# Service difficulty reports: Boeing 737-209

A list on [Boeing 737-209](https://openairdocs.org/model/boeing-737-209.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 81 reports

- [SDR 2021F00104](https://openairdocs.org/sdr/2021F00104.md): Overheat Sensor · dirty · May 4, 2021 · N809TA · Boeing 737209 · Overheat Detection
  > IN FLIGHT, CREW HAD WHEEL WELL OVERHEAT LIGHT AS WELL AS MASTER FIRE WARNING LIGHTS ILLUMINATE. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS EXTENDED. UPON LANDING, MAINTENANCE INSPECTION DETERMINED OVERHEAT SENSING LOOP CONNECTION WAS DIRTY, CLEANED AND PERFORME
- [SDR FY4Y202009118008](https://openairdocs.org/sdr/FY4Y202009118008.md): Skin · corroded · Sep 1, 2020 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT LT WING BOTTOM SKIN LOWER SURFACE AT WS 475 TO WS 525.
- [SDR FY4Y202008013](https://openairdocs.org/sdr/FY4Y202008013.md): Battery · failed · Aug 28, 2020 · N809TA · Boeing 737209 · Emergency Lighting
  > EMERGENCY LIGHT INOPERABLE ON FWD ENTRY DOOR AND FWD GALLEY SERVICE DOOR.
- [SDR FY4Y202008012](https://openairdocs.org/sdr/FY4Y202008012.md): Battery · inoperative · Aug 28, 2020 · N809TA · Boeing 737209 · Emergency Lighting
  > EMERGENCY LIGHT INOPERABLE ON FWD ENTRY DOOR AND FWD GALLEY SERVICE DOOR.
- [SDR FY4Y2020009118007](https://openairdocs.org/sdr/FY4Y2020009118007.md): Skin · corroded · Aug 28, 2020 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT AT LT WING BOTTOM SKIN LOWER SURFACE AT WS 315 TO WS 475.
- [SDR FY4Y202009118006](https://openairdocs.org/sdr/FY4Y202009118006.md): Skin · corroded · Aug 28, 2020 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT LT WING BOTTOM SKIN LOWER SURFACE AT INBOARD TO WS 195.
- [SDR FY4Y202009118005](https://openairdocs.org/sdr/FY4Y202009118005.md): Spar · corroded · Aug 26, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 135.
- [SDR FY4Y202009108002](https://openairdocs.org/sdr/FY4Y202009108002.md): Frame · corroded · Aug 26, 2020 · N809TA · Boeing 737209 · Fuselage Main, Frame
  > CORROSION WAS FOUND AT AFT CARGO FWD BULKHEAD LOWER CHORD AT BS 727 BETWEEN S-25L AND 25R.
- [SDR FY4Y202009118011](https://openairdocs.org/sdr/FY4Y202009118011.md): Lug · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Horizontal Stabilizer Structure
  > CORROSION WAS FOUND AT FWD & AFT SURFACE OF RT SIDE HORIZONTAL STABILIZER REAR SPAR UPPER LUG.
- [SDR FY4Y202009118010](https://openairdocs.org/sdr/FY4Y202009118010.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT RT WING FRONT SPAR LOWER CHORD AT FSS 442.3.
- [SDR FY4Y202009118009](https://openairdocs.org/sdr/FY4Y202009118009.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT RT WING FRONT SPAR LOWER CHORD AT FSS 416.8.
- [SDR FY4Y202009118004](https://openairdocs.org/sdr/FY4Y202009118004.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 422.
- [SDR FY4Y202009118003](https://openairdocs.org/sdr/FY4Y202009118003.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 307.
- [SDR FY4Y202009108001](https://openairdocs.org/sdr/FY4Y202009108001.md): Keelbeam · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Fuselage Main, Keel
  > CORROSION WAS FOUND AT KEEL BEAM LOWER CHORD AT AFT CARGO BS 727 S-27L (LENGTH: 3" WIDTH: 1"). REFER TO NRC CA1174-02-010.
- [SDR JRAA201807170001](https://openairdocs.org/sdr/JRAA201807170001.md): Connector · broken · Jul 17, 2018 · N737CS · Boeing 737209 · Fire Protection System Wiring
  > NUMBER 2 ENGINE FIRE LIGHT CAME ON IN FLIGHT. MX DISCOVERED BROKEN NUMBER 2 ENGINE FIRE DETECTOR LOOP CONNECTOR. ITEM PREVIOUSLY MEL'D PER MEL 737071618-1. PERFORMED SYSTEM OPS CHECKS PER AMM 26-11-00. OPS CHECK GOOD.
- [SDR JRAA2017081100446](https://openairdocs.org/sdr/JRAA2017081100446.md): Skin · corroded · Nov 10, 2016 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > DURING A C1 CHECK, FOUND THE LEFT WING UPPER SURFACE WAS CORRODED ON REAR SPAR BETWEEN WS 150 - 205. CORROSION WAS BLENDED OUT BEYOND SRM LIMIT. REPAIRED IAW DOCUMENT ROO3 REV 01.
- [SDR JRAA2017081100445](https://openairdocs.org/sdr/JRAA2017081100445.md): Skin · corroded · Oct 31, 2016 · N809TA · Boeing 737209 · Fuselage Main, Plate/Skin
  > DURING INSPECTION IAW CARD 53-30-00-101, FOUND FUSELAGE SKIN AT BS 1016 BETWEEN STRINGERS 24R - 25R WAS CORRODED. A REPAIR WAS CARRIED OUT IAW DOCUMENT 2016R002.
- [SDR 2017FA0000444](https://openairdocs.org/sdr/2017FA0000444.md): Skin · corroded · Oct 29, 2016 · N809TA · Boeing 737209 · Fuselage Main, Plate/Skin
  > DURING A C1 CHECK, IAW TASK CARD 53-30-00-101, FOUND A CRACK ON FUSELAGE SKIN AT BS 937, STRINGER 24L. REPAIRED IAW REPAIR PLAN DOCUMENT 2016R001.
- [SDR 2017FA0000443](https://openairdocs.org/sdr/2017FA0000443.md): Stringer Fitting · corroded · Oct 7, 2016 · N809TA · Boeing 737209 · Fuselage Main, Longeron/Stringer
  > DURING A C1 CHECK, DURING INSPECTION IAW TASK CARD53-88-80-101, FOUND BS 1016 STRINGER 17R FITTING CORRODED. THE STRINGER FITTING WAS REPLACED IAW ENGINEERING AUTHORIZATION B737-53-00-8.
- [SDR JRAA2016052504](https://openairdocs.org/sdr/JRAA2016052504.md): Sliding Window · cracked · May 25, 2016 · N737CS · Boeing 737209 · Flight Compartment Windows
  > COCKPIT L2 WINDOW CRACKED. APPEARS HEATING ELEMENT SHORTED, CRACKED OUTER PANE DETERMINED NON STRUCTURAL, FLIGHT CONTINUED, LANDED WINDOW INSPECTED AND ACFT RETURNED TO HOME BASE UNDER SPECIAL FERRY PERMIT. RESTRICTIONS, UNPRESSURIZED, BELOW 10,000FT. UNIT WA
- [SDR JRAA20160420002](https://openairdocs.org/sdr/JRAA20160420002.md): Sliding Window · cracked · Apr 19, 2016 · N737CS · Boeing 737209 · Flight Compartment Windows
  > COCKPIT L2 SLIDING WINDOW CRACKED. APPEARS HEATING ELEMENT SHORTED, CRACKED OUTER PANE DETERMINED NONSTRUCTURAL, FLIGHT CONTINUED & LANDED. WINDOW INSPECTED, ACFT RETURNED TO HOME BASE ON SPECIAL FERRY FLIGHT PERMIT, ISSUED 4 19 2016. REPLACEMENT WINDOW INS
- [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)

Next page: https://openairdocs.org/model/boeing-737-209/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 aircraft_model_key = '737209'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-209/reports

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