N7842A

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 64,777 hrs · 40,734 cycles

WHILE PROBO WAS OPENING THE FWD SERVICE DOOR SLIDE FELL OFF THE CASE<[01] REPOSITION FS SLIDE IN COMPARTMENT PER MT 725-61-06.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 61,924 hrs · 38,896 cycles

R2 SLIDE CAME OUT OF HOLDER. REINSTALLED SLIDE IAW AMM 25-66-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,619 hrs · 38,683 cycles

L/H EMERGENCY EXIT ROW WINDOW LIGHT INOP / [01] RELAMPED L/H EMERGENCY EXIT WINDOW LIGHT PER AMM 33-21-00 OPS CHECK GOOD

Part: LENS — MISSING (FWD CABIN) · airframe 60,788 hrs · 38,116 cycles

FWD ENTRY FLOOR LEVEL EMERGENCY EXIT COVER MISSING / [01] INSTALLED FWD ENTRY EMERGENCY EXIT LENS PER AMM 33-51-11 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 60,682 hrs · 38,045 cycles

PAX CABIN SIDEWALL LIGHTS INOP #1 - SEAT 5 F;E;D #2 -SEAT 12 F;ED (F/O SIDE OVER PAX CABIN SIDEWALL LIGHTS INOP #1 - SEAT 5 FED #2 -SEAT 12 FED (F/O SIDE OVERWING EXIT DOOR) #3 SEAT 23 ABC.<[01] REPLAMPED SEAT 5 FED AND 12 FED SIDEWALL LIGHTS PER AMM 33-21-00.;[02] REPLAMPED SEAT 5 FED AND 23 FED SIDEWALL LIGHTS PER AMM 33-21-00;[03] RELAMPED R/H OVERWING EXIT SIDEWALL LIGHT IAW B737 AMM 33-21-00. PLACARDS REMOVED. OPS CHECK GOOD.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 60,252 hrs · 37,744 cycles

SUPPLEMENTAL INFORMATION: LEFT OVERHEAD EMERGENCY LIGHT INOP (OVERWING) DOOR / [01] RELAMPED SIDEWALL LIGHT; NO HELP. OK TO CONTINUE PER MEL 33-20-03 SP1B. AUTH #62350;[02] REMOVED AND REPLACED L/H OVERWING DOOR EXIT BALLAST IAW AMM 33-21-00. OPS CHECK GOOD.;[03] REFERENCE LOGPAGE# 2027732 FOR WORK PERFORMED

Part: FITTING — LOOSE (L2 DOOR) · airframe 59,706 hrs · 37,397 cycles

L-2 DOOR AFT GIRT BAR FITTING IS LOOSE. / [01] SECURED L-2 DOOR AFT GIRT BAR FITTING AS PER B737 AMM 25-66-02-400-801;[02] VERIFIED GIRT BAR SECURED.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 59,706 hrs · 37,397 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. / [01] RELAMPED L1 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 59,706 hrs · 37,397 cycles

EMERGENCY LIGHT AT LEFT HAND OVERWING EXIT DOOR INOP. / [01] REPLACED BATTERY PACK POSITION M1668 AT LEFT HAND OVERWING EMERGENCY EXIT DOOR AND PERFORMED INSTALLATION TEST AS PER B737 AMM TASK 33-51-06-960-805. TEST OK.;[02] VERIFIED

Part: PANEL — DELAMINATED (L/H WING) · airframe 59,706 hrs · 37,397 cycles

ACCESS PANEL 543AB DELAMINATED AT AFT LOWER SKIN. MKD 126 / [01] PREPARED AREA FOR REPAIR DELAMINATED LOWER SKIN AT ACCESS PANEL#543 AB AS PER B737-700 SRM 51-70-04-2R-2;[02] VERIFIED STEP #1.;[03] REPAIRED DELAMINATED AREA AT ACCESS PANEL#543 AB ASPER B737-700 SRM 51-70-04-2R-2 MATERIAL USED PO#1753536 AND PO#1150387;[04] VERIFIED STEP #3.;[05] APPLIED TOPCOAT TO PANEL 543AB ASPER B737 AMM 51-21-73-370-803 <BR> ACCOMPLISHED BY MECH W.V.-2504;[06] VERIFIED 5

Part: NONE — CRACKED (R/H WING) · airframe 59,706 hrs · 37,397 cycles

FOUND CRACK ON RT WING O/B AFT FLAP LOWER SURFACE AT 43' FROM O/B EDGE AND 7.5' FROM T/E. PERFORMED VISUAL INSPECTION AND TAP TEST NO DELAMINATION AROUND THE CRACK SIZE 1/2'' IAW NTM 51-05-01 & TOP DRILLED END OF CRACK IAW SRM 51-10-02-0G-0 PARAGRAPH 12.A. APPLIED DRY PROCESS IAW SRM 51-70-10-2R-0 PARAGRAPH(7.A.3). FABRICATED FILLER & DOUBLE & APPLIED BOEGEL AC-130, ADH PRIMER, ADH FILM, & ALUMINUM IAW SRM 51-70-10-2R-0. REPAIRED DAMAGED AREA IAW SRM 51-70-10-2R-0 AND PERFORMED TAP TEST AROUND THE REPAIR NO DELAMINATION FOND PER B737 NTM 51-05-01. PAINTED REPAIR AREA IAW AMM 51-21-99-300-802.

Part: FRAME — CRACKED (L/H OVERWING DOO) · airframe 59,706 hrs · 37,397 cycles

L/H OVERWING EMERGENCY EXIT DOOR LINER VERTICAL FRAME CRACKED FWD LOWER 2ND FROM BLTTOM. / [01] REMOVED DAMAGE AT L/H OVERWING EMERGENCY EXIT DOOR LINER VERTICAL FRAME FWD LOWER 2ND FROM BLTTOM AS PER SRM 51-10-02-0G-0 AND 51-70-13-2R-1 REPAIR 1.;[02] EVALUATED SURFACE ROUGHNESS FOUND SMOOTHER THAN 63 MICROINCHES RA ON REWORKED AREA AS PER SRM 51-70-13-2R-1 REPAIR 1 USED TOOL B/C 171854.;[03] VERIFIED STEP 1; 2;[04] PERFORMED HFEC AT CUT OUT IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS<BR>[NORTEC 600;B/C 166316; CALIB.DUE-10/22];[05] FABRICATED REPAIR PARTS (DOUBLER AND SHIM) AS PER SRM 51-70-13-2R-1 REPAIR 1 AND 51-40-05-0G-0.;[06] VERIFIED STEP 5;<BR>OK TO TREAT AND PRIME FABRICATED PARTS;[07] TREATED AND PRIMED REPAIR PARTS AS PER SRM 51-20-01-0G-0.;[08] VERIFIED STEP 7.<BR>OK TO INSTALL PARTS;[09] INSTALLED REPAIR PARTS AT LEFT OVER WING EMERGENCY EXIT DOOR LINER VERTICAL FRAME FORWARD LOWER SECOND FROM BOTTOM (P/N 411A2730-5) AS PER SRM 51-70-13-2R-1 REPAIR 1 AND 51-40-02-0G-0.;[10] VERIFIED

Part: ANGLE — CORRODED (AFT CARGO) · airframe 59,706 hrs · 37,397 cycles

MULTIPLE SPOTS OF CORROSION FOUND ON LEFT AFT CARGO 'Z' CHANNEL TOP SURFACE AT FASTENER HOLES FROM BS 847 TO BS 727B +4. MULTIPLE SPOTS OF CORROSION FOUND ON LEFT AFT CARGO '' CHANNEL TOP SURFACE AT FASTENER HOLES FROM BS 847 TO BS 727B +4. / [01] REMOVED CORROSION AT L/H ZEE CHANNEL FROM 727B+4 TO 847 AS PER B737-700 SRM 51-10-02-0G-0;[11] SUMMARY=REMOVED CORROSION AT L/H ZEE CHANNEL FROM 727B+4 TO 847 AS PER B737-700 SRM 51-10-02-0G-0 EVALUATED REWORKED AREA ORG. MAT. 0.040 MAT. REMOVED 0.020 MAT REMAINING 0.020 FOUND TO BE OUT OF LIMITS IAW B 737-7 SRM 53-00-53-1A-2 LOCATED AND DRILLED NEW L/H Z-CHANNEL IAW B 737-7 SRM 51-40-05-0G-0 TREATED AND PRIMED NEW L/H ZEE CHANNEL AS PER B 737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 INSTALLED NUT PLATES ON NEW Z-CHANNEL IAW B 737-7 SRM 51-40-02-0G-0 INSTALLED NUT PLATES ON NEW Z-CHANNEL IAW B 737-7 SRM 51-40-02-0G-0;[12] VERIFIED SUMMARY ON STEP 11.

Part: PANEL — ELONGATED (L/H WING) · airframe 59,706 hrs · 37,397 cycles

LH WING PANEL 521ZB HAS TWO HOLE SCREWS ELONGED. / [01] PREPARED PANEL #521ZB FOR REPAIR AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED PREPARED AREA;[03] REPAIRED PANEL #521ZB AS PER B737 SRM 51-70-2R-6 AND SRM 51-70-06-2R-0. MATERIALS USED RESIN P/O#1753536 FABRIC P/O#1486409;[04] PAINTED PANEL #521ZB AS PER B737 AMM 51-21-99-300-801. MATERIALS USED GRAY PAINT P/O#1750464;[05] VERIFIED REPAIR

Part: BARRIER — PEELING (CENTER WING BOX) · airframe 59,706 hrs · 37,397 cycles

AREA ABOVE WING CENTER SECTION BETWEEN BS 580 TO BS 560 RBL-60 TO RBL-65 FUEL VAPOR BARRIER COATING PEELING OFF / [01] OPENED FLOOR PANEL 232 SF AS PER B-737-700 SRM 51-40-02-0G-0;[02] AREA CLEANED AND FUEL BARRIER SEALANT APPLIED ON AREA ABOVE WING CENTER SECTION BETWEEN BS 560-BS 580 AS PER B-737-700 AMM 28-11-00-300-804.;[03] VERIFIED STEP 1 AND 2.;[04] PERFORMED NDT THICKNESS CHECK ON APPLIED VAPOR BARRIER SEALANT IAW AMM 28-11-00-300-804. THICKNESS FOUND WITHIN ACCEPTABLE RANGE (NOT LESS THAN 0.007' OR MORE THAN 0.022') THICKNESS FOUND - 0.012'.;[05] APPLIED VAPOR SEAL AT WING CENTER SECTION BETWEEN BS 580 RLB 60 TO RBL 65 ON AREA ABOVE WING CENTER SECTION BETWEEN BS 560-BS 580 AS PER B-737-700 AMM 28-11-00-300-804.;[06] VERIFIED STEP 5.<BR>OK TO CLOSE FLOOR PANEL 232SF;[07] INSTALLED FLOOR PANEL 232SF IN REFERENCE B737 SRM 51-40-02-0G-0;[08] VERIFIED.

Part: PANEL — CRACKED (FUSELAGE) · airframe 59,706 hrs · 37,397 cycles

PANEL 193D AFT EDGE HOLES HAVE CRACKS DUE TO THE INCORRECT COUNTERSINK / [01] PREPARED FOR REPAIR AT PANEL 193D AS PER B737-700 SRM 51-70-04-2R-9;[02] VERIFIED STEP 1...O.K. TO INSTALL REPAIR..;[03] REPAIRED AT PANEL 193 D AS PER B737-700 SRM.51-70-04-2R -9 MATERIAL USED PO.1753536; PO1150387 AND PO.1713932;[04] VERIFIED STEP 3..O.K.TO PAINT..;[05] RESTORED FINISH TO ACCESS PANEL #193D IAW B 737-7 AMM=51-21-73-370-803;[06] SUMMARY=PREPARED FOR REPAIR AT PANEL 193D AS PER B737-700 SRM 51-70-04-2R-REPAIRED AT PANEL 193 D AS PER B737-700 SRM.51-70-04-2R -9 MATERIAL USED PO.1753536; PO1150387 AND PO.1713932RESTORED FINISH TO ACCESS PANEL #193D IAW B 737-7 AMM=51-21-73-370-803;[07] CORRECTED DAMAGE REPORT.;[08] VERIFIED STEPS 5 AND 6..

Part: LENS — MISSING (CABIN) · airframe 57,233 hrs · 35,962 cycles

R2 DOOR EXIT SIGN MISSING. DIRECTIONAL ARROW. / REPLACED LENS'S REF AMM 33-51-01

Part: BATTERY — FAILED (CABIN) · airframe 55,153 hrs · 34,680 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1669 AND M 1675. / REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATIONS M1669 AND M 1675 PER AMM 33-51-06

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 55,153 hrs · 34,680 cycles

RH HORIZ. STAB UPPER FWD SLIDER IS CRACKED / REMOVED AND REPLACED RH HORIZ. STAB UPPER FWD SLIDER PER AMM 53-31-31

Part: RETAINER — CRACKED (LT WING TE) · airframe 55,153 hrs · 34,680 cycles

LEFT WING I/B UPPER FIXED TE PANEL FWD. SEAL RETAINER BRACKET CRACKED / REMOVED AND REPLACED LEFT WING I/B UPPER FIXED TE PANEL FWD. SEAL RETAINER BRACKET PER SRM 51-40-02.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,420 hrs · 34,226 cycles

EMERGENCY LIGHT BATTERY CHARGER M2335 WOULD NOT CHARGE EMERGENCY BATTERY. R&R BATTERY CHARGER M2335 PER AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO COMPARTMENT BULKHEAD PANEL SUPPORT CORRODED AT BS 947, BETWEEN RBL 18 TO LBL 9. R&R SUPPORT IAW SRM AND DWG.

Part: FRAME — SHORTED (BS 294 S2-4L) · airframe 54,420 hrs · 34,226 cycles

FRAME REPAIR AT BS 294 STR 2-4 L/H FOUND TO HAVE SHORT ED ON INBOARD SPLICE ANGLE; REQUIRES REPLACEMENT. / REMOVED AND REPLACED FRAME SEGMENT B.S. 294 STR1-13 LH PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 141A1120 REV- SHT 17;18

Part: FRAME — ELONGATED (BS 947) · airframe 54,420 hrs · 34,226 cycles

WHILE WORKING CUSTOMER CARD 724899; ELONGATED HOLE IN FRAME ON INBOARD FLANGE; BS 947; RBL 20; WL 166 / REMOVED DAMAGE ON FRAME INBOARD FLANGE BS 947; RBL 20 W/L 166. REPAIRED FRAME IAW ATS ER 20-01284 REV IR AND SWA EA 1-753-36488 REV IR

Part: BAFFLE — DAMAGED (BS 947) · airframe 34,226 hrs · 54,420 cycles

WHILE WORKING CUSTOMER CARD 724899; ELONGATED HOLE IN BAFFLE ON INBOARD FLANGE; BS 947; RBL 20; WL 166. / REMOVED DAMAGED BAFFLE BS 927-947 RBL 20 W/L 166. INSTALLED NEW BAFFLE IAW SRM 51-40-02-0G-0 AND DWG 147A7500 REV :

Part: SUPPORT — DAMAGED (BS 945-947) · airframe 54,420 hrs · 34,226 cycles

WHILE WORKING CUSTOMER CARD 724899; ELONGATED HOLES IN FLOOR TO SIDEWALL SUPPORT ON INBOARD FLANGE; BS 945-947; RBL 20; WL 166. / REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT BS 890-947 RBL 20 W/L 166 INSTALL FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 147A7500 REV:

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 54,420 hrs · 34,226 cycles

FWD CARGO BAY DOOR CUTOUT AFT SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO DOOR CUTOUT AFT SCUFF PLATE IAW SWA EA 1-A53-2076; REV. 11.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO BAY DOOR CUTOUT AFT SCUFF PLATE IS CRACKED / AFT CARGO BAY DOOR CUTOUT AFT SCUFF PLATE FOUND TO BE CRACKED. SCUFF PLATE REPAIRED PER EA #1-A53-2076; REV 11 (ATTACHED)

Part: ANGLE — BROKEN (APU PLENUM) · airframe 34,226 hrs · 54,420 cycles

APU AIR INLET PLENUM I/B PANEL UPPER ANGLE ASSY BROKEN / REMOVED AND REPLACED APU AIR INLET PLENUM I/B UPPER ANGLE ASSY PER SRM 51-40-02-0G-0 PARA 4. SEC B. STEPS (1)-(3) AND SEC E. AND IPC 49-15-00-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,420 hrs · 34,226 cycles

BULKHEAD SUPPORT CORRODED AT BS 947, RBL 17.5. REPAIRED SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 54,420 hrs · 34,226 cycles

FORWARD ENTRY DOOR OPENING INTERCOSTAL CRACKED BETWEEN BS. 328 TO BS. 344, LBL 45.50. / REPAIRED INTERCOSTAL PER SRM AND EA.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 54,420 hrs · 34,226 cycles

FORWARD ENTRY DOOR OPENING INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 40.5. / REPAIRED INTERCOSTAL PER SRM AND EA.

Part: STRAP — NOT REPORTED (FUSELAGE) · airframe 54,420 hrs · 34,226 cycles

(SKYLINE DTIP) FRAME FAILSAFE REPAIR, BS727B, BETWEEN STR20L-22L, STRAP REPAIR NO FURTHER EVALUATION IS NECESSARY PER EA 1-751-1124. (REFERENCE SRL N1010042993) STRAP REPAIR FROM .10 THICK ,7075-T6 CLAD SHEET ON THE AFT SIDE OF THE CHORD AND INSTALLED FREEZE PLUGS IN THE CHORD AND WEB. (SAM735/S.CHIRAYIL/12MAR20)

Part: WEB — CORRODED (BS 440-480) · airframe 54,420 hrs · 34,226 cycles

CORROSION AT MULTIPLE SPOTS ON THE SUB THRESHOLD WEB BS 440 - 480, RBL 28, WL 157. REMOVED AND REPLACED THE SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0, AND DWG 143A8330.

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 54,420 hrs · 34,226 cycles

***CORROSION*** AFT CARGO BAY DOORWAY THRESHOLD WEB BS 792 TO BS 847 IS CORRODED ON UPPER SURFACE. WL 156 RBL 26 / ACB DOORWAY THRESHOLD WEB; REPAIRED BY REPLACEMENT ON CUSTOMER CARD U107373

Part: BRACKET — CRACKED (ASD) · airframe 54,420 hrs · 34,226 cycles

LOWER PAN AFT BRACKET CRACKED AFT SERVICE DOOR / REMOVED LOWER PAN AFT BRACKET; AFT SERVICE DOOR AND REPLACED WITH NEW PER SRM 51-40-02.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 54,420 hrs · 34,226 cycles

R/H HORIZONTAL STAB WAS CRACKED ON THE INSPAR RIB ASSY NR 5, STAB STA 129.50, STIFFENER 3 FROM FORWARD SPAR. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-4, PARA 4, & FIG 202.

Part: FLOOR SUPPORT — CORRODED (BS 767-787) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO BAY FLOOR SUPPORT BS 767 TO BS 787, RBL 21, WL 156 WAS CORRODED AT SEVERAL AREAS. THE FLOOR SUPPORT WAS FOUND TO BE DAMAGED BEYOND ALLOWABLE LIMITS. DAMAGED FLOOR SUPPORT REMOVED AND REPLACED. ALL WORK WAS ACCOMPLISHED ON NRC DEFECT U107369.

Part: ATTACH FITTING — MISSING (BS 727B) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO BAY, BS 727B, RBL 8 FLOOR SUPPORT TO FRAME ATTACH FITTING WAS MISSING FOUR EACH. FASTENERS AND TWO EACH. FASTENER HOLES NOT DRILLED. LOCATED, DRILLED AND INSTALLED ACB FLOOR SUPPORT TO FRAME ATTACH FITTING IAW SRM 51-40-05, SRM 51-40-02, AND DWG 146A1201.

Part: FLOOR SUPPORT — CORRODED (BS 727-767) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO BAY FLOOR SUPPORT BS 727 TO BS 767, RBL 21 WAS CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 146A7500, REV C.

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO THRESHOLD AT BS 803; RBL 25; HAS SURFACE CORROSION AROUND FASTENER HOLE. (MARKED) WL 156 / ACB DOORWAY THRESHOLD WEB; REPAIRED BY REPLACEMENT ON CUSTOMER CARD U107373 57049U 30DEC19

Part: BRACKET — CORRODED (AFT CARGO COMPT) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO COMP. SIDE-PLATE; BS 767 RBL 25; WL 156 ANGLE-BRACKET HAS SURFACE CORROSION. (MARKED) / REMOVED DAMAGED BRACKET IN AFT CARGO COMP; ON SIDE- PLATE AT BS 767; RBL 25. INSTALLED NEW ANGLE BRACKET; ALL WORK ACCOMPLISHED IAW SRM 51-40-02-0G-0 AND DWG 146A0081 SH13; REV A. DAMAGE TO ANGLE BRACKET FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND PER SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0

Part: FRAME — CORRODED (AFT CARGO COMPT) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO COMP. BS 947 FRAME RBL3 AND 12 WL 157 HAS SURFACE CORROSION. (MARKED) / BS947 FRAME AT RBL3 AND RBL12 W.L157 REPAIRED IAW EA 1-753-36477 REV IR AND ATS ER 20-01042 REV IR

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO COMP. SIDE-PLATE; BS 857 RBL 25; HAS SURFACE CORROSION AROUND FASTER HOLE. (MARKED) / SIDE PLATE IN ACB B.S 857 RBL 25 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. PART TO BE REPAIRED BY REPLACEMENT IAW: SRM 51-10-02 ITEM 9. REMOVED SHIELD IAW: SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SHIELD P/N 146A8121-6 PO/N 7240741. IAW: SRM 51-40-05 AND DWG 146A0081 REV B. INSTALLED SIDE PLATE SHIELD AT B.S. 857 RBL 25-B.S 867 RBL 25 IAW: SRM 51-40-02-0G-0 AND DWG 146A0081 88765U 3JAN20

Part: SUPPORT — CORRODED (BS 767-773) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO DOOR FLOOR TO SIDEWALL SUPPORT AT BS 767 - 773 RBL 25, HAD SURFACE CORROSION AROUND FASTENER HOLES. REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT. INSTALLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 146A0081, SH 13, REV A. DAMAGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. NO DAMAGE LIMITS GIVEN, REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0.

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 54,420 hrs · 34,226 cycles

AFT CARGO THRESHOLD BS 820 - 828 RBL 25; HAS SURFACE CORROSION AROUND FASTENER HOLES. (MARKED) WL 156 / ACB DOORWAX THRESHOLD WEB; REPAIRED BY REPLACEMENT ON CUSTOMER CARD U107373

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 54,420 hrs · 34,226 cycles

RIGHT HORIZONTAL STAB REMOVABLE L/E RIB NR 4 WAS CRACKED. REMOVED & REPLACED THE RIGHT HORIZONTAL STAB REMOVABLE L/E RIB IAW SRM 51-40-02-0G-0 PARA 4, & FIG D, & DWG 186A1001.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,420 hrs · 34,226 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT UPPER SURFACE CORRODED BETWEEN BS, 420 TO BS. 440, RBL 24, FASTENER HOLES. / R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,420 hrs · 34,226 cycles

FORWARD CARGO BAY CORRODED FLOOR TO SIDEWALL SUPPORT UPPER SURFACE BETWEEN BS. BS 500A TO BS. 500D, RBL 24, AT FASTENER HOLES. / R&R SUPPORT IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,420 hrs · 34,226 cycles

RIGHT HORIZONTAL STAB REMOVABLE L/E RIB NR 3 WAS CRACKED. REMOVED & REPLACED THE RIGHT HORIZONTAL STAB REMOVABLE L/E RIB IAW SRM 51-40-02-0G-0 PARA 4, & FIG 8, & DWG 186A1001.

Part: SUPPORT — CORRODED (FWD CARGO COMPT) · airframe 54,420 hrs · 34,226 cycles

***CORROSION*** FWD CARGO BAY BS500D RBL-24 TO LBL-24 WL155 FLOOR TO BULKHEAD SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLES. REJECTION: WRONG FASTENERS USED TO INSTALL SUPPORT. DRAWING SPECIFIES BAC R15BA*D RIVET. THERE ARE SCREWS INSTALLED. / INSTALLED SUPPORT AT FCB BS 500D RBL-24 TO LBL 24 WL 155 IAW SRM 51-40-02 & DWG 143A7902 REV. E 59191U 06JAN20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,420 hrs · 34,226 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT UPPER SURFACE CORRODED BETWEEN BS. 492 TO BS. 500A, RBL 24, AT FASTENER HOLES. / R&R SUPPORT IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,420 hrs · 34,226 cycles

LEFT HORIZONTAL STAB REMOVABLE L/E RIB NR 4 WAS CRACKED. REMOVED & REPLACED LEFT HORIZ STAB REMOVABLE L/E RIB NR 4 IAW SRM 51-40-02-0G-0 PARA 4 & FIG 8, & DWG 186A1001.

Part: SCUFF PLATE — CORRODED (AFT CARGO THRESH) · airframe 53,931 hrs · 33,918 cycles

AFT CARGO DOOR THERSHOLD PLATE (AFT) HAS CORROSION / REPLACED AFT CARGO DOOR THRESHOLD AFT PLATE IAW AMM 25-52-10.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 53,931 hrs · 33,918 cycles

AFT CARGO LH Z ANGLE CORRODED SURFACE OF Z ANGLE STA 729 + 4 TO STA 849 / REMOVED AND REPLACED LH TRANSISTION ANGLE FROM STATION 727 TO STATION 847 LBL 25 PER SRM 51-10-02 AND SRM 53-00-53-2R-5

Part: BRACKET — BROKEN (LOWER EXT FUSELA) · airframe 53,533 hrs · 33,663 cycles

PANEL 192E NUTPLATE FORWARD SUPPORT BRACKETS BROKEN / REMOVED AND REPLACED PER SRM 51-40-02

Part: SPLICE — BROKEN (CABIN) · airframe 53,533 hrs · 33,663 cycles

OVERWING EXIT LIGHT ASSY SPLICE DAMAGED. REPAIRED SPLICE REF SWPM AND AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 51,635 hrs · 32,474 cycles

FORWARD FLASHLIGHT STRAP BROKEN. INSTALLED STRAP PER MM.

Part: RIVET — BROKEN (L1 DOOR) · airframe 51,291 hrs · 32,260 cycles

L1 DOOR SLIDE CONTAINER GIRT BAR CLIP RIVET BROKEN. INSTALLED RIVET PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,007 hrs · 30,740 cycles

EMERGENCY LIGHTS INOP AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: FUSE — FAULTY (CABIN) · airframe 49,007 hrs · 30,740 cycles

LT OVERWING EMERGENCY EXIT LIGHTS FAULTY AT LOCATION M1668. R&R FUSE PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,007 hrs · 30,740 cycles

EMERGENCY LIGHTS INOP AT LOCATION M2335. R&R BATTERY PACK PER AMM.

Part: NONE — CRACKED (MAIN CABIN) · airframe 49,007 hrs · 30,740 cycles

PANEL BREAK CRACKED AT BS 540 LBL 25-45 WL 208. / REMOVED AND ISNTALLED NEW PANEL BREAK ASSYEMBLY AT BS 540 LBL 25-45 WL 208 IAW PER DRAWING #143A0060 REV: - SOPM 20-50-01 92421U 5-6-18

Part: SUPPORT ANGLE — CORRODED (BS 320-340) · airframe 49,007 hrs · 30,740 cycles

L1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 320 TO 340, LBL 60. R & R THE SUPPORT ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 244-360) · airframe 49,007 hrs · 30,740 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 244 TO 360, LBL 1. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 49,007 hrs · 30,740 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, RBL 31. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: CHANNEL — CORRODED (BS 312-325) · airframe 49,007 hrs · 30,740 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 312 TO 325, RBL 60. R & R THE MOPSILL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 49,007 hrs · 30,740 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294.5, RBL 1. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,007 hrs · 30,740 cycles

AFT LOWERED CEILING EMERGENCY EXIT LIGHT INSERTS DAMAGED. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 49,007 hrs · 30,740 cycles

AFT CABIN WET AREA FLOOR PNL 241ACF HAS BROKEN INSERT AT STA 1008; L/H SIDE / REPAIRED DAMAGE AND REPLACED DAMAGED INSERT ON FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-9. 56749U 27APR18

Part: DRAG BRACE — CRACKED (ECS BAY RH) · airframe 49,007 hrs · 30,740 cycles

VERTICAL DRAG BRACE IS CRACKED ON FWD SIDE OF BS 663 VAPOR BARRIER RBL 25 WL 154 / REMOVED AND REPLACED VERTICAL DRAG BRACE ON FWD SIDE OF BS 663 VAPOR BARRIER RBL 25 WL 154 IAW SRM 51-40-02 AND DWG 149A7210

Part: STIFFENER — CRACKED (ECS BAY RH) · airframe 49,007 hrs · 30,740 cycles

HORIZONTAL STIFFENER ON FWD SIDE OF BS663 RBL 8 IS CRACKED AT WL 160 / REMOVED AND REPLACED HORIZONTAL STIFFENER ON FWD SIDE OF BS 663 RBL8 WL160 IAW SRM 51-40-02 AND DWG 111A1000.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 49,007 hrs · 30,740 cycles

ORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 450 TO BS 480, RBL 28. R&R WEB PER SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 49,007 hrs · 30,740 cycles

ACB; FLOOR PANEL SPLICE STRAP AT BS 727D HAS AREAS OF CORROSION FROM RBL10 TO LBL10 / ACB FLOOR PANEL SPLICE STRAP AT BS 727D FOUND TO BE OUTTA LIMITS DUE TO NO ALLOWABLE LIMITS IN SRM. RECEIVED NEW FLOOR PLANEL SPLICE P.O. #684381

Part: SPLICE STRAP — CORRODED (BS 887) · airframe 49,007 hrs · 30,740 cycles

AFT CARGO BAY FLOOR PANEL SPLICE STRAP CORRODED AT BS 887, BETWEEN RBL 10 TO LBL 10. R & R THE SPLICE STRAP IAW SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 49,007 hrs · 30,740 cycles

VERTICAL BULKHEAD CRACKED AT BS 663, LBL 36. REPAIRED BULKHEAD IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,007 hrs · 30,740 cycles

RT CREASE BEAM WEB CORRODED AT BS 723. R&R WEB IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 49,007 hrs · 30,740 cycles

ACB; FLOOR PANEL SPLICE STRAP AT BS 772 HAS AREAS OF CORROSION FROM RBL10 TO LBL10 / ACB FLOOR PANEL SPLICE STRAP AT BS 772 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM. RECEIVED NEW FLOOR PANEL SPLICE P.O.# 681622.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 49,007 hrs · 30,740 cycles

FAIRING PANEL # 195CL IS CRACKED IN THE RADIUS OF PANEL ON AFT END / FAIRING PANEL 195CL CRACK IN THE RADIUS ON THE AFT END WAS REPAIRED IAW SRM 51-70-05-2R-6

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 49,007 hrs · 30,740 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727 TO BS. 767, RBL 23. R&R SUPPORT IAW SRM & DWG.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 49,007 hrs · 30,740 cycles

LOWER VAPOR BARRIER CRACKED AT BS 663, BETWEEN RBL 10 TO RBL15. REPAIRED BARRIER PER SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 49,007 hrs · 30,740 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 747 TO BS 847, LBL 23. REPAIRED SUPPORT IAW SRM.

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 49,007 hrs · 30,740 cycles

LOWER VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 10 TO LBL 15. REPAIRED BARRIER IAW SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,659 hrs · 30,526 cycles

LEFT AFT EMERGENCY LIGHTS INOPERATIVE IN THE CABIN. R & R THE BATTERY PACK IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 47,511 hrs · 29,778 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 47,511 hrs · 29,778 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 47,511 hrs · 29,778 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.

Part: BRACKET — CRACKED (LEFT WING) · airframe 47,231 hrs · 29,593 cycles

LT MLG UPPER INBD PNL SUPPORT Z BRACKET CRACKED / REMOVED AND REPLACED Z BRACKET PER SRM 51-40-02

Part: LENS — BROKEN (CABIN) · airframe 46,971 hrs · 29,422 cycles

R2 DOOR EXIT SIGN LENS BROKEN. INSTALLED LENS PER SIP.

Part: AIR DATA MODULE — MALFUNCTIONED (COCKPIT) · airframe 46,929 hrs · 29,397 cycles

RIGHT INERTIAL REFERENCE SYSTEM FAULT LIGHT CAME ON IN FLIGHT FL380 LOST ALL NAVIGATION SYSTEMS, BOTH CAPTAIN`S AND FIRST OFFICER`S SIDE. AIR TURNBACK, DECLARED EMERGENCY. R & R THE RT AIR DATA INERTIAL REFERENCE UNIT IAW MM.

Part: PIN — LOOSE (EVAC SLIDE) · airframe 44,807 hrs · 28,123 cycles

L1 DOOR EMERGENCY EVAC SLIDE PACK HITCH PIN LOOSE. SECURED PIN PER MT.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 44,413 hrs · 27,887 cycles

CEILING EMERGENCY LIGHT LENS LOOSE AT ROW 24. SECURED THE LENS IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 44,413 hrs · 27,887 cycles

L2 LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. R&R SIGN PER AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,460 hrs · 27,294 cycles

L2 DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. R & R THE FUSE IAW MM.

Part: DOOR FRAME — CORRODED (R2 DOOR) · airframe 43,460 hrs · 27,294 cycles

R2 DOOR UPPER FRAME AFT LIGHTNING HOLE PRESSURE NUT FOR UPPER GATE SEAL CORRODED. R & R FRAME IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 43,460 hrs · 27,294 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 101.90, SECOND AFT FROM FORWARD SPAR. REPAIRED THE RIB IAW SRM.

Part: SLIDE — FRAYED (L1 DOOR) · airframe 43,460 hrs · 27,294 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT FRAYED. R & R SLIDE IAW MAINTENANCE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,460 hrs · 27,294 cycles

FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (BS 1016) · airframe 43,460 hrs · 27,294 cycles

INTERCOSTAL CRACKED AT BS 1016, LBL 40. R & R THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 1016) · airframe 43,460 hrs · 27,294 cycles

INTERCOSTAL CRACKED AT BS 1016, LBL 14. R & R THE INTERCOSTAL IAW SRM.

Part: WEB — CRACKED (LT WING) · airframe 43,460 hrs · 27,294 cycles

LEFT WING TRANSVERSE WEB CRACKED JUST INBOARD OF FLAP ROLLER SUPPORT ARM, UPPER FLANGE. R & R THE WEB IAW SRM.

Part: SUPPORT — CORRODED (BS 847-867) · airframe 43,460 hrs · 27,294 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 - 867, RBL 21. REMOVED AND REPLACED THE SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (BS 492-500A) · airframe 43,460 hrs · 27,294 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 492 - 500A. R & R THE SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 420-440) · airframe 43,460 hrs · 27,294 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 - 440. R&R THE SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 43,460 hrs · 27,294 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER CENTER FLOOR PANEL SUPPORT CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 43,460 hrs · 27,294 cycles

RIGHT FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A - 500D. REPAIRED THE SUPPORT IAW SRM & DWG.

Part: SHIELD — CORRODED (BS 767-793) · airframe 43,460 hrs · 27,294 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO 793, RBL 21. R&R THE SHIELD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,460 hrs · 27,294 cycles

FRAME CRACKED AT BS 294, RBL 55. R & R FRAME IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 43,460 hrs · 27,294 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, LBL 12. R & R THE INTERCOSTAL IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,460 hrs · 27,294 cycles

LEFT 3 WINDOW FRAME E-F POST CRACKED, 2ND LOWER FASTENER HOLE. REPAIRED FRAME.

Part: WINDOW FRAME — CRACKED (R3) · airframe 43,460 hrs · 27,294 cycles

R3 WINDOW FRAME E-F POST CRACKED. REPAIRED THE WINDOW FRAME IAW ACO.

Part: FRAME — CRACKED (BS 727B) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 480) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 43,460 hrs · 27,294 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 787) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 360) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 500A) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 480) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 727D) · airframe 43,460 hrs · 27,294 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 727D) · airframe 43,460 hrs · 27,294 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 727B) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 360) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 43,460 hrs · 27,294 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 43,460 hrs · 27,294 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 43,460 hrs · 27,294 cycles

FRAME CRACKED AT BS 440 STRINGER 8R. REPAIRED THE FRAME IAW EA.