# Service difficulty reports: N818AL, cancelled Feb 27, 2008

A list on [N818AL, cancelled Feb 27, 2008](https://openairdocs.org/deregistered/N818AL-2008-02-27.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 3 · 135 reports

- [SDR TSAA0653061](https://openairdocs.org/sdr/TSAA0653061.md): Skin Panel · cracked · Aug 5, 2006 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > CRACK FOUND LT SIDE OF FUSELAGE SKIN DIRECTLY BELOW LAST PASSENGER WINDOW ON LOWER FUSELAGE BS 932 JUST BELOW STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMATELY 19 BY 16 EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3, FIGURE 48, DETA
- [SDR TSAA0626052](https://openairdocs.org/sdr/TSAA0626052.md): Fire Loop · false indication · Jul 2, 2006 · N818AL · Boeing 737230 · Fire Detection
  > 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 LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FIRE LOOP ELEMENT IAW AMM 26-15-1 FOR TROUBLESHOOTING,
- [SDR TSAA0653022](https://openairdocs.org/sdr/TSAA0653022.md): Skin Panel · cracked · Mar 22, 2006 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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. REPAIR APPROXIMATE SIZE 9 X 12 INCHES.
- [SDR TSAA0657023](https://openairdocs.org/sdr/TSAA0657023.md): Spar · corroded · Mar 21, 2006 · N818AL · Boeing 737230 · Wing Spar
  > 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.md): Spar · corroded · Mar 21, 2006 · N818AL · Boeing 737230 · Fuselage Structure (General)
  > 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.md): Spar · corroded · Mar 21, 2006 · N818AL · Boeing 737230 · Wing Spar
  > CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.
- [SDR TSAA0657024](https://openairdocs.org/sdr/TSAA0657024.md): Skin · gouged · Mar 21, 2006 · N818AL · Boeing 737230 · Leading Edge Devices
  > WING LEADING EDGE SKIN GOUGED AT WBL 340.
- [SDR TSAA0657021](https://openairdocs.org/sdr/TSAA0657021.md): Spar · corroded · Mar 21, 2006 · N818AL · Boeing 737230 · Wing Spar
  > CORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.
- [SDR TSAA0653020](https://openairdocs.org/sdr/TSAA0653020.md): Skin · cracked · Mar 20, 2006 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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. APPROXIMATE REPAIR SIZE 23" X 31". FAA 8100.9 RECEIVED.
- [SDR TSAA0653019](https://openairdocs.org/sdr/TSAA0653019.md): Skin Panel · cracked · Mar 20, 2006 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 APPROX 9 X 12 INCHES.
- [SDR TSAA0655005](https://openairdocs.org/sdr/TSAA0655005.md): Spar · corroded · Jan 22, 2006 · N818AL · Boeing 737230 · Horizontal Stabilizer, Spar/Rib
  > 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. FABRICATED EXTERNAL SKIN DOUBLER PER ECO 3392.
- [SDR TSAA0532015](https://openairdocs.org/sdr/TSAA0532015.md): Circuit Card · failed · Mar 9, 2005 · N818AL · Boeing 737230 · Landing Gear Position and Warning
  > 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 TELEFLEX CABLE. MEASURED PROXIMITY SENSOR AND GAP WITHIN TOLERANCE. REPLACED PROXIMITY CARD AND SWU
- [SDR TSAA0453025](https://openairdocs.org/sdr/TSAA0453025.md): Skin · cracked · Feb 1, 2004 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, DETAIL X. AIRCRAFT RETURNED TO SERVI
- [SDR TSAA0332193](https://openairdocs.org/sdr/TSAA0332193.md): Control Cable · out of adjust · Dec 2, 2003 · N818AL · Boeing 737230 · Landing Gear Retraction/Extension System
  > 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. PERFORMED GROUND SPOILER INTERLOCK VALVE CONTROL CABLE ADJUSTMENT AND TEST IAW MM 27-62-51. AIRCRAF
- [SDR TSAA0353215](https://openairdocs.org/sdr/TSAA0353215.md): Stringer · damaged · Nov 25, 2003 · N818AL · Boeing 737230 · Fuselage Main, Longeron/Stringer
  > 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, TYPE 1 PRIMER. INSTALLED REPAIR PARTS AND MADE A FAYING SURFACE SEAL PER SRM 53-10-03, FIGURE 1. RE
- [SDR TSAA0353208](https://openairdocs.org/sdr/TSAA0353208.md): Leg Assy · corroded · Nov 25, 2003 · N818AL · Boeing 737230 · Fuselage Miscellaneous Structure
  > 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 STRAP FROM 7075-T6 PER FIGURE 1. ALODINED AND TWO COATS BMS 10-11 TYPE II PRIMER TO REPAIR PAR
- [SDR TSAA0453007](https://openairdocs.org/sdr/TSAA0453007.md): Splice · corroded · Nov 20, 2003 · N818AL · Boeing 737230 · Fuselage Miscellaneous Structure
  > 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 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 53-10-3. AIRCRAFT RETURNED TO
- [SDR TSAA0451006](https://openairdocs.org/sdr/TSAA0451006.md): Stringer · corroded · Nov 20, 2003 · N818AL · Boeing 737230 · Fuselage Main, Longeron/Stringer
  > 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 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. INSTALLED REPAIR PARTS AND MADE A FAYING SEAL
- [SDR TSAA0451005](https://openairdocs.org/sdr/TSAA0451005.md): Stringer Splice · cracked · Nov 20, 2003 · N818AL · Boeing 737230 · Fuselage Miscellaneous Structure
  > 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 PRIMER TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 51-10-1. AIRCRAFT RETURNED TO SER
- [SDR TSAA0353217](https://openairdocs.org/sdr/TSAA0353217.md): Skin · cracked · Nov 19, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 46. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLE
- [SDR TSAA0357211](https://openairdocs.org/sdr/TSAA0357211.md): Skin · corroded · Nov 19, 2003 · N818AL · Boeing 737230 · Wing, Plate/Skin
  > BLENDED OUT THE CORROSION, VERIFIED FREE USING 10X VISUAL INSPECTION. FLAT PEEN BLENDOUT AREA. DRILLED AND SPOTFACE FASTENER HOLE. COLD WORKED FASTENER HOLE. ALODINED AND TWO COATS BMS 10-79 TYPE III PRIMER TO BLEND AND SPOT FACE AREA. INSTALLED 1/32 INCH
- [SDR TSAA0353207](https://openairdocs.org/sdr/TSAA0353207.md): Door · cracked · Nov 19, 2003 · N818AL · Boeing 737230 · Passenger/Crew Doors
  > TRIMMED OUT THE CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ACCOMPLISHED FASTENER HOLE INSPECTION ON HOLES COVERED BY REPAIR. UTILIZED REPAIR PARTS FROM KIT PER FIGURE 1. ALODINED AND TWO COATS BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFA
- [SDR TSAA0451004](https://openairdocs.org/sdr/TSAA0451004.md): Stringer Splice · damaged · Nov 18, 2003 · N818AL · Boeing 737230 · Fuselage Miscellaneous Structure
  > 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 TO REPAIR PARTS AND EXPOSED SURFACE. REPAIR COMPLETED IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERV
- [SDR TSAA0453010](https://openairdocs.org/sdr/TSAA0453010.md): Skin · cracked · Nov 18, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 BMS 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 24
- [SDR TSAA00453009](https://openairdocs.org/sdr/TSAA00453009.md): Skin · cracked · Nov 18, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGUR 24. REPAIR COMP
- [SDR TSAA0357216](https://openairdocs.org/sdr/TSAA0357216.md): Panel · corroded · Nov 17, 2003 · N818AL · Boeing 737230 · Wing, Plate/Skin
  > 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. ALODINED AND TWO COATS BMS 10-20 TYPE II PRIMER TO BLEND AND SPOT FACE AREAS. INSTALLED 1/32 INCH OV
- [SDR TSAA0453008](https://openairdocs.org/sdr/TSAA0453008.md): Skin · cracked · Nov 16, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 EXPOSED SURFACES. INSTALLED REPAIR PARTS WET WITH BMS 5-95 PER FIGURE 1. REPAIR COMPLETED IAW SRM
- [SDR TSAA0353206](https://openairdocs.org/sdr/TSAA0353206.md): Skin · cracked · Nov 15, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > TRIMMED OUT CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ENLARGED TRIM BY.040 INCH INSURANCE CUT. HFEC INSPECTED ALL FASTENER HOLES. FABRICATED A.071 INCH STRUCTURAL FILLER,.063 INCH INNER PLATE,.063 INCH PLATE,.125 OUTER PLATE AND.0180 INCH THIC
- [SDR TSAA0453011](https://openairdocs.org/sdr/TSAA0453011.md): Skin · cracked · Nov 11, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 33. REPAIR COMPL
- [SDR TSAA0453012](https://openairdocs.org/sdr/TSAA0453012.md): Skin · cracked · Nov 11, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 10-11 TYPE 1 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS PER FIGURE 34. R
- [SDR TSAA0353209](https://openairdocs.org/sdr/TSAA0353209.md): Vent · corroded · Nov 11, 2003 · N818AL · Boeing 737230 · Wing Miscellaneous Structure
  > 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 FROM 7075-T6. ALODINED AND ONE COAT BMS 10-11, TYPE I PRIMER TO REPAIR PARTS AND EXPOSED SURFAC
- [SDR TSAA0353212](https://openairdocs.org/sdr/TSAA0353212.md): Skin · cracked · Nov 11, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS EPR FIGURE 1. REPAIR COMPLE
- [SDR TSAA0353210](https://openairdocs.org/sdr/TSAA0353210.md): Skin · corroded · Nov 5, 2003 · N818AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 1/32 INCH OVERSIZE. RESTORE AERODYNAMIC SURFACE BY FILLING THE AREA WITH BMS 5-95 SEALANT. REPAIR
- [SDR TSAA0333109](https://openairdocs.org/sdr/TSAA0333109.md): Battery Pack · discharged · Apr 26, 2003 · N818AL · Boeing 737230 · Emergency Lighting
  > 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.md): Battery Pack · discharged · Mar 10, 2003 · N818AL · Boeing 737230 · Emergency Lighting
  > 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.md): Battery Pack · discharged · Mar 10, 2003 · N818AL · Boeing 737230 · Emergency Lighting
  > 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.md): Battery Pack · inoperative · Mar 10, 2003 · N818AL · Boeing 737230 · Emergency Lighting
  > 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.md): Pump · inoperative · Feb 7, 2003 · N818AL · Boeing 737230 · Hydraulic Pump (Electric/Engine), Main
  > 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 AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. THE HYDRAULIC PUMP WAS PUT ON MEL AS INOPERABLE A
- [SDR TSAA0233208](https://openairdocs.org/sdr/TSAA0233208.md): Battery Pack · discharged · Oct 11, 2002 · N818AL · Boeing 737230 · Emergency Lighting
  > 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.md): Skin · corroded · Jul 24, 2002 · N818AL · Boeing 737230 · Wing, Plate/Skin
  > 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 SURFACE FINISH OF 125 MICROINCHES RADIUS OR SMOOTHER, FLAT PEENED REWORKED AREA, ALODINED AND PRIME
- [SDR TSAA0251107](https://openairdocs.org/sdr/TSAA0251107.md): Floorbeam · cracked · Apr 12, 2002 · N818AL · Boeing 737230 · Fuselage Main, Floor Beam
  > 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, STIFFENERS AND FILLERS. REPAIR COMPLETED IAW ECO 2223 R1. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251111](https://openairdocs.org/sdr/TSAA0251111.md): Fitting · corroded · Apr 12, 2002 · N818AL · Boeing 737230 · Fuselage Miscellaneous Structure
  > 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. FABRICATED AND INSTALLED NEW WEB SECTION IAW SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251110](https://openairdocs.org/sdr/TSAA0251110.md): Fitting · corroded · Apr 12, 2002 · N818AL · Boeing 737230 · Fuselage Miscellaneous Structure
  > 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 SECTION IAW SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251109](https://openairdocs.org/sdr/TSAA0251109.md): Keelbeam · corroded · Apr 12, 2002 · N818AL · Boeing 737230 · Fuselage Main, Keel
  > 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, VIII AND IX. REPAIR COMPLETED IAW SRM 53-10-1, FIGURE 7, BS 685. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251108](https://openairdocs.org/sdr/TSAA0251108.md): Keelbeam · cracked · Apr 12, 2002 · N818AL · Boeing 737230 · Fuselage Main, Keel
  > 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. FABRICATED A REPAIR ANGLE AND FILLER. REPAIR COMPLETED IAW ECO 2726R3 PART II. AIRCRAFT RETURNED TO
- [SDR TSAA0253112](https://openairdocs.org/sdr/TSAA0253112.md): Stringer · corroded · Apr 12, 2002 · N818AL · Boeing 737230 · Fuselage Main, Longeron/Stringer
  > 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 PAGE 10. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251106](https://openairdocs.org/sdr/TSAA0251106.md): Floorbeam · cracked · Apr 12, 2002 · N818AL · Boeing 737230 · Fuselage Main, Floor Beam
  > FOUND A CRACK AT FUSELAGE STATION 665 FLOORBEAM BL 0 ON THE UPPER CHORD. FABRICATED AND INSTALLED REINFORCING DOUBLER, STIFFENERS, FILLERS, SPLICE PLATE AND ANGLE. REPAIR COMPLETED IAW ECO 2223 R1 PART II DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253116](https://openairdocs.org/sdr/TSAA0253116.md): Window Frame · cracked · Apr 4, 2002 · N818AL · Boeing 737230 · Fuselage Main, Structure
  > 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 BOTTOM FORWARD CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMAGED AREA. HFEC THE
- [SDR TSAA0253115](https://openairdocs.org/sdr/TSAA0253115.md): Window Frame · cracked · Apr 4, 2002 · N818AL · Boeing 737230 · Fuselage Main, Structure
  > 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 UPPER AFT CORNER USING HFEC METHODS. TRIMMED OUT THE THREE HOLES IN THE DAMAGED AREA. HFEC THE EDGE
- [SDR TSAA0253114](https://openairdocs.org/sdr/TSAA0253114.md): Structure · cracked · Apr 4, 2002 · N818AL · Boeing 737230 · Fuselage Main, Structure
  > 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 UPPER FORWARD CORNER USING HFEC METHODS. REPAIRED IAW SRM, AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N818AL-2008-02-27/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 = 'N818AL' AND deregistration_id = 'N818AL-2008-02-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N818AL-2008-02-27/reports

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