Boeing 737-33A

Service difficulty reports · 1,809

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '73733A'
  ORDER BY difficulty_date DESC"

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SDR AWXA0001291Floor Support · damagedFLOOR SUPPORT END FITTING AT BS 328 HAS A HOLE DRILLED IN THE RADIUS. DRILLED HOLE TO .159 THROUGH INTERNAL DOUBLER AND EXTERNAL SKIN; COUNTERSUNK SKIN; INSTALLED RIVET IAW AWA ER 03-5310-01024-SS2.Feb 8, 2001 · N509DC · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001290Skin · dentedHORIZONTAL STABILIZER LEADING EDGE SKIN DENTED STA 258.28. REPAIRED DENT IN LEADING EDGE SKIN OF LEFT HORIZONTAL STABILIZER IAW B737-300 SRM 55-10-01 FIG 203 WITH -1 PLATE, -2 FILLER.Feb 8, 2001 · N509DC · Boeing 73733A · Horizontal Stabilizer, Plate/SkinSDR AWXA0001289Floorbeam · corrodedCORROSION ON UPPER SURFACE OF TRANSVERSE FLOORBEAM AT BS 312 RBL 3 - 9. REMOVED UPPER T-ANGLE OF TRANSVERSE FLOORBEAM; REMOVED LT SPLICE ANGLES; FABED SPLICE PLATES, FABED T-ANGLE; TREATED, PRIMED, AND INSTALLED REPAIR IAW B737-300 SRM 51-20-01, 53-10-51.Feb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA0001288Bulkhead · crackedHFEC AND VISUAL (10X) CONFIRMS CRACK OF UNDETERMINED LENGTH UNDER STRAP AT BS 178 RBL 4 7/8 WL 199.5 TO 201.5. REMOVED STIFFENERS, RADOME ATTACH BRACKETS AND BACKUP STRIPS BS 178 WL 188 TO 218 RBL 10 TO LBL 4; LOCATED, DRILLED AND INSTALLED DOUBLER AND FILLERFeb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001287Bulkhead · crackedULTRASONIC INSPECTION REVEALED CRACK INDICATION BS 178 BULKHEAD WEB AT RBL 1.3 TO UNDETERMINED POINT BENEATH STRAP AT WL 205.7; CONFIRMED HFEC. REMOVED LOWER L-ANGLE BS 178 WL 184 RBL 18 TO LBL 18; CUTOUT DAMAGED AREA WHERE HFEC CONFIRMED CRACK; LOCATED, DRILFeb 8, 2001 · N509DC · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001285Strap · crackedFLOOR TRACK SUPPORT CRACKED AT STA 717B RBL 45.5. FABED, REPAIRED, AND INSTALLED IAW ER 5310-01010-SSI.Feb 8, 2001 · N167AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001284Stringer · corrodedAFT BULKHEAD STA 1016 CTR STRINGER FOUND CORRODED AT BOTTOM. REPAIRED IAW SRM 51-70-11 FIG 1.Feb 8, 2001 · N167AW · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA0001283Stringer · damagedSTR 28L STA 1016 HAS AN ELONGATED BOLT HOLE. REPAIRED IAW SRM 53-00-03 FIG 201 DETAIL V.Feb 8, 2001 · N167AW · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA0001259Frame · crackedSTA 178 BULKHEAD SKIN CRACKED IN 2 PLACES, INTERCOSTALS (2) CRACKED AT SIDE CHORDS, AND SIDE CHORDS CRACKED AT 3 PLACES STA 178 WL 184 TO 207 LBL 45.50 TO RBL 45.50. REPAIRED PER EO 53-12-07.Jan 29, 2001 · N167AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001244Frame · crackedFUSELAGE FRAME ANGLE CRACKED BELOW CABIN FLOOR STA 616 RT, WL 201, RBL 60. REPAIRED AS PER AWA ER 03-5311-01010-JL2.Jan 18, 2001 · N167AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001226Light · inoperativeSEAT EMERGENCY LIGHT AT SEAT 21C INOP. RESECURED LOOSE WIRE; LIGHT OPS CHECKS GOODJan 4, 2001 · N509DC · Boeing 73733A · Emergency LightingSDR AWXA0001172Wire · chafedEMERGENCY LIGHTING INOP ROWS 3-7. REPAIRED WIRING AT SEAT 3CJan 2, 2001 · N174AW · Boeing 73733A · Light System WiringSDR AWXA0001168Wire · brokenEMERGENCY ESCAPE PATH LIGHT AT SEAT 2B FAILED TO ILLUMINATE DURING TEST. FOUND BROKEN WIRE AT SEAT 2B; SPLICED THE WIRE AND LIGHT OPS CHECKED GOODJan 2, 2001 · N169AW · Boeing 73733A · Light System WiringSDR AWXA0001149Skin · crackedLIGHT AFT OF RT AFT WING-BODY FAIRING HAS TEMP REPAIR DOUBLER BS 727D STR 23R. REMOVED TEMP DOUBLER, FABED REPAIR PARTS AND INSTALLED IAW ER 03-5361-00347-001 AND SRM 53-00-01Dec 29, 2000 · N165AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001148Bracket · brokenRT A/C EXHAUST LOUVER MOUNT BRACKETS BROKEN. REMOVED, FABED REPLACEMENT BRACKET, INSTALLED IAW SRM 51-40-02 AND SRM 51-30-01Dec 29, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001147Floorbeam · corrodedFS 312 RBL 6 - RBL 12 FLOOR BEAM UPPER CHORD CORRODED OUT OF LIMITS. CUT OUT DAMAGED CHORD LBL 6 - RBL 26 AND REPAIRED IAW SRM 53-10-51 FIG 205Dec 29, 2000 · N165AW · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA0001146Bracket · brokenLT A/C EXHAUST LOWER MOUNT BRACKETS BROKEN. REMOVED, FABED REPLACEMENT BRACKET, INSTALLED IAW SRM 51-40-02 AND SRM 51-30-01Dec 29, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001145Skin · crackedLT PYLON SKIN CRACKED AT ACCESS PANEL 5727L. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-50-01, S/B 737-54-1035Dec 29, 2000 · N165AW · Boeing 73733A · Nacelle/Pylon, Plate/SkinSDR AWXA0001144Skin · corrodedLIGHT SURFACE CORROSION ON LT WING LOWER SKIN AT ACCESS PANEL 7212 FLANGE. REMOVED CORROSION W/I LIMITS IAW SRM 57-20-01 FIG 205; SHOT PEENED IAW 51-20-06 FIG 1; TREATED AND PRIMED IAW 51-20-01Dec 29, 2000 · N165AW · Boeing 73733A · Wing, Plate/SkinSDR AWXA0001143Skin · crackedLT O/B WING AFT FLAP L/E DEEP CHAFE WITH CRACK AT O/B ROLLERS. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS SKIN & SPLICE IAW SRM 57-53-01 FIG 204.Dec 29, 2000 · N165AW · Boeing 73733A · Wing, Plate/SkinSDR AWXA0001135Stiffener · crackedNR 6 FLAP TRACK FAIRING STIFFENER AND DOUBLER CRACKED. REMOVED RT. WING I/B FLAP ASSY BOTTOM I/B STIFFENER AND DOUBLER IAW SRM 51-40-02; INSTALLED NEW STIFFENER AND DOUBLER IAW 51-40-02Dec 21, 2000 · N165AW · Boeing 73733A · Trailing Edge FlapsSDR AWXA0001134Skin · crackedLEFT I/B AFT FLAP LEADING EDGE CRACKED AT 3RD HINGE OBD. REMOVED LEADING EDGE IAW SRM 51-40-02; CUTOUT DAMAGED PORTION IAW 57-53-01; FABED SKIN REPAIR AND SPLICE PLATE IAW 57-53-01; TREATED AND PRIMED REPAIR PARTS IAW 51-20-01; INSTALLED PARTS AND SEALED IAW 5Dec 21, 2000 · N165AW · Boeing 73733A · Trailing Edge FlapsSDR AWXA0001133Skin · brokenFLANGE ON A/C GROUND CONNECT BROKEN (INNER FLANGE INNER DOUBLER) ON FUSELAGE SKIN AT DOOR LANDING RING. CUT OUT DAMAGED FLANGE; HFEC SHOWS NO CRACKS; FABED REPAIR PLATE; PRIMED AND TREATED ALL FAY SURFACES; INSTALLED REPAIR PLATE AND CONICAL WASHERS IAW SRM 53Dec 21, 2000 · N165AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001132Skin · corrodedLIGHT SURFACE CORROSION ON LT WING LOWER SKIN AT ACCESS PANEL 7211 FLANGE. REMOVED CORROSION W/I LIMITS IAW SRM 57-20-01 FIG 205; SHOT PEENED IAW 51-20-06 FIG 1; TREATED AND PRIMED IAW 51-20-01 AS REQUIRED.Dec 21, 2000 · N165AW · Boeing 73733A · Wing, Plate/SkinSDR AWXA0001131Bulkhead · crackedULTRASONIC INSP. DETECTED CRACK APPROX. 4.0 INCHES LONG AT FWD PRESSURE BULKHEAD AT STA 178 WL 213 BETWEEN LBL 5 & LBL 17 ON WEB BEHIND HORIZ ANGLE STIFFENER. REMOVED ANGLE, STOP DRILLED CRACK IAW SRM 53-10-08; CRACK TERMINATED; FABED DOUBLER AND SHIMS IAW 53-Dec 21, 2000 · N165AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001130Frame · crackedCABIN RT I/B FWD OVERWING EXIT FRAME SUPPORT CRACKED AT BOTTOM FASTENER HOLE AREA BS 616 BELOW CABIN FLOOR PANEL STR 17R. REMOVED FASTENERS AND COLLARS IAW ER 03-5310-00339-JS1; CUT OUT DAMAGED AREA FROM FRAME IAW ER 03-5310-00339-JS1; NDT INSPECTED CUT OUT HFDec 21, 2000 · N165AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001129Strap · crackedFS 178 WL 187 BL 0 STRAP CRACKED. REMOVED STRAP; FABED REPAIR STRAP AND DOUBLER IAW SRM 51-70-13 FIG 1Dec 21, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001128Seat Track · corrodedCABIN SEAT TRACK RBL 24 I/B FLANGE HAS BARE METAL ON UNDERSIDE AT EACH FLOOR BOARD FASTENER HOLE - SOME WITH LIGHT SURFACE CORROSION - FROM BS 540 - 727. REMOVED LIGHT SURFACE CORROSION - .070 MATERIAL LOSS .001-.002 FOUND WITH IN LIMITED MECHANICAL MEASUREMENDec 21, 2000 · N165AW · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0001127Channel · corrodedCORROSION ON RT AFT LAV WALL LOWER SUPPORT CHANNEL STA 993 FROM RBL 23 - RBL 44 WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED HAT SECTION IAW SRM 51-40-02; FABED HAT SECTION IAW DWG 65C19883 AND SRM 51-30-01; ALODINED AND PRIMED IAW 51-20-01; INSTALLED HAT SEDec 21, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001126Web · crackedFLOOR WEB CRACKED FS 180 WL 207 LBL 26 (1.0L). REMOVED DAMAGED WEB; FABED NEW WEB; INSTALLED WEB IAW SRM 51-40-02 DWG 65-45833Dec 21, 2000 · N165AW · Boeing 73733A · Fuselage Floor PanelSDR AWXA0001124Skin · crackedNR 1 SLAT HAS CRACKS IN AFT ROW OF RIVETS LWR SURFACE, INBD OF ACTUATOR. REMOVED DAMAGED AREA; FABED AND INSTALLED REPAIR PARTS, FILLER AND SPLICE PLATE IAW SRM 57-43-01 FIG 206Dec 20, 2000 · N165AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001123Skin · scratchedFUSE SKIN FROM STA 1060-1070 L14L HAS DEEP SCRATCH UNDER W OF TAIL NUMBER; FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN; NDT NO CRACKS NOTED; FABED REPAIR PLATE; INSTALLED PLATE; INSTALLED CONICAL WASHERS IAW SRM 53-00-01, 51-40-02.Dec 20, 2000 · N165AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001122Web · crackedFLOOR WEB CRACKED FS 180 WL 207 RBL 26 (1.0L). REMOVED DMGD WEB IAW SRM 51-40-02; FABED REPLACEMENT WEB IAW DWG 65-45833; INSTALLED IAW 51-40-02Dec 20, 2000 · N165AW · Boeing 73733A · Fuselage Floor PanelSDR AWXA0001121Frame · crackedSIDE CHORD CRACKED FS 178 WL 207 LBL 26 (1.6L) AND WL 195 LBL 24 (1.3L). CUTOUT CRACKED SECTION OF CHORD WL 212-175 IAW ER 03-5310-00339-JS3; NDT NO CRACKS NOTED IAW 51-00-00 FIG 23; FABED AND INSTALLED REPAIR PARTS IAW ER 03-5310-0039-JS3Dec 20, 2000 · N165AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001120Web · crackedCENTER WEB CRACKED FS 178 WL 187 LBL 0.7 AND RBL 0.7. REMOVED DAMAGED AREA; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203Dec 20, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001119Web · crackedCENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.3L) AND WL 202 (0.9L). REMOVED DAMAGE; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209Dec 20, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001115Frame · gougedRT MLG WHEEL WELL, AFT CUTOUT VERTICAL ANGLE BRACKET GOUGED (LOCATED ADJACENT TO GROUNDING STUD). REMOVED RT HYD PANEL COVER MAIN LANDING GEAR RIGHT SIDE IAW SRM 51-40-02; REMOVED RT OUTBOARD AFT MAIN LANDING GEAR PANEL IAW 51-40-02; REMOVED AND REPLACED DAMAGDec 18, 2000 · N165AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001114Stiffener · crackedLT WING LWBL 184 TE AT NR 3 FLAP TRACK FAIRING INBOARD FORMER/STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02Dec 18, 2000 · N165AW · Boeing 73733A · Leading Edge DevicesSDR AWXA0001113Bulkhead · crackedCENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-18 FIG 209Dec 18, 2000 · N165AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001112Intercostal · crackedINTERCOSTAL CRACKED THRU FS 178 WL 195 RBL 24. REMOVED INTERCOSTAL IAW SRM 51-40-02; CUTOUT DAMAGE IAW 53-10-08 FIG 202; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 NO CRACKS NOTED; REPAIRED INTERCOSTAL WITH FILLER, ANGLE, AND RADIUS BLOCK; INSTALLED IAW SRMDec 18, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001111Intercostal · crackedINTERCOSTAL CRACKED THRU FS 178 WL 195 LBL 24. REMOVED INTERCOSTAL IAW SRM 51-40-02; CUTOUT DMG IAW 53-10-08 FIG 202; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 NO CRACKS NOTED; REPAIRED INTERCOSTAL WITH FILLER, ANGLE, AND RADIUS BLOCK; INSTALLED IAW SRM 53Dec 18, 2000 · N165AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA0001110Skin · crackedLAS - DURING SCHEDULED CHECK A 1.0 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN ON THE RT SIDE JUST AFT OF THE WING TO BODY FAIRING FS 727.0 STR 22R; CRACK CONFIRMED WITH HFEC. DAMAGED AREA WAS REMOVED AND CONFIRMED WITH HFEC AND THE SKIN WAS REPAIRED IAW SRM 53-Dec 18, 2000 · N173AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001049Skin · scratchedFUSELAGE SKIN STA 1060-1070 L14L HAS DEEP SCRATCH UNDER W OF TAIL NUMBER - FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN, NDT NO CRACKS NOTED; FABED REPAIR PLATE, INSTALLED REPAIR PLATE, INSTALLED CONICAL WASHERS IAW SRM 53-00-01, 51-40-02Dec 12, 2000 · N165AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA0001048Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 187 LBL 0.7 (1.9) AND RBL 0.7 (1.5L). REMOVED DAMAGED AREA, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203Dec 12, 2000 · N165AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001047Bulkhead · crackedCENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.3L) AND WL 202 (0.9L). REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209Dec 12, 2000 · N165AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001046Bulkhead · crackedCENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. REMOVED DAMAGE, FABED AND INSTALLED PARTS IAW SRM 53-10-08 FIG 209Dec 12, 2000 · N165AW · Boeing 73733A · Fuselage Main, BulkheadSDR AWXA0001050Frame · crackedCABIN RT I/B FWD OVERWING EXIT FRAME SUPPORT CRACKED AT BOTTOM FASTENER HOLE AREA STA 616 STR 17R BELOW CABIN FLOOR PANEL. REMOVED FASTENERS AND COLLARS, CUT OUT DAMAGE, NDT CUTOUT NO CRACKS NOTED, FABED AND INSTALLED REPAIR PARTS IAW ER-03-5310-00339-JS1 AND Dec 12, 2000 · N165AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA0001035Wire · brokenEMERGENCY LIGHT AT ROW 21 INOP. REPAIRED BROKEN WIREDec 6, 2000 · N172AW · Boeing 73733A · Light System WiringSDR AWXA0001030Wire · brokenEMERGENCY LIGHT AT SEAT 2B INOP. REPAIRED BROKEN WIRE, OPERATIONALLY CHECKS GOODDec 6, 2000 · N167AW · Boeing 73733A · Light System WiringSDR AWXA0001032Floorbeam · cutT CAP AT BS 328 CUT AND SCRAPED ON TOP SIDE RBL 12 TO RBL 55. FABED AND INSTALLED REPLACEMENT T CAP IAW SRM 53-10-51 PG 220-222 FIG 205Dec 6, 2000 · N175AW · Boeing 73733A · Fuselage Main, Floor Beam
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