# N821AL: 1985 Boeing 737-230, registration cancelled 2008-07-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 30, 2008
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-230](https://openairdocs.org/model/boeing-737-230) (registry code 1384401)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 23155
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 30, 1998
- Last registry action: July 30, 2008
- Mode S code: AB349D
- 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/N821AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=821AL
- Page: https://openairdocs.org/deregistered/N821AL-2008-07-30

From the FAA registry file of November 5, 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 (105, newest 50)

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

- [SDR TSAA0736042](https://openairdocs.org/sdr/TSAA0736042), Jul 31, 2007: DUCT. FAILED. NON-ETOPS FLIGHT 40 HNL - ITO, AFTER LANDING IN ITO THE CREW STARTED THE APU AND HAD A WING TO BODY OVERHEAT INDICATION. THE APU WAS SHUT DOWN. MAINTENANCE FOUN
- [SDR TSAA0732033](https://openairdocs.org/sdr/TSAA0732033), Jun 15, 2007: ACTUATOR. MALFUNCTIONED. FLIGHT 90 HNL- KOA. ON APPROACH TO KOA WHEN THE CREW LOWED THE GEAR HANDLE, THE TWO MAIN GEAR SHOWED DOWN AND LOCKED BUT THE NOSE GEAR SHOWED UP AND CREW DIDN’T
- [SDR TSAA0753021](https://openairdocs.org/sdr/TSAA0753021), May 3, 2007: SKIN PANEL. CRACKED. WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 2005-13-30 A CRACK APPROX 3" LONG, LOCATED AT BS947 +15 BETWEEN STR 21L AND STR 22L WAS DISCOVERED. [SUP 05-22-07
- [SDR TSAA0753020](https://openairdocs.org/sdr/TSAA0753020), May 3, 2007: SKIN PANEL. CRACKED. WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 2005-13 A CRACK APPROX 2" LONG WAS DISCOVERED AT BS887 +3 BETWEEN STR 23R AND STR 24R. [SUP 05-22-07] CRACK APPRO
- [SDR TSAA0753019](https://openairdocs.org/sdr/TSAA0753019), May 2, 2007: FRAME. CRACKED. DURING INSPECTION OF THE BS 178 WEB, CRACKS WERE DISCOVERED ON THE BS 188 FRAME AT WL 207 ON BOTH LEFT AND RIGHT SIDES. LEFT SIDE CRACK IS APPROX 1.75 INCHES LO
- [SDR TSAA0628029](https://openairdocs.org/sdr/TSAA0628029), Apr 3, 2006: WIRE. BROKEN. NR 1 ENGINE SHUT DOWN WITHOUT CREW ACTION AFTER NORMAL START, DURING PUSHBACK. FUEL VALVE CLOSED LIGHT ILLUMINATED. REMOVED AND REPLACED THE LT FUEL SHUT OFF VA
- [SDR TSAA0653014](https://openairdocs.org/sdr/TSAA0653014), Mar 8, 2006: SKIN PANEL. GOUGED. RIGHT HAND SIDE OF FUSELAGE GOUGED (3 LENGTH) AT BS 190 BELOW S19R. MAINTENANCE REPAIRED WITH FABRICATED .050 (2024-T3) EXTERNAL SKIN DOUBLER 9.5 X 6.75 INCHES 
- [SDR TSAA0553060](https://openairdocs.org/sdr/TSAA0553060), Oct 24, 2005: SKIN. CORRODED. SECTION 46 FUSELAGE SKIN WITH CORROSION AT BS 998.40, LBL 6.75.
- [SDR TSAA0553059](https://openairdocs.org/sdr/TSAA0553059), Oct 24, 2005: CLIP. CRACKED. BULKHEAD BS 727, WL 202.6, RBL 10.0", CLIP UPPER CRACKED.
- [SDR TSAA0557058](https://openairdocs.org/sdr/TSAA0557058), Oct 24, 2005: SPAR. CORRODED. RIGHT WING FRONT SPAR, LOWER CORD FWD FLANGE CORRODED AT SLAT STA 243.0 AND SLAT STA 254.0.
- [SDR TSAA0549035](https://openairdocs.org/sdr/TSAA0549035), Aug 7, 2005: CONNECTOR. DAMAGED. NON-ETOPS ON TAXI AFTER LANDING THE CREW GOT AN APU FIRE WARNING LIGHT, COMPLETED APU FIRE CHECK LIST, SHUTDOWN APU AND DISCHARGED APU FIRE BOTTLE. FIRE WARNING
- [SDR TSAA0532022](https://openairdocs.org/sdr/TSAA0532022), May 28, 2005: TIRE. FAILED. NON-ETOPS FLT 68, HNL-ITO: ON TAKEOFF ROLL, FELT LIKE BOTH RIGHT MAIN LANDING GEAR TIRES BLEW. FOLLOWED BY AN EXTREME STRUCTURAL POUNDING COMING FROM THE RIGHT 
- [SDR TSAA0429085](https://openairdocs.org/sdr/TSAA0429085), Dec 28, 2004: LINE. LEAKING. FLT 46, HNL-ITO: HYDRAULIC FLUID QUANTITY DECREASING DURING GEAR RETRACTION. RETURNED TO HNL. UNEVENTFUL LANDING. WHILE ON GROUND, HYDRAULIC FLUID QUANTITY CONT
- [SDR TSAA0479053](https://openairdocs.org/sdr/TSAA0479053), Jul 7, 2004: TRANSMITTER. FAILED. ON TAKEOFF ROLL, THE NR 2 ENGINE OIL QUANTITY INDICATOR DROPPED TO ZERO. REJECTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE NR 2 ENGINE OIL QUANTITY INDICA
- [SDR TSAA0479020](https://openairdocs.org/sdr/TSAA0479020), Feb 5, 2004: BYPASS SWITCH. FAULTY. NR 2 ENGINE OIL BYPASS LIGHT CAME ON. PERFORMED QRH PROCEDURES, ENGINE SHUTDOWN AND LANDED AT HNL. ACCOMPLISHED BREATHER PRESSURE CHECK PER FORM M-209. CHECK GO
- [SDR TSAA0253257](https://openairdocs.org/sdr/TSAA0253257), Dec 18, 2003: WINDOW FRAME. CRACKED. TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN.
- [SDR TSAA0253258](https://openairdocs.org/sdr/TSAA0253258), Dec 18, 2003: WINDOW FRAME. CRACKED. TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN.
- [SDR TSAA0253260](https://openairdocs.org/sdr/TSAA0253260), Dec 18, 2003: WINDOW FRAME. CRACKED. TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN.
- [SDR TSAA0353152](https://openairdocs.org/sdr/TSAA0353152), Jun 13, 2003: SKIN. CRACKED. REPAIRED FUSELAGE SKIN CRACK AT BS 767, STRINGER 19 RIGHT. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN. VERIFIED CRACK REMOVED USING HFEC METHOD. FABRICATED AND 
- [SDR TSAA0333125](https://openairdocs.org/sdr/TSAA0333125), May 24, 2003: BATTERY PACK. INOPERATIVE. REPLACED FORWARD ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0379008](https://openairdocs.org/sdr/TSAA0379008), Jan 25, 2003: ENGINE. FAILED. AT CRUISE ALTITUDE, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AND WOULD NOT GO OUT AT REDUCED THRUST SETTING. THE CREW SHUTDOWN THE NR 1 ENGINE AND LA
- [SDR TSAA0333013](https://openairdocs.org/sdr/TSAA0333013), Jan 24, 2003: BATTERY PACK. DISCHARGED. REPLACED LEFT AFT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253252](https://openairdocs.org/sdr/TSAA0253252), Jan 14, 2003: SKIN. CRACKED. CUT OUT DAMAGED SKIN AREA AT BS 520 MAINTAINING A .50 INCH MINIMUM RADIUS AND 2D EDGE MARGIN. VERIFIED EDGE OF TRIM USING HFEC METHOD. ENLARGED TRIMMED AREA BY 
- [SDR TSAA0253253](https://openairdocs.org/sdr/TSAA0253253), Jan 14, 2003: SKIN. CORRODED. CUTOUT DAMAGED SKIN ARE AT BS 908 MAINTAINING A .50 INCH MINIMUM RADIUS AND 2D EDGE MARGIN. VERIFIED CRACK REMOVED USING HFEC METHOD. ENLARGED TRIMMED AREA BY .
- [SDR TSAA0253254](https://openairdocs.org/sdr/TSAA0253254), Dec 20, 2002: SKIN. CORRODED. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN. HFEC INSPECTED THE EDGE OF TRIM. ENLARGED TRIMMED BY .04 INCH INSURANCE CUT. FABRICATED AND INSTALLED A .071 INCH RE
- [SDR TSAA0253259](https://openairdocs.org/sdr/TSAA0253259), Dec 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 FIGURE 1, MAINTAINING 2D EDGE MARGIN
- [SDR TSAA0233230](https://openairdocs.org/sdr/TSAA0233230), Nov 8, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 2 FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253216](https://openairdocs.org/sdr/TSAA0253216), Oct 13, 2002: STIFFENER. CRACKED. REPAIRED CRACK AT BS 178, WI 184 LBL 5.7 VERTICAL CHORD. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN AREA. VERIFIED CRACK REMOVED USING HFEC METHOD. FABRICATED A
- [SDR TSAA0253195](https://openairdocs.org/sdr/TSAA0253195), Sep 4, 2002: SKIN. CRACKED. TRIMMED OUT DAMAGE SKIN AT BS 749 STRINGER 18R. HFEC EDGE OF TRIMMED AREA, NO DEFECTS NOTED.
- [SDR TSAA0233160](https://openairdocs.org/sdr/TSAA0233160), Jun 29, 2002: BATTERY PACK. DISCHARGED. REPLACED NR FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233158](https://openairdocs.org/sdr/TSAA0233158), Jun 17, 2002: BATTERY PACK. DISCHARGED. REPLACED FORWARD SERVICE DOOR IDENT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233159](https://openairdocs.org/sdr/TSAA0233159), Jun 17, 2002: LIGHT. INOPERATIVE. REPLACED FORWARD SERVICE DOOR IDENT LIGHT ASSEMBLY DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233028](https://openairdocs.org/sdr/TSAA0233028), Jan 25, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253022](https://openairdocs.org/sdr/TSAA0253022), Jan 14, 2002: SKIN. CRACKED. REPAIRED CRACK AT FS 965 (AFT ENTRY DOOR). CUTOUT AND REMOVED CRACK PORTION OF SKIN AROUND LOWER FORWARD AREA. PERFORMED HFEC INSPECTION AROUND CUT OUT AREA NO 
- [SDR TSAA0133144](https://openairdocs.org/sdr/TSAA0133144), Oct 20, 2001: BATTERY PACK. DISCHARGED. REPLACED NR 5 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0179112](https://openairdocs.org/sdr/TSAA0179112), Aug 23, 2001: INDICATOR. FALSE INDICATION. FLT 246 - HNL-ITO - DIVERT TO OGG, DURING CLIMB AT APPROX 200 FT PILOT NOTICED THE NR 1 ENGINE OIL TEMPERATURE GAUGE IN THE YELLOW BAND, 140 DEGREES. CONTINUED 
- [SDR TSAA0133024](https://openairdocs.org/sdr/TSAA0133024), Mar 2, 2001: LIGHT. INOPERATIVE. REPLACED CENTER AISLE EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153006](https://openairdocs.org/sdr/TSAA0153006), Feb 15, 2001: FRAME. CRACKED. IDENTIFIED CRACK AT FASTENER HOLE CAUSED BY A SHORT EDGE DISTANCE AT BS 1112 FRAME. TRIM OUT THE DAMAGED AREA OF FRAME, FABRICATED AND INSTALLED FILLER OF 056 I
- [SDR TSAA0155001](https://openairdocs.org/sdr/TSAA0155001), Jan 8, 2001: SPAR. CRACKED. IDENTIFIED CRACK AT LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CHORD AFT UPPER CLEVIS LUG DURING SCHEDULED INSPECTION PER ECO 1384R6/SB 737-55-10
- [SDR TSAA0033252](https://openairdocs.org/sdr/TSAA0033252), Dec 22, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 2 AND NR 4 EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033242](https://openairdocs.org/sdr/TSAA0033242), Dec 13, 2000: BATTERY PACK. DISCHARGED. REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033234](https://openairdocs.org/sdr/TSAA0033234), Nov 17, 2000: BATTERY PACK. DISCHARGED. REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUR TO INOP. OPS CK OK.A/C RETURNED TO SERVICE.
- [SDR TSAA0033221](https://openairdocs.org/sdr/TSAA0033221), Oct 18, 2000: BATTERY PACK. DISCHARGED. REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033184](https://openairdocs.org/sdr/TSAA0033184), Aug 3, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033119](https://openairdocs.org/sdr/TSAA0033119), Apr 7, 2000: LIGHT. INOPERATIVE. REPLACED FORWARD ENTRY DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033118](https://openairdocs.org/sdr/TSAA0033118), Apr 7, 2000: LIGHT. INOPERATIVE. REPLACED FORWARD SERVICE DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033086](https://openairdocs.org/sdr/TSAA0033086), Mar 10, 2000: LIGHT. INOPERATIVE. REPLACED THE FORWARD AND AFT SERVICE DOOR EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933492](https://openairdocs.org/sdr/TSAA9933492), Dec 4, 1999: LIGHT. INOPERATIVE. REPLACED FORWARD SERVICE DOOR LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA9933491](https://openairdocs.org/sdr/TSAA9933491), Dec 4, 1999: BATTERY PACK. DISCHARGED. REPLACED FORWARD AND AFT EXTERIOR EMERGENCY SLIDE LIGHT BATTERY PACKS DUE TO INOPERABLE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA9933490](https://openairdocs.org/sdr/TSAA9933490), Dec 4, 1999: LIGHT. INOPERATIVE. REPLACED FORWARD SERVICE DOOR EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

All 105: https://openairdocs.org/deregistered/N821AL-2008-07-30/reports.md

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