# Service difficulty reports: Boeing 737-347

A list on [Boeing 737-347](https://openairdocs.org/model/boeing-737-347.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 8 · 359 reports

- [SDR DL733060250](https://openairdocs.org/sdr/DL733060250.md): Stiffener · cracked · Mar 29, 2006 · N306WA · Boeing 737347 · Wing Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF 05-086589-12AD, THE WING CENTER SECTION REAR SPAR STIFFENER AT LBL 6.15 WAS FOUND CRACKED. REPLACED REAR SPAR STIFFENER.
- [SDR DL733060111](https://openairdocs.org/sdr/DL733060111.md): Duct · unknown · Feb 9, 2006 · N308WA · Boeing 737347 · Air Distribution System
  > UNABLE TO MAINTAIN PRESSURIZATION WITH LT PACK AT FL 240. RT PACK CURRENTLY ON MCO. REPAIRING RT PACK. REPLACED DUCT ON RT PACK CLEARED MCO ON RT PACK A/C PRESSURIZATION CHECK NORMAL.
- [SDR DL733060098](https://openairdocs.org/sdr/DL733060098.md): Actuator · broken · Feb 2, 2006 · N308WA · Boeing 737347 · Drag Control Actuator
  > NR 4 O/B SPOILER ACTUATOR BROKE OFF AT REAR HINGE POINT, CAUSING HINGE POINT TO BREAK AT SPOILER PANEL. REPLACED BOTH UNITS. ACTUATOR P/N 273001083.
- [SDR DL733050836](https://openairdocs.org/sdr/DL733050836.md): Packing · split · Dec 28, 2005 · N312WA · Boeing 737347 · Hydraulic System, Main
  > DECLARED EMERGENCY HYD QTY A DROPPED TO 1/2. REPLACED LOWER PACKING ON A HYD SYS EMDP ACCOUSTIC FILTER, LEAK CK OK HYD SERVICED.
- [SDR DL733050659](https://openairdocs.org/sdr/DL733050659.md): Skin · cracked · Oct 20, 2005 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS APPROX 2 INCHES LONG AFT OF BS 727D, JUST BELOW STR 23L. REPAIRED WITH DOUBLER PER ER/A 451209-14AD, REF AD 2004-18-06.
- [SDR DL733050637](https://openairdocs.org/sdr/DL733050637.md): Skin · cracked · Oct 19, 2005 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACK WAS FOUND AT CHEM MILL LINE AT BS 727E, STR 24R. CRACK IS 3 INCHES LONG. DOULBER INSTALLED PER ER/A 451199-14AD, AD 2004-18-06, AND SRM 53-00-01.
- [SDR DL733050524](https://openairdocs.org/sdr/DL733050524.md): Skin · cracked · Sep 6, 2005 · N308WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > CRACK FOUND IN FUSELAGE SKIN AT CHEM-MIL WHILE ACCOMP OPN 57546. CRACK REPORTED TO BE 1.5 INCH LONG, LOCATED AT FS 727E, S-24L. REPAIRED PER SRM 53-00-01, FIGURE 201. RELATED TO AD 2004-18-06, S/B 737-53A1210, & S/B 737-53-1065.
- [SDR DL733050523](https://openairdocs.org/sdr/DL733050523.md): Skin · cracked · Sep 6, 2005 · N308WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > CRACK WAS FOUND IN THE FUSELAGE SKIN WHILE DOING OPN 57546 INSPECTIONS. REPAIRED PER SRM 53-00-01, FIGURE 201. REF AD 2004-18-06 / S/B 737-53A1210 / 737-53-1065.
- [SDR DL733050497](https://openairdocs.org/sdr/DL733050497.md): Indicator · unserviceable · Aug 29, 2005 · N309WA · Boeing 737347 · Engine Oil Pressure
  > DURING T/O ROLL AFTER 80 KTS NR 2 OIL PRESS ROLLED BACK TO BELOW THE RED DIAL. ALL OTHER IND NORMAL. CONTINUED T/O AND PERFORMED LOP CK LIST PROCEDURE PER QRH. ENG SHUTDOWN AND RETURNED TO DTW. SWAP INDICATORS. PROBLEM FOLLOWED. REPLACED NR 2 OIL PRESS I
- [SDR DL733050323](https://openairdocs.org/sdr/DL733050323.md): Outflow Valve · unserviceable · Jun 13, 2005 · N308WA · Boeing 737347 · Pressure Regulator/Outflow Valve
  > AIRCRAFT WOULD NOT PRESSURIZE. FOUND AUTO FLOW CONTROL VALVE NOT CLOSING PER CABIN PRESS LEAK TEST 05-51-91-702. REPLACED VALVE PER MM 21-58-31. OP CK OK. AIRCRAFT PRESSURIZED ON GROUND PER MM.
- [SDR DL733050214](https://openairdocs.org/sdr/DL733050214.md): Circuit Breaker · tripped · Apr 11, 2005 · N309WA · Boeing 737347 · DC Power Distribution System
  > ON CLIMBOUT, BATTERY ON DC- IRS LIGHTS ILLUMINATED. BATTERY VOLTS ZERO. RETURNED TO SLC. MTC IN WORK. FOUND HOT BATTERY BUS C/B POPPED P18 PNL. RESET C/B. PERFORMING DC POWER CHECK.
- [SDR DL733050197](https://openairdocs.org/sdr/DL733050197.md): Fire Loop · faulty · Apr 2, 2005 · N304WA · Boeing 737347 · Fire Detection
  > APU FIRE WARNING LIGHT/ALARM BELL IN FLIGHT APPROX 1 TO 2 MINS AFTER APU SHUTDOWN IN FLIGHT AT 10 TO 12,000 FT ALT FIRE BOTTLE USED. REMOVED APU SHROUD, APU INSPECTED FOUND NO EVIDENCE OF FIRE. REPLACED AFT DETECTOR LOOP.
- [SDR DL733050181](https://openairdocs.org/sdr/DL733050181.md): Apu · defective · Mar 19, 2005 · N305WA · Boeing 737347 · APU Core Engine
  > SMOKE SMELL IN CABIN WITH APU AIR. REPLACED APU.
- [SDR DL733050148](https://openairdocs.org/sdr/DL733050148.md): Skin · cracked · Mar 3, 2005 · N306WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK AT FS 870 JUST ABOVE THE BONDED DOUBLER MILL LINE AT STRINGER 23R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-300 S
- [SDR DL733050137](https://openairdocs.org/sdr/DL733050137.md): Apu · fuses · Feb 27, 2005 · N309WA · Boeing 737347 · Airborne Auxiliary Power Unit (APU) System
  > CREW REPORTS FUMES IN CABIN WHILE AT THE GATE. DEPLANED PASSENGERS AND TURNED OVER TO MAINTENANCE. REPLACED APU PER MM.
- [SDR DL733050107](https://openairdocs.org/sdr/DL733050107.md): Connector · damaged · Feb 14, 2005 · N302WA · Boeing 737347 · Emergency Lighting
  > EMERGENCY PATH LIGHTING INOP AT 22D/E/F. FOUND ON ROUTINE MAINTENANCE INSPECTION. REPAIRED DAMAGED SIDEWALL CONNECTOR AT 22D/E/F.
- [SDR DL733050050](https://openairdocs.org/sdr/DL733050050.md): Apu · fire · Jan 21, 2005 · N313WA · Boeing 737347 · APU Core Engine
  > AFTER LANDING STARTED APU. TAXIED TO GATE, DURING ENGINE SHUTDOWN HAD APU FIRE LIGHT. ACCOMPLISHED QRH PROCEDURE. MAINTENANCE INSPECTED, FIRE BOTTLE FOUND DISCHARGED. REMOVED BATHTUB AND INSPECTED APU FOR DAMAGE. FIRE WAS LIMITED TO TAILPIPE AREA. REAR F
- [SDR DL733050035](https://openairdocs.org/sdr/DL733050035.md): Outflow Valve · contaminated · Jan 15, 2005 · N2310 · Boeing 737347 · Pressure Regulator/Outflow Valve
  > AIRCRAFT FAILED TO PRESSURIZE. FOUND PRESSURE RELIEF VALVE STUCK OPEN.
- [SDR DL733041124](https://openairdocs.org/sdr/DL733041124.md): Skin · cracked · Dec 19, 2004 · N312WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVEALED A 3 INCH CRACK ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 15R AT FS 500D+7. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND PER E
- [SDR DL733041086](https://openairdocs.org/sdr/DL733041086.md): Switch · intermittent · Dec 7, 2004 · N311WA · Boeing 737347 · Leading Edge Slat Control System
  > AFTER TAKEOFF AND FLAPS WERE RAISED PILOT HAD NR 4 SLAT INDICATION PROBLEM ON THE FWD PANEL AND ON THE OVERHEAD. REPLACED SWITCH ON NR 4 SLAT ROD END.
- [SDR DL733041069](https://openairdocs.org/sdr/DL733041069.md): Wire Harness · burned · Nov 30, 2004 · N313WA · Boeing 737347 · Light System Wiring
  > JUST PRIOR TO T/O WHEN LANDING LIGHTS TURNED ON, SPARKS CAME FROM OVERHEAD PANEL. TURNED OFF LIGHTS SPARKS STOPPED. REPAIRED WIRE BUNDLE IN OVERHEAD.
- [SDR DL733040960](https://openairdocs.org/sdr/DL733040960.md): Skin · dented · Oct 11, 2004 · N304WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT STA 827 BETWEEN STR 26R - 28R. REPAIRED IAW ERA 093986-14.
- [SDR DL733040805](https://openairdocs.org/sdr/DL733040805.md): Skin · cracked · Aug 23, 2004 · N3301 · Boeing 737347 · Fuselage Main, Plate/Skin
  > TWO CRACKS WERE FOUND RUNNING ALONG THE BONDED SKIN DOUBLER LINE OF STRINGER 24L. ONE CRACK WAS JUST FWD AND THE OTHER JUST AFT OF A PREVIOUSLY INSTALLED SKIN REPAIR FOR REPAIR OF SIMILAR MILL LINE CRACKING. THE SKIN PANEL WAS CUT FROM THE STRINGER 20L LAP J
- [SDR DL733040802](https://openairdocs.org/sdr/DL733040802.md): Skin · cracked · Aug 23, 2004 · N3301 · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED AT FOUR LOCATIONS. THE CRACKS WERE ALL LOCATED ALONG THE EDGE OF THE UNDERLYING BONDED DOUBLER. A 1 INCH VERTICAL CRACK WAS FOUND AT FS 767 ABOVE STR 23R. A 3.5 INCH HORIZONTAL CRACK WAS JUST BELOW S-22R AT FS 760, A.25
- [SDR DL733040796](https://openairdocs.org/sdr/DL733040796.md): Wedge · debonded · Aug 23, 2004 · N3301 · Boeing 737347 · Trailing Edge Flaps
  > NR 4 FORE FLAP TE WEDGE WAS FOUND WITH A 42 INCH SECTION OF SKIN DISBONDED. REPAIRED PER ER/A 092865-14.
- [SDR DL733040776](https://openairdocs.org/sdr/DL733040776.md): Skin · cracked · Aug 18, 2004 · N3301 · Boeing 737347 · Fuselage Main, Plate/Skin
  > CRACK REPAIR, THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 757 JUST BELOW STRINGER 19R RUNNING ALONG THE UNDERLYING BONDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER IAW ER/A 092756-14.
- [SDR DL733040746](https://openairdocs.org/sdr/DL733040746.md): Skin · cracked · Aug 7, 2004 · N308WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > A SKIN CRACK WAS FOUND ALONG THE THE MILL LINE OF THE UNDERLYING BONDED DOUBLER JUST AFT OF FS 727D AND BELOW STRINGER 23L. THE CRACK WAS REMOVED WITH A 1.5 X 2.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 092528-1
- [SDR DL733040617](https://openairdocs.org/sdr/DL733040617.md): Skin · cracked · Jun 30, 2004 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STA 767 AND STR 22R AT A CHEM MILL LOCATION. REPAIRED IN ACCORDANCE WITH ERA 091533-14.
- [SDR DL733040616](https://openairdocs.org/sdr/DL733040616.md): Skin · cracked · Jun 30, 2004 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT CHEM MILL LINE AT STA 727E BETWEEN STR 23L AND 25L. REPAIRED IAW 091565-14.
- [SDR DL733040604](https://openairdocs.org/sdr/DL733040604.md): Odor · detected · Jun 26, 2004 · N302WA · Boeing 737347 · Buffet/Galleys
  > FLIGHT ATTENDANT SMELLS BURNING ODOR IN AFT GALLEY. INSPECTED AFT GALLEY EQUIPMENT FOR DEFECTS, NONE NOTED. NO SMELL PRESENT. APPLIANCES AND LIGHTS ALL CHECK NORMAL. OK FOR SERVICE.
- [SDR DL733040311](https://openairdocs.org/sdr/DL733040311.md): Psu · inoperative · Apr 5, 2004 · N309WA · Boeing 737347 · Passenger Oxygen System
  > PAX SEAT 19DEF 02 MASKS DID NOT DEPLOY WHEN SWITCH IN COCKPIT PUSHED. REPLACED PSU.
- [SDR DL733040313](https://openairdocs.org/sdr/DL733040313.md): Skin · cracked · Apr 3, 2004 · N303WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH 2 CRACKS ALONG THE BONDED DOUBLER EDGES AT STRINGERS 22R & 23R. AN EXISTING REPAIR FOR A SIMILAR CRACK WAS LOCATED AT STRINGER 24R. THE EXISTING REPAIR WAS REMOVED, ALL CRACKS REMOVED WITH CUTOUTS, AND THE CUTOUTS REPAIRED WI
- [SDR DL733040216](https://openairdocs.org/sdr/DL733040216.md): Wire · shorted · Mar 5, 2004 · N309WA · Boeing 737347 · Buffet/Galleys
  > AFT OVEN RIGHT SIDE DOUBLE HAD SMOKE COMING FROM BEHIND OVEN CONTROL. REMOVED OVEN, FOUND BURNED WIRES. REPAIRED SAME.
- [SDR DL733040188](https://openairdocs.org/sdr/DL733040188.md): Cylinder · sheared · Feb 24, 2004 · N311WA · Boeing 737347 · Nose/Tail Landing Gear
  > WHILE TAKING THE RUNWAY IN A LEFT TURN, HEARD A BANG. THOUGH THE A/C FELT OK, ELECTED TO PULL OFF THE RUNWAY AND HAVE MAINT INSPECT THE AIRCRAFT. FOUND THE LEFT NOSE WHEEL AND AXLE BROKEN. REPLACED NOSE GEAR.
- [SDR DL733040090](https://openairdocs.org/sdr/DL733040090.md): Extinguisher · discharged · Jan 27, 2004 · N305WA · Boeing 737347 · Fire Bottle, Portable
  > PORTABLE FIRE EXTINGUISHER PRESSURE LOW. REPLACED SAME.
- [SDR DL733040060](https://openairdocs.org/sdr/DL733040060.md): Skin · cracked · Jan 17, 2004 · N302WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST BELOW STRINGER 23R ALONG THE EDGE OF THE BONDED SKIN WAFFLE DOUBLER BETWEEN FS 727D & 727E. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386104-14, REV A.
- [SDR DL733040007](https://openairdocs.org/sdr/DL733040007.md): Tire · cut · Jan 4, 2004 · N302WA · Boeing 737347 · Tire
  > ON L/O FOUND NR 2 MLG TIRE CUT BEYOND LIMITS. REMOVED AND REPLACED NR 2 MLG TIRE PER MM.
- [SDR DL733030968](https://openairdocs.org/sdr/DL733030968.md): Engine · overtemp · Oct 29, 2003 · N312WA · Boeing 737347 · Engine (Turbine/Turboprop)
  > ON TAKEOFF ROLL, NR 1 ENGINE EGT WAS INCREASING TO 954 DEGREE CELSIUS. THROTTLES (AUTO THROTTLES) HAD TO BE DISCONNECTED TO KEEP ENGINE EGT FROM CLIMBING HIGHER. N1 WAS 91 PERCENT, N2 WAS 102 PERCENT AND INCREASING. FUEL FLOW NORMAL ON T/O ROLL. REPLACED E
- [SDR DL733030948](https://openairdocs.org/sdr/DL733030948.md): Fuse · blown · Oct 24, 2003 · N305WA · Boeing 737347 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 27DEF INOP. REPLACED 5 AMP FUSE ON BATTERY RACK.
- [SDR DL733030877](https://openairdocs.org/sdr/DL733030877.md): Skin · cracked · Sep 25, 2003 · N312WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE/SKIN/STA 500D - STA 520/STR 12R - REPAIR OF CRACK. THE CRACK IS CUT OUT OF THE FUSELAGE SKIN AND AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER ARE INSTALLED IN ACCORDANCE WITH ER/A 381822-14 REV C.
- [SDR DL733030876](https://openairdocs.org/sdr/DL733030876.md): Skin · dented · Sep 25, 2003 · N312WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE/SKIN/FS430-460, S23R TO S27R - DENTS AND WEAR. THE SUBJECT DAMAGE IS CUT OUT FROM THE FUSELAGE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLER, TRIPLER AND STRUCTURAL FILLER IN ACCORDANCE WITH ER/A 385699-14. DAMAGE DUE TO CONTACT WITH GROUND EQUIP
- [SDR DL733030855](https://openairdocs.org/sdr/DL733030855.md): Beam · corroded · Sep 17, 2003 · N312WA · Boeing 737347 · Nacelle/Pylon, Attach Fittings
  > CORROSION WAS FOUND IN THE AFT LUG BORE OF THE NR 1 PYLON CROWN BEAM FITTING AT NAC STA 257.25. THE BORE WAS OVERSIZED TO REMOVE THE CORROSION, HFEC INSPECTED, AND STEEL REPAIR BUSHINGS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385679-14.
- [SDR DL733030852](https://openairdocs.org/sdr/DL733030852.md): Wire Harness · inoperative · Sep 17, 2003 · N302WA · Boeing 737347 · Light System Wiring
  > WHILE REPOSITIONING HARNESS AT SEAT ROW 27 PINS PULLED OUT OF HARNESS AND SHORTED POWER SUPPLY. REPLACED HARNESS AT SEAT ROW 27 AND POWER SUPPLY/BATTERY PER M/M.
- [SDR DL733030850](https://openairdocs.org/sdr/DL733030850.md): Intercostal · cracked · Sep 16, 2003 · N312WA · Boeing 737347 · Fuselage Miscellaneous Structure
  > MODIFICATION OF THE FS 178 BULKHEAD REVEALED A CRACK IN THE LBL & RBL 28 COCKPIT FLOOR INTERCOSTAL WEB AND CHORD AT WL 107. THE CRACKED CHORD AND WEB WERE REMOVED AT BOTH LOCATIONS AND PARTS INSTALLED PER ER/A 385678-14AD.
- [SDR DL733030784](https://openairdocs.org/sdr/DL733030784.md): Sensor · out of tolerance · Aug 26, 2003 · N305WA · Boeing 737347 · Landing Gear Position and Warning
  > AFTER TAKEOFF GEAR WOULD NOT RETRACT NORMALLY, HAD TO USE OVERRIDE TO RAISE HANDLE. ONCE GEAR WAS UP AND FLAPS WERE RETRACTED TAKEOFF WARNING HORN SOUNDED UNTIL FLAPS WERE LOWERED AGAIN. AIRCRAFT RETURNED TO SFO. SFO LINE MTC T/S TAKEOFF WARNING SYSTEM, FOU
- [SDR DL733030626](https://openairdocs.org/sdr/DL733030626.md): Iru · faulty · Jul 10, 2003 · N312WA · Boeing 737347 · Inertial Guidance System
  > LOST LEFT IRU IN FLIGHT. UNABLE TO GET HEADING IN ATT. BOTH AUTOPILOTS INOP. REPLACED LEFT INERTIAL REFERENCE UNIT PER M/M.
- [SDR DL733030611](https://openairdocs.org/sdr/DL733030611.md): Light · inoperative · Jul 3, 2003 · N303WA · Boeing 737347 · Emergency Lighting
  > EMERGENCY LIGHTS INOP AT SEAT 2B OVERHEAD, AT 10D AND 14D. REPLACED OVERHEAD LIGHT ASSY AT 2B AND RELAMPED SEAT LIGHTS AT 10D & 14D CHECKS GOOD.
- [SDR DL733030568](https://openairdocs.org/sdr/DL733030568.md): Bulb · inoperative · Jun 21, 2003 · N303WA · Boeing 737347 · Emergency Lighting
  > ON L/O FOUND EMERGENCY OVERHEAD PATH LIGHTING AT SEATS 23ABC AND 17D INOP. RELAMPED SAME, OPS CHECK NORMAL.
- [SDR DL733030563](https://openairdocs.org/sdr/DL733030563.md): Bulkhead · corroded · Jun 19, 2003 · N311WA · Boeing 737347 · Fuselage Main, Bulkhead
  > CORROSION WAS FOUND ON THE FWD SIDE OF THE AFT PRESSURE BULKHEAD. THE DAMAGE IS TO THE WEB AND STIFFENER AT THE BOTTOM OF THE BULKHEAD AT BL 0 AND STA 1016. DAL ER/A 385133-14AD PROVIDES INSTRUCTIONS TO REPAIR THE WEB AND STIFFENER PER BOEING SB 737-53A1075,
- [SDR DL733030502](https://openairdocs.org/sdr/DL733030502.md): Skin · cracked · May 31, 2003 · N3301 · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST ABOVE STRINGER 24R AND A 2 INCH CRACK JUST BELOW STRINGER 24R. THE CRACKS RAN ALONG THE BONDED WAFFLE DOUBLER MILL LINE. THERE WAS AN EXISTING EXTERNAL DOUBLER REPAIR IN THE AREA FOR SIMILAR PREVIOUS CRACK

Next page: https://openairdocs.org/model/boeing-737-347/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 = '737347'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-347/reports

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