N8329B
Registered owner: UMB BANK NA TRUSTEE, UT (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
RIGHT AFT LWR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS RT AFT LWR EMERG LIGHT. (SLIDE/OVERWING) OPS CHKD GOOD. NO DEFECTS IAW AMM 33-51-04
R1 DOOR SLIDE PARTIALLY OUT OF SLIDE CONTAINER. PROVO OPENED DOOR WITH GIRT BAR NOT STOWED. REPACKED SLIDE INTO CONTAINER IAW MT 725-6106.
FWD ENTRY DOOR SLIDE GIRT BAR REQUIRES ADJUSTMENT. ADJUSTED THE GIRT BAR IAW M/T 725-61-06.
FWD ENTRY DOOR SLIDE GIRT BAR, AFT CLIP LOOSE. SECURED THE GIRT BAR AFT CLIP IAW SRM 51-40-02.
AFT SERVICE DOOR ASSIST HANDLE LOOSE ON DOOR. TIGHTENED THE BOLTS ON AFT SERVICE ASSIST DOOR HANDLE.
FWD SERVICE DOOR ASSIST HANDLE LOOSE. R & R THE LOWER NUT ON THE ASSIST HANDLE IAW AMM 52-41-31-400-802-NG.
FWD SERVICE DOOR SLIDE GIRT BAR REQUIRES ADJUSTMENT. ADJUSTED THE FWD SERVICE DOOR SLIDE GIRT BAR IAW M/T 725-61-01.
FWD MEGAPHONE DOES NOT TEST. R & R IAW AMM 25-64-00-201.
SMELL OF ELECTRICAL CIRCUIT IN CABIN NO SMELLS IN COCKPIT. SMELL WAS MID CABIN SOURCE UNKNOWN NO SMOKE JUST SMELL. BOTH ENGINE BLEEDS ON BOTH PACKS AUTO. APU OFF. FOUND LT RECIRC FAN CIRCUIT BREAKER OPEN; REMOVED AND REPLACED LT RECIRC FAN IAW AMM 21-25-02; OPS TEST GOOD; NO CABIN ODOR NOTED. PERFORMED CONDITIONAL INSPECTION FOR FUMES IN CABIN IAW AMM 05-51-56; NO DEFECTS NOTED.
FWD F/A OUTBD FLASH LIGHT INOP<[01] R&R FLASHLIGHT BATTERY PER AMM 25-64-00
CREW REPORTS MEGAPHONE INOPERATIVE. REPLACED BATTERIES PER SIP. OPS CHKD GOOD
SIDEWALL LIGHT CAPT SIDE ROW 19;20 STROBING.
LH OVERWING EXIT SIGN HAS ARROW POINTING IN WRONG DIRECTION<[01] RAR LH OVERWING EXIT SIGN IAW AMM 33-51-01. OPS CHECK GOOD NO FURTHER DEFECTS NOTED.
#1 ENGINE PYLON AFT STRUT FAIRING FWD SUPPORT IS CRACKED AT 2ND FROM UPPER FASTENER ON AIRCRAFT<[01] REMOVED AND REPLACED CRACK #1 ENGINE PYLON AFT STRUT FARING SUPPORT FITTING PER SRM 51-40-02.
#1 ENGINE AFT STRUT FAIRING FWD SUPPORT CRACKED AT 2ND FROM UPPER FASTENER<[01] REPAIRED #1 ENGINE AFT STRUT FAIRING FWD SUPPORT PER EA M-23-154-01884; SRM 51-10-02;[02] EDIT TO CHANGE STEP 3 TO 'YES'
ELECTRICAL SMELL IN COCKPIT ON TAXI IN. NOT NOTICEABLE IN CABIN. T/S REF FIM 21-00 TASK 806 RAN PACKS WITH APU AND ENGINE BLEED AIR NO SMELLS NOTED. VERIFIED OPERATION OF RECIRC FANS AND A GVI INSIDE THE PACK BAYS. NO DEFECTS NOTED AC OK FOR SERVICE.<[01] T/S REF FIM 21-00 TASK 806. RAN PACKS WITH APU AND ENGINE BLEED AIR; NO SMELLS NOTED. VERIFIED OPERATION OF RECIRC FANS AND A GVI INSIDE THE PACK BAYS. NO DEFECTS NOTED; A/C OK FOR SERVICE.
EMERGENCY EXIT BULB LIGHTS INOP ON AFT LAV LH<[01] RELAMPED AND TESTED EMERGENCY EXIT LIGHT BULBS ON AFT L/H LAV IAW AMM 33-51-01-960-801. NO DEFECTS NOTED.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
MULTIPLES EMERGENCY EXIT LIGHT BULBS INOP ON BOTH SIDE EMERGENCY EXIT DOOR INNER SIDE; (MARKED WITH RED TAPE.) MULTIPLE EMERGENCY EXIT LIGHT BULBS INOP ON BOTH SIDE EMERGENCY EXIT DOOR INNER SIDE (MARKED WITH RED TAPE.)<[01] RELAMPED FAULTY LAMPS AND TESTED OVERWING EMERGENCY EXIT DOOR INDICATOR LIGHTS PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
CRACK ON LH UPPER SIDE HORIZONTAL STABILIZER SLIDE SEAL.<[01] REMOVED AND REPLACED LH HORZ STAB UPPER FRONT SPAR SLIDING SEAL IAW AMM 53-31-31-400-802
CRACKED STR CLIP AT PAX CABIN BS727C S-7L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-7L IAW SRM 51-40-02-0G-0; AND BOEING DWG ID:0019 REV :-.;[02] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727C S-7L IAW SRM 51-40-02-0G-0; AND BOEING DWG 146A1103 ID:0019 REV :-.;[03] VERIFIED CORRECTIVE ACTION;[04] VERIFIED CORRECTIVE ACTION
THERE IS CRACK ON UPPER CHORD OF FRAME ASSEMBLY ON FED CUTOUT BETWEEN S-5L AND S-6L AT BS 312 .<[01] REPAIRED UPPER CHORD OF FRAME ASSEMBLY ON FED CUTOUT BETWEEN S-5L AND S-6L AT BS 312 PER EA M-22-153-01244.;[02] VERIFIED CORRECTIVE ACTION 1
CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] CORROSION ON FWD CARGO BAY AFT SHIELD BS500+1? TO BS500+19? RBL22 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED; REPLACED AND INSTALLED NEW SHIELD AT BS 492 TO BS 500A RBL 22 WL 156 PER SRM 51-40-02-0G-0; AND DWG 143A0080 REV: -.;[02] VERIFIED CORRECTIVE ACTION #1;[03] TASK C/W
CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4' TO BS 767 ; RBL 22 PER SRM 51-40-02 ; DWG:146A7500;ID:0213;REV:-;DWG:146A7500;ID:0216;REV:- AND DWG:146A0061;ID:0086;REV:A.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AND REPLACED SHIELD AT ACB BETWEEN BS 767 TO 787+6' ; RBL 22 ;WL 156 PER SRM 51-40-02 AND DWG:146A0081;ID:0046;REV:-;[02] VERIFIED CORRECTIVE ACTION #1
AED PANEL 834DZ AFT BRACKET IS CRACKED<[01] REMOVED AND REPLACED AED PANEL 834DZ AFT BRACKET PER SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
RT WINGLET VENTRAL STRAKE HAS CRACK AT T/E; 6' FROM BOTTOM. MARKED<
LT WINGLET VENTRAL STRAKE HAS CRACK AT T/E; 6' FROM BOTTOM. MARKED<
CRACKED FLOOR SUPPORT AT BS 391 LBL 52 WL 208<[01] REMOVED FLOOR SUPPORT AT BS 380 - BS 400 LBL 52 WL 208 PER SRM 51-40-02-0G-0 AND LOCATED AND DRILLED NEW FLOOR SUPPORT FOR BS 380 - BS 400 LBL 52 WL 208 PER DWG: 143A5400 ID: 0141 REV: - AND SRM 51-40-05-0G-0 AND REPLACED FLOOR SUPPORT AT BS 380 - BS 400 LBL 52 WL 208 PER DWG: 143A5400 ID: 0141 REV: - AND SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1
CORROSION ON ANGLE AT BS992 LBL37 AND LBL43 WL208<[01] REMOVED AND REPLACED WEB SUPPORT ANGLE BS992 LBL37 AND LBL43 WL208 I.A.W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; BOEING DWG 147A5700 REV: A
CORROSION ON PREVIOUS REPAIR ON FLOOR BEAM BS 947 LBL12; LBL23-25; LBL27.5 WL 208<[01] REMOVED AND REPLACED UPPER T-CHORD SECTION BS947 LBL3-LBL50 WL 208 I.A.W SRM 51-40-02-0G-0 AS SHOWN IN EA- 20-153-02267 WITHOUT ANY DEVIATION;[02] VERIFIED CORRECTIVE ACTION
CRACKED FLOOR SUPPORT AT BS 290 RBL 3 WL 208<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 53-00-04-1A-1 IS APPLICABLE TO THIS AIRCRAFT. PART FOUND TO BE OUT OF LIMITS PER SRM 53-00-04-1A-1. NO REPAIR REFERENCE FOR CRACK PART WILL BE REPLACED. COMPLETE MEASUREMENT TABLE. LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 353 RBL 3 WL 208. PER SRM 51-40-05 AND BOEING DWG 141A5400 REV - REMOVED FLOOR SUPPORT AT BS 290 RBL 3 WL 208 PER SRM 51-40-02. INSTALLED FLOOR SUPPORT AT BS 290 RBL 3 WL 208 PER SRM 51-40-02 AND BOEING DWG 141A5400 REV -;[02] VERIFIED CORRECTIVE ACTION 1
CRACKED FLOOR SUPPORT AT BS 323 RBL 35 WL 208<[01] REMOVED FLOOR SUPPORT AT BS 320 - BS 340 RBL 35 WL 208 PER SRM 51-40-02-0G-0 AND LOCATED AND DRILLED NEW FLOOR SUPPORT FOR BS 320 - BS 340 RBL 35 WL 208 PER DWG: 141A5400 ID: 0039 REV: - AND SRM 51-40-05-0G-0 AND REPLACED FLOOR SUPPORT AT BS 320 - BS 340 RBL 35 WL 208 PER DWG: 141A5400 ID: 0039 REV: - AND SRM 51-40-02-0G-0.;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
CRACKED FLOOR SUPPORT AT BS 353 RBL 3 WL 208<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 53-00-04-1A-1 IS APPLICABLE TO THIS AIRCRAFT. PART FOUND TO BE OUT OF LIMITS PER SRM 53-00-04-1A-1. NO REPAIR REFERENCE FOR CRACK PART WILL BE REPLACED. REMOVED FLOOR SUPPORT AT BS 353 RBL 3 WL 208. PER SRM 51-40-02.<BR><BR>REQUESTING OK TO INSTALL. COMPLETED MEASUREMENT TABLE. <BR>LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 353 RBL 3 WL 208. PER SRM 51-40-05 AND BOEING DWG 141A5400 REV - INSTALLED NEW REPLACE FLOOR SUPPORT AT BS 353 RBL 3 WL 208. PER SRM 51-40-02 AND BOEING DWG 141A5400 REV -;[02] VERIFIED CORRECTIVE ACTION 1
CRACKED FLOOR SUPPORT AT BS 353 RBL 15 WL 208<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 53-00-04-1A-1 IS APPLICABLE TO THIS AIRCRAFT. PART FOUND TO BE OUT OF LIMITS PER SRM 53-00-04-1A-1. NO REPAIR REFERENCE FOR CRACK PART WILL BE REPLACED. COMPLETE MEASUREMENT TABLE. REMOVED FLOOR SUPPORT AT BS 353 RBL 15 WL 208 PER SRM 51-40-02.<BR><BR>REQUESTING OK TO INSTALL. LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 353 RBL 15 WL 208 PER SRM 51-40-05 AND BOEING DWG 141A5400 REV - INSTALLED NEW FLOOR SUPPORT AT BS 353 RBL 15 WL 208.<BR> PER SRM 51-40-02 AND BOEING DWG 141A5400 REV -;[02] VERIFIED CORRECTIVE ACTION 1
CRACKED FLOOR SUPPORT AT BS 393 RBL 3 WL 208 CRACKED FLOOR SUPPORT BETWEEN BS 380-400 BL 0 WL 208.<[01] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 393 RBL 3 WL 208 IAW SRM 53-00-04-1A-1; SRM 51-40-05; BOEING DWG# 143A5400 REV:-; SRM 51-40-02;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
CRACKED FLOOR SUPPORT AT BS 393 RBL 8.283 WL 208 CRACKED FLOOR SUPPORT BETWEEN BS 380-400 RBL 8.283 WL 208<[01] STEP 3 RBL DOES NOT MATCH THE SIGNOFFS AND THERE IS NO OVERALL CORRECTIVE ACTION.;[02] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 393 RBL 13 WL 208 IAW SRM 51-40-05; BOEING DWG#143A5400 REV:-; SRM 51-40-02; SRM 53-00-04-1A-1;[03] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 380-400 RBL 8.283 WL 208 IAW SRM 51-40-05; BOEING DWG#143A5400 REV:-; SRM 51-40-02; SRM 53-00-04-1A-1;[04] CORRECTED RBL LOCATIONS ON STEPS;[05] VERIFIED CORRECTIVE ACTION 3
CRACKED FLOOR SUPPORT AT BS 391 RBL 42 WL 208<[01] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 391 RBL 42 WL 208 IAW SRM 51-40-02; SRM 51-40-05; BOEING DWG#143A5400 REV:-;[02] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 391 RBL 42 WL 208 IAW SRM 51-40-02; SRM 51-40-05; BOEING DWG#143A5400 REV:-; SRM 53-00-04-1A-1;[03] VERIFIED CORRECTIVE ACTION
CRACKED FLOOR SUPPORT AT BS 393 LBL 16 WL 208 CRACKED FLOOR SUPPORT BETWEEN BS 380-400 LBL13.24 WL 208.<[01] REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT BS 393 LBL 16 WL 208 IAW 51-40-05; BOEING DWG# 143A5400 REV:-; SRM 51-40-02; SRM 53-00-04-1A-1;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
PANEL 193D OUTER SKIN HAS AREAS OF DISBONDS. (MARKED)<[01] PANEL 193D OUTER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 51-70-05-2R-2-B00319 (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE - AIRFRAME - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
CRACK ON BRACKET UPPER SIDE OF RH MLG AFT TRUNNION (MARKED WITH RED TAPE.)<[01] REMOVED AND REPLACED BRACKET ON UPPER SIDE OF R/H MLG AFT TRUNNION IAW SRM 51-40-02-0G-0 PARA. 7.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
CRACKED PREVIOUS REPAIR VAPOR BARRIER BS 663 RBL 25 TO RBL 40 (MARKED)<[01] CRACKED PREVIOUS REPAIR VAPOR BARRIER; BS 663 RBL 25 TO RBL 40; WAS REMOVED AND REPLACED WITH A NEW REPAIR IAW SRM 51-70-04-2R-10.;[02] JOB COMPLETE.
L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
MULTIPLE AFT R/H EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED R/H AFT EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06. OPS CHECK GOOD
ON SHORT FINAL 400 POPPING NOISE HEARD & SLIGHT REDUCTION N1 #2 ENGINE. FLAMES OBSERVED BY TOWER & PAX. NO FIRE OR SMOKE INDICATION. PERFORMED INSPECTIONS OF NR 2 ENGINE AFTER ENGINE STALL PER FIM 71-05-00-810-805. PERFORMED HP COMPRESSOR BLADES BORESCOPE INSPECTION IAW AMM 72-00-00-200-804-F00. FOUND SEVERE DAMAGE TO ALL ROTOR & STATOR BLADES R&R NR 2 ENGINE PER MT 771-00-01-ETOPS REF: TTG8Q00SH3V7.
NOSE WHEEL STEERING PULLS HARD LEFT ON TAKE OFF SLOW SPEED ABORT APROX 60KTS<[01] TROUBLESHOT ISSUE OF AIRCRAFT PULLING TO THE LEFT. FOUND #1 BRAKE WITH A LEAK AND ALL BRAKE PISTONS WERE NOT OPERATING PROPERLY. R&R #1 BRAKE. OPS AND LEAK CHECKS GOOD PER AMM 32-41-41 AND FIM 32-51-00-810
FA REPORTS FWD GALLEY MEGAPHONE INOP<[01] REMOVED AND REPLACED FWD GALLEY MEGAPHONE IAW AMM 25-64-00.
LEFT OVER WING EXIT INTERIOR EMERGENCY LIGHTS INOP<[01] R&R EMERGENCY LIGHT BATTERY PACK FOR LEFT OVER WING EXIT INTERIOR EMERGENCY LIGHTS PER AMM 33-51-06. OPS CHECK GOOD.
FWD RIGHT ESCAPE SLIDE LIGHT INOP<[01] REPLACED M2816 BATTERY PACK PER AMM 33-51-06
EMERGENCY EXIT SIGN MISSING ROW 10F<[01] IMSTALLED R/H FWD OVERWING EXIT EMERGENCY EXIT LENS IAW SIP
AFT L/H OVERWING EXIT EMERGENCY LIGHT COVER MISSING.<[01] REPLACED COVER IAW SIP
L1 DOOR SLIDE FELL ONTO JETWAY UP ARRIVAL- NO DEPLOYMENT. / [01] INSPECTED FWD ENTRY DOOR; DOOR SLIDE AND DOOR SLIDE COVER. NO DEFAULTS NOTED. REPACKED DOOR SLIDE INTO SLIDE COVER AND INSTALLED ASSEMBLY ONTO FWD ENTRY DOOR. REF AMM 25-66-01 SLIDE PACK INSTALLATION UNSCHEDULED.
MAIN CABIN OVERHEAD EMERGENCY EXIT LIGHTS AND EXIT SIGN INOPS. R & R THE BATTERY PACKS IAW AMM 33-51-06. OPS CHECKED GOOD.
R/H RAM AIR INLET FWD LIP PANEL 191HR HAS SEVERAL ELONGATED HOLES (MARKED) R/H RAM AIR INLET FWD LIP PANEL 191HR HAS SEVERAL ELONGATED HOLES / [01] P/N 149A7160-8 S/N BN 178429 ORDERED ON TASK CARD TTG8Q00G25X9;[02] REMOVED AND REPLACED R/H RAM AIR INLET FWD LIP PANEL 191HR PER AMM 53-51-21.;[03] INSPECTED
BRACKET FOUND TO BE CRACKED ON PANEL 651FB ( MARKED ) FORWARD SIDE I/B OF PANEL 651DB. / [01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02.;[02] REMOVED AND REPLACED BRACKET PER SRM 51-40-02.<BR>INSPECTION C/W.
L/H WING O/B AFT FLAP INBD EDGE LOWER SURFACE DELAMINATED . / [01] REMOVED FOR FOM IN ACCORDANCE WITH AMM 27-51-22.;[02] REMOVED AND REPLACED O/B AFT FLAP IAW AMM 27-21-22.;[03] GAVE OK TO INSTALL LH OTBD AFT FLAP. VERIFIED THE INSTALLATION OF OF AFT FLAP<BR> IAW AMM 27-21-22. NO FAULT NOTED. (RII);[04] INFO: PARTS DATA FOR THIS LH OUTBD AFT FLAP IS ON FAULT ID TTG8R00894WF. MPN OFF 113A3700-25; MSN OFF 003964; MPN ON 113A3700-19; MSN ON 001103. CANNOT MOVE PARTS DATA TO THIS CARD SINCE IT WAS ALREADY PROCESSED ON THE OTHER CARD.;[05] CLEARANCE AND OPS CK GOOD PER MM 27-51-22.;[06] VERIFIED WORK PERFORMED IN C/A #5 (RII)
PASS CABIN FLOOR SUPPORT CRACKED AT STA 540; RBL1 (MARKED) / [01] STA. 540 LBL 1 FLOORBOARD PANEL HOLES LOCATED PER SRM 51-40-02.
PASS CABIN FLOOR SUPPORT CRACKED AT STA 540; LBL1 (MARKED) / [01] STA. 540 LBL 1 FLOORBOARD PANEL HOLES LOCATED PER SRM 51-40-02.
L/H OUTBOARD WING BENEATH PANEL 521ABB; COUNTERBALANCE WEIGHT CORRODED AND MISSING PROTECTIVE FINISH. / [01] REMOVED AND REINSTALL BALLAST WEIGHTS PER M/M 57-44-02 AND GENERAL EA;[02] COMPLIED WITH INSPECTION OF THE REMOVED AND REINSTALL BALLAST WEIGHTS PER M/M 57-44-02 AND GENERAL EA
-RIGHT WING UPPER T\E SHELF PNL O\B OF #7 SPOILER VERTICAL WEB CRACKED WHERE IT CONNECTS TO DEFLECTOR RIB. / [01] R&R RIGHT WING UPPER T\E SHELF PN VERTICAL WEB O\B OF #7 SPOILER REF SRM 51-40-02 AND SRM 51-10-02.
AISLE CEILING-EMERGENCY LIGHT LENS COVER MISSING ROW 17. / [01] REPLACED AISLE CEILING LENS AT ROW 17 EMERGENCY. IAW AMM 33-51-00. OP?S CHECKED GOOD.
R/H OVERWING EMERGENCY LIGHTS SINGS INOP. / [01] R+R R/H OVERWING SIGNS BATTERY PACK PER AMM 33-51-06. OPS CK GOOD.
FWD OVERHEAD #1 EMERGENCY STRONGBACK LIGHT ASSY MISSING LENS. / [01] REPLACED O/H #1 STRONGBACK EMERGENCY LIGHT LENS REF. AMM 33-51-03.
FOUND CRACK ON VAPOR BARRIER AT R/H WHEEL WELL FORWARD TO HYD RETURN FILTER BETWEEN RBL 31 AND RBL 45 SIX INCHES IN LENGTH.DAMAGE IS ALLOWABLE PER SRM 5710101A2. APPLIED ALUMINUM FOIL TAPE TO AREA OF CRACK. DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY REPETITIVE INSPECTION REQUIRED.
FOUND CRACK ON VAPOR BARRIER AT RH WHEEL WELL FORWARD TO HYD RETURN FILTER BETWEEN RBL 31 AND RBL 45 SIX INCHES IN LENGTH.DAMAGE IS ALLOWABLE PER SRM 5710101A2. APPLIED ALUMINUM FOIL TAPE TO AREA OF CRACK. DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY REPETITIVE INSPECTION REQUIRED. A) REPETITIVE ACTION REQUIRED COMPLIED WITH; NO ADDITIONAL DAMAGE OR DETERIORATION NOTED. OK TO CONTINUE SERVICE IN ACCORDANCE WITH REFERENCE SRM 5710101A2.
DURING PDSC FOUND CAB EMERGENCY LIGHT CB OPEN. CONTRCAT AMT: 3413604. RESET EMERGENCY LIGHT C/B. ALL OPERATIONS CHECK NORMAL, PER AMM 33-51-00, NO DEFECTS FOUND AT THIS TIME. OK FOR SERVICE. CNTRCT AMT: 3413604.
CENTER WING ROAR SPAR VAPOR WEB HAS A 10' DIAGONAL CRACK THAT EXTENDS FROM RBL 30.83 TO RBL .35. THE CRACK EXTENDS UNDER STIFFENOR AT REL 31.83. THIS IS THE LOWER RIGHT WEB (GFRP). REPAIRED PER SRN 57-10-10-2R-2.
FWD CARGO CENTER THRESHOLD BULLNOSE IS DAMAGED / REMOVED AND REPLACED FWD CARGO CENTER THRESHOLD BULLNOSE IAW MM 53-11-02 AND TASK CARD 753-140-00-01Y
AISLE EMERGENCY LIGHTS OF LEFT EMERGENCY EXITS INOPERABLE. REMOVED AND REPLACED BATTERY PACK AT 727L, PER MM 33-51-06. EMERGENCY LIGHTS OPERATIONS CHECKED GOOD, PER MM 33-51-00 P/N OFF D717-01-100 S/N OFF 217814P/N ON D717-01-100SWA S/N ON 29984.
FUSLEAGE SKIN STA 282 BETWEEN STR 1L AND 2L HAS DAMAGE FROM FWD LAV DOOR HINGE PIN MIGRATION, AREA PEVIOUSLY BLENDED 15 TOO DEEP. DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE INSTALLED FASTENER. ALL INSPECTIONS AND WORK ACCOMPLISHED, IAW SRM 53-00-01-2R-38. SEE SA-M 326: A1303913.
CORROSION ON ANGLE AT FLOOR STA 986.5 + 6 RBL 32. REMOVED AND REPLACED FLOOR SUPPORT ANGLE WITH NEW ANGLE AT STATION 986.5 + 6 RBL 32, IAW SRM 51-40-02.
INTERCOSTAL / BAFFLE CRACKED AT STATION 500E TO 500F UNDER RIGHT HAND TRANSITION ANGLE / REMOVED AND REPLACED INTERCOSTAL/BAFFLE FROM STA. 500E TO STA. 500F UNDER R/H TRANSITION ANGLE @ RBL 22' PER SRM 51-40-02
THE R/H TRANSITION ANGLE HAS CORROSION FROM STA 787-767 / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 767-787 PER SRM 51-40-02
THE LT TRANSITION ANGLE IN THE AFT CARGO PIT HAS CORROSION FROM STA 817 TO 727J. REMOVED AND REPLACED SECTION OF LT TRANSITION ANGLE IN AFT CARGO FROM STA 727H + 10' TO STA 807 +10' LBL 21', PER SRM 53-00-53-2R-5. SEE SA-M 326; S/N 1200891 FOR INDIVIDUAL WORK ACCOMPLISHMENT.
AFT CARGO FLOOR PANEL 140CF HAS LIGHT CORROSION ON FLOOR PANEL AROUND DOOR CUT OUT. / FABRICATED AFT CARGO FLOOR PANEL 140CF PER AMM 25-52-01 AND BOEING DRAWING 453A2610-18
RH FWD SKATE ANGLE IS WOEN OUT OF LIMITS / REMOVED AND REPLACED DAMAGED SKATE ANGLE PER SRM 51-40-02; RESTORED INTERIOR FINISH PER AMM 51-21-99.
THE RIGHT HAND TRANSITION ANGLE IN THE AFT CARGO PIT HAS CORROSION FROM STA 767 TO 727H / REMOVED PART; FABRICATED AND INSTALLED AFT CARGO R/H TRANSITION ANGLE FROM 727H TO 767 PER SRM 53-00-53-2R-5. INSTALLED AND PUSH TESTED NUTPLATES PER SRM 51-40-10.(SA-M 326 ATTACHED: A1303910)
FORWARD CARGO RIGHT SIDE TRANSITION HAS CORROSION FIS 500C + 500E / REPAIRED FWD CARGO R/H TRANSITION ANGLE STA 500C TO STA 500E IAW SRM 53-00-53-2R-5
FLIGHT DECK DOOR POST FLOOR ATTACH ANGLE ON R/H SIDE HAS 2 EA ELONGATED HOLES / 2EA ELONGATED FLOOR BOARD ATTACH HOLES AT FLIGHT DECK DOOR POST BS 273- BS 276; RBL 10 FOUND OUT OF LIMITS PER SRM 53-10-51-1A-1 REPAIRED DAMAGEDD HOLES IAW EA 20-153-02298
FWD CARGO CENTER THRESHOLD WEB CORRODED IN SEVERAL AREAS. / DAMAGE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. REPLACED WEB PER SRM 51-40-02. (SA-M 326 A1200878)
MAIN CABIN STA 344-360 LBL 12' INTERCOSTAL CRACKED,AREA MARKED. REMOVED AND REPLACED INTERCOASTAL AT STA 344-360 LBL 12, IAW SRM 51-40-02. SEE SAM FORM A1200877 FOR INDIVIDUAL SIGNOFFS OF WORK PERFORMED. (SA-M 326 A1200877)
CORROSION ON INTERCOSTAL BS 947+4 LBL 47. REMOVED DAMAGED INTERCOASTAL, PER SRM 51-40-02. DRILLED UP REPLACEMENT INTERCOASTAL, PER SRM 51-40-05. INSTALLED NEW REPLACEMENT INTERCOASTAL (P/N 147A5676-5), PER SRM 51-40-02.
CORROSION ON INTERCOASTAL BS 947& 4 LBL 31 AT FASTENER HOLE (UNDERSIDE). REMOVED DAMAGED INTERCOASTAL, PER SRM 51-40-02. DRILLED UP REPLACEMENT INTERCOASTAL, PER SRM 51-40-05. INSTALLED NEW REPLACEMENT INTERCOASTAL (P/N 147A5676-5) PER SRM 51-40-02.
MAIN CABIN STA 312-328 LBL 47' INTERCOSTAL CRACKED, AREA MARKED. R & R INTERCOSTAL IAW SRM 51-40-02.
CORROSION ON FLOOR BEAM BS 947 LBL 23+26 INBOARD &OUTBOARD SIDE OF MOUNT. REPAIRED FLOOR BEAM, PER SRM 53-70-51-2R-5 & EA 20-153-02267. SEE INDIVIDUAL SIGN OFFS FOR ALL WORK ACCOMPLISHED. SEE ALSO N/R 176708.
CORROSION ON FLOOR BEAM BS 947 RBL 50 BY LAV MOUNT. REMOVED CORROSION IAW EA 0-153-02269.
FWD GALLEY DOOR CUTOUT 2-ANGLE HAS CORROSION. BLENDED AREA ON FWD GALLEY DOOR CUTOUT Z-ANGLE. REMOVED .025' OF .090' FOUND OUT OF LIMITS, PER SRM 53-10-15-1A-2. REMOVED AND REPLACED ANGLE P/N 141A8312-5, IAW SRM 51-40-02. SEE SAM FORM A1200873 FOR INDIVIDUAL SIGN OFFS OF WORK PERFORMED.
FWD ENTRY DOOR GRIT BAR MOUNTS DAMAGED AT FASTENER HOLES FWD & AFT STA 312 AND 344. REMOVED & REPLACED FWD ENTRY DOOR GRIT BAR MOUNTS FWD & AFT, PER SOPM 25-50-01.
CORROSION ON L ANGLE BS 986.5 + 7 RBL 36 / REPLACED ANGLE PER SRM 51-40-02; SEE INDIVIDUAL SIGNOFFS FOR ALL WORK ACCOMPLISHED. (SA-M 326 A1200889)
CORROSION IN FASTENER HOLF FLOOR BEAM BS 947 LBL 53 (UNDERSIDE) / REMOVED CORROSION FROM NUT PLATE HOLE IAW SRM 51-10-02. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-5 & EA 20-153-00267. SEE INDIVIDUAL SIGN OFFS FOR ALL WORK ACCOMPLISHED. SEE ALSO N/R 176705SA-M 326 A1200876INSP D122
EMERGENCY EXIT LIGHT CENTER CABIN CEILING FWD LENS FELL OFF. R&R OVERWING EMERGENCY EXIT LIGHT ASSY, IAW MM 33-51-01.
LT AISLE EMERGENCY EXIT LIGHTS FROM ROW 4 TO 12 AND THE FWD EXTERIOR LT OVERWING EXIT LIGHT ARE INOP. REMOVED AND REPLACED M 2335 BATTERY PACK, IAW AMM 33-51-06.
EXIT SIGN INSTALLED IN CEILING AT MID-CABIN HAS BECOME LOOSE. RESECURED LIGHT ASSY, PER AMM 33-51-01.
FWD RH EXTERIOR EMERGENCY OVERWING EXIT LIGHT INOP. / REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1676 PER AMM 33-51-06. ALL ASSOCIATED LIGHTS OPS CHECK OK.
BAT DISCHARGE LIGHT ILLUMINATED. 'BAT' DISPLAYED ALTERNATING -1;-2;-7;+3;+5 DC AMPS 'ALT BAT' NORMAL / R+R BATT. CHARGER PER AMM 24-31-21 R&R MAIN BATT. PER AMM 24-31-11 OPS CHECK NORMAL BATT. DISCHARGE LT REMAINS EXTINGUISHED DC AMPS NORMAL PER AMM 24-31-21 ISSUE# 2842760 BATTERY CHARGER ISSUE# 2842770 BATTERY POS: 1 TAG# 939201 PN: 024147-000 SN OFF: 09052001BFD58 SN ON: 0905200217C64 POS: 1 TAG# 627115 PN: 8-930-03 SN OFF: C10579 SN ON: C3296
MID CABIN FORWARD FACING OVERHEAD EXIT SIGN MISSING. / INSTALLED LENS IAW MM.
AFT GALLEY SERVICE DOOR ESCAPE SLIDE IS NOT PACKED PROPERLY. / REPACKED AFT GALLEY SERVICE DOOR SLIDE PER WORK INSTRUCTION NO. 725-61-06.
FORWARD LIFE RAFT EGRESS LIGHT LENS WAS NOT SECURED. / SECURED LENS PER AMM.
L2 DOOR OUTSIDE EMERGENCY LIGHT INOP. / R&R LAMP PER AMM.
ON TAKEOFF ROLL WITH AUTO THROTTLE ENGAGED HAD A LARGE SPLIT IN THRUST LEVER AND N1 SETTINGS. R&R FUEL PUMP PER MT.
AFT CABIN EMERGENCY LIGHTS INOP AT LOCATION M1673. R&R BATTERY PACK IAW AMM.
FWD CARGO COMPARTMENT LOWER BULKHEAD ANGLE IS CORRODED AT BS 500I LBL 21 - RBL 21 / REMOVED DAMAGE ON FWD CARGO COMPARTMENT LOWER BULKHEAD ANGLE AT STA 500I LBL21- RBL21. ORIGINAL 'T' .071' REMAINING .050' LOSS OF .021' OUT OF LIMITS. REMOVED + REPLACED LOWER BULKHEAD ANGLE IAW SRM 51-40-02-0G-0 + DWG 143A9485 SHT 11 REV B ATAG:WN5257
FORWARD CARGO COMPARTMENT LOWER BULKHEAD ANGLE CORRODED AT BS 500I, BETWEEN LBL 21 TO RBL 21. REPAIRED ANGLE IAW SRM AND DWG.
PASS CABIN; FLOOR PANEL 232FF; UPPER FACE SHEET HAS MISSING FIBERS ON O/B AND I/B EDGE FROM FWD EDGE OF PANEL EXTEDING AFT 36' / REPAIRED AREA'S WITH DENTS ON UPPER SUFACE AS MARKED ON PANEL 242AF. IAW 737-800 SRM 53-00-50-2R-1 REPAIR 1; SRM 53-00-50-2R-0 REPAIR GENERAL
PASS CABIN; FLOOR PANEL 241AF; UPPER FACE SHEET HAS LARGE AREAS OF MISSING FIBERS / EVALUATED PASS. CABIN FLOOR PANEL #241AF; FOUND MORE THAN 2 PLIES GONE ON UPPER SURFACE FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-50-1A-1; STEPS 4B. MATERIAL VERIFIED FOR FABRICATION AS PN #BMX 4-23 TYPE II IAW B737 SRM 53-00-50-01-1; FABRICATED FLOOR PANEL REPLACEMENT #241AF IAW B737-800 SRM 53-00-50-2R-0; REPAIR GENERAL; AND DWG #144A5810-127.
PASS CABIN; FLOOR PANEL 241DF; UPPER FACE SHEET HAS LARGE AREAS OF MISSING FIBERS / FABRICATED NEW FLOOR PANEL 241DF DUE TO EXTENT OF DAMAGE ON EXISTING PANEL IAW SRM 53-00-50-2R-0 REV 65; DWG 144A5810-128; + BAC5085 REV E.
AFT CARGO COMPARTMENT THRESHOLD FWD TIE DOWN PLATE IS CORRODED / REPLACED AFT CARGO COMPARTMENT THRESHOLD FWD TIE DOWN; P/N: 453A2611-1 IAW B737 IPC: 25-52-10-04 AND SRM 51-10-02-0G-0. PARAGRAPH 9C.ATAG: A45860
AFT CARGO COMPARTMENT THRESHOLD AFT TIE DOWN PLATE IS CORRODED / REPLACED AFT CARGO COMPARTMEMT THRESHOLD AFT TIE DOWN; P/N: 453A2611-2 IAW B737 IPC 25-52-10-04 AND SRM 51-10-02-0G-0; PARAGARPH 9C. ISSUE TAG: A85826
AFT CARGO FLOOR PANEL 140DF UPPER SURFACE L/H EDGE HAS VARIOUS SPOTS OF CORROSION. / ORIGINAL PANEL WORN BEYOND LIMITS REPLACED PANEL P/N 453A2610-20 ATAG: WN9347 AS REQUIRED. I.A.W. SRM 53-00-53-1A-1/ AIPC 25-52-10-19
FORWARD CARGO COMPARTMENT FLOOR PANEL 120AF IS CORRODED ON EDGES / VERIFIED FWD CARGO COMPARTMENT FLOOR PANEL 120AF P/N 453A1610-14 S/I 7253765 IAW IPC 25-52-10-17; LIMIT FOUND TO BE OUT OF LIMIT WITH OVER 3 INCH IAW SRM 53-00-53-1-A1 ATG# WN9822
AFT CARGO COMPARTMENT; RH SIDE CAP STRIPS HAVE MULTIPLE AREAS OF CORROSION. (ON AFT PIT PANEL CART) / AFT CARGO R/H SIDE CAP STRIPS HAS CORROSION. REPLACED R/H SIDE AFT CARGO CAP STRIPS WITH NEW STRIPS P/N 453A2611-17; P/N 453A2611-19; P/N 453A2611-11; P/N 453A2611-3 STA 727TH TO STA 947.5 IAW BOEING DWG 453A2600 REV A.
AFT CARGO COMPARTMENT; LH SIDE CAP STRIPS HAVE MULTIPLE AREAS OF CORROSION. (ON AFT PIT PANEL CART) / AFT CARGO L/H SIDE CAP STRIPS HAVE AREAS OF CORROSION; REPLACED WITH NEW L/H SIDE CAP STRIPS P/N 453A2611-6 A-TAG#A44975; P/N 453A2611-10 A-TAG# A44992; P/N 453A2611-18 A-TAG# WN9073; P/N 453A2611-4 A TAG #ZF0038; 453A2611-16 A-TAG# WN9069 IAW BOEING DWG #453A2600 REV: A
FORWARD CARGO COMPARTMENT FLOOR PANEL 120BF IS CORRODED ON EDGES / VERIFED FORWARD CARGO COMPARTMENT FLOOR PANEL 120BF P/N 453A1610-16 SI 4250146 IAW IPC 25-52-1-17; LIMIT FOUND TO BE OUT WITH OVER 3 INCH OVER IAW SRM 53-00-53-1A-1 ATAG# WN0802
FORWARD CARGO COMPARTMENT FLOOR PANEL 120CF IS CORRODED ON EDGES / VERIFIED FORWARD CARGO COMPARTMENT FLOOR PANEL 120CF P/N 453A1610-103 S/I 4251047 IAW IPCC. 25-52-10-17 LIMIT FOUND TO BE OUT OF LIMIT WITH OVER 3 INCH IAW SRM 53-00-53-1A-1 A TAG #WN0483
FORWARD CARGO FLOOR PANEL 120DF IS CORRODED ON EDGES / VERIFIED NEW FORWARD CARGO FLOOR PANEL 120DF P/N 453A1610-20 S/I 4251048 IAW IPC 25-52-10-17; LIMIT FOUND TO BE OUT WITH 3 INCH OVER IAW SRM 53-00-53-1A-1 ATAG WN9991
AFT CARGO FLOOR PANEL 140CF HAS VARIOUS SPOTS OF CORROSION ON THE L/H EDGE FROM FRONT TO BACK. / REPLACED AFT CARGO FLOOR PANEL 140CF P/N: 453A2610-18 IAW B737 SRM 53-00-53-1A-1 AND SRM 51-10-02-0G-0.
AFT CARGO FLOOR PANEL 140BF UPPER SURFACE R/H EDGE HAS VARIOUS AREAS OF CORROSION. / REPLACED AFT CARGO FLOOR PANEL 140BF P/N: 453A2610-32 IAW B737-800 SRM 53-00-53-1-1 AND SRM 51-10-02-0G-0 ATAG: WN0739
AFT CARGO FLOOR PANEL 140AF UPPER SURFACE L/H EDGE HAS VARIOUS AREAS OF CORROSION. / CORROSION ON AFT CARGO FLOOR PANEL 140AF EXCEEDS MORE THAN 3.0' IN LENGTH FOUND TO BE OUT OF LIMITS VERIFIED NEW MATERIAL FOR FLOOR PANEL FABRICATED NEW FLOOR PANEL 140AF ALODINED + PRIMED IAW SRM 53-00-53-1A-1 + IPC 25-52-10-19 + BOEING DWG# 453A2610 REV K + BOEING DWG# 453A2610 REV R + AMM 51-21-41-370-803 + 51-21-72-370-804
AFT CARGO FLOOR PANEL 140EF L/H AND R/H EDGE HAS VARIOUS SPOTS OF CORROSION. / FOUND CORROSION ON AFT CARGO FLOOR PANEL 140EF TO BE OUT OF LIMITS ONE TO MORE 3' IAW B737-800 SRM 53-00-53-1A-1. FABRICATED NEW PANEL 140EF PN 453A2610-58 IAW B737 SRM 51-40-05 & DWG 453A2600 REV B.
PASSENGER CABIN FLOOR BOARD # 241BF TOP SKIN SURFACE L/H/S 37' FROM FWD CORNER EDGE COMPOSITE SKIN FIBERS DAMAGED / REPAIRED AREA OF FRAYED FIBERS ON UPPER SURFACE OF PANEL 241BF IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1; SRM 53-00-50-2R-0 REPAIR GENERAL (A26432) (A84141)
PASSENGER CABIN FLOOR BOARD # 242AF TOP SKIN SURFACE 37' FROM AFT CORNER EDGE OF BOARD AND 3' INBD FROM R/H EDGE HAS LARGE DENTS AS MARKED / REPAIRED AREA'S WITH DENTS ON UPPER SUFACE AS MARKED ON PANEL 242AF. IAW 737-800 SRM 53-00-50-2R-1 REPAIR 1; SRM 53-00-50-2R-0 REPAIR GENERAL
LEFT MAIN WHEEL WELL VAPOR BARRIER STA 663 IS CRACKED / REPAIRED L/H MAIN WHEEL WELL VAPOR BARRIER WEB IAW SRM 51-70-04-2R-10 STEP 4.
LT MAIN WHEEL WELL VAPOR BARRIER WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM.
R1 INTERIOR EXIT LIGHTS INOP. R&R BATTERY IAW MM.
R1 EXTERIOR EXIT LIGHTS INOP. R&R BATTERY IAW MM.
AFT ENTRY EMERGENCY LIGHTS INOP. R&R BATTERY PACK IAW AMM.
EMERGENCY EXIT LIGHT COVER MISSING AT ROW 15. INSTALLED COVER IAW AMM.
LT EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED BETWEEN ROW 8 TO ROW 15. R&R LENS IAW AMM.
LT PHOTOLUMINESCENT EMERGENCY EXIT LIGHT STRIP DAMAGED. R&R STRIP IAW AMM.
RT PHOTOLUMINESCENT EMERGENCY EXIT LIGHT STRIP DAMAGED. R&R STRIP IAW AMM.
OVERWING EMERGENCY EXIT SIGN MISSING THE LENS. INSTALLED THE LENS IAW MM.
RT WING NR 8 SLAT OUT OF ADJUST. R&R NR 8 SLAT IAW AMM.
ACCOMPLISH TAP TEST OF THE DAMAGED AREA BOUNDARY AND 5 INCHES BEYOND IN THE OUTBOARD DIRECTION FOR ANY FURTHER DISBOND. / REMOVED AND REPLACED LH OB AFT FLAP REF AMM 27-51-22. REF REPAIR-57EA-04563 AND NRC D287528.
#8 SLAT DELAMINATIED ON LOWER SURFACE OF T/E WEDGE OTBD CORNER. DELAMINATION MEASURES 2.5' X 3.5' AND IS LOCATED 3.5' FROM T/E / COMPLIED WITH REPAIR-57EA-04561. REFERENCE INSP-57EA-04564 AND REPAIR-57EA-04565 FOR REPEAT AND PERMANENT REPAIR.
L/H WING O/B T/E AFT FLAP I/B END LOWER T/E WEDGE SKIN DELAMINATED 1' FROM T/E AND 1' FROM I/B END. DELAMP MEASURES 9' X 8' / COMPLIED WITH REPAIR-57EA-04560 REFERENCE INSP-57EA-04562 AND REPAIR-57EA-04563 FOR REPEAT AND PERMANENT REPAIR
LT WING OUTBOARD TRAILING EDGE AFT FLAP INBOARD END LOWER TRAILING EDGE WEDGE SKIN DELAMINATED. REPAIRED AFT FLAP SRM.
DELAMINATION ON THE #8 SLAT AND ON THE L/H O/B AFT FLAP / C/W EA FOR TEMP REPAIR.
AFT LT OVERHEAD BIN EMERGENCY LIGHT LENS CRACKED. R&R LENS PER AMM.
LEFT EMERGENCY EXIT ROW EXIT SIGN FELL OFF. REPLACED THE SIGN ASSEMBLY IAW MM.
AISLE OVERWING EMER EXIT SIGN, FWD MOUNT COVER MISSING. INSTALLED COVER IAW SIP.
FORWARD CTR CABIN EMER EXIT SIGN, FASTENER COVER PLATE MISSING. INSTALLED COVER IAW MM.
R1 LOWER EMER EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.
L1 DOOR EMER EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK IAW SIP.
R1 DOOR EXIT SIGN LOOSE. R & R SIGN IAW MM.
LEFT MLG WW FIBERGLASS VAPOR BARRIER CRACKED OTBD OF A SYSTEM HYD RETURN FILTER BS 663, LBL 35. REPAIRED BARRIER IAW EA.
OVERWING "EXIT" SIGN LOOSE FROM CEILING MOUNT. RE-INSTALLED SIGN PER M/M.