# Service difficulty reports: Boeing 737-247 A list on [Boeing 737-247](https://openairdocs.org/model/boeing-737-247.md). Newest first. General aviation reporting is voluntary. Page 1 of 21 · 1,009 reports - [SDR DALA1205440382](https://openairdocs.org/sdr/DALA1205440382.md): Battery Pack · failed · Jan 31, 2012 · N382DL · Boeing 737247 · Door Warning System > FOUND ASPSU BATTERY PACK FAILED TEST ON WORK CARD 43-05528-0025. REPLACED BATTERY, OPS CHECK GOOD, SFO 514588 JAN 31. (2012-00050). - [SDR DL73S060680](https://openairdocs.org/sdr/DL73S060680.md): Throttle Cable · disconnected · Aug 23, 2006 · N376DL · Boeing 737247 · Power Lever > RT ENGINE ADVANCED TO MAX FIREWALL THRUST BY ITSELF WHEN A CLIMB WAS BEGAN OUT OF FL280 TO FL 350 USING VERT SPD CLIMB MODE A/P WITH AUTOTHROTTLES ENGAGED. ENG PEGGED AT RED LINE MAX INDS THERE WAS NO ENGINE RESPONSE TO THRUST LEVER MOVEMENT BY PILOT TO CLOSE - [SDR DL73S060558](https://openairdocs.org/sdr/DL73S060558.md): Charger · inoperative · Jul 7, 2006 · N376DL · Boeing 737247 · Emergency Lighting > ON LAYOVER CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EVACUATION FLOOD LIGHT INOP. REPLACED POWER SUPPLY CHARGER AND BATTERY PACK AFT RT SIDE. LIGHTS CHECK GOOD. - [SDR DL73S060410](https://openairdocs.org/sdr/DL73S060410.md): Skin · cracked · May 17, 2006 · N237WA · Boeing 737247 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 525 JUST ABOVE S-16L. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOULBER WAS INSTALLED. - [SDR DL73S060408](https://openairdocs.org/sdr/DL73S060408.md): Skin · cracked · May 17, 2006 · N237WA · Boeing 737247 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 524, JUST ABOVE S16R. THE CRACK WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060347](https://openairdocs.org/sdr/DL73S060347.md): Floor Support · cracked · Apr 29, 2006 · N238WA · Boeing 737247 · Fuselage Miscellaneous Structure > THE LBL 24 FLOOR SUPPORT IS CRACKED AND REQUIRES REPLACEMENT OF A CHANNEL AND WEB DOUBLER FOR COMPLIANCE WITH AD 2001-17-18. OVERSIZED THE CRACKED HOLE AND REPLACED THE WEB DOUBLER AND CHANNEL REF AD 2001-17-18. - [SDR DL73S060193](https://openairdocs.org/sdr/DL73S060193.md): Skin · punctured · Mar 14, 2006 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin > PUNCTURE DAMAGE TO DUE TO RUNNING A/C INTO TAILDOCK. PUNCTURE AT FS 940, BETWEEN S-19L & S-20L. TWO EXISTING REPAIRS NEAR BY. DAMAGE WAS CUT OUT AND A DOUBLER WAS INSTALLED. - [SDR DL73S060128](https://openairdocs.org/sdr/DL73S060128.md): Control Panel · intermittent · Feb 14, 2006 · N243WA · Boeing 737247 · Cabin Pressure Control System > LOST CONTROL OF CABIN PRESSURIZATION AT FL 230. SYSTEM REVERTED TO STBY MODE BUT STILL UNABLE TO CABIN ALT BELOW 1000 FT. OUTFLOW VALVE COULD BE SEEN SWINGING OPEN/CLOSED WITH EXPECTED SWING IN CABIN VSI RATES. REPLACED AUTO PRESS CONTROL PANEL. TESTS NORM - [SDR DL73S060064](https://openairdocs.org/sdr/DL73S060064.md): Floorbeam · cracked · Jan 15, 2006 · N242WA · Boeing 737247 · Fuselage Main, Floor Beam > THE LBL 24.8 OVERWING FLOORBEAM PREVIOUSLY MODIFIED PER 03-056673-03AD, BUT IT NO LONGER MEETS THE REQUIREMENT OF AD 2001-17-18. THE DISCREPANT CHANNEL WAS REPLACED WITH A NEW CHANNEL. - [SDR DL73S060030](https://openairdocs.org/sdr/DL73S060030.md): Smoke Detector · malfunctioned · Jan 9, 2006 · N243WA · Boeing 737247 · Smoke Detection > TEN MINUTES PRIOR TO LANDING LAV SMOKE LIGHT ON OVERHEAD PANEL CAME ON WITH CHIME ON P/A. FLT ATTENDANT HAD NO INDICATION OF SMOKE IN EITHER LAV OR CABIN. FIVE MINUTES TO LANDING LAV SMOKE LIGHT WENT OUT WITH NO CHIME. NO SMOKE WAS EVER DETECTED BY CREW. Q - [SDR DL73S060004](https://openairdocs.org/sdr/DL73S060004.md): Power Supply · inoperative · Jan 1, 2006 · N373DL · Boeing 737247 · Emergency Lighting > L1 AND R1 EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY. - [SDR DL73S050810](https://openairdocs.org/sdr/DL73S050810.md): Filter · bypassing · Dec 20, 2005 · N376DL · Boeing 737247 · Turbine Engine Oil System > NR 2 ENG FILTER BYPASS LIGHT ILLUM IN FLT. ALL ENG PARAMETERS NORMAL. PRESS STAYED GOOD WITH ENG SHUT DOWN. REPLACED FILTER AND DIFF PRESSURE SWITCH. - [SDR DL73S050807](https://openairdocs.org/sdr/DL73S050807.md): Sensor · out of rig · Dec 19, 2005 · N237WA · Boeing 737247 · Landing Gear Retraction/Extension System > GEAR HANDLE WOULD NOT COME UP. FOLLOWED QRH PROCEDURE TO GETGEAR UP AND THEN DOWN. ADJUST AIR SENSOR SAFETY GAP. - [SDR DL73S050802](https://openairdocs.org/sdr/DL73S050802.md): Rod End · broken · Dec 18, 2005 · N237WA · Boeing 737247 · Landing Gear Actuator > NOSE GEAR UNSAFE ALTERNATE EXTEND, GEAR STILL UNSAFE. NOSE GEAR LOCK ACTUATOR BROKEN ROD END. REPLACED LOCK ACTUATOR. - [SDR DL73S050805](https://openairdocs.org/sdr/DL73S050805.md): Floorbeam · cracked · Dec 16, 2005 · N244WA · Boeing 737247 · Fuselage Main, Floor Beam > THE RBL 24.8 FLOORBEAM HAD A PREVIOUS CHANNEL REPAIR INSTALLED THAT DOES NOT COMPLY WITH A RECENT AD. CHANNEL REPLACED PER ER/A 452157-14AD. - [SDR DL73S050804](https://openairdocs.org/sdr/DL73S050804.md): Floorbeam · cracked · Dec 16, 2005 · N244WA · Boeing 737247 · Fuselage Main, Floor Beam > THE OVERWING FLOORBEAM AT LBL 24.8 WAS PREVIOUSLY REPAIRED WITH A CHANNEL THAT DID NOT MEET THE REQUIREMENTS OF A RECENT AD. REPLACED THE C-CHANNEL REPAIR WITH A NEW CHANNEL. - [SDR DL73S050792](https://openairdocs.org/sdr/DL73S050792.md): Power Supply · inoperative · Dec 15, 2005 · N239WA · Boeing 737247 · Emergency Lighting > DURING LAYOVER, FOUND EMERGENCY ESCAPE PATH LIGHTING INOP FROM 1C TO 14DEF. REPLACED POWER SUPPLY AT FIRST CLASS CENTER AISLE OVERHEAD. - [SDR DL73S050756](https://openairdocs.org/sdr/DL73S050756.md): Fuse · blown · Dec 2, 2005 · N239WA · Boeing 737247 · Emergency Lighting > APPROX 1/3 OF EMERGENCY LIGHTS ARE INOP. FOUND BATTERY CHARGER FUSES BLOWN AT M9026. T/S FOUND EMERGENCY WIRES IN 3 LOCATION SHORTED TO GROUND. REPAIRED WIRING PER M/M. REPLACED BATTERY CHARGERS M9026 AND M1132, EMERGENCY LIGHTING OPS NORMAL. - [SDR DL73S050752](https://openairdocs.org/sdr/DL73S050752.md): Floorbeam · cracked · Nov 28, 2005 · N237WA · Boeing 737247 · Fuselage Main, Floor Beam > CRACKS WERE FOUND IN THE RBL 24.8 FLOORBEAM. REINFORCED CHORD AND WEB WITH ANGLES, CHANNELS, AND DOUBLERS REF AD 2001-17-18, 93-17-08, 90-06-02 AND 03-056673-03AD. - [SDR DL73S050751](https://openairdocs.org/sdr/DL73S050751.md): Floorbeam · cracked · Nov 28, 2005 · N237WA · Boeing 737247 · Fuselage Main, Floor Beam > CRACKS WERE FOUND IN THE OVERWING FLOORBEAMS AT LBL 24.8. EXISTING FLOORBEAM REPAIR/MODIFICATION WAS REMOVED AND STRUCTURAL REINFORCING WAS ADDED TO THE FLOORBEAM REF AD 2001-17-18, 93-17-08, 90-06-02, 3-056673-03AD. - [SDR DL73S050736](https://openairdocs.org/sdr/DL73S050736.md): Skin · cracked · Nov 21, 2005 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin > CRACKS WERE FOUND IN THE FUSELAGE SKIN AT BS 727B-750, STR 18R AT THE CHEM MILL. CRACKS WERE REMOVED AND A DOUBLER INSTALLED PER ER/A 451748-14AD AND THE SRM. REF AD 2004-18-06, 2005-13-30. - [SDR DL73S050680](https://openairdocs.org/sdr/DL73S050680.md): Floorbeam · cracked · Nov 3, 2005 · N243WA · Boeing 737247 · Fuselage Main, Floor Beam > CRACKS WERE FOUND IN THE LBL 0.07 FLOORBEAM UPPER CHORD AT THE FLOOR PANEL ATTACH HOLES BETWEEN BS 660-663. CHORD WAS REPAIRED AND MODIFIED PER ER/A 451389-14. REF S/B 737-57-1210 AND 3-062982-03AD. - [SDR DL73S050607](https://openairdocs.org/sdr/DL73S050607.md): Bulkhead · damaged · Oct 11, 2005 · N245WA · Boeing 737247 · Fuselage Main, Bulkhead > WHILE ACCOMPLISHING BOEING RECOMMENDED REWORK TO AN AFT PRESSURE BULKHEAD REDIAL STIFFENER REPAIR INSTALLED PER ER/A 089941-14AD, SEVERAL ELONGATED AND OVERSIZED HOLES WERE FOUND IN THE WEB AND STIFFENER. DAMAGE ALSO OCCURRED TO THE PAN DURING REWORK. INSTAL - [SDR DL73S050608](https://openairdocs.org/sdr/DL73S050608.md): Skin · cracked · Oct 5, 2005 · N376DL · Boeing 737247 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND IN THE FUSELAGE SKIN AS A RESULT OF INSPECTION PER DAL OPN 57546. THE CRACK IS APPROX 1.5 INCH LONG AT BS 525 ABOVE STRINGER 16L. INSTALLED DOUBLER REPAIR PER B737-200 SRM 53-30-3, FIG 48, DETAIL XI AND ER/A 450994-14AD. - [SDR DL73S050566](https://openairdocs.org/sdr/DL73S050566.md): Engine · malfunctioned · Sep 26, 2005 · N244WA · Boeing 737247 · Engine (Turbine/Turboprop) > MOMENTS AFTER ADDING T/O POWER HEARD A LOUD BOOM FROM RT SIDE OF A/C. ABORTED T/O APPROX 20 KTS. PAX REPORTED ORANGE FLAME FROM NR 2 ENG EXHAUST. SHUTDOWN NR 2 ENG AFTER CLEAR OF RUNWAY. NO ABNORMAL ENG INDICATIONS, NO FIRE INDICATION. INSP NR 2 INTAKE AN - [SDR DL73S050609](https://openairdocs.org/sdr/DL73S050609.md): Floorbeam · cracked · Sep 24, 2005 · N375DL · Boeing 737247 · Fuselage Main, Floor Beam > FUSELAGE/OVERWING LONGITUDINAL FLOORBEAMS, CRACK REPAIR DURING ACCOMPLISHMENT OF INSPECTIONS OF THE LT/RT BL 24.8 OVERWING LONGITUDINAL FLOORBEAMS PER SI 3-056673-12AD, FATIGUE CRACKS WERE DETECTED IN THE WEB DOUBLERS AND BS 678 VERTICAL STIFFENER. CRACKED DO - [SDR DL73S050563](https://openairdocs.org/sdr/DL73S050563.md): Acm · unserviceable · Sep 21, 2005 · N237WA · Boeing 737247 · Cabin Cooling System > A/C WOULD NOT MAINTAIN CABIN PRESSURE. REPLACED RT ACM AND FWD LAV FILL LINE CHECK VLV. - [SDR DL73S050625](https://openairdocs.org/sdr/DL73S050625.md): Floorbeam · cracked · Sep 19, 2005 · N373DL · Boeing 737247 · Fuselage Main, Floor Beam > DURING INSPECTION PER SI 3-56673-12, AN EXISTING REPAIR/MODIFICATION WAS FOUND TO BE CRACKED IN THE UPPER FORWARD HOLE OF THE WEB DOUBLER, WEB, UPPER CHORD, AND MOD CHANNEL AT RBL 24.8 AND LBL 24.8. CRACKS WERE REMOVED, WEB DOUBLERS, CHORDS, AND MOD CHANNELS - [SDR 05FDEA02933](https://openairdocs.org/sdr/05FDEA02933.md): Radar · malfunctioned · Sep 15, 2005 · N237FE · Boeing 737247 · Weather Radar System > RADAR INOP WITH RANGE AT 40 MILES, 15 LOW TILT, NO GND RETURN, LEVEL FLIGHT 80 MILE RANGE TILT 1.5 UP, RADAR SHOWED NUMEROUS RETURNS WITH VISUALLY NO WEATHER AHEAD. WEATHER RADAR OPS CHKS NORMAL ON GRND IAW 727-200AMM 34-41-000-0. - [SDR DL73S050449](https://openairdocs.org/sdr/DL73S050449.md): Transmitter · leaking · Aug 12, 2005 · N243WA · Boeing 737247 · Engine Thrust Reverser > ODOR IN CABIN, DIVERSION TO CLT. FOUND HYDRAULIC LEAK AT RT THRUST REVERSER PRESSURE TRANSMITTER LEAKING INTO RT PACK INLET. SECURED LEAK. CLEANED PACK INLET. REPLACED COALESCER. - [SDR DL73S050330](https://openairdocs.org/sdr/DL73S050330.md): Skin · cracked · Jun 20, 2005 · N245WA · Boeing 737247 · Fuselage Main, Plate/Skin > FUSELAGE, SKIN, STA 727B, STRINGER 18R AND 19R SKIN CRACK. FATIGUE CRACK AT CHEM-MIL LINE. SKIN CRACK WAS FOUND DURING INSPECTION FOR CHEM-MIL LINE CRACKS NEAR AN EXISTING REPAIR. ADJACENT REPAIR WAS REMOVED AND A SINGLE REPAIR ENCOMPASSING BOTH DAMAGE LOCA - [SDR DL73S050233](https://openairdocs.org/sdr/DL73S050233.md): Tire · damaged · Apr 22, 2005 · N373DL · Boeing 737247 · Tire > NR 2 MAIN TIRE LOST CAP ON OUTBOUND HOU /AFTER LOSS OF A-SYSTEM HYDRAULICS, CREW MANUALLY EXTENDED GEAR, LANDED IN ATL WITHOUT INCIDENT. TIRE REMAINED INFLATED /DAMAGE TO LEADING EDGE OF MID FLAP AND HYDRAULIC LEAK PRESENT DUE TO DAMAGED LINES IN WHEEL WELL. - [SDR DL73S050211](https://openairdocs.org/sdr/DL73S050211.md): Bulkhead · cracked · Apr 8, 2005 · N382DL · Boeing 737247 · Fuselage Main, Bulkhead > THE AFT PRESSURE P-DOME WEB WAS FOUND WITH CRACKS AS FASTENER HOLES COMMON TO THE Y-CHORD AT STRINGER 6L. THE CRACKS ARE TYPICAL OF AD 99-08-23. THE CRACKS WERE REMOVED WITH A CUTOUT AND REPAIRED WITH ALUMINUM DOUBLERS PER B737 SRM AND PER ER/A 097892-14AD. - [SDR DL73S050170](https://openairdocs.org/sdr/DL73S050170.md): Gusset · cracked · Mar 15, 2005 · N374DL · Boeing 737247 · Fuselage Miscellaneous Structure > THE GUSSET SURROUNDING THE LOWER HINGE CUTOUT FOR THE FWD FRAME ASSEMBLY OF THE L1 DOOR CUTOUT WAS FOUND WITH A SMALL CRACK IN THE RADIUS OF THE GUSSET. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 097525-14. - [SDR DL73S050126](https://openairdocs.org/sdr/DL73S050126.md): Skin · cracked · Feb 20, 2005 · N243WA · Boeing 737247 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND WITH A 1.2 INCH CRACK NEAR FS 767, RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 19R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B - [SDR DL73S050125](https://openairdocs.org/sdr/DL73S050125.md): Skin Panel · cracked · Feb 20, 2005 · N243WA · Boeing 737247 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND WITH A 1.5 INCH LONG CRACK AT APPROX FS 727B RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 18R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOU - [SDR DL73S041144](https://openairdocs.org/sdr/DL73S041144.md): Fuel Control · malfunctioned · Dec 27, 2004 · N239WA · Boeing 737247 · Fuel Control/Turbine Engines > AT APPROX 9800 FT DURING MANUAL POWER ADVANCE NR 2 ENGINE COMPRESSOR STALLED. REPLACED FUEL CONTROL. - [SDR DL73S041119](https://openairdocs.org/sdr/DL73S041119.md): Pump · failed · Dec 18, 2004 · N373DL · Boeing 737247 · Hydraulic Pump (Electric/Engine), Main > LOSS OF A-SYSTEM HYDRAULIC PRESSURE IN FLIGHT. REPLACED BOTH ENGINE PUMPS DUE A-SYSTEM CONTAMINATION. - [SDR DL73S041088](https://openairdocs.org/sdr/DL73S041088.md): Skin · corroded · Dec 6, 2004 · N243WA · Boeing 737247 · Fuselage Main, Plate/Skin > FOUND ON S2 LETTER CK, CORROSION ON LOWER FUSELAGE SKIN STA 727A BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. REPAIRED PER SRM 53-30-3 FIG 1. - [SDR DL73S041068](https://openairdocs.org/sdr/DL73S041068.md): Fitting · corroded · Nov 30, 2004 · N376DL · Boeing 737247 · Horizontal Stabilizer, Attach Fittings > HORIZONTAL STABILIZER RT AND LT CENTER AND OUTBOARD SECTION LUG FITTINGS AT THE FRONT AND REAR SPAR CORRODED AND DAMAGE. REPAIRED IAW ER/A 094975-14AD & 094865-14AD. - [SDR DL73S041066](https://openairdocs.org/sdr/DL73S041066.md): Stringer · damaged · Nov 29, 2004 · N376DL · Boeing 737247 · Fuselage Main, Longeron/Stringer > STRINGER 5L AND AFT ENTRY BEAR STRAP SUFFERED DAMAGE. REPAIRED IAW ERA 094945-14. - [SDR DL73S041059](https://openairdocs.org/sdr/DL73S041059.md): Shear Tie · damaged · Nov 24, 2004 · N376DL · Boeing 737247 · Fuselage Main, Structure > STATION 927 WEB AND SHEAR TIE REPAIRED AT STRINGER 5L DUE TO TOOLING DAMAGE. REPAIRED IAW ERA 095091-143. - [SDR DL73S041058](https://openairdocs.org/sdr/DL73S041058.md): Fitting · corroded · Nov 24, 2004 · N376DL · Boeing 737247 · Vertical Stabilizer, Attach Fittings > VERTICAL STABILIZER ATTACH FITTINGS NR 3 AND NR 6 LUGS WORN ON THE AFT FACES DUE TO CORROSION. REPAIRED IAW ERA 095030-14. - [SDR DL73S041057](https://openairdocs.org/sdr/DL73S041057.md): Skin · worn · Nov 24, 2004 · N376DL · Boeing 737247 · Wing, Plate/Skin > LT LOWER WING SKIN WORN AT FUEL TANK ACCESS DOOR CUTOUT. REPAIRED IAW ERA 094867-14. - [SDR DL73S041044](https://openairdocs.org/sdr/DL73S041044.md): Attach Fitting · corroded · Nov 20, 2004 · N376DL · Boeing 737247 · Fuselage, Stabilizer Attach Fittings > BODY CLEVIS LUGS FOR VERTICAL STABILIZER ATTACH FITTINGS CORRODED. REPAIRIED IAW ERA 095009-14. - [SDR DL73S041043](https://openairdocs.org/sdr/DL73S041043.md): Shear Beam · cracked · Nov 20, 2004 · N376DL · Boeing 737247 · Fuselage Main, Structure > STRINGER 18A SHEAR BEAM WEB CRACKED AT STA 727 ON BOTH THE LT AND RT SIDES. REPAIRED IAW ERA 094822-14. - [SDR DL73S041039](https://openairdocs.org/sdr/DL73S041039.md): Skin · damaged · Nov 17, 2004 · N376DL · Boeing 737247 · Fuselage Main, Plate/Skin > FUSELAGE SKIN DAMAGED AT THE C1 DOOR CUTOUT AT STATION 440 AND STR 23R - 24R. REPAIRED IAW ERA 257313-14 REV E. - [SDR DL73S041016](https://openairdocs.org/sdr/DL73S041016.md): Skin · cracked · Nov 4, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin > INSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVELED A 4 INCH LONG CRACK RUNNING ALONG THE BONDED DOUBLER EDGE AT STRINGER 18L AND FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 094729-14AD. - [SDR DL73S041015](https://openairdocs.org/sdr/DL73S041015.md): Skin · cracked · Nov 4, 2004 · N242WA · Boeing 737247 · Fuselage Main, Plate/Skin > INSPECTION OF THE SKIN PER AD 2004-18-06 REVEALED A 4.7 INCH CRACK ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 24L BETWEEN FS 937 & 947. THE CRACK WAS ADJACENT TO AN EXISTING REPAIR DOUBLER FOR ANOTHER SKIN CRACK CUTOUT. THE CRACK WAS REMOVED WITH A CU - [SDR DL73S041003](https://openairdocs.org/sdr/DL73S041003.md): Smoke Detector · false activation · Oct 30, 2004 · N243WA · Boeing 737247 · Smoke Detection > LAV SMOKE LIGHT CAME ON IN FLIGHT. SILENCED ALARM AND F/A INVESTIGATED. NO SIGN OF SMOKE. TESTED LAV SMOKE DETECTORS PER M/M. CHECKS GOOD. Next page: https://openairdocs.org/model/boeing-737-247/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 = '737247' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-737-247/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.