# Service difficulty reports: N807AL, cancelled Jul 30, 2008

A list on [N807AL, cancelled Jul 30, 2008](https://openairdocs.org/deregistered/N807AL-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 · 104 reports

- [SDR TSAA0631102](https://openairdocs.org/sdr/TSAA0631102.md): Lever · lack of lube · Nov 18, 2006 · N807AL · Boeing 7372T4 · Drag Control System
  > ON TAKEOFF, THE CREW NOTED THE TAKEOFF CONFIGURATION WARNING ALARM AND PERFORMED A LOW SPEED ABORTED TAKEOFF. CREW RECYCLED THE SPEED BRAKE AND THE ALARM CLEARED. CREW PROCEEDED ON TO LIH WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A TAKEOFF WARNING TES
- [SDR TSAA0663089](https://openairdocs.org/sdr/TSAA0663089.md): Skin Panel · cracked · Oct 18, 2006 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > A.5 INCH CRACK FOUND LT SIDE OF FUSELAGE SKIN AT BS 270 STRINGER 16L. MAINTENANCE REPAIRED WITH APPROXIMATELY 9"X14" EXTERNAL SKIN PTACH FABRICATED DOUBLER AND TRIPPLER PER ECO 3617. FORM 8100 RECEIVED.
- [SDR TSAA0653076](https://openairdocs.org/sdr/TSAA0653076.md): Bulkhead · cracked · Sep 20, 2006 · N807AL · Boeing 7372T4 · Fuselage Main, Bulkhead
  > 3 CRACKED HOLES COMMON TO BS 178 BULKHEAD WEB BETWEEN WL 240 AND WL 230.5
- [SDR TSAA0653068](https://openairdocs.org/sdr/TSAA0653068.md): Door Frame · cracked · Aug 23, 2006 · N807AL · Boeing 7372T4 · Fuselage Main, Structure
  > CRACK NOTED ON FWD CARGO DOOR CUTOUT, AFT LOWER CORNER UNDER DOOR STOP.
- [SDR TSAA0653030](https://openairdocs.org/sdr/TSAA0653030.md): Bulkhead · cracked · Apr 6, 2006 · N807AL · Boeing 7372T4 · Fuselage Main, Bulkhead
  > THREE CRACKS AROUND BS 1016 AFT PRESSURE BULKHEAD GORE WEBS NEAR DOME CAP. WEB SPLICE AND REPAIR DOUBLERS COMPLETED IAW ALOHA'S ECO 3567. HFEC COMPLIED IAW NDT MANUAL PART 5, 51-00-00 FIG 16. FAA FORM 8100-9 RECEIVED.
- [SDR TSAA0653028](https://openairdocs.org/sdr/TSAA0653028.md): Skin · cracked · Apr 4, 2006 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > APPROXIMATE 2 INCH SKIN CRACK AT BS 747 +10 STR 24L. REPAIR COMPLETED IAW SRM 53-30-3 FIG 48. REPAIR SIZE APPROX 15 X 11 INCHES. INSURANCE CUT MADE.040 INCH. DOUBLER.032 2024T3; TRIPLER.050 2024T3. HFEC HOLE LAY-OUT IAW NDT MANUAL 51-00-00 PT 6.
- [SDR TSAA0627026](https://openairdocs.org/sdr/TSAA0627026.md): Indication Sys · malfunctioned · Mar 27, 2006 · N807AL · Boeing 7372T4 · Trailing Flap Position Indicating System
  > ON APPROACH TO KOA, CREW NOTED TRAILING EDGE FLAP INDICATOR SHOWING LEFT SIDE AT 4 DEGREES AND RIGHT SIDE AT 7 DEGREES WITH 5 DEGREES OF FLAPS SELECTED. CREW UNABLE TO EXTEND FLAPS TO 15. CREW DECIDED TO RETURN TO HNL AND DECLARED AN EMERGENCY. WITH ALTERNA
- [SDR TSAA0652004](https://openairdocs.org/sdr/TSAA0652004.md): Skin · cracked · Jan 16, 2006 · N807AL · Boeing 7372T4 · Cargo/Baggage Doors
  > A 4.25 INCH SKIN CRACK ON AFT CARGO DOOR. CRACK LOCATED 18.5 INCHES FROM LOWER FWD CORNER AND 5 INCHES FROM FWD CUTOUT. MAINTENANCE REPAIRED WITH APPROXIMATELY 10 X 7 INCH EXTERNAL SKIN PATCH, FABRICATED DOUBLER (0502024-T3). REPAIR COMPLETED IAW ECO 3550.
- [SDR TSAA0529052](https://openairdocs.org/sdr/TSAA0529052.md): Filter · contaminated · Oct 23, 2005 · N807AL · Boeing 7372T4 · Hydraulic System, Main
  > NON-ETOPS FLIGHT 278 HNL - KOA, AFTER TAKEOFF, NR 1 ENGINE HYDRAULIC SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW DISENGAGED ENGINE DRIVEN HYDRAULIC PUMP AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CHANGED HYDRAULIC SYSTEM A CASE
- [SDR TSAA0529051](https://openairdocs.org/sdr/TSAA0529051.md): Hose · leaking · Oct 23, 2005 · N807AL · Boeing 7372T4 · Hydraulic System, Main
  > NON-ETOPS FLIGHT 88 LIH-HNL - AFTER GEAR UP, HYD PRESSURE INDICATOR SHOWED ZERO. LEFT MAIN LANDING GEAR INDICATOR LIGHTS SHOWED BOTH RED AND GREEN (UNSAFE). WHEN EXTENDING FLAPS AND GEAR, HYD SYSTEM A PRESSURE FLUCTUATED AND A SYSTEM LOW PRESSURE CAUTION LIG
- [SDR TSAA0532032](https://openairdocs.org/sdr/TSAA0532032.md): Circuit Breaker · failed · Jul 27, 2005 · N807AL · Boeing 7372T4 · Landing Gear Retraction/Extension System
  > FLT 71 OGG-HNL, AFTER DEPARTURE, CREW WAS UNABLE TO MOVE LANDING GEAR LEVER TO THE UP POSITION. CREW FOUND CIRCUIT BREAKER POPPED OUT AND THEN RESET IT. GEAR HANDLE WAS THEN MOVED TO THE UP POSITION. THE FLIGHT CONTINUED TO HNL WITHOUT FURTHER INCIDENT. MA
- [SDR TSAA0532028](https://openairdocs.org/sdr/TSAA0532028.md): Landing Gear · malfunctioned · Jul 15, 2005 · N807AL · Boeing 7372T4 · Landing Gear Retraction/Extension System
  > GEAR WOULD NOT RETRACT ON T/O FROM KONA. ISOLATION VALVE LIGHT CAME ON AND GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION. WITH GEAR HANDLE DOWN, WE HAD NO GEAR LIGHTS. VISUALLY CHECKED GEAR DOWN AND LANDED AT KONA. INSPECTED LANDING GEAR SYSTEM AND
- [SDR TSAA0526026](https://openairdocs.org/sdr/TSAA0526026.md): Element · failed · Jun 25, 2005 · N807AL · Boeing 7372T4 · Overheat Detection
  > DURING PUSHBACK AND PRIOR TO ENGINE START, THE CREW NOTED NR 2 ENGINE OVERHEAT INDICATION ILLUMINATED. THE CREW COMPLETED THE ENGINE OVERHEAT AND ENGINE FIRE CHECK LISTS AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AFTER DISCHARGING THE BOTTLES, THE
- [SDR TSAA0526025](https://openairdocs.org/sdr/TSAA0526025.md): Connector · dirty · Jun 19, 2005 · N807AL · Boeing 7372T4 · Fire Protection System Wiring
  > ON CLIMB BETWEEN 11,000 FT AND 13,00 FT, PILOTS REPORTED NR 2 ENGINE OVERHEAT LIGHT FLICKERING AND THEN BECOMING STEADY. THE ENGINE OVERHEAT CHECKLIST WAS COMPLETED AND LIGHT WAS EXTINGUISHED. ENGINE WAS NOT SHUTDOWN, EMERGENCY DECLARED, AND THE AIRCRAFT RET
- [SDR TSAA0425082](https://openairdocs.org/sdr/TSAA0425082.md): Slide · deployed · Dec 17, 2004 · N807AL · Boeing 7372T4 · Escape Slide
  > DURING GROUND MAINTENANCE, GROUND CREW INADVERTENTLY DEPLOYED THE FORWARD SERVICE DOOR ESCAPE SLIDE. NO INJURIES. REMOVED AND REPLACED THE FORWARD SERVICE DOOR SLIDE IN ACCORDANCE WITH MM 25-61-200.
- [SDR TSAA0477063](https://openairdocs.org/sdr/TSAA0477063.md): Transmitter · inoperative · Aug 26, 2004 · N807AL · Boeing 7372T4 · Engine Pressure Ratio (EPR)
  > ON TAKE-OFF ROLL THE NR 1 ENGINE ONLY INDICATED 1.76 EPR; THE THROTTLES WERE ADVANCED WITH NO RESPONSE FROM ANY INSTRUMENTS. REJECTED TAKE-OFF AND RETURNED TO GATE. REPLACED THE NR 1 ENGINE EPR TRANSMITTER AND CLEARED THE PT2 INLET PROBE OF DEBRIS. RAN NR 1
- [SDR TSAA0479046](https://openairdocs.org/sdr/TSAA0479046.md): Bearing · failed · Jun 9, 2004 · N807AL · Boeing 7372T4 · Accessory Gearboxes
  > NON-ETOPS FLIGHT 206, HNL-OGG: ON DESCENT ONTO OGG THE NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, THE OIL PRESSURE DECREASED TOWARD ZERO AND THE OIL QUANTITY BEGAN DROPPING WITH THE OIL TEMPERATURE IN THE NORMAL RANGE. FOLLOWED QRH AND SHUT DOWN THE NR 2 ENGINE.
- [SDR TSAA0453002](https://openairdocs.org/sdr/TSAA0453002.md): Skin · cracked · Dec 24, 2003 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > FOUND AN INCH AND A HALF AND A TWO INCH FUSELAGE CRACK AT BS 767 AND BS 792, ON STRINGER 18L. TRIMMED OUT CRACKS AND VERIFIED CUTOUTS USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED STRUCTURAL AND TAPERED FILLERS, DOUBLER, AND TRIPLER FROM CLAD
- [SDR TSAA0375198](https://openairdocs.org/sdr/TSAA0375198.md): Duct · failed · Dec 10, 2003 · N807AL · Boeing 7372T4 · Engine Bleed Air System
  > FLT 240 - HNL-OGG - ENGINE NR 1 OVERHEAT LIGHT CAME ON JUST AFTER TAKEOFF. PULLED THROTTLE BACK AND THE LIGHT WENT OUT. EGT IN GREEN THE ENTIRE TIME. REMOVED AND REPLACED NR 1 COWL ANTI-ICE UPPER DUCTING. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0329180](https://openairdocs.org/sdr/TSAA0329180.md): Hose · failed · Nov 15, 2003 · N807AL · Boeing 7372T4 · Hydraulic System, Main
  > AFTER GEAR RETRACTION LOST ENTIRE 'A'SYSTEM HYD QTY. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PRESSURE RETURN HOSE ASSEMBLY. (M)
- [SDR TSAA0333126](https://openairdocs.org/sdr/TSAA0333126.md): Battery Pack · inoperative · May 31, 2003 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 4 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0357059](https://openairdocs.org/sdr/TSAA0357059.md): Skin · dented · Apr 4, 2003 · N807AL · Boeing 7372T4 · Leading Edge Devices
  > GAINED ACCESS TO DENTED AREA. CUTOUT DAMAGE BY SLICING THE LEADING EDGE SKIN PER FIGURE 1. INSTALLED A SPLICE REPAIR AT SS205.46 AND SS 238.71. REPAIR COMPLETED IAW SRM 57-50-3, FIGURE 7 AND ECO 3354. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0352053](https://openairdocs.org/sdr/TSAA0352053.md): Guide · misaligned · Mar 18, 2003 · N807AL · Boeing 7372T4 · Service Doors
  > AFTER TAKEOFF, THE CABIN HAD AN EXCESSIVE RATE OF CLIMB, (2,500 FPM). AUTO FAILED ON THE PRESSURIZATION SYSTEM. LANDED HNL WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD SERVICE DOOR WAS IMPROPERLY CLOSED AND LOWER LEFT GUIDE MISALIGNED. MAINTENAN
- [SDR TSAA0251181](https://openairdocs.org/sdr/TSAA0251181.md): Strap · corroded · Aug 19, 2002 · N807AL · Boeing 7372T4 · Fuselage Miscellaneous Structure
  > KEEL BEAM VERTICAL STRAP CORRODED AT BS 532. BLENDED AND FLAP PEENED REPAIR AREA, FABRICATED TWO FILLER STRAPS, INSTALLED FILLERS AND STRAP.
- [SDR TSAA0251178](https://openairdocs.org/sdr/TSAA0251178.md): Stringer · corroded · Aug 16, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON BS 500 AT STRINGER 26R. CUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. FABRICATED REPAIR ANGLES AND DOUBLER IAW SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251180](https://openairdocs.org/sdr/TSAA0251180.md): Stringer · cracked · Aug 15, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Longeron/Stringer
  > CRACK LOCATED AT BS 767, S-14L. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES.
- [SDR TSAA0251177](https://openairdocs.org/sdr/TSAA0251177.md): Skin · cracked · Aug 15, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > SKIN CRACK AT BS 380 BETWEEN STRINGER 28L AND 28R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0251179](https://openairdocs.org/sdr/TSAA0251179.md): Stringer · cracked · Jun 17, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Longeron/Stringer
  > CRACKS BS 739, S-18R AND BS 745, S-19R. REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL USING HFEC METHOD, FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR TSAA0253038](https://openairdocs.org/sdr/TSAA0253038.md): Skin · cracked · Feb 12, 2002 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > REPAIRED 2.5 INCH LONG SKIN CRACK AT FUSELAGE BS 937 STRINGER 26R. CONFIRMED 2.5 INCH REMOVED USING HFEC METHOD. THE REPAIR CONSISTED OF CUTTING OUT THE SKIN CRACK AND FABRICATING A DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133182](https://openairdocs.org/sdr/TSAA0133182.md): Battery Pack · discharged · Dec 24, 2001 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0153149](https://openairdocs.org/sdr/TSAA0153149.md): Skin · cracked · Nov 5, 2001 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE CRACKED AT BS 767, S19L. TRIM OUT CRACK COMPLETED AND VERIFIED CUT OUT USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER. CLEANED AND TREATED ALL EXPOSED SURFACES IAW SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERV
- [SDR TSAA0133145](https://openairdocs.org/sdr/TSAA0133145.md): Battery Pack · discharged · Oct 27, 2001 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133023](https://openairdocs.org/sdr/TSAA0133023.md): Light · inoperative · Mar 1, 2001 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0157009](https://openairdocs.org/sdr/TSAA0157009.md): Spar · corroded · Jan 24, 2001 · N807AL · Boeing 7372T4 · Wing Spar
  > IDENTIFIED CORROSION AT RT WING FRONT SPAR LOWER CHORD FSS 475. REPAIRED CONSISTS OF REMOVING DAMAGED AREA AT HORIZONTAL FLANGE AND INSTALLING A TAPERED FILLER, HFEC COMPLETED ON ALL FASTENER HOLES AND REWORKED AREA. NO DEFECTS NOTED. CLEAN AND TREATED ALL
- [SDR TSAA0053255](https://openairdocs.org/sdr/TSAA0053255.md): Keel · corroded · Dec 27, 2000 · N807AL · Boeing 7372T4 · Fuselage Main, Keel
  > IDENTIFIED CORROSION AT THE VERTICAL LEG OF THE KEEL BEAM AT BS 535 APPROXIMATELY LBL 6.30. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AND TREATED AFFECTED AREA. REPAIR COMPLETED ON 12/26/00, IAW SRM 51-10-6. (M)
- [SDR TSAA0053253](https://openairdocs.org/sdr/TSAA0053253.md): Skin · cracked · Dec 22, 2000 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > IDENTIFIED 3.7 INCH CRACK AT BS 747, STRINGER 18L. CONFIRMED USING HFEC METHOD. (M)
- [SDR TSAA0057142](https://openairdocs.org/sdr/TSAA0057142.md): Beam · gouged · May 22, 2000 · N807AL · Boeing 7372T4 · Wing Miscellaneous Structure
  > REPAIRED LT MLG BEAM AT THE OUTBOARD STABILIZER ATTACH POINT. REPAIR CONSISTS OF BLENDING OUT GOUGE AND REAMING OUT FASTENER HOLES AND INSTALLATIONS OF BUSHINGS IAW ECO 3146. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053141](https://openairdocs.org/sdr/TSAA0053141.md): Skin · cracked · May 18, 2000 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN 3 INCH CRACK AT BS 886 STRINGER 24 IAW SRM 53-30-3 FIG 1. VERIFIED BY HFEC METHOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033117](https://openairdocs.org/sdr/TSAA0033117.md): Battery Pack · inoperative · Apr 12, 2000 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 1 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033116](https://openairdocs.org/sdr/TSAA0033116.md): Light · inoperative · Apr 9, 2000 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 1 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0053098](https://openairdocs.org/sdr/TSAA0053098.md): Skin · cracked · Mar 16, 2000 · N807AL · Boeing 7372T4 · Fuselage Main, Plate/Skin
  > REPAIRED 1.5 INCH CRACK ON FUSELAGE SKIN AT BS 744, STRINGER 19L IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033073](https://openairdocs.org/sdr/TSAA0033073.md): Battery Pack · inoperative · Mar 1, 2000 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED THE AFT SERVICE DOOR EXIT IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033072](https://openairdocs.org/sdr/TSAA0033072.md): Battery Pack · inoperative · Mar 1, 2000 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED THE FORWARD ENTRY EXIT IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA200033061](https://openairdocs.org/sdr/TSAA200033061.md): Battery Pack · inoperative · Feb 12, 2000 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 3 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933499](https://openairdocs.org/sdr/TSAA9933499.md): Battery Pack · inoperative · Dec 7, 1999 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 6 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA9933470](https://openairdocs.org/sdr/TSAA9933470.md): Battery Pack · discharged · Oct 24, 1999 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 2 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933469](https://openairdocs.org/sdr/TSAA9933469.md): Light · inoperative · Oct 24, 1999 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED NR 2 FLOOR LIGHT ASSY DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9972466](https://openairdocs.org/sdr/TSAA9972466.md): Bleed Valve · failed · Oct 20, 1999 · N807AL · Boeing 7372T4 · Compressor Bleed Valve
  > FLT 263 - HNL-LIH - COMPRESSOR STALL NR 2 ENGINE THROTTLE UP OFF OF IDLE. ABORTED TAKEOFF. RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE BLEED CONTROL VALVE. SYSTEM LEAK CHECK AND OPS CHECK GOOD PER MM 75-31-11. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA9933452](https://openairdocs.org/sdr/TSAA9933452.md): Light · inoperative · Oct 8, 1999 · N807AL · Boeing 7372T4 · Emergency Lighting
  > REPLACED FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9953404](https://openairdocs.org/sdr/TSAA9953404.md): Skin · cracked · Aug 16, 1999 · N807AL · Boeing 7372T4 · Aerodynamic Fairings
  > FOUND 4.125 INCH CRACK 2 INCH FORWARD OF BS 947 AT STRINGER 24L. SKIN REPAIR IAW SRM 53-30-3 FIGURE 6 SHEET 4 PAGE 12B. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N807AL-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 = 'N807AL' AND deregistration_id = 'N807AL-2008-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N807AL-2008-07-30/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.