N819AL, cancelled Nov 14, 2005

Service difficulty reports · 115

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 = 'N819AL' AND deregistration_id = 'N819AL-2005-11-14'
  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 TSAA0524018Circuit Breaker · damagedCREW REPORTED SMOKE IN THE COCKPIT. SMOKE FROM CB PANEL BEHIND F/O. SLIDING WINDOW OPENED TO VENT SMOKE. RETURNED TO GATE. REMOVED AND REPLACED THE APU GCU. DID NOT CURE PROBLEM. FOUND B-LEG ON APU GENERATOR DEAD. DEFER PER MEL 24-2. PLACARDS INSTALLEDApr 4, 2005 · N819AL · Boeing 73725A · DC Power Distribution SystemSDR TSAA0421081Clamp · loosePRESSURIZATION CHECKED BEFORE TAKEOFF, CABIN CLIMBED TO 1,000 FT BY THE TIME AIRCRAFT LEVELED AT 3,000 FT. RETURNED TO OGG. NOTE THAT THE RIGHT PACK WAS DEACTIVATED PRIOR TO THIS FLIGHT DUE TO REPORTS OF A WHOOSHING SOUND NEAR ROW 7 & 8. THE FIRST OFFICER FNov 30, 2004 · N819AL · Boeing 73725A · Air Distribution SystemSDR TSAA0472079Engine · failedNON-ETOPS FLT. 241, HNL-LIH: CLIMBING THROUGH 8,000 FEET, HEARD A LOUD BANG AND THE AIRCRAFT YAWED RIGHT. THE NR 2 ENGINE EPR DROPPED FROM 1.82 TO 1.76. REPORTED THAT A PASSENGER OBSERVED FLAMES EXITING THE NR 2 ENGINE EXHAUST. ALL OTHER ENGINE INDICATIONS Nov 27, 2004 · N819AL · Boeing 73725A · Engine (Turbine/Turboprop)SDR TSAA0473068Fcu · malfunctionedON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, ENGINE POWER ADVANCED NORMALLY UNTIL 1.96-1.97 EPR INDICATION. MAX-POWER OBTAINED WAS 1.97 EPR WITH N1 AT 94 PERCENT; FURTHER THRUST LEVER MOVEMENT HAD NO EFFECT. REMOVED AND REPLACED THE NR 1 ENGINE FCU Sep 14, 2004 · N819AL · Boeing 73725A · Fuel Control/Turbine EnginesSDR TSAA0431067Indicator · slowNON-ETOPS FLIGHT 62, HNL-OGG: ON TAKEOFF 80KTS CROSS-CHECK WAS OK, AFTER LIFTOFF THE FIRST-OFFICERS AIRSPEED INDICATOR READ 50KTS SLOWER THAN CAPTAIN’S STANDBY INDICATOR. RETURNED TO HNL. CLEARED FIRST-OFFICERS PITOT TUBE OF DEBRIS IAW AMM 34-11-0, LEAK AND Sep 12, 2004 · N819AL · Boeing 73725A · Airspeed/Mach IndicatorSDR TSAA0477066Engine · malfunctionedON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, MAX-EPR INDICATION OF 1.96. RETURNED TO HNL. CLEANED DEBRIS FROM PT2 LINE AND VERIFIED SECURITY OF ALL EPR LINES. PERFORMED ENGINE RUN FOR TAKEOFF POWER VERIFICATION, OPS CHECK OK. AIRCRAFT RETURNED TO SSep 11, 2004 · N819AL · Boeing 73725A · Engine (Turbine/Turboprop)SDR TSAA0452026Door Frame · corrodedFOUND CORROSION ON FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED REPAIR DOUBLERS AND TRIPLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETEDFeb 4, 2004 · N819AL · Boeing 73725A · Fuselage Main, StructureSDR TSAA0477018Circuit Breaker · trippedFLT 280 - HNL-KOA - ABORTED TAKEOFF DUE TO BOTH EPR GAUGES INOPERATIVE. C/B'S RESET, NO FLAGS. RAN BOTH NR 1 AND NR 2 ENGINE AFTER EPR C/B RESET. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jan 9, 2004 · N819AL · Boeing 73725A · Engine Pressure Ratio (EPR)SDR TSAA0333147Battery Pack · inoperativeREPLACED AFT ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jun 7, 2003 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA0333146Battery Pack · inoperativeREPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jun 7, 2003 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA0353150Crease Beam · corrodedFOUND CORROSION DISCOVERED ON LEFT CREASE BEAM BETWEEN BS 307 AND 310. REMOVED AND REPLACED SECTION BETWEEN BS 307 AND BS 310. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2 AND May 22, 2003 · N819AL · Boeing 73725A · Fuselage Main, StructureSDR TSAA0357117Web · corrodedCORROSION DISCOVERED ON RIGHT WING SPAR WEB AT FSS 540-552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED SECTION OF WEB. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED AND INSTALLED REPAIR PART WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REMay 7, 2003 · N819AL · Boeing 73725A · Leading Edge DevicesSDR TSAA0353133Floorbeam · corrodedFOUND CORROSION DISCOVERED AT BS 312 FLOORBEAM UPPER TEE. CUTOUT DAMAGED SECTION OF STRINGER. FABRIATED NEW CHORD SECTION AND SPLICE ANGLE. DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL.May 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Floor BeamSDR TSAA0353132Stringer · crackedCRACK DISCOVERED ON STRINGER 4 LEFT, LOCATED AT BS 907. CUTOUT DAMGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DIRLLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAWMay 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/StringerSDR TSAA0353120Skin · dentedDENT DISCOVERED ON FUSELAGE SKIN BETWEEN BS 981 AND 996 ALONG STRINGER 14L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED A REPAIR DOUBLER AND TRIPLER. ALODINE, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REMay 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0353119Stringer · dentedDENT DISCOVERED AT BS 376 ALONG STRINGER 17L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAMay 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/StringerSDR TSAA0353118Stringer · corrodedCORROSION DISCOVERED ON STRINGER LOCATED AT BS 967, LBL 7. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETEDMay 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/StringerSDR TSAA0353138Skin · dentedDISCOVERED A 15 INCH GOUGE WITH A DENT LOCATED AT BS 981 THROUGH BS 996, 4 INCHES ABOVE STRINGER 4 LT. CUTOUT GOUGE AND DENTED PORTION OF THE SKIN. FABRICATED DOUBLER AND TRIPLER, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0353139Skin · dentedDISCOVERED A DENT LOCATED AT BS 346, BETWEEN STRINGER 24 AND 25 RIGHT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED A REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIRMay 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0353137Skin · dentedDENT DISCOVERED AT BS 376 ALONG STRINGER 17 LT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0353141Stringer Clip · damagedDISCOVERED A DAMAGED STRINGER CLIP LOCATED AT BS 380, STRINGER 2 RIGHT. REMOVED AND REPLACED DAMAGED CLIP. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-2, FIGURE 1. (M)May 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous StructureSDR TSAA0353140Shear Tie · damagedDISCOVERED A DAMAGED SHEAR TIE LOCATED AT BS 360, BETWEEN STRINGER 14 AND 15 RIGHT. CUTOUT DENTED PORTION. FABRICATED A NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAMay 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, StructureSDR TSAA0351142Angle · crackedDISCOVERED A CRACKED ATTACHMENT ANGLE LOCATED AT BS 289, WL 239. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2. (M)May 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous StructureSDR TSAA0353136Stringer · corrodedCORROSION DISCOVERED AT BS 967, LBL 7, AND WL 171. CUTOUT DAMAGED PORTION OF THE STRINGER. FABRICATED NEW STRINGER SECTION, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETEMay 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/StringerSDR TSAA0353135Web · corrodedCORROSION DISCOVERED BETWEEN FSS 540 AND 552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED PORTION OF THE WEB. FABRICATED NEW WEB SECTION, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMay 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous StructureSDR TSAA0353134Shear Tie · damagedDAMAGED SHEAR TIE DISCOVERED AT BD 908 BETWEEN STRINGERS 14 AND 15 LEFT. CUTOUT DAMAGED SECTION. FABRICATED NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETEDMay 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, StructureSDR TSAA0351124Stringer Clip · crackedCLIP DISCOVERED CRACKED OR TORN ON STRINGER 2R LOCATED AT BS 380. REMOVED DAMAGED CLIP. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS. REPAIR COMPLETED IAW SRM 51-30-2, FIGURE 1. (M)May 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous StructureSDR TSAA0353121Shear Tie · damagedDAMAGE DISCOVERED ON SHEER TIE BETWEEN STRINGER 14 AND 15L AT BS 360. CUTOUT DAMAGED SECTION OF SHEAR TIE. FABRICATED A REPAIR SHEAR TIE AND RADIUS FILLER. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, StructureSDR TSAA0353123Skin · dentedDENT LOCATED AT BS 396 BETWEEN STRINGER 24 AND 25R. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED A NEW STRINGER REPAIR SECTION. ALODINE, PRIMED, AND INSTALLED REPAR PART IAW FASTENERS FROM TABLE 1 MAKING A FAYING SEAL. REPAIR COMPLETED IAW SRM 53-30-3, FMay 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0351143Stringer · damagedDAMAGED STRINGER 2 RIGHT WHILE REMOVING STRINGER CLIP. CUTOUT DAMAGED STRINGER SECTION BETWEEN BS 360 AND BS 389. FABRICATED NEW STRINGER SECTION, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETEDMay 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/StringerSDR TSAA0351148Channel · corrodedFOUND CORROSION ON C-CHANNEL UPPER STRUCTURE LOCATED BETWEEN BS 312 AND BS 344 AT WL 208, LBL 57. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 312 AND BS 344. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPMay 4, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous StructureSDR TSAA0353149Crease Beam · corrodedFOUND CORROSION ON RIGHT CREASE BEAM AROUND NUT PLATE HOLES BETWEEN BS 290 AND 358. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 290 AND BS 358. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED May 4, 2003 · N819AL · Boeing 73725A · Fuselage Main, StructureSDR TSAA0353151Stringer · gougedDAMAGED OR GOUGE STRINGER DISCOVERED AT BS 382. CUTOUT GOUGED AREA. FABRICATED FILLER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 3. (M)Apr 30, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/StringerSDR TSAA0353110Frame · crackedFOUND BS 244 FRAME CRACKED AT RIGHT CREASE BEAM. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-40-3, FIGURE 1. (M)Apr 23, 2003 · N819AL · Boeing 73725A · Fuselage Main, FrameSDR TSAA0353111Floorbeam · corrodedFOUND CORROSION ON UPPER FLOORBEAM AT BS 344 BLENDED OUT 1 INCH BY 1 INCH AREA IN TWO PLACES. CUTOUT DAMAGED AREA. FABRICATED NEW FLOORBEAM SECTION PER TABLE II, DETAIL I. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET MAKING A FAYING SURFACE SEAL. REPAIR COApr 23, 2003 · N819AL · Boeing 73725A · Fuselage Main, Floor BeamSDR TSAA0333021Battery Pack · incorrectREPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Feb 2, 2003 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA0233215Battery Pack · dischargedREPLACED NR 1,2,4, AND 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE.Oct 15, 2002 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA0253203Skin · gougedREMOVED DAMAGE ON FWD CARGO DOOR CUT OUT. PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. INSTALLED REPAIR IAW SRM. AIRCRAFT RETURNED TO SERVICE.(TSAA8003321)Oct 1, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0225160Slide · defectiveDURING A ROUTINE TRAINING EXERCISE AND AFTER SUCCESSFUL SLIDE DEPLOYMENT, THE SLIDE ASSEMBLY EXPLODED AT THE SEAM. NO HARM TO PERSONNEL. REMOVED AND REPLACED SLIDE; CONTINUED WITH EXERCISE. SLIDE SENT TO VENDOR FOR EVALUATION.Jul 11, 2002 · N819AL · Boeing 73725A · Escape SlideSDR TSAA0232137Switch · stuckANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON BOTH SYSTEMS DURING FLIGHT. DUE TO WEATHER CONDITIONS, RUNWAY LENGTH AND AIRCRAFT WEIGHT FOR THE AIRPORT, THE AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A DEFECTIVE LANDING GEAR LEVER UP SWITCHMay 12, 2002 · N819AL · Boeing 73725A · Landing Gear SelectorSDR TSAA0257032Structure · crackedREPAIRED CRACK AT NR 5 SLAT STATION 195.53. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .050 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRJan 8, 2002 · N819AL · Boeing 73725A · Leading Edge DevicesSDR TSAA0257033Structure · crackedREPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 2 DETAIL II. AIRCJan 8, 2002 · N819AL · Boeing 73725A · Leading Edge DevicesSDR TSAA0253034Floorbeam · crackedFOUND CABIN INTERIOR LONGITUDINAL FLOORBEAM UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITUDINAL FLOORBEAM IAW ECO 223R2 PART II, DEVIATION "C". AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Floor BeamSDR TSAA0253035Skin · crackedREPAIRED A 4 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 18 RT. VERIFEID CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0253036Skin · crackedREPAIRED A 2.5 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 19 RT. VERIFIED CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0253037Skin · delaminatedFOUND DELAMINATION ON LOWER SURFACE OF RIGHT ELEVATOR. TRIMMED OUT DAMAGED LAMINATION TO A SMOOTH SHAPE WITH ROUNDED CORNERS. FABRICATED, CLEANED AND INSTALLED HONEYCOMB REPLACEMENT CORE PLUG. PREPARED AND APPLIED REPAIR PLIES. INSTALLED HEATED BLANKET ANDJan 8, 2002 · N819AL · Boeing 73725A · Elevator, Plate/SkinSDR TSAA0257039Structure · crackedREPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRCRJan 8, 2002 · N819AL · Boeing 73725A · Leading Edge DevicesSDR TSAA0253040Skin · corrodedBLENDED OUT CORROSION ON THE FUSELAGE SKIN AT BS 990 STRINGER 27L BY CUTTING STRINGER 27L IAW SRM 51-10-2. VERIFIED CORROSION REMOVED, CLEANED AND TREATED IAW SRM 51-10-6. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-2 FIGURE 3. AIRCRAFT RETURNED TO Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0253041Floor Support · crackedFOUND CABIN INTERIOR LONGITUTIONAL FLOOR SUPPORT UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITIONAL FLOORBEAM IAW ECO 2223R2 PART II, DEVIATION 'C'. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Miscellaneous StructureSDR TSAA0257031Slat · crackedREPAIRED CRACK AT NR 6 SLAT STATION 370.56. BLENDED OUT THE DAMAGED AREA IAW SRM 57-20-1, FIG 1, PAGE 1. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Leading Edge Devices
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