N907NN

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 200) · airframe 36,218 hrs · 15,672 cycles

AIRCRAFT WAS NOT GROUNDED: AUTO BRAKE DISARM LIGHT ILLUMINATES DURING PREFLIGHT WHEN SWITCH SELECTED TO RTO, THIS IS A REPEAT ITEM. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: AUTOTHROTTLE SYS — FAULTED (ZONE 700) · airframe 36,218 hrs · 15,672 cycles

AIRCRAFT WAS NOT GROUNDED: AUTO BRAKE DISARM LIGHT ILLUMINATES DURING PREFLIGHT WHEN SWITCH SELECTED TO RTO, THIS IS A REPEAT ITEM. **SUPPLEMENTAL REPORT FOR (AALA202503132003): REPLACED RIGHT HAND (ATSP)-AUTO THROTTLE SWITCH PACK ASSEMBLY, OPERTIONAL CHECK GOOD. PER J/C 08L11276002 FOR ALL SIGNATURES AND WORK ACCOMPLISHED**(CLOSED).

Part: GIRT BAR — OUT OF TOLERANCE (ZONE 800) · airframe 36,080 hrs · 15,606 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED AFT SERVICE DOOR GIRT BAR HARD TO OPERATE. LEFT WITH TOO MUCH GREASE TO OPERATE SAFELY. VERIFIED AFT RIGHT EMERGENCY DOOR GRIT BAR RETAINER CLIPS ARE ABNORMALLY TIGHT. BENT RETAINER CLIPS TO THE RIGHT DIMENSIONS.

Part: CONTROL UNIT — FAILED (ZONE 100) · airframe 35,991 hrs · 15,562 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: DURING APPROACH AUTO THROTTLE MOVEMENT WAS NOT SYMMETRICAL WITH NUMBER 2 THRUST LEVER LEADING NUMBER 1 BY ONE KNOB LENGTH. AT GLIDESLOPE INTERCEPT NUMBER 2 THRUST LEVER ADVANCED TOWARD GO AROUND THRUST WITH NUMBER 1 THROTTLE LAGGING BY APPROXIMATELY 5 KNOB LENGTHS; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. REPLACED FLIGHT CONTROL COMPUTER-A. PER MM 22-11-33 AND ACCOMPLISHED DFCS TEST PER MM 23-11-00, OPERTIONAL CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,885 hrs · 15,511 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING CLIMB WE HAD A VERY STRONG BURNING SMELL. PLASTIC OR ELECTRICAL; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT MIA. ACCOMPLISHED W/C 08L00021001 AND NO ODOR FOUND, NO FAULT FOUND.

Part: BATTERY — NO TEST (ZONE 200) · airframe 35,290 hrs · 15,228 cycles

AIRCRAFT WAS NOT GROUNDED: AFT GALLEY FLASHLIGHT BLINKING RED. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT IN AFT FLIGHT ATTENDENT JUMPSEAT STOWAGE COMPARTMENT. OPERTIONAL CHECK GOOD. PER AMM 25-64-00.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL ANGLE FROM STA 380 TO STA 400, LBL 13. REPLACED ANGLE PER AARD 51-00-05-1.

Part: FLOORBEAM — OUT OF TOLERANCE (ZONE 200) · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES IN AFT PASSENGER CABIN GALLEY FLOOR STRUCTURE Z ANGLE AT STA 993, FROM RBL 37 TO RBL 43. REPLACED ANGLE PER AARD 51-00-05-1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, RBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM STA 320 TO STA 344, LBL 45. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, LBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL FROM STA 500B TO STA 500I, S25L. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947, RBL 53. REPAIRED CHORD PER SRM 53-70-51-2R-5.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT FLOOR STRUCTURE TRANSITION PANEL FROM STA 727 PLUS 4 INCHES TO 727B PLUS 7 INCHES, S25R. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R-5.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 947, FROM LBL 13 TO RBL 13. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-70-51-2R-8.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 948, RBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,214 hrs · 15,191 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION SHIELD FROM STA 767 TO STA 787, S25R. REPLACED TRANSITION SHIELD PER AARD 51-00-05-1A.

Part: SKIN — GOUGED (BS 1000-1016) · airframe 34,214 hrs · 14,670 cycles

AIRCRAFT WAS GROUNDED: FOUND GOUGE AFT OF RIGHT HAND AFT SERVICE DOOR BETWEEN BS 1000 TO 1016 AND STR 11R TO 12R. ACCOMPLISHED PERMINENT SKIN REPAIR. NO FURTHER DAMAGE NOTED. PER AARD 11-20-00.

Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 34,214 hrs · 14,670 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS GALLEY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FLIGHT ATTANDENT FLASHLIGHT IN THE FIRST CLASS GALLEY. OPERTIONAL CHECK GOOD. PER AMM 25-64-00.

Part: SEAL — UNSECURE (LAVATORY DOOR) · airframe 34,017 hrs · 14,577 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY-D ENTRY DOOR DIFFICULT TO OPEN OR CLOSE. SECURED DOOR SEAL BEARING, OPERTIONAL CHECK GOOD. PER AMM 25-40-14.

Part: LIGHT — UNSECURE (ROW 8ABC) · airframe 33,980 hrs · 14,560 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 8ABC EXIT LIGHTING HANGING FROM BOTTOM OF SEAT. RE-INSTALLED AND SECURED LIGHT COVER CAP ON ROW 8ABC. PER AMM 33-51-11.

Part: DOOR — OUT OF POSITION (LAVATORY) · airframe 33,788 hrs · 14,469 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR DIFFICULT TO OPEN. REPOSITIONED AFT LEFT LAVATORY DOOR. PER AMM 25-40-00.

Part: GIRT BAR — OUT OF POSITION (FWD SERVICE DOOR) · airframe 33,579 hrs · 14,372 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD SERVICE DOOR IS DIFFICULT TO ARM. GIRT BAR IS HAVING TROUBLE TO SLIDE INTO PLACE. FOUND 'Z' FOLD NOT IN CORRECT R1 DOOR FRONT SIDE. RESTABLISHED 'Z' FOLD IN GIRT.

Part: SLIDE RAFT — DISLODGED (R1 DOOR) · airframe 33,571 hrs · 14,368 cycles

AIRCRAFT WAS NOT GROUNDED: 1R DOOR SLIDE IS FALLING OUT OF ITS HOLDER. MAINTENANCE REMOVED, ADJUSTED, REINSTALL SLIDE PACK I.A.W. AMM 25-66-01.

Part: UNKNOWN — UNKNOWN (ZONE 900 - LAV/G) · airframe 33,035 hrs · 14,115 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY-D VERY DIFFICULT TO LOCK AND UNLOCK.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: SHADE — DAMAGED (ZONE 800 - DOORS) · airframe 31,874 hrs · 13,570 cycles

AIRCRAFT WAS NOT GROUNDED: 17A WINDOW SHADE CRUMPLED. **SUPPLEMENTAL REPORT FOR AALA202308014434: REPLACED WINDOW SHADE PER AMM 25-21-12.** (CLOSED)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 31,874 hrs · 13,570 cycles

AIRCRAFT WAS NOT GROUNDED: 17A WINDOW SHADE CRUMPLED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: SLIDE — LOOSE (ZONE 800 - DOORS) · airframe 31,704 hrs · 13,486 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT DOOR SLIDE IS VERY LOOSE. SECURED SLIDE MOUNTING SCREW PER AMM 25-66-00.

Part: HANDLE — LOOSE (ZONE 900 - LAV/G) · airframe 30,925 hrs · 13,093 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE IS LOOSE AND DIFFICULT TO OPEN. TIGHTENED SCREW ON FORWARD LAVATORY HANDLE. OPERATES NORMAL.

Part: SLIDE — OUT OF POSITION (ZONE 800 - DOORS) · airframe 28,591 hrs · 11,950 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE 4L EMERGENCY EQUIPMENT AND FLAPS ARE HANGING OUT NOT SECURE. RE-SECURED SAFETY POUCH AT DOOR 4L PER AMM 25-66-01.

Part: ENGINE — VIBRATION (ZONE 400 - NAC/P) · airframe 28,437 hrs · 11,873 cycles

AIRCRAFT WAS GROUNDED: CLIMBING THROUGH 22,000 FEET WITH ENGINE ANTI ICE ON, NUMBER 1 ENGINE LOST THRUST AND EXHIBITED EXCESSIVE VIBRATION. REDUCED THRUST BUT COULD NOT ACHIEVE MORE THAN 40% WITHOUT VIBRATION SO SHUT ENGINE DOWN. EMERGENCY WAS DECLARED AND AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED LEFT ENGINE PER JOBCARD 08L40072003.

Part: NONE — LOOSE (ZONE 900 - LAV/G) · airframe 28,170 hrs · 11,743 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HANDLE IS LOOSE. RESECURED DOOR HANDLE PER AMM 20-50-11.

Part: GIRT BAR — OUT OF POSITION (ZONE 800 - DOORS) · airframe 27,986 hrs · 11,656 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR GIRT BAR ARM FLAG TOO SHORT. ADJUSTED R1 DOOR GIRT BAR ARM FLAG PER B737 NG AMM 25-66-00-840-801.

Part: SMOKE DETECTOR — FAILED (ZONE 100 - FUSE) · airframe 27,985 hrs · 11,655 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD CARGO SMOKE DETECTOR M2240 FAILS BUILT IN TEST EQUIPMENT CHECK. REMOVED AND REPLACED CARGO SMOKE DETECTOR M2240, OPERATIONS TEST CHECKS GOOD PER B737NG AMM 26-16-01 & 26-16-00.

Part: LIGHT — OUT OF POSITION (ZONE 200 - FUSE) · airframe 27,985 hrs · 11,655 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT ASSEMBLY INSTALLED INCORRECTLY AT ROW 17. ADJUSTED EXIT LIGHT ASSEMBLY IAW BOEING 737NG AMM 33-51-01, OPS CHECK GOOD.

Part: WARNING HORN — ACTIVATED (CONFIGURATION) · airframe 27,844 hrs · 11,584 cycles

AIRCRAFT WAS NOT GROUNDED: INFO TO MAINTENANCE ABORTED TAKE OFF TUL. TAKE OFF CONFIGURATION HORN AND LIGHT APPROXIMATELY 60 KNOTS CONSULTED QUICK REFERENCE HANDBOOK. RECYCLED FLAPS AND STABILIZERS TRIM SPOILERS, 2ND TAKE OFF ATTEMPT NORMAL.

Part: LATCH — LACK OF LUBE (LAVATORY DOOR) · airframe 26,510 hrs · 10,973 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT AFT LAVATORY LOCK DIFFICULT TO OPERATE. LUBRICATED DOOR LATCH.

Part: MODULE — FAULTY (OVERHEAT SYS) · airframe 26,147 hrs · 10,822 cycles

AIRCRAFT WAS GROUNDED: AT APPROXIMATELY 10,000 FEET ENGINE 2 OVERHEAT LIGHT ILLUMINATED. ENGINE 1 FIRE LIGHT AND ENGINE 1 OVERHEAT DOES NOT TEST. RETURNED TO FIELD. REPLACED CHAFED HARNESS MW0325 (AALA202106189013) PER AMM 26-11-02 AND AMM 26-10-01. REPLACED ENGINE AND APU FIRE AND OVERHEAT DETECTION CONTROL MODULE (AALA202106219002) PER AMM 26-10-01.

Part: WIRE HARNESS — CHAFED · airframe 26,147 hrs · 10,822 cycles

AIRCRAFT WAS GROUNDED: AT APPROXIMATELY 10,000 FEET ENGINE 2 OVERHEAT LIGHT ILLUMINATED. ENGINE 1 FIRE LIGHT AND ENGINE 1 OVERHEAT DOES NOT TEST. RETURNED TO FIELD. **SUPPLEMENTAL REPORT: REPLACED CHAFED HARNESS MW0325 (AALA202106189013) PER AMM 26-11-02 AND AMM 26-10-01. REPLACED ENGINE AND APU FIRE AND OVERHEAT DETECTION CONTROL MODULE (AALA202106219002) PER AMM 26-10-01.

Part: WIRE HARNESS — FAULTED (NR 2 ENGINE) · airframe 26,143 hrs · 10,819 cycles

AIRCRAFT WAS GROUNDED: ENGINE 2 OVERHEAT INDICATION CLIMBING OUT OF 12000 MSL. REPLACED ENGINE 2 FIRE DETECTION HARNESS MW0326 PER AMM 26-11-00-710-801.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 25,998 hrs · 10,751 cycles

AIRCRAFT WAS NOT GROUNDED: ONE CABIN MEGAPHONE INOPERATIVE. REPLACED BATTERIES PER AMM 25-64-00.

Part: LATCH — BINDING (CLOSET) · airframe 25,952 hrs · 10,725 cycles

AIRCRAFT WAS NOT GROUNDED: CLOSET DOOR HARD TO OPEN BY 1L DOOR. ADJUSTED LATCH MECHANISM ON CLOSET DOOR BY L1 ENTRY DOOR AS REQUIRED

Part: STRAP — MISSING (R1 DOOR) · airframe 25,010 hrs · 10,317 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 1R INDICATION STRAP MISSING. AIRCRAFT DISPATCHED ON MEL 25-61A. REPLACED R1 DOOR ORANGE STRAP VISUAL INDICATOR, IAW AMM 52-11-31.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 21,792 hrs · 8,841 cycles

AIRCRAFT WAS GROUNDED: LEFT WING INBOARD AFT FLAP TRAILING EDGE DELAMINATED 29 INCHES OUT BOARD OF THE INBOARD END. REPAIRED FLAP PER EA 297024.

Part: TRANSITION PANEL — CORRODED (BS 500B-500I) · corrosion level 2 · airframe 19,288 hrs · 7,760 cycles

CORROSION ON FORWARD CARGO BA7 LEFT TRANSITION PANEL BETWEEN BS 500B AND 500I. REPLACED THE TRANSITION PANEL IAW SRM 53-00-532-2R5.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 19,287 hrs · 7,760 cycles

RIGHT WHEEL WELL BULKHEAD WEB, AT BS 663 WAS CRACKED. REPAIRED THE BULKHEAD WEB IAW 57-10-10-9, AND SRM 57-10-10-2R2.

Part: TRANSITION PANEL — CORRODED (BS 500A-500I) · corrosion level 2 · airframe 19,288 hrs · 7,760 cycles

CORROSION ON FORWARD CARGO COMPARTMENT RIGHT TRANSISTION PANEL, BETWEEN BS 500A AND 500I. REPLACED TRANSITION PANEL IAW SRM 53-00-53-2R5.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 19,288 hrs · 7,760 cycles

CRACKED CABIN FLOOR SUPPORT AT BS 540 AND RBL 2. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 19,288 hrs · 7,760 cycles

CRACKED CABIN FLOOR SUPPORT AT BS 540 AND LBL 2. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (BS 727G-727H) · corrosion level 2 · airframe 19,288 hrs · 7,760 cycles

CORROSION FOUND ON THE AFT CARGO, LEFT TRANSITION PANEL BETWEEN BS 727G AND 727H. REPLACED THE TRANSITION PANEL IAW 51-00-05-1, AND SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (BS 747-767) · corrosion level 2 · airframe 19,288 hrs · 7,760 cycles

CORROSION FOUND ON THE AFT CARGO RIGHT TRANSITION PANEL BETWEEN BS 747 AND 767. REPLACED THE TRANSISTION PANEL IAW SRM 53-00-53-2R, AND 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 19,288 hrs · 7,760 cycles

CRACKED CABIN FLOOR SUPPORT BETWEEN BS 312 TO 328, LBL 42. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 19,288 hrs · 7,760 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 312 AND 328, RBL 30. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 19,288 hrs · 7,760 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 344 -360, LBL 11. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 17,815 hrs · 7,121 cycles

AISLE EMERGENCY LIGHT LENS AT ROW 8 ABC IS DAMAGED. REPLACED THE LENS IAW AMM 33-21-03.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 17,578 hrs · 7,025 cycles

EXIT SIGN MISSING, AFT OF PASSNEGER DOOR NEXT TO TRASH CAN IN GALLEY RIGHT OF GALLEY DOOR. REPLACED THE EXIT SIGN AND LENS IAW 33-51-01.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 17,045 hrs · 6,809 cycles

AIRCRAFT WAS NOT GROUNDED: INTERMITTENT LAVATORY SMOKE MASTER CAUTION ON SIX PACK OVERHEAD LIGHTS IN CRUISE FLIGHT. MAINTENANCE ACCOMPLISHED LAVATORY SMOKE DETECTOR SYSTEM TEST PER AMM 26-14-00 ON ALL LAVATORIES. NO FAULTS NOTED AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 17,032 hrs · 6,802 cycles

AFT RIGHT EXIT DOOR EXIT SIGN IS MISSING. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-01.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 16,030 hrs · 6,374 cycles

AIRCRAFT WAS NOT GROUNDED. LAVATORY SMOKE LIGHT ILLUMINATED DURING CRUISE WITH NO KNOWN ISSUES, FLIGHT ATTENDANTS FOUND NO SMOKE OR HEAT IN LAVATORIES. SELF TESTED LAVATORY SMOKE DETECTORS PER AMM 26-14-00. UNABLE TO DUPLICATE FAULT. OPERATIONAL CHECK GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 15,716 hrs · 6,244 cycles

THE AIRCRAFT WAS NOT GROUNDED. LAVATORY SMOKE LIGHTS AND CHIME ON 2.5 HOURS INTO CRUISE. FLIGHT ATTENDANTS REPORTED NO FIRE OR SMOKE FROM LAVATORY L4, (AFT LEFT LAVATORY). ACCOMPLISHED CHECK AND UP TEST PER 26-14-00. OP CK NORMAL.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 15,594 hrs · 6,188 cycles

EMERGENCY EXIT SIGN BY THE R1 DOOR IS DAMAGED. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,164 hrs · 6,022 cycles

LENS FOR THE EMERGENCY LIGHT ABOVE THE R4 DOOR MISSING. MAINTENANCE REPLACED THE LENS IAW AMM 33-51-02.

Part: COVER — DAMAGED (GALLEY LIGHT) · airframe 14,821 hrs · 5,879 cycles

GALLEY LIGHT COVER BROKEN OFF. STRAIGHTENED LIGHT COVER AND INSTALLED, OK FOR SERVICE. THE AIRCRAFT WAS NOT GROUNDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,886 hrs · 5,506 cycles

AIRCRAFT NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 DOOR OUTBOARD SEAT HAS A LOW BATTERY. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 13,187 hrs · 5,207 cycles

FLOOR SUPPORT CRACKED AT LBL 46 BETWEEN BS 312 AND 328. REMOVED AND REPLACED IAW SRM 51-40-02, AARD 51-00-05-01 AND DRAWING 141A5410.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 13,187 hrs · 5,207 cycles

FORWARD LOWER PRESSURE SEAL LANDING FITTING AT L2 DOOR CUTOUT IS CRACKED. REMOVED AND REPLACED LANDING IAW 51-00-05 REPAIR 1, DRAWING 147A8204 AND EA 264380.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 13,187 hrs · 5,207 cycles

FLOOR SUPPORT CRACKED AT LBL 46 BETWEEN BS 328 AND 344. REMOVED AND REPLACED IAW SRM 51-40-02, 51-00-05-01 AND DRAWING 141A5410.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,967 hrs · 5,101 cycles

EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT ROWS 16 AND 20. REMOVED AND REPLACED EMERGENCY POWER SUPPLY M1671 IAW AMM 33-51-06. OPS CHECKED NORMAL.

Part: ADIRU — FAILED (ZONE 100) · airframe 10,858 hrs · 4,246 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB THE RT IRS FAULT & ALIGN LIGHT ILLUMINATED. R & R RT ADIRU IAW AMM 34-21-00. SYS CHECKED NORMAL.

Part: OVERHEAT LOOP — CHAFED (NR 2 ENGINE) · airframe 9,300 hrs · 3,630 cycles

DURING CRUISE PILOT REPORTED NUMBER 2 ENGINE OVERHEAT LIGHT ILLUMINATED. DIVERTED AND LANDED UNEVENTFULLY. FOUND NUMBER 2 ENGINE LOOP `A` WIRE CHAFED. R & R RT ENGINE OVERHEAT LOOP. PERFORMED OPERATIONAL CHECK IAW AMM 26-11-02. SYS CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,486 hrs · 2,577 cycles

LIGHT SURFACE CORROSION ON LOWER FUSELAGE SKIN FROM STATIONS 888 TO 1016 & STRINGERS 21 TO 25 LT. CORROSION R & R ACCOMPLISHED IAW EA B737-53-036943.

Part: SELECTOR VALVE — INOPERATIVE (LANDING GEAR) · airframe 5,271 hrs · 2,099 cycles

MIA CREW REPORTED LG WOULD NOT RETRACT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LG SELECTOR VLV. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: WIRE — GROUNDED (CABIN) · airframe 786 hrs · 322 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROWS 8 TO 12 INOPERATIVE. FOUND ROW 8 HAD ONE WIRE FOR LIGHT GOUNDING OUT ON SEAT FRAME. REPLACED BATTERY PACK AND ROW 8 LIGHT SOCKET ASSEMBLY. OPS CHECK NORMAL.