N3762Y

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 69,471 hrs · 26,249 cycles

DURING SVC CHK FOUND EMERGENCY EXIT LIGHT AT ROW 22 INOPERATIVE. R & R BATTERY PACK BP1670 PER AMM 33-51. OPS CHK GOOD.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 69,416 hrs · 26,228 cycles

(LOG 1106625) SEAT TRACK DAMAGE AT STA 727I AND SEAT ROW 27ABC. INSTALLED AND REPAIRED SEAT TRACK LH OTBD SECTION FROM 727G TO 727J PER B737-800 SRM 53-00-52-2R PROCEDURE 5 (001971) INSPECTED INSTALLATION OF REPAIR OF SEAT TRACK PER SRM 53-00-52-2R PROCEDURE 5 & ERA 627404-14 REV. A.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 69,416 hrs · 26,228 cycles

(LOG 1107169) WHILE IN SLC, MTC REPORTED DAMAGE COMMON TO THE OTBD SEAT TRACK LOCATED AT SEAT ROW 27 ABC. ACCOMPLISHED ERA 627404-14 REV A, PRI REV 0 SEAT TRACK REPAIR AT SEAT ROW 27 ABC.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 66,001 hrs · 24,704 cycles

(LOG 4543136) MULTIPLE EMERGENCY EXIT LIGHTS INOP. RED EEPL AT OVERWING EXITS INOP. 3 LIGHTS INOP AT RT OVERWING EXIT, LIGHT INOP AT LT OVERWING EXIT. R/R BATTERY PACK BEHIND RT LWR SIDEWALL PNL AT LOC 17 ABC PER B737 AMM 33-51. OPS CHK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,615 hrs · 24,520 cycles

(LOG 5451254) RT #3 AND #4 EXTERIOR EMERGENCY LIGHTS INOP. R/R POWER SUPPLY (M1671) REF B737 AMM 33-51, OPS CHECK GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 65,572 hrs · 24,501 cycles

(LOG 5451225) ROW 25 FED EMER LT INO. FOUND PINS OUT OF CONNECTOR FOR ROW 25 FED EMER LT. RE-PINNED CONNECTOR IN REF B737 SWPM 20-61. OPS CHECK GOOD AT THIS TIME.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,429 hrs · 24,452 cycles

(LOG 5094070) FWD GALLEY AISLE MOUNTED FLOOR PROXIMITY EMERG ESCAPE PATH MARKING LIGHT LENS MISSING. REPLACED EMERGENCY LIGHT PATH MARKING LIGHT ASSY PER B737 AMM 33-51 OP CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,421 hrs · 24,448 cycles

(LOG 5094055) L1 DOOR EMER LIGHTS INOP. REMOVED & REPLACED BATTERY PACK M1675 REF B737 AMM 33-51. OPS CHECK SAT OK FOR SVC.

Part: NONE — NONE · airframe 61,689 hrs · 22,679 cycles

SHIP 3762 -ATB- DUE TO HIGH FAN VIBRATION AFTER RIGHT ENGINE BIRD STRIKE ON TAKEOFF. CORRECTIVE ACTION: COMPLETED BSI WITH NO FINDINGS AND REPLACING 3 PAIRS OF BENT FAN BLADES

Part: NONE — NONE · airframe 59,495 hrs · 21,696 cycles

(LOG 7833031) DURING INSPECTION FOUND 2 EA SMALL BURN MARKS ON UPPER TRAILING EDGE OF RUDDER. C/C PERMANENT REPAIR PER B 737-800 SRM 55-40-01-2R.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2023776) DURING INSPECTION FOUND CORROSION ON S28 R BTW STA 500 TO 470 AT FWD CARGO COMPARTMENT. STRINGER 28 R BTW STA 500 TO 470 AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 595461-14 REV. ORIGINAL AND ETI-57-21-523 REV. 1.

Part: NONE — NONE · airframe 59,398 hrs · 21,617 cycles

(LOG 2023504) DURING INSPECTION FOUND BROKEN INBD SEAT TRACK AT INBD LH SEAT TRACK BETWEEN STA 500H AND 500I. LH SEAT TRACK BTWN STATION 500H AND 500I WAS REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 4, REPAIR 4.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2021644) DURING INSPECTION FOUND CORROSION ON STG 28R BTW STA 500F TO 500E AT FWD CARGO COMPARTMENT. CORROSION LEVEL 2. AREA WAS REPAIRED PER ETI-37-21-517 REV. 2 AND ERA 595435-14 REV. ORIGINAL.

Part: NONE — NONE · airframe 59,398 hrs · 21,617 cycles

(LOG 2020970) DURING INSPECTION FOUND CRACK ON PRESSURE BULKHEAD VAPOR BARRIER WEB LOWER AREA BTW LBL 45.64 TO LBL 40. CRACK ON PRESSURE BULKHEAD VAPOR BARRIER WEB LOWER AREA BTW LBL 45.64 TO LBL 40 WAS REPAIRED PER B737-800 SRM 57-10-10-2R PROCEDURE 2 REPAIR 2.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2021498) DURING INSPECTION FOUND CORROSION INSIDE STR 28R STA 500-500A. CORROSION LEVEL 2 INSIDE STR 28R STA 500-500A WAS REPAIRED PER ER/A 595445-14 REV. ORIGINAL AND ETI-37-21-513 REV. 2.

Part: NONE — NONE · airframe 59,398 hrs · 21,617 cycles

(LOG 2020965) DURING INSPECTION FOUND CRACK ON PREVIOUS REPAIR AT PRESSURE BULKHEAD VAPOR BARRIER WEB STA LBL 45.64. CRACK ON PREVIOUS REPAIR AT PRESSURE BULKHEAD VAPOR BARRIER WEB STA LBL 45.64 WAS REPAIRED PER B737-800 SRM 57-10-10 -2R PROCEDURE 2 REPAIR 2.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2017696) DURING INSPECTION FOUND CORROSION ON FLOOR STG RBL 17.70 BTW STATION 500C AND 500D AT FWD CARGO COMPARTMENT. DAMAGE ON FLOOR STRINGER BEAM WAS REPAIRED PER B737-800 ER/A 501407-14MA REV. ORIGINAL SECTION I PARAGRAPH 1. AND B737-800 SRM 53-00-53 REP 2.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2016728) DURING INSPECTION FOUND CORROSION ON TRANVERSE BEAM OF FWD PASSENGER FLOOR STRUCTURE WET AREA FROM STA 328 AND RBL 5. TRANVERSE BEAM OF FWD PASSENGER FLOOR STRUCTURE WET AREA FROM STA 328 AND RBL 5 APPROXIMATELY WAS REPAIRED PER B737-800 SRM 53-10-51-2R PROCEDURE 7 REPAIR 7.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2016662) DURING INSPECTION FOUND CORROSION RH OUTBD SEAT TRACK SECTION BTW STA 777 TO STA 887 WAS FOUND OUT OF LIMITS. RH OUTBD SEAT TRACK SECTION BTW STA 777 TO STA 887 WAS REPAIRED PER B737-800 SRM 53-00-52-2R REPAIR. 5

Part: NONE — NONE · airframe 59,398 hrs · 21,617 cycles

(LOG 2016102) DURING INSPECTION FOUND CRACK ON PRESSURE DECK WEB UPPER AREA ON RBL 40 TO 45.64. AREA WAS REPAIRED PER B737-800 SRM 57-10-10-2R PROCEDURE 3 REPAIR 3.

Part: PLATE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2015466) DURING INSPECTION FOUND CORROSION ON SIDE PLATE LH BTW STA 480 TO 400 AT FWD CARGO COMPARTMENT (C1). CORROSION LEVEL 2. SIDE PLATE LH BTW STATION 480 TO 400 AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-10-02-0G.

Part: SPLICE — GOUGED · airframe 59,398 hrs · 21,617 cycles

(LOG 2014933) DURING INSPECTION FOUND GOUGE IN FRAME SPLICE NEAR TO SIDEWALL STRAP (B STATION 727I, BTW S24 AND S25R APROX) C2. FRAME SPLICE NEAR TO SIDEWALL STRAP (B STA 727I, BTW S24 AND S25R APROX WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: PLATE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2015455) DURING INSPECTION FOUND CORROSION ON SIDE PLATE LH BTW STA 500I TO 500BAT FWD CARGO COMPARTMENT (C1). CORROSION LEVEL 2. SIDE PLATE LH BTW STATION 500I TO 500BAT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: PLATE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2015452) DURING INSPECTION FOUND CORROSION ON SIDE PLATE LH BTW STA 500B TO 480 AT FWD CARGO COMPARTMENT (C1). SIDE PLATE LH BTW STATION 500B TO 480 AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: PLATE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2014353) DURING INSPECTION FOUND CORROSION ON SIDE PLATE RH BTW STA 500I TO 500F AT FWD CARGO COMPARTMENT. SIDE PLATE RH BTW STATION 500I TO 500F AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: ANGLE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2014535) DURING INSPECTION FOUND CORROSION ON FRAME ANGLE AT STA 500H BTW STATION S28 R TO S28 L AT FWD CARGO COMPARTMENT. FRAME ANGLE AT STA 500H BTW STA S28R TO S28L AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: CHANNEL — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2012861) DURING INSPECTION FOUND SEVERAL CORROSION ON RH ZEE CHANNEL SIDE PLATE OF FLOOR STRUCTURE BTW STA 727 TO STA 794.3 APPROX. IN AFT CARGO COMPARTMENT. RH ZEE CHANNEL SIDE PLATE OF FLOOR STRUCTURE BTW STA 727 TO STA 794.3 APPROX. IN AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 RM 51-40-02.

Part: CHANNEL — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2012806) DURING INSPECTION FOUND SEVERAL CORROSION ON LH ZEE CHANNEL SIDE PLATE OF FLOOR STRUCTURE BTW STA 727 TO STA 847 APPROX. IN AFT CARGO COMPARTMENT. LH ZEE CHANNEL SIDE PLATE OF FLOOR STRUCTURE BTW STA 727 TO STA 847 APPROX. IN AFT CARGO COMPARTMENT WAS REPLACED PER. B737-800 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2012863) DURING INSPECTION FOUND CORROSION ON RH TRANSITION FLOOR SUPPORT UPPER LEG, LOWER SURFACE STATION 727A TO 727B BETWEEN STRINGERS 27R AND 26R. RH TRANSITION FLOOR SUPPORT UPPER LEG, LOWER SURFACE STATION 727A TO 727B BETWEEN STRINGERS 27R AND 26R WAS REPLACE PER B737-800 SRM 51-40-02-0G.

Part: NONE — NONE · airframe 59,398 hrs · 21,617 cycles

(LOG 2013378) DURING INSPECTION FOUND ELONGATE HOLES AND MATERIAL EXPOSED ON WHEEL WELL ACCESS PANEL 193D. PANEL 193D WAS REPAIRED PER B737-800 SRM 53-40-70-2R PROCEDURE 1, REPAIR 1, TABLE 202 AND SRM 51-70-05-2R PROCEDURE 6, REPAIR 6.

Part: NONE — NONE · airframe 59,398 hrs · 21,617 cycles

(LOG 2013365) DURING INSPECTION FOUND ELONGATE HOLE AND MATERIAL EXPOSED ON WHEEL WELL ACCESS PANEL 194E. L ACCESS PANEL 194E WAS REPAIRED PER B737-800 SRM 53-60-70-2R PROCEDURE REPAIR 1, TABLE 202 AND B-737-800 SRM 51-70-04-2R PROCEDURE 9, REPAIR 9.

Part: NONE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2012424) DURING INSPECTION FOUND CORROSION ON FRAME CLIPS AT STA 500F AND 500G AND BTW S28 R TO S28 L AT FWD CARGO COMPARTMENT. FRAME CLIPS AT STA 500F AND 500G AND BTW S28 R TO S28 L AT FWD CARGO COMPARTMENT WERE REPLACED PER B737-800 SRM 51-40-02-0G.

Part: CHANNEL — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2011653) DURING INSPECTION FOUND CORROSION ON LH ZEE CHANNEL SIDE PLATE ON RH ZEE CHANNEL SIDE PLATE OF FLOOR STRUCTURE BTW STA 867 TO 887 APPROX. IN AFT CARGO COMPARTMENT. RH SIDE PLATE WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: PLATE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2006126) DURING INSPECTION FOUND CORROSION ON SIDE PLATE RH BTW STA 440 TO 400 AT FWD CARGO COMPARTMENT. CORROSION 2, SIDE PLATE BTW STA: 400 TO 420 WAS REPLACED PER B737-800 SRM 51-40-02.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2007359) DURING INSPECTION FOUND RH INBOARD SEAT TRACK SECTION BTW STA 541 TO STA 543 CORROSION WAS FOUND OUT OF LIMITS. RH INBOARD SEAT TRACK SECTION BTW STA 541 TO STA 543 WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR. 9.

Part: PLATE — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2007242) DURING INSPECTION FOUND CORROSION ON SIDE PLATE RH BTW STA 500A TO 500 AT FWD CARGO COMPARTMENT. SIDE PLATE WAS REPLACED FOR NEW ONE PER B737-800 SRM 51-40-02-0G PAR 7C.

Part: WEB — CRACKED · airframe 59,398 hrs · 21,617 cycles

(LOG 2006296) DURING INSPECTION FOUND CRACK ON WEB BTW STA 663.75 AND RBL 45.57 TO RBL 64. CRACK ON WEB BTW STA 663.75 AND RBL 45.57 TO RBL 64 WAS REPAIRED PER B737-800 SRM 51-70-12-2R REP. 1.

Part: SUPPORT FITTING — CORRODED · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2005790) DURING INSPECTION FOUND CORROSION ON AFT WALL SUPPORT (LOWER AREA) AT STA 500I BTW S 26R TO S 26L AT FWD CARGO COMPARTMENT. CORROSION LEVEL2, AFT WALL SUPPORT (LOWER AREA) AT STA 500I BTW S 26R TO S 26L AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 2003959) DURING INSPECTION FOUND CORROSION ON CUT OUTS OF FUEL TANK ACCESS HOLES NBR. 531AB, 531BB, 532AB, 532BB, 532CB, 532DB, 532EB, 532FB, 532GB, 532HB, 532JB, 532KB, 532LB, 532MB, 532NB, 532PB AND 532QB AT LH WING. CORROSION AT LH WING WAS REMOVED PER B737-800 SRM 51-10-02-0G PAR 15 A. AND B737-800 SRM 57-20-01-2R-1. REPAIR 1.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

DURING INSPECTION FOUND CORROSION ON CUT OUTS OF FUEL TANK ACCESS HOLES NBR. 631AB, 631BB, 632AB, 632BB, 632CB, 632DB,632EB, 632FB, 632KB, 632LB, 632MB, 632NB, 632QB AND 632RB AT RH WING. CORROSION WAS REMOVED PER B737-800 SRM 51-10-02-0G PAR 15 A. AND B737-800 SRM 57-20-01-2R-1. REPAIR 1.

Part: NONE — NONE · corrosion level 2 · airframe 59,398 hrs · 21,617 cycles

(LOG 1999629) DURING INSPECTION FOUND CORROSION ON INTERNAL DOUBLES BTW STA 727G TO 727H AND BTW S-2L TO S-2R. CONNECTOR BTW STA 727G TO 727H AND BTW S-2L TO S-2R (3 EA) WERE FABRICATED AND REPLACED PER DWG. AR230-0134-00 REV ORIGINAL AND DWG. AR230-0136-00 REV ORIGINAL AND B737-800 SRM 51-40-02.

Part: NONE — NONE · corrosion level 2 · airframe 59,394 hrs · 21,616 cycles

(LOG 1959149) DURING INSPECTION FOUND RMLG FWD TRUNNION FTG O/B UPPER HOLE O/B FACE HAS PITTING ON FACE AND NEAR BORE. REPAIRED PER B737 SRM 57-20-90.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,358 hrs · 21,597 cycles

DURING INSPECTION FOUND AFT RT EXIT EMERGENCY LIGHTS AND AFT RT 9 SEAT ROW EMERGENCY FLOOR LIGHTS EXTINGUISH AFTER 10 SECONDS.REMOVED & REPLACED AFT BATTERY PACK LOC M01672 PER B737 AMM 33-51. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,181 hrs · 21,105 cycles

DURING INSPECTION FOUND 1L DOOR EMERG EXIT SIGN NOT ILLUMINATING. INSTALLED SERVICEABLE M1675 EMERG LIGHT BATTERY PER B737AMM33-51-06.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,685 hrs · 20,924 cycles

DURING INSPECTION FOUND EXIT SIGN BY 1R DOOR MISSING. INSTALLED NEW LENS IAW B737-800 AMM 33-51.

Part: SWITCH — FAULTY (HORIZ STAB) · airframe 56,291 hrs · 20,393 cycles

ATO, AT 70KTS DUE TO T/O CONFIGURATION WARNING. PERFORMED PSEU BITE. REPLACED STAB T/O WARNING SWITCHES S132 AND S546 PER AMM. SYSTEM TESTS NORMAL.

Part: STRINGER — CORRODED (BS 360) · airframe 54,601 hrs · 19,755 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 27L, BS 360+2. REPAIRED THE STRINGER IAW PRI 566493-14, REV 0, 1, 2, 3, 4, AND ERA 566493-14, REV ORIGINAL.

Part: STRINGER — CORRODED (BS 360) · corrosion level 3 · airframe 54,601 hrs · 19,755 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 28L, BS 360+2. REPAIRED THE STRINGER IAW PRI 566496-14, REV 0, 1, 2, 3, 4, AND ERA 566496-14, REV ORIGINAL.

Part: STRINGER — CORRODED (BS 360) · airframe 54,601 hrs · 19,755 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 25L, BS 360+2, AFT EQUIPMENT ELECTRONIC COMPARTMENT. MAINTENANCE PERFORMED A PERMANENT REPAIR TO THE STRINGER BETWEEN BS 330.62 TO 360+6 IAW PRI 566497-14 REV 0, 1, 2, 3, 4, 5, AND ERA 566497-14, REV ORIGINAL.

Part: SKIN — CORRODED (BS 348-360) · airframe 54,621 hrs · 19,761 cycles

DURING INSPECTION, FOUND CORROSION ON THE EXTERNAL SKIN, BS 348 TO 360, STRINGER 28R TO 28L. REPAIRED THE SKIN IAW PRI 566500-14, REV 0, 1, 2, AND ERA 566500-14, REV ORIGINAL.

Part: CHANNEL — CORRODED (BS 340) · airframe 54,601 hrs · 19,755 cycles

DURING INSPECTION, FOUND CORROSION ON THE ATC ANTENNA BASE INTERNAL STRUCTURE, BS 340+17 ON THE LOWER FUSELAGE. MAINTENANCE REPLACED THE CHANNEL IAW ERA 566519-14, REV ORIGINAL AND PRI REV.0.

Part: PLATE — CORRODED (BS 340) · corrosion level 2 · airframe 54,601 hrs · 19,755 cycles

DURING INSPECTION, FOUND CORROSION ON THE SKIN PLATE BS 340+17, STRINGER 28L. MAINTENANCE REPLACED THE PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A8511, REV C.

Part: TEE FITTING — CORRODED (BS 351) · corrosion level 2 · airframe 54,601 hrs · 19,755 cycles

DURING INSPECTION, FOUND CORROSION ON THE TEE FITTING AT STRINGER 28L LBL 5.47, BETWEEN BS 351+2 AND 351+4. REPAIRED THE TEE FITTING IAW PRI 566521-14, REV O, AND ERA 566521-14, REV ORIGINAL.

Part: SHEAR TIE — CORRODED (BS 400) · airframe 54,579 hrs · 19,746 cycles

DURING INSPECTION, FOUND CORROSION ON THE SHEAR TIE, BS 400, STRINGER 27L TO 28L IN THE FWD CARGO BAY. E REPLACED THE SHEAR TIE IAW SRM 51-10-02, ITEM 9, AND DWG 143A3230.

Part: STRINGER — CORRODED (BS 360) · corrosion level 2 · airframe 54,579 hrs · 19,746 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 24L, BS 360+10. MAINTENANCE REPAIRED THE STRINGER IAW PRI 566506-14, REV 0, 1, 2, AND ERA 566506-14, REV ORIGINAL.

Part: DOUBLER — CORRODED (BS 360-380) · corrosion level 2 · airframe 54,579 hrs · 19,746 cycles

DURING INSPECTION, FOUND CORROSION ON THE INTERNAL DOUBLER AIR DUCT EXHAUST, BS 360 TO 380+5, STRINGER 28L TO 28R. MAINTENANCE REPLACED THE INTERNAL DOUBLER IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG143A3230.

Part: SKIN — CORRODED (BS 360) · corrosion level 2 · airframe 54,579 hrs · 19,746 cycles

DURING HEAVY CHECK, CORROSION WAS FOUND ON THE FUSELAGE SKIN BELOW THE ATC ANTENNA AND AT BS 360, STRINGER 27L. MAINTENANCE REPAIRED THE SKIN IAW ERA 566500-14.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 54,579 hrs · 19,746 cycles

DURING INSPECTION, FOUND A CRACK ON THE PRESSURE BULKHEAD, BS 663 BETWEEN LBL 40 TO 24.92. MAINTENANCE REPAIRED THE BULHEAD WEB IAW SRM 57-10-10.

Part: PROXIMITY SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 54,152 hrs · 19,581 cycles

DURING FLIGHT, AIRCRAFT DIVERTED DUE TO WEATHER. ON APPROACH THE FLAPS STUCK AT 2 WHEN FLAP LEVER MOVED TO 5. DECLARED EMERGENCY NO FLAP SPLIT NOTED. USED ALTERNATE FLAPS TO LOWER FLAPS TO 15 FOR LANDING. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR S995 IAW AMM 27-88-11. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,142 hrs · 19,242 cycles

WHILE IN DTW FOR SCHEDULED MOD, MTC IS ACCOMPLISHING REMOVAL OF THE FWD ATG ANTENNA PER AMDS 2330-01344-01A AND GOGO DWG P19110-24406, REV B. UPON REMOVAL OF THE DOUBLER, MTC REPORTED MULTIPLE EXISTING HOLES WERE FOUND TO BE ELONGATED. MAINTENANCE REPAIRED PER ERA 551105-14

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,142 hrs · 19,242 cycles

DURING INSPECTION FOUND FUSELAGE SKIN STATION 727F-727G STRINGERS S-27R - S-27L AFT ATG ANTENNA EXISTING ELONGATED HOLES. MAINTENANCE REPAIRED PER ERA 551111-14.

Part: COVER — LOOSE (EXIT SIGN) · airframe 50,901 hrs · 18,473 cycles

DURING INSPECTION FOUND EMERGENCY EXIT SIGN COVER LOOSE. MAINTENANCE FOUND EXIT SIGN COVER IN OVERHEAD BIN. RE-INSTALLED COVER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,142 hrs · 19,242 cycles

WHILE IN DTW FOR SCHEDULED MOD, DAL MTC IS ACCOMPLISHING REMOVAL OF THE AFT ATG ANTENNA PER GOGO DWG P19112-24406, REV C. UPON REMOVAL OF THE DOUBLER, MTC REPORTED MULTIPLE EXISTING HOLES WERE FOUND TO BE ELONGATED. MAINTENANCE REPAIRED PER ERA 551111-14.

Part: STRUCTURE — PUNCTURED (L2 DOOR) · airframe 59,393 hrs · 21,615 cycles

DURING INSPECTION FOUND DOOR 2L HAS A 2" X 4" PUNCTURE; LOWER CENTER. MAINTENANCE REPAIRED DAMAGE INSTALLING DOUBLER PER B737 SRM 52-00-01 REPAIR 2.

Part: STRINGER — CORRODED (BS 294-312) · airframe 48,312 hrs · 17,632 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 24L BETWEEN BS 294 AND 312. MAINTENANCE REPAIRED PARTS IAW SRM 53-00-03, REPAIR 1. APPLIED CHEMICAL CONVERSION LAYER AND PRIMER. OK TO INSTALL, REPAIR QC1440. INSTALLED STRINGER REPAIR IAW SRM 53-00-03, REPAIR 1.

Part: FRAME — DAMAGED (BS 540) · airframe 46,452 hrs · 17,019 cycles

DURING INSPECTION, FOUND BS 540 BULKHEAD CHORD, BELOW S-22L IAW AA WC 5331-01257-04. WHEN AN OUT OF ROUND HOLE WAS FOUND. MAINTENANCE REPAIRED IAW ERA 539454-14.

Part: SKIN — CRACKED (BS 747-767) · airframe 39,741 hrs · 14,734 cycles

DURING INSPECTION, FOUND LOWER EXTERNAL FUSELAGE BS 747-767, BL 0, ANTENNA CRACKED. MAINTENANCE REPAIRED IAW ERA 519216-14, REV O AND ERA 519216-14, REV O, ANTENNA WAS REPLACED BY A DOUBLER IAW THE ERA.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT STATION 727B, LBL 45.50 HAS A CRACK INDICATION. MAINTENANCE REPAIRED SEAT TRACK IAW PRI 518619-14, REV 0 AND ERA 518619-14 REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT STATION 727B, LBL 24.75 INBD AFT HOLE HAS CRACK INDICATIONS. MX REPAIRED PASSENGER CABIN SEAT TRACK AT STATION 727B, LBL 24.75 INBD AFT HOLES IAW PRI 518619-14, REV 0 AND ERA 518619-14, REV ORIGINAL.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND FASTENER HOLES IN THE FLOORBEAM INBD AND OTBD FLANGES AT BS 727B, LBL 45.5, LBL 24.75, RBL 24.75 AND RBL 45.5 HAD CRACK INDICATIONS. MAINTENANCE REPAIRED THE DAMAGE IAW ERA 518619-14.

Part: ANGLE — CORRODED (BS 804-835) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 804 - 835, RBL 20, LOWER SURFACE OF WEB UPPER CHORD HAS CORROSION AROUND NUT PLATES. MAINTENANCE REPLACED WEB STATION 804 - 835 RBL 20 IAW SRM 51-40-02 AND DWG 146A8123, SN 2284054.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT STATION 727B, LBL 24.75 HAS CRACK INDICATIONS. MAINTENANCE REPAIRED PASSENGER CABIN SEAT TRACK IAW PRI 518619-14, REV 0 AND ERA 518619-14, REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT BS 727B, RBL 45.50 HAS A CRACK INDICATION. MAINTENANCE REPAIRED SEAT TRACK IAW PRI 518619-14, REV 0 AND ERA 518619-14, REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT STATION 727B, RBL 24.75 OTBD FWD AND OTBD AFT HOLES HAVE CRACK INDICATIONS. MAINTENANCE REPAIRED PASSENGER CABIN SEAT TRACK AT STATION 727B, RBL 24.75 OTBD FORWARD AND OTBD AFT HOLES IAW PRI 518619-14, REV 0 AND ERA 518619-14, REV ORIGINAL.

Part: ANGLE — CORRODED (BS 767-787) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AFT CARGO COMPARTMENT, BS 767 - 787, RBL 20 - 23, TRANSITION ANGLE HAS CORROSION ON UPPER AND LOWER SURFACES. MAINTENANCE R & R TRANSITION ANGLE AS REQUIRED REF DWG 146A0081, REV B, SN 2284042.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT BS 727B RBL 24.75 HAS CRACK INDICATIONS. MAINTENANCE REPAIRED SEAT TRACK IAW PRI 518619-14, REV 0 AND ERA 518619-14, REV ORIGINAL.

Part: WEB — CORRODED (CARGO BAY) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AFT CARGO THRESHOLD WEB HAS SEVERAL AREAS OF CORROSION. MAINTENANCE R & R WEB AS REQUIRED REF DWG 146A8120, REV E, SN 2284014.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT STATION 727B RBL 45.50 INBD FWD AND INBD AFT HOLES HAVE CRACK INDICATIONS. MAINTENANCE REPAIRED PASSENGER CABIN SEAT TRACK AT STATION 727B RBL 45.50 INBD FWD AND INBD AFT HOLES IAW PRI 518619-14, REV 0 AND ERA 518619-14, REV ORIGINAL.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND AD DRIVEN PASSENGER CABIN SEAT TRACK AT BS 727B, LBL 45.50 HAS A CRACK INDICATION. MAINTENANCE REPAIRED SEAT TRACK IAW PRI 518619-14, REV 0 AND ERA 518619-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 400) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND PASSENGER CABIN STA 400 RT RAIL ATTACHMENT FRAME CRACKED BETWEEN STRINGER 8 AND 9. MX REPAIRED PASSENGER CABIN STA 400 RT RAIL ATTACHMENT FRAME BETWEEN STRINGER 8 AND 9 IAW ERA 518615-14AD, REV ORIGINAL.

Part: SUPPORT ANGLE — CORRODED (BS 727) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 727 +4", LBL 20 -RBL 20 BULKHEAD PANEL LOWER SUPPORT ANGLE IS CORRODED AND BENT. MAINTENANCE REPLACED LOWER BULKHEAD ANGLE IAW SRM 51-40-02, SN 2284041.

Part: FLOOR SUPPORT — CORRODED (BS 771-773) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION, FOUND AFT CARGO BAY BS 771-773, RBL 13, FLOOR SUPPORT HAS SURFACE CORROSION. MAINTENANCE R & R FLOOR SUPPORT IAW SRM 53-00-53 REPAIR 4.

Part: FRAME — CRACKED (BS 480) · airframe 39,657 hrs · 14,703 cycles

DURING INSP, FOUND PASSENGER CABIN BS 480 RT RAIL ATTACHMENT FRAME CRACKED BETWEEN STRINGER 8 AND 9. MX REPAIRED PASSENGER CABIN STA 480 RT RAIL ATTACHMENT FRAME BETWEEN STRINGER 8 AND 9 IAW ERA 518615-14AD, REV ORIGINAL.

Part: STRINGER — CORRODED (BS 370) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION FOUND E & E BAY, BS 370, STRINGER 23L CORRODED. MAINTENANCE REPAIRED STRINGER IAW SRM 53-00-03.

Part: FRAME — CRACKED (BS 440) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND PASSENGER CABIN BS 440 LT RAIL ATTACHMENT FRAME CRACKED BETWEEN STRINGER 8 AND 9. MX REPAIRED PASSENGER CABIN STA 440 LT RAIL ATTACHMENT FRAME BETWEEN STRINGER 8 AND 9 IAW ERA 518615-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 480) · airframe 39,657 hrs · 14,703 cycles

DURING INSP, FOUND PASSENGER CABIN BS 480 LT RAIL ATTACHMENT FRAME CRACKED BETWEEN STRINGER 8 AND 9. MX REPAIRED PASSENGER CABIN STA 480 LT RAIL ATTACHMENT FRAME BETWEEN STRINGER 8 AND 9 IAW ERA 518615-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 727B) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND PASSENGER CABIN S 727B 58R, FRAME IS CRACKED. MX REPAIRED PASSENGER CABIN STA 727B, 58R FRAME IAW ERA 518615-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 440) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND PASSENGER CABIN BS 440, RT RAIL ATTACHMENT FRAME CRACKED BETWEEN STRINGER 8 AND 9. MX REPAIRED PASSENGER CABIN STA 440 RT RAIL ATTACHMENT FRAME BETWEEN STRINGER 8 AND 9 IAW ERA 518615-14AD, REV ORIGINAL.

Part: SKIN — GOUGED (BS 807-827) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION, FOUND TWO GOUGES WERE FOUND ON THE OUTER SURFACE ON THE AFT BILGE SKIN BETWEEN BS 807 AND 827 AND S25-27R. MX REPAIRED DAMAGE IAW ERA 519218-14.

Part: WEB — CORRODED (BS 319-325) · airframe 39,664 hrs · 14,708 cycles

DURING INSPECTION, FOUND E & E BAY LT SIDE BS 319 TO 325, S23L WEB CORRODED ON UPPER SURFACE. MX FABRICATED NEW WEB AND INSTALLED IAW DWG 141A8131, SN 2283897.

Part: FRAME — CRACKED (BS 867) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND PASSENGER CABIN BS 867, S8L FRAME IS CRACKED. MX REPAIRED PASSENGER CABIN STA 867, 58L FRAME IAW ERA 518615-14AD, REV ORIGINAL.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,684 hrs · 14,716 cycles

DURING INSPECTION FOUND CORROSION ON OUTER ANGLE OF THE FORWARD ENTRY DOOR, LOWER AUXILARY SILL STRUCTURE. MAINTENANCE REPAIRED IAW ERA 519213-14.

Part: FRAME — CRACKED (BS 380) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND PASSENGER CABIN BS 380 LT RAIL ATTACHMENT FRAME CRACKED BETWEEN STRINGER 8 AND 9. MX REPAIRED PASSENGER CABIN STA 380 LT RAIL ATTACHMENT FRAME BETWEEN STRINGER 8 AND 9 IAW ERA 518615-14AD, REV ORIGINAL.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND LOWER EXTERNAL FUSELAGE BS 787 TO 807 BL 0 ANTENNA CRACKED. MX REPAIRED IAW ERA 519216-14, REV 0 AND ERA 519216-14, REV 0. ANTENNA WAS REPLACED BY A DOUBLER IAW THE ERA SN 2283905.

Part: FRAME — CRACKED (BS 195) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND FWD NOSE COMPARTMENT BS 195 FRAME WEB CRACKED AT S24L. MX REPAIRED IAW SRM 51-70-03, REPAIR 4.

Part: ANGLE — CORRODED (BS 500C-500E) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND FWD CARGO BAY LT Z ANGLE BS 500C - 500E HAS SEVERAL AREAS OF CORROSION. MX FABRICATED "ZEE ANGLE" IAW SRM 53-00-53, PG 202, REPAIR 5. LOCATED AND DRILLED NEW "ZEE ANGLE" IAW SRM 51-40-05, PG 1-10 LOWER SINK HOLES IAW SRM 51-40-02, PG 1-3 TREATED AND PRIMED "ZEE ANGLE" IAW SRM 51-20-01, PG 1-5 INSTALLED LT "ZEE ANGLE" STA 400 TO 500I. INSTALLED FWD BULKHEAD ANGLE. INSTALLED FORWARD SIDEWALL. INSTALLED AFT BULKHEAD ANGLE INSTALLED AFT SIDEWALL SUPPORT STA 500I, ALL IAW SRM 51-40-02, PG 1-4 AND SRM 53-00-53.

Part: CREASE BEAM — CRACKED (BS 269) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND CABIN 1R DOOR CUT OUT LOWER SILL CREASE BEAM INBD CHORD OTBD CLIP IS CRACKED BS 296, STR 17R. MX R & R CLIP FRAME AT CABIN 1R DOOR CUT OUT LOWER SILL CREASE BEAM INBD CHORD, OTBD CLIP AND FRAME AT BS 296 IAW SRM 51-40-02, FIG 8 & 51-40-05, PAR 4.

Part: FLOOR SUPPORT — CORRODED (BS 771-773) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND AFT CARGO BAY BS 771 -773, LBL 17, FLOOR SUPPORT HAS SURFACE CORROSION. MX REPAIRED AFT CARGO FLOOR SUPPORT AT BS 771-773, LBL 17 C/W ERA PRI 518620-14, REV 0 AND ERA 518620-14, REV 0.

Part: SKIN — GOUGED (BS 727I-727J) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND LOWER FUSELAGE EXTERNAL SKIN, BS 727I-727J, STR 24 - 25R GOUGED. MX REPAIRED IAW ERA 519217-14, REV 0 AND ER/A 519217-14, REV ORIGINAL.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND FWD CARGO BAY THRESHOLD WEB HAS CORROSION IN SEVERAL AREAS. MAINTENANCE REMOVED CORROSION FROM WEB IAW SRM 51-10-02, ORIGINAL MATERIAL THICKNESS .040 MATERIAL LOSS IS GREATER THAN 50 PERCENT AND OUT OF LIMITS IAW SRM 51-40-02 PG 1-5 , 51-40-05, 51-40-08, PG 16-24 AND DWG 143A8120 AND 143A8122, SN 2283947.

Part: CREASE BEAM — CORRODED (BS 324-332) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND MAIN DECK R1 DOOR CREASE BEAM ZEE ANGLE, BS 324 -332 UPPER SURFACE HAS CORRODED. MX REPLACED FORWARD RT CREASE ZEE ANGLE IAW SRM 51-40-02.

Part: SEAT TRACK — CRACKED (BS 519-521) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK, BS 519 -521, RBL 24, UPPER CROWN GOUGED. MX REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — CRACKED (BS 519-521) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK, BS 519-521, LBL 24, UPPER CROWN GOUGED. MX REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — CRACKED (BS 519-521) · airframe 39,657 hrs · 14,703 cycles

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

Part: SEAT TRACK — CRACKED (BS 519-521) · airframe 39,657 hrs · 14,703 cycles

DURING INSP, FOUND PASSENGER CABIN SEAT TRACK, BS 519-521, LBL 45, UPPER CROWN GOUGED. MAINTENANCE REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: CREASE BEAM — CORRODED (BS 967-986) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND MAIN DECK L2 DOOR THRESHOLD AREA, LT CREASE BEAM UPPER FLANGE BS 967-986 UPPER AND LOWER SURFACES ARE CORRODED. MX R & R CREASE BEAM IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND AFT CABIN FLOORBEAM TEE CORRODED BS 987 LBL 28-45. MX INSTALLED REPAIR IAW ERA 464736-14MA, REV A.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND CABIN FLOORBEAM TEE CORRODED BS 987, RBL 29-45. REPAIRED IAW ERA 464736-14MA, REV A.

Part: CREASE BEAM — CORRODED (BS 967-986) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION, FOUND MAIN DECK R2 DOOR THRESHOLD AREA, RT CREASE BEAM UPPER FLANGE BS 967-986 UPPER AND LOWER SURFACES ARE CORRODED. MX R & R CREASE BEAM ASSY IAW DWG 147A8501, REV C AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 538) · airframe 39,657 hrs · 14,703 cycles

DURING INSPECTION FOUND PASSENGER CABIN FLOOR SUPPORT ANGLE, BS 538, RBL 3, CRACKED. MX R & R SUPPORT ANGLE IAW SRM 51-40-02, FIG 8, PG 33 AND DWG 143A5240, REV.

Part: TERMINAL — BROKEN (FIRE DETECTION) · airframe 34,675 hrs · 13,004 cycles

FAULT LIGHT ILLUMINATED ON ENGINE FIRE/OVERHEAT DETECTOR SYSTEM. RETERMINATED BROKEN TERMINAL ON A-LOOP AND REPLACED B-LOOP UPPER FAN.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 32,798 hrs · 12,362 cycles

DURING TRIPLE GEAR CHANGE, EA 12-487906-12 REV A CORROSION WAS FOUND ON THE OUTBOARD FACES OF SUPPORT FITTING ATTACHED TO THE REAR SPAR OF THE RIGHT WING. REPAIR WAS ACCOMPLISHED PER EA 12-487906-12 ME-06.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 233 hrs · 109 cycles

ACRID ODOR IN FWD CABIN SMOKE OBSERVED BY F/A. RETURN FOR LANDING. CHECKED LIGHTING AND FWD CABIN, ALL CHECK OK. FOUND F/C OVEN SMELL AS IF OVERTEMPED. REPLACED OVEN.