N249WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2019-03-27 – 2019-03-27 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2019-03-27 – 2019-03-27 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EXIT SIGN ABOVE COCKPIT FELL OFF. INSTALLED EXIT SIGN ABOVE COCKPIT IAW AMM 33-51-01-960-801, STEP 2.C.
EMERGENCY LIGHT ASSEMBLY OVER FWD ENTRY DOOR INOPERATIVE. SPLICED THE WIRE W4142-0059-20 IAW SWPM 20-30-12 AND PERFORMED GOOD FUNCTIONAL CHECK OF EMERGENCY LIGHT IAW AMM 33-51-00-710-801.
CORROSION ON ACB STRAP UNDER LOWER SILLWEB BS847 RBL21; WL156. REMOVED AND REPLACED ACB STRAP UNDER LOWER SILL WEB BS 847 RBL21, WL156 IAW SRM 51-40-02-0G-0 & DWG146A8340 REV-.
CENTER LINE CEILING EMERGENCY LIGHT BS 623 DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-960-802. TESTED GOOD.
AFT CARGO BAY ANGLE ATTACHED TO THE WEB, BS 827, RBL 19, WL 154 CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 146A8120, REV-.
CORROSION ON ACB LOWER SILL WEB BETWEEN BS 794 - 847, RBL 22, WL 156. REMOVED AND REPLACED THE ACB LOWER SILL WEB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 146A8121, REV-, & DWG 146A8120, REV-.
CORROSION ON ACD NUTPLATE STRAP BS 794 - 794+7, RBL 20, WL 156. REMODED AND REPLACED THE NUTPLATE STRAP IAW SRM 51-40-02-0G-0, & DWG 146A8340, REV-.
AFT CARGO BAY, BS 767 FRAME HAD AN ELONGATED FASTENER HOLE AT RBL 21, WL 156. FORMED A REPAIR FRAME IAW SRM 53-60-07-2R-2, REPAIR 2, DETAIL 4.D (7), TABLE 202. REPAIRED THE FRAMEIAW SRM 53-60-07-2R-2, REPAIR 2.
CORROSION ON ACB LOWER SILL WEB BETWEEN BS 847 - 856, RBL 22, WL 156. REMOVED AND REPLACED THE SILL WEB IAW SRM 51-40-02, AND DWG 146A8120, REV-, & APPLIED CAP SEAL TO THE FASTENERS IAW AMM 51-31-00.
ACB DOOR SURROUND STRUCTURE CORRODED ON THE LOWER INTERCOSTAL WEB, BS 791, RBL 25, WL 159. REMOVED AND REPLACED THE INTERCOSTAL WEB IAW SRM 51-40-02, & DWG 146A8320, REV D.
ACB LWR DOOR SURROUND STRUCTURE SILL STRAP CORRODED ON UPPER SURFACE AT FASTENER HOLE,BS 787 - 827, RBL 25. REMOVED & REPLACED THE SILL STRAP FROM BS 767+7 - 847+15, IAW SRM 51-40-02, DWG 146A8120, REV-, & DWG 146A8340, REV-.
CORROSION ON THE LOWER SILL WEB BETWEEN BS 787 - 794, RBL 22, WL 156. REMOVED AND REPLACED THE LOWER SILL WEB IAW SRM 51-40-05, AND DWG 146A0081, REV B.
ACB LWR DOOR SURROUND STRUCTURE NUTPLATE STRAP CORRODED ON LWR SURFACE AT FASTENER HOLE, BS 784; RBL 25. REMOVED AND INSTALLED THE NUTPLATE STRAP IAW SRM 51-40-02-0G-0, & DWG 146A0081, REV -.
CORROSION ON LT FWD BODY TO SIDEWALL SUPPORT, BS 396 - 495, LBL 21, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 4.A (2) (A) FIGURE 103, DETAIL D.
FORWARD CARGO BAY, CORROSION ON RT AFT BODY TO SIDE WALL SUPPORT, BS 500A - 500B, RBL 22, WL 156. REMOVED AND REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, SRM 53-00-53-1A-2, & DWG 143A7500, REV -.
FCB; CORROSION ON LH AFT BODY TO SIDE WALL SUPPORT STA 507-500D LBL22 WL156. REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT AT BS 395 - 500D, LBL 22, WL 156 IAW SRM 51-40-05 AND DWG 143A7501 0112, REV A.
AFT CARGO INTERCOSTAL BETWEEN BS 767 & 787, RBL 25 CORRODED, TWO LOCATIONS. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-05-0G-0, DWG 146A0081, REV-.
LEFT STABILIZER RIB NR 3, STFFENER NR 3 CRACKED. FOUND DURING AN INSPECTION. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-4.
LEFT WING TRANSVERSE ANGLE, JUST ABOVE AFT PYLON WAS CRACKED IN RADIUS. REMOVED AND REPLACED THE LT WING TRANSVERSE ANGLE IAW SRM 51-40-02 AND DWG 115A2512, REV B.
CORROSION ON THE BULKHEAD, BS 489, STRINGERS 26R - 26L, WL 152. REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD LOWER RAIL, BS 500D, RBL 24 - LBL 24, WL 152 IAW SRM 51-40-02, & DWG 143A7902, REV C.
CORROSION ON ACB FLOOR SUPPORT SPLICE AT BS 767+5 WL157. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02 AND DWG 146A7500 REV -.
AFT CARGO SIDEWALL SUPPORT AT BS 727A, LBL 22, WL 155 CORRODED. SIDEWALL SUPPORT RESOLVED ON CUSTOMER CARD TTG8Q01ASTYM.
AFT CARGO SIDEWALL SUPPORT AT RBL 22, BS 727 - 767 CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, & DWG 146A7500, REV -.
PLASTIC COVER PLATE ABOVE RT OVERWING EMERGENCY EXIT, CRACKED. REMOVED AND REPLACED THE PLASTIC COVER PLATE RT OVERWING WITH A NEW COVER IAW SRM 51-40-02, AND AMM 52-22-00-400-802.
AFT CARGO SIDEWALL SUPPORT AT LBL 22, BS 727 - 847 WAS CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, & DWG 146A7500, REV-.
FLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 232RF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 144A5810, 0151, DUE TO AMOUNT OF ALL DAMAGE.
CRACKED STRINGER 25R, BS 535, WL155. REPAIRED IAW EA 26-153-00644. THIS IS A CATEGORY A REPAIR AS DEFINED IN SRM 51-00-06.
FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241AF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG: 144A5810, 0127.
FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DRAWING 144A5810, SHEET 161.
CRACKED STRINGER 26R, BS 535, WL153. REPAIRED STRINGER 26R BTWN BS 500D & 540, AND APPLIED A FILLET SEAL & CIC IAW SRM 53-00-03-2R-1, REPAIR 1.
CRACKED STRINGER 23 LT, BS 535, WL164. REPAIRED STRINGER 23L BTWN BS 500D & 540, WL 164. APPLIED A FILLET SEAL AND CIC IAW SRM 53-00-03-2R-1, REPAIR 1.
FLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FLOOR PANEL 231XF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, 0126.
FLOOR PANEL 231ZF LOWER SKIN IS DEBONDED NEAR AFT EDGE. FLOOR PANEL 231ZF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 160.
FLOOR PANEL 241BF UPPER SKIN IS DEBONDED NEAR CENTER OF PANEL. FABRICATION OF A NEW FLOOR PANEL REPLACEMENT HAD BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
FLOOR PANEL 241DF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 241DF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 144A5810, 0128.
FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL 241EF & REPLACED IAW SRM 53-00-50-2R-0.
FLOOR PANEL 242AF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242AF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810, SHEET 189.
FLOOR PANEL 242BF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242BF WAS REPLACED IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 122. ;[02] ITEM 1
FLOOR PANEL 242DF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242DF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 150.
CORROSION ON ACD FWD SHIELD WEB BETWEEN BS 767 - 794, RBL 23, WL 156, REMOVED & REPLACED THE SHIELD IAW SRM 51-40-02, AND DWG 146A0081, 0034, REV-.
AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE WAS REPLACED IAW SRM 51-10-02-0G-0, PARAGRAPH 9.
CORROSION ON ACD AFT SHIELD WEB BETWEEN BS 847 - 867, RBL 23, WL 156. REMOVED & REPLACED THE SHIELD IAW SRM 51-40-02, AND DWG 146A0081, 0034, REV-.
CORROSION ON ACD SUB THRESHOLD WEB BETWEEN BS 794 - 847, RBL 26, WL 156. REMOVED AND REPLACED THE SUB THRESHOLD WEB IAW SRM 51-10-02-0G-0, PARAGRAPH 9,
CORROSION ON FCD SUB THRESHOLD WEB BETWEEN BS 440 - 492, RBL 26, WL 156. REMOVED AND REPLACED THE SUB THRESHOLD WEB, IAW SRM 51-40-02-0G-0, & DWG 143A8330, REV A.
CRACKED CROSSBEAM, BS 540, LBL 44, WL 208. REMOVED AND REPLACED CROSSBEAM, BS 540, LBL24 - 45, WL 208, IAW SRM 51-40-02, & DWG 143A5240, REV -.
AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1.
CORROSION ON SEAT TRACK LBL 45, BS 480+17, BS 500+8, BS 500A+8, BS 500B+18. THE SEAT TRACK WILL BE REPLACED ON FAULT TTG8Q01AR96P.
LEFT STABILIZER RIB NR 3, STFFENER NR 3 CRACKED. FOUND DURING AN INSPECTION. REPAIRED THE STIFFENER IAW SRM 55-10-09-2R-4.
FWD ENTRY DOOR SLIDE COVER DETACHED FROM FRAME. REPAIRED THE SLIDE COVER IAW AMM 25-66-01-340-001.
CRACK FOUND ON THE R1 DOOR STUB FRAME .3 INCHES ABOVE SEAL DEPRESSOR, BS 291.5+10, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED R1 DOOR UPPER STUB FRAME IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW STUB FRAME IAW SRM 51-50-05, AND DWG 141A8370, REV D. REINSTALLED R1 DOOR SEAL DEPRESSOR IAW SRM 51-40-02-0G-0 AND DWG: 141A8370 ID:0009 REV: D AND ADJUSTED R1 DOOR FORWARD UPPER LATCH RECIEVER IAW AMM 52-41-00-820-801; 2.N (1); (A); (B); AMM 20-50-11-910-801 AND SRM 51-40-02 PAR 9.
R2 GIRT BAR AFT PLASTIC SPACER IS NOT INSTALLED. INSTALLED SHIMS IN FLOOR BRAKETS AFT SERVICE DOOR IAW AMM 25-66-02-400-801.
FWD SERVICE DOOR GIRT BAR HOLDER LOOSE. REMOVED THE SLIDE & COVER IAW MM 25-66-01. R & R THE FWD SERVICE DOOR GIRT BAR BRACKET IAW SRM 51-40-02. INSTALLED THE SLIDE. REF MT 725-61-06..
OVERWING ESCAPE GROUND ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. REPLACED THE CHARGER ASSY, & BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-06.
OVERWING ESCAPE GROUND ILLUMINATION EMERGENCY LIGHTS INOPERATIVE. REPLACED THE CHARGER ASSY, & BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-51-06.
NUMBER 6 INBD FLAP SUPPORT, FORWARD FAIRING HAS SEVERAL OVERSIZED AND ELONGATED HOLES COMMON TO THE TAILCONE FROM FASTENERS PULLING THROUGH. R & R THE NR 6 FAIRING TAILCONE IAW SRM 51-40-02.
ENGINE FIRE/OVERHEAT DETECTOR FAULT LIGHT ILLUMINATED IN FLIGHT. REFERENCE TTG8Q0164YJ2 FOR REMOVAL AND REPLACEMENT OF #1 ENGINE CORE INBOARD FIRE DETECTION ASSEMBLY REPLACEMENT.
ENG 1 FIRE DETECT LOOP FAULT ILLUMINATED IN FLIGHT A + B. R & R ENG NR 1 FIRELOOP A HARNESS IAW AMM 26-11-02. OPS TEST GOOD.
INTERIOR EMERGENCY AREA LIGHT INOP AT ROW 12ABC. RELAMPED INTERIOR EMERGENCY AREA LIGHT AT ROW 12 ABC PER AMM 33-51-03
INTERIOR EMERGENCY AREA LIGHT AT ROW 9ABC INOPERATIVE. RELAMPED INTERIOR EMERGENCY AREA LIGHT AT ROW 9 ABC PER AMM 33-51-03.
MECHANICAL GRINDING NOISE DURING T/O & CLIMB. NO ABNORMAL ENGINE INDICATIONS NOTED. NOISE AT HIGH POWER SETTINGS ONLY.<[01] COMPRESSOR STALL BOROSCOPE REQUIRED REF AMM 72-00-00-200-804-F00. COMPLIED WITH POWER ASSURANCE RUN REF AMM 71-00-00 TEST 5. CYCLED ON AND OFF. ENGINE ACCESSORIES I.E. HYD PUMP; STBY; HYD PUMP; IDG; BLEED AIR; AIR CONDITIONING PACKS; CYCLED FLIGHT CONTROLS DURING ENGINE RUN. NO ABNORMAL CONDITIONS OBSERVED.;[02] PERFORMED COMPRESSOR STALL BOROSCOPE PER 72-00-00-200-804-F00.
AFT MEGAPHONE IS INOP<[01] R&R AFT MEGAPHONE BATT IAW AMM 25-64-00 OPS GOOD
RIGHT MAIN GEAR HYDRAULIC LEAK.<[01] R/R #4 MLG BRAKE PER AMM 32-41-41. OPS CHECK OK
R1 DOOR SLIDE LOOSE<[01] REMOVE AND REINSTALLED IAW MT725-61-06 AND AMM 25-66-01
PASSENGER CABIN AFT SERVICE DOOR FWD ASSIST HANGLE LOOSE<[01] AFJUSTED AFT SERVICE DOOR FWD ASSIST HANDLE PER AMM 25-21-25-420- STEP 3.B.(5);[02] CORRECTION TO ACTION 1: ADJUSTED AFT SERVICE DOOR FWD ASSIST HANDLE PER AMM 25-21-25-420-801; STEP 3.B.(5);[03] VERIFIED.
PASSENGER CABIN R/H OWE AFT UPPER EXIT LIGHT OUT 2EA<[01] REPLACED LAMPS PASSENGER CABIN R/H OWE AFT UPPER EXIT LIGHT PER AMM 33-51-01-960-801.;[02] REPLACED LAMPS PASSENGER CABIN R/H OWE AFT UPPER EXIT LIGHT PER AMM 33-51-01-960-801 PERFORMED GOOD INSTALLATION TEST.;[03] VERIFIED.
CRACK ON WEB LOCATED BTW BS 986.5 TO BS 1016 AND BTW RBL 36 TO RBL 44 AFT GALLEY AREA FLOOR STRUCTURE 2024-217772<[01] REPLACED WEB LOCATED BTW BS 986.5 TO BS 1016 AND BTW RBL 36 TO RBL 44 AFT GALLEY AREA FLOOR STRUCTURE IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DWG 147A5730 SHEET 22 REV C. SEE INDIVIDUAL SIGNOFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED <BR>RII
CORROSION ANGLE LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT 2024-217760<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 31 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 31 REV -. VERIFIED;[03] CORRECTED STEP ABOVE <BR>REPLACED ANGLE AND FASTENERS LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 31 REV -. RII VERIFIED
CORROSION WEB - INTERCOSTAL LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT 2024-217759<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 146A7500 SHEET 88 REV A; AND DWG 146A7502 SHEET 26 REV-.;[02] CORRECTED STEP 1<BR>REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 146A7500 SHEET 88 REV A; AND DWG 146A7502 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 146A7500 SHEET 88 REV A; AND DWG 146A7502 SHEET 26 REV-. VERIFIED
AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-217755<[01] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO RBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO RBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK ANGLE LOCATED BS540 AND LBL 6 AT AIR CONDITIONING BAY 2024-217745<[01] REPLACED ANGLE LOCATED BS540 AND LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9;[02] REPLACED ANGLE LOCATED BS540 AND LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9
CRACK ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY 2024-217744<[01] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9;[02] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9
AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-217751<[01] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO LBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO LBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK TRAILING EDGE ANGLE LOCATED ON ORSS 267 AT LT WING 2024-217729<[01] REPLACED ANGLE LOCATED TRAILING EDGE ON ORSS 267 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE LOCATED TRAILING EDGE ON ORSS 267 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>COMPLETED TASK
CRACK TRAILING EDGE ANGLE LOCATED ON ORSS 272 AT LT WING 2024-217730<[01] REPLACED ANGLE LOCATED ON ORSS 272 AT TRAILING EDGE LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0.;[02] REPLACED ANGLE LOCATED ON ORSS 272 AT TRAILING EDGE LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0.<BR>COMPLETED
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 290 AT LT WING 2024-217731<[01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE LOCATED ON ORSS 290 AT LT WING. IAW B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A3700 SHEET 38 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETED JOB
CRACK WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2024-217734<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED
CRACK WEB - INTERCOSTAL LOCATED BTW STA 500B TO STA 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT 2024-217737<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500B TO STA 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500B TO STA 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV -. VERIFIED
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING 2024-217732<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. SEE INDIVIDUAL SINGOFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. SEE INDIVIDUAL SIGNOFF BELOW;[03] CERTIFIED WORK PERFORMED
CRACK ON RIB LOCATED LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER 2024-217721<[01] REPLACED RIB AND FASTENERS LOC. LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV 10. SEE INDIVIDUAL SIGN OFF;[02] CORRECTED STEP 1<BR>REPLACED RIB AND FASTENERS LOC. LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED RIB AND FASTENERS LOC. LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV A. VERIFIED
CRACK FRAME ON BS 312 LOCATED BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-217707<[01] PERFORMED PERMANENT REPAIR IAW EA M-22-153-01244 ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA SEE INDIVIDUAL SIGNOFFS BELOW;[02] PERFORMED PERMANENT REPAIR IAW EA M-22-153-01244 ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA SEE INDIVIDUAL SIGNOFFS BELOW<BR>COMPLETED TASK
CRACK ANGLE AFT POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT 2024-217714<[01] REPLACED ANGLE AFT POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -;[02] REPLACED ANGLE AFT POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -
CRACK ANGLE FWD POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT 2024-217715<[01] REPLACED ANGLE FWD POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -;[02] REPLACED ANGLE FWD POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -
CRACK ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT 2024-217720<[01] REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8102 REV.-;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8102 REV.- TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B23316874 DUE DATE 31-JAN-25.;[03] REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8102 REV.- TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B23316874 DUE DATE 31-JAN-25.
CRACK TRACK LBBL 17.24 LOCATED AT BS 727E AFT CARGO COMPARTMENT 2024-217722<[01] TOOL USED ON STEP#4 AND #5; TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S/N: 220272712 CAL DUE DATE: 28-NOV-24.;[02] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 727D TO BS 747 LBBL 17.24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW;[03] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 727D TO BS 747 LBBL 17.24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW<BR>RII
CRACK REAR SPAR BRACKET LOCATED BTW RIB 2 AND RIB 3 ON MLG AREA AT LT WING 2024-217712<[01] REPLACED BRACKET LOCATED BTW RIB 2 AND RIB 3 ON MLG AREA AT LT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED
CRACK ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING 2024-217719<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A2930 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A2930 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>TASK CERTIFIED
CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA 2024-217708<[01] REPLACED NEW INTERCOSTAL; CLIP; STRAP AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DWG#141A8180 SHEET 27 REV. C SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ÿ½TEM 9 AND DWG#141A8180 REV. C SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ÿ½TEM 9 AND DWG#141A8180 REV. C SEE INDIVIDUAL SIGN OFF BELOW<BR>TASK RII CERTIFIED
CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-217709<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 141A1110 SHEET 18 REV -. AND DWG 141A8380 SHEET 21 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] ITEM RII VERIFIED <BR>REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 141A1110 SHEET 18 REV -. AND DWG 141A8380 SHEET 21 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK CHANNEL SUPPORT BETWEEN BS 420 TO BS 440 AND RBL 21 AT FWD CARGO COMPARTMENT 2023-217687<[01] REPLACED CHANNEL SUPPORT BETWEEN BS 420 TO BS 440 AND RBL 21 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED CHANNEL SUPPORT BETWEEN BS 420 TO BS 440 AND RBL 21 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV -. SEE INDIVIDUAL SIGN OFF BELOW.<BR>TASK CERTIFIED
CORROSION LOCATED ON FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-217678<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[04] PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW;[05] PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895-WIP1 24-153-00895-WIP2 EA 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW;[06] CORRECTED STEP 5<BR>PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895-WIP1 24-153-00895-WIP2 EA 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW;[07] CERTIFIED STEP 6 COMPLETE RII<BR>PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895-WIP1 24-153-00895-WIP2 AND EA 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW
CORROSION ON WEB FLOOR STRUCTURE LOCATED BTW BS 1016 TO BS 1040 WL 208.1 LBL 20 AT AFT GALLEY AREA 2024-217680<[01] REPLACED NEW WEB LOCATED ON FLOOR STRUCTURE BTW BS 1016 TO BS 1040 AND BTW BL 0 TO LBL 45 AT AFT GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG:147A5600; SHEET: 32; REV:B. SEE INDIVIDUAL SIGN OFF BELLOW;[02] CORRECTED STEP 1<BR>REPLACED WEB LOCATED ON FLOOR STRUCTURE BTW BS 1016 TO BS 1040 AND BTW BL 0 TO LBL 45 AT AFT GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG:147A5600; SHEET: 32; REV:B. SEE INDIVIDUAL SIGN OFF BELLOW;[03] REPLACED WEB LOCATED ON FLOOR STRUCTURE BTW BS 1016 TO BS 1040 AND BTW BL 0 TO LBL 45 AT AFT GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG:147A5600; SHEET: 32; REV:B. SEE INDIVIDUAL SIGN OFF BELLOW<BR>RII
CRACK TRACK BODY STATION 500A AND RBL 13.84 FWD CARGO COMPARTMENT 2024-217684<[01] TOOL USED ON STEP #4 AND #5; TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; CAL DUE DATE: 28-NOV-24;[02] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 500 TO BS 500B RBL 13.84 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW;[03] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 500 TO BS 500B RBL 13.84 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. RII VERIFIED
CORROSION LOCATED ON FLOOR BEAM 986.5 RBL 41 WL 208.1 AT AFT GALLEY AREA 2024-217689<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00SBPVK.SEE INDIVIDUAL SIGNOFFS BELOW;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00SBPVK.SEE INDIVIDUAL SIGNOFFS BELOW
CRACK ON WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2024-217640 CRACK ON WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 45.6 AT FWD GALLEY AREA<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -<BR>COMPLETED RII VERIFIED
CRACK ON WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA 2024-217639 CRACK ON WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 45.6 AT FWD GALLEY AREA<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -<BR>COMPLETED RII VERIFIED
CRACK ON WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA 2024-217638<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV. - SEE INDIVIDUAL SIGN OF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 REV. - SEE INDIVIDUAL SIGN OF BELOW.;[03] REPLACED WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 REV. - SEE INDIVIDUAL SIGN OF BELOW.
CRACK ON WEB INTERCOSTAL LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2024-217637<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400; SHEET 20; REV -<BR>SEE INDIVIDUAL SIGN OFF;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400; SHEET 20; REV -<BR>SEE INDIVIDUAL SIGN OFF<BR>COMPLETED TASK ITEM RII
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN 2024-217642<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A.
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-217644<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN 2024-217643<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5410; SHEET 38; REV: A SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 52 AT FWD GALLEY AREA 2024-217649<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 RBL 50.50 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 14 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 RBL 50.50 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 14 REV -. SEE INDIVIDUAL SIGN OFFS BELOW. CERTIFIED AS RII.
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-217645<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02; AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02; AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED RII
CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.980 INCHES. 2024-217575<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60007161486; CAL DUE DATE: 28-JUL-24;[02] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUAL SIGN OFF BELLOW.;[03] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUAL SIGN OFF BELLOW.<BR>RII VERIFIED
CRACK ENTRY DOOR CUT OUT BRACKET ASSY ON POSITION LOWER REVEAL PANEL AT FWD GALLEY AREA (1 EA) 2024-217479<[01] REPLACED ENTRY DOOR CUT OUT BRACKET ASSY ON POSITION LOWER REVEAL PANEL AT FWD GALLEY AREA (1 EA) IAW SOPM 20-50-01 REV.38;[02] REPLACED ENTRY DOOR CUT OUT BRACKET ASSY ON POSITION LOWER REVEAL PANEL AT FWD GALLEY AREA (1 EA) IAW SOPM 20-50-01 REV.38. VERIFIED
DETERIORATED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT FWD GALLEY AREA (2 EA) 2024-217333<[01] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-31-420-802 STEP 3.B.(6);[02] COMPLETED
DETERIORATED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT AFT GALLEY AREA (2 EA) 2024-217334<[01] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5);[02] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5). CERTIFIED
DETERIORATED SERVICE DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA (2 EA) 2024-217335<[01] REPLACED SERVICE DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5);[02] C REPLACED SERVICE DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5). CERTIFIED
(CUSTOMER REQUEST) DEBONDED OB AFT FLAP AT LT WING. PERFORMED INTERIM REPAIR OF OB AFT FLAP AT LT WING IAW B737-700 SRM 57-53-01-2R-16. REPAIR 16; AN REPAIR REQUIERES TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS;WHICHEVER COMES FIRST SEE INDIVIDUAL SIGN OFFS BELOW.;[10] PERFORMED INTERIM REPAIR OF OB AFT FLAP AT LT WING IAW B737-700 SRM 57-53-01-2R-16. REPAIR 16; AN REPAIR REQUIERES TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS;WHICHEVER COMES FIRST RII COMPLETED
DETERIORATED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2024-217337<[01] REPLACED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA IAW B737-700 AMM 25-21-31-420-802 STEP 3.B (6);[02] COMPLETED JOB
SCRATCH ON STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING FROM STA 727B TO 887 RT AND LT SIDE AT PASSENGER CABIN (6 EA) 2024-217317<[01] TASK AMM 33-51-15-400-802 COMPLETED;[02] STEP 1 CORRECTED<BR>REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING FROM STA 727B TO 887 RT AND LT SIDE AT PASSENGER CABIN (6 EA) IAW B737-700 AMM 33-51-15-400-802;[03] CERTIFIED WORK PERFORMED
EMX LIGHT BATT M01669 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01669 PER AMM 33-51-06
EMX LIGHT BATT M01672 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX LIGHT BATT M01672 PER AMM 33-51-06
LEFT FLAP EMERGENCY EXIT LIGHT IS OUT<[01] R/R THE LAMP FOR THE LEFT FLAP EMERGENCY EXIT LIGHT ASSY; OP?S CHECKS IAW AMM 33-51-04.
RIGHT OVERWING EMERGENCY EXIT LIGHT IS OUT.<[01] R/R THE LAMP FOR THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSY; OP?S CHECKS IAW AMM 33-51-04.
L-2 DOOR ASSIST HANDLE CLOSEST TO WINDSCREEN IS CRACKED IN HALF.<[01] REPLACED L2 DOOR ASSIST HANDLE CLOSEST TO WINDSCREEN IAW AMM-25-21-25-420-801 3 ; B; 5;[02] VERIFIED
DOT A24-1 LH WING I/B L/E. LEADING EDGE / PANEL SUPPORT ANGLE CRACKED AT FORWARD LOWER CORNER FOR PANEL 195AL.<[01] VERIFIED <BR>AUDIT C/W
CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE STA 663 AT LBL 8 (WL 167) HFEC CUT LINE IAW B737 NDT P6 51-00-00 P23. NO CRACKS NOTED;[02] REMOVED DAMAGED SECTION CENTER TANK LOWER ATTACH ANGLE AT STA 663; LBL 8; W/L 167 AND REPAIRED IAW SRM 57-10-10-2R-5 PERFORMED LEAK CHECK OF AREA IAW AMM 28-11-00-300-801 NO LEAKS NOTED. AUDIT C/W.
LEFT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT APPROX LBL 35<[01] RECEIVED NEW PART; VAPOR BARRIER WEB; PN 111A1151Y9 ATAG WN34116 IAW BOEING DWG 111A1001 ID:0354 REV B;[02] NEW VAPOR BARRIER PART TO BE INSTALLED ON WO# 45078 5000 0022 (TTG8Q00MVZBF);[03] UPDATED PARTS INFO
RIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT APPROX RBL 30<[01] REMOVED AND REPLACED WEB 111A1151-10 ON SHELF IAW DWG 111A1001 AND 111A1151;[02] VERIFIED ITEM 1<BR>AUDIT C/W
FLAP DISAGREE FLAP HANDLE AND GAUGE NOT IN AGREEMENT WITH HANDLE POSITION. RAN QRH FOR TRAILING FLAP FLAP DISAGREE. LANDERS FLAPS 15 W/ALTERNATE EXTENSION. FC 27-52259<[01] REPLACED L/H FLAP POSITION X-MITTER REF. AMM 27-58-01. ALSO REPLACED CANNON PLUG D00275 REF. SWPM 20-61-00. OPS CHECKS GOOD.
FORWARD L/H WIND SCREEN ; LOWER FLASHLIGHT ATTACH HOUSING BROKEN. FORWARD L/H WIND SCREEN LOWER FLASHLIGHT ATTACH HOUSING BROKEN.<[01] PLACED ON MEL 25-12-01 SP1B<BR>AUTHORIZATION # 123521;[02] REMOVED AND REPLACED EMERGENCY FLASHLIGHT HOLDER REF CMM <BR>25-31-08
L/H AFT EMERGENCY LIGHT INOPERATIVE. R & R AFT BATTERY PACK AT M1673 POWER SUPPLY IAW AMM 33-51-06; OPS CHECKED GOOD.
PART OF LEFT OVER WING EXIT DOOR MISSING.<[01] UPON INSPECTION; FOUND LOWER CLOSEOUT PANEL DOWN AND NOT IN CORRECT POSITION. OPENED AND CLOSED DOOR; AND INSURED CLOSEOUT PANEL IN CORRECT POSITION PER AMM 52-22-00
BOTTOM PORTION OF R2 ESCAPE SLIDE IS IMPEDING DOOR OPERATION. / [01] ADJUSTED BOTTOM PORTION OF R2 SLIDE PER AMM 25-66-01.
AFT SERVICE DOOR SLIDE GAUGE IN RED / [01] RR AFT SERVICE DOOR SLIDE PER TASK CARD 725-61-06-AS
PASSENGER CABIN R/H OVER-WING EXIT DOOR EMERGENCY LIGHT INOP. / [01] RELAMPED PASSENGER CABIN R/H OVER-WING EXIT DOOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.
FWD CARGO SIDEWALL SUPPORT BRACKET;SHOWS INB SURFACE CRACKED AT B.S.540D STR 18L MKD / [01] REMOVED AND REPLACE SUPPORT BRACKET AT FWD CARGO STA 500D STR 18L IRW SRM 51-40-02;[02] VERIFIED 1;COMPLETE
FWD CARGO SIDEWALL SUPPORT BRACKET;SHOWS INB SURFACE CRACKED AT B.S.540D STR 18R MKD / [01] REMOVED AND REPLACED FWD CARGO SUPPORT BRACKET AT STA 500D STR 18R IRW B737-700 SRM 51-40-02;[02] VERIFIED 1;COMPLETE
AFT CARGO L/H Z CHANNEL HAVE MULTIPLE CORROSION EVIDENCE AROUND THE HOLES FASTENER FROM STA 727 TO STA 847. / [01] REMOVED CORROSION AFT CARGO COMP Z CHANEL L/H FROM STA 727 TO STA 847;[02] CORRECTION: REMOVED CORROSION AFT CARGO COMP Z CHANEL L/H FROM STA 727 TO STA 847 AS PER B737 SRM 51-10-02-0G-0.;[03] VERIFIED STEP 1 AND 2.;[04] EVALUATED REWORKED AREA AT AFT CARGO COMP. L/H Z CHANNEL;CORROSION PASS THRU ALONG Z CHANNEL FROM STA 727 TO STA 847. FOUND OUTS OF LIMITS PER REF B737-700 SRM 53-00-53-1A-2.;[05] VERIFIED STEP 4.;[06] RECEIVED NEW ZEE CHANNEL FROM STA 727 TO STA 847 L/H AFT CARGO COMP. INSTALLATION OF THIS ZEE CHANNEL IS ACCOMPLISHED ON CARD.(TTG8Q004D650).;[07] REMOVED CORROSION AFT CARGO COMP ZEE CHANEL;EVALUATED REWORKED AREA AT ZEE CHANNEL;CORROSION PASS THRU;FOUND OUT OF LIMITS;RECEIVED NEW ZEE CHANNEL FROM STA 727 TO STA 847 L/H AFT CARGO COMP. INSTALLATION OF THIS ZEE CHANNEL IS ACCOMPLISHED ON CARD.(TTG8Q004D650). PER REF B737-700 SRM 53-00-53-1A-2.;[08] VERIFIED STEP 6 AND 7.
AFT CARGO COMP. DOOR CUTOUT SECTION AFT SHIELDS HAVE CORROSION EVIDENCE AROUND THE HOLE FASTENER. / [01] REMOVED CORROSION AFT CARGO COMP DOOR CUTOUT AFT SHIELDS PER B-737-700 REF SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.024'<BR>TOOL USED :DAKOTA ULTRA SONICS B/C: 16686 CALIBRATION DUE : 06/22;[04] EVALUATED REWORKED AREA.ORIG.MAT. 0.050'';MAT:REMAINIG 0.024'; MAT.LOST. 0.026'; FOUND TO BE.OUT OF LIMITS. PER REF; B737-700-SRM 53-60-15-1A-1;[05] VERIFIED STEP 4.;[06] LOCATED DRILLED NEW SHIELDS PLATE AT AFT CARGO COMP PER B 737-700 SRM 51-40-05-0G-0;[07] VERIFIED STEP 6. OK TO TREAT AND PRIMER.;[08] TREATED AND PRIMED PER B737-700 SRM 51-21-41-370-802; 51-21-72-370-804.;[09] REMOVED CORROSION AFT SHIELDS; EVALUATED REWORKED AREA.ORIG.MAT. 0.050'';MAT:REMAINIG 0.024'; MAT.LOST. 0.026'; FOUND TO BE.OUT OF LIMITS. PER REF; B737-700-SRM 53-60-15-1A-1; RECEIVED NEW PART LOCATED DRILLED NEW SHIELDS PLATE AT AFT CARGO COMP PER B 737-700 SRM 51-40-05-0G-0.;[10] VERIFIED STEPS 8 AND 9.
AFT CARGO R/H Z CHANNEL HAVE MULTIPLE CORROSION EVIDENCE AROUND THE HOLES FASTENER FROM STA 727E TO STA 767. / [01] REMOVED CORROSION AFT CARGO COMP R/H Z CHANNEL FROM STA 727E TO STA 767 PER B-737-700 REF SRM 51-10-02-0G-0;[02] EVALUATED DAMAGE ZEE CHANNEL AT AFT CARGO COMP. CORROSION PASS THRU; ALONG ZEE CHANNEL; FOUND TO BE OUT OF LIMITS PER REF B737-700 SRM 53-00-53-1A-2.;[03] VERIFIED STEPS 1AND 2.;[04] REMOVED CORROSION; EVALUATED DAMAGE ZEE CHANNEL FROM STA 727E TO STA 767 R/H AT AFT CARGO COMP.FOUND EXFOLIATING CORROSION PASS THRU ; OUT OF LIMITS PER REF B737-700 SRM 53-00-53-1A-2 ; RECEIVED NEW ZEE CHANNEL AFT CARGO COMP FROM STA 727 TO STA 767 R/H SIDE; ZEE CHANNEL INSTALLATION IS ACCOMPLISHED ON CARD TTG8Q004D650.;[05] VERIFIED STEP 4.
AFT CARGO COMP. FLOOR BOARD SPLICE STRAP AT STA 772.5 HAVE CORROSION EVIDENCE AROUND THE HOLE FASTENER. / [01] REMOVED CORROSION AFT CARGO COMP SPLICE STRAP AT STA 772.5 PER B737-700-SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.056'<BR>TOOL USED : OLYMPUS 45MG B/C 167381 11/22;[04] EVALUATED REWORKED AREA; ORIGI. MAT. 0.070'; MAT. REMAINING 0.056'; MAT LOST 0.014';FOUND TO BE OUT OF LIMITS; PER REF B737-700 SRM 53-00-53-1A-2.;[05] VERIFIED STEP 4.;[06] REMOVED CORROSION;EVALUATED AREA;MAT.ORIGINAL 0.070'; MAT. REMAINING 0.056'; MAT. LOST 0.014';FOUND TO BE OUT OF LIMITS; RECEIVED NEW FLOOR BOARD SPLICE STRAP AT STA 772.5 AFT CARGO COMP.; INSTALLATION IS ACCOMPLISHED ON CARD TTG8Q004D650.;[07] VERIFIED STEP 6.
AFT CARGO COMP. DOOR CUTOUT SECTION FWD SHIELDS HAVE CORROSION EVIDENCE AROUND THE HOLE FASTENER. / [01] REMOVED CORROSION AFT CARGO COMP DOOR CUTOUT FWD SHIELDS PER B737-700 REF SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.031'<BR>TOOL USED :DAKOTA ULTRA SONICS B/C: 16686 CALIBRATION DUE 06/22;[04] EVALUATED REWORKED AREA .ORIG. MAT. 0.050';MAT.REMAINING 0.031';MAT. LOST 0.019';FOUND TO BE OUT OF LIMITS. PER REF B737-700 SRM 53-60-15-1A-1;[05] VERIFIED STEP 4.;[06] LOCATED AND DRILLED NEW SHIELDS PLATE PER B 737-700 REF SRM 51-40-05-0G-0;[07] VERIFIED STEP 6. OK TO TREAT AND PRIMER.;[08] TREATED AND PRIMED HOLES ON NEW SHIELDS PLATE PER B 737-700 AMM 51-21-41-370-802 AND AMM 51-21-72-370-804;[09] VERIFIED STEP 8.;[10] REMOVED CORROSION AT AFT CARGO COMPART FWD SHIELD; PERFORMED NDT INSPECTION AND FOUND OUT OF LIMITS AS PER REF B737 SRM 51-10-02-0G-0 AND SRM 53-60-15-1A-1; LOCATED AND DRILLED NEW FWD SHIEL AS PER REF B737 SRM 51-40-05-0G-0.;[11] VERIFIED STEP 10.
AFT CARGO PANEL FWD CUTOUT 142KW LOWER SIDE IS DETERIORATED (228-012). / [01] RECEIVED NEW PANEL 142KW AFT CARGO COMP. FWD DOOR CUTOUT; PANEL 142KW INSTALLATION IS ACCOMPLISHED ON CARD TTG8Q00B7SW6.;[02] VERIFIED STEP 1.
L/H MLG MIDDLE DOOR HAS CRACK / [01] REMOVED L/H MLG CENTER DOOR PER REF 737 AMM 32-13-11-000-802;[02] OK TO INSTALL L/H MLG NEW CENTER DOOR.;[03] OK TO INSTALL L/H MLG NEW INNER DOOR.;[04] INSTALLED L/H MLG CENTER DOOR IAW-AMM-B737/700-32-13-11-420-802 UP TO STEP 3.H 5(H) AND INSTALLED L/H MLG INNER DOOR IAW-AMM-B737/700/32-13-11-420-804 UP TO STEP 5.H (H);[05] VERIFIED STEP 4.;[06] FINALIZED INSTALLATION AND ADJUSTMENT OF LEFT MLG CENTER AND INNER DOOR AS PER B737 AMM 32-13-11-420-802 AND AMM 32-13-11-420-804.;[07] TORQUE WRENCH USED B/C 167849 AND BONDING METER USED B/C 168692.;[08] VERIFIED FINAL INSTALLATION AND ADJUSTMENT;STEP 6 AND 7.
F/A REPORTS AFT SERVICE DOOR ASSIST HANDLE IS NOT PROPERLY SECURED / [01] R&R AFT SERVICE DOOR ASSIST HANDLE LOWER NUT. REFERENCED AMM 25-21-25.
AFT SERVICE DOOR ASSIST HANDLE IS BROKEN / [01] REMOVED AND REPLACED AFT SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31
FWD LEFT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP / [01] R&R'D LEFT FORWARD CABIN EMERGENCY EXIT LIGHTS BATTERY PACK PER AMM 33-51-06
RAMP REPORTS FWD CARGO FLOOR AREA C HAS 2 INCH CRACK IN FLOOR BOARD ; / [01] REAIRED FLOOR BOARD IAW AMM 25-52-01
SUPPLEMENTAL INFORMATION: M1670 EMERGENCY EXIT BATTERY PACK INOP. ; / [01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK. OPS NORMAL. REF AMM 33-51-06.
ON APPROACH WENT FROM FLAPS 5 TO 15; FLAPS SPLIT AT FLAPS 10; FLAPS LOCKED OUT; UNEVENTFUL LANDING; PSEU LIGHT ILLUMINATED AFTER LANDING. ; / [01] R&R FLAP POSITION INDICATOR;PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.; [02] R&R FLAP POSITION INDICATOR; PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.
ON APPROACH WENT FROM FLAPS 5 TO 15; FLAPS SPLIT AT FLAPS 10; FLAPS LOCKED OUT; UNEVENTFUL LANDING; PSEU LIGHT ILLUMINATED AFTER LANDING. ; / [01] R&R FLAP POSITION INDICATOR;PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.; [02] R&R FLAP POSITION INDICATOR; PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.
AFT GALLEY F/O SIDE EXIT/SLIDIA SIGN DISCONNECTED ; / [01] REINSTALLED SIGN IAW AMM 33-51-01
AFT LAV FIRE ALARM SOUNDED ON APPROACH. NO SMOKE, FIRE OR FUMES NOTED. REMOVED & REPLACED AFT LAV SMOKE DETECTOR, IAW MM 26-14-01. ALSO COMPLIED WITH SELF TEST TASK 26-14-00-710-802. OPERATIONS CHECKED OK. ALSO INSPECTED THE AFT LAV SMOKE TEMP STRIP. NO ABNORMALITY NOTED, IAW MM REF 26-24-01.
RT OVERWING EMERGENCY LIGHT INOPERABLE. RELAMPED PER AMM 33-51-00.
DORSAL FIN #8 RIB ASSY (P/N 174A1008-2) CRACKED AT LH AND R/H SIDES JUST OUTBD OF MOUNT BRACKETS / REMOVED AND REPLACED DORSAL FIN #8 RIB ASSY (P/N 174A1008-2) PER SRM 51-10-02;INSTALLED FASTENERS PER SRM 51-40-02.
EMERGENCY LIGHT AT 11DEF INOP. / REMOVED; REPLACED AND OPS CHECKED GOOD EMERGENCY LIGHT AT 11DEF PER AMM 33-51-03.
CABIN FLOOR BOARD 231ZF HAS A DAMAGED INSERT. (MARKED) / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00.
CABIN FLOOR BOARD 241BF HAS NUMEROUS DENTS. / REMOVED AND REPLACED PNL 241BF PER AMM 53-21-00
REMOVED CABIN FLOOR PANEL 231WF FOM. ( # 1 SEAT TRACK REPAIR ) / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00.
CABIN FLOOR BOARD 242BF HAS NUMEROUS DENTS. / REMOVED AND REPLACED PNL 242BF PER AMM 53-21-00
CABIN FLOOR BOARD 242AF HAS NUMEROUS DENTS. / REMOVED AND REPLACED FLOOR BOARD 242AF WITH NEW FLOOR BOARD PER AMM 53-21-00.
AFT CARGO LH CAP STRIP CORRODED. / REMOVED AND REPLACED CAP STRIP PER SRM 51-10-02
PASSENGER CABIN #2 SEAT TRACK STA 520 TOP FLANGE HAS DAMAGE. / REMOVED AND REPLACED #2 SEAT TRACK BS 500C +10- 520 PER SRM 53-00-52-2R-4.
FWD SERVICE DOOR UPPER -15 BEAM ; H.F.E.C CRACK INDICATION IN RADIUS. / REMOVED AND REPLACED FWD GALLEY SERVICE DOOR PER SI 14079. PRESSURE LEAK WILL BE PREFORMED ON NRC G725120. TAG NO: 669660 PN ON: 141A6516-3M SN ON: 000015 PN OFF: SN OFF: 000378
AFT CARGO RH CAP STRIP CORRODED. / REMOVED AND REPLACED CAP STRIP PER SRM 51-10-02
FWD ENTRY DOOR SLIDE GIRT HAS BLACK COVERING WORN / REPLACED SLIDE PER SWA TASKCARD 725-61-06 TAG NO: 693248 PN ON: 5A3307-7 SN ON: BNG15711 PN OFF: SN OFF: BNG9273
FWD CARGO AFT SCUFF PLATE HAS CRACK. / REMOVED AND REPLACED AFT CORNER SCUFF PLATE PER AMM 53-11-02-420-801.
MAIN CABIN #1 SEAT TRACK STA 673 LUG BROKEN / REMOVED; AND REPLACED SEAT TRACK. REF. SRM. 51-40-02
AFT CORNER SCUFF PLATE CASTING ON AFT CARGO DOOR OPENING IS CRACKED / REMOVED AND REPLACED AFT CORNER SCUFF PLATE PER AMM 53-11-02. PRESSURIZATION LEAK CHECK GOOD PER AMM 05-51-91.
R/H WING #8 SLAT LOWER SKIN IS CRACKED AT 2EA. FASTNER HOLES AT ACTUATOR RIB. VERIFIED WITH 10X MAGNIFICATION. MRKD / REPAIRED #8 SLAT PER SRM 57-42-01-2R-8 ALTERNATIVE 1; SEE WIPS AND SUB TASKS FOR INDIVIDUAL SIGNOFFS
COCKPIT FLOOR DENTED UNDER SECOND OBSERVERS SEAT / REPAIRED COCKPIT FLOOR PER EA 1-A53-33179 AND SRM 53-10-51
FIRST OFFICERS AFT I/B SEAT TRACK IS WORN. / REMOVED AND REPLACED SEAT TRACK PER M/M 25-11-11.
CAPTAINS AFT I/B SEAT TRACK IS WORN. / REMOVED AND REPLACED SEAT TRACK PER M/M 25-11-11.
R1 DOOR EMERGENCY EXIT SLIDE NOT ALIGNED. REPOSITIONED SLIDE PER MT.
L2 DOOR EVACSLIDE EMERGENCY LIGHT INOP. CLEANED BULB & CONTACT. OP CK GOOD REF AMM
L/H HORIZONTAL STABILIZER CRACKED OUTBOARD OF STA. 285.90, ON THE LOWER FRONT SPAR. R&R ELEVATOR IAW AMM.
FORWARD ENTRY GALLEY LIGHT ASSEMBLY HAD STRONG BURNT ELECTRICAL SMELL COMING FROM ABOVE. R&R BATTERY PER AMM.
FORWARD ENTRY GALLEY LIGHT ASSEMBLY HAD STRONG BURNT ELECTRICAL SMELL COMING FROM ABOVE. R&R POWER SUPPLY CHARGER PER AMM.
RT LOWER FORWARD EMERGENCY OVERWING DOOR SIGN INOP. RELAMPED SIGN PER AMM.
FORWARD LAVATORY AFT WALL EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED L1 DOOR. R&R LIGHT ASSEMBLY IAW AMM.
VERTICAL STAB LEADING EDGE PANEL 322B; INTERNAL SHIELD PANEL IS CRACKED 47' FROM LOWER EDGE; BL0 / REMOVED AND REPLACED VERTICAL STAB L/E PANEL 322B INTERNAL SHIELF PANEL IAW BOEING DWG 176A 1001 REV:B AND B737 SRM 51-40-02-0G0 ATAG SPO368
LEFT MAIN WHEEL WELL BOWTIE FAIRING IS CRACKED BS 727+2' LBL 24-48 / PERFORMED FIBERGLASS REPAIR ON CRACKED AREA OF LEFT W/W BOWTIE FAIRING IAW 737-700 SRM 51-70-04-2R-10
PASSENGER CABIN FLOOR PANEL 221BF 'EAR' IS BROKEN / EVALUATED; PREPPED; CLEANED AND REPAIRED DAMAGE TO UPPER AND LOWER FACESHEETS INCLUDING CORE AREA ON FLOORBOARD 221BF IAW B737 SRM 53-00-50-2R-6; PAR 3(A-K1; L1-M1) REV 64.
FWD CARGO COMPARTMENT L/H BAFFLE AT BS500 TO 500A CRACKED AT FORWARD END. / REMOVED AND REPLACED BAFFLE; P/N 143A7510-15; IN FWD PIT AT STA500 TO STA 500A IAW B737 DRAWING 143A7505 REV- AND SRM 51-40-02-0G-0 STEP 4
CENTER WING BOX LOWER VAPOR BARRIER UPPER CHORD CRACKED AT BS 663, RBL 7. REPAIRED CHORD IAW EA.
MAIN CABIN FLOORBOARD 242VF LARGE STRAND COMPOSITE PEELING OFF. / EVALUATED AND REPAIRED MAIN CABIN FLOORBOARD 242VF OF UPPER SHEET DAMAGE ONLY IAW B737 SRM 53-00-50-2R-0 REV 64 AND B737 SRM 53-00-50-2R-1 REV 64
R2 DOOR CREASE BEAM CORRODED BETWEEN BS 951 TO 992.8. R & R THE CREASE BEAM IAW SRM & DWG.
CABIN FLOOR SUPPORT STA 540 BL 0 TO LBL 24 CRACKED. / REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 BLO-LBL 24 IAW BOEING 737-700 SRM 51-40-02-0G-0 PG. 3 AND BOEING DWG 143A0060 A-TAG WN8486
CABIN FLOOR SUPPORT STA 540 RBL 26 TO RBL 44 CRACKED / REMOVED AND REPLACED FLOOR SUPPORT STA 540 RBL 26 TO RBL 44 IAW 737-700 DWG 143A0060 ATAG WN0414
CABIN FLOOR SUPPORT STA 540 BL 0 TO RBL 24 CRACKED. / REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 BLO-RBL 24 IAW BOEING 737-700 SRM 51-40-02-0G-0 PG 3 AND BOEING DWG 143A0060 A-TAG WN0034
FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW DWG AND SRM.
L1 DOOR AT UPPER SILL WEB AT BS 312, BETWEEN STRINGERS 5L TO 6L, STIFFENER CRACKED. REPAIRED THE STIFFENER IAW EA.
L1 DOOR SURROUND STRUCTURE CREASE BEAM CRACKED AT BS 299, AT FASTENER IN VERTICAL FLANGE. R & R THE CREASE BEAM IAW SRM AND DWG.
L1 DOOR SURROUND STRUCTURE CREASE BEAM ATTACH ANGLE CORRODED BETWEEN BS 316 TO BS 340, LBL 60. R&R ANGLE IAW SRM AND DWG.
FORWARD ENTRY (L-1) DOOR SURROUND STRUCTURE CREASE BEAM SCUFF PLATE SUPPORT 'Z' STA 319-340 LBL 63 HAS CORROSION / REMOVED CORROSION IAW SRM 51-10-02-0G-0; VISUAL INSPECTION WITH A 10X MAG GLASS; NO DEFECTS FOUND; ORIGINAL .080 REMAIN .060 LOSS .020 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-01-1. REMOVED AND REPLACED FWD ENTRY DOOR SURROUND STUCTURE CRESE BEAM SCUFF PLATE SUPPORT Z ANGLE STA 319-340 LBL 63 IAW BOEING DWG 141A8110 SHT 11 REV:-. RESTORED FINISH IAW AMM 51-21-91-620-802. TOOL 40084 DUE 24AUG18 ATAG WN0658
FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM & DWG.
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 11. R&R INTERCOSTAL IAW DWG AND SRM.
R1 DOOR SURROUND STRUCTURE FORWARD LOWER STUB FRAME CRACKED AT BS 294, RBL 53. REPAIRED STUB FRAME IAW EA.
R1 DOOR SURROUND STRUCTURE CREASE BEAM CORRODED BETWEEN BS 319 TO BS 328, RBL 58. R&R CREASE BEAM IAW SRM AND DWG.
R1 DOOR SURROUND STRUCTURE CREASE BEAM ATTACH ANGLE CORRODED BETWEEN BS 301 TO 325, RBL 59. R & R THE ATTACH ANGLE IAW SRM AND DWG.
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW DWG AND SRM.
BULK HEAD 663; LEFT HAND SIDE LOWER SECTION CRACKED AT HEAT EXCHANGER COMMON RIB [MARKED] / REPAIRED BULKHEAD 663 L/H LOWER SIDE VAPOR BARRIER WEB IAW B737-700 SRM 51-70-02-02R-10; 51-70-04-2R-0
CAPTAIN'S FWD SEAT TRACK CORRODED. R & R THE SEAT TRACK IAW SRM & MM.
FIRST OFFICER'S FWD SEAT TRACK CORRODED. R & R THE SEAT TRACK IAW SRM & MM.
RUDDER MIDDLE BALANCE WEIGHT IS CORRODED. / REMOVED AND REPLACED RUDDER MIDDLE BALANCE WEIGHT IAW AMM 51-21-73-370-804 STEPS 4E (1-4). B737 CMM 55-40-09 PG 201 STEPS 2C3 (A;B). ATAG-540181
RIGHT WING TRAILING EDGE JUST INBOARD OF NR 6 FLAP TRACK, WAFFLE PLATE CRACKED. R & R THE PLATE IAW SRM.
L1 DOOR LOWER THRESHOLD CRACKED AT AFT END / REPAIRED L1 DOOR THRESHOLD IAW 1-A53-2076 REV 11 ACCOMPLISHED ON SHOP W/O 37353-2400-0001.
FORWARD CARGO LT SIDE ZEE ANGLE CRACKED AT FORWARD SIDE OF BS 500B, STRINGER 25L. R & R THE ANGLE IAW SRM AND DWG.
AFT CARGO BAY FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 727C TO 727E+10. REPAIRED THE FLOOR SUPPORT ANGLE IAW SRM.
AFT CARGO PIT THRESHOLD WEB HAS CORROSION AS MARKED. / REMOVED AND REPLACED AFT CARGO PIT THRESHOLD WEB IAW BOEING DWG 146A8240 REV:- AND B737 ARM 51-40-02-0G-0
AFT CARGO COMPARTMENT FLOOR STRUCTURE 767+6' LBL 22 TO RBL 22: FLOOR PANEL SPLICE STRAP CORRODED. / REPLACED FLOOR PANEL SPLICE PLATE IN AFT CARGO COMPARTMENT FLOOR STRUCTURE 767+6' LBL 22 TO RBL 22. PART RETURNED TO SHELF. 'A'TAG WN0693
FWD CARGO RH SIDE; AFT OF CARGO DOOR CUT-OUT; SIDE SHIELD HAS MULTIPLE AREAS OF CORROSION FROM STA-492 TO STA-500A STR-25R. (MARKED) / REMOVED CORROSION AT BS 492-BS 500A STR 25R SIDE SHIELD I/A/W SRM 51-10-02 USED 10X NO FURTHER CORROSION. VERIFIED MAT. LOSS ORIG 'T' .032'' MAT. LOSS .006' REMAINING 'T' .026' OUT OF LIMITS I/A/W SRM 53-00-53-1A-2 STEP 4A(2)(A) DETAIL D. LOCATED; DRILLED AND INSTALLED I/AW SRM 51-40-05; SRM 51-40-02 AND BOEING DWG 143A0080
AFT CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE ZEE ANGLE CORRODED BETWEEN BS 727C TO BS 727E+10. R&R ZEE ANGLE IAW SRM.
AFT CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE ZEE ANGLE CORRODED BETWEEN BS 727E+10 TO BS 787. R&R Z ANGLE IAW SRM.
R1 DOOR TOP AFT EMERGENCY SLIDE COVER ATTACH GROMMET STAND CRACKED. R & R THE ISOLATOR IAW SRM.
FUSELAGE ZEE ANGLE CORRODED AT BS 400 TO 442, STRINGER 25L. REPAIRED THE ANGLE IAW SRM.
AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE STA 767-787 RBL 22; ZEE SHIELD CORRODED AROUND FASTENER HOLES. / REMOVED AND REPLACED ZEE AHIELD AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE STA 767-787 RBL 22 IAW BOEING DWG 146A0081 REV:- AND B737 SRM 51-40-+02-0G-0
AFT CARGO FLOOR PANEL 140DF; AFT CAP STRIP HAS CORROSION ON BOTTOM SIDE / FABRICATED NEW CAP STRIP AFT CARGO PANEL # 140DF IAW BOEING DWG # 453A2610 REV D AND BOEING DWG# 453A2600 REVD. SMAL GRANTED FOR NEW CAP STRIP P/N 453A2611-5 ON CONTROL#270176094
AFT CARGO COMPARTMENT; AFT TIE DOWN PLATE AT THRESHOLD HAS CORROSION ON LOWER SIDE / REPLACED AFT CARGO COMPARTMENT AFT TIE DOWN PLATE AT THRESHOLD. PART RETURNED TO SHELF 'A'TAG A35905
AFT CARGO COMPARTMENT; FWD TIE DOWN PLATE AT THRESHOLD HAS CORROSION ON LOWER SIDE / REPLACED AFT CARGO FWD TIE DOWN P/N 453A2611-1 ATAG A44060 REFERENCE IPC 25-52-10-02 ITEM 440 DUE TO PLATE FOUND TO BEOUT OF LIMITS I/A/W SRM 53-00-53-1A-2.
R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REINSTALLED THE LENS IAW AMM.
R1 FORWARD SIDEWALL EXIT LIGHT LENS DETACHED. SECURED LENS PER EA.
RIGHT WING INBD T/E FLAP DELAMINATED. R & R THE FLAP IAW MM.
RH WING INBD T/E FLAP DELAMINATED AT OUTBD T/E SIDE. / R&R FLAP ASSY PER MM.
L1 DOOR EMERGENCY EVAC SLIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
L1 DOOR ESCAPE SLIDE OUT OF POSITON. REPOSITIONED SLIDE PER MT.
SUPPLEMENTAL INFORMATION: AFT GALLEY SERVICE DOOR; LOWER PAN HAS CRACKED ATTACH ANGLES. / R&R PAN AS PER AMM 52-41-31.
R1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR CLIP OUT OF ADJUST IN HOLDER. ADJUSTED CLIP PER AMM.
CENTER OVERWING EMERGENCY EXIT SIGN LOOSE. R&R SIGN PER AMM.
OVERWING EXIT SIGN LOOSE. SECURED THE SIGN IAW AMM.
OVERWING EXIT SIGN LOOSE. SECURED THE SIGN IAW MM.
AFT CABIN RIGHT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.
AFT CABIN LEFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.
RIGHT OVERWING EXIT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.
FORWARD CABIN LEFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.
LEFT ROW 17 EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.
LEFT OVERWING EXIT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.
FORWARD CABIN RIGHT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.
AFT STATION EMERGENCY EXIT LIGHT SWITCH GUARD SPRING BROKEN. R &R THE SWITCH GUARD BUTTON IAW AMM.
RT MLG FORWARD TRUNNION SUPPORT FITTING FACE CORRODED. R & R FITTING IAW EA.
LEFT MLG TRUNNION SUPPORT FITTING FACE CORRODED. R & R FITTING IAW EA.
LEFT MLG FORWARD TRUNNION SUPPORT FITTING FACE CORRODED. R & R FITTING IAW EA.
IN FLIGHT LT CEILING LIGHT SLIGHT BURNED ELECTRICAL ODOR AT ROW 11. R & R LIGHT ASSEMBLY IAW AMM.
CAPTAIN SLIDING WINDOW ARCED. R & R L2 SLIDING WINDOW IAW MT.
R1 DOOR SLIDE FALLING OUT OF CONTAINER. R & R SLIDE ASSEMBLY IAW MM.
FORWARD EMER EQUIPMENT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.
RIGHT MID CABIN OVERHEAD EMER EXIT SIGN LIGHT LOOSE. R & R LIGHT HOUSING IAW AMM.
R1 DOOR ESCAPE SLIDE LATCH LOOSE. R & R SLIDE ASSEMBLY IAW MT.
R1 DOOR EMER EVAC SLIDE FWD GIRT BAR RETAINING CLIP LOOSE. R & R CLIP ASSEMBLY IAW SRM.
CROSS FEED VLV CB ON P6 PANEL P63B7 POPPED INFLIGHT. R & R CROSS FEED VLV ACTUATOR IAW AMM.
RIGHT WING INBD AFT FLAP LOWER SKIN DELAMINATED 26 INCHES FROM INBD END, 4 INCHES FROM AFT EDGE. REPAIRED AFT FLAP IAW EA.
AFT CARGO FLOORBEAM TRACK CORRODED AT BS 727A+10, RBL 13. R & R TRACK IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 405 TO BS 420, RBL 13. R & R INTERCOSTAL IAW SRM.
AFT CARGO TRACK FLOORBEAM CORRODED AT BS 772, LBL 17. REPAIRED TRACK IAW EA.
INTERCOSTAL CRACKED AT BS 350, CBL 0. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED AT BS 285, CBL 0. R & R INTERCOSTAL IAW SRM.
LEFT WING NR 3 CANOE FAIRING CRACKED ON INSIDE 12 INCHES FWD OF HORSE SHOE FITTING. REPAIRED FAIRING IAW EA.
INTERCOSTAL CRACKED AT BS 309, RBL 15. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED AT BS 354, LBL 11. R & R INTERCOSTAL IAW SRM.
AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 13. R & R BEAM IAW SRM.
AFT CARGO FLOORBEAM TRACK CORRODED AT BS 772, RBL 13. R & R TRACK IAW SRM.
AFT CARGO DOORWAY THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847, BETWEEN RBL 19 TO RBL 27. R & R WEB IAW SRM.
AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 3. R & R BEAM IAW SRM.
AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 8. R & R BEAM IAW SRM.
AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 2. R & R BEAM IAW SRM.
AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 7. R & R BEAM IAW SRM.
RIGHT HORIZONTAL STABILIZER LE INTERNAL RIB DAMAGED AT STAB STATION 160.93 TO STATION 188.93. R & R STABILIZER IAW MM.
FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW EA.
FLOORBEAM CRACKED AT BS 727B, LBL 24.75. REPAIRED BEAM IAW EA.
FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW EA.
FLOORBEAM CRACKED AT BS 727B, RBL 24.75. REPAIRED BEAM IAW EA.
LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 101.9, 11 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
RIGHT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 147.9, 24 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
RIGHT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 101.9, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 184.7, 26 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 175.5, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 138.7, 33 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 125.5, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED AT BS 321, LBL 50. R & R INTERCOSTAL PER SRM.
INTERCOSTAL CRACKED AT BS 335, LBL 50. R & R INTERCOSTAL IAW SRM.
OVERWING EMERGENCY EXIT LIGHT DAMAGED. R&R LIGHT IAW MM.
RT FWD OVERWING EXIT LENS LOOSE. R&R LENS IAW AMM.
AFT ENTRY DOOR EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.
LEFT EEPLS COVERS CRACKED AT ROW 1. REMOVED AND REPLACED COVERS PER M/M.
LEFT EEPLS COVERS CRACKED AT ROW 10. REMOVED AND REPLACED COVERS PER M/M.
LEFT EEPLS COVER CRACKED AT ROW 17. REMOVED AND REPLACED COVER PER AMM.
LEFT EMERGENCY EXIT LIGHT LAMP INOP AT ROW 1. RELAMPED LAMP IAW AMM.
EEPLS COVER LOOSE AT ROW 2. SECURED COVER PER M/M
EEPLS COVER LOOSE AT ROW 1. SECURED COVERS PER M/M.
FWD EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP IAW M/M.
MID CABIN EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS IAW M/M.
RIGHT HORIZONTAL STABILIZER LOWER SKIN RIB CRACKED AT STA 92.70. REPAIRED RIB IAW SRM.
VERTICAL PRESSURE BULKHEAD CRACKED AT BS 663, RBL 40. REPAIRED BULKHEAD PER ER AND EA.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER M/M.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 16. R&R LENS PER MM.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.
FWD GALLEY EEPLS COVER LOOSE. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 10. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 10 TO ROW 20. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 11. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS COVER MISSING BETWEEN ROW 8 TO ROW 10. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 13 TO ROW 14. RELAMPED LIGHT PER MM.
EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
DIVERSION - B-HYD ELECTRIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. FOUND B-SYSTEM ELECTRIC PUMP CONNECTION WITH LOOSE PINS. REMOVED AND REPLACED PUMP PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED HC1 CHECK, EMERGENCY LIGHTS BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS END CAP MISSING AT ROW 1. INSTALLED END CAP PER MM.
FWD EEPLS WIRES OUT OF POSITION. REPOSITIONED WIRING PER MM.
L1 DOOR LOWER EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. SECURED SLIDE PER MM.
FOUND EMERGENCY EXIT EGRESS LIGHT LOOSE AT FIRST ROW. SECURED LIGHT PER MM.
EEPLS ASSY LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS LENS BROKEN AT ROW 1ABC. REMOVED AND REPLACED LENS PER MM.
EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.
L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
MID CABIN EEPLS COVER LOOSE. SECURED COVER PER MM.
FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.
EEPLS INOP AT ROW 1 ABC. SECURED EEPLS CONNECTOR PER MM.
FOUND FWD RT EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.