# Service difficulty reports: N808AL, cancelled Jun 16, 2008

A list on [N808AL, cancelled Jun 16, 2008](https://openairdocs.org/deregistered/N808AL-2008-06-16.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 · 140 reports

- [SDR TSAA0832009](https://openairdocs.org/sdr/TSAA0832009.md): Valve · leaking · Feb 18, 2008 · N808AL · Boeing 7372T4 · Hydraulic System, Main
  > NON-ETOPS FLIGHT 88 HNL-KOA, DURING TAKEOFF, THE CREW NOTED THE HYDRAULIC QUANTITY DROP FROM 3 GALLONS TO LESS THAN 1 GALLON. THE CREW ELECTED TO ABORT THE TAKEOFF AT LESS THAN 80 KNOTS INDICATED AIRSPEED. MAINTENANCE FIRST REPLACED A LEAKING O-RING SEAL ON
- [SDR TSAA0653101](https://openairdocs.org/sdr/TSAA0653101.md): Door Frame · damaged · Nov 13, 2006 · N808AL · Boeing 7372T4 · Fuselage Main, Structure
  > AFT CARGO DOOR CUT-OUT DAMAGED (LOWER AFT CORNER). ALOHA ECO 3622 ISSUED.
- [SDR TSAA0624080](https://openairdocs.org/sdr/TSAA0624080.md): Switch · failed · Sep 29, 2006 · N808AL · Boeing 7372T4 · Stabilizer Position Indicating
  > NON-ETOPS FLIGHT 206 HNL OGG. ON TAKEOFF THE CONFIGURATION WARNING ALARM SOUNDED WHEN THROTTLES WERE ADVANCED. CREW ABORTED TAKEOFF AT 15 KTS. AIRCRAFT WAS CONFIGURED PROPERLY FOR TAKEOFF WITH THE SPEED BRAKE DOWN, FLAPS SET TO 5 AND TRIM AT 5.5 UNITS. CRE
- [SDR TSAA0678059](https://openairdocs.org/sdr/TSAA0678059.md): Warning Light · illuminated · Jul 29, 2006 · N808AL · Boeing 7372T4 · Engine Thrust Reverser
  > NON-ETOPS FLT 224 LIH-HNL. ON TAKE OF ROLL, CREW NOTED THE NR 2 ENGINE THRUST REVERSER UNLOCKED LIGHT ON WITH ALL OTHER ENGINE INDICATIONS NORMAL. CREW ABORTED TAKEOFF AT 60 KTS AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE OPENED AND INSPECT
- [SDR TSAA0678054](https://openairdocs.org/sdr/TSAA0678054.md): Latch · lack of lube · Jul 15, 2006 · N808AL · Boeing 7372T4 · Engine Thrust Reverser
  > ON TAKEOFF ABOVE 80 KNOTS AND CLIMB, CREW NOTED NR 2 THRUST REVERSER UNLOCKED LIGHT ILLUMINATED INTERMITTENTLY. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED PER MEL 78-2 AND RELEASED THE AIRCRAFT FOR SERVICE. ON 7/16/06 MAINTENANCE CL
- [SDR TSAA0653046](https://openairdocs.org/sdr/TSAA0653046.md): Skin Panel · cracked · Jun 12, 2006 · N808AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > 2.25 INCH SKIN CRACK FOUND LEFT SIDE OF FUSELAGE BS 786 JUST ABOVE STRINGER 24L. MAINTENANCE REPAIRED WITH APPROXIMATELY 11 IN X 15 IN EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3, PROCEDURE VII, DETAIL VII.
- [SDR TSAA0653045](https://openairdocs.org/sdr/TSAA0653045.md): Skin Panel · cracked · Jun 12, 2006 · N808AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > 2.5 INCH SKIN CRACK FOUND RIGHT SIDE OF FUSELAGE AT BS 941 JUST ABOVE STRINGER 24R. MAINTENANCE REMOVED TWO EXISTING REPAIRS AND REPAIRED WITH 36 IN X 46 IN EXTERNAL SKIN PATCH, FABRICATED FILLERS, DOUBLER, AND TRIPLER PER SRM 53-30-3, PROCEDURE VII, DETAIL X
- [SDR TSAA0653042](https://openairdocs.org/sdr/TSAA0653042.md): Skin Panel · cracked · Jun 11, 2006 · N808AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > 3 INCH CRACK FOUND RT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR CUTOUT AS BS 867 STRINGER 23R. MAINTENANCE REMOVED ONE EXISTING REPAIR AND REPAIRED WITH APPROXIMATELY 19-1/2 IN X 19-1/2 IN EXTERNAL SKIN PATCH, FABRICATED DOUBLER AND TRIPLER PER SRM 53-30-3,
- [SDR TSAA0627016](https://openairdocs.org/sdr/TSAA0627016.md): Slat · bird strike · Mar 11, 2006 · N808AL · Boeing 7372T4 · Leading Edge Devices
  > ON CLIMB AT 1000 FT AIRCRAFT STRUCK A LARGE BIRD AT NR 1 LEADING EDGE SLAT. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH FORM M-106 BIRD STRIKE INSPECTION AND FOUND A LARGE DENT APPROXIMATELY 1.5 INCH WIDE ON THE OUTBOARD LEAD
- [SDR TSAA0653010](https://openairdocs.org/sdr/TSAA0653010.md): Skin · cracked · Feb 8, 2006 · N808AL · Boeing 7372T4 · Leading Edge Devices
  > FOUND 3 CRACKS AROUND CENTER UPSTOP OF NR 2 SLAT; WING LEADING EDGE. BETWEEN LEFT WS 453 AND WS 479. L/E SKIN FABRICATED, TRIMMED, CLEANED, ALODINED, PRIMED, AND SEALED IAW SRM 57-30-04. REPAIR SIZE APPROX 14" BY 25".
- [SDR TSAA0672008](https://openairdocs.org/sdr/TSAA0672008.md): Engine · defective · Feb 2, 2006 · N808AL · Boeing 7372T4 · Engine (Turbine/Turboprop)
  > OGG-HNL: ON TAKEOFF NR 2 ENGINE EGT ROSE TO 650 DEGREES CELSIUS. ENGINE THROTTLED BACK UNTIL EGT WAS WITHIN LIMITS AND AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE IAW FORM M-211, M-212, M-213, AND M-215. NO FAULTS NOTED. A
- [SDR TSAA0553057](https://openairdocs.org/sdr/TSAA0553057.md): Skin Panel · cracked · Dec 13, 2005 · N808AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > A 3.5 INCH CRACK FOUND RIGHT SIDE OF FUSELAGE SKIN AFT OF AFT CARGO DOOR AT BS 927 STRINGER 23R. CUT OUT CRACK.040 INCH INSURANCE CUT. PERFORMED HFEC AROUND CUTOUT, NO CRACK PROPAGATION NOTED IAW BOEING NDT MANUAL 51-00-00, PART 6. REPAIRED WITH 10 X 13 IN
- [SDR TSAA0527048](https://openairdocs.org/sdr/TSAA0527048.md): Actuator · leaking · Oct 19, 2005 · N808AL · Boeing 7372T4 · Drag Control System
  > CREW HAD INDICATION OF HYDRAULIC SYSTEM A, DROP IN PRESSURE. CREW DECLARED AN EMERGENCY AND WERE ABLE TO DEPLOY THE LANDING GEAR. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 SPOILER ACTUATOR AND INSPECTED AND REPLACED BOTH ENGINE CASE DRA
- [SDR TSAA0527047](https://openairdocs.org/sdr/TSAA0527047.md): Actuator · failed · Oct 12, 2005 · N808AL · Boeing 7372T4 · Leading Edge Slat Actuator
  > COOPESA TO BROWNSVILLE TX FERRY FLIGHT 808. NR 5 SLAT DID NOT RETRACT. LEFT WING TO BODY OVERHEAT INDICATION. THE CREW RETURNED TO COOPESA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 5 SLAT ACTUATOR AND PNEUMATIC DUCT AND CLAMP. OPS AND LEAK CHE
- [SDR TSAA0557027](https://openairdocs.org/sdr/TSAA0557027.md): Slat · inflt separation · Jul 18, 2005 · N808AL · Boeing 7372T4 · Leading Edge Devices
  > AFTER ARRIVAL IN LIH A PASSENGER ADVISED THE FLIGHT ATTENDANT THAT PART OF THE WING SEPARATED IN FLIGHT. CAPTAIN THEN OBSERVED A SECTION OF THE NUMBER THREE LEADING EDGE SLAT MISSING. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE LEADING EDGE SLAT ASSEMB
- [SDR TSAA0529014](https://openairdocs.org/sdr/TSAA0529014.md): Seal · leaking · Mar 8, 2005 · N808AL · Boeing 7372T4 · Hydraulic Handpump, Main
  > NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP DUE TO INPUT SHAFT SEAL LEAKING PER AMM 29-11-
- [SDR TSAA0529013](https://openairdocs.org/sdr/TSAA0529013.md): Seal · leaking · Mar 8, 2005 · N808AL · Boeing 7372T4 · Hydraulic Handpump, Main
  > NON-ETOPS FLT 104, HNL-KOA: LOST A SYSTEM HYDRAULICS DURING CLIMB-OUT. RETURNED TO HNL. FLAPS WOULD NOT EXTEND TO 15 USING ALTERNATE FLAP SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRAULIC PUMP DUE TO INPUT SHAFT SEAL LEAKING PER AMM 29-11-
- [SDR TSAA0529012](https://openairdocs.org/sdr/TSAA0529012.md): Line · leaking · Mar 7, 2005 · N808AL · Boeing 7372T4 · Hydraulic System, Main
  > LOST A SYSTEM HYDRAULICS ON SHORT FINAL. MAINTENANCE MET THE AIRCRAFT ON THE RUNWAY. MAINTENANCE REPLACED THE NOSE GEAR DOWN ACTUATOR LINE PER AMM 32-3-11. SERVICED HYDRAULIC SYSTEM TO FULL. LEAK CHECK OKAY. REPLACED THE NR 1 AND NR 2 CASE DRAIN FILTERS,
- [SDR TSAA0529008](https://openairdocs.org/sdr/TSAA0529008.md): Line · leaking · Feb 23, 2005 · N808AL · Boeing 7372T4 · Landing Gear Actuator
  > FLT 89, KOA-HNL: A SYSTEM HYDRAULICS FAILED ON SHORT FINAL. LEFT MAIN GEAR LEAKING. FOUND THE LEFT HAND MAIN LANDING GEAR ACTUATOR UP PRESSURE HOSE ASSEMBLY LEAKING. REMOVED AND REPLACED THE HYDRAULIC PRESSURE HOSE ASSEMBLY AND SERVICED THE HYDRAULIC RESERV
- [SDR TSAA0432083](https://openairdocs.org/sdr/TSAA0432083.md): Downlock Sensor · defective · Dec 17, 2004 · N808AL · Boeing 7372T4 · Landing Gear Position and Warning
  > NON-ETOPS FLT. 82, HNL-KOA - DURING DESCENT, LEFT GEAR RED LIGHT WAS ON WITH THE LANDING GEAR HANDLE IN THE DOWN POSITION. FLEW BY TOWER TO VERIFY GEAR DOWN. UNEVENTFUL LANDING AT KOA. VERIFIED LEFT DOWNLOCK SENSOR BAD. REPLACED PROXIMITY SENSOR PER AMM 32
- [SDR TSAA0427065](https://openairdocs.org/sdr/TSAA0427065.md): Indicator · failed · Sep 7, 2004 · N808AL · Boeing 7372T4 · Trailing Flap Position Indicating System
  > NON-ETOPS FLIGHT 110, HNL-OGG: FLAPS DID NOT DEPLOY DURING NORMAL FLAP EXTENSION, USED ALTERNATE MODE TO DEPLOY LEADING EDGE FLAPS. THE TRAILING EDGE FLAPS WERE ASYMMETRICALLY SPLIT AT LESS THAN ONE UNIT. RETURNED TO HNL. REMOVED AND REPLACED THE FLAP POSIT
- [SDR TSAA0456033](https://openairdocs.org/sdr/TSAA0456033.md): Windshield · failed · Mar 15, 2004 · N808AL · Boeing 7372T4 · Flight Compartment Windows
  > CAPTAIN'S NR 1 WINDOW OUTER PANE CRACKED. RETURNED TO HNL. REMOVED AND REPLACED CAPTAIN'S NR 1 WINDOW IAW AMM 56-11-11, PAGES 401-411 AND 580. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0475030](https://openairdocs.org/sdr/TSAA0475030.md): Duct · failed · Feb 20, 2004 · N808AL · Boeing 7372T4 · Engine Bleed Air System
  > FLT 286 - LIH-HNL - PASSING 10,000 FEET ON CLIMB-OUT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. ALL OTHER ENGINE INSTRUMENTS IN GREEN. RETARDED NR 1 ENGINE AND THE LIGHT WENT OUT. REPLACED NR 1 ENGINE FUEL HEAT DUCT DUE TO CRACKED WELD. LEAK CHECK OK, AI
- [SDR TSAA0433024](https://openairdocs.org/sdr/TSAA0433024.md): Battery Pack · inoperative · Jan 16, 2004 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0453003](https://openairdocs.org/sdr/TSAA0453003.md): Skin · cracked · Dec 17, 2003 · N808AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > TRIMMED OUT THE SKIN CRACK. VERIFIED HFEC CUTOUT AND ROTARY PROBE INSPECTION OF LAP SPLICE FASTENER HOLES. FABRICATED AND INSTALLED STRUCTURAL FILLERS, A DOUBLER, AND TEARSTRAP PER FIGURE 48. ALODINED AND PRIMED ALL REPAIR PARTS AND BARE SURFACES. APPLIED
- [SDR TSAA0326199](https://openairdocs.org/sdr/TSAA0326199.md): Fire Detector · failed · Dec 9, 2003 · N808AL · Boeing 7372T4 · Fire Detection
  > APPROXIMATELY 25 MILES FROM HNL, A WHEEL WELL FIRE LIGHT CAME ON. DEFER IAW MEL 26-4, SYSTEM DEACTIVATED IAW MEL. PLACARDS INSTALLED. REMOVED AND REPLACED WHEEL WELL FIRE AND OVERHEAT ELEMENT. OPS CHECK OK. PLACARD REMOVED FROM AIRCRAFT AND LOGBOOK. AIRC
- [SDR TSAA0333204](https://openairdocs.org/sdr/TSAA0333204.md): Battery Pack · discharged · Nov 29, 2003 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333203](https://openairdocs.org/sdr/TSAA0333203.md): Battery Pack · discharged · Nov 29, 2003 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED RIGHT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333202](https://openairdocs.org/sdr/TSAA0333202.md): Battery Pack · discharged · Nov 29, 2003 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED LT OVERWING IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333020](https://openairdocs.org/sdr/TSAA0333020.md): Battery Pack · inoperative · Feb 2, 2003 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333019](https://openairdocs.org/sdr/TSAA0333019.md): Battery Pack · inoperative · Jan 31, 2003 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED FORWARD PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333018](https://openairdocs.org/sdr/TSAA0333018.md): Battery Pack · inoperative · Jan 31, 2003 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED AFT PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0353035](https://openairdocs.org/sdr/TSAA0353035.md): Keelbeam · corroded · Jan 18, 2003 · N808AL · Boeing 7372T4 · Fuselage Main, Frame
  > TRIMMED OUT FUSELAGE SKIN BETWEEN KEEL BEAMS AND AFT OF BS 727. REMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM FROM BS 500 TO BS 727 PLUS 16. VISUALLY AND HFEC INSPECTED TRIMLINE AND AREA UNDER REPAIR FOR SIGNS OF CORROSION AND DISBONDING. FABRICATED AND INS
- [SDR TSAA0353027](https://openairdocs.org/sdr/TSAA0353027.md): Skin · damaged · Jan 18, 2003 · N808AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > REMOVED ALL EXISTING REPAIRS COMMON TO THE LAP JOINT AREAS. ACCOMPLISHED A HFEC OF FASTENERS HOLES TO ASSURE CRACK FREE CONDITION. FABRICATED TWO TAPERED FILLERS, A.032 INCH THICK FILLER AND FOUR.071 INCHE THICK FILLERS, A.032 INCH THICK SPLICE STRAP, A.
- [SDR TSAA0351036](https://openairdocs.org/sdr/TSAA0351036.md): Splice · corroded · Jan 15, 2003 · N808AL · Boeing 7372T4 · Fuselage Miscellaneous Structure
  > TRIMMED WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PERSSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOUR DOUBLER I BEAM TIE STRAPS AND TEE STIFFENERS. ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS
- [SDR TSAA0355034](https://openairdocs.org/sdr/TSAA0355034.md): Fitting · corroded · Jan 15, 2003 · N808AL · Boeing 7372T4 · Horizontal Stabilizer Structure
  > THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LOWER FITTING ASSEMBLY FAIL/SAFE AND LOWER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW SLEEVE BUSHING AND FLANGE BUSHING PER DRAW
- [SDR TSAA0351031](https://openairdocs.org/sdr/TSAA0351031.md): Splice · corroded · Jan 15, 2003 · N808AL · Boeing 7372T4 · Fuselage Miscellaneous Structure
  > TRIMMED LEFT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO LBL 24.5. FABRICATED NEW PRESSURE WEB SECTION AND STEP FILLERS FOR TRANSVERSE I BEAM. FABRICATED FOUR DOUBLER I BEAM TIE STRAPS AND TEE STIFFENERS. ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR P
- [SDR TSAA0351029](https://openairdocs.org/sdr/TSAA0351029.md): Pressure Panel · corroded · Jan 15, 2003 · N808AL · Boeing 7372T4 · Fuselage Main, Bulkhead
  > FABRICATED NEW PRESSURE WEB REPAIR DOUBLER. ALODINED AND PRIMED ALL BARE ALUMINUM. FAY SURFACE SEAL INSTALLED REPAIR DOUBLER WITH BMS 5-95 AND FASTENERS IDENTIFIED. APPLIED CORROSION INHIBITING COMPOUND TO THE INTERNAL SURFACES. REPAIR COMPLETED IAW ECO 33
- [SDR TSAA0351030](https://openairdocs.org/sdr/TSAA0351030.md): Web · corroded · Jan 15, 2003 · N808AL · Boeing 7372T4 · Fuselage Miscellaneous Structure
  > TRIMMED RIGHT WEB SECTION FROM BS 675 TO BS 695 FROM BL 0 TO RBL 70. FABRICATED NEW PRESSURE WEB SECTION, STIFFENERS AND FILLERS. SHOT PEENED, ALODINED AND PRIMED ALL BARE SURFACES AND REPAIR PARTS. INSTALLED REPAIR PARTS PER FIGURE 3. REPAIR COMPLETED IAW
- [SDR TSAA0355032](https://openairdocs.org/sdr/TSAA0355032.md): Fitting · cracked · Jan 15, 2003 · N808AL · Boeing 7372T4 · Horizontal Stabilizer Structure
  > THE LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR ATTACHMENT FITTING CLEVIS LUGS BUSHINGS REMOVED. EDDY CURRENT INSPECTED LUGS FOR CRACKS BEFORE AND AFTER OVERSIZING AND SHOT PEENING. MACHINED, SHOT PEENED, AND FINISHED THE LUG/CLEVIS. INSTALLED BUSHI
- [SDR TSAA0355033](https://openairdocs.org/sdr/TSAA0355033.md): Fitting · corroded · Jan 14, 2003 · N808AL · Boeing 7372T4 · Horizontal Stabilizer Structure
  > THE LEFT HORIZONTAL STABILIZER CENTER CENTER SECTION REAR SPAR UPPER FITTING ASSEMBLY UPPER CLEVIS LUG REQUIRED REWORK BEYOND THE LIMITS PROVIDED IN SB 737-55-1055. REFINISHED THE LUG BORE AND FABRICATED A NEW OVERSIZED BUSHING PER DRAWING. SHOT PEENED, REFI
- [SDR TSAA0353026](https://openairdocs.org/sdr/TSAA0353026.md): Skin · canning · Jan 11, 2003 · N808AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > TRIMMED OUT THE SKIN SNAP DAMAGE AND OIL-CANNING. VISUALLY INSPECTED FOR DISBONDING. FABRICATED AND INSTALLED THREE STRUCTURAL FILLERS, AND DOUBLER AND TEARSTRAP PER FIGURE 1. ALODINED AND PRIMED. APPLIED CORROSION INHIBITING COMPOUND. REPAIR COMPLETED IA
- [SDR TSAA0134180](https://openairdocs.org/sdr/TSAA0134180.md): Gps · failed · Oct 14, 2002 · N808AL · Boeing 7372T4 · Global Positioning System
  > ENROUTE, THE NR 1 AND NR 2 GPS WERE UNABLE TO LOCK ON TO THE SATELLITE SIGNAL. THE AIRCRAFT RETURNED FOR MAINTENANCE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED THE NR 1 AND NR 2 GPS NPU. GROUND OPS CHECKS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR TSAA0233207](https://openairdocs.org/sdr/TSAA0233207.md): Battery Pack · discharged · Oct 11, 2002 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED, OK. AIRCRAFT RETURNED TO SERVICE. (TSAA80003325)
- [SDR TSAA0133168](https://openairdocs.org/sdr/TSAA0133168.md): Battery Pack · discharged · Dec 2, 2001 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133167](https://openairdocs.org/sdr/TSAA0133167.md): Light · inoperative · Nov 30, 2001 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 2 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133166](https://openairdocs.org/sdr/TSAA0133166.md): Battery Pack · inoperative · Nov 29, 2001 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 2001F00721](https://openairdocs.org/sdr/2001F00721.md): Coupler · defective · Nov 16, 2001 · N808AL · Boeing 7372T4 · HF Communications System
  > FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AND THE TRANSMIT WAS INOPERATIVE. RETURNED TO HNL FOR AN OVERWEIGHT LANDING, VERY LOW SINK RATE. REPLACED NR 1 HF TRANSCEIVER (P/N 622337100
- [SDR TSAA0123113](https://openairdocs.org/sdr/TSAA0123113.md): Transceiver · malfunctioned · Nov 16, 2001 · N808AL · Boeing 7372T4 · HF Communications System
  > FLT 351 - HNL-JON - DURING THE VERIFICATION PHASE OF FLIGHT AND CHECKING THE HF RADIO SYSTEM, THE NR 1 HF HAD NO TUNE AND THE TRANSMIT WAS INOPERATIVE. RETURNED TO HNL FOR AN OVERWEIGHT LANDING, VERY LOW SINK RATE. REPLACED NR 1 HF TRANSCEIVER (P/N 622337100
- [SDR TSAA0133142](https://openairdocs.org/sdr/TSAA0133142.md): Battery Pack · discharged · Oct 20, 2001 · N808AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED AFT OVERHEAD PATH EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N808AL-2008-06-16/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 = 'N808AL' AND deregistration_id = 'N808AL-2008-06-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N808AL-2008-06-16/reports

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