# Service difficulty reports: Boeing 737-2T5

A list on [Boeing 737-2T5](https://openairdocs.org/model/boeing-737-2t5.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA030417011](https://openairdocs.org/sdr/CA030417011.md): Pcu · inoperative · Apr 15, 2003 · Boeing 7372T5 · Aileron Control System
  > (CAN) AFTER PUSHBACK AND START, FLAP 2 SELECTED AND HYDRAULIC SYSTEM A LOW PRESSURE ILLUMINATED AND HYD QTY GUAGE DECREASED TO ZERO. MAINTENANCE FOUND THE A SYSTEM AILERON POWER CONTROL UNIT (PCU) FILTER BOWL HAD FRACTURED RESULTING IN LOSS OF HYD PRESS/FLUID.
- [SDR CA030225003](https://openairdocs.org/sdr/CA030225003.md): Oxygen Mask · misinstalled · Feb 23, 2003 · Boeing 7372T5 · Passenger Oxygen System
  > (CAN) A/C EXPERIENCED RAPID DEPRESSURIZATION. CLIMBED TO 15,000 FT IN APPROX 5-10 SECONDS. O2 SYS DEPLOYED AUTOMATIC. STANDBY MODE DID NOT OPERATE NORMALLY BUT CABIN PRESSURE WAS RECAPTURED. DURING EMER DESCENT WITH MANUAL MODE MAINT REPLACED CABIN PRESSUR
- [SDR CA030121007](https://openairdocs.org/sdr/CA030121007.md): Bearing · Jan 9, 2003 · Boeing 7372T5 · Leading Edge Slat Control System
  > (CAN) LOG SNAG - ON FLAP SELECTION TO ONE UNIT, LE FLAP TRANSIT LIGHT REMAINED ON. NO. 4 SLAT REMAINED AMBER. ALL OTHERS GREEN. ON SELECTION OF FLAP 10, NO. 4 WENT GREEN FULL EXTEND WITH OTHER LE DEVICES.THE MAINTENANCE MECHANICS DISCOVERED THE NO. 4 LE SLAT O
- [SDR CA030106004](https://openairdocs.org/sdr/CA030106004.md): Connector · burned · Jan 3, 2003 · Boeing 7372T5 · Flight Control System Wiring
  > (CAN) ON OVERNIGHT CHECK OF AUTO PILOT STAB TRIM, C/B FOUND TRIPPED AND UNABLE TO RESET. SMOKE NOTED IN STAB COMPARTMENT AND UPON INVESTIGATION FOUND CONNECTOR AND 3 INCHES OF ASSOCIATED WIRING DAMAGED ATA/P STAB TRIM MOTOR CONNECTION. WIRING REPAIRED, CONN
- [SDR CA030103020](https://openairdocs.org/sdr/CA030103020.md): Connector · burned · Jan 2, 2003 · Boeing 7372T5 · Stabilizer Actuator
  > (CAN) DURING OVERNIGHT CHECK IN THE HANGER, AVIONICS FOUND THE A/P STAB TRIM MOTOR C/B WAS POPPED. TRIED A RESET BUT NO JOY AND C/B FELT ODD. TURNED A/C POWER OFF AND C/B WOULD NOT RESET. C/B REPLACED. C/B RESET BUT POPPED A FRACTION OF A SECOND LATER. AVION
- [SDR CA030121003](https://openairdocs.org/sdr/CA030121003.md): Bearing · loose · Jan 1, 2003 · Boeing 7372T5 · Leading Edge Slat Actuator
  > (CAN) ON 9 JAN 2003 IT WAS FOUND THAT THE ROLLER BEARING ON THE NR 5 SLAT OUTBOARD TRACK HAD BECOME DETACHED AND THE CONTROL ARM HAD WORN THROUGH THE TOP WING SKIN FORWARD OF THE FRONT SPAR. UPON REMOVAL OF THE ACCESS PANEL ALL THE PARTS WERE FOUND INSIDE INCL
- [SDR P2EA2001M0004](https://openairdocs.org/sdr/P2EA2001M0004.md): Computer · Sep 23, 2001 · N120NJ · Boeing 7372T5 · Autopilot System
  > Auto Pilot twitches in pitch on VG1. Auto Pilot pulls back on controls continuiously when operated on system "A". Corrective action: Removed and replaced Pitch Computer IAW MM 22-11-151A, operatoinal check normal. See A/C 120 Log pages 92743 and 92744. This re
- [SDR P2EA2001M0006](https://openairdocs.org/sdr/P2EA2001M0006.md): Control Panel · Sep 22, 2001 · N120NJ · Boeing 7372T5 · Autopilot System
  > Heading Hold will not hold heading with Auto Pilot in B channnel. Corrective action: Deffered Heading Hold per MEL 22-1, CI#M120076 per MX CNTL Mic. Replaced Mode Control Panel, operational check normal IAW MM 22-11-191, This clears CI#M120079. See A/C 120 Log
- [SDR P2EA2001M0003](https://openairdocs.org/sdr/P2EA2001M0003.md): Gyro · faulty · Sep 21, 2001 · N120NJ · Boeing 7372T5 · Attitude Gyro and Indicating System
  > AUTO PILOT ON HDG2 HOLD WILL NOT MAINTAIN BANK AND ROLL LEVEL AND OCCASIONALLY JERKS ABRUPTLY. REPLACED NR 1 VERTICAL GYRO PER MM 34-22-11, OPERATIONAL CHECK OKAY.
- [SDR P2EA01167](https://openairdocs.org/sdr/P2EA01167.md): Skin · cracked · Aug 20, 2001 · N120NJ · Boeing 7372T5 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, RIGHT WING OUTBOARD MID FLAP WBL 304.5, SKIN WITH CRACK. RIGHT WING OUTBOARD MID FLAP L/E OF CENTER TRACK CAVITY SKIN SECTION REPAIRED IAW COOPESA EO NR COO-3-57-452-01. (M)
- [SDR P2EA01162](https://openairdocs.org/sdr/P2EA01162.md): Skin · dented · Aug 18, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > SJO - DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 500A PLUS 12, BETWEEN STRINGER 1 AND STRINGER 2L. REPAIRED FUSELAGE SKIN SECTION FROM BS 500A PLUS 7 INCHES TO 500B, BETWEEN STRINGER 2 LEFT AND STRINGER 2 RIGHT DUE TO DENT IAW SRM 53-30-3 FI
- [SDR P2EA01163](https://openairdocs.org/sdr/P2EA01163.md): Cargo Track · corroded · Aug 15, 2001 · N120NJ · Boeing 7372T5 · Fuselage, Seat/Cargo Attach Fittings
  > DURING Q-CHECK, FOUND FORWARD CARGO COMPARTMENT FROM BS 380 TO BS 520 LBL 18.5, CARGO TRACK WITH CORROSION. (M)
- [SDR P2EA01164](https://openairdocs.org/sdr/P2EA01164.md): Floor Support · corroded · Aug 15, 2001 · N120NJ · Boeing 7372T5 · Fuselage Miscellaneous Structure
  > DURING Q-CHECK, AFT CARGO COMPARTMENT BETWEEN BS 767 AND BS 847 AT STRINGER 25 RIGHT FLOOR SUPPORT WITH CORROSION. (M)
- [SDR P2EA01156](https://openairdocs.org/sdr/P2EA01156.md): Doubler · cracked · Aug 14, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > SJO - DURING Q-CHECK, EXTERNAL FUSELAGE DOUBLER WITH CRACK AT BS 1138, WL 266 LEFT SIDE. (M)
- [SDR P2EA01159](https://openairdocs.org/sdr/P2EA01159.md): Skin · canning · Aug 13, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > DURING Q-CHECK, FOUND EXTERNAL FUSELAGE WITH OIL CAN AT BS 901, BETWEEN STRINGER 21 AND 22 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 898.5 TO BS 902.5 BETWEEN STRINGER 21 AND 22 RT DUE TO OIL CAN IAW SRM 53-30-3, FIG 05. (M)
- [SDR P2EA01158](https://openairdocs.org/sdr/P2EA01158.md): Stringer · dented · Aug 12, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Longeron/Stringer
  > SJO - DURING Q-CHECK, LOWER FUSELAGE TAIL CONE STRINGER 27 LEFT WITH DENT AT BS 1035. REPAIRED STRINGER 27 LEFT FROM BS 1032 TO BS 1045 DUE TO DENT IAW SRM 53-10-3, FIG 01. (M)
- [SDR P2EA01157](https://openairdocs.org/sdr/P2EA01157.md): Bulkhead · cracked · Aug 10, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Bulkhead
  > DURING Q-CHECK INSPECTION PER S/B 737-53A1173, FOUND PRESSURE BULKHEAD BS 178, WEB CRACKED AT RBL 11.5-WL 213, PRESSURE BULKHEAD BS 178 FLOOR WEB SECTION CRACKED AT SL 207, PRESSURE BULKHEAD BS 178 LEFT SIDE LATERAL CHORD CRACKED AT WL 207, PRESSURE BULKHEAD B
- [SDR P2EA01151](https://openairdocs.org/sdr/P2EA01151.md): Frame · cracked · Aug 9, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Frame
  > DURING Q-CHECK, FUSELAGE AFT CARGO COMPARTMENT AT FRAME BS 807, BETWEEN STRINGER 27 LEFT AND 27 RIGHT, LOWER SECTION WITH CRACK. S/D - REPAIRED FRAME SECTION AT BS 807 BETWEEN STRINGER 27 RIGHT AND STRINGER LEFT DUE TO CRACK IAW SRM 53-10-4, FIG 06. (M)
- [SDR P2EA01154](https://openairdocs.org/sdr/P2EA01154.md): Skin · dented · Aug 8, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > DURING Q-CHECK, FOUND EXTERNAL SKIN WITH DENT AT BS 500A PLUS 12 INCHES, BETWEEN STRINGER 1 AND 2 LEFT. (M)
- [SDR P2EA01153](https://openairdocs.org/sdr/P2EA01153.md): Skin · dented · Aug 8, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 590, STRINGER 1. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 590 TO BS 599 BETWEEN STRINGER 2 LEFT AND 2 RIGHT DUE TO DENT IAW SRM 53-30-3, FIG 7. (M)
- [SDR P2EA01150](https://openairdocs.org/sdr/P2EA01150.md): Skin · dented · Aug 6, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > DURING Q-CHECK, FOUND EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1040, BETWEEN STRINGER 27 LEFT AND 27 RIGHT. S/D - REPAIRED FUSELAGE SKIN SECTION FROM BS 1030 TO BS 1057 BETWEEN STRINGER 27 RIGHT AND STRINGER 24 LEFT DUE TO DENT IAW SRM 53-30-3, FIG 06. (M)
- [SDR P2EA01145](https://openairdocs.org/sdr/P2EA01145.md): Skin · dented · Aug 6, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > DURING Q-CHECK, FOUND TWO DENTS RIGHT SIDE OF AFT OUT FLOW VALVE. REPAIRED FUSELAGE SKIN SECTION FROM BS 907 TO BS 922 BETWEEN STRINGER 21 RIGHT AND 23 RIGHT DUE TO DENTS IAW SRM 53-30-3, FIG 28. (M)
- [SDR P2EA01146](https://openairdocs.org/sdr/P2EA01146.md): Skin · dented · Aug 6, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 1051, BETWEEN STRINGER 16 LEFT AND 17 LEFT. REPAIRED FUSELAGE SKIN SECTION FROM BS 1047.5 TO BS 1055.5 BETWEEN STRINGER 16 LEFT AND 17 LEFT DUE TO DENT IAW SRM 53-30-3, FIG 19. (M)
- [SDR P2EA01152](https://openairdocs.org/sdr/P2EA01152.md): Floorbeam · corroded · Aug 5, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Floor Beam
  > SJO - DURING Q-CHECK, FOUND PAX CABIN AT BS 294, BETWEEN BL 0 AND RBL 40 INCHES, WL 208, UPPER SECTION AND BS 294.5 BETWEEN BL 0 AND LBL 30, FLOORBEAM WITH CORROSION. (M)
- [SDR P2EA01149](https://openairdocs.org/sdr/P2EA01149.md): Stringer · corroded · Aug 4, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Longeron/Stringer
  > DURING Q-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 968, STRINGER 27 RIGHT WITH CORROSION. S/D - REPAIRED STRINGER 27 RIGHT FROM BS 958.5 TO BS 976 DUE TO CORROSION IAW SRM 53-10-3, FIG 01. (M)
- [SDR P2EA01148](https://openairdocs.org/sdr/P2EA01148.md): Skin · dented · Aug 3, 2001 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > SJO - DURING Q-CHECK, EXTERNAL FUSELAGE SKIN WITH DENT AT BS 807, BETWEEN STRINGER 26 LEFT AND 27 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 789.5 TO BS 815 BETWEEN STRINGER 25 LEFT TO STRINGER 26 RT DUE TO DENT IAW SRM 53-30-3, FIG 06. (M)
- [SDR P2EA01122](https://openairdocs.org/sdr/P2EA01122.md): Indicator · inoperative · Jul 7, 2001 · N120NJ · Boeing 7372T5 · Air Conditioning System
  > MCI - FLT 350 - DURING CRUISE AT 33,000 FEET CABIN RATE OF CHANGE WAS PLUS 250 FEET PER MINUTE AND CABIN PRESSURE WAS AT 9,500 FEET AND SHOULD BE AT 800 FEET FOR NORMAL. STANDBY WAS SELECTED WITH NO IMPROVEMENT. DURING DESCENT WITH THROTTLES AT IDLE, CABIN R
- [SDR CA010522007](https://openairdocs.org/sdr/CA010522007.md): Csd · unreliable · May 1, 2001 · Boeing 7372T5 · AC Generation System
  > (CAN) AT FL 230, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. FLIGHT ELECTED TO RETURN DUE APU ELECTRICS WERE UNRELIABLE. REPLACED NR 1 CSD AS PER WORK CARD 1182-1. APU AND NR 1 CSD CHECKED SERVICEABLE DURING GROUND RUN.
- [SDR CA010404008](https://openairdocs.org/sdr/CA010404008.md): Windshield · leaking · Mar 18, 2001 · Boeing 7372T5 · Flight Compartment Windows
  > (CAN) CLIMBING THROUGH 13,000 FEET, APPROXIMATELY 4 PSI CABIN PRESSURE, CAPTS WINDSHIELD POPPED WITH A NOTICEABLE PRESSURIZATION LEAK. RETURNED. WINDOW INSPECTED, NO DEFECTS NOTED. WINDOW ATTACHED BOLTS WERE RETORQUED. AIRCRAFT PRESSURIZED TO 3 PSI, NO PRESSUR
- [SDR P2EA00221](https://openairdocs.org/sdr/P2EA00221.md): Gasper Fan · malfunctioned · Jul 12, 2000 · N120NJ · Boeing 7372T5 · Air Conditioning System
  > FLT 307 - MYR - SMOKE AND FUMES NOTED IN COCKPIT. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO MYR LANDING UNEVENTFUL. FOUND FAULTY GASPER FAN, DEFERRED PER MEL 21-24, CONTROL M120626 PER MX CONTROL. REMOVED AND REPLACED GASPER FAN PER MM 21-24-21, OPERATINO
- [SDR P2EA00212](https://openairdocs.org/sdr/P2EA00212.md): Control Cable · loose · Jul 11, 2000 · N120NJ · Boeing 7372T5 · Power Lever
  > MCI - FLT 589 - EMERGENCY DECLARED, NR 1 ENGINE SHUT DOWN 5 MINUTES BEFORE LANDING, AIRCRAFT RETURNED TO MCI, LANDING UNEVENTFUL. LOST THROTTLE CONTROL NR 1 ENGINE: EPR 2.09, N1 91 PERCENT, EGT 450, N2 91 PERCENT, AND FUEL FLOW NORMAL. FOUND LOOSE HARDWARE
- [SDR P2EA00202](https://openairdocs.org/sdr/P2EA00202.md): Skin · delaminated · Jun 2, 2000 · N120NJ · Boeing 7372T5 · Leading Edge Devices
  > YYC - DURING C-CHECK, RIGHT OUTBOARD FOREFLAP, REPAIR DELAMINATED ON UPPER SURFACE 87 INCHES OUTBOARD OF INBOARD END. REPAIRED FOREFLAP IAW SRM 51-40-6, PAGE 8 PARAGRAPH 11. (M)
- [SDR P2EA00203](https://openairdocs.org/sdr/P2EA00203.md): Skin · dented · Jun 1, 2000 · N120NJ · Boeing 7372T5 · Fuselage Main, Plate/Skin
  > YYC - DURING C-CHECK, FOUND DENT WITH SHARP CREASE AT BS 860, BETWEEN STRINGERS 15L AND 16L. REPAIRED DENT AT BS 860 BETWEEN STRINGERS 15L AND 16L IAW SRM 53-30-3, FIG 1. (M)
- [SDR CA000209003](https://openairdocs.org/sdr/CA000209003.md): Bolt · broken · Feb 1, 2000 · Boeing 7372T5 · Leading Edge Devices
  > (CAN) NR 4 SLAT BOLT BROKEN THROUGH GREASE PASSAGE DUE TO LACK OF LUBRICATION, BOLT WORN. REPLACED.
- [SDR P2EA99275](https://openairdocs.org/sdr/P2EA99275.md): Engine · bird strike · Sep 13, 1999 · N120NJ · Boeing 7372T5 · Engine (Turbine/Turboprop)
  > MDW - FLT 815 - ABORTED TAKEOFF, NO EMERGENCY DECLARED, RETURNED TO BLOCKS. AT APPROXIMATELY 100 KNOTS DURING TAKEOFF ROLL, INGESTED BIRD IN NR 1 ENGINE. (X)
- [SDR CA981125024](https://openairdocs.org/sdr/CA981125024.md): Sensor · malfunctioned · Nov 16, 1998 · Boeing 7372T5 · Landing Gear Position and Warning
  > (CAN) AT TOP OF DESCENT, RT RED GEAR WARNING LIGHT FLICKERED WITH GEAR SELECTED UP. REPLACED RT MLG UPLOCK SENSOR.
- [SDR CA970904013](https://openairdocs.org/sdr/CA970904013.md): Rod End Bearing · broken · Aug 18, 1997 · Boeing 7372T5 · Landing Gear Door Retract Section
  > (CAN) ROD END BEARING SHEARED AT NECK. DETACHED FROM MAIN LANDING GEAR PANEL. REPLACED.
- [SDR CA970327007](https://openairdocs.org/sdr/CA970327007.md): Line · failed · Mar 13, 1997 · Boeing 7372T5 · Hydraulic System, Main
  > (CAN) ONE HOUR OUT 'B' SYSTEM QTY LOSS, AIRCRAFT RETURNED. FOUND 'B' PUMP PRESSURE LINE FAILED. REPLACED.
- [SDR CA970318002](https://openairdocs.org/sdr/CA970318002.md): Bearing · failed · Feb 2, 1997 · Boeing 7372T5 · Wheel/Ski/Float
  > (CAN) ON LANDING CREW REPORTED NOSE WHEEL SHIMMY. INBOARD BEARING OF THE L/H WHEEL WAS FOUND TO HAVE FAILED. THE ROLLER AND CAGE ASSEMBLY DEPARTED THE AIRCRAFT AND THE SECTION IN CONTACT WITH THE AXEL WELDED ITSELF TO THE AXLE. SEVERAL PIECES OF THE BEARING

## 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 = '7372T5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-2t5/reports

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