N748SW

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 78,863 hrs · 47,095 cycles

AFT ENTRY DOOR EMER EXIT LIGHT LENS BROKEN. R & R LIGHT ASSY & OPS CK OK PER M/M 33-51-01

Part: COVER — MISSING (ZN 800 DOOR) · airframe 78,331 hrs · 46,745 cycles

AFT SERVICE DOOR SLIDE EMERGENCY PULL HANDLE COVER MISSING / [01] FOUND MISSING HANDLE COVER AND REATTACHED IAW AMM 25-66-01.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 78,206 hrs · 46,662 cycles

EMERGENCY LIGHTS AT ROWS 3&6 FED; 9&12 ABC AND FWD ENTRY EXIT SIGNS INOP. / [01] R&R BATTERY PACKS AT LOCATIONS M1674 AND M1670 PER AMM 33-51-06. OPS CHECK GOOD.

Part: COVER — LOOSE (PAX CABIN) · airframe 77,825 hrs · 46,407 cycles

18F EMERGENCY EXIT LIGHT COVER / [01] SECURED EMERGENCY EXIT LIGHT COVER PER SIP

Part: SLIDE — OUT OF POSITION (AFT SERVICE DOOR) · airframe 76,734 hrs · 45,702 cycles

AFT SERVICE DOOR SLIDE COVER HAS A GAP AS REPORTED BY FA. / [01] R&R AFT SERVICE DOOR SLIDE & COVER PER MT 725-61-06 INSP PER AMM 25-66-01 REINSTALLED SLIDE & COVER.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 76,163 hrs · 45,352 cycles

AFT ENTRY DOOR SLIDE NOT SECURED PROPERLY ; / [01] FOUND DOOR SLIDE SECONDARY PULL COVER NOT IN PLACE. SECURED ASS NEEDED REF AMM 25-66-01 ( AFT ENTRY DOOR)

Part: FLOOR PANEL — ELONGATED (AFT CARGO) · airframe 73,763 hrs · 43,887 cycles

ELONGATED HOLE FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT (15 EA). FABRICATED NEW FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 DWG NR 453A2610 SHEET 10 REV F FABRICATED FROM ALUMINUM SHEET 0.080' PN 2024T3 CLAD 0.080' PO 2020 213566.

Part: STUB FRAME — CRACKED (FWD GALLEY) · airframe 73,763 hrs · 43,887 cycles

CRACK AREA SERVICE DOOR STUD FRAME AT LEVEL BS297.5 AND BTW STR 7R TO STR 10R AT FWD GALLEY AREA. REPLACED SERVICE DOOR STUD FRAME AT LEVEL BS 297.5 AND BTW STR 7R TO STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG # 141A8370 REV C PART NUMBER USED 141A8371U7 (FRAME) PO # 2021 105650.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 73,763 hrs · 43,887 cycles

CORROSION STRINGER 23R LOCATED BS540 AT WL 156 FWD CARGO COMPARTMENT. REPAIRED STRINGER 23R LOCATED BETWEEN BS500D TO BS 540 AT WL 156 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 PARAGRAPH 4. MADE REPAIR PARTS MATERIAL USED 7075-T0-0-036-7075-T0 0.040 PO (2021-110046) PO (2020-203286) HEAT TREATED AND CONVERTED FROM 7075-T0 0.036/7075-T0 0.040 TO CONDITION T6 IAW BAC5602 TOOL USED TERMPERATURE CONTROLLER PN P3015GOES00000 SN 112820025 DUE DATE 22JAN22.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 73,763 hrs · 43,887 cycles

CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 26R LOCATED BS500D+10' TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 PARAGRAPH 4. DWG 143A1215 SHEET 58 REV - DWG 143A3230 SHEET 10 REV B. MADE REPAIR PARTS STRINGER SECTION (1EA) ANGLE (2EA) CHANNEL (1EA) IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED 7075T0/0.045' 0.050'. HEAT TREATMENT REPAIR PARTS CONVERTED FROM 7075T0 TO CONDITION T6 IAW BAC5602 TOOL USED TEMPERATURE CONTROLLER PN P3015G06500000 SN 112031023 DUE DATE 22JAN22 LENGTH CRACK 1.800'.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,763 hrs · 43,887 cycles

CORROSION LOWER SKIN BS 545.8 STR 14 LT AND WING CENTER SECTION FRONT SPAR LBL 49 IN CENTER FUEL TAN. PERFORMED INTERIM REPAIR LOWER SKIN LOCATED BTW BS540 TO BS545.8 STR 14L AND WING CENTER SECTION FRONT SPAR LBL 49 IN CENTER FUEL TANK IAW EA # 57-0104-21 REV 0 AND EA # 21-157-00772 REV IR FOR INSPECTION REQUIREMENTS SEE TLD # T080539.

Part: ANGLE — DAMAGED (LT WING) · airframe 73,763 hrs · 43,887 cycles

ELONGATED HOLE ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT LT WING IAW B737-700 DWG 115A5300 REV D AND SRM 51-40-02.

Part: ANGLE — CRACKED (RT WING) · airframe 73,763 hrs · 43,887 cycles

CRACK FRONT SPAR WEB SUPPORT ANGLE LOC AT (FUEL BOOST PUMP) UPPER SIDE APPROX WBL 94.24 AT RT WING. REPLACED SUPPORT ANGLE AT FRONT SPAR WEB (FUEL BOOST PUMP) UPPER SIDE APPROX WBL 94.24 AT RT WING IAW DWG 112A2004 REV A AND DWG 116A3001 REV A B737-700 SRM 51-40-02 P/N USED (EXTRUSION) 7050-T7451AMS4050 PO 2021-124805.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 73,763 hrs · 43,887 cycles

CRACK STRINGER 27L LOCATED BS540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 27L LOC BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 PARAGRAPH 4; DWG 143A3230 REV A - SHEET 7 DWG 143A1215 SHEET - REV B; MADE REPAIR PART STRINGER SECTION 1 (1EA) ANGLE (2EA) CHANNEL (1EA) IAW B737-700 SRM 53-00-03-2R-1 MATERIAL USED 7075 TO 0.056';0.063' HEAT TREATMENT REPAIR PARTS CONVERTED FROM 7075 TO CONDITION T6 IAW BAC5602 TOOL USED TEMPERATURE CONTROLLER PN P301560B00000 SN 112031023 DUE DATE 22-JAN-22.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 73,763 hrs · 43,887 cycles

CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 26 L LOC BTW BS 500D TO BS 540 FWD C.C IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 DWG NR 143A3230 REV A MATERIAL USED 7075-TO 0.045' PO NR 2021113097; 7075-TO 0.050' PO NR 2020 213289 AND HEAT TREATMENT AND CONVERTED TO TO T6 AND MEASURE OF CRACK L=0.375' TOOL USED CALIPER PN 700-113-10 SN 0033178 DUE DATE 30-JUL-21 NDT USED PN 35DL SN 091419910 DUE DATE 30-NOV-21 PN NORTEC 500D SN N500X12101V022237 DUE DATE 24-AUG-21.

Part: WEB — CRACKED (VERTICAL STAB) · airframe 73,763 hrs · 43,887 cycles

(CRACK ON WEB AT DORSAL FIN PANEL STA 867.95.) REPLACED WEB AT DORSAL FIN PANEL STA 867.95 IAW B737-700 SRM 51-10-02 PARAG 9 AND DWG NR 174A0101 REV B.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 73,763 hrs · 43,887 cycles

CRACK STRINGER 25L LOCATED BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 25L LOC BTW 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 DWG 143A3230 REV A MATERIAL USED 7075-T0 0.050' PO NR 202021328900101; 7075 TO 0.045' PO#2021 11309700101 AND HEAT TREATMENT AND CONVERTED TO TG AND MEASURE OF CRACK L=0.605' TOOL USED CALIPER PN 500-752-20 SN B16101278 DUE DATE 14-SEP-21 NDT USED PN NORTEC 500D SN NSWX22101V022237 DUE DATE 24-AUG-21 ULTRASONIC GAUGE PN 45MG SN 130064101 DUE DATE 08-APR-21.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 73,763 hrs · 43,887 cycles

CRACK STRINGER 23L LOCATED BS540 FWD CARGO COMPARTMENT. REPAIRED STR 23L LOC BTW BS500D +10 TO BS540 FWD COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 PARAGRAPH 4(1C) DWG 143A3210 REV B SHEET 19 ADN DWG 143A0060 SHEET 1 REV F MATERIAL USED 7075 TO 0.036' 0.040' TO CONDITION T6 MAKE REPAIR PARTS STRINGER SECTION ANGLE (2EA) CHANNEL (1E/A) 70757 TO 0.036 0.040' TO CONDITION T6 TOOL USED TEMPERATURE CONTROLLER PN P3015G0E00000 SN 112031023 DUE DATE 22-JAN-22 LENGTH CRACK 0.880'.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,763 hrs · 43,887 cycles

CRACK SUPPORT ANGLE LOCATED BS540 AND BETWEEN BL0 TO RBL24.5 CENTER SECTION. REPLACED SUPPORT ANGLE LOCATED BS540 BTW BL0 TO RBL 24.5 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PN USED 143A5240U34 PLATE PO 2021-124879.

Part: BEAR STRAP — CRACKED (ZONE 200) · airframe 73,763 hrs · 43,887 cycles

CRACK INDICATION FOUND (2 E/A) ON THE BEAR STRAP. LOC FWD GALLEY DOOR R1 BS CUT OUT FROM BS 290 TO BS 296 BTW S-8R AND S-9R. CRACK 1 DIRECTION IS 9 O’CLOCK OF FASTENER AND LENGTH 0.240 INCH. CRACK 2 DIRECTION IS 3 O’CLOCK OF FASTENER AND LENGTH 0.400 INCH. REPAIRED BEAR STRAP LOC AREA FWD GALLEY DOOR R1 FUSELAGE SKIN AREA IAW B737-700 EA NR 53-0094-21 PART NR 1; 53-0094-21 REV NR 0 AND EA NR 21-153-00788 REV IR FOR INSPECTION REQUIREMENTS SEE TLD T080537.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,763 hrs · 43,887 cycles

CRACK SUPPORT ANGLE LOCATED BS695 AND RBL0 AT LEVEL FLOOR STRUCTURE CENTER SECTION (1 EA). REPLACED SUPPORT ANGLE LOC BS695 AND RBL0 AT LEVEL FLOOR STRUCTURE CENTER SECTION (1EA) IAW B737-700 SRM 51-10-02 NEW SUPPORT ANGLE P/N IS=BAC1490-2883 IAW DWG 273A9112 SHEET 31 REV - (PO # 2020 195975).

Part: SUPPORT ANGLE — ELONGATED (CABIN) · airframe 73,763 hrs · 43,887 cycles

ELONGATED HOLE SUPPORT ANGLE LOCATED BS540 AND BETWEEN LBL 24.5 TO LBL 45 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 540 BETWEEN LBL 24.5 TO LBL 45 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 DWG 143A5240 SHEET 12 REV -.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,763 hrs · 43,887 cycles

CRACK SUPPORT ANGLE LOCATED BS540 AND BETWEEN BL0 TO LBL24.5 CENTER SECTION (1 EA). REPLACED SUPPORT ANGLE LOCATED BS540 AND BETWEEN BLO TO LBL 24.5 CENTER SECTION (1EA) DUE TO NO FOUND ALLOWABLE DAMAGE PART NUMBER WEB 143A5240U33 2021 11390 IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A5240 SHEET 3 REV B.

Part: SKIN — DENTED (EXTERIOR) · airframe 73,763 hrs · 43,887 cycles

DENT EXTERNAL SKIN LOC. AT BS 420 MORE 8 INCHES AND 2 INCH BELOW STR 21R AT LOWER FUSELAGE (1 EA).

Part: SKIN — CRACKED (LT WING SLAT) · airframe 73,763 hrs · 43,887 cycles

CRACK LOWER SURFACE SLAT SKIN LOCATED SLAT STATION 85.19 AT LT WING. NO MAINTENANCE ACTION REQUIRED DUE TO SLAT 4 AT LT WING WILL BE REPLACED AND IS DOCUMENTED ON NRC L198721 AND ACCESS PANEL 522CB; 522DB; 522EB MUST BE DOCUMENTED ON NRC L198721.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 73,763 hrs · 43,887 cycles

CRACK LEADING EDGE RIB STAB STA 95.96 AT RT HORIZONTAL STABILIZER. REPLACED NEW RIB ON LEADING EDGE STAB STA 95.96 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10- 02 AND DWG 186A1303 SHEET 1 REV - PN USED CHORD 186A1352-6 P/O 2021-127001.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 73,763 hrs · 43,887 cycles

CRACK INSPAR RIB 129.50 AT 27 INCHES OF FRONT SPAR LT HORIZONTAL STAB. REPAIRED INSPAR RIB 129.50 AT 27 INCHES OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09 -2R-4 REPAIR 4.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,733 hrs · 43,870 cycles

EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M01669 AND M01672 FAILED CAPACITY CHECK / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M01669 AND M01672 PER AMM 33-51-06

Part: SEAL — CRACKED (ACCESS DOOR) · airframe 73,733 hrs · 43,870 cycles

FWD ACCESS DOOR PRESSURE SEAL IS CRACKED ON RH AND LH SIDES / REMOVED AND REPLACED FWD ACCESS DOOR PRESSURE SEAL PER AMM 52-09-11.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 73,318 hrs · 43,611 cycles

LT OVERWING EMERGENCY EXIT LOCATOR SIGN BROKEN. REMOVED & REPLACED EMERGENCY EXIT SIGN AT LT OVERWING EXIT TOPS NORMAL, IAW AMM 33-51-01.

Part: ANGLE — CRACKED (RT WING) · airframe 72,646 hrs · 43,172 cycles

RIGHT WING TRAILING EDGE FLAP DEFLECTOR BEAM TO UPPER PANEL 'L' ANGLE IS CRACKED AT DEFLECTOR BEAM. / R&R RIGHT WING TRAILING EDGE FLAP DEFLECTOR BEAM TO UPPER PANEL 'L' ANGLE PER MM.20-50-11

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,814 hrs · 42,652 cycles

EMERGENCY BATTERY PACK AT M1675 WOULD NOT CHARGE. / R&R EMERGENCY LIGHT BATTERY PACK M1675 IAW AMM.

Part: STRINGER — CRACKED (BS 1016) · airframe 71,814 hrs · 42,652 cycles

STRINGER AT BS. 1016, STR. 21R AFT HOLE ON OUTBOARD VERTICAL ROW SHOWED CRACK INDICATION. / REPAIRED STRINGER PER ER AND EA.

Part: TEE FITTING — CORRODED (BS 1016) · airframe 71,814 hrs · 42,652 cycles

FORWARD SIDE ON T-FITTING CORRODED AT BS. 1016, STR. 21R. / R&R T FITTING PER SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (BS 360) · airframe 71,814 hrs · 42,652 cycles

STRINGER FLANGE CORRODED AT BS. 360-1, STR. 24R. / R&R STRINGER SPLICE PER SRM AND DWG.

Part: TEE FITTING — CORRODED (BS 1016) · airframe 71,814 hrs · 42,652 cycles

T-FITTING CORRODED ON FORWARD SIDE OF BS. 1016, STR. 23R. / R&R T-FITTING IAW SRM & DWG.

Part: SIGN — MISSING (CABIN) · airframe 69,466 hrs · 41,122 cycles

R/H OVERWING EXIT SIGN MISSING. / R&R SIGN PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,206 hrs · 40,952 cycles

M1673 AFT EMERGENCY POWER SUPPLY INOP AT BS. 952, LBL 13. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,206 hrs · 40,952 cycles

M1668 MID EMERGENCY POWER SUPPLY INOP AT BS. 603, LBL 67. R&R BATTERY PACK PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,206 hrs · 40,952 cycles

M1673 AFT EMERGENCY POWER SUPPLY INOP AT BS. 952, LBL 13. R&R POWER SUPPLY PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,206 hrs · 40,952 cycles

M1668 MID EMERGENCY POWER SUPPLY INOP AT BS. 603, LBL 67. R&R POWER SUPPLY PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,206 hrs · 40,952 cycles

M1674 FORWARD EMERGENCY POWER SUPPLY INOP AT BS. 322, RBL 7. R&R BATTERY PACK PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,206 hrs · 40,952 cycles

M1674 FORWARD EMERGENCY POWER SUPPLY INOP AT BS. 322, RBL 7. R&R POWER SUPPLY PER AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO COMPT) · airframe 69,206 hrs · 40,952 cycles

FORWARD CARGO BAY FWD SCUFF PLATE IS CRACKED / REMOVED AND REPLACED FWD CARGO BAY FWD SCUFF PLATE IAW AMM 53-11-02-420-801 AND AIPC 53-13-00-08 81489U 26APR19

Part: GUSSET — CRACKED (BS 500D) · airframe 69,206 hrs · 40,952 cycles

GUSSET JUST FWD OF STA 500D FRAME AT S-19L CRACKED. REMOVED & REPLACED GUSSET PER SRM

Part: FLOOR SUPPORT — CRACKED (BS 500C-500D) · airframe 69,206 hrs · 40,952 cycles

FORWARD CARGO BAY INTERCOSTAL AT BS 500C TO BS 500D LBL 24 WL 156 IS CRACKED REMOVED AND REPLACED FORWARD CARGO BAY INTERCOSTAL IAW SRM

Part: FLOOR SUPPORT — CRACKED (BS 400-420) · airframe 69,206 hrs · 40,952 cycles

FORWARD CARGO BAY INTERCOSTAL AT BS 400 TO BS 420, LBL 24, WL 156 IS CRACKED / REMOVED AND REPLACED INTERCOSTAL PER SRM

Part: FLOOR SUPPORT — DAMAGED (BS 500A-500B) · airframe 69,206 hrs · 40,952 cycles

FWD CARGO BAY INTERCOSTAL AT BS 500A-500B, LBL 22, WL 156 WAS DAMAGED. REMOVED AND INSTALLED INTERCOSTAL IAW SRM 5

Part: SUPPORT FITTING — CRACKED (BS 949) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY AFT BULKHEAD SUPPORT FITTING CRACKED AT BS. 949, LBL 6. R&R FITTING PER DWG AND SRM.

Part: STRINGER — OUT OF TOLERANCE (EMPENNAGE) · airframe 69,206 hrs · 40,952 cycles

HOLE 6L AT STR 2L STA 1016 MEASURES .359 OUT OF TOLERANCE PER SI 12107-53 / REPAIRED HOLE 6L STR 2L BS 1016 PER SI 12107-53 STEP 5C & 5D

Part: WEB — NONE (AFT CARGO BAY) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY VERTICAL WEB HAS OVERSIZED AND ELONGATED HOLES BS787-794; RBL20; WL155. / REMOVED VERTICAL WEB B.S. 787-794 RBL 20; FABRICATED FROM 7075TO .045 LOT # 891881 HEAT TREATED TO T62; LOCATED; DRILLED; APPLIED CHEMICAL CONVERSION COATING; PRIMED & INSTALLED PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 DWG 146A0081; DWG 146A8123

Part: WEB — NONE (AFT CARGO BAY) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY VERTICAL WEB HAS OVERSIZED AND ELONGATED HOLES BS767-787; RBL20; WL155. / REMOVED ACB VERTICAL WEB COATED DRILLED NEW WEB + INSTALLED PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A0081

Part: WEB — CORRODED (FUSELAGE) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY ON VERTICAL WEB CORRODED BETWEEN BS. 787 TO BS. 807, RBL 6. R&R WEB PER SRM AND DWG.

Part: FORMER — CRACKED (LWR FUSELAGE) · airframe 69,206 hrs · 40,952 cycles

LOWER FAIRING FORMER AT BS 663 RBL 27 IS CRACKED / REPAIRED PER: EA 1-757-16198 REV IR AND ATS ER 19-02781 REV IR

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,206 hrs · 40,952 cycles

VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT BS. 663, RBL 10. REPAIRED ANGLE PER EA AND ER.

Part: FRAME — CRACKED (BS 947) · airframe 69,206 hrs · 40,952 cycles

BS 947 FRAME IS CRACKED BETWEEN STR 26R AND STR 27R ON UPPER FLANGE. REMOVED AND REPLACED THE FRAME PER SRM 5

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 69,206 hrs · 40,952 cycles

***CORROSION*** IN MULTIPLE PLACES IN ACB ON R/H FLOOR TO SIDEWALL SUPPORT STA 727-767 RBL 22 WL 156 / CORROSION IN ACB R/H FLOOR TO SIDEWALL SUPPORT STA 727-767 RBL 22 WL156 WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES; REPLACED R/H FLOOR TO SIDEWALL SUPPORT FOR A NEW SUPPORT # 146A7502-51; LOCATED AND DRILLED; INSTALLED FLOOR TO SIDEWALL SUPPORT STA 727-767 RBL22 WL156 PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; SRM 53-00-53-1A-2 FIG 103 DETAIL D; SRM 51-40-05-0G-0; SRM 51-40-02 AND DWG 146A7500 93046U 93046U 11APR19

Part: SHIELD — CORRODED (BS 767-787) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787+7, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY FRAME UPPER FLANGE CORRODED AT BS. 767, BETWEEN RBL 7 TO RBL 24. REPAIRED FLANGE PER EA AND ER.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BIN L/H FLOOR TO SIDEWALL SUPPORT CORRODED AT STA 727-847, LBL 22 WL 158 REPLACED L/H FLOOR TO SIDEWALL SUPPORT PER SRM

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,206 hrs · 40,952 cycles

FRAME CRACKED AT BS. 259, STR. 9L. REPAIRED FRAME IAW ER & EA.

Part: SUPPORT — BROKEN (AFT CARGO) · airframe 69,206 hrs · 40,952 cycles

BROKEN ACB FWD BULKHEAD SUPPORT AT STA 727 RBL 5 WL 163 (MARKED) / REMOVED AND REPLACED BRACKET SUPPORT AT BS 727 RBL 5 WL 163 IAW SRM 51-40-02 AND DWG 144A2600

Part: SUPPORT — CORRODED (BS 400-440) · airframe 69,206 hrs · 40,952 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 440+8, LBL 24. / R&R SUPPORT PER SRM AND DWG.

Part: WEB — CORRODED (BS 440-500) · airframe 69,206 hrs · 40,952 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 500, RBL 26. R&R WEB PER SRM AND DWG.

Part: SUPPORT — CORRODED (BS 867-887) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT CORRODED BETWEEN BS. 867 TO BS. 887, RBL 21. / R&R SUPPORT PER SRM AND DWG.

Part: SHIELD — CORRODED (BS 420-440) · airframe 69,206 hrs · 40,952 cycles

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

Part: SHIELD — CORRODED (BS 494-500) · airframe 69,206 hrs · 40,952 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 494 TO BS. 500, RBL 22. / R&R SHIELD PER SRM AND DWG.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 69,206 hrs · 40,952 cycles

***CORROSION*** FLOOR TO SIDEWALL SUPPORT BEAM; BS 400-420; RBL 24; WL 156 (MARKED) / CORROSION WAS FOUND TO BE OUT OF LIMITS DUE TO THE PROXCIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D. REMOVED & REPLACED FLOOR TO SIDEWALL SUPPORT BEAM; BS 400-420 RBL 24 WL156 AS PER DWG 143A7500 & SRM 51-40-02-0G-0

Part: SUPPORT — CORRODED (BS 500D) · airframe 69,206 hrs · 40,952 cycles

SIDEWALL TO BULKHEAD SUPPORT CORRODED AT BS. 500D, LBL 25. / R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 69,206 hrs · 40,952 cycles

FORWARD CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 22. / R&R SUPPORT IAW SRM

Part: WEB — CORRODED (BS 767-787) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY ON VERTICAL WEB CORRODED BETWEEN BS. 767 TO BS. 787, RBL 7. / R&R WEB PER SRM & DWG.

Part: SEAT TRACK — DAMAGED (BS 480-520) · airframe 69,206 hrs · 40,952 cycles

SEAT TRACK MECHANICALLY DAMAGED BETWEEN BS. 480 TO BS. 520, LBL 45. / R&R SEAT TRACK PER SRM AND DWG.

Part: WEB — CORRODED (BS 627 THRESHOLD) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED AT BS. 827, RBL 25. R&R WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,206 hrs · 40,952 cycles

CREASE BEAM WEB CORRODED BETWEEN BS. 500C TO BS. 500D, RBL 67. R&R CREASE BEAM WEB PER ER & EA.

Part: PANEL — DEBONDED (RH PYLON) · airframe 69,206 hrs · 40,952 cycles

#2 ENGINE PYLON PANEL 441EL IS DISBONDED LWR AFT CORNER / RECEIVED NEW ACCESS PANEL 441EL. POSITIONED NEW PANEL 441EL MATCH DRILLED TO AIRCRAFT STRUCTURE; AND APPLIED PAINT TO EXTERIOR SURFACE. IAW DWG 311A2531; SRM 51-20-07-0G-0; AMM 51-21-99-300-801

Part: SIDEWALL SUPPORT — CORRODED (BS 887-947) · airframe 69,206 hrs · 40,952 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 887 TO BS. 947, RBL 21. / R&R SUPPORT PER SRM & DWG.

Part: SHIELD — CORRODED (BS 857) · airframe 69,206 hrs · 40,952 cycles

AFT SHIELD AT AFT CARGO BAY CORRODED AT BS. 857, RBL 21. / R&R SHIELD IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 69,206 hrs · 40,952 cycles

SEAT TRACK CORRODED BETWEEN BS. 540 TO BS. 727B, RBL 25. / R&R SEAT TRACK PER SRM AND DWG.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 69,206 hrs · 40,952 cycles

FAIRING PANEL 194GR HAS CRACKS AROUND FASTER HOLES TOP MIDDLE SIDE ON INTERNAL SURFACE / REPAIRED FASTENER HOLE TOP SIDE MIDDLE ON INTERNAL SURFACE ON FAIRING PANEL 194GR IAW SRM 51-70-05-2R-6 7062U 4-18-19

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 69,206 hrs · 40,952 cycles

***CORROSION*** ON FLOOR SPLICE SUPPORT AT AFT CARGO BAY BS887 RBL20 TO LBL9 WL168. MARKED / DAMAGE EVALUATION ON ACB FLOOR SPLICE BS887; RBL20-LBL9; WL168; WAS FOUND TO BE OUT OF LIMITS. DUE TO NO DAMAGE LIMITS GIVEN IN SRM. REMOVED AND INSTALLED NEW FLOOR SPLICE. PER DWG 146A7500; DWG 149A8104; AND SRM 51-40-02 87713U 18APR19

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,206 hrs · 40,952 cycles

***CORROSION*** ON BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS847 LBL20 WL162. MARKED / CORROSION ON BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS 847 LBL 20 WL162 WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN SRM. REPLACED BULKHEAD TO FLOOR ANGLE FOR A NEW BULKHEAD TO FLOOR ANGLE. LOCATED AND DRILLED; INSTALLED BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS847 LBL20 WL162 PER SRM 51-40-02M SRM 51-40-05; AND DWG 149A8102 593046U 15APR19

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,206 hrs · 40,952 cycles

RT HORIZONTAL STABILIZER RIB AT STAB. STA. 120.30 3RD VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM & MM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 69,206 hrs · 40,952 cycles

RT HORIZ. STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED & REPLACED RT HORIZ STAB UPPER FWD SLIDE SEAL IAW AMM 53-31-31-000-802 & AMM 53-31-31-400-802 56304U 24APR19

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 69,206 hrs · 40,952 cycles

LT HORIZ. STAB LWR FWD SLIDE SEAL IS CRACKED. / REMOVED & REPLACED LT HORIZ STAB LWR FWD SLIDE SEAL IAW AMM 53-31-31-000-801 & AMM 53-31-31-400-801 56304U 23APR19

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,206 hrs · 40,952 cycles

R1 DOOR NR 4 LOWER BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. REPAIRED DOOR PER RO.

Part: RETAINER — CRACKED (LEFT WING) · airframe 69,206 hrs · 40,952 cycles

LT WING UPPER T/E PANEL JUST AFT OF #1 PYLON; HORIZ. SEAL RETAINER IS CRACKED. / REMOVED CRAKED SEAL RETAINER LT WING UPPER TE PANEL JUST AFT OF #2 PYLON IAW SRM 51-40-02-0G-0 89813U 04-07-19 LEAD 28 07APR19 REPLACED LT WING UPPER T/E PANEL JUST AFT OF #1 PYLON; HORIZ. SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25 89813U 04-08-19

Part: BRACKET — BROKEN (R1 DOOR GIRT BAR) · airframe 69,206 hrs · 40,952 cycles

R1 DOOR ESCAPE SLIDE SHROUD GIRT BAR BRACKET BROKEN. R&R BRACKET IAW SRM.

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 69,206 hrs · 40,952 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN LBL 25 TO LBL 60. REPAIRED WEB PER SRM.

Part: PRESSURE DECK — CRACKED (BS 665) · airframe 69,206 hrs · 40,952 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS. 665, RBL 40. / REPAIRED WEB IAW SRM.

Part: COVER — CRACKED (LEFT WING) · airframe 69,206 hrs · 40,952 cycles

#3 CANOE FAIRING IB BOLT COVER (542CR) IS CRACKED / REPLACED #3 CANUE FAIRING I/B BOLT COVER (542CR) IAW GERNAL INDUSTRIES PROCEDURES. WILL BE INSTALL ON JPANEL INSTALLATION CUSTOMER CARD NUMBER JPANEL 540 CLOSE. 56260U 12APR19

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 69,206 hrs · 40,952 cycles

NR 4 RT STOW BIN EMERGENCY LIGHT INOP. R&R M1669 POWER SUPPLY FUSE IAW AMM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 69,206 hrs · 40,952 cycles

RT LOWER VAPOR BARRIER CRACKED AT BS. 663, BETWEEN RBL 15 TO RBL 5. R&R BARRIER PER SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 68,950 hrs · 40,798 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 68,949 hrs · 40,798 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: NONE — CORRODED (LH NACELLE) · airframe 68,733 hrs · 40,651 cycles

#1 ENG I/B FAN COWL HAS CORROSION 1.5' LONG AT 3 O'CLOCK 5' FROM AFT EDGE WITH PIN HOLES / REF LP 0870150 FOR RESOLUTION

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 68,144 hrs · 40,283 cycles

FORWARD GALLEY FLASHLIGHT STRAP BROKEN. R&R STRAP PER SIP & AMM.

Part: PROXIMITY SENSOR — FAULTY (KRUEGER FLAP) · airframe 67,650 hrs · 39,958 cycles

AIR TURNBACK, NR 1 KRUEGER FLAP SHOWED FULL EXTEND ON CLIMB OUT SLIGHT LEFT ROLL WAS NOTICED WITH AUTOPILOT OFF. R&R K-FLAP NR 1 EXTEND PROXIMITY SENSOR PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,565 hrs · 39,899 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,565 hrs · 39,899 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 67,361 hrs · 39,776 cycles

L2 DOOR SLIDE GIRT OUT OF ADJUST. ADJUSTED GIRT PER MT.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,361 hrs · 39,776 cycles

L1 DOOR SLIDE GIRT OUT OF ADJUST. ADJUSTED GIRT PER MT.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 66,892 hrs · 39,478 cycles

L1 DOOR SLIDE PARTIALLY DISLODGED FROM COVER. REINSTALLED SLIDE PER MM AND MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 66,462 hrs · 39,216 cycles

L1 DOOR EMERGENCY ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,870 hrs · 38,847 cycles

L1 DOOR SLIDE FLAP LOOSE. SECURED THE SLIDE IAW SIP.

Part: HOOK AND LOOP — LOOSE (COVER) · airframe 64,626 hrs · 38,035 cycles

RIGHT EMERGENCY EXIT DOOR OVERWING LOWER HANDLE COVER HOOK AND LOOP LOOSE. R & R THE HOOK AND LOOP STRIP IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,335 hrs · 37,825 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 63,836 hrs · 37,500 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER SIP.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 62,724 hrs · 36,820 cycles

MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED THE EXIT SIGN IAW MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 62,526 hrs · 36,699 cycles

LEFT EMERGENCY LIGHT LENS LOOSE AT ROW 14. INSTALLED THE LENS IAW AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,526 hrs · 36,699 cycles

EMERGENCY LIGHT INOPERATIVE AT LOCATION M1673. R&R BATTERY CHARGER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,526 hrs · 36,699 cycles

R1 DOOR EMERGENCY EXIT AISLE LIGHT INOP BETWEEN ROW 11 TO ROW 13. REPAIRED LIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (BS 946) · airframe 62,526 hrs · 36,699 cycles

INTERCOSTAL CRACKED AT BS 946, RBL 20. R & R THE INTERCOSTAL IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 62,526 hrs · 36,699 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,526 hrs · 36,699 cycles

L1 DOOR THRESHOLD WEB ANGLE CORRODED. R&R ANGLE PER SRM.

Part: SUPPORT — CORRODED (BS 767) · airframe 62,526 hrs · 36,699 cycles

FUSELAGE FRAME SUPPORT CORRODED AT BS 767, RBL 25. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,526 hrs · 36,699 cycles

AFT CARGO BAY AFT BULKHEAD RT PANEL LOWER SUPPORT CORRODED. R&R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727-767) · airframe 62,526 hrs · 36,699 cycles

FLOOR SUPPORT CORRODED AT BS 727 TO 767, RBL 25. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: STIFFENER — BROKEN (BS 663) · airframe 62,526 hrs · 36,699 cycles

HORIZONTAL SUPPORT STIFFENER BROKEN AT BS 663, RBL 12. R&R THE SUPPORT STIFFENER IAW SRM.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 62,526 hrs · 36,699 cycles

AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED. R & R THE SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 500-500D) · airframe 62,526 hrs · 36,699 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO 500D, RBL 25. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (BS 294-344) · airframe 62,526 hrs · 36,699 cycles

R1 DOOR THRESHOLD WEB CORRODED AT BS 294 TO 344. REPAIRED THE WEB IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,526 hrs · 36,699 cycles

AFT CARGO BAY DOOR SURROUND THRESHOLD SUB WEB CORRODED. R&R WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 62,526 hrs · 36,699 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, RBL 30. R & R THE INTERCOSTAL IAW SRM.

Part: BULKHEAD — CRACKED (BS 663) · airframe 62,526 hrs · 36,699 cycles

RIGHT WHEEL WELL FORWARD BULKHEAD CRACKED AT BS 663, RBL 12. REPAIRED THE BULKHEAD IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 62,526 hrs · 36,699 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO 344, LBL 47. R & R INTERCOSTAL IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 62,526 hrs · 36,699 cycles

FUSELAGE BULKHEAD PLATE CORRODED AT STA 767 TO STA 787, LBL 25. REPAIRED PLATE PER SRM.

Part: STRAP — CORRODED (BS 733-860) · airframe 62,526 hrs · 36,699 cycles

AFT CARGO BAY FLOOR SUPPORT STRAP CORRODED BETWEEN BS 773 TO 860, RBL 20. R & R THE STRAP IAW SRM.

Part: SUPPORT — CORRODED (BS 494-500A) · airframe 62,526 hrs · 36,699 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO 500A, RBL 25. R&R SUPPORT IAW SRM & DWG.

Part: WEB — CORRODED (THRESHOLD) · airframe 62,526 hrs · 36,699 cycles

L1 DOOR THRESHOLD WEB CORRODED AT BS 310 TO 344. R & R THE WEB IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,526 hrs · 36,699 cycles

AFT CARGO BAY DOOR SURROUND AFT SHIELD CORRODED. R&R SHIELD IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 500-500D) · airframe 62,526 hrs · 36,699 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO 500D, LBL 25. R & R THE SIDEWALL SUPPORT IAW SRM & DWG.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 62,526 hrs · 36,699 cycles

AFT CARGO BAY DOOR SURROUND FORWARD SHIELD CORRODED. R & R THE SHIELD IAW SRM AND DWG.

Part: WEB — CORRODED (THRESHOLD) · airframe 62,526 hrs · 36,699 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R & R THE WEB IAW SRM.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 62,526 hrs · 36,699 cycles

R1 DOOR THRESHOLD WEB ANGLE CORRODED. REPAIRED THE WEB ANGLE IAW SRM.

Part: WEB — CORRODED (BS 986-1016) · airframe 62,526 hrs · 36,699 cycles

FLOOR WEB CORRODED AT BS 986 TO 1016, LBL 40.55, WL 208. REPAIRED THE WEB IAW SRM.

Part: SUPPORT — CORRODED (BULKHEAD) · airframe 62,526 hrs · 36,699 cycles

FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED BETWEEN LBL 25 TO RBL 25. R & R THE BULKHEAD SUPPORT SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 772) · airframe 62,526 hrs · 36,699 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772. R&R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 62,526 hrs · 36,699 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, LBL 47. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 787-860) · airframe 62,526 hrs · 36,699 cycles

FLOOR SUPPORT CORRODED AT BS 787 TO 860, RBL 14. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 420-440) · airframe 62,526 hrs · 36,699 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO 440, RBL 25. R&R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 344-294) · airframe 62,526 hrs · 36,699 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO 294, BL 0. R & R INTERCOSTAL IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 62,526 hrs · 36,699 cycles

LT CLOSE OUT PANEL 231YJW ABOVE THE OVERWING EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED WIRE PER WDM AND SWPM.

Part: WEB — CORRODED (THRESHOLD) · airframe 62,526 hrs · 36,699 cycles

R2 DOOR THRESHOLD WEB CORRODED AT BS 986. REPAIRED THE WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,526 hrs · 36,699 cycles

FLOORBEAM CORRODED AT BS 986, RBL 50 TO LBL 5. REPAIRED FLOORBEAM IAW ER AND EA.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 62,526 hrs · 36,699 cycles

NR 1 L/E SLAT LOWER SKIN CRACKED NEAR ACTUATOR RIB ATTACH FASTENER. REPAIRED THE SKIN IAW SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,526 hrs · 36,699 cycles

EMERGENCY LIGHT LENS MISSING AT ROW 5 DEF. INSTALLED THE LENS IAW MM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 62,503 hrs · 36,685 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,100 hrs · 35,847 cycles

LEFT WING NR 3 SLAT SKIN CRACKED AT T/E. R & R SKIN IAW SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 61,100 hrs · 35,847 cycles

LEFT WING NR 2 SLAT SKIN CRACKED. REPAIRED SLAT SKIN IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 57,838 hrs · 33,922 cycles

LEFT OVERHEAD BIN, EMER LIGHT LENS MISSING AT ROW 17. INSTALLED LENS IAW SIP.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 57,300 hrs · 33,608 cycles

RIGHT EMERGENCY EXIT LIGHT FAULTY BETWEEN ROW 11 TO 14. R & R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,214 hrs · 33,554 cycles

EXTERNAL EMER EXIT LIGHT ASSEMBLY INOPERATIVE AFT OF AFT CARGO DOOR. RELAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,214 hrs · 33,554 cycles

EXTERNAL EMER EXIT LIGHT ASSEMBLY INOPERATIVE AT RT OVERWING DOOR. RELAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,214 hrs · 33,554 cycles

RIGHT OVERHEAD EMER EXIT LIGHT INOPERATIVE AT ROW 13. R & R LAMP IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 663 TO 685. REPAIRED WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

LEFT CREASE WEB CORRODED BETWEEN BS 500B TO 500C. R & R CREASE WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

LEFT BULKHEAD FRAME WEB CRACKED AT BS 727, WL 201. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

LEFT FRAME WEB CRACKED AT WL 200. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 727A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 559, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FUSELAGE FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

LEFT NR 1 COCKPIT WINDOW FRAME CRACKED, AT 5TH & 7TH HOLE UP FROM BOTTOM OTBD SIDE OF FRAME. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,214 hrs · 33,554 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,177 hrs · 33,535 cycles

LEFT WING OTBD TE AFT FLAP INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.

Part: BEAM — CRACKED (LT WING) · airframe 57,177 hrs · 33,535 cycles

LEFT WING UPPER FIXED TE WING PANEL BEAM CRACKED. REPAIRED BEAM IAW EA & DWG.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 57,177 hrs · 33,535 cycles

RIGHT PHOTO LUMINESCENT STRIP CRACKED AT ROW 1. R & R STRIP IAW MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 57,141 hrs · 33,513 cycles

R2 DOOR SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 56,717 hrs · 33,254 cycles

LEFT EMER EXIT SIGN BULLNOSE LENS LOOSE AT ROW 9. SECURED LENS IAW AMM.

Part: LINE — LEAKING (MLG WW) · airframe 56,144 hrs · 32,937 cycles

DIVERSION, HYD B SYS LOSS. FOUND HYD POWER TRANSFER UNIT LINE LEAKING. R & R LINE IAW MM.

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 56,112 hrs · 32,918 cycles

L1 DOOR EMER EXIT SLIDE PULL HANDLE COVER OUT OF POSITION. REPOSITIONED COVER IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 52,725 hrs · 30,942 cycles

RT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED LONG TEST. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 52,725 hrs · 30,942 cycles

LT EMERGENCY LIGHT BATTERY PACK FAILED LONG TEST AT ROW 17. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 52,725 hrs · 30,942 cycles

AFT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED LONG TEST. R & R BATTERY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,582 hrs · 29,641 cycles

RT OVERWING EXIT IDENTIFIER INOPERATIVE. R&R BATTERY PACK IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 50,582 hrs · 29,641 cycles

LT NR 3 WINDOW E-F POST 3RD FROM BOTTOM FASTENER CRACKED. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,582 hrs · 29,641 cycles

LT NR 3 WINDOW E-F POST 2ND FROM BOTTOM FASTENER CRACKED. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 50,582 hrs · 29,641 cycles

LT WINDOW C-D POST CRACKED IN UPPER RADIUS. REPAIRED POST IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 50,582 hrs · 29,641 cycles

VERTICAL ANGLE FRAME ATTACH FITTING CRACKED AT STATION 947, LBL 8.0.. R&R FITTING IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 50,582 hrs · 29,641 cycles

LT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 1. SECURED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,160 hrs · 29,391 cycles

FORWARD ENTRY FLOOR EEPLS INOP. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,459 hrs · 28,978 cycles

EGRESS BULL NOSE LIGHTS INOP BETWEEN AT ROWS 13 AND 22. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 49,279 hrs · 28,859 cycles

FLT ATT REPORTS RT OVERWING EXIT SIGN HANGING LOW ABOVE DOOR. RE-ATTACHED HARDWARE AND RESECURED PER M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,122 hrs · 28,750 cycles

EMERGENCY EXIT LIGHT OUTSIDE AND AFT OF AFT SERVICE DOOR INOP. REMOVED AND REPLACED BULB IN EMERGENCY EXIT LIGHT OUTSIDE OF AND AFT OF AFT SERVICE DOOR AND LIGHT CHECKED GOOD PER MM

Part: LENS — BROKEN (CABIN) · airframe 48,490 hrs · 28,361 cycles

LENS COVER FOR EXIT LIGHT AT FORWARD SERVICE DOOR BROKEN. REPLACED BASE LENS ASSY PER AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 48,369 hrs · 28,277 cycles

RIGHT WHEEL WELL BULKHEAD CRACKED AT BS 663, RBL 37. REPAIRED BULKHEAD PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 48,358 hrs · 28,270 cycles

RIGHT WING OUTBOARD AFT FLAP UPPER INBOARD CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER M/M.

Part: FLAP — DELAMINATED (RT WING) · airframe 48,358 hrs · 28,270 cycles

RIGHT WING OUTBOARD AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: SIGN — LOOSE (CABIN) · airframe 47,473 hrs · 27,681 cycles

R2 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 45,939 hrs · 26,769 cycles

LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 45,939 hrs · 26,769 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 44,836 hrs · 26,101 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,846 hrs · 26,106 cycles

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

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 44,690 hrs · 26,024 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — BROKEN (CABIN) · airframe 44,595 hrs · 25,962 cycles

R2 DOOR EMERGNECY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, BETWEEN RBL 37 TO RBL 47. REMOVED AND REPLACED T-CAP IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 19. REMOVED AND REPLACED BULB PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT LT Z ANGLE CORRODED AT BS 727A. REMOVED AND REPLACED Z ANGLE IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM AND MT.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN 500 TO 500D. REMOVED AND REPLACED Z ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN BS 807 TO BS 847. REPAIRED Z ANGLE IAW SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE IAW MM AND MT.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CUTOUT, CREASE BEAM STRAP CORRODED. REMOVED AND REPLACED STRAP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CHORD CORRODED BETWEEN BS 294 TO BS 328. REPAIRED CHORD PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CREASE BEAM ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME ANGLE CRACKED AT BS 867, STR 8L. REPAIRED ANGLE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,905 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 439,005 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 439,005 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 439,005 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 439,005 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 439,005 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME IAW EA.

Part: FITTING — LOOSE (GIRT BAR) · airframe 439,005 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINING CLIP LOOSE. REMOVED AND REPLACED CLIP IAW SRM AND MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 439,005 hrs · 25,564 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 43,801 hrs · 25,508 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 41,066 hrs · 23,896 cycles

R2 DOOR OVERHEAD EMERGENCY EXIT SIGN LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,709 hrs · 23,693 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: WEB — CRACKED (LT MLG WW) · airframe 37,189 hrs · 21,557 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT MLG VERTICAL WEB CRACKED AT BS 663.75, LBL 36. REPAIRED WEB PER SWA EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 36,017 hrs · 20,849 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: FITTING — CORRODED (RT WING) · airframe 35,502 hrs · 20,544 cycles

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

Part: FITTING — CORRODED (LT WING) · airframe 35,502 hrs · 20,544 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 34,901 hrs · 20,169 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 8 SLAT OUTER SKIN CRACKED AT FASTENER HOLE. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,358 hrs · 18,612 cycles

DURING SCHEDULED HC1 CHECK, RIGHT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,177 hrs · 17,331 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 17 TO RBL 13. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,177 hrs · 17,331 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D, LBL 17 TO RBL 13. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,177 hrs · 17,331 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 29 AND LBL 41. REPAIRED FLOORBEAM PER SRM.

Part: ENGINE — VIBRATION (RIGHT) · airframe 28,190 hrs · 16,143 cycles

FELT STRONG VIBRATION CLIMBING THROUGH FL 235 AND FL 270 FOR 5 SECONDS EACH, THEN AT CRUISE FL 380. VIBRATION 2 TO 3 MINUTES. DURING FERRY FLIGHT TO DAL, CONFIRMED VIBRATION COMING FROM NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 28,183 hrs · 16,136 cycles

AIRCRAFT HAD TWO INCIDENTS OF HIGH FREQUENCY LATERAL OSCILLATIONS AT FL 390. TURNED YAW DAMPNER OFF NO EFFECT, RUDDER TRIM 1-2 UINTS EITHER SIDE, SLIGHT DAMPENING EFFECT. REMOVED AND REPLACED NR 2 ENGINE HMU, FUEL PUMP AND RUDDER PCU PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 27,669 hrs · 15,872 cycles

DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 27,071 hrs · 15,540 cycles

EEPLS COVER LOOSE AT ROW 8 ABC. SECURED EEPLS COVER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,857 hrs · 14,871 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY LIGHT INOP AT BS 727A. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,857 hrs · 14,871 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY LIGHT INOP AT BS 727D. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 25,345 hrs · 14,568 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,503 hrs · 14,096 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,333 hrs · 13,464 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ENGINE — SHUTDOWN (RIGHT) · airframe 22,921 hrs · 13,240 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY. NR 2 ENGINE SHUTDOWN DUE TO SUSPECTED FUEL LEAK. NR 1 FUEL TANK DECREASED FUEL QUANTITY BY 700 NR IN 20 MINUTES. CHECKED FOR FUEL LEAKS, NONE FOUND. PERFORMED BITE CHECK, NO FAULTS RECORDED.

Part: BELLCRANK — CRACKED (LT WING) · airframe 22,917 hrs · 13,238 cycles

DURING SCHEDULED MV2 CHECK, FOUND OUTBOARD AFT FLAP ACTUATING MECHANISM BELLCRANK CASTING CRACKED AT INBOARD SIDE OF LT WING. REMOVED AND REPLACED AFT FLAP ACTUATING MECHANISM BELLCRANK CASTING PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,409 hrs · 12,947 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD & AFT GALLEY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,679 hrs · 12,549 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 21,538 hrs · 12,474 cycles

DURING SCHEDULED MV2, FOUND R2 DOOR EVACUATION SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,563 hrs · 11,933 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: COWLING — DEPARTED (NR 1 ENGINE) · airframe 18,523 hrs · 10,776 cycles

ON TOUCHDOWN AND REVERSER DEPLOYMENT LOST BOTH SIDES OF NR 1 ENGINE COWLING, WITH DAMAGE TO LT FUSELAGE, LT UPPER WING AND LT HORIZONTAL STAB L/E. ACCOMPLISHED CONDITIONAL INSP OF FUSELAGE, HORIZONTAL STAB, AND PYLON. INSP DUE TO FAN COWLING DEPARTING FROM AIRCRAFT PER EA.

Part: LIGHT — LOOSE (ROW 1) · airframe 16,863 hrs · 9,842 cycles

EEPLS FLOOR TRACK LIGHTING LOOSE AT ROW 1. SECURED TRACK PER MM.

Part: BUSHING — WORN (LT/RT ELEVS) · airframe 13,042 hrs · 7,727 cycles

DURING SCHEDULED C4 CHECK, BOTH LT/RT ELEVATOR TABS FAILED FREEPLAY CHECKS. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TAB NR 1 HINGE BUSHINGS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 10,635 hrs · 6,331 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 11. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,445 hrs · 6,521 cycles

EEPLS IN FWD CABIN INOP AND MISSING COVER. INSTALLED COVER AND REPAIRED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 7,486 hrs · 4,506 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER. REINSTALLED EVAC SLIDE PER MM.

Part: RETAINER — LOOSE (FWD ENTRY DOOR) · airframe 7,144 hrs · 4,294 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. R&R RIVET PER MM.

Part: LENS — BROKEN (CABIN) · airframe 7,020 hrs · 4,219 cycles

EEPLS LIGHT LENS BROKEN AT FWD CABIN. Removed and replaced EEPLS LENS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 6,579 hrs · 3,968 cycles

DURING SERVICE CHECK (SWA SI 11038-55), FOUND EXCESSIVE PLAY AT RT ELEVATOR TAB ATTACH BOLTS AT NR2, NR3 & NR4 HINGES. R&R ELEVATOR TAB PER MM.

Part: SWITCH — CONTAMINATED (AFT CARGO DOOR) · airframe 4,227 hrs · 2,556 cycles

AIR TURNBACK, AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. REMOVED DEBRIS FROM AFT CARGO DOOR SWITCH. OPS CK GOOD PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 3,242 hrs · 1,982 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 2,665 hrs · 1,637 cycles

AIR TURNBACK, AFT CARGO DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROTATION. REPOSITIONED AFT CARGO DOOR BUNGEE CHORD PER MM.