# Service difficulty reports: N372PA, cancelled Dec 6, 2006

A list on [N372PA, cancelled Dec 6, 2006](https://openairdocs.org/deregistered/N372PA-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 · 84 reports

- [SDR PIDA06027](https://openairdocs.org/sdr/PIDA06027.md): Window Post · cracked · Feb 24, 2006 · N372PA · Boeing 737306 · Fuselage Main, Structure
  > LEFT SIDE COCKPIT WINDOW POST CRACKED AT THE UPPER OUTBOARD CORNER. REPAIRED PER SRM 53-10-01 FIGURE 201 DETAIL II.
- [SDR PIDA06025](https://openairdocs.org/sdr/PIDA06025.md): Structure · cracked · Feb 24, 2006 · N372PA · Boeing 737306 · Nacelle/Pylon Miscellaneous Structure
  > LEFT ENGINE PYLON PANEL 5724 LT HAS A SMALL CRACK AT THE EDGE OF THE CUTOUT. REPAIRED CRACK IN THE UPPER FORWARD CORNER OF THE CUTOUT PER BOEING SB 737-54-1032.
- [SDR PIDA06024](https://openairdocs.org/sdr/PIDA06024.md): Structure · cracked · Feb 20, 2006 · N372PA · Boeing 737306 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON OUTBOARD MID ACCESS CUTOUT FOR PANEL 5824R IS CRACKED AT THE UPPER FORWARD AND LOWER AFT CORNERS. REPAIRED PER BOEING SB 737-54-1032.
- [SDR PIDA06023](https://openairdocs.org/sdr/PIDA06023.md): Fairing · cracked · Feb 17, 2006 · N372PA · Boeing 737306 · Wing, Plate/Skin
  > FAIRING ON TOP OF LEFT WING AT NR 3 FLAP TRACK HAS A CRACK AT THE FORWARD EDGE. REPLACED FAIRING PER SRM 51-00-05 AND 51-40-02.
- [SDR PIDA20050063](https://openairdocs.org/sdr/PIDA20050063.md): Lamp · inoperative · Aug 9, 2005 · N372PA · Boeing 737306 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT ON EXTERIOR OF FUSELAGE INOP. RELAMPED L1 DOOR EXTERIOR LIGHT PER MM 33-50. OPS CHECKS GOOD.
- [SDR 372PA0080](https://openairdocs.org/sdr/372PA0080.md): Light · inoperative · Mar 24, 2005 · N372PA · Boeing 737306 · Emergency Lighting
  > RIGHT BULL NOSE EMERGENCY LIGHT (OVERHEAD BAGGAGE BIN) INOP. REPLACED EXIT LIGHT, OPS CHECKS GOOD.
- [SDR 372PA0079](https://openairdocs.org/sdr/372PA0079.md): Bulb · inoperative · Nov 9, 2004 · N372PA · Boeing 737306 · Emergency Lighting
  > L2 DOOR EMERGENCY LIGHT INOP AND LENS CRACKED. REPLACED BULB AND LENS. OPS CHECKS NORMAL.
- [SDR 372PA0055](https://openairdocs.org/sdr/372PA0055.md): Floorbeam · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM AT BS 947 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 46 TO RBL 46. REPLACED T-CAP PER SRM 53-00-51 AND SRM 53-60-51.
- [SDR 372PA0052](https://openairdocs.org/sdr/372PA0052.md): Pan · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > AFT LAV SERVICE PANEL PAN HAS CORROSION AROUND DUMP SHOOT CONNECTION. REPLACED CORRODED CHANNELS P/N 69-36677-1 AND 69-36677-2 PER SRM 51-40-02 AND DRAWING 65-45781. REMOVED MINOR CORROSION FROM PAN PER SRM 51-20-01 AND SRM 51-40-00.
- [SDR 372PA0078](https://openairdocs.org/sdr/372PA0078.md): Frame · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Frame
  > FRAME CRACKED IN RADIUS AT BS 480 AT STR 25 LT. REPAIRED PER SRM 51-70-11.
- [SDR 372PA0077](https://openairdocs.org/sdr/372PA0077.md): Frame · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Frame
  > FRAME CRACKED IN RADIUS AT BS 460 AT STR 25 LT. REPAIRED PER SRM 51-70-11.
- [SDR 372PA0076](https://openairdocs.org/sdr/372PA0076.md): Angle · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > DRAG ANGLE CRACKED ABOVE RIGHT RAM AIR INLET. REPLACED ANGLE PER EA 53-235.
- [SDR 372PA0074](https://openairdocs.org/sdr/372PA0074.md): Frame · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Frame
  > AFT CARGO AFT FRAME AT BS 847 AT STR 23 RT DOOR STOP ATTACH FITTING CRACKED. REPLACED FITTING PER SRM 51-10-2.
- [SDR 372PA0073](https://openairdocs.org/sdr/372PA0073.md): Intercostal · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL FROM BS 328 TO BS 344 AT RBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2.
- [SDR 372PA0072](https://openairdocs.org/sdr/372PA0072.md): Strap · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Floor Beam
  > STRAP ON LOWER SURFACE OF FLOORBEAMS CRACKED AT BS 312 AND BS 344 AT BL 0. REPLACED STRAP IAW SRM 51-10-2.
- [SDR 372PA0071](https://openairdocs.org/sdr/372PA0071.md): Strap · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Floor Beam
  > STRAP CRACKED ON LOWER SURFACE OF FLOORBEAMS AT BS 312 AND BS 344 AT RBL 32. REPLACED STRAP IAW SRM 51-10-2.
- [SDR 372PA0070](https://openairdocs.org/sdr/372PA0070.md): Attach Angle · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ATTACH ANGLE CRACKED AFT SIDE OF BS 344 FLOORBEAM AT LBL 12. REPLACED ANGLE PER SRM 53-10-51, SRM 51-20-01 AND SRM 51-40-00.
- [SDR 372PA0069](https://openairdocs.org/sdr/372PA0069.md): Floorbeam · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Floor Beam
  > SEVERAL AREAS OF CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 344. REPLACED SECTION OF (T) CAP IAW SRM 53-10-51.
- [SDR 372PA0068](https://openairdocs.org/sdr/372PA0068.md): Floorbeam · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Floor Beam
  > UPPER SURFACE OF FLOORBEAM AT BS 312 HAS SEVERAL AREAS OF CORROSION. REPLACED SECTION OF T-CAP PER SRM 53-10-51.
- [SDR 372PA0067](https://openairdocs.org/sdr/372PA0067.md): Floorbeam · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Floor Beam
  > UPPER SURFACE OF FLOORBEAM AT BS 294 HAS SEVERAL AREAS OF CORROSION. REPLACED T-CAP PER SRM 53-10-51 AND SRM 51-10-2.
- [SDR 372PA0066](https://openairdocs.org/sdr/372PA0066.md): Web · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > CLOSE OUT WEB ON FWD FRAME AT BS 794 HAS CORROSION FROM STR 25 RT TO STR 23 RT. REPLACED WEB PER SRM 53-60-15 AND SRM 51-70-13.
- [SDR 372PA0065](https://openairdocs.org/sdr/372PA0065.md): Seat Track · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 45 CORRODED IN NUMEROUS PLACES FROM BS 328 TO BS 480. REPLACED SEAT TRACK PER SRM 51-10-02, SRM 53-00-52, AND DWG 65-46814.
- [SDR 372PA0064](https://openairdocs.org/sdr/372PA0064.md): Support Angle · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > AFT CARGO BIN BS 767 AT STR 19 LT UPPER SIDE WALL PANEL SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-02.
- [SDR 372PA0063](https://openairdocs.org/sdr/372PA0063.md): Web · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > FWD CARGO BIN WEB FROM BS 460 TO BS 480 AT STR 25 LT CRACKED. REPLACED INTERCOSTAL WEB PER SRM 51-10-02 AND SRM 51-20-01.
- [SDR 372PA0062](https://openairdocs.org/sdr/372PA0062.md): Failsafe · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Structure
  > FAILSAFE LINK BETWEEN BS 967 AND BS 986.5 AT LBL 46 CORRODED. REPLACED FAILSAFE LINK PER SRM 51-10-2.
- [SDR 372PA0061](https://openairdocs.org/sdr/372PA0061.md): Stringer · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Longeron/Stringer
  > LOWER LOBE STR 26 RT CORRODED FROM BS 1006 TO BS 1016. REPLACED SECTION OF STRINGER PER DRAWING 65-45776-8 AND SRM 51-10-2.
- [SDR 372PA0060](https://openairdocs.org/sdr/372PA0060.md): Strap · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > FLOORBEAM STRAP AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES FROM RBL 7 TO LBL 7. REPLACED STRAP PER SRM 51-10-2 AND SRM 51-40-0.
- [SDR 372PA0059](https://openairdocs.org/sdr/372PA0059.md): Galley Track · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage, Seat/Cargo Attach Fittings
  > GALLEY SUPPORT AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES AT BL 0. REPLACED GALLEY SUPPORT PER SRM 51-10-2 AND SRM 51-40-00.
- [SDR 372PA0058](https://openairdocs.org/sdr/372PA0058.md): Floorbeam · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM AT BS 986.5 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 45 TO RBL 45. REPLACED T-CAP PER EA 53-234.
- [SDR 372PA0057](https://openairdocs.org/sdr/372PA0057.md): Intercostal · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL HAS CORROSION, AFT CABIN BS 967 TO BS 986.5 AT RBL 18. REPLACED INTERCOSTAL PER SRM 51-10-01.
- [SDR 372PA0056](https://openairdocs.org/sdr/372PA0056.md): Intercostal · corroded · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > INTERCOSTAL HAS CORROSION, AFT CABIN FROM BS 967 TO BS 986.5 AT LBL18. REPLACED INTERCOSTAL PER SRM 51-10-01.
- [SDR 372PA0054](https://openairdocs.org/sdr/372PA0054.md): Attach Angle · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > SIDEWALL ATTACH ANGLE CRACKED AT BS 767 LBL 54. REPLACED ANGLE PER SRM 51-10-02.
- [SDR 372PA0053](https://openairdocs.org/sdr/372PA0053.md): Skin · damaged · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage Main, Plate/Skin
  > OUTFLOW VALVE CUTOUT DOUBLER AT BS 986 BETWEEN STR 23 RT AND STR 24 RT HAS CORROSION. REPLACED DOUBLER PER SRM 51-20-01.
- [SDR 372PA0051](https://openairdocs.org/sdr/372PA0051.md): Acoustic Liner · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE FWD ACOUSTICAL PANEL AT 6 O'CLOCK POSITION CRACKED. REPLACED PANEL PER MM 72-33-02.
- [SDR 372PA0050](https://openairdocs.org/sdr/372PA0050.md): Seat Track · damaged · Sep 9, 2004 · N372PA · Boeing 737306 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGED AT BS 470 AT RBL 24. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 53-00-52.
- [SDR 372PA0049](https://openairdocs.org/sdr/372PA0049.md): Angle · cracked · Sep 9, 2004 · N372PA · Boeing 737306 · Nacelle/Pylon Miscellaneous Structure
  > ANGLE CRACKED ON I/B SIDE OF LEFT PYLON AT THE I/B CUTOUT FOR THE MID FLAP TORQUE TUBE. REPLACED ANGLE PER SRM 51-10-02.
- [SDR 372PA0048](https://openairdocs.org/sdr/372PA0048.md): Switch · out of adjust · Jul 19, 2004 · N372PA · Boeing 737306 · Leading Edge Slat Position Indicating System
  > LEADING EDGE FLAPS TRANSIT LIGHT AND CONFIGURATION HORN ON DURING TAKEOFF, BELOW 80 KTS. REJECTED TAKEOFF. CHECKED FLAP INDICATION SYSTEM AND ADJUSTED NR 1 LEADING EDGE FLAP SWITCH. SYSTEM OPERATES NORMAL.
- [SDR 372PA0047](https://openairdocs.org/sdr/372PA0047.md): Computer · failed · Jul 16, 2004 · N372PA · Boeing 737306 · Autopilot System
  > FIRST OFFICER'S FLIGHT DIRECTOR INOPERATIVE AND SPEED TRIM FAIL AND MACH TRIM LIGHTS ILLUMINATED ON RECALL DURING LANDING CHECKS (SINGLE CHANNEL FAILURE). REPLACED B-CHANNEL FCC. BITE TEST AND OPS CHECKS NORMAL PER MM 22-10.
- [SDR 372PA0046](https://openairdocs.org/sdr/372PA0046.md): Battery Pack · inoperative · Jul 6, 2004 · N372PA · Boeing 737306 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT INOP. REPLACED RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-00.
- [SDR 372PA0045](https://openairdocs.org/sdr/372PA0045.md): Computer · malfunctioned · Jun 5, 2004 · N372PA · Boeing 737306 · Auto Throttle System
  > AUTO THROTTLE DISENGAGES IN LEVEL FLIGHT. WILL NOT RE-ENGAGE. REPLACED AUTO THROTTLE COMPUTER. OPS CHECK AND BITE TEST OK. REF ATA 22-30.
- [SDR 372PA0044](https://openairdocs.org/sdr/372PA0044.md): Actuator · shorted · Apr 7, 2004 · N372PA · Boeing 737306 · Autopilot System
  > DFCS HISTORY SHOWS AUTO-PILOT TRIM SERVO HAS NO RESPONSE. AUTO-PILOT COLUMN SWITCHING MODULE CHECKS OK PER MM 27-41-00. FOUND OPEN IN AUTO-PILOT STABILIZER TRIM ACTUATOR. REPLACED AUTO-PILOT STABILIZER TRIM SERVO AND OPS CHECKED PER MM 22-11-81.
- [SDR 372PA0043](https://openairdocs.org/sdr/372PA0043.md): Computer · malfunctioned · Mar 21, 2004 · N372PA · Boeing 737306 · Auto Throttle System
  > AUTO THROTTLE WILL NOT ARM. RELEASED ON MEL 22-4. 03/23/2004: REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-10. BITE CHECKS GOOD.
- [SDR 372PA0041](https://openairdocs.org/sdr/372PA0041.md): Light · inoperative · Feb 16, 2004 · N372PA · Boeing 737306 · Emergency Lighting
  > AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. DRIED MOISTURE FROM FLOOR PATH LIGHTING AND OPS CHECKED OK.
- [SDR 372PA0042](https://openairdocs.org/sdr/372PA0042.md): Light · contaminated · Feb 12, 2004 · N372PA · Boeing 737306 · Emergency Lighting
  > FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. CLEANED AND DRIED WATER FROM TRACK AND CONTACTS. OPS CHECKS NORMAL.
- [SDR 372PA0040](https://openairdocs.org/sdr/372PA0040.md): Computer · malfunctioned · Jan 10, 2004 · N372PA · Boeing 737306 · Auto Throttle System
  > AUTOTHROTTLE DISCONNECTED ON TAKEOFF AND INITIAL CLIMB THROUGH 16,000. PLACED ON MEL 22-4. REPLACED AUTOTHROTTLE COMPUTER PER MM 22-31-10. OPS CHECKS NORMAL.
- [SDR 372PA0039](https://openairdocs.org/sdr/372PA0039.md): Syncronizer · out of adjust · Jan 6, 2004 · N372PA · Boeing 737306 · Auto Throttle System
  > AUTO THROTTLES DISENGAGED ON TAKE OFF ROLL. ADJUSTED PLA SYNCHRO. OPS NORMAL IAW MM 22-31-00.
- [SDR 372PA0038](https://openairdocs.org/sdr/372PA0038.md): Connector · dirty · Oct 24, 2003 · N372PA · Boeing 737306 · Autopilot System
  > AUTO PILOT B WILL NOT ENGAGE AND AUTO PILOT A IS INTERMITTENT. REMOVED DIRT FROM AUTO PILOT A AND AUTO PILOT B CONNECTORS. A AND B SYSTEMS TEST OK IAW MM 22-10-00.
- [SDR 372PA0037](https://openairdocs.org/sdr/372PA0037.md): Power Unit · inoperative · Oct 23, 2003 · N372PA · Boeing 737306 · Emergency Lighting
  > RIGHT OVERWING EXIT LOWER LUMINESCENT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT POWER UNIT PER MM 33-51-51. OPS CHECKS NORMAL.
- [SDR 372PA0036](https://openairdocs.org/sdr/372PA0036.md): Power Supply · inoperative · Oct 22, 2003 · N372PA · Boeing 737306 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY/BATTERY CHARGER PER MM 33-51-51. OPS CHECKS OK.
- [SDR 372PA0075](https://openairdocs.org/sdr/372PA0075.md): Angle · cracked · Sep 9, 2003 · N372PA · Boeing 737306 · Fuselage Miscellaneous Structure
  > DRAG ANGLE CRACKED ABOVE LEFT RAM AIR INLET. REPLACED ANGLE PER EA 53-235.

Next page: https://openairdocs.org/deregistered/N372PA-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 = 'N372PA' AND deregistration_id = 'N372PA-2006-12-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N372PA-2006-12-06/reports

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