N820AL, cancelled Oct 17, 2006

Service difficulty reports · 84

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 = 'N820AL' AND deregistration_id = 'N820AL-2006-10-17'
  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 TSAA0678033Isolation Valve · malfunctionedTHRUST REVERSER ISOLATION VALVE ILLUMINATED DURING CLIMBOUT AT 1000 FT. SOCC ADVISED AIRCRAFT TO RETURN TO HNL. LIGHT WENT OUT ON FINAL APPROACH WITH GEAR DOWN. FOUND NOSE GEAR AIR GROUND SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH PER AMM 78-34-61. OPS CHEApr 15, 2006 · N820AL · Boeing 737230 · Engine Thrust ReverserSDR TSAA0678034Isolation Valve · malfunctionedTHRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED DURING CLIMBOUT AT 1000 FT. SOCC ADVISED AIRCRAFT TO RETURN TO HNL. LIGHT WENT OUT ON FINAL APPROACH WITH GEAR DOWN. RE-RIGGED THE NOSE GEAR AIR GROUND CABLE AND SWITCH PER AMM 78-34-61 PG 501. OPS CHECK OKApr 15, 2006 · N820AL · Boeing 737230 · Engine Thrust ReverserSDR TSAA0678032Frame · crackedBS 737 FRAME CRACKED AT STR 18L. REPLACED 727 FRAME AT STR 18L IAW ALOHA'S ECO 1785.Apr 10, 2006 · N820AL · Boeing 737230 · Fuselage Main, FrameSDR TSAA0678031Isolation Valve · malfunctionedTHRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED ON CLIMBOUT. SOCC ADVISED AIRCRAFT TO RETURN TO HNL. REPLACED AB CARD IN ENGINE ACCESSORY UNIT. OPS TEST OK PER MM 78-36-01. AIRCRAFT CLEARED FOR SERVICE. ON THE NEXT FLIGHT (208), THE THRUST REVERSER ISOLApr 8, 2006 · N820AL · Boeing 737230 · Engine Thrust ReverserSDR TSAA0553056Skin Panel · crackedFOUND TWO FUSELAGE SKIN CRACKS AFT OF LT AFT WING-TO-BODY FAIRING: .5 INCH CRACK AT BS 767, STRINGER 17L AND 3 INCH CRACK AT BS 787, STRINGER 18L. CUT CRACKS OUT .040 INCH INSURANCE CUT. PERFORMED HFEC AROUND CUTOUTS, NO CRACK PROPAGATION NOTED IAW BOEING NDec 14, 2005 · N820AL · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0529053Pump · malfunctionedNON-ETOPS FLT 266 HNL-OGG, AFTER TAKEOFF, HYD SYS QUANTITY INDICATION DROPPED TO 1.5 GAL. AND SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC RESERVOIR TO FULL, PERFORMED ENGINE RUN, OPERNov 1, 2005 · N820AL · Boeing 737230 · Hydraulic Pump (Electric/Engine), MainSDR TSAA0457016Spar · corrodedDISCOVERED CORROSION AT WBL 349 AND 503 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED ARE PER SRM 57-30-1, FIGURE 1A AND 1B INSTRUCTIONS. FABRICATED AN .020 INCH THICK EXTERNAL REPAIR DOUBLER FROM 7075-T6 SHEET. CLEAN ANDDec 20, 2003 · N820AL · Boeing 737230 · Wing SparSDR TSAA0457015Spar · corrodedDISCOVERED CORROSION AT WBL 245, 254, 336, AND 341 ON THE UPPER WING SURFACE REAR SPAR. REPAIR CONSISTED OF BLENDING OUT THE DAMAGED AREA PER SRM 57-30-1, FIGURES 1A AND 1B INSTRUCTIONS. REMOVED FASTENERS IN THE BLEND OUT AREA. INSTALLED HI-LOCKS WET WITH BDec 20, 2003 · N820AL · Boeing 737230 · Wing SparSDR TSAA0451014Frame · crackedDISCOVERED CRACK AT BS 727 OUTBOARD CHORD. REMOVED FASTENERS AS REQUIRED COMMON TO BS 727 OUTER CHORD FROM S-27 UP TO S-18. TRIM END OF VERTICAL STIFFENER TO PROVIDE CLEARANCE FOR CHORD SPLICE COMPONENTS. LAID OUT LOCATION FOR CUTTING CHORD. USED REMOVED SDec 12, 2003 · N820AL · Boeing 737230 · Fuselage Main, FrameSDR TSAA0457017Skin · corrodedREMOVED CORROSION FROM RIGHT FIXED LEADING EDGE AT WBL 375. TRIMMED OUT DAMAGED AREA. FABRICATED A FILLER AND DOUBLER PER TABLE 1. ALODIZED ALL TRIMMED EDGES AND BARE SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 57-4Dec 3, 2003 · N820AL · Boeing 737230 · Wing, Plate/SkinSDR TSAA0451013Stringer · corrodedAPU INLET LONGERON STIFFENER, TORQUE BOX, EXFOLIATED. CUT AND REMOVED DAMAGED PORTION OF FORMED STRUCTURE. FABRICATED REPAIR PARTS FROM MATERIALS SPECIFIED IN TABLE 1. APPLIED ONE COAT OF BMS 10-11, TYPE 1 PRIMER, AND INSTALLED REPAIR PARTS WET WITH FASTENENov 29, 2003 · N820AL · Boeing 737230 · APU Cowling/ContainmentSDR TSAA0253247Window Frame · crackedTRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 FILLERS AND REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN, MIN .5 INCH OUTSIDE CORNER RADIUS WITH 2.0 INCH INSIDE CORNER RADIUS AND 5D-6D SPACING AT NEW FASTENER LONov 18, 2003 · N820AL · Boeing 737230 · Fuselage Main, StructureSDR TSAA0253251Skin · gougedTRIMMED OUT DAMAGED AREA. HFEC INSPECTED THE EDGE OF CUTOUT. ENLARGED TRIM BY .04 AS AN INSURANCE CUT. ALODINED AND PRIEMD REWORKED AREA WITH BMS 10-11, TYPE 1. FABRICATED EXTERNAL DOUBLER FROM .063 INCH 2024-T3 CLAD. FABRICATED REPAIR FILLERS FROM 2024-TNov 7, 2003 · N820AL · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0253245Structure · corrodedBLENDED REWORK AREA TO A 10 TO 1 RATION SPANWISE. PERFORMED 10X VISUAL TO ENSURE CORROSION COMPLETELY REMOVED. FLAT PEENED, ALODINED AND PRIMED REWORKED AREA WITH BMS 10-11, TYPE 1. FABRICATED EXTERNAL DOUBLER AND REPAIR STRAP FROM .150 INCH 7075-T7351 PLATNov 7, 2003 · N820AL · Boeing 737230 · Fuselage Main, StructureSDR TSAA0253246Web · crackedTRIMMED OUT DAMAGED WEB. HFEC INSPECTED THE EDGE OF CUTOUT. ENLARGED TRIM BY .04 AS A INSURANCE CUT. FABRICATED A .50 INCH THICK REPAIR WEB, TOW .063 INCH THICK DOUBLERS AND A .063 INCH THICK TAPER FILLER FROM 2024-T3 CLAD SHEET. FABRICATED THREE EACH REPANov 7, 2003 · N820AL · Boeing 737230 · Fuselage Miscellaneous StructureSDR TSAA0377105Line · leakingDURING TAKEOFF ROLL, UNABLE TO ACHIEVE TAKEOFF POWER ON ENGINE NR 2, FIREWALL ONLY GAVE 1.86 EPR. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND A LEAK IN THE TURBINE EXHAUST LINE, REPLACED THE PT7 TUBE ASSY IAW MM 77-00. LEAK CHECK OF LINE OK. JETCAL ACCOMPLJun 16, 2003 · N820AL · Boeing 737230 · Turbine SectionSDR TSAA0377041Pressure Switch · malfunctionedDURING TAKEOFF, WITH TAKEOFF POWER SET THE NR 1 ENGINE EPR WAS 0.25 TOO HIGH. THE AIRCRAFT RETURNED TO HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FOD IN THE NR 1 ENGINE PT2 LINE. THE PT2 LINE WAS CLEANED, AND ENGINE PERFORMANCE RUN WAS COMPLMar 11, 2003 · N820AL · Boeing 737230 · Engine EGT/TIT Indicating SystemSDR TSAA0333048Battery Pack · inoperativeREPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 10, 2003 · N820AL · Boeing 737230 · Emergency LightingSDR TSAA0253240Frame · corrodedBLENDED SURFACE IS SMOOTHLY RADIUSED AND RIDGES BLENDED TO A 10 TO 1 RATIO SPANWISE. VERIFIED CORROSION REMOVED USING NDT METHOD. FLAT PEENED REWORKED AREA. APPLIED ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER TO REPAIR WASHERS AND REWORKED SURFACE. APPLNov 20, 2002 · N820AL · Boeing 737230 · Fuselage Main, FrameSDR TSAA0251248Window Frame · crackedTRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS ONov 18, 2002 · N820AL · Boeing 737230 · Standard Practices/StructuresSDR TSAA0253242Web · crackedREMOVED EXISTING FASTENERS, STIFENERS, FILLERS, AND DAMAGED SECTION OF WEB AS SHOWN ON FIGURE 5. FABRICATED A .050 INCH THICK REINFORCING DOUBLER FROM 7075-T6. ALODINE AND APPLIED BMS 10-11 TYPE 1 PRIMER TO ALL BARE SURFACES. INSTALLED RE-ENFORCING DOUBLER,Nov 7, 2002 · N820AL · Boeing 737230 · Fuselage Miscellaneous StructureSDR TSAA0221175Controller · malfunctionedON CLIMB OUT, AIRCRAFT WAS UNABLE TO MAINTAIN PRESSURIZATION. AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. BITE AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.Aug 17, 2002 · N820AL · Boeing 737230 · Cabin Pressure ControllerSDR TSAA0221093Controller · failedFLT 66 - HNL-OGG - PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED AT 14,000 FT AND STANDBY LIGHT CAME ON. SWITCHED TO STANDBY MODE. CABIN RATE STARTED CLIMBING AND DESCENDING AT 4,000 FPM. SWITCHED TO MANUAL DC THEN AC MODE AND STILL UNABLE TO CONTROL PRESSURIZMar 10, 2002 · N820AL · Boeing 737230 · Cabin Pressure ControllerSDR TSAA0153161Skin · crackedDISCOVERED CRACK AT BS 727A, S-15R. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)Nov 21, 2001 · N820AL · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0133150Battery Pack · dischargedREPLACED FORWARD SERVICE AND ENTRY DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 8, 2001 · N820AL · Boeing 737230 · Emergency LightingSDR TSAA0153079Skin · damagedAIRCRAFT SKIN AND FRAME DAMAGED AT BS 847 THROUGH BS 887, STRINGER 25L THROUGH STRINGER 25R. REMOVED DAMAGED AREA ,PERFORMED HFEC INSPECTION AROUND CUT OUT NO DEFECTS NOTED. REPAIRED STRINGER S27L AT BS 847 IAW SRM 53-10-3 FIG INSTALLATION OF REPAIR DOUBLER Jun 19, 2001 · N820AL · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0055254Spar · corrodedIDENTIFIED SURFACE CORROSION ON THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD SS 101.90. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AND TREATED CORRODED AREA. REPAIR COMPLETED ON 12/26/00 IAW SRM 57-10-1 PAGE 6. (M)Dec 27, 2000 · N820AL · Boeing 737230C · Horizontal Stabilizer, Spar/RibSDR TSAA0033251Battery Pack · inoperativeREPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 26, 2000 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA0073187Power Supply · failedFLT 302 - HNL-OGG - AFTER ENGINE START BOTH NR 1 AND NR 2 FF INDICATORS HAD INDICATION HOWEVER BOTH WERE PULSING. ABORTED TAKEOFF RY8L, NO INDICATION OF FUEL FLOW. TAXIED BACK TO GATE. UPON POWER APPLICATION NEITHER FF INDICATOR ROSE ABOVE MINIMUM SETTINGS.Aug 11, 2000 · N820AL · Boeing 737230C · Powerplant SystemSDR TSAA0033180Battery Pack · inoperativeREPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 28, 2000 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA0027148Sensor · inoperativeFLT 278 - HNL-OGG - RIGHT KRUEGER FLAP (NR 4 LED) WOULD NOT RETRACT AFTER TAKEOFF. CALLED IN WITH SLAT INDICATION PROBLEM. RETURNED TO HONOLULU. NO EMERGENCY DECLARED, AIRCRAFT LANDED WITH NO FURTHER PROBLEMS. REMOVED AND REPLACED EXTEND SENSOR ON THE NR 4Jun 15, 2000 · N820AL · Boeing 737230C · Leading Edge Slat Control SystemSDR TSAA0033113Battery Pack · inoperativeREPLACED NR 3, NR 4 AND NR 6 FLOOR EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Apr 5, 2000 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA0033208Battery Pack · inoperativeREPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 9, 2000 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9933517Battery Pack · dischargedREPLACED NR 1 FLOOR EMERGENCY POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 30, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9905519Engine · bird strikeFLT 63 - HNL-LIH - BIRD STRIKE NR 1 ENGINE. ENGINE ROLLED BACK INITIALLY AND RETURNED TO NORMAL PARAMETERS. RETURNED TO HNL. UNEVENTFUL LANDING. PERFORMED BIRD STRIKE CONDITION INSPECTION IAW FORM M-106. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (Dec 30, 1999 · N820AL · Boeing 737230C · Engine (Turbine/Turboprop)SDR TSAA9933477Battery Pack · dischargedREPLACED AFT SERVICE EMERGENCY EXIT LIGHT POWER PACK DUE TO FLICKERING. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 3, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9933446Battery Pack · dischargedREPLACED NR 4 AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Sep 29, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9933429Battery Pack · dischargedREPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Sep 11, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9957305Skin · corrodedFOUND CORROSION ON LEFT WING AT WS 382. CLEANED AND TREATED. MATERIAL REMOVAL EXCEEDED SRM 57-30-1 LIMITS. ACCOMPLISHED FINAL REPAIR PER ECO 1684R10. (M)Jul 21, 1999 · N820AL · Boeing 737230C · Wing, Plate/SkinSDR TSAA9933261Battery Pack · dischargedREPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jun 17, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9933230Battery Pack · dischargedREPLACED NR 1, NR 2, AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)May 4, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9953179Skin · gougedAIRCRAFT SUSTAINED SKIN DAMAGE BETWEEN BS 867 AND BS 887 AT STRINGER 27 RIGHT. THREE GOUGES NOTED. REPAIRED IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)Apr 1, 1999 · N820AL · Boeing 737230C · Fuselage Main, Plate/SkinSDR TSAA9933149Light · inoperativeFORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSEMBLY NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 16, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9933008Battery · dischargedREPLACED AFT EMERGENCY SLIDE BATTERY POWR SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M)Jan 6, 1999 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9833661Battery Pack · dischargedAFT EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 31, 1998 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9833640Battery Pack · dischargedREPLACED AFT SLIDE EMERGENCY BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 16, 1998 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9833626Light · inopFORWARD SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER ASSY INOP. REPLACED IDENTIFIER LIGHT ASSY, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 11, 1998 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9833623Battery Pack · dischargedFORWARD SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER ASSY INOP. REPLACED ASSY BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 11, 1998 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9833609Control Module · inoperativeCENTER EMERGENCY EXIT CONTROL MODULE ASSY INOP. REPLACED CENTER EMERGENCY EXIT CONTROL MODULE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 3, 1998 · N820AL · Boeing 737230C · Emergency LightingSDR TSAA9833607Battery Pack · dischargedAFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY POWER PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 1, 1998 · N820AL · Boeing 737230C · Emergency Lighting
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