# Service difficulty reports: Boeing 737-297

A list on [Boeing 737-297](https://openairdocs.org/model/boeing-737-297.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 10 · 454 reports

- [SDR KNNA147071110KACY](https://openairdocs.org/sdr/KNNA147071110KACY.md): Hydraulic Line · leaking · Jul 11, 2010 · N147AW · Boeing 737297 · Hydraulic System, Main
  > THE "A" SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT TO KACY (ATLANTIC CITY IAP, NJ). COMPLETED CHECKLIST 6.77 OF THE AFM.
- [SDR KNNA20090001](https://openairdocs.org/sdr/KNNA20090001.md): Seal · failed · Apr 3, 2009 · N147AW · Boeing 737297 · Turbine Engine Oil System
  > NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO DURING FLIGHT FOLLOWED BY DROP IN OIL PRESSURE LEADING TO ENGINE SHUT DOWN AND DECLARATION OF AN EMERGENCY. IT WAS DISCOVERED DURING TROUBLE SHOOTING THAT BOTH THE STARTER SEAL AND THE FUEL PUMP SEALS WERE LEAKING. B
- [SDR PIDR07001](https://openairdocs.org/sdr/PIDR07001.md): Skin · cracked · Aug 24, 2007 · N147AW · Boeing 737297 · Fuselage Main, Plate/Skin
  > CRACK IN THE FUSELAGE SKIN AT BS 727B+4 AT STR 17 RT WAS REPAIRED BY REPLACING THE DAMAGED SECTION OF SKIN FROM BS 727 TO BS 757 FROM STR 14 RT TO STR 20 RT DUE PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PRO
- [SDR PIDR07002](https://openairdocs.org/sdr/PIDR07002.md): Skin · cracked · Aug 24, 2007 · N147AW · Boeing 737297 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN AT BS 727A+14.5 AT STR 17 LT WAS REPAIRED BY REPLACING SECTION OF SKIN FROM BS 727A +8 TO BS 767 FROM STR 16 LT TO STR 18 LT DUE TO PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURE
- [SDR PIDR07003](https://openairdocs.org/sdr/PIDR07003.md): Stringer · damaged · Aug 24, 2007 · N147AW · Boeing 737297 · Fuselage Main, Longeron/Stringer
  > STRINGER 16 RT AT BS 727B HAS A DAMAGED FASTENER HOLE. REPAIRED IN ACCORDANCE WITH SRM 53-10-3 FIGURE 2.
- [SDR KNNA200700011](https://openairdocs.org/sdr/KNNA200700011.md): Frame · misdrilled · Feb 5, 2007 · N147AW · Boeing 737297 · Fuselage Main, Frame
  > FOUND MISDRILLED HOLE AT SKIN OF SIDE FRAME, WL 212 LT, STA 179. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF MISDRILLED FASTENER HOLE BS 178 W/L 212.
- [SDR KNNA200700018](https://openairdocs.org/sdr/KNNA200700018.md): Frame · cracked · Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, Frame
  > FOUND STA 178, LT SIDE FRAME IS CRACKED AT W/L 195. PROVIDE INSTRUCTION ON REPAIR CRACK BY INSTALLING A SPLICE OVER THE (LEFT SIDE) SIDE CHORD AT WL 212.
- [SDR KNNA200700017](https://openairdocs.org/sdr/KNNA200700017.md): Vertical Beam · cracked · Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, Bulkhead
  > FOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERTICAL CHORD AT STA 178.
- [SDR KNNA200700015](https://openairdocs.org/sdr/KNNA200700015.md): Bulkhead · cracked · Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, Bulkhead
  > FOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12.
- [SDR KNNA200700014](https://openairdocs.org/sdr/KNNA200700014.md): Frame · cracked · Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, Frame
  > FOUND STA 178 RT SIDE FRAME IS CRACKED AT WL 207. PROVIDE INSTRUCTION TO REPAIR CRACK BY INSTALLING A SPLICE OVER THE (RIGHT SIDE) SIDE CHORD AT WL 212.
- [SDR KNNA200700012](https://openairdocs.org/sdr/KNNA200700012.md): Bulkhead · cracked · Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, Bulkhead
  > FOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213.5, RBL 1,
- [SDR KNNA200700010](https://openairdocs.org/sdr/KNNA200700010.md): Bulkhead · cracked · Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, Bulkhead
  > FOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10.
- [SDR KNNA200700013](https://openairdocs.org/sdr/KNNA200700013.md): Skin · damaged · Jan 19, 2007 · N147AW · Boeing 737297 · Electrical/Electronic Compartment Doors
  > E/E BAY ACCESS DOOR EXTERIOR SURFACE, RT EDGE BEND. PROVIDE INSTRUCTIONS ON REPAIR OF E/E BAY DOOR.
- [SDR KNNA200700016](https://openairdocs.org/sdr/KNNA200700016.md): Stringer Splice · active · Jan 12, 2007 · N147AW · Boeing 737297 · Fuselage Main, Longeron/Stringer
  > FOUND CRACKED CHORD OF STRINGER 14L AT BS 663.75. PROVIDE INSTRUCTION ON REPAIR OF S14L AT BS 663.75.
- [SDR KNNA200300001](https://openairdocs.org/sdr/KNNA200300001.md): Skin · cracked · Feb 24, 2003 · N147AW · Boeing 737297 · Fuselage Main, Plate/Skin
  > AIRCRAFT AT MAINT. BASE FOR "A3" CHECK COMPLIANCE. IN C/W TASK CARD A-07A A 1.8 INCH CRACK WAS FOUND IN EXTERIOR FUSELAGE SKIN AT LT BS 757 BELOW STR 17. A NON-ROUTINE T030446 AND ACO 035313R00 WAS ISSUED TO DOCUMENT SRM REPAIR CH 53-30-3 FIG 25. CRACK IN SK
- [SDR CA020528005](https://openairdocs.org/sdr/CA020528005.md): Duct · ruptured · May 16, 2002 · Boeing 737297 · Engine Bleed Air System
  > (CAN) SHORTLY AFTER TAKEOFF CREW OBSERVED NR 1 ENGINE OVERHEAT - WHEN POWERLEVER RETARDED, IND. EXTINGUISHED. WHEN POWERLEVER FOR NR 1 ENGINE ADVANCED, OVERHEAT WARNING ILLUMINATED. CREW DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. CFR ON STANDBY.
- [SDR CA020502004](https://openairdocs.org/sdr/CA020502004.md): Fitting · missing · Apr 27, 2002 · Boeing 737297 · Accessory Gearboxes
  > (CAN) ENROUTE PILOT NOTICED THE OIL QUANTITY WAS AT ZERO ON THE NR 1 ENGINE - BOTH OIL PRESSURE AND OIL TEMPERATURE WERE NORMAL. SHORTLY THERE AFTER THE OIL PRESSURE STARTED TO FLUCTUATE AND THE OIL PRESSURE WARNING LIGHT ILLUMINATED.FLIGHT CREW SHUTDOWN NR 1
- [SDR CA020408017](https://openairdocs.org/sdr/CA020408017.md): Wheel · cracked · Apr 5, 2002 · Boeing 737297 · Wheel/Ski/Float
  > (CAN) FLIGHT CREW REPORTED ON TAXI THE AIRCRAFT SEEMED TO REQUIRE MORE POWER THAN NORMAL - AIRCRAFT DEPARTED WITHOUT INCIDENT.ON NEXT LANDING THE CREW NOTICED THE SAME AND REPORTED TO YLW MAINTENANCE. INSPECTION FOUND THE MAIN BRAKE ON NR 2 MAIN WHEEL ASSEMBLY
- [SDR CA020305003](https://openairdocs.org/sdr/CA020305003.md): Wire · chafed · Feb 22, 2002 · Boeing 737297 · Fire Protection System Wiring
  > (CAN) DURING FLT A/C EXPERIENCED FLICKERING LT WING BODY OVERHEAT INDICATION WITH INCREASING FREQ. OVERHEAT LIGHT ILLUMINATED OFF & FLICKERED ON & OFF CONTINUOUSLY WHEN LT ENGINE BLEED VALVE & ISOLATION VALVE WERE CLOSED (WITH APU OFF). FLT CREW CONTACTED MC
- [SDR P2EA2002M001](https://openairdocs.org/sdr/P2EA2002M001.md): Actuator · cracked · Jan 10, 2002 · Boeing 737297 · Hydraulic System, Main
  > After Landing Lost A System Hydraulics upon exiting taxi way at MCI.Inspected and found the #1 Ground Spoiler actuator with crack. R&R #1 Ground Spoiler actuator IAW Boeing MM 27-62-101 op's check and leak checks good.
- [SDR CA011120004](https://openairdocs.org/sdr/CA011120004.md): Control Unit · leaking · Nov 16, 2001 · Boeing 737297 · Hydraulic System, Main
  > (CAN) RETURNED TO YHM DUE TO LOSS OF 'A' SYS HYDRAULIC FLUID. SHORTLY AFTER TAKEOFF OUT OF YHM CREW NOTICED HYD MASTER CAUTION LIGHT HAD ILLUMIINATED, THE 'A' SYS HYDRAULIC FLUID HAD DEPLETED & THE HYDRAULIC LOW PRESSURE WARNING LIGHTS HAD ILLUMINATED. CREW
- [SDR P2EA2001M0005](https://openairdocs.org/sdr/P2EA2001M0005.md): Coupler · Sep 24, 2001 · Boeing 737297 · Speed-Attitude Correction System
  > Mach Trim "fail" light illumimnates intermitently. Corrective action: Defferred Mach Trim system per MEL 22-5, CI#M005089 per MX CNTL Mic. Removed and replaces Mach Trim Coupler IAW MM 22-21-31, operational check normal. This clears MEL CI#M005089. See 005 Log
- [SDR P2EA01193](https://openairdocs.org/sdr/P2EA01193.md): Computer · faulty · Sep 16, 2001 · N120NJ · Boeing 737297 · Autopilot Computer
  > FLT 451 - MCI - WITH AUTOPILOT IN HGD HOLD AIRCRAFT ROLLS TO APPROXIMATELY WINGS LEVEL FROM AND BANK ANGLE AND TURNS AT ABOUT 1 DEGREE PER MINUTE TO THE LEFT. ALL OTHER AUTO PILOTS FUNCTIONS ARE NORMAL. REMOVED AND REPLACED ROLL COMPUTER AND OPERATIONAL CHEC
- [SDR P2EA01089](https://openairdocs.org/sdr/P2EA01089.md): Hydraulic Line · inoperative · Jun 7, 2001 · N5WM · Boeing 737297 · Hydraulic Power System
  > FLT 408 - MCI - WHILE ON APPROACH INTO MCI, AIRCRAFT A SYSTEM HYDRAULIC FAILED. DECLARED AN EMERGENCY. INSPECTED HYDRAULIC SYSTEM A AND FOUND LEAK IN FORWARD LEFT MAIN WHEEL WELL. REMOVED AND REPLACED HYDRAULIC LINE LEAK CHECKED GOOD PER BOEING MM 29-00 PAR
- [SDR CA010504024](https://openairdocs.org/sdr/CA010504024.md): Tube · worn · Apr 13, 2001 · Boeing 737297 · Engine Pressure Ratio (EPR)
  > (CAN) CREW REPORTED NR 1 ENGINE EPR INDICATION FLUCTUATING TO.20 EPR LOWER THAN NR 1 ENGINE. N1, N2 AND FUEL FLOWS WERE STEADY. INSPECTION FOUND A CHAFED WIRE AT THE R/H ANTI-ICE VALVE HAD ARCHED AND WORN A HOLE THRU THE SIDE OF THE LINE FROM THE PT 7 PROBE.
- [SDR P2EA01025](https://openairdocs.org/sdr/P2EA01025.md): Skin · punctured · Apr 8, 2001 · N5WM · Boeing 737297 · Fuselage Main, Plate/Skin
  > FLT 350 - MDW - PUNCTURE THROUGH SKIN AT BS 933 WL 203 BETWEEN STRINGER 20L AND 21L. (M)
- [SDR P2EA01028](https://openairdocs.org/sdr/P2EA01028.md): Skin · punctured · Apr 8, 2001 · N5WM · Boeing 737297 · Fuselage Main, Plate/Skin
  > MDW - FLT 350 - PUNCTURE THROUGH SKIN AT BS 933, WL 203 BETWEEN STRINGER 20L AND 21L. REPAIRED IAW SRM 53-30-3. (M)
- [SDR TSAA0133015](https://openairdocs.org/sdr/TSAA0133015.md): Battery Pack · discharged · Feb 16, 2001 · N726AL · Boeing 737297 · Emergency Lighting
  > REPLACED BATTERY FOR THE NR 3 AND NR 4 POSITION FOR THE EMERGENCY FLOOR PROX LIGHT. OPS CHECK OK. AIRCRAFT RETURNED SERVICE. (M)
- [SDR 2001F00633](https://openairdocs.org/sdr/2001F00633.md): Tire · separated · Jan 26, 2001 · N147AW · Boeing 737297 · Tire
  > LOSS OF A SYSTEM HYDRAULICS. LEFT INBOARD TIRE LOST TREAD DURING TAKEOFF ROLL. PIECES OF THE TIRE TREAD DAMAGED HYDRAULIC LINES AND CONTROL CABLES LOCATED IN THE LEFT WHEEL WELL. ALSO, DAMAGE FROM FLYING RUBBER TO LEFT FORE FLAP, MID FLAP AND TRAILING EDGE
- [SDR P2EA00460](https://openairdocs.org/sdr/P2EA00460.md): Skin · cracked · Dec 8, 2000 · N5WM · Boeing 737297 · Service Doors
  > SJO - DURING Q-CHECK, FOUND THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 WITH CRACK. L = 1.1250 INCHES. W = 0.001 INCH. REPAIRED THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 IAW BOEING SRM 52-00-3 FIG 3. (X)
- [SDR P2EA00451](https://openairdocs.org/sdr/P2EA00451.md): Fitting · cracked · Dec 2, 2000 · N5WM · Boeing 737297 · Horizontal Stabilizer, Tab Structure
  > SJO - DURING Q-CHECK, FOUND LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO WITH CRACK L = 2.00 INCHES. W = 0.002 INCH. REPLACED THE LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X)
- [SDR P2EA00424](https://openairdocs.org/sdr/P2EA00424.md): Clip · cracked · Nov 23, 2000 · Boeing 737297 · Fuselage Miscellaneous Structure
  > DURING Q CHECK, FOUND THE FRAME SUPPORT CLIP AT BS 663.75 STR 10L WITH CRACK. REPLACE THE FRAME SUPPORT CLIP AT BS 663.75 STR 10L.
- [SDR P2EA00414](https://openairdocs.org/sdr/P2EA00414.md): Floor Support · cracked · Nov 22, 2000 · Boeing 737297 · Fuselage Miscellaneous Structure
  > DURING Q CHECK, FOUND THE PASSENGER CABIN AT BS 727 RBL 65 WITH CRACKED ANGLE ON FLOOR SUPPORT. L/0.050 W/0.005 REPAIRED THE PASSENGER CABIN FLOOR SUPPORT ANGLE AT BS 727 RBL 65.
- [SDR P2EA00407](https://openairdocs.org/sdr/P2EA00407.md): Bulkhead · cracked · Nov 22, 2000 · N5WM · Boeing 737297 · Fuselage Main, Bulkhead
  > SJO - DURING Q-CHECK, FOUND THE BS 178 BULKHEAD AT WL 196 FROM LBL 25 TO RBL 25 WITH CRACK. L = 1.00 INCH. W = 0.001 INCH. REPLACED THE BS 178 BULKHEAD INTERCOSTAL AT WL 196 FROM LBL 25 TO RBL 25 IAW BOEING SB 737-53A1173 REV 3 DATED MAY 6, 1999, SECTION II
- [SDR P2EA00396](https://openairdocs.org/sdr/P2EA00396.md): Channel · corroded · Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, THE CABIN FLOOR CHANNEL AT BS 296.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS, LENGTH 2.5 INCH, WIDTH 2 INCHES, DEPTH.025 INCH. REPLACED THE CABIN FLOOR CHANNEL AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 IA
- [SDR P2EA00413](https://openairdocs.org/sdr/P2EA00413.md): Floor Support · corroded · Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 0.50 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5
- [SDR P2EA00412](https://openairdocs.org/sdr/P2EA00412.md): Floor Support · corroded · Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO BS 312 LBL 11 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 1.00 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO
- [SDR P2EA00449](https://openairdocs.org/sdr/P2EA00449.md): Channel · cracked · Nov 17, 2000 · Boeing 737297 · Wing Main, Frame Structure
  > DURING Q CHECK, FOUND THE RT HAND WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK L/0.50 W/0.005 REPLACED RT HAND WING TE CAVITY LOWER CHORD CHANNEL.
- [SDR P2EA00389](https://openairdocs.org/sdr/P2EA00389.md): Channel · cracked · Nov 17, 2000 · N5WM · Boeing 737297 · Wing Miscellaneous Structure
  > SJO - DURING Q-CHECK, FOUND THE RIGHT WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK. (M)
- [SDR P2EA00457](https://openairdocs.org/sdr/P2EA00457.md): Web · cracked · Nov 16, 2000 · Boeing 737297 · Cargo/Baggage Doors
  > DURING Q CHECK, FOUND THE FORWARD CARGO DOOR NR5 CROSS BEAM WEB, AFT END, WITH CRACK. L/1.00 W/0.001. REPAIRED FORWARD CARGO DOOR NR5 CROSS BEAM WEB, AFT END.
- [SDR P2EA00387](https://openairdocs.org/sdr/P2EA00387.md): Crossbeam · cracked · Nov 16, 2000 · N5WM · Boeing 737297 · Passenger/Crew Doors
  > SJO - DURING Q-CHECK, FOUND THE FORWARD CARGO DOOR NR 5 CROSSBEAM WEB AFT END WITH CRACK. (M)
- [SDR P2EA00455](https://openairdocs.org/sdr/P2EA00455.md): Flap Track · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NR'S 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS.313 LENGTH,.001 INCH WIDE, AND.250 INCH LENGTH,.001 INCH WIDE. REPLACED THE RIGHT WING OUTBOARD FLAP TR
- [SDR P2EA00459](https://openairdocs.org/sdr/P2EA00459.md): Angle · corroded · Nov 14, 2000 · Boeing 737297 · Fuselage Main, Structure
  > DURING Q CHECK, FOUND APU TORQUE BOX RT SIDE ANGLE FROM BS 1118 TO 1138 WITH CORROSION, OUT OF LIMITS L/12.00 W/1.250 D/0.50. REPLACED THE APU TORQUE BOX RT SIDE ANGLE.
- [SDR P2EA00435](https://openairdocs.org/sdr/P2EA00435.md): Frame · cracked · Nov 14, 2000 · Boeing 737297 · Fuselage Main, Frame
  > DURING Q CHECK, FOUND FORWARD CARGO FRAME WEB AT BS 440 BETWEEN STR 23, 24R WITH CRACK L/0.250 W/0.005. REPAIRED FORWARD CARGO FRAME WEB AT BS 440 BETWEEN STR 23,24R.
- [SDR P2EA00440](https://openairdocs.org/sdr/P2EA00440.md): Frame · cracked · Nov 14, 2000 · Boeing 737297 · Fuselage Main, Frame
  > DURING Q CHECK, FOUND FORWARD CARGO FRAME WEB AT BS 492.4 BETWEEN STR 23, 24R WITH CRACK L/0.250 W/0.005. REPAIRED FORWARD CARGO FRAME WEB AT BS 492.4 BETWEEN STR 23, 24R.
- [SDR P2EA00384](https://openairdocs.org/sdr/P2EA00384.md): Flap Track · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Trailing Edge Flaps
  > SJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NRS 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS. (M)
- [SDR P2EA00386](https://openairdocs.org/sdr/P2EA00386.md): Angle · corroded · Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, FOUND THE APU TORQUE BOX RIGHT ANGLE FROM BS 1118 TO 1138 WITH CORROSION OUT OF LIMITS. (M)
- [SDR P2EA00379](https://openairdocs.org/sdr/P2EA00379.md): Web · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, FOUND THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 WITH CRACK. L = 0.500 INCH. W = 0.005 INCH. REPAIRED THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 IAW BOEING SRM 51-40-2 FIG 1. (X)
- [SDR P2EA00380](https://openairdocs.org/sdr/P2EA00380.md): Channel · cracked · Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous Structure
  > SJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL WITH CRACK. L = 0.50 INCH. W = 0.005 INCH. REPLACED THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X)
- [SDR P2EA00393](https://openairdocs.org/sdr/P2EA00393.md): Slat Track · cracked · Nov 13, 2000 · N5WM · Boeing 737297 · Leading Edge Devices
  > SJO - DURING Q-CHECK, FOUND THE LT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK LENGTH.50 INCH, WIDTH.50 INCH. REWORKED THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER AND WAS FOUND TO BE WITHIN LIMITS IAW BOEING SRM 57-20-1 F

Next page: https://openairdocs.org/model/boeing-737-297/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 = '737297'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-297/reports

---
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