# Service difficulty reports: N302DL, cancelled May 8, 2008 A list on [N302DL, cancelled May 8, 2008](https://openairdocs.org/deregistered/N302DL-2008-05-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL73S060309](https://openairdocs.org/sdr/DL73S060309.md): Skin · cracked · Apr 18, 2006 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN AT THE FWD ENTRY DOOR UPPER HINGE CUTOUT IS CRACKED AT THE UPPER CORNER. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060246](https://openairdocs.org/sdr/DL73S060246.md): Floor Support · cracked · Apr 3, 2006 · N302DL · Boeing 737232 · Fuselage Miscellaneous Structure > THE LONGITUDINAL OVERWING FLOOR SUPPORT HAS CRACKS IN THE WEB AND LOWER CHORD. A DOUBLER WAS INSTALLED TO REPAIR THE WEB AND A STRAP WAS INSTALLED TO REPAIR FLOOR SUPPORT. - [SDR DL73S060199](https://openairdocs.org/sdr/DL73S060199.md): Skin · cracked · Mar 15, 2006 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > INSPECTIONS OF THE STRINGER 4L SKIN LAP REVEALED A SINGLE CRACKED FASTENER HOLE NEAR FS 490. THE CRACKED AREA OF SKIN WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR PER B737 SRM 53-30-3 FIG 42 AND ER/A 454521-14AD. - [SDR DL73S060192](https://openairdocs.org/sdr/DL73S060192.md): Skin · cracked · Mar 15, 2006 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > FATIGE CRACK IN SKIN IN LOWER ROW OF S-4R LAP JOINT AT FS 410. CUT OUT SKIN AND INSTALLED REPAIR PARTS PER ER/A. - [SDR DL73S060191](https://openairdocs.org/sdr/DL73S060191.md): Skin · cracked · Mar 15, 2006 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > FATIGUE CRACK IN LOWER ROW OF S-14L LAP JOINT, FS 380. CUT OUT CRACK AND REPAIRED PER ER/A. - [SDR DL73S060190](https://openairdocs.org/sdr/DL73S060190.md): Skin · cracked · Mar 15, 2006 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > FATIGUE CRACK AT FASTENER IN LOWER ROW OF S-4L LAP JOINT, APPROX FS 490. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER ER/A. - [SDR DL73S060187](https://openairdocs.org/sdr/DL73S060187.md): Skin · cracked · Mar 11, 2006 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > CRACK INDICATIONS WERE FOUND AT STA 385 IN THE S-4 L LAP SPLICE, FUSELAGE SKIN. ACCOMPLISHED BOLT HOLE EDDY CURRENT INSPECTION TO CONFIRM CRACK. INSPECTION FOUND NO CRACK. NO REPAIR REQUIRED. - [SDR DL73S060186](https://openairdocs.org/sdr/DL73S060186.md): Skin · cracked · Mar 10, 2006 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > CRACK INDICATIONS WERE FOUND BETWEEN STA 827-847 IN THE S-4L LAP SPLICE, FUSELAGE SKIN. ACCOMPLISHED BOLT HOLE EDDY CURRENT INSPECTION TO CONFIRM CRACK. INSPECTION FOUND NO CRACK. NO REPAIR REQUIRED. - [SDR DL73S060008](https://openairdocs.org/sdr/DL73S060008.md): Window · cracked · Jan 3, 2006 · N302DL · Boeing 737232 · Flight Compartment Windows > R1 WINDOW CRACKED WITH ARCING - REPLACED SAME. - [SDR DL73S041051](https://openairdocs.org/sdr/DL73S041051.md): Module · malfunctioned · Nov 22, 2004 · N302DL · Boeing 737232 · Fire Detection > ON CLIMBOUT AT 14,000 FEET NR 1 ENG OVERHEAT LIGHT ILLUM. IAW CK LIST THRUST LEVER RETARDED. LIGHT WENT OUT. REPLACED ENG FIRE/OVERHEAT MODULE. RAN ENGS AT T/O AND CLIMB PWR, ALL TEST NORMAL. - [SDR DL73S040958](https://openairdocs.org/sdr/DL73S040958.md): Actuator · failed · Oct 10, 2004 · N302DL · Boeing 737232 · Drag Control Actuator > AFTER LANDING A-SYS HYD QTY DROPPED TO 0. REPLACED NR 1 SPOILER ACTUATOR FOR LEAKING. - [SDR DL73S040402](https://openairdocs.org/sdr/DL73S040402.md): Rmi · smoke · May 6, 2004 · N302DL · Boeing 737232 · Visual Omnirange (VOR) System > NR 2 RMI STARTED TO SMOKE. REPLACED SAME - [SDR DL73S040259](https://openairdocs.org/sdr/DL73S040259.md): Skin · cracked · Mar 20, 2004 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > INSPECTION OF THE SKIN LAPS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 10R SKIN LAP SPLICE AT FS 432. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE CRACKED AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B - [SDR DL73S040258](https://openairdocs.org/sdr/DL73S040258.md): Skin · cracked · Mar 20, 2004 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 14R SKIN LAP JOINT. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE DAMAGED AREA AND AN ALUMINUM REPAIR DOUBLER INSTALLED PER B737 SRM AND DOCUMENTED P - [SDR DL73S040248](https://openairdocs.org/sdr/DL73S040248.md): Stringer · cracked · Mar 12, 2004 · N302DL · Boeing 737232 · Fuselage Main, Longeron/Stringer > STRINGER 4L DAMAGED IN LWR RADIUS AT STA 797. REPAIRED PER SRM 53-10-3 FIG 4. - [SDR DL73S040045](https://openairdocs.org/sdr/DL73S040045.md): Charger · inoperative · Jan 15, 2004 · N302DL · Boeing 737232 · Emergency Lighting > MCO OVERHEAD EMERGENCY LIGHT BULLNOSE INOP 19D. FOUND BATTERY CHARGER RACK AT M1134 STA 629L INOP. REPLACED CHARGER RACK. - [SDR DL73S030899](https://openairdocs.org/sdr/DL73S030899.md): Duct · damaged · Oct 3, 2003 · N302DL · Boeing 737232 · Engine Start Valves/Controls > RT ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB, WENT OUT WITH THROTTLE AT IDLE. FOUND DAMAGED STARTER DUCT. REPLACED SAME. - [SDR DL73K030140](https://openairdocs.org/sdr/DL73K030140.md): Bulkhead · cracked · Feb 8, 2003 · N302DL · Boeing 737232 · Fuselage Main, Bulkhead > FUSELAGE / BULKHEAD / FS 178 / WEB AND SIDE CHORDS: CRACK REPAIR THE FS 178 BULKHEAD WEB AND SIDE CHORDS WERE FOUND WITH CRACKS TYPICAL OF BAC S/B 737-53-1173 AND AD 2000-05-29. THE WEB HAD SEVERAL - [SDR DL73K010691](https://openairdocs.org/sdr/DL73K010691.md): Floorbeam · cracked · Apr 28, 2001 · N302DL · Boeing 737232 · Fuselage Main, Floor Beam > THE LONGITUDINAL FLOOR BEAM AT RBL 24 WAS FOUND WITH A TYPICAL CRACK IN THE BEAM WEB AND WEB DOUBLER AT FS 678. THE BEAM UPPER CHORD WAS FOUND CRACKED AT FS 674. THE UPPER CHORD WAS REMOVED AND REPLACED. THE WEB DOUBLER WAS REPLACED PER BAC S/B 737-57-1 - [SDR DL73K010617](https://openairdocs.org/sdr/DL73K010617.md): Power Supply · discharged · Apr 14, 2001 · N302DL · Boeing 737232 · Emergency Lighting > RT AFT AISLE EMERGENCY LIGHT INOP. REPLACED BATTERY POWER SUPPLY CKS NORMAL - [SDR DL73K010475](https://openairdocs.org/sdr/DL73K010475.md): Mount · worn · Mar 23, 2001 · N302DL · Boeing 737232 · Engine Mount Section > FWD ENGINE MOUNT FOUND WITH MIGRATING BEARING RESULTING IN OVERSIZED MOUNT HOLES. REPAIR PER ER/A 401250-14AD. - [SDR DL73K002050](https://openairdocs.org/sdr/DL73K002050.md): Pcu · malfunctioned · Oct 18, 2000 · N302DL · Boeing 737232 · Rudder Control System > ON T/O ROLL 125 KNOTS FELT A UNCOMMANDED YAW TO THE RIGHT, FELT LIKE SOMEONE KICKED THE RUDDER PEDAL. REPLACED RUDDER PCU PER M/M. - [SDR DL73K001174](https://openairdocs.org/sdr/DL73K001174.md): Coffeemaker · burned · Jun 18, 2000 · N302DL · Boeing 737232 · Buffet/Galleys > ON T/O, STRONG SMELL OF SMOKE/ELECTRICAL/SULFUR. RETURN TO LAND MCO OVERWEIGHT LANDING AT 200 FPM, LANDING WEIGHT 112.8. REPLACED BOTH COALESCER BAGS. BOTH CLEAN, NO ODOR. PULLED FLIGHT INSTRUMENTS, NO SMELL. OPENED C/B PANELS, NO SMELLS. FOUND BURNT COF - [SDR DL73K001089](https://openairdocs.org/sdr/DL73K001089.md): Smoke Detector · will not test · Jun 3, 2000 · N302DL · Boeing 737232 · Smoke Detection > AFT LAV SMOKE DETECTOR WOULD NOT TEST. REPLACED SMOKE DETECTOR. - [SDR DL73K000595](https://openairdocs.org/sdr/DL73K000595.md): Unknown · odor · Mar 29, 2000 · N302DL · Boeing 737232 · Air Distribution System > FLT 2452 MCO-EWR, HAD ELECTRICAL ODOR AROUND THE FWD F/A JUMPSEAT. CREW DIVERTED TO RIC. TROUBLESHOOTING WITH CONTRACT MTC AND NOTHING FOUND. SENT MECH FROM CVG DUE TO ATL FLT DELAYED DUE TO MECHANICAL. DAL MECH ALSO FOUND NOTHING WRONG WITH ACFT. - [SDR DL73K000557](https://openairdocs.org/sdr/DL73K000557.md): Doubler · worn · Mar 22, 2000 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > AN EXISTING DOUBLER WAS WORN ALONG IT'S AFT EDGE LOCATED AT THE FORWARD EDGE OF THE C1 DOOR. THE DOUBLER WAS REMOVED AND REPLACED PER ERA 334214-14. THE DAMAGE WAS FOUND AT HMV. - [SDR DL73K000539](https://openairdocs.org/sdr/DL73K000539.md): Spar · corroded · Mar 20, 2000 · N302DL · Boeing 737232 · Horizontal Stabilizer, Spar/Rib > CORROSION WAS FOUND ON THE FRONT AND REAR SPAR OF THE HORIZONTAL STABILIZER CENTER SECTION ATTACH FITTING. CORROSION WAS FOUND ON THE FORWARD AND AFT FACES AND IN THE BORE. THE DAMAGE WAS REMOVED, TREATED AND PAINTED PER ERA 334168-14 AT HMV. - [SDR DL73K000538](https://openairdocs.org/sdr/DL73K000538.md): Fitting · corroded · Mar 20, 2000 · N302DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings > CORROSION WAS FOUND ON THE REAR SPAR ATTACH LUGS OF THE HORIZONTAL STABILIZER. THE CORROSION WAS TO THE FORWARD AND AFT FACES OF THE FITTING AND INSIDE THE LOWER BORE. THE CORROSION WAS REMOVED, TREATED AND PAINTED PER ERA 334170-14AT HMV. - [SDR DL73K000526](https://openairdocs.org/sdr/DL73K000526.md): Fitting · corroded · Mar 17, 2000 · N302DL · Boeing 737232 · Vertical Stabilizer > CORROSION WAS FOUND ON THE FORWARD AND AFT FACE OF BOTH THE INNER LUGS OF THE VERTICAL STABILIZER ATTACH FITTING. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED AND PAINTER PER ERA 334169-14. THE DAMAGE WAS FOUND AT HMV. - [SDR DL73K000525](https://openairdocs.org/sdr/DL73K000525.md): Fitting · corroded · Mar 17, 2000 · N302DL · Boeing 737232 · Fuselage Main, Attach Fittings > CORROSION WAS FOUND ON ALL EIGHT OF THE AFT SPAR ATTACH LUGS ON THE BODY ATTACHMENT POINT FOR THE VERTICAL STABILIZER AT APPROXIMATELY FS 1080. CORROSION WAS REMOVED AND THE AREA TREATED AND PAINTED PER ERA 334185-14 AT HMV. - [SDR DL73K000518](https://openairdocs.org/sdr/DL73K000518.md): Doubler · worn · Mar 16, 2000 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > WEAR WAS FOUND ON THE LAP JOINT LOWER INTERNAL BONDED DOUBLER AT APPROXIMATELY FS 310 AND STR 10L JUST BELOW THE L1 DOOR UPPER HINGE CUTOUT. THE WEAR WAS.25 IN DIAMETER AND A MAXIMUM OF.011 DEEP. THE AREA WAS BLENDED AND TREATED PER ERA 334203-14. THE DAM - [SDR DL73K992800](https://openairdocs.org/sdr/DL73K992800.md): Seal · separated · Dec 20, 1999 · N302DL · Boeing 737232 · Turbine Engine Compressor Section > NR 1 ENG HAD MULTIPLE COMPRESSOR STALLS AT FL310 AS THROTTLES RETARDED FROM CLIMB EPR TO CRUISE EPR OF 1.96. COMPRESSOR STALLS STOPPED AS THROTTLES WERE PULLED TO IDLE THE ENG WAS NOT SHUTDOWN AND OPERATED NORMALLY AT IDLE. REPLACED C2 FAN FOR SEAL LIBERATIO - [SDR DL73K992651](https://openairdocs.org/sdr/DL73K992651.md): Light · inoperative · Dec 4, 1999 · N302DL · Boeing 737232 · Emergency Lighting > EMERGENCY EXIT LIGHTING INOP ROWS 1 THRU 3. REPLACED PWR SUPPLY AND FOUND WIRES SHORTED AT ROW 4 D, E, F. REPAIRED SAME, OPS CKS NORMAL. - [SDR DL73K991413](https://openairdocs.org/sdr/DL73K991413.md): Light · inoperative · Jun 22, 1999 · N302DL · Boeing 737232 · Emergency Lighting > ON MTC INSPECTION, FOUND FWD CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH AFTER TEST. REPLACED POWER SUPPLY AND TEST GOOD. - [SDR DL73K991221](https://openairdocs.org/sdr/DL73K991221.md): Fitting · corroded · May 28, 1999 · N302DL · Boeing 737232 · Fuselage, Landing Gear Attach Fittings > THE LT AND RT FS 685 MLG SIDE STRUT SUPPORT FITTINGS WERE FOUND WITH CORROSION IN THE STRUT ATTACH LUG BORES. THE LUGS WERE OVERSIZED TO CLEAN UP THE CORROSION, INSPECTED, AND REPAIRED WITH STELL BUSHINGS PER ER/A 367450-14, REV A. - [SDR DL73K982186](https://openairdocs.org/sdr/DL73K982186.md): Skin · cracked · Oct 20, 1998 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > FUSELAGE SKIN, FS 520, S-16L SKIN CRACK REPAIR. THE FUSELAGE SKIN WAS FOUND WITH A CRACK ABOVE STRINGER 16L AT FS 520. THE CRACK WAS CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 1. THE REPAIR WAS DOCUMENTED PER ER/A 365917-14. THE - [SDR DL73K981000](https://openairdocs.org/sdr/DL73K981000.md): Skin · punctured · May 6, 1998 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS PUNCTURED DUE TO GROUND EQUIPMENT IMPACT AT FS 920 AND STRINGERS 21L-22L. ALSO, STRINGER 22L WAS DAMAGED. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUM DOUBLER PER SRM 53-30-3 WITH MINOR FASTENER CHANGES AND THE STRINGER WAS REPAIRED PER - [SDR DL73K970606](https://openairdocs.org/sdr/DL73K970606.md): Fuel Control · failed · Apr 3, 1997 · N302DL · Boeing 737232 · Fuel Control/Turbine Engines > PUSHED PWR UP FOR T/O AND ENGAGED, ATS NOTICED NR 2 ENG INST ROLLING BACK AS IF FLAMING OUT. PERFORMED ABORT PROCEDURES AND REALIZED NR 1 ENG WAS STILL OPER AT T/O PWR WITH BOTH THROTTLES AT IDLE. SHUT DOWN NR 1 ENG AFTER EXITING RUNWAY. REPLACED NR 1 ENGIN - [SDR DL73S961474](https://openairdocs.org/sdr/DL73S961474.md): Bulkhead Web · cracked · Jun 11, 1996 · N302DL · Boeing 737232 · Fuselage Main, Bulkhead > THREE CRACKS FOUND ON THE FWD FACE OF THE STA 178 BLKHD WEB. THE FIRST CRACK WAS LOCATED NEAR LBL 5.7 VERTICAL STRAP AT APPROX WL 195, THE SECOND CRACK WAS LOCATED NEAR RBL 5.7 VERTICAL STRAP AT APPROX WL 200 AND THE THIRD CRACK WAS LOCATED NEAR BL 0 AT APPRO - [SDR DL73S961353](https://openairdocs.org/sdr/DL73S961353.md): Floor Beam · cracked · May 27, 1996 · N302DL · Boeing 737232 · Fuselage Main, Floor Beam > THE BL.07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT FS 660. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BACO SB 737-57-1210. THIS ERA WILL INSTALL THE SERVICE BULLETIN REPAIR FOR THIS CONDITION. - [SDR DL73S960840](https://openairdocs.org/sdr/DL73S960840.md): Track Light · cracked · Apr 11, 1996 · N302DL · Boeing 737232 · Emergency Lighting > ON LAYOVER, FOUND FLOOR TRACK TOP COVER CRACKED BETWEEN ROWS 15 AND 18. REPLACED TOP TRACK BETWEEN ROWS 15 AND 18. - [SDR DL73S960744](https://openairdocs.org/sdr/DL73S960744.md): Actuator Fitting · failed · Mar 15, 1996 · N302DL · Boeing 737232 · Drag Control Actuator > ONE OF THE ACTUATOR FITTINGS HAS FAILED ON THE RT INBOARD GROUND SPOILER. THE FITTING IS THE SUBJECT OF S/B 737-57-1207. ACCOMPLISHED REPAIRS PER DL ERA 357237-14. - [SDR DL73S952370](https://openairdocs.org/sdr/DL73S952370.md): Skin · dented · May 31, 1995 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > FOUND ON LAY OVER-DENT AFT OF AFT B/B DOOR APPROX..25 INCH IN DIAMETER. REPAIRED PER SRM 53-30-3 FIG. 23. - [SDR DL73S953104](https://openairdocs.org/sdr/DL73S953104.md): Skin · damaged · Jan 19, 1995 · N302DL · Boeing 737232 · Fuselage Main, Plate/Skin > DURING LAYOVER IN ATLANTA, THE FUSELAGE SKIN WAS DAMAGED JUST AFT OF STATION 360 AND JUST ABOVE STRINGER 19R WHEN STRUCK BY A BAGGAGE CONTAINER. DAMAGE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER IN ACCORDANCE WITH B737-200 SRM 53-30-3 FIG 1 PER ER/A 30 ## 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 n_number = 'N302DL' AND deregistration_id = 'N302DL-2008-05-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N302DL-2008-05-08/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.