Boeing 727-224

Service difficulty reports · 2,252

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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 = '727224'
  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 CALA9800228Light · inoperativeINSPECTION FOUND THE RT AFT GALLEY DOOR EMERGENCY EXIT LIGHT TOO DIM. THE LIGHT ASSEMBLY WAS REPLACED IAW MM 33-50-101.Feb 12, 1998 · N69735 · Boeing 727224 · Emergency LightingSDR CALA9800227Frame · corrodedINSPECTION FOUND C-3 DOOR FRAME CORRODED AT CUTOUT AT FORWARD LOWER END WHERE IT MEETS THRESHOLD AT BS 1090. THE CORRODED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-40-3.Feb 12, 1998 · N69735 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9800226Rib · crackedINSPECTION FOUND A 2 CRACK IN NR 2 LEADING EDGE SLAT RIB OUTBOARD OF ANTI-ICE DUCT. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.Feb 12, 1998 · N69735 · Boeing 727224 · Leading Edge DevicesSDR CALA9800225Skin · dentedINSPECTION FOUND LEFT FUSELAGE SKIN DENTED AT STA 1333 JUST ABOVE AIRSTAIR. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-30-03.Feb 12, 1998 · N79746 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9800222Splice Plate · crackedINSPECTION FOUND A 2 INCH CRACK AT SPLICE PLATE INSIDE LEFT WING UPPER LEADING EDGE ABOVE NR 2 LEADING EDGE FLAP ACTUATOR/ANTI-ICE DUCT AREA, WS 224.5. THE SPLICE PLATE WAS REMOVED AND A STRAP WAS FABRICATED AND INSTALLED IAW SRM 57-50-2 AND 51-30-2.Feb 12, 1998 · N69735 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9800221Angle · crackedINSPECTION FOUND A .5 AND 1 INCH CRACK AT FASTENERS IN CURVED ANGLE INSIDE LEFT WING LEADING EDGE RIB OUTBOARD SIDE AT SLAT STA 0 (AFT OF NR 4 SLAT INBOARD MOST END). THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2Feb 12, 1998 · N79746 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9800220Skin · dentedINSPECTION FOUND LEFT WING INBOARD LEADING EDGE SKIN DENTED BETWEEN INBOARD LANDING LIGHT AND NR 3 LEADING EDGE FLAP AREA. THE DENT WAS REWORKED IAW ECRA 5750-01352.Feb 12, 1998 · N79746 · Boeing 727224 · Wing, Plate/SkinSDR CALA9800219Skin · crackedINSPECTION FOUND A .375 CRACK AT LEFT WING FIXED LEADING EDGE SKIN ABOVE NR 4 SLAT INBOARD TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-05.Feb 12, 1998 · N79746 · Boeing 727224 · Wing, Plate/SkinSDR MZZA98079Switch · inoperativeGUM - FLT 0949 - L/P 7950069 - AIR RETURN DUE TO LEFT LANDING GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE REQUESTED FOR FLY-BY TO CONFIRM GEAR DOOR CLOSED. MAINTENANCE TROUBLESHOT SYSTEM, FOUND LEFT LANDING GEAR DOOR SWITCH BAD. PLACARDEDFeb 8, 1998 · N69741 · Boeing 727224 · Landing Gear Position and WarningSDR CALA9800099Structure · damagedTHE AIRCRAFT SUSTAINED GROUND DAMAGE TO THE FUSELAGE SKIN, STRINGER, AND FRAMES AT STA 440-480, STRINGERS 14-19L. THE FUSELAGE SKIN AND STRINGER WERE REPAIRED IAW ECRA 5330-02621. THE FRAMES WERE REPAIRED IAW ECRA 5310-03656, SRM 51-40-3, AND 53-10-3.Jan 22, 1998 · N79750 · Boeing 727224 · Fuselage Main, StructureSDR GAIA9805Retract Mech · malfunctionedFLT 740 - DFW-MSY - CREW REPORTED ON LOG PAGE 1086-11 AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. RETURNED TO DFW WITHOUT INCIDENT. INSPECTED GEAR. PERFORMED GEAR SWING IAW BOEING MM 32-32-0 PAGE 501. COULD NOT DUPLICATE PROBLEM AIRCRAFT RETURNED TO SERVICEJan 19, 1998 · N69740 · Boeing 727224 · Landing Gear Retraction/Extension SystemSDR MZZA98048Skin · separatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING INBOARD T/E AFT FLAP UPPER SKIN AT WBL 208. THE DAMAGED SKIN 3 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEMJan 12, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98047Skin · delaminatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING T/E INBOARD AFT FLAP T/E UPPER SKIN AT WBL 182. THE DAMAGED SKIN 11.5 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTIJan 12, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR CALA9800018Control Module · leakingTHE A-SYSTEM HYDRAULIC OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF WHILE CLIMBING THROUGH 6000 FEET. A MINUTE LATER, THE A-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. THE HYDRAULIC FAILURE CHECKLIST WAS PERFORMED, FUEL WAS DUMPED, AND THE AIRCRAFT WAS RETURNED TO IJan 12, 1998 · N32725 · Boeing 727224 · Aileron Control SystemSDR MZZA98044Skin · delaminatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WS FOUND ON LEFT WING OUTBOARD T/E AFT FLAP LOWER SURFACE AT WBL 450. THE DAMAGED SKIN 6 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINEJan 5, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98043Skin · delaminatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIR, DELAMINATION WERE FOUND ON LEFT WING OUTBOARD AFT FLAP UPPER SURFACE AT THE FOLLOWING LOCATION, WBL 301, WBL 359, WBL 363 AND WBL 492. THE DAMAGED SKIN WERE TRIMMED AND REPAIRED PER B727 SRM 51-40-6. Jan 5, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98042Skin · delaminatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING INBOARD T/E AFT FLAP UPPER SURFACE BETWEEN WBL 86 AND WBL 96. THE DAMAGED SKIN 10 INCH BY 2 INCH IN SIZE WAS TRIMMED AND REPAIRED PER B727 SRM 51-40-6. REF, HANGARJan 5, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98039Frame · crackedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON FORWARD CARGO COMPRTMENT FRAME UPPER CHORD AT BS 580, RBL 3. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM Jan 5, 1998 · N79745 · Boeing 727224 · Fuselage Main, FrameSDR MZZA98038Support Fitting · corrodedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WERE FOUND ON NLG W/W AFT MOUNT SUPPORT FITTING PLATES AT BS 337 RBL 17.5 AND LBL 17.5. THE CORRODED MOUNT SUPPORT FITTING PLATES WERE REMOVED AND REPLACED PER B727 SRM 51-30-2. REF,Jan 5, 1998 · N79745 · Boeing 727224 · Fuselage Miscellaneous StructureSDR MZZA98052Skin · separatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING T/E OUTBOARD AFT FLAP UPPER SKIN AFT EDGE AT WBL 388. THE DAMAGED SKIN 8 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF HANGAR NON ROUTINE REJan 2, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98051Skin · separatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING T/E OUTBOARD AFT FLAP UPPER SKIN AFT EDGE AT WBL 342. THE DAMAGED SKIN 7 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE RJan 2, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98050Skin · disbondedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DISBONDED WAS FOUND ON RT WING T/E OUTBOARD AFT FLAP UPPER SURFACE EXISTING REPAIR DOUBLER AT WBL 468. THE DAMAGED EXISTING REPAIR DOUBLER WAS REMOVED AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NJan 2, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98049Skin · separatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING T/E INBOARD AFT FLAP UPPER SKIN AT WBL 127. THE DAMAGED SKIN 7 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEMJan 2, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98046Skin · delaminatedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING T/E INBOARD AFT FLAP AT WBL 234. THE DAMAGED SKIN 4 INCHES BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRD PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CAJan 2, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98045Skin · disbondedTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DISBONDED WAS FOUND ON RT WING INBOARD AFT FLAP OUTBOARD AFT CORNER. THE DAMAGED SKIN 5 INCH BY 5.5 INCH WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NRJan 2, 1998 · N79745 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98037Channel · corrodedDURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON NLG LEFT TRUNNION SUPPORT FITTING FORWARD LEG ATTACH EXTRUDED 'U' CHANNEL AT BS 303.9. THE CORRODED 'U' CHANNEL WAS CLEANUP AND REPAIRED PER EC/RA NR 5340-01310. REF, HANGAR NDec 31, 1997 · N79745 · Boeing 727224 · Fuselage Miscellaneous StructureSDR MZZA98036Web · canningTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WERE FOUND ON VERTRAL STAIRWELL TORQUE BOX WEB AT THE FOLLOWING LOCATION, LEFT SIDE AT BS 1233, RT SIDE AT BS 1233, RT SIDE BETWEEN BS 1283 AND BS 1313, LEFT SIDE AT 1293. THE DAMAGED WEB Dec 31, 1997 · N79745 · Boeing 727224 · Fuselage Main, StructureSDR MZZA98041Tab Skin · delaminationTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 5 INCH LONG DELAMINATION WAS FOUND ON LEFT ELEVATOR TAB TRAILING EDGE SKIN EDGE. THE DELAMINATION SKIN EDGE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 84Dec 30, 1997 · N79745 · Boeing 727224 · Elevator, Tab StructureSDR MZZA98040Skin · delaminationTNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 3 INCH LONG DELAMINATION WAS FOUND ON RT ELEVATOR TAB TRAILING EDGE SKIN EDGE. THE DELAMINATION SKIN EDGE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 8408Dec 30, 1997 · N79745 · Boeing 727224 · Elevator, Tab StructureSDR CALA9701786Actuator · failedTHE NR 2 KRUGER FLAP WOULD NOT RETRACT AFTER TAKEOFF FROM MGA. THE AIRCRAFT WAS RETURNED TO MGA WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 KRUGER FLAP ACTUATOR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Dec 21, 1997 · N79749 · Boeing 727224 · Leading Edge Slat ActuatorSDR CALA9701753Switch · malfunctionedTHE AIRCRAFT HAD A BRIEF HISTORY OF THE NOSE GEAR DOOR LIGHT ILLUMINATING AT BOTH THE FORWARD PANEL AND SECOND OFFICER'S PANEL WHILE IN FLIGHT. BOTH NOSE GEAR DOOR UP SWITCHES WERE REMOVED AND REPLACED IAW MM 32-62-11. IN ADDITION, BOTH NOSE GEAR DOOR CABLESDec 12, 1997 · N32725 · Boeing 727224 · Landing Gear Position and WarningSDR CALA9701739Skin · corrodedINSPECTION FOUND RT INBOARD MIDFLAP LOWER TRAILING EDGE CORRODED AND DISBONDED IN AFT FLAP COVE BETWEEN TEARDROP FAIRINGS. THE MIDFLAP LOWER TRAILING EDGE WAS REMOVED IAW SRM 51-30-2, TREATED AND PRIMED IAW SRM 51-10-2, AND INSTALLED IAW SRM 51-10-1 AND 51-20Dec 9, 1997 · N69736 · Boeing 727224 · Trailing Edge FlapsSDR CALA9701738Skin · delaminatedINSPECTION FOUND TWO AREAS OF DELAMINATION IN RT TRAILING EDGE INBOARD FOREFLAP UPPER SURFACE. THE DELAMINATION WAS LOCATED 90 INCHES FROM INBOARD EDGE AND 25 INCHES FROM OUTBOARD EDGE. THE FOREFLAP WAS REMOVED AND REPAIRED IAW SRM 57-50-02. THE FOREFLAP WASDec 9, 1997 · N69736 · Boeing 727224 · Trailing Edge FlapsSDR CALA9701737Skin · damagedINSPECTION FOUND FASTENERS PULLING THROUGH SKIN FORWARD OF INLET GUIDE VANES AROUND CIRCUMFERENCE AT NR 2 ENGINE INLET. THE FASTENERS WERE REMOVED AND REPLACED IAW EA 5410-01328 AND SRM 51-30-2.Dec 9, 1997 · N69736 · Boeing 727224 · Engine Air Intake SystemSDR CALA9701736Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 8 SLAT OUTBOARD UPSTOP BOLT BRACKET AND LOWER LEADING EDGE SKIN FLANGE BROKEN. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Dec 9, 1997 · N69736 · Boeing 727224 · Leading Edge DevicesSDR CALA9701735Wedge · delaminatedINSPECTION FOUND RT WING OUTBOARD AILERON TRAILING EDGE WEDGE DELAMINATED ON LOWER SURFACE AT OUTBOARD EDGE. THE TRAILING EDGE WEDGE WAS REMOVED, REPAIRED AND INSTALLED IAW SRM 51-30-2.Dec 9, 1997 · N69736 · Boeing 727224 · AileronsSDR CALA9701734Skin · debondedINSPECTION FOUND LT WING OUTBOARD MIDFLAP LOWER TRAILING EDGE DEBONDED ON TOP 108 INCHES FROM INBOARD END AND ON BOTTOM 128 INCHES FROM INBOARD END. REMOVED MIDFLAP, REPAIRED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-1, AND 51-20-4.Dec 9, 1997 · N69736 · Boeing 727224 · Trailing Edge FlapsSDR CALA9701733Skin · debondedINSPECTION FOUND LT WING OUTBOARD FOREFLAP DEBONDED AT UPPER INBOARD TRAILING EDGE AREA. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-4.Dec 9, 1997 · N69736 · Boeing 727224 · Trailing Edge FlapsSDR CALA9701732Skin · corrodedINSPECTION FOUND CORROSION AND DEBONDING 65 INCHES FROM INBOARD END OF LT WING INBOARD MIDFLAP UPPER TRAILING EDGE. THE LT WING INBOARD MIDFLAP UPPER TRAILING WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2, 51-10-6, 51-10-1, AND 51-20-4.Dec 9, 1997 · N69736 · Boeing 727224 · Trailing Edge FlapsSDR CALA9701731Skin · corrodedINSPECTION FOUND RT FUSELAGE SKIN CORRODED JUST BELOW CABIN WINDOW NR 11 AT STA 620. THE FASTENERS WERE REMOVED, THE CORROSION WAS CLEANED, AND FASTENERS WERE INSTALLED IAW SRM 51-30-2.Dec 9, 1997 · N69736 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9701730Fitting · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD LUG OF LT MLG UPLOCK SUPPORT FITTING. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1. A LANDING GEAR RETRACTION AND ROTATIONAL CHECK WAS ACCOMPLISHED AND ALL CHECKED GOOD.Dec 9, 1997 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9701729Skin · corrodedINSPECTION FOUND E AND E DOOR RT SIDE SKIN CORRODED. THE DOOR WAS REMOVED AND REPLACED IAW MM 52-40-11.Dec 9, 1997 · N69736 · Boeing 727224 · Electrical/Electronic Compartment DoorsSDR CALA9701695Skin · crackedINSPECTION FOUND A .125 AND .0937 INCH CRACK AT FASTENER OF NR 6 SLAT SKIN UPPER LEADING EDGE, IN FORWARD ROW OF FASTENERS 50 FROM INBOARD END. THE FASTENERS WERE REMOVED, THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED INov 25, 1997 · N69736 · Boeing 727224 · Leading Edge DevicesSDR MZZA97304Beam · crackedKUL - NRC: 813821 - SPOILER SUPPORT BEAM, LOWER CHORD, FOUND CRACKED. FABRICATED DOUBLER IAW SRM 51-40-4, FIG 1, ALODINED AND PRIMED PER SRM 51-10-2. CARRIED OUT REPAIR IAW SRM 51-40-4. INSTALLED FASTENERS IAW SRM 51-30-2, AND PL, REF DRAWING NR 65-24966. Nov 14, 1997 · N69741 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9701632Fitting · brokenINSPECTION FOUND AFT CARGO C-3 DOOR FORWARD LOWER STOP FITTING BROKEN OFF. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1.Nov 13, 1997 · N93738 · Boeing 727224 · Cargo/Baggage DoorsSDR CALA9701626Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LOWER SURFACE OF LT WING NR 4 SLAT SKIN, OUTBOARD OF INBOARD TRACK. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-5, 51-40-2, AND 51-10-2.Nov 13, 1997 · N93738 · Boeing 727224 · Leading Edge DevicesSDR CALA9701625Skin · dentedINSPECTION FOUND LT WING OUTBOARD MIDFLAP LEADING EDGE DENTED APPROXIMATELY 32 INCHES FROM INBOARD END. THE DENTED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-4 AND 51-10-2.Nov 13, 1997 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9701624Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN LOWER SKIN OF RT WING TIP JUST OUTBOARD OF NR 8 SLAT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-01. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-20-4.Nov 13, 1997 · N93738 · Boeing 727224 · Wing, Plate/SkinSDR CALA9701623Rib · crackedINSPECTION FOUND A 6 INCH CRACK IN RIB AT OUTBOARD SIDE OF LT WING FLUX VALVE CUTOUT. THE CRACK WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.Nov 13, 1997 · N93738 · Boeing 727224 · Wing, Rib/BulkheadSDR CALA9701622Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING UPPER TRAILING EDGE SKIN PANEL AT SECOND FROM INBOARD HINGE CUTOUT FOR NR 4 SPOILER. THE FASTENERS WERE REMOVED AND THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-04.Nov 13, 1997 · N93738 · Boeing 727224 · Wing, Plate/Skin
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