# Service difficulty reports: N824AL, cancelled Oct 29, 2013

A list on [N824AL, cancelled Oct 29, 2013](https://openairdocs.org/deregistered/N824AL-2013-10-29.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 2 · 78 reports

- [SDR TSAA0821016](https://openairdocs.org/sdr/TSAA0821016.md): Fan · failed · Mar 13, 2008 · N824AL · Boeing 737282 · Air Distribution Fan
  > FLIGHT 93 OGG - HNL - THE CREW NOTED AN UNPLEASANT BURNING ODOR IN THE CABIN DURING FLIGHT WITH NO SMOKE PRESENT. THE ODOR DECREASED WITH ENGINES AT LOWER THROTTLE SETTINGS. THE AIRCRAFT LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLAC
- [SDR TSAA0853003](https://openairdocs.org/sdr/TSAA0853003.md): Bulkhead · cracked · Jan 8, 2008 · N824AL · Boeing 737282 · Fuselage Main, Bulkhead
  > WHILE PERFORMING ECO 1822 PART I (REFERENCE AD 93-08-08 AND AD 90-06-02) A CRACK WAS DISCOVERED ON THE LT BULKHEAD BS 1156 ALONG THE LAST ROW OF RIVETS APPROX WL 272-275. REPAIRED CRACK IN ACCORDANCE WITH ECO 1822 PART II (S/B 737-53-1-86 R3).
- [SDR TSAA0721046](https://openairdocs.org/sdr/TSAA0721046.md): Sensor · failed · Aug 15, 2007 · N824AL · Boeing 737282 · Cabin Temperature Control System
  > NON-ETOPS FLIGHT 63 HNL-LIH, DURING CLIMB, THE CREW NOTED LOUD NOISE AND ICE EMANATING FROM THE AIR CONDITIONING SYSTEM. THE CREW ATTEMPTED TO CONTROL THE NOISE AND ICE BY SELECTING A WARMER TEMPERATURE WITH NO CHANGE IN CONDITION. THE NOISE WAS DISRUPTIVE T
- [SDR TSAA0675112](https://openairdocs.org/sdr/TSAA0675112.md): Control Valve · failed · Nov 24, 2006 · N824AL · Boeing 737282 · Engine Bleed Air System
  > FLT 206 HNL-OGG: DURING TAKEOFF ROLL, NR 1 ENGINE EPR WOULD NOT INCREASE ABOVE 1.53 WITH MORE THAN A TWO THROTTLE KNOB WIDTH SPLIT AND EGT RISING TO 580 DEGREES. NR 2 ENGINE STABILIZED AT 1.89 EPR AND EGT AROUND 530 DEGREES. TAKEOFF WAS ABORTED AROUND 80 KNO
- [SDR TSAA0632094](https://openairdocs.org/sdr/TSAA0632094.md): Uplock · dirty · Nov 2, 2006 · N824AL · Boeing 737282 · Landing Gear Position and Warning
  > AFTER TAKEOFF, THE RT MLG DID NOT RETRACT. CREW CYCLED THE LANDING GEAR LEVER AND WAS ABLE TO RETRACT THE GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE RT MLG UPLOCK SENSOR AND PERFORMED THE MAIN LANDING GEAR EXTENSION AND RETR
- [SDR TSAA0672088](https://openairdocs.org/sdr/TSAA0672088.md): Nose Bullet · loose · Oct 16, 2006 · N824AL · Boeing 737282 · Engine (Turbine/Turboprop)
  > NON-ETOPS FLT 281: CLIMBING THRU 16,000 FEET WITH THE ENGINE ANTI-ICE ON, THE CREW HEARD A LOUD BANGING SOUND COMING FROM THE LT SIDE OF THE AIRCRAFT. ENGINE INDICATIONS WERE NORMAL. THE CREW RETARDED THE NR 1 ENGINE THRUST LEVER AND THE BANGING STOPPED. T
- [SDR TSAA0629060](https://openairdocs.org/sdr/TSAA0629060.md): Hose · failed · Jul 28, 2006 · N824AL · Boeing 737282 · Hydraulic System, Main
  > NON-ETOPS FLT 77 ITO-HNL: DURING LANDING ROLLOUT, THE AIRCRAFT EXPERIENCED SYSTEM ‘A’ HYDRAULIC FAILURE. THE CREW BROUGHT THE AIRCRAFT TO A STOP, NOTIFIED TOWER, AND PERFORMED THEIR QRH CHECK LIST. THE AIRCRAFT WAS TOWED BY MAINTENANCE TO THE GATE. R & R NO
- [SDR TSAA0652044](https://openairdocs.org/sdr/TSAA0652044.md): Slide · out of position · Jun 6, 2006 · N824AL · Boeing 737282 · Escape Slide
  > NON-ETOPS: FLT 206 HNL - OGG: ON THE GROUND, FWD SVC DOOR EMERGENCY SLIDE ACCIDENTALLY DISLODGED FROM THE DOOR BUT DID NOT INFLATE. REMOVED AND REPLACED FORWARD SERVICE DOOR SLIDE CHUTE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0653002](https://openairdocs.org/sdr/TSAA0653002.md): Skin Panel · cracked · Jan 5, 2006 · N824AL · Boeing 737282 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACK LOWER BL-0, BETWEEN S-28L AND R AT BS 370. TWO 1/2 INCH FUSELAGE SKIN CRACKS LOWER BL-0, BETWEEN S-28L AND R AT BS370 AND BS380. MAINTENANCE REPAIRED WITH APPROXIMATELY 40" X 20" SKIN PATCH, FABRICATED DOUBLER)1002024-T3). REPAIR COMPLE
- [SDR TSAA0532055](https://openairdocs.org/sdr/TSAA0532055.md): Tire · failed · Nov 11, 2005 · N824AL · Boeing 737282 · Tire
  > DURING TAXI AFTER LANDING, CREW HEARD A LOAD POP FOLLOWED BY VIBRATION FROM THE NOSEWHEEL AND STEERING DIFFICULTY. CREW STOPPED AIRCRAFT ON TAXIWAY. MAINTENANCE FOUND HOLE IN LT NOSEWHEEL AND BOTH TIRES FLAT. REMOVED AND REPLACED BOTH NOSEWHEEL TIRES, INSPE
- [SDR TSAA0532050](https://openairdocs.org/sdr/TSAA0532050.md): Anti-Skid Sys · deactivated · Oct 20, 2005 · N824AL · Boeing 737282 · Brake Anti-Skid Section
  > ON CLIMB OUT, PILOT OBSERVED THE LT ANTI-SKID LIGHT ON AND STAYED AND RETURNED BACK TO DEPARTURE. THE ANTI-SKID SYSTEM WAS MEL’D WAITING FOR AN ANTI-SKID CONTROL BOX. THE ANTI-SKID SYSTEM AND ANTI-SKID BRAKES WERE DEACTIVATED.
- [SDR TSAA0552009](https://openairdocs.org/sdr/TSAA0552009.md): Warning Light · false indication · Feb 25, 2005 · N824AL · Boeing 737282 · Door Warning System
  > FLT 211, OGG-HNL, FORWARD CARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF PRIOR TO 80 KTS. RETURNED TO GATE. MAINTENANCE OPENED AND CLOSED THE FORWARD CARGO DOOR AND CHECKED LOCKS FOR SECURITY. OPS CHECK OK AND LIGHTS CHECK GOOD. IN HNL, FWD
- [SDR TSAA0527002](https://openairdocs.org/sdr/TSAA0527002.md): Sensor · defective · Jan 16, 2005 · N824AL · Boeing 737282 · Leading Edge Slat Position Indicating System
  > FLT 278, HNL-KOA: ON INITIAL TAKEOFF ROLL, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED (NR 4 SLAT) WITH THE CONFIGURATION WARNING HORN. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 4 LEADING EDGE FLAP EXTEND SENSOR. OPS CHECK OK PER
- [SDR TSAA0434084](https://openairdocs.org/sdr/TSAA0434084.md): Indicator · inoperative · Dec 22, 2004 · N824AL · Boeing 737282 · Airspeed/Mach Indicator
  > FLT 220, HNL-OGG: FIRST OFFICE AIRSPEED INDICATOR INOP. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE MACH AIR SPEED INDICATOR. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0436069](https://openairdocs.org/sdr/TSAA0436069.md): Bleed Air Sys · malfunctioned · Sep 17, 2004 · N824AL · Boeing 737282 · Pneumatic System
  > FLIGHT 280, HNL-KOA: PASSING THROUGH 8000 FT ON CLIMB-OUT, THE RT DUCT PRESSURE WAS OBSERVED AT ABOUT 40PSIG WITH THE ISOLATION VALVE CLOSED AND THE RT BLEED & RT PACK OFF. THE PRESSURE THEN DECREASED TO 14 PSIG, AND THEN DECREASED FURTHER WHEN POWER WAS REDUC
- [SDR TSAA0353219](https://openairdocs.org/sdr/TSAA0353219.md): Skin · corroded · Nov 2, 2003 · N824AL · Boeing 737282 · Wing, Plate/Skin
  > FOUND LT UPPER WING SURFACE CORRODED BETWEEN FRONT & REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 6 AS NR 1 - 19 AT LOCATIONS, NR 1, 2, & 3 AT WBL 227, NR 4 AT WLB 228, NR 5 AT WBL 254, NR 6 AT WBL 264, NR 7 AT WBL 268, NR 8 AT WBL 234, NR 9 AT WBL 236, NR 10 AT
- [SDR TSAA0353218](https://openairdocs.org/sdr/TSAA0353218.md): Skin · corroded · Nov 2, 2003 · N824AL · Boeing 737282 · Wing, Plate/Skin
  > FOUND RIGHT UPPER WING SURFACE CORROSION BETWEEN THE FRONT AND REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 5 AS NR 1 TO NR 15 AT THE FOLLOWING LOCATIONS, NR 1 AT WBL 92.5, NR 2, 3, 4, 5 AND 6 BETWEEN WBL 198.6 AND WBL 227.0, NR 7 AND 8 AT WBL 157, NR 9 AND 10 BE
- [SDR TSAA0253267](https://openairdocs.org/sdr/TSAA0253267.md): Skin · cracked · Sep 24, 2003 · N824AL · Boeing 737282 · Fuselage Main, Plate/Skin
  > CLEANED OUTER SKIN AT EACH MOUNTING HOLE. OVER-DRILLED ELONGATED HOLES TO RESTORE HOLES TO CIRCULAR SHAPE. TRIMMED OUT CRACK DAMAGED HOLE LARGE ENOUGH TO REMOVE CRACK TO RECTANGULAR SHAPE. HFEC VERIFIED HOLES CRACK FREE. FABRICATED CIRCULAR AND RECTANGULAR
- [SDR TSAA0253249](https://openairdocs.org/sdr/TSAA0253249.md): Floorbeam · cracked · Sep 17, 2003 · N824AL · Boeing 737282 · Fuselage Main, Floor Beam
  > REMOVED EXISTING FASTENERS, STIFFENERS, ANGLE AND A SECTION OF THE WEB. REMOVED AND DISCARDED REINFORCING ANGLE, DOUBLER AND A SECTION OF THE WEB. DRILL AND COLD WORKED THE HOLES IN THE CHORD. INSTALLED SPLICE ANGLE AND STIFFENERS WITH FASTENERS SHOWN IN SE
- [SDR TSAA0253268](https://openairdocs.org/sdr/TSAA0253268.md): Lap Joint · damaged · Sep 10, 2003 · N824AL · Boeing 737282 · Fuselage Main, Plate/Skin
  > TRIMMED BONDED DOUBLER ABOVE EXISTING FASTENER PATTERN LEAVING ED FOR FINAL FASTENER INSTALL. OPENED DISCREPANT COUNTERSINK HOLE TO.75 INCH DIAMETER. VERIFIED CRACK FREE USING HFEC. HOLE OPENED UP TO 1 INCH INSURANCE CUT. FABBED.032/.036 INCH THICK CIRCUL
- [SDR TSAA0255264](https://openairdocs.org/sdr/TSAA0255264.md): Skin · gouged · Sep 5, 2003 · N824AL · Boeing 737282 · Horizontal Stabilizer, Plate/Skin
  > CUT AND REMOVED GOUGE AREA. FABRICATED REPAIR.063 DOUBLER AND.040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0255266](https://openairdocs.org/sdr/TSAA0255266.md): Skin · gouged · Sep 5, 2003 · N824AL · Boeing 737282 · Horizontal Stabilizer, Plate/Skin
  > CUT OUT DAMAGED AREA. FABRICATED REPAIR.063 DOUBLER AND.040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0255265](https://openairdocs.org/sdr/TSAA0255265.md): Skin · dented · Sep 5, 2003 · N824AL · Boeing 737282 · Empennage Structure
  > CUT OUT DAMAGED AREA. FABRICATED REPAIR.063 DOUBLER AND.040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253236](https://openairdocs.org/sdr/TSAA0253236.md): Pressure Panel · damaged · Oct 27, 2002 · N824AL · Boeing 737282 · Fuselage Main, Bulkhead
  > PERFORMED MODIFICATION TO THE WEB AND DOUBLER OF THE MAIN WHEEL WELL PRESSURE FLOOR TRANSVERSE BEAM BETWEEN BS 650 AND BS 727 AND BETWEEN RT AND LT BBL 45. FABRICATED WEB FILLER AND REPAIR DOUBLER IAW FIGURE 7. REPLACED ANGLE, CHANNEL AND DOUBLER WITH PARTS
- [SDR TSAA0253235](https://openairdocs.org/sdr/TSAA0253235.md): Beam · damaged · Oct 27, 2002 · N824AL · Boeing 737282 · Wing, Landing Gear Attach Fittings
  > OVERSIZED 4 HOLES IN THE RIGHT MLG LOWER BEAM CHORD FLANGE. FABRICATED FOUR FREEZE PLUGS. FABRICATED FOUR 1 INCH DIAMETER RETAINING WASHERS. INSTALLED FREEZE PLUGS AND OPENED ID HOLES TO THE EXISTING.1875 INCH DIAMETER PANEL ATTACH BOLTS. INSTALLED RETAIN
- [SDR TSAA0253232](https://openairdocs.org/sdr/TSAA0253232.md): Structure · cracked · Oct 27, 2002 · N824AL · Boeing 737282 · Fuselage Miscellaneous Structure
  > TRIMMED OUT THE DAMAGE OF THE HOLES TO A RECTANGULAR SHAPE. VERIFIED CRACK REMOVED USING HFEC. FABRICATED CIRCULAR DOUBLERS FOR EACH HOLE. REPAIR COMPLETED IAW ECO 3302. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253231](https://openairdocs.org/sdr/TSAA0253231.md): Fitting · damaged · Oct 27, 2002 · N824AL · Boeing 737282 · Trailing Edge Flaps
  > REMOVED DAMAGE FROM THE NR 2 AND NR 7 FLAP TRACK ATTACHMENT FITTING HOLE. FABRICATED A 'NEW' REPLACEMENT TUBE AND BUSHING INCREASING THE OUTSIDE DIAMETER.0015 TO.0020 INCH INTERFERENCE FIT ON THE FINISHED DIAMETER OF THE HOLE. INSTALLED NEW TUBE AND BUSHIN
- [SDR TSAA0253234](https://openairdocs.org/sdr/TSAA0253234.md): Structure · corroded · Oct 18, 2002 · N824AL · Boeing 737282 · Horizontal Stabilizer Miscellaneous Structure
  > BLENDED THE DAMAGE ON THE LUG. SPOTFACED THE INBOARD AND OUTBOARD SURFACES. OVERSIZED THE TAPERED/ELONGATED HOLE OF THE INBOARD LUG ON THE ORIGINAL CENTERLINE TO OBTAIN A ROUND AND TRUE CONDITION. FABRICATED NEW REPAIR SLEEVE BUSHING TO FIT THE OVERSIZED IN
- [SDR TSAA0253233](https://openairdocs.org/sdr/TSAA0253233.md): Structure · cracked · Oct 18, 2002 · N824AL · Boeing 737282 · Fuselage Miscellaneous Structure
  > TRIM OUT ALL THREE HOLES IN THE DAMAGED ZONE. HFEC THE EDGE OF THE TRIM. FABRICATED A DOUBLER AND A TRIPLER. INSTALLED DOUBLER AND TRIPLER. REPAIR COMPLETED IAW ECO 3250, FIGURE 24. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0233136](https://openairdocs.org/sdr/TSAA0233136.md): Battery Pack · discharged · May 9, 2002 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED NR 6, EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233054](https://openairdocs.org/sdr/TSAA0233054.md): Battery Pack · discharged · Feb 18, 2002 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133184](https://openairdocs.org/sdr/TSAA0133184.md): Battery Pack · discharged · Dec 27, 2001 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0126181](https://openairdocs.org/sdr/TSAA0126181.md): Fire Loop · defective · Dec 23, 2001 · N824AL · Boeing 737282 · Fire Detection
  > FLT 205 - HNL-LIH - EN ROUTE TO LIH, THE APU FIRE WARNING ILLUMINATED THOUGH THE APU WAS PREVIOUSLY MEL'D. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT RETURNED TO HNL WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS OPERATING UNDER MEL 49-1 FOR A PREVIOUS
- [SDR TSAA0133164](https://openairdocs.org/sdr/TSAA0133164.md): Battery Pack · discharged · Nov 26, 2001 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED LEFT OVERWING IDENT BATTERY PACKED DUE TO LOW VOLTAGE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153151](https://openairdocs.org/sdr/TSAA0153151.md): Bulkhead · cracked · Oct 31, 2001 · N824AL · Boeing 737282 · Fuselage Main, Bulkhead
  > FOUND RIVET HOLES CRACKED AT BS 178 LEFT AND RIGHT LBL 9 WL 234. REMOVED CRACK PER SRM 53-10-11 PAGE 1, PROCEDURE 1. VERIFIED CRACK REMOVED USING HFEC. INSTALLED REPAIR DOUBLER IAW ECO 3138 PART 1. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133096](https://openairdocs.org/sdr/TSAA0133096.md): Battery Pack · corroded · Jul 18, 2001 · N824AL · Boeing 737282 · Lighting System
  > FOUND LEFT OVERWING EMERGENCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133095](https://openairdocs.org/sdr/TSAA0133095.md): Battery Pack · corroded · Jul 18, 2001 · N824AL · Boeing 737282 · Lighting System
  > AFT ENTRY DOOR EMEREGNCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133082](https://openairdocs.org/sdr/TSAA0133082.md): Battery Pack · inoperative · Jul 7, 2001 · N824AL · Boeing 737282 · Lighting System
  > REPLACED NR 1 AND NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153021](https://openairdocs.org/sdr/TSAA0153021.md): Frame · cracked · Feb 20, 2001 · N824AL · Boeing 737282 · Fuselage Main, Frame
  > IDENTIFIED A CRACK AT 2 PLACES ON THE RIGHT SIDE OF BS 1156 CHORD BETWEEN WL 281-269. STOP DRILLED ENDS OF CRACKS, REMOVED FASTENERS ON AFFECTED CHORD ASSEMBLY AND INSTALLED REPAIR STIFFENER ANGLE IAW ECO 1822. APPLIED ALODINE AND PRIMER BMS 10-11 TYPE 1 PRI
- [SDR TSAA0153019](https://openairdocs.org/sdr/TSAA0153019.md): Frame · cracked · Feb 17, 2001 · N824AL · Boeing 737282 · Fuselage Main, Frame
  > IDENTIFIED CRACK AT RIGHT UPPER CHORD BS 727, STRINGER 18A AFT HOLE BY UTILIZING HFEC AND ULTRASONIC METHOD. REMOVED AND REPLACED RIGHT UPPER CHORD ASSEMBLY CLEANED AND TREATED ALL EXPOSED AREAS AND APPLIED CORROSION INHIBITING COMPOUND IAW ECO 1785. AIRCRAF
- [SDR TSAA0153020](https://openairdocs.org/sdr/TSAA0153020.md): Frame · dented · Feb 16, 2001 · N824AL · Boeing 737282 · Fuselage Main, Frame
  > IDENTIFIED DENT ON FRAME ASSEMBLY 5 INCHES BY 7 INCHES AT BS 360-380 STRINGER 17L. (M)
- [SDR TSAA0033206](https://openairdocs.org/sdr/TSAA0033206.md): Battery Pack · inoperative · Sep 5, 2000 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED NR 1, NR 4 AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA200033056](https://openairdocs.org/sdr/TSAA200033056.md): Battery Pack · inoperative · Feb 3, 2000 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED POSITION 1 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA200032031](https://openairdocs.org/sdr/TSAA200032031.md): Valve · inoperative · Jan 22, 2000 · N824AL · Boeing 737282 · Landing Gear Brake System
  > HNL/ITO - FLT 108 - ON TAKOFF ROLL, PARKING BRAKE LIGHT AND ANTI-SKID INOPERABLE. INBOARD/OUTBAORD LIGHT REMAINED ILLUMINATED. PARKING BRAKE LEVER WAS IN RELEASED POSITION WITH NO BRAKE DRAG FELT. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED
- [SDR TSAA9933518](https://openairdocs.org/sdr/TSAA9933518.md): Battery Pack · discharged · Dec 29, 1999 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED BATTERY PACK FOR NR 2 EMERGENCY FLOOR PROX LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933447](https://openairdocs.org/sdr/TSAA9933447.md): Battery Pack · discharged · Sep 29, 1999 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED BATTERY PACK FOR CENTER AISLE EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNE TO SERVICE. (M)
- [SDR TSAA9957416](https://openairdocs.org/sdr/TSAA9957416.md): Beam · corroded · Aug 26, 1999 · N824AL · Boeing 737282 · Wing Miscellaneous Structure
  > LEFT MLG BEAM CORRODED BEYOND LIMITS. REPLACED LEFT MLG BEAM (PERFORMED BY BOEING AOG TEAM). AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9952415](https://openairdocs.org/sdr/TSAA9952415.md): Frame · cracked · Aug 26, 1999 · N824AL · Boeing 737282 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR FRAME CORRODED AT LWR AFT CORNER ABOVE DOOR SILL. REPAIRED IAW ECO 2992. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933411](https://openairdocs.org/sdr/TSAA9933411.md): Battery · discharged · Aug 23, 1999 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED BATTERY PACKS FOR NR 2, NR 4 AND NR 5 EMERGENCY FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933390](https://openairdocs.org/sdr/TSAA9933390.md): Battery Pack · discharged · Aug 12, 1999 · N824AL · Boeing 737282 · Emergency Lighting
  > REPLACED BATTERY PACK IN AFT CONTROL MODULE DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)

Next page: https://openairdocs.org/deregistered/N824AL-2013-10-29/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 = 'N824AL' AND deregistration_id = 'N824AL-2013-10-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N824AL-2013-10-29/reports

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