# Service difficulty reports: N294WA, cancelled Jul 18, 2013 A list on [N294WA, cancelled Jul 18, 2013](https://openairdocs.org/deregistered/N294WA-2013-07-18.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 94 reports - [SDR DL72W020161](https://openairdocs.org/sdr/DL72W020161.md): Battery Pack · discharged · Feb 8, 2002 · N294WA · Boeing 727247 · Emergency Lighting > DURING L/O FOUND FIRST CLASS OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. - [SDR DL72W020041](https://openairdocs.org/sdr/DL72W020041.md): Battery Pack · discharged · Jan 11, 2002 · N294WA · Boeing 727247 · Emergency Lighting > MID FIRST CLASS CEILING EXIT SIGN IDENTIFIER BATTERY PACK INOP. REMOVED AND REPLACED SAME. CHECKS GOOD. - [SDR DL72W011827](https://openairdocs.org/sdr/DL72W011827.md): Accessory Unit · failed · Nov 19, 2001 · N294WA · Boeing 727247 · Landing Gear Position and Warning > AFTER T/O AND GEAR RETRACTION WHEN GEAR HANDLE WAS PLACED TO THE OFF POSITION IT DID NOT CATCH IN THE DETENT. GEAR DISAGREE LIGHT AND DOORS LIGHT ILLUMINATED. GEAR WAS THEN CYCLED WITH A/C SPEED AT 230 KNOTS CAUSING OVERSPEED CONDITION ON GEAR. GEAR WAS RET - [SDR DL72W011720](https://openairdocs.org/sdr/DL72W011720.md): Spar · cracked · Oct 25, 2001 · N294WA · Boeing 727247 · Elevator, Spar/Rib > INSPECTION OF THE LT ELEVATOR REAR SPAR PER BAC S/B 727-55-0089 AND AD 96-06-05 REVEALED A TYPICAL CRACK EMANATING FROM A TAB HINGE SHEAR PLATE. THE CRACK WAS WITHIN LIMITS OF THE S/B AND WAS STOP DRILLED ON A TEMPORARY BASIS UNTIL THE SPAR MOD IS ACCOMPLISH - [SDR DL72W011716](https://openairdocs.org/sdr/DL72W011716.md): Elevator · cracked · Oct 24, 2001 · N294WA · Boeing 727247 · Empennage Structure > 1/4" CRACK AT RIVET UPPER SKIN OF R/H ELEVATOR APPROX. 14" FWD OF TAB CENTER HINGE. REPAIRED PER DRD 55-20-3D,AND RESTENCILED ELEVATOR - [SDR DL72W010880](https://openairdocs.org/sdr/DL72W010880.md): Filter Housing · cracked · May 31, 2001 · N294WA · Boeing 727247 · Hydraulic Filter, Main > LOST A-SYS HYDRAULICS ON LANDING GEAR RETRACTION PRESSURE AND QTY DECREASED TO ZERO. FOUND A-SYS FILTER MODULE CRACKED AT CHECK VALVE REPLACED SAME. - [SDR DL72W010470](https://openairdocs.org/sdr/DL72W010470.md): Power Supply · inoperative · Mar 22, 2001 · N294WA · Boeing 727247 · Emergency Lighting > F/C SEAT ROWS EMER LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK. OPS CKS NML - [SDR DL72W010428](https://openairdocs.org/sdr/DL72W010428.md): Bulkhead · cracked · Mar 14, 2001 · N294WA · Boeing 727247 · Fuselage Main, Bulkhead > THE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH LONG CRACK AT RBL 26 AND WL 169. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 380315-14. - [SDR DL72W010423](https://openairdocs.org/sdr/DL72W010423.md): Angle · cracked · Mar 14, 2001 · N294WA · Boeing 727247 · Leading Edge Devices > COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT NBR 8 SLAT. REPAIR PER MM 57-54-000-8 - [SDR DL72W010278](https://openairdocs.org/sdr/DL72W010278.md): Window · cracked · Feb 16, 2001 · N294WA · Boeing 727247 · Flight Compartment Windows > UPON LANDING, NOTICED R-1 WINDOW CRACKED. REPLACED R-1 WINDOW AND WINDOW HEAT CONTROLLER. - [SDR DL72W002168](https://openairdocs.org/sdr/DL72W002168.md): Battery · discharged · Nov 5, 2000 · N294WA · Boeing 727247 · Emergency Lighting > COCKPIT OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES. - [SDR DL72W001904](https://openairdocs.org/sdr/DL72W001904.md): B-Nut · loose · Sep 29, 2000 · N294WA · Boeing 727247 · Hydraulic System, Main > A-SYS HYD FAILURE. QTY WENT TO -0-, BOTH LOW PRESS LIGHTS ILLUM ON SHORT FINAL. FOUND B-NUT AT LOWER NR 1 PYLON LOOSE. TIGHTENED SAME. INSPECTED CASE DRAIN FILTERS AND SERVICED. - [SDR DL72W001898](https://openairdocs.org/sdr/DL72W001898.md): Oxygen Mask · damaged · Sep 29, 2000 · N294WA · Boeing 727247 · Crew Oxygen System > O2 MASK HEAD PIECE MISSING RUBBER STRIP. REPLACED MASK, OPS CHECK OK. - [SDR DL72W010246](https://openairdocs.org/sdr/DL72W010246.md): Angle · cracked · Jul 21, 2000 · N294WA · Boeing 727247 · Trailing Edge Flaps > DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 32.5 INCH FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER 727 M/M 57-52-0 BY INSTALLING A NEW SECTION OF ANGLE AND A DOUBLER PER THE ABOVE M/M. - [SDR DL72W001289](https://openairdocs.org/sdr/DL72W001289.md): Stiffener · cracked · Jul 7, 2000 · N294WA · Boeing 727247 · Fuselage Miscellaneous Structure > A CRACK WAS FOUND IN THE LBL 36.83 VERTICAL STIFFENER ON THE FORWARD SIDE OF THE 1183 BULKHEAD. THE CRACK WAS LOCATED BETWEEN WL 230 AND WL 254. THE DAMAGE WAS REPAIRED PER S/B 727-53-0192 AT MV2. - [SDR DL72W001308](https://openairdocs.org/sdr/DL72W001308.md): Skin · cracked · Jun 29, 2000 · N294WA · Boeing 727247 · Elevator, Plate/Skin > AT MV THE RT ELEVATOR UPPER SURFACE HAS A DENT WITH CRACK JUST O/B OF ELEV STA 136.5 6 IN FWD OF T/E. THE ELEVATOR WAS REPLACED PER NR 852. S/N OFF DL90136RH, S/N ON DL90091RH. - [SDR DL72W001274](https://openairdocs.org/sdr/DL72W001274.md): Attach Fitting · corroded · Jun 29, 2000 · N294WA · Boeing 727247 · Trailing Edge Flaps > AT MV THE NR 3 FLAP TRACK FWD ATTACH LUG WAS FOUND TO BE CORRODED. CORROSION WAS REMOVED PER MM 57-52-0. EDDY CURRENT INSP, NO INDICATIONS. AREA PEENED AND CAD PLATED PER MM 57-52-0. REPAIR COMPLETED PER MM 57-52-0. - [SDR DL72W001241](https://openairdocs.org/sdr/DL72W001241.md): Skin · damaged · Jun 27, 2000 · N294WA · Boeing 727247 · Trailing Edge Flaps > DURING MV2 VISIT THE NR 4 MIDFLAP LEADING EDGE WAS FOUND WORN AT THE IB END. THE LEADING EDGE WAS REPAIRED BY TRIMMING OUT THE WORN AREA AND INSTALLING A DOUBLER AND FILLER PER 727 MM 57-52-0,FIG. 803. THIS REPAIR WAS ACCOMPLISHED IN THE SHOP PER SO B097 - [SDR DL72W000561](https://openairdocs.org/sdr/DL72W000561.md): Transceiver · inoperative · Mar 22, 2000 · N294WA · Boeing 727247 · Flight Environment Data > NR 2 NAV INOP, SPECIFICALLY NR 2 VOR, LOC AND GS INOP. AND OFF FLAG IN VIEW. DME WORKS NORMALLY. NAV TUNED TO MULTIPLE FREQUENCIES AT VARIOUS DISTANCE BUT EQUIP STILL UNRELIABLE. REPLACED XCVR ATTENUATE TO-60 ON VOR -50 ON ILS, OPS CK NORMAL. - [SDR DL72W991877](https://openairdocs.org/sdr/DL72W991877.md): Connector · dirty · Aug 22, 1999 · N294WA · Boeing 727247 · Smoke Detection > LAV SMOKE CAUTION LIGHT ILLUMINATED ON S/O PANEL AND CHIMES IN PAX CABIN. NO FIRE WAS LOCATED AND SYSTEM WAS DEACTIVATED BY PULLING CIRCUIT BREAKER. FOUND LEFT AFT LAV SMOKE DETECTOR WOULD NOT TEST AFTER RESETTING C/B. CLEANED CONNECTIONS AT CANNON PLUG AND - [SDR DL72W991261](https://openairdocs.org/sdr/DL72W991261.md): Skin · cracked · Jun 4, 1999 · N294WA · Boeing 727247 · Leading Edge Devices > A 1.125 INCH VISABLE CRACK ON AFT SKIN OF NR 6 SLAT AT O/B TRAILING EDGE. SPLICED SKIN PER M/M 57-54-0, NR 1. - [SDR DL72W990421](https://openairdocs.org/sdr/DL72W990421.md): Web · damaged · Feb 27, 1999 · N294WA · Boeing 727247 · Wing Spar > WHILE ACCOMPLISHING THE CENTER WING REAR SPAR WEB MOD PER BAC S/B 57A0182, SEVERAL FASTENER HOLE LOCATIONS WERE DAMAGED. THE MODIFICATION DOUBLERS AND FILLERS WERE EXTENDED TO REPAIR THE EXTRA DAMAGE PER ER/A 366706-14AD. - [SDR DL72W982173](https://openairdocs.org/sdr/DL72W982173.md): Support · cracked · Oct 21, 1998 · N294WA · Boeing 727247 · Leading Edge Slat Actuator > NR 1 LE FLAP ACT SUPPORT BOX CRACKED AT UPPER IB CORNER. REPAIRED PER MM 57-21-21. - [SDR DL72W981996](https://openairdocs.org/sdr/DL72W981996.md): Heat Valve · failed · Sep 27, 1998 · N294WA · Boeing 727247 · Fuel Heater > NR 3 ENGINE OIL TEMPERATURE ROSE TO YELLOW BAND RANGE. FOLLOWED POM PROCEDURES FOR HIGH OIL TEMPERATURE. SHUTDOWN NR 3 ENGINE ACCORDING TO CHECKLIST PROCEDURES. REPLACED NR 3 ENGINE FUEL HEAT VALVE. LEAK AND FUNCTION CHECKS OK. INSPECTED ENGINE FOR OIL TE - [SDR DL72W981308](https://openairdocs.org/sdr/DL72W981308.md): Light · inoperative · Jun 20, 1998 · N294WA · Boeing 727247 · Emergency Lighting > AFT LT O/W EMERG LIGHT INOP. REPLACED M955 RACK, OPS CKS GOOD. - [SDR DL72W980583](https://openairdocs.org/sdr/DL72W980583.md): Skin · corroded · Mar 13, 1998 · N294WA · Boeing 727247 · Fuselage Main, Plate/Skin > THE SKIN WAS FOUND CORRODED AT STRINGER 28R BETWEEN FS 1050 AND 1070. THE DAMAGE WAS CUTOUT OVER A 3 X 16 AREA. THE SKIN WAS REPAIRED WITH A DOUBLER PER THE GUIDLINES OF B727 SRM 53-30-3 AND DOCUMENTED PER ER/A 364236-14. - [SDR DL72W980610](https://openairdocs.org/sdr/DL72W980610.md): Bracket · cracked · Mar 9, 1998 · N294WA · Boeing 727247 · Leading Edge Slat Actuator > FOUND.125 INCH VISIBLE CRACK AT NR 5 L/E FLAP ACTUATOR MOUNT BOX I/B LOWER CORNER MARKED. REPAIRED PER MM 57020-21 P 811. - [SDR DL72W971657](https://openairdocs.org/sdr/DL72W971657.md): Web · cracked · Aug 25, 1997 · N294WA · Boeing 727247 · Fuselage Miscellaneous Structure > FOUND DURING B-2 LETTER CHECK, VERT WEB ABOVE S-DUCT AT STA 1303 HAS 2 CRACKS AT LT SIDE. ONE CRACK AT LWR CORNER AND ONE APPROX 6.5 INCHES ABOVE LWR CORNER. REPAIRED PER M/M 53-11-0. - [SDR DL72W971495](https://openairdocs.org/sdr/DL72W971495.md): Battery Pack · discharged · Jul 29, 1997 · N294WA · Boeing 727247 · Emergency Lighting > AFT CROSS AISLE EMERGENCY EXIT LIGHTS FLASH WHEN TESTED. REPLACED BATTERY PACK, LIGHTS CK OK. - [SDR DL72W961452](https://openairdocs.org/sdr/DL72W961452.md): Channel · cracked · Jun 15, 1996 · N294WA · Boeing 727247 · Fuselage Miscellaneous Structure > DURING INSPECTION, FOUND CHANNEL AT FS 1263 TORQUE BOX CRACKED. CRACK LENGTH WAS APPROXIMATELY 1.5 INCH. REPLACED CHANNEL PER AD 94-07-08 AND B727 S/B 53-0129, R 4. - [SDR DL72W961435](https://openairdocs.org/sdr/DL72W961435.md): Angle · cracked · Jun 14, 1996 · N294WA · Boeing 727247 · Leading Edge Devices > NR 6 SLAT LOWER COVE SKIN ANGLE CRACKED 1.5 INCH INBD OF ACTUATOR. REPAIRED PER M/M 57-54-0. - [SDR DL72W954398](https://openairdocs.org/sdr/DL72W954398.md): Actuator Bracket · cracked · Nov 15, 1995 · N294WA · Boeing 727247 · Leading Edge Slat Control System > FOUND ON A-1 LETTER CK, NR 2 LE FLAP O/B ACTUATOR BRACKET CRACKED. REPAIRED PER MM 57-20-21. - [SDR DL72W954395](https://openairdocs.org/sdr/DL72W954395.md): Web · cracked · Nov 15, 1995 · N294WA · Boeing 727247 · Fuselage Miscellaneous Structure > FOUND DURING A-1 LETTER CHECK,.125 INCH CRACK IN LWR TORQUE BOX VERT WEB LIGHTENING HOLE FS 1223 LEFT SIDE. REPAIRED PER M/M 53-11-0 PAR 15. - [SDR DL72W953580](https://openairdocs.org/sdr/DL72W953580.md): Doubler · cracked · Sep 1, 1995 · N294WA · Boeing 727247 · Leading Edge Devices > PREVIOUS DOUBLER REPAIR CRACKED BENEATH NR 7 L/E SLAT I/B DOWN STOP PAD. CRACK WAS FOUND AT F-1 LTR CHECK. REPLACED DOUBLER PER MM 57-54-0. - [SDR DL72W953406](https://openairdocs.org/sdr/DL72W953406.md): Element · shorted · Aug 16, 1995 · N294WA · Boeing 727247 · Overheat Detection > ON TAKEOFF OUT OF ORF, HAD THE LOWER/AFT BODY OVERHEAT ILLUM. FOLLOWED PROCEDURES, LIGHT STAYED ILLUM. ISOLATED THE NR 1, NR 2, NR 3 ENG PNEUMATICS, LIGHT REMAINED ILLUM. OFF-LANDED IN CAE. FOUND RT OVERHEAT DET M365 SEC 48 SHORTED. REPLACED SAME, RAN ENG - [SDR DL72W951953](https://openairdocs.org/sdr/DL72W951953.md): Skin · corroded · Apr 24, 1995 · N294WA · Boeing 727247 · Fuselage Main, Plate/Skin > CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT ALONG THE AFT EDGE. REPAIRS WERE ACCOMPLISHED PER ERA 301584-14. - [SDR DL72W951586](https://openairdocs.org/sdr/DL72W951586.md): Seat Track · corroded · Apr 17, 1995 · N294WA · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings > AT HMV, RT INBD SEAT TRACK CORRODED STA 1030 TO 1136, RT OUTBD TRACK CORRODED AT FS 1090 TO 1136 AND RT GALLEY TRACK CORRODED FS 1070 TO 1136. REPLACED SECTIONS OF TRACK PER SRM 53-10-5. - [SDR DL72W951650](https://openairdocs.org/sdr/DL72W951650.md): Frame · cracked · Apr 16, 1995 · N294WA · Boeing 727247 · Service Doors > THE L2 DOOR FRAME (ON DOOR) IS CRACKED AT UPPER HINGE, LWR O/B CORNER. REPAIRED PER SRM 52-40-2 PG13-15. - [SDR DL72W951568](https://openairdocs.org/sdr/DL72W951568.md): Skin · damaged · Apr 16, 1995 · N294WA · Boeing 727247 · Elevator, Plate/Skin > DURING SHOP INSP, AN ELONGATED HOLE WAS DISCOVERED IN THE 4TH ACCESS PANEL FROM O/B. REPAIRED PER SRM 55-10-3. DURING SHOP INSP, AN UNIDENTIFIED REPAIR WAS DISCOVERED ON THE LWR SKIN 12 INCHES FROM I/B END. REPAIRED PER SRM 55-20-3 FOR RIGHT ELEVATOR ASSEMB - [SDR DL72W951567](https://openairdocs.org/sdr/DL72W951567.md): Skin · dented · Apr 16, 1995 · N294WA · Boeing 727247 · Elevator, Plate/Skin > FOUND DURING SHOP INSP, RT ELEV UPPER I/B SURFACE DENTED. REPAIRED SKIN PER SRM 55-20-3. - [SDR DL72W951544](https://openairdocs.org/sdr/DL72W951544.md): Seat Track · corroded · Apr 13, 1995 · N294WA · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings > DURING HMV, FOUND LT INBD SEAT TRACK CORRODED STA 350. REPAIRED PER SRM 53-10-5. - [SDR DL72W951543](https://openairdocs.org/sdr/DL72W951543.md): Seat Track · corroded · Apr 13, 1995 · N294WA · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings > DURING HMV, FOUND RT INBD SEAT TRACK CORRODED STA 344-380. REPLACED PER SRM 53-10-5 FIG 8. - [SDR DL72W951617](https://openairdocs.org/sdr/DL72W951617.md): Panel · disbonded · Apr 12, 1995 · N294WA · Boeing 727247 · Spoilers > DURING HMV, FOUND SPOILER PANEL DISBONDING. NR 12 SPOILER PANEL REPAIRED PER SRM 57-50-6. - [SDR DL72W951616](https://openairdocs.org/sdr/DL72W951616.md): Panel · disbonded · Apr 12, 1995 · N294WA · Boeing 727247 · Spoilers > DURING HMV, FOUND SPOILER PANEL DISBONDING. NR 11 SPOILER PANEL REPAIRED PER SRM 57-50-6. - [SDR DL72W951518](https://openairdocs.org/sdr/DL72W951518.md): Frame · cracked · Apr 12, 1995 · N294WA · Boeing 727247 · Fuselage Main, Frame > AT HMV, FOUND FUSELAGE FRAME FS 1030 ABOVE STRINGER 25L CRACKED. CUT OUT DAMAGE SECTION AND REPAIRED PER DL ERA 301494-14. - [SDR DL72W951512](https://openairdocs.org/sdr/DL72W951512.md): Stringer · cracked · Apr 12, 1995 · N294WA · Boeing 727247 · Fuselage Main, Longeron/Stringer > AT HMV, STRINGER 15R FOUND CRACKED AT AFT SIDE OF RT WING LEADING EDGE ICE LIGHT HOUSING AT FS 720C. REPAIRED PER SRM 53-10-3. - [SDR DL72W951555](https://openairdocs.org/sdr/DL72W951555.md): Skin · cracked · Apr 11, 1995 · N294WA · Boeing 727247 · Leading Edge Devices > SKIN CRACKED, NR 4 SLAT HAS 6 CRACKS AT FENCE ATTACH POINTS. REPAIRED PER MM 57-54-0 PG 817. FOUND AT HMV. - [SDR DL72W951531](https://openairdocs.org/sdr/DL72W951531.md): Skin · cracked · Apr 11, 1995 · N294WA · Boeing 727247 · Leading Edge Devices > AT HMV, FOUND RT WING NR 5 L/E SLAT WITH CRACKS IN THE SKIN AT WING FENCE ATTACH HOLE. REPAIRED PER MM 57-54-0 PG 817. - [SDR DL72W951513](https://openairdocs.org/sdr/DL72W951513.md): Stringer · cracked · Apr 11, 1995 · N294WA · Boeing 727247 · Fuselage Main, Longeron/Stringer > AT HMV, STRINGER 15R FOUND CRACKED AT FWD SIDE OF RT WING L/E ICE LIGHT HOUSING AT FS 720C. REPAIRED PER SRM 53-10-3. - [SDR DL72W951462](https://openairdocs.org/sdr/DL72W951462.md): Rib · cracked · Apr 11, 1995 · N294WA · Boeing 727247 · Leading Edge Devices > RIB CRACKED NR 2 L/E SLAT NR 3 RIB CRACKED (MARKED). STOP DRILLED CRACK AS PER SRM 57-50-3. FABRICATED DOUBLER AS PER SRM 57-50-3 FIG 9 SHEET 1 AND 2. Next page: https://openairdocs.org/deregistered/N294WA-2013-07-18/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 n_number = 'N294WA' AND deregistration_id = 'N294WA-2013-07-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N294WA-2013-07-18/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.