N852NN

Part: DOOR — LACK OF LUBE (ZONE 800) · airframe 45,213 hrs · 19,249 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFTER LAVATORY DOOR STICKING. LUBED LAVATORY-D DOOR. PER CMM 25-44-49.

Part: LIGHT — DETACHED (ZONE 200) · airframe 44,656 hrs · 18,991 cycles

AIRCRAFT WAS NOT GROUNDED: LIGHT ABOVE OVERHEAD BIN AT ROW 25-27 (LEFT SIDE) IS DETACHED. RESECURED EMERGENCY LIGHT ABOVE OVERHEAD BIN ROW 25-27(LEFT SIDE).

Part: LIGHT — UNSECURE (ZONE 200) · airframe 44,575 hrs · 18,953 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT FRAME OVER ROW 12DEF IS LOOSEN. SECURED EMERGENCY LIGHT FRAME. PER AMM 33-51-00.

Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 44,035 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD AND AFT FLIGHT ATTANDENT SEAT EMERGENCY FLASHLIGHTS MISSING. INSTALLED FORWARD (AALA202507134816) AND AFT (AALA202507133586) FLIGHT ATTANDENT SEAT EMERGENCY FLASHLIGHTS AND PERFORMED SATISFACTORY TEST. PER B737-NG AMM 25-64-00.

Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 44,035 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD AND AFT FLIGHT ATTANDENT SEAT EMERGENCY FLASHLIGHTS MISSING. INSTALLED FORWARD (AALA202507134816) AND AFT (AALA202507133586) FLIGHT ATTANDENT SEAT EMERGENCY FLASHLIGHTS AND PERFORMED SATISFACTORY TEST. PER B737-NG AMM 25-64-00.

Part: STRINGER — CORRODED (ZONE 100) · airframe 44,034 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER 25L BETWEEN BS 845 AND BS 849. REPAIRED STRINGER PER SRM 53-00-03-2R-1.

Part: SKIN — CORRODED (ZONE 100) · airframe 44,034 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT AFT LAVATORY SERVICE PANEL BETWEEN BS 847 AND BS 867, BETWEEN S24L AND S25L. REPAIRED SKIN PER EA 365990.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 44,035 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: MULTIPLE EMERGENCY LIGHTS ARE OUT. SUSPECT BATTERY POWER SUPPLYTO BE BAD. REMOVED AND REPLACED 9RH BATTERY PACK. PER B737-NG-AMM 33-51-06 AND PERFORMED SATISFACTORY OPERATIONAL TEST OF EMERGENCY LIGHTS, PER B737NG AMM 33-51-00.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 44,034 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER, LEFT HAND WHEEL WELL, AT STA 663.75 FROM LBL 31.83 TO LBL 40. REPAIRED VAPOR BARRIER PER SRM 57-10-10-2R-2.

Part: DOOR — CRACKED (ZONE 700) · airframe 44,035 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT MLG CENTER DOOR LOWER FORWARD CORNER AREA CRACKED. REPAIRED LEFT MLG CENTER DOOR LOWER FORWARD CORNER. PER B737-SRM 52-80-02-2R-2- REPAIR 2.

Part: LIFE RAFT — MISINSTALLED (ZONE 800) · airframe 44,035 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER EMERGENCY ESCAPE LIFE RAFT NUMBER 3 IS POSITIONED INCORRECTLY. REMOVED AND REINSTALLED PASSENGER EMERGENCY ESCAPE LIFE RAFT NUMBER 3. PER B737NG AMM 25-24-40 AND 25-60-00 AND DWG DBF 2000 REV N.

Part: LIFE RAFT — MISINSTALLED (ZONE 800) · airframe 44,035 hrs · 18,700 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER EMERGENCY ESCAPE LIFE RAFT NUMBER 4 IS POSITIONED INCORRECTLY. REMOVED AND REINSTALLED PASSENGER EMERGENCY ESCAPE LIFE RAFT NUMBER 4. PER B737NG AMM 25-24-40 AND 25-60-00 AND DWG DBF 2000 REV N.

Part: PROBE — INACCURATE (NR 1 ENGINE) · airframe 43,413 hrs · 18,415 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: ENGINE NUMBER 1 EGT IN AMBER DURING CLIMB OUT MAX TEMP SEEN WAS 935. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SFO. CLEANED ALL CONNECTORS (AALA202504145215) J9 AND J10 HARNESS TO THE CJ9 AND CJ10 JUNCTION BOX. PER FIM 77-05 TASK 801. ADDTIONALLY, FOUND S3 INDICATION HIGH AND S4 BLANK. REPLACED S3 (AALA202504149958) AND S4 (AALA202504146002) T49.5 PROBE. PER AMM TASK77-21-01. OPERTIONAL CHECK NORMAL.

Part: PROBE — CONTAMINATED (NR 1 ENGINE) · airframe 43,413 hrs · 18,415 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: ENGINE NUMBER 1 EGT IN AMBER DURING CLIMB OUT MAX TEMP SEEN WAS 935. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SFO. CLEANED ALL CONNECTORS (AALA202504145215) J9 AND J10 HARNESS TO THE CJ9 AND CJ10 JUNCTION BOX. PER FIM 77-05 TASK 801. ADDTIONALLY, FOUND S3 INDICATION HIGH AND S4 BLANK. REPLACED S3 (AALA202504149958) AND S4 (AALA202504146002) T49.5 PROBE. PER AMM TASK77-21-01. OPERTIONAL CHECK NORMAL.

Part: PROBE — INACCURATE (NR 1 ENGINE) · airframe 43,413 hrs · 18,415 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: ENGINE NUMBER 1 EGT IN AMBER DURING CLIMB OUT MAX TEMP SEEN WAS 935. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SFO. CLEANED ALL CONNECTORS (AALA202504145215) J9 AND J10 HARNESS TO THE CJ9 AND CJ10 JUNCTION BOX. PER FIM 77-05 TASK 801. ADDTIONALLY, FOUND S3 INDICATION HIGH AND S4 BLANK. REPLACED S3 (AALA202504149958) AND S4 (AALA202504146002) T49.5 PROBE. PER AMM TASK77-21-01. OPERTIONAL CHECK NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 43,248 hrs · 18,352 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT HAND FORWARD EMERGENCY EXIT DOOR LIGHT INOPERATIVE. EMERGENCY LIGHT SYSTEM RESET. PER AMM 33-51-00. RIGHT HAND FORWARD EMERGENCY EXIT DOOR LIGHT OPERTIONAL TEST GOOD.

Part: WARNING LIGHT — ILLUMINATED (FUEL SYS) · airframe 42,021 hrs · 17,820 cycles

AIRCRAFT WAS GROUNDED: MASTER CAUTION FUEL WITH FLASHING AMBER LOW OIL PRESSURE NUMBER 1 ENGINE WHILE AT CRUISE FOR APPROXIMATELY FOR 30 SEC. THIS HAPPENED 2 TIMES AT CRUISE. ALL ENGINE INSTRUMENT READINGS WERE INDICATING NORMAL WITH NO ABNORMAL ENGINE OPERATION. **SUPPLEMENTAL REPORT FOR (AALA202410296040): AFTER REVIEWING THE FINAL ACTION, DETERMINED NOT TO BE A FUEL FLOW ISSUE, SO NOT REPORTABLE**(CLOSED).

Part: WARNING LIGHT — FALSE INDICATION (ENGINE OIL) · airframe 42,021 hrs · 17,820 cycles

AIRCRAFT WAS GROUNDED: MASTER CAUTION FUEL WITH FLASHING AMBER LOW OIL PRESSURE NUMBER 1 ENGINE WHILE AT CRUISE FOR APPROXIMATELY FOR 30 SEC. THIS HAPPENED 2 TIMES AT CRUISE. ALL ENGINE INSTRUMENT READINGS WERE INDICATING NORMAL WITH NO ABNORMAL ENGINE OPERATION. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: WEDGE — MISSING (RT TE FLAP) · airframe 41,532 hrs · 17,573 cycles

AIRCRAFT WAS GROUNDED: NOTICED MISSING FLAP REPAIR ON RIGHT HAND WING TRAILING EDGE FLAP. INSTALLED NEW WEDGE ASSEMBLY ON RIGHT HAND INBOARD. PER AMM 27-51-22.

Part: WEDGE — PUNCTURED (RT TE FLAP) · airframe 41,476 hrs · 17,541 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND INBOARD FLAP TRANSLATING WEDGE HAS PUNCTURE REQUIRES REPLACEMENT. Ï¿½ **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: WEDGE — PUNCTURED (ZONE 600 FLAP) · airframe 41,476 hrs · 17,541 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND INBOARD FLAP TRANSLATING WEDGE HAS PUNCTURE REQUIRES REPLACEMENT. Ï¿½ **SUPPLEMENTAL REPORT FOR (AALA202408138484): INSTALLED NEW WEDGE ASSEMBLY RIGHT HAND INBOARD, PER 27-51-22 AND EA 356992**(CLOSED).

Part: LIGHT — UNSECURE (ZONE 200) · airframe 41,349 hrs · 17,475 cycles

AIRCRAFT WAS NOT GROUNDED: LIGHT ASSEMBLY ABOVE THE OVERHEAD BIN AT 10 ABC NEEDS TO BE SECURED CURRENTLY HELD WITH TAPE. RESECURED ABOVE 10 ABC OVERHEAD BIN EMERGENCY AISLE LIGHT ASSEMBLY. PER AMM 33-51-03-960.

Part: GIRT BAR — OUT OF ADJUST (FWD SERVICE DOOR) · airframe 41,079 hrs · 17,354 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD RIGHT GALLEY DOOR GIRT BAR HARD TO OPERATE. REQUIRES LUBE AND ADJUSTMENT. ADJUSTED ATTACH FITTING AS NEEDED.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 39,754 hrs · 16,704 cycles

AIRCRAFT WAS NOT GROUNDED: CHRONIC HISTORY LAVATORY D DOOR DIFFICULT TO OPEN AND CLOSE.**SUPPLEMENTAL REPORT FOR (AALA202401291857): ADJUST LAVATORY D BIFOLD DOOR CENTER HINGE PIN. PER CMM 25-47-21. OPERATIONAL CHECK GOOD. **(OPEN).

Part: DOOR — FAULTED (LAVATORY) · airframe 39,754 hrs · 16,704 cycles

AIRCRAFT WAS NOT GROUNDED: CHRONIC HISTORY LAVATORY D DOOR DIFFICULT TO OPEN AND CLOSE.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: DOOR — LOOSE (ZONE 900 - LAV/G) · airframe 39,697 hrs · 16,675 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAVATORY DOOR HARD TO CLOSE AND HARD TO OPEN, GETTING STUCK. FOUND THE LAVATORY DOOR LOOSE. ADJUSTED THE LEFT LAVATORY DOOR. PER AMM 25-40-15.

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 39,668 hrs · 16,663 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR IS DIFFICULT TO OPEN AND CLOSE. ACCOMPLISHED READJUSTMENT OF AFT LEFT LAVATORY DOOR. PER AMM 52-00-00.

Part: HINGE — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 39,645 hrs · 16,650 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR DIFFICULT TO OPEN AND CLOSED. ADJUSTED AFT LAVATORY DOOR HINGE. PER CDA AMM 25-44-49. OPERATIONAL CHECK GOOD.

Part: HINGE — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 39,550 hrs · 16,596 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR DIFFICULT TO OPEN AND WON'T CLOSE. **SUPPLEMENTAL REPORT FOR (AALA202401058823): ADJUSTED AFT LAVATORY DOOR HINGE. PER CDA AMM 25-44-49. OPERATIONAL CHECK GOOD.**(CLOSED).

Part: UNKNOWN — UNKNOWN (ZONE 200 - FUSE) · airframe 39,550 hrs · 16,596 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR DIFFICULT TO OPEN AND WON'T CLOSE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

Part: STARTER — SEIZED (ZONE 400 - NAC/P) · airframe 37,880 hrs · 15,808 cycles

AIRCRAFT WAS GROUNDED: AFTER PUSHBACK, ENGINE #1 START, N2 AT ZERO. START ABORTED. ON SECOND START ATTEMPT, ABORTED START AGAIN, ENGINE FIRE INDICATION. BOTH FIRE BOTTLES DISCHARGED. MAINTENANCE FOUND #1 ENGINE STARTER SEIZED CAUSING AN OVERHEAT AND FIRE INDICATION. REPLACED STARTER PER AMM 80-11-01.

Part: WEB — CRACKED (ZONE 100 - FUSE) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON CENTER WING SECTION KEEL BEAM WEB AT STA 727 BETWEEN RIGHT BUTT LINE 31.83 AND RIGHT BUTT LINE 40.00. INSTALLED A REINFORCING MODIFICATION PER SRM 57-10-10-2R,

Part: SUPPORT — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON AFT BULKHEAD LOWER L SUPPORT RIGHT SIDE. LOCATED BETWEEN STA 360 AND 540 AND RIGHT BUTT LINE 43

Part: BAFFLE — CRACKED (ZONE 100) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND BAFFLE LOCATED BELOW FORWARD CARGO COMPARTMENT FROM BS 460 TO BS 480 AT LBL 21. REPLACED BAFFLE PER DWG 143A7505 SHEET 4. AND AARD 51-00-05-1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT STRUCTURE BREAK ASSEMBLY LOCATED AT BS 540 BETWEEN BL 0 AND RBL 23. REPLACED BREAK ASSEMBLY PER AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200 - FUSE) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN CABIN FLOOR SUPPORT LOCATED AT BS 540 BETWEEN BL 0 AND LBL 23. REPLACED FLOOR SUPPORT PER AARD 51-00-05-01.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM FASTENER HOLE LOCATED AR BS 986.5 AND RBL 43. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6, PROCEDURE 4.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR RIGHT HAND CREASE ANGLE AT 2R DOOR, LOCATED FROM BS 947 TO BS 986.5 AT RBL 46. REPLACED CREASE ANGLE PER AARD 51-00-05-1 AND SRM 51-40-01.

Part: INTERCOSTAL — CORRODED (ZONE 200 - FUSE) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN AFT ENTRY FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN BS 947 AND BS 962, AT LBL 25. REPLACED INTERCOSTAL PER SRM 53-70-51.**SUPPLEMENTAL REPORT FOR AALA202209296528: ENGINEERING REVIEWED THIS EVENT AND DETERMINED THE CORRECT LEVEL WAS LEVEL 2 NOT LEVEL 1. SECTION 7 CORROSION LEVEL FIELD WAS CORRECTED ACCORDINGLY**

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED BETWEEN BS 727B AND BS 727I, AT LBL 45. REPAIRED TRANSITION PANEL PER SRM 53-00-53-2R REPAIR 5.

Part: RIB — CRACKED (ZONE 300) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER RIB LOCATED AT STABILIZER STA 92.70, SECOND STIFFENER FROM FRONT. REPLACED RIB PER AARD 55-10-00-2 AND DWG 182A5301 AND SRM 51-40-02.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED BETWEEN BS 727B AND BS 727D, AT RBL 45. REPAIRED PER SRM 53-00-53-2R 5, EA339032 AND EA339032A.

Part: FLOOR SUPPORT — CORRODED (BS 947-957) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN INTERCOSTAL FLOOR SUPPORT LOCATED BETWEEN BS 947 AND 957, AT LBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1, SRM 51-40-02, AND SRM 51-10-02-0G.

Part: FLOORBEAM — CORRODED (BS 967 RBL 47) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION AROUND FLOORBEAM FASTENER HOLE LOCATED AT BS 967, AT RBL 47. REPAIRED FLOORBEAM PER EA 339080.

Part: FLOOR SUPPORT — CORRODED (BS 947-967 RBL50) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT INTERCOSTAL LOCATED FROM BS 947 TO BS 967, AT RBL 50. REPLACED INTERCOSTAL PER EA 339080 AND AARD 51-00-05.

Part: FLOOR SUPPORT — CORRODED (BS 947-962) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN AFT ENTRY FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN BS 947 AND BS 962, AT LBL 25. REPLACED INTERCOSTAL PER SRM 53-70-51.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM FASTENER HOLE LOCATED AT BS 986.5 AND LBL 43. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR SUPPORT LOCATED AT BS 951 AND RBL 17. REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER RIB, LOCATED AT STABILIZER STA 92.70. THIRD STIFFENER FROM THE FRONT. REPLACED RIB PER AARD 55-40-02, BOEING DWG #182A5301 AND SRM 51-40-02.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 147.90, 8 INCHES FROM FORWARD SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 138.70, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (ZONE 300 - STABS) · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 101.90, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.

Part: SUPPORT BRACKET — CORRODED (BS 360 S26L) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND SUPPORT L BRACKET LOCATED AT BS 360 AND S26L AT BL 0 REPLACED L BRACKET PER AARD 51-00-05-1 AND DWG 143A9485.

Part: ANGLE — CORRODED (BS 294-328 RBL57) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR CREASE ANGLE LOCATED FROM BS 294.5 TO BS 328 AT RBL 57. REPLACED CREASE ANGLE PER SRM 51-00-05-1.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT DOOR THRESHOLD WEB, LOCATED FROM BS 440 TO BS 490 AT RBL 25. REPLACED WEB PER AARD 51-00-05-1 AND BOEING DWG 143A8122.

Part: NONE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT LEFT HAND TRANSITION PANEL LOCATED BETWEEN BS 500A AND BS 500I, AT S26L, AND LBL 15. REPLACED TRANSITION PANEL PER SRM 51-40-02 AND AARD 51-00-05-1.

Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOORWAY WEB LOCATED FROM BS 807 TO BS 813, AT STR 25R. REPLACED WEB PER AARD 51-00-05.

Part: TRANSITION PANEL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 360 TO BS 540 AT RBL 15, S26R. REPLACED TRANSITION PANEL PER SRM 51-40-02.

Part: WEB — CORRODED (BS 500-500A) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT HAND TRANSITION SHIELD WEB LOCATED FROM BS 500 TO BS 500A, AT RBL 24. REPLACED TRANSITION SHIELD WEB PER SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 767-787) · corrosion level 2 · airframe 36,012 hrs · 14,913 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND TRANSITION PANEL LOCATED FROM BS 767 TO BS 787, S26R, RBL 15. REPLACED TRANSITION PANEL PER SRM 51-00-05-02.

Part: NONE — NONE · airframe 35,287 hrs · 14,568 cycles

AIRCRAFT WAS GROUNDED: #2 ENGINE OIL QUANTITY DROPPED TO ZERO. OIL PRESSURE DROPPED TO RED LINE. CREW SHUT DOWN #2 ENGINE. EMERGENCY DECLARED; FLIGHT DIVERTED TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: ENGINE — LEAKING (ZONE 400 - NAC/P) · airframe 35,287 hrs · 14,568 cycles

AIRCRAFT WAS GROUNDED: #2 ENGINE OIL QUANTITY DROPPED TO ZERO. OIL PRESSURE DROPPED TO RED LINE. CREW SHUT DOWN #2 ENGINE. EMERGENCY DECLARED; FLIGHT DIVERTED TO PLS LANDING SAFELY. **SUPPLEMENTAL REPORT FOR AALA202205311741: REPLACED #2 ENGINE PER JOB CARD 08L40072003. ACCOMPLISHED SATISFACTORY OPERATIONAL AND LEAK CHECKS.** (CLOSED)

Part: NONE — NONE · airframe 33,806 hrs · 13,906 cycles

AIRCRAFT WAS NOT GROUNDED: CENTER AISLE FLOORBOARD AT ROW 2 MAKES A POPPING NOISE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)

Part: FLOORBOARD — DAMAGED (ZONE 200 - FUSE) · airframe 33,806 hrs · 13,906 cycles

AIRCRAFT WAS GROUNDED: CENTER AISLE FLOORBOARD AT ROW 2 MAKES A POPPING NOISE. **SUPPLEMENTAL REPORT: REPLACED CENTER AISLE FLOORBOARD AT ROW 2 WITH NEW IAW AMM 53-21-00.** (CLOSED)

Part: HANDLE — UNSECURE (LAVATORY DOOR) · airframe 32,652 hrs · 13,374 cycles

AIRCRAFT WAS NOT GROUNDED: FWD LAVATORY DOOR HANDLE FALLING OFF FRAME OF DOOR. SECURED FWD LAV DOOR HANDLE IAW AMM 25-40-11, OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (ZONE 200 - FUSE) · airframe 31,945 hrs · 13,078 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT OVERWING EXIT LIGHT INTERMITTENT. FLICKERS RED AND WHITE. RESECURED CONNECTOR AT LEFT AFT OVERWING EXIT LIGHT PER AMM 33-21-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,867 hrs · 13,040 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND LEFT AFT EMERGENCY EXIT HATCH LIGHT INOPERATIVE. RELAMPED LEFT AFT EMERGENCY LIGHT EXIT HATCH.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 28,482 hrs · 11,560 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL PRESSURE WEB CRACKED AT BS 663 AND RBL 33 AT WL 204. REPAIRED PRESSURE WEB PER SRM 57-10-10-2R-4 AND EA 298605.

Part: FLOOR PANEL — CORRODED (BS 500D-500I) · corrosion level 2 · airframe 27,158 hrs · 10,937 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT FLOOR PANEL BETWEEN BS 500D AND BS 500I, BETWEEN LBL 21 AND RBL 21. REPLACED FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 26,072 hrs · 10,458 cycles

MAIN CABIN FLOOR PANEL WAS SOFT BETWEEN SEATS 4AB - 4EF. REPLACED THE FLOOR PANEL IAW AMM 53-21-00.

Part: LENS — MISSING (CABIN) · airframe 23,564 hrs · 9,346 cycles

AIRCRAFT WAS NOT GROUNDED. DURING CRUISE IT WAS DISCOVERED THE 4L DOOR EMERGENCY LIGHT COVER WAS MISSING. REPLACED MISSING LENS PER AMM 33-51-01-201.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 23,569 hrs · 9,348 cycles

DURING CRUISE, DISCOVERED THAT THE L4 DOOR EMERGENCY LIGHT LENS WAS MISSING. REPLACED THE LENS IAW AMM 33-51-01-201. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 22,515 hrs · 8,888 cycles

THE AIRCRAFT WAS NOT GROUNDED. EXIT SIGN OVER AFT ENTRY DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY (EXIT) AT L-2 DOOR PER AMM 52-20-00 OK FOR SVC.

Part: LIGHT — BROKEN (CABIN) · airframe 21,390 hrs · 8,431 cycles

EMERG EXIT LENS MISSING AT DOOR AFT ENTRY. REMOVED & REPLACED BROKEN EMERGENCY LIGHT ASSEMBLY AT AFT LEFT DOOR ENTRY. OPS GOOD IAW MM 33-51-00. THE AIRCRAFT WAS GROUNDED.

Part: BEAM — WORN (BS 540-550) · airframe 19,633 hrs · 7,714 cycles

CENTER WING SUPPPORT BEAM WORN BY DOOR 192DR OUTBOARD LATCH. REPAIRED BEAM IAW EA 263080.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 19,633 hrs · 7,714 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED 18 INCHES AFT OF LEADING EDGE AT HSS 129.5. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,633 hrs · 7,714 cycles

AIRCRAFT WAS GROUNDED. FORWARD CARGO COMPARTMENT FLOORBOARD SUPPORT AT FS 500I IS CORRODED BETWEEN RBL 24 AND LBL 24. R & R FLOORBOARD SUPPORT IAW AARD 51-00-05.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,731 hrs · 7,356 cycles

AIRCRAFT WAS NOT GNDED. EMER PATH LIGHT ASSEMBLY AT SEAT ROW 20 DEF IS INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 33-51-11 & ACCOMPLISHED OPERATIONAL CHECK. SYS CHECKED GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 16,343 hrs · 6,402 cycles

POWER SUPPLY M1671 FAILED DURING EMER FUNCTIONAL CHECK. R & R POWER SUPPLY M1671 IAW AMM 33-51-06. SYS CHECKED NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 13,743 hrs · 5,366 cycles

FORWARD GALLEY EMER FLOOD LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM 33-51-01. SYS CHECKED NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 13,743 hrs · 5,366 cycles

AFT LEFT GALLEY EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM 33-51-01. SYS CHECKED NORMAL.

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,581 hrs · 5,307 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING APPROACH FLAPS STOPPED AT 5 DEGREES. ACCOMPLISHED QRH PROCEDURES & LANDED WITH FLAPS AT 15 DEGREES. SYS TESTED NORMAL NO FINDINGS.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 907 TO 927, STRINGERS 26 TO 27 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 907 TO 927, STRINGERS 21 TO 22 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 907 TO 927, STRINGERS 22 TO 24 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 907 TO 927, STRINGERS 24 TO 25 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · airframe 6,536 hrs · 2,593 cycles

CORROSION ON SKIN FROM STATIONS 927 TO 947, STRINGERS 21 TO 22 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 888 TO 907, STRINGERS 24 TO 26 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 1016 TO 1040, STRINGERS 21 TO 23 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 967 TO 986, STRINGERS 22 TO 24 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 927 TO 947, STRINGERS 22 TO 24 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 888 TO 907, STRINGERS 26 TO 27 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 1064 TO 1088, STRINGERS 20 TO 23 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 947 TO 967, STRINGERS 22 TO 24 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 947 TO 967, STRINGERS 21 TO 22 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 986 TO 1006, STRINGERS 23 TO 24 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 967 TO 986, STRINGERS 21 TO 22 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 986 TO 1016, STRINGERS 21 TO 23 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

AFT LAVATORY VENT EXTERIOR SKIN CORRODED. REMOVED CORROSION PER SRM 51-10-02 AND REPLACED DAMAGED FASTENERS PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 907 TO 927, STRINGERS 24 TO 26 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 1040 TO 1064, STRINGERS 19 TO 20 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,511 hrs · 2,582 cycles

CORROSION ON SKIN FROM STATIONS 1016 TO 1040, STRINGERS 20 TO 21 LEFT. ACCOMPLISHED CORROSION REMOVAL PER EA B737-53-026145.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 6,384 hrs · 2,538 cycles

SIDEWALL EXIT IDENTIFIER SIGNS AT ROW 15 LEFT AND RIGHT SIDE WOULD NOT REMAIN ON. REPLACED BATTERY PACK M1695. OPS CHECK NORMAL.