N26210

Part: SLIDE — UNSECURE (ZONE 800) · airframe 82,214 hrs · 30,589 cycles

EXCESSIVE SLACK ON DOOR 1L ESCAPE SLIDE. REMOVED 1L. SLIDE AND ADJUSTED GIRT, THEN REINSTALLED SLIDE REF AMM 25-66-01. CW INSPECTION OF ESCAPE SLIDE IAW GMM 9-25-05.

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 81,957 hrs · 30,471 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK, EXTERIOR REAR RIGHT OVERWING EMERGENCY LIGHT AND RT GROUND ILLUMINATION EMERGENCY LIGHT INOPERATIVE IAW AMM 33-51-06. REPLACED THE FUSE FOR M1671. VERIFIED LIGHTS OPERATIONAL.

Part: LIGHT — DETACHED (ZONE 200) · airframe 81,899 hrs · 30,435 cycles

RED EMERGENCY LIGHT ON SEAT 20C FELL OFF. RESECURED 20C RED AISLE LIGHT IAW CMM 25-23-54, OPS CHECK GOOD.

Part: BULB — BURNED OUT (ZONE 200) · airframe 81,509 hrs · 30,245 cycles

FORWARD CARGO, AND EMERGENCY EXIT LIGHTS ANNUNCIATORS 1/2 ILLUMINATED. REMOVED FORWARD CARGO AND EMERGENCY EXIT LIGHTS ANNUNCIATORS REMOVED AND REPLACED BURNED OUT #387 LIGHT BULBS. OPS CHECK GOOD.

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 81,414 hrs · 30,205 cycles

20A OVERWING EMERGENCY EXIT LIGHT INOP 20A. DURING REMOVAL OF 20A SIDEWALL LIGHT ASSY, FOUND CONNECTOR FOR EMERGENCY LIGHT DISCONNECTED. RECONNECTED CONNECTOR. OPS CHECKED GOOD REF AMM 33-21-01.

Part: SKIN — CRACKED (ZONE 500) · airframe 81,409 hrs · 30,201 cycles

ON THE LH WING LOWER OUTBOARD SKIN PANEL EXTERNAL REPAIR LOCATED AT STRINGER L-9 AND WSTA 556, SKIN CRACK REPAIRED AT OTBD FASTENER OF STR 9. FLANGE. BETWEEN STA. 564.5 - STA. 537.5. PER ECRA: 5725-01165. ON THE LH WING LOWER OUTBOARD SKIN PANEL EXTERNAL REPAIR LOCATED AT STRINGER L-9 AND WSTA 556, ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF EC/RA 5725-01165 ON OR BEFORE 14 FEBRUARY 2027. TOMC APPROVED FOR DIP ?ON THE LH WING LOWER OUTBOARD SKIN PANEL EXTERNAL REPAIR LOCATED AT STRINGER L-9 AND WSTA 556,

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 80,452 hrs · 29,758 cycles

REMOVED R1 SLIDE PACK IAW B737 AMM 25-66-01 TO FOM REQUESTING CLEARANCE TO REINSTALL R1 SLIDE PACK CLEAR TO REINSTALL ORIGINAL DOOR R1 EMERGENCY ESCAPE SLIDE PACK PER GMM 09-25-05. INSTALLED R1 SLIDE PACK IAW B737 AMM 25-66-01. VERIFIED REINSTALLATION OF DOOR R1 ORIGINAL EMERGENCY ESCAPE SLIDE PACK PER GMM 09-25-05.

Part: SNUBBER — OUT OF ADJUST (ZONE 800) · airframe 80,277 hrs · 29,676 cycles

L2 DOOR SNUBBER IS CONTACTING DOOR SKIN WHEN OPENING. AND IS GOUGED. REMOVED LINER FROM AFT ENTRY DOOR (L2) REF 52-13-31. ADJUSTED AFT ENTRY DOOR (L2) VERTICALLY REF AMM 52-13-00. REINSTALLED DOOR LINER REF AMM 52-13-00. REINSTALLED SLIDE PACK REF AMM 25-66-01-400-803. ADD EMP:U103849 VERIFIED RII REQUIREMENTS OF DOOR ADJUSTMENT REF AMM 52-13-00, SLIDE INSTALLATION REF AMM 25-66-01-803. HAND BLENDED EDGE OF DOOR SKIN WHERE SKIN WAS MAKING CONTACT WITH TOP OF SNUBBER. REF. AMM. 52-10-01-1A-3. PARA 4.A.(3)(A) DETAIL "C". MATERIAL LOSS = 0.003 ON SKIN EDGE OUT OF 0.100". ALLOWABLE. O.K TO CONTINUE PER FIGURE 105 AND TABLE 101 OF THIS REFERENCE.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 80,277 hrs · 29,676 cycles

M1670 BATTERY PACK FAILED EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED EMERG BATTERY #M1670, OPS CHK GOOD PER MM # 33-51-06-960-805.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 79,971 hrs · 29,548 cycles

POSSIBLE BIRD STRIKE ON 1 ENGINE SPINNER FEATHERS ON SPINNER HUB UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CAPT REPORTS #1 ENG SPINNER CONE SHOWS SIGNS OF BIRD STRIKE OCM PERFORMED #1 ENGINE BIRD STRIKE INSPECTION IAW AMM 71-00-00-800-802-F00. INBOUND FLIGHT CREW DID NOT REPORT ANY PARAMETER SHIFTS OR ODORS IN THE CABIN. OCM REPORTS SINGLE BIRD IMPACT ON #1 ENGINE SPINNER AND DOWN THE BYPASS. NO EVIDENCE OF BIRD INGESTION INTO THE CORE. NO MISSING MATERIAL FROM FAN BLADES AND NO OTHER DEFECTS NOTED IN INLET AN D BYPASS. OCM CLEANED ALL REMAINS OF BIRD. . OCM PERFORMED #1 ENGINE BIRD STRIKE INSPECTION IAW AMM 71-00-00-800-802-F00. INBOUND FLIGHT CREW DID NOT REPORT ANY PARAMETER SHIFTS OR ODORS IN THE CABIN. OCM REPORTS SINGLE BIRD IMPACT ON #1 ENGINE SPINNER AND DOWN THE BYPASS. NO EVIDENCE OF BIRD INGESTION INTO THE CORE. NO MISSING MATERIAL FROM FAN BLADES AND NO OTHER DEFECTS NOTED IN INLET AN D BYPASS. OCM CLEANED ALL REMAINS OF BIRD.

Part: DOOR — MISSING (ZONE 100) · airframe 79,413 hrs · 29,303 cycles

PDA 2 REF L/P 3032232, LAVATORY SERVICE DOOR MISSING FROM AIRCRAFT. REF L/P # 3032232 FOR CDL DEFERRAL. THIS LOG TO IDENTIFY PDA ONLY.C/W CDL 52 D FOR MISSING AFT LAV PANEL.

Part: UNKNOWN — ODOR (CABIN) · airframe 79,202 hrs · 29,200 cycles

STRONG ENG FUME SMELL ON TAKEOFF AND TAXI IN INSPECTED INLETS AND EXHAUST FOR DAMAGE AND CONTAMINATION. SLIGHT DISCOLORATION ON #1 AROUND SPINNER, POSSIBLE GREASE FROM FAN HUB.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,480 hrs · 28,843 cycles

EMERGENCY POWER PACK, M1670M FAILS EMERGENCY LIGHTING FUNCTIONAL CHECK, BATTERY DISCHARGES IN LESS THAN 13 MINS (REF. AAR NR 100 010615). REPLACED BATTERY PACK (M1670) IAW B737 AMM 33-51-06-960-805, OPS CHECKS GOOD (WORK ACCOMPLISHED BY V934989 AND AAR QC A-15 V93157 5)(SDR NO. 1036813).

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 76,597 hrs · 27,950 cycles

LOW PRESSURE LIGHT FOR ELEC PUMP 1 ON WHILE IN FLIGHT. RAN ELEC PUMP 1 (SYS B). PRESSURE CLIMBS TO ONLY APPROX 1600 PSI THEN QUICKLY DROPS PSI. PUMP, HYD ELECT OFF 29-2910-9-0002 8366 ON 0000 PUMP, HYD ELECT OFF 29-2910-9-0002 8366 ON 29-2910-9-0002 1383 REMOVED AND REPLACED SYSTEM B ELECTRIC MOTOR DRIVEN PUMP REF AMM 29-11-21. DURING REMOVAL OF ELECTRIC PUMP, FOUND QUICK DISCONNECT SUPPLY LINE COLLAPSED. REMOVED AND REPLACED SUPPLY LINE REF AMM 29-11-21. REMOVED AND INSPECTED ACOUSTIC FILTER AND ADD EMP:U399308 FOUND NO DEBRIS, REINSTALLED ACOUSTIC FILTER REF AMM 29-11-27. PERFORMED OPS CHECK OF SYS B EDMP SEVERAL TIMES, SYS B HOLDS PRESSURE AT 3100 PSI. CYCLED FLIGHTS CONTROLS SEVERAL TIMES, NO DESPCREPANCIES NOTED, LEAK CHECK GOOD AT THIS TIME. PARTS USED: 00-0583-3-9845,QTY :1 40-0595-3-1983,QTY :1 00-0585-3-0397,QTY :1 40-0595-3-1976,QTY :1 29-2910-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1772283 SN OFF 8366

Part: DOOR — MISSING (LAV SERVICE) · airframe 75,213 hrs · 27,312 cycles

PDA 1 ON WALKAROUND FLIGHT CREW FOUND THAT EXTERNAL LAVATORY SERVICE ACCESS DOOR IS MISSING. THE APPROXIMATE DIMENSION IS 14 INCH BY 15 INCH

Part: ADIRU — FAILED (ADIRU) · airframe 74,016 hrs · 26,796 cycles

IAS DISAGREE ALTITUDE DISAGREE SPEED TRIM FAIL EECS WENT TO ALTE RNATE R&R RT ADIRU IAW 34-21 -01 AND PERFORMED OPERATIONAL TEST 34-21-00 SYSTEM OPS CHECK NORMAL A/C OK TO CONTINUE. LAND VERIFY SUCCESSFULLY ROTABLE PARTS CHANGE WAS INDICATED - TT # 1815203 SN OFF 2675 IPC REFERENCE # 34-21-00 FYI LAND VERIFY WAS NOT ACCOMPLISHED BY TECHNICIAN U178307 DUE TO HIS CAT STATUS BEING EXPIRED ...LOG PG 9361701 HAS BEEN GENERATED TO ACCOMPLISH LAND VERIFY TEST BY A CAT QUALIFIED TECHNICIAN

Part: ANGLE — CRACKED (RH PACK DIFFUSER) · airframe 73,470 hrs · 26,556 cycles

PDA 3 RIGHT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED AND PARTIALLY MISSING -- SEE SAFETY BULLETIN 20SFY020 -- SEE PHOTO,S PHOTO,S ADDED THE DOOR STOP (L-ANGLE) IS APPROX 40-50% BROKEN OFF & MISSING AND THE REST OF THE DOOR STOP (L-ANGLE) CRACKED ALMOST TO THE END. IPC 21-51-03-06A...

Part: LIGHT — DAMAGED (SEAT ROW 20ABC U) · airframe 71,724 hrs · 25,844 cycles

UPPER RED SEAT MOUNTED EMERGENCY LIGHT AT 20ABC DAMAGED. REMOVED AND REPLACED RED LIGHT ASSY REF CONFIG DRAWING 3350DD14743 AND MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS FOR EMERGENCY LIGHT REPLACEMENT.

Part: LIGHT — DAMAGED (SEAT ROW 31ABC) · airframe 71,724 hrs · 25,844 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 31ABC DAMAGED. REMOVED AND REPLACED WHITE LIGHT ASSY REF MM 33-51-11 AND CONFIG DRAWING 3350DD14743. OPS CK OK. VERIFIED IDT REQUIREMENTS FOR EMERGENCY LIGHT REPLACEMENT.

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED LP 6229107 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW ECRA 5714-01058 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECTION U 358176 2/8/2020

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED LP 6229106 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW ECRA 5714-01057 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECTION U 358176 2/8/2020

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED LP 6229103 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAW B737 -800 DWG 111A200 AND SRM 51-40-02 SSFR REPORT FORM 46-0024 ENTER ED BY UAL INSPECTION U358176 2/8/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED LP 6229148 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW ECRA 5714-01060

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED LP 6229108 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW ECRA 5714-01059

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED LP 6229105 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 32.40 IAW B737 -800 DWG 111A2000 AND SRM 51-40-02

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED LP 6229109 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87 IAW B737 -800 DWG 111A2000 AND SRM 51-40-02.

Part: FITTING — CRACKED (BS 540) · airframe 68,986 hrs · 24,762 cycles

SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED LP 6229104 SPT REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW ECRA 5714-01056 SSFR REPORT FORM 46-0024

Part: FUSE — INOPERATIVE (CABIN) · airframe 63,588 hrs · 22,608 cycles

ROWS 21-34 AND DOOR 2R EMERG EXIT LIGHTS INOP INSPECTED EMERGENCY BATTERY PACK 1695, SECURED BATTERY TO PACK AND REPLACED FUSE, OPS CHECKS GOOD. OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,063 hrs · 21,597 cycles

EXTERIOR EMERGENCY LIGHT INOP AT A/C LEFT AFT OVERWING HATCH DOOR. RELAMPED EXTERIOR EMERGENCY LIGHT AT A/C LEFT AFT OVERWING DOOR HATCH. OPS CHECK GOOD.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 60,568 hrs · 21,402 cycles

RT MLG H FITTING LOWER INBD HOLE CORRODED. REMOVED AND REPLACED RT MLG TRUNNION SUPPORT FITTING IAW DWG 115A5002 AND SRM 51-40-02.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 60,568 hrs · 21,402 cycles

HEAVY CORROSION AT LEFT MLG TRUNNION SUPPORT ASSY, FWD LOWER INBD ATTACH POINT BUSHING. REMOVED AND REPLACED THE LT MLG TRUNNION SUPPORT FITTING IAW DWG 115A5002 AND SRM 51-40-02.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 60,568 hrs · 21,402 cycles

LT HORIZ STAB LOWER SKIN CRACKED 2 PLACES STA 147.9 APPROX 16" AND 24.5" AFT OF FRONT SPAR. CATEGORY B REPAIR INSTALLED PER SRM 55-10-01, REPAIR 11.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 60,568 hrs · 21,402 cycles

LT HORIZ STAB LOWER SKIN CRACKED AT STA 129.5 APPROX 9.5" AFT OF FRONT SPAR. CATEGORY B REPAIR INSTALLED PER SRM 55-10-01, REPAIR 11.

Part: STRAP — GOUGED (STA794 ST25-26R) · airframe 60,568 hrs · 21,402 cycles

INNER FAIL SAFE STRAP AT FRAME 794.37 HAS DEEP GOUGE ON UPPER SURFACE BETWEEN STR 25RT AND 26RT. REMOVED AND REPLACED FAIL SAFE STRAP AT FRAME 794.37 AFT CARGO BIN RT SIDE FWD OF CARGO DOOR REF SRM 51-40-02.

Part: SKIN — CRACKED (BS 540) · airframe 60,568 hrs · 21,402 cycles

BS 540, RT SKIN HAD A CRACK INDICATION BETWEEN STRINGER 22 AND 23R. REPAIRED THE SKIN IAW EA 5310-05878, OPS 5, REV D.

Part: SWITCH — DIRTY (MLG) · airframe 52,454 hrs · 18,449 cycles

AFTER TAKEOFF LG WOULD NOT RETRACT. PERFORMED QRH & RETURNED TO AIRPORT. NON O/W LANDING. DIRT DEBRIS FOUND IN & UNDER MANUAL GEAR EXTENSION FLOOR PANEL, SWITCH WAS NOT MAKING & BREAKING. REMOVED DEBRIS FROM MAN GEAR EXTENSION SWITCH, JACKED ACFT IAW AMM 07-11-01 & 32-09-00. SWUNG GEAR SEVERAL TIMES IAW AMM 32-34-00. OPERATIONS CHECKED NORMAL. IDT PERFORMED, OK TO CONTINUE.

Part: SWITCH — FAULTY (COCKPIT) · airframe 51,909 hrs · 18,267 cycles

TAKEOFF CLIMB OUT AT APPROX 1000 FT SPEED TRIM LIGHT ILLUMINATED & STAB TRIM DID NOT WORK. FOLLOWED QRH MANUAL TRIMMED ACFT FLAPS 15 LANDING OVERWEIGHT AT 148000 LBS. TROUBLE SHOT TO THE COLUMN SWITCH MODULE M1201. R & R SWITCH IAW MM 27-41-51-400-801. OPERATIONS TESTS CHECKED GOOD PERFORMED LAND VERIFY ALL TESTS PASS ACFT IS FULL CAPABLE DISCREPANCY CLOSED. ROTABLE PARTS CHANGE WAS INDICATED TT 1096678, SN OFF 00083 SWITCH, CONTROL OFF 29-2741-9-0002 0083 ON 29-2741-9-0002 3858.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,677 hrs · 16,424 cycles

APU 6 PACK LIGHT ON, SEEMS TO BE INDICATION PROBLEM. INSPECTED TAIL AREA OF A/C IN BALLPARK, DEPARTED MEL 49-01. AFTER T/O F/A REPORTED BURNING ODOR, DECLARED EMERGENCY, AIR RETURN TO DEPARTURE. ACCOMPLISHED CONDITIONAL INSPECTION IAW CARD 05-51-26-800-801C1. NO SOURCE OF BURNING ODOR FOUND. ACFT OK FOR SERVICE. APU OPERATION AND INDICATION ALL NORMAL.

Part: TRANSITION PANEL — CORRODED (BS 727D-727G) · airframe 44,570 hrs · 15,691 cycles

AFT CARGO, CORROSION RT TRANSITION PANEL BS 727D TO SPLICE PLATE AT BS 727G CTN 53-140-00. REMOVED AND REPLACED TRANSITION PANEL REF SRM 53-00-53 AND SRM 51-40-02.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 44,570 hrs · 15,691 cycles

C-2 DOOR INTERIOR SKIN HAS CORROSION 15 IN FROM LEADING EDGE AT LOWER EDGE AT SNAP. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED REF ECRA 5240-01657.

Part: WEB — CORRODED (BS 847) · airframe 44,570 hrs · 15,691 cycles

AFT CARGO, CORROSION ON FLOOR WEB BS 847 S27R CTN 53-140-00. INSTALLED WEB PER SRM 51-10-02 AND 51-40-02.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 44,570 hrs · 15,691 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN HAS 1 INCH CRACK AT LES 142.45 AND ABOUT 6" FROM AFT SPAR. COMPLETED REPAIR LT HORIZONTAL STABILIZER LOWER SKIN REF SRM 55-10-01.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 44,570 hrs · 15,691 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN HAS 2.25 INCH CRACK AT LES 142. 45 AND ABOUT 16.5" FROM AFT SPAR. COMPLETED REPAIR LT HORIZONTAL STABILIZER LOWER SKIN REF SRM 55-10-01.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 44,570 hrs · 15,691 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN HAS 3 INCH CRACK AT LES 142.45" FROM AFT SPAR. COMPLETED REPAIR LT HORIZONTAL STABILIZER LOWER SKIN REF SRM 55-10-01.

Part: INTERCOSTAL — CORRODED (BS 847) · airframe 44,570 hrs · 15,691 cycles

CORROSION AT AFT SURROUND AND RT TRANSITION PANEL (INSIDE BOX AREA) OF AFT CARGO DOOR CUTOUT BS 847 AND BETWEEN STRINGERS 25 AND 26R. REMOVED AND REPLACED INTERCOSTAL AND INSTALLED TRANSITION PANEL IAW SRM 51-40-02.

Part: CARGO TRACK — CRACKED (BS 727G-767) · airframe 44,570 hrs · 15,691 cycles

AFT CARGO TRACK CRACKED 4 PLACES BETWEEN STA 727G AND 767. CTN 53-140-00 REMOVED AND SPLICED IN NEW CARGO TRACK IAW SRM 53-0053 REPAIR 3.

Part: TRANSITION PANEL — CORRODED (BS 767-787) · airframe 44,570 hrs · 15,691 cycles

AFT CARGO, RT TRANSITION PANEL CORRODED STA 767 TO 787. CTN 53-140-00. REMOVED DAMAGED TRANSITION PANEL, LOCATED AND DRILLED NEW PANEL INSTALLED NEW PANEL REF SRM 51-10-02, 51-40-02, AND AMM 51 21-00.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 44,570 hrs · 15,691 cycles

COCKPIT FLOORBEAM ANGLE HAS LIGHT CORROSION ON UPPER SURFACE BS 270 LBL 6 TO RBL 12. REPAIRED IAW ECRA-5321 -01566.

Part: FRAME — CRACKED (BS 440) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT BS 440 BETWEEN S-8R AND S-9R. REPAIRED PER EA 5310-04716 REV C.

Part: FRAME — CRACKED (BS 727B) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT BS 727B BETWEEN S-8L AND S9-L. COMPLETED REPAIRED FRAME AT BS 727B STRINGER 8L-9L REF ECRA 5310-04716 REV C.

Part: FRAME — CRACKED (BS 440) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT STA 440L BETWEEN S-8L AND S-9L. REMOVED SUPPORT BRACKET, CUT OUT DAMAGE, NDT AREA, FABRICATED REPAIR ANGLES A&B TREATED & PRIMED, COLD WORKED 6 HOLES & INSTALLED, INSTALLED SUPPORT BRACKET, APPLIED FILLET SEAL REF EA 5310-04716 REV C FIG 3.

Part: FRAME — CRACKED (BS 480) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT BS 480L BETWEEN STR 8L AND 9L. REPAIRED PER EA 5310-04716 REV C OP 2.

Part: FRAME — CRACKED (BS 500) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT BS 500C BETWEEN S-8L AND S9L. FABRICATED AND INSTALLED REPAIR ANGLES A, B COLD WORKED HOLES, REF EA 5310-04716 REV C OPERATION 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT STA 400 BETWEEN S-8R AND S-9R. REPAIRED FRAME, REF-EA 5310-04716 OP 02, PG, 26-28 STEPS 1-13. NO EC/RA REQUIRED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,570 hrs · 15,691 cycles

FRAME CRACKED AT STA 380 BETWEEN S-8R AND S-9R. REPAIRED FRAME PER EA 5310-04716 REV C OP 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT STA 500C BETWEEN S-8R AND S-9R. REPAIRED FRAME PER EA-5310-04716 OP 02 PAGE 26 TO 28 STEPS 1 TO 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,570 hrs · 15,691 cycles

FRAME IS CRACKED AT STA 480 BETWEEN S-8R AND S-9R. REPAIRED FRAME AT STA 480 BETWEEN STR-8R AND STR-9R. COMPLIED WITH STEPS 1-13, PAGES 26, AND 27 OF EA 5310-0471602 OP 02.

Part: COFFEEMAKER — MALFUNCTIONED (FWD GALLEY) · airframe 43,200 hrs · 15,181 cycles

FLT ATTD REPORTED LARGE SPARK (BLUE FLASH) AND HEARD A LOUD POP NOISE AT FWD C/M`S. SHUT BOTH C/MAKERS OFF. NOT SURE WHICH ONE COULD NOT DUPLICATE TROUBLES ABOVE. INSPECTED C/MAKER CAVITY AND ASSOCIATED WIRING. NO DEFECTS OR EVIDENCE NOTED. REMOVED AND REPLACED BOTH C/M AKERS PRECAUTIONARY. THIS PAGE C/M #108. OP AND LEAK CHECK GOOD. OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1490659 SN OFF 00863 COFFEEMAKER, A/ OFF 29-2599-9-0001 0863 ON 29-2599-9-0001 1003

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,764 hrs · 15,013 cycles

C/B "PASS CABIN" LIGHTING EMERG CHGR CB POPPED IN FLIGHT. TROUBLESHOT SYSTEM PER AMM 20-60-01. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER AMM 33-51-06. OPS CKS GOOD ACFT OK TO CONTINUE. BAT AND CHARGE REMOVED AND REPLACED WAS M1673.

Part: TIRE — BLOWN (MLG) · airframe 32,401 hrs · 11,316 cycles

NORMAL LANDING AND ROLLOUT UNTIL 80-100 KTS. AIRCRAFT VEERED LEFT WITH AN ASSOCIATED LOUD POP. TOWER AND AIR CREW VERIFIED RIGHT MAIN OUTBOARD TIRE SEPARATION. NUMBER 3 AND 4 TIRES REMOVED AND REPLACED. PER AMM 05-51-54-210-801, TIRE BURST INSPECTION OK PER AMM 05-51-16-210-801, FLAT SPOTTED TIRE INSPECTION FAILED TRANSDUCER OPS CHECK PORTION. FOUND NUMBER 3 TRANSDUCER HARNESS ON NUMBER 4 AND NUMBER 4 ON NUMBER 3. UNCROSSED HARNESS IN AXLE, TRANSDUCER OPS CHECK PASSED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,990 hrs · 10,200 cycles

THE FIRST CLASS EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 2,806 hrs · 9,902 cycles

CENTER FLOOR PANEL SUPPORT MEMBER CORRODED. REPAIRED IAW ECRA 5310-04614.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,833 hrs · 9,128 cycles

THE R-2 DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,019 hrs · 7,735 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 8 TO LBL 12. REPAIRED IAW ECRA 5321-01219.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 22,019 hrs · 7,735 cycles

INSPECTION FOUND R-2 DOOR FRAME CORRODED AT Z-CHANNEL SILL, STA 990, RBL 64 TO LBL 24. THE FRAME WAS REPAIRED IAW ECRA 5311-01225.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,019 hrs · 7,735 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, BL 0 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01220.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,019 hrs · 7,735 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE NEAR R-1 DOOR, STA 320, BL 0 TO RBL 24. REPAIRED FLOORBEAM IAW ECRA 5321-01216.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,019 hrs · 7,735 cycles

INSPECTION FOUND THE L-2 DOOR AREA FLOORBEAM NUT CLIP HOLES CORRODED AT STA 986.5, LBL 22.5 TO LBL 43. REPAIRED IAW ECRA 5321-01215.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 22,019 hrs · 7,735 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 947-967, RBL 50, I/B OF R-2 DOOR FRAME. THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01218.

Part: MODULE — LOOSE (CABIN) · airframe 21,895 hrs · 7,686 cycles

AISLE LIGHTING IN THE FIRST CLASS CABIN LOOSE AT G7 GALLEY. REPLACED LIGHT MODULE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,360 hrs · 5,625 cycles

THE FUSELAGE SKIN SUSTAINED DAMAGE BELOW L-2 DOOR AT BS 958 BETWEEN S22L AND S23L. THE DAMAGE WAS REPAIRED IAW ECRA 5330-03261. A DIP WAS ISSUED TO ACCOMPLISH AN EXTERNAL DETAIL VISUAL INSPECTION OF THE FILLER AND DOUBLER LOOKING FOR CRACKS AND LOOSE OR MISSING FASTENERS. INITIAL INSPECTION THRESHOLD IS 56,000 TOTAL AIRFRAME CYCLES WITH REPEAT INSPECTION EVERY 12,000 CYCLES.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 16,361 hrs · 5,625 cycles

INSPECTION FOUND A HOLE PUNCTURED INTO THE FUSELAGE SKIN THREE FEET BELOW THE L-2 DOOR AT BS 958, S22L-S23L. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5330-03261.

Part: ACTUATOR — INOPERATIVE (NLG) · airframe 12,336 hrs · 4,146 cycles

THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE NLG UNSAFE LIGHT AND VIBRATION FROM THE NOSE GEAR AREA. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NLG LOCK ACTUATOR AND LOCK MANIFOLD VALVE WERE REMOVED AND REPLACED IAW MM 32-33-21 AND 32-33-31. AN OPERATIONAL TEST WAS PERFORMED IAW MM 32-33-00 AND SYSTEM CHECKS WERE NORMAL.