N816AL, cancelled Jul 9, 2008

Service difficulty reports · 147

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N816AL' AND deregistration_id = 'N816AL-2008-07-09'
  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 TSAA0753059Skin · crackedIN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED LT SKIN CRACKED INSIDE LT WING TO BODY FAIRING. CRACK LOCATED AT BS 747 +19 BETWEEN STRINGER 21L AND 22L. CRACK APPROXIMATELY 1.5 INCHES LONG. CRACK WAS REPAIRED IN ACCORDANCE WITH ECO 3684.Oct 28, 2007 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0753058Skin · crackedIN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED RT SKIN CRACKED IS BETWEEN LAP JOINT AND LARGE EXISTING REPAIR. CRACK LOCATED AT BS 927 +13 BETWEEN STRINGER 20R AND 21R. CRACK APPROXIMATELY 3.5 INCHES LONG. 11/11/07 - CRACK WAS REPAIRED IN ACCORDANCE WITOct 28, 2007 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0734041Hsi · failedCARGO FLIGHT 944 HNL-KOA - DURING CLIMB, THE CAPTAIN NOTED THE NR 1 HORIZONTAL SITUATION INDICATOR HAD THE COMPASS FLAG IN VIEW. THE CAPTAIN ATTEMPTED TO TRANSFER THE COMPASS INDICATION TO BOTH ON NR 2 BUT THE FLAG REMAINED IN VIEW. THE CREW RETURNED TO HNL Jul 18, 2007 · N816AL · Boeing 7372X6C · Directional Gyro and Indicating SystemSDR TSAA0752039Proximity Sensor · dirtyFLIGHT 940 HNL-KOA - ON TAKEOFF ROLL, CREW NOTED THE DOOR ANNUNCIATOR LIGHT ILLUMINATED AND ABORTED THE TAKEOFF AT 110 KNOTS INDICATED AIRSPEED. CREW RETURNED TO THE CARGO RAMP WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AND OPS CHECKED THE FORWARD ENTRY DJun 29, 2007 · N816AL · Boeing 7372X6C · Door Warning SystemSDR TSAA0652092Pitot Tube · obstructedFLIGHT 940 HNL-KOA. AFTER TAKEOFF, CREW NOTED THE LOSS OF FIRST OFFICER'S AIRSPEED INDICATION AND THE ILLUMINATION OF THE DOOR ANNUNCIATOR LIGHT. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED DEBRIS FROM THE FIRST OFFICER'S PITOT TUBE AOct 29, 2006 · N816AL · Boeing 7372X6C · Pitot/Static SystemSDR TSAA0649012Speed Switch · failedFLIGHT 922 HNL OGG- APU OVER-SPEED INDICATION ILLUMINATED AND THE APU AUTO SHUT-DOWN. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 3- SPEED SWITCH; OPS CHECKED NORMAL AND RETURNED THE AIRCRAFT TO SERVICE.Feb 11, 2006 · N816AL · Boeing 7372X6C · APU Core EngineSDR TSAA0527019Sensor · failedNON-ETOPS CARGO FLIGHT 913, HNL-LIH: AFTER TAKEOFF, THE STICK-SHAKER ENGAGED AND REMAINED ON UNTIL LANDING. RETURNED TO HNL. REMOVED AND REPLACED AOA SENSOR VANE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Apr 20, 2005 · N816AL · Boeing 7372X6C · Stall Warning SystemSDR TSAA0471076Line · obstructedFLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS FROM THE PT2 SENSE TUBE BETWEEN THE ENGINE AND TRANSDUCER. ENGINE RUN-UP AND EPR CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.Nov 11, 2004 · N816AL · Boeing 7372X6C · Engine ControlsSDR TSAA0429054Pump · failedHYDRAULIC SYSTEM FAILED. TURNED TO HNL. REMOVE AND REPLACE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-32. LEAK AND OPS CHECK GOOD. REMOVE AND REPLACE NR 1 AND NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTERS. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Jul 16, 2004 · N816AL · Boeing 7372X6C · Hydraulic Pump (Electric/Engine), MainSDR TSAA0352107Skin · corrodedREMOVED DAMAGED AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR DOUBLER FROM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED DOUBLER PER FIGURE 1. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3360. (M)Apr 27, 2003 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0352106Door Frame · crackedREMOVED DAMAGED INBOARD DORR FRAME AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED AN ANGLE DOUBLER FROM .063 INCH 2024-T3 CLAD MATERIAL. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED ANGLED DOUBLER PER FIGURE B. VERIFIED 8110-3 RECEIVED. REPAIR COMPLApr 27, 2003 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0233256Battery Pack · inoperativeREPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 20, 2002 · N816AL · Boeing 7372X6C · Emergency LightingSDR TSAA0233219Battery Pack · dischargedREPLACED NR 3 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Oct 29, 2002 · N816AL · Boeing 7372X6C · Emergency LightingSDR TSAA0234226Indicator · faultyPRIOR TO TAXI, THE CREW NOTICED A STRONG SMELL OF ELECTRIC FUMES FOLLOWED BY SMOKE IN COCKPIT. THE AIRCRAFT WAS SECURED FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE RADAR TRANSCEIVER AND RADAR INDICATOR. OPERATIONAL CHECK OF THE RADAR SYSTEM WAS GOOct 22, 2002 · N816AL · Boeing 7372X6C · Weather Radar SystemSDR TSAA0277212Line · contaminatedON TAKEOFF, THE NR 2 ENGINE WAS AT W.01 EPR, N1-80 PERCENT, EGT-400 DEGREES C, N2-82 PERCENT WITH FUEL FLOW AT 4000 LBS. THE AIRCRAFT RETURNED AND LANDED, WITH NOT FURTHER INCIDENT. MAINTENANCE REMOVED DEBRIS (BUGS) FROM THE NOSE DOME AND CLEARED THE LINES FOct 17, 2002 · N816AL · Boeing 7372X6C · Engine Pressure Ratio (EPR)SDR TSAA0229193Relief Valve · dirtyAT THE TOP OF CLIMB WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE THE NR 2 ENGINE MADE A LOUD BANG LIKE A COMPRESSOR STALL. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. REPLACED THE SAFETY RELIEF VALVE. GROUND OPS CHECKED WERE GOOD. AIROct 14, 2002 · N816AL · Boeing 7372X6C · Cabin Pressure Control SystemSDR TSAA0275194Bleed Valve · malfunctionedTHE NR 2 ENGINE COMPRESSOR STALLED WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE AT TOP OF DECENT. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE PRESSURE RATIO BLEED CONTROL VALVE (PRBC). GROUND OPERATIONAL CHECKSSep 5, 2002 · N816AL · Boeing 7372X6C · Compressor Bleed ValveSDR TSAA0233135Battery Pack · dischargedREPLACED LEFT OVERWING IDENT EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.May 13, 2002 · N816AL · Boeing 7372X6C · Emergency LightingSDR TSAA0233118Battery Pack · dischargedREPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Apr 18, 2002 · N816AL · Boeing 7372X6C · Emergency LightingSDR TSAA0252092Guide · out of adjustFLT 46 - HNL-ITO - FORWARD ENTRY DOOR LIGHT CAME ON DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUSTED THE ROLLER GUIDE SERRATED PLATES AND GUIDE ARM. OPERATIONAL CHECKS WEREMar 27, 2002 · N816AL · Boeing 7372X6C · Passenger/Crew DoorsSDR TSAA0251083Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 26 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTEFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251066Bulkhead · corrodedREMOVED CORROSION AT 1016 SKIN BULKHEAD AND ATTACHING FRAME AFT SIDE OF BULKHEAD BETWEEN LBL 5 TO RBL 5 IAW SRM 53-10-1 FIGURE 1 DETAIL 16. CUT OUT ACCESS HOLE AFT OF BULKHEAD PER DRAWING 65C28106. DOUBLER AND FILLER COMPLETED IAW DRAWING 65C28106. CUT OUT Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, BulkheadSDR TSAA0251075Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 10 RT AT BS 500B PLUS 10 UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251076Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10, BS 4200 PLUS 10 AND BS 500 PLUS 10 ON WINDOW NR 1 RIGHT LOWER AFT CORNER. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251077Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 1 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRIFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251078Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 2 RIGHT UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251079Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S14L BS 727 PLUS 10 ON WINDOW NR 20 LEFT LOWER FORWARD HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, QFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251080Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10L BS 827 PLUS 10 ON WINDOW NR 24 LEFT UPPER AFT HOLES NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251081Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 25 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251082Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R AND S14R ON WINDOW NR 24 RT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, DOUBLER AND TFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251067Floorbeam · corrodedFOUND CORROSION ON THE EXISTING UPPER FLANGE FLOORBEAM REPAIR AT STATION 1016, WL 208 BBI 0 TO LBL 15. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR TSAA0251069Keelbeam · corrodedFOUND CORROSION ON THE KEEL BEAM ON RIGHT LOWER FLANGE IN RIGHT AC BAY AT STATION 557 TO STATION 567, STATION 584 AND STATION 608. BLENDOUT THE CORROSION THEN FLAT PEENED IAW SOPM CHAPTER 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, KeelSDR TSAA0255063Spar · corrodedFOUND CORROSION ON LEFT REAR SPAR CHORD 6 INCHES UP FROM VERTICAL STABILIZER ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Vertical Stabilizer, Spar/RibSDR TSAA0255064Spar · corrodedFOUND CORROSION ON LEFT REAR SPAR CHORD 46 INCHES UP FROM VERTICAL STABILIZER FIN BETWEEN STATION 99.5 AND 108.7 ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Vertical Stabilizer, Spar/RibSDR TSAA0251074Floor Support · corrodedIDENTIFIED CORROSION ON FLOOR SUPPORT DIAGONAL LEFT BETWEEN STATION 1006 AND STATION 1016 LBL 5. REMOVED CORROSION IAW SRM 53-10-1 DETAIL I, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR TSAA0251068Keelbeam · corrodedFOUND CORROSION ON THE KEEL BEAM LOWER CHORD. CONFIRMED CORROSION REMOVED AND NO EVIDENCE OF CRACKS USING HFEC METHOD. REPAIR COMPLETED IAW ECO 3269. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, KeelSDR TSAA0251084Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R ON WINDOW NR 26 RIGHT LOWER FORWARD HOLE NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREA. FABRICFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251085Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R AND S14R ON WINDOW NR 26 RIGHT UPPER AFT HOLES NR 9 AND NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251086Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R BS 867 PLUS 10 ON WINDOW NR 29 RIGHT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED ARFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251087Window Frame · crackedPEFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S-14R BS 420 ONWINDOW NR 4 RIGHT LOWER AFT CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS.Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251088Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 5 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251089Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 6 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251090Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATION ON WINDOW NR 8 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251091Stringer · crackedFOUND CRACKES ON STRINGER 6L AND 7L FORWARD LAV SIDEWALL AREA. TRIMMED OUT DAMAGED PORTIONS OF INTERCOSTAL IAW SRM 51-40-3 FIGURE 1. VERIFIED NO FURTHER CRACKS USING HFEC METHODS AROUND THE TRIMMED OUT AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR TSAA0251094Rib · crackedFOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CRACKS ON VARIOUS SUPPORT RIBS LISTED FROM INBOARD TO OUTBOARD NR 2, 3, 4, 5, 6, 7, AND 8. CUT AND REMOVED PORTIONS OF FORMED SECTIONS. FABRICATED REPAIR PARTS FROM .040 AND .050 INCH THICK 2024 T3. ASSEMBLFeb 26, 2002 · N816AL · Boeing 7372X6C · Horizontal Stabilizer, Spar/RibSDR TSAA0251095Stringer · damagedDAMAGED STRINGER BETWEEN FS 1040 AND FS 1064 STRINGER 27L. REMOVED DAMAGED SECTION IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR DOUBLER USING .040 INCH THICK 2024 T3 IAW SRM 51-20-1 PAGES 10A TO 22. PROTECTED MATERIAL USING AN IRIDITE SOLUTION APPLICATION IAFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR TSAA0133170Battery Pack · dischargedREPLACED AFT ENTRY EMERGENCY IDENT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 1, 2001 · N816AL · Boeing 7372X6C · Emergency LightingSDR TSAA0124097Circuit BreakerFLT 242 - LIH-OGG - THE CREW NOTICED A STRONG ELECTRICAL SMELL COMING FROM THE CENTER OF THE CABIN DURING DESCENT. SMELL DISSIPATED AFTER LANDING. MAUI MAINTENANCE PERSONNEL INSPECTED AND RELEASED THE AIRCRAFT WHEN NO EVIDENCE OF ELECTRICAL FUMES OR ORIGIN CJul 27, 2001 · N816AL · Boeing 7372X6C · Electrical Power SystemSDR TSAA0133093Battery Pack · inoperativeREPLACED AFT SERVICE DOOR IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jul 25, 2001 · N816AL · Boeing 7372X6C · Lighting SystemSDR TSAA0133081Battery Pack · inoperativeREPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 7, 2001 · N816AL · Boeing 7372X6C · Lighting System
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