# Service difficulty reports: N371PA, cancelled Dec 6, 2006

A list on [N371PA, cancelled Dec 6, 2006](https://openairdocs.org/deregistered/N371PA-2006-12-06.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 · 98 reports

- [SDR PIDA06018](https://openairdocs.org/sdr/PIDA06018.md): Skin · cracked · Feb 9, 2006 · N371PA · Boeing 737306 · Cargo/Baggage Doors
  > AFT CARGO DOOR HAS CRACK IN SKIN OF DOOR HANDLE CUTOUT (AFT UPPER END OF FLIP OPEN COVER). REPAIRED DAMAGE PER PACE AIRLINES EA 52-037.
- [SDR PIDA06016](https://openairdocs.org/sdr/PIDA06016.md): Channel · cracked · Feb 3, 2006 · N371PA · Boeing 737306 · Nacelle/Pylon Miscellaneous Structure
  > U-CHANNEL CRACKED BEHIND PANEL 5843R ON THE RIGHT ENGINE PYLON. REPLACED CHANNEL PER BOEING DWG 313A1355.
- [SDR PIDA06014](https://openairdocs.org/sdr/PIDA06014.md): Skin · dented · Jan 30, 2006 · N371PA · Boeing 737306 · Cargo/Baggage Doors
  > AFT CARGO DOOR HAS TWO DENTS BELOW THE DOOR HANDLE. REPAIRED DAMAGE PER SRM 52-00-01.
- [SDR PIDA06013](https://openairdocs.org/sdr/PIDA06013.md): Fuse · inoperative · Jan 28, 2006 · N371PA · Boeing 737306 · Emergency Lighting
  > EMERGENCY LIGHT IN BULLNOSE PANEL AT ROW 6ABC IS INOP. REPLACED FUSE IN M1132 AT BS 330 RT. EMERGENCY LIGHTS OPS CHECK GOOD PER MM 33-52-11.
- [SDR PIDA06012](https://openairdocs.org/sdr/PIDA06012.md): Skin · cracked · Jan 28, 2006 · N371PA · Boeing 737306 · Leading Edge Devices
  > NUMBER 6 SLAT HAS A CRACK BETWEEN FASTENERS ON THE LOWER SKIN JUST I/B OF THE I/B AUX TRACK. REPAIRED PER SRM 57-43-01.
- [SDR PIDA06011](https://openairdocs.org/sdr/PIDA06011.md): Skin · cracked · Jan 28, 2006 · N371PA · Boeing 737306 · Leading Edge Devices
  > NUMBER 5 SLAT HAS A CRACK BETWEEN FASTENERS ON THE LOWER SKIN. REPAIRED PER SRM 57-43-01.
- [SDR PIDA06010](https://openairdocs.org/sdr/PIDA06010.md): Skin · cracked · Jan 28, 2006 · N371PA · Boeing 737306 · Leading Edge Devices
  > NUMBER 1 SLAT HAS A CRACK BETWEEN SIX FASTENERS ON THE LOWER SKIN JUST BELOW THE ACTUATOR. REPAIRED PER SRM 57-43-01.
- [SDR PIDA20050181](https://openairdocs.org/sdr/PIDA20050181.md): Pressure Panel · cracked · Oct 17, 2005 · N371PA · Boeing 737306 · Fuselage Main, Bulkhead
  > EVIDENCE OF CRACK AT PRESSURE WEB AT BS663 AT LBL33. REPAIRED PRESSURE WEB IAW SRM 53-60-51.
- [SDR PIDA20050175](https://openairdocs.org/sdr/PIDA20050175.md): Control Panel · malfunctioned · Oct 11, 2005 · N371PA · Boeing 737306 · Autopilot System
  > AIRSPEED IN THE IAS/MACH WINDOW IS FROZEN IN PLACE AND CANNOT BE MANUALLY SET. REPLACED MODE CONTROL PANEL PER MM 22-11-01.
- [SDR PIDA20050174](https://openairdocs.org/sdr/PIDA20050174.md): Actuator · malfunctioned · Oct 5, 2005 · N371PA · Boeing 737306 · Autopilot System
  > ALTITUDE OCCASIONALLY CLIMBS 300 FEET WITH STAB OUT OF TRIM LIGHT (LEAVES FLIGHT DIRECTOR). REPLACED AUTO PILOT STAB TRIM ACTUATOR PER MM 22-11-81. OPS CHECKS GOOD PER MM 22-11-81.
- [SDR PIDA20050163](https://openairdocs.org/sdr/PIDA20050163.md): Control Panel · malfunctioned · Oct 5, 2005 · N371PA · Boeing 737306 · Autopilot System
  > "B" AUTO PILOT CMD WILL NOT ENGAGE WITHOUT PAUSING IN CWS AND "A" AUTO PILOT WILL NOT ENGAGE (INTERMITTENT). REPLACED MODE CONTROL PANEL PER MM 22-11-34. BITE TEST ACCOMPLISHED SATISFACTORY.
- [SDR PIDA06003](https://openairdocs.org/sdr/PIDA06003.md): Force Limiter · malfunctioned · Jan 3, 2005 · N371PA · Boeing 737306 · Autopilot System
  > A & B AUTO PILOT DISCONNECTS. REPLACED AILERON FORCE LIMITER PER MM 22-11-13. OPS CHECKS GOOD.
- [SDR 371PA0085](https://openairdocs.org/sdr/371PA0085.md): Indicator · false indication · Oct 18, 2004 · N371PA · Boeing 737306 · Autopilot System
  > YAW DAMPER INDICATOR INDICATES FULL RT. REPLACED YAW DAMPER INDICATOR. SYSTEM OPS CHECKS GOOD IAW MM 22-12-01..
- [SDR 371PA0051](https://openairdocs.org/sdr/371PA0051.md): Keelbeam · corroded · Oct 8, 2004 · N371PA · Boeing 737306 · Fuselage Main, Keel
  > LT KEELBEAM HAS CORROSION AFT OF BS 540 AND COMMON TO A PREVIOUSLY INSTALLED REPAIR SPLICE. REPAIRED IAW EA 53-257.
- [SDR 371PA0084](https://openairdocs.org/sdr/371PA0084.md): Attach Fitting · cracked · Oct 4, 2004 · N371PA · Boeing 737306 · Fuselage Main, Attach Fittings
  > HFEC INSPECTION OF PREVIOUS REPAIR INDICATES A CRACK AT THE BS 616 STUB BEAM TO LONGITUDINAL FLOORBEAM ATTACH POINT AT LBL 45.5. FURTHER INVESTIGATION DETERMINED THAT THE DAMAGE TO BE A PREVIOUS PLUG INSTALLED IN THE FASTENER HOLE. REPAIRED AREA IAW MFG MESS
- [SDR 371PA0048](https://openairdocs.org/sdr/371PA0048.md): Skin · delaminated · Sep 29, 2004 · N371PA · Boeing 737306 · Landing Gear Doors
  > LEFT AND RIGHT MAIN LANDING GEAR DOORS HAVE DELAMINATION IN THE SKIN AT THE DOOR ATTACH FITTING. REPAIRED DAMAGE PER SRM 51-70-17 AND EA 53-258.
- [SDR 371PA0058](https://openairdocs.org/sdr/371PA0058.md): Sill · corroded · Sep 28, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > AFT CABIN, AFT ENTRY DOOR LOWER SILL ASSEMBLY FROM BS 947.5 TO BS 986.5 HAS CORROSION. REPAIRED IAW SRM 53-60-15.
- [SDR 371PA0057](https://openairdocs.org/sdr/371PA0057.md): Stringer · corroded · Sep 28, 2004 · N371PA · Boeing 737306 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 25 LT AT BS 360 BEHIND E-2 RACK. REPAIRED PER SRM 53-10-03 AND EA 53-255.
- [SDR 371PA0080](https://openairdocs.org/sdr/371PA0080.md): Angle · corroded · Sep 27, 2004 · N371PA · Boeing 737306 · Wing Miscellaneous Structure
  > CORROSION IN ANGLE FOR LEFT WHEEL WELL TO WING CLOSEOUT PANEL. REPLACED ANGLE PER BAC DWG 65-45687.
- [SDR 371PA0049](https://openairdocs.org/sdr/371PA0049.md): Drag Angle · cracked · Sep 26, 2004 · N371PA · Boeing 737306 · Aerodynamic Fairings
  > DRAG ANGLE CRACKED ABOVE RT RAM AIR DOOR. REPAIRED IAW EA 53-250.
- [SDR 371PA0050](https://openairdocs.org/sdr/371PA0050.md): Angle · cracked · Sep 25, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > DRAG ANGLE CRACKED ABOVE LEFT RAM AIR DUCT. REPAIRED PER EA 53-250.
- [SDR 371PA0063](https://openairdocs.org/sdr/371PA0063.md): Channel · cracked · Sep 21, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > LOWER ANTENNA SUPPORT CHANNEL HAS SEVERAL CRACKS. REPLACED ANTENNA CHANNEL PER SRM 51-10-02.
- [SDR 371PA0060](https://openairdocs.org/sdr/371PA0060.md): Intercostal · cracked · Sep 21, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD HOLD OPEN LATCH WEB CRACKED. REPLACED INTERCOSTAL IAW SRM 51-10-2 AND SRM 51-40-02.
- [SDR 371PA0056](https://openairdocs.org/sdr/371PA0056.md): Intercostal · cracked · Sep 21, 2004 · N371PA · Boeing 737306 · Auxiliary Power Unit (APU) Doors
  > APU DOOR INTERCOSTAL CRACKED AT HINGE ATTACH BOLT. REPAIRED IAW SRM 51-70-11.
- [SDR 371PA0055](https://openairdocs.org/sdr/371PA0055.md): Tab · delaminated · Sep 21, 2004 · N371PA · Boeing 737306 · Aileron Tabs
  > RT AILERON TAB IS DELAMINATED AT OB END. REPLACED RT AILERON TAB MM 27-11.
- [SDR 371PA0071](https://openairdocs.org/sdr/371PA0071.md): Floorbeam · corroded · Sep 20, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > FWD CABIN FLOORBEAM AT BS 294.5 HAS CORROSION FROM LBL 12 TO RBL 45. REPAIRED PER SRM 53-10-51.
- [SDR 371PA0070](https://openairdocs.org/sdr/371PA0070.md): Skin · cracked · Sep 20, 2004 · N371PA · Boeing 737306 · Fuselage Main, Plate/Skin
  > R1 DOOR CUT OUT, LOWER AFT CORNER HAS SUSPECT CRACK, VERIFIED BY HFEC. REPAIRED IAW SRM 53-10-01.
- [SDR 371PA0062](https://openairdocs.org/sdr/371PA0062.md): Frame · cracked · Sep 20, 2004 · N371PA · Boeing 737306 · Fuselage Main, Frame
  > FRAME CRACKED AT RIVET AT BS 500 AND STR 25LT. REPAIRED IAW SRM 51-70-11.
- [SDR 371PA0061](https://openairdocs.org/sdr/371PA0061.md): Attach Angle · cracked · Sep 20, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > ATTACH ANGLE CRACKED AT BS 807 AND RBL 20. REPLACED ANGLE IAW SRM 53-60-15 AND SRM 51-40-02.
- [SDR 371PA0059](https://openairdocs.org/sdr/371PA0059.md): Transition Panel · broken · Sep 20, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > TRANSITION PANEL AT APU BLEED DUCT AT BS 767 BROKEN. REPLACED PANEL IAW SRM 51-20-1 AND SRM 51-40-1.
- [SDR 371PA0053](https://openairdocs.org/sdr/371PA0053.md): Angle · corroded · Sep 20, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > THRESHOLD Z-ANGLE AT L2 DOOR HAS CORROSION AT CLIP NUT HOLES. REPLACED Z-ANGLE PER DWG. 65-52878497.
- [SDR 371PA0078](https://openairdocs.org/sdr/371PA0078.md): Strap · corroded · Sep 18, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > STRAP ON PREVIOUS BLEND OUT ON FLOORBEAM AT BS 328 AT LBL 12 HAS CORROSION. REMOVED STRAP AND REPAIRED FLOORBEAM PER SRM 53-10-51.
- [SDR 371PA0076](https://openairdocs.org/sdr/371PA0076.md): Intercostal · corroded · Sep 18, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FROM BS 312 TO BS 328 AT LBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2.
- [SDR 371PA0074](https://openairdocs.org/sdr/371PA0074.md): Strap · broken · Sep 18, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > STRAP ON LOWER SIDE OF FLOORBEAM AT BS 312 TO BS 328 AT RBL 45 BROKEN. REPLACED STRAP IAW SRM 51-10-2.
- [SDR 371PA0073](https://openairdocs.org/sdr/371PA0073.md): Intercostal · corroded · Sep 18, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL HAS CORROSION AT BS 294 TO BS 312 AT RBL 12. REPLACED INTERCOSTAL IAW SRM.
- [SDR 371PA0054](https://openairdocs.org/sdr/371PA0054.md): Floorbeam · corroded · Sep 18, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 344 HAS CORROSION FROM LBL 40 TO RBL 20. REPAIRED IAW SRM 53-10-51.
- [SDR 371PA0083](https://openairdocs.org/sdr/371PA0083.md): Floorbeam · corroded · Sep 17, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 967 CORRODED AT LBL 18. REPAIRED IAW SRM 53-00-51.
- [SDR 371PA0072](https://openairdocs.org/sdr/371PA0072.md): Intercostal · corroded · Sep 17, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FROM BS 1006 TO BS 1016 AT RBL 37 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL IAW SRM 51-40-1.
- [SDR 371PA0079](https://openairdocs.org/sdr/371PA0079.md): Intercostal · corroded · Sep 16, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 328 TO BS 344 AT RBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2.
- [SDR 371PA0077](https://openairdocs.org/sdr/371PA0077.md): Intercostal · corroded · Sep 16, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FROM BS 328 TO BS 344 AT LBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2.
- [SDR 371PA0069](https://openairdocs.org/sdr/371PA0069.md): Intercostal · corroded · Sep 16, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FROM BS 966 TO BS 986 AT RBL 18 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL IAW SRM 51-30-00.
- [SDR 371PA0065](https://openairdocs.org/sdr/371PA0065.md): Frame · cracked · Sep 16, 2004 · N371PA · Boeing 737306 · Fuselage Main, Frame
  > FRAME CRACKED AT RIVET AB BS 460 AND STR 25 LT. REPAIRED IAW SRM 51-70-11.
- [SDR 371PA0064](https://openairdocs.org/sdr/371PA0064.md): Frame · cracked · Sep 16, 2004 · N371PA · Boeing 737306 · Fuselage Main, Frame
  > FRAME CRACKED IN RADIUS AT BS 480 AND STR 25 LT. REPAIRED PER SRM 51-70-11.
- [SDR 371PA0082](https://openairdocs.org/sdr/371PA0082.md): Floorbeam · corroded · Sep 15, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 967 CORRODED ON THE AFT SIDE AT RBL 18. REPAIRED FLOORBEAM IAW SRM 53-00-51.
- [SDR 371PA0075](https://openairdocs.org/sdr/371PA0075.md): Floorbeam · corroded · Sep 15, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 312 FROM RBL 9 TO LBL 34 HAS CORROSION. REPAIRED IAW SRM 51-10-51 AND SRM 53-10-51.
- [SDR 371PA0052](https://openairdocs.org/sdr/371PA0052.md): Floorbeam · corroded · Sep 15, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 986 HAS CORROSION AT CLIP NUT HOLES FROM LBL 36 TO RBL 36. REPAIRED PER SRM 53-00-51.
- [SDR 371PA0081](https://openairdocs.org/sdr/371PA0081.md): Scuff Plate · cracked · Sep 14, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUT OUT FWD AND AFT SCUFF PLATES CRACKED. REPAIRED IAW MFG PROCESS SPEC. 5975 AND 8.6.
- [SDR 371PA0068](https://openairdocs.org/sdr/371PA0068.md): Floorbeam · corroded · Sep 14, 2004 · N371PA · Boeing 737306 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 946 HAS CORROSION AT CLIP NUT HOLES FROM LBL 18 TO RBL 18. REPAIRED PER SRM 53-00-51 AND SRM 53-60-51.
- [SDR 371PA0067](https://openairdocs.org/sdr/371PA0067.md): Scuff Plate · cracked · Sep 14, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > FWD AND AFT SCUFF PLATES OF FWD CARGO DOOR CUTOUT CRACKED IN RADIUS. REPAIRED IAW MFG PROCESS SPEC. 5975, 8.6.
- [SDR 371PA0066](https://openairdocs.org/sdr/371PA0066.md): Angle · corroded · Sep 13, 2004 · N371PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > CORROSION ON RIGHT TRANSIT IN ANGLE BETWEEN BS 867 AND BS 902. REPAIRED IAW SRM 53-60-53 AND SRM 51-10-02.

Next page: https://openairdocs.org/deregistered/N371PA-2006-12-06/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 = 'N371PA' AND deregistration_id = 'N371PA-2006-12-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N371PA-2006-12-06/reports

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