N463WN
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
ON APPROACH TE FLAP STUCK ON '1'. USED ALTERNATE FLAPS TO LOWER FLAPS TO '15'. NO BRAKE COOLING ISSUES ON LANDING. TAXING TO GATE. REMOVED LT T/E FLAP POSITION TRANSMITTER IAW AMM 27-58-01.
RH OVER WING EXIT INDICATOR LENS COVER MISSING. REPLACED LENS COVER REF AMM 33-51-01.
CRACKED CROSSBEAM, BS 540 BTWN BL 0 - RBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 36, REV A.
CRACKED CROSSBEAM, BS 540, BTWN BL 0 - LBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 36, REV A.
CRACK TRAILING EDGE BRACKET, ORSS 270, LT WING. REPLACED THE BRACKET IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 115A2030, SHEET 6, REV-.
CRACK TRAILING EDGE BRACKET, ORSS 280 INTERNAL CAVITY AT RT WING. REPLACED THE BRACKET IAW SRM 51-10-02, PARA 9, SRM-51-40-02-0G-0, & DWG 115A2930, SHEET 6, REV-.
ELONGATED HOLE ON THE RT WING ACCESS PANEL 651GB SUPPORT BRACKET. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, SRM 51-40-02, & DWG 115A2714, SHEET 4, REV-.
ELONGATED HOLE ON LT WING ACCESS PANEL 561AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACKED TRAILING EDGE SUPPORT ANGLE, LT WING ORSS 269. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02-0G-0, PARAGRAPH 9.
CRACKED VERTICAL STIFFENER, BS 540, LBL 24.75. REPLACED THE VERTICAL STIFFENER IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND DRAWING 111A2001, REV -, SHEETS 53;54, & 55.
CORRODED LOWER LUG FITTING, AFT FACE OF LT HORIZONTAL STAB. REPAIRED LOWER LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STAB IAW 26-155-00498-WIP1, 26-155-00498-WIP2, 26-155-00498-WIP3, 26-155-00498-WIP4, 26-155-00498-WIP5, & EA 26-155-00498.
CORRODED LOWER LUG FITTING, AFT FACE POSITION OF THE RT HORIZONTAL STAB. REPAIRED LOWER LUG FITTING ON THE RT HORIZONTAL STAB IAW 26-155-00499-WIP1, 26-155-00499-WIP2, 26-155-00499-WIP3, 26-155-00499-WIP4, AND EA 26-155-00499.
CRACKED CROSSBEAM, BS 540, RBL 24.75 - RBL 45.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, STEP 9, & DWG 143A0060, SHEET 36, REV A.
ELONGATED HOLE ON THE RT WING T/E ACCESS PANEL 661AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
ELONGATED HOLE ON THE RT WING ACCESS PANEL 661CB TRAILING EDGE. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
BROKEN EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 242YAW AT PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 242YAW IAW AMM 33-51-01-960-801, STEP 2C, (1), (A), 4) & STEP 2C, (4).
CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 35 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.150 INCH APPROXIMATELY. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LBL 30 TO LBL 62 STA 663 TO STA 675 AT PASSENGER CABIN AND FASTENERS IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2.
CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED BY WELDING AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
CRACK ON FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
BROKEN EMERGENCY LENS ON OVERHEAD STOWAGE BIN RT SIDE IN THE PASSENGER CABIN. REPLACED THE LENS IAW AMM 33-51-03-960-801, STEP 2.D, (3), (A), & (B).
DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ON SEVERAL POSITION IN PASSENGER CABIN, REPLACED PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802.
BROKEN EMERGENCY LENS OVERHEAD STOWAGE BIN LT SIDE PASSENGER CABIN. REPLACED THE LENS IAW AMM 33-51-03-960-801, STEP 2.D,(3), (A), (C).
PERFORMED ADJUSTMENT ON SEAT ROW 14B FOR RECLINING AT EMERGENCY EXIT AREA AT PASSENGER CABIN. VERIFIED ADJUSTMENT OF PASSENGER SEAT 14B RECLINE IS NOT NECCESSARY. WAS LEFT LOCKED IAW REV.6, CMM 25-21-45 TABLE 1 AND DRAWING DG306-142007C, STEP 6, PAGE 8006.
RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL HAS A THREE VERTICAL CRACKS ALONG LEADING EDGE. R & R THE RT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL HAS TWO VERTICAL CRACKS ALONG LEADING EDGE. R & R THE CRACKED LT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
FWD SERVICE DOOR SLIDE MECHANISM HAS CHORD AND COTTER PIN EXPOSED. SECURED FWD SVC DOOR BONDING JUMPER PER AMM 25-66-01.
EXIT ROW SEAT 11B SHOULD NOT RECLINE BUT DOES RECLINE. DISABLED SEAT 11B RECLINE REF AMM 25-22-00.
RH OVERWING EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED RH OVERWING EXTERIOR EMERGENCY LIGHT OPS OK IAW AMM 33-51-04
FWD SERVICE DOOR ESCAPE SLIDE NEEDS RE-ADJUSTED <[01]. RE-ADJUSTED ESCAPE SLIDE AND COVER PER MM25-66-01 AND MT 725-61-06.
F.O. SIDE OVER WING EXIT SIGN COVER LOOSE.<[01] SECURED F.O. SIDE OVERWING EXIT SIGN COVER PER AMM 33-51-01.
EXIT SIGN FO SIDE EMERGENCY EXIT COVER CAME OFF<[01] REINSTALLED EMERGENCY EXIT LIGHT COVER ON FOS SIDE IAW AMM 33-51-01
1 DOOR SLIDE MATERIAL EXCESSIVE IN LENGTH<[01] ADJUSTED GIRT BAR MATERIAL WITHOUT REMOVING SLIDE; COMPLIED WITH ESCAPE SLIDE PACK CHECK IAW MM 25-66-01. NO DEFECTS NOTED
RIGHT AFT OVER WING EXIT EMERGENCY EXIT INDICATOR LIGHT INOP (L1358)<[01] RE-LAMPED EXIT INDICATOR LIGHT L1358 WITH NO HELP FOUND CONNECTOR D12392 NOT FULLY SEATED RE-CONNECTED PER AMM 33-51-01 OPS CHECK GOOD
AFT LEFT EXIT SIGN OVER DOOR (COVER) LOOSE<[01] REMOVED AND REPLACED EXIT SIGN LIGHT ASSY IAW AMM 33-51-01
R2 DOOR SLIDE TOO LOW<[01] RE-SECURED ESCAPE SLIDE IN COVER (R2) REF AMM 25-66-01 AND MT 725-61-06
AFT EXIT EMERGENCY SIGN COMING OFF<[01] REMOVED AND REPLACED EXIT SIGN LIGHT ASSY IAW AMM 33-51-01
OUTSIDE AFT SERVICE DOOR EMEGENCY LIGHT INOP<[01] RELAMPED EXTERIOR AFT SERVICE DOOR EMERGENCY LIGHT; L733; PERFORMED A GOOD FUNCTIONAL TEST PER AMM 33-51-04-960-801;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
RIGHT HORIZ STAB TIP 345A HAS AREA WITH DELAMINATION<[01] UPDATED PARTS FIELD.;[02] RECEIVED NEW RT HORIZONTAL STAB TIP. INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q00RDE0M.;[03] UPDATED PARTS REQUIREMENT;[04] VERIFIED. TASK CARD COMPLETE.
CORROSION ON AFT CARGO BAY FLOOR TRACK AT BS 927+17 WL 156.<[01] REMOVED AND REPLACED AFT CARGO FLOOR TRACK RAIL<BR>BS 887 TO BS 947 RBL 3 WL 156 <BR>IAW BOEING SRM 51-40-02<BR>AND DWG 147A7500
CORROSION ON AFT CARGO BAY FLOOR TRACK AT RBL 8; STA 887+2 AND 887+15; WL 156.<[01] REMOVED AND REPLACED ON AFT CARGO BAY FLOOR TRACK AT RBL 8 STA 887 TO STA 907; WL 156 IAW SRM 53-00-53-2R-4 REPAIR 4 AND DWG 147A7500.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 807+10; LBL 21; WL 156.<[01] REOMVED AND REPLACED ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 847 LBL 21 IAW SRM 51-40-02 AND DWG 146A7500
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 807+10; LBL 21; WL 156.<[01] TASK CARD WILL BE COMPLETED ON FAULT TTG8Q00S4HL0;[02] VERIFIED TASK CARD WILL BE COMPLETED ON FAULT TTG8Q00S4HL0;[03] VERIFIED TASK CARD WILL BE COMPLETED ON FAULT TTG8Q00S4HL0
CORROSION ON AFT CARGO BAY DOOR FWD SHIELD FROM STA 767 TO 787; RBL 22; WL 156.<[01] REMOVED AND REPLACED ACB AFT SHIELD IAW SRM 51-40-02 AND DWG 146A0081.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM STA 727B+6 TO STA 767; RBL 21; WL 156.<[01] REMOVED AND REPLACED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 767 RBL 21 PER SRM 51-40-02 AND DWG 146A7500;[02] VERIFIED
CORROSION ON AFT CARGO BAY DOOR CUT-OUT SHIELD AT STA 847+; RBL22; WL 150. CORRECTION: STA847+5<[01] UPDATED P/N IN MEASURES TABLE.;[02] REMOVED AND REPLACED ACB AFT SHIELD FROM BS 847 TO BS867 IAW SRM 51-40-02 AND DWG 146A0081.
FWD ENTRY DOOR IS SAGGING AND CONTACTING UPPER AFT AND LOWER FWD LOWER REVEALS<[01] UPON FURTHER INVESTIGATION FED NEEDED ADJUSTMENT. PERFORMED ADJUSTMENT AND OPC ON FED ON FAULT TTG8Q00S5BF2;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
AFT CARGO BAY SUB-THRESHOLD WEB IS CORRODED FROM STA 787+4 TO STA 827+11; RBL 23-28; WL 156.<[01] REMOVED AND REPLACED SUB-THRESHOLD WEB FROM BS 787 TO BS 847 IAW SRM 51-40-02 AND DWG 146A8340.;[02] VERIFIED
FWD CARGO TRACK TIE DOWN HAS CORROSION AT BS 420+16; LBL 19; WL 156. ALL PROCESS WILL BE ACCOMPLISHED AND COMPLETED WITH TASK CARD#TTG8Q00S418F.
FWD CARGO FLOOR TO SIDEWALL SUPPORT IS CORRDED AT BS 500A - 500B; LBL 24; WL 156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT <BR>BS 396 TO BS 500D LBL 24 WL 156 <BR>IAW SRM 51-40-02-0G-0 AND DWG 143A7500.
FWD CARGO CENTER THRESHOLD IS CORRDED AT BS 440+10 - 480+5; RBL 23 - 30; WL 155<[01] REMOVED AND REPLACED FWD CARGO CENTER THRESHOLD BETWEEN BS 440 - 492.4 RBL24 WL 156.5 I.A. W SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG 143A8330.;[02] VERIFIED CORRECTIVE ACTION 1
FWD CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 500D; LBL 19 - RBL 24; WL 156<[01] REMOVED CORROSION ON FWD CARGO BULKHEAD FOUND TO BE WITHIN LIMITS IAW SRM 53-30-08-1A-1 PARA 4 (2) FIG.103 DET.C.<BR>TOOL USED<BR>ID:ATS2473<BR>DUE:09/2024<BR>S/N UNKNOW;[02] VERIFIED
FWD CARGO AFT SHIELD IS CORRODED AT BS 480+14 - 500A; RBL 24; WL 156<[01] REMOVED AND REPLACED FWD. SHIELD ASSY P/N 143A8126-31 LOT: 1553496-2 IAW SRM 51-10-02; SRM 51-40-02; AND DWG 143A0080.;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
FWD CARGO TRACK TIE DOWN HAS CORROSION AT BS 480+17; LBL 19; WL 156<[01] UPDATED PART REQUIREMENTS.;[02] REMOVED AND REPLACED FCB FLOOR TRACK FROM BS 396 TO BS 500D; LBL 19; WL 156 IAW SRM 51-40-02-0G-0 AND DWG# 143A7500;[03] VERIFIED
MAIN E-BAY O2 BOTTLE FWD SUPPORT BRACKET; LOWER ATTACH ANGLE IS CRACKED AT O/B FASTENER BS 360+2; RBL 14; WL 164<[01] REMOVED AND REPLACED MAIN E-BAY O2 BOTTLE FWD SUPPORT BRACKET BS 360 ; RBL 14; WL 164 IAW SOPM 20-50-01;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
FWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 27R; BS 520+19<[01] PERFORMED STRINGER REPAIR PER REF SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED
FWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 25R; BS 520+19<[01] DAMAGE WAS REPAIRED PER EA 24-153-00727. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06;[02] VERIFIED TASK COMPLETED
FWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 26L; BS 520+19<[01] REPARED STRINGER 26L; APPLIED CIC ON REPAIR IAW SRM 53-00-03-2R-1
FWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 23R; BS 520+19<[01] 02 - INSPECTED PER [REFERENCE];[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 24-153-00709.;[03] VERIFIED CORRECTIVE ACTION #2
FWD CARGO HAS A CRACKED STR AT AFT FASTENER; STR 23L; BS 520+19<[01] REPAIRED FCB STR 23L BS 500D-540 IAW SRM 53-00-03-2R-1 REPAIR 1 AND EA # 24-153-00708;[02] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 24-153-00708
TAIL CONE LOWER LOBE RIGHT SIDE WAS FOUND A DELAMINATION SPOT; 9 IN BEHIND STA 1156 L=3 IN W= 2.750 IN. REPAIRED IAW SRM 51-70-05-2R-2.
FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0128.;[02] VERIFIED CORRECTIVE ACTION #1
FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WITH AREAS OF PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0008;[02] VERIFIED FLOOR PANEL 241AF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0008
FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0126.;[02] VERIFIED CORRECTIVE ACTION #1
RH HORIZONTAL STAB RIB #4; STAB STA 120.30; CRACKED 2ND AND 4TH VERTICAL STIFFENERS.<[01] NDT HFEC INSPECTED SURFACE; 2ND AND 4TH VERTICAL STIFFENERS PER 737 NDTM PART 6; 51-00-00; PROC 23; CRACKS .500' LONG NOTED AT THE LOWER ENDS. EQUIP ID IS000680 DUE 05/24;[02] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 120.30 RIB 2ND AND 4TH VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-5;[03] 02 - INSPECTED PER [SRM 55-10-09-2R-5-A01102 (REPAIR 5 - HORIZONTAL STABILIZER MACHINED INSPAR RIB LOWER CHORD AND VERTICAL STIFFENER CRACK REPAIR - CAT A REPAIR - PERMANENT)]
G1 GALLEY HAS CORROSION ON THE SHELF UNDER THE COFFEE MAKEER RAILS<[01] UPDATED PARTS REMOVAL;[02] RECEIVED NEW G1 GALLEY; P/N: 980001-1; S/N: 366.<BR>ORIGINAL G1 GALLEY REMOVED ON TASK CARD TTG8Q001S17C.<BR>INSTALLATION OF NEW G1 GALLEY TO BE ACCOMPLISHED ON TASK CARD TTG8Q001S16V.;[03] CORRECTION TO ACTION 2:<BR>RECEIVED SERVICEABLE G1 GALLEY; P/N: 980001-1; S/N: 366.<BR>ORIGINAL G1 GALLEY REMOVED ON TASK CARD TTG8Q001S17C.<BR>INSTALLATION OF SERVICEABLE G1 GALLEY TO BE ACCOMPLISHED ON TASK CARD TTG8Q001S16V.;[04] VERIFIED CORRECTIVE ACTION. JOB COMPLETE.
G4 GALLEY HAS CORROSION ON THE SHELF UNDER THE COFFEE MAKEER RAILS<[01] UPDATED PARTS REMOVAL;[02] ADDED PART;[03] REMOVED AND REPLACED GALLEY 4 IAW AMM 25-31-45-000-802-004 AND AMM 25-31-45-400-802-004.;[04] REMOVAL AND INSTALLATION OF G-4 GALLEY TO BE ACCOMPLISH ON <BR>TC# 725-031-41-04Y<BR>TTG8Q001VERF;[05] VERIFIED CORRECTIVE ACTION #4
PANEL 192AL OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 192AL OUTER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
EMERGENCY LIGHTING BATTERY PACKS M1668; M1669; M1670; M1672; M1673; M1674 AND M1675 FAIL EMERGENCY LIGHTING CAPACITY CHECK.<[01] REMOVED AND REPLACED M1668; M1669; M1670; M1672; M1673; M1674 AND M1675 EMERGENCY LIGHTING BATTERY PACKS IAW AMM 33-51-06-960-805 STEP 4.E.(1)-(5);[02] VERIFIED REMOVAL AND REPLACEMENT OF M1668; M1669; M1670; M1672; M1673; M1674 AND M1675 EMERGENCY LIGHTING BATTERY PACKS IAW AMM 33-51-06-960-805 STEP 4.E.(1)-(5);[03] VERIFIED CORRECTIVE ACTION STEP 1.;[04] PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHTS PER STEP 1. TASK COMPLETED.;[05] CERTIFIED TASK CARD COMPLETED;[06] VERIFIED COMPLETION CORRECTIVE ACTION 4-5 AND MEASUREMENT TABLE.
RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.
LT. HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.
EMERGENCY AREA LIGHT AT SEAT 1 (ABC) INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-03-960-801-NG (AREA LIGHT - LAMP REPLACEMENT - PERMANENT)]
AFT ENTRY DOOR SLIDE FLAP CONTACTING FRAME WHEN CLOSING.<[01] ADJUSTED AFT ENTRY DOOR SLIDE IN CASE. OPS NORMAL. REF AMM25-66-01.
FRONT SERVICE DOOR EXIT SIGN LOOSE. REPLACED EMERGENCY LIGHT ASSY IAW AMM 33-51-01.
FWD GALLEY EXIT LIGHT COVER MISSING. INSTALLED MISSING FWD EXIT LIGHT COVER IAW SIP
ELECTRIC TRIM INOPERATIVE AFTER TAKEOFF. HORIONTAL STABILIER TRIM. / [01] -SPEED TRIM FAIL LIGHT ILLUMINATES ON RECALL.<BR>-NO C/B?S POPPED.<BR>-FAULT MESSAGE 22-11182. (DFCS BITE);[02] R&R STAB TRIM CUTOUT RELAY (R384) OPS CHECK AND CLOSE UP REQUIRED.;[03] PERFORMED FIM 22-13 TASK 813. R&R STAB TRIM CUTOUT RELAY (R384) PER FIM. OPS CHECKS AND CLOSE UP REQUIRED.;[04] REMOVED AND REPLACED STABILIZER TRIM ACTUATOR IAW AMM 27-41-71 <BR>AND PERFORMED OPS CHECKS IAW AMM 27-41-00 AND CLOSED UP CENTER PANEL
ELECTRIC TRIM INOPERATIVE AFTER TAKEOFF. HORIZONTAL STABILIER TRIM. / [01] -SPEED TRIM FAIL LIGHT ILLUMINATES ON RECALL.<BR>-NO C/B?S POPPED.<BR>-FAULT MESSAGE 22-11182. (DFCS BITE);[02] R&R STAB TRIM CUTOUT RELAY (R384) OPS CHECK AND CLOSE UP REQUIRED.;[03] PERFORMED FIM 22-13 TASK 813. R&R STAB TRIM CUTOUT RELAY (R384) PER FIM. OPS CHECKS AND CLOSE UP REQUIRED.;[04] REMOVED AND REPLACED STABILIZER TRIM ACTUATOR IAW AMM 27-41-71 <BR>AND PERFORMED OPS CHECKS IAW AMM 27-41-00 AND CLOSED UP CENTER PANEL
EMERGENCY EXIT ROW; FO SIDE; DOOR PANEL LOOSE / [01] RESECURED R/H EMERGENCY EXIT DOOR PANEL PER SIP
EMERGENCY EXIT LIGHT COVER; FO SIDE OVER WING. DETACHED. / [01] COMPLIED WITH EA-GENERAL M-21-133-00720.
CRACK ON FIXED LEADING EDGE SKIN AT LEVEL KRUEGER FLAP ACTUATOR 1 2022-148404 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[02] REPAIRED INB FIXED LE SKIN BTW KRAS 166.32 TO KRAS 190.52 (KRUEGER FLAP ACTUATOR 1) IAW E/A 22-157-01102 BARCODE (TTG8Q00BW4T); E/A 22-157-01102-WIP 1 BARCODE (TTG8Q00BVJAQ); E/A 22-157-01102-WIP 2 BARCODE (TTG8Q00BW1TN) MATERIAL USED: ALUMINUM SHEET 2024T3 0.063? P/O 2021164780; 2024T3 0.071? P/O 202111049; 2024T3 0.080? P/O 2022126808. SEE INDIVIDUAL SIGN OFF BELOW;[05] REPAIRED ON INB FIXED LE SKIN BTW KRAS 166.32 TO KRAS 190.52 (KRUEGER FLAP ACTUATOR 1) IAW EA 22-157-01102 BARCODE (TTG8Q00BWE4T); EA 22-157-01102-WIP 1 BARCODE (TTG8Q00BVJAQ); EA 22-157-01102-WIP 2 BARCODE (TTG8Q00BW1TN) MATERIAL USED: ALUMINUM SHEET P/N: 2024T3 0.063? P/O 2021164780; P/N: 2024T3 0.071? P/O 202111049; P/N: 2024T3 0.080? P/O 2022126808. SEE INDIVIDUAL SIGN OFF BELOW
CRACK ON FIXED LEADING EDGE SKIN AT LEVEL KRUEGER FLAP ACTUATOR 4 2022-148405 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[02] REPAIRED ON INB FIXED LE SKIN BTW KRAS 180.52 & KRAS 190.52 (KRUEGER FLAP ACTUATOR 4) RH WING; IAW EA 22-157-01101 BARCODE (TTG8Q00BWCRN); EA 22-157-01101-WIP1 BARCODE (TTG8Q00BVZAN); EA 22-157-01101-WIP2 BARCODE (TTG8Q00BVZ67). MATERIAL USED: ALUMINUM SHEET P/N:2024T3 0.063? P/O: 164780; P/N: 2024T3 0.071? P/O: 111049; SEE INDIVIDUAL SIGNOFF BELOW;[03] REPAIRED ON INB FIXED LE SKIN BTW KRAS 180.52 & KRAS 190.52 (KRUEGER FLAP ACTUATOR 4) RH WING; IAW EA 22-157-01101 BARCODE (TTG8Q00BWCRN); EA 22-157-01101-WIP1 BARCODE (TTG8Q00BVZAN); EA 22-157-01101-WIP2 BARCODE (TTG8Q00BVZ67). MATERIAL USED: ALUMINUM SHEET P/N:2024T3 0.063? P/O: 164780; P/N: 2024T3 0.071? P/O: 111049; SEE INDIVIDUAL SIGNOFF BELOW
CRACK ON WEB INTERCOSTAL LOCATED BTW BS 380 TO BS 400 BL 0 FLOOR STRUCTURE OF PASSENGER CABIN 2022-148402 / [01] REPLACED ANGLE LOC BTW BS 380 TO BS 400 BL0 FLOOR STRUCTURE OF PASSENGER CABIN. IAW B737-700 SRM 51-40-02 AND DWG 143A5400; SHEET 38 AND REV A.;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE LOC BTW BS 380 TO BS 400 BL0 FLOOR STRUCTURE OF PASSENGER CABIN. IAW B737-700 SRM 51-40-02 AND DWG 143A5400; SHEET 38 AND REV A. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ON WEB FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2022-148363 / [01] TOOL USED CALIPER P/N 500-197-30 S/N A18135101 DUE DATE 06-AUG-22 <BR>GAGE RADIUS P/N 06457055 S/N AE-28115 DUE DATE 05-JUL-22;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[03] REPLACED WEB LOC. FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02 ITEM; 51-40-02 AND DWG 147A01103 REV: A SHEET 3;[04] CORRECTED STEP 3.<BR>REPLACED WEB LOC. FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 147A01103 REV: A SHEET 3. SEE INDIVIDUAL SIGN OFFS BELOW;[05] CORRECTED STEP 4.<BR>REPLACED WEB LOC. FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 147A0103 REV: A SHEET 3. SEE INDIVIDUAL SIGN OFFS BELOW;[06] CORRECTED STEP 5.<BR>REPLACED WEB LOC. FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 174A0103 REV: A SHEET 3. SEE INDIVIDUAL SIGN OFFS BELOW;[07] REPLACED WEB LOC. FWD POSITION ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 174A0103 REV: A SHEET 3. SEE INDIVIDUAL SIGN OFFS BELOW
WEAR ON SEAT TRACK BS 520 LBL 45.5 AT PASSENGER CABIN 2022-148311 / [01] REPAIRED SEAT TRACK LOC BS 500C TO BS 520 LBL 45.5 AT PASSENGER CABIN I.A.W B737-700 SRM 53-00-52-2R-4 AND REPAIR IS CATEGORY A AND DOES NOT REQUIRED INSPECTIONS SE INDIVIDUAL SING OFF BELOWS.;[02] REPAIRED SEAT TRACK LOC BS 500C TO BS 520 LBL 45.5 AT PASSENGER CABIN I.A.W B737-700 SRM 53-00-52-2R-4 AND REPAIR IS CATEGORY A AND DOES NOT REQUIRED INSPECTIONS SE INDIVIDUAL SING OFF BELOW<BR>RII ACCOMPLISHED
BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) 2022-148319 / [01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 PART USED P/N:207377DME1009;[02] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801. STEP 2.C(1) (A) AND (4). PART USED PMA ITEM (268) P/N:207377DME1009;[03] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801. STEP 2.C(1) (A) AND (4).
CORROSION ON TIE DOWN LOC BS 495 BTW STR 18L TO STR 25L FWD CARGO COMPARTMENT 2022-148308 / [01] REPLACED TIE DOWN LOC BS 495 BTW STR 18L TO STR 25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;[02] REPLACED TIE DOWN LOC BS 495 BTW STR 18L TO STR 25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02.
BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) 2022-148243 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801;[02] CORRECTED STEP 1 : REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 STEP 2. C (1) (4);[03] CORRECTED STEP 2:REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 STEP 2. C (1)A AND (4);[04] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 STEP 2. C (1)A AND (4)
CRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2022-148237 / [01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 01-OCT-22.;[02] TOOL USED MULTIMETER P/N: FLUKE 87 ; S/N: 43050123 ; DUE DATE: 03-FEB-23;[03] REPAIRED ACCESS PANEL 561CB LT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9 SEE INDIVIDUAL SIGNOFFS BELOW TOOL USED SCALE; P/N: <BR>CL5000; S/N: AE-409558; DUE DATE: 19/MAY/22; HOT BONDER; P/N: HCS9200B; S/N: 15102320; DUE DATE: 16/JAN/23; HOT BONDER P/N: HCS9200B; S/N:18175478; DUE <BR>DATE: 05/AUG/22.;[04] STEP 3 CORRECTED. REPAIRED ACCESS PANEL 561CB LT WING IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9 SEE INDIVIDUAL SIGNOFFS BELOW TOOL USED SCALE; P/N: <BR>CL5000; S/N: AE-409558; DUE DATE: 19/MAY/22; HOT BONDER; P/N: HCS9200B; S/N: 15102320; DUE DATE: 16/JAN/23; HOT BONDER P/N: HCS9200B; S/N:18175478; DUE <BR>DATE: 05/AUG/22.;[05] JOB TASK COMPLETED.
CRACK ANGLE TRAILING EDGE LOCATED WS228.25 AND WS253 AFT POSITION RT WING 2022-148189 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 AND WS253 AFT POSITION RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 P/N USED 115A2982-10 PO 2022-102850.
ELONGATED HOLE PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 RT WING 2022-148246 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV-.;[02] REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV-.
CORROSION WEB LOCATED BS1016 AND LBL14; WL208.1 AT LEVEL FLOOR STRUCTURE AT AFT GALLEY AREA 2022-148127 / [01] REPLACED WEB LOCATED BS1016 AND LBL14; WL208.1 AT LEVEL FLOOR STRUCTURE AT AFT GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9 AND DWG:147A5600 SHEET:32 REV:B;[02] REPLACED WEB LOCATED BS1016 AND LBL14; WL208.1 AT LEVEL FLOOR STRUCTURE AT AFT GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9 AND DWG:147A5600 SHEET:32 REV:B<BR>RII
CRACK SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM 2022-148145 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM IAW SRM B737-700 51-10-02. TOOL USED DIGITAL CALIPER P/N: 500-197-30N S/N: A21043225; DUE DATE: 10/AUG/22.;[02] REPLACED SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM IAW SRM B737-700 51-10-02. TOOL USED DIGITAL CALIPER P/N: 500-197-30N S/N: A21043225; DUE DATE: 10/AUG/22.
CRACK SUPPORT BRACKET BODY STATION 540 AT LBL6 KEEL BEAM 2022-148142 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM IAW SRM B737-700 51-10-02. TOOL USED DIGITAL CALIPER P/N: 500-197-30N S/N: A21043225; DUE DATE: 10/AUG/22.;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT BRACKET BODY STATION 540 LBL6 KEEL BEAM IAW SRM B737-700 51-10-02. TOOL USED DIGITAL CALIPER P/N: 500-197-30N S/N: A21043225; DUE DATE: 10/AUG/22.;[03] REPLACED SUPPORT BRACKET BODY STATION 540 LBL6 KEEL BEAM IAW SRM B737-700 51-10-02. TOOL USED DIGITAL CALIPER P/N: 500-197-30N S/N: A21043225; DUE DATE: 10/AUG/22.
CRACK LOWER ANGLE LOCATED BS 663 AT LBL 9 REAR LOWER EDGE IN CENTER FUEL TANK 2022-148140 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23.;[02] REPLACED ANGLE AND FASTENERS LOC BS 663 AND BTW LBL 9 TO LBL 46 REAR LOWER EDGE IN CENTER FUEL TANK IAW B737-700 SRM 51-10-02 ÿ½TEM 9; SRM 51-40-02 AND DRAWING # 111A1000 SHEET 141 REV: -;[03] REPLACED ANGLE AND FASTENERS LOC BS 663 AND BTW LBL 9 TO LBL 46 REAR LOWER EDGE IN CENTER FUEL TANK IAW B737-700 SRM 51-10-02 ÿ½TEM 9; SRM 51-40-02 AND DRAWING # 111A1000 SHEET 141 REV: -<BR>CERTIFIED AS RII <BR>TASK COMPLETED;[04] CORRECTED REPLACED ANGLE AND FASTENERS LOC BS 663 AND BTW LBL 9 TO LBL 46 REAR LOWER EDGE IN CENTER FUEL TANK IAW B737-700 SRM 51-10-02 ÿ½TEM 9; SRM 51-40-02 AND DRAWING # 111A1000 SHEET 141 REV: - AND PERFORMED FUEL LEAK CHECK IAW B737-700 AMM 28-11-00-790-801 STEP 4.N. NOT FOUND LEAK EXTERNAL AREA SEE INDIVIDUAL SING OFF BELOW <BR>TASK COMPLETED [06] CORRECTED STEP 4: REPLACED ANGLE AND FASTENERS LOC BS 663 AND BTW LBL 9 TO LBL 46 REAR LOWER EDGE IN CENTER FUEL TANK IAW B737-700 SRM 51-10-02 ÿ½TEM 9; SRM 51-40-02 AND DRAWING # 111A1000 SHEET 141 REV: - AND PERFORMED FUEL LEAK CHECK IAW B737-700 AMM 28-11-00-790-801 STEP 4.N. NOT FOUND LEAK EXTERNAL AREA SEE INDIVIDUAL SING OFF BELOW <BR>TASK COMPLETED
CORROSION FLOOR STRUCTURE BEAM STA 986.5 AT LBL 42 WL208.1 AT AFT GALLEY AREA 2022-148122 / [01] TOOL USED ULTRASONIC EQUIPMENT PN:45MG; SN: 130063701; DUE DATE: 11-MAY-22;[02] EDDY CURRENT P/N: NORTEC500D; S/N: N500X12101U102020; DUE DATE: 01-JUN-22.;[03] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 2000053402; CAL DUE DATE: 23-APR-22;[04] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-70-51-2R-6 REPAIR 6 AND EA 22-153-0101;[05] CORRECTED STEP 4 THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-70-51-2R-6 REPAIR 6 AND EA 22-153-0101 SEE INDIVIDUAL SIGNOFFS BELOW;[06] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK DORSAL FIN FWD CLOSURE ANGLE RH SIDE AT VERTICAL STABILIZER 2022-148134 / [01] REPLACED CLOSURE ANGLE AND FASTENERS LOCATED RH SIDE AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02. AND DWG 147A0030. REV. ?B?. SEE INDIVIDUAL SIGN OFFS BELOW;[02] JOB COMPLETE <BR>RII.
CORROSION WEB LOCATED BS 1028 RBL 9 WL 208.1 AT AFT GALLEY AREA 2022-148125 / [01] REPLACED WEB LOCATED BTW BS 1006 BS 1028; BTW BL 0 TO RBL 40 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9 AND DWG:147A5730 SHEET:23 REV:C.;[02] CORRECTED STEP 1 <BR>REPLACED WEB LOCATED BTW BS 1006 BS 1028; BTW BL 0 TO RBL 40 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9 AND DWG:147A5730 SHEET:23 REV:C SEE INDIVIDUAL SIGNS OFF BELOW;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 CENTER SECTION 2022-148133 / [01] TOOL USED RADIUS GAUGE SET P/N: S167C S/N: AE-28454 DUE DATE: 17-JUL-22;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 02-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 02-FEB-23;[03] REPLACED ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 CENTER SECTION IAW SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #273A9110 SHEET 6 REV A. MATERIAL USED ALUMINUM SHEET CONVERTED FROM 7075-T0 TO CONDITION T73 0.050?. SEE INDIVIDUAL SIGNSOFF BELOW.;[04] REPLACED ANGLE FLOOR STRUCTURE LOCATED AT BS 695 BL0 CENTER SECTION IAW SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #273A9110 SHEET 6 REV A. MATERIAL USED ALUMINUM SHEET CONVERTED FROM 7075-T0 TO CONDITION T73 0.050?. SEE INDIVIDUAL SIGNSOFF BELOW<BR>RII .
CRACK ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 FWD POSITION LT WING 2022-148112 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 FWD POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 ;SHEET 7 ;REV -.;[02] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 FWD POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 ;SHEET 7 ;REV -.;[03] TASK CARD COMPLETED
CRACK ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING 2022-148115 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1; REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[03] REPLACED ANGLE TRAILING EDGE LOCATED WS228.25 TO WS253 AFT POSITION LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.
CRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING 2022-148117 / [01] REPLACED PLATE ASSY AND FASTENERS ON TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG:115A2001 SHEET:30 REV:A;[02] CORRECTED STEP 1:<BR>REPLACED PLATE ASSY AND FASTENERS ON TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG:115A2001 SHEET:30 REV:A SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED PLATE ASSY AND FASTENERS ON TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG:115A2001 SHEET:30 REV:A SEE INDIVIDUAL SIGN OFFS BELOW.
CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 AND BETWEEN BL0 TO RBL44; WL208.1 AT AFT GALLEY AREA 2022-148123 / [01] TOOL USED ULTRASONIC EQUIPMENT PN:45MG; SN: 130063701; DUE DATE: 11-MAY-22;[02] TOOL USED ULTRASONIC THICKNESS GAGE PN 45MG SN 130060401 DUE DATE 26-JAN-23.;[03] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 2000053402; CAL DUE DATE: 23-APR-22;[04] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[05] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 AND BETWEEN BL0 TO RBL44; WL208.1 AT AFT GALLEY AREA IAW EA 22-153-01028 SEE INDIVIDUAL SIGN-OFFS BELOW;[06] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFFS BELOW
CRACK ANGLE LOCATED BS294.5 AND RBL53 AT LEVEL FLOOR STRUCTURE AT PASSENGER CABIN 2022-148046 / [01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A20231804 DUE DATE: 26-AUG-22;[02] REPLACED ANGLE LOCATED BS294.5 AND RBL53 AT LEVEL FLOOR STRUCTURE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV:B; SEE INDIVIDUAL SING OFF BELOW.;[03] REPLACED ANGLE LOCATED BS294.5 AND RBL53 AT LEVEL FLOOR STRUCTURE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV:B; SEE INDIVIDUAL SING OFF BELOW. RII
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 AND BS 294.5 BL0 FWD GALLEY AND LAV 2022-148035 / [01] REPLACED NEW INTERCOSTAL LOC. BETWEEN BS 277 AND BS 294.5 BL0 FWD GALLEY AND LAVATORY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV:-SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED NEW INTERCOSTAL LOC. BETWEEN BS 277 AND BS 294.5 BL0 FWD GALLEY AND LAVATORY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV:-SEE INDIVIDUAL SING OFF BELOW. RII
CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-148040 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 141A1110 SHEET 18 REV - PART NUMBER USED: 141A1250-92 P.O: 2021 226356; SEE INDIVIDUAL SING OFFS BELOW.;[02] TASK CARD COMPLETED <BR>RII
CRACK FWD SERVICE DOOR CUTOUT STUD FRAME AT LEVEL STR8R AT PASSENGER CABIN 2022-148049 / [01] REPLACED FWD SERVICE DOOR CUTOUT STUD FRAME AT LEVEL STR8R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ÿ½TEM 9; SRM 51-40-02 AND DWG 141A8370 SHEET 10 REV: D. SEE INDIVIDUAL SING-OFFS BELOW.;[02] REPLACED FWD SERVICE DOOR CUTOUT STUD FRAME AT LEVEL STR8R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ÿ½TEM 9; SRM 51-40-02 AND DWG 141A8370 SHEET 10 REV: D. SEE INDIVIDUAL SING-OFFS BELOW. AS RII
CORROSION INNER CHORD LOCATED BETWEEN BS 270 AND BS 360 LBL57 WL208.1 AT FWD GALLEY AREA 2022-148050 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N: A21143429 DUE DATE:11-OCT-22;[02] REPLACED NEW INER CHORD LOC. BETWEEN BS 270 AND BS 360 LBL57 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8110 SHEET 11 REV:* AND DWG 143A5900 SHEET 137 REV: A SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED NEW INER CHORD LOC. BETWEEN BS 270 AND BS 360 LBL57 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8110 SHEET 11 REV:* AND DWG 143A5900 SHEET 137 REV: A SEE INDIVIDUAL SIGN-OFF BELOW AS RII
CRACK WEB LOCATED BETWEEN BS 303.9 AND BS 294.5 S-16L AT FWD GALLEY AREA 2022-148033 / [01] REPLACED WEB LOCATED BETWEEN BS 303.9 AND BS 294.5 S-16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8180 SHEET 27 REV; C SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED WEB LOCATED BETWEEN BS 303.9 AND BS 294.5 S-16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8180 SHEET 27 REV; C RII .SEE INDIVIDUAL SING OFF BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL46 FWD GALLEY AND LAV 2022-148037 / [01] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL46 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:- SHEET 39; P/N USED IS: 141A5410U140; TOOL USED CALIPER P/N: 500-196-30 S/N: A21033535 DUE DATE: 09-OCT-22.SEE INDIVIDUAL SIGNOFFS BELOW;[02] CORRECTED STEP 1<BR>REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL46 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:- SHEET 29; P/N USED IS: 141A5410U140; TOOL USED CALIPER P/N: 500-196-30 S/N: A21033535 DUE DATE: 09-OCT-22.SEE INDIVIDUAL SIGNOFFS BELOW;[03] CORRECTED STEP 2.<BR>REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL46 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:- SHEET 26; P/N USED IS: 141A5410U140; TOOL USED CALIPER P/N: 500-196-30 S/N: A21033535 DUE DATE: 09-OCT-22.SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL46 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:- SHEET 26; P/N USED IS: 141A5410U140; TOOL USED CALIPER P/N: 500-196-30 S/N: A21033535 DUE DATE: 09-OCT-22.SEE INDIVIDUAL SIGNOFFS BELOW RII
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 360 AND BS 344 BL0 FWD GALLEY AND LAV 2022-148034 / [01] REPLACED NEW WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 360 AND BS 344 BL0 FWD GALLEY AND LAVATORY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV: -SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED NEW WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 360 AND BS 344 BL0 FWD GALLEY AND LAVATORY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV: -SEE INDIVIDUAL SING OFF BELOW. RII
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL46 FWD GALLEY AND LAV 2022-148036 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED NEW WEB LOC. FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL46 FWD GALLEY AND LAVATORY IAW B737-700 SRM 51-40-01 AND DWG 141A5400 SHEET 44 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2 REPLACED NEW WEB LOC. FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL46 FWD GALLEY AND LAVATORY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED NEW WEB LOC. FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL46 FWD GALLEY AND LAVATORY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL31 FWD GALLEY AND LAV 2022-148038 / [01] TOOL USED CALIPER P/N: 500-196-30 S/N: A21033535 DUE DATE: 09-OCT-22;[02] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL31 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:- SHEET 39; P/N USED IS: 141A5410U140.SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL31 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:- SHEET 39; P/N USED IS: 141A5410U140.SEE INDIVIDUAL SIGNOFFS BELOW RII
CORROSION WEB INTERCOSTAL LOCATED BETWEEN BS 294 AND BS 312 LBL 12 WL208.1 AT FWD GALLEY AREA 2022-148039 / [01] REPLACED NEW WEB INTERCOSTAL LOCATED BETWEEN BS 294 AND BS 312 LBL 12 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 ÿ½TEM 9 AND DWG 141A5600 SHEET 1 REV: N. SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1 REPLACED NEW WEB INTERCOSTAL LOCATED BETWEEN BS 294 AND BS 312 LBL 12 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5600 SHEET 1 REV: N. SEE INDIVIDUAL SIGN OFFS BELOW;[03] CORRECTED STEP 2 REPLACED NEW WEB INTERCOSTAL LOCATED BETWEEN BS 294 AND BS 312 LBL 12 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND 51-10-02 ÿ½TEM 9 AND DWG 141A5600 SHEET 1 REV: N. SEE INDIVIDUAL SIGN OFFS BELOW;[04] REPLACED NEW WEB INTERCOSTAL LOCATED BETWEEN BS 294 AND BS 312 LBL 12 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND 51-10-02 ÿ½TEM 9 AND DWG 141A5600 SHEET 1 REV: N. SEE INDIVIDUAL SIGN OFFS BELOW
CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN BS312 AND BS328 RBL10 WL208.1 AT FWD GALLEY AREA 2022-148041 / [01] REPLACED NEW INTERCOSTAL LOC. BETWEEN BS312 AND BS328 RBL10 WL208.1 AT FWD GALLEY AREA IAW B737-700 DWG 141A5400 SHEET 10 REV; - ;SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW
CORROSION FLOOR BEAM STA 312 AT LBL16 WL208.1 AT FWD GALLEY AREA 2022-148042 / [01] TOOL USED ULTRASONIC EQUIPMENT PN:45MG; SN:130064101; DUE DATE: 11-MAY-22;[08] REPAIRED FLOOR BEAM BS 312 BTW LBL 40 TO RBL 28. IAW B737 SRM 53-10-51-2R-17 REPAIR 17 REMOVED COVER PROTECTIVE CONTROL CABLES BTW BS294.5 TO BS 328 AND RBL45 TO LBL45 AT FWD GALLEY AREA IAW B737-700 AMM 51-21-91-620-801 AND REMOVED EWIS PROTECTION LOCATED BTW BS294.5 TO BS 328 AND RBL45 TO LBL45 AT FWD GALLEY AREA IAW B737-700 AMM 20-60-07-913-801 RII. SEE INDIVIDUAL SING-OFF BELLOW
CORROSION ANGLE BRACKET LOCATED BS312 AND LBL55; WL208.1 AT PASSENGER CABIN 2022-148056 / [01] REPLACED ANGLE BRACKET LOCATED ON BS312 AND LBL55; WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5220; SHEET 1; REV -. DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM B737-700 REMOVED P/N:141A5220-2 AND NOMINAL THICKNESS IS:0.080? TOOL DIGITAL CALIPER USED P/N:500-464 S/N: 11228551 DUE DATE: 25-SEP-22;[02] REPLACED ANGLE BRACKET LOCATED ON BS312 AND LBL55; WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5220; SHEET 1; REV -. DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM B737-700 REMOVED P/N:141A5220-2 AND NOMINAL THICKNESS IS:0.080? RII
CRACK FRAME ON BS 312 LOCATED AT FWD UPPER EDGE CUT OUT DOOR LH SIDE AT FWD GALLEY AREA 2022-148032 / [01] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 02-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 02-FEB-23;[03] REPAIRED FRAME ON BS 312 LOCATED AT FWD UPPER EDGE CUT OUT DOOR LH SIDE AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-07-2R-1 THIS REPAIR IS CATEGORY B REQUIRED INSPECTION TO 50;000 FLIGHT CYCLES OR 12;000 FLIGHT CYCLES AFTER REPAIR INSTALLATION; WHICHEVER IS LATER. SEE INDIVIDUAL SING OFF BELOWS.;[04] REPAIRED FRAME ON BS 312 LOCATED AT FWD UPPER EDGE CUT OUT DOOR LH SIDE AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-07-2R-1 THIS REPAIR IS CATEGORY B REQUIRED INSPECTION TO 50;000 FLIGHT CYCLES OR 12;000 FLIGHT CYCLES AFTER REPAIR INSTALLATION; WHICHEVER IS LATER. SEE INDIVIDUAL SING OFF BELOWS.
BROKEN SUPPORT BRACKET INSULATOR LOCATED BS578 TO BS663.75 AND BETWEEN STR10R TO STR16R AT PASSENGER CABIN (4 EA) 2022-147999 / [01] REPLACED INSOLATER BRAKET (1E/A) AND INSOLATOR BRACKET (3E/A) LOCATED ON BS578 AND BETWEEN STR10R TO STR16R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 144A1312; SHEET 4; REV -.;[02] REPLACED INSOLATER BRAKET (1E/A) AND INSOLATOR BRACKET (3E/A) LOCATED ON BS578 AND BETWEEN STR10R TO STR16R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 144A1312; SHEET 4; REV -.
CORROSION FUEL STATION PANEL WEB LOCATED OFSS 385 AT RT WING 2022-148009 / [01] REPLACED FUEL STATION PANEL WEB LOCATED OFSS 385 AT RT WING IAW B737-700 AMM 28-41-61-401-NG TEST IS OK. TOOL USED: P/N: T477W; S/N: 2073; DUE DATE: 17-NOV-22.;[02] CORRECTED STEP 1:<BR><BR>REPLACED FUEL STATION PANEL WEB LOCATED OFSS 385 AT RT WING IAW B737-700 AMM 28-41-61-401-NG TEST IS OK. TOOL USED: P/N: T477W; S/N: 2073; DUE DATE: 17-NOV-22.<BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK LOWER SURFACE SLAT 8 OF THE LEADING EDGE SLAT NOSE SKIN LOCATED SLAT STA451.97 RT WING (2 EA) 2022-148007 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022236 ; DUE DATE: 02-JUN-22;[02] REPAIRED LOWER SURFACE SLAT 8 OF THE LEADING EDGE SLAT NOSE SKIN LOCATED SLAT STA451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED LOWER SURFACE SLAT 8 OF THE LEADING EDGE SLAT NOSE SKIN LOCATED SLAT STA451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNOFF BELOW... RII ITEM
CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.250 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.000 INCH 2022-148014 / [01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[02] REPAIRED LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN BTW STAB STATION 184.70 TO STAB STATION 203.10. IAW B737 700 SRM 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SING-OFF BELOW;[03] REPAIRED LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN BTW STAB STATION 184.70 TO STAB STATION 203.10. IAW B737 700 SRM 55-10-01-2R-11 REPAIR 11.RII . SEE INDIVIDUAL SING-OFF BELOW
MISSING STUD HANDLE DOOR AT FWD CARGO COMPARTMENT 2022-148012 / [01] INSTALLED NEW STUD HANDLE DOOR AT FWD CARGO COMPARTMENT IAW: CMM (HARTWELL CORPORATION) 52-36-15 STEP 4.B PAGE 702;[02] INSTALLED NEW STUD HANDLE DOOR AT FWD CARGO COMPARTMENT IAW: CMM (HARTWELL CORPORATION) 52-36-15 STEP 4.B PAGE 702
CRACK SLAT 4 NOSE SKIN AT THE ACTUATOR LEADING EDGE AT LT WING 2022-147829 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 60009161631; DUE DATE: 03-DEC-22;[02] TOOL USED; CALIPER; PN: 700-113-10; SN: 0033158; DUE DATE: 01-OCT-22; PRECISION RADIUS GAUGE; PN: S167C; SN: AE-28454; DUE DATE: 17-JUL-22.;[03] REPAIRED SLAT 4 NOSE SKIN AT THE ACTUATOR LEADING EDGE AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 FIGURE 202 SHEET 4. THIS REPAIR IS CATEGORY A AND RE-INSPECTION IS NOT REQUIRED. SEE INDIVIDUAL SING-OFFS BELOW.;[04] REPAIRED SLAT 4 NOSE SKIN AT THE ACTUATOR LEADING EDGE AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 FIGURE 202 SHEET 4. THIS REPAIR IS CATEGORY A AND RE-INSPECTION IS NOT REQUIRED. SEE INDIVIDUAL SING-OFFS BELOW... RII ITEM
CUSTOMER REQUEST - DEBONDED EXISTING REPAIR ON OB AFT FLAP UPPER SURFACE ON IB EDGE AT RT WING 2022-147848 / [01] TOOL USED: CALIPER PN: 500-464; S/N: 15331926; DUE DATE: 28/SEP/22.;[02] UT TOOL USED PN: S-3; SN: 064. DUE DATE: 12-JUL-22;[03] TOOL USED HOT BONDER P/N HCS9000B-AV S/N 18164925 DUE DATE 16/JAN/23;[04] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196127 DUE DATE 16/JAN/23;[05] TOOL USED: ULTRASONIC EQUIPMENT P/N: EPOCH 650; S/N: 190859705; DUE DATE: 08-JUN-22;[06] TOOL USED: SCALE: P/N:CL5000 S/N:AE-39088 DUE DATE:17-MAY-22;[07] REPAIRED O/B AFT FLAP UPPER SURFACE ON I/B EDGE AT RT WING AS PER B737-700 SRM 57-53-01-2R-16 REPAIR 16. SEE INDIVIDUAL SIGN OFFS BELOW;[08] TASK COMPLETED RII.
EMERGENCY EXIT CEILING SIGN DAMAGED. RESECURED LIGHT COVER PANEL PER SIP;NO DAMAGE NOTICE.
LOOSE SCREW FOUND ON AFT CARGO THRESHOLD. ; / [01] R/R AFT DOOR CENTER SCUFF PLATE PER AMM 53-11-02. A/C OK FOR SERVICE.
A/C 463 FLAP LOCK OUT ; FLAPS FAILED TO MOVE AT 10 DURING APPROACH / [01] FOUND FAULT TE SENSOR R MSG 27-52260. CLEANED SENSOR AND CANNON PLUG PER SWPM 20-60-01. OPS CK'D FLAPS OK PER AMM 27-51-00. ALL WORK COMPLETED BY E28906.
RH MOST FWD PHOTO ILLUM STRIP HAS CONDENSATION / R&R PHOTO ILLUM STRIP PER AMM 25-27-31
AFT SERVICE DOOR HANDLE WOULD NOT STAY STOWED IN FLIGHT. MOVED UP ON ITS OWN SEVERAL TIMES. / ACCOMPLISHED FIM 52-10 TASK 808; TIGHTENED HANDLE FASTENERS TO HUB. OPS NORMAL
BROKEN STRUT FAIRING RING STOP ON FWD COMPRESSION ROD AT ENGINE 2 (2 EA) / REPLACED STRUT FAIRING RING STOP ON FWD COMPRESSION ROD AT ENGINE 2 (2EA) IAW B737-700 SRM 51-10-02-0G-0 STEP 9
CRACK INSPAR RIB LOCATED ON STAB STA 120.30 AND 18 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER (1 EA) REPAIRED INSPAR RIB LOCATED ON STAB STA 120.30 AND 18 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER (1EA) IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4
CORROSION STRUCTURE PLATE LOCATED 8 INCHES AFT OF BS 787 AT LEVEL STR 25R AND RBL 22 AT AFT CARGO COMPARTMENT (1 EA) / EVALUATED REWORK ON PLATE STRUCTURE LOCATED 8' AFT BS787 AT LEVEL STR.25R AND RBL.22 AT AFT CARGO COMPARTMENT IAW SRM B737-700 53-60-15-1A-1 ALLOWABLE DAMAGE 1 FIG 103 DETAIL G; TABLE 101. PARAGRAPH 4G(3) AND APPLIED PROTECTIVE TREATMENT IAW SRM B737-700 51-20-01-0G-0
INOP EMERGENCY LIGHT BATTERY PACKS M1672 AND M1673 AT AFT GALLEY AREA (2 EA) / REPLACED EMERGENCY LIGHT BATTERY PACKS M1672 AND M1673 AND PERFORMED OPERATIONAL TEST IAW B737-700 AMM 33-51-06-960-805. TEST IS OK.
CRACK STIFFENER FLOOR STRUCTURE AT BS 540 AND BETWEEN LBL 0.07 TO RBL 24.82 CENTER SECTION (1 EA) REPLACED STIFFENER LOC FLOOR STRUCTURE AT BS540 AND BETWEEN LBL 0.07 TO RBL 24.82 CENTER SECTION (1EA) IAW B737-700 SRM 51-40-02 AND DWG 143A0060 AND SRM 51-10-02 ITEM 9 DUE TO ALLOWABLE DAMAGE NOT FOUND IN SRM
CORROSION STRAP LOCATED AT LEVEL BS 887 BTW STR 25R TO STR 27L AND BTW RBL 22 TO LBL 8 AT AFT CARGO COMPARTMENT (1 EA) / REPLACED STRAP LOCATED AT LEVEL BS 887 BETWEEN STR 25R TO STR27L AND BETWEEN RBL 22 TO LBL 8 AT AFT CARGO COMPARTMENT (1EA) IAW B737-700 SRM 51-10-02 AND DRAWING 146A7500 REV
CRACK STIFFENER FLOOR STRUCTURE AT BS 540 AND BETWEEN LBL 0.07 TO LBL 24.82 CENTER SECTION (1 EA) REPLACED STIFFENER LOC. FLOOR STRUCTURE AT BS540 AND BETWEEN LBL 0.07 TO LBL 24.82 CENTER SECTION (1EA) IAW B737-700 SRM 51-40-02 AND DWG 143A0060 AND SRM 51-10-02 ITEM 9 DUE TO ALLOWABLE DAMAGE NOT FOUND IN SRM
CORROSION LOWER SILL WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R AND RBL 22 AT AFT CARGO COMPARTMENT / REPLACED LOWER SILL WEB LOC BTW BS 767 TO BS 787 AT LEVEL OF STR 25R AND RBL 22 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; 51-10-02 ITEM 9 AND DWG #146A0081 REV A
CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 787 AT LEVEL STR 25L AND LBL 22 AT AFT CARGO COMPARTMENT (1EA) / REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 787 AT LEVEL STR25L AND LBBL22 AT AFT CARGO COMPARTMENT; IAW SRM B737-700-51-10-02; 51-40-02; DWNS 146A7500; 146A7502 MATERIAL USED BAC1496-377 7075-T62_PO: 2020-109561
CRACK SUPPORT ZEE LOCATED BTW BS 727D TO BS 727E AT LEVEL STR 25R AFT CARGO COMPARTMENT (1 EA) / REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG #146A7500 DWG #146A7502; MATERIAL P/N:BAC1496-377-7075-162 PO:2020-109561
CRACK INSPAR RIB LOCATED ON STAB STA 120.30 AND 18 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER REPAIRED INSPAR RIB LOC. ON STAB STA 120.30 AND 18 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4
CRACK GUSSET LOCATED AT BS 500D STRINGER 19 LEFT SIDE FWD CARGO COMPARTMENT REPLACED GUSSET LOCATED AT VS 500D STR 19 LEFT SIDE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 14347902
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 492 AND BS 500A ; STR 26R ; RBL 24 ;WL156 AT FWD CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL (SHIELD ASSY) LOCATED BETWEEN BS492 AND BS500A STR 26R RBL 24; WL 156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING 143A0080 REV-
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 420 AND BS 440 AT LEVEL STR 26R ;RBL 24 ;WL 156 AT FWD CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS.420 AND BS.440 AT LEVEL STR 26R; RBL 24 AND WL 156 AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 STEP 9 AND DRAWING #143A0080.
CRACK ANGLE - SUPPORT LOCATED BS 400 AFT SIDE ; BS 500B FWD SIDE AND B S 500C FWD SIDE AT LEVEL STRINGER 26 LEFT FWD CARGO COMPARTMENT (3 EA ) / REPLACED ANGLE SUPPORT LOC. BS 400 AFT SIDE; BS 500B FWD SIDE; AND BS 500C FWD SIDE AT LEVEL STR 26L FWD CARGO COMPARTMENT (3EA) IAW B737-700 SRM 51-10- 02 ITEM 9 AND DWG 143A7505 REV R.
CRACK GUSSET LOCATED BS500D AT STRINGER 19 RIGHT SIDE FWD CARGO COMPARTMENT REPLACED GUSSET LOCATED AT BS 500D AT STR 19 RIGHT SIDE FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 14347902
CRACK INSPAR RIB LOCATED ON STAB STA 120.30 AND 9 INCH FROM REAR SPAR AT LT HORIZONTAL STABILIZER REPAIRED INSPAR RIB LOCATED ON STAB STA 120.30 AND 9 INCHES FROM REAR SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4
CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB (1 EA) REPLACED SEAL PLATE LOCATED ON ACCESS PANEL # 333AB AT LT HORIZONTAL STABILIZER (1 EA) IAW B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02-OG-0 ITEM 9 SEAL PLATE PN 186A3004-17
CRACK INSPAR RIB LOCATED ON STAB STA 120.30 AND 18 INCH FROM REAR SPAR AT LT HORIZONTAL STABILIZER REPAIRED INSPAR RIB LOCATED ON STAB STA 120.30 AND 18 INCHES FROM REAR SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4
INOP EMERGENCY LIGHT BATTERY PACK M1668 AND M1669 AT PASSENGER CABIN / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1668 AND M1669 IAW AMM 33-51-06-960-805 AND PERFORMED EMERGENCY LIGHT BATTERY PACK INSTALLATIONT TEST IAW AMM 33-51-06-960-805 TEST IS GOOD.
CRACK LEADING EDGE RIB LE STA 86.66 AT RT HORIZONTAL STABILIZER (1 EA ) / REPLACED 4E RIB STA 95.96 AT RH HORIZONTAL STABILIZER AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 186A1001 REV A
DELAMINATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) / REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802
CRACK INDICATION ON FWD SERVICE DOOR BEAM ÿ½4 LOWER FACE, CRACK LENGTH=0.990 INCH APPROX. AT PASSENGER (1 EA) REPLACED FWD SERVICE DOOR BEAM #4 LOWER FACE AT PASSENGER CABIN (1EA) IAW B737-700 SRM 51-40-02 AND DRAWING 141A6516.
CRACK VAPOR BARRIER BS 663 AT LBL 10 AT MAIN WHEEL WELL COMPARTMENT REPAIRED VAPOR BARRIER BS 663 AT LBL 10 AT MAIN WHEEL WELL COMPARTMENT ASPER B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED CALIPER P/N 700-113-10 S/N 0016645 , DUE DATE 13-FEB-21 ,HOT BONDER P/N HCS 9000B, S/N 15092096 DUE DATE 27-NOV-20, SCALE P/N CL5000 S/N AE-39882, DUE DATE 05-NOV-20
CRACK STRAP LOC BETWEEN BS 947 TO BS 867 AND LBL 11 ON AREA FLOOR PANEL 140DF AND 140CF AT AFT CARGO COMPARTMENT / REPLACED STRAP LOC BETWEEN BS 947 TO BS 867 AND LBL 11 ON AREA FLOOR PANEL 140DF AND 140CF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; PARAGRAPH #9.
BROKEN STRUT FAIRING RING STOP ON AFT COMPRESSION ROD AT RT PYLON (2 EA) / REPLACED RING STOP ON AFT COMPRESSION ROD AT RT PYLON IAW B737-700 SRM 51-10-02-0G-0 DWG 315A2080-6
RUDDER COUNTER BALANCE WEIGHT HAS SURFACE CORROSION / REMOVED AND REPLACED RUDDER COUNTER BALANCE WEIGHT PER CMM 55-40-09
LEFT EMERGENCY EXIT LIGHTS INOP AT BULLNOSE 9 AND 11. R&R BATTERY PACK PER AMM.
R2 DOOR EMERGENCY LIGHT INOP. R&R BATTERY PER AMM.
R2 DOOR EMERGENCY LIGHT INOP. R&R BATTERY CHARGER PER AMM.
RT EMERGENCY LIGHT ABOVE R1 DOOR INOP. FOUND CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR IAW AMM.
R1 DOOR SLIDE EMERGENCY LIGHT INOP. FOUND CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR IAW AMM.
GALLEY FWD EMERGENCY EXIT SIGN INOP. REPLACED EXIT SIGN ASSY OPS CK GOOD REF AMM 33-51-01
LIGHTS CONNECTED TO M1674 EMERGENCY LIGHT BATTERY PACK FAULTY. R&R BATTERY PACK PER AMM.
LT AFT FUSELAGE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
EMERGENCY EXIT PULL CORD COVER MISSING HOOK AND LOOP MISSING. R&R COVER PER AMM.
R2 WINDOW ARCED AND DELAMINATED AT FORWARD EDGE. R&R WINDOW HEAT CONTROL UNIT PER AMM.
R2 WINDOW ARCED AND DELAMINATED AT FORWARD EDGE. R&R WINDOW PER AMM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. R&R SLIDE PER MT.
R1 DOOR ESCAPE SLIDE INADVERTENTLY FELL OUT OF BRACKET, DID NOT DEPLOY, STILL OPERATIONAL. R&R SLIDE PER MT.
L/H STA 663 WEB STIFFENER AT LBL 25 CRACKED N / REMOVED LOCATED AND DRILLED NEW BS 663 LBL25' VERTICAL STIFFENER I/A/W SPM 51-40-02. 51-40-05 AND BOEING DWB 149A7210 INSTALLED I/A/W SRM 51-40-02 AND BOEING DWG 149A7210
FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED. / REPAIR ACCOMPLISHED IAW EA 1-A53-2076 REV 11 ON B/S W/O 37212-1000-0002 (FWD CORNER SCUFF PLATE FWD CARGO - WELDED)
LEFT WING LOWER TRAILING EDGE, INBOARD NR 3 FLAP TRACK, WAFFLE BOARD CRACKED AT FASTENER HOLE. R & R THE WAFFLE BOARD IAW DWG.
R/H WING LOWER CURVED BULB SEAL RETAINER 10' INBD OF THE DEFLECTOR RIB IS CRACKED / REMOVED CRACKED BULB SEAL RETAINER BRKT. LOCATED AND DRILLED NEW PART N 115A29553-2 IAW SRM 51-40-05. WING STRUCTURE IAW RAM 51-40-02-0G-0 AND BOEING DWG 115A2930 REV- A27861
FWD CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED. / REPAIR ACCOMPLISHED IAW EA1-A53-2076 REV 11 ON B/S W/O 37212-1400-0001 (AFT SCUFF PLATE FWD CARGO - WELDED)
CENTER WING SECTION REAR SPAR LT LOWER VAPOR BARRIER WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM AND DWG.
AFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED / REPAIR ACCOMPLISHED ON B/S 37212-1000-0001 IAW EA 1-A53-2076 REV 11 (FWD CORNER SCUFF PLATE FOR AFT CARGO - WELDED)
LT OVERWING EMERGENCY EXIT LOWER IDENTIFIER LIGHT INOP. R&R BATTERY PACK PER AMM.
EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01669. R&R BATTERY PACK PER AMM.
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01668. R&R BATTERY PACK PER AMM.
SUPPLEMENTAL INFORMATION: FWD CARGO MIDDLE SCUFF PLATE IS GOUGED AND CRACKED FROM CARGO DOOR LOWER STOPS. / R&R FWD CARGO DOOR MIDDLE SCUFF PLATE IAW M/M 53-11-02.
FORWARD ENTRY LIGHT EGRESS LENS BROKEN. R&R LIGHT IAW AMM.
R1 DOOR SLIDE GIRT BAR LOOSE. ADJUSTED SLIDE IAW MM.
SIDEWALL EXIT LIGHT INOPERATIVE AT ROW 12 DEF. R & R LIGHT ASSEMBLY IAW MM.
LEFT WING EMER LIGHT LENS AFT DIRTY. CLEANED LENS IAW AMM.
L2 DOOR EMER LIGHT BULB AFT OF DOOR INOPERATIVE. RELAMPED LIGHT IAW AMM.
RIGHT OVERWING EMER EXIT LIGHT AFT OF DOOR BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
AFT CARGO BAY INTERCOSTAL ANGLE CORRODED, BETWEEN BS 767 - 787. R & R ANGLE IAW SRM.
CREASE BEAM WEB CORRODED, BETWEEN BS 380 - 400, RBL 63. R & R CREASE BEAM WEB IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB CRACKED, AT STATION 92.70, IN LOWER AREA. REPAIRED RIB IAW SRM.
FRAME WEB CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 360, STRINGER 8R. REPAIRED WEB IAW EA.
FRAME CRACKED AT BS 294.5, RBL 56. REPAIRED FRAME IAW ER & EA.
FRAME WEB CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.
MAIN WW VERTICAL SPAR WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW SRM.
FRAME WEB CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, AT 2ND & 3RD STIFFENERS IN LOWER AREA. REPAIRED RIB IAW SRM.
THRESHOLD SUPPORT ANGLE CORRODED, BETWEEN BS 308 - 340, RBL 61. R & R ANGLE IAW SRM.
FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 5 - 35. REPAIRED FLOORBEAM IAW EA.
AFT CARGO BAY FWD RT SHIELD CORRODED, BETWEEN BS 767 - 792. R & R SHIELD IAW SRM.
AFT CARGO BAY, BULKHEAD FITTING CRACKED AT BS 947.5, LBL 10.5. R & R FITTING IAW SRM & DWG.
AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R & R WEB IAW SRM.
LEFT WING FLAP TRACK FAIRING 542BB CRACKED AT TE INBD LOWER CORNER. REPAIRED FAIRING IAW EA.
EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1675. R&R BATTERY PACK PER DWG.
EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1668. R&R BATTERY PACK PER DWG.
LT WING FIXED TRAILING EDGE PANEL BEHIND NR 3 PYLON AFT SEAL BRACKET CRACKED. R&R SEAL BRACKET PER SRM.
LT WING LOWER FIXED TRAILING EDGE PANEL BEHIND NR 3 PYLON WIGGLE PLATE CRACKED. R&R WIGGLE PLAT IAW SRM.
R1 DOOR HANDLE TORQUE BOX LOWER SUPPORT FRAME CRACKED AT LOWER INBOARD FORWARD ATTACH BOLT. R&R DOOR PER AMM.
EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1673. R&R BATTERY PACK PER DWG.
L1 DOOR EMER EVAC SLIDE LOW PRESS. R & R SLIDE IAW MT.
R1 DOOR EMER SLIDE LOOSE. SECURED SLIDE IAW MT.
L1 DOOR EMER LIGHT LENS LOOSE. R & R LENS IAW MM.
L1 DOOR SLIDE INADVERTENTLY FELL OUT OF ITS HOLDER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
L2 DOOR EMER EVAC SLIDE COVER LOOSE. SECURED COVER IAW AMM.
MID CABIN EMER EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW MM.
R1 DOOR EMER EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.
RIGHT WING NR 6 SLAT TE WEDGE DELAMINATED. REPAIRED WEDGE IAW SRM & EA.
L1 DOOR LOWER EMER EXIT LIGHT COVER LENS MISSING. R & R LENS ASSEMBLY IAW MM.
FLIGHT DECK FLOORBEAM CORRODED AT BS 270, BETWEEN LBL 12 TO RBL 12. REPAIRED BEAM IAW EA.
WAFFLE PLATE UNDER NR 6 FLAP TRACK CRACKED. REPAIRED PLATE IAW SRM.
NR SEAT TRACK CRACKED AT BS 727B, RBL 45.5, OTBD FWD HOLE. REPAIRED SEAT TRACK IAW SRM.
RIGHT WING TE VERTICAL WEB CRACKED IN FLAP WELL ABOVE PANEL 651GB. R & R PANEL IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 157.1 INBD SIDE OF RIB 9.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.50 INBD SIDE OF RIB 9.5 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 175.5 INBD SIDE OF RIB 10.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 138.70 INBD SIDE OF RIB 9 INCHES AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 138.7 INBD SIDE OF RIB 10 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
VERTICAL STIFFENER CRACKED AT STATION 663.75, LBL 27.5. R & R STIFFENER IAW SRM.
RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 101.9, 28 INCHES, AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 101.9, 18 INCHES AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.
LT OVERWING EXIT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R LIGHT POWER SUPPLY IAW MM.
R1 DOOR EVAC SLIDE GIRT BAR RIGHT HOOK LOOSE. SECURED HOOK PER MM.
DRAIN MAST ON WING TO BODY FAIRING BS 727B +10 LBL 65 TRAILING EDGE DELAMINATED. REMOVED AND REPLACED MAST IAW AMM.
BS 663 BULKHEAD CRACKED RIGHT W/W RBL 37 WL 198. REPAIRED BULKHEAD IAW SRM.
EEPLS LENS MISSING AT ROW 9. INSTALLED LENS IAW M/M.
MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED FUSE PER M/M.
FORWARD SIDE WALL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED FUSE PER M/M.
LEFT EEPLS COVER MISSING AT ROW 12. INSTALLED COVER PER MM.
EEPLS END CAP MISSING AT ROW 1. INSTALLED END CAP PER MM.
RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT BS 105.26. REPAIRED SKIN PER SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT 35.5 INCHES FROM I/B END OF STABILIZER, 31 INCHES FROM TRAILING EDGE. REPAIRED SKIN PER SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT 82 INCHES FROM I/B END OF STABILIZER, 26 INCHES FROM TRAILING EDGE. REPAIRED SKIN PER SRM.
LEFT HORIZONTAL STABILIZER SKIN CRACKED AT BS 105.26. REPAIRED SKIN PER SRM.
STRINGER CHAFED AT BS 335, STR 5R. REPAIRED STRINGER PER SRM.
CENTER OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.
FWD EEPLS BROKEN. REMOVED AND REPLACED FWD EEPLS ASSY PER MM.
R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER M/M & SRM.
L1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR STORAGE HOOK LOOSE.SECURED HOOK PER M/M & SRM.
R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER M/M AND MT.
LT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.
LT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 23. REMOVED AND REPLACED COVER PER AMM.
LT EEPLS ENDCAP MISSING AT ROW 1. REMOVED AND REPLACED ENDCAP PER M/M.
RT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.
RT AFT GALLEY EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER AMM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
EEPLS BULB MISSING AT ROW 1. INSTALLED BULB PER MM.
EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.
DURING SCHEDULED MV1 CHECK FOUND, R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.
DURING SCHEDULED MV2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS END CAP MISSING AT ROW 1. INSTALLED END CAP PER MM.
EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.
EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LOOSE AT ROW 2. REMOVED AND REPLACED EEPLS PER MM.
FWD GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS COVER MISSING AT ROW 6. INSTALLED COVER PER MM.
DURING SCHEDULED 6Y CHECK, FOUND EEPLS TRACKS BROKEN. REMOVED AND REPLACED EEPLS TRACK COVERS PER MM.
DURING SCHEDULED 6Y CHECK, FOUND CRACK INDICATION AT WING CENTER SECTION FRONT SPAR UPPER CHORD AT LBL 7 AFT END. R&R FITTING PER SRM AND BAC DWG.
DURING SCHEDULED 6Y CHECK, FOUND CRACK INDICATION AT WING CENTER SECTION FRONT SPAR UPPER CHORD AT LBL 32 AFT END. R&R FITTING PER SRM AND BAC DWG.
DURING SCHEDULED 6Y CHECK, FOUND CRACK INDICATION AT WING CENTER SECTION FRONT SPAR UPPER CHORD AT LBL 14.5 AFT END. R&R FITTING PER SRM AND BAC DWG.
DURING SCHEDULED 6Y CHECK, FOUND CRACK INDICATION AT WING CENTER SECTION FRONT SPAR UPPER CHORD AT RBL 7 AFT END. R&R FITTING PER SRM AND BAC DWG.
DURING SCHEDULED 6Y CHECK, FOUND CRACK INDICATION AT WING CENTER SECTION FRONT SPAR UPPER CHORD AT RBL 14.5 AFT END. R&R FITTING PER SRM AND BAC DWG.
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER EA.
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER EA.
DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 15 TO ROW 21. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVER PER MM.
EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND FWD ENTRY EXTERNAL EGRESS LIGHT INOP. RELAMPED PER MM.
FWD ENTRY EEPLS COVER LOOSE. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM.
FOUND LT EMERGENCY EXIT LIGHT COVERS LOOSE. R&R COVER PER MM.
FOUND RT EMERGENCY EXIT LIGHT COVERS LOOSE. R&R COVER PER MM.
FOUND L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, LEFT MID CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
R2 COCKPIT WINDOW ARCING. REMOVED AND REPLACED R2 COCKPIT WINDOW PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 19 ABC. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 3 ABC AND ROW 8 ABC. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 10 ABC. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 12 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
EEPLS COVER MISSING AT ROW 11 ABC. INSTALLED EEPLS COVER PER MM.
DURING SCHEDULED MV3 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 14 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.
EEPLS TRACK LOOSE AT FWD END. SECURED EEPLS PER MM.
EEPLS TRACK COVER LOOSE AT ROW 2. REMOVED AND REPLACED COVER PER MM.
EEPLS STRIP LOOSE AT ROW 11. SECURED STRIP PER MM.