# Service difficulty reports: Boeing 737-296

A list on [Boeing 737-296](https://openairdocs.org/model/boeing-737-296.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 60 reports

- [SDR CA050125007](https://openairdocs.org/sdr/CA050125007.md): Skin · cracked · Jan 21, 2005 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) AN OUTER FUSELAGE CRACK WAS FOUND DURING A PHASE EIGHT CHECK AT STRINGER 16L, STATION 727+14.5 APPROXIMATELY 1.5 INCHES IN LENGTH. FUSELAGE CRACK REPAIRED IAW REO-L00889 REV 1R TIMES - 59761:05 HOURS AND 54470 CYCLES
- [SDR CA041201004](https://openairdocs.org/sdr/CA041201004.md): Skin · cracked · Nov 29, 2003 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) TWO INCH CRACK WAS FOUND ON OUTER FUSELAGE BETWEEN STA 727A, 727B AT STR. 16L. FUSELAGE CRACK REPAIRED IAW SRM 53-30-3 FIG.48 SHEET 34 DETAIL XII. TIMES- 59472:22 CYCLES- 54285.
- [SDR CA031117003](https://openairdocs.org/sdr/CA031117003.md): Skin · cracked · Nov 11, 2003 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) 2.34 CRACK IN FUSELAGE TOP OF S18L BETWEEN BS 727A AND BS 727B. REPAIRED IAW SRM 53-30-3,FIG 48, SHEET 33, DETAIL XI REFERENCE PROCEDURE IV AND VII. AIRCRAFT TIME 56,880:17 CYCLES52,484 C
- [SDR CA031117002](https://openairdocs.org/sdr/CA031117002.md): Skin · cracked · Nov 11, 2003 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) 3 INCH CRACK IN FUSELAGE SKIN AFT OF REAR WING TO BODY FAIRING TOP OF 18L BETWEEN BS 747 - BS 767. REPAIRED SRM IAW 53-30-3 FIG 48 (SHEET 33) DETAIL XI, REF PROCEDURE IV AND VII. AIRCRAFT TIME 56,88:17CYCLES52,484 C
- [SDR CA021018004](https://openairdocs.org/sdr/CA021018004.md): Skin · cracked · Oct 17, 2002 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) TWO INCH CRACK FOUND ON FUSELAGE SKIN ABOVE STRINGER 16 LT, AT BODY STATION 787. CRACK REPAIR CARRIED OUT IAW SRM 53-30-3.
- [SDR CA020702005](https://openairdocs.org/sdr/CA020702005.md): Engine · leaking · Jun 29, 2002 · Boeing 737296 · Turbine Section
  > (CAN) NR 2 ENGINE HAD REPORT LOW OIL QUANTITY ON ARRIVAL. MAINTENANCE SERVICED ENGINE WITH 11 LITRES. OIL TRENDS DID NOT INDICATE HIGH CONSUMPTION. RAN ENGINE AND FOUND OIL SMOKE COMING FROM EXHAUST. RETURN OIL FILTER FOUND FOULED WITH CARBON. SUSPECT CARBON S
- [SDR CA020730007](https://openairdocs.org/sdr/CA020730007.md): Skin · cracked · Jun 27, 2002 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) TWO FATIGUE CRACKS FOUND IN RT FUSELAGE SKIN BETWEEN STA. 727A & 727B AND BETWEEN STR 14R & 19R ABOVE EXISTING REPAIR AT SAME LOCATION. ONE CRACK IS HORIZONTAL 1.5 INCHES AND OTHER VERTICAL 1 INCH LONG. EXISTING DOUBLER REMOVED AND REPAIR CARRIED OUT AS
- [SDR CA010727027](https://openairdocs.org/sdr/CA010727027.md): Clamp · Jul 5, 2001 · Boeing 737296 · Hydraulic Filter, Main
  > (CAN) HYDRAULIC LOSS OF SYSTEM A AFTER TAKE OFF, AIRCRAFT RETURNED. BROKEN CLAMP ON THE RETURN FILTER BOWL. NEW CLAMP INSTALLED, AND FILTER ELEMENT CHANGED.
- [SDR 2001F00149](https://openairdocs.org/sdr/2001F00149.md): Engine · damaged · Jul 5, 2001 · N232TA · Boeing 737296 · Engine (Turbine/Turboprop)
  > SAL - FLT TA220 - DURING INITIAL TAKEOFF, A STRONG NOISE WAS HEARD, WHEN APPLYING TAKEOFF TRUST, REJECTED THE TAKEOFF AND STRONG VIBRATION WAS FELT IN THE NR 2 ENGINE. ENGINE SHUTDOWN WAS ACCOMPLISHED, AIRCRAFT RETURNED TO GATE. DUE TO INTERNAL DAMAGES, ENGI
- [SDR CA010703002](https://openairdocs.org/sdr/CA010703002.md): Skin · cracked · Jun 11, 2001 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88 & 88A.
- [SDR CA010625004](https://openairdocs.org/sdr/CA010625004.md): Skin · cracked · Jun 11, 2001 · Boeing 737296 · Fuselage Main, Plate/Skin
  > (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L. REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88 & 88A.
- [SDR 2001F00081](https://openairdocs.org/sdr/2001F00081.md): Hose · leaking · Apr 16, 2001 · N232TA · Boeing 737296 · Pitot/Static System
  > FLT 410 - SAL - DURING CLIMB, THE CAPTAIN REPORTED THAT DURING INITIAL CLIMB THERE WAS A DIFFERENCE OF 100 FEET BETWEEN CAPTAIN AND FIRST OFFICER ALTIMETER, AT 17,000 FEET, THE DIFFERENCE INCREASE TO 1000 FEET AND WHEN LEVEL AT FL270, THE DIFFERENCE INCREASE T
- [SDR CA010502004](https://openairdocs.org/sdr/CA010502004.md): Module · defective · Apr 5, 2001 · Boeing 737296 · Trailing Edge Flap Control System
  > (CAN) AS THE POWER LEVERS WERE ADVANCED FOR TAKEOFF AT 1.2 EPR A WARNING HORN SOUNDED. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT PROCEEDED BACK TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP/SLAT POSITION ACCESSORY UNIT P/N 65-52807-26 S/N D00235.
- [SDR CA010105005](https://openairdocs.org/sdr/CA010105005.md): Bushing · damaged · Dec 21, 2000 · Boeing 737296 · Turbine Engine Accessory Drive
  > (CAN) A/C 732, NR 2 ENGINE SHUT DOWN DUE LOW OIL QUANTITY AND PRESSURE WARNING. FOUND BUSHING BANJO PULLED OUT FROM GEARBOX HOUSING. THREAD FAILURE CONFIRMED. WHEN ATTEMPTING REPAIR PER JT8D OVRHAUL MANUAL 72-61-01/8401 IT WADS FOUND THAT A VOID EXISTED IN THE
- [SDR CA010119003](https://openairdocs.org/sdr/CA010119003.md): Fitting · broken · Dec 17, 2000 · Boeing 737296 · Leading Edge Devices
  > (CAN) DURING INSPECTION THE LEFT OUTBOARD FORE FLAP ATTACHMENT BRACKET WAS FOUND CRACKED.
- [SDR 20001212SH001](https://openairdocs.org/sdr/20001212SH001.md): Line · damaged · Nov 26, 2000 · N232TA · Boeing 737296 · Altimeter, Barometric/Encoder
  > SAL - FLT TA-380 - AFTER TAKEOFF, THE FIRST OFFICER AIRSPEED INDICATOR WENT TO ZERO KNOTS AND FIRST OFFICER''S ALTIMETER HAD A READ-OUT OF 4,000 FEET AT FL 260. THE AIRCRAFT RETURNED TO EL SALVADOR STATION FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING AT SAL
- [SDR CA001201005](https://openairdocs.org/sdr/CA001201005.md): Indicator · inaccurate · Nov 12, 2000 · Boeing 737296 · Fuel Quantity Indicator
  > (CAN) LOG SEQUENCE 0154872. APPROXIMATELY 20 MINUTES FROM LANDING FUEL QUANTITY INDICATORS SHOWED 3000 POUND IMBALANCE. SUSPECTED A FUEL LEAK AND DECLARED AN EMERGENCY TO LAND. STOPPED ON RUNWAY AND CONFIRMED NO LEAK. MAINTENANCE FOUND NR 1 COCKPIT INDICATOR
- [SDR CA001107021](https://openairdocs.org/sdr/CA001107021.md): Controller · failed · Oct 17, 2000 · Boeing 737296 · Flight Compartment Windows
  > (CAN) CAPTAINS NR 2 SLIDING WINDOW - EXTERIOR PANE SHATTERED ON CLIMB OUT. WINDOW HEAT SHORTED RESULTING IN SPARKS AND SMOKE FROM ARCING.WINDOW AND CONTROLLER REPLACED. TEARDOWN REPORT CONFIRMED THE WINDOW HEAT CONTROL FAILED.
- [SDR CA001122003](https://openairdocs.org/sdr/CA001122003.md): Control Unit · failed · Sep 20, 2000 · Boeing 737296 · Aileron Control System
  > (CAN) EN ROUTE CREW REPORTED AILERONS WERE STIFF, BEYOND 5 DEGREES INPUT WITH AUTOPILOT SELECTED OFF. AUTOPILOT ON AILERONS WERE BETTER. AIRCRAFT TAKEN OUT OF SERVICE FOR TOURBLESHOOTING. AILERON POWER CONTROL UNIT RIGGING CARRIED OUT AS PER WORK CARD 51143, I
- [SDR CA000901004](https://openairdocs.org/sdr/CA000901004.md): Engine · overtemp · Aug 15, 2000 · Boeing 737296 · Engine (Turbine/Turboprop)
  > (CAN) AC 734, AUGUST 15/2000, YYZ, LOG SEQUENCE 0295891. AIR TURNBACK DUE NR 2 ENGINE EGT AT 520 DEGREES AFTER CLIMB. ON TAKEOFF, NR 2 EGT APPROACHED 590 DEGREES C. DUE TO HIGH EGT TREND NR 2 ENGINE REPLACED AS PER WORK CARD 1125-2. OFF CANADIAN PART NUMBER 7-
- [SDR 20001004AP002](https://openairdocs.org/sdr/20001004AP002.md): Control Box · inoperative · Jun 23, 2000 · N232TA · Boeing 737296 · Elevator Control System
  > SAL-MIA - FLT TA314 - DURING CRUISE, THE AIRCRAFT HAD PITCH OSCILLATIONS WITH AUTOPILOT ENGATED, DUE THIS SITUATION THE AIRCRAFT RETURNED TO SAL AIRPORT. AFTER UNEVENTFUL LANDING MAINTENANCE TECHNICIANS PERFORMED COMPLETE INSPECTION OF THE ELEVATOR SYSTEM AND
- [SDR CA000224015](https://openairdocs.org/sdr/CA000224015.md): Shaft · binding · Feb 15, 2000 · Boeing 737296 · Power Lever
  > (CAN) START LEVER STIFF AND SPONGY. FOUND ENGINE CROSS SHAFT BINDING. INNER AND OUTER CROSS SHAFT REPLACED.
- [SDR USAA000161](https://openairdocs.org/sdr/USAA000161.md): Skin · cracked · Feb 7, 2000 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > CLT - FOUND 2 CRACKS 1.75 INCH AND 1.5 INCH, LEFT FUSELAGE SKIN STATION 759 AND 781 AT STRINGER 17L. REPAIRED WITH DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA000162](https://openairdocs.org/sdr/USAA000162.md): Skin · cracked · Feb 7, 2000 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > CLT - FOUND 1 INCH SKIN CRACK LEFT FUSE SKIN BETWEEN STATION 763 AND 764, STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA991262](https://openairdocs.org/sdr/USAA991262.md): Skin · cracked · Nov 13, 1999 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A SECTION OF SKIN REMOVED TO GAIN ACCESS TO AFT PRESSURE BULKHEAD SKIN. INSTALLED DOUBLER PER BOEING DWG 65C28106 SHEET 1. (M)
- [SDR USAA991261](https://openairdocs.org/sdr/USAA991261.md): Bulkhead · corroded · Nov 13, 1999 · N238US · Boeing 737296 · Fuselage Main, Bulkhead
  > TPA - DURIGN CX-2 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA AFT PRESSURE BULKHEAD STATION 1016, LOWER CENTER FUSELAGE WEB AND STIFFENERS, CORROSION LEVEL 2. REPAIRED PER EA 65691 AND SB 737-53A1075 BOEING DWG 65C28106. (M)
- [SDR USAA991248](https://openairdocs.org/sdr/USAA991248.md): Skin · cracked · Nov 13, 1999 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH SKIN CRACK STATION 1156 BETWEEN STRINGER 2L AND 3L. INSTALLED DOUBLER PER SB 737-53-1095. (M)
- [SDR USAA990867](https://openairdocs.org/sdr/USAA990867.md): Aileron · missing · Aug 12, 1999 · N238US · Boeing 737296 · Ailerons
  > PIT - DURING FLIGHT THERE WAS A VIBRATION AND A PASSENGER NOTICED A PORTION OF THE RIGHT AILERON OUTBOARD END TRAILING EDGE COMING OFF OF AIRCRAFT. REPAIRED PER BOEING MANUAL 737-200 NR 27-11-11. (M)
- [SDR USAA990861](https://openairdocs.org/sdr/USAA990861.md): Skin · cracked · Aug 2, 1999 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > BOS - DURING RON, FOUND 1.25 INCH CRACK IN SKIN AT STRINGER 16L STATION 767. INSTALLED DOUBLER.080/2024T42 FASTENER 20426D5 PER SRM 53-30-3 FIG 6. (M)
- [SDR USAA990469](https://openairdocs.org/sdr/USAA990469.md): Skin · cracked · May 17, 1999 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 2.75 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT STRINGER 17R, 5 INCHES FORWARD OF STATION 727B FRAME. REMOVED DAMAGED MATERIAL, INSTALLED DOUBLER PER SRM 53-30-03. (M)
- [SDR USAA990468](https://openairdocs.org/sdr/USAA990468.md): Skin · cracked · May 17, 1999 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S18R, 2 INCH FORWARD OF STATION 727B FRAME. CRACK CUT OUT, INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 6 AND FIG 17. (M)
- [SDR USAA990467](https://openairdocs.org/sdr/USAA990467.md): Skin · cracked · May 17, 1999 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1.9 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S17R, 5 INCH FORWARD OF STATION 747 FRAME. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR 20000424AP011](https://openairdocs.org/sdr/20000424AP011.md): Fire Detector · malfunctioned · Mar 19, 1999 · N232TA · Boeing 737296 · Fire Detection
  > CUN - FLT TA410 - ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLISHED BY THE CREW, DUE THIS SITUATION THE AIRCRAFT LANDED AT CANCUN. CANCUN MX TECHS PERFORMED A COMPLETE VISUAL INSPECTION AT ENGINE NR 2, N
- [SDR 20000420AP003](https://openairdocs.org/sdr/20000420AP003.md): Fire Loop · damaged · Mar 19, 1999 · N232TA · Boeing 737296 · Fire Detection
  > DURING FLIGHT TA410 (SAL-IAH) ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLISHED BY THE CREW, DUE TO THIS SITUATION THE A/C LANDED AT CANCUN AIRPORT. AT CANCUN, MAINTENANCE TECHS PERFORMED A COMPLETE VISU
- [SDR USAA980564](https://openairdocs.org/sdr/USAA980564.md): Floor Angle · corroded · Oct 30, 1998 · N238US · Boeing 737296 · Fuselage Miscellaneous Structure
  > TPA - DURING C-1 CHECK VISUAL INSPECTION, FOUND ANGLE CORRODED AT LAV ATTACH POINT TO FLOOR AFT LAV ATTACH ANGLE FLOORBOARD. FABRICATED DOUBLER PER EA 62883. (M)
- [SDR CA981125020](https://openairdocs.org/sdr/CA981125020.md): Valve · malfunctioned · Oct 24, 1998 · Boeing 737296 · Engine Thrust Reverser
  > (CAN) RETURN TO GATE DUE THRUST REVERSER ISOLATION VALVE LIGHT ON AT ROTATION. VALVE REPLACED.
- [SDR CA980916023](https://openairdocs.org/sdr/CA980916023.md): Csd · malfunctioned · Aug 25, 1998 · Boeing 737296 · Alternator-Generator Drive
  > (CAN) NR 1 ENGINE GENERATOR AND CONSTANT SPEED DRIVE (CSD) WENT FULL VOLTS AND FREQUENCY. THE GENERATOR WAS TURNED OFF. VIBRATION WAS NOTICED, SO THE CSD WAS DISCONNECTED. A SEAL ON THE GEARBOX WAS FOUND NICKED. THE ENGINE WAS REPLACED.
- [SDR CA980707021](https://openairdocs.org/sdr/CA980707021.md): Door · chafed · Jun 10, 1998 · Boeing 737296 · Landing Gear Doors
  > (CAN) NOSE LANDING GEAR DOOR WORN ON INNER SURFACE. NO MENTION OF CLEARANCE CHECK IN AMM. DOOR REPLACED.
- [SDR USAA980167](https://openairdocs.org/sdr/USAA980167.md): Skin · lightning strike · Apr 20, 1998 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > ROA - DURING B-CHECK VISUAL INSPECTION, FOUND.75 INCH DAMAGED AREA (LIGHTNING STRIKE) AT BS 737-B STR 10, RT FUSELAGE SKIN. REMOVED DAMAGED AREA AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (X)
- [SDR USAA980166](https://openairdocs.org/sdr/USAA980166.md): Skin · lightning strike · Apr 20, 1998 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > ROA - DURING B-CHECK, VISUAL INSPECTION FOUND.50 INCH DAMAGED AREA (LIGHTNING STRIKE) BS 569, STR 7, RT FUSELAGE SKIN. REMOVED DAMAGED AREA, AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3. (X)
- [SDR CA971216021](https://openairdocs.org/sdr/CA971216021.md): Transmitter · failed · Mar 17, 1998 · Boeing 737296 · Trailing Flap Position Indicating System
  > (CAN) AIR TURN BACK TO BLOCKS DUE TO STICK SHAKER STALL WARNING AT TAKEOFF. REPLACED FLAP POSITION TRANSMITTER.
- [SDR CA971113018](https://openairdocs.org/sdr/CA971113018.md): Pump · worn · Oct 22, 1997 · Boeing 737296 · Fuel Boost Pump
  > (CAN) 5 PUMPS REPLACED IN LH AND RH CENTRE FUEL TANK DUE TO IMPELLER WEAR AT TIPS CAUSES LOW FLOW AND FUEL PRESSURE WARNING LIGHTS.
- [SDR CA970731003](https://openairdocs.org/sdr/CA970731003.md): Switch · intermittent · Jul 21, 1997 · Boeing 737296 · Engine Thrust Reverser
  > (CAN) HISTORY OF THRUST REVERSER ISOLATION LIGHT ON BRIEFLY AFTER TAKEOFF. ON NEXT FLIGHT ISOLATION LIGHT REMAINED ON.AIRCRAFT RETURNED. SWITCH S529 REPLACED.
- [SDR CA970626003](https://openairdocs.org/sdr/CA970626003.md): Plug · leaking · Jun 23, 1997 · Boeing 737296 · Alternator-Generator Drive
  > (CAN) ON TAKEOFF ROLL A FLICKERING WARNING LIGHT WAS OBSERVED. THE TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE MAGNETIC PLUG ON THE #2 ENGINE CONSTANT SPEED SPEED DRIVE (CSD) WAS LEAKING. THE PLUG WAS REPLACED AND THE OIL SYSTEM SERVICED. AFTER THE ENGINE WAS G
- [SDR CA970618008](https://openairdocs.org/sdr/CA970618008.md): Push Pull Rod · threads worn · Jun 16, 1997 · Boeing 737296 · Elevator Tab Control System
  > (CAN) RH ELEVATOR TAB OUTER PUSH PULL ROD FOUND WITH EYE AND JAM NUT BACKED OFF. THREADED END OF ROD DESTROYED DUE TO VIBRATION OF EYE END. ROD AND TWO EYE ENDS REPLACED.
- [SDR USAASB97035](https://openairdocs.org/sdr/USAASB97035.md): Bleed Valve · failed · Jan 28, 1997 · N238US · Boeing 737296 · Compressor Bleed Valve
  > MSP - FL 856 - AFTER TAKEOFF FROM MSP, THE NR 2 ENGINE EGT BEGAN TO RISE AND THE EPR STARTED TO DROP. DURING CLIMB, CAPTAIN HAD TO KEEP PULLING THE NR 2 THROTTLE BACK TO KEEP EGT WITHIN LIMITS. WHEN FLIGHT LEVELED OFF WITH POWER REDUCED TO LET THINGS STABILI
- [SDR USAA970036](https://openairdocs.org/sdr/USAA970036.md): Stringer · corrosion · Jan 23, 1997 · N238US · Boeing 737296 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 6 INCH IN LENGTH STRINGER 26L AT STATION 296. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)
- [SDR USAA970035](https://openairdocs.org/sdr/USAA970035.md): Stringer · corrosion · Jan 23, 1997 · N238US · Boeing 737296 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STRINGER 25L AT STATION 305. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)
- [SDR USAA970034](https://openairdocs.org/sdr/USAA970034.md): Skin · cracked · Jan 23, 1997 · N238US · Boeing 737296 · Fuselage Main, Plate/Skin
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 727 PLUS 16 STRINGER 15R SKIN. REMOVED EXISTING REPAIR, INSTALLED NEW REPAIR DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)
- [SDR USAA970033](https://openairdocs.org/sdr/USAA970033.md): Stringer · corrosion · Jan 23, 1997 · N238US · Boeing 737296 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CORROSION BS 366 STRINGER 27L. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)

Next page: https://openairdocs.org/model/boeing-737-296/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 = '737296'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-296/reports

---
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