# Service difficulty reports: N820AL, cancelled Oct 17, 2006 A list on [N820AL, cancelled Oct 17, 2006](https://openairdocs.org/deregistered/N820AL-2006-10-17.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 84 reports - [SDR TSAA0678033](https://openairdocs.org/sdr/TSAA0678033.md): Isolation Valve · malfunctioned · Apr 15, 2006 · N820AL · Boeing 737230 · Engine Thrust Reverser > THRUST 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 CHE - [SDR TSAA0678034](https://openairdocs.org/sdr/TSAA0678034.md): Isolation Valve · malfunctioned · Apr 15, 2006 · N820AL · Boeing 737230 · Engine Thrust Reverser > THRUST 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 OK - [SDR TSAA0678032](https://openairdocs.org/sdr/TSAA0678032.md): Frame · cracked · Apr 10, 2006 · N820AL · Boeing 737230 · Fuselage Main, Frame > BS 737 FRAME CRACKED AT STR 18L. REPLACED 727 FRAME AT STR 18L IAW ALOHA'S ECO 1785. - [SDR TSAA0678031](https://openairdocs.org/sdr/TSAA0678031.md): Isolation Valve · malfunctioned · Apr 8, 2006 · N820AL · Boeing 737230 · Engine Thrust Reverser > THRUST 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 ISOL - [SDR TSAA0553056](https://openairdocs.org/sdr/TSAA0553056.md): Skin Panel · cracked · Dec 14, 2005 · N820AL · Boeing 737230 · Fuselage Main, Plate/Skin > FOUND 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 N - [SDR TSAA0529053](https://openairdocs.org/sdr/TSAA0529053.md): Pump · malfunctioned · Nov 1, 2005 · N820AL · Boeing 737230 · Hydraulic Pump (Electric/Engine), Main > NON-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, OPER - [SDR TSAA0457016](https://openairdocs.org/sdr/TSAA0457016.md): Spar · corroded · Dec 20, 2003 · N820AL · Boeing 737230 · Wing Spar > DISCOVERED 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 AND - [SDR TSAA0457015](https://openairdocs.org/sdr/TSAA0457015.md): Spar · corroded · Dec 20, 2003 · N820AL · Boeing 737230 · Wing Spar > DISCOVERED 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 B - [SDR TSAA0451014](https://openairdocs.org/sdr/TSAA0451014.md): Frame · cracked · Dec 12, 2003 · N820AL · Boeing 737230 · Fuselage Main, Frame > DISCOVERED 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 S - [SDR TSAA0457017](https://openairdocs.org/sdr/TSAA0457017.md): Skin · corroded · Dec 3, 2003 · N820AL · Boeing 737230 · Wing, Plate/Skin > REMOVED 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 57-4 - [SDR TSAA0451013](https://openairdocs.org/sdr/TSAA0451013.md): Stringer · corroded · Nov 29, 2003 · N820AL · Boeing 737230 · APU Cowling/Containment > APU 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 FASTENE - [SDR TSAA0253247](https://openairdocs.org/sdr/TSAA0253247.md): Window Frame · cracked · Nov 18, 2003 · N820AL · Boeing 737230 · Fuselage Main, Structure > TRIMMED 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 LO - [SDR TSAA0253251](https://openairdocs.org/sdr/TSAA0253251.md): Skin · gouged · Nov 7, 2003 · N820AL · Boeing 737230 · Fuselage Main, Plate/Skin > TRIMMED 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-T - [SDR TSAA0253245](https://openairdocs.org/sdr/TSAA0253245.md): Structure · corroded · Nov 7, 2003 · N820AL · Boeing 737230 · Fuselage Main, Structure > BLENDED 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 PLAT - [SDR TSAA0253246](https://openairdocs.org/sdr/TSAA0253246.md): Web · cracked · Nov 7, 2003 · N820AL · Boeing 737230 · Fuselage Miscellaneous Structure > TRIMMED 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 REPA - [SDR TSAA0377105](https://openairdocs.org/sdr/TSAA0377105.md): Line · leaking · Jun 16, 2003 · N820AL · Boeing 737230 · Turbine Section > DURING 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 ACCOMPL - [SDR TSAA0377041](https://openairdocs.org/sdr/TSAA0377041.md): Pressure Switch · malfunctioned · Mar 11, 2003 · N820AL · Boeing 737230 · Engine EGT/TIT Indicating System > DURING 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 COMPL - [SDR TSAA0333048](https://openairdocs.org/sdr/TSAA0333048.md): Battery Pack · inoperative · Mar 10, 2003 · N820AL · Boeing 737230 · Emergency Lighting > REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0253240](https://openairdocs.org/sdr/TSAA0253240.md): Frame · corroded · Nov 20, 2002 · N820AL · Boeing 737230 · Fuselage Main, Frame > BLENDED 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. APPL - [SDR TSAA0251248](https://openairdocs.org/sdr/TSAA0251248.md): Window Frame · cracked · Nov 18, 2002 · N820AL · Boeing 737230 · Standard Practices/Structures > TRIMMED 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 O - [SDR TSAA0253242](https://openairdocs.org/sdr/TSAA0253242.md): Web · cracked · Nov 7, 2002 · N820AL · Boeing 737230 · Fuselage Miscellaneous Structure > REMOVED 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, - [SDR TSAA0221175](https://openairdocs.org/sdr/TSAA0221175.md): Controller · malfunctioned · Aug 17, 2002 · N820AL · Boeing 737230 · Cabin Pressure Controller > ON 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. - [SDR TSAA0221093](https://openairdocs.org/sdr/TSAA0221093.md): Controller · failed · Mar 10, 2002 · N820AL · Boeing 737230 · Cabin Pressure Controller > FLT 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 PRESSURIZ - [SDR TSAA0153161](https://openairdocs.org/sdr/TSAA0153161.md): Skin · cracked · Nov 21, 2001 · N820AL · Boeing 737230 · Fuselage Main, Plate/Skin > DISCOVERED CRACK AT BS 727A, S-15R. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0133150](https://openairdocs.org/sdr/TSAA0133150.md): Battery Pack · discharged · Nov 8, 2001 · N820AL · Boeing 737230 · Emergency Lighting > REPLACED FORWARD SERVICE AND ENTRY DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0153079](https://openairdocs.org/sdr/TSAA0153079.md): Skin · damaged · Jun 19, 2001 · N820AL · Boeing 737230 · Fuselage Main, Plate/Skin > AIRCRAFT 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 - [SDR TSAA0055254](https://openairdocs.org/sdr/TSAA0055254.md): Spar · corroded · Dec 27, 2000 · N820AL · Boeing 737230C · Horizontal Stabilizer, Spar/Rib > IDENTIFIED 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) - [SDR TSAA0033251](https://openairdocs.org/sdr/TSAA0033251.md): Battery Pack · inoperative · Dec 26, 2000 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0073187](https://openairdocs.org/sdr/TSAA0073187.md): Power Supply · failed · Aug 11, 2000 · N820AL · Boeing 737230C · Powerplant System > FLT 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. - [SDR TSAA0033180](https://openairdocs.org/sdr/TSAA0033180.md): Battery Pack · inoperative · Jul 28, 2000 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0027148](https://openairdocs.org/sdr/TSAA0027148.md): Sensor · inoperative · Jun 15, 2000 · N820AL · Boeing 737230C · Leading Edge Slat Control System > FLT 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 4 - [SDR TSAA0033113](https://openairdocs.org/sdr/TSAA0033113.md): Battery Pack · inoperative · Apr 5, 2000 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 3, NR 4 AND NR 6 FLOOR EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033208](https://openairdocs.org/sdr/TSAA0033208.md): Battery Pack · inoperative · Mar 9, 2000 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933517](https://openairdocs.org/sdr/TSAA9933517.md): Battery Pack · discharged · Dec 30, 1999 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 1 FLOOR EMERGENCY POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9905519](https://openairdocs.org/sdr/TSAA9905519.md): Engine · bird strike · Dec 30, 1999 · N820AL · Boeing 737230C · Engine (Turbine/Turboprop) > FLT 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. ( - [SDR TSAA9933477](https://openairdocs.org/sdr/TSAA9933477.md): Battery Pack · discharged · Nov 3, 1999 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED AFT SERVICE EMERGENCY EXIT LIGHT POWER PACK DUE TO FLICKERING. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933446](https://openairdocs.org/sdr/TSAA9933446.md): Battery Pack · discharged · Sep 29, 1999 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 4 AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933429](https://openairdocs.org/sdr/TSAA9933429.md): Battery Pack · discharged · Sep 11, 1999 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9957305](https://openairdocs.org/sdr/TSAA9957305.md): Skin · corroded · Jul 21, 1999 · N820AL · Boeing 737230C · Wing, Plate/Skin > FOUND 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) - [SDR TSAA9933261](https://openairdocs.org/sdr/TSAA9933261.md): Battery Pack · discharged · Jun 17, 1999 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933230](https://openairdocs.org/sdr/TSAA9933230.md): Battery Pack · discharged · May 4, 1999 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED NR 1, NR 2, AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9953179](https://openairdocs.org/sdr/TSAA9953179.md): Skin · gouged · Apr 1, 1999 · N820AL · Boeing 737230C · Fuselage Main, Plate/Skin > AIRCRAFT 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) - [SDR TSAA9933149](https://openairdocs.org/sdr/TSAA9933149.md): Light · inoperative · Mar 16, 1999 · N820AL · Boeing 737230C · Emergency Lighting > FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSEMBLY NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933008](https://openairdocs.org/sdr/TSAA9933008.md): Battery · discharged · Jan 6, 1999 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED AFT EMERGENCY SLIDE BATTERY POWR SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833661](https://openairdocs.org/sdr/TSAA9833661.md): Battery Pack · discharged · Dec 31, 1998 · N820AL · Boeing 737230C · Emergency Lighting > AFT EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833640](https://openairdocs.org/sdr/TSAA9833640.md): Battery Pack · discharged · Dec 16, 1998 · N820AL · Boeing 737230C · Emergency Lighting > REPLACED AFT SLIDE EMERGENCY BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833626](https://openairdocs.org/sdr/TSAA9833626.md): Light · inop · Dec 11, 1998 · N820AL · Boeing 737230C · Emergency Lighting > FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER ASSY INOP. REPLACED IDENTIFIER LIGHT ASSY, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833623](https://openairdocs.org/sdr/TSAA9833623.md): Battery Pack · discharged · Dec 11, 1998 · N820AL · Boeing 737230C · Emergency Lighting > FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER ASSY INOP. REPLACED ASSY BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833609](https://openairdocs.org/sdr/TSAA9833609.md): Control Module · inoperative · Dec 3, 1998 · N820AL · Boeing 737230C · Emergency Lighting > CENTER EMERGENCY EXIT CONTROL MODULE ASSY INOP. REPLACED CENTER EMERGENCY EXIT CONTROL MODULE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833607](https://openairdocs.org/sdr/TSAA9833607.md): Battery Pack · discharged · Dec 1, 1998 · N820AL · Boeing 737230C · Emergency Lighting > AFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY POWER PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) Next page: https://openairdocs.org/deregistered/N820AL-2006-10-17/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N820AL-2006-10-17/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.