Boeing 737-301

Service difficulty reports · 4,797

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 = '737301'
  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 USAASB03220Switch · failedPHL - FLT 579 - AFTER TAKEOFF FROM PHL, EN ROUTE TO IND, RT PACK WOULD NOT PRESSURIZE THE AIRCRAFT. LT PACK WAS ALREADY ON MEL 21-1A. CAPTAIN ELECTED TO RETURN TO FIELD AT PHL. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINTENANCE OPERATIONALLY CHECDec 23, 2003 · N353US · Boeing 737301 · Cabin Cooling SystemSDR USAASB03219Connector · inoperativeMAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS, AT ROWS 12 THROUGH 16, INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR AT SEAT ROW 12 LOOSE. RESEATED CONNECTOR. OPS CHECK GOOD. (M)Dec 22, 2003 · N353US · Boeing 737301 · Emergency LightingSDR USAA030323Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, BS 727 D PLUS 13 INCHES S-24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Dec 19, 2003 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA030319Skin Panel · crackedPIT - FOUND SKIN PANEL CRACKED 2 INCHES, STATION 720 KEEL BEAM. INSTALLED DOUBLER PER EA 77147 AND SRM 53-10. (M)Dec 19, 2003 · N335US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200301638Inlet · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK NR 1 ENGINE NOSE COWL WAS FOUND DELAMINATED AT 12:00 POSITION. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-08, FIG 7 & 9, PG 28-29, 47-49.Dec 19, 2003 · N325AW · Boeing 737301 · Engine Cowling SystemSDR AWXA200301602Clip · crackedMCN - MAJOR REPAIR - DURING -18 CHECK A 1 INCH CRACK WAS FOUND ON L-1 DOOR LOWER HINGE SPRING COVER ATTACH CLIP. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR LOWER HINGE SPRING COVER ATTACH CLIP IAW SOPM 20-50-01 PG 1-9.Dec 16, 2003 · N325AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200301613Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON FLOOR SUPPORT CHANNEL AT BS 540, RBL 0 TO RBL 25. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT CHANNEL AT BS 540, RBL 0 TO RBL 25; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-52894; INSTADec 15, 2003 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200301612Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON FLOOR SUPPORT CHANNEL AT BS 540, LBL 0 TO LBL 25. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT CHANNEL AT BS 540, LBL 0 TO LBL 25; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-52894; INSTADec 15, 2003 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200301631Skin · corrodedDURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AT STR 26 LT, BS 727A & BS 727B. MAINTENANCE CUT OUT DAMAGED SKIN AT STR 26 LT, BS 727A & BS 727B; FABRICATED A REPAIR PLATE AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-0Dec 14, 2003 · N325AW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200301632Stringer · corrodedDURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 26 LT BETWEEN BS 727A & BS 727B. MAINTENANCE CUT OUT DAMAGED STRINGER 26 LT BETWEEN BS 727A & BS 727B; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER PER DWG 65-52928 AND A STRINGER SPLICE CHANNEDec 12, 2003 · N325AW · Boeing 737301 · Fuselage Main, Longeron/StringerSDR SWAA032720Fitting · crackedDURING SCHEDULED C4 CHECK, FOUND LT MLG ACTUATOR BEAM HANGER FWD MOUNT FITTING CRACKED. REMOVED AND REPLACED HANGER MOUNT FITTING PER MM.Dec 12, 2003 · N660SW · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR AWXA200301623Frame · chafedMCN - MAJOR REPAIR - DURING C-18 CHECK A HOLE WAS FOUND CHAFED THROUGH FRAME AT BS 500A BETWEEN STR 1 LT AND STR 1 RT. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 500A BETWEEN STR 1 LT AND STR 1 RT; FABRICATED 2 EACH REPAIR CHANNELS AND A FILLER; INSTADec 10, 2003 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA200301621Slat · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE NR 3 SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER TRAILING EDGE. MAINTENANCE REMOVED DELAMINATION ON INBOARD UPPER TRAILING EDGE OF NR 3 SLAT; FABRICATED REPAIR DOUBLERS; BONDED DOUBLERS ON SLAT IAW B737-300 SRM 5Dec 9, 2003 · N325AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200301601Skin · delaminatedMCN - MAJOR REPAIR - DURING -18 CHECK THE NR 2 SLAT INBOARD UPPER TRAILING EDGE WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED EXISTING REPAIR AND DELAMINATED SKIN ON NR 2 SLAT INBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; INSTALDec 9, 2003 · N325AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200301630Angle · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON RT AIR CONDITIONING BAY AFT WALL L-ANGLE AT INBOARD END ABOVE TURBO FAN BS 663, RBL 23. MAINTENANCE REMOVED CRACKED L-ANGLE AT BS 663, RBL 23; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-Dec 8, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301616Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND IN 5 PLACE ON UPPER SURFACE OF FLOORBEAM AT BS 328, BETWEEN RBL 18 AND RBL 50. MAINTENANCE CUT OUT AND REMOVED DAMAGED SECTION OF FLOORBEAM AT BS 328, BETWEEN RBL 18 AND RBL 50; FABRICATED A NEW REPLDec 8, 2003 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200301590Frame · crackedDURING C-18 CHECK A.6250 INCH CRACK WAS FOUND ON FRAME AT BS 294.5, STR 7 RT. MAINTENANCE REMOVED DAMAGED AREA OF FRAME AT BS 294.5, STR 7 R/H; FABRICATED 2 EACH REPAIR CHANNELS AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG. 201, PG. 202Dec 8, 2003 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA200301572Intercostal · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND IN TWO PLACES ON UPPER SURFACE OF INTERCOSTAL AT BS 294.5, LBL 12. MAINTENANCE REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS, REMOVED INTERCOSTAL AT BS 294.5, LBL 12; FABRICATED A NEW REPDec 8, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301561Stringer · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER 10 RT AT BS 294. MAINTENANCE REMOVED CRACKED STRINGER 10 RT FROM BS 280 TO BS 294; FABRICATED A NEW REPLACEMENT STRINGER PER DWG 65C34778; INSTALLED REPAIR PART IAW B737-300 SRM 51Dec 8, 2003 · N325AW · Boeing 737301 · Fuselage Main, Longeron/StringerSDR AWXA200301546Strap · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN TIE STRAP BELOW CABIN FLOOR IN E&E COMPARTMENT BS 344, LBL 45. MAINTENANCE STOP DRILLED CRACK IN TIE STRAP BS 344, LBL 45; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53Dec 8, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301545Strap · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN TIE STRAP BELOW CABIN FLOOR IN E&E COMPARTMENT BS 328, LBL 12. MAINTENANCE STOP DRILLED CRACK IN TIE STRAP BS 328, LBL 12; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM Dec 8, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301544Strap · crackedDURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN TIE STRAP BELOW CABIN FLOOR IN E&E COMPARTMENT BS 328, BL -0-. MAINTENANCE STOP DRILLED CRACK IN TIE STRAP BS 328, BL -0-; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51, PG 1, & 219, Dec 8, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301539Reveal · crackedDURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN R-1 DOOR UPPER REVEAL BS 298-328. MAINTENANCE REMOVED R-1 DOOR UPPER REVEAL BS 298-328; FABRICATED A NEW REPLACEMENT UPPER REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 11-12, 38, FIG 8.Dec 8, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301628Strap · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT LAVATORY MAIN DECK STIFFENER STRAP BS 1016 TO BS 1025, LBL 17. MAINTENANCE REMOVED CORRODED STIFFENER STRAP BS 1016 TO BS 1025, LBL 17; FABRICATED A NEW REPLACEMENT STRAP; INSTALDec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301626Pan · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT LAVATORY MAIN DECK DRIP PAN AT BS 1018, LBL 14. MAINTENANCE REMOVED CORRODED LT AFT LAVATORY MAIN DECK DRIP PAN AT BS 1018, LBL 14; FABRICATED A NEW REPLACEMENT DRIP PAN PER DWG 65-Dec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301624Skin · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN AT NR 2 SLAT OUTBOARD AUXILIARY TRACK CUTOUT WS 346 TO WS 349. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16 PG 27, REPAIR 11.Dec 7, 2003 · N325AW · Boeing 737301 · Wing, Plate/SkinSDR AWXA200301622Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM BS 1016, LBL 4 TO LBL 16. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM BS 1016, LBL 4 TO LBL 16; FABRICATED 2 EACH SUPPORT ANGLES & 4 EACH STRAPS; INSTALLED REPAIR PARTS IDec 7, 2003 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200301620Strap · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT LAVATORY MAIN DECK STIFFENER STRAP BS 1016, LBL 6 TO RBL 6. MAINTENANCE REMOVED CORRODED STIFFENER STRAP BS 1016, LBL 6 TO RBL 6; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED Dec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301619Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 961, RBL 25. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 961, RBL 25; FABRICATED A T-ANGLE AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12, PG 1 & 45.Dec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301618Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT BS 951-964, LBL 45. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 951 TO BS 964, LBL 45; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT AND FILLERS; INSTALDec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301615Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1011-1016, RBL 6. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 1011 TO BS 1016, RBL 6; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPADec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301614Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 1011-1016, LBL 6. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 1011 TO BS 1016, LBL 6; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DDec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301606Plate · corrodedMCN - MINOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND UPPER SURFACE OF SUPPORT FILLER PLATE AT BS 951, RBL 47. MAINTENANCE REMOVED CORRODED FILLER PLATE AT BS 951, RBL 47; FABRICATED A NEW REPLACEMENT FILLER PLATE PER DWG 65C10592; INSTALLED REPAIR PART Dec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301587Crease Beam · corrodedMAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF CREASE BEAM (INNER CHORD) BETWEEN BS 952 AND BS 985, LBL 53 AND LBL 56. MAINTENANCE REMOVED AND REPLACED INNER CHORD FROM BS 952 TO BS 985, LBL 53 TO LBL 56 IAW B737-300 SRM 51-Dec 7, 2003 · N325AW · Boeing 737301 · Fuselage Main, StructureSDR AWXA200301584Skin · debondedMCN - MINOR REPAIR - DURING C-18 CHECK A FOUND UPPER SURFACE OF TAIL CONE DISBONDED 28 INCHES FROM FORWARD EDGE BS 1185 TO BS 1188, WL 289. MAINTENANCE PREPARED TAIL CONE UPPER SURFACE BS 1185 TO BS 1188, WL 289; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-1Dec 7, 2003 · N325AW · Boeing 737301 · Aerodynamic FairingsSDR AWXA200301573Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 967, RBL 18, WL 208. MAINTENANCE REMOVED CORROSION; FABRICATED A STRAP REPAIR; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 203 PG 212-214.Dec 7, 2003 · N325AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200301556Floor Support · corrodedDURING C18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT AT BS 954, RBL 43, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BS 954, RBL 43, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C10592; INSTALLED REPAIR PARTDec 7, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301524Stringer Clip · crackedDURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER CLIP AT BS 360, STR 14 RT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 360, STR 14 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-46882; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1.Dec 7, 2003 · N325AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200301611Intercostal · chafedMCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE L-1 DOOR INTERCOSTAL CHAFED AT LOWER HINGE CUTOUT BS 303.9, STR 13 LT. MAINTENANCE REMOVED INTERCOSTAL AT LOWER HINGE CUTOUT BS 303.9, STR 13 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART Dec 6, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB03211Servo · failedDURING FLIGHT, EN ROUTE, THE STABILIZER OUT OF TRIM LIGHT ILLUMINATED. THE AUTOPILOT WOULD NOT TRIM. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT SERVO MOTOR. OPS CHECK AND BITE TEST NORMAL. (M)Dec 5, 2003 · N355US · Boeing 737301 · Autopilot Main ServoSDR AWXA200301625Intercostal · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT INTERCOSTAL AT RBL 21, BETWEEN BS 927 AND BS 947. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT RBL 21, BS 927 TO BS 947; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-353Dec 5, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301610Channel · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT SPLICE CHANNEL UNDER STR 21 LT, AT BS 907, LBL 45. MAINTENANCE REMOVED CORRODED SPLICE CHANNEL UNDER STR 21 LT, FROM BS 901 TO BS 913, LBL 45; FABRICATED A NEW REPDec 5, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301532Support · crackedDURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON THE AFT CARGO DOOR UP LATCH HOOK CATCH SUPPORT ON CEILING AT BS 847. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO DOOR UP LATCH HOOK CATCH SUPPORT IAW B737-300 SRM 51-40-02, FIG 8 &12, PG 1 & 45.Dec 5, 2003 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200301617Tip Cap · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LT HORIZONTAL STABILIZER TIP LEADING EDGE LBL 252.10. MAINTENANCE BLENDED OUT CRACK ON LT HORIZONTAL STABILIZER TIP LEADING EDGE; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-16, REPAIR 11.Dec 4, 2003 · N325AW · Boeing 737301 · Horizontal Stabilizer, Plate/SkinSDR AWXA200301547Angle · crackedDURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN RADIUS OF AFT MOUNT ANGLE OF L-1 DOOR UPPER LINER ATTACH PAN ASSEMBLY BS 316, STR 6 LT. MAINTENANCE REMOVED CRACKED AFT MOUNT ANGLE BS 316, STR 6 LT; RECEIVED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW BDec 4, 2003 · N325AW · Boeing 737301 · Fuselage Internal Mounting StructureSDR AWXA200301637Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE LT WING OUTBOARD AFT FLAP WAS FOUND DELAMINATED FROM WS 480 TO WS 495. MAINTENANCE REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP IAW T/C R85M27002.Dec 3, 2003 · N325AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200301634Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE RIGHT WING NR 4 SLAT WAS FOUND DELAMINATED AT INBOARD LOWER TRAILING EDGE. MAINTENANCE CUT OUT DELAMINATED SECTION OF SKIN AT INBOARD LOWER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TO SLAT SKIN IDec 3, 2003 · N325AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200301633Skin · delaminatedDURING C-18 CHECK THE LT WING NR 3 SLAT WAS FOUND DELAMINATED AT OUTBOARD UPPER TRAILING EDGE, SLAT STA 329.75. MAINTENANCE REMOVED DELAMINATED SECTION OF SKIN AT OUTBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TO SLAT SKIN IAW B7Dec 3, 2003 · N325AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200301629Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE LT WING NR 2 SLAT WAS FOUND DELAMINATED AT OUTBOARD UPPER TRAILING EDGE, SLAT STA 246.27-254.27. MAINTENANCE CUT OUT DELAMINATED SKIN AT OUTBOARD UPPER TRAILING EDGE; FABRICATED REPAIR DOUBLERS; BONDED REPAIR PART TODec 3, 2003 · N325AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200301574Door Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON AFT SIDE OF R-1 DOOR FRAME, 3RD STOP CUTOUT FROM THE BOTTOM AT INBOARD SIDE, BS 327, STR 12 RT. MAINTENANCE REMOVED DAMAGE AT AFT SIDE OF R-1 DOOR FRAME, 3RD STOP CUTOUT FROM THE BOTTOM BS Dec 3, 2003 · N325AW · Boeing 737301 · Fuselage Main, Structure
Back to Boeing 737-301