# Service difficulty reports: N816AL, cancelled Jul 9, 2008

A list on [N816AL, cancelled Jul 9, 2008](https://openairdocs.org/deregistered/N816AL-2008-07-09.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 · 147 reports

- [SDR TSAA0753059](https://openairdocs.org/sdr/TSAA0753059.md): Skin · cracked · Oct 28, 2007 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > IN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED LT SKIN CRACKED INSIDE LT WING TO BODY FAIRING. CRACK LOCATED AT BS 747 +19 BETWEEN STRINGER 21L AND 22L. CRACK APPROXIMATELY 1.5 INCHES LONG. CRACK WAS REPAIRED IN ACCORDANCE WITH ECO 3684.
- [SDR TSAA0753058](https://openairdocs.org/sdr/TSAA0753058.md): Skin · cracked · Oct 28, 2007 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > IN THE PROCESS OF SSIP, NDT INSPECTION DISCOVERED RT SKIN CRACKED IS BETWEEN LAP JOINT AND LARGE EXISTING REPAIR. CRACK LOCATED AT BS 927 +13 BETWEEN STRINGER 20R AND 21R. CRACK APPROXIMATELY 3.5 INCHES LONG. 11/11/07 - CRACK WAS REPAIRED IN ACCORDANCE WIT
- [SDR TSAA0734041](https://openairdocs.org/sdr/TSAA0734041.md): Hsi · failed · Jul 18, 2007 · N816AL · Boeing 7372X6C · Directional Gyro and Indicating System
  > CARGO FLIGHT 944 HNL-KOA - DURING CLIMB, THE CAPTAIN NOTED THE NR 1 HORIZONTAL SITUATION INDICATOR HAD THE COMPASS FLAG IN VIEW. THE CAPTAIN ATTEMPTED TO TRANSFER THE COMPASS INDICATION TO BOTH ON NR 2 BUT THE FLAG REMAINED IN VIEW. THE CREW RETURNED TO HNL
- [SDR TSAA0752039](https://openairdocs.org/sdr/TSAA0752039.md): Proximity Sensor · dirty · Jun 29, 2007 · N816AL · Boeing 7372X6C · Door Warning System
  > FLIGHT 940 HNL-KOA - ON TAKEOFF ROLL, CREW NOTED THE DOOR ANNUNCIATOR LIGHT ILLUMINATED AND ABORTED THE TAKEOFF AT 110 KNOTS INDICATED AIRSPEED. CREW RETURNED TO THE CARGO RAMP WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AND OPS CHECKED THE FORWARD ENTRY D
- [SDR TSAA0652092](https://openairdocs.org/sdr/TSAA0652092.md): Pitot Tube · obstructed · Oct 29, 2006 · N816AL · Boeing 7372X6C · Pitot/Static System
  > FLIGHT 940 HNL-KOA. AFTER TAKEOFF, CREW NOTED THE LOSS OF FIRST OFFICER'S AIRSPEED INDICATION AND THE ILLUMINATION OF THE DOOR ANNUNCIATOR LIGHT. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED DEBRIS FROM THE FIRST OFFICER'S PITOT TUBE A
- [SDR TSAA0649012](https://openairdocs.org/sdr/TSAA0649012.md): Speed Switch · failed · Feb 11, 2006 · N816AL · Boeing 7372X6C · APU Core Engine
  > FLIGHT 922 HNL OGG- APU OVER-SPEED INDICATION ILLUMINATED AND THE APU AUTO SHUT-DOWN. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 3- SPEED SWITCH; OPS CHECKED NORMAL AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR TSAA0527019](https://openairdocs.org/sdr/TSAA0527019.md): Sensor · failed · Apr 20, 2005 · N816AL · Boeing 7372X6C · Stall Warning System
  > NON-ETOPS CARGO FLIGHT 913, HNL-LIH: AFTER TAKEOFF, THE STICK-SHAKER ENGAGED AND REMAINED ON UNTIL LANDING. RETURNED TO HNL. REMOVED AND REPLACED AOA SENSOR VANE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0471076](https://openairdocs.org/sdr/TSAA0471076.md): Line · obstructed · Nov 11, 2004 · N816AL · Boeing 7372X6C · Engine Controls
  > FLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS FROM THE PT2 SENSE TUBE BETWEEN THE ENGINE AND TRANSDUCER. ENGINE RUN-UP AND EPR CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0429054](https://openairdocs.org/sdr/TSAA0429054.md): Pump · failed · Jul 16, 2004 · N816AL · Boeing 7372X6C · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC SYSTEM FAILED. TURNED TO HNL. REMOVE AND REPLACE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-32. LEAK AND OPS CHECK GOOD. REMOVE AND REPLACE NR 1 AND NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTERS. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0352107](https://openairdocs.org/sdr/TSAA0352107.md): Skin · corroded · Apr 27, 2003 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > REMOVED DAMAGED AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR DOUBLER FROM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED DOUBLER PER FIGURE 1. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3360. (M)
- [SDR TSAA0352106](https://openairdocs.org/sdr/TSAA0352106.md): Door Frame · cracked · Apr 27, 2003 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > REMOVED DAMAGED INBOARD DORR FRAME AREA, VERIFIED CRACK FREE USING HFEC. FABRICATED AN ANGLE DOUBLER FROM.063 INCH 2024-T3 CLAD MATERIAL. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED ANGLED DOUBLER PER FIGURE B. VERIFIED 8110-3 RECEIVED. REPAIR COMPL
- [SDR TSAA0233256](https://openairdocs.org/sdr/TSAA0233256.md): Battery Pack · inoperative · Dec 20, 2002 · N816AL · Boeing 7372X6C · Emergency Lighting
  > REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0233219](https://openairdocs.org/sdr/TSAA0233219.md): Battery Pack · discharged · Oct 29, 2002 · N816AL · Boeing 7372X6C · Emergency Lighting
  > REPLACED NR 3 AND NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0234226](https://openairdocs.org/sdr/TSAA0234226.md): Indicator · faulty · Oct 22, 2002 · N816AL · Boeing 7372X6C · Weather Radar System
  > PRIOR TO TAXI, THE CREW NOTICED A STRONG SMELL OF ELECTRIC FUMES FOLLOWED BY SMOKE IN COCKPIT. THE AIRCRAFT WAS SECURED FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE RADAR TRANSCEIVER AND RADAR INDICATOR. OPERATIONAL CHECK OF THE RADAR SYSTEM WAS GO
- [SDR TSAA0277212](https://openairdocs.org/sdr/TSAA0277212.md): Line · contaminated · Oct 17, 2002 · N816AL · Boeing 7372X6C · Engine Pressure Ratio (EPR)
  > ON TAKEOFF, THE NR 2 ENGINE WAS AT W.01 EPR, N1-80 PERCENT, EGT-400 DEGREES C, N2-82 PERCENT WITH FUEL FLOW AT 4000 LBS. THE AIRCRAFT RETURNED AND LANDED, WITH NOT FURTHER INCIDENT. MAINTENANCE REMOVED DEBRIS (BUGS) FROM THE NOSE DOME AND CLEARED THE LINES F
- [SDR TSAA0229193](https://openairdocs.org/sdr/TSAA0229193.md): Relief Valve · dirty · Oct 14, 2002 · N816AL · Boeing 7372X6C · Cabin Pressure Control System
  > AT THE TOP OF CLIMB WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE THE NR 2 ENGINE MADE A LOUD BANG LIKE A COMPRESSOR STALL. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. REPLACED THE SAFETY RELIEF VALVE. GROUND OPS CHECKED WERE GOOD. AIR
- [SDR TSAA0275194](https://openairdocs.org/sdr/TSAA0275194.md): Bleed Valve · malfunctioned · Sep 5, 2002 · N816AL · Boeing 7372X6C · Compressor Bleed Valve
  > THE NR 2 ENGINE COMPRESSOR STALLED WHEN THE THRUST LEVERS WERE BROUGHT BACK TO IDLE AT TOP OF DECENT. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE PRESSURE RATIO BLEED CONTROL VALVE (PRBC). GROUND OPERATIONAL CHECKS
- [SDR TSAA0233135](https://openairdocs.org/sdr/TSAA0233135.md): Battery Pack · discharged · May 13, 2002 · N816AL · Boeing 7372X6C · Emergency Lighting
  > REPLACED LEFT OVERWING IDENT EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0233118](https://openairdocs.org/sdr/TSAA0233118.md): Battery Pack · discharged · Apr 18, 2002 · N816AL · Boeing 7372X6C · Emergency Lighting
  > REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0252092](https://openairdocs.org/sdr/TSAA0252092.md): Guide · out of adjust · Mar 27, 2002 · N816AL · Boeing 7372X6C · Passenger/Crew Doors
  > FLT 46 - HNL-ITO - FORWARD ENTRY DOOR LIGHT CAME ON DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUSTED THE ROLLER GUIDE SERRATED PLATES AND GUIDE ARM. OPERATIONAL CHECKS WERE
- [SDR TSAA0251083](https://openairdocs.org/sdr/TSAA0251083.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 26 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTE
- [SDR TSAA0251066](https://openairdocs.org/sdr/TSAA0251066.md): Bulkhead · corroded · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Bulkhead
  > REMOVED CORROSION AT 1016 SKIN BULKHEAD AND ATTACHING FRAME AFT SIDE OF BULKHEAD BETWEEN LBL 5 TO RBL 5 IAW SRM 53-10-1 FIGURE 1 DETAIL 16. CUT OUT ACCESS HOLE AFT OF BULKHEAD PER DRAWING 65C28106. DOUBLER AND FILLER COMPLETED IAW DRAWING 65C28106. CUT OUT
- [SDR TSAA0251075](https://openairdocs.org/sdr/TSAA0251075.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 10 RT AT BS 500B PLUS 10 UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS A
- [SDR TSAA0251076](https://openairdocs.org/sdr/TSAA0251076.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10, BS 4200 PLUS 10 AND BS 500 PLUS 10 ON WINDOW NR 1 RIGHT LOWER AFT CORNER. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED
- [SDR TSAA0251077](https://openairdocs.org/sdr/TSAA0251077.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 1 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRI
- [SDR TSAA0251078](https://openairdocs.org/sdr/TSAA0251078.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 2 RIGHT UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FIL
- [SDR TSAA0251079](https://openairdocs.org/sdr/TSAA0251079.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S14L BS 727 PLUS 10 ON WINDOW NR 20 LEFT LOWER FORWARD HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, Q
- [SDR TSAA0251080](https://openairdocs.org/sdr/TSAA0251080.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10L BS 827 PLUS 10 ON WINDOW NR 24 LEFT UPPER AFT HOLES NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILL
- [SDR TSAA0251081](https://openairdocs.org/sdr/TSAA0251081.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 25 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS.
- [SDR TSAA0251082](https://openairdocs.org/sdr/TSAA0251082.md): Skin · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/Skin
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R AND S14R ON WINDOW NR 24 RT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, DOUBLER AND T
- [SDR TSAA0251067](https://openairdocs.org/sdr/TSAA0251067.md): Floorbeam · corroded · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Floor Beam
  > FOUND CORROSION ON THE EXISTING UPPER FLANGE FLOORBEAM REPAIR AT STATION 1016, WL 208 BBI 0 TO LBL 15. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251069](https://openairdocs.org/sdr/TSAA0251069.md): Keelbeam · corroded · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Keel
  > FOUND CORROSION ON THE KEEL BEAM ON RIGHT LOWER FLANGE IN RIGHT AC BAY AT STATION 557 TO STATION 567, STATION 584 AND STATION 608. BLENDOUT THE CORROSION THEN FLAT PEENED IAW SOPM CHAPTER 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0255063](https://openairdocs.org/sdr/TSAA0255063.md): Spar · corroded · Feb 26, 2002 · N816AL · Boeing 7372X6C · Vertical Stabilizer, Spar/Rib
  > FOUND CORROSION ON LEFT REAR SPAR CHORD 6 INCHES UP FROM VERTICAL STABILIZER ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0255064](https://openairdocs.org/sdr/TSAA0255064.md): Spar · corroded · Feb 26, 2002 · N816AL · Boeing 7372X6C · Vertical Stabilizer, Spar/Rib
  > FOUND CORROSION ON LEFT REAR SPAR CHORD 46 INCHES UP FROM VERTICAL STABILIZER FIN BETWEEN STATION 99.5 AND 108.7 ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251074](https://openairdocs.org/sdr/TSAA0251074.md): Floor Support · corroded · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Miscellaneous Structure
  > IDENTIFIED CORROSION ON FLOOR SUPPORT DIAGONAL LEFT BETWEEN STATION 1006 AND STATION 1016 LBL 5. REMOVED CORROSION IAW SRM 53-10-1 DETAIL I, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251068](https://openairdocs.org/sdr/TSAA0251068.md): Keelbeam · corroded · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Keel
  > FOUND CORROSION ON THE KEEL BEAM LOWER CHORD. CONFIRMED CORROSION REMOVED AND NO EVIDENCE OF CRACKS USING HFEC METHOD. REPAIR COMPLETED IAW ECO 3269. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0251084](https://openairdocs.org/sdr/TSAA0251084.md): Window Frame · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R ON WINDOW NR 26 RIGHT LOWER FORWARD HOLE NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREA. FABRIC
- [SDR TSAA0251085](https://openairdocs.org/sdr/TSAA0251085.md): Window Frame · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R AND S14R ON WINDOW NR 26 RIGHT UPPER AFT HOLES NR 9 AND NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMM
- [SDR TSAA0251086](https://openairdocs.org/sdr/TSAA0251086.md): Window Frame · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R BS 867 PLUS 10 ON WINDOW NR 29 RIGHT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AR
- [SDR TSAA0251087](https://openairdocs.org/sdr/TSAA0251087.md): Window Frame · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > PEFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S-14R BS 420 ONWINDOW NR 4 RIGHT LOWER AFT CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS.
- [SDR TSAA0251088](https://openairdocs.org/sdr/TSAA0251088.md): Window Frame · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 5 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICAT
- [SDR TSAA0251089](https://openairdocs.org/sdr/TSAA0251089.md): Window Frame · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 6 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICAT
- [SDR TSAA0251090](https://openairdocs.org/sdr/TSAA0251090.md): Window Frame · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Structure
  > PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATION ON WINDOW NR 8 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO.40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS.
- [SDR TSAA0251091](https://openairdocs.org/sdr/TSAA0251091.md): Stringer · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > FOUND CRACKES ON STRINGER 6L AND 7L FORWARD LAV SIDEWALL AREA. TRIMMED OUT DAMAGED PORTIONS OF INTERCOSTAL IAW SRM 51-40-3 FIGURE 1. VERIFIED NO FURTHER CRACKS USING HFEC METHODS AROUND THE TRIMMED OUT AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-
- [SDR TSAA0251094](https://openairdocs.org/sdr/TSAA0251094.md): Rib · cracked · Feb 26, 2002 · N816AL · Boeing 7372X6C · Horizontal Stabilizer, Spar/Rib
  > FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CRACKS ON VARIOUS SUPPORT RIBS LISTED FROM INBOARD TO OUTBOARD NR 2, 3, 4, 5, 6, 7, AND 8. CUT AND REMOVED PORTIONS OF FORMED SECTIONS. FABRICATED REPAIR PARTS FROM.040 AND.050 INCH THICK 2024 T3. ASSEMBL
- [SDR TSAA0251095](https://openairdocs.org/sdr/TSAA0251095.md): Stringer · damaged · Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Longeron/Stringer
  > DAMAGED STRINGER BETWEEN FS 1040 AND FS 1064 STRINGER 27L. REMOVED DAMAGED SECTION IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR DOUBLER USING.040 INCH THICK 2024 T3 IAW SRM 51-20-1 PAGES 10A TO 22. PROTECTED MATERIAL USING AN IRIDITE SOLUTION APPLICATION IA
- [SDR TSAA0133170](https://openairdocs.org/sdr/TSAA0133170.md): Battery Pack · discharged · Dec 1, 2001 · N816AL · Boeing 7372X6C · Emergency Lighting
  > REPLACED AFT ENTRY EMERGENCY IDENT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0124097](https://openairdocs.org/sdr/TSAA0124097.md): Circuit Breaker · Jul 27, 2001 · N816AL · Boeing 7372X6C · Electrical Power System
  > FLT 242 - LIH-OGG - THE CREW NOTICED A STRONG ELECTRICAL SMELL COMING FROM THE CENTER OF THE CABIN DURING DESCENT. SMELL DISSIPATED AFTER LANDING. MAUI MAINTENANCE PERSONNEL INSPECTED AND RELEASED THE AIRCRAFT WHEN NO EVIDENCE OF ELECTRICAL FUMES OR ORIGIN C
- [SDR TSAA0133093](https://openairdocs.org/sdr/TSAA0133093.md): Battery Pack · inoperative · Jul 25, 2001 · N816AL · Boeing 7372X6C · Lighting System
  > REPLACED AFT SERVICE DOOR IDENT POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0133081](https://openairdocs.org/sdr/TSAA0133081.md): Battery Pack · inoperative · Jul 7, 2001 · N816AL · Boeing 7372X6C · Lighting System
  > REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N816AL-2008-07-09/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 = 'N816AL' AND deregistration_id = 'N816AL-2008-07-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N816AL-2008-07-09/reports

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