# N818AL: 1980 Boeing 737-230, registration cancelled 2008-02-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 27, 2008
- Status when cancelled: Sale reported
- Airframe: [Boeing 737-230](https://openairdocs.org/model/boeing-737-230) (registry code 1384401)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 22117
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Airworthiness date: April 2, 1996
- Last registry action: September 29, 2006
- Mode S code: AB271F
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Individual
- 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/N818AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=818AL
- Page: https://openairdocs.org/deregistered/N818AL-2008-02-27

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 (135, newest 50)

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

- [SDR TSAA0653061](https://openairdocs.org/sdr/TSAA0653061), Aug 5, 2006: SKIN PANEL. CRACKED. CRACK FOUND LT SIDE OF FUSELAGE SKIN DIRECTLY BELOW LAST PASSENGER WINDOW ON LOWER FUSELAGE BS 932 JUST BELOW STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMAT
- [SDR TSAA0626052](https://openairdocs.org/sdr/TSAA0626052), Jul 2, 2006: FIRE LOOP. FALSE INDICATION. APU FIRE WARNING LIGHT ILLUMINATED IN FLIGHT. APU WAS NOT OPERATING AT THE TIME OF INDICATION; THE FIRE BOTTLE WAS DISCHARGED. AIRCRAFT RETURNED TO HNL AND LAND
- [SDR TSAA0653022](https://openairdocs.org/sdr/TSAA0653022), Mar 22, 2006: SKIN PANEL. CRACKED. A 1.75 INCH CRACK AT BS 787 STR 19L. CRACK CUT OUT AND REPAIRED IAW SRM 53-30-3 FIGURE 48 DETAIL XI. NDT ACCOMPLISHED IAW BOEING NDT MANUAL 51-00-00 PT 6. REPAI
- [SDR TSAA0657023](https://openairdocs.org/sdr/TSAA0657023), Mar 21, 2006: SPAR. CORRODED. WBL 157 CORROSION BY WING REAR SPAR. REMOVED CORROSION AND REPLACED RIVETS. REPAIR COMPLETED IAW ALOHA'S ECO 3091. FAA 8100.9 RECEIVED.
- [SDR TSAA0653021](https://openairdocs.org/sdr/TSAA0653021), Mar 21, 2006: SPAR. CORRODED. CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-301. REMOVED CORROSION AND INSTALLED REPAIR FILLER IAM ALOHA'S ECO 3560. FAA 8100.9 RECEIVED.
- [SDR TSAA0657025](https://openairdocs.org/sdr/TSAA0657025), Mar 21, 2006: SPAR. CORRODED. CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.
- [SDR TSAA0657024](https://openairdocs.org/sdr/TSAA0657024), Mar 21, 2006: SKIN. GOUGED. WING LEADING EDGE SKIN GOUGED AT WBL 340.
- [SDR TSAA0657021](https://openairdocs.org/sdr/TSAA0657021), Mar 21, 2006: SPAR. CORRODED. CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.
- [SDR TSAA0653020](https://openairdocs.org/sdr/TSAA0653020), Mar 20, 2006: SKIN. CRACKED. A 2.75 INCH CRACK AT BS 727A + 15 STR 18R. A 15 MONTH INTERIM REPAIR COMPLETED IN ACCORDANCE WITH ALOHA'S ECO 3521. DOUBLER 0.032 INCH, TRIPLER 0.050 INCH. APPR
- [SDR TSAA0653019](https://openairdocs.org/sdr/TSAA0653019), Mar 20, 2006: SKIN PANEL. CRACKED. A 1.5 INCH CRACK AT BS 747 + 8 STR 17R. REPAIR DOUBLER COMPLETED IAW 53-30-3 FIG 48 DET VIII. NDT PERFORMED IAW BOEING NDT MANUAL 51-00-00 PT 6. REPAIR SIZE APP
- [SDR TSAA0655005](https://openairdocs.org/sdr/TSAA0655005), Jan 22, 2006: SPAR. CORRODED. LEFT HAND HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORROSION SS 111.1 - SS 101.9. MAINTENANCE REPAIRED WITH FILLERS TO SEAT IN BLEND OUTS AND SKIN TRIM OUT. 
- [SDR TSAA0532015](https://openairdocs.org/sdr/TSAA0532015), Mar 9, 2005: CIRCUIT CARD. FAILED. LANDING GEAR LEVER WOULD NOT GO TO UP POSITION AFTER TAKEOFF. NO GREEN OR RED GEAR LIGHTS ILLUMINATED. RETURNED TO HNL. MAINTENANCE INSPECTED AND LUBED THE TELE
- [SDR TSAA0453025](https://openairdocs.org/sdr/TSAA0453025), Feb 1, 2004: SKIN. CRACKED. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AR
- [SDR TSAA0332193](https://openairdocs.org/sdr/TSAA0332193), Dec 2, 2003: CONTROL CABLE. OUT OF ADJUST. AFTER TAEKOFF, DURING CLIM THE LANDING GEAR CONTROL LEVER WOULD NOT MOVE UP AND SIMULTANEOUSLY THE TAKEOFF WARNING HORN SOUNDED WHEN THE FLAPS WERE RETRACTED. P
- [SDR TSAA0353215](https://openairdocs.org/sdr/TSAA0353215), Nov 25, 2003: STRINGER. DAMAGED. CUT OUT AND REMOVED DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES IAW TABLE 1. ALODINE AND APPLIED ONE LAYER OF BMS 10-11, TYP
- [SDR TSAA0353208](https://openairdocs.org/sdr/TSAA0353208), Nov 25, 2003: LEG ASSY. CORRODED. BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. REMOVED ANGLES. FABRICATED A FILLER AND
- [SDR TSAA0453007](https://openairdocs.org/sdr/TSAA0453007), Nov 20, 2003: SPLICE. CORRODED. TRIMMED OUT THE DAMAGED AREA, VERIFIED CORROSION FREE USING 10X INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PR
- [SDR TSAA0451006](https://openairdocs.org/sdr/TSAA0451006), Nov 20, 2003: STRINGER. CORRODED. TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE PER TABLE 1. ALODINED AND TWO COATS BMS 10-11 
- [SDR TSAA0451005](https://openairdocs.org/sdr/TSAA0451005), Nov 20, 2003: STRINGER SPLICE. CRACKED. TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIME
- [SDR TSAA0353217](https://openairdocs.org/sdr/TSAA0353217), Nov 19, 2003: SKIN. CRACKED. TRIMMED OUT THE SKIN, BONDED DOUBLER, AND BEARSTRAP, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED THE REPAIR PARTS AS SHOWN IN 737 SRM 53-30-3, FIGURE 
- [SDR TSAA0357211](https://openairdocs.org/sdr/TSAA0357211), Nov 19, 2003: SKIN. CORRODED. BLENDED OUT THE CORROSION, VERIFIED FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. DRILLED AND SPOTFACE FASTENER HOLE. COLD WORKED FASTENER HOLE. AL
- [SDR TSAA0353207](https://openairdocs.org/sdr/TSAA0353207), Nov 19, 2003: DOOR. CRACKED. TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ACCOMPLISHED FASTENER HOLE INSPECTION ON HOLES COVERED BY REPAIR. UTILIZED REPAIR PARTS FROM K
- [SDR TSAA0451004](https://openairdocs.org/sdr/TSAA0451004), Nov 18, 2003: STRINGER SPLICE. DAMAGED. TRIMMED OUT THE DAMAGED AREA, VERIFIED CRACK FREE USNG HFEC INSPECTION. FABRICATED AND INSTALLED STRINGER SPLICE. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER
- [SDR TSAA0453010](https://openairdocs.org/sdr/TSAA0453010), Nov 18, 2003: SKIN. CRACKED. TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED TAPERED FILLERS AND PLATES FROM 2024-T3 CLAD, PER TABLE 1. ALODINED AND TWO COATS B
- [SDR TSAA00453009](https://openairdocs.org/sdr/TSAA00453009), Nov 18, 2003: SKIN. CRACKED. TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED TAPERED FILLERS AND PLATES FROM 2024-T3 CLAD. ALODINED AND TWO COATS BMS 10-11 TYPE
- [SDR TSAA0357216](https://openairdocs.org/sdr/TSAA0357216), Nov 17, 2003: PANEL. CORRODED. BLENDED OUT THE CORROSION TO A 20:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. REMOVED FASTENERS IN REPAIR AREA. FLAT PEEN BLENDOUT AREA. ALODI
- [SDR TSAA0453008](https://openairdocs.org/sdr/TSAA0453008), Nov 16, 2003: SKIN. CRACKED. TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED REPAIR DOUBLER. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND 
- [SDR TSAA0353206](https://openairdocs.org/sdr/TSAA0353206), Nov 15, 2003: SKIN. CRACKED. TRIMMED OUT CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ENLARGED TRIM BY .040 INCH INSURANCE CUT. HFEC INSPECTED ALL FASTENER HOLES. FABRICATED A .071 INC
- [SDR TSAA0453011](https://openairdocs.org/sdr/TSAA0453011), Nov 11, 2003: SKIN. CRACKED. TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED DOUBLER AND FILLER FROM .063 INCH, 2024-T3. ALODINED AND TWO COATS BMS 10-11 TYPE 1
- [SDR TSAA0453012](https://openairdocs.org/sdr/TSAA0453012), Nov 11, 2003: SKIN. CRACKED. TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED FILLER, DOUBLER, AND TRIPLER FROM 2024-T3 PER TABLE I. ALODINED AND TWO COATS BMS 1
- [SDR TSAA0353209](https://openairdocs.org/sdr/TSAA0353209), Nov 11, 2003: VENT. CORRODED. BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. FABRICATED A .020 INCH EXTERNAL DOUBLER
- [SDR TSAA0353212](https://openairdocs.org/sdr/TSAA0353212), Nov 11, 2003: SKIN. CRACKED. TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED DOUBLER AND FILLER FROM .063 INCH, 2024-T3. ALODINED AND TWO COATS BMS 10-11 TYPE 1
- [SDR TSAA0353210](https://openairdocs.org/sdr/TSAA0353210), Nov 5, 2003: SKIN. CORRODED. BLENDED OUT THE CORROSION TO A 10:1 RATIO. VERIFIED CORROSION FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. AT EXISTING RIVET LOCATION, INSTALL 1/3
- [SDR TSAA0333109](https://openairdocs.org/sdr/TSAA0333109), Apr 26, 2003: BATTERY PACK. DISCHARGED. REPLACED AFT ENTRY IDENTICAL POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333049](https://openairdocs.org/sdr/TSAA0333049), Mar 10, 2003: BATTERY PACK. DISCHARGED. REPLACED FORWARD ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333050](https://openairdocs.org/sdr/TSAA0333050), Mar 10, 2003: BATTERY PACK. DISCHARGED. REPLACED AFT SERVICE DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333051](https://openairdocs.org/sdr/TSAA0333051), Mar 10, 2003: BATTERY PACK. INOPERATIVE. REPLACED AFT ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0329025](https://openairdocs.org/sdr/TSAA0329025), Feb 7, 2003: PUMP. INOPERATIVE. DURING TAKEOFF AT 100 KNOTS, THE NR 2 HYDRAULIC SYSTEM 'B' PUMP LIGHT CAME ON STEADY WITH NO OTHER ABNORMAL INDICATIONS. THE TAKEOFF WAS ABORTED AND THE AIRCRAF
- [SDR TSAA0233208](https://openairdocs.org/sdr/TSAA0233208), Oct 11, 2002: BATTERY PACK. DISCHARGED. REPLACED CENTER EMERGENCY CONTROL MODULE BATTERY PACK DUE TO LOW VOLTAGE. OP CHECK, OK. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0257184](https://openairdocs.org/sdr/TSAA0257184), Jul 24, 2002: SKIN. CORRODED. LEFT LOWER OUTBOARD WING TRAILING EDGE CORRODED AT WSL 453. BLENDOUT TO REMOVE ALL CORROSION CONFIRMED USING 10X VISUAL INSPECTION NO DEFECTS NOTED, OBTAINED A 
- [SDR TSAA0251107](https://openairdocs.org/sdr/TSAA0251107), Apr 12, 2002: FLOORBEAM. CRACKED. FOUND A 2.5 INCH CRACK AT BS 710 FLOORBEAM BBL .07 ON THE WEB. CUT OUT DAMAGED AREA ON THE WEB. FABRICATED A REPAIR DOUBLER IAW FIGURE 6. INSTALLED DOUBLER, STI
- [SDR TSAA0251111](https://openairdocs.org/sdr/TSAA0251111), Apr 12, 2002: FITTING. CORRODED. FOUND CORROSION ON THE FORWARD LOWER EXTRUSION, LOWER FRAME SECTION IN THE RIGHT WHEEL WELL BETWEEN BS 680 AND BS 690. CUT OUT DAMAGED SECTION OF WEB. FABRICATE
- [SDR TSAA0251110](https://openairdocs.org/sdr/TSAA0251110), Apr 12, 2002: FITTING. CORRODED. FOUND CORROSION ON THE FORWARD LOWER EXTRUSION ON THE FRAME IN THE LEFT WHEEL WELL AT BS 680. REMOVED THE FORWARD LOWER EXTRUSION. INSTALLED NEW EXTRUSION SECTI
- [SDR TSAA0251109](https://openairdocs.org/sdr/TSAA0251109), Apr 12, 2002: KEELBEAM. CORRODED. FOUND CORROSION ON THE KEEL BEAM LOCATED IN THE MAIN WHEEL WELL AT BS 685 LEFT CHORD AT THE MOUNT SCREW HOLES. REPAIRED BY REMOVING CORROSION IAW DETAIL VII, VI
- [SDR TSAA0251108](https://openairdocs.org/sdr/TSAA0251108), Apr 12, 2002: KEELBEAM. CRACKED. FOUND CRACK ON THE LOWER CHORD IN THE LEFT MAIN WHEEL WELL AT BS 652 KEEL BEAM FUSELAGE SKIN AREA. TRIMMED OUT CRACK AND VERIFIED REMOVED USING HFEC METHOD. FAB
- [SDR TSAA0253112](https://openairdocs.org/sdr/TSAA0253112), Apr 12, 2002: STRINGER. CORRODED. FOUND EXFOLIATION CORROSION ON STRINGER 27L AT BS 967. REMOVED THE DAMAGED SECTION OF THE STRINGER. FABRICATED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3 PA
- [SDR TSAA0251106](https://openairdocs.org/sdr/TSAA0251106), Apr 12, 2002: FLOORBEAM. CRACKED. FOUND A CRACK AT FUSELAGE STATION 665 FLOORBEAM BL 0 ON THE UPPER CHORD. FABRICATED AND INSTALLED REINFORCING DOUBLER, STIFFENERS, FILLERS, SPLICE PLATE AND ANG
- [SDR TSAA0253116](https://openairdocs.org/sdr/TSAA0253116), Apr 4, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDICATION AT BS 867 RIGHT WINDOW BO
- [SDR TSAA0253115](https://openairdocs.org/sdr/TSAA0253115), Apr 4, 2002: WINDOW FRAME. CRACKED. PERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDICATION AT BS 787 RIGHT WINDOW UP
- [SDR TSAA0253114](https://openairdocs.org/sdr/TSAA0253114), Apr 4, 2002: STRUCTURE. CRACKED. PERFORMED WINDOW CORNER FASTENERS HOLE INSPECTION PER S/B 737-53A1177R 6 AND DISCOVERED DEFECTS IN WINDOW CORNERS WITH CRACK INDCIATION AT BS 440 RT WINDOW UPPE

All 135: https://openairdocs.org/deregistered/N818AL-2008-02-27/reports.md

## FAA accident and incident reports (2)

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 20000421023289I](https://openairdocs.org/incident/20000421023289I), Apr 21, 2000: Boeing 737230 (N818AL), Honolulu, HI. (-23)Pilots reported during landing phase aircraft made an uncommanded yaw. Maintenance replaced the D295 connector. This is the airframe side connector for…
- [Incident 20000413023299I](https://openairdocs.org/incident/20000413023299I), Apr 13, 2000: Boeing 737230 (N818AL), Honolulu, HI. (-23)At FL 190, autopilot on, in climb, the aircraft started rolling/yawing, increasing in severity. Autopilot was disengaged and aircraft continued rolling…

## Other aircraft with N818AL

- [Registered now](https://openairdocs.org/aircraft/N818AL): Boeing 787-8, S/N 40636, built 2017

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