N250WN
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 | 2024-10-19 – 2024-10-19 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2024-10-19 – 2024-10-19 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
CORRODED SUPPORT ZEE, BTWN BS 727+10 - 847 LBL 21. REPAIRED SUPPORT ZEE IAW SRM 53-00-53-2R, REPAIR 5.
DETERIORATED ACCESS PANEL 193AL AT BODY FAIRING LT SIDE. REPAIRED ACCESS PANEL 193AL AT BODY FAIRING IAW SRM 51-70-05-2R-6 REPAIR 6.
ELONGATED HOLE ON FRAME, BS 727C, WL 156.4, RBL 22. PERFORMED OVERSIZE HOLE LOCATED ON FRAME BS 727C IAW SRM 51-40-02-0G-0.
CRACKED STRAP LOCATED BTW BS 312 & 328, BL 0 UPPER AREA AT E/E COMPARTMENT. REPLACED THE STRAP IAW SRM 51-40-02, AND DWG 141A5400, SHEET 37, REV -.
BS 663.75 VAPOR BARRIER CRACKED BTWN LBL 45 AND LBL 55. REPAIRED VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.
BS 663.75 VAPOR BARRIER CRACKED BTWN LBL 45 AND LBL 55. REPAIRED VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.
BS 663.75 VAPOR BARRIER CRACKED BTWN LBL 45 AND LBL 55. REPAIRED VAPOR BARRIER IAW SRM 51-70-04-2R-10 REPAIR 10.
BS 663.75 VAPOR BARRIER CRACKED BTWN LBL 45 AND LBL 55. REPAIRED VAPOR BARRIER IAW SRM 51-70-04-2R-10 REPAIR 10.
BS 663.75 VAPOR BARRIER CRACKED BTWN LBL 45 AND LBL 55. REPAIRED VAPOR BARRIER IAW SRM 51-70-04-2R-10 REPAIR 10.
CRACKED SUPPORT BRACKET IB FLAP INTERNAL CAVITY AT RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOC IB FLAP INTERNAL CAVITY AT RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 113A2100, SHEET 58, REV -.
CRACKED ANGLE ON AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED ANGLE ON AUXILIARY TRACK SLAT 1 AT LT WING IAW SOPM 20-50-01, REV 40, AND SRM 51-40-02.
CRACK ON SUPPORT BRACKET LOCATED BS 867, BTW S2R & S3R. REPLACED SUPPORT BRACKET LOCATED BS867 AND BTW STR2R TO STR3R AT PASSENGER CABIN IAW SRM 51-10-02, ITEM 9 AND DWG 146A7901, SHEET 66, REV A. APPLIED PROTECTIVE TREATMENT ON HOLES IAW SRM 51-20-01.
CORRODED SUPPORT ZEE BTWN BS 727 - 847, LBL 21, WL 156. REPLACED SUPPORT ZEE AND CLIP SECTION IAW SRM 51-40-02-0G, DWG 146A7500, SHEET 86, REV A, & DWG 146A7502 SHEET 27 REV-. EVALUATED REEWORK AREAS LOC ON SUPPORT ZEE, AND FOUND WITHIN LIMITS IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, STEP 4.A(2), DETAIL D, FIGURE 103. NOMINAL THICKNESS IS 0.040; IAW SRM 53-60-53-0I-2 AND BAC1496-377.MRT IS;0.039 INCH.
CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. PERFORMED REPAIR STRINGER 23L LOCATED BETWEEN BS 500D MORE 10 INCHES TO BS 540 AT FWD CARGO COMPARTMENT IAW SRM 53-00-03-2R-1. REPAIR 1, AND DRAWING 143A3210, SHEET 74, REV B.
CRACKED INTERCOSTAL, BTW BS 500D - 520, S28R IN THE FWD CARGO BAY. REPLACED INTERCOSTAL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A.
CORROSION SUPPORT ZEE BETWEEN BS 727 TO 767, RBL 21, WL 156. REPLACED SUPPORT ZEE IAW SRM 51-40-02, AND DWG 146A7500, SHEET 85, REV A.
ELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING . REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.
CORROSION ON THE INTERNAL SKIN, TOILET SERVICE DOOR 145AL PERFORMED PERMANENT REPAIR LOCATED ON EXTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE IAW SRM 52-40-01-2R-8, REPAIR 8.
CRACKED GUSSET, BS 500D, STR 19L. REPLACED GUSSET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902 SHEET 174 REV -.
CRACKED ANGLE, BS 500C, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV -.
CORRODED SHIELD WEB BTW BS 492 TO 500A, STR 26R, WL 156 IN THE FWD CARGO. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02, AND DWG 143A0080, SHEET 23, REV-.
CRACKED GUSSET, BS 500D, STR 19R. REPLACED GUSSET BS 500D AND STR 19R FWD CARGO COMPARTMENT IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND 143A7902 SHEET 174 REV -.
CRACKED STRINGER 9 INTERNAL AREA FUEL TANK UPPER POSITION, BTW RIB 21 AND RIB 22 AT LT WING. PERFORMED REPAIR ON STRINGER 9 INTERNAL LT WING FUEL TANK UPPER POSITION IAW EA- 26-157-01136-WIP1 AND EA- 26-157-01136-WIP2.
CRACKED STIFFENER FRONT SPAR LOCATED BS 540, LBL 24.75 AT CENTER SECTION. REPLACED STIFFENER FRONT SPAR, IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 111A6000, SHEET 245, REV-, AND DWG 111A2001, SHEET 77, REV-.
CRACK INDICATION FOUND ON THE HORIZONTAL PRESSURE DECK WEB, RBL 42, BS 663 - 675. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK, BS 663 - 675, RBL 30 - 60 IAW SRM 53-40-51-2R-2,. REPAIR 2.
ELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACK INDICATION FOUND ON STUB FRAME, BS 294.5, 4.2 INCHES BELOW STRINGER 8R. REPLACED STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A8370, SHEET 9, & 10, REV D.
MISSING RETAINER ON EMERGENCY EXIT DOOR LIFE LINE RT AND LT SIDES. INSTALLED RETAINER ON EMERGENCY EXIT DOOR LIFE LINE RT AND LT SIDE IAW AMM 25-61-10-710-801, STEP 7 E (7).
BS 663.75 VAPOR BARRIER CRACKED BTWN LBL 45 AND LBL 55. REPAIRED VAPOR BARRIER IAW SRM 51-70-04-2R-10 REPAIR 10.
FORWARD ENTRY DOOR ESCAPE SLIDE COVER CAME OFF AND SLIDE FELL OUT. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE BACK INTO COMPARTMENT REF. AMM 25-66-01 AND MT 725-61-06.
BATTERY PACK AT 14DEF FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK AT 14 DEF IAW AMM 33-51-00.
BATTERY PACK AT 20 ABC FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK AT 20 ABC IAW AMM 33-51-06.
AFT ENTRY DOOR ON THE LEFT SIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT ENTRY DOOR OUTER EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.
FWD ENTRY EXIT/SALIDA SIGN COVER ADJACENT (OUTBOARD) OF FAS JUMPSEAT FELL OFF. RESECURED FWD ENTRY DOOR EXIT/SALIDA SIGN LENS PER AMM 33-51-01. OPS CHECK GOOD.
FORWARD ENTRY DOOR SLIDE FELL OUT OF BOX<[01] REINSTALLED FWD ENTRY DOOR ESCAPE SLIDE IN THE COMPARTMENT AND THE COMPARTMENT ASSEMBLY PER MT 725-61-06 & AMM 25-66-01.
CENTER OVERHEAD EMERGENCY EXIT SIGN IS BROKEN. <[01] CENTER OVERHEAD EMERGENCY EXIT SIGN ASSEMBLY WAS REMOVED AND REPLACED IN REF TO AMM 33-51-01. LIGHT OPS CHECKS GOOD.
AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-286868<[01] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO LBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO LBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9
AFT CARGO BAY SPLICE STRAP MOD HAS SHORT FASTENER INSTALLED AT BS 727B, LBL 45.5. REPLACED SHORE FASTENER ON SPLICE STRAP MOD INSTALLED AT BS 727B, LBL45.5 IAW EA 1-753-33801 AND SRM 51-40-02.
AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2024-286867<[01] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>SEE INDIVIDUAL SING OFF BELOW.
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS450 TO ORSS472 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS450 TO ORSS472 AT LT WING IAW SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW SRM 51-40-02 AND DRAWING # 115A3760 REV -.
CORRODED WEB, FUEL INDICATOR LOCATED INTERNAL CAVITY LE AT RT WING. PERFORMED PERMANENT REPAIR ON WEB IAW EA 24-157-01348 AND EA 24-157-01348-WIP1.
CRACK WEB TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING. REPLACED WEB AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9 & DWG 115A2512, SHEET 14, REV A. MEASURE OF CRACK IS L: 0.725.
CRACK ANGLE TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 275 AT LT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB IAW SRM 51-40-02; SRM 51-10-02,ITEM 9 AND DWG 115A6200 SHEET 11 REV B. MEASURE OF CRACK IS: L 1.727.
CRACK ANGLE TRAILING EDGE LOCATED ORSS 267 RT WING. REPLACED ANGLE ON TRAILING EDGE LOCATED ORSS 267 IAW SRM 51-40-02;SRM 51-10-02 AND DWG 115A2930 SHEET: 8 REV. -. MEASURES OF CRACK IS : L=1.062 INCH.
CRACK WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING. REPLACED WEB AND FASTENERS ON TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 115A 2512 SHEET 14; REV. A.
CRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SH 8; REV -.
CRACK FITTING CONTROL RIB LOCATED ORSS278 AT LT WING. PERFORMED REPAIR ON DEFLECTION CONTROL RIB AREA LT WING IAW SRM 57-51-02-2R-3 REPAIR 3 & SRM 57-51-02-2R-1 REPAIR 1.
ELONGATED HOLE STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286832<[01] REPLACED STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 146A8340 SHEET: 24 REV: A.;[02] REPLACED STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 146A8340 SHEET: 24 REV: A.
CRACK LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING 2024-286837<[01] ON STEP 3. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 23-MAY-24.;[02] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[03] PERFORMRD REPAIR ON LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING IAW B737-700 SRM SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED REPAIR ON LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING IAW B737-700 SRM SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN OFF BELOW
CRACK TRACK RBBL 13.84 LOCATED STA767 AFT CARGO COMPARTMENT 2024-286835<[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] PERFORMED REPAIR ON TRACK RBBL 13.84 BETWEEN BS 727D + 13? TO BS 767 + 10? AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK TRACK RBBL 13.84 LOCATED STA727E AFT CARGO COMPARTMENT 2024-286833<[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] FAULT WAS RESOLVED ON ANOTHER FAULT SEE TTG8Q00T580W;[04] CORRECTED STEP 3 <BR>FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 13 INCHES TO BS 767 PLUS 10 INCHES SEE TTG8Q00T580W;[05] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 13 INCHES TO BS 767 PLUS 10 INCHES SEE TTG8Q00T580W
CRACK ANGLE LOCATED STA947.5 AND LBL10 AFT CARGO COMPARTMENT 2024-286829<[01] REPLACED ANGLE AND FASTENERS LOCATED BS947.5 AT LEVEL STR26L LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 149A8103 SHEET: 7 REV: A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LOCATED BS947.5 AT LEVEL STR26L LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 149A8103 SHEET: 7 REV: A SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED.
CRACK ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT 2024-286830<[01] REPLACED ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. AND DWG 149A8102 SHEET: 16 REV:-; DWG 149A8104 SHEET: 1 REV: B.;[02] REPLACED ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. AND DWG 149A8102 SHEET: 16 REV:-; DWG 149A8104 SHEET: 1 REV: B.
ELONGATED HOLE STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286831<[01] REPLACED STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. AND DWG 146A0081 SHEET: 34 REV:-.;[02] TASK COMPLETED
CRACK BRACKET ANGLE LOCATED BS 540 PLUS 3 INCHES LBL18 AT AIR CONDITIONING BAY. REPLACED THE BRACKET ANGLE IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.367.
CRACK WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2024-286774<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02-0G-0 ITEM 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A7505 SHEET 81 REV-:.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02-0G-0 ITEM 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A7505 SHEET 81 REV-:.SEE INDIVIDUAL SIGN OFF BELOW.
DETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2024-286711<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-700-AMM 25-66-02-400-801 STEP 3.D.(1) (A) TO (J);[02] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-700-AMM 25-66-02-400-801 STEP 3.D.(1) (A) TO (J)
CRACK AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B, STEPS (2) & (4) TO (7).
BROKEN ACCESS PANEL 551FB SUPPORT ANGLE AT LT WING. REPLACED THE SUPPORT ANGLE ON ACCESS PANEL 551FB IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2710 SHEET: 7 REV -.
CRACK WEB LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA 2024-286678<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV: ?. SEE INDIVIDUAL STEP SING-OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV: ?. SEE INDIVIDUAL STEP SING-OFF BELOW
CRACK INNER CHORD LOCATED BS303 LBL55 AND WL208 AT FWD GALLEY AREA 2024-286679<[01] REPLACED INNER CHORD AND FASTENERS LOCATED BETWEEN BS 270 TO BS 360 LBL55 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET: 11; REV: -. AND DWG #141A5220 SHEET: 1; REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BETWEEN BS 270 TO BS 360 LBL55 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET: 11; REV: -. AND DWG #141A5220 SHEET: 1; REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
CRACK WEB LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA 2024-286680<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV:? .SEE INDIVIDUAL STEP SING-OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV:? .SEE INDIVIDUAL STEP SING-OFF BELOW
CORROSION INNER CHORD LOCATED BETWEEN BS312 TO BS328 RBL60 AND WL208 AT FWD GALLEY AREA. REPLACED INNER CHORD INNER CHORD LOC. BTW BS 259.5 - 360; ANGLE & STRAP LOC. ON INNER CHORD IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 & DWG 141A8310 SHEET 25 REV, DWG 141A8310 SHEET 23 REV.
CRACK WEB LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA 2024-286676<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AMD DWG 141A5400 SHEET 20 REV:?.SEE INDIVIDUAL STEP SIGNOFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AMD DWG 141A5400 SHEET 20 REV:?.SEE INDIVIDUAL STEP SIGNOFF BELOW<BR>RII CERTIFIED
CORROSION ON FLOOR BEAM LOCATED BS986.5 RBL43 AND WL208 AFT GALLEY AREA. PERFORMED REPAIR ON FLOOR BEAM LOCATED BS986.5 BTW RBL40 TO RBL 50 AND WL208 AFT GALLEY AREA. IAW EA 24-153-01239.
CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK LBL 31 STA 663 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.312 INCH APPROX 2024-286661<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[03] STEP 14 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 08-JAN-25;[04] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK BTW BS 663.75 TO BS STA 675 AND LBL 25 TO LBL 60 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG 203 . SEE INDIVIDUAL SIGN-OFF BELOW.;[05] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK BTW BS 663.75 TO BS STA 675 AND LBL 25 TO LBL 60 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG 203 . SEE INDIVIDUAL SIGN-OFF BELOW.<BR>AS RII
CORRODED WEB LOCATED BS 1016 PLUS 11INCH, LBL12 AND WL208, AFT GALLEY AREA. REPLACED WITH A NEW WEB AND FASTENERS IAW 51-40-02, SRM 51-10-02 ITEM 9, & DRAWING 147A5600 SHEET 32 REV B.
CRACK ON SUPPORT BRACKET LOCATED BS695 AND RBL24.75 AT PASSENGER CABIN 2024-286612<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLACED SUPPORT BRACKET LOCATED BS695 AND RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET:6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTIVE ACTION CERTIFIED
CRACK ON SUPPORT BRACKET LOCATED ON BS695 AND BL0 RH SIDE AT PASSENGER CABIN 2024-286610<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLACED SUPPORT BRACKET LOCATED ON BS695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT BRACKET LOCATED ON BS695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.
DETERIORATED INSOLATER MOUNT ON FWD ENTRY DOOR CUTOUT PANELS 3(EA) 2024-286532<[01] REPLACED INSOLATER MOUNT ON FWD ENTRY DOOR CUTOUT PANELS 3(EA) IAW B737-700 SRM 51-10-02-0G ITEM 9 AND B737-700 SRM 51-40-02.;[02] JOB COMPLETED
CRACK INDICATION FOUND ON INBOARD RADIUS ADJACENT TO FASTENER HOLE; ON 141A6536-14 BEAM #4 ON FWD SERVICE DOOR. CRACK LENGTH = 0.860 INCHES. 2024-286507<[01] REPLACED BEAM #4 LOCATED BTW BSTA 299 TO BSTA 328. AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. SRM 51-10-02 PARAGRAPH 9. AND DWG # 141A6516 SHEET 92. REV. ?-?. SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED BEAM #4 LOCATED BTW BSTA 299 TO BSTA 328. AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. SRM 51-10-02 PARAGRAPH 9. AND DWG # 141A6516 SHEET 92. REV. ?-?. SEE INDIVIDUAL SING OFF BELOW.<BR>AS RII
DELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN 2024-286467<[01] TOOL USED: CALIPER P/N:500-196-30 S/N: A23327546 DUE DATE: 04-MAR-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:16122983; DUE DATE: 15-FEB-25;[03] TOOL USED:SCALE PN: CR5200 SN:8342514551 DUE Dÿ½TE: 17-FEB-25.;[04] TOOL USED SCALE P/N: CR5200; S/N: 8342514551; DUE DATE: 17-FEB-25.;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185847; DUE DATE: 25-OCT-24;[06] REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] CORRECTIVE ACTION 6 ENTERED IN ERROR. <BR>CORRECT CORRECTIVE ACTION IS: REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW;[08] REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII COMPLETED
DELAMINATED FLOOR PANEL 241FF AT PASSENGER CABIN 2024-286469<[01] TOOL USED: CALIPER P/N:500-196-30 S/N: A23327546 DUE DATE: 04-MAR-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:16122983; DUE DATE: 15-FEB-25;[03] TOOL USED:<BR>SCALE PN: CR5200 SN:8342514551 DUE Dÿ½TE: 17-FEB-25.;[04] TOOL USED SCALE P/N: CR5200; S/N: 8342514551; DUE DATE: 17-FEB-25;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185847; DUE DATE: 25-OCT-24;[06] REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] STEP 6 ENTERED IN ERROR ; CORRECT CORRECTIVE ACTION IS: REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] CORRECTIVE ACTION 6; 7 ENTERED IN ERROR. <BR>CORRECT CORRECTIVE ACTION IS: REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[09] REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII COMPLETED
CRACK ON FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) 2024-286474<[01] REPLACED FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) I.A.W B737-700 AMM-25-11?11-400-801<BR>TOOL USED: TRACK SETTING FIXTURE NG BOEING<BR>P/N: 0T900-0247<BR>S/N: AE-33472;[02] REPLACED FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) I.A.W B737-700 AMM-25-11?11-400-801<BR>TOOL USED: TRACK SETTING FIXTURE NG BOEING<BR>P/N: 0T900-0247<BR>S/N: AE-33472
DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA 2024-286419<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA) IAW B737-700 AMM-33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA) IAW B737-700 AMM-33-51-15-400-802
DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE OB SIDE AT LT WING. PERFORMED PERMANENT REPAIR ON I/B MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING IAW SRM 57-53-01-2R-7 REPAIR 7.
FORWARD CARGO FLOOR HAS CRACK<[01] OK TO CONT PER MEL 25-16-01 SP1B;[02] 01 - REMOVED AND REPLACED PER [AMM 25-52-10-401-NG (CARGO FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT)]
RIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT EXISTING REPAIR AT APPROX RBL 32 AND RBL 57<[01] REMOVED AND REPLACED WEB 111A1151Y10 ON SHELD IAW SRM 51-40-05-0G-0DWG 111A1151 REV A;[02] VERIFIED STEP 1<BR>AUDIT C/W
DOT A24-7 MID CABIN FLOOR PANEL 232RF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MULTIPLE AREAS OF DAMAGE TO FLOOR BOARD AND IS B.E.R. FABRICATE NEW FLOOR BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4<BR><BR>VERIFIED MATERIALS AS FLOOR BOARD STOCK (A1257); INSERTS (A201251); ADHESIVE (A186981); FOAM TAPE (A197687) IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204 AND BOEING DRW. 144A5810;[02] VERIFIED MATERIAL FOR STEP 1.;[03] FABRICATED NEW FLOORBOARD PER SAMPLE BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4; BOEING DRW; 144A5810 AND BAC5085 PARAGRAPH 8.4.2.;[04] VERIFIED ITEM 3.<BR>AUDITED.
DOT A24-3 MID CABIN FLOOR PANEL 231XF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT 4; 51-00-03. NO DEFECTS NOTED. TOOL#36285; DUE 16DEC23. REF EA 23-153-02790-WIP1 STEP 2;[02] EVALUATED PANEL 231XF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A; C; E&F. VERIFIED MATERIALS AS: BMS 8-201 (A197641); BMS 9-3 (A178073). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[03] VERIFIED STEPS 1 AND 2 C/W AND OK TO BOND GRANTED;[04] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M.;[05] REPAIRED UPPER SURFACE ON PANEL 231XF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[06] REFER TO FAULT TTG8Q00NDBZJ WHERE EA 23-153-02790 WAS ADDED AS A SUBTASK.;[07] VERIFIED STEPS 4-6.<BR>AUDIT C/W.
DOT A24-4 MID CABIN FLOOR PANEL 241AF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT 4; 51-00-03. NO DEFECTS NOTED. TOOL#36285; DUE 16DEC23. REF EA 23-153-02790-WIP1 STEP 2;[02] EVALUATED PANEL 241AF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 A; C; E&F. VERIFIED MATERIALS AS: BMS 8-201 (A197641); BMS 9-3 (A178073). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[03] VERIFIED STEP 1 AND 2 C/W AND OK TO BOND GRANTED;[04] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M.;[05] REPAIRED DAMAGE TO UPPER SURFACE ON PANEL 241AF. IAW B737-700 53-00-50-2R-1; SRM 53-00-50-2R-0& EA 23-153-02790.;[06] VERIFIED STEPS 4-5.<BR>AUDIT C/W.
DOT A24-5 MID CABIN FLOOR PANEL 241BF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND FLOOR PANEL TO B.E.R.. REPLACE BY FABRICATION IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204 AND DWG 144A5810-189. NEW FLOOR BOARD (A1257); EPIBOND 420 (A186981); INSERTS (A201251); FOAM TAPE (A197687);[02] VERIFIED MATERIAL FOR STEP 1.;[03] REPLACED BY FABRICATION AND SAMPLE OF MID CABIN FLOOR PANEL 241BF IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARA 4; DWG 144A5810-189 AND BAC5085 STEP 8.4.2;[04] VERIFIED ITEM 3.<BR>AUDITED.
DOT A24-6 MID CABIN FLOOR PANEL 242AF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND FLOOR PANEL TO B.E.R.. REPLACE BY FABRICATION IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204 AND DWG 144A5810-189. NEW FLOOR BOARD (A1257); EPIBOND 420 (A186981); INSERTS (A201251); FOAM TAPE (A197687);[02] REPLACED BY FABRICATION AND SAMPLE OF MID CABIN FLOOR PANEL 242AF IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARA 4; DWG 144A5810-189 AND BAC5085 STEP 8.4.2;[03] VERIFIED STEPS 1-2.<BR>AUDIT C/W.
CABIN STOWBIN BULLNOSE EMERGENCY LIGHT AT ROW 12 ABC IS INOP<[01] REPLACED LAMPED STOWBIN BULLNOSE EMERGENCY LIGHT AT ROW 12 ABC IAW AMM 33-51-03-960-801 OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR>C/W
EMERGENCY LIGHTS L1 &R1 BATTERY PACK INOP<[01] R&R BATTERY PACK FOR EMERGENCY LIGHTS R1&R2 M-01674 PER 33-51-06 .OPS CHK GOOD .
AFT W4142 EMERGENCY LIGHT BATTERY PACK NEEDS TO BE REPLACED.<[01] REMOVED AND REPLACED AFT W4142 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.
2 FORWARD LH BULLNOSE EMERGENCY LIGHTS INOP / [01] R & R LH FWD. BULLNOSE EMERGECY LIGHT BATTERY PACK IAW AMM 33-51-06.
BURNED EMERGENCY EXIT LIGHT ON SIDEWALL DOOR LH SIDE AND AFT FUSELAGE RH SIDE AT PASSENGER CABIN (2 EA) 2022-228627 / [01] REPLACED EMERGENCY EXIT LIGHT ON SIDEWALL DOOR LH SIDE AND AFT FUSELAGE RH SIDE AT PASSENGER CABIN (2 EA) I.A.W B737-700 AMM 33-51-01-960-802 AND AMM 33-51-04-960-801. TESTS ARE OK.;[02] TASK CARD COMPLETED
CRACK VAPOR BARRIER LOCATED ON BS 663 LBL 65 ON MAIN WHEEL WELL LH SIDE 2022-228599 / [01] TOOL USED CALIPER P/N 500-197-30; S/N A18234378; DUE DATE: 21-SEP-22.;[02] TOOL USED HOT BONDER P/N: HCS9000B; S/N: 15092096; DUE DATE: 16-JAN-23;[03] TOOL USED SCALE P/N CL5000; S/N AE-407336; DUE DATE: 16-AUG-22.;[04] REPAIRED VAPOR BARRIER LOCATED ON BS 663 LBL 65 ON MAIN WHEEL WELL LH SIDE IAW B737-700 SRM 51-70-04-2R-10 REPAIR # 10 AND SRM 51-70-04-2R-0 REPAIR GENERAL TOOL USED CALIPER P/N 500-197-30 S/N A18234378 DUE DATE 21-SEP-22; HOT BONDER P/N ;HCS9000B; S/N: 15092096; DUE DATE: 16-JAN-23; SCALE P/N CL5000; S/N AE-407336; DUE DATE: 16-AUG-22.
ELONGATE HOLE ON BRACKET LOCATED ON ACCESS PANEL 145AL AT LOWER FUSELAGE 2022-228600 / [01] REPLACED BRACKET LOCATED ON ACCESS PANEL 145AL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PART USED HINGE ASSY P/N USED: 146A7414-9 PO: 2022-123293 1;[02] TASK CARD COMPLETED
(CUSTOMER REQUEST) CRACK ON BRACKET LOCATED AT BS 663 BETWEEN LBL 45.64 TO LBL 54.21 L/H SIDE MAIN WHEEL WELL 2022-228593 / [01] TOOLS USED: POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 26-JAN-23; MULTIMETER P/N: FLUKE 87-5; S/N: 98740068; DUE DATE: 08-NOV-22; THERMOMETER P/N: 42510A; S/N: 200813258; DUE DATE: 29-JUN-22.;[02] REPLACED ANGLE ON BS 663 LBL 45.64 A I.A.W SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DRAWING #276A9183 REV:-; 111A1001 REV:A ; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED ANGLE ON BS 663 LBL 45.64 A I.A.W SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DRAWING #276A9183 REV:-; 111A1001 REV:A ; SEE INDIVIDUAL STEP SIGN OFFS BELOW
CORROSION SUPPORT ZEE LOCATED BTW BS 727D TO BS 847 LBL 31.1 WL 156 AFT CARGO COMPARTMENT 2022-228573 / [01] INSPECTION REJECT IN STEP 11 SEE TTG8Q00CK7LW;[02] REPLACED SUPPORT ZEE LOCATED BTW BS 727D TO BS 847 LBL 31.1 WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02;SRM 51/10/02 ITEM 9 AND DRAWING 146A7500 SHEET 85 REV A. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED SUPPORT ZEE LOCATED BTW BS 727D TO BS 847 LBL 31.1 WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02;SRM 51/10/02 ITEM 9 AND DRAWING 146A7500 SHEET 85 REV A. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL STEP SIGN OFFS BELOW
CRACK ANGLE - SUPPORT LOCATED BTW BS 907 TO BS 927 AND STR 25/27R AFT CARGO COMPARTMENT 2022-228571 / [01] REPLACED ANGLE - SUPPORT LOCATED BTW BS 907 TO BS 927 AND STR 25/27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 REV. D;[02] REPLACED ANGLE - SUPPORT LOCATED BTW BS 907 TO BS 927 AND STR 25/27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 REV. D. SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED.
CRACK TRACK RBBL 13.84 LOCATED BS 747 AT AFT CARGO COMPARTMENT 2022-228574 / [01] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22;[02] PERFORMED REPAIR ON TRACK LOCATED BS 727E TO BS 767 RBBL 13.84 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR . SEE INDIVIDUAL SIGN-OFF BELOW;[03] PERFORMED REPAIR ON TRACK LOCATED BS 727E TO BS 767 RBBL 13.84 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR . SEE INDIVIDUAL SIGN-OFF BELOW;[04] CORRECTED STEP 3<BR>PERFORMED REPAIR ON TRACK LOCATED BS 727E TO BS 767 RBBL 13.84 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR . SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII
CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 WL 156.1 RBL 21.84 AFT CARGO COMPARTMENT 2022-228575 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 WL 156.1 RBL 21.84 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM-51-40-02; SRM 51-10-02 ITEM 9 AND DWG-146A7500 REV: A;[02] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 WL 156.1 RBL 21.84 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM-51-40-02; SRM 51-10-02 ITEM 9 AND DWG-146A7500 REV: A<BR>CERTIFIED AS RII
CORROSION STRAP LOCATED BTW BS 807 TO BS 827 WL 156.1 RBL 18.84 AT AFT CARGO COMPARTMENT 2022-228576 / REPLACED STRAP LOCATED BTW BS 807 TO BS 827 WL 156.1 RBL 18.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 146A8120 REV
CORROSION LOWER SILL LOCATED BTW BS 794.37 TO BS 847 RBL 26.84 WL 157.1 AFT CARGO COMPARTMENT 2022-228572 / [01] REPLACED LOWER SILL LOCATED BTW BS 794.37 TO BS 847 RBL 26.84 WL 157.1 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A8330 SHEET 30 REV:- <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW
CORROSION ON SUPPORT ANGLE LOCATED ON BS 500D BTW STR 26R TO STR 26L WL 152.2 AND BTW LBL 23.3 TO RBL 23.3 FWD CARGO COMPARTMENT 2022-228551.REPLACED SUPPORT ANGLE LOCATED ON BS 500D BTW STR 26R TO STR 26L WL 152.2 AND BTW LBL 23.3 TO RBL 23.3 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; P/N USED: 143A9485Y35
CORROSION WEB - INTERCOSTAL LOCATED BTW BS 460 TO BS 500A RBL 23.4 AND WL 152.2 AT FWD CARGO COMPARTMENT 2022-228549 / [01] REPLACE NEW WEB INTERCOSTAL LOCATED BTW BS 460 TO BS 500A RBL 23.4 AND WL 152.2 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING 143A0080 REV- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACE NEW WEB INTERCOSTAL LOCATED BTW BS 460 TO BS 500A RBL 23.4 AND WL 152.2 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING 143A0080 REV- SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII
CRACK ON ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-228539 / [01] REPLACED ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT I.A.W. B737-700 SR 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT I.A.W. B737-700 SR 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT I.A.W. B737-700 SR 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII
CRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2022-228544 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331926; DUE DATE: 28-SEP-22.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 24-FEB-23.;[03] TOOL USED SCALE P/N: SCA-301; S/N: AE-412125; DUE DATE: 14-MAR-23.;[04] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 24-FEB-23.;[05] TOOL USED SCALE P/N: SCA-301 S/N: AE-412123 DUE DATE: 14-MAR-23.;[06] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: AE-23149 DUE DATE: 10-NOV-22.;[07] REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] COMPLETED TASK.
CORROSION ON WEB-INTERCOSTAL (SHIELDS) LOCATED BTW BS 420 TO BS 440 AT LEVEL STR 26R RBL 23.3 AND WL 152.2 FWD CARGO COMPARTMENT 2022-228543 / [01] REPLACED NEW WEB INTERCOSTAL SHIELDS LOCATED BTW BS 420 TO BS 440 AT LEVEL STR 26R RBL 23.3 AND WL 152.2 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 REV -. SEE INDIVIDUAL SIGN OFF BELLOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
(CUSTOMER REQUEST) CRACK ON SUPPORT ANGLE LOCATED AT BS 663 LH SIDE A T MAIN WHEEL WELL COMPARTMENT 2022-228566 / INSPECTION REJECT IN STEP 8 SEE TTG8Q00CJGX6;[05] REPLACED SUPPORT ANGLE LOCATED AT BS 663 LH SIDE A T MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40?02 AND DRAWING # 111A1000 REV. A . SEE INDIVIDUAL SIGN OFF BELOW;[06] REPLACED SUPPORT ANGLE LOCATED AT BS 663 LH SIDE A T MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40?02 AND DRAWING # 111A1000 REV. A .
CORROSION ON BRACKET LOCATED ON ACCESS PANEL DOOR 145AL AT LOWER FUSELAGE 2022-228523 / [01] REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL DOOR 145AL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM-51-40-02; P/N USED: 149A7414-9 PO: 2022/123293;[02] REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL DOOR 145AL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM-51-40-02; P/N USED: 149A7414-9 PO: 2022/123293
BROKEN SIDEWALL PANEL 231YHW EMERGENCY EXIT COVER LENS AT PASSENGER CABIN (1 EA) 2022-228494 / [01] REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT COVER LENS AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 2 C (3);[02] REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT COVER LENS AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 2 C (3)
CRACK FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2022-228529 PERFORMED REPAIR ON FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY B IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 STEP 2 A FOR INSPECTION THRESHOLD SEE STEP 5. SEE INDIVIDUAL SIGN-OFF BELOW; PERFORMED REPAIR ON FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY B IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 STEP 2 A FOR INSPECTION THRESHOLD SEE STEP 5.
CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-228520 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A18135080;DUE DATE:31-JUL-22.;[02] REPAIRED BY WELD CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1. AND BAC 5975 SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK COMPLETED
CRACK STRINGER 26L BS 540 AT FWD CARGO COMPARTMENT 2022-228530 / [01] TOOL USED: P/N: 45MG; S/N:130061901; DUE DATE: 08-APR-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210136503 DUE DATE: 11-APR-23;[03] PERFORMED PERMANENT REPAIR CATEGORÿ½A ?A? ON STRINGER LOC BTW BS 500D TO BS 540 AND STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED PERMANENT REPAIR CATEGORÿ½A ?A? ON STRINGER LOC BTW BS 500D TO BS 540 AND STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW AS RII
CRACK STRINGER 25R BS 540 AT FWD CARGO COMPARTMENT 2022-228528 PERFORMED REPAIR ON STRINGER 25R BTW BS 500C TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. PERFORMED REPAIR ON STRINGER 25R BTW BS 500C TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
BROKEN SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 2022-228510 / [01] REPLACED SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 I.A.W B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 I.A.W B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW
CRACK GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT 2022-228449 / [01] REPLACED GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW RII
CRACK GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT 2022-228450 / [01] REPLACED GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW RII
CRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2022-228392 REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REP.2; REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REP.2;
CRACK ANGLE - SUPPORT LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT 2022-228452 / [01] REPLACED ANGLE - SUPPORT LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE - SUPPORT LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII
CRACK ANGLE INBOARD FAN COWL LOC. INTERNAL AREA IDG SERVICE DOOR ON ENGINE 2 (1 EA) 2022-228463. / [01] REPLACED NEW ANGLE INBOARD FAN COWL LOC. INTERNAL AREA IDG SERVICE DOOR ON ENGINE 2 IAW B737-700 SRM 51-10-02 ITEM 9 AND CMM <BR>71-13-30;[02] TASK COMPLETED
CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.600 INCH 2022-228133 PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB <BR>IAW EA 22-155-01485 WIP 1 AND EA COVER 22-155-01485 SEE INDIVIDUAL SIGN OFF BELOW;[06] CERTIFIED RII MAJOR REPAIR PERFORMED.
CRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING 2022-228136 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331926; DUE DATE: 28-SEP-22.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 24-FEB-23.;[03] TOOL USED SCALE P/N: SCA-301; S/N: AE-412125; DUE DATE: 14-MAR-23.;[04] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 24-FEB-23.;[05] TOOL USED SCALE P/N: SCA-301 S/N: AE-412123 DUE DATE: 14-MAR-23.;[06] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: AE-23149 DUE DATE: 10-NOV-22.;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] COMPLETED TASK.
CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.100 INCH 2022-228134 / [01] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22. CALIPER TOOL USED: PN: 500-197-30; SN: A21043164. DUE DATE : 01-SEP-22.;[02] FAULT TTG8Q00C79K0 WHERE EA 22-155-01485 HAS BEEN ATTACHED AS A SUBTASK;[03] REFER TO FAULT TTG8Q00C79K0 WHERE EA 22-155-01485 HAS BEEN ATTACHED AS A SUBTASK;[04] REFER TO FAULT TTG8Q00C79K0 WHERE EA 22-155-01485 HAS BEEN ATTACHED AS A SUBTASK.
CUSTOMER REQUEST CRACK VAPOR VARRIER LOCATED ON BS 663 LBL 54 AND WL 141.5 ON MAIN WHEEL WELL LH SIDE AT MAIN WHEEL WELL COMPARTMENT 2022-228077 / [01] TOOL USED; HOT BONDER PN: HCS9200B; SN: 18175478; DUE DATE: 05/AUG/22.;[02] TOOL USED; SCALE PN: SCA-301; SN: AE-412138; DUE DATE: 14/MAR/23.;[03] REPAIRED VAPOR BARRIER LOCATED ON BS 663 LBL 54 AND WL 141.5 ON MAIN WHEEL WELL LH SIDE AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED CALIPER PN: 500-197-30; SN: A21147745; DUE DATE: 09/APR/23. SCALE P/N:SCA-301 S/N:AE-412123 DUE DATE:14-MAR-23.;[04] JOB TASK COMPLETED. RII INSPECTION COMPLETED.
RAMP PERSONEL FOUND 13 CRACK AT FWD COMP FLOOR CENTER MID AREA PANEL 120CF / [01] INSTALLED PERMANENT REPAIR FIBERGLASS REINFORCEMENT AT FWD CARGO COMPARTMENT REF. AMM 25-52-01
RAMP PERSONEL FOUND 15 CRAC AT AFT CARGO FLOOR AFT AREA .PANEL 140BF / [01] PERFORMED REPAIR ON AFT CARGO PANEL PER AMM 25-52-01. WORK ACCOMPLISHED BY E78913
AFT GALLEY OB FLASHLIGHT HAS DEAD BATTERY ; / [01] REPLACED BATTERY IAW CMM 25-60-02 OPS CHECK GOOD
L/H HORIZONTAL LEADING EDGE RIB AT STA 142.45 DAMAGED / REMOVED AND REPLACED RIB AT STA 142.45 PER SRM 51-40-02
CARD # TTG8Q00537XS L/H HORIZONTAL LEADING EDGE RIB AT STA 142.45 DAMAGED; SIGNED OFF WITHOUT RII. ; / REMOVED AND REPLACED RIB AT STA 142.45 PER SRM 51-40-02.<BR>SEE FAULT # TTG8Q00537XS FOR COMPLETED WORK AND SIGN-OFFS.
GROUND POWER RECEPTACLE SURROUND REPAIR BROKEN AT BOTTOM TAB. PERFORMED REPAIR OF GROUND POWER RECEPTACLE SURROUND DOUBLER WITH FABRICATION AND INSTALLATION OF NEW DOUBLER, PER SRM 53-10-15-2R-4 REPAIR 4. WORK PERFORMED UNDER CAT A REPAIR. NO FURTHER INSPECTION REQUIRED.
CABIN FLOOR PANEL 241KF IS DELAMINATED. / REMOVED AND REPLACED CABIN FLOOR PANEL 241KF PER AMM 53-21-00.
R/H HORIZ. STAB RIB #5 ;SS.129.50 HAS CRACKED #2 VERT. STIFFENER. / PERFORMED REPAIR PER SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFFS FOR WORK ACCOMPLISHED.
R/H HORIZ. STAB RIB #5 ;SS.129.50 HAS CRACKED #3 VERT. STIFFENER. / REPAIRED R/H HORIZ STAB RIB #5; SS129.50; #3 VERTICAL STIFFENER PER SRM 55-10-09-2R-4 REPAIR 4.
AFT CARGO; AFT CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED PER AMM.53-11-02
PASSENGER SEAT TRACK #1 AT STA 520 HAS DAMAGE TO UPPER CROWN. REPAIRED PER SRM 53-00-52-2R-4; SEE WIPS AND SUBTASKS FOR INDIVIDUAL SIGNOFFS
CABIN FLOOR PANEL 241AF IS DELAMINATED. REMOVED AND REPLACED CABIN FLOOR PANEL 241AF PER AMM 53-21-00.
CABIN FLOOR PANEL 241DF IS DELAMINATED. / REMOVED AND REPLACED FLOOR PANEL 241DF PER AMM 53-21-00
CABIN FLOOR PANEL 241NF IS DELAMINATED. / REMOVED AND REPLACED CABIN FLOOR PANEL 241NF PER AMM 53-21-00.
R/H HORIZONTAL STABILIZER LEADING EDGE HAS A DENT AT LE STATION 130 MEASURING 9.5'L X 3'W X .265' DEEP FROM RIB TO RIB WHICH IS OUT OF ALLOWABLE LIMITS PER SRM / REMOVED AND REPLACED R/H HORIZONAL LEADING EDGE PER AMM 27-41-21. TAG NO: 684872 PN ON: 186A1001-16 SN ON: WN259 PN OFF: SN OFF: WN250
FWD CARGO; FWD CORNER SCUFF PLATE CRACKED. / REPAIRED PER W/O#RA22N0. INSTALLED FWD CARGO FWD SCUFF PLATE PER AMM 53-11-02.
FWD CARGO; AFT CORNER SCUFF PLATE CRACKED. / REPAIRED PER W/O#RA22N1. INSTALLED FWD CARGO AFT SCUFF PLATE PER AMM 53-11-02.
AFT CARGO; FWD CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED PER AMM.53-11-02
LEFT WING TRAILING EDGE STRUCTURE HAS A CRACKED WIGGLE PLATE I/B OF #3 FLAP TRACK AND O/B OF PANEL 551DB. / REMOVED AND REPLACED L/H WING LOWER SURFACE WIGGLE PLATE; I/B OF #3 FLAP TRACK AND O/B OF PANEL 551DB IAW SRM 51-40-05; SRM 51-20-01;SRM 51-40-02.
RIGHT WING TRAILING EDGE STRUCTURE HAS A CRACKED WIGGLE PLATE I/B OF #7 FLAP TRACK AND O/B OF PANEL 651DB. / REMOVED DAMAGED WIGGLE PLATE AND INSTALLED NEW PLATE PER SRM 51-40-02.
EMERGENCY LIGHT LENS IS NOT SECURE IN BULLNOSE ABOVE SEAT 1ABC / REMOVED AND REPLACED LENS PER AMM 33-51-03
CO-PILOT SIDE EMER EXIT TUBE LIGHT INOP. (SIDE WALL LIGHT) / DMA # 0167599 R&R R/H OVERWING SIDEWALL LIGHT BALLAST IAW MM 33-21-00. CL # 37516
RT FLASHLIGHT AFT GALLEY INOP OK TO CONT PER MEL 25-12-01 SP 1B TRACKING # 35103 / R&R AFT FLIGHT ATTENDANT FLASH LIGHT BATTERY PER 'SIP'. CLEARING # 35110
AFT GALLEY EMERGENCY FLASHLIGHT RED LIGHT WON'T BLINK. / R&R BATTERY IAW AMM 25-64-00
AFT EMERGENCY FLASHLIGHT INOP RESEATED AFT EMERGENCY FLASHLIGHT IN HOLDER. OPS CHECKS GOOD PER AMM 25-64-00
OVERHEAD OVERWING EXIT EMERGENCY LIGHT INOP AND ALL L/H OVERWING EMERGENCY LIGHTS INOP R&R L/H OVERWING EXIT BATTER PACK PER AMM 33-51-06 OPS NORMAL
OVERHEAD OVERWING EXIT EMERGENCY LIGHT INOP AND ALL L/H OVERWING EMERGENCY LIGHTS INOP / R&R L/H OVERWING EXIT BATTER PACK PER AMM 33-51-06 OPS NORMAL
BATTERY PACKS AT M01670 AND M01673 WILL NOT ILLUMINATE EMERGENCY LIGHTS FOR 15 MINUTES. REMOVED AND REPLACED PER AMM 33-51-06
RT EMERGENCY EXIT LIGHTS INOP NEAR OVERWING EXIT. R&R BATTERY PER AMM.
L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED MAIN DOOR SLIDE IAW AMM.
PANEL 193B HAS ELONGATED/ENLARGED FASTENER HOLES WITH PULLING THROUGH FASTENERS AT LOCATIONS 3; 4; 5; 6; 7; 8; 12; 13; 14; 15; 16; 19; 20; 21; 22; 28; 29; 30; 31; 32; 33; 34; 35; AND 36 / REPLACED PANEL B193 AS PER AMM 53-51-21
L/H OVERHEAD EMERGENCY LIGHT INOP BETWEEN SEAT 17 TO SEAT 20. / R&R POWER SUPPLY ASSEMBLY PER AMM.
L/H OVERHEAD EMERGENCY LIGHT INOP BETWEEN SEAT 17 TO SEAT 20. / R&R LIGHT ASSEMBLY PER AMM.
R2 DOOR EMERGENCY SLIDE EGRESS LIGHT INOP. RELAMPED LIGHT PER MM.
INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, STR 26R. R&R INTERCOSTAL PER SRM.
FWD CARGO AFT CORNER SCUFF PLATE CRACKED / REMOVED AND REPLACED CORNER SCUFF PLATE PER AMM 53-11-02.
FORWARD GALLEY OUTBOARD LOWER EMERGENCY EXIT LIGHT INOP. R&R SIGN PER MM.
BOW-TIE PANEL IN L/H WHEEL WELL BROKEN PN# 149A7656-1. / REMOVED AND REPLACED BOW-TIE PANEL IN L/H WHEEL WELL PN# 149A7656-1 PER SRM 51-40-02
FWD CARGO; FWD CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED SCUFF PLATE PER AMM 53-11-02.
LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON LOWER FLANGE NEXT TO STIFFENER RADIUS AT APPROX 18" FROM FORWARD EDGE. REPAIRED RIB PER SRM.
FORWARD CARGO INTERCOSTAL CRACKED ABOVE STR 26L AT STA 500A. / REMOVED AND REPLACED INTERCOSTAL AT STA. 500A-500B ABOVE STR 26L IAW SRM 51-40-02. SEE TASK AND WIPS FOR INDIVIDUAL SIGN OFFS.
AFT CARGO COMPARTMENT RT WALL SUPPORT IN LAV TANK AREA ANGLE CRACKED AT BS 867, LBL 10. R&R ANGLE PER SRM.
FORWARD CARGO STRINGER CLIP CRACKED AT BS 500D, STR 19R. R&R CLIP IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, BL 0. R&R ANGLE PER SRM.
AFT CARGO; LEFT HAND TRANSITION ANGLE; FROM STATION 727D TO 807; HAS MULTIPLE AREAS OF CORROSION. / REMOVED CORROSION AT MARKED AREAS AND IS OUT OF LIMITS I/A/W SRM 53-00-53-1A-2. CUT OUT DAMAGED AREA FROM STATION 727C+7 TO 814 LBL 24 I/A/W SRM 53-00-53-2R-5. REMOVED AND REPLACED TRANSITION ANGLE FROM STA.727C+10 TO STA.807+10 PER SRM.53-00-53-2R-5
INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C, STR 25L. R&R INTERCOSTAL PER SRM.
INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, RBL 9. R&R ANGLE PER SRM.
INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, BL 0. R&R INTERCOSTAL PER SRM.
INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, BETWEEN LBL 12 TO LBL 13. R&R ANGLE PER SRM.
AFT GALLEY WEB CORRODED AT BS 1026, LBL 18.5. R&R WEB PER SRM.
GALLEY FLOORBEAM CORRODED AT BS 986, LBL 44. REPAIRED BEAM PER SRM.
AFT CARGO FLOOR BOARD STRAP SPLICE IS CORRODED AT STA 887. / REMOVED AND REPLACED SPLICE STRAP PER SRM 51-40-02. SEE INDIVIDUAL WIPS FOR PROGRESSION.
FORWARD GALLEY DOOR L ANGLE CRACKED AT BS 294.5, STR 17L. R&R L ANGLE IAW SRM.
INTERCOSTAL CRACKED AT BS 328, RBL 35. R&R INTERCOSTAL PER SRM.
AFT CARGO FLOOR BOARD STRAP SPLICE IS CORRODED AT STA 772 / R&R AFT CARGO FLOOR BOARD STRAP SPLICE AT STA 772 PER SRM 51-40-02
FORWARD GALLEY DOOR SURROUND STRUCTURE STRINGER CLIP CRACKED EAT BS 277, STR 10R. R&R CLIP IAW SRM.
LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON VERTICAL STIFFENER, 19" AFT OF FORWARD SPAR STAB STA 120.30. REPAIRED RIB PER SRM.
LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON VERTICAL STIFFENER, 36" AFT OF FORWARD SPAR STAB STA 120.30. REPAIRED RIB PER SRM.
LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON VERTICAL STIFFENER 27" AFT OF FORWARD SPAR AT STAB STA 120.30. REPAIRED RIB IAW EA.
GALLEY FLOOR BEAM AT STA. 986 RBL 44 HAS EXFOLIATED INNER GRANULAR CORROSION AT FASTENER HOLE.((MARKED) / REPAIRED FLOOR BEAM UPPER CHORD AT STA 986.5 PER EA 1-753-32834 SEE EA FOR INDIVIDUAL WORK. C/W EA 1-753-32834
R2 DOOR THRESHOLD Z ANGLE CORRODED ON UPPER SURFACE BETWEEN BS 960 TO BS 980. R&R Z ANGLE IAW SRM.
STRINGER CLIP CRACKED AT BS 500D, STR 19L. R&R CLIP PER SRM.
THE FWD CARGO COMPARTMENT L/H TRANSITION ANGLE HAS CORROSION AROUND THE FASTENER HOLES FROM STA 509 TO 500B +11. / WP:E41753-CHAPPA; LEE - 06/20/2018 09:28 COMPLETE: REMOVED AND REPLACED DAMAGED SECTION OF L/H TRANSITION ANGLE FROM STA. 480 TO STA. 500D PER SRM 53-00-53-2R-5. SEE INDIVIDUAL SUB TASKS AND WIPS FOR PROGRESSION.
LEFT WING PANEL 561AB HAS SEVERAL SCREW HOLES BULGEDAND CRACKING ON LEADING EDGE UNDER SEAL AREA MARKED / REPAIRED HOLES PER SRM 51-70-04; REPAIR #9. RESTORED FINISH PER AMM 51-21-73 AND AMM 51-21-81.
LT EMERGENCY LIGHT LENS CRACKED AT ROW 1. R&R LENS PER AMM.
RT CLEAR EMERGENCY LIGHT LENS CRACKED ABOVE SEATS BETWEEN ROW 13 TO ROW 19. R&R LENS PER MM.
LT CLEAR EMERGENCY LIGHT LENS CRACKED ABOVE SEATS BETWEEN ROW 14 TO ROW 24. R&R LENS PER MM.
LT EMERGENCY LIGHT LENS CRACKED AT ROW 9. R&R LENS PER MM.
R1 DOOR SLIDE AFT GIRT BAR RETAINER LOOSE. SECURED RETAINER IAW MM.
R1 DOOR SLIDE FWD GIRT BAR RETAINER LOOSE. SECURED RETAINER IAW MM.
R1 DOOR EMERGENCY LIGHT IN THE LOWER FORWARD CORNER INOPERATIVE. R & R THE LIGHT ASSEMBLY IAW AMM.
L2 DOOR ASSIST HANDLE BROKEN. R&R HANDLE PER MM.
AFT OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
R2 DOOR OUTER SIGN LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
R2 DOOR INNER SIGN INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
CABIN FLOOR INTERCOSTAL LOCATED BETWEEN STA 344 AND STA 360 AT LBL 0 IS CRACKED. / REMOVED AND REPLACED REF SRM 51-40-02.
CABIN FLOOR INTERCOSTAL LOCATED BETWEEN STA 312 AND STA 328 ON THE LH SIDE BELOW THE FWD. ENTRY DOORWAY IS CRACKED. / REMOVED AND REPLACED REF SRM 51-40-02.
DIVERSION, SHORTLY AFTER LEVELING AT CRUISE, HEARD A POP FOLLOWED BY NR 1 FORWARD AND NR 2 AFT FUEL PUMP LOW PRESSURE LIGHTS ILLUMINATED, AS WELL AS FORWARD LEFT AND RIGHT SIDE WINDOW HEAT OVERHEAT LIGHTS ON. R&R PG1 PANEL PER AMM.
NR 2 MAIN TANK HAD POSSIBLE FUEL LEAK, LEFT MAIN AT 8500 RIGHT MAIN AT 8480. AT 1505Z LEFT MAIN AT 8100 RIGHT MAIN AT 7720 - 380LB IMBALANCE IN 14 MINUTES. COMPLIED WITH QRH AND SHUT DOWN NR 2. FUEL FLOW AT FL 370 WAS DEAD EVEN. CENTER TANKS WERE BEING USE PRIOR TO QRH AND NR 2 MAIN WAS NOTICEABLY DECREASING FUEL QUANTITY WHERE NR 1 MAIN REMAINED AS EXPECTED WITH CENTERS ON.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITIONED. REPOSITIONED SLIDE IAW MAINTENANCE.
LOWER COMPOSITE WEB CRACKED AT BS 663, BETWEEN RBL 30 TO RBL 33. REPAIRED WEB IAW EA.
RIGHT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB IAW SRM.
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY PACK IAW AMM.
R1 DOOR SLIDE, AFT GIRT BAR HOOK LOOSE. SECURED HOOK IAW SRM.
R2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.
FORWARD RT EMER LIGHT BATTERY PACK FAILED LONG TEST. R & R BATTERY IAW AMM.
RIGHT WING INBD LE FLAP CRACKED. R & R LE FLAP ASSEMBLY IAW MM.
R1 DOOR ABOVE EMER EXIT LIGHT INOPERATIVE. SECURED LIGHT IAW AMM.
EMERGENCY EXIT LIGHT ON AFT WALL OF FWD LAVATORY LENS BROKEN. R & R LENS IAW MM.
FLOORBEAM CRACKED AT STATION 727B, RBL 45. REPAIRED BEAM IAW EA.
LONGITUDINAL FLOORBEAM INBD FLANGE CRACKED AT BS 727B RBL 45. REPAIRED BEAM IAW EA.
LONGITUDINAL FLOORBEAM, INBD FLANGE CRACKED AT BS 727B LBL 45. REPAIRED FLANGE IAW EA.
LONGITUDINAL FLOORBEAM OTBD FLANGE CRACKED AT BS 727B RBL 24. REPAIRED FLANGE IAW EA.
CENTER WING WEB CRACKED AT STATION 663, LBL 42. REPAIRED WEB IAW SRM.
RIGHT NR 3 COCKPIT WINDOW FRAME POST E - F 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SI.
LEFT NR 3 COCKPIT WINDOW FRAME POST E - F, 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SI.
AFT CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN STATION 747 TO 767, RBL 22. R & R Z ANGLE IAW SRM.
AFT CARGO COMPARTMENT Z ANGLE DAMAGED AT STATION 727D+10, LBL 22. REPAIRED Z ANGLE IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STATION 92.70. REPAIRED STIFFENER IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STATION 120.30. REPAIRED RIB IAW SRM.
LEFT EXTERIOR EMERGENCY LIGHT NR 3 INOPERATIVE. RELAMPED IAW MM.
R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS ASSEMBLY IAW MM.
R2 DOOR EMERGENCY EXIT LENS BROKEN. R & R LENS IAW AMM.
FWD ENTRY DOOR EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY IAW M/M.
R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM.
DIVERSION -- FUEL TANKS BOOST PUMPS LOW PRESS LIGHTS INDICATIOS, LEFT FWD & RIGHT FWD COCKPIT WINDOWS OVHT LIGHTS IND, ACARS INOP. ALL OTHER INDICATIONS NORMAL. FOUND TRANSFER BUS SEC-2 C/B TRIPPED. REMOVED AND REPLACED NR 1 ENGINE IDG & GCU.
LEFT EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.
EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.
FWD EEPLS INOP. RELAMPED EEPLS PER MM.
FLOORBEAM CORRODED AT BS 767+7 , LBL 8.1. REPAIRED BEAM IAW EA.
Z-CHANNEL CORRODED AT BS 907. REPAIRED Z-CHANNEL IAW SRM.
RIGHT HORIZONTAL LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL LOWER SKIN CRACKED AT STA 175.5. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN IAW SRM.
EMERGENCY EGRESS LIGHT INOP AT ROW 2. REMOVED AND REPLACED LIGHT IAW MM.
L1 DOOR EMERGENCY EVAC SLIDE BRACKET LOOSE. SECURED BRACKET PER MM.
CENTER OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
L1 DOOR EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
R2 DOOR LOWER EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT FWD END. SECURED EEPLS WIRING PER MM.
LT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER EPR MM.
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED CLIP PER MM.
EMERGENCY LIGHTS ARE BROKEN AT ROW 1. REMOVED & REPLACED EMERGENCY LIGHTS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 4. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 4. RELAMPED PER MM.
L1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INSPECTION WINDOW CRACKED. REMOVED AND REPLACED LENS PER MM.
AFT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS LIGHT BROKEN NEAR FWD GALLEY. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
R1 DOOR AFT GIRT BAR HOOK LOOSE. REPLACED HOOK PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 15 ABC. INSTALLED COVER PER MM.
EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.