# Service difficulty reports: N810AL, cancelled Jan 26, 2009

A list on [N810AL, cancelled Jan 26, 2009](https://openairdocs.org/deregistered/N810AL-2009-01-26.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 · 76 reports

- [SDR TSAA0732043](https://openairdocs.org/sdr/TSAA0732043.md): Module · failed · Jul 31, 2007 · N810AL · Boeing 7372Y5 · Landing Gear Retraction/Extension System
  > NON-ETOPS FLIGHT 221 OGG - HNL. WHEN THE CREW SELECTED THE LANDING GEAR TO UP, THE LT MAIN GEAR DOWN LIGHT TOOK A FEW SECONDS LONGER TO EXTINGUISH THAN THE OTHER GEAR INDICATIONS. AFTER THE GEAR LEVER WAS SELECTED TO OFF, THE LT MAIN GEAR EXTENDED UNCOMMANDE
- [SDR TSAA0729040](https://openairdocs.org/sdr/TSAA0729040.md): Hose · failed · Jul 7, 2007 · N810AL · Boeing 7372Y5 · Hydraulic System, Main
  > FLIGHT 26 HNL-OGG - AFTER TAKEOFF FROM HNL, CREW NOTED LOSS OF SYSTEM A HYDRAULIC PRESSURE. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE TOWED THE AIRCRAFT TO THE GATE AND REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR HYDRAULIC SURGE RELIEF L
- [SDR TSAA0726029](https://openairdocs.org/sdr/TSAA0726029.md): Fire Detector · failed · May 31, 2007 · N810AL · Boeing 7372Y5 · Fire Detection
  > FLIGHT 93 HNL-LIH - AFTER STARTING THE NR 1 ENGINE, THE CREW NOTED THE NR 1 ENGINE FIRE INDICATION LIGHT ILLUMINATED. CREW FOLLOWED THE QRH PROCEDURES: SHUT DOWN NR 1 ENGINE AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AIRCRAFT WAS TOWED BACK TO THE
- [SDR TSAA0632057](https://openairdocs.org/sdr/TSAA0632057.md): Wheel · separated · Jul 24, 2006 · N810AL · Boeing 7372Y5 · Wheel/Ski/Float
  > ON LANDING, CREW HEARD AN UNUSUAL (BUMP) NOISE WITH NORMAL LANDING. TAXI TO GATE WITHOUT FURTHER INCIDENT. CREW FOUND NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY HAD SEPARATED FROM THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NR 1 MLG BRAKE ASSEMBLY AND THE
- [SDR TSAA0651040](https://openairdocs.org/sdr/TSAA0651040.md): Spar · corroded · May 24, 2006 · N810AL · Boeing 7372Y5 · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL STABILIZER RT REAR SPAR UPPER CHORD CORROSION (3 AREAS).
- [SDR TSAA0651039](https://openairdocs.org/sdr/TSAA0651039.md): Spar · corroded · May 24, 2006 · N810AL · Boeing 7372Y5 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER RIGHT T/E REAR SPAR CORROSION (3 AREAS).
- [SDR TSAA0653018](https://openairdocs.org/sdr/TSAA0653018.md): Skin Panel · cracked · Mar 17, 2006 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/Skin
  > A 2 INCH SKIN CRACK AT BS 929 STR 24L. A.04 INSURANCE MADE IAW SRM 53-30-3. RIVET PATTERN LAID OUT AND DRILLED AND MANUFACTURED REPAIR DOUBLER, TRIPLER, AND 2 FILLERS PER SRM 53-30-3 FIG 48 DET XIX. HFEC RIVET HOLES IAW BOEING NDT MANUAL 51-00-00 PT 6. RE
- [SDR TSAA0653017](https://openairdocs.org/sdr/TSAA0653017.md): Spar · corroded · Mar 11, 2006 · N810AL · Boeing 7372Y5 · Leading Edge Devices
  > CORROSION ON UPPER & LOWER SURFACE OF FRONT SPAR LOWER CORD BETWEEN FSS 297 & FSS-306 AT SLAT NR 4. BLENDED INBOARD - OUTBOARD DIRECTION 10:1 DEPTH TO BLEND RATION. SHOT/FLAP PEEN BLENDED ARE PER SRM. FABRICATED SOLID FILLERS TO REPLACE REMOVED MATERIAL. F
- [SDR TSAA0621007](https://openairdocs.org/sdr/TSAA0621007.md): Fan · defective · Jan 27, 2006 · N810AL · Boeing 7372Y5 · Air Distribution Fan
  > ON APPROACH THE PILOT SMELLED SMOKE AND AFTER LANDING THE SMELL GREW STRONGER. AIRPLANE TAXIED BACK TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED GASPER FAN. OPS CHECK GOOD, NO HELP. THE CABIN AUGMENTATION FAN WAS FOUND TO BE INOP. REMOVED AND REPLAC
- [SDR TSAA0653006](https://openairdocs.org/sdr/TSAA0653006.md): Skin · cracked · Jan 24, 2006 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/Skin
  > A 4 INCH FUSELAGE SKIN CRACK BS 937 AT STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMATELY 24 X 20 INCH SKIN PATCH, FABRICATED DOUBLER, TRIPLER, AND STRUCTURAL FILLER NR 5 AND 6 PER SRM 53-30-3, FIG 48, DET XII.
- [SDR TSAA0575031](https://openairdocs.org/sdr/TSAA0575031.md): Bleed Valve · defective · Jul 20, 2005 · N810AL · Boeing 7372Y5 · Compressor Bleed Valve
  > ON TAKE-OFF NR 2 ENGINE COMPRESSOR STALL ON INITIAL RUN-UP FROM IDLE. R & R NR 2 ENG PRBC IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED PER P&W MM 72-00-00. R.I.I. COMPLETED FOR NR 2 ENG PRBC VALVE CHANGE IAW MM 75-31-11. DID NOT FIX OFF IDLE STALL. L
- [SDR TSAA0575029](https://openairdocs.org/sdr/TSAA0575029.md): Bleed Valve · defective · Jul 12, 2005 · N810AL · Boeing 7372Y5 · Compressor Bleed Valve
  > RUNNING UP ENGINES FOR TAKE-OFF, GOT STEADY BANGING. RPM BARELY PAST IDLE. FLIGHT ATTENDANTS GUESS THE NR 2 ENGINE. TAKE-OFF ABORTED. R&R PRBC IAW MM 75-31-11 OPS CHECK OK ON NR 2 ENGINE. BLEED VALVE SCHEDULING COMPLETED PER PWA MM 72-00-00. LUBED 8TH AN
- [SDR TSAA0479019](https://openairdocs.org/sdr/TSAA0479019.md): Engine · leaking · Jan 16, 2004 · N810AL · Boeing 7372Y5 · Turbine Engine Oil System
  > FLT 224 - LIH-HNL - LOW OIL PRESSURE ILGHT ON NR 1 ENGINE ILLUMINATED. OIL PRESSURE DROPPED TO 20 PSI. FOLLOWED QRH AND SHUTDOWN THE NR 1 ENGINE. DECLARED EMERGENCY AND HAD UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 1 ENGINE PER FORMS M-211 THROUGH M-
- [SDR TSAA0429001](https://openairdocs.org/sdr/TSAA0429001.md): Line · failed · Dec 30, 2003 · N810AL · Boeing 7372Y5 · Hydraulic System, Main
  > FLT 240 - HNL-OGG - ON GEAR RETRACTION 'A' SYSTEM HYDRAULIC ANNUNCIATOR LIGHT CAME ON. SYSTEM QUANTITY AT 1.5 GALLONS. RETURNED TO HNL. FOUND RIGHT MAIN GEAR UPLOCK ACTUATOR FLEX-LINE RUPTURED. REMOVED AND REPLACED FLEX-LINE. LEAK CHECK OK. SERVICED HYDRA
- [SDR TSAA0333205](https://openairdocs.org/sdr/TSAA0333205.md): Battery Pack · inoperative · Nov 29, 2003 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED AFT ENTRY DOOR IDENT EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0353037](https://openairdocs.org/sdr/TSAA0353037.md): Skin · cracked · Feb 9, 2003 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/Skin
  > NINE RIVETS ON STRINGER 16R SHOW SIGNS OF STRESS CRACKS EMANATING FROM THE FASTENER HOLES. REMOVED RIVETS, OVERSIZED HOLES BY 1/16, HFEC VERIFIED FASTENER HOLES CRACK FREE. FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPA
- [SDR TSAA0233228](https://openairdocs.org/sdr/TSAA0233228.md): Battery Pack · discharged · Nov 8, 2002 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0233229](https://openairdocs.org/sdr/TSAA0233229.md): Light · inoperative · Nov 8, 2002 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED LT OVERWING IDENT LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0253201](https://openairdocs.org/sdr/TSAA0253201.md): Structure · gouged · Oct 2, 2002 · N810AL · Boeing 7372Y5 · Cargo/Baggage Doors
  > CUTOUT DAMAGE, PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER STRUCTURAL FILLER. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0253183](https://openairdocs.org/sdr/TSAA0253183.md): Frame · corroded · Jun 29, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Frame
  > AUXILIARY POWER UNIT COMPARTMENT CORRODED AT BS 1156 REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER FROM SRM, AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0253152](https://openairdocs.org/sdr/TSAA0253152.md): Skin · cracked · Jun 17, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/Skin
  > FOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFECTS NOTED. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0253142](https://openairdocs.org/sdr/TSAA0253142.md): Skin · corroded · May 15, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/Skin
  > FOUND CORROSION ON THE LEFT HAND OUTBOARD WING MAIN BOX UPPER SKIN AT WBL 71.24, STR 5, 7 AND WBL92.5 STR 1, 5. BLENDED OUT CORROSION AT A 10:1 RATIO MINIMUM PER SRM. ULTRASOUND INSPECTED TO ENSURE NO REMAINING CORROSION. HFEC AFFECTED FASTENER HOLE BORE FO
- [SDR TSAA0253141](https://openairdocs.org/sdr/TSAA0253141.md): Skin · worn · May 13, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/Skin
  > FOUND SKIN WORN THROUGH ON THE RIGHT LEADIN EDGE LOWER WING SKIN SURFACE AT FS 413. CUT OUT DAMAGED LEADING EDGE FILLER AND SKIN. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED THE REPAIR PARTS WITH FASTENERS. APPLIED BMS 5-95 SEALANT TO THE MATING
- [SDR TSAA0253134](https://openairdocs.org/sdr/TSAA0253134.md): Pressure Panel · corroded · May 13, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Bulkhead
  > FOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INSTALLED CHORD AND REPAIR ANGLES. COMPLETED REPAIR.
- [SDR TSAA0251133](https://openairdocs.org/sdr/TSAA0251133.md): Skin · gouged · May 10, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/Skin
  > FOUND GOUGE IN SKIN AT STRINGER 16L AT BS 843. BLENDED OUT DAMAGED AREA TO A SMOOTH SURFACE. VERIFIED NO CRACKS USING HFEC. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251132](https://openairdocs.org/sdr/TSAA0251132.md): Bracket · chafed · May 10, 2002 · N810AL · Boeing 7372Y5 · Trailing Edge Flaps
  > FOUND NR 8 FLAP JACKSCREW TRAILING EDGE MOUNT BRACKET CHAFFING AT FLAP TRACK FAIRING. BLENDED OUT DAMAGED AREA. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251130](https://openairdocs.org/sdr/TSAA0251130.md): Slat · corroded · May 10, 2002 · N810AL · Boeing 7372Y5 · Leading Edge Devices
  > FOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0253146](https://openairdocs.org/sdr/TSAA0253146.md): Skin · worn · Apr 25, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE LOWER SKIN AT FSS 413 WORN BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER, SPLICE PLATE AND DOUBLER. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0253125](https://openairdocs.org/sdr/TSAA0253125.md): Spar · corroded · Apr 25, 2002 · N810AL · Boeing 7372Y5 · Wing Spar
  > FOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSION BY BLEND OUT. HFEC AREA TO ENSURE FREE OF CRACKS AND CORROSION. FABRICATED A REPAIR FILLER. INSTALLED REPAIR FILLER. REPAIR COMPLETED
- [SDR TSAA0253127](https://openairdocs.org/sdr/TSAA0253127.md): Bulkhead · cracked · Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Bulkhead
  > FOUND CRACK ON THE BLK 178 AT WL 212, RBL 5.7 DURING INSPECTION. CUTOUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PART.
- [SDR TSAA0253126](https://openairdocs.org/sdr/TSAA0253126.md): Bulkhead · cracked · Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Bulkhead
  > FOUND CRACK ON THE BLK 178 AT WL 212, LBL 5.7 DURING INSPECTION PER ECO 3137. CUT OUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PARTS. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0253128](https://openairdocs.org/sdr/TSAA0253128.md): Stringer · dented · Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Longeron/Stringer
  > FOUND DENT ACROSS STRINGER 15L AT BS 900. CUTOUT STRINGER SEGMENT AT BS 900. REMOVED THE SEGMENT OF THE STRINGER AFT TO THE PRODUCTION SPLICE. FABRICATED NEW STRINGER SEGMENT. INSTALLED STRINGER PER SRM 53-10-3. COMPLETED REPAIR. AIRCRAFT RETURNED TO SER
- [SDR TSAA0253131](https://openairdocs.org/sdr/TSAA0253131.md): Floorbeam · cracked · Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Floor Beam
  > FOUND CRACKS AT BL 0 FLOOR BEAM AT BS 663 AND BETWEEN BS 700-717 WEB. REMOVED AND DISCARDED A SECTION OF THE WEB AND DOUBLER CONTAINING THE CRACKS. FABRICATED ALL REPAIR PARTS. INSTALLED SPLICE ANGLES AND STRAPS WITH NUT PLATES. COMPLETED INSTALLATION OF R
- [SDR TSAA0253006](https://openairdocs.org/sdr/TSAA0253006.md): Frame · corroded · Jan 1, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Frame
  > REMOVED CORROSION DAMAGE ON STRINGER 5R UPPER CHORD AT BS 1093. REMOVED FORWARD PORTION OF DAMAGED CHORD. FABRICATED REPLACEMENT CHORD AND SPLICE ANGLES AND INSTALLED REPAIR PARTS PER FIGURE 1 IAW ECO 3259. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133092](https://openairdocs.org/sdr/TSAA0133092.md): Battery Pack · discharged · Jul 20, 2001 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0132070](https://openairdocs.org/sdr/TSAA0132070.md): Downlock Sensor · failed · Jun 13, 2001 · N810AL · Boeing 7372Y5 · Landing Gear Position and Warning
  > INBOUND TO HNL FROM LIH - REPORTED TO MAINTENANCE CONTROL OF THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ON IN-FLIGHT. CAPTAIN PERFORMED FLYBY FOR TOWER TO CHECK GEARS DOWN WHILE F/O ALSO CHECKED BY GOING TO BACK OF AIRCRAFT. GEARS RECYCLED ONCE AND LIGHT STILL
- [SDR TSAA0033216](https://openairdocs.org/sdr/TSAA0033216.md): Battery · inoperative · Oct 16, 2000 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA0053198](https://openairdocs.org/sdr/TSAA0053198.md): Skin · dented · Jul 30, 2000 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/Skin
  > REPAIRED A DENT AT LEFT FUSELAGE BS 360-380 STRINGER 17L, AFT OF FORWARD ENTRY DOOR. CUT OUT DAMAGED AREA PERFORMED HFEC INSPECTION. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033182](https://openairdocs.org/sdr/TSAA0033182.md): Battery · inoperative · Jul 30, 2000 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0073139](https://openairdocs.org/sdr/TSAA0073139.md): Fcu · failed · May 29, 2000 · N810AL · Boeing 7372Y5 · Fuel Controlling System
  > FLT 71 - OGG-HNL - THE NR 1 ENGINE RPM GAGE IMMEDIATELY DECREASED TO ZERO THE MOMENT THE AIRCRAFT LIFTED OFF THE RUNWAY. DID NOT ATTEMPT A RESTART, ACCOMPLISHED NORMAL SINGLE ENGINE LANDING WITH NO FURTHER PROBLEMS NOTED. REMOVED AND REPLACED NR 1 ENGINE FUE
- [SDR TSAA9933479](https://openairdocs.org/sdr/TSAA9933479.md): Battery · discharged · Nov 9, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 3, 4, 5, AND 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 99ZZZM807](https://openairdocs.org/sdr/99ZZZM807.md): Sensor · intermittent · Oct 26, 1999 · N810AL · Boeing 7372Y5 · Landing Gear Position and Warning
  > FLT 101 - OGG-HNL - LEFT MAIN GEAR RED UNSAFE GEAR LIGHT COMES ON INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED UPLOCK SENSOR LEFT GEAR PER MM 32-61-21 AND ALSO CHECKED UPLOCK MECHANISM PER MM 32-32-31. ALL OK, OPS OK ON GEAR SWING. AIRCRAFT RETURNED T
- [SDR TSAA9933408](https://openairdocs.org/sdr/TSAA9933408.md): Battery Pack · discharged · Aug 21, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 3 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933368](https://openairdocs.org/sdr/TSAA9933368.md): Battery Pack · discharged · Jul 31, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 5 EMERGENCY FLOOR BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933362](https://openairdocs.org/sdr/TSAA9933362.md): Battery Pack · discharged · Jul 25, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 4 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9921300](https://openairdocs.org/sdr/TSAA9921300.md): Relief Valve · failed · Jul 6, 1999 · N810AL · Boeing 7372Y5 · Cabin Pressure Control System
  > HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED, BUT DIDN'T CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTR
- [SDR TSAA9921292](https://openairdocs.org/sdr/TSAA9921292.md): Controller · failed · Jul 6, 1999 · N810AL · Boeing 7372Y5 · Cabin Pressure Controller
  > HNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED BUT DID NOT CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTR
- [SDR TSAA9933285](https://openairdocs.org/sdr/TSAA9933285.md): Battery · discharged · Jun 8, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933246](https://openairdocs.org/sdr/TSAA9933246.md): Battery · discharged · May 31, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED NR 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933223](https://openairdocs.org/sdr/TSAA9933223.md): Battery · discharged · Apr 19, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT POWER SUPPLY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N810AL-2009-01-26/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 = 'N810AL' AND deregistration_id = 'N810AL-2009-01-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N810AL-2009-01-26/reports

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