N924WN
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
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
NR 2 ENGINE COMPRESSOR STALL AT FL370 IN CLIMB. THROTTLE MOVEMENT AND LIGHT TURBULENCE PRECEDED STALL. CLEARED WITHIN 15-20 SECONDS. RAN NORMALLY AFTERWARDS. WORKED ENGINE STALL/SURGE FIM 71-05 TASK 805 THROUGH STEP E. 2. R & R NR 2 ENGINE IAW M/T 771-00-00.
R1 SLIDE FELL OUT OF CASING. CW MT 725-61-06.
LOWER EXIT SIGN OF RIGHT OVER WING EXIT DOOR BROKE OFF<[01] R AND R ASSY PER AMM 33-51-01 OPS CHECK GOOD
LEFT WING BODY OVERHEAT LIGHT ILLUMINATED PASSING FL260 ON CLIMBOUT<[01] INSPECTED FOR LEAKS; NONE FOUND. OK TO CONTINUE PER MEL 26-12-01 SP1 AUTH# 311416.;[02] TROUBLESHOT AND FOUND WIGGINS CLAMP FROM NGS HEAT EXCHANGER MISSING. FOUND ASM INSULATION BURNED AND MISSING FROM ASM. SUSPECT OPEN DUCT BURNED INSULATION FROM ASM AND CAUSED WING TO BODY OVERHEAT TO OCCUR;[03] REMOVED AND REPLACED WIGGINS CLAMP ON NGS HEAT EXCHANGER AND NGS ASM REF AMM 47-11-01. OPS CHECKS GOOD NO LEAKS NOTED
FWD CARGO COMPARTMENT BAFFLE CORRODED, BS 500A+6, 500A+10, 500A+14, & 500A+18, RBL 25, WL 156. REPAIRED THE BAFFLE IAW SRM 53-30-53-2R-1.
LH SIDE INTERCOSTAL CRACKED BTWN BS 294.5 & 303.9, STRINGER 16L. REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, DWG 1418180, SHEET 22, 23, & 25, REV-, AMM 25-80-00-000-801, AMM 25-80-00-400-801, & AMM 51-21-91-620-802.
FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BS 500A+6, 500A+10, 500A+14, & 500A+18, RBL 25, WL 156. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G, AND DRAWING 143A7500, REV -.
CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 400-500D; LBL22; WL 156. REMOVED AND REPLACED FWD. CARGO FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G AND DRAWING 143A7500 REV -.
FWD CARGO COMPARTMENT FLOOR TO BULKHEAD SUPPORT CORRODED, BS 500D, LBL22 - RBL 22, WL 156. REMOVED AND REPLACED THE FLOOR TO BULKHEAD SUPPORT IAW SRM 51-40-02-0G, AND DRAWING 143A9481, REV -.
AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ZF WAS REPAIRED IAW SRM 53-00-50-2R-1.
FLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 232FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
AFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ACF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
CORROSION ON RT FLOOR TO SIDEWALL SUPPORT BS 727+4 - 767, RBL 22, WL 156 AT VARIOUS SPOTS. AFT CARGO COMPARTMENT. REMOVED AND INSTALLED A NEW RT FLOOR TO SIDEWALL SUPPORT BS 727+4 -767, RBL 22, WL 156 IAW SRM 51-40-02-0G-0.
FLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 231JF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 & DRAWING 146A5810, SHEET 577.
CORRODED RT DOOR SUB THRESHOLD WEB, BS 767 - 787, RBL 27, WL 154. REMOVED AND REPLACED THE SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0-A00729.
CORROSION ON L/H FLOOR TO SIDEWALL SUPPORT STA 727+4-847; LBL 22; WL 156 AT VARIOUS SPOTS. IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED L/H FLOOR TO SIDEWALL SUPPORT (ZEE ANGLE) AT STA 727+4-847; LBL 22; WL 156. PER SRM 51-40-02-0G .
AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1.
CORROSION ON R/H FLOOR TO SHIELD STA 767-787; RBL 22; WL 155 AT VARIOUS SPOTS. IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED. INSTALLED NEW SHIELD BS 767-787, RBL 22, WL 155 IAW SRM 51-40-02-0G AND DRAWING 146A0081, REV A.
FAD LAVATORY EXIT LIGHT AND COVER ARE BROKEN. INSTALLED LAVATORY EXIT LIGHT AND COVER PER AMM 33-51-01/201;[02] REMOVED AND REPLACED LAV A EMERGENCY EXIT LIGHT AND COVER ON AFT FACE OF LAV PER AMM 33-51-01-960-802;[03] OP CHECK OF LIGHT IS GOOD PER AMM 33-51-01-960-802 STEP C.(7)
FAD LAVATORY EXIT LIGHT AND COVER ARE BROKEN<[01] INSTALLED LAVATORY EXIT LIGHT AND COVER PER AMM 33-51-01/201. REMOVED AND REPLACED LAV A EMERGENCY EXIT LIGHT AND COVER ON AFT FACE OF LAV PER AMM 33-51-01-960-802. OP CHECK OF LIGHT IS GOOD PER AMM 33-51-01-960-802 STEP C.(7).
RIGHT INLET COWL LIP SKIN HAS SHEARED FASTENERS HEAD AT 2; 3 AND 10 O'CLOCK POSITIONS; MARKED<[01] COMPLETED STEP 1;[02] REMOVED AND REPLACED RH INLET COWL IAW AMM 71-11-01-400-802-F00 LEAK TEST GOOD;[03] VERIFIED CORRECTIVE ACTION 2.;[04] VERIFIED STEPS 2 AND 3.
CORROSION ON SEAT TRACK CROWN, BS 639+13, 706+17, 727+15, RBL 25, WL 208. THE SEAT TRACK WAS REPLACED ON CUSTOMER CARD TTG8Q01AN5EX.
CORRODED SEAT TRACK CROWN, BS 616+19, 662-664, 685+8-11, 727A+8, RBL 25, WL 208. REMOVED AND REPLACED THE DAMAGED SEAT TRACK, BS 540 - 727B, RBL 25, WL 208 IAW SRM 51-10-02-0G-0; SRM 51-40-02-0G-0, & DWG 114A6300, REV E, REF AIPC 53-43-11-01. TOURQUED THE SEAT TRACK IAW AMM 20-50-11-910-801. REPLACEMENT FOR CORRSION BEING OUT OF LIMITS IAW SRM 53-00-52-1A-1.
CORRODED SEAT TRACK CROWN, BS 727C+2-4, 747+3-7, 767+13-16, 807+1-2, 827+14-19, LBL 45, WL 208. REMOVED AND REPLACED THE SEAT TRACK BS 727B - 887, LBL45, WL 208 IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 146A5300, REV -.
LEFT WING TRAILING EDGE SUPPORT BEAM ATTACHMENT HAS WEAR DAMAGE AND ELONGATED HOLE ON TWO FASTENER LOCATIONS. REPAIRED IAW SRM 57-51-02-2R-1-A01271, REPAIR 1.
WHILE REMOVING FLOOR PANEL 241DF, IDENTIFIED A DAMAGED INSERT (PULLED THROUGH PANEL) AFT LH SIDE OF THE PANEL. FABRICATED OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
CRACK FOUND ON LT LOWER HORIZONTAL STAB SKIN 17.75' FROM FWD L/E AT HSS 193.90, L:0.32'. REPAIRED THE LT HORIZONTAL STAB SKIN IAW SRM 55-10-01-2R-11
RIGHT HORIZONTAL STAB REMOVABLE L/E 4TH FROM INBD RIB IS CRACKED. REMOVED AND REPLACED THE RT HORIZONTAL STAB REMOVABLE L/E RIB; 4TH FROM INBD IAW SRM 51-40-02, STEP 4 B;C.
AFT SERVICE DOOR ASSIST HANDLE BROKEN. REPLACED THE AFT SERVICE DOOR ASSIST HANDLE IAW MM 52-41-31.
EMERGENCY EXIT SLIDE EMERGENCY EXIT SLIDE AT FWD SERVICE DOOR PARTIALLY OUT OF COVER. INSPECTED PER AMM 25-66-00-201-NG.
L1 DOOR ASSIST HANDLE IS LOOSE<[01] TIGHTENED THE L1 DOOR ASSIST HANDLE IAW B737-700 AMM SUBTASK 25-21-31-420-007.;[02] TIGHTENED THE L1 DOOR ASSIST HANDLE IAW B737-700 AMM SUBTASK 25-21-31-420-007.
UPON REMOVAL OF #2 ENGINE EXHAUST PLUG FOUND ENGINE FLANGE ASSY FLANGE CRACKED AT MULTIPLE LOCATIONS.
FWD SERVICE DOOR EMERGENCY SLIDE LIGHT INOP.<[01] REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY SLIDE LAMP PER AMM 33-51-04.
FWD ENTRY DOOR COVER PLATE UNDER HANDLE BROKEN<[01] REMOVED AND REPLACED FWD ENTRY DOOR UPPER COVER PLATE UNDER HANDLE PER AMM 52-11-31.;[02] 02 - INSPECTED PER [AMM 52-11-31-401-NG (FORWARD ENTRY DOOR LINING - REMOVAL/INSTALLATION - PERMANENT)]
EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY BATTERY PACK M1674 ARE INOP<[01] REPLACED AND GOOD TEST PERFORMED AT BATTERY PACK M1674 IAW 33-51-06-960-805.;[02] VERIFIED REPLACEMENT AND GOOD TEST PERFORMED AT BATTERY PACK M1674 IAW 33-51-06-960-805.;[03] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PASSENGER CABIN FLOOR BOARD 241FF HAS BAD INSERT. FOUND ADDITION UPPER SURFACE SKIN DAMAGE AND LOWER SURFACE DAMAGETO SKIN AND CORE. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241FF FLOOR PANEL, INSERTS INSTALLED, APPLIED TAPE AND PART MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 1A, PARA 4A, PARA 5S1, TABLE 204, & DWG 144A5810-131.
PASSENGER CABIN FLOOR BOARD 241RF IS DELAMINATED AND HAS 1 BROKEN INSERT. DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241RF FLOOR PANEL, INSERTS INSTALLED, APPLIED TAPE AND PART MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 1A, PARA 5S1 & DWG 146A5810-466.
CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED DAMAGED SHIELD; LOCATED; DRILLED AND INSTALLED NEW SHILED IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 143A0080.;[02] TASK CARD COMPLETE
AFT CARGO BAY R/H CARGO FLOOR TRACK IS CRACKED BS 747 RBL 14 WL 155<[01] CRACK WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACE TRACK AS PER SRM 53-00-53-2R-3 AND EA 24-153-00838.;[02] VERIFIED CORRECTIVE ACTION 1
CORROSION FWD CARGO BAY FWD SHIELD BS420+1 TO BS420+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED AND REPLACED FWD SHIELD BETWEEN BS 420 TO BS 440;RBL 22;WL 156 PER SRM 51-40-02 AND DWG:143A0080.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-5.
CORROSION ON PASSENGER CABIN SEAT TRACK BS373 LBL45 WL208. COMPLETED STEPS 1 AND 2.;[02] UPDATED MEASUREMENTS TABLE. UPDATED MEASUREMENTS TABLE.;[04] EDITED STEP 2;[05] VERIFIED;[06] UPDATED STEP 1 PARTIAL. CORROSION ON PASSENGER CABIN SEAT TRACK BS373 LBL45 WL208. SRM 53-00-52-1A-1 IS APPLICABLE ALLOWABLE DAMAGE. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK BS373 LBL45 WL208. PER SRM 51-10-02-0G-0. MAX MATERIAL REMOVED WAS L= 5' BY W= 1' X .048 IN WELL. OUT OF LIMITS PER SRM 53-00-52-1A-1. MEASURED DEPTH WITH DIAL DEPTH GAUGE. FABRICATION WAS ACCOMPLISHED IAW DWG 143A5310(-51) AND ATS JOB 569781. LOCATED; DRILLED; AND COUNTERSINK SEAT TRACK PER SRM 51-40-05; REF BOEING DWG 143A5300; SHEET 17. APPLIED PRIMER TO SEAT TRACK BS373 LBL45 WL208 PER BOEING DRAWING 143A5310-51 REV:C. INSTALLED NEW SEAT TRACK AT BS373 LBL45 WL208 IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5300.;[08] VERIFIED CORRECTIVE ACTION 7.
CORROSION ON PASSENGER CABIN SEAT TRACK BS867+5 CROWN RBL25 WL208.<[01] UPDATED MEASUREMENTS TABLE;[02] UPDATED STEPS 1 AND 2;[03] UPDATED STEP 3.;[04] UPDATED STEP 4;[05] COMPLETED STEP 4.;[06] COMPLETED STEP 5;[07] PARTIAL UPDATE ON STEP 3.;[08] UPDATED STEP 3.;[09] CORROSION ON PASSENGER CABIN SEAT TRACK BS867+5 CROWN RBL25 WL208. SRM 53-00-52-1A-1 IS APPLICABLE ALLOWABLE DAMAGE. REMOVED CORROSION ON SEAT TRACK TOP OF CROWN BS867 + 5 IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS L2' X W1' X D.041 PER SRM 53-00-52-1A-1. DEPTH GAUGE ID#ATS400 DUE DATE:10/2024. REMOVED SEAT TRACK BS727B-887 RBL25; WL208 PER SRM 51-40-02. LOCATED FASTENER HOLES; DRILLED & DEBURRED A NEW ATSHFAB-100-316 SEAT TRACK FOR BS 727B-887; RBL25; WL208 PER SRM 51-40-05 AND BOEING DWG 146A5300 SH72. OKAY TO INSTALL. INSTALLED ALL FASTENERS ON PASSENGER CABIN SEAT TRACK AT BS 787 - 867; RBL25; WL208 IAW BOEING DWG 146A5300 SH 72 AND BOEING DWG 146A5300 SH 73 AND SRM 51-40-04-0G-0. EQUIPMENT USED: ATS1353 DUE DATE 08/2024.;[10] VERIFIED ALL STEPS COMPLETED; CARD COMPLETE.
CORROSION ON PASSENGER CABIN SEAT TRACK BS500C LBL45 WL208.<[01] COMPLETED STEPS 1 -2;[02] PASSENGER CABIN SEAT TRACK STA 480-520; LBL 45; WL 208 WILL BE REPLACED ON CUSTOMER CARD# TTG8Q00SCM3L.;[03] VERIFIED CORRECTIVE ACTION STEP 2. TASK CARD COMPLETE.
CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 727+4' TO BS 867; LBL 22; WL 156 PER SRM 51-40-02 AND DWG:146A7500.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. COMPLETED THROUGH STEPS 1-5.
LEFT ELEVATOR TAB MAST FAIRING (P/N 183A8500-5) IS DELAMINATED. (PHOTO ATTACHED)<[01] REMOVED AND REPLACED LT. ELEVATOR TAB IAW AMM 27-31-31-000-801 & AMM 27-31-31-400-801;[02] VERIFIED COMPLETE;[03] FCF REQUIRED DUE TO REPLACEMENT OF L/H ELEVATOR TAB. ENTERED FCF REQUIREMENT ON LOG PAGE# 2118562
LH SECTION 3 OF LBL 45 SEAT TRACK HAS CORROSION ON CROWN BS 500C; WL 208<[01] FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q00SCLMF
AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01] COMPLETED STEP 5;6.;[02] VERIFIED TASK COMPLETED
CRACKED BREAK PANEL STA 540; LBL 1; WL 207.<[01] REMOVED AND INSTALLED NEW BREAK PANEL LOT 1548854-1; PER SRM 51-40-02 AND DWG 143A0060.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
CRACKED FLOOR SUPPORT BS 328-344 LBL 47 WL 208.<[01] UPDATED STEPS 1 AND 2.;[02] VERIFIED;[03] COMPLETED STEPS 1 AND 2.
CRACKED INTERCOSTAL LOWER ATTACH ANGLE STA 692; RBL 24; WL 204.<[01] REMOVED CRACK DAMAGED LOWER ATTACH ANGLE AT BS 692 RBL 24 WL 204 IAW SRM 51-40-02-0G-0;[02] FABRICATED NEW ATTACH ANGLE FOR BS 692 RBL 24 WL 204 FROM HFAB53-BR-012 (BAC1490-2782 7075 TO CLAD .050 LOT# 1482272-2) HEAT TREATED TO T73 CONDITION ON SWA PO# 857530 DATED 21 FEB 2022 LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 APPLIED CHEMICAL CONVERSION COAT AND PRIMED IAW SRM 51-20-01-0G-0 AND BOEING DWG 273A9112 OK TO INSTALL;[03] VERIFIED ACTION #2; OK TO INSTALL;[04] INSTALLED NEW INTERCOSTAL LOWER ATTACH ANGLE AT STA BS 692 RBL 24 WL 204 IAW SRM 51-40-02-0G-0 AND BOEING DWG 273A9112;[05] VERIFIED CORRECTIVE ACTION #4
CORROSION AROUND FASTENER HOLE BS 986 BEAM RBL 44 WL 208.<[01] EVALUATED DAMAGE AND FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.D(2)(A) FIGURE 103/DETAIL E .<BR>PERFORMED REPAIR ON THE UPPER CHORD OF THE<BR>FLOOR BEAM AT STA 986.5 AT RBL44 WL 208 IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 3.
PASSENGER CABIN FLOOR PANEL 242TF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242TF WITH UPPER SKIN DELAMINATION WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 222DF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 222DF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 235.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABIN FLOOR PANEL 221FF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221FF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221EF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221EF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221CF IS DELAMINATED<[01] CABIN FLOOR PANEL 221CF DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221GF IS DELAMINATED. PASSENGER CABIN FLOOR PANEL 221GF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
PASSENGER CABIN FLOOR PANEL 222CF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 222CF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 275.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABIN FLOOR PANEL 231AF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 231AF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 231BF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 231BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 430.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABIN FLOOR PANEL 231CF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 231CF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 222BF IS DELAMINATED AND HAS BAD INSERTS. (MARKED) PASSENGER CABIN FLOOR PANEL 222BF IS DELAMINATED AND HAS BAD INSERTS.<[01] PASSENGER CABIN FLOOR PANEL 222BF WITH UPPER SKIN DELAMINATION AND BAD INSERTS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221DF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221DF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION. JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221AF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 221AF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 221BF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 221BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 95.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 232AF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 232AF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 400.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABIN FLOOR PANEL 241AAF IS DELAMINATED.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-1 PARA 1A(NOTE) AND BOEING DWG 147A5810-8.;[02] VERIFIED CORRECTIVE ACTION #1
PASSENGER CABIN FLOOR PANEL 241YF IS DELAMINATED<[01] DELAMINATION ON PASSENGER CABIN FLOOR PANEL 241YF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1
PASSENGER CABIN FLOOR PANEL 241XF IS DELAMINATED<[01] CABIN FLOOR PANEL 241XF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 242UF IS DELAMINATED AND HAS BAD INSERTS MARKED<[01] DELAMINATION AND BAD INSERTS ON PASSENGER CABIN FLOOR PANEL 242UF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1
PASSENGER CABIN FLOOR PANEL 242SF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242SF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 241AEF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 241AEF WITH UPPER SKIN DELAMINATION WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 242PF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242PF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 242QF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 242QF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-63A ITEM 380.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
PASSENGER CABIN FLOOR PANEL 241UF IS DELAMINATED<[01] DUE TO EXCESSIVE DAMAGE; FLOOR PANEL 241UF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED
PASSENGER CABIN FLOOR PANEL 241ABF IS DELAMINATED.<[01] CABIN FLOOR PANEL 241ABF DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 242RF IS DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242RF WITH UPPER SKIN DELAMINATION WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
FLOORBOARD 241AF UPPER SURFACE DAMAGED. (DELAMINATED)<[01] FLOORBOARD 241AF WILL BE REPAIRED OR REPLACED ON FAULT TTG8Q00S9RVV;[02] VERIFIED CORRECTIVE ACTION 1.
CORROSION ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; RBL 12; AND LBL 12.<[01] VERIFIED STEPS 1; 2; 5.;[02] REMOVED DAMAGE ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; 10'X2.0' AREA; RBL 12;1.4'X0.800' AREA AND LBL 12; 12.3'X2.3' ALL I.A.W SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 PAR 4.C(2)(A) DETAILS C.D AND MAINTENANCE WAS ACCOMPLISHED ON STEPS 1-6 AND WIP1 AND 2;[03] VERIFIED RII ITEMS COMPLETE.
PANEL 191D OUTER SKIN HAS SMALL DISBOND. (MARKED)<[01] PANEL 191D OUTER SKIN SMALL DISBOND WAS REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
2ND FWD STIFFENER CRACK AT LH HSTAB AT STAB STA 120.30<[01] OK TO INSTALL GIVEN;[02] OKAY TO CAP-SEAL GIVEN STEP # 2 COMPLETE.;[03] CAP SEALED FASTENERS AT LEFT HAND HORIZONTAL STABILIZER FRONT SPAR WEB AT STAB STA 111.10 - 136 IAW AMM 51-31-00-390-805.;[04] VERIFIED CORRECTIVE ACTION ENTRY 3.;[05] VERIFIED CORRECTIVE ACTION COMPLETED WITH STEPS.
FWD ENTRY DOOR ASSIST HANDLE LOOSE<[01] RESECURED FWD ENTRY DOOR ASSIST HANDLE REF M/M 52-11-31
CUSTOMER WALK - R1 DOOR ASSIST HANDLE (DOOR SIDE) LOOSE.<[01] RESECURED R-1 DOOR ASSIST HANDLE.(DOOR SIDE )AS PER AMM 52-41-31-400-802.;[02] VERIFIED RESECURED R-1 DOOR ASSIST HANDLE.(DOOR SIDE )
CUSTOMER WALK - L1 DOOR ASSIST HANDLE (DOOR SIDE) LOOSE.<[01] RESECURED L-1 DOOR ASSIST HANDLE ( DOOR SIDE ) AS PER AMM 52-11-31-400-802.;[02] VERIFIED RESECURED L-1 DOOR ASSIST HANDLE ( DOOR SIDE )
MAIN CABIN AFT ENTRY AREA SEVERAL EMERGENCY LIGHTS INOP<[01] REPLACED EMERGENCY BATTERY PACK AT POWER SUPPLY M1672 FOR MAIN CABIN AFT ENTRY INOP EMERGENCY LIGHTS AS PER REF AMM TASK 33-51-06-960-805. OPERATION TESTED NORMAL.;[02] VERIFIED REPLACED EMERGENCY BATTERY PACK AT POWER SUPPLY M1672 AND OP'S TESTED NORMAL.
REJECT - L/H VAPOR BARRIER WEB HAS MULTIPLE ELONGATED HOLES.<[01] COMPLETED INSTALLATION OF L/H VAPOR BARRIER WEB; ANGLES; SUPPORT STRUCTURES; BRACKETS AND STRAPS ON REFERENCE TO SRM 51-40-02-0G-0; DWG NO: 111A1000; 111A1001.;[02] SUMMARY: REMOVED & REINSTALLED L/H VAPOR BARRIER FOR ACCESS TO REPAIR AS PER B-737 SRM 51-40-02-0G AND DRAWING NUMBER 111A1001 AND 111A1000. APPLIED PERMANENT REPAIR ON DAMAGE AREA AT L/H VAPOR BARRIER AS MARKED AS PER B737 SRM 57-10-10-2R-2; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED PO#2040614 AND PO# 1738577; EQUIPMENT USED TEMPERATURE CONTROL ID160354 DUE DATE 02-16-24; VACUUM GAGE ID 173239 DUE DATE 02-23-24.;[03] RII- VERIFIED REMOVAL; REINSTALLATION AND REPAIR OH LH VAPOR BARRIER
LT HAND VAPOR BARRIER STIFFENER AT LBL 25' CRACKED.<[01] SUMMARY :REMOVED CRACKED STIFFENER AT LBL25' AS PER B 737 SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW STIFFENER AS L/H VAPER BARRIER AT LBL 25' AS PER REF B/737 SRM 51-40-05-0G-0.INSTALLED NEW STIFFENERS AT L/H VAPOR BARRIER AT LBL 25' AS PER REF B/737 SRM 51-40-02-0G-0AND DW111A1001.;[02] ALL STEPS COMPLETED.;[03] RII... VERIFIED REMOVED AND INSTALLED NEW STIFFENERS AT L/H VAPOR BARRIER AT LBL 25'
CENTER WING REAR SPAR VAPOR BARRIER CRACKED; APPROXIMATELY 19 INCHES LONG (EXCEEDING SRM LENGTH LIMIT).<[01] APPLIED REPAIR AT L\H VAPOR BARRIER REAR SIDE PER B737 SRM 57-10-10-2R-2;SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0 PARAGRAPH 4.N.2 AND PARAGRAPH 4.L.7 MATERIAL USED RESIN EY 3804 PO# 2040614 FIBER GLASS PO#1690463 TOOL USED TEMPERATURE CONTROLLER ID 34748712 DUE DATE 06-07-24. RESTORED FINISH TO FORWARD AND AFT SIDES OF VAPOR BARRIER AS PER B 737 AMM 51-21-81-370-802 ANDD AMM 51-21-72-370-804;[02] RII. VERIFIED REPAIR AT L\H VAPOR BARRIER
CENTER WING REAR SPAR VAPOR WEB HAS AN APPROXIMATE 18 INCH CRACK BEGINNING INBOARD OF THE SYS.A HYD. PRESSURE MODULE INBOARD MOUNT AND EXTENDING APPROX. 6 INCHES TO LEFT OF LBL 45.64 STIFFENER.<[01] C/W EA 23-157-02932;[02] COMPLIED WITH EA 23-157-02932. ALSO REFERENCE PREVIOUS DOCUMENTATION OF CRACK; PERMANENT REPAIR AND INTERIM REPAIR. TTG8Q00M8KD2; TTG8Q00M8B6K; TSR 2023005578; TTG8Q00NBF8B; TTG8Q00NBFEQ AND TTG8Q00M8RRZ
L/H 663.75 LOWER BULKHEAD CRACKED. CRACKS STARTS APPROXIMATELY LBL 54.21 AND TRAVELS TO LBL 40.00. CRACK MEASURES AT 15 1/2 INCHES BEFORE IT GOES BEHIND THE HYDRAULIC MODULE BRACKET.<[01] ACCOMPLISHED PERMANENT REPAIR OF 4 INCHES OF CRACK IAW SRM 51-70-04-2R-10. REMAINING CRACK REPAIRED ON TTG8Q00NBFEQ.;[02] ACCOMPLISHED POST REPAIR INSPECTION PER 737 NDT MANUAL PART 4 51-00-02. NO DEFECTS NOTED.
AT ROTATION ALL ENG; APU & WHEEL WELL FIRE INDICATION ILLUMINATED WITH ASSOCIATED FIRE BELL<[01] R/R?D ENGINE AND APU FIRE OVERHEAT CONTROL MODULE (M279)AS PER EMM 26-10-01.ALL OPERATIONAL TESTS NORMAL. R/R?D ENGINE AND APU FIRE CONTROL PANEL (P8-1) AS PER AMM 26-10-01. ALL OPERATIONAL TESTS NORMAL.
AT ROTATION ALL ENG; APU & WHEEL WELL FIRE INDICATION ILLUMINATED WITH ASSOCIATED FIRE BELL<[01] R/R?D ENGINE AND APU FIRE OVERHEAT CONTROL MODULE (M279)AS PER EMM 26-10-01.ALL OPERATIONAL TESTS NORMAL. R/R?D ENGINE AND APU FIRE CONTROL PANEL (P8-1) AS PER AMM 26-10-01. ALL OPERATIONAL TESTS NORMAL.
AFTER TOUCHDOWN ALL FIRE INDICATIONS ILLUMINATED WITH ASSOCIATED FIRE BELL AND ANNUNCIATORS<[01] R&R ENG & APU FIRE DETECTION MODULE PER AMM 26-10-01<BR>OPS CHK NORMAL
L/H 663.75 LOWER BULKHEAD CRACKED. CRACKS STARTS APPROXIMATELY LBL 54.21 AND TRAVELS TO LBL 40.00. CRACK MEASURES AT 15 1/2 INCHES BEFORE IT GOES BEHIND THE HYDRAULIC MODULE BRACKET. ONCE CRACK GOES BEHIND HYDRAULIC MODULE BRACKET IT CAN NO LONGER BE MEASURED DUE TO THE FACT THAT IT IS HIDDEN. ALLOWABLE DAMAGE IS NO MORE THAN 16 INCHES PER SRM 57-10-10-1A-2. FIRST 7 INCHES OF CRACK IS ALL THE WAY THROUGH FIBERGLASS MATERIAL.<[01] CW;[02] CW;[03] REMOVED HYDRAULIC SYSTEM A AND B PRESSURE MODULE PER AMM 29-11-71.;[04] REMOVED A AND B PRESSURE MODULE MOUNTING BRACKET PER AMM 29-11-71. REMOVED NGS RAM AIR VALVE EXHAUST DUCT AND PANEL AMM 47-32-05.;[05] UPON REMOVAL OF PRESSURE MODULE MOUNTING BRACKET FOUND THAT CRACK EXTENDS AN ADDITIONAL 3.0 INCHES.;[06] REINSTALLED LH WHEEL WELL PRESSURE MODUEL MOUNTING BRACKET REF 737 SRM 51-40-02;[07] INSTALLED A SYS HYDRAULIC PRESSURE MODULE IAW AMM 29-11-71;[08] INSTALLED NGS RAM AIR VALVE EXHAUST DUCT AND PANEL IAW AMM 47-32-05.;[09] INSTALLED A SYS HYDRAULIC PRESSURE MODULE IAW AMM 29-11-71. ENG SIDE PRESSURE MODULE REQUIRES LEAK CHECK.;[10] A SYS HYDRAULIC PRESSURE MODULE LEAK CHECK COMPLIED WITH ON TTG8Q00M8SV4;[11] REPAIRED LH 663.75 LOWER BULKHEAD CRACK PER EA 23-157-02209 REF WO# TTG8Q00M8KD2
DURING NORMAL GEAR EXTENSION; L/H GEAR RED INDICATION WHILE NOSE AND R/H GEAR GREEN; PERFORMED LOW PASS AND ATC CONFIRMED PARTIAL L/H GEAR EXTENSION. RAN QRH CHECKLIST; AND MANUALLY EXTENDED GEAR. DURING NORMAL GEAR EXTENSION L/H GEAR RED INDICATION WHILE NOSE AND R/H GEAR GREEN PERFORMED LOW PASS AND ATC CONFIRMED PARTIAL L/H GEAR EXTENSION. RAN QRH CHECKLIST AND MANUALLY EXTENDED GEAR AFTER 2-3 MINUTES GEAR FULLY EXTENDED.<[01] OK TO CONTINUE PER MEL 32-16-01 SP1.;[02] PERFORMED FIM TASK 32-32 TASK802 NO DISCREPANCIES.NOTED AS COMPANY PRECAUTION REMOVED AND REPLACED MLG TRANSFER FLOW CYLINDER AND MAIN LANDING GEAR HYDRALIC FLOW REGULATOR LEFT SIDE AMM 32-32-71 AMM 32-32-72
DURING NORMAL GEAR EXTENSION; L/H GEAR RED INDICATION WHILE NOSE AND R/H GEAR GREEN; PERFORMED LOW PASS AND ATC CONFIRMED PARTIAL L/H GEAR EXTENSION. RAN QRH CHECKLIST; AND MANUALLY EXTENDED GEAR. DURING NORMAL GEAR EXTENSION L/H GEAR RED INDICATION WHILE NOSE AND R/H GEAR GREEN PERFORMED LOW PASS AND ATC CONFIRMED PARTIAL L/H GEAR EXTENSION. RAN QRH CHECKLIST AND MANUALLY EXTENDED GEAR AFTER 2-3 MINUTES GEAR FULLY EXTENDED.<[01] OK TO CONTINUE PER MEL 32-16-01 SP1.;[02] PERFORMED FIM TASK 32-32 TASK802 NO DISCREPANCIES.NOTED AS COMPANY PRECAUTION REMOVED AND REPLACED MLG TRANSFER FLOW CYLINDER AND MAIN LANDING GEAR HYDRALIC FLOW REGULATOR LEFT SIDE AMM 32-32-71 AMM 32-32-72
FWD MEGAPHONE INOP<[01] REPLACE MEGAPHONE PER AMM 25-99-99
EXTERNAL POWER DOOR CUTOUT LOWER FLANGE IS CRACKED<[01] NDT IAW B737-700 SRM 53-10-15-2R-4; PAGE 2; STEP 4.C (7) AND D; TOOL # 44291; DUE 03NOV23; NO DEFECTS NOTED.;[02] OK TO TREAT AND PRIME;[03] LOCATED AND DRILLED EXTERNAL POWER DOOR CUTOUT DOUBLER AND FILLER IAW SRM51-40-02-0G-0 AND SRM 53-10-15-2R-4;[04] TREATED AND PRIMED IWA SRM 53-10-15-2R-4 STEP 4-K AND L;[05] VERIFIED STEPS 3 AND 4<BR><BR>OK TO INSTALL REPAIR PARTS;[06] INSTALLED DOUBLER AND FILLER ON TO POWER DOOR CUTOUT IAW SRM 53-10-15-2R-4 STEPS 4.M 1THRU 5 AND SRM 51-40-02-0G-0;[07] VERIFIED STEP 6 COMPLETE<BR><BR>OK TO TOP COAT;[08] APPLIED TOP COAT IAW SRM 53-10-15-2R-4 STEP 4.N;[09] VERIED TASK COMPLETE
ONE OF THE CABIN FLASHLIGHTS IN THE FRONT JUMPSEAT IS NOT FLASHING<[01] R/R?D 1 CABIN FLASHLIGHT REF AMM 25-64-00. LED BLINKS. OPS NORMAL. THIS CLEARS MEL
A FLT ATTNDT FLASHLIGHT INOP<[01] REPLACED BATTERY ON FWD FLT ATTNDT FLASHLIGHT PER AMM 25-64-00. OPS CHECK OK.
L/H EXTERIOR OVER WING EXIT LT INOP<[01] REPLACED BATTERY PACK ON LT EXTERIOR EMERGENCY OVER WING LIGHT PER AMM 33-51-06. OP?S CHECK GOOD OK PER AMM 33-51-06.
AISLE EMER LT INOP 6 ABC<[01] REPLACED BATTERY PACK ON LT EMERGENCY EXIT AT ROW 12A PER AMM 33-51-06. (LIGHT SUPPLY ON AISLE 6ABC ARE CONNECTED WITH LT EMERGENCY EXIT LIGHT POWER SUPPLY). OP?S CHECK GOOD PER AMM 33-51-06.
LEFT HAND INTERIOR OVER WING EMER EXIT EMER EXIT LIGHT INOP<[01] REPLACED BATTERY PACK ON LT INTERIOR OVER WING EMERGENCY EXIT PER AMM 33-51-06. OP?S CHECK GOOD PER AMM 33-51-06.
R/H OVERWING MULTIPLE EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED R/H OVERWING EMERGENCY EXIT LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD
MULTIPLE FWD ENTRY EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD
EXTERNAL FUSELAGE LH/RH OVER WING SCAPE EMERGENCY LIGHTS AND MAIN CABIN AISLE LIGHTS ROW 9 AND 11 LH INOP. / [01] REMOVED AND REPLACED BATTERY CHARGER ASSY AS PER REF B737 AMM- 33-51-06-960-806.;[02] REMOVED AND REPLACED BATTERY CHARGER ASSY AT POSITION M1670 AND PERFORMED INSTALLATION TEST FOUND NORMAL AS PER REF B737-AMM-33-51-06-960-806.;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1670 AND PERFORMED OPS TEST FOUND NORMAL AT LH/RH OVER WING SCAPE EMERGENCY LIGHT AND MAIN CABIN AISLE LIGHTS ROW 9 AND 11.;[04] VERIFIED STEP 1;2;3
L/H OVERWING EXIT WINDOW LIGHT INOP. / [01] REPLACED L/H OVERWING EXIT WINDOW LIGHT LAMP AS PER B737 AMM 33-21-00-960-801; AND NO HELP.;[02] PERFORMED T/S AS PER WDM 33-21-11; WDM 33-21-12; AND FOUND FUSE DEFECTIVE.;[03] VERIFIED 1; 2;[04] REPLACED FUSE AS PER B737 AMM 33-21-00-960-803; AND NO HELP. NEED TO REPLACE BALLAST.;[05] REPLACED AND PERFORMED LIGHT ASSEMBLY REPLACEMENT TEST AT L/H OVERWING EXIT WINDOW LIGHT AS PER B737 AMM 33-21-00-960-802. TEST OK.;[06] VERIFIED REPLACEMENT AND TEST
G-1 GALLEY EXIT SIGN BROKEN / [01] REMOVED AND REPLACED EXIT SIGN AT GALLEY 1 AS PER BOEING 737-700 AMM 33-51-01-960-802.;[02] PART TRANSITION ONLY;[03] VERIFIED REPLACEMENT
FOUND CORROSION AT AFT CARGO L/H Z CHANNEL BETWEEN STA 847 TO 727 / [01] REMOVED CORROSION AT AFT CARGO L/H Z CHANNEL BETWEEN STA 727 TO STA 847 FOUND BETWEEN STA 747 TO STA 767 OUT LIMITS IAW B737 SRM 51-10-02-0G-0.;[11] REMOVED CORROSION AT AFT CARGO L/H Z CHANNEL BETWEEN STA 727 TO STA 847 AS PER B737-700 SRM 51-10-02-0G-0. EXFOLIATED CORROSION FOUND BETWEEN STA 747 TO STA 767 SECTION FOUND TO BE OUT OF LIMITS AS PER B737 SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW SECTION OF L/H ZEE CHANNEL FROM 747 TO 847 AS PER B737-700 SRM 51-40-05-0G-0. TREATED AND PRIMED NEW SECTION OF L/H ZEE CHANNEL AS PER B737-700 AMM 51-21-41-370-803 AND 51-21-72-370-802. INSTALLED 100% NUT PLATE ON NEW PART OF L/H ZEE CHANNEL AS PER B737-700 SRM 51-40-02-0G-0. SPLICED UP TOGETHER AFT CARGO L/H ZEE CHANNEL AS PER B737-700 SRM 51-40-02-0G-0 AND 53-00-53-2R-5 REPAIR 5.;[12] VERIFIED STEP 11
R/W FRONT SPAR L/E PANEL 621HB EDGE DELAMINATED / [01] MEASUREMENTS;[02] REPAIRED SMALL EDGE DAMAGE SIZE .750 DIA. ON R/W FRONT SPAR L/E LOWER ACCESS PANEL 621HB AS PER B737 SRM 51-70-04-2R-7 ; MATERIALS USED PO#11533636; PO#1690463 AND PO#1753794;[03] VERIFIED REPAIR
CORROSION ** AFT FUS. TOILET SERVICE COMPARTMENT. ACCESS PANEL 145AL AT BONDING LEAD ATTACHED POINT / [01] REMOVED BONDING LEAD SCREW FOR ACCESS AT TOILET SERVICE ACCESS PANEL 145AL PER BOEING 737-700 SRM 51-40-02-0G-0.;[02] REMOVED CORROSION AT ACCESS PANEL 145AL AT BONDING LEAD ATTACH POINT. ORIGINAL MATERIAL THICKNESS 0.070'; MATERIAL LOSS 0.030'; REMAINING MATERIAL THICKNESS 0.040'. FOUND OUT OF LIMITS PER 737-700 SRM 52-40-01-1A-4 PARR. 4. FIG. 103. DETAIL D. TOOL MICROMETER B/C 11369 CALIBRATION DUE DATE 08-SEP-2022.;[03] VERIFIED STEP 1; 2;[04] REMOVED AND REPLACED AFT FUS TOILET SERVICE COMPARTMENT ACCESS PANEL145AL; IN REFERENCE B-737 SRM 51-40-02-0G-0. PENDING FOR PAINT AND PLACARD;[05] PAINTED TOILET SERVICE PANEL 145AL PER B737-700 AMM 51-21-72-370-804 / 51-21-73-370-803. INSTALLED PLACARDS AS PER B737-700 AMM 11-00-00-201.;[06] VERIFIED REPLACEMENT & PAINT
FWD ENTRY DOOR ASSIST HANDLE BROKEN. REF AMM 52-11-31 SWAPPED FWD LAV ASSIST HANDLE WITH ENTRY DOOR HANDLE. ENTRY DOOR HANDLE OPS GOOD. INSTALLED NEW FWD LAV ASSIST HANDLE PER AMM 52-11-31. OPS CHECKED GOOD.
SUPPLEMENTAL INFORMATION: LH HORIZONTAL STAB. FWD UPPER SLIDER IS CRACKED ; / [01] REMOVE AND REPLACED LH HORIZONTAL STAB. FWD UPPER SLIDER PER MM.53-31-31
RH HORIZONTAL STAB. FWD UPPER SLIDER IS CRACKED ; / [01] REMOVED AND REPLACED RH HORIZONTAL STAB. FWD UPPER SLIDER PER MM;53-31-31
FOUND 3 ELONGATED FASTENER HOLES ON TRAILING EDGE OF 193D PANEL; AS MARKED. ; FOND 3 ELONGATED FASTENER HOLES ON TRAILING EDGE OF 193D PANEL; AS MARKED. / [01] ADDED EA 21-153-03169 AS A SUBTASK.; [02] REPAIRED PANEL PER EA 21-153-03169
SLIDE PACK ON GALLEY SERVICE DOOR APPEARS LOOSE ; / [01] TIGHTENED GIRT BAR J-HOOKS PER SIP.
2 EXTERNAL EMERGENCY LIGHTS BEHIND BOTH LH AND RH WING ROOT INOP. ; / REMOVED AND REPLACED BOTH LH AND RH EXTERNAL EMERGENCY AREA LIGHTS AS PER AMM 33-51-03.
2 EACH EMERGENCY LIGHT LENS. 12ABC & 9DEF LOOSE / RESECURED 2 EACH 2 EACH EMERGENCY LIGHT LENS. ON 9 DEF & 12 ABC AMM 33-51-02
L-2 DOOR SLIDE GIRT NEEDS REINSTALLED TOO LONG. RESECURED L-2 DOOR SLIDE GIRT BAR, PER MT725-61-06.
RT AFT EMERGENCY LIGHT BULB INOPERABLE. REMOVED AND REPLACED RT AFT EMERGENCY LIGHT CHARGER ASSEMBLY, REF AMM 33-51-06. OPERATIONS CHECK GOOD.
LT AFT EMERGENCY BATTERY PACK INOPERABLE. REMOVED AND REPLACED LT AFT EMERGENCY BATTERY PACK, IAW 737 AMM 33-51-51. OPERATIONS CHECK GOOD.
DURING CLIMBOUT THE NR 2 ENGINE EGT GAUGE TURNED AMBER AND INDICATED A TEMPERATURE OF APPROXIMATLY 915-920 FOR APPROXIMATLY 2 SECONDS. AFTER PERFORMING QRH PROCEDURE WE OPERATED AT REDUCED THRUST AND ALL INDICATORS WERE NORMAL. AIRCRAFT WAS AT REDUCED CLIMB TOWER PROFILE. COMPLIED WITH TASK 777-21-01. FOUND J10 HARNESS OUT OF LIMITS AT PINS B- TO V- AND H TO A-. REMOVED AND REPLACED J10 HARNESS, PER AMM 73-21-00 AND PREFORMED FIM TASK 77-21-804. OPS CHECK NORMAL
FWD SERVICE DOOR EXIT SIGN DETACHED. REINSTALLED THE EXIT SIGN COVER PER S.I.P
HAS A DENT EXTERNAL SKIN LOC. BS 259.5 TO BS 268.25 AND BETWEEN S-16L TO S-17L AT UPPER FUSELAGE / REPAIRED FUSELAGE SKIN BTW BSTA 259.5 AND BSTA 277 S-15L AND S-18L IAW EA #20-153-00758 REV IR AND EA #53-0487-20 REV.0
CRACK INSPAR RIB LOWER OUTBOARD AFT FLANGE AT STAB STA 120.30 LT HORIZONTAL STAB / REPAIRED INSPAR RIB LOWER OUTBOARD AFT FLANGE AT STAB STA 120.30 LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02 SRM 55-10-09-2R REPAIR 5
CORROSION ANGLE - SUPPORT ZEE LOCATED BETWEEN BS 400 AND BS420 WL 156.5 STR 26R AT FWD CARGO COMPARTMENT. REPLACED SUPPORT ZEE. LOC BTW BS 400 AND BS 420 WL 156.5 STR 26R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 DWG 143A7500 REV-.
CORROSION SUPPORT ANGLE STRINGER 23L BETWEEN BS 300 TO BS 312 AT LEVEL WL 165.5 AT EQUIPMENT ELECTRONIC COMP. REPLACED CHORD SUPPORT ANGLE STRINGER 23L BETWEEN BS260 TO BS360 AT LEVEL WL 165.5 AT EQUIPMENT ELECTRONIC COMPARTMENT IAW SRM 51-40-02 AND DRAWING 141AB240 REV O.
CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 26.5 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / REPAIRED INSPAR RIB LOC STAB STA 120.30 AT 26.5' FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 AND BS 767 STR 25R WL 156.5 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS 727 AND BS 767 STR 25R WL 156.5 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02; 51-10-02 ITEM 9 AND DRAWING 146A7502 REV A.
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 490 TO BS 500A STR 26 R; WL156.5 AT FWD CARGO COMPARTMENT / REPLACED SHIELD LOCATED BTW BS 490 TO BS 500A STR 26 R WC 156.5 FWD C/C IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A0080 REV
CORROSION TRACK RBBL 13.84 BTW STA 767 TO STA 787 AT AFT CARGO COMPARTMENT (1 EA) / REPAIRED TRACK RBBL 13.84 BTW STA 767 TO STA 787 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00- 53-2R-3 REPAIR 3
BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) / REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA IAW SRM 51-10-02 ITEM 9.
CRACK WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 BLO FWD GALLEY AND LAV / REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 BLO FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400-27
CRACK WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 TO BS 328 AND LBL 46 FWD GALLEY AND LAV / REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOC BTW BS 312 TO BS 328 AND LBL 46 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 ITEM 9
CRACK ACCESS PANEL 341B RIB AT RT HORIZONTAL STABILIZER. REPLACED RIB ON ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER IAW SRM 51-10-02 ITEM 9 51-40-02 AND DRAWING 186A1303 SHEET 2 REV -.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL 31 FWD GALLEY AND LAV / REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL 31 FWD GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DRAWING #141A5400 REV
CRACK VAPOR BARRIER LT AT MAIN WHEEL WELL COMPARTMENT / REPAIRED VAPOR BARRIER LT AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED CALIPER P/N: 700-113-10 S/N:0023187 DUE DATE: 28-OCT-20; HOT BONDER P/N: HCS9200B S/N:16122983 DUE DATE: 27-NOV-20; SCALE P/N:CL5000 S/N:AE-39582 DUE DATE: 05-NOV-20; HOT BONDER P/N: HCS9200B S/N:18165044 DUE DATE: 02-DEC-20.
CRACK STRINGER 7L BETWEEN BS 294 AND BS 303.9 AT PASSENGER CABIN / REEMPLACED STRINGER 7L BETWEEN B5294 AND B5303A AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 141A3120 SHEET 52 REV.
CRACK INNER CHORD FLOOR STRUCTURE LOCATED ON BS303 AT LEVEL STR17L AT PASSENGER CABIN / REPLACED INNER CHORD AND FASTENERS LOC BS 277 TO BS 360 AT LEVEL STRINGER 17L AT PASSENGER CABIN IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING #141A8110 REV.E
ELONGATED HOLE SUPPORT ZEE BETWEEN BS 727D TO BS 727E AND STR 25R AFT CARGO COMPARTMENT (1 EA) / REPLACED SUPPORT ZEE BTW BS 727D TO BS 727E AND STR 25 AFT CARGO COMPARTMENT ALL STEPS HAS BEEN DOCUMENTED ON L170586
CRACK TRACK LBBL 17.24 AND BS 727E AFT CARGO COMPARTMENT (1 EA) / REPAIRED TRACK LOCATED LBBL 17.24 AND BS 727E ON AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.
CRACK TIE CLIP LOCATED BS259 AND STR10R AT PASSENGER CABIN (1 EA). REPLACED TIE CLIP LOCATED BS 259 AND STR 10R AT PASSENGER CABIN 1EA IAW SRM 51-40-02 AND DWG 141A1110.
CRACK ANGLE - SUPPORT BS 867 AND STR 26L AT AFT CARGO COMPARTMENT (1 EA). REPLACED ANGLE - SUPPORT LOCATED AT BS 867 AND STR 26L AFT CARGO COMPARTMENT IAW SRM 51-10-02 STEP 9 AND DRAWING 149A8102.
CRACK BRACKET GUSSET LOCATED ON BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT (1 EA) / REPLACED BRACKET GUSSET LOCATED ON BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 AND 51-40-02 DWG # 143A7902
CRACK BRACKET GUSSET LOCATED ON BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT (1 EA) / REPLACED GUSSET LOCATED ON BS 500D AT LEVEL STR.19R AT FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 14349481
CRAZING IN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING R/H AT PASSENGER CABIN (5 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (5EA) IAW B737-700 AMM 33-51-15-400-802
CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975
CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPART MENT / REPAIRED BY WELD AFTER CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975
CRAZING IN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING L/H AT PASSENGER CABIN (6 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN (6EA) IAW B737-700 AMM 33-51-15-400-802
CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975
DETERIORATED GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA / REPLACED GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02
CRACK COVER LENS EXIT AT HEADER CEILING PANEL L/H SIDE AT AFT GALLEY AREA(1 EA) / REPLACED COVER LENS EXIT AT HEADER CEILING PANEL L/H AT AFT GALLEY AREA(1EA)IAW AMM 33-51-01-960-801
DETERIORATED GIRT BAR FITTINGS HARDWARE AND PLATES AT FWD GALLEY AREA / REPLACED GIRT BAR FITTINGS HARDWARE AND PLATES AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3 D(1)ITEM (A)(B)
CRACK INDICATION ON RADIUS NEAR OF THE FIRST HOLE FROM INBOARD SIDE OF 141A6536-14 BEAM # 4 AT SERVICE DOOR / REPLACED BEAM 4 AT SERVICE DOOR AS PER B737-700 SRM 51-40-02;51-10-02 AND DWG 141A6516 SHEET 4 REV D
CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 18 INCH FROM REAR SPAR RT HORIZONTAL STAB / REPAIRED INSPAR RIB LOC STAB STA 120.30 AND 18' FROM REAR SPAR RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4
CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 9 INCH FROM REAR SPAR LT HORIZONTAL STAB / PERFORMED REPAIR ON RIB LOCATED STAB STA 120.30 AND 9 INCH FROM REAR SPAR LT HORIZONTAL STABILIZER IAW SRM B737-700 55-10-09-2R-4 REPAIR 4 FIG 202
CRACK INDICATION ON RADIUS NEAR OF THE FIRST HOLE FROM INBOARD SIDE OF 141A6536-15 BEAM #5 AT SERVICE DOOR / REPLACED BEAM #5 AND FASTENERS ON FWD SERVICE DOOR INTERNAL AREA IAW SRM 737-700;51-40-02;51-10-02 STEP 9 AND DRAWING #141A6516 AND 141A6535 AND DOC NUMBER: 52-41-14093
DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SKIN LOC AT 3IN FROM O/B EDGE ON T/E AREA AT RT WING / REPAIRED I/B MAIN FLAP WEDGE PANEL LOWER SKIN LOC AT 3 IN FROM O/B EDGE ON T/E AREA AT RT WING AS PER B737-700 SRM 57-53-01-2R-7 REPAIR 7 TOOL USED CALIPER PN:700-113-10; S/N:0013226; DUE DATE:10/MAR/21; HOT BONDER PN:HCS9200B; SN:15102320; DUE DATE:14/JUN/20; COATING THICKNESS GAUGE PN:PROSITECTOR 6000N53; SN:767584; DUE DATE:16/JUL/20
REF L/P #1385539 L1 DOOR OUTER SKIN UPPER AFT CORNER BENT REINSPECT EVERY F/C & PERM WITHIN 10 F/C / (CLOSING DMA # 0160237) REPAIRED PER E.A. 1-A52-2338 CLEARING # 29962
L1 ENTRY DOOR OUTER SKIN UPPER AFT CORNER BENT / (CLOSING DMA # 0160236) REPAIRED PER E.A. # 1-A52-2338 CLEARING # 29961
EMERGING EXIT SIGN IN MID CABIN CEILING FELL DOWN HANGING BY WIRE. / INSTALLED LIGHT ASSEMBLY PER AMM.
RT FORWARD WING TO BODY FAIRING TO INBOARD WING LEADING EDGE ATTACH POINT, ATTACH ANGLE CRACKED. R&R ANGLE IAW SRM.
LT FRONT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PACK IAW AMM.
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
INFLIGHT SHUTDOWN/DIVERSION/DECLARED EMERGENCY, PRECAUTIONARY SHUTDOWN OF NR 1 ENG. DUE TO LOW OIL PRESS LIGHT ILLUMINATED. R&R NR 1 ENGINE IAW MT.
RT OVERHEAD BIN EMERGENCY EXIT LIGHT INOP BETWEEN ROW 3 TO ROW 6. R&R BATTERY PACK PER AMM.
AFT CARGO FLOOR PANEL SUPPORT AT-TEE BS780 HAS CORROSION / REMOVED AND REPLACED FLOOR PANEL SUPPORT-TEE PER SRM 51-40-02.
# 6 FLAP TRACK CANOE HAS SKIN CRACK INSIDE AFT SURFACE BELOW LINKAGE / REPAIRED PER EA 1-A57-6168.
# 3 FLAP TRACK CANOE HAS SKIN CRACK INSIDE AFT SURFACE BELOW LINKAGE / REPAIRED PER EA #1-A57-6168.
CABIN FLOOR SUPPORT CRACKED AT BS 540, LBL 1. R&R SUPPORT IAW SRM.
RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REPAIRED AFT FLAP PER SRM.
#1 SEAT TRACK STA 520 TOP OF CROWN HAS WEAR DAMAGE / AREA REPAIRED PER SRM 53-00-52-2R-4.
LT WING TRAILING EDGE WIGGLE PLATE CRACKED AT IRSS 218. R&R WIGGLE PLATE PER SRM.
L1 DOOR SLIDE INADVERTENTLY FELL OUT OF THE CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE IAW MT.
R1 FORWARD WINDOW HEAT ELEMENT ARCED. R & R THE WINDOW IAW AMM.
R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
OVERWING EXIT SIGN LOOSE. SECURED THE SIGN IAW SIP.
MID CABIN CEILING EMERGENCY EXIT LIGHT LENS LOOSE. REINSTALLED THE LENS IAW MM.
R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.
R1 DOOR SLIDE LOOSE. SECURED THE SLIDE IAW MT.
FORWARD ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. RELAMPED LIGHT PER AMM.
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOP RELEASE BROKEN. R & R THE GIRT BAR IAW CMM.
AFT CARGO TRANSITION ANGLE CRACKED AT BS 727B, RBL 21.5. R & R ANGLE IAW SRM.
AFT CARGO TRANSITION ANGLE CORRODED, BETWEEN BS 767 - 727C, RBL 21.5. R & R ANGLE IAW SRM.
AFT CARGO TRANSITION ANGLE CORRODED, BETWEEN BS 767 - 792, RBL 21.5. R & R ANGLE IAW SRM.
AFT CARGO DOOR THRESHOLD WEB CORRODED. R & R WEB IAW SRM.
DOUBLER LOWER FORWARD CORNER CRACKED AT BS 229. REPAIRED DOUBLER IAW EA.
FLOORBEAM CORRODED ON UPPER SURFACE AT BS 312, BETWEEN LBL 14 - 22. REPAIRED BEAM IAW SRM.
SKIN CRACKED AT BS 540, BETWEEN STRINGER 22R - 23R. REPAIRED SKIN IAW EA.
AFT GALLEY FLOOR STRAP CORRODED AT BS 1028, LBL 3. R & R STRAP IAW SRM.
AFT GALLEY FLOOR STRAP CORRODED AT BS 1020, RBL 3. R & R STRAP IAW SRM.
RIGHT OVERWING EXIT EMER LIGHT LENS LOOSE. SECURED LENS IAW MM.
R2 DOOR EMER EXIT LIGHT BROKEN. R & R LIGHT IAW MM.
L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.
LEFT WING EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
FORWARD ENTRY LOWER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.
R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
L1 DOOR SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE IAW MM.
LEFT EEPLS COVER BROKEN. R & R EEPLS IAW AMM.
RIGHT EEPLS COVER BROKEN. R & R EEPLS IAW AMM.
SEAT TRACK AT SPLICE STRAP OTBD FWD FASTENER HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED STRAP IAW EA.
SEAT TRACK AT SPLICE STRAP CRACKED AT BS 727B, LBL 24.75. REPAIRED STRAP IAW EA & ER.
SEAT TRACK AT SPLICE STRAP CRACKED AT BS 727B, LBL 45.5. REPAIRED STRAP IAW EA.
FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED OTBD UPPER CORNER COMMON TO INNER SURFACE & INNER EDGE. REPAIRED FRAME IAW ACO.
LEFT HORIZONTAL STABILIZER RIB CRACKED IN VERTICAL WEB STAB STATION 120.3 AT VERTICAL STIFFENER NR 3. REPAIRED RIB IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED IN VERTICAL WEB STAB STATION 92.7 AT VERTICAL STIFFENER RT NR 3 & 4. REPAIRED RIB IAW SRM.
PRESSURE BULKHEAD CRACKED AT BS 663, BETWEEN RBL 34 TO RBL 34.5. REPAIRED BULKHEAD IAW SRM.
RT OVERWING LOWER EMERGENCY EXIT SIGN MISSING LENS. INSTALLED LENS IAW AMM.
FIBERGLASS PANEL AT CTR WING REAR SPAR VAPOR WEB CRACKED AT LBL 40. REPAIRED PANEL IAW SRM.
L1 DOOR EGRESS LIGHT LENS BROKEN. R&R LIGHT ASSEMBLY IAW MM.
R1 DOOR EGRESS LIGHT LENS BROKEN. R&R LIGHT ASSEMBLY IAW MM.
FORWARD ENTRY LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
L1 DOOR EMERGENCY EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
L1 DOOR EMERGNECY EXIT LIGHT LENS COVER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS LENS MISSING AT ROW 17. INSTALLED LENS PER MM.
EEPLS LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND FWD EELS COVER CRACKED. REMOVED AND REPLACED COVER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 23. RELAMPED PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER MISSING. INSTALLED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT FWD EEPLS COVER CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM.
LT EEPLS COVER DAMAGED AT ROW 1. REMOVED AND REPLACED COVERED PER MM.
EEPLS DAMAGED AT ROW 1. REMOVED AND REPLACED EEPLS LENS PER MM.
L1 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.
DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED MV3 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 1. REMOVED AND REPLACED LENS PER MM.
FWD EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
R1 DOOR WOULD NOT OPEN. CONNECTED BOLT PER MT.
AT FL 390 FLIGHT CREW REPORTED A POSSIBLE ELECTRICAL ODOR IN CABIN, NO SMOKE. TURNED OFF GASPER AND RECIRC FANS ODOR DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM.