N328AW
Registered owner: STEELE MICHAEL W, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICA WEST AIRLINES | Operator | on 1998-12-13 | Operator named in NTSB report |
Accident & incident history
Operated by AMERICA WEST AIRLINES, INC. (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
125 reports on file, 1996-01-01 – 2006-02-20.
Part: SKIN — CRACKED (BS 943) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT BS 943 AND STR 24L. MAINTENANCE REPAIRED SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5360-06023-RC1. MAINTENANCE REPAIRED SKIN AT BS 943 AND STR 24L BY CUTTING OUT AND REMOVING DAMAGED SKIN AND DOUBER IAW BOEING 7373-00SRM 53-00-01-2R31. FABRICATED AND DRILLED REPAIR DOUBLER, REPAIR TRIPLER, FILLER AND SPLICE STRAP IAW A.W.A. E.R. NO. 03-5360-06023-RC1. INSTALLED FABRICATED REPAIR PARTS AT BS 943 AND STR 24L IAW A.W.A. E.R. NR 03-5360-06023-RC1.
Part: SKIN — CORRODED (BS 1006) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CORROSION BULGE ON FUSELAGE EXTERIOR SKIN AT BS 1006 AND STR 27R. MAINTENANCE REPAIRED IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-06047-ES1. MAINTENANCE REPAIRED SKIN BY REMOVING DAMAGED SKIN IAW AWAER NR 03-5361-06047-ES1. FABRICATED REPAIR DOUBLER, TRIPLER, STRUCTURAL FILLER AND FILLER IAW AWAER NR 03-5361-06047-ES1. INSTALLED FABRICATED REPAIR PARTS AT BS 1006 AND STR 27R IAW AWAER NR 03-5361-06047-ES1.
Part: SHEAR TIE — CORRODED (BS 987) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CORROSION ON SHEAR TIE AT BS 987 AND BL 6R ON LOWER SURFACE. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 987 AND BL 6R IAW BOEING 737-300 SRM 51-40-05-0G FIG 2.
Part: SHEAR TIE — CORRODED (BS 967) · corrosion level 2 · airframe 61,088 hrs · 37,339 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE UPPER SURFACE OF SHEAR TIE AT BS 967 AND BL 20R. MAINTENANCE REMOVED AND INSTALLED NEW REPLACEMENT SHEAR TIE AT BS 967 AND BL 20R IAW BOEING 737-300 SRM 51-40-02-0G.
Part: STRINGER — CORRODED (BS 960-1020) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - MAJOR REPAIR - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON STR 25R AT BS 960 TO BS 1020. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1 FIG 101. MAINTENANCE REMOVED DAMAGED STRINGER SECTION IAW BOEING 737-300 SRM 53-00-03-2R1 FIG 101. RECEIVED REPLACEMENT STRINGER SECTION, FORMED CHANNEL AND FORMED ANGLES IAW BOEING 737-300 SRM 53-00-03-2R1. INSTALLED FABRICATED REPAIR PARTS ON STR 25R AT BS 960 TO BS 1020 IAW BOEING 737-300 SRM 53-00-03-2R1.
Part: SHEAR TIE — CORRODED (BS 986) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CORROSION ON SHEAR TIE AT BS 986 AND BL 16R ON LOWER SURFACE. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 986 AND BL 16R IAW BOEING 737-300 SRM 51-40-05-0G FIG 2.
Part: BULKHEAD — CANNING (BS 1016) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK, DISCOVERED THE AFT PRESSURE BULKHEAD OIL CANNING JUST ABOVE STR 24L AT BS 1016, END FITTING BELOW APU DUCT. MAINTENANCE FABRICATED REPAIR CHANNEL, FILLER AND STRAP IAW BOEING 737-300S RM 53-80-08-2RF FIG 201. INSTALLED FABRICATED REPAIR PARTS ON THE AFT PRESSURE BULKHEAD, BS 1016, JUST ABOVE STR 24L IAW BOEING 737-300 SRM 53-80-08-2R4.
Part: ANGLE — CRACKED (L1 DOOR FRAME) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED L1 DOOR FRAME ANGLE CRACKED, .5 INCHES, AT 7TH FROM TOP AFT STOP FITTING. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE ON THE L1 DOOR FRAME, 7TH FROM THE TOP AFT STOP FITTING IAW BOEING 737-300 SRM 51-40-02-0G PAR 4B FIG 3, 4, AND 8.
Part: SHEAR TIE — CORRODED (BS 1006) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON SHEAR TIE AT BS 1006, BL 0 AND BETWEEN STR 27L AND STR 27R. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 1006, BL 0 AND BETWEEN STR 27L AND STR 27R IAW BOEING 737-300 SRM 51-40-05-0G FIG 2.
Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED 2 CRACKS, .5 INCHES IN LENGTH EACH, ON THE L1 DOOR FRAME ADJACENT TO THE 7TH FROM THE TOP AFT STOP FITTING AND ON THE INTERIOR SKIN AT THE AFT SIDE DOOR STOP PIN CUTOUTS AT BS 347.30 AND WL 246. MAINTENANCE TRIMMED OUT CRACKS IN DOOR FRAME FLANGE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5210-06038-SS1. FABRICATED DOUBLER, TRIPLER AND 4 SKIN FILLERS IAW AWA ER 03-5210-06038-SS1. INSTALLED FABRICATED REPAIR PARTS ON THE L1 DOOR FRAME ADJACENT TO THE 7TH FROM THE TOP AFT STOP FITTING AND ON THE INTERIOR SKIN AT THE AFT SIDE DOOR STOP PIN CUTOUTS AT BS 347.30 AND WL 246 IAW AWA ER NR 03-5210-06038-SS1.
Part: CHANNEL — CORRODED (BS 540) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON STR 26L CHANNEL AT BS 540. MAINTENANCE REMOVED FABRICATED AND REPLACED STR 26L CHANNEL AT BS 540 IAW B737-300 SRM 51-40-02-0G PARA 7D FIGS 8, 12 AND BAC DWG 65-49564.
Part: SKIN — CRACKED (NR 4 SLAT) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED 6 CRACKS, .189 INCHES LONG, ON THE BOTTOM OF THE NR 4 SLAT SKIN BELOW THE OUTBOARD AUXILIARY TRACK FROM SS 80R TO SS 100R. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE NR 4 SLAT IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 57-43-01-2R6. INSTALLED FABRICATED REPAIR PARTS ON THE NR 4 SLAT SKIN BELOW THE OUTBOARD AUXILIARY TRACK FROM SS 80R TO SS 100R IAW BOEING 737-300 SRM 57-43-01-2R6.
Part: STIFFENER — CORRODED (THRESHOLD) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON 3 ZEE STIFFENERS SUPPORTS FOR THE R1 DOOR THRESHOLD PLATE, FROM BS 312 TO BS 328, WL 208 AND BL 62R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED 3 REPLACEMENT ZEE STIFFENERS FOR THE R1 THRESHOLD PLATE SUPPORTS IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7, 8 AND BACK DWG 65-45875.
Part: SILL — CORRODED (BS 294) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE UPPER SURFACE OF THE R1 LOWER SILL WEB AT BS 294.5 TO BS 332.1, BL 60R AND WL 208. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB ON R1 UPPER SILL FROM BS 294.5 TO BS 332.1, BL 60R AND WL 208 IAW BOEING737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7, 8, 12 AND BAC DWG 65-45875.
Part: STRAP — CORRODED (BS 799-835) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION AROUND NUT PLATE HOLES ON STRAP FROM BS 799 TO BS 835, BL 0R AND BENT AT BS 821. CORROSION WAS FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW STRAP FROM BS 799 TO BS 835, BL 20R IAW BOEING 737-300 SRM 51-40-02-0G FIGS 3, 6, 7 AND 8.
Part: ATTACH ANGLE — CORRODED (BS 847) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CORROSION ON WEB ATTACH ANGLE AT BS 847, WL 157 AND BL 20R. MAINTENANCE REMOVED AND INSTALLED NEW WEB ATTACH ANGLE AT BS 847, WL 157 AND BL 20R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8, 12, AND 13.
Part: SILL — CORRODED (BS 294) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON MOD REPAIR ANGLE BELOW THE R1 LOWER SILL, AFT SIDE OF FRAME AT BS 294.5, WL 208 AND FROM BL 43R TO BL 60R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT MOD REPAIR ANGLE AT BS 294.5, AFT SIDE OF FRAME, AT WL 208 FROM BL 43R TO BL 60R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7, 8 AND DWG 65-45808.
Part: DOUBLER — CORRODED (FBS 294) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON DOUBLER ON UPPER SIDE OF B/S FRAME 294.5, BL 57R AND RT OUTBOARD END AT CIRCUMFERENTIAL. MAINTENANCE REMOVED CORROSION ON UPPER SIDE OF B/S FRAME 294.5, RT O/B END AND DETERMINED IT TO BE OUT OF LIMITS IAW B737-300 SRM 53-10-15-1A1, FIG 101. REMOVED, FABRICATED AND REPLACED DOUBLER ON UPPER SIDE OF B/S FRAME 294.5, BL 57R AND RT O/B END AT CIRCUMFERENTIAL IAW B737-300 SRM 51-40-02-0G, PAR 4, FIG'S 3, 4, 6, 7, 8 AND BAC DWG 65-45875.
Part: FRAME — CORRODED (BS 1006) · corrosion level 2 · airframe 61,088 hrs · 37,339 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON FRAME AT BS 1006 AND BL 0. MAINTENANCE REMOVED DAMAGE FROM FRAME AT BS 1006 IAW BOEING 737-300 SRM 53-00-07-2R5. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-00-07-2R5. INSTALLED FABRICATED REPAIR PARTS ON FRAME AT BS 1006 AND BL 0 IAW BOEING 737-300 SRM 53-00-07-2R5.
Part: WEB — CORRODED (BS 794-821) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CORROSION ON WEB LOCATED AT BS 794 TO BS 821 AND BL 20R. MAINTENANCE REMOVED AND INSTALLED NEW WEB FROM BS 794 TO BS 821 AND BL 20R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8, 12, 13 AND PAR 7D.
Part: STRINGER CLIP — CRACKED (BS 693) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED TWO INTERCOSTAL SUPPORT CLIPS CRACKED, .4 INCHES, AT BS 693.75 AND BL .25R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL SUPPORT CLIPS AT BS 693.75 AND BL .25R IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-06031-SS2.
Part: SKIN — DEBONDED (ZONE 600) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED DISBOND AREA ON THE RT OUTBOARD AFT FLAP TRAILING EDGE, SEPERATING 8" AT THE INBOARD END. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE RT OUTBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED FABRICATED REPAIR PARTS TO THE RT OUTBOARD AFT FLAP TRAILING EDGE IAW BOEING 737-300 SRM 51-70-10-2R4.
Part: ANGLE — CORRODED (BS 294-333) · corrosion level 2 · airframe 61,088 hrs · 37,339 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE R1 INNER CHORD AT BS 294 TO BS 300 AND BS 333 AT BL 59R AND WL 208. MAINTENANCE REMOVED AND INSTALLED NEW R1 INNER CHORD FROM BS 294 TO BS 360, BL 59R AND WL 208 IAW BOEING 737-300 SRM 51-40-02-0G.
Part: FLOORBEAM — CRACKED (BS 663) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED FLOORBEAM CRACKED, .25 INCHES, AT BS 663 AND BL 24L. MAINTENANCE STOP DRILLED CRACK IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NR 03-5702-06039-HF1. FABRICATED REPAIR CHANNEL IAW AWA ER 03-5702-06039-HF1. INSTALLED FABRICATED REPAIR PARTS AT BS 663 AND BL 24L IAW AWA ER 03-5702-06039-HF1.
Part: ANGLE — CRACKED (BS 277) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED STIFFENER ANGLE CRACKED, .25 INCHES, AT BS 277 AND STR 12R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER ANGLE AT BS 277 AND STR 12R IAW BOEING 737-300 SRM 51-40-02-0G PAR 4B.
Part: CLIP — CRACKED (BS 693) · airframe 61,088 hrs · 37,339 cycles
MCN - DURING C24 CHECK DISCOVERED INTERCOSTAL SUPPORT CLIP CRACKED. 500 INCHES IN LENGTH, AT BS 693.75, WL 207 AND BL. 25L. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL SUPPORT CLIP AT BS 693.75, WL 207 AND BL .25L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5361-06031-SS2.
Part: SILL — CORRODED (BS 297) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON THE BOTTOM SURFACE OF THE R1 LOWER SILL WEB AT BS 297, BL 60R AND WL 208. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB ON R1 LOWER SILL AT BS 297, BL 60R AND WL 208 IAW BOEING737-300 SRM 51-40-02-0G FIGURES 3, 4, 6, 7, 8, 12 AND BAC DWG 65-45875.
Part: STRINGER CLIP — CRACKED (BS 847) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .125 INCHES IN LENGTH, AT BS 847 AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS 847 AND STR 4L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.
Part: SKIN — DEBONDED (ZONE 600) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED DISBOND AREA AT THE OUTBOARD AFT CORNER OF THE RT INBOARD AFT FLAP, UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE RT INBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND CORE IAW BOEING 737-300 SRM 57-53-02. BONDED FABRICATED REPAIR PARTS TO THE RT INBOARD AFT FLAP, UPPER AND LOWER SURFACE IAW BOEING 737-300 SRM 51-70-10-2R4.
Part: STRINGER CLIP — CRACKED (BS 663) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .25 INCHES, AT BS 663 AND STR 10L. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT STRINGER TIE CLIP AT BS 663 AND STR 10L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8, 12 AND BAC DWG 69-41437.
Part: STRINGER CLIP — CRACKED (BS 616) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED STRINGER CLIP CRACKED, .125 INCHES IN LENGTH, 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 FIGURES 8 AND 12.
Part: STRINGER CLIP — CRACKED (BS 639) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED TWO STRINGER CLIPS CRACKED, .125 INCHES IN LENGTH EACH, AT BS 639 STR 2L AND STR 4L. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP AT BS 639 2L AND 4L IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8 AND 12.
Part: FRAME — CRACKED (BS 663) · airframe 61,088 hrs · 37,339 cycles
MCN - DURING C24 CHECK DISCOVERED MAIN CABIN FRAME AT BS 663 CRACKED .5 INCHES IN LENGTH AT STR 2R. MAINTENANCE ROUTED OUT DAMAGED AREA IAW BOEING 737-300 SRM 53-00-07-2R9 FIG 201. FABRICATED REPAIR ANGLE, FILLERS, AND STRINGER TIE IAW BOEING 737-300 SRM 53-00-07-2R9 FIG 201. INSTALLED FABRICATED REPAIR PARTS AT BS 663 AND STR 2R IAW BOEING 737-300 SRM 53-00-07-2R9 FIG 201.
Part: ATTACH ANGLE — CORRODED (BS 304-324) · airframe 61,229 hrs · 37,424 cycles
DURING C24 CHECK DISCOVERED CORROSION ON THE R1 LOWER SILL, INBOARD ATTACH ANGLE FROM BS 304 TO BS 324, BL 62R AND WL 209. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-15-1A1. MAINTENANCE REMOVED AND INSTALLED NEW ATTACH ANGLE AT THE R1 LOWER SILL, INBOARD ATTACH ANGLE FROM BS 304 TO BS 324, BL 62R AND WL 209 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 8 AND 12.
Part: SHEAR TIE — CRACKED (BS 328) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED BS 328 FRAME SHEAR TIE CRACKED, .25 INCHES, OUTBOARD SIDE OF STRINGER 28L. MAINTENANCE REMOVED AND INSTALLED NEW SHEAR TIE AT BS 328, OUTBOARD SIDE OF STR 28L IAW BOEING 737-300 SRM 51-40-02-0G PAR 4B, FIG 8 AND FIG 12.
Part: FRAME — CRACKED (BS 616) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED MAIN CABIN FRAME AT BS 616 CRACKED, 2.2 INCHES, AT RT SIDE BOTTOM END, UNDER MAIN CABIN FLOOR AT BL 60R AND WL 200. MAINTENANCE REMOVED DAMAGED AREA FROM BS 616 FRAME IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) NO. 03-5311-01143-DD1. FABRICATED REPAIR FILLER AND STIFFENER ANGLE IAW AWA ER 03-5311-01143-DD1. INSTALLED FABRICATED REPAIR PARTS AT BS 616 FRAME, WL 200 AND BL 60R IAW AWA ER 03-5311-01143-DD1.
Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 61,088 hrs · 37,339 cycles
MCN - DURING C24 CHECK DISCOVERED RT HORIZONTAL STAB LEADING EDGE SPAR WEB CRACKED, .890 INCHES IN LENGTH, AT THE THIRD LIGHTENING HOLE FROM THE OUTBOARD END AT STAB STATION 198.5R. MAINTENANCE REMOVED CRACK IAW BOEING 737-300 SRM 55-10-10-1A1 FIG 101. FABRICATED REPAIR DOUBLER IAW BOEING 737-300 SRM 55-10-10-02R3. INSTALLED FABRICATED REPAIR PARTS ON THE R/H HORIZONTAL STAB LEADING EDGE SPAR WEB AT SS 198.50R IAW BOEING 737-300 SRM 55-10-02R3.
Part: DOOR FRAME — CORRODED (BS 800-847) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CORROSION ON THE AFT CARGO COMPARTMENT DOOR, LOWER DOOR SURROUND STRUCTURE WEB FROM BS 800 TO BS 847, WL 158 AND FROM BL 17R TO BL 22R. MAINTENANCE REMOVED AND INSTALLED NEW WEB AT THE AFT CARGO DOOR CUTOUT FROM BS 800 TO BS 847, WL 158 AND FROM BL 17R TO BL 22R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 9 AND 10.
Part: STRINGER — CORRODED (BS 1006-1012) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CORROSION ON STRINGER 26R FROM BS 1006 TO BS 1012. MAINTENANCE REMOVED STRINGER AND FABRICATED REPLACEMENT STRINGER IAW BOEING 737-300 SRM 51-30-01-0G. INSTALLED FABRICATED REPLACEMENT STRINGER AT STR 26R AND FROM BS 1006 TO BS 1012 IAW BOEING 737-300 SRM 51-40-04-0G.
Part: FRAME — CORRODED (BS 727C) · corrosion level 2 · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON FLOOR FRAME, LOWER ATTACH AND FORWARD SIDE AT BS 727C AND STR 26L. MAINTENANCE CUT OUT DAMAGED PORTION OF FRAME IAW BOEING 737-300 SRM 53-00-07-2R7 FIG 201. FABRICATED REPAIR FILLER AND SHEAR TIE IAW BOEING 737-300 SRM 53-00-07-2R7. INSTALLED FABRICATED REPAIR PARTS ON THE FLOOR FRAME, LOWER ATTACH AT BS 727C AND STR 26L.
Part: ATTACH ANGLE — CRACKED (TORQUE BOX) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED CRACK, 1.1 INCHES LONG, ON THE R1 DOOR LOWER FORWARD TORQUE BOX FLOOR WEB ATTACH ANGLE AT BS 298, WL 208 AND BL 53R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT WEB ATTACH ANGLE AT BS 298, WL 208 AND BL 53R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 8, 12, AND 13.
Part: WEDGE — DEBONDED (ZONE 500) · airframe 61,229 hrs · 37,424 cycles
MCN - DURING C24 CHECK DISCOVERED DISBOND AREA ON THE LT INBOARD AFT FLAP AT THE OUTBOARD CORNER, UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE LT INBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED DOUBLER AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4. BONDED FABRICATED REPAIR PARTS TO THE LT INBOARD AFT FLAP, UPPER AND LOWER SURFACE IAW BOEING 737-300 SRM 51-70-10-2R4.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 61,229 hrs · 37,424 cycles
MCN - EEL - DURING C34 CHECK, DISCOVERED ESCAPE PATH WIRING HARNESS WITH MULTIPLE DAMAGED CONNECTORS FROM BS 344 TO BS 947 AT WL 208. MAINTENANCE REPAIRED THE ESCAPE PATH WIRING HARNESS IAW BOEING 737-300 SWPM 20-30-12 STEP 14C. OPERATIONAL CHECKS WERE GOOD IAW AMERICA WEST AIRLINES TASK CARD A1C33006.
Earlier reports · 1996–2005 · 82 reports
2005
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,020 hrs · 37,298 cycles
PHX - DURING INSPECTION DISCOVERED FUSELAGE SKIN CRACK, 1.0 INCHES LONG, ON THE LT SIDE OF THE AIRCRAFT JUST AFT OF WING TO BODY FAIRING BELOW STRINGER 23L AND 1.5 INCHES AFT OF BS 727D. MAINTENANCE TRIMMED OUT CRACK DAMAGE IAW BOEING 737-300 SRM 53-00-01 REPAIR 31. FABRICATED DOUBLER, TRIPLER AND TEAR STRAP DOUBLER IAW BOEING 737-300 SRM 51-00-00 FIG 16. INSTALLED FABRICATED REPAIR PARTS ON THE LT SIDE OF THE AIRCRAFT JUST AFT OF WING TO BODY FAIRING BELOW STRINGER 23L AND 1.5 INCHES AFT OF BS 727D IAW BOEING 737-300 SRM 51-00-01 REPAIR 31 AND AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-05345-RA1.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,978 hrs · 37,273 cycles
EEL - DURING INSPECTION DISCOVERED EMERGENCY LIGHT AT ROW 5, LT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.
Part: DOOR — DAMAGED (APU) · airframe 60,530 hrs · 36,995 cycles
PHX - DISCOVERED PREVIOUS BLEND OUT AT STA 1088, ABOVE THE FORWARD RT CORNER OF THE APU DOOR. WAS DETERMINED TO BE CHAFFING DAMAGE ABOUT 6" AFT OF STA 1088 AT STR 20R. DEEP BLENDED OUT AREA WAS NOT COVERED IN THE BOEING 737-300 SRM. MAINTENANCE CLEANED AND INSPECTED THE DAMAGED AREA TO ENSURE NO CRACKS EXISTED, NONE WERE ALLOWED AND NONE WERE FOUND. FABRICATED EXTERNAL DOUBLER FROM 2024-T3 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 03-5381-05285-HF1. FABRICATED REPAIR PARTS WERE INSTALLED WET AT BS 1088, STR 20R IAW AWA ER NO. 03-5381-05285-HF1.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 60,374 hrs · 36,905 cycles
PHX - EEL - CREW REPORTED TO MAINTENANCE THE FORWARD GALLEY FLASH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.
Part: STIFFENER — CORRODED (PRESSURE BLKHD) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK FOUND CORROSION PRESENT ON STIFFENER CHANNEL LOCATED AT AFT PRESSURE BULKHEAD FORWARD SIDE AT BS 1016, WL 155, BL 0. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-80-08-1 FIG 101. MAINTENANCE REMOVED CORROSION ON STIFFENER CHANNEL LOCATED AT AFT PRESSURE BULKHEAD BS 1016, WL 155, AND BL 0. MAINTENANCE REMOVED DAMAGE STIFFENER ON THE AFT PRESSURE BULKHEAD AT STATION 1016, WL 150, BL 0 AND FABRICATED REPAIR STIFFENER IAW BOEING 737-300 SRM 53-80-08-2 FIG 201. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-80-08-2 FIG 201.
Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK, FOUND CORROSION IN FORWARD CARGO PIT ON 20 NUT PLATES LOCATED ON THRESHOLD WEB FROM STA 450 TO STA 490. MX FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-30-15-1 FIG 101. REMOVED THRESHOLD WEB FROM STA 450 TO STA 490 AND FABRICATED NEW FORWARD PIT THRESHOLD WEB IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 AND BOEING DWG 65-20726. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-40-05 FIG 2.
Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK FOUND INTERCOSTAL CRACKED, .25 INCHES IN LENGTH INSIDE FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, STRINGER 23R. MAINTENANCE REMOVED INTERCOSTAL AT FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, STRINGER 23R AND FABRICATED NEW INTERCOSTAL IAW BOEING DWG 69-41861. INSTALLED FABRICATED REPAIR PARTS AT FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, STRINGER 23R IAW BOEING 737-300 SRM 51-40-02-0 FIG 3, 4, 6 AND BOEING 737-300 SRM 51-40-04 FIG 2.
Part: SKIN — CRACKED (R1 DOOR) · airframe 59,750 hrs · 36,526 cycles
MAJOR REPAIR. DURING C-13 CHECK FOUND R1 DOOR OUTER SKIN CRACKED AT UPPER HINGE CUTOUT. CRACK .125 INCHES IN LENGTH. MAINTENANCE CUT OUT CRACKED AREA AT R1 DOOR OUTER SKIN. CRACKED AT UPPER HINGE. CUTOUT IAW AMERICA WEST AIRLINES ENGINEERING REQUEST (E.R.) NO. 03-5241-05166-SS2. FABRICATED REPAIR DOUBLER IAW E.R. NO. 03-5241-05166-SS2. INSTALLED FABRICATED REPAIR PARTS AT R1 DOOR OUTER SKIN CRACKED AT UPPER HINGE CUTOUT IAW E.R. NO. 03-5241-05166-SS2.
Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 59,750 hrs · 36,526 cycles
FOUND ON FORWARD SIDE OF L1 DOOR CUTOUT INTERCOSTAL WEB CRACKED AT STR 7L AND BS 294. MAINTENANCE REMOVED INTERCOSTAL WEB AND CLIP ON L1 DOOR IAW BOEING 737-300 SRM 51-40-01. FABRICATED INTERCOSTAL WEB, AUXILIARY INTERCOSTAL AND SHEAR TIE CLIP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5300-05172-RC1. FABRICATED REPAIR PARTS WERE INSTALLED IAW AWA ER NR 03-5300-05172-RC1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK, FOUND CORROSION ON FLOORBEAM STA 328, FROM BL 10R TO BL 30R. MAINTENANCE REMOVED CORROSION. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED DAMAGED AREA FROM FLOORBEAM AT STA 328 IAW BOEING 7637-300 SRM 53-10-51-2 FIG 205. RECEIVED NEW UPPER CHORD AND PREPPED FOR INSTALL IAW BOEING 737-300 SRM 53-10-51. FABRICATED REPAIR ANGLE, ANGLE SPLICES, STIFFENERS, AND SHIMS IAW BOEING 737-300 SRM 53-10-51. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 35-10-51-2 FIG 205.
Part: PRESSURE BLKHD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK DISCOVERED CORROSION ON AFT PRESSURE BULKHEAD STA 1016, WL 150 TO WL 155, STR 27R, ON FORWARD SIDE AND RUNNING UNDER LEVELING COMPOUND. MAINTENANCE REMOVED CORROSION ON AFT PRESSURE BULKHEAD STA 1016, WL 150 TO WL 155, STR 27R, ON FORWARD SIDE AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-80-01-1 FIG 101. MAINTENANCE CUT OUT DAMAGE AREA ON AFT PRESSURE BULKHEAD AT STATION 1016, WL 150, STR 27R AND FABRICATED REPAIR DOUBLER, STIFFENER, SPLICES AND FILLER IAW BOEING 737-300 SRM 53-80-08-2 FIG 201. INSTALLED AND SEALED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 53-80-08-2 FIG 201.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK, FOUND CORROSION ON INTERCOSTAL SUPPORT AT STATION 297, WL 208, BL 31R. CORROSION OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED CORRODED INTERCOSTAL SUPPORT AT STATION 297, WL 208, BL 31R AND FABRICATED NEW INTERCOSTAL SUPPORT IAW BOEING 737-300 SRM 51-40-05 FIG 2-4, BOEING 737-300 SRM 51-40-02 FIG 8 AND BOEING DWG 65-45834. INSTALLED FABRICATED REPAIR PARTS AT STATION 297, WL 208, BL 31R IAW BOEING 737-300 SRM 51-40-02-0 FIG 4.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK FOUND CORROSION ON FLOORBEAM AT BS 312, WL 208, BL 12R. MAINTENANCE REMOVED CORROSION ON FLOORBEAM AT BS 312, WL 208, BL 12R AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. FABRICATED REPAIR ANGLES IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. CUT AND DRILLED EXTRUSION FOR UPPER CHORD IAW BOEING 737-300 SRM 53-10-51-2 FIG 205. INSTALLED FABRICATED REPAIR PARTS AT BS 312, WL 208, BL 12R IAW BOEING 737-300 SRM 53-10-51-2 FIG 205.
Part: STIFFENER — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK, FOUND GALVANIC CORROSION ON FLOORBEAM STIFFENER LOCATED AT BS 325, BL 12R, WL 208. MX REMOVED CORROSION AT BS 325, BL 12R, WL 208 IAW BOEING 737-300 SRM 51-10-02 AND DETERMINED CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-10-51-1 FIG 101. REMOVED FLOORBEAM STIFFENER AT BS 325, BL 12R, WL 208 AND INSTALLED NEW FLOORBEAM STIFFENER IAW BOEING 737-300 SRM 51-40-02-2 FIG 12.
Part: SKIN — CRACKED (NR 2 PYLON) · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK, FOUND CRACK, .650 INCHES IN LENGTH, LOCATED ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R, ON THE NR 2 PYLON. MAINTENANCE STOP DRILLED CRACK ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R IAW AMERICA WEST AIRLINES ENGINEERING REQUEST (ER) NR 03-5400-05175-RC1. FABRICATED REPAIR DOUBLER IAW ER 03-5400-05175-RC1. INSTALLED FABRICATED REPAIR PARTS ON KEEL SKIN AT EDGE OF ACCESS PANEL 5823R ON THE NR 2 PYLON IAW ER 03-5400-05175-RC1.
Part: SKIN — CRACKED (LT PYLON) · airframe 59,750 hrs · 36,526 cycles
FOUND TOP LT PYLON CRACKED AT ACCESS PANEL 5727L. MAINTENANCE STOP DRILLED CRACK AT LT PYLON PANEL 5727L AND INSTALLED DOUBLER AT LT PYLON ACCESS PANEL 5727L IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5430-05166-SS1.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK DISCOVERED CORROSION ON HAT CHANNEL LOCATED AT BS 956.5 + 7 AND FROM BL 14R TO BL 44R, WL 204. MAINTENANCE REMOVED CORROSION AT BS 956.5 + 7, FROM BL 14R TO BL 44R, WL 204 AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51-1 FIG 101. ALSO, DISCOVERED TO BE A PREVIOUS BLEND OUT OF SECTION. REMOVED HAT CHANEL AT BS 956.5 + 7, FROM BL 14R TO BL 44R, WL 204 FOR REPLACEMENT AND FABRICATED HAT SECTION IAW BOEING 737-300 SRM 51-40-02-0 FIG 13, BOEING 737-300 SRM 51-40-05-0 PAR 4A AND BOEING DWG 65C19883. INSTALLED FABRICATED REPAIR PARTS AT BS 956.5 + 7, FROM BL 14R TO BL 44R, WL 204 IAW BOEING 737-300 51-40-02-0 FIG 12.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK DISCOVERED CORROSION ON FLOOR SUPPORT JUST FORWARD OF BS 967, BL 18L, WL 204. MAINTENANCE BLENDED OUT CORROSION JUST FORWARD OF BS 967, BL 18L, WL 204 AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-51. REMOVED FLOOR SUPPORT JUST FORWARD OF BS 967, BL 18L, WL 204 IAW BOEING 737-300 SRM 51-70-04-0 FIG 1. PREPARED REPLACEMENT FLOOR SUPPORT FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 6. INSTALLED REPLACEMENT FLOOR SUPPORT JUST FORWARD OF BS 967, BL 18L, WL 204 IAW BOEING 737-300 SRM 51-70-04-0 FIG 1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,750 hrs · 36,526 cycles
DURING C-13 CHECK, FOUND CORROSION ON FLOORBEAM FROM BS 986.5 TO BS 1006, WL 204, BL 16R. OUT OF LIMITS IAW BOEING 737-300 SRM 56-60-51 FIG 101. REMOVED CORRODED BEAM AT BS 986.5 TO BS 1006, WL 204, BL 16R IAW BOEING 737-300 SRM 53-60-51-1. INSTALLED NEW BEAM FROM BS 986.5 TO BS 1006, WL 204, BL 16R IAW BOEING 737-300 SRM 51-40-02-0 FIG 12.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,750 hrs · 26,526 cycles
MAJOR REPAIR. DURING C-13 CHECK, FOUND CRACK ON STRINGER 18A AT STATION 727 ON THE RT SIDE. MAINTENANCE REMOVED CRACK ON STRINGER 18A AT STATION 727 ON THE RT SIDE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (E.R.) NR 03-5361-05175-ES2. FORMED FILLER AND RADIUS FILLER IAW AWA ER 03-5361-057175. INSTALLED FABRICATED REPAIR PARTS IN ADDITION TO REPAIR GUSSET AND ORIGINAL ANGLE IAW AWA ER NO 03-5361-05175-ES2.
Part: SKIN — DEBONDED (NR 3 SLAT) · airframe 597,500 hrs · 36,526 cycles
DURING C-13 CHECK DISCOVERED DISBONDED AREA LOCATED AT TOP OF NR 3 SLAT WEDGE INBOARD END FROM SS 12.25 TO SS 16.25. MX REMOVED DISBONDED AREA AT TOP OF NR 3 SLAT WEDGE INBOARD END FROM SS 12.25 TO SS 16.25 IAW BOEING 737-300 SRM 51-70-10 FIG 16. FABRICATED REPAIR CORE AND REPAIR DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED FABRICATED REPAIR CORE AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-0 FIG 16.
Part: SKIN — DELAMINATED (TE FLAPS) · airframe 59,750 hrs · 36,526 cycles
FOUND DISBOND AREA AT OUTBOARD END OF RT INBOARD AFT FLAP UPPER AND LOWER SURFACE. MAINTENANCE REMOVED DAMAGED AREA ON OUTBOARD END OF RT INBOARD AFT FLAP AND FABRICATED REPAIR DOUBLER AND REPAIR CORE IAW BOEING 737-300 SRM 51-70-10-0 FIG 16. BONDED FABRICATED REPAIR PARTS TO THE OUTBOARD END OF THE RT INBOARD AFT FLAP IAW BOEING 737-300 SRM 51-70-10-0, REPAIR 7, FIG 16.
Part: SKIN — DEBONDED (ZONE 500) · airframe 59,750 hrs · 36,526 cycles
MCN - MAJOR REPAIR - DURING C-13 CHECK FOUND DISBONDED AREA ON UPPER SURFACE OF THE LT INBOARD AFT FLAP 3.0 INCH FROM INBOARD END AT WBL 73 TO WBL 79. MAINTENANCE REMOVED DAMAGED AREA FROM UPPER SURFACE OF THE LT INBOARD AFT FLAP 3.0 INCH FROM INBOARD END AT WBL 73 TO WBL 79 AND CLEANED REPAIR AREA IAW BOEING 737-300 SRM 51-70-10-0 FIG 31. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 57-53-02 FIG 1. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-300 SRM 51-70-10-0.
2004
Part: WIRE — BROKEN (SEAT ROW 2 LT) · airframe 58,116 hrs · 35,574 cycles
PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL CHECK OF EMERGENCY LIGHTING FOUND THE EMERGENCY LIGHT AT SEAT ROW 2 LT INOPERATIVE, WIRES PULLED LOOSE FROM CONNECTORS. MAINTENANCE INSTALLED NEW WIRE HARNESS AT EMERGENCY LIGHT AT SEAT ROW 2 LT, OPERATIONAL CHECK WAS GOOD.
Part: SKIN — CORRODED (FUSELAGE) · airframe 57,131 hrs · 35,003 cycles
DURING 4-DAY CHECK CORROSION WAS FOUND ON SKIN AT AFT AIR PHONE ANTENNA UNDER AFT CARGO DOOR AT BS 794.6, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE CUTOUT DAMAGED SKIN AT AFT AIR PHONE ANTENNA BS 794.6, BETWEEN STR 27 LT AND STR 27 RT AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER, INSTALLED REPAIR PART IAW AWA ER 03-5331-04200-SS1.
Part: SKIN — CRACKED (NR 3 SLAT) · airframe 56,201 hrs · 34,501 cycles
LCQ - MAJOR REPAIR - DURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND BETWEEN TWO RIVET HOLES ON LOWER EDGE OF NR 3 SLAT WS 321.5. MAINTENANCE CUT OUT DAMAGE ON LOWER EDGE OF NR 3 SLAT AT WS 321.5; FABRICATED A FILLER & DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219.
Part: SKIN — CRACKED (NR 6 SLAT) · airframe 56,201 hrs · 34,501 cycles
LCQ - MAJOR REPAIR - DURING C-12 CHECK A 2 INCH CRACK WAS FOUND AT RIVET HOLE ALONG LOWER AFT EDGE OF NR 6 SLAT, SPAR STA 597. MAINTENANCE CUT OUT DAMAGE ON NR 6 SLAT AT SPAR STA 597; FABRICATED A FILLER & REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,201 hrs · 34,501 cycles
LCQ - MAJOR REPAIR - DURING C-12 CHECK A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN BELOW THE LT HORIZONTAL STABILIZER AFT OF ATTACH POINT AT BS 1138, STR 7 LT. MAINTENANCE REMOVED CRACKED SECTION OF SKIN BELOW THE LT HORIZONTAL STABILIZER AT BS 1138, STR 7 LT; FABRICATED A NEW REPLACEMENT SECTION OF SKIN PER DWG 65-48240; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1.
Part: VERTICAL BEAM — CRACKED (BULKHEAD) · airframe 56,201 hrs · 34,501 cycles
LCQ - MAJOR REPAIR - DURING C-12 CHECK .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE ON VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195. MAINTENANCE REMOVED VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,201 hrs · 34,501 cycles
LCQ - MAJOR REPAIR - DURING C-12 CHECK A .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE IN BS 178 BULKHEAD VERTICAL WEB BEAM RBL 5, WL 195. MAINTENANCE REMOVED CRACKED SECTION OF BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 5, WL 195; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1.
Part: FRAME — CRACKED (BULKHEAD) · airframe 56,201 hrs · 34,501 cycles
LCQ - MAJOR REPAIR - DURING C-12 CHECK A .75 INCH CRACK WAS FOUND IN RADIUS OF BS 178 BULKHEAD LT SIDE CHORD AT LBL 55, WL 207. MAINTENANCE REMOVED DAMAGED SECTION OF LT SIDE CHORD AT LBL 55, WL 207; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,201 hrs · 34,501 cycles
LCQ - MAJOR REPAIR - DURING C-12 CHECK A .75 INCH CRACK WAS FOUND ON INBOARD LOWER SIDE OF FUSELAGE FRAME AT BS 616, STR 17 LT. MAINTENANCE CUT OUT CRACKED FUSELAGE FRAME AT BS 616, STR 17 LT; FABRICATED A FILLER, DOUBLER & STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1.
Part: WIRE — BROKEN (SEAT ROW 10 LT) · airframe 55,873 hrs · 34,305 cycles
PHX - EEL - DURING 8-DAY CHECK FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 LT. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD.
2003
Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 55,441 hrs · 34,046 cycles
DURING TAKEOFF ROLL AT MSY EN ROUTE FOR PHX THE FIRST OFFICERS AIRSPEED INDICATOR FLAGGED MOMENTARILY, REJECTED TAKEOFF. RESET NO FURTHER EVENTS ON SUBSEQUENT TAKEOFF.
Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 54,835 hrs · 33,679 cycles
AS AIRCRAFT PULLED ON RUNWAY AT BUR FOR TAKEOFF FIRST OFFICERS AIRSPEED INDICATOR WAS FROZEN AT 315 KIAS, REJECTED TAKEOFF AND RETURNED TO GATE. CONTRACT MAINTENANCE INSPECTED AND RECYCLED THE FIRST OFFICERS AIRSPEED INDICATOR CIRCUIT BREAKER (C5) ON THE P6-1 PANEL, OPERATIONAL CHECK WAS GOOD.
Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 53,512 hrs · 32,898 cycles
DURING TAKEOFF AT BOI EN ROUTE FOR PHX HEARD LOUD POP ON LT SIDE OF AIRCRAFT, SUSPECTED COMPRESSOR STALL AND REJECTED TAKEOFF AT 90 KTS. BOISE MAINTENANCE PERFORMED INSPECTION OF THE NR 1 ENGINE IAW BMM 71-00-00 PG. 248 & 249, ENGINE RUN AT ALL PARAMETERS WAS GOOD.
2002
Part: FRAME — CRACKED · corrosion level 0 · airframe 53,074 hrs · 32,628 cycles
LCQ - MAJOR REPAIR - DURING C-11 CHECK A 1/2" CRACK WAS FOUND IN THE RADIUS OF FRAME ON THE FORWARD PRESSURE BULKHEAD BS 178, WL 207, RBL 28. MAINTENANCE REMOVED R/H FORWARD PRESSURE BULKHEAD WEB AND THE CRACKED R/H FORWARD PRESSURE BULKHEAD FRAME AT BS 178, WL 207, RBL 28; FABRICATED A NEW REPLACEMENT FRAME; AND INSTALLED REPAIR PART AND REMOVED R/H FORWARD PRESSURE BULKHEAD WEB IAW B737-300 SRM 51-40-02, FIG. 8, PG. 38.
Part: ANGLE — CRACKED · corrosion level 0 · airframe 53,074 hrs · 32,628 cycles
LCQ - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND ON THE UNDERSIDE RADIUS OF FLOOR BEAM SUPPORT ANGLE BS 540, BL "O". MAINTENANCE REMOVED CRACKED FLOOR BEAM SUPPORT ANGLE AT BS 540, BL "0"; FABRICATED A NEW REPLACEMENT FLOOR BEAM SUPPORT ANGLE; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 1-2.
Part: SKIN — CRACKED · corrosion level 0 · airframe 53,074 hrs · 32,628 cycles
LCQ - MAJOR REPAIR - DURING C-11 CHECK A 1/2" CRACK WAS FOUND ON LOWER AFT INNER SKIN OF L-1 DOOR ON INBOARD SIDE. MAINTENANCE REMOVED CRACKED ANGLE AND STOP DRILLED CRACK ON INNER SKIN; HFEC INSPECTION WAS ACCOMPLISHED TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR ANGLE AND REPAIR DOUBLER; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PG. 16-19, AND SRM 51-70-13, PG. 1-5.
Part: SKIN — CRACKED · corrosion level 0 · airframe 53,074 hrs · 32,628 cycles
LCQ - MAJOR REPAIR - DURING C-11 CHECK 2 CRACKS WERE FOUND ON THE R-1 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT BS 300. MAINTENANCE STOP DRILLED CRACKS ON R-1 DOOR EXTERNAL SKIN AT THE LOWER HINGE CUTOUT BS 300; PERFORMED HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW AWA E.R. 03-5241-02350-SS2.
Part: ANGLE — CRACKED · corrosion level 0 · airframe 53,074 hrs · 32,628 cycles
LCQ - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND AROUND FASTENER HOLE OF CABIN FLOOR SUPPORT ANGLE BETWEEN BS 500D AND BS 500E AT BL "0". MAINTENANCE REMOVED DAMAGE ON CABIN FLOOR SUPPORT ANGLE BETWEEN BS 500D AND BS 500E AT BL "0"; FABRICATED 3 EACH REPAIR ANGLES; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-30-51, PG. 103, AND SRM 51-30-01, PG. 12.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,074 hrs · 32,628 cycles
LCQ - MAJOR REPAIR - DURING C-11 CHECK EXFOLIATION CORROSION WAS FOUND AROUND 3 FASTENER HOLES ON FLOOR SUPPORT AT BS 995 - 1006, LBL 13. MAINTENANCE REMOVED THE DAMAGED FLOOR SUPPORT AT BS 995 - 1006, LBL 13; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 6.
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 52,305 hrs · 32,145 cycles
TUS - EMERGENCY EQUIPMENT - DURING INSPECTION THE 2 FORWARD GALLEY EMERGENCY FLASHLIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS IN THE 2 FORWARD GALLEY EMERGENCY FLASHLIGHTS, OPERATIONAL CHECK WAS GOOD.
Part: LIGHT — MISSING (SEAT ROW 9) · airframe 51,863 hrs · 31,842 cycles
FAA RAMP CHECK IDENTIFIED THE WHITE EMERGENCY LIGHT MISSING FROM SEAT ROW 9 LT. MAINTENANCE INSTALLED WHITE EMERGENCY LIGHT ON SEAT ROW 9 LT PER E.O. 33-50-37, AND DWG BR 2013-P-7373HP.
Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 51,628 hrs · 31,669 cycles
CLIMB-OUT A BURNT RUBBER SMELL WAS NOTICED BY THE F/A IN THE AFT GALLEY. RETURNED TO PHX & LANDED UNEVENTFULLY. PRIOR TO TAKEOFF ACFT HAD RETURNED TO GATE FOR THE SAME PROBLEM. DURING THIS EVENT MX HAD IDENTIFIED NR 2 COFFEEMAKER AS BEING VERY HOT & HAVING A BURNT ODOR, BOTH COFFEEMAKERS WERE REPLACED. THE SECOND EVENT (AIR TURNBACK) MX TROUBLESHOT FOR SMOKE OR FUMES FROM THE AIR CONDITIONING SYSTEM USING AMM 21-00-01, NO SMOKE OR FUMES WERE NOTED. AFT GALLEY WIRING WAS INSPECTED BEHIND BOTH COFFEEMAKERS AND IN THE OVERHEAD PANEL, MX ALSO INSPECTED THE SMOKE DETECTORS IN THE AFT LAVATORIES FINDING NO DEFECTS OR BURNING SMELL.
Part: WIRE HARNESS — DEFECTIVE (NR 2 ENGINE) · airframe 51,195 hrs · 31,381 cycles
AIR TURN BACK - FLT 0332 - AFTER T/O ENROUTE FROM OMA TO PHX, NR 2 ENGINE EGT FLUXUATED FULL SCALE FROM 0 TO 1250, RED LIGHT CAME ON AND DIGITS DISAPPEARED, FLUXUATED BACK TO 0 AND DIGITS DISAPPEARED AGAIN. IN LIGHT CHOP TO SMOOTH CONDITIONS EGT GAUGE FAILED INTERMITTENTLY THROUGH OUT RETURN TO OMA, EGT DID NOT RESPOND TO THROTTLE MOVEMENT, NR 1 ENGINE OPERATED NORMALLY. NOTE: AIRCRAFT EXPERIENCED NR 2 ENGINE EGT OVERTEMP IN LIGHT TO MODERATE TURBULANCE (5 SECONDS) ON PREVIOUS FLT INTO OMA (FLT 0512), MAINTENANCE REMOVED AND REPLACED 2 EACH WIRING HARNESSES IAW BMM 77-21-01-4 FOR THIS EVENT. (FLT 0332) MAINTENANCE PERFORMED 70 PERCENT POWER RUN, NR 2 EGT WENT FROM NORMAL TO 1250 DEGREES C TO 0 DEGREES C A
2001
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,446 hrs · 30,847 cycles
MCN - MAJOR REPAIR - C - CORROSION FOUND ON UPPER FLOORBEAM BS 986.5, LBL 45 TO RBL 45. REMOVED AND REPLACED ENTIRE UPPER T-CORD OF CORRODED FLOORBEAM AT BS 986.5, LBL 52 TO RBL 52 IAW AWA ER 03-5310-01334-JS2.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,446 hrs · 30,847 cycles
MCN - MAJOR REPAIR - C - LT WHEEL WELL UPPER PRESSURE WEB HAS 1.5 INCH CRACK AT BS 664, LBL 32. MAINTENANCE CUT OUT DAMAGED SECTION OF PRESSURE WEB AND PERFORMED HFEC INSPECTION FOR CRACKS, NO CRACKS NOTED. FABRICATED AND INSTALLED DOUBLER, FILLERS, AND STIFFENERS IAW B737-300 SRM 51-40-02.
Part: FRAME — CORRODED · corrosion level 2 · airframe 50,446 hrs · 30,847 cycles
MCN - MAJOR REPAIR - "C" - 4" X 1" AREA OF FUSELAGE FRAME AND 6" X 4" AREA OF FUSELAGE SKIN CORRODED AT BS 499, WL 158, LBL 2 TO RBL 2. MAINTENANCE REMOVED CORROSION ON SKIN AND FRAME AT BS 499, LBL 2 TO RBL 2 IAW B737-300 SRM 51-10-02, PG 19 & 20. SKIN WITHIN LIMITS IAW B737-300 SRM 530-00-01, PG 102-108, FRAME WAS OUT OF LIMITS IAW B737-300 SRM 53-00-07 PG 101-104. CUT OUT CORRODED SECTION OF FRAME; FABRICATED AND INSTALLED FILLER AND SUPPORT IAW B737-300 SRM 51-40-02 PG 2-4 AND SRM 53-00-07, 201 PG 210-212.
Part: FRAME — CRACKED (FUSELAGE) · airframe 50,446 hrs · 30,847 cycles
MCN - MAJOR REPAIR - C - FRAME HAS .5 INCH CRACK AT BS 500 NEAR UPPER FLANGE RBL 2 IN FORWARD CARGO COMPARTMENT AREA. MAINTENANCE CUT OUT CRACKED AREA OF FRAME AT BS 500 BETWEEN RBL 2 AND RBL 3, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW B737-300 SRM 51-70-11 PG 1, 2, 4, & 5, SRM 51-20-01 PG 10, & 47, AND SRM 51-20-01 PG 2-4.
Part: STRINGER — CRACKED · airframe 50,446 hrs · 30,847 cycles
MCN - MAJOR REPAIR - "C" - STR 16 L/H BS 504C HAS .5" CRACK, VISUALLY CONFIRMED BY 10X MAGIFICATION. MAINTENANCE CUT OUT CRACKED AREA ON STR 16 L/H BS 504C, FABRICATED A NEW CHANNEL AND INSTALLED IAW AWA ER 03-5312-01094-DD1.
Part: FRAME — DENTED · airframe 50,446 hrs · 30,847 cycles
MCN - MAJOR REPAIR - "C" - FRAME BS 787 UPPER FLANGE BETWEEN STR 24 AND 25 R/H SIDE DENTED OUT OF LIMITS PER B737-300 SRM 53-00-07, PG 101, 102, FIG 1. REMOVED DENTED PORTION OF FRAME AT BS 787 BETWEEN STR 24 AND 25 R/H SIDE IAW B737-300 SRM 51-70-11, PG 1-6, FIG 1.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,446 hrs · 30,847 cycles
MCN - MAJOR REPAIR - C - CORROSION FOUND ON INNER CHORD UNDER THRESHOLD DRAIN OF R2 DOOR. MAINTENANCE REMOVED CORROSION AND FOUND REMAINING MATERIAL TO BE OUT OF LIMITS IAW B737-300 SRM 51-40-02, PG 104-107. REMOVED AND REPLACED RT INNER CHORD FROM BS 917 TO 1016 IAW B737-300 SRM 51-40-02, PG 38 FIG 8, AND PG 10-11.
Part: WIRE — BROKEN (ROW 18) · airframe 48,105 hrs · 29,275 cycles
AFT SECTION OF EMERGENCY TRACK LIGHTING SYSTEM DOES NOT ILLUMINATE. FOUND BROKEN WIRE AT ROW 18; REPAIRED WIRE; EMERGENCY LIGHT OPS CHECK NORMAL.
2000
Part: SKIN — DENTED (HORIZONTAL STAB)
DENT ON LT HORIZONTAL STABILIZER LEADING EDGE AT APPROX STA 135. REPAIRED IAW ENG. REPAIR 03-5510-00356-552
Part: SKIN — DENTED (CARGO DOOR)
AFT CARGO DOOR EXT SKIN DENTED BEYOND LIMITS (A/Y = 23.8). FABED REPAIR OUTER SKIN AND REPLACED DAMAGED SKIN IAW SRM 52-30-01 FIG 202
Part: DOOR FRAME — CRACKED (FUSELAGE)
AFT CARGO DOOR FWD PAN HAS CRACKS AT SPRING PULLEY BRACKET ATTACHMENTS (AT PAN SPLICE). STOP DRILLED CRACKS; INSTALLED INTERNAL FORMED SECTION REPAIR AND AN EXTERNAL WEB REPAIR IAW SRM 51-70-11 AND 51-70-13
Part: SKIN PANEL — DENTED (FUSELAGE)
INSPECTION OF LOWER LOBE NOSE FUSELAGE FOUND DENT TO BE OUT OF LIMITS AT BS 211.8 STR 24R. REPAIRED IAW SRM 53-00-01, SKIN LAP JOINT REPAIR
Part: INTERCOSTAL — CRACKED (FUSELAGE)
DURING INSPECTION OF THE BS 178 BULKHEAD, FOUND ATTACHING INTERCOSTAL AT RBL 24 AND WL 195 ON THE AFT SIDE OF BULKHEAD TO BE CRACKED AT FLOOR BEAM ATTACHMENT FLANGE. CUTOUT DAMAGE AND INSTALLED REPAIR ANGLE IAW SRM 53-10-08 FIG 207
Part: FLOORBOARD — CORRODED (CABIN)
CORROSION AROUND AND BENEATH FASTENERS IN CREASE BEAM STA 727D STR 17R. REMOVED FLOORBOARD AND WEB, FABRICATED WEB AND INSTALLED IAW SRM 51-40-02 & 53-60-13 FIG 1.
Part: WIRE — EXPOSED (SEAT 1) · airframe 47,270 hrs · 28,758 cycles
NON ROUTINE LINE, FLOOR LIGHT AT SEAT 1C HAS EXPOSED WIRE. REMOVED AND REPLACED LIGHT ASSEMBLY.
Part: PANEL — LEAKING (LT WING) · airframe 46,428 hrs · 28,250 cycles
DIVERTED TO ELP DUE TO POSSIBLE FUEL LEAK ON TOP OF NR 1 ENGINE. ISOLATED LEAK TO UPPER PYLON FAIRING PANEL (5 FASTENERS AND DOME SEALED), LEAK CHECK GOOD.
1999
Part: SKIN — DELAMINATED (AILERON)
LOWER FLANGE OF LT AILERON FWD SPAR WAS DAMAGED IN 2 SPOTS, 1 AT I/B END AND 2 AT 24 FROM I/B END. REPAIRED LOWER FLANGE OF AILERON AS PER ER 03-5751-99306-EY1.
Part: FLOORBEAM — CORRODED (BS 344)
STA 344 BL 0 LIGHT CORROSION AT CLIP-NUT HOLE ON BOTTOM OF FLOORBEAM T CAP FLANGE. CORROSION REMOVED, MATERIAL LOSS IS BEYOND LIMITS. REPAIRED PER SRM 53-10-51 FIG 206.
Part: ANGLE — CRACKED (WS 537)
RT AILERON HINGE ATTACH FITTING ON WING, O/B SUPPORT LOWER ANGLE CRACKED AT 2ND I/B HINGE. FABRICATED AND INSTALLED NEW ATTACH ANGLE FITTING AS PER DWG NR 65-63461 AND SRM 51-10-02.
Part: CLIP — CRACKED (BS 616)
STR 3L CLEAT CRACKED AT FRAME STA 616. REPLACED CLIP PER SRM 51-40-02.
Part: WEB — CRACKED (BS 277)
WEB CRACKED AT STA 277 STR 14R. REPAIRED PER ER 03-5310-99309-EY1, FPI PER BOEING 20-20-02 PAINTED PER M/M 51-21-00.
Part: HINGE — CRACKED (RT AILERON)
RT AILERON FRONT SPAR LOWER FLANGE DELAMINATED, FIBER MISSING AT I/B HINGE AREA AT I/B END. ALSO, CRACKED AT 2ND I/B HINGE. REPAIRED PER ER 03-5751-99306-EYI.
1998
Part: WIRE — BROKEN (CABIN)
'D FLOOR TRACK EMERG LIGHT AT ROW 4 INOP. REPAIRED WIRE AT ROW 4 SYSTEM, OPS CHECK GOOD STC NR SA1889SO.
Part: LIGHT — INOPERATIVE (CABIN)
EMERGENCY TRACK LIGHT OUT AT ROW 14, RELEASED UNDER MEL33-19 CONTROL NUMBER 93666. REPLACED LIGHT ASSY, CK GOOD, MEL CLEARED.
1997
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED C-6 INSPECTION, FOUND POSSIBLE CRACK AT FASTENER AT BS 178, LBL 15, WL 184. REPAIRED BS 178 BULKHEAD LBL 15, WL 184, PER ER 3-53-12-21.
Part: SKIN — DENTED (BS 310)
DURING SCHEDULED C-6 INSPECTION, FOUND DENT IN SKIN BS 310 BETWEEN STRINGER 4 AND 5 LT. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED WET WITH SEAL AND APPLIED AERODYNAMIC SEALER IAW WITH ER-3-53-12-22. TCO-PAN-97-2205RR, 8110-3.
Part: CARRIAGE — CORRODED (NR 4 TE FLAP)
DURING SCHEDULED C-6 INSPECTION, FOUND L/W NR 4 MAIN CARRIAGE FORWARD O/B ROLLER BORE CORRODED. REMOVED AND REPLACED L/W NR 4 O/B CARRIAGE HALF PER MM 27-51-14.
Part: WIRE — BROKEN (CABIN)
DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP FROM ROW 11 TO 17. REPAIRED WIRE. STC - SA3140NM.
Part: WIRE — DISCONNECTED (CABIN)
DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP. REPAIRED WIRING AND INSTALLED LENS COVERS. STC - SA3140NM.
Part: FLASHLIGHT — INOPERATIVE (CABIN)
DURING ROUTINE MAINTENANCE CHECK, FOUND FWD I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FWD I/B FLASHLIGHT, OPS CHECK GOOD STC - SA3140NM.
1996
Part: BRAKE — LEAKING (LT MLG)
LT MAIN BRAKE WAS REPORTED TO BE SMOKING BY GROUND CONTROL. EMERGENCY DECLARED. FOUND NR 1 BRAKE LEAKING. REMOVED AND REPLACED BRAKE PER AWM 353.
Part: WIRE — BROKEN (CABIN)
PHX - FLT 2278 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTING INOP AT ROWS 13 AND 14. REPAIRED WIRING AS REQUIRED. OPS CHECK GOOD. (M)
Part: WIRE — TORN (CABIN)
PHX - FLT 2035 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR LIGHTING WIRE TORN FROM FLOOR. REPAIRED EMERGENCY FLOOR LIGHTING WIRES AND TRACK SYSTEM. OPS CHECK GOOD. (M)
Part: WIRE — BROKEN (CABIN)
PHX - FLT NR 1649 - PHX-SNA - CALL AT PUSH, FLOOR PROX EMERGENCY LIGHTS INOP. REPAIRED BROKEN WIRE, CHECKS GOOD. (M)
Part: FAN — FAILED (CABIN)
CMH/MCO - FLT 3105 - PILOT REPORTED NOISE AND SMOKE IN CABIN. FOUND A BAD RECIRCULATION FAN. REMOVED AND REPLACED RECIRCULATION FAN. OPS CHECK GOOD. (X)
Part: STOP PAD — JAMMED (R-1 DOOR)
TPA\CMH - FLT 3105 - R-2 ENTRY DOOR JAMMED CLOSED. FOUND DOOR STOP JAMMED BETWEEN LOWER DOOR LEAF AND THRESHOLD PLATE. REMOVED STOP PAD, DOOR OPERATES NORMALLY. (X)