# Service difficulty reports: N314DA, cancelled Mar 5, 2022 A list on [N314DA, cancelled Mar 5, 2022](https://openairdocs.org/deregistered/N314DA-2022-03-05.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL73S060261](https://openairdocs.org/sdr/DL73S060261.md): Lap Joint · cracked · Apr 6, 2006 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN HAS 3 CRACKS IN THE LAP JOINT AT S-10R, BS 500-500A. THE CRACKED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S060259](https://openairdocs.org/sdr/DL73S060259.md): Lap Joint · cracked · Apr 6, 2006 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > FIVE CRACKS WERE FOUND IN THE FUSELAGE LAP JOINT AT S14L BETWEEN BS 480-500A. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL73S050527](https://openairdocs.org/sdr/DL73S050527.md): Skin · cracked · Sep 8, 2005 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST ABOVE THE BONDED DOUBLER MILL LINE OF STRINGER 16R AT FS 525. THE CRACK WAS 1 INCH LONG AND TYPICAL OF THOSE DOCUMENTED IN AD 2004-18-06 AND BAC S/B 737-53A1210. THE CRACK WAS REMOVED WITH A CUT OUT AND REPAIRED - [SDR DL73S050032](https://openairdocs.org/sdr/DL73S050032.md): Proximity Switch · out of adjust · Jan 14, 2005 · N314DA · Boeing 737232 · Leading Edge Slat Control System > SELECTED FLAPS AND L/E TRANSIT AMBER LIGHT ILLUMINATED. CONFIRMED BY L/E AMBER LIGHTT ON OVERHEAD PNL. FOLLOWED QRH PROCEDURES AND PLANNED FLAP 15 LANDING. ON SHORT FINAL L/E FLAP GREEN LIGHT ILLUMINATED AND SELECTED FLAPS 30. RIGGED NR 1 L/E FLAP EXTENDED - [SDR DL73S040932](https://openairdocs.org/sdr/DL73S040932.md): Skin · cracked · Sep 27, 2004 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN AT THE L1 DOOR OPENING WAS FOUND CRACKED AT THE CUTOUT EDGE JUST ABOVE THE LOWER AFT CORNER. THE CRACKS WERE SMALL AND TYPICAL OF BAC S/B 737-53-1083. THE CRACKS WERE TRIMMED OUT OF THE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLE - [SDR DL73S040931](https://openairdocs.org/sdr/DL73S040931.md): Door Frame · cracked · Sep 27, 2004 · N314DA · Boeing 737232 · Fuselage Main, Structure > INSPECTION OF THE C2 DOOR OPENING FRAME AT FS 794 PER AD 93-14-10 REVEALED CRACK IN THE DOOR FRAME WEB AND FLANGE JUST BELOW THE NR 5 DOOR STOP FITTING. THE CRACKS WERE REMOVED WITH A CUT OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND AN EXTERNAL ALUMINUM - [SDR DL73S040883](https://openairdocs.org/sdr/DL73S040883.md): Skin · cracked · Sep 15, 2004 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK INDICATION IN A FASTENER HOLE AT FS 690. THE CRACKED AREA WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 093308-14AD. - [SDR DL73S030530](https://openairdocs.org/sdr/DL73S030530.md): Fitting · gouged · Jun 6, 2003 · N314DA · Boeing 737232 · Horizontal Stabilizer, Attach Fittings > THE UPPER ATTACH LUG OF THE HORIZONTAL STABILIZER CENTER SECTION WAS FOUND WITH A GOUGE FROM INTERFERENCED WITH AN IMPROPERLY INSTALLED FASTENER ON ADJACENT STRUCTURE. THE GOUGE WAS BLENDED TO A SMOOTH CONTOUR AND NDT INSPECTED. THE GOUGED FITTING WAS AUTHOR - [SDR DL73S030520](https://openairdocs.org/sdr/DL73S030520.md): Skin · cracked · Jun 6, 2003 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN AT FS 750 WAS FOUND WITH A 2 INCH CRACK RUNNING ALONG THE EDGE OF THE BONDED DOUBLER AT STRINGER 18R. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385222-14. - [SDR DL73S030113](https://openairdocs.org/sdr/DL73S030113.md): Bulkhead · canning · Jan 29, 2003 · N314DA · Boeing 737232 · Fuselage Main, Bulkhead > INSPECTION OF THE AFT P-DOME REVEALED A 10 X 8 X.25 INCH OIL CAN IN THE LOWER WEB AREA OF NEAR BL 0. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOULBER PER BAC S/B 737-53A1075 AND ER/A 384318-14AD. - [SDR DL73K020573](https://openairdocs.org/sdr/DL73K020573.md): Tee Fitting · cracked · May 20, 2002 · N314DA · Boeing 737232 · Hydraulic Power System > IRREG/ LOSS OF A SYSTEM HYDRAULIC QUANTITY FOLLOWED BY A LOSS OF PRESSURE AFTER LOWERING THE LANDING GEAR CA/ FOUND TEE FITTING IN THE NOSE WHEEL WELL CRACKED ____REPLACED SAME SERVICED SYSTEM NO LEAKS FOUND - [SDR DL73K011885](https://openairdocs.org/sdr/DL73K011885.md): Compressor · stalled · Dec 2, 2001 · N314DA · Boeing 737232 · Turbine Engine Compressor Section > IR - COMPRESSOR STALL NR 1 ENG ON TAKE TAKE OFF. INITIATED ABORT BETWEEN 70-80 KTS. DEAD HEATING CAPT REPORTED BRIGHT FLASH FROM NR 1 ENG SHORTLY AFTER T/O PWR ADDED. REPLACED ENGINE. - [SDR DL73K011673](https://openairdocs.org/sdr/DL73K011673.md): Frame · cracked · Oct 16, 2001 · N314DA · Boeing 737232 · Fuselage Main, Structure > 1" CRACK IN R-2 DOOR CUTOUT FRAME, JUST BELOW UPPER FWD. ROLLER CASTING REMOVE & REPLACE FRAME SECTION PER DRAWING - [SDR DL73K010311](https://openairdocs.org/sdr/DL73K010311.md): Light · intermittent · Feb 21, 2001 · N314DA · Boeing 737232 · Landing Gear Position and Warning > ON LANDING GEAR EXTENSION, RT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. BULB CK WAS GOOD. CYCLED GEAR WITH SAME INDICATION. PUSHED LIGHT ASSY SEVERAL TIMES. THEN RT GEAR LIGHT CAME ON. ALL INDICATIONS GOOD. CONFIRMED GEAR DOWN WITH CONFIG HORN A - [SDR DL73K010292](https://openairdocs.org/sdr/DL73K010292.md): Fan · faulty · Feb 18, 2001 · N314DA · Boeing 737232 · Air Distribution Fan > SMOKE AND FUMES IN COCKPIT DURING PREFLIGHT. FOUND CONTROL CABIN AUGMENTATION FAN PUTTING FUMES INTO COCKPIT. FWD TO MCO AND PLACARD. - [SDR DL73K002498](https://openairdocs.org/sdr/DL73K002498.md): Skin · corroded · Dec 22, 2000 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STATION 887 AND 907 IN THE UPPER SKIN WHERE THE VERTICAL STABILIZER FAIRING ATTACHES AT ABOUT RBL 4 AND 5. THE MAXIMUM DEPTH OF DAMAGE WAS.012" CONTAINED WITHIN A 1/5" DIAMETER. THE DAMAGE WAS REMOVED AND AN EXTER - [SDR DL73K002488](https://openairdocs.org/sdr/DL73K002488.md): Fitting · corroded · Dec 21, 2000 · N314DA · Boeing 737232 · Fuselage, Stabilizer Attach Fittings > THE RT FUSELAGE CLEVIS LUGS ATTACHING THE HORIZONTAL STABILIZER WERE FOUND CORRODED ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND NEW BUSHINGS WERE INSTALLED PER ERA 396532-14AD AT HMV. - [SDR DL73K002455](https://openairdocs.org/sdr/DL73K002455.md): Floor Support · cracked · Dec 15, 2000 · N314DA · Boeing 737232 · Fuselage Miscellaneous Structure > CRACKS WERE FOUND IN THE WEB, DOUBLER AND UPPER CHORD OF THE LBL 24 LONGITUDINAL FLOOR SUPPORT AT FS 675. THE CRACKS WERE REMOVED AND THE DAMAGE REPAIRED PER ERA 396570-14AD AT HMV. - [SDR DL73K002218](https://openairdocs.org/sdr/DL73K002218.md): Skin · cracked · Nov 11, 2000 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND WITH A 1 INCH CRACK NEAR FS 520 AND STRINGER 16L. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM 53-30-3, FIG 1 AND ER/A 379238-14. - [SDR DL73K001485](https://openairdocs.org/sdr/DL73K001485.md): Power Supply · failed · Aug 4, 2000 · N314DA · Boeing 737232 · Emergency Lighting > EMERGENCY POWER SUPPLY WOULD NOT TEST AT ROWS 14, 15 DEF. REPLACED POWER SUPPLY. - [SDR DL73K992023](https://openairdocs.org/sdr/DL73K992023.md): Fuse · blown · Sep 11, 1999 · N314DA · Boeing 737232 · Emergency Lighting > E-PATH LIGHTS INOP ROW 10 TO 18. REPLACED FUSE IN PWR SUPPLY. - [SDR DL73K990909](https://openairdocs.org/sdr/DL73K990909.md): Skin · cracked · Apr 23, 1999 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > FUSELAGE AFT GALLEY DOOR CUTOUT SKIN UPPER HINGE CUTOUT, CRACK REPAIR. THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT SKIN WAS FOUND WITH A.25 LONG TYPICAL CRACK AT THE UPPER CORNER. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DOUBLER PER ER/A 36723 - [SDR DL73K990358](https://openairdocs.org/sdr/DL73K990358.md): Blades · damaged · Feb 23, 1999 · N314DA · Boeing 737232 · Turbine Engine Compressor Section > AT CRUISE, CREW NOTE COMPRESSOR SURGING. DIVERTED TO BOS. FOUND NOSE BULLET LOOSE. DAMAGE INCURRED TO FIRST AND SECOND STAGE FAN BLADES, NOSE COWL ACCOUSTIC LINER AND N1 TACH GENERATOR HOUSING BULLET MOUNT STUDS. REPLACING 1ST AND 2ND STAGE FANS, INLET - [SDR DL73K990345](https://openairdocs.org/sdr/DL73K990345.md): Gcu · malfunctioned · Feb 21, 1999 · N314DA · Boeing 737232 · AC Regulator > ON CLIMBOUT, APU OFF BOTH GEN ON, RECEIVED A SPIKE. LOST ALL ELECTRICAL PWR IN COCKPIT AND CABIN FOR A SPLIT SECOND. NO C/B POPPED, NO EQUIP LOSS. INSPECTED LT AND RT GEN HARNESS, NTF INSPEC ENG GEN AND BUSS TIE BREAKERS. NTF RAN GCU DIODE TEST, BATTERY TE - [SDR DL73K981505](https://openairdocs.org/sdr/DL73K981505.md): Line · ruptured · Jul 20, 1998 · N314DA · Boeing 737232 · Hydraulic System, Main > LOSS OF A/B HYDRAULICS RESULTED IN DIVERSION BACK TO MCO. FOUND 01 ENG PRESS LINE RUPTURED. REPLACED SAME, LEAK CKS OK. REPLACED ALL CASE DRAIN FILTERS. - [SDR DL73K970080](https://openairdocs.org/sdr/DL73K970080.md): Bulkhead Web · cracked · Jan 10, 1997 · N314DA · Boeing 737232 · Fuselage Main, Bulkhead > DURING ACCOMPLISHMENT OF SI 3-69482-12, SEVEN CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE FS 178 BULKHEAD WEB. SEVEN INDEPENDENT CUTOUTS WERE REQUIRED TO REMOVE THE CRACKS. REPAIRED PER DALA ER/A 304632-14. - [SDR DL73K970041](https://openairdocs.org/sdr/DL73K970041.md): Skin · cracked · Jan 7, 1997 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > A CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE L2 DOOR CUTOUT IN THE UPPER AFT CORNER. THE CRACK WAS IN THE INNER LAYER OF THE BONDED SKIN ASSEMBLY AND WAS APPROX 1.75 IN LENGTH. REPAIRED PER BACO S/B 737-53-1149. - [SDR DL73S961819](https://openairdocs.org/sdr/DL73S961819.md): Skin · cracked · Jul 23, 1996 · N314DA · Boeing 737232 · Fuselage Main, Plate/Skin > FOUND A 2.25 INCH CRACK IN THE R-2 DOORWAY. REPAIRED PER B737-200 SRM 53-30-3, FIG 24. - [SDR DL73S951630](https://openairdocs.org/sdr/DL73S951630.md): Nose Cowl · damaged · Mar 17, 1995 · N314DA · Boeing 737232 · Engine Cowling System > DURING SHOP INSPECTION, A DEEP NICK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 ENGINE NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4. - [SDR DL73S951629](https://openairdocs.org/sdr/DL73S951629.md): Nose Cowl · cracked · Mar 17, 1995 · N314DA · Boeing 737232 · Engine Cowling System > DURING SHOP INSPECTION, A.5 INCH CRACK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4. ## 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 = 'N314DA' AND deregistration_id = 'N314DA-2022-03-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N314DA-2022-03-05/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.