N8626B
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
AFT GALLEY FLASHLIGHT WILL NOT TEST. R & R AFT GALLEY MOST RT EMERGENCY FLASHLIGHT AND BATTERY IAW AMM 25-64-00. WORKING MEL 25-12-01. AFT GALLEY FLASHLIGHT WILL NOT TEST. R & R AFT GALLEY MOST RH EMERGENCY FLASHLIGHT AND BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
AFT GALLEY FLASHLIGHT WILL NOT TEST. R & R AFT GALLEY MOST RT EMERGENCY FLASHLIGHT AND BATTERY IAW AMM 25-64-00. WORKING MEL 25-12-01. AFT GALLEY FLASHLIGHT WILL NOT TEST, R & R AFT GALLEY MOST RT EMERGENCY FLASHLIGHT AND BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
FORWARD GALLEY SERVICE DOOR ESCAPE SLIDE MANUAL INFLATION STRAP/HANDLE STUCK. SECURED THE R1 DOOR ESCAPE SLIDE MANUAL STRAP COVER AND HOOK AND LOOP IAW SIP.
RIGHT AFT OTBD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-04-960-801.
CRACK ON SUPPORT ANGLE LOC BTW ORSS 279 TO ORSS 330 TRAILING EDGE LT WING. REPLACED SUPPORT ANGLE LOC BTW ORSS 279 TO ORSS 330 TRAILING EDGE LT WING IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG 115A3700, SHEET 81, REV A.
CRACKED WEB, BS 847 - 867, LBL 22. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DRAWING 149A8100, SHEET 1, REV-.
CRACKED FLOOR SUPPORT BTW BS 380 - 400, BL 0, WL 208.1. REPLACED FLOOR SUPPORT IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A5400, SHEET 182, & 184, REV-.
ELONGATE HOLES ON ACCESS PANEL 193AR BODY FAIRING, LOWER FUSELAGE. REPAIRED THE ACCESS PANEL 193AR IAW SRM 51-70-05-2R-9, REPAIR 9.
ELONGATE HOLES ON ACCESS PANEL 193AL ON THE BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AL BODY FAIRING IAW SRM 51-70-05-2R-9, REPAIR 9.
CRACKED FLOOR SUPPORT, BS 380 - 400, LBL 15, WL208.1. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 143A5400, SHEET 182, & 184, REV-.
CRACK ANGLE SUPPORT TRAILING EDGE LOCATED ORSS267 AT LT WING . REPLACED ANGLE SUPPORT TRAILING EDGE LOCATED ORSS267 AT LT WING IAW SRM 51-40-02 AND DWG: 115A2930; SHEET: 17; REV: -..
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS297 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS297 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3700 SHEET 82 REV A.
CORRODED WEB - INTERCOSTAL, BS 747 - 767, RBL 21, WL 155.3. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 146A7502, SHEET 50, REV-.
CORRODED STRAP, BS 797, RBL 20, WL 155.3. REPLACED THE STRAP & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A8120, SHEET 40, REV A, & DWG 146A0081, SHEET 49, REV A.
CRACK CARGO TRACK, BS 727I, RBL 13.84, WL 152.7 IN THE AFT CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE CARGO TRACK, BTW BS 727H + 8 INCHES - BS 727I + 16 INCHES IAW SRM 53-00-53-2R-3.
CORRODED SHIELD, BS 767 - 787, RBL 21, WL 155.3. REPLACED THE SHIELD IAW SRM 51-40-02, & DWG 146A0081, SHEET 49, REV A.
CORRODED NUT PLATES, BS 787 - 794, RBL 20, WL 155.3. REPLACED THE NUT PLATES IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 146A0081, SHEET 49, REV A.
CRACKED ZEE CHANNEL, BS 887 - 947.5, RBL 21, WL 155.3. REPLACED THE ZEE CHANNEL IAW SRM 51-10-02-0G-0, ITEM 9, DWG 147A7500, SHEET 36 & 37, REV-, & DWG 146A7502, SHEET 54, REV-.
CORROSION ZEE CHANNEL LOCATED BETWEEN BS 727E+10 INCHES - BS 847, LBL 21, WL 155.3. REPLACED THE ZEE CHANNEL, & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, SRM 53-00-53-2R-6, & DWG 146A7500, SHEET 233, REV -. MAJOR REPAIR.
CORROSION ON THE GIRT BAR FITTING, BS 312, LBL 53, WL 208.1. REPLACED THE GIRT BAR FITTING IAW SRM 51-10-02-0G-0, ITEM 9, & SRM 51-40-02, PERFORMED A VISUAL INSPECTION ON THE AFFECTED AREA & NO DAMAGE FOUND.
CRACK RIB LOCATED LE STA 114.55 ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED RIB LOCATED LE STA 114.55 ACCESS PANEL 341B AT RT HORIZONTAL STAB IAW SRM 51-10-02, AND SRM 51-40-02, DWG 186A1305, SHEET 1, REV A, AND DWG 186A1001, SHEET 19, REV -.
CRACK RIB LOCATED LE HSS 151.95 ACCESS PANEL 341B ON RT HORIZONTAL STAB. REPLACED RIB LOCATED LE STA 151.95 ACCESS PANEL 341B AT RT HORIZONTAL STAB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 186A1001, SHEET 19, REV-.
CRACKED SUPPORT ANGLE, BS663, LBL 10. PERFORMED A PERMANENT REPAIR, CATEGORY -A-, IAW SRM 57-10-10-2R-5.
CRACK RIB LOCATED LE STA 105.26 ACCESS PANEL 341B AT RT HORIZONTAL STAB. REPLACED RIB LOCATED LE STA 105.26 ACCESS PANEL 341B AT RT HORIZONTAL STAB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 186A1001, SHEET 19, REV-.
CRACKED SUPPORT ANGLE, BS 663, RBL35. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG:111A1000, SHEET 329, REV A.
EMERGENCY LIGHT BALLAST INOPERATIVE. REPLACED THE BALLAST IAW AMM 33-51-01-960-802. TESTED OK.
CRACKED SUPPORT BEAM 4. REPLACED THE SUPPORT BEAM 4 IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 141A6516, SHEET, 144, REV -.
CORROSION RAIL PLATE ON INTERNAL CAVITY OFSS 426, LT WING LE. REPLACED RAIL PLATE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
CRACKED FRAME, BS 312, S5L - S6L. PERFORMED A REPAIR ON THE FRAME IAW EA M 22-153-01244.
CORROSION RAIL PLATE, ON INTERNAL CAVITY LEADING EDGE OFSS 573, LT WING. REPLACED THE RAIL PLATE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
CORROSION RAIL NUT PLATE LOCATED ON INTERNAL CAVITY LEADING EDGE OFSS334 AT LT WING. REPLACED RAIL PLATE LOC INTERNAL CAVITY LEADING EDGE OFSS334 AT LT WING IAW SRM 51-10-02, ITEM 9, DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM AND INSTALLED FASTENERS IAW SRM 51-40-02.
CRACKED WEB, BS 328 - 344, LBL 46. PERFORMED GENERAL VISUAL INSPECTION ON THE WEB - INTERCOSTAL & NO DAMAGE FOUND IAW SRM 51-00-06-0G-0. REMOVED & RE INSTALLED THE WEB - INTERCOSTAL IAW SRM 51-40-02,& DWG 141A5400, SHEET 28, REV -.
CRACKED WEB, BS 312 - 328, RBL 31. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A5400, SHEET 39, REV -.
CORROSION RAIL PLATE ON INTERNAL CAVITY OFSS 409, LT WING LE. REPLACED RAIL PLATE IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9.
CRACKED WEB, BS 277 - 294.5, BL 0. REPLACED THE WEB INTERCOSTAL & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 20, REV-.
CORRODED RAIL NUT PLATE, SS 604, LT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02, DWG 112A4402, SHEET 41, REV A, & PERFORMED A VISUAL INSPECTION OF AFFECTED AREA AND NO DAMAGE FOUND.
CORRODED RAIL NUT PLATE, SS527, LT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.
CORRODED RAIL NUT PLATE SS 706, LT WING LE. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, REV A, SHEET 41.
CORRODED RAIL NUT-PLATE, OFSS 290, LT WING LE. REPLACED THE RAIL NUT-PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHEET 40, REV A.
CORRODED RAIL NUT PLATE LOCATED INTERNAL CAVITY LEADING EDGE OFSS 308, LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHEET 40, REV A.
CORRODED RAIL PLATE, INTERNAL CAVITY OFSS 549, LT WING LE. REPLACED RAIL PLATE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.
CRACKED WEB, BS 344 - 360, LBL 11 IN THE FWD GALLEY AND LAVATORY. REPLACED THE WEB INTERCOSTAL, & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A5400, SHEET, 46, REV A.
CORROSION RAIL PLATE ON INTERNAL CAVITY OFSS 421, LT WING LE. REPLACED THE RAIL PLATE IAW SRM 51-10-02, ITEM 9 DUE TO NO FOUND ALLOWABLE DAMAGE IAW SRM AND INSTALLED FASTENERS IAW SRM 51-40-02.
CRACKED TIE CLIP, BS 277, S10R IN THE PAX CABIN. REPLACED THE TIE CLIP IAW SRM 51-10-02-0G-0, ITEM 9, DWG 141A1110, SHEET 18, REV -, & DWG 141A8380, SHEET 33, REV -.
CORROSION RAIL PLATE LOC ON INTERNAL CAVITY OFSS 540, LT WING LE. REPLACED THE RAIL PLATE IAW SRW 51-40-02, SRM 51-10-02-0G-0, ITEM 9, & DWG 112A4402, SHEET 40, REV A. PERFORMED VISUAL INSPECTION ON AFFECTED AREA AND NO FOUND DAMAGE.
CRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02. EASUREMENT OF CRACKS: L:0.295 INCHES.
CORRODED SUPPORT ZEE, BS 500C - 500I, LBL 22, WL 156. PERFORMED A PERMANENT REPAIR ON THE SUPPORT ZEE IAW SRM 53-00-53-2R-5, REPAIR 5, & EA M-22-153-01550.
CRACKED SEAL PLATE ACCESS PANEL 431AT ON LT PYLON (1 EA). MEASUREMENT OF CRACK: L: 0.988 INCH. REPLACED THE SEAL PLATE ON ACCESS PANEL 431AT LT PYLON IAW SRM 51-40-02, AND SRM 51-10-02, STEP 9, NO ADDITIONAL DAMAGE.
CORRODED FLOORBEAM, BS 986.5, LBL 44, WL 208.1. PERFORMED A REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
CRACK LEADING EDGE RIB LOCATED LE HSS 105.26, LT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 19, REV -.
CRACKED ACCESS PANEL 331B RIB LOCATED LE HSS 114.55 AT LT HORIZONTAL STAB. REPLACED THE RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 186A1001, SHEET 19, REV -.
CORRODED FLOORBEAM BS 986.5, RBL 44, WL 208.1. PERFORMED A REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
DETERIORATED NUT ON THE ASSIST HANDLE LINING, ENTRY DOOR. REPLACED THE NUT IAW AMM 52-11-31-400-802, STEP 3.G (2).
CRACKED GUSSET ANGLE, BS 500I, S21L, IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE & FASTENERS IAW SRM 51-40-02-0G, & DWG-143A7902, SHEET 256, REV B.
CRACKED ACCESS PANEL 191D, LOWER FUSELAGE. REPAIRED THE ACCESS PANEL PANEL 191D IAW SRM 51-70-05-2R-2, REPAIR 2.
CRACKED ANGLE, BS 500H, S26R. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 137, & 138, REV-.
CRACKED ANGLE, BS 500H, S26R. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 137, & 138, REV-.
LAVATORY D FLASHLIGHT INBD INOPERATIVE. REPLACED THE FLASHLIGHT IAW CMM 25-60-02, REV 10, FIGURE 1, ITEM 17, PAGE 10006, & PAGE 10007.
CRACKED SCUFF PLATE AFT CORNER, IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1; & BAC 5975.
CRACKED GUSSET ANGLE, 500I, S19R, IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE & FASTENERS IAW SRM 51-40-02-0G, & DWG-143A7902, SHEET 256, REV B.
BURNED OUT OVERWING EXIT LIGHT ROW 14 LEFT. REPLACED THE LIGHT IAW AMM 33-21-00-960-805, STEP 10.A. - 10.C.(11) EXCEPT 10.C.(4)(D) AND 10.C.(5)(D). PERFORMED A TEST, TESTED OK.
BROKEN EMERGENCY LIGHT LENS. REPLACED THE LENS IAW AMM 33-51-03-960-803, STEP 4.D.(1)(2).
BURNED OUT OVERWING EXIT LIGHT, ROW 14 RIGHT. REPLACED THE LIGHT IAW AMM 33-21-00-960-805, STEP 10.A. - 10.C.(11), EXCEPT 10.C.(4)(D) AND 10.C.(5)(D). TESTED OK.
DETERIORATED NUT ON THE ASSIST HANDLE OF THE AFT SERVICE DOORWAY LINING. REPLACED THE NUT IAW AMM 25-21-25-420-801, STEP 3.B.(5), & SOPM 20-50-01, REV 39.
R1 DOOR GIRT BAR FITTINGS LOOSE. TORQUED THE R1 DOOR GIRT BAR FITTINGS IAW AMM 25-66-02-400-801.
RIGHT OVERWING LIGHTS INOPERATIVE. R & R IAW AMM 33-51-06-960-805-NG POWER SUPPLY BATTERY PACK.
RIGHT OVERWING LIGHTS INOPERATIVE. R & R IAW AMM 33-51-06-960-805-NG POWER SUPPLY - BATTERY PACK.
BOTH L/H INTERIOR OVER WING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.
ON APPROACH SELECTED FLAPS 30; FLAP DISPLAYED 15 & 25. WENT AROUND AND SELECTED FLAPS 15; FLAPS DISPLAYED BOTH AT 25 AND STAYED THERE FOR THE REMAINDER OF THE FLIGHT. OVERSPEED FLAPS 25 TO SPEED 193KT MOMENTARILY. LANDED NORMALLY AND ONCE AT THE GATE WITH FLAP HANDLE AT 15 BOTH FLAPS DISPLAYED 15 MARK. AIRCRAFT DID NOT HAVE ANY ROLL WITH SPLIT FLAPS<[01] BITE CKD FSEU FOUND FAULT 27-52260. T/S PER FIM 27-51 TASK 820 R&R R/H FLAP POSITION TRANSMITTER PER MM 27-58-01 AND FLAP POSITION INDICATOR PER MM 27-58-02. ACCOMPLISHED PHASE 1 CONDITIONAL OVERSPEED INSP PER MM 05-51-08. NO FAULTS NOTED.
EMERGENCY EXIT SIGN ARE POINTING IN THE WRONG DIRECTION<[01] RETURNED OVER-WING EMERGENCY EXIT LIGHT LENSES AT LEFT SIDE TO CORRECT POSITION PER SIP
LH OVERWING EXITS; FORWARD AND AFT; EMERGENCY LIGHTS AT DOOR FRAMES HAS SEVERAL BULBS INOP. <[01] RELAMPED L/H OVERWING EXITS; FORWARD AND AFT; EMERGENCY LIGHTS AND PERFORMED A SATISFACTORY TEST OF THE NEW LAMPS IAW AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
TRAYTABLE ARM STOP FAILED 14D<[01] REPLACED TRAY TABLE ARM PIVOT SPRING AT 14D PER CMM 25-22-46.
FORWARD SERVICE DOOR PLASTIC HANDLE BROKEN.<[01] R+R FWD SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31.
ON APPROACH; WITH FLAPS 30 SELECTED; FLAPS WOULD ONLY GO TO FLAPS 15<[01] CLEANED LEFT FLAP TRANSMITTER ELECTRICAL CONNECTOR AND PERFORMED OPS TEST IAW AMM 27-58-01. OPS TEST GOOD. A/C OK FOR SERVICE
RIGHT FWD OVERWING ESCAPE LIGHT INOP BATTERY PACK M1676 LOCATED IN CABIN BEHIND AIR RETURN AT 8DEF<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1676 WITH NEW FROM STOCK IAW AMM 33-51-06. OPS CHECK GOOD.
L/H AFT OVERWING ESCAPE LIGHT AND ESCAPE GROUND LIGHT INOP EMERGENCY BATTERY M1670 LOCATED IN CABIN BEHIND AIR RETURN AT FWD SIDE OF 21ABC<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1670 WITH NEW FROM STOCK. OPS CHECK GOOD.;[02] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1670 WITH NEW FROM STOCK IAW AMM 33-51-06. OPS CHECK GOOD.;[03] IAW AMM 33-51-06
L/H FWD OVERWING ESCAPE LIGHT INOP BATTERY PACK M2335 LOCATED IN CABIN BEHIND AIR RETURN AT 8ABC<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M2335 WITH NEW FROM STOCK IAW AMM 33-51-06. OPS CHECK GOOD.;[02] IAW AMM 33-51-06
R/H AFT OVERWING ESCAPE LIGHT INOP BATTERY PACK M1671 LOCATED IN CABIN BEHIND AIR RETURN AT 21DEF<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1671 WITH NEW FROM STOCK IAW AMM 33-51-06. OPS CHECK GOOD.;[02] IAW AMM 33-51-06
LWR ANGLE BEHIND PANEL 141PW CRACKED.<[01] REMOVED AND REPLACED LWR ANGLE BEHIND PANEL 141PW IAW SRM 51-40-02.
4 EA. FWD CARGO CAP STRIPS HAVE MULTIPLE AREAS OF CORROSION ON LOWER SURFACE (MARKED)<[01] PARTS DATA UPDATE ONLY;[02] INSTALLED NEW FWD CARGO CAP STRIPS PER AMM 25-52-06;[03] REMOVED AND REPLACED 4 EA. FWD CARGO CAP STRIPS IAW AMM 25-52-10.;[04] VERIFIED REMOVED AND REPLACED 4 EA. FWD CARGO CAP STRIPS IAW AMM 25-52-10.
RH OTBD AFT FLAP INBD LOWER SURFACE HAS DELAMINATION.<[01] REMOVED RIGHT WING O/B T/E FLAP ASSY PER AMM 27-51-22;[02] OK TO INSTALL AFT FLAP.;[03] INSTALLED NEW AFT FLAP IN REF TO AMM 27-51-22;[04] INSPECTION C/W FOR CA #3;[05] DUE TO FAILED RIG CHECK REMOVED INSTALLED FLAP WITH NEW FROM STOCK SEE CARD TTG8Q00SFM9V FOR SIGN OFFS AND WORK PERFORM.;[06] VERIFIED WORK ACCOMPLISHED ON CARD TTG8Q00SFM9V . RII IS C/W
#1ENG. INBD.COWL;PNL. 414; WEB SUPPORT ATTACHMENT AT OIL SERV. DOOR OPENING CRACKED.<[01] REMOVED AND REPLACED WEB PER CMM 71-13-30.;[02] INSPECTED CA #1
FLIGHT DECK PANEL 211AF DEFORMED<[01] LOCATED; DRILLED AND DEBURRED REPLACEMENT PANEL PER SRM 51-40-05.;[02] LOCATED; DRILLED AND DEBURRED REPLACEMENT PANEL PER SRM 51-40-05.;[03] REPAIR COMPLETED AND PANEL INSTALLED ON NON ROUTINE TTG8Q00S4P95 AND EA M21-153-00734;[04] VERIFIED REPAIR COMPLETED AND PANEL INSTALLED ON NON ROUTINE TTG8Q00S4P95 AND EA M21-153-00734
L/H WING OUTBD UPPER FIXED T/E PANEL BULB SEAL WEB CLIP THAT ATTACHES TO DEFLECTION CONTROL RIB CRACKED AT LOWER FASTENER ( PHOTO ATTACHED )<[01] INSTALLED NEW CLIP ANGLE WITH FASTENERS PER SRM 51-40-02.;[02] INSTALLED NEW CLIP ANGLE WITH FASTENERS PER SRM 51-40-02.;[03] INSTALLED NEW CLIP ANGLE WITH FASTENERS PER SRM 51-40-02.
LEFT HAND OUTBOARD AFT FLAP UPPER SURFACE INBOARD END DELAMINATED<[01] C/W;[02] REMOVED AND REPLACED AFT O/B L/H AFT FLAP. PER AMM 27-51-22;[03] COMPLIED WITH REMOVAL AND REPLACEMENT OF AFT O/B L/H AFT FLAP. PER AMM 27-51-22
FWD SERVICE DOOR GRIT BAR HOLDER IS LOOSE<[01] TIGHTEN GRIT BAR RESTRAINT PER SIP
FORWARD ENTRY DOOR GIRT BAR BRACKET IS LOOSE / [01] ADJUSTED MOUNTING BRACKET ON ENTRY DOOR SLIDE HOUSING IAW SIP
SUPPLEMENTAL INFORMATION: ENG FAILURE;#1 ENG . ENGINE FAILED AT APPROXIMATELY 1800 MSL ON CLIMB NO N2 ROTATION / [01] C/W INSP;[02] C/W INSP;[03] R&R #1 ENGINE ASSY PER MT 71-00-01.
AFT SERVICE DOOR ASSIST HANDLE IS BROKEN / [01] REMOVED AND REPLACED HANDLE IAW AMM. 52-41-31.
FWD GALLEY FWD L/H EMERGENCY IIGHTS INOP / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 315L PER MM 33-51-06;[02] INSPECTED REPLACEMENT OF EMERGENCY LIGHT BATTERY PACK AT STA 315L PER MM 33-51-06.;[03] REPLACED BATTERY PACK AND OPS CH3CK GOOD PER AMM 33-51-06.
APU FEED CABLE IN CABIN R/H STA 867 STRINGER 3 HANGER BRACKET CRACKED / BROCKEN. / [01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02.;[02] VERIFIED REPAIR.
#8 SLAT O/B LOWER SURFACE OF THE WEDGE IS CRUSHED AND DELAM. / [01] DELAMINATION TO LOWER SURFACE OF #8 SLAT IS OUT OF LIMITS IAW SRM 57-42-01-1A-1;[02] ACCOMPLISHED PRE #8 SLAT INSTALLATION BORESCOPE INSPECTION. NO DEFECT NOTED.;[03] OK TO INSTALL #8 SLAT.;[04] ACCOMPLISHED POST SLAT CAN BORESCOPE INSPECTION. NO DEFECT NOTED.;[05] R&R #8 SLAT PER M/M 27-81-21.;[06] C/W INSPECTION.;[07] SEE INDIVIDUAL SIGN OFFS FOR RII INSPECTION.
FWD CARGO FLOOR INTERCOSTAL LBL 32 STA. 500F TO 500G IS CRACKED. / [01] REMOVED DAMAGED INTERCOSTAL.;[02] DRILLED UP REPAIR ANGLE PER SRM 53-30-53-2R-1.;[03] INSPECTED AS REQUIRED FABRICATED REPAIR DOUBLER AND OK TO INSTALL REPAIR.;[04] INSTALLED REPAIR PARTS PER SRM 53-30-53-2R-1.;[05] INSTALLED NEW INTERCOSTAL PER SRM 51-40-02.;[06] C/W INSPECTION
FWD CARGO FLOOR INTERCOSTAL LBL 32 STA. 500G TO 500H IS CRACKED. / [01] REMOVED DAMAGED INTERCOSTAL.;[02] INSTALLED NEW INTERCOSTAL PER SRM 51-40-02.;[03] C/W INSPECTION
R/H TRANSITION ANGLE STA 727G THROUGH STA 727G+10; RBL 21 SHOWS EVIDENCE OF CORROSION. / [01] REMOVED CORR. R/H TRANSITION ANGLE STA. 727G THROUGH 727G+10 ; PER SRM 51-10-02 ; MATERIAL REMOVED MESUMENT ( .005 ) FOUND OUT OF LIMITS PER SRM. 53-00-53-1A-1;[02] REPLACED SECTION OF TRANSITION ANGLE FROM STA. 727F +10 TO 767 ON NR# TTG8Q00BU45D;[03] C/W INSPECTION.
AFT CARGO DOOR THRESHOLD WEB HAS EVIDENCE OF CORROSION FROM STA 794 THROUGH STA 847; S-25R / [01] CORROSION FOUND OUT OF LIMITS PER SRM 53-00-53-1A-1<BR>REMOVED FASTENERS OF AFT CARGO THRESHOLD WEB PER SRM 51-40-02.;[02] INSTALLED AFT CARGO WEB P/N 146A8123U25 PER SRM 51-40-02.;[03] INSTALLED AFT CARGO WEB P/N 146A8123U25 PER SRM 51-40-02;[04] REMOVED FASTENERS OF AFT CARGO THRESHOLD WEB PER SRM 51-40-02.<BR>INSTALLED AFT CARGO WEB P/N 146A8123U25 PER SRM 51-40-02;[05] C/W INSPECTION<BR>REMOVED FASTENERS OF AFT CARGO THRESHOLD WEB PER SRM 51-40-02. <BR>INSTALLED AFT CARGO WEB P/N 146A8123U25 PER SRM 51-40-02
R/H TRANSITION ANGLE STA 727F +10; RBL 21 SHOWS EVIDENCE OF CORROSION. / [01] REMOVED CORR. R/H TRANSITION ANGLE STA. 727F- ; PER SRM 51-10-02 ; MATERIAL REMOVED MESUMENT ( .005 ) FOUND OUT OF LIMITS PER SRM. 53-00-53-1A-105;[02] REMOVE AND REPLACE R/H TRANSITION ANGLE STA 727F+ 10-767 PER SRM 53-00-53-2R-5.;[03] REMOVE AND REPLACE R/H TRANSITION ANGLE STA 727F+ 10-767 PER SRM 53-00-53-2R-5. REPAIRED SPLICE AT 727F+10 PER SRM 53-00-53-2R-5. INSTALLED NUT PLATES PER SRM 51-40-10.;[04] C/W RII INSPECTION <BR>REMOVE AND REPLACE R/H TRANSITION ANGLE STA 727F+ 10-767 PER SRM 53-00-53-2R-5. REPAIRED SPLICE AT 727F+10 PER SRM 53-00-53-2R-5. INSTALLED NUT PLATES PER SRM 51-40-10.
R/H TRANSITION ANGLE STA 727I THROUGH STA 727J; RBL 21 SHOWS EVIDENCE OF CORROSION. / [01] REMOVED CORR. R/H TRANSITION ANGLE STA. 727I-727J ; PER SRM 51-10-02 ; MATERIAL REMOVED MESUMENT ( .006 ) FOUND OUT OF LIMITS PER SRM. 53-00-53-1A-1;[02] REPLACED SECTION OF TRANSITION ANGLE FROM STA. 727F +10 TO 767 ON NR# TTG8Q00BU45D;[03] C/W INSPECTION.
R/H TRANSITION ANGLE STA 727J THROUGH STA 747; RBL 21 SHOWS EVIDENCE OF CORROSION. / [01] REMOVED CORR. R/H TRANSITION ANGLE STA. 727J-747 - PER SRM 51-10-02 ; MATERIAL MESUMENT ( .006 ) FOUND OUT OF LIMITS PER SRM. 53-00-53-1A-1;[02] REPLACED SECTION OF TRANSITION ANGLE FROM STA. 727F +10 TO 767 ON NR# TTG8Q00BU45D;[03] C/W INSPECTION.
R/H TRANSITION ANGLE STA 747 THROUGH STA 767; RBL 21 SHOWS EVIDENCE OF CORROSION. / [01] REMOVED CORR. R/H TRANSITION ANGLE STA. 747 - 767 PER SRM 51-10-02 ; MATERIAL MESUMENT ( .006 ) FOUND OUT OF LIMITS PER SRM. 53-00-53-1A-1;[02] REPLACED SECTION OF TRANSITION ANGLE FROM STA. 727F +10 TO 767 ON NR# TTG8Q00BU45D;[03] C/W INSPECTION.
R/H TRANSITION ANGLE STA 767 THROUGH STA 787; RBL 21 SHOWS EVIDENCE OF CORROSION. / [01] REPLACED SECTION OF TRANSITION ANGLE FROM STA. 727F +10 TO 767 ON NR# TTG8Q00BU45D;[02] C/W INSPECTION.
AFT CARGO FWD SCUFF PLATE IS CRACKED AT AFT EDGE / [01] LOCATE DRILL AND INSTALL SCUFF PLATE MPN: 146A8341-7 PER SRM 51-10-02;[02] C/W INSPECTION.
THE FWD CARGO ENTRY THRESHOLD WEB HAS AREAS OF CORROSION FORM STATION 440 TO 492. / [01] REMOVED .020' MATERIAL; OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] DRILLED UP NEW WEB COUNTERSUNK AND ATTACHED NUTPLATES PER SRM 51-40-02;[03] OK TO INSTALL FWD CARGO DOOR CUTOUT THRESHOLD WEB.;[04] REMOVED AND REPLACED FWD CARGO ENTRY THRESHOLD WEB IAW SRM 51-40-02.
LEFT HAND TRANSITION ANGLE AT STATION 500H TO 500I HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .006' MATERIAL; OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE SECTION FROM STA. 460+10 TO 500I TO BE REPLACED ON CARD TTG8Q00BSUBU.;[03] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 500G TO 500H HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .005' MATERIAL ; OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE SECTION FROM STA 460+10 TO STA 500 I TO BE REPLACED ON CARD TTG8Q00BSUBU;[02] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 500F TO 500G HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .020' MATERIAL ; OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE SECTION TO BE REPLACED ON CARD TTG8Q00BSUBU;[02] LINE 1 UNDER CORRECTIVE ACTIONS WRITTEN ERROR.....<BR>REMOVED .007' MATERIAL ; OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE SECTION TO BE REPLACED ON CARD TTG8Q00BSUBU;[03] REMOVED .007' MATERIAL ; OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE SECTION FROM STA 460+10 TO STA 500 I TO BE REPLACED ON CARD TTG8Q00BSUBU;[04] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 500E TO 500F HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .010' MATERIAL ; OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE SECTION TO BE REPLACED ON CARD TTG8Q00BSUBU.;[02] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 500B TO 500C HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .008' MATERIAL ; OUT OF LIMITS PER SRM 53-00-53-1A-2. L/H L?L <BR>L/H TRANSITION ANGLE FROM STA 460+10 TO 500 I TO BE REPLACED ON CARD TTG8Q00BSUBU.;[02] C/W INSPECTION.;[03] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 500A TO 500B HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .008' MATERIAL; OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE TO BE REPLACED FROM STA 460+10 TO 500I ON CARD TTG8Q00BSUBU.;[03] C/W INSPECTION
LEFT HAND TRANSITION ANGLE AT STATION 500D HAS CORROSION ON UPPER SURFACE. / [01] REMOVED .014' MATERIAL OUT OF LIMITS PER SRM 53-00-53-0-1A-2.;[02] TRANSITION ANGLE TO BE REPLACED FROM STA 460+10 TO 500I ON CARD TTG8Q00BSUBU.;[03] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 480+14 HAS CORROSION AROUND THE FASTENER HOLE. / [01] TRANSITION ANGLE FROM STA 460+10 TO 500 I TO BE REPLACED ON<BR>CARD TTG8Q00BSUBU.;[02] TRANSITION ANGLE FROM STA 460+10 TO 500 I TO BE REPLACED ON<BR>CARD TTG8Q00BSUBU.;[03] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 500 TO 500A HAS CORROSION AROUND THE FASTENER HOLES. / [01] C/W INSPECTION.
RIGHT HAND TRANSITION ANGLE AT STATION 500H TO 500I HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED AND REPLACED FWD CARGO; R/H TRANSITION/SIDEPLATE ANGLE FROM STA. 500A TO STA. 500I IAW SRM 51-40-02.
LEFT HAND TRANSITION ANGLE AT STATION 500D HAS EVIDENCE OF CORROSION AT THE INBD ATTACH FASTENER POINT. / [01] REMOVED .014' MATERIAL; OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] SECTION OF TRANSITION ANGLE TO BE REPLACED FROM STA. 460+10 TO 500I ON CARD TTGQ00BSUBU.;[03] C/W INSPECTION.
AT STATION 500I ON THE AFT SIDEWALL ATTACH STRIP; THE AREA THAT SITS ABOVE THE RIGHT HAND TRANSITION ANGLE OTBD SIDE HAS EVIDENCE OF CORROSION. / [01] R&R AFT SIDEWALL ATTACH STRIP (PN 143A9485Y34) PER SRM 51-40-02
CORROSION ON FLOOR BEAM UPPER SURFACE STA 947.5 LBL 24 UNDER LAV MOUNT / [01] BLENDED SURFACE CORROSION ON UPPER CHORD OF FLOOR BEAM AT STA. 947.5; LBL 24? PER SRM 51-10-02. REMOVED .037? OF MATERIAL FROM UPPER SURFACE CHORD. DAMAGE REMOVAL OUT OF LIMITS PER SRM 53-70-51-1A-1.;11] REPAIRED CABIN FLOOR BEAM AT STA. 947.5; LBL 24 PER SRM 53-70-51-2R-8; ALTERNATIVE 3 AND EA 22-153-01109-WIP1; (TTG8Q00BUT7K) AND (TTG8Q00BXWHU);[12] VERIFIED CABIN FLOOR BEAM REPAIRED AT STA. 947.5; LBL 24 PER SRM 53-70-51-2R-8; ALTERNATIVE 3 AND EA 22-153-01109-WIP1; (TTG8Q00BUT7K) AND (TTG8Q00BXWHU) COMPLETE.
CORROSION ON INTERCOSTAL AT AFT LAV MOUNT STA 947.5+2 LBL50 / [01] BLENDED CORROSION ON INTERCOSTAL AT AFT LAV MOUNT ; STA. 947.5; LBL 50 PER SRM 51-10-02. REMOVED .050 OF MATERIAL. DAMAGE REMOVAL OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] VERIFIED CORROSION REMOVAL AND DAMAGE REMOVAL OUT OF LIMITS.;[03] REMOVED AND REPLACED DAMAGED INTERCOSTAL PER SRM 51-40-02.;[04] VERIFIED CORRECTIVE ACTION #3
CORROSION ON INTERCOSTAL AT AFT LAV MOUNT STA 947.5+2 RBL50 / [01] REMOVED CORROSION ON INTERCOSTAL (STA 947.5+2 RBL 50) REMOVED 0.050' OF MATERIAL FOUND TO BE OUT OF LIMITES PER SRM 53-70-51-1A-1.;[02] VERIFIED CORROSION REMOVAL AND DAMAGE REMOVAL OUT OF LIMITS.;[03] LOCATED HOLES IN REPLACEMENT INTERCOSTAL IAW SRM 51-40-05.;[04] VERIFIED HOLE LOCATIONS AND PREP.;[05] OK TO INSTALL.;[06] REMOVED AND INSTALLED NEW INTERCOSTAL AT RBL 50 STA 947.5 TO STA 967 IAW SRM 51-40-02. SEE STEPS FOR ALL WORK ACCOMPLISHED.;[07] VERIFIED INTERCOSTAL REPLACEMENT AND INSTALLATION.
RIGHT HAND TRANSITION ANGLE AT STATION 420 TO 440 HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED DAMAGE PER SRM 51-10-02. REMAINING MATERIAL OUT OF LIMITS PER SRM 53-00-53.;[02] DRILLED FASTENER HOLES IN NEW PANEL AND INSTALLED NUTPLATES. OKAY TO INSTALL.;[03] VERIFIED NEW HOLES AND NUT PLATE INSTALLATION.;[04] OK TO INSTALL TRANSITION SHIELD GRANTED.;[05] REMOVED CORROSION DAMAGE PER SRM 51-10-02. REMAINING MATERIAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED SHIELD PER SRM 51-40-02.;[06] C/W INSPECTION<BR>REMOVED CORROSION DAMAGE PER SRM 51-10-02. REMAINING MATERIAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED SHIELD PER SRM 51-40-02.
LEFT HAND TRANSITION ANGLE AT STATION 500C TO 500D HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .005' MATERIAL; OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE TO BE REPLACED FROM STA 460+10 TO 500I ON CARD TTG8Q00BSUBU.;[03] C/W INSPECTION.
LEFT HAND TRANSITION ANGLE AT STATION 500D TO 500E HAS CORROSION AROUND THE FASTENER HOLES. / [01] REMOVED .014' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] SECTION OF TRANSITION ANGLE TO BE REPLACED FROM STA. 460+10 TO 500I ON CARD TTGQ00BSUBU.;[03] C/W INSPECTION.
CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED AT FASTENER HOLE; LOCATED BETWEEN STA 312 AND STA 328 LBL 45. MRKD / [01] REMOVED AND REPLACED CABIN FLOOR SUPPORT INTERCOSTAL FROM STA 312 TO STA 328 LBL45 IAW SRM 51-40-02.;[02] INSPECTED WORK PERFORMED.
AT STATION 500I; THE STRINGER CLIP BELOW THE RIGHT HAND TRANSITION ANGLE HAS EVIDENCE OF CRACKS AROUND THE TWO VERTICAL FASTENERS. PICTURE ATTACHED / [01] STRINGER CLIP WAS REMOVED AND REPLACE PER EA-22-153-01161; FAULT CODE TTG8Q00C2DF6.;[02] C/W INSPECTION.
LEFT ELEVATOR FWD UPPER SLIDER SEAL CRACKED. / [01] REMOVED AND REPLACED L/H UPPER SLIDER SEAL PER AMM 53-31-31
#1 ENGINE I/B FAN COWL WEB ATTACHED TO 3RD STRINGER FROM AFT EDGE IS CRACKED. (MARKED) / [01] REMOVED AND REPLACED NEW WEB BRACKET FOR #1 ENGINE I/B FAN COWL PER SRM 51-40-02;[02] UPDATED PARTS INFO;[03] INSPECTED WORK PERFORMED.
FWD CARGO; FWD CORNER SCUFF PLATE CRACKED. (MARKED) / [01] DRILLED UP REPLACEMENT FWD CORNER SCUFF PLATE PER SRM 51-40-02.;[02] C/W INSPECTION;[03] INSTALLED FWD CARGO FWD CORNER SCUFF PLATE PER AMM 53-11-02;[04] INSTALLED FWD CARGO FWD CORNER SCUFF PLATE PER AMM 53-11-02. C/W
RIGHT ELEVATOR FWD UPPER SLIDER SEAL CRACKED. / [01] REMOVED AND REPLACED R/H UPPER SLIDER SEAL PER AMM 3-31-31;[02] REMOVED AND REPLACED R/H UPPER SLIDER SEAL PER AMM 53-31-31
#2 ENGINE O/B FAN COWL HAS CRACK IN WEB ATTACHED TO 3RD STRINGER FROM AFT EDGE. (MARKED) / [01] LOCATED AND DRILLED NEW #2 ENGINE O/B FAN COWL WEB ATTACHED TO 3RD STRINGER FROM AFT EDGE PER CMM 71-13-30 AND SRM 51-40-05;[02] VERIFIED CORRECTIVE ACTION STEP #1. OK TO INSTALL;[03] INSTALLED NEW #2 ENGINE O/B FAN COWL WEB ATTACHED TO 3RD STRINGER FROM AFT EDGE PER CMM 71-13-30 AND SRM 51-40-05
CORROSION ON L/H FWD EMERGENCY EXIT DOOR CLOSEOUT PANEL KICKSTAND BRACKET / [01] BLENDED LIGHT SURFACE CORROSION PER SRM 51-10-02. REMOVED .003?OF MATERIAL. REMAINING THICKNESS .047?.;[02] VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS.;[03] REPAIRED BLENDED AREA L/H FWD EMERGENCY EXIT DOOR CLOSEOUT PANEL KICKSTAND BRAKET (P/N 411A2854-9) PER EA 22-125-01200 (TTG8Q00C0D3M) AND (TTG8Q00C4DCT);[04] REPAIRED BLENDED AREA L/H FWD EMERGENCY EXIT DOOR CLOSEOUT PANEL KICKSTAND BRACKET (P/N 411A2854-9) PER EA 22-125-01200 (TTG8Q00C0D3M) AND (TTG8Q00C4DCT). INSPECTION C/W.
CORROSION ON R/H FWD EMERGENCY EXIT DOOR CLOSEOUT PANEL KICKSTAND BRACKET / [01] BLENDED LIGHT SURFACE CORROSION PER SRM 51-10-02. REMOVED .004?OF MATERIAL. REMAINING THICKNESS .046?.;[02] VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS.;[03] REPAIRED BLENDED AREA R/H FWD EMERGENCY EXIT DOOR CLOSEOUT PANEL KICKSTAND BRAKET (P/N 411A2854-9) PER EA 22-125-01200 (TTG8Q00C0D3M) AND (TTG8Q00C4DCT);[04] REPAIRED BLENDED AREA R/H FWD EMERGENCY EXIT DOOR CLOSEOUT PANEL KICKSTAND BRACKET (P/N 411A2854-9) PER EA 22-125-01200 (TTG8Q00C0D3M) AND (TTG8Q00C4DCT).<BR>INSPECTION C/W.
NORMAL FLAP EXTENSION FROZE AT THE FLAPS 5 POSITION. LANDED FLAPS 15 USING ALTERNATE EXTENSION. ; / [01] PERFORMED TRAILING EDGE FLAP SYSTEM TEST. BITE CHECK OF FSEU SHOWED NO CURRENT FAULTS. FAULT HISTORY SHOWED NO RECORDED FAULTS. TESTS OF TRAILING EDGE FLAP SYSTEM CHECKED GOOD WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK ACCOMPLISHED IN REF TO M/M 27-51-00-730-801. - PILOT REPORTED NORMAL LANDING USING ALTERNATE FLAPS.
FWD R/H OUTSIDE EMERGENCY LT INOP ; / [01] R+R?D FWD R/H BATTERY PACK ASSY. OP?S CK GOOD. REF AMM 33-51-06
AFT R/H OUTSIDE EMERGENCY LT INOP ; / [01] R+R?D AFT R/H EMERGENCY LT BATTERY PACK AND CHARGER ASSY. OP?S CK GOOD. REF AMM 33-51-06
AFT R/H OUTSIDE EMERGENCY LT INOP ; / [01] R+R?D AFT R/H EMERGENCY LT BATTERY PACK AND CHARGER ASSY. OP?S CK GOOD. REF AMM 33-51-06
AFT L/H OUTSIDE EMERGENCY LT INOP ; / [01] R+R?D AFT L/H SIDE EMERGENCY LT BATTERY PACK ASSY. OP?S CK GOOD.REF AMM 33-51-06
FA REPORTED FWD MEGAPHONE MISSING SCREW ON HANDLE / R&R F/A FWD MEGAPHONE PER AMM 25-64-00. CKS OK.
AFT ENTRY EMERGENCY LIGHT INOP / RELAMPED AFT ENTRY EMERGENCY LIGHT IAW MM 33-51-04
FLIGHT ATTENDANT REPORTS PHOTO ILLUMINATING STRIP COMING LOOSE BETWEEN ROWS 11 AND 13 ( CAPT SIDE ) / SECURED PHOTO ILLUMINATING STRIP USING SIP
AFT GALLEY SERVICE DOOR LOWER PAN CRACKED / REMOVED AND REPLACED AFT GALLEY SERVICE DOOR LOWER PAN PER AMM 52-41-31 (INSP 74102)
LEFT WING MAIN FLAP; STRUCTURE UNDER ACCESS 553DT; INSPAR RIB; OUTBOARD OF BELLCRANK HAS AN ELONGATED PANEL ATTACH HOLE ON LOWER ROW OF FASTENERS. (MISDRILLED) / L/H MAIN FLAP I/B WAS REPLACED ON N/R Y198371.
CABIN; WHILE REPAIRING FLOOR BOARD 241FF ON NR 40638/2700/0001 FOUND ADDITIONAL DAMAGE; PUNCTURE IN UPPER SURFACE IN AREA OF FIBER DAMAGE. / REPAIRED PUNCTURE IN FLOOR PANEL 241FF IAW SRM 53-00-50-2R-2 PARA 3
AFT PIT RH Z-ANGLE IS CORRODED IN MANY AREAS FROM STATION 727D THROUGH 767; RBL 22; WL 156. / REMOVED CORROSION IAW SRM 51-10-02-0G-0 PAR 15 AND INSTALLED WITH 10X MAG GLASS. NO DEFECTS NOTED. EVALUATED MATERIAL LOSS TO BE: ORIGINAL T=.040' REMAINING =.030' LOSS= .010 LIMIT-.004'. FOUND TO BE OUT OF LIMITS IAW SRM 55-00-53-1A-2 FIG 103 DETAIL D. REMOVED DAMAGED ZEE ANGLE AFT CARGO STA 727+4' TO STA 767 IAW SRM 51-40-02-0G-0. FABRICATED NEW ZEE ANGLE IAW SRM 53-00-53-2R-5 INSTALLED NEW ZEE ANGLE IN AFT CARGO BAY STA 727+4 TO STA 767 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV C. APPLIED CIC TO TOP AND BOTTOM OF ZEE ANGLE IAW AMM 51-21-91-620-802 P/N 146A7502-14
AFT PIT LH Z-ANGLE IS CORRODED IN MANY AREAS FROM STATION 727D THROUGH 827; LBL 22 ; WL 156. / REMOVED CORROSION AT AFT PIT L/H ZEE-ANGLE FROM STA 727+4 TO 847 LBL 22 WL 156 I/A/W SRM 53-00-53-1A-2 CORROSION IS OUT-OF LIMITS; REMOVED AND INSTALLED NEW ZEE-ANGLE AT AFT CARGO L/H STA 727+4 TO STA 847 LBL 22 WL156 I/A/W SRM 51-40-02-0G-0 AND BOEING DWG# 146A7500 REV:C
AFT CARGO COMPT; FLOOR PANEL 140BF HAS APPROXIMATELY 80' SQ OF CORROSION ON UPPER SURFACE. / ACCOMPLISHED REPLACING NEW FLOOR PANEL 140BF PER W/O # 40638/1600/0003; DEFECT # Y198146.
AFT CARGO COMPT; FLOOR PANEL 140AF HAS APPROXIMATELY 30' SQ OF CORROSION ON UPPER SURFACE. / REPLACED DAMAGE (CORROSION OLD PNL II 140AF WITH A NEW FABRICATED PNL # 140AF USING 20-24-73. A TAG # A39940. APPLIED ALODINE & PRIMER. I/A/W DWG# 453A 2610-38; REV. D. AMM: 25-52-01-201-801; AMM: 51-21-41-701 PL # 453A 2010-38; REV P. EVALAUTED CORROSION ON AFT CARGO PIT FLOOR PANEL 140AF; FOUND TO BE OUT OF LIMITS; CORROSION EXCEEDS 20' IAW SRM 53-00-53-1A-1 P/N 453A2610-38
AFT CARGO COMPT; FLOOR PANEL 140CF HAS APPROXIMATELY 50' SQ OF CORROSION ON UPPER SURFACE. / FABRICATED NEW FLOOR PANEL 140CF I.A.W. SRM 51-40-05-0G-0 & BOEING DWG # 453A2610; REV: 16; EVALUATED CORROISON ON AFT CARGO FLOOR PANEL 140CF; FOUND TO BE OUT OF LIMITS; CORROSION EXTENDS 20' IAW SRM 53-00-53-1A-1 P/N 453A 2610-18
AFT CARGO COMPT; FLOOR PANEL 140BF HAS APPROXIMATELY 30' SQ OF CORROSION ON UPPER SURFACE. / FABRICATED NEW FLOOR PANEL 140BF I.A.W. SRM 51-40-05-0G-0 & BOEING DWG # 453A2610A REV: K; TY: PL
CABIN FLOOR BOARD 241BF LOWER SURFACE HAS A PUNCTURE 23' FROM FORWARD EDGE AND 0.25' FROM OUTBOARD EDGE / REPAIRED CABIN FLOOR BOARD 241 BF LOWER SURFACE PUNCTURE 23' FROM FWD EDGE AND 0.25' FROM O/B EDGE I.A.W. B737-800 SRM'S 53-00-50-2R-1 REV 69 & 53-00-50-2R-0 REV 69 (A13438) (A98115) (A89509)
CABIN FLOOR BOARD 231MF HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPAIRED CABIN FLOORBOARD 231MF FIBER DAMAGE IAW B737 SRM 53-00-50-2R-1
AFT CARGO COMPT; FLOOR PANEL 140DF HAS APPROXIMATELY 65' SQ OF CORROSION ON UPPER SURFACE. / AFT CARGO COMPT. FLOOR PANEL 140DF HAS APPROXIMATELY 65' SQ OF CORROSION ON UPPER SURFACE. DAMAGE DECLARED OUT OF LIMITS (OVER 20') IAW SRM 53-00-53-1A-1. FABRICATED NEW PANEL 140DF IAW BOEING DWG #453A2610-20 REV E AND SRM 51-40-05-0G-0. TREATED IAW AMM 51-21-41-370-802. PRIMED IAW AMM 51-21-72-370-804.
CABIN FLOOR BOARD 241FF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPAIRED UPPER SURFACE FIBER DAMAGE ON FLOOR PANEL 142FF WITH A BONDED REPAIR IAW SRM 53-00-50-2R-1 PARA 3
RH T/E FLAP FAIRING PANEL 651FB HAS A CRACKED BRACKET / REPLACED BRACKET ON R/H TIE FLAP FAIRING PANEL 651FB I.A.W SRM 51-40-02-0G ATAG A42437
FWD CARGO PIT CORROSION ON FLOOR SUPPORT AT STA 500I BETWEEN LBL 25 AND RBL 25 WL 155 / REMOVED AND REPLACED FWD CARGO PIT FLOOR SUPPORT RAIL P/N 143A9485-35 TAG #WN3190 IAW B737 SRM 51-40-02-0G-0 AND DWG 143A9481 REV:-
RH WING TRAILING EDGE; ORSS 297 - 16; 15' AFT OF REAR SPAR. LATTERAL WEB IS CRACKED IN UPPER FLANGE AT RIVET COMMON TO UPPER TRAILING EDGE PANEL / REMOVED CRACKED WEB AT R/H WING TRAILING EDGE AFT OF REAR SPAR LATTERAL WEB IA-W SRM 51-40-02-0G-0. DRILLED NEW WEB IA-W SRM 51-40-05-0G-0 AND BOEING DWG 115A2512 INSTALL NEW WEB IA-W SRM 51-40-02-0G-0 AND BOEING DWG 115A2512
FWD PIT FLOOR PANEL 120DF HAS CORROSION / EVALUATED CORROSION ON FWD PIT FLOOR PANEL 120DF FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG. 102 FABRICATED NEW FWD CARGO PIT FLOOR PANEL 120DF IAW AMM 25-52-01-201-802
FWD PIT FLOOR PANEL 120CF HAS CORROSION / REMOVED CORROSION FROM FWD CARGO PANEL # 120CF 30 INS OF CORROSION FROM R/H SIDE OF PANEL ALLOWED 20' OUT OF LIMITS I/A/W 737-800 SRM 53-00-53-1A-1 FABRICATED PANEL # 120 CF I/A/W 737 AMM 25-52-01-201-801; 737 AMM 51-21-41-370-801 AND 737 AMM 51-21-72-370-804. A TAG 39942.
FWD PIT FLOOR PANEL 120AF HAS CORROSION / EVALUATED CORROSION ON FWD PIT FLOOR PNL 120AF FOUND TO BE OUT OF LIMITS AS ACCUMULATED DAMAGE IS OVER 20' IAW SRM 53-00-53-1A-1 FIG 103; VERIFIED MAT IAW AIPC 25-52-10-17; SRM 53-30-53-01-1; AND BOEING DWG 452A1610 REV F; FABRICATED PNL 120AF IAW BOEING DWG 453A1610 REV F; TREATED AND PRIMED PNL IAW AMM 51-21-41-370-803; AND AMM 51-21-72-370-804 PN 453A 1610-14 ATAG A3941
RIGHT HAND A/C BAY EVIDENCE OF CRACK AT FASTENER ON VAPOR BARRIER ATTACH ANGLE AT STA 663 APPROX RBL 9 / TRIMMED DAMAGED VAPOR BARRUER ATTACH ANGLE OUT FROM R/H STA 663 VAPOR BARRIER; FABRICATED P/N 4064019 00001 REPAIR ANGLE ; P/N 4064019 000002 REPAIR SPLICE ANGLE; PERFORMED HFEC IN INITIAL REPAIR HOLES; AND CUT OUT EDGES (FOUND NO DEFECTS) INSTALLED -1; -2; REPAIR ANGLE; CAPS SEALED FASTENERS C/T FUEL TANK AND AFT OF VAPOR BARRIER; PERFORMED ELECTRICAL REISTANCE CHECK (FOUND IT ACCEPTABLE 0.35 MR; 0.5 MR; 0.5 MSL MAX) APPLIED C.I.C AND LEAK CHECKED REPAIR AREA (FOUND IN LEAK). I/A/W SRM: 57-10-10-2R-5; SRM- 51-40-02-0G-0; SWPM: 20-20-00; AMM: 28-11-00-400-801.
DIVERSION/DECLARED EMERGENCY, IN CRUISE FLIGHT ATTENDANTS AND PASSENGERS REPORTED STRONG ELECTRICAL BURNING ODOR. FOUND LT RECIRCULATION FAN INOP. R&R FAN PER AMM.
OVERWING EXIT SIGN KNOCKED FROM CEILING. / R&R SIGN PER MM.
L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
RT OVERHEAD BIN EMERGENCY EXIT LIGHT LOOSE AT ROW 7. SECURED LIGHT PER SIP.
L1 DOOR ESCAPE SLIDE ASSEMBLY OUT OF POSITION. R&R SLIDE ASSEMBLY PER MT.
FLAPS LOCKED OUT ON APPROACH. DIVERTED AND DECLARED AN EMERGENCY. R & R FLAPS POSITION INDICATOR IAW AMM.
FLAPS LOCKED OUT ON APPROACH. DIVERTED AND DECLARED AN EMERGENCY. R & R THE SKEW SENSOR IAW AMM.
FLAPS LOCKED OUT ON APPROACH. DIVERTED AND DECLARED EMERGENCY. R & R THE FLAPS/SLATS ELECTRONIC UNIT IAW AMM.
L2 DOOR ESCAPE SLIDE FAILED INSPECTION. R & R THE SLIDE IAW MT.
LT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 157.1 ON UPPER OUTBOARD FLANGE. REPAIRED RIB IAW EA.
LT HORIZONTAL STABILIZER VERTICAL STIFFENER BENT FLANGE AT STAB STA 157.1. REPAIRED STIFFENER IAW EA.
RIGHT HORIZONTAL STABILIZER LE CRACKED AT STATION 230. R & R LE IAW AMM.
RIGHT EMER EXIT LIGHT LOOSE AT ROW 6. REPAIRED LIGHT IAW MM.
R1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SIP.
LEFT EMERGENCY EXIT SIGN LOOSE AT ROW 15. SECURED SIGN IAW MM.