# Service difficulty reports: Boeing 737-39A

A list on [Boeing 737-39A](https://openairdocs.org/model/boeing-737-39a.md).

Newest first. General aviation reporting is voluntary.

- [SDR 6VAR20190428001](https://openairdocs.org/sdr/6VAR20190428001.md): Skin Panel · corroded · Apr 22, 2019 · N444HE · Boeing 73739A · Wing, Plate/Skin
  > RIGHT WING UPPER SURFACE SKIN CORRODED AT WBL71.24.
- [SDR 2019F00195](https://openairdocs.org/sdr/2019F00195.md): Skin · corroded · Apr 22, 2019 · N444HE · Boeing 73739A · Wing, Plate/Skin
  > RIGHT WING UPPER SURFACE SKIN CORRODED AT WBL71.24.
- [SDR NOCA01806](https://openairdocs.org/sdr/NOCA01806.md): Tire · failed · Feb 17, 2006 · N760NA · Boeing 73739A · Tire
  > ON WALKAROUND FOUND NR 8 TIRE FLAT. BOTH TIRES NR 7 AND NR 8 TIRES REPLACED. WHEN NR 8 TIRE WENT FLAT THE THREAD SEPARATED CAUSING DAMAGE TO NR 7 SPOILER, UNDER WING PANELS, INBOARD AFT AND MAIN FLAP.
- [SDR PIDA20050059](https://openairdocs.org/sdr/PIDA20050059.md): Battery Pack · inoperative · Jul 15, 2005 · N375PA · Boeing 73739A · Emergency Lighting
  > AFT CENTER AISLE EMERGENCY LIGHT INOP. REPLACED AFT RIGHT BATTERY PACK PER MM 33-50.
- [SDR 375PA0044](https://openairdocs.org/sdr/375PA0044.md): Skin · cracked · Feb 21, 2005 · N375PA · Boeing 73739A · Cargo/Baggage Doors
  > AFT CARGO DOOR INNER SKIN CRACKED AROUND LIGHTENING HOLE NEAR CENTER OF DOOR. REPAIRED PER SRM 51-70-13.
- [SDR 375PA0046](https://openairdocs.org/sdr/375PA0046.md): Seat Track · corroded · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FROM BS 344 TO BS 380 AT LBL 25 CORRODED. REPLACED SECTION OF SEAT TRACK PER SRM 53-00-52.
- [SDR 375PA0045](https://openairdocs.org/sdr/375PA0045.md): Attach Fitting · cracked · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage Main, Attach Fittings
  > INTERCOSTAL ATTACH CLIP CRACKED UNDER AFT END OF RIGHT TRANSITION ANGLE AT BS 947 BETWEEN STR 26 RT AND STR 25 RT. REPLACED ATTACH CLIP PER SRM 51-10-02.
- [SDR 375PA0043](https://openairdocs.org/sdr/375PA0043.md): Door Frame · cracked · Feb 21, 2005 · N375PA · Boeing 73739A · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT FRAME CRACKED APPROX 16 INCHES ABOVE LOWER AFT CORNER. REPLACED FRAME PER SRM 51-40-05, 51-40-08, AND 51-10-01.
- [SDR 375PA0040](https://openairdocs.org/sdr/375PA0040.md): Floorbeam · cracked · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage Main, Floor Beam
  > AFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D +7 AT LBL 7. REPAIRED PER SRM 53-00-53.
- [SDR 375PA0038](https://openairdocs.org/sdr/375PA0038.md): Support Angle · cracked · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE CRACKED AT BS 767 ABOVE STR 28 LT. REPLACED ATTACH ANGLE PER SRM 51-40-01.
- [SDR 375PA0037](https://openairdocs.org/sdr/375PA0037.md): Skin · cracked · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage Main, Plate/Skin
  > AFT SERVICE DOOR TOP HINGE CUTOUT IN FUSELAGE SKIN CRACKED. REPAIRED PER SRM 53-60-01.
- [SDR 375PA0036](https://openairdocs.org/sdr/375PA0036.md): Panel · gouged · Feb 21, 2005 · N375PA · Boeing 73739A · Air Conditioning Doors
  > LEFT RAM AIR CLOSE OUT PANEL GOUGED. REPAIRED PER SRM 51-70-13.
- [SDR 375PA0034](https://openairdocs.org/sdr/375PA0034.md): Plate · cracked · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage Main, Plate/Skin
  > L1 DOOR FORWARD SILL PLATE CRACKED. WELDED PER BAC SPEC 5975.
- [SDR 375PA0033](https://openairdocs.org/sdr/375PA0033.md): Stiffener · damaged · Feb 21, 2005 · N375PA · Boeing 73739A · Wing Miscellaneous Structure
  > VERTICAL STIFFENER FOR THE FRONT SPAR BULKHEAD AT RBL 6.25 WAS TRIMMED OFF TO ALLOW FOR REPAIR OF KEEL BEAM (SDR 375PA0032). REPAIRED PER EA 57-029.
- [SDR 375PA0029](https://openairdocs.org/sdr/375PA0029.md): Floorbeam · corroded · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM T-CAP AT BS 312 AT LBL 19. REPAIRED PER SRM 53-10-51.
- [SDR 375PA0028](https://openairdocs.org/sdr/375PA0028.md): Floorbeam · corroded · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM T-CAP AT BS 344 FROM LBL 19 TO LBL 30. REPAIRED PER SRM 53-10-51.
- [SDR 375PA0027](https://openairdocs.org/sdr/375PA0027.md): Seat Track · corroded · Feb 21, 2005 · N375PA · Boeing 73739A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN FORWARD END OF RIGHT O/B SEAT TRACK UNDER THE WIND SCREEN. REPLACED SECTION OF SEAT TRACK PER SRM 53-00-52.
- [SDR 375PA0022](https://openairdocs.org/sdr/375PA0022.md): Light · inoperative · Dec 7, 2003 · N375PA · Boeing 73739A · Emergency Lighting
  > EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY MISSING AT ROW 16 AREA. INSTALLED EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY PER MM 33-51-81. OPS CHECKS NORMAL.
- [SDR 375PA0021](https://openairdocs.org/sdr/375PA0021.md): Battery Pack · discharged · Nov 6, 2003 · N375PA · Boeing 73739A · Emergency Lighting
  > MID TO AFT EMERGENCY FLOOR LIGHTING INOP. REPLACED BATTERY PACK LEFT SIDE MID CABIN. OPS NORMAL PER MM 33-51-00.
- [SDR 375PA0019](https://openairdocs.org/sdr/375PA0019.md): Coupler · inoperative · Aug 16, 2003 · N375PA · Boeing 73739A · Autopilot System
  > YAW DAMPER INOPERATIVE. RELEASED ON MEL 22-3-1. 8/16/2003: REPLACED YAW DAMPER COUPLER IAW MM22-12-32 PG.401 AND ACCOMPLISHED OPS. TEST, SELF TEST, SERVO TEST AND RUDDER PRESSURE REDUCER TEST. ALL OK.
- [SDR 375PA0014](https://openairdocs.org/sdr/375PA0014.md): Bulb · burned out · Apr 27, 2003 · N375PA · Boeing 73739A · Emergency Lighting
  > THREE EACH BULBS NOT WORKING ON EMERGENCY EXIT LIGHT TEST ON SERVICE CHECK. RECONNECTED WIRING AT SOCKETS. ALL LIGHTS OPS CHECK GOOD PER MM 33-50-00.
- [SDR 98ZZZX4418](https://openairdocs.org/sdr/98ZZZX4418.md): Cvr · inoperative · Jul 14, 1998 · N253DV · Boeing 73739A · Audio/Video Monitoring
  > CVR FAILED OPERATIONAL TEST DURING ROUTINE SCHEDULED TESTING. REMOVED AND REPLACED CVR WITH OVERHAULED UNIT, SAME PORT NUMBER, SAME MODEL NUMBER. (TEARDOWN AND BENCH EVALUATION OF FAILED UNIT INDICATED SEVERAL PROBLEMS. FAILED MOTOR, BELT, TAPE, ETC.) A RE
- [SDR 98ZZZX4420](https://openairdocs.org/sdr/98ZZZX4420.md): Stiffener · corroded · Jun 22, 1998 · N253DV · Boeing 73739A · Fuselage Miscellaneous Structure
  > STIFFENER AND STRINGER FOUND CORRODED IN TORQUE BOX APU BAY. SUBMITTER SUGGESTED MORE FREQUENT AND MORE DETAILED INSPECTIONS OF THE SECTION 48 TORQUE BOX AREA INCORPORATED INTO THE CPCP PROGRAMS. THIS COULD HAVE AFFECTED MORE CRITICAL AREAS HAD IT NOT BEEN CA
- [SDR 98ZZZX4419](https://openairdocs.org/sdr/98ZZZX4419.md): Stringer · corroded · Jun 22, 1998 · N253DV · Boeing 73739A · Fuselage Main, Frame
  > STIFFENER AND STRINGER FOUND CORRODED IN TORQUE BOX APU BAY. SUBMITTER SUGGESTED MORE FREQUENT AND MORE DETAILED INSPECTIONS OF THE SECTION 48 TORQUE BOX AREA INCORPORATED INTO THE CPCP PROGRAMS. THIS COULD HAVE AFFECTED MORE CRITICAL AREAS HAD IT NOT BEEN CA

## 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 = '73739A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-39a/reports

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