N3759

Part: DOOR — CORRODED (311AL DOOR) · corrosion level 2 · airframe 74,224 hrs · 27,952 cycles

(LOG 0694120) SUSPECTED CORROSION ON AND ADJCENT TO THE 311AL DOOR DUE TO SUSPECTED HUMAN WASTE FROM LAV TANK VENT. ALL REPAIRS ACCOMPLISHED PER ER/A 622268-14.

Part: BRACKET — CORRODED (ACCESS DOOR 311) · corrosion level 2 · airframe 74,224 hrs · 27,952 cycles

(LOG 0692387) ACCESS DOOR 311AL HINGE BRACKET PN 65-54861-1 AND 65-54863-1 SHOW SIGNS OF CORROSION. REMOVED AND REPLACED HINGE BRACKETS PER ER/A 622268-14.

Part: BRACKET — CORRODED (ACCESS DOOR 311) · corrosion level 2 · airframe 74,224 hrs · 27,952 cycles

(LOG 0692361) ACCESS DOOR 311AL HINGE BRACKET PN 148A6140-6 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED HINGE BRACKET PER ER/A 622268-14.

Part: ACCESS DOOR — CORRODED (311AL) · corrosion level 2 · airframe 74,224 hrs · 27,952 cycles

(LOG 0692371) ACCESS DOOR 311AL ADAPTER ASSY PN 148A6121-7 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED DOOR ADAPTER PER ER/A 622268-14.

Part: DOOR — CORRODED (AFT FUSE SER DOO) · corrosion level 2 · airframe 74,224 hrs · 27,952 cycles

(LOG 0681341) WHILE IN MSP DURING A HYDRAULIC LEAK INVESTIGATION, THE 311AL AFT FUSELAGE SERVICE DOOR WAS FOUND WITH CORROSION ON THE DOOR AND DOOR SURROUND STRUCTURE. REPAIRED CORROSION DAMAGE PER ERA 622268-14 .

Part: TRIM SYSTEM — INOPERATIVE (ZONE 300) · airframe 73,809 hrs · 27,765 cycles

SHIP 3759 -ATB- RETURNED TO BOS DUE TO STABILIZER TRIM ELECTRICALLY INOPERATIVE. CORRECTIVE ACTION: REPLACED STAB TRIM CONTROL RELAY R64 AND STABILIZER TRIM MOTOR. OPS TEST NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,403 hrs · 26,231 cycles

SHIP 3759 -ATB- DUE TO RIGHT ENGINE FUEL BYPASS LIGHT. CORRECTIVE ACTION: PERFORMED OVERWEIGHT LANDING INSPECTION, INSPECTED FUEL FILTER WITH NO DEBRIS NOTED. R&R FFDPS AND NUMBER 1 , NUMBER 2 FUEL FILTERS. REFERENCE AMM 73-34-01 AND 73-11-

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,271 hrs · 26,168 cycles

(LOG 4680611) DURING EMERGENCY LIGHT TEST FOUND L ENTRY DOOR LOWER SIGN LIGHT INOP. FOUND BROKEN WIRE ON L LOWER EXIT SIGN ASSY. REPAIRED SAME PER B737. SPM 20. OPS CHECKS NORMAL.

Part: BATTERY PACK — INOPERATIVE · airframe 69,888 hrs · 26,006 cycles

(LOG 4816442) DURING INSPECTION FOUND AFT LEFT DOOR EMERGENCY LIGHTS OUT. R/R BATTERY FOR EMERGENCY LIGHTS IAW B737 AMM 33-51. OPS CHECK GOOD.

Part: MOTOR — INOPERATIVE (X) · airframe 69,656 hrs · 25,889 cycles

SHIP 3759 -MISC/DE- DUE TO FLAP LOCKOUT ON APPROACH. CORRECTIVE ACTION: REPLACED THE #3 FLAP TRANSMISSION AND SKEW SENSOR.

Part: BATTERY PACK — INOPERATIVE · airframe 68,398 hrs · 25,301 cycles

(LOG 8911413) DURING INSPECTION FOUND STATION 727A+8 EXIT LOCATOR SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1670 AT STATION 727C+13, WATER LINE 212 PER B737 AMM 33-51.

Part: BATTERY PACK — INOPERATIVE · airframe 68,398 hrs · 25,301 cycles

(LOG 8911400) DURING INSPECTION FOUND 4 EMERGENCY SIGNAL LIGHT INOP BY THE EXIT L/T FWD AND AFT WINDOW AND 1 R/T FWD/BOTTOM EXIT WINDOW LIGHT INOP. R/R L/T BOTTOM BATTERY PACK IAW B737 AMM 33-51. PERFORMED OPS CKS GOOD.

Part: NONE — NONE · airframe 67,904 hrs · 25,076 cycles

(LOG 2329877) DURING INSPECTION FOUND THICKNESS MEASUREMENT INSPECTION WAS ACCOMPLISHED ON HOUSING HANDLE AT FWD CARGO DOOR WITH A REMAINING THICKNESS=0.034 INCHES, THEREFORE IT IS OUT OF LIMITS. HOUSING HANDLE AT FWD CARGO DOOR WAS REPAIRED PER ER/A 600962-14.

Part: NONE — NONE · airframe 67,901 hrs · 25,075 cycles

(LOG 2329899) DURING INSPECTION FOUND WORN INNER /LOWER SURFACE ALSO AROUND ON HOLES TO ATTACH NUT PLATE STA 727 + 2.7 BTW LBL 23.0 TO RBL 16.0 AT FAIRING SUPPORT STRUCTURE. FAIRING SUPPORT STRUCTURE WAS REPAIRED PER ER/A 600887-14AD REV. ORIGINAL.

Part: NONE — NONE · airframe 67,913 hrs · 25,082 cycles

(LOG 2328866) DURING INSPECTION FOUND ENLOGATED HOLES ON FWD POSITION (4 EAS) ALSO ENLOGATED HOLES AFT POSITION (3EAS) AT ACCESS PANEL 194E. ACCESS PANEL 194E WAS REPAIRED PER B-737-800 S.R.M. 51-70-05-2R-8 PAR. 4. E. TO G. IN REFERENCE WITH B 737-800 S.R.M. 53-60-70-2R-1.

Part: NONE — NONE · airframe 67,904 hrs · 25,076 cycles

(LOG 2328601) DURING INSPECTION FOUND WEAR AT AFT BRACKET OF FAIRING FLAP SUPPORT #6 RH WING. AFT BRACKET OF FAIRING FLAP SUPPORT #6 RH WING WAS REPAIRED PER ER/A 600872-14 REV. ORIGINAL & PRI 600872-14 REV. 0.

Part: NONE — NONE · airframe 67,904 hrs · 25,076 cycles

(LOG 2329499) DURING INSPECTION FOUND WING-TO-BODY FAIRING STRUCTURE / SUPPORT FRAMES, STA. 727 +2.7 / WEAR. MAINTENANCE REPAIRED DAMAGE PER ERA 600887-14.

Part: NONE — NONE · airframe 67,901 hrs · 25,075 cycles

(LOG 2328871) DURING INSPECTION FOUND ENLOGATED HOLES ON FWD POSITION (3 EAS) ALSO ENLOGATED HOLES AFT POSITION (4 EAS) AT ACCESS PANEL 193D. ACCESS PANEL 193D WAS REPAIRED PER B737-800 SRM 51-70-05 -2R PROCEDURE 6 REPAIR 6 & B737-800 SRM 51-70-05-2R PROCEDURE 8 REPAIR 8.

Part: BATTERY PACK — INOPERATIVE · airframe 67,898 hrs · 25,074 cycles

(LOG 7682248) DURING INSPECTION FOUND RH FIRST CLASS EMX LIGHTS NOT WORKING. R/R RH FIRST CLASS EMX LIGHTS BATTERY PACK PER B737 AMM 33-55. OPS CHECK GOOD.

Part: WINDOW — LEAKING (X) · airframe 66,598 hrs · 24,480 cycles

SHIP 3759 -ATB- DUE TO LOUD AIR NOISE FROM THE AREA OF THE CAPTAIN'S SLIDING (L2) WINDOW. CORRECTIVE ACTION: PRESSURIZED AIRCRAFT TO LEAK CHECK. FOUND LEAK AT L2 WINDOW AND REPLACED SAME.

Part: BATTERY PACK — INOPERATIVE · airframe 66,598 hrs · 24,480 cycles

(LOG 8202947) DURING INSPECTION FOUND EMERGENCY LIGHTS INOP AT L1 ENTRY DOOR AND SEATS 10DEF TO 15DEF. REPLACED BATTERY FOR M1675 AND M1676 PER B737 AMM 33-51-06. OPS CHECKS GOOD.

Part: NONE — NONE · airframe 66,524 hrs · 24,444 cycles

(LOG 8202900) DURING INSPECTION FOUND ELECTRICAL ARC DAMAGE 3FT AFT OF L1 DOOR AT LAP JOINT -ARC CAUSED DUE TO POWER CORD INSTALLED UPSIDE DOWN + ENERGIZED AIRCRAFT ARCED TO AUTO LEVEL ARM ON JETWAY. MAINTENANCE REPAIRED DAMAGE PER ERA 596192-14.

Part: BATTERY — INOPERATIVE · airframe 66,509 hrs · 24,436 cycles

(LOG 8202902) DURING INSPECTION FOUND RT. SIDE AFT O/W LIGHT, SEAT ROWS 19-23 AND RT. O/W ESCAPE LIGHT INOP. REPLACED BATTERY FOR RT. SIDE O/W LIGHT, SEAT ROWS 19-23 AND RT. O/W ESCAPE LIGHT PER B737 AMM 33-51-06. OPS CKS GOOD.

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 65,700 hrs · 24,090 cycles

(LOG 1935999) DURING INSPECTION FOUND RMLG FORWARD TRUNION INBD LOWER FITTING CORRODED ON INNER FACE AT LOWER BUSHING. REPAIRED PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 65,700 hrs · 24,090 cycles

(LOG 1935997) DURING INSPECTION FOUND RMLG FORWARD TRUNION INBD UPPER FITTING CORRODED ON INNER FACE AT UPPER BUSHING. REPAIRED PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 65,700 hrs · 24,090 cycles

(LOG 1935994) DURING INSPECTION FOUND LMLG FORWARD TRUNNION INBOARD FITTING CORRODED ON INNER FACE AT UPPER BUSHING. REPAIRED PER B737 SRM 57-20-90.

Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 65,700 hrs · 24,090 cycles

(LOG 1935992) DURING INSPECTION FOUND LMLG FORWARD TRUNNION INBOARD FITTING CORRODED ON INNER FACE AT LOWER BUSHING. REPAIRED PER B737 SRM 57-20-90

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,108 hrs · 23,371 cycles

(LOG 6317366) DURING INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT O/W EXIT POSTION. REPLACED BATTERY PACK AT POSITION M1695 PER B737 AMM 33-51-06. EMERGENCY LIGHTS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ROW 13) · airframe 61,830 hrs · 22,249 cycles

(LOG 6938953) DURING INSPECTION FOUND ROW 13 ISLE EMERGENCY LIGHT INOPERATIVE. R/R ISLE EMERGENCY LIGHT FIXTURE AT ROW 13 IAW B737 AMM 33-51.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,997 hrs · 21,878 cycles

(LOG 6610414) DURING INSPECTION FOUND EMERGENCY EXIT LIGHT AT RIGHT SIDE FWD DOOR FLOOR LEVEL IS INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT ASSY. MFN BR9476G145-01 LIGHTS WORK GOOD.

Part: SKIN — CORRODED (BS 888-1060) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CORROSION ON OUTER FUSELAGE SKIN FROM STA 888 TO 1060 STR 4RH TO STR 4LH. REPAIR WAS PERFORMED ON OUTER FUSELAGE SKIN FROM STA 888 TO 1060 STR 4RH TO STR 4LH. PER ETI-37-19-309 REV. 2 AND ERA 580799-14.

Part: SUPPORT BRACKET — CORRODED (BS 1040) · corrosion level 2 · airframe 60,564 hrs · 21,653 cycles

(LOG 1238602) DURING INSPECTION FOUND CORROSION LEVEL 2. HINGE SUPPORT BRACKET AT AFT ACCESSORY DOOR (311AL) ON STA F.S 1040 BTW S16L TO S22L. REPLACED PER B737-800 SRM 51-40-02.

Part: FRAME — CRACKED (BS 500A) · airframe 60,564 hrs · 21,653 cycles

CRACK ON RH FRAME STA 500A BTW STRINGER 8 AND STRINGER 9 AT PAX CAB (RE-WRITE FROM NRC S/N 00276) REASON FOR RE-WRITE: ELONGATED HOLE ON REPAIR DOUBLER ON FRAME AT STA 500A BTW LONG 9 AND 8. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED ON RH FRAME STA 500A BTW STRINGER 8 AND STRINGER 9 AT PAX CAB PER ER/A 580270-14AD REV. ORIGINAL (1234460).

Part: CARGO TRACK — CORRODED (BS 727A-774) · corrosion level 2 · airframe 60,564 hrs · 21,653 cycles

SHIP 3759 AWR AFTER CORROSION REMOVAL IN CARGO TRACK TIE-DOWN STA 727A+ 15.5" AND STA 727A+17.5" AND BTW STA 771 AND STA 774 AREAS FOUND OUT LIMITS . CORRECTIVE ACTION: CORROSION LEVEL 2. TRACK TIE-DOWN STA 727A +15.5" AND STA 727A+17.5" AND BTW STA 771 AND STA 774 AREAS WAS REPAIRED PER B737-800 SRM 53-00-53 REP. 2 (1234629).

Part: FRAME — CRACKED (BS 297) · airframe 60,564 hrs · 21,653 cycles

CRACK ON FRAME AT STA 297 AND STA RBL 58 AT PAX CABIN (CPAX). THE FRAME WAS REPAIRED IAW SRM TEMPORARY REVISION 53-141 53-10-15 REP. 7 FIG 201.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 60,564 hrs · 21,653 cycles

THREE CRACKS FOUND ON THE RT HORIZONTAL STABILIZER LOWER SKIN, MID SECTION AT LE STA=140 APPROX (EHV).

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 60,564 hrs · 21,653 cycles

THREE CRACKS FOUND ON THE RH HORIZONTAL STABILIZER LOWER SKIN, MID SECTION AT LE STA 140 APPROX (EHV).

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION, CRACKED RIB ON RH HORIZONTAL STABILIZER STA. 92.70. (EHV). THE RIB WAS REPAIRED IAW SRM 55-10-09 REP 4 FIG 202 DETAIL A.

Part: FRAME — CRACKED (BS 867) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACK ON FRAME FROM STA 867 BTW S-8L TO S-9L AT PAX CABIN. FRAME WAS REPAIRED PER ERA 580270-14 AD REV ORIG.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 60,564 hrs · 21,653 cycles

(LOG 1231149) DURING INSPECTION FOUND CORROSION ON FLOOR BEAM STA 986, FROM RBL 64 TO LBL 64 AT PASSENGER COMPARTMENT. REPAIR WAS PERFORMED ON FLOOR BEAM STA 986, FROM RBL 64 TO LBL 64 AT PASSENGER COMPARTMENT W2 PER ETI-37-19-306 REV.1 AND ERA 580505-14 REV. ORIGINAL.

Part: FRAME — CRACKED (BS 380) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACK ON FRAME FROM STA 380 BTW S-8L TO S-9L AT PAX CABIN. FRAME WAS REPAIRED PER ERA 580270-14 AD REV ORIG.

Part: FRAME — CRACKED (BS 400) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACK ON RH FRAME STA 400 BTW STRINGER 8 AND STRINGER 9 AT PAX CAB. FRAME WAS REPAIRED PER ERA 580270-14 AD REV ORIG.

Part: FRAME — CRACKED (BS 400) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACK ON FRAME FROM STA 400 BTW S-8L TO S-9L AT PAX CABIN. FRAME WAS REPAIRED PER ERA 580270-14 AD REV ORIG.

Part: FRAME — CRACKED (BS 380) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACK ON FRAME BS 380 BETWEEN STRINGER 8R AND STRINGER 9R AT PAX CABIN. FRAME WAS REPAIRED PER ERA 580270-14 AD REV ORIG.

Part: FRAME — CRACKED (BS 500A) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACK ON FRAME FROM STA 500A BTW S-8L TO S-9L AT PAX CABIN. FRAME WAS REPAIRED PER ERA 580270-14 AD REV ORIG.

Part: FRAME — CRACKED (BS 727B) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACK ON FRAME FROM BS 727B BTW S-8L TO S-9L AT PAX CABIN. FRAME WAS REPAIRED PER ERA 580270-14 AD REV ORIG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION FOUND CRACKS ON VAPOR BARRIER STA 663.75 LBL 15.54 AND LBL 45.64, 8" UP FROM LOWER SKIN AT LH WHEEL WELL. REPAIR WAS PERFORMED ON VAPOR BARRIER STA 663.75 LBL 15.54 AND LBL 45.64, 8" UP FROM LOWER SKIN AT LH WHEEL WELL PER. B737-800 SRM 57-10-10.

Part: FLOOR SUPPORT — CORRODED (BS 951-967) · corrosion level 2 · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT RBL 50 BETWEEN BS 951 TO 967. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02 PAR 7, AND DWG 147A5660, REV B.

Part: WEDGE — DAMAGED (NR 5 SLAT) · airframe 60,564 hrs · 21,653 cycles

DURING INSPECTION, FOUND AWR WORN OUT OF LIMITS. WORN IN WEDGE AREA OUT LIMITS BTW SS 27.19 TO SS 32.19 AND SS 81.19 TO SS 93.19, 142.19 TO 144.19 AT SLAT NR 5. WEDGE AREAS OUT OF LIMITS BTW SS 27.19 TO SS 32.19 AND SS 81.19 TO SS 93.19, 142.19 TO 144.19 AT SLAT NR 5 WERE REPAIRED PER SRM 57-42-01, REPAIR 6.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 60,564 hrs · 21,653 cycles

(LOG 1219712) DURING INSPECTION FOUND CRACK ON INTERCOSTAL FROM STATION 344 TO STATION 360 BTW BL 0 AT PAX CABIN. INTERCOSTAL FROM STA 344 TO STA 360 BTW BL0 WAS REPLACED PER B737-800 SRM 53-10-51 IDENTIFICATION 2 FIG 4, SRM 51-40-02 PAR 7 AND DWG 141A5410 REV. B.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 60,564 hrs · 21,653 cycles

(LOG 1219555) DURING INSPECTION FOUND CRACKED INNER PRODUCTION DOUBLER ON EXTERNAL POWER RECEPTACLE FWD LWR CORNER AREA. REPAIR WAS PERFORMED AT INNER PRODUCTION DOUBLER (2 EAS) ON EXTERNAL POWER RECEPTACLE FWD LWR CORNER AREA. PER B737-800 SRM 53-10-15 REPAIR 5.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,061 hrs · 21,060 cycles

(LOG 5195502) DURING INSPECTION FOUND EXIT SIGN AT L1 DOOR MISSING. INSTALLED NEW LENS PER B737 AMM 33-51. OPS NORMAL.

Part: LENS — DAMAGED (CABIN) · airframe 57,024 hrs · 20,252 cycles

DURING INSPECTION FOUND EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. MAINTENANCE REINSTALLED LENS. OPS CK OK PER AMM 33-51.

Part: LENS — DAMAGED (CABIN) · airframe 57,024 hrs · 20,252 cycles

DURING INSPECTION FOUND EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. MAINTENANCE REINSTALLED LENS OP CKS OK PER AMM 33-51.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 55,699 hrs · 19,769 cycles

DURING INSPECTION, FOUND THE LT MAIN WHEEL WELL BULKHEAD CRACKED AT BS 663, LBL 32, 16 INCHES UP FROM LOWER SKIN. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A PERMANENT SEAL REPAIR IAW SRM 47-10-10.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 55,699 hrs · 19,769 cycles

DURING INSPECTION, FOUND THE RT MAIN WHEEL WELL. VERTICAL BULKHEAD WEB AT BS 663 HAS .5 INCH CRACK ABOUT 4 INCHES DOWN FROM W/W CEILING, JUST ABOVE DITCHING BALL. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, REPAIR 3.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 55,699 hrs · 19,769 cycles

DURING INSPECTION, FOUND THE LT MAIN WHEEL WELL. VERTICAL WEB AT BS 663 HAS A .5 INCH CRACK ABOUT 4 INCHES DOWN FROM THE W/W CEILING. JUST ABOVE DITCHING BALL. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, REPAIR 3.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 55,699 hrs · 19,769 cycles

DURING INSPECTION, FOUND THE FWD CARGO FLOOR PANEL 120DF CORRODED ON THE UNDERSIDE. MAINTENANCE FABRICATED A NEW FLOOR PANEL IAW SRM 51-40-05, & DRAWING 453A1610, SHEET 25, REV B.

Part: INTERCOSTAL — CORRODED (BS 907-927) · corrosion level 2 · airframe 55,699 hrs · 19,769 cycles

DURING INSPECTION, FOUND THE AFT CARGO BAY VACUUM WASTE AREA. INTERCOSTAL BETWEEN BS 907 - 927, STRINGER 23 - 24L CORRODED. MAINTENANCE FABRICATED AND INSTALLED A NEW INTERCOSTAL IAW IAW SRM 51-40-02, 51-40-05, & DWG 147A7401, SHT 9, REV B.

Part: FLOOR SUPPORT — CORRODED (BS 500H-500I) · corrosion level 2 · airframe 55,699 hrs · 19,769 cycles

DURING INSPECTION, FOUND THE FWD CARGO BAY FLOOR STRUCTURE BS 500H TO 500I, RT ZEE ANGLE HAS CORROSION. MAINTENANCE INSTALLED IAW SRM 51-40-02. OUT OUT OF LIMITS IAW SRM 53-00-53.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 53,151 hrs · 18,865 cycles

DURING INSPECTION FOUND 18 FED EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED LIGHT ASSY FOUND WIRE ON CIRCUIT BOARD UNSECURE. SECURED THE WIRE. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LENS — DETACHED (EXIT SIGN) · airframe 51,382 hrs · 18,280 cycles

DURING INSPECTION FOUND EXIT SIGN FELL OFF. MAINTENANCE REINSTALLED LENS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,523 hrs · 17,995 cycles

DURING TEST, FOUND RIGHT AFT EMERGENCY LIGHT INOPERATIVE, WONT TEST. MAINTENANCE R & R THE RIGHT AFT EMERGENCY LIGHT PACK ASSY BATTERY IAW AMM 33-51. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 44,345 hrs · 16,015 cycles

DURING INSPECTION, FOUND LT SIDE AFT EMERGENCY OVERWING LIGHT INOPERATIVE. MAINTENANCE R & R EMERGENCY OVERWING LIGHT IAW AMM 33-51-04.

Part: DOOR FRAME — DAMAGED (BS 787) · airframe 39,850 hrs · 14,472 cycles

DURING INSP FOUND AFT CARGO BAY BA 787 +6" AND 3" BELOW S-20R SCREW HOLE ELONGATED ON FWD DOOR FRAME. MX C/W PRI 518616-14, REV 0 AND ERA 518616-14, REV ORG.

Part: FLOORBEAM — CORRODED (BS 767) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 767 + 6" RBL 14" FLOORBEAM HAS CORROSION. MX REMOVED O/D PART AND INSTALLED NEW. WORK DONE IAW SRM 53-00-53.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 39,842 hrs · 14,467 cycles

DURING INSP, FOUND AFT CARGO BAY THRESHOLD HAS SEVERAL AREAS OF CORROSION. MX R & R THRESHOLD WITH NEW PN 146A5123-10, ATAG=27698. ALL WORK DONE IAW SRM 51-0-02, PG 39, FIG10, DWG 146A8123, ID 0006, REV C, SRM 51-40-05, PG 1, PAR 4AZ AND SRM 51-40-02, PG 3, PAR 5.

Part: FLOORBOARD — CORRODED (BS 887) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 887, FLOORBOARD SPLICE PLATE CORRODED. MX R & R AS REQ REF SRM 51-40-02, PG 1-9, AS REQ'D IAW AMM 51-21-91-620-802, SN 2220690.

Part: BRACKET — CRACKED (R2 DOOR SEAL) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND R2 DOOR LOWER SEAL BRACKET ATTACH ANGLES CRACKED. LOCATED AND DRILLED NEW BRACKETS IAW SRM 51-40-05. INSTALLED NEW BRACKETS ON R2 LOWER DOOR SEAL IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 867) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND CABIN SIDEWALL FRAME CRACKED S8R BS 867. MX REPAIRED FRAME IAW PRI ERA 517826-14AD, REV ORIGINAL, PRI ERA 517826-14AD, REV 1 AND FINAL ERA 517826-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 440) · airframe 39,842 hrs · 14,467 cycles

DURING INPECTION, FOUND CABIN SIDEWALL FRAME CRACKED S8L BS 440. MX REPAIRED FRAME IAW PRI ERA 517826-14AD, REV ORIGINAL, PRI ERA 517826-14AD, REV 1 AND FINAL ERA 517826-14AD REV ORIGINAL.

Part: FRAME — CRACKED (BS 440) · airframe 39,842 hrs · 14,467 cycles

DURING INSP, FOUND CABIN SIDEWALL FRAME CRACKED S8R BS 440. MX REPAIRED FRAME IAW PRI ERA 517826-14AD, REV ORIGINAL, PRI ERA 517826-14AD REV 1 AND FINAL ERA 517826-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 480) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND CABIN SIDEWALL FRAME CRACKED S8L BS 480. MX REPAIRED FRAME IAW PRI ERA 517826-14AD, REV ORIGINAL, PRI ERA 517826-14AD, REV 1 AND FINAL ERA 517826-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 500I) · airframe 39,842 hrs · 14,467 cycles

DURING INSP, FOUND CABIN SIDEWALL FRAME CRACKED S8R BS 500I. MX REPAIRED FRAME IAW PRI ERA 517826-14AD, REV ORIGINAL, PRI ERA 517826-14AD, REV 1 AND FINAL ERA 517826-14AD, REV ORIGINAL.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND FWD CARGO BAY DOOR THRESHOLD CORRODED BS 460 - 480. MX R & R THRESHOLD IAW SRM 51-40-02.

Part: SEAT TRACK — GOUGED (BS 519-521) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK, BS 519 -521, RBL 45, UPPER CROWN IS GOUGED. REPAIRED SEAT TRACK, 500H - 520, IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 519-521) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK, BS 519 - 521, LBL 22, UPPER CROWN GOUGED. MX REPAIRED SEAT TRACK BS 500H-520 IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B, RBL 24.75, SEAT TRACK INBD FLANGE FWD AND AFT FASTENER HOLES CRACKED. MX ACCOMPLISHED REPAIR IAW ERA 517840-14, REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B, LBL 45.50 SEAT TRACK INBD FLANGE FWD AND AFT FASTENER HOLES CRACKED. MX REPAIRED IAW ERA 517840-14, REV ORIGINAL.

Part: SPLICE PLATE — PUNCTURED (BS 500) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND FWD CARGO COMPARTMENT RT SPLICE PLATE AT BS 500+6 RBL 26 IS PUNCTURED. MX INSTALLED NEW SHIELD IN FORWARD PIT, RT STA 500A TO 500 IAW SRM 51-40-02, PG1, SRM 51-40-05.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B, LBL 45.50 SEAT TRACK OTBD FLANGE FWD AND AFT FASTENER HOLES CRACKED. MX ACCOMPLISHED REPAIR IAW ERA 517840-14, REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B, LBL 24.75 SEAT TRACK INBD FLANGE FWD AND AFT FASTENER CRACKED. MX ACCOMPLSIHED REPAIR IAW ERA 517840-14, REV ORIGINAL.

Part: SEAT TRACK — GOUGED (BS 519-521) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK, BS 519 -521, LBL 45, SEAT TRACK UPPER CROWN GOUGED. MX REPAIRED SEAT TRACK BS 500H -520, IAW SRM 53-00-52, REPAIR 4.

Part: PLATE — PUNCTURED (BS 500) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND FWD CARGO BAY RT SPLICE PLATE AT BS 500+6 RBL 26 IS PUNCTURED. MX REMOVED SHIELD LOCATED AND DRILLED NEW PART INSTALLED SHIELD IN FWD PIT RT BS 500 TO 500A IAW SRM 51-40-02, PG1, SRM 51-40-05, PG 1, PS 900-2, NR 04, PG 1-9.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B, RBL 45.50 SEAT TRACK INBD FLANGE FWD AND AFT FASTENER HOLES CRACKED. MX ACCOMPLISHED REPAIR IAW ERA 517840-14, REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B RBL 45.50 SEAT TRACK OTBD FLANGE, FWD AND AFT FASTENER HOLES CRACKED. MX ACCOMPLISHED REPAIR IAW ERA 517840-14, REV ORIGINAL.

Part: SEAT TRACK — GOUGED (BS 519-521) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK, BS 519-521, RBL 22, UPPER CROWN IS GOUGED. MX REPAIRED SEAT TRACK BS 500H -520, IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B, RBL 24.75, SEAT TRACK OTBD FLANGE FWD AND AFT FASTENER HOLES CRACKED. MX ACCOMPLISHED REPAIR IAW ERA 517870-14, REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND PASSENGER CABIN, JUST FWD OF BS 727B, LBL 24.75 SEAT TRACK OTBD FLANGE FWD AND AFT FASTENER HOLES CRACKED. MX ACCOMPLISHED REPAIR IAW ERA 517840-14, REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 767) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 767 + 6", RBL 3, FLOORBEAM CORRODED. MX REPAIRED FLOORBEAM IAW ERA 492969-14MA AND SRM 53-00-53, REPAIR 2.

Part: FLOORBEAM — CORRODED (BS 727I) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 727I + 5" LBL 12" FLOORBEAM HAS CORROSION. MX CUT OUT DAMAGED TOP FLANGE & REMOVED JOGGLES IAW ERA 492969-14MA, SH 2, STEP 1. FABRICATED CHANNEL SPLICE IAW ERA 492969-14MA, SH 2, STEP 1, 3 APPLIED ALODINE AND PRIMER IAW SRM 53-00-53. REPAIR 2, PG 205, STEP I AND J, INSTALLED IAW ER/A 492969-14MA.

Part: FLOORBEAM — CORRODED (BS 727I) · airframe 39,842 hrs · 14,467 cycles

DURING INSP, FOUND AFT CARGO BAY BS 727I + 5" LBL 8, FLOORBEAM HAS CORROSION. MX FABRICATED CHANNEL SPLICE IAW ERA 492969-14MA SH 2, STEP 1, 3. APPLIED ALODINE & PRIMER IAW SRM 53-00-53, REPAIR 2. INSTALLED CHANNEL SPLICE IAW ERA 492969-14MA.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND AFT CABIN FLOORBEAM BS 986.5, LBL 44, DOME NUT FASTENER HOLE CORRODED. MX REPAIRED FLOORBEAM IAW ERA 464 736-14MA AND SRM 51-40-02, AMM 20-60-07, AMM 53-11-01, PS 900-5-1 AND PS 900-2.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 39,842 hrs · 14,467 cycles

DURING INSPECTION, FOUND CABIN AFT WET AREA BS 986 HAS CORROSION ON FLOORBEAM TEE BELOW R2 DOOR. MX REPAIRED FLOORBEAM IAW ERA 46736-14MA AND SRM 51-40-02, PG 2 , AMM 20-60-07, PG 4-8 , AMM 53-11-01, PG 1-8 , PS-900-5-1 PG 4 , PS 900-2, PG 4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,852 hrs · 13,794 cycles

DURING INSPECTION, FOUND L1 DOOR AREA EMERGENCY EXIT SIGNS AND LIGHTING INOPERATIVE. MX REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW AMM 33-50. OPS CHECK OK.

Part: FITTING — CORRODED (LT WING) · airframe 32,810 hrs · 12,056 cycles

DURING TRIPLE GEAR CHANGE, EA 12-487906-12 REV A ME 03 OPN 0301 AND ME 06 OPN 0601 WAS WORKED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,382 hrs · 11,575 cycles

MAINTENANCE FOUND RIGHT OVERWING AND RIGHT GROUND EMERGENCY EGRESS LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY M1671, AND THE SYSTEM NOW CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,288 hrs · 10,859 cycles

EMERGENCY EGRESS LIGHTING INOPERATIVE AT R1 DOOR AND AISLE ROWS 1-4. MX REPLACED THE FWD POWER SUPPLY. SYS CHECKS OPS.

Part: SKIN — DENTED (BS 496 S-19R/20R) · airframe 12,325 hrs · 5,287 cycles

THE FUSELAGE SKIN AT BS 469 BETWEEN S-19R AND S-20R WAS DENTED AND GOUGED. DENT WAS APPROXIMATELY 1 INCH DIA. REPAIRED BY INSTALLING A DOULBER PER ER/A 452385-14.

Part: VALVE — FAILED (NR 2 ENG PRECOOL) · airframe 9,404 hrs · 4,154 cycles

AS POWER WAS SET FOR T/O RT BLEED TRIP OFF LIGHT ILLUMINATED, 20 KTS ABORTED T/O. ACCOMPLISHED NNC PROCEDURE. THERE WAS A SPLIT ON LT AND RT DUCT PRESSURE. AFTER RESET, BLEED OPENED AND LT AND RT DUCT PRESSURE RETURNED TO NORMAL. REMOVED AND REPLACED PRECOOLER VALVE. RAN ENGINE PER PFHB. MSG DID NOT RETURN.