Boeing 737-33A

Service difficulty reports · 1,809

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = '73733A'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AWXA200600260Frame · crackedMCN - DURING C19 CHECK DISCOVERED 188 FRAME CRACKED, 2.1 INCHES, IN RADIUS AT WL 208 AND BL 31L. MAINTENANCE CUT OUT AND REMOVED DAMAGED PORTION OF CHORD WEB AT BS 188 FRAME IAW BOEING 737-300 SRM 53-00-07-2R11. PERFORMED HFEC INSPECTION, NO CRACKS NOTED. FJan 17, 2006 · N166AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200600398Fuse · blownMCN - EEL - DURING C19 CHECK DISCOVERED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP. MAINTENANCE FOUND TWO BLOWN FUSES IN THE AFT AND FORWARD POWER PACKS. REMOVED AND REPLACED FUSES AS REQUIRED. OPERATIONAL CHECKS WERE GOOD IAW AMERICA WEST AIRLINES TASK Jan 15, 2006 · N166AW · Boeing 73733A · Light System WiringSDR AWXA200600399Skin · delaminatedMCN - DURING C19 CHECK DISCOVERED THE LT OUTBOARD AFT FLAP; INBOARD AFT CORNER HAD SIGNS OF DELAMINATION. MAINTENANCE CUT OUT AND REMOVED THE DAMAGED AREA FROM THE LT OUTBOARD AFT FLAP INBOARD AFT CORNER IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLEJan 13, 2006 · N166AW · Boeing 73733A · Trailing Edge FlapsSDR AWXA200600138Intercostal · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED INTERCOSTAL CRACKED, .5 INCHES, AT AFT PRESSURE BULKHEAD BS 1019, WL 208 AND BL 37R. MAINTENANCE DRILLED OUT DAMAGED AREA IAW BOEING 737-300 SRM 51-70-11-0G ITEM 1 FIG 1. FABRICATED ANGLE AND FILLER IAW BOEINGJan 11, 2006 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600008Terminal Block · looseLAS - AIR TURN BACK - FLT 421 - AFTER CLIMB-OUT, CREW REPORTED THAT THE NR 2 ENG OVERHEATED WITH AN EGT INDICATION OF 1130 DEG C FOR 2 TO 3 SECONDS WITH ASSOCIATED RED LIGHT. CREW REDUCED POWER AND EGT RETURNED WITHIN LIMITS. CREW RETURNED TO LAS AND LANDED Jan 2, 2006 · N174AW · Boeing 73733A · Engine Indicating System WiringSDR AWXA200600113Frame · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON FRAME ATTACH FLANGE AT BS 827, WL 148, AND FROM BL 3L TO BL 6L. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-07-1A1 FIG 101. MAINTENANCE CUT OUT DAMAGED AREA OF FRAME ATTACH FLANGE IAW BDec 29, 2005 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200600143Beam · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON BS 1006 BEAM AT SCREW LOCATED AT BL 10L. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE FABRICATED REPAIR STRAP AND INSTALLED AT BS 1006 BEAM AT BL 1Dec 27, 2005 · N168AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200501610Windshield · crackedDURING CRUISE, DEPARTED FROM DFW EN ROUTE TO LAS, AT FL 340 CREW REPORTED CAPT OUTER WINDSHIELD CRACKED. CREW DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX R & R CAPT WINDSHIELD. OPS CHECKS GOOD. HIGH TIME WINDOW. WINDOW WAS SCRAPPED AT VENDOR.Dec 27, 2005 · N174AW · Boeing 73733A · Flight Compartment WindowsSDR AWXA200600144Frame · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED AFT GALLEY DOORWAY FRAME CRACKED, .5 INCHES AT BS 957, WL 257 AND BL 58R. MAINTENANCE REMOVED AND INSTALLED NEW REPLACEMENT DOORWAY FRAME AT BS 957, WL 257 AND BL 58R IAW BOEING 737-300 SRM 52-13-31-404-010-800Dec 26, 2005 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200600112Door Frame · crackedMCN - DURING C19 CHECK DISCOVERED THE L2 DOORWAY STOP FITTING, LOWER FASTENER HOLE CRACKED .125 INCHES. MAINTENANCE REMOVED THE L2 DOOR FORWARD FRAME IAW BOEING 737-300 SRM 51-40-02-0G FIG 8. INSTALLED NEW L2 DOOR FORWARD FRAME IAW BOEING 737-300 SRM 51-40-0Dec 26, 2005 · N168AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200600111Bulkhead · crackedMCN - DURING C19 CHECK DISCOVERED VERTICAL WEB CRACKED, .25 INCHES, AT BS 178, WL 176 AND FROM BL 5L TO BL 7L. MAINTENANCE CUT OUT CRACKED SECTION OF WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. FABRICATED REPLACEMENT WEB IAW BOEING 737-300 SRM 53-10-08Dec 26, 2005 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA200600110Vertical Beam · crackedMCN - DURING C19 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .5 INCHES, AT BS 178, WL 183 AND BL 5.7R. MAINTENANCE CUT OUT CRACKED SECTION OF WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. FABRICATED REPLACEMENT WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIDec 26, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600160Bulkhead · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON THE AFT PRESSURE BULKHEAD, LOWER FORWARD FACE SKIN, RT OUTBOARD SIDE OF THE CENTER CHANNEL AT BS 1016, WL 201 AND BL 2R. MAINTENANCE CUT OUT DAMAGED SECTION OF BULKHEAD IAW BOEING DWG 65C28106. RECEIVED AND INSTDec 24, 2005 · N168AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA200600136Channel · corrodedMCN - MAJOR REPAIR - CORROSION FOUND DURING C19 CHECK ON THE RT OUTBOARD SIDE ON THE AFT PRESSURE BULKHEAD FORWARD FACE CENTER CHANNEL ON THE BOTTOM END FROM BS 1016 TO BS 1019, WL 193 TO WL 195 AND FROM BL 2L TO BL 4R. MAINTENANCE REMOVED DAMAGED SECTION OF Dec 24, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600121Floorbeam · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON BS 1016 FLOORBEAM FROM BL 17R TO BL 17L, WL 208. MAINTENANCE REMOVED DAMAGED AREA AND FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. FABRICATED REPAIR STRAPS IAW BOEING 737-300 Dec 24, 2005 · N168AW · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA200600120Floor Support · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON BOTTOM SURFACE OF FLOOR ANGLE AT BS 994 TO BS 1004, BL 42R AND WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. MAINTENANCE REMOVED AND FABRICATED ANGLE IAW BOEING 737Dec 24, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600119Angle · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON THE R2 INNER CHORD LOWER ANGLE FROM BS 975 TO BS 985, BL 47R AND WL 207.5. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED AND FABRICATED REPLACEMENT ANGLDec 24, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600107Structure · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON THE R2 INNER CHORD FROM BS 947 TO BS 973, WL 208 AND BL 47R. EVIDENCE OF PREVIOUS BLEND OUT PRESENT. REMOVED CORROSION AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINDec 24, 2005 · N168AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200600038Vertical Beam · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .375 INCHES, AT BS 178, WL 229 AND BL 17.1R. MAINTENANCE REMOVED WEB AT BS 178 IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED REPLACEMENT WEB IAW BOEING DRAWING 65-17582. INSTALLED Dec 24, 2005 · N168AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200600198Retainer · corrodedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON 1016 BULKHEAD LOWER GASKET RETRAINING STRIP FROM BL 2L TO BL 4R. MAINTENANCE REMOVED CORROSION ON THE -10 STRIP IAW BOEING 737-300 SRM 51-10-02-0G AND WAS WITHIN LIMITS. REMOVED CORROSION ON THE -Dec 23, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600165Skin · damagedDURING C19 CHECK DISCOVERED SKIN CRACK AT FASTENER HOLE AT BS 570 AND STR 4R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN IAW BOEING 737-300 SRM 53-00-01-2R30. FABRICATED FILLERS, DOUBLERS AND TRIPLER IAW BOEING 737-300 SRM 53-00-01-2R30. INSTALLED FABRICATED Dec 23, 2005 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200600166Panel · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN CRACK AT FASTENER HOLE AT BS 591 AND STR 4L. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN IAW BOEING 737-300 SRM 53-00-01-2R30. FABRICATED FILLERS AND DOUBLERS IAW BOEING 737-300 SRM 53-00-01-2R31. INSTALLEDDec 23, 2005 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200600164Panel · crackedMCN - DURING C19 CHECK DISCOVERED SKIN CRACK AT FASTENER HOLE AT BS 628 AND STR 4R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN IAW BOEING 737-300 SRM 53-00-01-2R30. FABRICATED FILLERS AND DOUBLERS IAW BOEING 737-300 SRM 53-00-01-2R30. INSTALLED FABRICATED REPDec 23, 2005 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200600158Skin · crackedMCN - DURING C19 CHECK DISCOVERED SKIN CRACKED AT FASTENER HOLE AT STR 4L, BS 690 ON THE LOWER ROW OF FASTENERS. MAINTENANCE REPAIRED CRACKED SKIN AT FASTENER HOLE, BS 690, S4L IAW BOEING 737-300 SRM 53-00-01-2R31.Dec 23, 2005 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200600142Strap · corrodedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON FLOORBEAM STRAP AT BS 1024 TO BS 1029 AND BL 3R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1. REMOVED AND INSTALLED FABRICATED REPLACEMENT FLOORBEAM STRAP FROM BS 1Dec 23, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600141Floor Support · corrodedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON FLOOR SUPPORT FROM BS 1006 TO BS 1016, BL 5L TO BL 10L AND WL 208. MAINTENANCE FOUND THE CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1A1 FIG 101. REMOVED FLOOR SUPPORT AND INSTALDec 23, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600140Frame · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED BS 188 FRAME CRACKED, .25 INCHES, AT WL 207 AND BL 30L. MAINTENANCE CUT OUT AND REMOVED DAMAGED PORTION OF FLANGE AND CHORD FLANGE FROM BS 188 FRAME IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. FABRICATED REPDec 23, 2005 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200600118Attach Angle · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON SHEAR WEB ATTACH ANGLE AT BS 1028, WL 207 AND BL 17R. NO ALLOWABLE LIMITS IAW BOEING 737-300 SRM 53-60-51-1A FIG 101. MAINTENANCE REMOVED AND FABRICATED ATTACH ANGLE IAW BOEING 737-300 SRM 51-40-05-0G AND BOEINDec 23, 2005 · N168AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200600162Pan · corrodedMCN - DURING C19 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON THE RT AFT LAV FLOOR PAN AT BS 1006 TO BS 1016, WL 208 AND FROM BL 9R TO BL 36R. MAINTENANCE REMOVED AND INSTALLED NEW LAV FLOOR PAN IN THE RT AFT LAV FROM BS 1006 TO BS 1016, WL 208 AND FROM BL 9Dec 22, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600161Pan · corrodedMCN - DURING C19 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON THE LT AFT LAV FLOOR PAN AT BS 1006 TO BS 1016, WL 208 AND FROM BL 9L TO BL 36L. MAINTENANCE REMOVED AND INSTALLED NEW LAV FLOOR PAN IN THE LT AFT LAV FROM BS 1006 TO BS 1016, WL 208 AND FROM BL 9Dec 22, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600155Cargo Track · corrodedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED CORROSION ON TIE DOWN TRACK LOCATED IN THE AFT PIT AT BS 787, BL 17.2L AND WL 160. MAINTENANCE BLENDED OUT THE CORROSION AND FABRICATED REPAIR STRAP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5365-06017Dec 22, 2005 · N168AW · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200600122Floor Support · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON BS 1000 TO BS 1016 FLOOR SUPPORT FROM BL 5L TO BL 10R, WL 208. MAINTENANCE REMOVED DAMAGED AREA AND FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. REMOVED AND INSTALLED NEW FLOODec 22, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600116Clip · crackedMCN - DURING C19 CHECK DISCOVERED CLIP CRACKED, .25 INCHES, AT BS 787 AND BL 19R. MAINTENANCE REMOVED CRACKED CLIP AND FORMED REPLACEMENT CLIP IAW BOEING 737-300 SRM 51-40-02-0G AND B737 DWG 69-43934. INSTALLED REPAIR PARTS AT BS 787 AND BL 19R IAW BOEING 73Dec 22, 2005 · N168AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200600115Frame · crackedMCN - DURING C19 CHECK DISCOVERED BS 188 FRAME CRACKED IN RADIUS AT WL 207 AND BL 30R. MAINTENANCE REMOVED DAMAGED AREA ON BS 188 FRAME IAW BOEING 737-300 SRM 53-00-07-2R11 FIG 201. FABRICATED REPAIR ANGLE AND FILLERS IAW BOEING 737-300 SRM 53-00-07-2R11. IDec 22, 2005 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200600114Frame · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON FUSELAGE FRAME ATTACH ANGLE AT AFT PIT BS 827, BL 13.80R AND WL 148. CORROSION WAS OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-07-1A1 FIG 101. MAINTENANCE REMOVED ANGLE AND FABRICATED REPLACEMENT ANGLE IAW BOEINGDec 22, 2005 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200600109Web · crackedMCN - DURING C19 CHECK DISCOVERED WEB CRACKED, .5 INCHES, AT BS 197, WL 207 AND BL 30L. MAINTENANCE REMOVED FLOOR WEB AT BS 197, WL 207 AND BL 30L IAW BOEING 737-300 SRM 53-10-51-2R8 FIG 201. FABRICATED NEW WEB AND INSTALLED AT BS 197, WL 207 AND BL 30L IAW Dec 22, 2005 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200600169Skin · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED 4 CRACKS, RANGING FROM .250 INCHES UP TO .500 INCHES IN LENGTH, ON THE BOTTOM NR 2 SLAT SKIN, BELOW THE OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED THE DAMAGE FROM THE NR 2 SLAT SKIN IAW BOEING 737-300 SRM 57Dec 21, 2005 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AWXA200600156Skin · crackedMCN - DURING C19 CHECK DISCOVERED 6 CRACK ON THE BOTTOM OF THE NR 1 SLAT SKIN, BELOW OUTBOARD AUX TRACK. MAINTENANCE REMOVED THE DAMAGED AREA ON THE BOTTOM OF THE NR 1 SLAT SKIN IAW BOEING 737-300 SRM 57-13-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEIDec 21, 2005 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AWXA200600137Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .5 INCHES, AT BS 616 AND STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS 616 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 3, 8 AND 51-40-02-0G FIG 8 AND 12.Dec 21, 2005 · N168AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200600117Stringer Clip · crackedMCN - DURING C19 CHECK DISCOVERED STRINGER TO STRINGER CLIP CRACKED, .25 INCHES, AT BS 639 AND STRINGER 4L. MAINTENANCE REMOVED CRACKED CLIP AND FORMED REPLACEMENT CLIP IAW BOEING 737-300 SRM 51-40-02-0G. INSTALLED NEW REPLACEMENT CLIP AT BS 639 AND STRINGERDec 21, 2005 · N168AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200600040Wedge · debondedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE TOP OF THE NO. 6 SLAT WEDGE ABOVE THE INBOARD AUX TRACK AT WS 344R TO WS 348.5R. MAINTENANCE REMOVED DAMAGED AREA ON THE NO. 6 SLAT WEDGE IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILDec 21, 2005 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AWXA200600039Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED STRINGER CLIP CRACKED, .5 INCHES, AT BS 685 AND STR 4R. MAINTENANCE REMOVED AND ISNTALLED NEW CLIP AT BS 685 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND FIG 12.Dec 21, 2005 · N168AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200600037Clip · crackedMCN - MAJOR REPAIR - DURING C19 DISCOVERED FLOOR WEB ATTACH CLIP CRACKED, .25 INCHES, AT BS 178, WL 208, FROM BL 25L TO BL 29L. MAINTENANCE REMOVED AND INSTALLED NEW FLOOR WEB ATTACH CLIP AT BS 178, WL 208 AND BL 25L TO BL 29L IAW BOEING 737-300 SRM 51-40-02-Dec 21, 2005 · N168AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200600241Skin · crackedMCN - DURING C19 CHECK DISCOVERED FUSELAGE SKIN CRACK JUST BELOW STRINGER 12R AND BS 500D+18". MAINTENANCE REMOVED DAMAGED AREA IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5331-06013-ES2. FABRICATED DOUBLER, TRIPLER AND FILLER IAW AWA ER NODec 19, 2005 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200600139Skin · chafedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED LOWER SKIN CHAFED AT O/B END OF THE RT O/B FORE FLAP, RT WING. MAINTENANCE REPAIRED LOWER SKIN AREA BY REMOVING CHAFED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT DOUBDec 19, 2005 · N168AW · Boeing 73733A · Trailing Edge FlapsSDR AWXA200501564Trim System · malfunctionedPHX - ABORTED TAKEOFF - FLT 227 - CREW REPORTED THAT THE TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. ABORTED TAKEOFF AT APPROXIMATELY 45 KNOTS. CAPTAINS TRIM SHOWED 4.8 WHILE THE F/O'S SHOWED 5.2. CREW RESET STAB TRIM AND RECEIVED NO FURTHER WARNINGS.Dec 19, 2005 · N173AW · Boeing 73733A · Stabilizer Position IndicatingSDR AWXA200501484Generator · inoperativePILOTS REPORTED LOSS OF NR 1 ENG A/C GEN SYS FELL OFFLINE AT FL 350 & WOULD NOT RESET. VOLTS & FREQUENCY READING ZERO. NO CSD LOW OIL PRESSURE LIGHT PRESENT. RESIDUAL VOLTS AT 115. ATTEMPT TO START APU UNSUCCESFUL DIVERTED SLC FOR REPAIRS. MX PLACED NR 1 ENGINDec 5, 2005 · N168AW · Boeing 73733A · Alternator-Generator DriveSDR AWXA200501506Frame · crackedMCN - DURING C19 CHECK DISCOVERED MAIN CABIN FRAME CRACKED, .7 INCHES, ON THE LOWER LEG AT BS 616, BL 60L AND WL 200. MAINTENANCE CUT OUT DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-01143-DD1. FABRICATED FILLER AND REPAIR ANGLE IAW Dec 2, 2005 · N164AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200501535Channel · crackedMCN - DURING C19 CHECK DISCOVERED VERTICAL WEB CHANNEL CRACKED, 1.0 INCH, AT BS 663.75, BL 25R AND WL 206. MAINTENANCE NOTCHED OUT REMAINING MATERIAL ON VERTICAL WEB CHANNEL IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5702-05346-HF1. FABRICATED CHANNDec 1, 2005 · N164AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200501505Frame · crackedMCN - DURING C19 CHECK DISCOVERED MAIN CABIN FRAME CRACKED, 1.1 INCHES, AT THE LOWER LEG THROUGH FASTENER AT BS 616, BL 60R AND WL 200. MAINTENANCE CUT OUT DAMAGED AREA IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5311-01143-DD1. FABRICATED FILLER AND Dec 1, 2005 · N164AW · Boeing 73733A · Fuselage Main, Frame
Back to Boeing 737-33A