# Service difficulty reports: N821AL, cancelled Jul 30, 2008

A list on [N821AL, cancelled Jul 30, 2008](https://openairdocs.org/deregistered/N821AL-2008-07-30.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 · 105 reports

- [SDR TSAA0736042](https://openairdocs.org/sdr/TSAA0736042.md): Duct · failed · Jul 31, 2007 · N821AL · Boeing 737230 · Pneumatic Distribution System
  > 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 FOUND THE APU BLEED AIR DUCT HAD RUPTURED CAUSING THE OVERHEAT AND ALSO CAUSING THE APU FIRE EXTINGUIS
- [SDR TSAA0732033](https://openairdocs.org/sdr/TSAA0732033.md): Actuator · malfunctioned · Jun 15, 2007 · N821AL · Boeing 737230 · Landing Gear Actuator
  > 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 HEAR THE NLG EXTEND. AFTER APPROXIMATELY 20 SECONDS, THE NLG EXTENDED AND SHOWED DOWN AND LOCKED.
- [SDR TSAA0753021](https://openairdocs.org/sdr/TSAA0753021.md): Skin Panel · cracked · May 3, 2007 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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] CRACK APPROX 3 LONG, LOCATED AT BS 947 + 15 BETWEEN STR 21L AND STR 22L WAS REPAIRED IAW SRM 53
- [SDR TSAA0753020](https://openairdocs.org/sdr/TSAA0753020.md): Skin Panel · cracked · May 3, 2007 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 APPROX 2 LONG WAS REPAIRED AT BS 887 + 3 BETWEEN STR 23R AND STR 24R IAW SRM 53-30-3 PROCEDURE VII. CU
- [SDR TSAA0753019](https://openairdocs.org/sdr/TSAA0753019.md): Frame · cracked · May 2, 2007 · N821AL · Boeing 737230 · Fuselage Main, Frame
  > 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 LONG. RIGHT SIDE CRACK IS APPROX. 2 INCHES LONG. [SUP 05-10-07] INTERIM REPAIR PERFORMED PER ECO 3
- [SDR TSAA0628029](https://openairdocs.org/sdr/TSAA0628029.md): Wire · broken · Apr 3, 2006 · N821AL · Boeing 737230 · Fuel System Wiring
  > 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 VALVE IAW MM 28-22-11, LEAK CHECK OKAY. THIS DID NOT FIX THE PROBLEM. FURTHER INVESTIGATION REVEAL
- [SDR TSAA0653014](https://openairdocs.org/sdr/TSAA0653014.md): Skin Panel · gouged · Mar 8, 2006 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 PER ECO 5330.
- [SDR TSAA0553060](https://openairdocs.org/sdr/TSAA0553060.md): Skin · corroded · Oct 24, 2005 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > SECTION 46 FUSELAGE SKIN WITH CORROSION AT BS 998.40, LBL 6.75.
- [SDR TSAA0553059](https://openairdocs.org/sdr/TSAA0553059.md): Clip · cracked · Oct 24, 2005 · N821AL · Boeing 737230 · Fuselage Main, Attach Fittings
  > BULKHEAD BS 727, WL 202.6, RBL 10.0", CLIP UPPER CRACKED.
- [SDR TSAA0557058](https://openairdocs.org/sdr/TSAA0557058.md): Spar · corroded · Oct 24, 2005 · N821AL · Boeing 737230 · Wing Spar
  > 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.md): Connector · damaged · Aug 7, 2005 · N821AL · Boeing 737230 · Pneumatic Distribution System
  > 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 LIGHT EXTINGUISHED. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED APU F
- [SDR TSAA0532022](https://openairdocs.org/sdr/TSAA0532022.md): Tire · failed · May 28, 2005 · N821AL · Boeing 737230 · Tire
  > 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 SIDE UNTIL SLOWED TO ABOUT 60KTS. DECLARED AN EMERGENCY. NO SMOKE OR FIRE. MAINTENANCE REMOVED
- [SDR TSAA0429085](https://openairdocs.org/sdr/TSAA0429085.md): Line · leaking · Dec 28, 2004 · N821AL · Boeing 737230 · Engine Thrust Reverser
  > FLT 46, HNL-ITO: HYDRAULIC FLUID QUANTITY DECREASING DURING GEAR RETRACTION. RETURNED TO HNL. UNEVENTFUL LANDING. WHILE ON GROUND, HYDRAULIC FLUID QUANTITY CONTINUED TO DECREASE SLOWLY. MAINTENANCE FOUND LEAKS AT THE NR 2 THRUST REVERSER LINE AND NR 4 SPOI
- [SDR TSAA0479053](https://openairdocs.org/sdr/TSAA0479053.md): Transmitter · failed · Jul 7, 2004 · N821AL · Boeing 737230 · Engine Oil Indicating System
  > 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 INDICATOR IAW MEL 79-1, CONTROL NR 0778B-10. SERVICED THE NR 2 ENGINE TO FULL AND INSTALLED PLACARDS ON
- [SDR TSAA0479020](https://openairdocs.org/sdr/TSAA0479020.md): Bypass Switch · faulty · Feb 5, 2004 · N821AL · Boeing 737230 · Turbine Engine Oil System
  > 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 GOOD. DRAINED AND SERVICED OIL TANK AND GEARBOX. LEAK AND OPS CHECK GOOD. REPLACED THE NR 2 ENGI
- [SDR TSAA0253257](https://openairdocs.org/sdr/TSAA0253257.md): Window Frame · cracked · Dec 18, 2003 · N821AL · Boeing 737230 · Fuselage Main, Structure
  > 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. MAINTAINED A MINIMUM.5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INSIDE CORNER RADIUS. FINISH
- [SDR TSAA0253258](https://openairdocs.org/sdr/TSAA0253258.md): Window Frame · cracked · Dec 18, 2003 · N821AL · Boeing 737230 · Fuselage Main, Structure
  > 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. MAINTAINED A MINIMUM.5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2 INCH INSIDE CORNER RADIUS. FINI
- [SDR TSAA0253260](https://openairdocs.org/sdr/TSAA0253260.md): Window Frame · cracked · Dec 18, 2003 · N821AL · Boeing 737230 · Fuselage Main, Structure
  > 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. MAINTAINED A MINIMUM.5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INCH INSIDE CORNER RADIUS. FI
- [SDR TSAA0353152](https://openairdocs.org/sdr/TSAA0353152.md): Skin · cracked · Jun 13, 2003 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 INSTALLED A REPAIR FILLER AND PLATE FROM 2024-T3 MATERIAL IAW SRM 53-30-3, FIGURE 3. AIRCRAFT RE
- [SDR TSAA0333125](https://openairdocs.org/sdr/TSAA0333125.md): Battery Pack · inoperative · May 24, 2003 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Engine · failed · Jan 25, 2003 · N821AL · Boeing 737230 · Engine (Turbine/Turboprop)
  > 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 LANDED AT HNL WITH NO FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED THE NR 1 EN
- [SDR TSAA0333013](https://openairdocs.org/sdr/TSAA0333013.md): Battery Pack · discharged · Jan 24, 2003 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Skin · cracked · Jan 14, 2003 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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.04 INCH AS AN INSURANCE CUT. FABRICATED TWO.063 INCH STRUCTURAL FILLERS AND A.071 INCH DOUBLER
- [SDR TSAA0253253](https://openairdocs.org/sdr/TSAA0253253.md): Skin · corroded · Jan 14, 2003 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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.04 INCH AS AN INSURANCE CUT. FABRICATED TWO STRUCTURAL FILLERS, A REPAIR FILLER, DOUBLER, AND TRI
- [SDR TSAA0253254](https://openairdocs.org/sdr/TSAA0253254.md): Skin · corroded · Dec 20, 2002 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 REPAIR FILLER AND.080 INCH DOUBLER FROM CLAD SHEET 2024-T3 MATERIAL IAW SRM 53-30-3. FINISHED ALL
- [SDR TSAA0253259](https://openairdocs.org/sdr/TSAA0253259.md): Window Frame · cracked · Dec 18, 2002 · N821AL · Boeing 737230 · Fuselage Main, Structure
  > 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. MAINTAINED A MINIMUM.5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INCH INSIDE CORNER RADIUS. F
- [SDR TSAA0233230](https://openairdocs.org/sdr/TSAA0233230.md): Battery Pack · discharged · Nov 8, 2002 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Stiffener · cracked · Oct 13, 2002 · N821AL · Boeing 737230 · Fuselage Miscellaneous Structure
  > 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 AND INSTALLED A REPAIR ANGLE IAW SRM. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0253195](https://openairdocs.org/sdr/TSAA0253195.md): Skin · cracked · Sep 4, 2002 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > TRIMMED OUT DAMAGE SKIN AT BS 749 STRINGER 18R. HFEC EDGE OF TRIMMED AREA, NO DEFECTS NOTED.
- [SDR TSAA0233160](https://openairdocs.org/sdr/TSAA0233160.md): Battery Pack · discharged · Jun 29, 2002 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED NR FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233158](https://openairdocs.org/sdr/TSAA0233158.md): Battery Pack · discharged · Jun 17, 2002 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR IDENT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233159](https://openairdocs.org/sdr/TSAA0233159.md): Light · inoperative · Jun 17, 2002 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR IDENT LIGHT ASSEMBLY DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233028](https://openairdocs.org/sdr/TSAA0233028.md): Battery Pack · discharged · Jan 25, 2002 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253022](https://openairdocs.org/sdr/TSAA0253022.md): Skin · cracked · Jan 14, 2002 · N821AL · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 DEFECTS NOTED. FABRICATED AND INSTALLED A REPAIR FILLER AND PLATE IAW SRM 53-30-3. AIRCRAFT RETU
- [SDR TSAA0133144](https://openairdocs.org/sdr/TSAA0133144.md): Battery Pack · discharged · Oct 20, 2001 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Indicator · false indication · Aug 23, 2001 · N821AL · Boeing 737230 · Engine Oil Temperature
  > 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 TO FL250 FT, POWER WAS REDUCED AND OIL TEMP INCREASED TO 150 DEGREES THEN WENT OFF SCALE MOMENTARIL
- [SDR TSAA0133024](https://openairdocs.org/sdr/TSAA0133024.md): Light · inoperative · Mar 2, 2001 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Frame · cracked · Feb 15, 2001 · N821AL · Boeing 737230 · Fuselage Main, Frame
  > 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 INCH 7075-T6, FABRICATED AND INSTALLED 063 INCH REPAIR STRAP, CLEANED AND TREATED ALL EXPOSED AREAS
- [SDR TSAA0155001](https://openairdocs.org/sdr/TSAA0155001.md): Spar · cracked · Jan 8, 2001 · N821AL · Boeing 737230 · Horizontal Stabilizer, Spar/Rib
  > IDENTIFIED CRACK AT LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CHORD AFT UPPER CLEVIS LUG DURING SCHEDULED INSPECTION PER ECO 1384R6/SB 737-55-1033R1. (M)
- [SDR TSAA0033252](https://openairdocs.org/sdr/TSAA0033252.md): Battery Pack · inoperative · Dec 22, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Battery Pack · discharged · Dec 13, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Battery Pack · discharged · Nov 17, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Battery Pack · discharged · Oct 18, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Battery Pack · inoperative · Aug 3, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Light · inoperative · Apr 7, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED FORWARD ENTRY DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033118](https://openairdocs.org/sdr/TSAA0033118.md): Light · inoperative · Apr 7, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033086](https://openairdocs.org/sdr/TSAA0033086.md): Light · inoperative · Mar 10, 2000 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Light · inoperative · Dec 4, 1999 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA9933491](https://openairdocs.org/sdr/TSAA9933491.md): Battery Pack · discharged · Dec 4, 1999 · N821AL · Boeing 737230 · Emergency Lighting
  > 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.md): Light · inoperative · Dec 4, 1999 · N821AL · Boeing 737230 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Next page: https://openairdocs.org/deregistered/N821AL-2008-07-30/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 = 'N821AL' AND deregistration_id = 'N821AL-2008-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N821AL-2008-07-30/reports

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