N773AS

Part: HYDRAULIC SYSTEM — MALFUNCTIONED

APPROX 1200 FT, ACFT ROLLED RT AND PITCHED DOWN. AUTOPILOT WAS ENGAGED AT THE TIME AND FO WAS PF. ACFT WAS FULLY CONFIGURED FOR LANDING, PF DISCONNECTED A/P. PM (CAPT) COMPLETED CHECKLIST. "A" SYSTEM ENGINE HYD LOW PRESSURE LIGHT ILLUMINATED ON OVERHEAD HYD PANEL FOLLOWED BY THE "A" SYSTEM ELECTRIC HYD LOW PRESSURE LIGHT. HYD FLUID LEVELS ON THE FORWARD CENTER INSTRUMENT PANEL INDICATED "A" SYSTEM FLUID AT 2 PERCENT (B SYS NORMAL). ALL PRIOR INDICATIONS WERE NORMAL SO IT APPEARED TO BE A SUDDEN LOSS OF FLUID IN "A" SYSTEM.

Part: CONTROL VALVE — FAULTY (AC BAY)

DEPARTED AFTER PUTTING LT PACK ON DMI, AFTER T/O RT PACK KEPT TRIPPING OFF, ACFT HALFWAY TO DESTINATION DECIDED TO DIVERT, NO EMERGENCY DECLARED. AFTER T/S SYS FOUND THAT WHEN RT PACK WENT INTO HIGH THE PACK WOULD FALL OFF LINE INTERMITTENTLY, PERFORMED A PACK CONTROLLER INTEROGATION AND FOUND THAT THE TEMP CONTROL VALVE WAS AT FAULT. THE LT PACK HAD A CONTROLLER THAT WAS FAULTING ALSO.

Part: PROXIMITY SWITCH — OUT OF TOLERANCE (RT MLG)

AFTER T/O THE LANDING GEAR WOULD NOT GO UP. GEAR HANDLE WOULD NOT PASS THROUGH THE "OFF" POSITION. ACFT AIR RETURNED AND MX T/S FOUND GAP ON MLG SAFETY SENSOR (PROX SWITCH) TO TARGET EXCEEDING TOLERANCE.

Part: FRAME — CRACKED (BS 951) · airframe 56,161 hrs · 31,836 cycles

FUSELAGE PRODUCTION FASTENER HOLE CRACKED, BS 951 AND BOTTOM FASTENER HOLE ON STRINGER 17L. REPAIRED ON FASI WO 21067, NR 09399, 09400, 09401 AND 09408.

Part: STINGER — CRACKED (BS 960 S17L) · airframe 56,161 hrs · 31,836 cycles

LT SIDE OF FUSELAGE SKIN, BS 960 AND STRINGER 17L, CRACKED AT L2 DOOR CUTOUT FWD/LWR CORNER. REPAIRED ON FASI WO 21067, NR 09398.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,161 hrs · 31,836 cycles

AFT MAIN CABIN DECK AT BS 947.5, TOP CAP OF FLOORBEAM AT BL 0 HAS TOP SURFACE CORROSION. REPAIRED ON FASI WO 21067, NR 09178.

Part: BULKHEAD — CORRODED (BS 1016) · corrosion level 2 · airframe 56,161 hrs · 31,836 cycles

FWD SIDE OF BS 1016 AFT PRESSURE BULKHEAD HAS AREA OF CORROSION LBL2 TO RBL2 AT WL 191...REPAIRED ON FASI WO 21067, NR 09058.

Part: STIFFENER — CORRODED (BS 1016 BULKHEAD) · corrosion level 2 · airframe 56,161 hrs · 31,836 cycles

FOUND CORROSION ON BS 1016 BULKHEAD STIFFENER ANGLE AFT SIDE BETWEEN RBL 3 AND LBL 3. REPAIRED ON FASI WO 21067, NR 09301.

Part: FRAME — CRACKED (BS 601) · airframe 56,161 hrs · 31,836 cycles

LEFT FUSELAGE FRAME AT BS 601 IS CRACKED AT LWR FASTENER HOLE ON INBD FLANGE BELOW STRINGER 17L CREASE WEB. REPAIRED ON FASI WO 21067, NR 08996.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 56,161 hrs · 31,836 cycles

LEFT WING, INBD FORE FLAP HAS 2 EACH GOUGES ON INBD UPPER SURFACE. REPAIRED ON FASI W/O 21067, NR 09336.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 56,161 hrs · 31,836 cycles

LEFT WING INBD FORE FLAP HAS AREA DISBONDED ON UPPER SURFACE. REPAIRED ON FASI WO 21067 NR09335.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 56,161 hrs · 31,836 cycles

DENTED HORIZONTAL STAB STA 129.5. REPAIRED ON FASI W/O 21067, NR 09285.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED BS 520-695 RBL 24. REPAIRED ON FASI W/0 21067, NR 09193.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT STA 787-907 LBL 24. REPAIRED ON FASI W/O 21067 NR 09181.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT BS 460, RBL 24. REPAIRED ON FASI W/O 21067, NR 09083.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK RBL 45 BS 485-500G IS DAMAGED. REPAIRED ON FASI W/O 21067, NR 09194.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK AT LBL 24 FROM BS 375-500C IS DAMAGED. REPAIRED ON FASI W/O 21067, NR 09190.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT STA 727-727A, LBL 45. REPAIRED ON FASI W/O 21067, NR 09347.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT STA 727B-907, RBL 45. REPAIRED ON FASI W/O 21067, NR 09176.

Part: FRAME — CRACKED (ZONE 100) · airframe 56,161 hrs · 31,836 cycles

RT FUSELAGE FRAME AT BS 601 IS CRACKED AT LOWER FASTENER HOLE BELOW STR 17R. REPAIRED ON FASI W/O 21067, NR 08995.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT BS 520-695 LBL.45. REPAIRED ON FASI W/O 21067, NR 09189.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT STA 710, LBL 45. REPAIRED ON FASI W/O 21067, NR 09174.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED STA 727C- 907, LBL45

Part: SEAT TRACK — DAMAGED · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT STA 684, RBL 24. REPAIRED ON FASI W/O 21067, NR 09222.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 56,161 hrs · 31,836 cycles

CORROSION AT STA 747 AND STR 28R. REPAIRED ON FASI W/O 21067.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 56,161 hrs · 31,836 cycles

SEAT TRACK DAMAGED AT STA 500C-660 LBL 24. REPAIRED ON FASI W/O 21067 NR 09191.

Part: FIRE LOOP — FALSE ACTIVATION (ZONE 100) · airframe 55,214 hrs · 31,338 cycles

ON FINAL APPROACH, STARTED THE APU. THE APU FIRE WARNING LIGHT AND BELL ACTIVATED. PROCEEDED WITH THE APU FIRE IMMEDIATE ACTION ITEMS. THE FIRE WARNING LIGHT EXTINGUISHED. COMPLETED THE APU NON-NORMAL CHECKLIST AND NOTIFIED THE TOWER. REQUESTED A FIRE TRUCK COME AND INSPECT THE AIRPLANE FOR SMOKE AND HEAT. THE FIRE TRUCK DID NOT NOTE ANY PROBLEM SO WE CONTINUED TO PARKING. AFTER PASSENGERS DE-PLANNED, CALLED MX CONTROL. THEY INFORMED ME OF THE ACTIONS REQUIRED TO INSPECT AND DEFER THE APU. WITH APU DEFERRED, BOARDED PASSENGERS AND RETURNED TO DEPARTURE.

Part: DOOR — STUCK (MAIN PAX) · airframe 54,298 hrs · 30,553 cycles

L1 DOOR DIFFICULT TO CLOSE. REPLACED L I DOOR ASSY. ADJUSTMENT AND OPS TEST GOOD.

Part: SNUBBER — WORN (L1 DOOR) · airframe 52,430 hrs · 29,432 cycles

L1 DOOR VERY HEAVY AND HARD TO OPERATE. REMOVED AND REPLACED L1 DOOR SNUBBER, OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

MISS DRILLED HOLE SKIN STA 260. REPAIRED PER ASA EA 400 53EA 00474.

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

PREVIOUS FLUSH REPAIR AT BS 259 SPLICE AND STR 17L. REPAIRED PER ASA EA 400 53EA 00474.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

FUSELAGE SKIN DENT 4" AFT OF LT FUSELAGE SENSOR. REPAIRED PER ATS ER 08 4027 ASAS EA 400 53EA 00474.

Part: BUSHING — MIGRATED (RT PYLON) · airframe 52,113 hrs · 29,203 cycles

RT PYLON DIAGONAL BRACE AFT OB FUSE PIN BUSHING MIGRATED. R&R DIAGONAL BRACE.

Part: PLATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION FWD ENTRY DOOR UPPER HINGE LOWER GUIDE PLATE. REPLACED GUIDE PLATE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

CORROSION ON UPPER FLANGE OF INTERCOSTAL BETWEEN FRAMES AT BS 767 787 RBL 24. BLENDED CORROSION 1X2 .050" REMAINING THICKNESS. .000 REMAINING. OUT OF LIMITS R&R PER 51 40 02.

Part: TORQUE TUBE — GOUGED (PAX DOOR) · airframe 52,113 hrs · 29,203 cycles

FWD ENTRY DOOR FUSELAGE TORQUE TUBE IS GOUGED. R&R FWD ENTRY DOOR FUSELAGE TORQUE TUBE.

Part: THRESHOLD — DAMAGED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

FOUND MISDRILLED HOLE IN THRESHOLD WEB AND LOWER STRAP IN AFT CARGO BAY BS 845 RBL 23. R&R THRESHOLD WEB AND LOWER STRAP.

Part: THRESHOLD — DAMAGED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

FOUND MISDRILLED HOLE IN THRESHOLD WEB AND LOWER STRAP IN AFT CARGO BAY BS 845 RBL 23. R&R THRESHOLD WEB AND LOWER STRAP IN AFT CARGO.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,113 hrs · 29,203 cycles

NR 1 SLAT LWR SKIN CRACKED AT MIDDLE AUX TRACK 4 FASTENER HOLES. REPAIRED USING DOUBLER SPLICE PLATE AND FILLER.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

FWD ENTRY DOOR UPPER HINGE FITTING CRACKED. R&R HINGE FITTING.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

FORWARD ENTRY DOOR UPPER HINGE FITTING CRACKED. R&R HINGE FITTING.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 52,113 hrs · 29,203 cycles

AFT CARGO BAY FLOOR PANEL BS 772 TO 859 IS CORRODED. FABRICATED PANEL ALADINED AND PRIMED.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 52,113 hrs · 29,203 cycles

AFT CARGO BAY FLOOR PANEL BS 727E TO 727G IS CORRODED. FABRICATED FLOOR BOARD AT BS 727E TO 727G.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

FLOOR PANEL BS 775 857 AFT CARGO BAY HAS CORROSION. BLENDED CORROSION ON FLOOR PANEL BEYOND ACCEPTABLE LIMITS. R&R FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 52,113 hrs · 29,203 cycles

AFT CARGO BAY FLOOR PANEL BS 727+4 TO 727D IS CORRODED. REPLACED FLOOR PANEL.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON STRAP BS 794 RBL 25 WL 25. STRAP REPLACED PER SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

FOUND INTERCOSTAL BS 227.8 - 235.8 AT STR 19L, WL 201 CRACKED AT FWD HOLE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

FOUND INTERCOSTAL BS 227.8 235.8 STR 19L WL 201 CRACKED AT FWD HOLE. R&R INTERCOSTAL.

Part: ATTACH BRACKET — CORRODED (BS 794) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

INTERCOSTAL ATTACH BRACKET BS 794 RBL 6 WL 153 HAS CORROSION. R&R BRACKET.

Part: FRAME — CORRODED (BS 794) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FRAME BS 794.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FAILSAFE STRAP. REPLACED FAILSAFE STRAP.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FRAME BS 794. REPLACED BS 794 IN AFT CARGO BAY.

Part: DOUBLER — CORRODED (BS 794) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON INTERNAL DOUBLER ON FRAME BS 794 RBL 30 WL 160.

Part: FAILSAFE — CORRODED (BS 794) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FAILSAFE STRAP.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON INTERNAL DOUBLER ON FRAME STA 794 RBL 30 WL 160. R&R INTERNAL DOUBLER PER SRM 51 40 02.

Part: SKIN — DAMAGED (LWS 589) · airframe 52,113 hrs · 29,203 cycles

LT WING FIXED LE HAS FIBER DAMAGE AT NR 1 SLAT I/B AUX TRACK CUTOUT.

Part: SKIN — DAMAGED (LT WING) · airframe 52,113 hrs · 29,203 cycles

LT WING FIXED LE HAS FIBER DAMAGE AT NR 1 SLAT IB AUX TRACK CUTOUT. REPAIRED LT WING FIXED LEADING FIBER DAMAGE AT NR 1 SLAT IB AUX TRACK CUTOUT.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 52,113 hrs · 29,203 cycles

NR 1 SLAT LWR SKIN CRACKED I/B AUX TRACK AND 4 EA FASTENER HOLES. REPAIRED USING DOUBLER SPLICE PLATE AND FILLER PER SRM 57-43-01 FIG 201

Part: FRAME — CORRODED (BS 727B) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FRAME AT BS 727B LBL 15 WL 155. REPAIRED FRAME PER SRM 53-00-07 REPAIR 4

Part: CARGO TRACK — CORRODED (BS 947.5-577) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON AFT CARGO TRACK BS 945 RT RBL 13. REPLACED AFT CARGO BAY FLOOR TIE DOWN TRACK FROM BS 847 945 RBL 13.

Part: STRAP — CRACKED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

E BAY FLOORBEAM TENSION STRAP IS CRACKED BS 344 BL 0 STOPPED DRILLED CRACK AND ACCOMPLISHED REPAIR 4 PER SRM 53 10 51.

Part: FRAME — ELONGATED (BS 727F) · airframe 52,113 hrs · 29,203 cycles

AFT CARGO FRAME HAS 1 EA ELONGATED HOLE BS 727F LBL 22 MARKED. REPLACED BS 727F FRAME PER SRM 51-70-11, 51-30-01, 51-20-01 & 51-40-02.

Part: FRAME — DAMAGED (BS 767F) · airframe 52,113 hrs · 29,203 cycles

AFT CARGO FRAME HAS 1 EA ELONGATED HOLE BS 767F LBL 28 MARKED. REPLACED BS 767F FRAME PER SRM 51-70-11, 51-30-01, 51-20-01, 51-40-02.

Part: FRAME — DAMAGED (BS 787F) · airframe 52,113 hrs · 29,203 cycles

AFT CARGO FRAME HAS 1 EA ELONGATED HOLE BS 787F LBL 22 MARKED. REPLACED BS 787F FRAME PER SRM 51-70-11, 51-30-01, 51-20-01, 51-40-02.

Part: FLOORBEAM — CORRODED (BS 795) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON AFT CARGO FLOOR BEAM. BS 795 RBL 15 RBL 19 LOWER SURFACE AT NUTPLATE HOLE. R&R SUPPORT CLIP PER SRM.

Part: INTERCOSTAL — CORRODED (BS 787-795) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON INTERCOSTAL WEB BETWEEN FRAMES AT BS 787-795 RBL 24. R&R INTERCOSTAL.

Part: SHEAR WEB — CORRODED (BS 787-794) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

WHILE WORKING CARD 5140578 FOUND SHEAR WEB CORRODED. STA. 787-794 WL 156 RBL 25 REPLACED

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON AFT CARGO TRACK BS 945 LBL 13. R&R CARGO TRACK.

Part: SUPPORT — CORRODED (BS 867-947) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 867 947 RBL 25

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPLACE FLOOR TO SIDEWALL SUPPORT PER SRM 53-60-53 FIG 201.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT. BS 867 947 RBL 25. R&R FLOOR TO SIDEWALL SUPPORT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON SHEAR TIE AT BS 927-947 RBL 17. REMOVED AND REPLACED INTERCOSTAL.

Part: SUPPORT — CORRODED (BS 727B) · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPLACED SUPPORT PLATE PERRM 53-60-53 FIG 201.

Part: CARGO TRACK — DAMAGED (CARGO BAY) · airframe 52,113 hrs · 29,203 cycles

MECHANICAL DAMAGE DOUBLE HOLES ON CARGO TIE DOWN STRAP.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON INTERCOSTAL UPPER FLANGE BETWEEN FRAME AT BS 767 TO 787 RBL 24. R&R INTERCOSTAL BS 767 787 RBL 24.

Part: SUPPORT — CORRODED (BS 727E-837) · airframe 52,113 hrs · 29,203 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPLACE SUPPORT PLATE PER SRM 53-60-53.

Part: INTERCOSTAL — CORRODED (BS 747-767) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON INTERCOSTAL BETWEEN FRAMES BS 747 TO BS 767 RBL 24. REPLACED INTERCOSTAL.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON LOWER SUPPORT STRAP BS 782 800 RBL 25 WL 155. LOWER SUPPORT STRAP WILL BE REPLACED ON CARD 5140637.

Part: STRAP — CORRODED (BS 830-846) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

FOUND CORROSION ON LOWER STRAP BS 830-846 RBL 25. R&R STRAP.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON RT FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY RBL 25 BS 727+4 BS 767 OUT OF LIMITS. REPLACED RT FLOOR TO SIDEWALL SUPPORT PER SRM 53 60 53 REPAIR 5.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON AFT CARGO LOWER BULKHEAD SUPPORT RBL 12 (OUT OF LIMITS). FABRICATED AND INSTALLED NEW BULKHEAD SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

CORROSION ON RT FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY RBL 25 BS 727+4-767. REPLACED RT FLOOR TO SIDEWALL SUPPORT PER SRM 53-60-53.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,113 hrs · 29,203 cycles

AFT CARGO COMPARTMENT CORROSION FOUND ON STRUCTURE BENEATH FLOOR PANEL AT CARGO DOOR LOWER THRESHOLD SILL AREA. R&R CARGO TIEDOWN TRACK BS 777 877 RBL 13 SRM 53 00 53.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 51,847 hrs · 29,069 cycles

L1 DOOR DOES NOT CLOSE. ADJUSTED GUIDE ARM ONE FLAT TO PARALLEL DOOR CLOSING. OPS CHECK NORMAL REF 52 11 21.

Part: SKIN — DENTED (RT FORE FLAP) · airframe 49,343 hrs · 27,770 cycles

RT WING INBOARD AFT FORE FLAP DENTED ON LOWER SURFACE IN 2 EACH PLACES 28" AND 29" FROM INBOARD END AND 6" FROM TRAILING EDGE. PREPARED AREA FOR REPAIR: FABRICATED REPAIR PARTS AND BONDED IAW B737 400 51 70 4 REPAIR 4.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 49,343 hrs · 27,770 cycles

LT MLG INNER GEAR DOOR AFT EDGE CRACKED PREPARED DAMAGED AREA APPLIED SEVERAL LAYERS OF BMS 3 FIBERGLASS CLOTH AND BONDED IN ACCORDANCE WITH B737 400 SRM 52 80 02 REPAIR 2 AND 52 40 02 PG 203.

Part: SKIN — DAMAGED (RT AILERON) · airframe 49,343 hrs · 27,770 cycles

RT AILERON LWR SURFACE SMALL AREA OF COMPOSITE SKIN DAMAGE AT O/B TAB ATTACH BEARING AREA PREPARED DAMAGED AREA WET LAY UP IAW 737 400 SRM 51 70 17 AND BONDED IAW B737 400 SRM 51 70 17 REPAIR 1 AND ASA EA 5760 01072 WEIGHT AND BALANCE ACCOMPLISHED ON MIG 5 NR 5085463.

Part: SKIN — DENTED (TE FLAPS) · airframe 49,343 hrs · 27,770 cycles

LT INBOARD AFT FORE FLAP LWR SURFACE CLUSTER OF DENTS BEHIND NR 1 TIRE PREPARED AREA OF DENT DAMAGE. FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 49,343 hrs · 27,770 cycles

LT INBOARD AFT FORE FLAP DENTED 11" FROM O B AND 3" FROM T/E ON UPPER SURFACE PREPARED DAMAGED AREA. FABRICATED EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 49,343 hrs · 27,770 cycles

LT OUTBOARD T/E FLAP LWR SURFACE CLUSTER OF DENTS 2 INCHES TO 22 INCHES FROM INBOARD END AND 1 2" TO 8" FROM T/E. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAPS) · airframe 49,343 hrs · 27,770 cycles

LT INBOARD AFT FORE FLAP LWR SURFACE CLUSTER OF DENTS BEHIND NR 2 TIRE. PREPARED DAMAGED AREA, FABRICATED EXTERAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAPS) · airframe 49,343 hrs · 27,770 cycles

LT OUTBOARD AFT T/E FLAP DENTED ON UPPER SURFACE 68" FROM OUTBOARD B AND 1.5 INCH FROM T/E REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER PREPARED AREA AND BONDED IAW B737 400 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 49,343 hrs · 27,770 cycles

RT OUTBOARD AFT FLAP HAS AN AREA OF MULTIPLE DENTS ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 6 SPOILER) · airframe 49,343 hrs · 27,770 cycles

NR 6 SPOILER HAS MULTIPLE DENTS IN CENTER AREA OF LOWER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DELAMINATED (LT WING LE SLAT) · airframe 49,343 hrs · 27,770 cycles

LT WING NR 1 L E SLAT T/E WEDGE INBOARD FWD UPPER AND LOWER SURFACES DELAMINATED PREPARED AREA FOR REPAIR. REMOVED DAMAGED CORE, FABRICATED REPAIR CORE, REPAIR SKIN DOUBLER INSTALLED AND BONDED IAW B737 400 SRM 57 43 02 FIG 1 AND 51 70 10.

Part: SKIN — DAMAGED (LT LE STABLIZER) · airframe 47,189 hrs · 26,612 cycles

DAMAGE TO LEFT LEADING EDGE HORIZ STAB. REMOVED L/E AND ACCOPMLISHED REPAIR IAW SRM 55-10-01 REPAIR 3.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 46,446 hrs · 26,190 cycles

FLIGHT ATTENDANT UNABLE TO CLOSE THE L1 DOOR. ADJUSTED L1 GUIDE ARM AND HORIZONTAL PUSHROD PER AMM 52-11-00 PG 501, 518.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 45,940 hrs · 25,874 cycles

RIGHT O/B AFT FLAP I/B END DISBONDING. RIGHT O/B AFT FLAP I/B END REPAIRED IAW EA 57 50 02309.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 45,940 hrs · 25,874 cycles

INBOARD CORNER FOUND DEBONDING ON THE RIGHT NR 6 SLAT. REPAIRED IAW SRM 51-70-10.

Part: SKIN — DEBONDED (NR 6 SLAT) · airframe 45,940 hrs · 25,874 cycles

IB CORNER FOUND DEBONDING ON THE RT NUMBER 6 SLAT. REPAIRED NR 6 SLAT PER SRM 51 70 10.

Part: FLOORBEAM — CORRODED (FS 947)

PAE - FOUND FLOORBEAM CORRODED. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED PER EA 5310-02515. (M)

Part: SILL — CRACKED (FS 947-996)

PAE - FOUND CORROSION AT AFT ENTRY DOOR MOPSILL BS 947-996, LBL 52, WL 208 AND CRACKED AT BS 994. REMOVED AND REPLACED AFT ENTRY MOPSILL PER B737-400 SRM 51-40-02. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AT AFT CARGO BAY ON SHEAR TIE. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED PER B737-400 SRM 53-00-07. (M)

Part: SILL — CORRODED (FS 947-996)

PAE - FOUND CORROSION AT AFT ENTRY DOOR MOPSILL BS 947-996, LBL 52, WL 208 AND CRACKED AT BS 994. REMOVED AND REPLACED AFT ENTRY MOPSILL PER B737-400 SRM 51-40-02. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

PAE - PREVIOUS REPAIR CRACKED AT FRAME. REMOVED AND REPLACED REPAIR ANGLES IAW EA. (K)

Part: SKIN — DENTED (FUSELAGE)

PAE - DENT IN FUSELAGE SKIN. REPAIRED SKIN IAW EA. (K)

Part: DOOR — SCRATCHED (FWD CARGO DOOR)

PAE - FWD CARGO DOOR LWR AFT SIDE FRAME IS SCRATCHED. REMOVED AND REPLACED FRAME IAW SRM. (K)

Part: SKIN — CORRODED (FUSELAGE)

PAE - CORROSION ON SKIN UNDER NR 2 DME ANTENNA. REMOVED AND REPLACED SKIN IAW SRM. (K)

Part: FRAME — GOUGED (FUSELAGE)

PAE-MECHANICAL DAMAGE TO FLOOR BEAM AT BSTA 312, LBL 11-54, WL 208. REMOVED AND REPLACED FLOOR BEAM UPPER CHORD AT BSTA 312, WL 208 IAW SRM. (K)

Part: FRAME — TOOL DAMAGE (FUSELAGE)

PAE- DRILL START ON FRAME AT BSTA 767, RBL 12, WL 154. REPAIRED FRAME IAW SRM. (K)

Part: FRAME — TOOL DAMAGE (FUSELAGE)

PAE - AFT CARGO BAY DRILL START ON FRAME UPPER FLANGE. REPAIRED FRAME IAW SRM. (K)

Part: SKIN — CORRODED (FS 580)

PAE - FOUND CORROSION ON SKIN UNDER NR 2 DME ANTENNA. REMOVED AND REPLACED SKIN PER SRM 51-40-02. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - FOUND FRAME CRACKED AT FORWARD ENTRY DOOR LOWER STOP PAD FITTING. REMOVED DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED NEW FRAME, FITTINGS, REPAIR PARTS, AND INSTALLED IAW ASA EA 5310-02518. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AROUND FASTENER AT BS 631, RBL 1, BETWEEN STRINGER 28 RT AND 28 LEFT. PERFORMED BUTT SPLICE STRAP REPAIR PER ASA EA 5310-02516. (M)

Part: REPAIR — CRACKED (FUSELAGE)

PAE - PREVIOUS REPAIR CRACKED AT FRAME. REMOVED AND REPLACED REPAIR ANGLES PER ASA EA 5310-02517. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

KEEL BEAM HAS CORROSION AT LT OB LWR EDGE. BLENDED CORROSION, MAX MATERIAL REMOVED .051, ORIGINAL THICKNESS .140. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW EA. (K)

Part: FRAME — SCRATCHED (CARGO DOOR)

PAE - FOUND SCRATCH IN FORWARD CARGO DOOR SIDE FRAME. REPLACED FRAME PER B737-400 SRM 51-40-02. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - FOUND DENT IN FUSELAGE SKIN. REPAIRED SKIN PER ASA EA 5330-02014. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - FOUND DENT IN FUSELAGE SKIN. REPLACED SKIN PER ASA EA 5330-02014. (M)

Part: FRAME — CHAFED (FS 794)

PAE - FOUND AFT CARGO DOOR LOWER FORWARD SIDE FRAME HAS MULTIPLE NICKS AND CHAFING FROM LOWER STOP CUTOUT TO LOWER EDGE OF DOOR. REMOVED AND REPLACED FRAME SECTION PER B737-400 SRM 51-40-02. (M)

Part: SKIN — CORRODED (FS 628)

PAE - FOUND CORROSION ON MOUNTING AREA AROUND MARKER BEACON. REMOVED AND REPLACED SKIN PANEL AT MARKER BEACON PER B737-400 SRM 51-40-02. (M)

Part: FITTING — CORRODED (FS 340)

PAE - FOUND FITTING CORRODED. REPLACED CORRODED FITTING PER B737-400 SRM 51-40-02. (M)

Part: ANGLE — CORRODED (FS 317)

PAE - FOUND Z-ANGLE CORRODED. REPLACED CORRODED Z-ANGLE PER B737-400 SRM 51-40-02. (M)

Part: ANGLE — CORRODED (FS 270)

PAE - FOUND CORROSION ON Z-ANGLE. REMOVED CORRODED Z-ANGLE, FABRICATED NEW Z-ANGLE AND INSTALLED PER B737-400 SRM 51-40-02. (M)

Part: FITTING — CORRODED (FS 313)

PAE - FOUND FITTING CORRODED. REPLACED CORRODED FITTING PER B737-400 SRM 51-40-02. (M)

Part: FRAME — CORRODED (FS 380)

PAE - FOUND CORROSION ON FRAME. REMOVED DAMAGED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR PARTS PER B737-400 SRM 53-00-07. (M)

Part: SEAT TRACK — CORRODED (FS 340-360)

PAE - FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER B737-400 SRM 51-40-52. (M)

Part: INTERCOSTAL — CORRODED (FS 270)

PAE - FOUND CORROSION ON INTERCOSTAL. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW AND INSTALLED PER B737-400 SRM 51-40-02. (M)

Part: WEB — CORRODED (FS 294-340)

PAE - FOUND CORROSION ON SUBTHRESHOLD WEB COMMON TO MOPSILL. REMOVED DAMAGED WEB, FABRICATED NEW WEB AND INSTALLED PER B737-400 SRM 51-40-02. (M)

Part: SILL — CORRODED (FS 320-339)

PAE - FOUND MOPSILL CORRODED. REPLACED MOPSILL PER B737-400 SRM 51-40-02. (M)

Part: FITTING — CORRODED (FS 313)

PAE - FOUND CORROSION ON FITTING. REMOVED AND REPLACED FITTING PER B737-400 SRM 51-40-02. (M)

Part: FITTING — CORRODED (FS 340)

PAE - FOUND CORROSION ON FITTING. REMOVED AND REPLACED FITTING PER B737-400 SRM 51-40-02. (M)

Part: SEAT TRACK — CORRODED (FS 340-360)

PAE - FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED CORRODED SEAT TRACK PER B737-400 SRM 53-00-52. (M)

Part: SILL — CORRODED (FS 294-340)

PAE - FOUND CORROSION ON MOPSILL. REMOVED AND REPLACED MOPSILL PER B737-400 SRM 51-40-52. (M)

Part: REVEAL — CRACKED (FS 328)

PAE - FOUND FORWARD SERVICE DOOR CUTOUT AFT LOWER SEAL DEPRESSOR IS CRACKED. REMOVED AND REPLACED PER B737-400 SRM 51-40-02. (M)

Part: SUPPORT ANGLE — CRACKED (FS 296)

PAE - FOUND CRACKED SUPPORT ANGLE. REPLACED SUPPORT ANGLE PER B737-400 SRM 51-40-02. (M)

Part: SILL — CORRODED (FS 320-339)

PAE - FOUND MOPSILL CORRODED. REPLACED MOPSILL PER B737-400 SRM 51-40-02. (M)

Part: ANGLE — CORRODED (FS 317)

PAE - FOUND CORROSION ON Z-ANGLE. REPLACED Z-ANGLE PER B737-400 SRM 51-40-02. (M)

Part: FRAME — CHAFED (FS 992)

PAE - FOUND FRAME CHAFED. REPAIRED FRAME PER B737-400 SRM 51-40-02. (M)

Part: FLOOR SUPPORT — CORRODED (FS 312)

PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT PER B737-400 SRM 51-40-02. (M)

Part: STRINGER CLIP — CRACKED (FS 500E)

PAE - FOUND BS 500E STRINGER 12AR AND 12BR STRINGER CLIPS CRACKED. REMOVED AND REPLACED STRINGER 12BR. STRINGER 12AR WAS NDI`D AND FOUND NOT TO BE CRACKED. (M)

Part: FLOORBEAM — GOUGED (FS 344)

PAE - FOUND CORRODED FLOORBEAM. REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED T-CHORD, REPAIR PARTS AND INSTALLED. (M)

Part: SUPPORT — CORRODED (FS 328-340)

PAE - FOUND CORROSION ON FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT IAW 737-400 SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FS 360)

PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGED UPPER CHORD, FABRICATED NEW UPPER CHORD, REPAIR PARTS AND INSTALLED IAW 737-400 SRM 53-00-51. (M)

Part: FLOORBEAM — CORRODED (FS 328)

PAE - FOUND CORROSION ON FLOORBEAM. REMOVED CORRODED UPPER CHORD, FABRICATED AND INSTALLED NEW CHORD, REPAIR SPLICES, AND ANGLES IAW 737-400 SRM 53-10-51. (M)

Part: WEB — GOUGED (FS 211.8)

PAE - FRAME GOUGED ON WEB. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW 737-400 SRM 51-70-03. (M)

Part: FRAME — CRACKED (FS 360)

PAE - FOUND FRAME CRACKED. REPAIRED FRAME IAW 737-400 SRM 53-00-07. (M)

Part: FLOORBEAM — DAMAGED (FS 294.5)

PAE - MECHANICAL DAMAGE TO FLOORBEAM. REMOVED AND REPLACED FLOORBEAM UPPER CHORD AT BS 294.5 IAW 737-400 SRM 53-10-81. (M)

Part: FLOORBEAM — CORRODED (FS 312)

PAE - FOUND CORROSION ON FLOORBEAM. REMOVED AND REPLACED FLOORBEAM UPPER CHORD AT BS 312 WL 208, LBL 65-23, IAW 737-400 SRM 53-10-51. (M)

Part: SILL — CORRODED (FS 947-996)

PAE - FOUND CORROSION ON MOPSILL. REMOVED AND REPLACED MOPSILL IAW 737-400 SRM 51-40-02. (M)

Part: ANGLE — CORRODED (FS 300-320)

PAE - FOUND CORROSION ON L-ANGLE AT BS 300-320, RBL 59, WL 208. REPLACED ANGLE PER B737-200 SRM 51-40-02. (M)

Part: SKIN — BIRD STRIKE (RT MIDFLAP)

DURING COMPLETION OF T/C 48357001 FOUND RT WING IB MIDFLAP LEADING EDGE SKIN DAMAGED BY BIRD STRIKE. SKIN DENTED 8 INCHES LONG X 4 INCHES WIDE AND 1.5 INCHES DEEP. SKIN WAS ALSO RIPPED APPROX 2 INCHES LONG. REPAIRED RT WING IB MIDFLAP LEADING EDGE IAW SRM. (K)

Part: SKIN — CORRODED (FUSELAGE)

OKC - FOUND AFT CARGO DOOR FORWARD INNER SURROUND SKIN IS CORRODED BETWEEN STRINGER 23R AND 26R FUSELAGE STATION 793. REMOVED CORRODED SKIN, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 51-40-5 AND 51-40-2. (M)

Part: SHEAR TIE — CORRODED (FS 500B)

OKC - FOUND CORROSION AT BS 500B STRINGER 26L-27L. REMOVED CORROSION AND REPAIRED SHEAR TIE AT BS 500B IAW B737-400 SRM 53-00-07 FIG 203. (M)

Part: SKIN — CHAFED (NR 4 SLAT)

OKC - FOUND NR 4 SLAT INBOARD LOWER SKIN T/E IS CHAFED TO THE COMPOSITE. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M)

Part: SHEAR TIE — CORRODED (FS 847)

OKC - BS 847 FRAME SHEAR TIE IS CORRODED BETWEEN STRINGER 27L AND 27R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR SHEAR TIE AND FLOOR SUPPORT CLIP IAW 737-400 SRM 53-00-7, 51-30-01, AND 51-40-1. (M)

Part: WEB — CORRODED (FS 440-492.4)

OKC - FOUND FORWARD PIT THRESHOLD ATTACH WEB HAS CORROSION AT FASTENER HOLES. REMOVED WEB, FABRICATED AND INSTALLED WEB IAW 737-400 SRM 51-40-05 AND 51-40-02. (M)

Part: SKIN — CHAFED (TE FLAP)

OKC - FOUND RIGHT INBOARD FORE FLAP UPPER SURFACE CHAFED. REPAIRED IAW 737-400 SRM 51-70-10 REPAIR. (M)

Part: SKIN — DELAMINATED (NR 2 SLAT)

FOUND NR 2 SLAT OUTBOARD T/E DELAMINATED. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — DENTED (FS 460)

OKC - FOUND DENT AT STATION 460 BETWEEN STRINGERS 26 AND 27 RIGHT, A=.750 Y=19.73. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW AAR EA 11020 AND ASA EA 5330-01954. (M)

Part: FRAME — CUT (FS 787)

OKC - FOUND FRAME DAMAGED ON UPPER LIP AT BS 787 BETWEEN STRINGER 25 AND 26 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-07 FIGURE 201. (M)

Part: THRESHOLD — CORRODED (FS 804-845)

OKC - FOUND AFT PIT DOOR THRESHOLD INNER WEB IS CORRODED. REMOVED WEB, FABRICATED AND INSTALLED WEB IAW 737-400 SRM 51-40-02. (M)

Part: SKIN — DELAMINATED (NR 2 SLAT)

OKC - FOUND NR 2 SLAT INBOARD T/E DELAMINATED AT CORNER. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400-SRM 51-70-10. (M)

Part: STRINGER — CORRODED (FS 500B)

OKC - FOUND CORROSION AT BS 500B STRINGER 26-27 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 53-00-07 FIG 203. (M)

Part: SKIN — DELAMINATED (TE FLAP)

OKC - FOUND RT OB AFT FLAP DELAMINATED AT IB AFT CORNER.

Part: FRAME — CORRODED (FS 727D)

OKC - FOUND FRAME AT BS 727D BETWEEN STRINGER 26 AND 27 LEFT ARE CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-07 FIGURE 208. (M)

Part: WEDGE — DENTED (TE FLAPS)

OKC - FOUND LEFT INBOARD MID FLAP T/E WEDGE HAS TWO EACH SHARP DENTS. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — CRACKED (NR 4 SLAT)

OKC - FOUND NR 4 SLAT, LOWER SURFACE OUTER SKIN CRACKED AT OUTBOARD END. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW 737-400 SRM 57-43-01 FIGURE 206. (M)

Part: BEAM — CRACKED (FS 685)

OKC - THE STUB BEAM 69-37253-10 WAS FOUND TO BE CRACKED AT UPPER CORNER OUTBOARD SIDE DURING 685 FRAME REPLACEMENT. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW BOEING FAILED REWORK RECORD DD2 UNDER BOEING REPAIR AGREEMENT NR 6-1171-RE-01389. (M)

Part: SKIN — DAMAGED (NR 2 SLAT)

OKC - FOUND NR 2 SLAT INBOARD UPPER CORNER DAMAGED. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED SKIN AND DOUBLER IAW 737-400 SRM 51-70-10. (M)

Part: SKIN — DELAMINATED (NR 4 SLAT)

OKC - FOUND NR 4 SLAT IS DELAMINATED ON T/E AT INBOARD END. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW B737-400 SRM 51-70-10 REPAIR 21. (M)

Part: FRAME — BROKEN (FS 685)

OKC - FOUND RIGHT FRAME BS 685 IS BROKEN ON THE LOWER FLANGE. REMOVED AND REPLACED FRAME ASSEMBLY IAW DWG INSTRUCTIONS 65C36758-41-6. (M)

Part: SHEAR TIE — CORRODED (FS 500B)

OKC - FOUND CORROSION AT BS 500B STRINGER 26L-27L. REMOVED CORROSION ON SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW B737-400 SRM 53-00-07 FIG 101 AND 203. (M)

Part: SKIN — DENTED (FS 370)

OKC - FOUND DENT IN FUSELAGE EXTERIOR SKIN BS 370 BELOW STRINGERS 17R. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR IAW 737-400 SRM 53-00-01 FIGURE 231. (M)

Part: FRAME — CORRODED (FS 500F)

OKC - FOUND FRAME AT BS 500F STRINGER 27-28 LEFT ARE CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 737-400 SRM 53-00-07 FIGURE 203. (M)

Part: SKIN — DENTED (FS 202.6-414.4)

OKC - RIGHT OUTBOARD FORE FLAP HAS 4 EACH DENTS ON UPPER AFT SURFACE. REPAIRED RIGHT OUTBOARD FORE FLAP UPPER SURFACE IAW 737-400 SRM 51-70-10 REPAIR 21. (M)

Part: FAILSAFE — CUT (FS 787)

OKC - FOUND CORROSION ON FAIL/SAFE CHORD STATION 787 AT STRINGER 26R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 737-400 SRM 51-70-11. (M)

Part: SKIN — PUNCTURED (FS 202.6-414.4)

OKC - FOUND RIGHT OUTBOARD AFT FLAP INBOARD END HAS A PUNCTURE IN THE LOWER SURFACE. REMOVED DAMAGE AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW B737-400 SRM 51-70-1 REPAIR 22. (M)

Part: FRAME — CORRODED (FUSELAGE)

FRAME AT STA 727D BETWEEN STR 26 AND 25L IS CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW SRM. (K)

Part: SLIDE — FAILED (R1 DOOR)

OKC - DURING HEAVY MX, R1 DOOR ESCAPE SLIDE OP-CHECK WAS ACCOMPLISHED ON 737-400. OPS CHECK OF THIS EES INCLUDED ARMING THE DOOR SLIDE AND OPENING THE DOOR. THE SLIDE COMPART OPENED AND THE SLIDE FELL, ACTIVATING THE INFLATION PROCESS PROPERLY. TE INFLATABLE BEGAN TO FILL, REACHING, BUT NO BREAKING THE FRANGIBLE LINKS. THE COMPRESSED GAS FLOWED UNTIL THE BOTTLE WAS EMPTY HOWEVER THE FRANGIBLE LINKS NEVER PARTED. THE SLIDE WAS NOT USEABLE AS AN EXIT ROUTE AND FAILED THE CHECK. DUE TO THE SIMILARITY OF THESE FAILURES, FEEL THE ROOT CAUSE OF THIS FAILURE WAS INGESTIONS OF BUBBLE WRAP INTO THE ASPIRATOR, STALLING INFLATION, PREVENTING THE FRANGIBLE LINKS FROM BREAKING AND RENDERING THE INFLATABLE UNUSABLE.

Part: SHEAR TIE — CORRODED (FUSLEAGE)

B-STA 847 FRAME SHEAR TIE IS CORRODED BETWEEN STRINGER 27L AND 27R. REMOVED CORROSION, FABRICATED REPAIR SHEAR TIE AND FLOOR SUPPORT CLIP, AND INSTALLED REPAIR PARTS IAW SRM. (K)

Part: SKIN — PUNCTURED (TE FLAP)

RT OB AFT FLAP IB END HAS A PUNCTURE IN THE LWR SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K)

Part: SKIN — DELAMINATED (TE FLAP)

RT OB AFT FLAP DELAMINATED AT IB AFT CORNER. REPAIRED IAW SRM. (K)

Part: SKIN — CORRODED (FUSELAGE)

AFT CARGO DOOR FWD INNER SURROUND SKIN IS CORRODED BETWEEN STRINGER 23R AND 26R, FS 793. REMOVED CORRODED SKIN, FABRICATED AND INSTALLED IAW SRM. (K)

Part: SKIN — DENTED (RT TE FLAP)

RT OB FORE FLAP HAS 4 EACH DENTS ON UPPER AFT SURFACE. REPAIRED RT OB FORE FLAP UPPER SURFACE IAW SRM. (K)

Part: SKIN — DELAMINATED (NR 2 SLAT)

NR 2 SLAT IB T/E DELAMINATED AT CORNER. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K)

Part: SKIN — DELAMINATED (NR 2 SLAT)

NR 2 SLAT OB T/E DELAMINATED AT CORNER. REMOVED DAMAGE, FABRICATED SKIN AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM. (K)

Part: SKIN — CHAFED (TE FLAP)

RT IB FORE UPPER SURFACE CHAFED. REPAIRED IAW SRM. (K)

Part: SKIN — CRACKED (NR 4 SLAT)

NR 4 SLAT LOWER SURFACE OUTER SKIN CRACKED AT OB END. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM. (K)

Part: RIB — CRACKED (LT WING)

GYR - FOUND LEFT WING INTERNAL RIB AT STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOWER CHORD PER THE BOEING 737-57-1186 SERVICE BULLETIN. (M)

Part: ANGLE — CRACKED (NR 2 PYLON)

PAE - DURING C-CHECK, FOUND NR 2 PYLON OUTBOARD ATTACK ANGLE CRACKED. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR TO SIDEWALL SUPPORT AT BS 727 TO BS 767. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR SUPPORT BS 773 RBL 13 WL 152. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY. REPAIRED IAW SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT ANGLE. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT SHEAR TIE AT BS 787 RBL 18 AND WL 156. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON THRESHOLD STRAP AT BS 847-860 RBL 20 AND WL 155. REPAIRED IAW SRM. (M)

Part: BEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON THRESHOLD BEAM FROM BS 795-846 RBL 21 AND WL 153. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727F RBL 10 AND WL 159. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FS)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 767 RBL 13 AND WL 160. REPAIRED IAW SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND UPPER FLANGE OF INTERCOSTAL AT BS 867-877 WL 156 AND RBL 23 CORRODED. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON STRAP AT BS 839-859 WL 160 AND RBL 19. REPAIRED IAW SRM. (M)

Part: ANGLE — CRACKED (RT WING)

DURING C-CHECK, FOUND CRACKED INBOARD UPPER RIGHT WING TRAILING EDGE PANEL INBOARD SUPPORT ANGLE AFT END. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE BS 727E RBL 11 AND EL 159. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727D RBL 1 AND WL 159. REPAIRED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON DOOR FRAME CLOSE OUT WEB AT BS 847 WL 156 AND RBL 24. REPAIRED IAW SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND RT AC BAY RAM AIR INLET PLENUM ANGLE CRACKED. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSON ON SHEAR TIE BS 727F LBL 4 AND WL 158. REPAIRED IAW SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON UPPER FLANGE OF INTERCOSTAL AT BS 847-867 WL 156 AND RBL 22. REPAIRED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND WEB AT BS 847-867 WL 16 AN RBL 18 HAS CORROSION DAMAGE. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR SUPPORT BS 773 RBL 8 WL 152. REPAIRED IAW EA. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON RT KEELBEAM AT BS 500G PLUS 3. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE BS 727C RBL 9 AND WL 159. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE BS 727B RBL 11 AND WL 159. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON TOP FO FLOOR TO SIDEWALL SUPPORT BS 727 LBL 21. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE AT BS 727B RBL 1 AND WL 159. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE AT BS 727D LBL 2 AND WL 159. REPAIRED IAW SRM. (M)

Part: WEB — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR TO SIDEWALL WEB AT BS 847 TO 867. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE AT BS 727D RBL 8 AND WL 159. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT BASE OF SHEAR TIE BS 827 LBL 2 AND WL 158. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR TO SIDEWALL SUPPORT BS 747-767 RBL 21 TO WL 158. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT BASE OF THE SHEAR TIE AT BS 727B LBL 2 AND WL 159. REPAIRED IAW SRM. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON CARGO TIE DOWN FITTING. REPAIRED IAW SRM. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON NR 3 VHF ANTENNA CHANNEL. REPAIRED IAW SRM. (M)

Part: SUPPORT FITTING — CORRODED (FS)

PAE - DURING C-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM TO SIDEWALL SUPPORT AT BS 727E PLUS 8. REPAIRED IAW SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 727A 727B LBL 2 WL 159. REPAIRED IAW SRM. (M)

Part: STRAP — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON TOP OF FLOOR SUPPORT STRAP AT BS 772 LBL 21 AND RBL 21. REPAIRED IAW SRM. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON SUB THRESHOLD AT RBL 23 AND WL 155. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FRAME BS 500C RBL 5 AND WL 148. REPAIRED IAW SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT BS 727A-B AND RBL 3 WL 159. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FS)

PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 500D RBL 5 AND WL 148. REPAIRED IAW SRM. (M)

Part: ANCHOR — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT PIT FORWARD NET LEFT LOWER ANCHOR CRACKED. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727F BETWEEN STRINGER 25R AND 26R. REPAIRED IAW SRM. (M)

Part: FRAME — GOUGED (FUSELAGE)

DURING C-CHECK, FOUND GOUGE ON FRAME AT BS 727D RBL 14 AND W165. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 867 TO BS 487 RBL 21 AND WL 152. REPAIRED IAW SRM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727G BETWEEN STRINGER 25R AND 26R. REPAIRED IAW SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON FRAME BS 500B LBL5 RBL 5 AND WL 148. REPAIRED IAW SRM. (M)

Part: FRAME — DENTED (FUSELAGE)

PAE - DURING C-CHECK, FOUND DENTS ON RADIUS OF FRAME AT BS 847 RBL 21-22 WL 156. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FRAME AT BS 500E LBL 5, RBL 5 AND WL 148. REPAIRED IAW SRM. (M)

Part: MOUNT — CORRODED (ANTENNA)

PAE - FOUND CORROSION ON MOUNTING AREA AROUND MAKER BEACON ANTENNA AT BS 628, WL 148.5, BL 00. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)

Part: LIGHT — DISCONNECTED (CABIN)

ANC - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 10. RECONNECTED EMERGENCY FLOOR TRACK LIGHTING WIRE. OPERATIONS CHECK GOOD. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - BEFORE FLIGHT, FOUND EMERGENCY TRACK LIGHTS AT ROW 17-19 INOPERATIVE, WIRE DISCONNECTED. RECONNECTED WIRES. OPS CHECKED NORMAL. (M)

Part: WIRE — DISCONNECTED (ROW 17, 19) · airframe 26,044 hrs · 15,159 cycles

PDX-DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROWS 17 AND 19. DISCONNECTED WIRING. RECONNECTED WIRE, OPERATIONAL CHECK, NORMAL.

Part: SKIN — GOUGED (FUSELAGE)

PAE DURING MAINTENANCE S1 CHECK THE FUSELAGE SKIN AT STA 796 BETWEEN STR 19R AND 20R, WAS FOUND TO BE GOUGED. REPAIRED PER BFG ENGINEERING REPAIR 00-1101P1.

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 13 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND CONNECTOR, LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (CABIN)

SEA - PRIOR TO FLIGHT 727, THE L2 DOOR EXIT SIGN WAS FOUND BROKEN. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO FLT 256, THE FORWARD 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATAIVE. RECONNECTED WIRIGN AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (ROW 13) · corrosion level 3 · airframe 6,214 hrs · 3,538 cycles

PDX - DURING MAINTENANCE CHECK, 2 EACH EMERGENCY EXIT TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 13. REPLACED 2 EACH LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (X)

Part: LIGHTS — INOPERATIVE (ROW 1)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 1 WERE FOUND LOOSE AND INOPERATIVE. REPLACED WIRING, LIGHTS AND TRACK COVER IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — LOOSE (ROW 1)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 1 WERE FOUND LOOSE AND INOPERATIVE. REPLACED WIRING, LIGHTS AND TRACK COVER IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — FAILED (ROW 14)

SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT TRACK LIGHTS INOPERATIVE AT ROW 14. REPAIRED WIRING AND RELAMPED SEVERAL RECEPTICLE, LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 14)

LAX - PRIOR TO FLIGHT 137 - CREW REPORTED THAT THE EMERGENCY EXIT TRACK LIGHTS WERE INOPERATIVE AT ROW 14. RECONNECTED WIRING TO LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: OVEN — MALFUNCTIONED (GALLEY)

OAK - DURING FLT 528 - FLIGHT ATTENDANT REPORTED THAT ALL AFT GALLEY LIGHTS WERE FLICKERING AND AN ELECTRICAL ODOR WAS PRESENT. AIRCRAFT DIVERTED TO OAK FOR INSPECTION. MAINTENANCE COULD NOT DUPLICATE FLICKERING LIGHTS AND NO ELECTRICAL ODOR OR SMOKE WAS PRESENT. AS A PRECAUTIONARY MEASURE, MAINTENANCE PULLED AND COLLARED THE AFT GALLEY OVEN CIRCUIT BREAKERS AND DEFERRED AS PASSENGER CONVENIENCE ITEM. PDX MAINTENANCE RAN OVEN ON HIGH FOR 30 MINUTES AND FOUND A GREY/BLACK SMOKE COMING FROM BOTH SIDES OF THE DUAL BAY OVEN. REPLACED OVEN, OPERATED NORMALLY. THE OVEN WAS SUBSEQUENTLY ROUTED TO THE ALASKA AIRLINES AVIONICS SHOP IN SEA WHERE IT WAS CLEANED AND TESTED. UPON TESTING, THE OVEN OPERATED NORMALLY W

Part: BOTTLE — DISCHARGED (SLIDE)

SEA - DURING CREW TRAINING, THE AFT EVACUATION SLIDE FAILED TO FULLY DEPLOY, BOTTLE PRESSURE OBSERVED TO BE VERY LOW. BOTTLE PRESSURE BEFORE DEPLOYMENT READ OPERATIONAL. REMOVED AND REPLACED EVAC SLIDE BOTTLE AND REGULATOR. BOTTLE AND REGULATOR SENT TO AIR CRUISERS FOR EVALUATION AND REPAIR AS NECESSARY. BOTTLE WAS OVERHAULED AND HYDRO TESTED ON 3/4/98 BY AIR CRUISERS. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, 5 EACH EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 15. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, ALL 4 OVERWING EXIT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: SNAP RING — BROKEN (L1 DOOR)

ANC - FLT 66 - PRIOR TO PUSHBACK, THE CREW REPORTED THAT THE L1 DOOR GUST LOCK WOULD NOT DISENGAGE AND ALLOW DOOR TO CLOSE. REPLACED SNAP RING AT BOTTOM OF UPPER GUIDE HINGE SUPPORT ARM AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 15. RECONNECTED WIRING AND THE FLOOR TRACK LIGHTS OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L2 DOOR)

PDX - FLT 437 - CREW REPORTED, L2 SERVICE DOOR DIFFICULT TO OPEN. LUBED L2 SERVICE DOOR AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE, ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — BROKEN (CABIN)

OAK - FLT 445 - CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE KICKED OFF AT ROWS 15 AND 16. REPLACED LIGHT RECEPTACLE AND RECONNECTED WIRING AT ROW 15 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ROWS 15-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - FLIGHT 66 - PRIOR TO DEPARTURE, THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE AT THE AFT OVERWING EXIT AREA. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - FLT 106 - EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROW 15 (3 RED AND 2 WHITE). RECONNECTED WIRING TO LAMP SOCKETS AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 15. REMOVED AND REPLACED WIRING AT ROW 15 AND LIGHTS OPERATED NORMALLY. (M)

Part: TRACK LIGHT — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15-18. RECONNECTED TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: OPENING MECH — LACK OF LUBE (R-1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE R-1 DOOR, P/N 65458491, WOULD NOT OPEN ALL THE WAY. INSPECTED DOOR, FOUND ROLLERS ON CAM DRY. LUBED ROLLERS AND RODENDS. (M)

Part: SLIDE — FAILED TO DEPLOY (L-2 DOOR)

SEA - THE L-2 EMERGENCY EVACUATION ESCAPE SLIDE FAILED TO DEPLOY FULLY DURING TESTING. REPLACED SLIDE ASSEMBLY. THOROUGH INVESTIGATION AND FUNCTIONAL EVALUATION BY AIRCRUISERS COMPANY SHOWED NO ABNORMALITIES IN THE HARDWARE OR FUNCTIONING OF THE SLIDE. NO REASON FOR THE DEPLOYMENT PROBLEM COULD BE FOUND. (M)

Part: WIRE — DAMAGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15-17 WERE FOUND INOPERATIVE. REPLACED DAMAGED WIRE HARNESS AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 16. RECONNECTED WIRING AT ROW 16 AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS BETWEEN ROWS 14 AND 17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 14 AND LIGHTS OPERATED NORMALLY. (M)

Part: LINK — LACK OF LUBE (R1 DOOR HINGE)

SFL- FLT 113 - UNABLE TO OPEN R1 DOOR FROM OUTSIDE OF AIRCRAFT DURING CATERING. FOUND TOP DOOR HINGE TO BE DRY OF LUBRICANT; LUBED TOP HINGE AND DOOR OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE MID CABIN EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED WIRING CONNECTION IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M)

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)

SEA - FLT 385 - CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM OAK. USED OVERRIDE TO RETRACT GEAR. FOUND LATCH AND PRESS WARNING CIRCUIT BREAKER TRIPPED. RESET BREAKER. LANDED WITHOUT INCIDENT. PERFORMED MAIN GEAR EXTENSION/RETRACTION TEST AND UNABLE TO DUPLICATE PROBLEM. CYCLED GEAR SEVERAL TIMES AND OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

JNU - DURING CHECK, EMERGENCY TRACK LIGHTING WAS OUT AT ROW 11-14. MAINTENANCE RECONNECTED WIRE AT ROW 11. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING CHECK, FOUND LAST 5 FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE RECONNECTED LOOSE WIRING AND FUNCTION CHECKED NORMAL. (W)

Part: CONTROL CABLE — OUT OF ADJ (LANDING GEAR)

LAX - FLT 88 - ON ARRIVAL, CREW REPORTED ALL THREE RED INTRANSIT LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR EXTENSION DURING APPROACH. RECYCLED GEAR AND RED LIGHTS EXTINGUISHED NORMALLY WHEN GEAR WAS EXTENDED. LANDED WITHOUT INCIDENT. FOUND LANDING GEAR CONTROL CABLES OUT OF TOLERANCE. RERIGGED PER THE MM AND OPERATED NORMALLY. (W)

Part: EEL LAMP — INOP (CABIN)

LAX - DURING CHECK, THE EMERGENCY TRACK LIGHTS INTERMITTENTLY INOP. MAINTENANCE RELAMPED LIGHT AT ROW 2. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W)