# N820AL: 1981 Boeing 737-230, registration cancelled 2006-10-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 17, 2006
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-230](https://openairdocs.org/model/boeing-737-230) (registry code 1384401)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22138
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 8, 1996
- Certificate issued: October 17, 2006
- Last registry action: October 17, 2006
- Mode S code: AB30E6
- Owner when cancelled: [Stewart Industries International LLC](https://openairdocs.org/faa-owner/STEWART%20INDUSTRIES%20INTERNATIONAL%20LLC)
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Corporation
- Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N820AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=820AL
- Page: https://openairdocs.org/deregistered/N820AL-2006-10-17

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-230: https://openairdocs.org/model/boeing-737-230.md

## Service difficulty reports (84, newest 50)

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

- [SDR TSAA0678033](https://openairdocs.org/sdr/TSAA0678033), Apr 15, 2006: ISOLATION VALVE. MALFUNCTIONED. 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.
- [SDR TSAA0678034](https://openairdocs.org/sdr/TSAA0678034), Apr 15, 2006: ISOLATION VALVE. MALFUNCTIONED. 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
- [SDR TSAA0678032](https://openairdocs.org/sdr/TSAA0678032), Apr 10, 2006: FRAME. CRACKED. 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), Apr 8, 2006: ISOLATION VALVE. MALFUNCTIONED. 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 PE
- [SDR TSAA0553056](https://openairdocs.org/sdr/TSAA0553056), Dec 14, 2005: SKIN PANEL. CRACKED. 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 OU
- [SDR TSAA0529053](https://openairdocs.org/sdr/TSAA0529053), Nov 1, 2005: PUMP. MALFUNCTIONED. 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 WITH
- [SDR TSAA0457016](https://openairdocs.org/sdr/TSAA0457016), Dec 20, 2003: SPAR. CORRODED. 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 
- [SDR TSAA0457015](https://openairdocs.org/sdr/TSAA0457015), Dec 20, 2003: SPAR. CORRODED. 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, FIGUR
- [SDR TSAA0451014](https://openairdocs.org/sdr/TSAA0451014), Dec 12, 2003: FRAME. CRACKED. 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 PR
- [SDR TSAA0457017](https://openairdocs.org/sdr/TSAA0457017), Dec 3, 2003: SKIN. CORRODED. 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 AN
- [SDR TSAA0451013](https://openairdocs.org/sdr/TSAA0451013), Nov 29, 2003: STRINGER. CORRODED. APU INLET LONGERON STIFFENER, TORQUE BOX, EXFOLIATED. CUT AND REMOVED DAMAGED PORTION OF FORMED STRUCTURE. FABRICATED REPAIR PARTS FROM MATERIALS SPECIFIED IN T
- [SDR TSAA0253247](https://openairdocs.org/sdr/TSAA0253247), Nov 18, 2003: WINDOW FRAME. CRACKED. 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
- [SDR TSAA0253251](https://openairdocs.org/sdr/TSAA0253251), Nov 7, 2003: SKIN. GOUGED. 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.
- [SDR TSAA0253245](https://openairdocs.org/sdr/TSAA0253245), Nov 7, 2003: STRUCTURE. CORRODED. 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 WI
- [SDR TSAA0253246](https://openairdocs.org/sdr/TSAA0253246), Nov 7, 2003: WEB. CRACKED. 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
- [SDR TSAA0377105](https://openairdocs.org/sdr/TSAA0377105), Jun 16, 2003: LINE. LEAKING. 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 TURB
- [SDR TSAA0377041](https://openairdocs.org/sdr/TSAA0377041), Mar 11, 2003: PRESSURE SWITCH. MALFUNCTIONED. 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 FOUN
- [SDR TSAA0333048](https://openairdocs.org/sdr/TSAA0333048), Mar 10, 2003: BATTERY PACK. INOPERATIVE. 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), Nov 20, 2002: FRAME. CORRODED. 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. APP
- [SDR TSAA0251248](https://openairdocs.org/sdr/TSAA0251248), Nov 18, 2002: WINDOW FRAME. CRACKED. 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 
- [SDR TSAA0253242](https://openairdocs.org/sdr/TSAA0253242), Nov 7, 2002: WEB. CRACKED. 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. 
- [SDR TSAA0221175](https://openairdocs.org/sdr/TSAA0221175), Aug 17, 2002: CONTROLLER. MALFUNCTIONED. ON CLIMB OUT, AIRCRAFT WAS UNABLE TO MAINTAIN PRESSURIZATION. AIRCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESS
- [SDR TSAA0221093](https://openairdocs.org/sdr/TSAA0221093), Mar 10, 2002: CONTROLLER. FAILED. 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 
- [SDR TSAA0153161](https://openairdocs.org/sdr/TSAA0153161), Nov 21, 2001: SKIN. CRACKED. 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), Nov 8, 2001: BATTERY PACK. DISCHARGED. 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), Jun 19, 2001: SKIN. DAMAGED. 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 D
- [SDR TSAA0055254](https://openairdocs.org/sdr/TSAA0055254), Dec 27, 2000: SPAR. CORRODED. IDENTIFIED SURFACE CORROSION ON THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD SS 101.90. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AN
- [SDR TSAA0033251](https://openairdocs.org/sdr/TSAA0033251), Dec 26, 2000: BATTERY PACK. INOPERATIVE. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0073187](https://openairdocs.org/sdr/TSAA0073187), Aug 11, 2000: POWER SUPPLY. FAILED. 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 FL
- [SDR TSAA0033180](https://openairdocs.org/sdr/TSAA0033180), Jul 28, 2000: BATTERY PACK. INOPERATIVE. 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), Jun 15, 2000: SENSOR. INOPERATIVE. 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 DE
- [SDR TSAA0033113](https://openairdocs.org/sdr/TSAA0033113), Apr 5, 2000: BATTERY PACK. INOPERATIVE. 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), Mar 9, 2000: BATTERY PACK. INOPERATIVE. 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), Dec 30, 1999: BATTERY PACK. DISCHARGED. 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), Dec 30, 1999: ENGINE. BIRD STRIKE. 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 
- [SDR TSAA9933477](https://openairdocs.org/sdr/TSAA9933477), Nov 3, 1999: BATTERY PACK. DISCHARGED. 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), Sep 29, 1999: BATTERY PACK. DISCHARGED. 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), Sep 11, 1999: BATTERY PACK. DISCHARGED. 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), Jul 21, 1999: SKIN. CORRODED. 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), Jun 17, 1999: BATTERY PACK. DISCHARGED. 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), May 4, 1999: BATTERY PACK. DISCHARGED. 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), Apr 1, 1999: SKIN. GOUGED. 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), Mar 16, 1999: LIGHT. INOPERATIVE. FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSEMBLY NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933008](https://openairdocs.org/sdr/TSAA9933008), Jan 6, 1999: BATTERY. DISCHARGED. REPLACED AFT EMERGENCY SLIDE BATTERY POWR SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9833661](https://openairdocs.org/sdr/TSAA9833661), Dec 31, 1998: BATTERY PACK. DISCHARGED. AFT EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9833640](https://openairdocs.org/sdr/TSAA9833640), Dec 16, 1998: BATTERY PACK. DISCHARGED. REPLACED AFT SLIDE EMERGENCY BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9833626](https://openairdocs.org/sdr/TSAA9833626), Dec 11, 1998: LIGHT. INOP. 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), Dec 11, 1998: BATTERY PACK. DISCHARGED. 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), Dec 3, 1998: CONTROL MODULE. INOPERATIVE. 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), Dec 1, 1998: BATTERY PACK. DISCHARGED. AFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY POWER PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

All 84: https://openairdocs.org/deregistered/N820AL-2006-10-17/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020310003469I](https://openairdocs.org/incident/20020310003469I), Mar 10, 2002: Boeing 737230 (N820AL), Kahului, HI. (-23) Tsaa flt 66, B737-200 aircraft, enroute hnl to ogg experienced loss of pressurization control approximately 5 minutes out of ogg. Declared emergency and…

## Other aircraft with N820AL

- [Registered now](https://openairdocs.org/aircraft/N820AL): Boeing 787-9, S/N 40639, built 2016

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