Boeing 737-2B7

Service difficulty reports · 1,360

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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 = '7372B7'
  ORDER BY difficulty_date DESC"

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SDR USAA991290Fitting · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT BS 1016, STRINGER 20R TIE FITTING. CORROSION LEVEL 1. REMOVED CORROSION AND PRIMED PER SRM 51-10-06. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991289Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 20 INCH BY 2 FT AT STATION 344, LBL 10 RBL 10 T-CAP. CORROSION LEVEL 2. FABRICATED NEW T-CAP PER TR 53-10-13. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA991284Skin · corrodedCLT - DURNG Q-6 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY4 INCH AREA OF CORROSION AT STATION 500B STRINGER 27R SKIN. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-30-3. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99285Controller · failedBDL - FLT 2743 - AIRCRAFT DEPARTED BDL WITH MEL 21-14A APPLIED, CABIN PRESSURE CONTROL SYSTEM AUTOMATIC MODE INOPERABLE. AFTER TAKEOFF, THE CAPTAIN REPORTED THE STANDBY MODE WOULD NOT WORK AND THE AIRCRAFT WOULD NOT PRESSURIZE PROPERLY. FLIGHT RETURNED TO FINov 30, 1999 · N271AU · Boeing 7372B7 · Cabin Pressure ControllerSDR USAASB99272Gcu · malfunctionedTPA - FLT 2674 - FLIGHT LOST THE NR 1 TRANSFER BUS AND ALL INSTRUMENTS ON BOTH SIDES DURING ROTATION. CREW RESET THE NR 1 TRANSFER BUS CIRCUIT BREAKER WHICH BROUGHT BACK ALL INSTRUMENTS EXCEPT THE MACH AIRSPEED INDICATION. FLIGHT RETURNED TO FIELD AT TPA ANDNov 17, 1999 · N286AU · Boeing 7372B7 · DC Generating SystemSDR USAA991247Skin · crackedTPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK IN FORWARD ENTRY DOOR UPPER HINGE CUTOUT DOOR SKIN. INSTALLED DOUBLER PER TR 52-10-05 AND EA 65479. (M)Nov 6, 1999 · N279AU · Boeing 7372B7 · Passenger/Crew DoorsSDR USAA991246Skin · crackedTPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT FORWARD EDGE OF LOWER HINGE CUTOUT OF MAIN ENTRY DOOR. INSTALLED DOUBLER PER SRM 53-30-3 FIG 31. (M)Nov 6, 1999 · N279AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99260Acm · weakBWI - FLT 2741 - FLT ON MX DELAY IN BDL, WHEREAS MX PLACED THE RT PACK ON MEL. FLT DEPARTED BDL AND WHILE FLYING OVER PHL, THE LT PACK WOULD ONLY HOLD CABIN PRESSURE TO 9,500 FT. CAPT ELECTED TO DIVERT TO BWI WHERE THE FLT LANDED W/O FURTHER INCIDENT. NO EMOct 27, 1999 · N269AU · Boeing 7372B7 · Cabin Cooling SystemSDR USAASB99257Indication · malfunctionedTPA - FLT 2637 - UPON SELECTING FIVE DEGREES FLAP SETTING ON APPROACH, THE FLAP INDICATOR NEEDLES SPLIT AND THE FLAPS FROZE AT ONE DEGREE FLAPS. AN EMERGENCY WAS DECLARED. FLIGHT LANDED AT A HIGHER THAN NORMAL LANDING SPEED BUT OTHERWISE HAD A NORMAL LANDINGOct 22, 1999 · N270AU · Boeing 7372B7 · Trailing Flap Position Indicating SystemSDR USAASB99249Hydrauic Line · failedBOS - FLT 2674 - FLT WAS ON 4 MILE FINAL INTO BOS WHEN COMPLETE LOSS OF SYSTEM 'A' HYDRAULICS OCCURRED AFTER GEAR WAS SELECTED DOWN. CAPT DECLARED AN EMERGENCY AND ACCOMPLISHED GO-AROUND TO COMPLETE CHECKLIST. CABIN WAS PREPPED FOR AN EMERGENCY LANDING. FLIOct 15, 1999 · N275AU · Boeing 7372B7 · Hydraulic System, MainSDR USAA991073Skin · crackedTPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SKIN L-2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNER. INSTALLED DOUBLER PER REPAIR DOCUMENT 53-30-3 FIG 34 AND TR 53-30-10 REV A. (M)Oct 11, 1999 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA991072Skin · crackedTPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN SKIN R-2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNER. INSTALLED DOUBLER PER REPAIR DOCUMENT 53-30-3 FIG 33. (M)Oct 11, 1999 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99246Csd · failedMCO - FLT 2646 - FLIGHT DEPARTED MIA WITH THE NR 1 GENERATOR ON MEL. DURING CRUISE, THE NR 2 GENERATOR LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE NR 2 CSD AND DIVERTED TO MCO WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS Oct 10, 1999 · N267AU · Boeing 7372B7 · Alternator-Generator DriveSDR USAASB99236Connector · dirtyTPA - FLT 2642 - DURING CLIMB-OUT FROM TPA, THE NR 2 ENGINE FUEL SHUTOFF VLV CLOSED LIGHT BEGAN FLICKERING ON AND OFF THEN ILLUMINATED STEADY. ENGINE INDICATIONS WERE NORMAL. FLIGHT RETURNED TO FIELD AT TPA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY Sep 23, 1999 · N283AU · Boeing 7372B7 · Fuel Selector/Shut-Off ValveSDR USAASB99235Valve · failedORD - FLT 2704 - AFTER TAKEOFF FROM BWI, THE INBOARD ANTI-SKID LIGHT ILLUMINATED AND DID NOT EXTINGUISH AFTER GEAR RETRACTION. FLIGHT DIVERTED TO ORD FOR MAINTENANCE AND LONGER RUNWAYS. LIGHT REMAINED ON WHEN LANDING GEAR WAS DOWN AS WELL. FLIGHT LANDED WITSep 22, 1999 · N267AU · Boeing 7372B7 · Brake Anti-Skid SectionSDR USAA991015Skin · crackedTPA - DURING A CX-6 CHEK VISUAL INSPECTION, FOUND A .25 INCH CRACK ON DOOR CUTOUT SKIN FOR HANDLE STATION 817, WL 178. INSTALLED DOUBLER PER SRM 52-00-03 FIG 2. (M)Sep 22, 1999 · N284AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA990964Skin · crackedTPA - DURING CX-4 VISUAL INSPECTION, FOUND A 1 INCH CRACK STA 727B, STR 18L SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (X)Sep 17, 1999 · N275AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA990963Skin · crackedTPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK STA 747, STR 19L SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (X)Sep 17, 1999 · N275AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA991009Skin · crackedRDU/PIT - DURING UNSCHEDULED MAINTENANCE FROM PILOT REPORT IN RDU, FOUND .625 INCH CRACK IN FUSELAGE SKIN AT STATION 380 BETWEEN STRINGER 28 LEFT/28 RIGHT OF CENTER LINE. INSTALLED EXTERNAL DOUBLER PER TYPICAL REPAIR 53-30-04. (M)Sep 9, 1999 · N278AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99226Power Supply · inoperativeBOS - MAINTENANCE FOUND THE AFT EMERGENCY LIGHT INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)Sep 4, 1999 · N267AU · Boeing 7372B7 · Emergency LightingSDR USAASB99213Battery Pack · dischargedBWI - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Aug 28, 1999 · N284AU · Boeing 7372B7 · Emergency LightingSDR USAASB99200Fuel · failedMCO - FLT 2666 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED AT REDUCED THRUST. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 2 ENGINE FUELAug 12, 1999 · N277AU · Boeing 7372B7 · Engine Anti-Icing SystemSDR USAASB99199Compressor · stalledBOS - FLT 2851 - AT ROTATION, CREW HEARD AND FELT A LOUD BANG. ALL ENGINE INDICATIONS WERE NORMAL. FLAMES OR A FLASH WERE LATER REPORTED BY A PASSENGER OFF THE RIGHT SIDE OF THE AIRCRAFT. AT APPROXIMATELY 5,000 FT. CAPTAIN DECLARED AN EMERGENCY AND PREPPEDAug 11, 1999 · N268AU · Boeing 7372B7 · Turbine Engine Compressor SectionSDR USAASB99217Light · inoperativeCLT - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT IN THE COCKPIT REMAINS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AS PER THE MM. OPERATIONAL CHECK GOOD. (M)Aug 8, 1999 · N276AU · Boeing 7372B7 · Emergency LightingSDR USAASB99195Duct · deterioratedBUF - FLT 2689 - AFTER TAKEOFF FROM BUF, WHILE ACCOMPLISHING AFTER TAKEOFF CHECKLIST, CREW HEARD A LOUD BANG AS PACKS WERE TURNED ON. FLIGHT ATTENDANT IN REAR OF AIRCRAFT REPORTED A WHITE/GRAY SMOKE IN THE REAR OF THE CABIN. CREW TURNED PACKS OFF AND SMOKE AAug 8, 1999 · N281AU · Boeing 7372B7 · Cabin Cooling SystemSDR USAA990828Skin · crackedTPA - DURING CX-2 CHECK EDDY CURRENT INSPECTION, FOUND A .2 5INCH CRACK IN SKIN AT UPPER HINGE CUTOUT STATION 950.5 STRINGER 13R AND 11R. REMOVED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 78A FIG 21A SHEET 1/2. (M)Aug 7, 1999 · N288AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA990827Skin · crackedTPA - DURING CX-2 CHECK EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK LOWER HINGE CUTOUT FORWARD SERVICE DOOR SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER SB 737-52-1096 AND SRM 51-10-01. (M)Aug 7, 1999 · N288AU · Boeing 7372B7 · Service DoorsSDR USAA990826Skin · crackedTPA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK ABOVE RIVET .125 INCH CRACK BELOW RIVET STRINGER 17R, WL STATION 344 SKIN. INSTALLED REPAIR DOUBLER PER SB 737-53-1083 FIG 3C. (M)Aug 7, 1999 · N274US · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99189Engine · bird strikeBWI - FLT 2704 - ON TAKEOFF ROLL, NR 2 ENGINE INGESTED A BIRD. CREW SHUT DOWN NR 2 ENGINE POWER PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS TEN MINUTES. MAINTENANCEJul 31, 1999 · N271AU · Boeing 7372B7 · Engine (Turbine/Turboprop)SDR USAASB99185Light · inoperableATL - PILOT REPORTED THE EMERGENCY EXIT LIGHTS REMAIN ON IN THE ARMED POSITION. MAINTENANCE FOUND LOOSE HARDWARE AT THE FORWARD SERVICE DOOR EMERGENCY LIGHT POWER SUPPLY CAUSING A SHORT AND TRIPPING THE 'EMERG LIGHTS PWR' CIRCUIT BREAKER. SECURED HARDWARE ATJul 26, 1999 · N278AU · Boeing 7372B7 · Emergency LightingSDR USAA990731Floorbeam · corrodedTPA - DURING RON, FOUND 8 SQUARE INCH OF CORROSION ON FLOORBEAM AT STATION 1016 AND BL 0. SPLICED NEW SECTION OF BEAM PER SRM 53-10-9 FIG 2. (M)Jul 17, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAASB99174Engine · failedRDU - FLT 2695 - APPROXIMATELY 60 MILES SOUTH OF ORF AT FL 350, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND STARTED TO LOSE POWER. AIRFRAME VIBRATION WAS ALSO NOTED. CREW BROUGHT THROTTLE BACK AND RESTORED PARTIAL ENGINE POWER. FLIGHT DIVERTED TO RDUJul 14, 1999 · N283AU · Boeing 7372B7 · Engine (Turbine/Turboprop)SDR USAASB99172O-Ring · damagedPBI-BWI - FLT 2615, DURING CRUISE, THE SYSTEM 'B' HYDRAULIC QUANTITY LIGHT ILLUMINATED FOLLOWED BY LOSS OF PRESSURE ON HYDRAULIC GAUGE. SHORTLY AFTER, THE LOW PRESSURE LIGHTS ON THE 'B' PUMPS ILLUMINATED. CREW SHUT OFF THE 'B' PUMPS AND DECLARED AN EMERGENCYJul 14, 1999 · N283AU · Boeing 7372B7 · Hydraulic System, MainSDR USAASB99170Epr Transmitter · failedCLE - FLT 8027 - APPROXIMATELY 7 MINUTES AFTER TAKEOFF, CREW ENCOUNTERED PROBLEMS WITH THE NR 2 ENGINE EPR AND THE AUTOTHROTTLE DISCONNECTING. WITH FUEL FLOW AT 5.3, NR 1 ENGINE EPR WAS AT 1.78 AND THE NR 2 ENGINE AT 1.41. WHEN AUTOTHROTTLE WAS RE-ENGAGED, TJul 13, 1999 · N272AU · Boeing 7372B7 · Engine Pressure Ratio (EPR)SDR USAASB99168Battery Pack · dischargedCLE - PILOT REPORTED THE OVERWING AND FORWARD GALLEY EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH SWITCH IN ARMED POSITION. WITH SWITCH OFF, ALL LIGHTS EXTINGUISHED. SWITCHING LIGHTS BACK ON, FORWARD GALLEY EEMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE Jul 11, 1999 · N278AU · Boeing 7372B7 · Emergency LightingSDR USAASB99161Light · inoperableBWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE DOORS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT ASSEMBLY AND THE BATTJul 3, 1999 · N267AU · Boeing 7372B7 · Emergency LightingSDR 99ZZZX2823Battery Pack · dischargedBWI - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT ASSEMBLY INOPERABLE AND THE FORWARD ESCAPE SLIDE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND FORWARD SERVICE DOORS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT ASSEMBLY AND THE BATTJul 3, 1999 · N267AU · Boeing 7372B7 · Emergency LightingSDR USAASB99159Fire Loop · failedMCO-BWI - FLT 2662, AT APPROX FL330, CREW RECEIVED AND APU FIRE DETECTION LIGHT. CREW SHUTDOWN THE APU. WITH A/C BEING DOWN TO ONE SOURCE OF ELECT POWER, CREW DIVERTED FLIGHT TO THE NEAREST SUITABLE AIRPORT AT RDU. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NJun 30, 1999 · N269AU · Boeing 7372B7 · Fire DetectionSDR USAA990626Skin · crackedTPA - DURING CX-3 VISUAL INSPECTION, FOUND TWO CRACKS, ONE CRACK .125 INCH AND ONE CRACK .25 INCH LOWER HINGE CUTOUT AT FORWARD SERVICE DOOR SKIN. INSTALLED FILLER, DOUBLER AND FASTENERS PER TR 52-10-01A. (M)Jun 28, 1999 · N276AU · Boeing 7372B7 · Service DoorsSDR USAASB99150Wire Harness · failedRDU - FLT 2826 - EN ROUTE FROM MCO TO BOS, DURING CRUISE, CAPT REPORTED PROBLEMS WITH THE NR 2 FUEL GAUGE. GAUGE WAS UNRELIABLE WITH ITS READINGS AND THE NR 1 FUEL GAUGE WAS ALREADY ON MEL. CREW TRIED RESETTING CIRCUIT BREAKER WITH NO HELP. THE NR 2 FUEL GAJun 20, 1999 · N268AU · Boeing 7372B7 · Fuel System WiringSDR USAASB99134Engine · failedPVD - FLT 2663 - JUST AFTER TAKEOFF, AT APPROXIMATELY 600 FEET, THE CREW HEARD A LOUD BANG. INDICATIONS FOR THE NR 1 ENGINE EGT WERE IN THE YELLOW ARC, REACHING 600 DEGREES MAXIMUM. ALL OTHER INDICATIONS WERE NORMAL. AFTER RETARDING THE THROTTLE ON THE NR 1Jun 2, 1999 · N288AU · Boeing 7372B7 · Engine (Turbine/Turboprop)SDR USAA990477Floorbeam · corrodedTPA - DURING CX-6 CHECK, FOUND CORRODED ARM AT FLOORBEAM, APPROX 6 INCH AT STATION 1016, CENTER LINE OF AIRCRAFT CENTER WEB. CORROSION LEVEL 1. ACCOMPLISHED REPAIR PER EA 64270, FASTENERS WERE BACB30FP6 EXCEPT 13 EXISTING BACB30FP88, MATERIAL .050, 301.5 HARMay 25, 1999 · N270AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA990475Stringer · corrodedTPA - DURING CX-6 CHECK, FOUND CORROSION IN STRINGER 27L APPROX 20 INCH LONG AT STATION 996 TO 1016, CORROSION LEVEL 1. REPLACED CORRODED SECTION OF STRINGER, SPLICED IN NEW STRINGER AT STATION 956 TO 1016 PER SRM 53-10-3 FIG 1. (M)May 25, 1999 · N270AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA990474Skin · corrodedTPA - DURING CX-6 CHECK, FOUND CORROSION IN FUSELAGE SKIN APPROX 3 INCH IN LENGTH LOCATED BELOW STRINGER 27 LEFT AT STATION 976. CORROSION LEVEL 1. ACCOMPLISHED FUSELAGE SKIN EXTERNAL DOUBLER REPAIR PER SRM 53-30-3 FIG 6. (M)May 25, 1999 · N270AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99126Switch · failedBWI - MAINTENANCE FOUND THE CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL SWITCH IN THE COCKPIT. OPERATIONAL CHECK GOOD. (M)May 16, 1999 · N272AU · Boeing 7372B7 · Emergency LightingSDR USAA990438Skin · crackedTPA - DURING CX-2 CHECK, FOUND .375 INCH LONG SKIN CRACK, LEFT FUSELAGE, 2 INCH AFT OF BS 727B AT LOWER EDGE OF STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. DOUBLER MADE OF 2024T3 - .063 PER BOEING SRM 53-30-3 FIG 1. (M)May 7, 1999 · N272AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99120Transformer · failedIAD - FL2721 - ON DESCENT, CREW NOTICED AN ELECTRICAL SMELL IN THE FORWARD CABIN. FOUND THE CIRCUIT BREAKER FOR THE FORWARD PASSENGER CABIN CEILING LIGHT TRIPPED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT CABIN CEILINGMay 3, 1999 · N279AU · Boeing 7372B7 · Passenger Compartment LightingSDR USAASB9918Battery Pack · dischargedCLE - MAINTENANCE FOUND THE CENTER CABIN CEILING EMERGENCY EXIT SIGN LIGHT DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)May 2, 1999 · N270AU · Boeing 7372B7 · Emergency LightingSDR USAASB99117Batteries · dischargedCLE - MAINTENANCE FOUND THE EMERGNCY LIGHT IN THE COCKPIT CEILING WILL NOT ILLUMINATE WHEN TESTED. MAINTENANCE FOUND BATTERIES CORRODED WHICH IN TURN HAD SPREAD TO THE LIGHT ASSEMBLY. REMOVED AND REPLACED ENTIRE LIGHT ASSEMBLY (P/N 10-0067-9) INCLUDING BATTEMay 2, 1999 · N280AU · Boeing 7372B7 · Emergency LightingSDR USAA990433Skin · crackedTPA - DURING CX-4 CHECK VISUAL CONFIRMED BY EDDY CURRENT INSPECTION, FOUND A .125 INCH CRACK IN SKIN AT DOOR SILL IN RIVET HOLE STATION 343. INSTALLED DOUBLER PER EA 64494. (M)May 2, 1999 · N271AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
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