# Service difficulty reports: N827AL, cancelled Sep 28, 2006

A list on [N827AL, cancelled Sep 28, 2006](https://openairdocs.org/deregistered/N827AL-2006-09-28.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 · 60 reports

- [SDR TSAA0653009](https://openairdocs.org/sdr/TSAA0653009.md): Skin · cracked · Feb 7, 2006 · N827AL · Boeing 737209 · Fuselage Main, Plate/Skin
  > 2 INCH CRACK AT BS 887 + 2 BETWEEN STR 24R AND 25R. CRACK CUT OUT +.40 OVER CUT. HFEC FINAL LAY OUT HOLES IAW NDT MANUAL 53-00-00 PART 6. REPAIRED COMPLETED IAW SRM 53-30-3 FIG 48. REPAIR: APPROX SIZE = 20" BY 22" FABRICATED TRIPLER. MATERIAL; DOUBLER
- [SDR TSAA0523044](https://openairdocs.org/sdr/TSAA0523044.md): Skin · lightning strike · Sep 23, 2005 · N827AL · Boeing 737209 · Fuselage Main, Plate/Skin
  > FLIGHT 270 (HNL-KOA) LIGHTNING STRIKE DURING CLIMB-OUT AT 10,000’. NO MALFUNCTIONS. MTX ACTION COMPLIED WITH M-118 LIGHTNING STRIKE INSPECTION. REMOVED AND REPLACED DAMAGED RIVETS ON STATION 188R AND STATIC WICK.
- [SDR TSAA0526005](https://openairdocs.org/sdr/TSAA0526005.md): Connector · defective · Feb 11, 2005 · N827AL · Boeing 737209 · Fire Protection System Wiring
  > FLT 71, HNL-OGG - THE NR 2 ENGINE FIRE WARNING LIGHT CAME ON INTERMITTENTLY DURING FLIGHT. DECIDED TO RETURN TO HNL. THE NR 2 ENGINE FIRE WARNING LIGHT CAME ON STEADY AT TOUCHDOWN. ENGINE SHUTDOWN. BOTTLE DISCHARGED. REPLACED THE NR 2 ENGINE FIRE DETECTOR
- [SDR TSAA04790620](https://openairdocs.org/sdr/TSAA04790620.md): Bypass Switch · failed · Aug 22, 2004 · N827AL · Boeing 737209 · Turbine Engine Oil System
  > NON-ETOPS FLIGHT 67, OGG-HNL: NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. SHUT-DOWN NR 1 ENGINE IAW QRH. REPLACED NR 1 ENGINE OIL FILTER BYPASS SWITCH IAW AMM 79-35-11. OPS/LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0456058](https://openairdocs.org/sdr/TSAA0456058.md): Windshield · failed · Jul 27, 2004 · N827AL · Boeing 737209 · Flight Compartment Windows
  > NON-ETOPS FLIGHT 46, HNL-ITO: OUTER PANE OF WINDOW R1 CRACKED. RETURN TO HNL. REMOVE AND REPLACE WINDOW R1 IAW AMM 56-11-11. AIRCRAFT RETURNED TO SERVICE.
- [SDR TSAA0433027](https://openairdocs.org/sdr/TSAA0433027.md): Battery Pack · inoperative · Feb 9, 2004 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED FORWARD SERVICE DOOR IDENT EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0453028](https://openairdocs.org/sdr/TSAA0453028.md): Skin · cracked · Feb 2, 2004 · N827AL · Boeing 737209 · Fuselage Main, Plate/Skin
  > TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW ECO 2840R2, DEVIATION C. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0233261](https://openairdocs.org/sdr/TSAA0233261.md): Battery Pack · inoperative · Dec 21, 2003 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 1 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333115](https://openairdocs.org/sdr/TSAA0333115.md): Battery Pack · discharged · May 11, 2003 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED AFT ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0357064](https://openairdocs.org/sdr/TSAA0357064.md): Flange · corroded · Apr 10, 2003 · N827AL · Boeing 737209 · Wing Miscellaneous Structure
  > REMOVED CORROSION DAMAGE BY SMOOTHLY BLENDING REWORK AREA. PERFORMED HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAT PEENED REWORKED SURFACE. FABRICATED A FILLER FROM 2024-T3 SIZED TO FIT BLENDOUT AREA AND RESTORE TO ORIGINAL CONTOUR. APPLIED ALOD
- [SDR TSAA0357061](https://openairdocs.org/sdr/TSAA0357061.md): Access Door · corroded · Apr 10, 2003 · N827AL · Boeing 737209 · Wing, Plate/Skin
  > REMOVED CORROSION DAMAGE BY BLENDOUT REPAIR PER GUIDANCE IN SRM 57-30-3, FIGURE 5, DETAL III. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II TO BLENDOUT LOCATIONS. FILLED DEPRESSION WITH BMS 5-26, TYPE II SEALANT TO RESTORE SURFACE TO ORGINAL CONTOUR.
- [SDR TSAA0357062](https://openairdocs.org/sdr/TSAA0357062.md): Leg Assy · corroded · Apr 10, 2003 · N827AL · Boeing 737209 · Wing Miscellaneous Structure
  > CUTOUT THE DAMAGED FROM THE VERTICAL LEG. BLENDED OUT REMAINING AREA OF THE CHORD MAINTAINING A GREATER THAN.050 INCH THICKNESS. PERFORMED 10X VISUAL AND HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAP PEENED REWORKED SURFACES. FABRICATED REPAIR
- [SDR TSAA0357063](https://openairdocs.org/sdr/TSAA0357063.md): Leg Assy · corroded · Apr 10, 2003 · N827AL · Boeing 737209 · Wing Miscellaneous Structure
  > REMOVED CORROSION DAMAGE BY BLENDING TO A 20 TO 1 RATION. PERFORMED 10X VISUAL AND HFEC INSPECTON TO VERIFY CRACK AND CORROSION FREE. FABRICATED A TAPERED SHIM FROM 2024-T3. FLAT PEENED SURFACE. APPLIED ALODINE AND TWO COATS OF BMS 10-11, TYPE I PRIMER TO B
- [SDR TSAA0253238](https://openairdocs.org/sdr/TSAA0253238.md): Spar · corroded · Nov 7, 2002 · N827AL · Boeing 737209 · Wing Spar
  > FOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD VERTICAL WEB SURFACE AT WSL 554. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH HFEC INSPECTION. FABRICATED TAPERED FILLERS TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR DOUBLER AND REPAIR ANGLE. INSTALLED TH
- [SDR TSAA0253239](https://openairdocs.org/sdr/TSAA0253239.md): Spar · corroded · Nov 7, 2002 · N827AL · Boeing 737209 · Wing Spar
  > FOUND CORROSION ON RIGHT FRONT SPAR LOWER CHORD SURFACE AT WSL 557. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH HFEC INSPECTION. FABRICATED A REPAIR FILLER TO FIT IN THE BLENDOUT AREA. FABRICATED A REPAIR STRAP. REPAIR COMPLETED IAW ECO. AIRCRAFT RETURNE
- [SDR TSA2002F00001](https://openairdocs.org/sdr/TSA2002F00001.md): Bearing · broken · Jun 11, 2002 · N827AL · Boeing 737209 · Turbine Engine Oil System
  > CLIMBING THROUGH 15,000 FEET THE NUMBER 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI AND OIL TEMPERATURE CLIMBED TO 130 DEGREES. THE NUMBER 2 ENGINE WAS SHUTDOWN IAW THE QRH. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 2 ACCE
- [SDR TSAA0251056](https://openairdocs.org/sdr/TSAA0251056.md): Spar · corroded · Feb 21, 2002 · N827AL · Boeing 737209 · Horizontal Stabilizer, Spar/Rib
  > DURING HEAVY CHECK, FOUND CORROSION ON HORIZONTAL STABILIZER REAR SPAR UPPER CHORD. THE CORROSION WAS TRIMMED OUT PER SRM AND VERIFIED REMOVED USING HFEC METHOD. FABRICATED A EXTERNAL DOUBLER AND REPAIR FILLER TO FIT SKIN CUTOUT. FABRICATED REPAIR ANGLE AND
- [SDR TSAA0251057](https://openairdocs.org/sdr/TSAA0251057.md): Keelbeam · corroded · Feb 21, 2002 · N827AL · Boeing 737209 · Fuselage Main, Keel
  > DURING HEAVY CHECK, FOUND CORROSION ON LEFT KEEL BEAM LOWER CHORD AT BS 727 STRINGER 27L. THE CORROSION WAS TRIMMED OUT PER SRM. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR PARTS USING SRM 51-30-2. VERIFIED APPROVAL RECEIVED AND COMPLETED REPAIR IAW EC
- [SDR TSAA0253042](https://openairdocs.org/sdr/TSAA0253042.md): Skin · corroded · Feb 9, 2002 · N827AL · Boeing 737209 · Wing, Plate/Skin
  > FOUND CORROSION ON LOWER SKIN SURFACE AT WS 435.5, WS 542, WS 567, WS 514.5, AND WS 461. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH A 10X VISUAL INSPECTION. EVALUATED REMAINING WING SKIN THICKNESS AND FILLED DEPRESSIONS WITH BMS 5-95 SEALANT REFERRING TO S
- [SDR TSAA0253043](https://openairdocs.org/sdr/TSAA0253043.md): Keelbeam · corroded · Feb 9, 2002 · N827AL · Boeing 737209 · Fuselage Main, Keel
  > FOUND CORROSION ON LOWER KEEL BEAM SURFACE AT BS 727. CUT OUT SKIN AREA AS REQUIRED TO ACCESS KEEL BEAM LOWER SURFACE. BLENDOUT KEEL BEAM LOWER CHORD SURFACE CORROSION. FABRICATED A FILLER FROM.71 TO.12 INCH 2024-T3. FABRICATED TWO DOUBLERS FROM.063 AND
- [SDR TSAA0253020](https://openairdocs.org/sdr/TSAA0253020.md): Skin · cracked · Jan 7, 2002 · N827AL · Boeing 737209 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE CRACK AT BS 940 S-21R. TRIMMED OUT DAMAGE AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED, INSTALLED FILLER AND DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0129152](https://openairdocs.org/sdr/TSAA0129152.md): Hydraulic Line · leaking · Nov 13, 2001 · N827AL · Boeing 737209 · Hydraulic System, Main
  > FLT 62, HNL-OGG, THE HYDRAULIC ANNUNCIATOR CAME ON AFTER TAKEOFF. BOTH 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED. THE 'A' SYSTEM QUANTITY READ '0'. DECLARED EMERGENCY AND RETURNED TO HNL FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT LANDING GEAR
- [SDR TSAA0130036](https://openairdocs.org/sdr/TSAA0130036.md): Harness · burned · Sep 5, 2001 · N827AL · Boeing 737209 · Windshield/Door Rain/Ice Removal
  > FLT - 41 - ITO-HNL - INBOUND FROM HILO, HAD STRONG ELECTRICAL SMOKE SMELL IN COCKPIT AND SOME SMOKE SMELL IN CABIN AROUND ROW 5. DECLARED EMERGENCY. LANDED SAFELY IN HNL. FOUND WINDOW HARNESS AT THE RIGHT SIDE WINDOW BURNED AT THE QUICK DISCONNECT. WINDOW
- [SDR TSAA0152111](https://openairdocs.org/sdr/TSAA0152111.md): Door Frame · cracked · Aug 16, 2001 · N827AL · Boeing 737209 · Fuselage Main, Structure
  > DURING HEAVY CHECK INSPECTION FOUND A CRACK ON THE AFT LOWER CARGO DOORWAY FRAME. THE CRACK EXTENDS FROM A FASTENER HOLE DOWN INTO A FRAME FLANGE. THE REPAIR INVOLVED TRIMMING OUT THE DAMAGE, PERFORMING A HFEC INSPECTION TO ENSURE THE CRACK AND ANY CORROSION
- [SDR TSAA0153098](https://openairdocs.org/sdr/TSAA0153098.md): Skin · cracked · Jul 27, 2001 · N827AL · Boeing 737209 · Fuselage Structure (General)
  > IDENTIFIED 1.25 INCH SKIN CRACK AT FORWARD SERVICE DOOR LOWER AFT SECTION. (M)
- [SDR TSAA0157068](https://openairdocs.org/sdr/TSAA0157068.md): Skin · corroded · Jun 1, 2001 · N827AL · Boeing 737209 · Wing, Plate/Skin
  > DISCOVERED CORROSION AT RIGHT WING LOWER SURFACE WS 581.5, BLENDOUT TO REMOVE ALL CORROSION, OBTAINED A SURFACE OF 125 MICROINCHES RADIUS, CONFIRMED COMPLETE REMOVAL OF CORROSION BY 10 BY GLASS VISUAL INSPECTION, FLAP PEEN REWORKED AREAS PER SOPM 20-10-03, APP
- [SDR TSAA0157066](https://openairdocs.org/sdr/TSAA0157066.md): Skin · corroded · Jun 1, 2001 · N827AL · Boeing 737209 · Wing, Plate/Skin
  > DISCOVERED CORROSION AT RIGHT WING LOWER SURFACE WS 581.5, BLENDOUT TO REMOVE ALL CORROSION, OBTAINED A SURFACE OF 125 MICROINCHES RADIUS, CONFIRMED COMPLETE REMOVAL OF CORROSION BY 10 BY GLASS VISUAL INSPECTION, FLAP PEEN REWORKED AREAS PER SOPM 20-10-03, APP
- [SDR TSAA0157101](https://openairdocs.org/sdr/TSAA0157101.md): Skin · corroded · Oct 3, 2000 · N827AL · Boeing 737209 · Wing, Plate/Skin
  > CORROSION FOUND ON LOWER SKIN SURFACE AT WS 435.5, WS 567, WS 542, WS 514.5, AND WS 461. CONFIRMED COMPLETE REMOVAL OF CORROSION WITH A 10X VISUAL INSPECTION. EVALUATED REMAINING WING SKIN THICKNESS AND FILLED DEPRESSIONS WITH BMS 5-95 SEALANT REFERRING TO S
- [SDR TSAA0033207](https://openairdocs.org/sdr/TSAA0033207.md): Battery Pack · inoperative · Sep 6, 2000 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0032165](https://openairdocs.org/sdr/TSAA0032165.md): Tire · failed · Jul 7, 2000 · N827AL · Boeing 737209 · Tire
  > FLT 66 - HNL-OGG - ON TAKEOFF, REPORTED TIRE BLOWN ON MLG. DECLARED EMERGENCY. RETURNED TO HNL WITHOUT FURTHER INCIDENT. FOUND NR 4 MLG TIRE RECAP SEPARATED. REMOVED AND REPLACED THE NR 4 MAIN WHEEL ASSY IAW FORM M-139. INSTALLATION, SPIN AND SECURITY CHE
- [SDR TSAA0079138](https://openairdocs.org/sdr/TSAA0079138.md): Pressure Switch · failed · May 18, 2000 · N827AL · Boeing 737209 · Engine Oil Pressure
  > FLT 224 - HNL-OGG - NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT APPROXIMATELY 70 KNOTS. TAKEOFF ABORTED. ALL OTHER ENGINE PARAMETERS WERE NORMAL. ALL QRH PROCEDURES REVIEWED. RETURNED TO HNL RAMP. REMOVED AND REPLACED NR 1 ENGINE OIL BYPASS SWITCH.
- [SDR TSAA200052034](https://openairdocs.org/sdr/TSAA200052034.md): Stop · out of adjust · Jan 26, 2000 · N827AL · Boeing 737209 · Passenger/Crew Doors
  > HNL/OGG - FLT 264 - FORWARD DOOR ENTRY WARNING LIGHT ILLUMINATED MOMENTARILY AFTER TAKEOFF. PRESSURIZATION REMAINED NORMAL. ABORTED TAKEOFF. CHECKED DOOR LEVER AND WARNING EXTINGUISHED. ALL OTHER INDICATIONS WERE NORMAL. AIRCRAFT TAXIED BACK FOR DEPARTURE
- [SDR TSAA0033081](https://openairdocs.org/sdr/TSAA0033081.md): Battery Pack · inoperative · Jan 21, 2000 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED POWER PACKS IN FORWARD AND AFT INTERVALVE CONTROL MODULES DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0033082](https://openairdocs.org/sdr/TSAA0033082.md): Battery Pack · inoperative · Jan 21, 2000 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 1 AND NR 5 POSITION BATTERY PACK IN FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933450](https://openairdocs.org/sdr/TSAA9933450.md): Battery Pack · discharged · Oct 5, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9922442](https://openairdocs.org/sdr/TSAA9922442.md): Battery Pack · discharged · Sep 22, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933433](https://openairdocs.org/sdr/TSAA9933433.md): Battery Pack · discharged · Sep 12, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933432](https://openairdocs.org/sdr/TSAA9933432.md): Light · inoperative · Sep 10, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 5 FLOOR EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933420](https://openairdocs.org/sdr/TSAA9933420.md): Battery Pack · discharged · Aug 27, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933400](https://openairdocs.org/sdr/TSAA9933400.md): Light · inoperative · Aug 19, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 2 EMERGENCY FLOOR LIGH TASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933399](https://openairdocs.org/sdr/TSAA9933399.md): Light · inoperative · Aug 19, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933398](https://openairdocs.org/sdr/TSAA9933398.md): Battery Pack · discharged · Aug 19, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933387](https://openairdocs.org/sdr/TSAA9933387.md): Battery Pack · discharged · Aug 11, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA933302](https://openairdocs.org/sdr/TSAA933302.md): Battery Pack · discharged · Jul 21, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR TSAA9933239](https://openairdocs.org/sdr/TSAA9933239.md): Battery Pack · discharged · Mar 27, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9933025](https://openairdocs.org/sdr/TSAA9933025.md): Battery Pack · discharged · Jan 16, 1999 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9833643](https://openairdocs.org/sdr/TSAA9833643.md): Battery Pack · discharged · Dec 16, 1998 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED BATTERY FOR RIGHT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9833642](https://openairdocs.org/sdr/TSAA9833642.md): Battery Pack · discharged · Dec 16, 1998 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED BATTERY FOR FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9833641](https://openairdocs.org/sdr/TSAA9833641.md): Battery Pack · discharged · Dec 16, 1998 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED BATTERY FOR POSITION NR 4 FLOOR PROX LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA9833536](https://openairdocs.org/sdr/TSAA9833536.md): Light · inoperative · Oct 2, 1998 · N827AL · Boeing 737209 · Emergency Lighting
  > REPLACED AFT ENTRY EMERGENCY EXIT IDENTIFIER LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/deregistered/N827AL-2006-09-28/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 = 'N827AL' AND deregistration_id = 'N827AL-2006-09-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N827AL-2006-09-28/reports

---
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