N782SA

Part: LIGHT — UNSECURE (CABIN) · airframe 68,642 hrs · 40,454 cycles

FWD R/H SERVICE DOOR FLOOR EMERGENCY EXIT LIGHT WILL NOT SECURE. REMOVED AND REPLACED ASSEMBLY PER AMM 33-51-01.

Part: FLAP — DELAMINATED (LT WING) · airframe 68,636 hrs · 40,452 cycles

L/H O/B AFT FLAP I/B CORNER IS DELAMINATED REMOVED AND REPLACED LH WING OUTBOARD AFT FLAP PER AMM 27-51-22 TAG NO: B67498 PN ON: 113A3700-7 SN ON: 000016 PN OFF: SN OFF: 00619

Part: SLIDE — LOOSE (AFT SERVICE DOOR) · airframe 68,333 hrs · 40,250 cycles

FLIGHT ATTENDANTS REPORTS THAT EMERGENCY ESCAPE SLIDE AT AFT SERVICE DOOR ASKEW. / REPOSITIONED SERRVICE AFT DOOR SLIDE IN CONTAINER REF MT 725-61-06.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 68,014 hrs · 40,049 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 68,014 hrs · 40,049 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 68,014 hrs · 40,049 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 68,014 hrs · 40,049 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 68,014 hrs · 40,049 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 68,014 hrs · 40,049 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: ATTACH ANGLE — DAMAGED (LT MLG) · airframe 40,049 hrs · 68,014 cycles

L/H MLG AFT OF GEAR SNAP PANEL;LOWEST SHELF PANEL ATTACH ANGLE SUPPORT ROD ATTACH POINT HOLE IS DAMAGED / REMOVED AND REPLACED ATTACH ANGLE FOR SHELF PANEL PER SRM 51-40-02

Part: ANGLE — CRACKED (RT WING) · airframe 40,049 hrs · 68,014 cycles

R/H UPPER WING PANEL ABOVE GEAR I/B FWD SUPPORT BEAM FWD ATTACH '2' ANGLE IS CRACKED / REMOVED AND REPLACED RH MLG UPPER WING PANEL I/B FWD SUPPORT BEAM FWD ATTACH '2' ANGLE PER SRM 51-40-02

Part: LIGHT — PEELING (CABIN) · airframe 66,740 hrs · 39,222 cycles

L/H PHOTOLUMINESCENT STRIP PEELED BETWEEN ROWS 7 TO ROW 8. / SECURED STRIP PER AMM.

Part: BRACKET — OUT OF ADJUST (R1 DOOR) · airframe 64,607 hrs · 37,881 cycles

R1 DOOR GIRT BAR OUT OF ADJUST. ADJUSTED SLIDE BRACKET PER SIP & AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 64,260 hrs · 37,653 cycles

L2 DOOR SLIDE OUT OF POSITION. R&R SLIDE IAW MT.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 64,101 hrs · 37,559 cycles

LT REAR SPAR CENTER WING CRACKED AT BS 633, LBL 14. REPAIRED VAPOR BARRIER PER SRM.

Part: LENS — UNSECURE (CABIN) · airframe 63,604 hrs · 37,234 cycles

FORWARD EMERGENCY EXIT LIGHT LENS FELL OFF. R&R LIGHT ASSEMBLY PER AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 63,449 hrs · 37,128 cycles

L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,449 hrs · 37,128 cycles

LT OVERWING EMERGENCY EXIT LIGHT LOOSE. R&R LIGHT PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,449 hrs · 37,128 cycles

FORWARD RT EMERGENCY BATTERY INOP. R&R POWER SUPPLY IAW AMM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,449 hrs · 37,128 cycles

LATE INCOMING INSPECTION FINDING. FLOOR PANEL 242WF DISBANDED AND MISSING INSERT / REPAIRED DISBOND AND INSTALLED INSERT ON FLOOR PANEL 242WF PER SRM 53-00-50-2R-9

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,449 hrs · 37,128 cycles

FWD CARGO COMPARTMENT LOWER FWD CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW SCUFF PLATE FOR FWD CARGO LOWER FWD CORNER IAW BOEING DRAWING 143A8331 AND SRM 51-40-05. SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD 753-140-00-014

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

INTERCOSTAL CRACKED BETWEEN BS 1006 TO BS 1016, RBL 45. R&R INTERCOSTAL IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 63,449 hrs · 37,128 cycles

*CORROSION* AFT CARGO FLOOR STRUCTURES TEE HAS CORROSION AROUND FASTENER HOLES AT STA.767 RBL.21 TO LBL.21 / RECIEVED NEW FLOOR TEE STRAP P/O 688537 DISCARDED OLD TEE STRAP AT STA. 767 AND REPLACED WITH NEW STRAP I/A/W SRM 51-10-02-0G-0 + BOEING DWG 146A9401

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

FLOORBOARD SUPPORT CRACKED BETWEEN BS 277 TO BS 298, RBL 2. R&R INTERCOSTAL IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 63,449 hrs · 37,128 cycles

*CORROSION* AFT CARGO FLOOR STRUCTURES TEE HAS CORROSION AROUND FASTENER HOLES AT STA.727D RBL.21 TO LBL.21 / RECIEVED NEW FLOOR TEE STRAP P/O 598123 DISCARDED OLD TEE STRAP AT STA. 727D AND REPLACED WITH NEW STRAP I/A/W SRM 51-10-02-G-0 + BOEING DWG 146A9401

Part: SKIN — CRACKED (RT WING) · airframe 63,449 hrs · 37,128 cycles

RT WING FIXED LEADING EDGE SKIN CRACKED AT WS 180. R&R SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 63,449 hrs · 37,128 cycles

FORWARD CARGO COMPARTMENT LOWER AFT CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW SCUFF PLATE FOR FWD CARGO LOWER AFT CORNER IAW BOEING DRAWING 143A8331 AND SRM 51-40-05. SCUFF PLATE TO BE INSTALLED ON CUSTOMER CARD 753-140-00-01Y

Part: PANEL — DELAMINATED (RT WING) · airframe 63,449 hrs · 37,128 cycles

621DB HAS POSSIBLE DELAMINATION ON LEADING EDGE. / REPAIRED 621DB DELAMINATION ON LEADING EDGE IAW SRM 57-41-01-2R-1 TABLE 202 PARA. 4. E + IAW SRM 51-70-05-2R-10

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO COMPARTMENT CENTER SCUFF PLATE IS CRACKED / REMOVED AFT CARGO COMPARTMENT CENTER SCRUFF PLATE IAW AMM 53-11-02-020-801 LOCATED AND DRILLED CENTER SCUFF PLATE IAW SRM 51-40-05-0G-0 INSTALLED AFT CARGO CENTER SCUFF PLATE IAW 53-11-02-420-801 REMOVED AFT CARGO CENTER SCUFF PLATE IAW AMM 53-11-02-020-801

Part: FLOORBEAM — ELONGATED (MAIN CABIN) · airframe 63,449 hrs · 37,128 cycles

FLOOR BEAM AT BS 294 LBL 11 FOUND SECOND HOLE FROM BOTTOM THROUGH WEB TO BE OUT OF ROUND / FLOOR BEAM AT BS 294 LBL 11 SECOND HOLE FROM BOTTOM THROUGH WEB TO BE OUT OF ROUND REPAIRED IAW ER 18-03655 REV IR DTD 8/16/18 SWA EA 1-753-33122.IR

Part: ATTACH ANGLE — CORRODED (MAIN CABIN) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** ON GALLEY DOOR SILL UPPER ATTACH ANGLE AT BS 312 TO BS 328 WL 208 / BLENDED OUT CORROSION OR R-1 DOOR SILL UPPER ATTACH ANGLE AT BS 312 TO BS 328. OUT OF LIMITS. REMOVED ATTACH ANGLE; I.A.W. S.R.M. 51-40-02-0G-0. INSTALLED NEW ATTACH ANGLE PART #7530250; I.A.W. S.R.M. 51-40-02-0G-0 AND DRAWING #141A8312.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, RBL 44. REPAIRED CHORD IAW EA & ER.

Part: BRACKET — BROKEN (LT WING) · airframe 63,449 hrs · 37,128 cycles

BRACKET BROKEN OFF BOTTOM OF L/H WING ACCESS PANEL #551FB / REMOVED BROKEN BRACKET ON BOTTOM OF L/H WING ACCESS PANEL #551FB; I.A.W. S.R.M. 51-40-02-0G-0. REPLACED WITH NEW BRACKET; PART # 287A9152; I.A.W. S.R.M. 51-40-02-0G-0 AND DRAWING #115A2710. HOLE SIZE S.R.M. 51-40-05-0G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

INTERCOSTAL CRACKED BETWEEN BS 747 TO BS 767, STR 25R. R&R INTERCOSTAL IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 63,449 hrs · 37,128 cycles

LT WING NR 1 (544AB) FORWARD FLAP TRACK FAIRING CRACKED ON INNER SURFACE. R&R FAIRING PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

INTERCOSTAL CORRODED AT BS 310, LBL 11. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,449 hrs · 37,128 cycles

FLOOR PANEL 242UF HAS 4 AREAS OF DAMAGED HONEYCOMB STRUCTURE / REPAIRED 4 AREAS OF DAMAGED HONEYCOMB STRUCTURE OF FLOOR PANEL 242UF PER SRM 53-00-50-2R-3

Part: FLOOR PANEL — WORN (CABIN) · airframe 63,449 hrs · 37,128 cycles

FLOOR PANEL 242XF HAS EXPOSED HONEYCOMB STRUCTURE / REPAIRED EXPOSED HONEYCOMB STRUCTURE FLOOR PANEL 242XF IAW 737-700 SRM 53-00-50-2R-1 TABLE 201 AND SRM 53-00-50-2R-0

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** MULTIPLE AREAS OF POSSIBLE CORROSION UNDERNEATH DORSAL FIN / REMOVED CORROSION ON EXTERNAL FUSELAGE SKIN UNDERNEATH DORSAL FIN BS 907 TO BS 1006 STR 2L TO STR 2R IN MULTIPLE AREAS. REPAIRED EXTERNAL FUSELAGE SKIN BS 907 TO BS 1006 STR 2L TO STR 2R PER EA 1-753-33113 REV IR AND ER 18-03654 REV IR

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C TO BS 847, STR 25L. R&R SUPPORT IAW SRM & DWG.

Part: BEAM — CRACKED (FSD) · airframe 63,449 hrs · 37,128 cycles

WHILE ACCOMPLISHING CC# 14079 FOUND FWD SERVICE DOOR #4 BEAM CRACKED COMMON TO I/B SIDE OF RADIUS. / FWD SERVICE DOOR TO BE REPLACED ON CUSTOMER CARD N151915

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO FORWARD OF THE DOOR SHIELD CORRODED. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 947.5, STR 25L. R&R SUPPORT IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO DOOR SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: NONE — DELAMINATED (VERTICAL STABILI) · airframe 63,449 hrs · 37,128 cycles

DORSAL FIN IS DELAMINATED AT RIGHT HAND SIDE LOWER AFT CORNER. / REPAIRED DELAM AT RIGHT HAND SIDE LOWER AFT CORNER OF DORSAL FIN IAW SRM 55-30-01-2R-12 TABLE 202 + SRM 51-70-05-2R-6 80733U 08AUG18

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 807 TO BS 827, STR 26R. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** AFT CARGO FLOOR BOARD SUPPORT STA. 887 STR 25R TO 25L HAS CORROSION (MARKED) / EVALUATED CORROSION; NO LIMITS FOUND. PART TO BE REPLACED IAW SRM 51-10-02-0G-0 (9) FABRICATED NEW AFT CARGO FLOOR BOARD SUPPORT LOCATED AT STA 887 STR 25R TO 25L FROM BAL 1505-100543# 7075-T6511 LOT #5069212-1 IAW DWG 146A9401 REV C; AMM 51-21-41-370-802 AND 51-21-72-370-804. SRM 53-60-53-01-2 57403U 07/30/2018 SWITCHED OUT DAMAGED FLOOR BOARD SUPPORT 'TEE' WITH FABRICATED REPLACEMENT 'TEE' ON PARTS STORAGE SHELF; 20325C 20AUG18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 767, STR 25R. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

AFT CARGO AFT OF THE DOOR SHIELD CORRODED. R&R SHIELD IAW SRM AND BOEING DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** AFT CARGO FLOOR BOARD SUPPORT STA. 767 STR 25R TO 25L HAS CORROSION (MARKED) / EVALUATED CORRSION; NO LIMITS FOUND. PART TO BE REPLACED IAW SRM 51-10-02-0G-0 (9). FABRICATED NEW AFT CARGO FLOOR BOARD SUPPORT LOCATED AT STA 767 STR 25R TO 25L FROM BAL 1505-100581# 7075-T6511 LOT# 5059621-1 IAW SRM 53-60-53-01-2; 51-40-02-0G-02 D; (1); (2); AMM 51-21-41-370-802; 51-21-12-370-804; AND SRM 51-40-02-0G-0 4; B-C. 57403U 07/30/2018 SWITCHED OUT DAMAGED FLOOR BOARD SUPPORT 'TEE' WITH FABRICATED REPLACEMENT 'TEE' ON PARTS STORAGE SHELF. 50325C 20AUG18

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** ON FWD CARGO DOOR SUB THRESHOLD WEB STA442-480; RBL29; WL156 / REMOVED CORROSION ON SUB THERSHOLD WEB DAMAGE FOUND TO BE OUT OF LIMITS DUE TO PROX. OF FASTENER HOLE .3' X 2'. LOCATED; DRILLED AND INSTALLED NEW SUB THERSHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

FORWARD CARGO FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 403 TO BS 500D, LBL 24. REPAIRED ANGLE IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,449 hrs · 37,128 cycles

LT HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663+2, LBL 34. REPAIRED WEB IAW ER AND EA.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** ON FWD CARGO AFT BULKHEAD LOWER SUPPORT STA 500D; LBL21-RBL20; WL156 / REMOVED DAMAGE BULKHEAD LOWER SUPPORT AT STA. 500D LBL21 TO RRL20; WL156 IAW SRM 51-40-02-0G-0; INSTALLED NEW BULKHEAD SUPPORT IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED IAW SRM 51-40-05-0G-0. RECEIVED NEW PART ITEM 7530142 P.O. 691988

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

FLOORBOARD 221DF CORRODED AT INSERTS. REPAIRED FLOORBOARD IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

FORWARD CARGO DOOR FORWARD SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 24. R&R SHIELD IAW SRM AND DWG.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

FLOORBOARD 221BF CORRODED AT INSERTS. R&R FLOORBOARD IAW SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 63,449 hrs · 37,128 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** FLOOR BEAM HAS SMALL AREA OF CORROSION AT BS 328; RBL 45; WL 208. / BLENDED OUT CORROSION AT STA 328 RBL 45 WL 208. I-A-W SRM 51-10-02-0G-0. L = 1' W = 1' DEEP = .030 OUT OF LIMITS PER SRM 53-10-51-1A-1. SHOT PEENED AREA PER BSOPM 20-10-03 FABRICATED REPAIR STRAP PER SRM 53-10-51-2R-8. MATERIAL USED 7075T6.100' LOT# 617256. TREATED AND PRIMED PER AMM 51-10-02-0G-0. INSTALLED REPAIR PER SRM 53-10-51-2R-8. AT STA 328 RBL 49 WL 208.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

FORWARD CARGO FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500C+10, RBL 24. R&R ANGLE IAW SRM AND DWG.

Part: NONE — CORRODED (FED THRESHOLD) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** L1 DOOR SILL PLATE ASSEMBLY HAS CORROSION ON CORD STA 294 - 344; WL 208; LBL 60 TO 65 / L-1 DOOR LOWER SILL CHORD PN: 654A0004-1073 REMOVED AND REPLACED I/A/W B737 SRM 51-40-02 PARA 4;5;7; DRW 141A8110 SH 3;5;9 DRW 141A5220 SH 1. EWIS PROTECTION APPLIED AND REMOVED I/A/W B737 AMM 20-60-07- CIC APPLIED I/A/W B737 AMM 21-21-91 PARA 3. LOCATION: L-1 DOOR SILL PLATE STA. 294-344 WL 208; LBL 60 TO 65 57256U 08/08/18 L1 DOOR SILL FOUND TO BE OUT OF LIMITS IAW SRM 53-10-05-1A-1 56415R 8/8/18

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

R1 DOOR MOP SILL CORRODED. R&R MOP SILL IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,449 hrs · 37,128 cycles

RT HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663+2, RBL 40. REPAIRED WEB PER EA.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** FLOOR BOARD 222BF HAS INSERTS CORRODED WITH SMALL AREA OF DELAM. / REPAIRED FLOOR BOARD 222BF CORRODED INSERTS WITH SMALL AREA OF DELAMINATION I.A.W 737 SRM 53-00-50-2R-3; PARA 1; 3 A.B.C.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

INTERNAL SURFACE OF FILLER OF EXISTING SKIN CORRODED AT BS 801, BETWEEN STR 25R TO STR 26R. R&R SKIN PER SRM & EA.

Part: BLOCK — CORRODED (CABIN) · airframe 63,449 hrs · 37,128 cycles

***CORROSION*** FLOOR BEAM TO SEAT TRACK ATTACH BLOCK CORRODED AT BS 360; RBL 45; WL 208. / REMOVED AND REPLACED WITH SERVICEABLE FILLER IAW SRM 51-40-02-0G-0 SRM 53-10-52-01-1; DWG# 141A5300. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS IN SRM 57042C 08AUG18 PART #149A5510-217; PO #695329

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 63,449 hrs · 37,128 cycles

R2 DOOR INNER CHORD CORRODED BETWEEN BS 887 TO BS 1016. R&R CHORD IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,449 hrs · 37,128 cycles

L2 DOOR MOP SILL CORRODED. R&R MOPSILL IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,449 hrs · 37,128 cycles

FLOOR PANEL 232FF AFT L/H CORNER SMASHED . / FLOOR PANEL 232FF AFT L/H CORNER SMASHED REPAIRED IAW SRM 53-00-50-2R-4 TABEL 201 AND IAW SRM 53-00-50-2R-0

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 63,449 hrs · 37,128 cycles

FWD CARGO DOOR LOWER FWD CORNER SCUFF PLATE CRACKED / RECEIVED NEW FWD CARGO DOOR LOWER FWD CORNER SCUFF PLATE PO# 698740. TO BE INSTALLED ON CUSTOMER CARD 753-140-00-01Y PLACED ON RACK

Part: BRACKET — CRACKED (LEFT WING) · airframe 63,449 hrs · 37,128 cycles

SEAL RETAINER; ATTACH BRACKET CRACKED; T/E OF L/H WING; JUST ABOVE L/H ENG SAIL FIN / REMOVED SEAL RETAINER ATTACH BRACKET. REMOVED AND REPLACED SEAL RETAINER ON ATTACH BRACKET T/E OF L/H WING JUST ABOVE L/H ENGINE SAIL FIN. ALL WORK COMPLETED IN ACCORDANCE WITH SRM 51-40-02-0G-0; AND AMM 20-50-11 59025U 06AUG18.

Part: SKIN — CRACKED (SLAT) · airframe 63,449 hrs · 37,128 cycles

#3 SLAT CRACKED AT ACTUATOR ATTACHMENT FASTENER / #3 SLAT SKIN CRACK REPAIRED I/A/W B737 SRM 57-42-01-2R-8.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 62,349 hrs · 36,439 cycles

R1 DOOR ESCAPE SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: HOOK — LOOSE (L1 DOOR) · airframe 61,754 hrs · 36,068 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: PLATE — BROKEN (RIGHT WING) · airframe 60,626 hrs · 35,361 cycles

WIGGLE PLATE ON LOWER PANEL JUST AFT AND INBOARD OF #2 ENGINE STRUT HAS 3 FASTENERS BROKEN. / REMOVED AND REPLACED PLATE AND FASTENERS PER 51-40-02 SRM.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 60,626 hrs · 35,361 cycles

SEAL CHANNEL BRACKET AT MID SPAN DEFLECTION RIB CRACKED AT ATTACHING BOLTS. / REMOVED AND REPLACED SEAL BRACKET REF SRM 51-40-02.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 60,626 hrs · 35,361 cycles

RIGHT WING FIXED UPPER TRAILING EDGE PANEL JUST AFT OF #2 ENGINE STRUT SEAL CHANNEL BRACKET CRACKED AT ATTACH POINT. / REMOVED AND REPLACED SEAL BRACKET REF SRM 51-40-02.

Part: LIGHT — LOOSE (CABIN) · airframe 59,458 hrs · 34,628 cycles

L1 DOOR LOWER EXIT LIGHT LENS LOOSE. R&R LIGHT ASSEMBLY PER MMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,568 hrs · 34,104 cycles

LT OVER WING EXIT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. R&R BATTERY PACK PER M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,568 hrs · 34,104 cycles

RT OVER WING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. R&R BATTERY PACK PER M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,568 hrs · 34,104 cycles

LT EMERGENCY BATTERY PACK FAILED CAPACITY TEST AT ROW 17. R&R BATTERY PACK PER M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,568 hrs · 34,104 cycles

AFT GALLEY LT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. R&R BATTERY PACK PER M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,568 hrs · 34,104 cycles

AFT GALLEY RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. R&R BATTERY PACK PER M/M.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 57,751 hrs · 33,612 cycles

AFT GALLEY EMERGENCY EXIT LIGHT SIGN LOOSE. R&R LIGHT ASSEMBLY PER MM.

Part: STRAP — DETACHED (EMERGENCY EQUIP) · airframe 57,324 hrs · 33,358 cycles

RIGHT EMERGENCY EXIT ROW STRAP COVER DETACHED. R & R STRAP ASSEMBLY IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,147 hrs · 33,244 cycles

LEFT SIDEWALL EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,147 hrs · 33,244 cycles

RIGHT EMERGENCY LIGHT INOPERATIVE BETWEEN ROW 8 TO ROW 13. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,147 hrs · 33,244 cycles

AFT GALLEY AREA EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,147 hrs · 33,244 cycles

FORWARD GALLEY AREA CENTER EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,147 hrs · 33,244 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 24.75. REPAIRED FLOORBEAM IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 57,147 hrs · 33,244 cycles

LEFT WING, NR 3 FLAP TRACK FAIRING CRACKED ON FORWARD EDGE. REPAIRED NR 3 FAIRING IAW SRM.

Part: FAIRING — CRACKED (LT WING TE FLAP) · airframe 57,147 hrs · 33,244 cycles

LEFT WING NR 3 FLAP TRACK FAIRING CRACKED. REPAIRED THE FAIRING IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,147 hrs · 33,244 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON LEADING EDGE ACCESS PANEL ON HSS 83.50. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,147 hrs · 33,244 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED LOCATED LEADING EDGE ACCESS PANEL ON HSS 83.50. R & R THE RIB IAW SRM AND DWG.

Part: SEAT TRACK — CRACKED (BS 727B-727C) · airframe 57,147 hrs · 33,244 cycles

SEAT TRACK CRACKED BETWEEN BS 727B - 727C+10, RBL 24.7. REPAIRED THE SEAT TRACK IAW SRM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 57,147 hrs · 33,244 cycles

LEFT WING FLAP TRACK FAIRING 544BB CRACKED ON INTERNAL CAVITY. REPAIRED FAIRING IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 57,147 hrs · 33,244 cycles

RIGHT WING LEADING EDGE SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB SLAT STATION 202.45. REPAIRED THE SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,147 hrs · 33,244 cycles

LEFT WING L/E NR 4 SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB, SLAT STA 85.19. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 57,147 hrs · 33,244 cycles

RIGHT WING LEADING EDGE SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB SLAT STA 451.97. REPAIRED THE SKIN IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,333 hrs · 32,175 cycles

MID LEFT CABIN EMER LIGHT BATTERY INOPERATIVE. R & R BATTERY IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,333 hrs · 32,175 cycles

MID LT CABIN EMER LIGHT BATTERY INOPERATIVE. R & R CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,333 hrs · 32,175 cycles

LEFT FWD CABIN EMER LIGHT BATTERY INOPERATIVE. R & R CHARGER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,241 hrs · 32,121 cycles

DIVERSION & DECLARED EMER. FLIGHT ATTENDANTS & PAXS REPORTED THE SMELL OF SMOKE OR ELEC FIRE, MID CABIN CAPTAINS SIDE. FOUND INOPERATIVE CEILING LIGHT AT ROW 15DEF. R & R LIGHT IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 55,175 hrs · 32,076 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT & MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 54,132 hrs · 31,460 cycles

R2 DOOR EMER SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,057 hrs · 31,411 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 53,327 hrs · 30,991 cycles

L1 DOOR GIRT BAR BRACKET LOOSE. SECURED BRACKET IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 53,057 hrs · 30,849 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,267 hrs · 30,391 cycles

L1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,267 hrs · 30,391 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,008 hrs · 30,245 cycles

L1 DOOR EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 51,767 hrs · 30,112 cycles

REAR OVERHEAD EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: PLATE — CORRODED (L2 DOOR) · airframe 50,825 hrs · 29,591 cycles

R2 DOOR GIRT BAR PLATE CORRODED. R & R PLATE IAW MMM.

Part: PLATE — CORRODED (L2 DOOR) · airframe 50,825 hrs · 29,591 cycles

L2 DOOR GIRT BAR PLATE CORRODED. R & R PLATE IAW MMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK INBD FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK INBD FASTENER HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK OTBD FASTENER HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK OTBD FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK OTBD FASTENER HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK INBD FASTENER HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK OTBD FASTENER HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

FORWARD SEAT TRACK INBD FASTENER HOLE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

SEAT TRACK FASTENER HOLE D CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST CRACKED AT FASTENER HOLE 2ND FROM THE BOTTOM. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME E - F POST CRACKED AT FASTENER HOLE 2ND FROM THE BOTTOM. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

LEFT NR 1 FLIGHT DECK WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST CRACKED AT FASTENER HOLE 3RD FROM THE BOTTOM. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,825 hrs · 29,591 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME E - F POST FASTENER HOLE 4TH FROM THE BOTTOM CRACKED. REPAIRED POST IAW ACO & SRM.

Part: COVER — MISSING (CABIN) · airframe 50,374 hrs · 29,318 cycles

OVERWING EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,993 hrs · 29,107 cycles

MID CABIN EMER LIGHT BATTERY PACK FAIL CAPACITY CHECK. R & R BATTERY PACK IAW AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,993 hrs · 29,107 cycles

FORWARD ENTRY EMER LIGHT BATTERY PACK FAIL CAPACITY CHECK. R & R BATTERY PACK IAW AMM & DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,993 hrs · 29,107 cycles

FORWARD EMER LIGHT BATTERY PACK FAIL CAPACITY CHECK. R & R BATTERY PACK IAW AMM & DWG.

Part: SLIDE — TORN (L2 DOOR) · airframe 48,051 hrs · 27,971 cycles

L2 DOOR SIDE SLIDE GIRT BAR ATTACHMENT FLAP SECTION TORN. R & R SLIDE ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 47,863 hrs · 27,856 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SIGN — BROKEN (CABIN) · airframe 46,985 hrs · 27,344 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. R&R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,147 hrs · 26,870 cycles

LEFT AFT EMERGENCY SIGN LIGHT INOP. RELAMPED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,147 hrs · 26,870 cycles

LEFT OVERWING EMERGENCY LIGHT INOP. RELAMPED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 46,147 hrs · 26,870 cycles

RIGHT OVERWING EMERGENCY LIGHT INOP. RELAMPED SIGN IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,475 hrs · 26,469 cycles

RIGHT MID CABIN EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 45,475 hrs · 26,469 cycles

L1 DOOR ESCAPE SLIDE GIRT BAR FORWARD RETAINING CLIP LOOSE. SECURED CLIP PER THE MM.

Part: LENS — BROKEN (CABIN) · airframe 43,923 hrs · 25,508 cycles

LEFT OVERWING DOOR SLIDE LIGHT NUT PLATE LENS ASSY BROKEN. REMOVED AND REPLACED LENS ASSY PER SRM & AMM.

Part: CONNECTOR — DISCONNECTED (L1 DOOR) · airframe 43,923 hrs · 25,508 cycles

L1 DOOR EMERGENCY EXIT SLIDE LIGHT INOP. RECONNECTED CONNECTOR PER SWPM & MM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 43,923 hrs · 25,508 cycles

LEFT OVERWING EMERGENCY EXIT SLIDE LIGHT INOP. RECONNECTED CONNECTOR PER SWPM & MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FLOORBEAM CRACKED AT BS 294.5, RBL 16. REPAIRED BEAM PER ATS ER AND EA.

Part: SILL — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FORWARD SERVICE DOOR CUTOUT FLOOR SILL WEB CRACKED AT BS 294, WL 208. REMOVED AND REPLACED WEB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

STRINGED CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW ER AND EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

SHEAR TIE CRACKED AT BS 344, BETWEEN STR 5L TO STR 6L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

R1 DOOR CUTOUT FWD FRAME CRACKED AT I/B FLANGE, BS 295, WL 208. REPAIRED FRAME PER EA AND ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

FLOORBEAM UPPER "T" CHORD CORRODED AT BS 986, RBL 43. REMOVED AND REPLACED "T" CHORD PER SRM.

Part: WEB — CANNING (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

OIL CANNED WEB AT BS 1018 TO BS 1025, WL 208, LBL 5 TO LBL 11. REPAIRED WEB PER EA AND ER.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

STRINGER SUPPORT ANGLE CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED ANGLE PER SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 43,923 hrs · 25,508 cycles

STRINGER SUPPORT ANGLE CRACKED BS 500D, STR 19L. REMOVED AND REPLACED ANGLE PER SRM & DWG.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 42,811 hrs · 24,835 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,822 hrs · 24,265 cycles

EMERGENCY EXIT DOOR LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LATCH — LOOSE (R1 DOOR) · airframe 41,692 hrs · 24,183 cycles

R1 DOOR, FRONT GIRT BAR HOLDER LATCHES LOOSE. SECURED LATCHES PER MM.

Part: CHECK VALVE — LOCKED (NR 2 ENGINE) · airframe 41,601 hrs · 24,122 cycles

IN FLIGHT SHUTDOWN AT 34,000FT, IN A SLIGHT DESCENT RT ENGINE RPM ROLLED TO ABOUT 44 PERCENT ALONG WITH "POPPING SURGING" VIBRATION. FOUND 5TH STAGE CHECK VALVED LOCKED IN CLOSE POSITION. REMOVED AND REPLACED NR 2 ENG 5TH STAGE CHECK VALVED PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,342 hrs · 23,962 cycles

DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,342 hrs · 23,962 cycles

DURING SCHEDULED HC1 CHECK, CENTER RT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 40,239 hrs · 23,331 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 36,605 hrs · 21,215 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN PUNCTURED. REPAIRED AFT FLAP PER EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 36,605 hrs · 21,215 cycles

DURING SCHEDULED 10Y CHECK, FOUND LOWER CHORD CRACKED AT BS 663.75, LBL 4.1. REPAIRED CHORD PER EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 36,605 hrs · 21,215 cycles

DURING SCHEDULED 10Y CHECK, FOUND HORIZONTAL STIFFENER CRACKED AT BS 663.75, BETWEEN LBL 6 TO LBL 32. REPAIRED STIFFENER PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,605 hrs · 21,215 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 9. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,605 hrs · 21,215 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,605 hrs · 21,215 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,605 hrs · 21,215 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 35,681 hrs · 20,682 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER LOOSE BETWEEN ROW 9 TO ROW 10. REMOVED AND REPLACED EEPLS PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,091 hrs · 20,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,091 hrs · 20,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 34,568 hrs · 20,015 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 7 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED NR 7 SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,373 hrs · 19,893 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 32,237 hrs · 18,628 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS ASSY BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 32,105 hrs · 18,503 cycles

AFT RT EMERGENCY EXIT LIGHT LENS BROKEN BY R1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 31,367 hrs · 18,063 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 31,367 hrs · 18,063 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LOWER LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 31,199 hrs · 17,975 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVACUATION SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 31,100 hrs · 17,913 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B AFT FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,408 hrs · 17,495 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. SECURED CONNECTOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,360 hrs · 17,462 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,215 hrs · 17,381 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,215 hrs · 17,381 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,215 hrs · 17,381 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, BETWEEN RBL 5 TO LBL 5. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,215 hrs · 17,381 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,215 hrs · 17,381 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 36 TO RBL 5. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,215 hrs · 17,381 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AT BS 947, BETWEEN LBL 5 TO RBL 5. REPAIRED BEAM PER SWA EA.

Part: BATTERY PACK — FAILED (COCKPIT) · airframe 30,119 hrs · 17,314 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT FAILED FUNCTION TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,979 hrs · 17,228 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 28,427 hrs · 16,304 cycles

FWD CABIN EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: PUMP — FAILED (NR 1 ENGINE) · airframe 27,621 hrs · 15,829 cycles

NR 1 ENGINE FAILED DURING TAXI. REMOVED AND REPLACED FUEL PUMP AND HMU PER MM.

Part: COALESCER BAG — ODOR (A/C PACK) · airframe 26,879 hrs · 15,399 cycles

AIR TURNBACK. SMOKE ODOR ALONG WITH BURNING ODOR IN COCKPIT DURING TAKEOFF AND CLIMB. RETURNED TO BASE. REMOVED AND REPLACED A/C COALESCER BAGS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 26,352 hrs · 15,091 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,937 hrs · 13,141 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 22,937 hrs · 13,141 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,937 hrs · 13,141 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,899 hrs · 11,423 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HEAT EXCHANGER — FAULTY (NR 1 ENGINE) · airframe 19,758 hrs · 11,341 cycles

DIVERSION/INFLT SHUTDOWN/DECLARED EMERGENCY. NR 1 ENGINE LEAKING FUEL. NR 1 ENGINE SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE FUEL/OIL HEAT EXCHANGER PER MM.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 19,327 hrs · 11,105 cycles

AIR TURNBACK/DECLARED EMERGENCY, 2 LOUD BANGS HEARD, ALONG WITH MODERATE TO SEVERE VIBRATIONS FELT FROM NR 2 ENGINE. NR 2 ENGINE FUEL FLOW ERRATIC. ALL OTHER INDICATIONS NORMAL. FLAME SEEN FROM NR 2 ENGINE EXHAUST. REMOVED AND REPLACED NR 2 EEC, T12 SENSOR, 5TH STAGE PNEUMATIC BLEED CHECK VALVE AND N2 SENSOR PER MM. DURING TEST FLIGHT FOR COMPRESSOR STALL, NR 2 ENGINE STALLED TWICE DURING CLIMB. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: HMU — FAULTY (RT ENGINE) · airframe 19,319 hrs · 11,097 cycles

LOUD BANG HEARD FROM RT SIDE OF AIRCRAFT. FLAME SEEN FROM NR 2 ENGINE EXHAUST. ENGINE PARAMETERS NORMAL. SUSPECT COMPRESSOR STALL. PERFORMED ENGINE BOROSCOPE. NO DAMAGE FOUND. REMOVED AND REPLACED NR 2 ENGINE HMU PER MM.

Part: SIGN — BROKEN (AFT GALLEY) · airframe 18,613 hrs · 10,713 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,399 hrs · 7,785 cycles

DURING SPV, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 12,302 hrs · 7,166 cycles

FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVACUATION SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 11,538 hrs · 6,720 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS CRACKED (10 EA) ROWS NR 1, 3, 5, 7, 8, 11, 12, 16, 17 AND 18. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 10,825 hrs · 6,300 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,193 hrs · 5,425 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS INOP AT ROW 23. RELAMPED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 7,948 hrs · 4,724 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FITTING — WORN (RT ELEVATOR) · airframe 7,082 hrs · 4,212 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB NR 2 ATTACH LUG WORN. REMOVED AND REPLACED RT ELEVATOR ATTACH LUG PER MM.

Part: COVER — CRACKED (CABIN) · airframe 6,780 hrs · 4,037 cycles

DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: THROTTLE — MALFUNCTIONED (NR 1 ENGINE) · airframe 4,723 hrs · 2,840 cycles

IN FLIGHT ENGINE SHUT DOWN, DECLARED EMERGENCY. AT FL 390, NR 1 ENG THROTTLE WOULD NOT RESPOND. CAME BACK TO 85.1 PERCENT N1, AFTER 30 MINUTES WENT TO 79 PERCENT N1. NO OTHER ABNORMAL INDICATION FOUND BEFORE SHUT DOWN. C/W NR 1 ENG INSP, C/W NR 1 EEC BITE CK. NO DEFECT, FAULTS NOTED. C/W TWO POWER ASSURANCE ENG RUNS AND OPS CK GOOD. ACFT OK FOR SERVICE PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 3,384 hrs · 2,013 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RH ELEVATOR TAB # 2 HINGE BUSHING WORN. R&R HINGE BUSHING PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 2,902 hrs · 1,701 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND RH ELEVATOR TAB # 2 HINGE BUSHING WORN. R&R ELEVATOR TAB BUSHING PER MM.

Part: RETAINER — OUT OF POSITION (ESCAPE SLIDE) · airframe 1,219 hrs · 720 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE RETENTION BAR HITTING FUSELAGE DURING DOOR CLOSING/OPENING. REMOVED AND REPLACED EVAC SLIDE COVER PER MM.