, STRINGER TO FRAME CLIP CORRODED. REPLACED CLIP PER SRM 51-10-1, 5 BY 1.375 BY 1.375 BY .875.Jan 3, 1997 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9774022CPlenum · corrodedAT C-CHECK, CORROSION ON UPPER WALL OF RIGHT RAM AIR PLENUM CHAMBER 18 INCHES FROM AFT END. SHOT PEENED DAMAGED AREA, COLD WORKED FASTENER HOLES, INSTALLED DOUBLER REPAIR PER SRM 57-30-3, 14' BY 4' AND 11' BY 4.Jan 2, 1997 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9774017CFrame · crackedAT C-CHECK, FWD CARGO FRAME IS DENTED AND CRACKED AT STA 540 RBL 9. STOP DRILLED CRACK, HFEC CRACK, ENDS IN STOP HOLE. INSTALLED FRAME REPAIR PER SRM 53-10-4, 14 BY 3.Jan 2, 1997 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL9774012CSkin · delaminatedAT C-CHECK, RIGHT ELEVATOR TAB IS DELAMINATED ON BOTTOM SKIN BETWEEN OUTBOARD BOB WEIGHTS. INSTALLED BONDING REPAIR PER SRM 51-40-6, 7 BY 4. NO BALANCING REQUIRED PER SRM 51-80-7.Jan 2, 1997 · N740DH · Boeing 7272Q9 · Elevator, Tab StructureSDR DHL9774003CSkin · gougedAT C-CHECK, FUSELAGE SKIN IS GOUGED AT STA 1030 AND STR 23 RT. CUT OUT DAMAGED AREA PER SRM. INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 2.25 BY 3.5.Jan 2, 1997 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL9774021CSkin · corrodedCORROSION ON INTERCOSTAL AND WATER DRAIN VALVE AREA STA 228, LBL 4. REMOVED DRAIN VALVE, INTERCOSTAL AND NOSE W/W SEAL. CUT OUT DAMAGED AREA, REMOVED CORROSION ON AJOINING AREA, INSTALLED REPAIR PER SRM 51-40-4, 2 BY 2. REINSTALLED SEAL, DRAIN VALVE AND INTDec 31, 1996 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL9774020CAngle · crackedAT C-CHECK, AFT AIRSTAIRS TORQUE BOX SIDEWALL TO SHELF UPPER CHORD AND REPLACEMENT CHORD CRACKED FROM FS 1265 TO 1275 RBL 21. REMOVED AFT AIRSTAIR ACTUATOR AND SPRING, REPLACED CHORD ANGLE PER SRM 51-10-1, 22 BY 1.5 BY 1. INSTALLED ACTUATOR AND SPRING.Dec 31, 1996 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9774019CBulkhead Angle · crackedAT C-CHECK, AFT AIRSTAIRS RT TORQUE BOX FS 1263 RBL 23 AIRSTAIRS OPERATING MECHANISM SUPPORT STRUCTURE ATTACH ANGLES UNDER SHELF CRACKED FWD AND AFT SIDE OF BULKHEAD FS 1263. REPLACED DAMAGE ATTACH ANGLES PER SRM 51-10-1, 2.25 BY 7.5 BY 1.Dec 31, 1996 · N740DH · Boeing 7272Q9 · Fuselage Main, BulkheadSDR DHL9774018CAngle · crackedAT C-CHECK, AFT AIRSTAIRS RT TORQUE BOX FS 1275 RBL 21 TO 28 WEB ATTACH ANGLE PREVIOUS REPAIR CRACKED UNDER AIRSTAIRS OPERATING MECHANISM FWD SIDE OF WEB. REPLACED DAMAGED ATTACH WEB ANGLES PER SRM 51-10-1, 7.5 BY 2 BY 1.Dec 31, 1996 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL9774009CTail Pipe · crackedAT C-CHECK, NR 1 ENGINE EXHAUST PIPE ACCOUSTIC LINER HAS APPROX 18 INCH CRACK AT 12 O'CLOCK. WELDED CRACK PER AVIATION EQUIPMENT OHM 727-23-5.Dec 31, 1996 · N740DH · Boeing 7272Q9 · Engine Collector/Tailpipe/NozzleSDR DHL9774006CActuator Mount · crackedAT C-CHECK, NR 5 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED AT INBOARD CORNERS. REMOVED AND REPLACED ACTUATOR MOUNT AT L/E FLAP PER SRM 51-10-1, REPAIR 6.5 BY 8.Dec 31, 1996 · N740DH · Boeing 7272Q9 · Leading Edge Slat ActuatorSDR DHL9774008CDuct · missingAT C-CHECK, NR 2 ENGINE INLET SHORT METAL CONNECTOR DUCT BETWEEN S-DUCT AND FWD FLANGE HAS APPROX 6 INCH SECTION OF FWD EDGE MISSING. REMOVED AND REPLACED INLET DUCT PER M/M 71-00-21.Dec 30, 1996 · N740DH · Boeing 7272Q9 · Nacelle/Pylon StructureSDR DHL9774005CSkin · crackedAT C-CHECK, FWD SERVICE DOOR SKIN CRACKED FROM THE RIVET AT UPPER CORNER OF LOWER HINGE CUTOUT. STOP DRILLED PER SRM 51-10-1, HFEC INSP, INSTALLED DOUBLER PER SRM 52-00-3, 5 BY 5.Dec 30, 1996 · N740DH · Boeing 7272Q9 · Service DoorsSDR DHL9774004CSkin · corrodedAT C-CHECK, FOUND SKIN OIL CANNING AND HAS BULGE AT BS 450 BELOW STR 17R. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3, DOUBLER 9 BY 6.5, FILLER 2.5 BY 1.5.Dec 30, 1996 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL9774001CFrame · crackedAT C-CHECK, CRACK IN FRAME AT STA 203.8, APPROX RBL 18. ACCOMPLISHED HFEC, NO NEW CRACKS, CRACK FROM PREVIOUS STOP DRILL. INSTALLED ANGLE DOUBLER PER SRM 51-40-4, 16 INCHES LONG.Dec 30, 1996 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL96741004Door Seal · frozenON APPROACH, NOSE GEAR DOOR LIGHT ILLUMINATED WITH GEAR LOWERING AND WOULD NOT EXTINGUISH WHEN GEAR WAS DOWN AND LOCKED. ALSO, RED GEAR DOOR LIGHT ILLUMINATED. VISUALLY CHECKED GEAR DOWN AND LOCKED INDICATOR AFTER GO-AROUND. INDICATOR INDICATED DOWN AND LODec 19, 1996 · N741DH · Boeing 7272Q9 · Landing Gear DoorsSDR DHL96740004Oxy Regulator · leakingAFTER TAKEOFF CHECKLIST, CREW OXYGEN WAS READING 100 LBS. SWAPPED CAPTAINS AND SECOND OBSERVERS REGULATOR, REPLACED OXYGEN REGULATOR, NO LEAKS NOTED MM 35-10Jul 9, 1996 · N740DH · Boeing 7272Q9 · Crew Oxygen SystemSDR DHL96741003Adc · malfunctionedAT TAKEOFF, FIRST OFFICERS AIRSPEED, ALTITUDE AND RATE OF CLIMB INDICATORS FLAGGED. FOUND AIR DATA NR 2 COMPUTER CIRCUIT BREAKER POPPED AND WOULD NO RESET. FOUND METAL SHAVINGS ON BENCH PLUG. CLEANED WITH CONTACT CLEANER AND BLEW OUT BENCH PLUG WITH NITROGEJun 17, 1996 · N741DH · Boeing 7272Q9 · Air Data ComputerSDR DHL9674103APwr Supply · failedDURING CLIMB, NR 1, 2 AND 3 FUEL FLOW ERRATIC. FOUND NR 2 FUEL FLOW TRANSMITTER CAUSING FAULTS IN NR 1 AND NR 3 FUEL FLOW INDICATIONS. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY PER M/M 73-31-12. REPLACED NR 2 ENGINE FUEL FLOW TRANSMITTER PER M/M 73-30-0, Jun 14, 1996 · N741DH · Boeing 7272Q9 · Fuel Flow IndicatingSDR DHL96740001Actuator · wornON DESCENT, NOSE GEAR DOOR LIGHT ILLUMINATED. PLACED LEVER UP AND DOWN, LIGHT EXTINGUISHED. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR MM 32-60.Apr 19, 1996 · N740DH · Boeing 7272Q9 · Landing Gear Door ActuatorSDR DHL95742004Waste Drain · leakingLAVATORY DUMP LEAKING AND FORMING BLUE ICE. DRAINED LAVATORY AND DEFERRED PER DHL GENERAL MAINTENANCE MANUAL.Dec 23, 1995 · N742DH · Boeing 7272Q9 · Waste Disposal SystemSDR DHL95742002Connector · looseTHE NR 2 EGT INOP, DUMPED FUEL, PERFORMED AIR TURNBACK. REPLACED K AND L SOCKETS IN CONNECTOR D376J. ALL OTHER CONNECTORS CLEANED AND RESECURED, PERFORMED EGT CHECK PER JRH 06-01 AND NR 2 EGT CHECKS NORMAL.Nov 2, 1995 · N742DH · Boeing 7272Q9 · Engine EGT/TIT Indicating SystemSDR DHL95741008Switch · failedNR 5 KRUGER FLAP LIGHTS REMAIN ON AT FORWARD AND S/O PANEL. REMOVED AND REPLACED NR 5 LEADING EDGE FLAP SWITCH PER M/M 27-81-0. OPS CHECK GOOD.Oct 31, 1995 · N741DH · Boeing 7272Q9 · Leading Edge Slat Position Indicating SystemSDR DHL95741007Smoke Light · illuminatedMAIN CARGO SMOKE DETECTOR INDICATOR LIGHT ILLUMINATED IN-FLIGHT. EXTINGUISHED ON FINAL APPROACH. INSPECTED MAIN CARGO DECK SMOKE DETECTOR SYSTEM. NO DEFECTS NOTED. SYSTEM OPS CHECKS NORMAL PER B727 M/M 26-10-7.Oct 28, 1995 · N741DH · Boeing 7272Q9 · Smoke DetectionSDR DHL95741006Pack · malfunctionedAT FL 240, LOWER AFT BODY OVERHEAT LIGHT CAME ON. REDUCED NR 2 THRUST TO IDLE. TEN MINUTES LATER WHEN RT PACK WAS TURNED OFF WITH NR 2 THRUST AT IDLE, LIGHT WENT OFF. OVERHEAT SMELL EVIDENT THROUGHOUT COCKPIT. RAN BOTH ENGINGES, CHECKED FOR LEAKS AT AFT STJul 5, 1995 · N741DH · Boeing 7272Q9 · Cabin Cooling SystemSDR 95ZZZM272Switch · lack of lubeDURING TAKEOFF ROLL, BEFORE AIRSPEED CALL OUT, AMBER LEADING EDGE FLAP LIGHT FLICKERED. DURING TAXI BACK NR 6 LEADING EDGE SLAT GREEN LIGHT FLICKERED OFF AND ON, ON SECOND OFFICERS PANEL. CLEANED AND SECURED NR 6 LEADING EDGE SLAT POSITION INDICATOR SWITCH. Jun 17, 1995 · N740DH · Boeing 7272Q9 · Leading Edge Slat Position Indicating SystemSDR DHL95740002Hyd Pump · failedA SYSTEM LOSS SHUT DOWN NR 1 A PUMP OFF AND FLUID LOSS SLOWED CONSIDERABLY. REMOVED AND REPLACED NR 1 A SYSTEM PUMP AND DRAIN FILTER PER M/M 29-11-41 AND 29-11-33, BLED SYSTEM. A SYSTEM OPS AND LEAK CHECK GOOD .May 18, 1995 · N740DH · Boeing 7272Q9 · Hydraulic Pump (Electric/Engine), MainSDR DHL95741004Wire · failedAPPROACHING V1, EXPERIENCED PARTIAL LOSS OF ELECTRICAL POWER WITH ARCHING AND SMOKE FROM LOWER P6 PANEL. ABORTED TAKEOFF AND RETURNED TO BLOCKS. NR 1 GEN BKR AND FIELD RELAY TRIPPED AND NR 1 DIFFERENTIAL FAULT ILLUMINATED. ARCHING AND SMOKE CONTINUED UNTIL NMay 12, 1995 · N741DH · Boeing 7272Q9 · Electrical Power System WiringSDR DHL95740001Reservoir · failedON CLIMB, LOST STANDBY HYDRAULIC QUANITY. ALL OTHER PRESSURES AND QUANITIES OK. REMOVED AND REPLACED STANDBY HYDRAULIC RESERVOIR AND LEFT WING TAI DUCT.Apr 29, 1995 · N740DH · Boeing 7272Q9 · Hydraulic Reservoir, AuxiliarySDR DHL95741003Vertical Gyro · inoperativeON TAKE OFF, F/O ADI FAILED INTERMITTANTLY AT BANK ANGLES GREATER THAN 4 DEGREES. DIVERTED TO CVG, LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 VERTICAL GYRO PER DHL 727 MM 34-22-21, ALL INICATIONS NORMAL.Apr 14, 1995 · N741DH · Boeing 7272Q9 · Attitude Gyro and Indicating SystemSDR 95ZZZW625Vertical Gyro · inopON TAKEOFF, FLIGHT OFFICER ADI FAILED INTERMITTENTLY AT BANK GREATER THAN 4 DEGREE. DIVERTED TO CVG. LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 VERTICAL GYRO, PER DHL 727 MM 34-22-21. ALL INDICATIONS NORMAL.Apr 14, 1995 · N741DH · Boeing 7272Q9 · Attitude Gyro and Indicating SystemSDR 95ZZZW584Connector · dirtyDURING CLIMB, LEADING EDGE DEVICES FAILED TO RETRACT ON SCHEDULE. PERFORMED AIR TURNBACK, LANDED WITHOUT INCIDENT. CLEANED CONNECTORS ON SLAT ACTUATORS AND LUBED SLAT TRACKS. GROUND CHECKS OK.Apr 14, 1995 · N741DH · Boeing 7272Q9 · Leading Edge Slat Control SystemSDR DHL95741001Lamp · failedDURING CRUISE, ELEVATOR DIFFERENTIAL PRESSURE LIGHT ON INTERMITTENTLY FOR SEVERAL MINUTES. FOUND ELEVATOR FEEL LIGHT BULB SHORTING. RELAMPED. NO OTHER DEFECTS NOTED.Apr 11, 1995 · N741DH · Boeing 7272Q9 · Elevator Control SystemSDR 95ZZZZ226Bulb · shortedDURING CRUISE, ELEVATOR DIFFERENTIAL PRESSURE LIGHT ON INERMITTENTLY FOR SEVERAL MINUTES. FOUND ELEVATOR FEEL LIGHT BULB SHORTING. NO OTHER DEFECTS NOTED.Apr 11, 1995 · N741DH · Boeing 7272Q9 · Elevator Control SystemSDR 95ZZZZ198Stringer · corrodedDURING D-CHECK, AFT CARGO HEAVY CORROSION IN STRINGER CHANNEL AND STRINGER CRACKED BELOW FUSELAGE FRAME 1010 AT STRINGER 29L. REMOVED SPLICE PER SRM 51-30-2. REMOVED CORROSION PER SRM 51-10-6, MATERIAL LOSS .002, TREATED ALODINE AND PRIMED PER SRM 51-10-2. Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ197Stringer · corrodedDURING D-CHECK, AFT CARGO CORROSION INSIDE STRINGER AT STRINGER 30 BETWEEN FS 1030 AND FS 1050. CUT OUT STRINGER DAMAGED AREA AND FABRICATED PART IAW SRM 53-10-3 AND INSTALLED 20 INCHES STRINGER BAC 1498-131 .71 7075-T6. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ196Stringer · corrodedDURING D-CHECK, AFT CARGO, CORROSION AT SEVERAL AREAS IN STRINGER 30 CHANNEL BETWEEN FS 1050 AND FS 1070. REMOVED CORROSION PER SRM 51-10-6. CUT OUT DAMAGED AREA AND FABRICATED PART PER SRM 53-10-3 2 INCHES .71 7075-T62 AND 12 INCHES .90 7075-T62, TREATED ANFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ195Stringer · corrodedDURING D-CHECK, AFT CARGO, STRINGER 30 IS CORODED AND CRACKED INSIDE STRINGER CHANNEL BETWEEN FS 1070 AND FS 1090. CORROSION FOUND OVERLIMIT. REMOVED FASTENERS FOR REPAIR STRINGER. CUT OUT STRINGER DAMAGE AREA AND FABRICATED PART PER SRM 53-10-3, 20 INCHES Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ194Floor Support · corrosionDURING D-CHECK, AFT CARGO, SURFACE CORROSION AROUND NUT PLATES AT LOWER SURFACE OF FLOOR SUPPORT ANGLES AT FS 1170 LBL 5 AND RBL 8. REMOVED CORROSION PER SRM 51-10-6 AND FOUND OUT OF LIMITS. INSTALLED ANGLE REPAIR PER SRM 51-40-4, MAT USED .050 2 INCHES BY 8Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZZ193Intercostal · corrosionDURING D-CHECK, AFT CARGO, SURFACE CORROSION ON INTERCOSTAL LOWER FLANGE BETWEEN STRINGER 29R AND STRINGER 28R BETWEEN FS 1150 AND FS 1170. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED WEB REPAIR AT PREVIOUS CRACK PER SRM 5Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZZ192Stringer · corrodedDURING D-CHECK, AFT CARGO FUSELAGE STATION 1183 CIRCUMFERENTIAL 'T' FITTING AND STRINGER BADLY CORRODED AT STRINGER 29L. REMOVED CORROSION ON FS 1183, OUT OF LIMTS (APPROX .080). INSTALLED CHORD ANGLE REPAIR AS PER (A/E NR LBN-MLB DRAWING). REMOVED AND REPLFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ191Floor Beam · holeDURING D-CHECK, STATION 1030 FLOOR BEAM TOP FLANGE HAS DRILLED HOLE AT CENTER OF FLANGE 'T' HOLE CONTINUES DOWN LOWER LEG OR WEB OF BEAM APPROXIMATELY .75 OF AN INCH. FABRICATED REPAIR PARTS PER SRM 53-10-8 AND 51-40-2. INSTALLED PARTS PER SRM 53-10-8. TOTAFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZZ190Floor Beam · corrosionDURING D-CHECK, FOUND CORROSION ON FLOOR BEAM RT BS 1130 BL 0 TO RBL 64 AND ON LEFT SIDE BS 1130 BL 0 TO LBL 26. REMOVED CORROSION PER SRM 51-10-6, OUT OF LIMITS. TREATED AND PRIMED AREA PER SRM 51-10-2. FABRICATED AND INSTALLED REPAIR AT RBL 27 AND LBL 28 Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZZ189Stringer · corrodedDURING D-CHECK, AFT BAG BIN STRINGER 27R HAS HEAVY CORROSION AT STATION 1176 APPROXIMATELY. REMOVED AND REPLACED STRINGER 27R FROM STATION 1183 TO 1144 AS PER SRM 51-10-1 PAR 4. INSTALLED DOUBLER REPAIR AS PER SRM 53-30-3 APPROX 54 INCHES BY 12 INCHES. TOTAFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ188Frame · corrosionDURING D-CHECK, INSIDE STATION 300-320, CHORD BELOW STRINGER 26R, SHOWS CORROSION AT AND UNDER LEVELING COMPOUND. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. CUT OUT DAMAGED SECTION OF CHORD AND REPAIRED PER SRM 51-40-4. DIM 16 INCHES BY 4 INCHES BY 4Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZZ187Stringer · corrodedDURING D-CHECK, AFT BAG BIN STRINGER 27L HAS HEAVY CORROSION AT STATION 1176. REMOVED AND REPLACED STRINGER 27L FROM STATION 1183 TO 1166 AS PER SRM 51-10-1 PARA 4. INSTALLED DOUBLER REPAIR AS PER SRM 53-30-3 APPROX 54 INCHES BY 12 INCHES. TOTAL CYCLES 29,5Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ186Frame · corrodedDURING D-CHECK, AFT CARGO COMPARTMENT STATION 1148 AT STRINGER 27R CORROSION ON FRAME UPPER AND LOWER FLANGES. REMOVED AND REPLACED LOWER CLIP AT STATION 1148 STRINGER 27R. INSTALLED FRAME REPAIR ON UPPER FLANGE AS PER SRM 53-10-4 5 INCHES BY 2 INCHES BY 1 IFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZZ185Skin · erodedDURING D-CHECK, FORWARD BAG DOOR, AFT LOWER EDGE SKIN ERODED AND FAIRING MATERIAL MISSING. REMOVED FASTENERS AS PER SRM 51-30-2. CUT OUT DAMAGED AREA AS PER SRM 51-10-1. TREATED AND PRIMED AREA AS PER SRM 51-10-3. MANUFACTURED DOUBLER 6 INCHES BY 8 INCHES Feb 28, 1995 · N740DH · Boeing 7272Q9 · Cargo/Baggage DoorsSDR 95ZZZZ184Shear Web · corrodedDURING D-CHECK, CORROSION NUMEROUS AREAS MARKED ON SHEAR WEBB TO SURFACE FROM BS 1137 AFT TO CHORD ANGLE RBL 24 TO RBL 48. INSTALLED NEW SHEAR WEBB PER SRM 51-10-1 AND 51-30-2. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous Structure
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