# Service difficulty reports: Boeing 737-205

A list on [Boeing 737-205](https://openairdocs.org/model/boeing-737-205.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 9 · 436 reports

- [SDR MJYA20250613003](https://openairdocs.org/sdr/MJYA20250613003.md): Engine · damaged · Jun 13, 2025 · N467TW · Boeing 737205 · Engine (Turbine/Turboprop)
  > 112000 LBS TAKEOFF, FLAPS 1, V1=144 VR=147 V2=153, RIGHT SEAT TAKEOFF. AFTER NORMAL START AND TAXI OUT FROM WILSON AIR CENTER TO RUNWAY 18L WE PROCEEDED TO TAKE THE RUNWAY AS CLEARED. ROLL OUT WAS NORMAL WITH NORMAL ENGINE SPOOL UP TO STABILIZE ENGINE PARAMETE
- [SDR MJYA201812076003](https://openairdocs.org/sdr/MJYA201812076003.md): Hose · failed · Dec 4, 2018 · N467TW · Boeing 737205 · Hydraulic System, Main
  > DURING CRUISE FLIGHT PORTION ENROUTE FROM KCKB TO KEWR WE EXPERIENCED AN A SYSTEM HYDRAULIC LOSS. AS SOON AS THE ADVISORY LIGHT ILLUMINATED BOTH THE F.O. AND MYSELF VERIFIED 0 (ZERO) QUANTITY ON HYDRAULIC SYSTEM A. THE LOSS OF SYSTEM A CHECKLIST WAS PERFORME
- [SDR MJYA20170108001](https://openairdocs.org/sdr/MJYA20170108001.md): Transmitter · failed · Jan 8, 2017 · N467TW · Boeing 737205 · Trailing Flap Position Indicating System
  > DURING CLIMB, THE PILOT TRIED TO SELECT FLAP UP WITH NO RESPONSE. THE FLAP INDICATION SHOWED THE RT FLAP AT 1 DEGREE AND THE LT FLAP AT 5 DEGREES. WITH NO RESPONSE TO THE FLAP HANDLE POSITION. DECLARED AN EMERGENCY AND LANDED AT AN ALTERNATE AIRPORT. THE AI
- [SDR 2017F00024](https://openairdocs.org/sdr/2017F00024.md): Transmitter · faulty · Jan 8, 2017 · N467TW · Boeing 737205 · Trailing Flap Position Indicating System
  > FLAP ASYMMETRY ISSUE AFTER TAKE OFF. DECLARED AN EMERGENCY AND LAND AT ALTERNATE AIRPORT. AFTER TROUBLESHOOTING IT WAS DISCOVERED THAT THE RT FLAP TRANSMITTER AND THE FLAP INDICATOR WERE FAULTY. REPLACED FAULTY UNITS AND THE DISCREPANCY WITH THE FLAP ASYMMET
- [SDR MJYA20150811009](https://openairdocs.org/sdr/MJYA20150811009.md): Stiffener · corroded · Aug 10, 2015 · N465TW · Boeing 737205 · Fuselage Miscellaneous Structure
  > IN THE AUXILIARY POWER UNIT COMPARTMENT CORROSION WAS FOUND, MAIN AIR INLET MATING FACE STIFFENER SUPPORTS. SRM REPAIR.
- [SDR MJYA20150811008](https://openairdocs.org/sdr/MJYA20150811008.md): Stiffener · corroded · Aug 10, 2015 · N465TW · Boeing 737205 · Fuselage Miscellaneous Structure
  > IN THE AUXILIARY POWER UNIT COMPARTMENT, CORROSION WAS FOUND ON THE LOWER T CHANNEL STIFFENER ON THE MAIN AIR INLET MATING FACE. THIS IS A SRM REPAIR.
- [SDR MJYA20150811006](https://openairdocs.org/sdr/MJYA20150811006.md): Pan · corroded · Aug 10, 2015 · N465TW · Boeing 737205 · Fuselage Miscellaneous Structure
  > FLOOR PAN WEB CORROSION ON UPPER SURFACE. SRM REPAIR.
- [SDR MJYA20150810005](https://openairdocs.org/sdr/MJYA20150810005.md): Floor Support · corroded · Aug 10, 2015 · N465TW · Boeing 737205 · Fuselage Miscellaneous Structure
  > FLOOR PAN WEB CORROSION ON UPPER SURFACE AT STATION 1025, LBL 10, WL232. THIS IS A SRM REPAIR WITH LEVEL 2 CORROSION.
- [SDR MJYA201311060018](https://openairdocs.org/sdr/MJYA201311060018.md): Skin · corroded · Nov 4, 2013 · N467TW · Boeing 737205 · Horizontal Stabilizer, Plate/Skin
  > RT STABILIZER, TOP SIDE SKIN WITH CORROSION SURROUNDING FASTENERS NEAR T/E.
- [SDR SROM2012032000019](https://openairdocs.org/sdr/SROM2012032000019.md): Duct Clamp · worn · Jun 19, 2012 · N733PA · Boeing 737205 · Pneumatic Distribution System
  > ON CLIMBOUT, RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. REDUCED POWER ON RIGHT ENGINE LIGHT EXTINGUISHED. RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. REPLACED BLEED AIR CLAMP ON RIGHT BLEED AIR DUCT ON RIGHT ENGINE. SUBSEQUENT LEAK CHECK OF DUCT WAS SA
- [SDR SROM201203200018](https://openairdocs.org/sdr/SROM201203200018.md): Sill · corroded · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION FOUND ON L1 DOOR INNER SILL. SECOND BLEND ON THIS PART'S HISTORY.
- [SDR SROM201203200017](https://openairdocs.org/sdr/SROM201203200017.md): Sill · corroded · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Miscellaneous Structure
  > LEVEL 1 CORROSION FOUND ON FORWARD SERVICE DOOR SILL CHORD. SECOND BLEND IN THIS PART'S HISTORY.
- [SDR SROM2012032000016](https://openairdocs.org/sdr/SROM2012032000016.md): Bear Strap · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, CRACKS WERE FOUND IN THE BEAR STRAP RE-INFORCEMENT OF THE L1 DOOR, BS 304 S10-13L.
- [SDR SROM201203160002](https://openairdocs.org/sdr/SROM201203160002.md): Stringer · corroded · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Longeron/Stringer
  > LEVEL 1 CORROSION FOUND ON STRINGER.
- [SDR SROM201203200014](https://openairdocs.org/sdr/SROM201203200014.md): Spar · corroded · Mar 16, 2012 · N733PA · Boeing 737205 · Wing Spar
  > CORROSION FOUND ON LOWER SPAR CHORD.
- [SDR SROM201203200013](https://openairdocs.org/sdr/SROM201203200013.md): Shear Tie · damaged · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Internal Mounting Structure
  > DAMAGED SHEAR TIE FRAME.
- [SDR SROM20120320013](https://openairdocs.org/sdr/SROM20120320013.md): Strap · damaged · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Miscellaneous Structure
  > STRAP DAMAGED.
- [SDR SROM201203200012](https://openairdocs.org/sdr/SROM201203200012.md): Frame · damaged · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Frame
  > DAMAGED FRAME AT BS 867 S26R.
- [SDR SROM201203160001](https://openairdocs.org/sdr/SROM201203160001.md): Frame · damaged · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Frame
  > DAMAGE /DRILL START ON FRAME.
- [SDR SROM201203200011](https://openairdocs.org/sdr/SROM201203200011.md): Frame · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Frame
  > FRAME CRACKED AT AIR CONDITIONING BRACKET.
- [SDR SROM201203200010](https://openairdocs.org/sdr/SROM201203200010.md): Frame · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Frame
  > CRACKED FRAME AT AIR CONDITIONING SUPPORT BRACKET.
- [SDR SROM201203200009](https://openairdocs.org/sdr/SROM201203200009.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED AT BS 360 S5L.
- [SDR SROM201203200008](https://openairdocs.org/sdr/SROM201203200008.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED AT BS 400 S18R.
- [SDR SROM201203200007](https://openairdocs.org/sdr/SROM201203200007.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 500A S19R.
- [SDR SROM201203200006](https://openairdocs.org/sdr/SROM201203200006.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED AT BS 908 S4R.
- [SDR SROM201203200005](https://openairdocs.org/sdr/SROM201203200005.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED AT BS 767 S22L.
- [SDR SROM201203200004](https://openairdocs.org/sdr/SROM201203200004.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED AT BS 907 S21R.
- [SDR SROM201203200003](https://openairdocs.org/sdr/SROM201203200003.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 706 S13R.
- [SDR SROM201203200002](https://openairdocs.org/sdr/SROM201203200002.md): Stringer Clip · cracked · Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach Fittings
  > STRINGER CLIP AT BS 663 S9R IS CRACKED.
- [SDR SROM2012001](https://openairdocs.org/sdr/SROM2012001.md): Contactor · burned · Jan 9, 2012 · N733PA · Boeing 737205 · External Power System
  > EXPERIENCED SMOKE IN THE COCKPIT AT THE GATE PRIOR TO DEPARTURE. THE FLIGHT CREW QUICKLY POWERED DOWN THE AIRCRAFT; NO PASSENGERS WERE ON BOARD. MAINTENANCE FOUND THE GROUND SERVICE CONTACTOR TO BE THE PROBLEM AND ONE PHASE OF THE THREE PHASE GROUND POWER CI
- [SDR SROM2011010](https://openairdocs.org/sdr/SROM2011010.md): Case · cracked · Jul 20, 2011 · N736BP · Boeing 737205 · Turbine Engine Air Inlet Section
  > REPLACED NR 1 ENGINE FAN INLET CASE DUE TO CRACKED FLANGE B WELD WITH OVERHAULED ASSEMBLY; FAN CASE P/N 786269, S/N DX6417, NR 1 BEARING HOUSING P/N 765471, S/N JU7622 AND REAR SUPPORT P/N 5003534-01, S/N LX9712 IN ACCORDANCE WITH PRATT AND WHITNEY MAINTENANCE
- [SDR SROM2011009](https://openairdocs.org/sdr/SROM2011009.md): Window Frame · corroded · Jul 20, 2011 · N736BP · Boeing 737205 · Fuselage Main, Structure
  > CORROSION ON LT FLIGHT WINDOW FRAME JUST ABOVE THE NR 2 SLIDING WINDOW REPAIRED BY REMOVING AND REPLACING THE WINDOW FRAME WITH A NEW FRAME FROM APPROXIMATELY BS 217 TO BS 236 IN ACCORDANCE WITH BOEING DRAWING NOS 05-71773 AND 65-45800. FASTENERS INSTALLED IN
- [SDR SROM2011008](https://openairdocs.org/sdr/SROM2011008.md): Skin · nicked · Jul 20, 2011 · N736BP · Boeing 737205 · Fuselage Main, Plate/Skin
  > NICK ON FUSELAGE SKIN AT BS 867 S-25L REPAIRED IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011, SECTION 53-30-3, FIGURE 48. HFEC OPEN HOLE INSPECTION OF ALL FASTENER HOLES COMMON TO THE REPAIR IN ACCORDANCE WITH B
- [SDR SROM2011007](https://openairdocs.org/sdr/SROM2011007.md): Skin · nicked · Jul 19, 2011 · N736BP · Boeing 737205 · Fuselage Main, Plate/Skin
  > NICK ON FUSELAGE SKIN AT BS 847 S-25R REPAIRED IN ACCORDANCE WITH MESSAGE NOS. KFC-ATR-11-0004-01C, DATED JUNE 24, 2011, KFC-ATR-11-0004-05B, DATED JUNE 29, 2011, KFC-ATR-11-0004-06C, DATED JULY 13, 2011 AND BOEING APPROVED FAA FORM 8100-9, DATED JULY 14, 201
- [SDR SROM2011006](https://openairdocs.org/sdr/SROM2011006.md): Skin · gouged · Jul 19, 2011 · N736BP · Boeing 737205 · Wing, Plate/Skin
  > GOUGE IN RT UPPER INSPAR WING SKIN UPPER SURFACE ABOVE AFT SPAR AT WBL 77R REPAIRED IN ACCORDANCE WITH MESSAGE NOS. KFC-ATR-11-0003-01C, DATED JUNE 23, 2011, KFC-ATR-11-0003-05B, DATED JUNE 29, 2011, KFC-ATR-11-0003-06C, DATED JULY 4, 2011 AND BOEING APPROVED
- [SDR SROM2011005](https://openairdocs.org/sdr/SROM2011005.md): Skin · gouged · Jul 19, 2011 · N736BP · Boeing 737205 · Wing, Plate/Skin
  > GOUGE IN LT UPPER INSPAR WING SKIN UPPER SURFACE ABOVE AFT SPAR AT WBL 77L REPAIRED IN ACCORDANCE WITH MESSAGE NOS. KFC-ATR-11-0002-01C, DATED JUNE 23, 2011, KFC-ATR-11-0002-07B, DATED JUNE 29, 2011, KFC-ATR-11-0002-08C, DATED JULY 4, 2011 AND BOEING APPROVED
- [SDR SROM2011004](https://openairdocs.org/sdr/SROM2011004.md): Stringer · cracked · Jul 19, 2011 · N736BP · Boeing 737205 · Fuselage Main, Longeron/Stringer
  > REPLACED CRACKED STRINGER CLIP AT BS 907 S-9R IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011, SECTION 51-30-2, PAGE 5, CH 7 AND 51-10-1, PAGE 9 CH 7. REFERENCE NON-ROUTINE WORK ORDER NR 1014192, DATED 25 JUNE 201
- [SDR SROM2011003](https://openairdocs.org/sdr/SROM2011003.md): Bulkhead · dented · Jul 19, 2011 · N736BP · Boeing 737205 · Fuselage Main, Bulkhead
  > DENT ON FORWARD FACE OF AFT PRESSURE BULKHEAD 3 ABOVE S-5R REPAIRED IN ACCORDANCE WITH MESSAGE NOS KFC-ATR-11-0001-01C, DATED JUNE 21, 2011, KFC-ATR-11-0001-05B, DATED JUNE 28, 2011, KFC-ATR-11-0001-06C, DATED JULY 7, 2011, AND BOEING APPROVED FAA FORM 8100-9,
- [SDR SROM2011002](https://openairdocs.org/sdr/SROM2011002.md): Sill · corroded · Jul 19, 2011 · N736BP · Boeing 737205 · Fuselage Miscellaneous Structure
  > L1 DOOR SILL CHORD CORRODED BEYOND LIMITS IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011, SECTION 53-10-1. REPLACED CHORD WITH NEW P/N 65-17688U165 FROM BS 277 - BS370 LT, LBL65 IN ACCORDANCE WITH BOEING 737-200
- [SDR SROM2011001](https://openairdocs.org/sdr/SROM2011001.md): Channel · corroded · Jul 19, 2011 · N736BP · Boeing 737205 · Fuselage Miscellaneous Structure
  > CORRODED AFT LAVATORY FORWARD PARTITION WALL FLOOR HAT-SECTION AT BS 990 LBL 17-30 AROUND TWO CLIPNUT HOLES (AFT SIDE) AND CORROSION ON FORWARD SIDE OF HAT-SECTION AT BS 990 LBL 50-60. REPAIRED BY FABRICATION AND REPLACEMENT IN ACCORDANCE WITH BOEING 737-200
- [SDR SROM2010009](https://openairdocs.org/sdr/SROM2010009.md): Skin · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN BLEND OUT BELOW STRINGER S-25R, STA BS 885.25 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MAR 10, 2010, SECTION 53-30-3, PAGES 254, 257 TO 263 AND 286 AND 51-30-1, PAGE 3. REFERENCE NON-ROUTINE TASK CARD 6
- [SDR SROM2010015](https://openairdocs.org/sdr/SROM2010015.md): Shear Tie · cracked · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Internal Mounting Structure
  > REPAIRED SHEAR TIE BETWEEN STRINGERS 20L AND S-21L, STA: BS 907 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-10-4, FIGURE 8. REFERENCE NON-ROUTINE TASK CARD 813, DATED APRIL 01, 2010.
- [SDR SROM2010014](https://openairdocs.org/sdr/SROM2010014.md): Skin · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN BLEND OUT 0.4 INCHES BELOW STRINGER S-20L, STA: BS 896 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 799, DATED MARCH 25, 2
- [SDR SROM2010013](https://openairdocs.org/sdr/SROM2010013.md): Skin · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN SCRIBE LINES LEFT WING TO BODY FAIRING AT STRINGERS S-16L TO 3 INCHES BELOW S-17L, STA: BS 500B - 516 IN ACCORDANCE WITH MESSAGE KFC-ATR-10-0001-01C, DATED MARCH 30, 2010, KFC-ATR-10-0001-05B, DATED MARCH 31, 2010, KFC-ATR-10-0001-06B,
- [SDR SROM2010012](https://openairdocs.org/sdr/SROM2010012.md): Skin · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN BLEND OUT AT STRINGER S-20L, STA: BS 974 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48, DETAIL XV. REFERENCE NON-ROUTINE TASK CARD 743, 742 AND 744, DATED MARCH 18
- [SDR SROM2010011](https://openairdocs.org/sdr/SROM2010011.md): Skin · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN BLEND OUT 1.6 INCHES ABOVE STRINGER S-23L, STA: BS 926.5 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48, PAGES 256 TO 260 AND 264, DETAIL VII, PAGES 261 AND 281 AND
- [SDR SROM2010010](https://openairdocs.org/sdr/SROM2010010.md): Skin · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN BLEND OUT ABOVE STRINGER S-26R, STA: BS 838.5 IN ACCORDANCE WITH MESSAGE KFC-ATR-10-0001-01C, DATED MARCH 31, 2010, KFC-ATR-10-0001-05B, DATED APRIL 05, 2010, KFC-ATR-10-0001-06C, DATED APRIL 19, 2010, BOEING REPAIR DRAWING 65-45775, SH
- [SDR SROM2010008](https://openairdocs.org/sdr/SROM2010008.md): Skin · nicked · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE NICK 3 INCHES ABOVE STRINGER S-20R, STA: BS 914 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 617, DATED MARCH 18, 2010.
- [SDR SROM2010007](https://openairdocs.org/sdr/SROM2010007.md): Intercostal · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Miscellaneous Structure
  > REPAIRED STRINGER INTERCOSTAL AT STRINGER S-4L, STA: BS 305 BY REPLACEMENT WITH NEW PART 50-8261-62 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-30-3 AND BOEING DRAWING 50-8261, REV H. REFERENCE N
- [SDR SROM2010006](https://openairdocs.org/sdr/SROM2010006.md): Skin · damaged · Apr 26, 2010 · N733PA · Boeing 737205 · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN BLEND OUT 1.75 INCHES ABOVE STRINGER S-23R, STA: BS 904.8 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 380, 374, 375, AND 383, DA

Next page: https://openairdocs.org/model/boeing-737-205/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 = '737205'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-205/reports

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