N23708

Part: LATCH — SEIZED (ZONE 800) · airframe 82,557 hrs · 30,176 cycles

DOOR WARNING ANNUNCIATOR IS ON EQUIP EQUIP LT ON AT FL230 IN CLIMB AC NOT PRESSURIZE LT WENT OUT AT 9 000 AND 0 PSID REF L/P 4920965. INSPECTED DOOR AND DOOR SEAL REF AMM 52-48-41. NO DEFECTS NOTED. PERFORMED ACCESS DOOR INDICATION SWITCH TEST REF AMM 52-71-42. OPS CHECK GOOD. PERFORMED LEAK CHECK OF E&E ACCESS DOOR VIA CABIN PRESSURIZATION REF AMM 21-31-00. PRESSURIZED CABIN TO 5 PSI. NO DROP IN PRESSURE. NO LEAKS NOTED ON E&E DOOR. INPUTED INCORRECTLY PRESSURIZED CABIN TO 4 PSI. REMOVED AND REPLACED HANDLE ASSY. REF AMM 52-48-41. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 82,148 hrs · 29,953 cycles

EMERGENCY EXIT HATCH WINDOW LIGHT INOP AT ROW 21F. REPLACED LAMP, LIGHTS UP OK.

Part: GIRT BAR — MISINSTALLED (ZONE 800) · airframe 81,616 hrs · 29,732 cycles

L1 DOOR SLIDE NOT BRACKETED PROPERLY. WE CANT CLOSE MCD AND DON T FEL COMFORTABLE OPENING FOUND GIRT BAR STOWED INCORRECTLY, INSTALLED THE GIRT BAR BACK INTO THE SLIDE COMPARTMENT GIRT BAR RETAINERS REF: TASK 25-66-01-400-801

Part: FITTING — LEAKING (HYD SYSTEM) · airframe 80,682 hrs · 29,259 cycles

HYDRAULIC LEAK FROM RT FRANGIBLE FITTING. REMOVED THE AFFECTED FRANGIBLE FITTING AND NUT AND REPLACE WITH A HYDRAULIC CAP ASSEMBLY. PLACED ON MEL 3220A NOT LEAKING. REMOVED THE AFFECTED FRANGIBLE FITTING AND NUT AND REPLACE WITH A HYDRAULIC CAP ASSEMBLY. PLACED ON MEL 3220A NOT LEAKING DEFERRED DIRECTLY BY TOMC UPDATED M&L, REF IPC 32-32-52-02 ITEM 20, P/N 273A2801-4 M&E 29-3212-3-0005. NIS CLE.

Part: SKIN — UNKNOWN (L1 DOOR) · airframe 78,210 hrs · 28,212 cycles

CREATED LOG PAGE TO ADD ESFR FOR NR# 001571532 OF L1 DOOR REPAIR INNER SKIN, WHILE INDUCTED FOR HEAVY MAINTENANCE VIST. VERIFIED ESFR #1033749 ADDED AND COMPLIED WITH PER EC/RA#:5211-01832

Part: LIGHT — INOPERATIVE (ROWS 3 & 11) · airframe 77,587 hrs · 27,870 cycles

EMERGENCY ISLE LIGHTING INOP BETWEEN ROWS 3 AND ROW 11 EMERGENCY BATTERY IS REMOVED FROM CHARGER AT 12 WINDOWS BACK ON THE RIGHT SIDE. NEW CHARGER AND OLD BATTERY ARE IN THE AVIONICS OFFICE ON THE TABLE. BATTERY IS ON AOG. REF AMM 33-51-00 REPLACED BATTERY PACK AT M1676 REF MM 33-51-06. EMER LIGHTS BETWEEN CROWS 3 AND 11 OPS CHECK NORMAL

Part: MOTOR — UNKNOWN (FLAPS) · airframe 77,443 hrs · 27,804 cycles

TRIM INOP WITH FLAPS UP FOUND UNDERNEATH BONDING GROUND WIRE. DURING INSPECTION FOUND AIRFRAME BONDING WIRE GROUND STUD LOOSE, (GD4801S), UNABLE TO TIGHTEN. WILL REQUIRE REPLACEMENT BEFORE FURTHER INSTALLATION. THE PROBLEM IS THE AIRCRAFT DOES NOT TRIM NOSE DOWN WITH FLAPS U REMOVED STABILIZER TRIM MOTOR IAW AMM 27-41-71. P/N: OFF: P. NOSE UP WORKS NORMALLY. POWER AT MOTOR IS GOOD. WILL NEED MOT 6355C0001-02. S/N: OFF: 08127. DURING INSTALLATION OF NEW TRIM OR REPLACED. MOTOR, ELECTRICAL BONDING RESISTANCE CHECK IS MEASURING OUT OF LIMITS 15MILLIOHMS. RECLEANED MATING SURFACES, AND REMOVED PAINT 22-11-81-710-801 PARTS USED: 29-2741-9-0011,QTY :1 LAND VERIFY BITE NOT COMPLETED, TRIM SWITCH NOW FUNCTIONING ROTABLE PARTS CHANGE WAS INDICATED - TT # 1765123 SN OFF 8127 NORMALLY ,REQUIRES FURTHER TROUBLESHOOTING. TEMPORARY GROUND NEEDS TO BE REMOVED AND ALL TEST NEED PERFORMED AGAIN. C/W INSPECTION OF STAB TRIM MOTOR INSTALLATION AS PER MM 27-41-71-400-801 UP TO AND INCLUDING STEP 6 REVISION TO SIGN OFF REQUIRED. BONDING WIRE ATTATCHMENT MOUNTING BRACKET HAS EXCESSIVE PLAY EXCISSIVE MOVEMENT OF BOLT INSTALLED STAB TRIM MOTOR AS PER MM 27-41-71-400-801 UP TO STEP INSTALLED STAB TRIM MOTOR AS PER MM 27-41-71-400-801 UP STEP 7. INSTALLED TEMPORARY GROUND FOR TROUBLESHOOTING PURPOSES, INSTALLED PRE-INSTALLED GROUND STUD IAW SWPM 20-20-10 PAGE 27. 7. TRIM MOTOR WILL REQUIRE THE FOLLOWING TESTS. STAB TRIM MOTOR NEED TO COMPLETE INSTALLATION AND PERORM FOLLOWING TESTS STAB PERFORMED ST

Part: SCREW — MISSING (LH WING SURGE TA) · airframe 77,401 hrs · 27,786 cycles

PDA 3 REF LOGPAGE 4124213, FOUND 2 MISSING SCREWS ON THE LEFT WING SURGE TANK ACCESS PANEL. INSTALLED 2 NEW SCREWS IS MISSING FASTENER LOCATIONS IN LEFT WING SUREGE TANK ACCESS PANEL. TIGHTENED ALL REMAINING SCREWS REF AMM 28-11-11, LEAK CHECKS GOOD, OK FOR SERVICE.

Part: PANEL — MISSING (LH WING) · airframe 77,327 hrs · 27,750 cycles

PDA 3 REF LOGPAGE 4124213, FOUND 2 MISSING SCREWS ON THE LEFT WING SURGE TANK ACCESS PANEL. INSTALLED 2 NEW SCREWS IS MISSING FASTENER LOCATIONS IN LEFT WING SUREGE TANK ACCESS PANEL. TIGHTENED ALL REMAINING SCREWS REF AMM 28-11-11, LEAK CHECKS GOOD, OK FOR SERVICE.

Part: MOTOR — INOPERATIVE (HORIZ STAB) · airframe 77,035 hrs · 27,626 cycles

ELECTRIC STAB INOP FOUND VLTAGE AND GROUND AT ELEC TRIM MOTOR, WILL REQUIRE REMOVED EXISTING STAB TRIM ELECTRIC MOTOR PER MM STABILIZER TRIM MOTOR. 27-41-71-000-801. BEGAN INSTALLATION OF NEW ELECTRIC TRIM MOTOR PER MM 27-41-71-400-801. COMPLETED THROUGH STEP F(4)(A). COMPLETED INSTALLATION OF HORIZ STAB MOTOR FROM STEP F.4.A ON.OPS TEST NORMAL PER REF. AMM 27-41-71-400-801. PARTS USED: 29-2741-9-0011,QTY :1 ADD EMP:097599 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1765433 SN OFF 3387 MOTOR, STAB, HO OFF 29-2741-9-0011 3387 ON 29-2741-9-0011 8127

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 69,713 hrs · 24,645 cycles

EMERGENCY LIGHTS INOP AT SEAT 3 DEF THUR 11 DEF 6485392-SPT- REMOVED AND REPLACED BATTERY CHARGER FROM M1676 IAW B737 AMM 33- / 51-06-960-806 PERFORMED OPS CHECK FOR SEATS 3DEF THUR 110EF OPS CHECK GOOD IAW B737 AMM 33-51-06-960-806. REMOVED P/N AD D717-01 / -100, S/N 2805. P/N INSTALLED AD-D717-01-100 ,S/N 206561. -SPT-6485392 SSFR REPORT, FORM 46-0024 ENTERED BY UAL INSPECTION U35

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,713 hrs · 24,645 cycles

AISLE LIGHT AT SEAR ROW 12 ABC, 21 ABC AND 27DEF ARE INOP. EMERG ENCY LIGHTS -SPT- 6482787

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,713 hrs · 24,645 cycles

R 2 LOWER EXIT SIGN IS INOP -SPT-6482786 TROUBLE SHOT SYSTEM FOUND BATTERY PACK CM1672 INOP REMOVED AND R EPLACED BATTERY PACK IAW B737-800 WDM 33-51-14 AND AMM 33-51-06+ STA 952 WL290 ROL14. OPS CHECK GOOD IAW B737-800 AMM 33-51-06. SSFR REPORT , FORM 46-0024 BY U075598 2/18/2020

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,713 hrs · 24,645 cycles

R 2 EMERGENCY SLIDE LIGHT INOP -SPT- 6482784 TROUBLESHOOT AND FOUND BATTERY PACK INOP IAW B737-800 WDM 33-51-14. REMOVED AND REPLACED BATTERY PACK AT STA 952 WL 290 LBL 13 A ND OPS GOOD IAW 737-800 AMM 33-15-06. SSFR REPORT . FORM 46-002 4 ENTERED BY U075598 2/18/2020

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,713 hrs · 24,645 cycles

EMERGENCY SEAT PROXIMITY LIGHTS ARE INOP ROW 22 THUR 34 ABC -SPT - 6482788 REMOVED AND REPLACED BATTERY PACK M1672 PROX LIGHTS ON SFF AT RO W 22-34 ABC OP CHECK NORMAL IAW 33-51-06. SSFR REPORT, FORM 46-0 024, ENTERED BY U354980 2/18/2020

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,713 hrs · 24,645 cycles

L 2 OVERHEAD LIGHT INOP -SPT- 6482785 TROUBLESHOOT AND FOUND BATTERY PACK M1672 INOP. IAW B737-800 WDM 33-51-14. REMOVED AND REPLACED BATTERY PACK AT STA 952 WL 290 RBL 14 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06. SSFR REPORT, FORM 46-0024 ENTERED BY UAL INSPECTION U075598 2/18/2020

Part: FITTING — CRACKED (BS 549) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED LP 6482825 SPT REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND ECRA 5714-01066 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECT ION U075598 2/15/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTINGS AT STA 540 LBL 32.40 IS CRACKED -SPT- 6481052 REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND ECRA 5714-01071 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECT ION U075598 2/15/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTINGS AT STA 540, LBL 40.87 IS CRACKED. -SPT-6481053 REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND ECRA 5714-01070 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECT ION U075598 2/15/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTINGS AT STA 540 LBL 15.04 IS CRACKED. SPT-6481054- REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND ECRA 5714-01067 SSFR REPOT FORM 46-0024 ENTERED BY UAL INSPECTI ON U075598 2/15/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. LP 6471119 SPT REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-60-02 AND ECRA 5714-01068 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECT ION U354980 2/15/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED LP 6482823 SPT REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND ECRA 5714-01071 SSFR REPORT FROM 46-0024 ENTERED BY UAL INSPECT ION U075598 2/15/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED LP 6482824 SPT REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND ECRA 5714-01069 SSFR REPORT FORM 46-0024 ENTERED BY UAL IMSPECT ION U075598 2/15/2020 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,713 hrs · 24,645 cycles

SHEAR FITTING AT STA 540 RBL 6.44 IS CRACKED LP 6482826 SPT REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND DWG 111A2000 SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECTION U075598 2/15/2020 INSPECTION ACCEPTED

Part: WARNING MESSAGE — ILLUMINATED (ANTI-ICE SYSTEM) · airframe 68,840 hrs · 24,325 cycles

ENG 1 AND WING A/I INDICATIONS INOP ON OVHD PANEL. BREAKER A6 FO UND POPPED. T/S REF FIM 30-11 & WDM 30-21&30-11 RESET C/B AND OPS CK NORMAL AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,429 hrs · 22,039 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED THE LAMPS IAW AMM 33-51-04-960-801, OPS CHECKED NORMAL.

Part: COVER — OUT OF POSITION (CABIN) · airframe 61,789 hrs · 21,409 cycles

21F EMERGENCY EXIT LIGHT COVER MISSING. COVER IS BY EXIT FLOOR LOCATION INSTALLED MISSING EMERGENCY EXIT LIGHT COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,689 hrs · 21,355 cycles

L1 SLIDE LIGHT INOP. RELAMP L1 SLIDE LIGHT IAW AMM 33-51-04-960-801. OPS CHECK GOOD.

Part: SLIDE — DAMAGED (R2 DOOR) · airframe 61,637 hrs · 21,333 cycles

R2 DOOR SLIDE HAS DAMAGE AND DISBONDING AT SLIDE SEAM UNDER PRESSURE GAUGE. REMOVED AND REPLACED THE R2 DOOR SLIDE PACK IAW AMM 25-66-01-400-801.

Part: WINDOW FRAME — CRACKED (L1 WINDOW) · airframe 61,637 hrs · 21,333 cycles

L1 WINDOW POST FOUND CRACKED. THE WINDOW POST WAS REPAIRED IAW EC/RA 5610-01406.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 61,637 hrs · 21,333 cycles

RIGHT HORIZONAL STAB IN SPAR LOWER SKIN HAS A CRACK INDICATION AT HSS 129.50, ONE INCH LONG, TWO INCHES INBD OF DRAIN HOLE, THREE INCHES FWD OF REAR SPAR. REPAIRED IAW SRM 55-10-01, REP 11.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 60,183 hrs · 20,760 cycles

EMERGENCY LIGHTS ARE ON FROM ROW 7-10. RESET CIRCUIT BREAKER, ALL LIGHTS NOW OPS. CHECKED GOOD IAW 33-51-00-720-801.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,100 hrs · 19,074 cycles

HFEC SHOWS CRACK INDICATION AT STATION 727B, RBL 24 ON BOTH INBD HOLES TWO EACH & ON OTBD AFT HOLE OF SEAT TRACK. REPAIRED IAW CDL-15-05-12-01 & ECRA 5320-02508.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,100 hrs · 19,074 cycles

HFEC SHOWS CRACK INDICATION ON ALL FOUR SEAT TRACK HOLES STATION 727B AT RBL 45. REPAIRED IAW CDL-15-05-12-01 & ECRA 5320-02508.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,100 hrs · 19,074 cycles

ACCOMPLISH PART C REPAIR STRAP INSTALLATION OF CDL-15-05-1 2-01 TO STATION 727B, LBL 24.75. REPAIRED IAW CDL-15-05-12-01 & ECRA 5320-02508.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 56,100 hrs · 19,074 cycles

ACCOMPLISH PART C REPAIR STRAP INSTALLATION OF CDL-15-05-12 -01 TO STATION 727B, LBL 45.50. REPAIRED IAW CDL-15-05-12-01 & ECRA 5320-02508.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 56,100 hrs · 19,074 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 138.70. REPAIRED IAW SRM 55-10-01 REPAIR 11. PLACED ON DIP FOR REPETITIVE INSPECTIONS IAW SRM 55-10-01 REPAIR 11 PARAGRAPH 5 TABLE 204

Part: SKIN — DENTED (FUSELAGE) · airframe 56,100 hrs · 19,074 cycles

FUSELAGE SKIN AT STATION 193 BETWEEN STRINGER 20R & 21R HAS TOOLING DENT AROUND RIVET THAT WAS REPLACED. MEASURES 1" IN DIAMETER & .047 IN DEPTH. IAW SRM 53-00-01 AD 5 FIG 102 SH 6 IS OUT OF LIMITS Y RATIO 21.27. REPAIRED IAW SRM 53-00-01 REP 6.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 56,100 hrs · 19,074 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STATION 101.90. REPAIRED RT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01 REPAIR 11.

Part: SWITCH — INTERMITTENT (E&E BAY) · airframe 53,566 hrs · 18,108 cycles

E & E BAY DOOR LIGHT ON, ON TAKEOFF ROLL. REJECTED TAKEOFF & INITIATED REJECT AT 95 KTS TOP SPEED 100 WEIGHT 145,000. PLACED ITEM ON MEL. TROUBLE SHOT IAW WD 52-71-12. FOUND S197 ELEC ACCESS DOOR SWITCH INTERMITTENT OPEN FAULT. MEL REMAINS EXT 280422. REPLACED ELEC EQUIPMENT ACCESS DOOR INDICATION SWITCH IAW MM 52-71-42. OPERATIONS CHECKED OK.

Part: BULKHEAD WEB — CRACKED (BS 663)

BS 663, VERTICAL PRESSURE WEB AT RBL 35, WL 196 HAS .5" CRACK. REPAIRED REF SRI 2448724048 AND EDRA 5710-02286.

Part: BULKHEAD WEB — CRACKED (BS 663)

BS 663, VERTICAL PRESSURE WEB AT LBL 43, LW 195 HAS 2.1250" CRACK. REPAIRED REF SRM 57-10-10.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 49,614 hrs · 16,627 cycles

2.1250 INCH CRACK BS 663 VERTICAL PRESSURE BULKHEAD WEB AT LBL 43 & WL-195,. REPAIRED IAW SRM 57-10-10, REPAIR 3.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 49,614 hrs · 16,627 cycles

.5 INCH CRACK IN BS 663 VERTICAL PRESSURE BULKHEAD WEB AT RBL 35" & WL 196. REPAIRED IAW ECRA 5710-02 286.

Part: ANGLE — CRACKED (BS 294.5) · airframe 48,240 hrs · 16,136 cycles

THE INBD STRUCTURE OF THE ZEE STUB FRAME AT BS 294.5 JUST ABOVE THE R1 DOOR SILL. ZEE ANGLE IS CRACKED ACROSS THE LOWER 2 HOLES. REPAIR IAW ECRA 5311-01572.

Part: FRAME — CRACKED (BS 727D) · airframe 48,240 hrs · 16,136 cycles

CABIN FRAME CRACKED STA 727D BETWEEN S8L AND S9L INSTALLED REPAIR DOUBLERS REF EA 5310-04716, REV D.

Part: FRAME — CRACKED (BS 727D S8-9R) · airframe 48,240 hrs · 16,136 cycles

CABIN FRAME CRACKED BS 727D BETWEEN S8 AND 9R.. FABRICATED, & INSTALLED REPAIR IAW EA5310-04716, REV "D".

Part: FRAME — CRACKED (BS 500) · airframe 48,240 hrs · 16,136 cycles

CABIN FRAME CRACKED BS 500A BETWEEN STRINGERS 8 AND 9L. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES . EDGED SEALED REPAIR AND TREATED WITH CORROSION INHIBITING COMPOUND.

Part: FRAME — CRACKED (BS 867) · airframe 48,240 hrs · 16,136 cycles

FUSELAGE CRACKED BETWEEN STRINGERS 8 & 9 LT, BS 867, INSTALLED REPAIR ANGLES; B REF EA 5310-04716, REV D.

Part: FRAME — CRACKED (BS 380) · airframe 48,240 hrs · 16,136 cycles

FRAME CRACKED AT BS 380 BETWEEN STR 8 & 9L. CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5310-04716, REV D, FIG 3.

Part: FRAME — CRACKED (BS 500C) · airframe 48,240 hrs · 16,136 cycles

FRAME CRACKED BS 500C BETWEEN S8 AND 9R. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5310-04716, REV D.

Part: FRAME — CRACKED (BS 520) · airframe 48,240 hrs · 16,136 cycles

CABIN FRAME CRACKED, BS 520, BETWEEN S8-9R. FABRICATED & INSTALLED REPAIR REF EA5310-04716, REV "D".

Part: FRAME — CRACKED (BS 747) · airframe 48,240 hrs · 16,136 cycles

FUSELAGE FRAME CRACKED BETWEEN STR 8 & 9 RT, BS 747, RT INSTALLED REPAIR ANGLES A AND B AND REINSTALLED BRACKET, EDGE SEALED, AND PRESERVED AREA REF EA5310-04716, REV D, OP1.

Part: FRAME — CRACKED (BS 440) · airframe 48,240 hrs · 16,136 cycles

CABIN FRAME CRACKED BS 440 BETWEEN S8L AND S9L. REPAIRED FRAME IAW EA 5310-04716, REV D.

Part: FRAME — CRACKED (BS 440) · airframe 48,240 hrs · 16,136 cycles

CABIN FRAME CRACKED STA 440, BETWEEN S8R AND S9R INSTALLED REPAIR ANGLES A AND B AND REINSTALLED BRACKET, EDGE SEALED, AND PRESERVED AREA REF EA 5310-04716, REV D OP 1.

Part: FRAME — CRACKED (BS 787) · airframe 48,240 hrs · 16,136 cycles

FUSLAGE FRAME CRACKED BETWEEN STR 8 & 9L, STA 787. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW EA 5310-04716, REV D.

Part: FRAME — CRACKED (BS 400) · airframe 48,240 hrs · 16,136 cycles

CABIN FRAME CRACKED STA 400 BETWEEN S8L AND S9L. CUT OUT DAMAGE AREA AND INSTALLED REPAIR ANGLE A; B REF EA 531 0-04716, REV D, OPS 01.

Part: FRAME — CRACKED (BS 747) · airframe 48,240 hrs · 16,136 cycles

FUSELAGE FRAME CRACKED BETWEEN STR 8L BS 747, LT CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ANGLES. EDGED SEALED REPAIR AND TREATED WITH CORROSION INHIBITING COMPOUND REF EA 5310-04716, REV D.

Part: FRAME — CRACKED (BS 480) · airframe 48,240 hrs · 16,136 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8 AND 9R. INSTALLED REPAIR DOUBLERS EDGE SEALED AND PRESERVED AREA REF EA 5310-04716, REV D, OPERATION 1.

Part: FRAME — CRACKED (BS 500) · airframe 48,240 hrs · 16,136 cycles

FRAME CRACKED AT BS 500A BETWEEN STR 8 AND 9R. REPAIRED FRAME IAW EA 5310-0471 6, REV D.

Part: FRAME — CRACKED (BS 827) · airframe 48,240 hrs · 16,136 cycles

FUSELAGE FRAME CRACKED BETWEEN STR 8 - 9 LT BS 827. FABRICATED, INSTALLED REPAIR PARTS,REF-EA 5310-04716, REV D.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 48,240 hrs · 16,136 cycles

LIGHT SURFACE CORROSION AROUND FASTENER HOLES ON FLOORBEAM BS 986.5 ALONG 25 INCHES FROM L2 DOOR ZEE ANGLE. ACCOMPLISHED REPAIR B IAW ECRA 5321-01429, REV C.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 45,487 hrs · 15,222 cycles

R2 SLIDE HAS LOOSE SKIRT. REPLACED SLIDE IAW 25-66-01 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1475270 SN OFF 03534 SLIDE, B737NG, OFF 29-2561-9-0003 3534 ON 29-2561-9-0003 3241.

Part: PUMP — DEFECTIVE (NR 1 ENGINE) · airframe 36,844 hrs · 12,112 cycles

AIR RETURN, LOSS OF "A" HYDRAULIC FLUID. ENG 1 HYD PUMP OFF PRESSURE WOULD INTERMITTENTLY RETURN ON AND OFF WITH GROWL NOISES. REPLACED NR 1 ENG "A" PUMP PER AMM 29-11-11-400-802-0022. REPLACED RETURN FILTER PER AMM 29-15-61 AND EDP FILTER PER 29-15-91. RAN ENG NR 1, NO LEAKS NOTED. ROTABLE PARTS CHANGE INDICATED: PUMP, HYD ENGINE DRIVEN, PART NUMBER OFF 849589, SERIAL NUMBER OFF MX675875.

Part: CARGO TRACK — CORRODED (BS 787-827) · airframe 33,726 hrs · 10,973 cycles

AFT CARGO RIGHTHAND TIE DOWN RAIL HAS SURFACE CORROSION AT FASTENER HOLES BETWEEN STATION 787 AND 827. REMOVED TIE DOWN RAIL, FABRICATED AND INSTALLED REPAIR STRAP PER ECRA 5321-01550 AND REINSTALLED TIE DOWN RAIL.

Part: FRAME — CRACKED (BS 867 S9R) · airframe 33,726 hrs · 10,973 cycles

FRAME CRACKED AT STATION 867 ABOVE S9R. INSTALLED REPAIR PARTS PER EC/RA 5310-04763, REPAIRED FRAME PER EC/RA 5310-04763.

Part: FRAME — CRACKED (BS 827 S9R) · airframe 33,726 hrs · 10,973 cycles

FRAME CRACKED AT STATION 827 ABOVE S9R. INSTALLED REPAIR PARTS PER EC/RA 5310-04763, REPAIRED FRAME PER EC/RA 5310-04763.

Part: FRAME — CRACKED (BS 787 S9R) · airframe 33,726 hrs · 10,973 cycles

FRAME CRACKED AT STATION 787 ABOVE S9R. INSTALLED REPAIR PARTS PER EC/RA 5310-04763, REPAIRED FRAME PER EC/RA 5310-04763.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,726 hrs · 10,973 cycles

FRAME CRACKED AT STA 380 ABOVE S9R B737-53-3-0739. REPAIRED CRACKED FRAME BS 380 S9R PER EC/RA 5310-04763.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,726 hrs · 10,973 cycles

FRAME CRACKED AT STA 400 ABOVE S9R B737-53-3-0739. REPAIRED CRACKED FRAME BS 400 S9R PER EC/RA 5310-04763.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,726 hrs · 10,973 cycles

CABIN FLOOR SUPPORT CRACKED STATION 312 STATION 328 RBL 31.60. REMOVED AND REPLACED FLOOR SUPPORT LOCATED AT RBL 31.60 BETWEEN STATIONS 312-328 REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,726 hrs · 10,973 cycles

CABIN FWD ENTRY, INTERCOSTAL BETWEEN FLOORBEAMS STATION 312 TO 328 BY L-1 DOOR CRACKED. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,726 hrs · 10,973 cycles

CABIN FWD ENTRY, INTERCOSTAL BETWEEN STA 312 TO 328 BY L-1 DOOR CRACKED. REMOVED & REPLACED INTERCOSTAL REF SRM 51-40-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,685 hrs · 9,636 cycles

THE LEFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE DURING TEST. THE LEFT OVERWING BATTERY PACK WAS REPLACED IAW MM 33-51-06-960-804.

Part: FLOORBEAM — CORRODED (STA 986.5) · airframe 25,075 hrs · 8,143 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 24 TO RBL 38. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01312.

Part: INTERCOSTAL — CORRODED (STA 947.5-986.5) · airframe 25,075 hrs · 8,143 cycles

INSPECTION FOUND R-2 DOOR INTERCOSTAL CORRODED AT DRAIN HOLE, STA 947.5 TO 986.5, RBL 38. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (STA 967-986.5) · airframe 25,075 hrs · 8,143 cycles

INSPECTION FOUND R-2 DOOR CHORD CORRODED AT STA 967-986.5, RBL 45. THE R-2 DOOR CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (STA 967) · airframe 25,075 hrs · 8,143 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 0 TO RBL 51. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 25,075 hrs · 8,143 cycles

INSPECTION FOUND L-2 DOOR INTERCOSTAL CORRODED AT STA 947.5-967, LBL 62.

Part: BOLT — GALLED (LT HOR STAB) · airframe 19,488 hrs · 6,362 cycles

INSPECTION FOUND UPPER BOLT GALLED ON LT HORIZONTAL STABILIZER FORWARD POSITION. THE BOLT WAS REPLACED IAW EA 5510-01696, REV B, OP 1.

Part: PIN — CORRODED (LT HOR STAB) · airframe 19,488 hrs · 6,362 cycles

INSPECTION FOUND LT HORIZONTAL STABILIZER AFT MIDDLE AND AFT LOWER FAILSAFE PINS CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696, REV B, OP 1.

Part: PIN — CORRODED (HORIZ STAB) · airframe 19,488 hrs · 6,362 cycles

INSPECTION FOUND LT HORIZONTAL STABILIZER AFT UPPER FAILSAFE PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696, REV B, OP 1.

Part: SKIN — DENTED (CARGO DOOR) · airframe 17,143 hrs · 5,588 cycles

INSPECTION FOUND A DENT IN OUTER SKIN OF FORWARD CARGO DOOR AT AFT CENTER EDGE, BS 487.65. THE DENTED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01724 AND SRM 51-20-01.

Part: LIGHT — INOPERATIVE (ROW 14)

INSPECTION FOUND BOTH RED AND WHITE EMERGENCY EXIT AND AISLE LOCATOR LIGHTS AT ROW 14 INOPERATIVE. BOTH LIGHT FIXTURES WERE REPLACED.