N917WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
L1 GIRT BAR LOOSE. REMOVED FORWARD ENTRY ESCAPE SLIDE, REMOVED & REPLACED RIVETS FOR GIRT BAR HOOK, & REINSTALLED FORWARD ENTRY ESCAPE SLIDE IAW MT 725-61-06 & SRM 51-40-02.
NR 1 ENG SLOW TO SPEED (NR 2 AT +50% BEFORE NR 1 MOVED FROM 10%) (6-8 SECONDS BEHIND NR 2) ONCE STABILIZED ALL INDICATIONS NORMAL. RESPONDED NORMAL ONCE ABOVE 45%. REMOVED AND REPLACED NR 1 HMU IAW AMM 73-21-10 AND MT 773-21-10. PERFORMED TEST NR 8 IAW AMM 71-00-00.
SLIDE AT DOOR 1L FELL OUT OF DOOR LINER WHEN DOOR WAS OPENED. REPACKED L1 FWD ENTRY EMERGENCY SLIDE IAW MT 725-61-06.
FWD ENTRY DOOR SLIDE GIRT BAR STOW HOOK LOOSE;NEEDS TO BE SECURED. INSPECTED GIRT BAR HOOK IAW AMM 25-66-01;GIRT BAR IS SECURED IN STOWED POSITION ;OK FOR SERVICE
NR 1 ENGINE SLOW TO SPOOL FOR TAKE OFF. RT ENGINE AT TAKE OFF THRUST & LT ENGINE AT 45%. IAW FIM 73-05, TASK 814. PERFORMED TEST 8 ACCELERATION CHKD AMM 71-00-00. TEST PASSED; NO DEFECTS FOUND.
COCKPIT EMERGENCY LIGHT LENS WILL NOT SECURE IN PLACE. OK TO CONT IAW MEL 33-1-01 SP1. LIGHT REMAINS OPERATIONAL. NSTALLED LENSE IAW AMM 33-14-00.
R1 DOOR; DOOR-ASSIST HANDLE LOOSE. ADJUSTED R1 DOOR ASSIST HANDLE IAW AMM 52-11-00.
ELONGATED HOLES ON ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACKED ANGLE, TRAILING EDGE ACCESS PANEL 551FB ON LT WING. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, AND DWG 115A2710, SHEET 9, REV A.
MAIN CABIN FLOORBEAM CRACKED AT BS 540, BL 0 - LBL 24.75. REPLACED FLOORBEAM IAW SRM 51-40-02, AND DWG 143A5240, SHEET 14, REV -.
MAIN CABIN, FWD WET AREA FLOOR SUPPORT CRACKED, BTW BS 312 - 328, RBL 27. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 39, REV-.
CORROSION WEB LOWER SILL LOCATED BETWEEN BS 440 TO BS 492.4, RBL 22, WL156 FWD CARGO BAY. REPLACED THE WEB LOWER SILL LOCATED BETWEEN BS 440 - 492.4, RBL 22, WL156 IAW SRM 51-10-02, ITEM 9 AND DWG 143A8330, SHEET 42, REV A.
CORROSION WEB LOWER SILL LOCATED BETWEEN BS 440 - 492.4, RBL 22, WL 156 IN THE FWD CARGO BAY. REPLACED WEB LOWER SILL IAW SRM 51-10-02, ITEM 9, & DWG 143A8330, SHEET 42, REV A.
DELAMINATED FLOOR PANEL 231WF IN THE PASSENGER CABIN. REPAIRED THE FLOOR PANEL 231WF IAW SRM 53-00-50-2R-4, REPAIR 4.
AMAIN CABIN, FWD WET AREA FLOOR SUPPORT HAD A CRACK BTW BS 312 & 328, RBL 27.
CRACKED CORRUGATED PLATE, TRAILING EDGE ORSS 462 ON LT WING. REPLACED CORRUGATED PLATE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND SRM 51-40-02-0G-0. LENGTH OF CRACK: 0.528 INCHES.
CRACKED SUPPORT BRACKET, TRAILING EDGE MLG SUPPORT BEAM REAR SPAR UPPER AREA, LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0, AND SRM-51-10-02-0G-0, ITEM 9. LENGTH OF CRACK: 0.986.
CORROSION ANGLE LOCATED ON UPPER MAIN SILL AT LEVEL BS 827, S18R, WL 200 IN THE AFT CARGO BAY. REPLACED ANGLE LOCATED ON UPPER MAIN SILL IAW SRM 51-10-02, SRM 51-40-02, AND DWG 146A8313, SHEET 2, REV-.
CRACKED SUPPORT ANGLE BS 663.75 AND LBL 42. PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE IAW SRM 57-10-10-2R-5, REPAIR 5. CERTIFIED RII MAJOR REPAIR WORK PERFORMED.
CORROSION STRAP LOCATED BTW BS 787 - 794.3, S25R - 26R, WL 156 IN THEAFT CARGO BAY. REPLACED STRAP & FASTENERS LOCATED IAW SRM 51-40-02-0G-0, AND DWG 146A0081, SHEET 37, REV -.
CORROSION LOWER SILL LOCATED BTW BS 794.3 - 847, RBL 22, WL 156 IN THE AFT CARGO BAY. REPLACED LOWER SILL AND FASTENERS IAW SRM 51-40-02, & DWG 146A8340, SHEET 28, REV -.
CRACKED CORRUGATED PLATE, TRAILING EDGE IRSS 215, RT WING. REPLACED THE CORRUGATED PLATE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND SRM 51-40-02-0G-0. LENGTH OF CRACK: 1.117 INCHES.
CRACKED WEB TRAILING EDGE FIXED PANEL ORSS 271, LT WING. REPLACED THE WEB AND FASTENERS IAW SRM-51-10-02-0G-0, ITEM 9, SRM-51-40-02-0G, & DWG 115A2512, SHEET 16, REV-.
CRACK INDICATION FOUND ON RT HORIZONTAL STAB, LOWER IN-SPAR SKIN AT HSS 193.90, RIB, 9 INCH REAR SPAR IN SIDE OF RIB. CRACK LENGTH = 1.000 INCH. PERFORMED A REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11.
CRACK INDICATION FOUND ON RT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 193.90, RIB, 9 INCHES REAR SPAR INSIDE OF RIB. CRACK LENGTH = 1.000 INCH. PERFORMED REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11.
CRACK ON TIE CLIP LOCATED BS 277, STR 10R IN PASSENGER CABIN. REPLACED TIE CLIP IAW SRM 51-10-02-0G-0, STEP 9, SRM 51-40-02-0G-0, AND DWG 141A1110, SHEET 18, REV -.
CRACK ON LOWER STUB FRAME LOCATED BS 294.5, S17R IN FWD GALLEY AREA. REPLACED LOWER STUB FRAME IAW SRM 51-10-02, ITEM 9, & DWG 141A8370, SHEET 10, REV D.
CORRODED SUPPORT ZEE, LOCATED BETWEEN BS 727C - 787, LBL 22, WL156 IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ZEE BS 727 - 847, LBL 22, WL156 IAW SRM 53-00-53-2R-5, REPAIR 5, SRM 51-10-02, ITEM 9, DWG 146A7500, SHEET 113, REV -, & DWG: 146A7502, SHEET 27, REV - .
CORRODED STRAP FLOOR SUPPORT LOCATED BETWEEN BS 787 - 794.3, RBL 20, WL 156 IN THE AFT CARGO BAY. TASK CARD WAS DUPLICATED; FOR RESOLUTION SEE TTG8Q018SGUS.
CRACKED KEELBEAM, BS 727 - 727A, S27R, REPAIRED THE KEELBEAM IAW EA 25-153-03151-WIP1, EA 25-153-03151, & SRM 53-60-12-2R-1, REPAIR 1.
CORRODED SHIELD WEB BETWEEN BS 767 - 794.3, RBL 22, WL 156 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A0081, SHEET 37, REV-.
CORRODED SUPPORT ZEE, BS 727E - 767, RBL 22, WL 156, IN THE CARGO BAY. REPLACED THE SUPPORT ZEE & FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 146A7500, SHEET 13, REV-,
CORROSION UPPER MAIN SILL LOCATED BETWEEN BS 794.3 - 847, S18R, WL 200 IN THE CARGO BAY. REPLACED UPPER MAIN SILL IAW SRM 51-40-02-0G-0, DWG 146A8110, SHEET 25, REV A, & DWG 146A8111, SHEET 16, REV -.
CRACKED LOWER STUB FRAME, BS 294.5, S17R IN THE FWD GALLEY AREA. REPLACED THE LOWER STUB FRAME IAW SRM 51-10-02, ITEM 9, & DWG 141A8370, SHEET 10, REV D.
CORRODED SHIELD WEB, BETWEEN BS 492.4 - 500A, RBL 22, WL 156 IN THE FWD CARGO BAY. REPLACED THE SHIELD WEB & FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 143A0080, SHEET 23, REV -.
CRACKED ANGLE, LOCATED BS 500C, S26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV -.
CRACKED SUPPORT BEAM, TRAILING EDGE ORSS 280 ON LT WING. REPLACED THE SUPPORT BEAM IAW SRM 51-10-02-0G-0, 51-40-02, & DWG 115A3712, SHEET 5, REV -.
CRACK INDICATION FOUND LOCATED AT BS 291.5 PLUS 10 INCHES, S7R BELOW 4.200 INCHES. PERFORMED REPAIR ON BEAR STRAP HOLE IAW EA 25-153-03090-WIP1, & 25-153-03090-WIP2.
CORROSION ON LATERAL INTERCOSTAL, BS 269, BL0, WL 208.1. PERFORMED REPAIR ON LATERAL INTERCOSTAL IAW EA 25-153-03197-WIP1, AND EA 25-153-03197.
CORRODED FLOORBEAM LOWER FLANGE, BS 986.5, RBL 40, WL 208.5. REPAIRED THE FLOORBEAM IAW EA 25-153-03177-WIP1, EA 25-153-03177, AND SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.
CRACKED FLOOR SUPPORT BTW BS 344 - 360, BL 0, IN THE FWD GALLEY AND LAV. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, AND DWG 141A5400, SHEET 32, REV-.
CRACKED FLOOR SUPPPORT BTW BS 277 - 294.5, BL 0, IN THE FWD GALLEY & LAV. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400, SHEET 20, REV -.
CORRODED ZEE ANGLE, BS 312, LBL 55, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE ZEE ANGLE IAW SRM 51-40-02-0G-0.
CORRODED ZEE ANGLE, BS 312, LBL 55, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE ZEE ANGLE IAW SRM 51-40-02-0G-0.
ELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE ON RT WING. REPAIRED THE ACCESS PANEL 661CB TRAILING EDGE IAW SRM 51-70-04-2R-10, REPAIR 10.
ELONGATED HOLES ON ACCESS PANEL 661AB ON RT WING. REPAIRED ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10.
ELONGATED HOLES ON ACCESS PANEL 661BB ON RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACK WEB FLOOR STRUCTURE, BETWEEN BS 328 - 344, LBL 45 IN THE FWD GALLEY AND LAVATORY. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02, & DWG 141A5400, SHEET 44, REV -.
CRACK SUPPORT BEAM NR 4, LOCATED FOR THE FWD GALLEY DOOR. REPLACED SUPPORT BEAM NR 4 LOCATED FWD GALLEY DOOR IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A6516, SHEET 102, REV B.
CRACKED WEB FLOOR STRUCTURE LOCATED BTW BS 312 - 328, LBL 45. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02, & DWG 141A5400, SHEET 26, REV -.
DETERIORATED ENTRY AND SERVICE DOOR GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA. REPLACED ENTRY AND SERVICE DOOR GIRT BAR FITTING HARDWARE AT FWD GALLEY AREA IAW AMM 25-66-02-400-801.
CRACK ON VERTICAL STIFFENER, BS 540, BL 0, BULKHEAD AREA IN THE FWD CARGO BAY. REPLACED THE VERTICAL STIFFENER IAW SRM 51-10-02; SRM 51-40-02, DWG 111A2001, SHEET 113, REV B, AND DWG 111A2001, SHEET 114, REV B.
DETERIORATED ENTRY DOORWAY LINNING ASSIST HANDLE NUT AT FWD GALLEY AREA (2 EA). REPLACED ENTRY DOORWAY LINNING ASSIST HANDLE NUT AT FWD GALLEY AREA IAW MT 725-025-00-01Y FOR INSTALLATION REFER TO TTG8Q002EN3T STEP 12.
INOPERATIVE BATTERY PACK ON POWER SUPPLY M1668 IN PAX CABIN. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
INOPERATIVE BATTERY PACK ON POWER SUPPLY M1669 IN PAX CABIN. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
CRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, BTW S8 - 9R IN THE FWD GALLEY DOOR AREA, CRACK LENGTH 0.437 IN. REPLACED THE STUB FRAME IAW SRM 51-10-02, ITEM 9, DWG 141A8370, SHEET 9, REV-, AND DWG 141A8370, SHEET 10, REV-.
INOPERATIVE BATTERY PACK ON POWER SUPPLY M1670 IN PAX CABIN. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
INOPERATIVE BATTERY PACK ON POWER SUPPLY M1669 AT PAX CABIN. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805, TESTED OK.
CRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR BETWEEN BS 291 TO BS 294.5 AND BETWEEN S-8R TO S-9R. CRACK LENGTH 0.250 IN. APPROX. REPAIRED BEAR STRAP EXTERNAL SKIN IAW SRM 53-10-01-2R-6, AND EA M-25-153-01539.
CRACKED ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACKED LOWER SURFACE OF LEADING EDGE SLAT 3 NOSE SKIN AT THE ACTUATOR, AROUND FASTENER, LT WING. PERFORMED PERMANENT REPAIR ON LEADING EDGE SLAT 3 NOSE SKIN AT LT WING IAW B737-700 SRM 57-42-01-2R REPAIR 8.
CRACKED VAPOR BARRIER, LT SIDE BS 663.75. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACKED LOWER SURFACE OF LEADING EDGE SLAT 8 NOSE SKIN AT ACTUATOR, AROUND FASTENER, RT WING. PERFORMED PERMANENT REPAIR ON LEADING EDGE LOCATED ON SLAT 8 LOWER SKIN RT WING IAW SRM 57-42-01-2R, REPAIR 8.
CRACKED FLOOR PANEL 140DF IN THE AFT CARGO BAY. FABRICATED A NEW FLOOR PANEL 140DF IAW AMM 25-52-01-201-801, STEP 1 F, AND DWG 453A2610, SHEET 2, REV C.
AIRPLANE WAS NOT ABLE TO PRESSURIZE IN AUTO MODE. CABIN CLIMB GAGE WAS ERRATIC. OK ON MANUAL MODE. PERFORMED FIM 36-10 TASK 810. FOUND #2 ENGINE HIGH STAGE REGULATOR REGULATES CONTROL PRESSURE TOO LOW. REMOVED AND REPLACED #2 ENG. HIGH STAGE REGULATOR IAW AMM 36-11-07. OP'S CHECK GOOD. ENGINE SUPPLY PRESSURE WITHIN NORMAL OPERATION LIMITS AT IDLE.
AFT GALLEY SERVICE DOOR EMERGENCY ESCAPE SLIDE SKIRT WORN AND RUBBER COATING MISSING. REMOVED AND REPLACED SLIDE PER MT 725-61-06, INSPECTION C/W.
ONE OVERWING ESCAPE GROUND ILLUMINATION AND TWO AISLE EMERGENCY LIGHTS ON L/H SIDE INOP <[01]. REMOVED AND REPLACED E-LIGHT BATTERY PACK (M1670) PER AMM 33-51-06. ALL E-LIGHTS OPS CHECK GOOD.
F/E DOOR HANDLE PLATE CAME APART.<[01] R/R IAW SIP
FWD PASSENGER CABIN EMERGENCY LIGHTS INOP<[01] REPLACED FWD EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06.
FWD UPPER ISOLATOR IS CRACKED ON AFT ENTRY DOOR FOR SLIDE MOUNT.<[01] R&R FWD UPPER ISOLATOR ON AFT ENTRY DOOR IAW SRM 51-40-02.
FWD SERVICE DOOR CAM PLATE IS LOOSE<[01] SECURED FWD SERVICE DOOR CAM PLATE IAW AMM 20-50-11.;[02] C/W INSPECTION
FORWARD SERVICE DOOR (R1) HANDLE LOOSE<[01] REMOVED FORWARD SERVICE DOOR LINER AND HANDLE AND PNL 841BZ PER AMM 52-41-31;[02] TIGHTENED FORWARD SERVICE DOOR HUB HANDLE ATTACH BOLT AND REINSTALLED DOOR LINER 841BZ PER AMM PER 52-41-31.
FWD SERVICE DOOR ( 1R) SLIDE RAFT ; TOO MUCH MATERIAL EXPOSED BELOW CONTAINER.<[01] REPACKED FWD SERVICE DOOR SLIDE PER MT 725-61-06.
FWD SERVICE DOOR LOWER EMERGENCY EXIT LENS MISSING DIRECTIONAL ARROW<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]
LOOSE GIRT BAR FITTING AT AFT GALLEY AREA L2 DOOR 2023-694906<[01] TIGHTENED GIRT BAR FITTING AT AFT GALLEY AREA L2 DOOR IAW SOPM 20-50-01 REV.38;[02] CORRECTED STEP 1 TIGHTENED GIRT BAR FITTING AT AFT GALLEY AREA L2 DOOR IAW AMM 25-66-02-400-801.;[03] CERTIFIED WORK PERFORMED.
CRACK ON ANGLE BS 663 AND LBL 25 COMMON TO VAPOR BARRIER LOWER POSITIO<BR>N MAIN WHEEL WELL COMPARTMENT 2023-694871 CRACK ON ANGLE BS 663 AND LBL 25 COMMON TO VAPOR BARRIER LOWER POSITION MAIN WHEEL WELL COMPARTMENT<[01] REPLACED ANGLE BS 663 AND LBL 25 COMMON TO VAPOR BARRIER LOWER POSITION MAIN WHEEL WELL IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 111A1000 SHEET: 249 REV: A AND DWG 149A7210 SHEET: 13 REV: -<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW. RII.
CRACK TRACK RBBL 13.84 BS 727D AFT CARGO COMPARTMENT 2023-694859<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24;[02] REWORK CARGO TRACK LOCATED RBBL 13.84 BS 727D AFT CARGO COMPARTMENT EVALUATED AND FOUND WITH LIMIT IAW B737-700 SRM 53-00-53?1A-2 ALLOWABLE DAMAGE 2 PARAGRAPH 4.B;(1); FIGURE 103 DETAIL A. SEE INDIVIDUAL SIGN-OFF BELOW;[03] REWORK CARGO TRACK LOCATED RBBL 13.84 BS 727D AFT CARGO COMPARTMENT EVALUATED AND FOUND WITH LIMIT IAW B737-700 SRM 53-00-53?1A-2 ALLOWABLE DAMAGE 2 PARAGRAPH 4.B;(1); FIGURE 103 DETAIL A. SEE INDIVIDUAL SIGN-OFF BELOW
CRACK ACCESS PANEL 321A WEB ON RIB 8 AT VERTICAL STABILIZER 2023-694829<[01] TOOL USED TEMPERATURE CONTROLLER P/N:P3015GOES00000;S/N:142811620;DUE DATE:25-JAN-24.;[02] REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 SHEET 7 REV.-<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 SHEET 7 REV.-<BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE LOCATED BS 500C STR 26L AFT FACE FWD CARGO COMPARTMENT 2023-694800<[01] REPLACED ANGLE LOCATED BS 500C STR 26L AFT FACE FWD CARGO COMPARTMENT IAW SRM 51-10-02 ÿ½TEM 9 AND SRM 51-40-02 AND DWG 143A7505 SHEET 82 REV.-;[02] REPLACED ANGLE LOCATED BS 500C STR 26L AFT FACE FWD CARGO COMPARTMENT IAW SRM 51-10-02 ÿ½TEM 9 AND SRM 51-40-02 AND DWG 143A7505 SHEET 82 REV.-
CRACK STRINGER 25L LOCATED BS 540 FWD CARGO COMPARTMENT 2023-694799<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 12-MAR-24.;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[04] PERFORMED PERMANENT REPAIR ON STRINGER 25L LOCATED BETWEEN BS500C AND BS540 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 AND B737-700 SRM 51-40-02<BR>SEE INDIVIDUAL SIGN OFF BELOW;[05] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ANGLE LOCATED BS 400 STRI 26L FWD CARGO COMPARTMENT 2023-694802<[01] REPLACED ANGLE LOCATED BS 400 STRI 26L FWD CARGO COMPARTMENT IAW SRM 51-10-02 ÿ½TEM 9 AND SRM 51-40-02 AND DWG 143A7505 SHEET 82 REV.-;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE LOCATED BS 400 STRI 26L FWD CARGO COMPARTMENT IAW SRM 51-10-02 ÿ½TEM 9 AND SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV.-;[03] TASK CARD COMPLETED
CRACK ANGLE LOCATED BTW BS 907 TO BS 927 BTW STR 25R TO STR 27R AFT CARGO COMPARTMENT 2023-694809<[01] REPLACED ANGLE LOCATED BTW BS 907 TO BS 927 BTW STR 25R TO STR 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 147A7221 ; SHEET 27 ; REV -.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED BTW BS 907 TO BS 927 BTW STR 25R TO STR 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 147A7221 ; SHEET 24 ; REV -.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK CARD COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW
CRACK TRACK LBBL 17.24 LOCATED BS 727E AFT CARGO COMPARTMET 2023-694807<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24;[03] REPAIRED CARGO TRACK RBBL 17.24 LOCATED BTW BSTA 727D AND BSTA 747 IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 TABLE 201 FIGURE 203.;[04] CORRECTED STEP 3 <BR>REPAIRED CARGO TRACK RBBL 17.24 LOCATED BTW BSTA 727D AND BSTA 747 IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 TABLE 201 FIGURE 203. SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED STEP 4.<BR>REPAIRED CARGO TRACK LBBL 17.24 LOCATED BTW BSTA 727D AND BSTA 747 IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 TABLE 201 FIGURE 203. SEE INDIVIDUAL SIGN OFF BELOW;[06] REPAIRED CARGO TRACK LBBL 17.24 LOCATED BTW BSTA 727D AND BSTA 747 IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 TABLE 201 FIGURE 203. SEE INDIVIDUAL SIGN OFF BELOW. RII
CRACK ANGLE - SUPPORT LOCATED BS 867 AT LEVEL STR 26L AFT CARGO COMPARTMENT 2023-694808<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 867 AT LEVEL STR 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ; DWG 149A8102 ; SHEET 17 ; REV -.;[02] JOB COMPLETED
CRACK TRACK RBBL 13.84 LOCATED BTW BS 727D TO BS 767 AT AFT CARGO COMPARTMENT (4 EA) 2023-694804<[01] TOOL USED : EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N 00X12101V022237 DUE DATE: 26-JAN-24.;[02] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BTW BSTA 727D AND BSTA 787 IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND 2; TABLE 201 FIGURE 203.;[03] CORRECTED STEP 2.<BR>REPAIRED CARGO TRACK RBBL 13.84 LOCATED BTW BSTA 727D AND BSTA 787 IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND 2; TABLE 201 FIGURE 203. SEE INDIVIDUAL SIGN OFF BELOW;[04] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BTW BSTA 727D AND BSTA 787 IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND 2; TABLE 201 FIGURE 203. SEE INDIVIDUAL SIGN OFF BELOW. RII.
CRACK FRAME ON BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2023-694805<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] REPLACED FRAME LOCATED ON BS 947.5 AND BTW STR24R TO STR24L AT AFT CARGO COMPARTMENT I.A.W SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING 147A1047-112 REV.- ;DWG 147A0002-11 REV.-; DWG 147A0040-12 REV.- ;DWG 147A7500-19 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED FRAME LOCATED ON BS 947.5 AND BTW STR24R TO STR24L AT AFT CARGO COMPARTMENT I.A.W SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING 147A1047-112 REV.- ;DWG 147A0002-11 REV.-; DWG 147A0040-12 REV.- ;DWG 147A7500-19 REV.- SEE INDIVIDUAL SIGN OFF BELOW. RII
CORROSION BILGE AREA SHEAR PLATE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT 2023-694811<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ;DWG 146A0081 ; SHEET 37 ; REV 0.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ;DWG 146A0081 ; SHEET 37 ; REV -.;[03] CORRECTED STEP 1 ; 2.<BR>REPLACED ANGLE AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ;DWG 146A0081 ; SHEET 37 ; REV -.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[04] REPLACED ANGLE AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ;DWG 146A0081 ; SHEET 37 ; REV -.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW. ITEM RII
CORROSION BILGE AREA ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT 2023-694812<[01] REPLACED ANGLE AND FASTENERS LOCATED BILGE AREA ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 51-40-02 AND DWG 146A8123 REV -<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE AND FASTENERS LOCATED BILGE AREA ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ;DWG 146A8123 REV -<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPLACED ANGLE AND FASTENERS LOCATED BILGE AREA ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ;DWG 146A8123 REV -<BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII
CRACK WEB - INTERCOSTAL LOCATED BS 947.5 AT LEVEL STR 25R AFT CARGO COMPARTMENT 2023-694810<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ÿ½TEM 9 AND DWG 147A7500 SHEET 29 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ÿ½TEM 9 AND DWG 147A7500 SHEET 29 REV-. SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION ON INNER CHORD LOCATED ON FLOOR STRUCTURE BTW BS 312 TO BS 328 AT FWD GALLEY AREA WL 208.1 2023-694787<[01] REPLACED INNER CHORD LOCATED ON FLOOR STRUCTURE BTW BS270 TO BS360 AT FWD GALLEY AREA WL 208.1 .IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 11 REV- DWG 141A8110 SHEET 9 REV A DWG 142A0050 SHEET 15 REV- DWG 141A8310 SHEET 25 REV B;[02] CORRECTED STEP 1<BR>REPLACED INNER CHORD LOCATED ON FLOOR STRUCTURE BTW BS270 TO BS360 AT FWD GALLEY AREA WL 208.1 .IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 11 REV- DWG 141A8110 SHEET 9 REV A DWG 142A0050 SHEET 15 REV- DWG 141A8310 SHEET 25 REV B SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED INNER CHORD LOCATED ON FLOOR STRUCTURE BTW BS270 TO BS360 AT FWD GALLEY AREA WL 208.1 .IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 11 REV- DWG 141A8110 SHEET 9 REV A DWG 142A0050 SHEET 15 REV- DWG 141A8310 SHEET 25 REV B SEE INDIVIDUAL SIGN OFF BELOW.AS RII.JOB COMPLETED.
CORROSION ON FITTING LOCATED ON FLOOR STRUCTURE BS 344 AND LBL 54 FWD GALLEY AREA WL 208.1 2023-694786<[01] REPLACED FITTING LOCATED ON FLOOR STRUCTURE BS 344 AND LBL 54 FWD GALLEY AREA WL 208.1 IAW SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED FITTING LOCATED ON FLOOR STRUCTURE BS 344 AND LBL 54 FWD GALLEY AREA WL 208.1 IAW SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII
CORROSION ON FITTING LOCATED ON FLOOR STRUCTURE AT BS 312 AND LBL 52 WL 208.1 2023-694785<[01] REPLACED FITTING LOCATED ON FLOOR STRUCTURE AT BS 312 AND LBL 52 WL 208.1 IAW SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FITTING LOCATED ON FLOOR STRUCTURE AT BS 312 AND LBL 52 WL 208.1 IAW SRM B737-700 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW<BR>RII
CORROSION ON FLOOR BEAM BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA 2023-694782<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24;[02] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24;[03] PERFORMED PERMANENT REPAIR FLOOR BEAM BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR FLOOR BEAM BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW.AS RII
CRACK WATER SERVICE DOOR 146AR SUPPORT ANGLE AT LOWER FUSELAGE 2023-694779<[01] REPLACED SUPPORT ANGLE LOCATED WATER SERVICE DOOR 146AR AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 147A7221 ; SHEET 15 ; REV B.;[02] TASK CARD COMPLETED
CRACK ON SUPPORT ANGLE LOCATED BS 695 BL0 AT CENTER WING BOX 2023-694773<[01] REPLACED SUPPORT ANGLE LOCATED BS 695 BL0 AT CENTER WING BOX IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9111 SHEET: 10 REV: - <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED BS 695 BL0 AT CENTER WING BOX IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9111 SHEET: 10 REV: - <BR>SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK ANGLE LOCATED BS 540; LBL 1 AT CENTER WING BOX 2023-694770<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 540; LBL 1 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND SRM 51-10-02.;[02] REPLACED ANGLE AND FASTENERS LOCATED BS 540; LBL 1 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND SRM 51-10-02.
CRACK ON SUPPORT ANGLE LOCATED BS 695; RBL 24.75 AT CENTER WING BOX 2023-694772<[01] REPLACED NEW ANGLE AND FASTENER LOCATED BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV.A<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED NEW ANGLE AND FASTENER LOCATED BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV.A<BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ON SUPPORT ANGLE LOCATED BS 540; RBL 1 AT CENTER WING BOX 2023-694771<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 540; RBL 1 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND SRM 51-10-02.;[02] REPLACED ANGLE AND FASTENERS LOCATED BS 540; RBL 1 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND SRM 51-10-02
CRACKED SIDEWALL TO CEILING SUPPORT ANGLE IN AFT CARGO COMPARTMNET BS 727C LT. WL 200 2023-694724<[01] REPLACED ANGLE AND FASTENERS LOCATED AT CEILING UPPER POSITION LH SIDE BETWEEN BS727A TO BS747 IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 149A9490 REV- . SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS LOCATED AT CEILING UPPER POSITION LH SIDE BETWEEN BS727A TO BS747 IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 149A9490 REV- . SEE INDIVIDUAL SIGN OFF BELOW.
INOP BATTERY POWER SUPPLY LT AND RT IN LOWERED CEILING AT AFT GALLEY AREA (2 EA) 2023-694601<[01] REPLACED BATTERY PACK LT IN LOWERED CEILING AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED <BR>TEST OK
CRACK GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT 2023-694655<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW
CRACK GUSSET LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT 2023-694656<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.
CUSTOMER REQUEST CRACK ON VAPOR BARRIER LH SIDE LOCATED STA 663 BTW LBL 31 TO LBL 45 2023-694536<[01] TOOL USED: CALIPER PN: 500-197-30 SN:B20189527 DUE DATE: 26-DEC-23.;[02] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18185781 DUE DATE: 24/JAN/24.;[03] TOOL USED: SCALE PN: CR5200 S/N: 8342514527 DUE DATE: 13/FEB/2024.;[04] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 24-JAN-24.;[05] TOOL USED: ULTRASONIC EQUIPMENT PN: EPOCH 6LT; SN: 230529908; DUE DATE: 22-AUG-24;[06] REPAIRED VAPOR BARRIER LH SIDE LOCATED STA 663 BTW LBL 31 TO LBL 45 IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED: SCALE P/N: CR5200; S/N: 8343110878; DUE DATE: 21-FEB-24. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED VAPOR BARRIER LH SIDE LOCATED STA 663 BTW LBL 31 TO LBL 45 IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. RII COMPLETED
R2 EMERENCY EXIT SIGN WILL NOT STAY UP<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY ABOVE R2 SERVICE DOOR IAW AMM 33-51-01. OPS CHECK GOOD.
AFT MEGAPHONE BATTERIES INOP<[01] R/R AFT MEGAPHONE BATTERIES AS PER REF AMM 25-64-00.NEW EXP DATE 03/24
FORWARD MEGAPHONE WILL NOT TEST. REPLACED FORWARD MEGAPHONE IAW AMM 25-64-00. OPS CHECKED GOOD.
FWD ENTRY DOOR EMERGENCY HANDLE LOOSE / [01] TIGHTENDED FWD ENTRY DOOR EMERGENCY HANDLE PER AMM 25-21-31-420-802 STEP 3B(6);[02] VERIFIED CORRECTIVE ACTION #1
AFT GALLEY POWER SUPPLY (BATTERY) M1673 INOP. AFT EMERGENCY EXIT LIGHTS NOT WORKING / [01] R&R AFT GALLEY EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06<BR>OPS CHECK GOOD.
THE 3 BELLY DRAINS AT STA 500B HAVE SURFACE CORROSION AROUND DRAIN ON THE EXTERNAL FUSELAGE. ; / [01] REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS IAW SRM 53-30-01-1A-1.; [02] C/W NDT INSPECTION PER SRM 53-30-01-1A-1. AND 737 NDT PART 6 51-00-00 PROCEDURE 23.; [03] VERIFIED CORRECTIVE ACTION STEP #1; [04] ALODINED AND PRIMED BARE METAL IAW SRM 53-30-01-1A-1.; [05] REMOVED CORROSION PER SRM 51-10-02 .WITHIN LIMITS PER SRM 53-30-01-1A-1 SEE STEPS 1 THROUGH 4 FOR ADDITIONAL WORK PREFORMED
PASSENGER CABIN FORWARD LOWERED CEILING PANEL EXIT SIGN TO FLIGHT ATTENDANT CALL INDICATOR LIGHT CLIP BROKEN. ; / [01] REMOVED AND REPLACED LIGHT ASSY. PER AMM 33-51-01<BR> OPS CHECK OK; [02] INSPECTED
RIGHT EMERGENCY EXIT DOOR LIGHT LENS IS CRACKED AT AFT FASTENER. ; / [01] REMOVED AND REPLACED R/H EMERG. LIGHT LENS PER AMM 33-51-01; [02] INSPECTED WORK PERFORMED.
BOTH OVERWING SIDEWALL LIGHTS ARE NOT PROPERLY INSTALLED. ; / [01] ADJUSTED BOTH OVERWING SIDEWALL LIGHT COVERS PER AMM 33-21-00.; [02] INSPECTED
AFT CARGO COMPARTMENT THRESHOLD ACT CORNER SCUFF PLATE IS CRACKED ; AFT CARGO COMPARTMENT THRESHOLD AFT CORNER SCFF PLATE IS CRACKEDACT IS A TYPO AND SHOLD SAY AFT / [01] AFT CARGO COMPARTMENT REMOVED AND REPLACED THRESHOLD AFT CORNER SCUFF PLATE PER AMM 53-11-02-401; [02] PRESSURIZATION LEAK CHECK WILL BE PERFORMED ON TASK TTG8Q00A0E2S LINE #613.; [03] PARTS INFO ONLY.
FWD CARGO FWD CORNER SCUFF PLATE CRACKED ; / [01] LOCATED AND DRILLED FWD CORNER SCUFF PLATE PER SRM 51-40-02; [02] INSP C/W TASK CARD CORRECTIVE ACTION #1.; [03] CORNER SCUFF PLATE TO BE INSTALLED ON TTG8Q002ELJ2 AND LEAK CHECK ON TTG8Q00A0DA3; [04] VERIFIED C/A #3
VARIOUS BULLNOSE EMERGENCY LIGHTS ARE OUT. ; / [01] REPLACED FWD L/H CIELING EMERG. BATTERY PACK AND CHARGING UNIT PER MM 33-51-06 OPS CHECKS GOOD.; [02] C/W INSPECTION
WIGGLE PLATE ON RIGHT WING AT STATION ORSS 375 + 27 PHENOLIC STRIPE CRACKED IPC 57-50-00-20 ITEM 253 ; / [01] REMOVED AND REPLACED WIGGLE PLATE ON RIGHT WING AT STATION ORSS 375 + 27 PER SRM 51-40-02; [02] C/W
SUPPLEMENTAL INFORMATION: AFT CARGO THRESHOLD WEB HAS SURFACE CORROSION AROUND FASTENER HOLES. MARKED ; / [01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] INSPECTION C/W ON CA #1.; [03] PARTS DATA UPDATE ONLY; [04] LOCATED AND DRILLED NEW THRESHOLD WEB PER SRM 51-40-05.; [05] AFT CARGO THRESHOLD WEB REMOVED FOR REPLACEMENT PER SRM 51-40-02; [06] VERIFIED LOCATED AND DRILLED; [07] INSTALLED NEW WEB PER SRM 51-40-02
R/H WING LOWER TRAILING EDGE WIGGLE PLATE PHENOLIC STRIP CRACKED IN TWO PLACES BETWEEN #7 AND #8 FLAP TRACK FAIRINGS APPROXIMATED ORSS 409 -440 (MARKED) ; / [01] REMOVED AND REPLACED R/H WING LOWER TRAILING EDGE WIGGLE PLATE BETWEEN #7 AND #8 FLAP TRACK FAIRINGS APPROXIMATED ORSS 409 -440 PER SRM 51-40-02; [02] C/W
SUPPLEMENTAL INFORMATION: ATTACH BRACKET HAS ELONGATED HOLE FOR AFT CARGO DOOR CUTOUT FWD SHIELD AT STA 767. ; / [01] REMOVED AND REPLACED ATTACH BRACKET IAW SRM 51-40-02.
SUPPLEMENTAL INFORMATION: AFT GALLEY DOOR SLIDE SAFETY PIN NOT STOWED (INSIDE THE SLIDE COVER) ; / [01] STOWED AFT GALLEY DOOR SLIDE SAFETY PIN PER AMM 25-66-01.; [02] VERIFIED SELECT REFERENCE ADDED
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+3. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .007? ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE.
AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE AT STA.727B+6 ; / [01] LINE 13 IN MEASUREMENTS IS INCORRECTLY NA. IT SHOULD READ 155.5; [02] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA 767; [03] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA 767 PER SRM 51-40-02; [04] INSPECTED.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+7. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .009?; ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.747 TO STA.767. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .006? .ALL WORK DONE IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.727E TO STA.747. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS. ALL WORK DONE IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727D+7. ; / [01] REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [03] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [04] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2)
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+14. ; / [01] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2)
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+6. ; / [01] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [02] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2)
AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE FROM STA.727D TO 727E' ; / [01] REMOVED AND REPLACED AFT CARGO RIGHT TRANSITION ANGLE FROM STA. 727 TO STA. 767 PER SRM 51-40-02; [02] INSPECTED.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+2. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS;M REMOVED .OO5? ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+9. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .005?. ALL WORK DONE IAW SRM 53-00-53-1A-1.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+11. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS. REMOVED .006?. ALL WORK DOWN IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE.
AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+14. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS. REMOVED .008? ALL WORK DONE IAW SRM 53-00-53-1A-1.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2)
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+10. ; / [01] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [02] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2)
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE AT STA.727C+2 ; / [01] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA 767 PER SRM 51-40-02; [02] INSPECTED.
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727E+15. ; / [01] INSPECTED.; [02] REMOVED AND REPLACED AFT CARGO R/H TRANSITION FROM STA. 727 TO STA. 767 PER SRM 51-40-02
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.747 TO STA.767. ; / [01] REMOVED AND REPLACE AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA. 767 PER SRM 51-40-02; [02] INSPECTED.
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+5. ; / [01] REMOVED END REPLACED TRANSITION ANGLE STA 767 TO 794.3 PER SRM 51-40-02.
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+14. ; / [01] UPDATED CORROSION QUESTIONS; [02] REMOVED DAMAGE PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-60-15-1A-1.; [03] LOCATED; DRILLED AND DEBURRED REPLACEMENT SHIELD PER SRM 51-40-05.; [04] REMOVED DAMAGE PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-60-15-1A-1. LOCATED; DRILLED AND DEBURRED REPLACEMENT SHIELD PER SRM 51-40-05. INSPECTION C/W ON CA #2 AND #3.; [05] REMOVED AND REPLACED FWD SHIELD; STA 767 TO STA 794.3 PER SRM 51-40-02.
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727B+10. ; / [01] UPDATED PARTS INFORMATION.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-10-02.; [03] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [04] INSPECTED.; [05] CORRECTED CORROSION QUESTIONS
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+9. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .005?. ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2)
SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727D+14. ; / [01] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2)
FWD CARGO SMALL TRANSITION ANGLE JUST FWD OF DOOR CUTOUT IS DEFORMED AFT END.(MARKED) ; / [01] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01; [02] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01.<BR>INSPECTION C/W.; [03] INSTALLED PER SRM 51-40-02; [04] INSTALLED PER SRM 51-40-02. INSPECTION C/W.
FWD CARGO STA 500D LOWER BULKHEAD 'L' ANGLE HAS CORROSION AROUND RBL 17 THRU RBL 22. (MARKED) ; / [01] REMOVED CORROSION FOUND TO BE OUT OF LIMITS; INSTALL OF NEW P/N 143A9485Y35 WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42 PER SRM 53-00-53 AND 5330-E-16461-NG; [02] 1. MICHAEL STANLEY (TECHNICIAN); 11-JAN-2022 15:53 UTC<BR>REMOVED CORROSION FOUND TO BE OUT OF LIMITS; INSTALL OF NEW P/N 143A9485Y35 WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42 PER SRM 53-00-53 AND 5330-E-16461-NG INSPECTED.; [03] REMOVED AND REPLACEMENT OF PART WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42.
FWD CARGO AFT R/H BULKHEAD LOWER CURVED 'L' ANGLE AT STA 500D HAS CORROSION LOWER END. (MARKED) ; / [01] FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1.; [02] 1. DANIEL ANDERSON (TECHNICIAN); 11-JAN-2022 05:56 UTC<BR>FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1. INSPECTED.; [03] LOCATED AND DRILL NEW R/H BULKHEAD ANGLE PER SRM 51-40-05.; [04] 3. DANIEL ANDERSON (TECHNICIAN); 11-JAN-2022 08:48 UTC<BR>LOCATED AND DRILL NEW R/H BULKHEAD ANGLE PER SRM 51-40-05. INSPECTED.
FWD CARGO L/H TRANSITION ANGLE HAS CORROSION AROUND NUMEROUS FASTENER HOLES BETWEEN STA 500+14 THRU STA 500C+8. OUT OF LIMITS IAW SRM 53-00-53-1A-2.; REMOVED FWD CARGO LT TRANS ANGLE. LOCATED AND BACK DRILLED HOLES IN NEW LT TRANSITION ANGLE IAW SRM 51-40-05-0G-0. ALODINED AND PRIMED LT TRANSITION ANGLE IAW SOPM 20-41-02.; INSPECTED ALODINED AND PRIMED LT TRANSITION ANGLE IAW SOPM 20-41-02. INSTALLED NUTPLATES ON LT TRANSITION ANGLE IAW SRM 51-40-10-2R-0. APPLIED PAINT TO LT TRANS ANGLE IAW SOPM 20-41-02. INSTALLED REPLACEMENT LT TRANS ANGLE FWD CARGO WITH FASTENERS IAW SRM 51-40-02. INSTALLED REPLACEMENT LT TRANS ANGLE FWD CARGO WITH FASTENERS PER SRM 51-40-02.
FWD CARGO RT TRANSITION ANGLE HAS CORROSION AROUND NUMEROUS FASTENER HOLES BETWEEN BS 500A THRU 500D. REMOVED FWD CARGO RH TRANS ANGLE FROM STA 500A TO 500D. OUT OF LIMITS PER SRM 53-00-53-1A-2. LOCATED AND BACK DRILLED HOLES IN NEW RH TRANSITION ANGLE FROM BS 500A TO 500D IAW SRM 51-40-05-0G-0. C/W INSPECTION STEPS 1-3. ALODINED AND PRIMED RT TRANSITION ANGLE FROM BS 500A TO 500D IAW SOPM 20-41-02. INSPECTED ALODINED AND PRIMED LH TRANSITION ANGLE FROM BS 396 TO 500D IAW SOPM 20-41-02. INSTALLED NUTPLATES ON RT TRANSITION ANGLE IAW 51-40-10-2R-0. APPLIED PAINT TO RH TRANS ANGLE IAW SOPM 20-41-02. INSTALLED REPLACEMENT TRANS ANGLE PER SRM 51-40-02. INSTALLED REPLACEMENT TRANS ANGLE IAW SRM 51-40-02.
FWD CARGO TRANSITION ANGLE JUST AFT OF DOOR CUTOUT R/H HAS CORROSION ON NUMEROUS FASTENER HOLES BETWEEN STA 480+15 THRU STA 500A. (MARKED) ; / [01] LOCATED AND DRILLED NEW TRANSITION ANGLE IAW SRM 53-40-01.; [02] LOCATED AND DRILLED NEW TRANSITION ANGLE IAW SRM 53-40-01. ANGLE ENAMELED AND INSTALLED ON ROUTINE CARD TTG8Q004G007.; [03] LOCATED AND DRILLED NEW TRANSITION ANGLE IAW SRM 51-40-02. ANGLE ENAMELED AND INSTALLED ON ROUTINE CARD TTG8Q004G007.
FWD SERVICE DOOR ; BEAM #4 HAS CRACK INDICATION IN RADIUS AT INBOARD HOLE. REMOVED AND REPLACED R1 DOOR GUIDE ARM AND ROLLER PER AMM 52-41-21.; [03] REMOVED AND REPLACED R1 DOOR UPPER TORQUE TUBE LINK ASSEMBLY PER AMM 52-41-41.; [04] INSPECTED WORK PERFORMED IN C/A #2 & #3; [05] REMOVED AND REPLACED R1 DOOR PER AMM 52-41-00.; [06] RIGGED R1 DOOR PER AMM 52-41-00.; [07] APPLIED CIC TO R1 DOOR PER AMM 51-00-59.; [08] INSPECTED WORK PERFORMED IN C/A #7; [09] RIGGED FWD SERVICE DOOR (R-1) PER AMM 52-41-00.; [10] C/W; [11] C/W; [12] ALL INSPECTION WORK COMPLIED WITH.
LEFT HORIZONTAL LOWER STABILIZER SKIN HAS CRACK INDICATION ON RIB 193.90 ON INBOARD FASTENER ROW APPROX 16.5' FROM LEADING EDGE BETWEEN (2 RIVETS) ; / [01] GAINED ACCESS AND REMOVED DAMAGED AREA PER SRM 55-10-01-2R-11.; [02] HFEC VERIFIED DAMAGE REMOVAL PER NDT MANUAL 51-00-00 PROCEDURE 23 PART 6 .NO DEFECTS NOTED.; [03] PERFORMED HFEC INSPECTION OF EXISTING HOLES IAW BOEING NDT 51-00-00 PT. 6 PROCEDURE 16. NO DEFECTS NOTED.; [04] FABRICATED LOCATED AND DRILLED REPAIR PARTS PER SRM 55-10-01-2R-11.; [05] INSPECTION C/W FABRICATED LOCATED AND DRILLED REPAIR (CA #4); [06] TREATED AND PRIMED REPAIR PARTS AND BARE SURFACES IN REPAIR AREA PER SRM 55-10-01-2R-11.; [07] INSPECTED THE PRIMED REPAIR PARTS AND BARE SURFACES IN REPAIR AREA; [08] OK THE INSTALL REPAIR PARTS.; [09] INFORMATION ONLY: DUE TO STEPPING UP ALL ORIGINAL FASTENER HOLES IN REPAIR AREA; NO REPAIR WASHERS ARE NEEDED.; [10] INSTALLED REPAIR PARTS PER SRM 55-10-01-2R-11.; [11] INSPECTED INSTALLATION OF REPAIR PARTS; [12] EDGE SEALED REPAIR DOUBLER PER SRM 55-10-01-2R-11.; [13] INSPECTED EDGE SEAL; [14] REINSTALLATION OF L/H WEB PANEL 331BZ DOCUMENTED ON STEP 2 IN ERROR.; [15] RE-INSTALLED L/H WEB PANEL 331BZ PER SOPM 20-50-01.; [16] INSPECTED INSTALLATION OF PANEL 331BZ; [17] ADDED MEASUREMENTS AS NECESSARY; [18] REPAIRED PER SRM 55-10-01-2R-11. (THIS REPAIR ITS A CATEGORY B REPAIR); C/W COMPLETE REPAIRED PER SRM 55-10-01-2R-11. (THIS REPAIR ITS A CATEGORY B REPAIR)
LT WING WAFFLE PLATE CRACKED I/B #3 FLAP TRACK ; / [01] REMOVED FASTENERS PER SRM 51-40-02; [02] REMOVED AND REPLACED PER SRM 51-40-02.; [03] INSPECTION C/W R@R OF WAFFLE PLATE PER SRM 51-40-02
LT WING I/B UPPER WING ROOT PANEL SUPPORT CLIP CRACKED ABOVE TANK 1 BOOST PUMP ; / [01] R/R SUPPORT CLIP PER SRM 51-40-02
LT WING I/B AFT FLAP WEDGE LOWER SURFACE HAS PLUG O/B AREA ; / [01] CLEANED AND PRIMED PER SRM 51-70-10 REPAIR #4.; CLEANED AND PRIMED PER SRM 51-70-10 REPAIR #4. OK TO INSTALL REPAIR.; [03] APPLIED REPAIR DOUBLER PER SRM 51-70-10; REPAIR #4.; APPLIED REPAIR DOUBLER PER SRM 51-70-10; REPAIR #4. INSPECTED.; [05] REPAIRED PER SRM 51-70-10;REPAIR #4; RESTORED FINISH PER M/M 51-21-99.
FORWARD CARGO DEPARTMENT FLOOR PANEL HAS DAMAGE ( REPORTED BY RAMP PERSONNEL) ; / [01] OK TO CONTINUE PER MEL25-16-01 SP1B. AUTH 21670 FWD CARGO INOP FOR USE; [02] R&R FWD CARGO FLOOR PANEL 120CF REF A.M.M 125-52-10<BR>THIS CLEARS MEL 25-16-01
RH OVERWING EXIT FLUORESCENT LIGHT LENS CRACKED / LOG PAGE 1800653 R&R'D RH OVERWING EXIT FLOURESCENT LIGHT LENSE PER AMM 33-51-11 CL#77252
IN FLIGHT DECK; PANEL BELOW L/H STAB TRIM WHEEL IS CRACKED / REMOVED AND REPLACED PER AMM 25-11-21.
AFT SERVICE DOOR EXIT LIGHT COVER MISSING. R & R AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS, IAW M/M 33-51-01.
FWD SERVICE DOOR UPPER HANDLE BROKEN. R&R ASSIST HANDLE BASE IAW AMM 52-41-31
EXIT SIGN COVER AT OVERWING EXIT ON CAPTAIN'S SIDE IS BROKEN. REPLACED LENS COVER PER AMM 33-51-03.
SUPPLEMENTAL INFORMATION: RT. WING EMERGENCY EXIT DOOR OVERHEAD LIGHT COVER IS LOOSE. / CLOSING ACTION LOG# 0161814 R&R EXIT SIGN LIGHT ASSEMBLY IAW AMM 33-51-01. OPS CHECK SATIS NO OTHER DEFECTS NOTED. CLEARING# 39594
FORWARD SERVICE DOOR EXIT SIGN LENS HAD COME OFF. / REPAIRED LENS PER EA.
L/H AFTER WING EMERGENCY ESCAPE LIGHTS INOP. R&R POWER SUPPLY M1670 IAW AMM.
R1 DOORS EMERGENCY EXIT SIGN INOP. / CLEANED CONNECTOR AT BATTERY PACK M1674 PER AMM.
R/H AFTER WING EMERGENCY ESCAPE LIGHTS INOP. R&R POWER SUPPLY M1670 IAW AMM.
R/H EMERGENCY OVERHEAD BINS LIGHTS INOP AT POSITIONS 3 TO 6. / RELAMPED LIGHT PER AMM.
L1 DOORS EMERGENCY EXIT SIGN INOP. CLEANED CONNECTOR AT BATTERY PACK M1674 PER AMM.
L/H EMERGENCY OVERHEAD BINS LIGHTS INOP AT POSITIONS 6 TO 12. RELAMPED LIGHT PER AMM.
L/H OVERWING EMERGENCY EXIT SIGNS UPPER AND LOWER POSITION INOP. R&R BATTERY PACK PER AMM.
L/H OVERWING EMERGENCY EXIT SIGNS UPPER AND LOWER POSITION INOP. R&R POWER SUPPLY PER AMM.
L/H OVERWING EMERGENCY EXIT SIGNS UPPER AND LOWER POSITION INOP. ACCOMPLISHED DISCREPANCY ON N/R 2015426/ 1000/ 0148
AFT L/H DOOR EXIT SIGN HOUSING DAMAGED AT LOWER FORWARD SIDE. R&R SIGN HOUSING PER AMM.
EMERGENCY EXIT LIGHT ASSEMBLY CRACKED AT CEILING PANEL ABOVE SEAT ROW 11. R&R LIGHT ASSEMBLY PER AMM.
FWD MAIN CABIN FLOOR PANEL 221BF CORNER CRACKED / RECEIVED NEW FLOOR PANEL 221BF; PANEL INSTALLATION WILL BE ACCOMPLISHED ON WORK CARD (JPANEL-221-CLOSE)
L-1 DOOR FWD I/B SCUFF PLATE FOUND CRACK AT FASTNER HOLE / RECEIVED NEW SCUFF PLATE FOR L-1 DOOR FWD I/B SECTION PART#7252178. SCUFF PLATE WILL BE INSTALLED JOB CARD:J725-025-00-01Y(2015423/2000/0007)
AFT CARGO COMP SCUFF PLATE FWD CORNER FOUND CRACK / RECEIVED NEW PART (P# 7530063) SCUFF PLATE FWD CORNER THIS SCUFF PLATE FWD CORNER WILL BE INSTALL ON J-753-721-00-01
L/H BODY FAIRING ATTACH FRAME CRACKED AT BS. 520, STR. 20L. / R&R FRAME PER SRM AND DWG.
FORWARD CARGO HAD GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM.
FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 21L. / R&R GUSSET PER SRM AND DWG.
MAIN CABIN FLOOR SUPPORT INTERCOSTAL UPPER ANGLE CRACKED BETWEEN BS. 500D TO BS. 520, APPROXIMATELY BL 0. / R&R ANGLE PER SRM.
FORWARD CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS. 380 TO BS. 400, BL 0. / R&R INTERCOSTAL IAW SRM.
FWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKS BETWEEN STA 380 & 400 AT RBL 10 MKD / REMOVED AND INSTALLED NEW FLOOR SUPPORT INTERCOSTAL BETWEEN STA 380 TO 400 RBL 10' AT FWD CABIN IAW B737 SRM 51-40-02-0G-0
AFT CARGO COMPARTMENT FLOOR STRUCTURE L/H ZEE CHANNEL CORRODED SPOTS BETWEEN BS. 727D TO BS. 827. / R&R ZEE CHANNEL IAW SRM AND DWG.
CRACK ON ANGLE AT AFT CARGO COMPARTMENT FWD BULKHEAD STA 727 AND BL-0 [MARKED WITH RED DOT] / REMOVED AND REPLACED AFT CARGO COMPT FWD BULKHEAD STA 727 AND BL-0 BRACKET PER B737-700 SRM 51-40-02-0G-0 AND B DWG 144A9401
AFT CARGO COMPARTMENT FLOOR STRUCTURE R/H ZEE CHANNEL CORRODED BETWEEN BS. 727E TO BS. 787. / R&R "Z" CHANNEL IAW SRM & DWG.
SUPPLEMENTAL INFORMATION: FOUND CRACK AT FRAME STRUCTURE STA 312 AT L1 DOOR UPPER SILL BETWEEN STRINGER 5L AND STRINGER 6L . / PERFORMED HFEC AT L1 DOOR UPPER SILL BETWEEN STR 5L AND STR 6L VERIFIED CRACK. TRIMMED OUT FRAME AND REMOVED DAMAGE. PERFORMED HFEC ON TRIM OUT; NO CRACKS FOUND. PERFORMED HFEC ROTO ON OPEN HOLES; NO CRACKS FOUND. FABRICATED AND HEAT TREATED REPAIR ANGLE. TREATED AND PRIMED REPAIR ANGLE AND REPAIR AREA. INSTALLED REPAIR ANGLE IN REF B737 SRM 51-40-02-0G-0; AAR RES #2015426-2 REV IR AND SWA EA #1-753-36114 REV IR
CABIN AREA FLOOR SUPPORT ANGLE 312 TO 328 LBL 45 CRACKED AT UPPER SURFACE / REMOVED & REPLACED FLOOR SUPPROT ANGLE BETWEEN STA ; 312 THRU STA 328 AND LBL 45 AS PER BOEING DRAW . # 141A5400 AND B737-7 SRM 51-40-02-0G-0 .
SUPPLEMENTAL INFORMATION: ELEVATOR HINGE PANEL 344GB HAS A CRACK ON UNDERSIDE / REPAIRED AT ELEVATOR PANEL 344GB PER B737-700 SRM 51-70-06-2R-6. MATERIAL USED P.O 1150381; P.O 1624260 AND P.O 1614988
LEFT WING FLAP SUPPORT FAIRING PANEL#542AB; SEAL SUPPORT BRACKET IS CRACK; OUTBOARD SIDE; FOWARD. DOT# 005 / REMOVED AND REPLACED CRACKED SEAL SUPPORT BRACELET AT LEFTFLAP SUPPORT FAIRING PANEL #542 AB IN REF WITH B737-700 SWA SRM 51-40-02-0G-0
L/H HORIZONTAL STABILIZER RIB ASSEMBLY 4 STAB. STA. 120.30 STIFFENER #3 CRACKED. / REPAIR #4 RIB PER SRM.
GROUND POWER DOOR FRAME SKIN CRACKED AFT OF DOOR. / REPAIRED SKIN PER SRM.
FAIRING 193B HAS NUMEROUS ELONGATED HOLES / REMOVED AND REPLACED 193B FAIRING PER AMM 53-51-21
LT PHOTOLUMINESCENT STRIP DAMAGED, 1ST SECTION. R&R STRIP REF AMM.
RT PHOTOLUMINESCENT STRIP DAMAGED, 1ST SECTION. R&R STRIP REF AMM.
L1 EMERGENCY LIGHT INOP. RELAMPED BULB PER MM.
R2 DOOR EMERGENCY SLIDE CONTAINER LOOSE. SECURED DOOR IAW SIP.
REF. MX NOTE ON LOG PG 0338186 - CRACK NOTED ON ELECTRIC POWER RECEPTACLE DOOR FRAME. / REPAIRED PER SRM 53-10-15-2R-4 FIG. 203 ZONE 1. SEE. SAM 326 FOR INDIVIDUAL SIGN OFF.
CRACK NOTED AT EXTERNAL POWER RECEPTICLE DOOR. / REPAIRED PER SRM 53-10-15-2R-4 SEE N/R D317613 FOR WORK ACCOMPLISHED. CL# 91269 DMA # 0074914
R2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOP. RELAMPED LIGHT PER AMM.
LT OVERWING EMERGENCY ESCAPE LIGHT INOP. RELAMPED LIGHT PER AMM.
ANTI-SKID INOPERATIVE LIGHT INTERMITTENTLY CAME ON DURING CLIMB OUT. R & R THE NR 3 TRANSDUCERS IAW AMM.
RIGHT OVERWING EXIT SIGN LIGHT CAP LOWER LEFT SIDE MISSING. INSTALLED THE LENS IAW AMM.
RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.
LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.
RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.
FWD CARGO - INTERCOSTAL CRACKED BETWEEN STA 500A - 500B; LBL 24. / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.
FWD CARGO L/H SIDEWALL TRANSITION ANGLE HAS CORROSION BETWEEN STA.500-500C. / REMOVED AND REPLACED DAMAGED SECTION OF TRANSITION ANGLE PER SRM 51-40-02 AND SRM 53-00-53-2R-5.
FWD CARGO R/H SIDEWALL TRANSITION ANGLE HAS CORROSION BETWEEN STA.500-500B / WP:E105601-WONG; JOHN - 12/02/2017 10:07 COMPLETE: REMOVE AND REPLACED FWD CARGO R/H SIDEWALL TRANSITION ANGLE BETWEEN STA.500-500B IAW SRM 53-00-53-2R-5 AND SEE BELOW FOR INDIVIDUAL SIGN OFFS. AND CHANGED CORROSION ITEMS.
AFT. CARGO COMPARTMENT CORROSION ON L/H TRANSITION ANGLE AROUND FLOOR PANEL FASTENER HOLES IN BETWEEN STA. 767+3 AND STA. 807+10.5 / REMOVED AND REPLACED L/H TRANSITION ANGLE SECTION STA. 755-817 PER SRM 53-00-53-2R-5. SEE WIP'S AND TASK'S FOR INDIVIDUAL SIGN OFFS.
AFT. CARGO COMPARTMENT CORROSION ON L/H TRANSITION ANGLE AROUND FLOOR PANEL FASTENER HOLE AT STA. 747+9. / L/H TRANSITION ANGLE REMOVED AND REPLACED FROM STA. 747+8 TO 807+11; ALL WORK ACCOMPLISHED ON G509781
AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRAP CORRODED AT BS 887, RBL 16. R&R SPLICE TEE ASSEMBLY PER SRM.
AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRAP CORRODED AT BS 767+6, RBL 19. R&R SPLICE TEE ASSEMBLY PER SRM.
WHILE PERFORMING DAMAGE CUTOUT INSPECTION; FOUND TOOLING DAMAGE ON COCKPIT FLOOR MOUNT CHANNEL ALONG L/H EDGE OF DAMAGE CUTOUT. / REPAIRED COCKPIT FLOOR MOUNT CHANNEL IAW EA 1-753-31995 PART 2.
FLOOR SUPPORT CRACKED AT BS 540, LBL 1. R & R THE FLOOR SUPPORT IAW SR.
RUDDER BALANCE WEIGHT CORRODED L/H O/B SIDE. / REMOVED AND REPLACED RUDDER BALANCE WEIGT PER SRM 51-60-07-0G-0 PARAGRAPH (11) STEP (C) TO D).CORROSION AND ATA QUESTIONS ANSWERED.
L2 DOOR EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW. R & R THE SIGN IAW MM.
L2 DOOR EMERGENCY SLIDE GIRT BAR PLASTIC STOP MISSING. INSTALLED THE PIN IAW SIP.
RT LOWER EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED COVER PER MM.
DIVERSION, DECLARED EMERGENCY, LOSS OF CABIN PRESSURE AT 38,000 FT INITIATED EMERGENCY DESCENT. LANDED, R & R NR 1 LT PACK VALVE IAW AMM.
CABIN ALTITUDE WARNING HORN AND LIGHT INDICATION. EMERGENCY DECLARED AND DIVERTED. R & R THE NR 1 CABIN PRESSURE CONTROLLER IAW MM.
CABIN ALTITUDE WARNING HORN AND LIGHT INDICATION. EMERGENCY DECLARED AND DIVERTED. R & R THE OUTFLOW VALVE IAW MM.
R2 DOOR GALLEY EXIT SIGN LENS COVER LOOSE. R & R COVER IAW AMM.
FORWARD SERVICE DOOR EMER EXIT SIGN BROKEN LENS. R & R BASE ASSEMBLY IAW AMM.
OVERHEAD EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM.
RIGHT PAX CABIN PHOTO LUMINESCENT STRIP WORN. R & R STRIP IAW MT.
LEFT PAX CABIN PHOTO LUMINESCENT STRIP WORN. R & R STRIP IAW MT.
RIGHT HORIZONTAL STABILIZER RIB CRACKED, STAB. STATION 166.30 AT FWD SPAR OTBD FASTENER. REPAIRED RIB IAW SRM.
AFT GALLEY FLOOR, STRUCTURE WEB STRAP CORRODED, BETWEEN BS 1016 - 1030, LBL 3. R & R WEB STRAP IAW SRM.
FORWARD ENTRY DOOR, Z ANGLE CRACKED AT FASTENER HOLE AT BS 303.9. R & R Z ANGLE IAW SRM.
AFT GALLEY FLOOR, STRUCTURE WEB STRAP CORRODED, BETWEEN BS 1016 - 1030, RBL 3. R & R WEB STRAP IAW SRM.
FORWARD GALLEY DOOR, Z ANGLE ON OTBD SIDE CRACKED AT BS 294.5, RBL 53. R & R Z ANGLE IAW SRM.
FORWARD GALLEY THRESHOLD SUPPORT ANGLE, CORRODED AT BS 299, RBL 54. R & R ANGLE IAW SRM.
AFT CARGO FLOOR SUPPORT, CORRODED AT BS 767. R & R SUPPORT IAW SRM.
FORWARD GALLEY DOOR, Z ANGLE ON INBD SIDE CRACKED, BETWEEN BS 294.5 - 328, RBL 54. R & R ANGLE IAW SRM.
AFT CARGO THRESHOLD BEAD WEB CORRODED. R & R WEB IAW SRM.
FORWARD CARGO SUPPORT, Z ANGLE CORRODED BETWEEN BS 485 - 500D. R & R Z ANGLE IAW SRM.
WHEEL WELL DECK CRACKED AT BS 663, BETWEEN LBL 33.5 - LBL 34.75, 4" BELOW THE WW DECK. REPAIRED DECK IAW SRM.
WHEEL WELL DECK CRACKED AT BS 663, BETWEEN RBL 32.5 TO LBL 33, 4" FROM TOP OF FUEL TANK. REPAIRED DECK IAW SRM.
DIVERSION, FLIGHT ATTENDANT REPORTED SOUND & ODOR MID CABIN. TURNED RECIRCULATING FAN OFF & SMELL DISSIPATED. R & R RECIRCULATING FAN IAW MM.
LONGITUDINAL FLOORBEAM AFT OTBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA.
LONGITUDINAL FLOORBEAM FWD OTBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA.
LONGITUDINAL FLOORBEAM FWD INBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA.
LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA.
FORWARD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.
R1 DOOR EMER EVAC SLIDE GIRT HOLDER BAR DIRTY. CLEANED HOLDER IAW AMM.
FORWARD ENTRY EMER BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG.
SERVICE ENTRY EMER BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG.
OVERWING EXIT SIGN BROKEN. R & R SIGN IAW AMM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK IAW SRM.
R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR IAW MM.
L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER COLLAR CRACKED. R 7 R GIRT BAR STOP IAW MM.
CABIN FLOOR INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24. REPAIRED INTERCOSTAL IAW SRM.
RT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.
LEFT EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 11. REMOVED AND REPLACED COVER PER MM.
R2 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER MM AND MT.
L1 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER MM AND MT.
LEFT EEPLS LENS CRACKED AT ROW 12. REMOVED AND REPLACED LENS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
LEFT EEPLS LENS CRACKED AT ROW 23. REMOVED AND REPLACED LENS PER MM.
L1 DOOR EMERGENCY SLIDE FELL OUT OF CONTAINER (STILL OPERABLE). REINSTALLED SLIDE PER MM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER HOOK LOOSE. SECURED HOOK ASSY PER SRM.
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER HOOK LOOSE. SECURED HOOK ASSY PER SRM.
L2 DOOR EMERGENCY EVAC SLIDE COVER LENS CRACKED. REMOVED AND REPLACED LENS PER M/M & MT.
EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.
LT CABIN BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER M/M.
RT CABIN BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER M/M.
EGRESS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.
L1 DOOR EEPLS COVER MISSING. REMOVED AND REPLACED COVER PER MM.
EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 20. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED MV1 CHECK, FOUND LT EELS LENS MISSING AT ROW 8. INSTALLED LENS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.
FWD EEPLS LOOSE. SECURED EEPLS PER MM.
EMERGENCY EXIT LIGHT LENS COVER LOOSE. REMOVED AND REPLACED COVER PER MM.
FWD CABIN EEPLS LOOSE. SECURED EEPLS PER MM.
FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
AT START OF DESCENT INTO TUL - FLT ATTENDANT CALLED AND COMPLAINED OF ODOR SIMILAR TO BURNING RUBBER MID CABIN, NO SMOKE. TURNED OFF RECIRC FAN AND ODOR WENT AWAY. REMOVED AND REPLACED RECIRC FAN PER MM.
L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF IT'S CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE PER MT.
DURING SCHEDULED MV1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.