N260WN
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
261 reports on file, 2008-04-03 – 2026-08-10.
Part: MEC — LEAKING (ZONE 100) · airframe 64,581 hrs · 38,863 cycles
LOSS OF SYSTEM B HYD SYS. R & R NR 2 ENG EDP IAW AMM 29-11-11, LEAK CHECKED GOOD, OPS CHECKED GOOD.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 64,580 hrs · 38,862 cycles
AFT SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED PER AMM 33-51-04. OPS CHECK GOOD
Part: FIRE WARNING — NO TEST (NR 2 ENGINE) · airframe 64,536 hrs · 38,832 cycles
NR 2 ENGINE OVERHEAT AND FIRE LIGHTS FAILED TO LIGHT DURING TEST IN NORMAL POSITION. LIGHTS UP WITH SELECTOR IN A & B POSITIONS. NR 2 ENGINE OVERHEAT LIGHT ON IN B POSITION. OK TO CONTINUE ON MEL 26-2-01. SP#1.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 64,376 hrs · 38,735 cycles
EMERGENCY EXIT LIGHT BEHIND L1 DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT LAMP BEHIND L1 DOOR IAW AMM 33-51-04. OPS CHKD GOOD.
Part: FAIRING — CUT (ZONE 500) · airframe 64,200 hrs · 38,631 cycles
TWO ELONGATED HOLES ON AFT STRAKE FAIRING AT WINGLET SCIMITAR LT. REPAIRED AFT STRAKE FAIRING AT WINGLET SCIMITAR LT IAW SRM 51-70-04-2R-9 REPAIR 9.
Part: WEB — DAMAGED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
ELONGATED HOLE ON WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STRG 26L ON FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STRG 26L ON FWD CARGO BAY IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7505; SHEET 81 REV -
Part: RIB — CRACKED (ZONE 800) · airframe 64,200 hrs · 38,631 cycles
CRACK LEADING EDGE RIB LOC LE STA 95.96 AT LT HORIZONTAL STAB. REPLACED RIB AND FASTENERS LOC LE STA 95.96 AT LT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND DWG 186A1303, SHEET 1, REV A, & DWG 186A1001, SHEET 19, REV-.
Part: RIB — CRACKED (ZONE 300) · airframe 64,200 hrs · 38,631 cycles
CRACK ON INSPAR RIB LOWER CHORD LOCATED ON STAB STA 120.30 AND 36 INCHES FROM FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB 120.30 AT 36 INCHES FROM FRONT SPAR AT LT HORIZONTAL STAB IAW SRM 55-10-09-2R-5. REPAIR 5.
Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 64,200 hrs · 38,631 cycles
CRACKED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 500D, STR 28L AT FWD CARGO BAY. REPLACED SUPPORT ANGLE LOCATED AFT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7902 SHEET 126 REV A.
Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK ON CARGO TRACK LOCATED BS 767 LBL 17.24 WL 156.1 AT AFT CARGO BAY. PERFORMED PERMANENT REPAIR LOCATED BETWEEN BS 747 MORE 5 INCH TO BS 767 MORE 15 INCH LBL 17.24 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3; REPAIR 3<BR>SEE INDIVIDUAL SIGN OF BELOW.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 787 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR LOC BTW BS727E MORE 10 INCH TO BS847 AND (CLIP) SIDE PLATE (1E/A) LOCATED BTW STA 767 TO STA 787 LBL22 AND WL156 AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-5 REPAIR 5.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CORROSION ON SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 RBL 22 WL 156.1 AT AFT CARGO BAY. REPLACED SUPPORT ZEE LOCATED WL156 BTW BS727 TO BS767 AND RBL22 WL 156.1 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 146A7500, SHEET 85, REV A.
Part: STRINGER — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACKED STRINGER 23R, BS 540 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 23R LOCATED BS 500D TO BS 540 IAW SRM 53-00-03?2R-1, REPAIR 1.
Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACKED SUPPORT BRACKET, BS 540 AIR CONDITIONING BAY LT SIDE. INSPECTED AND REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY IAW DWG 212A1101, SHEET 3, REV - AND SOPM 20-50-00.
Part: ACCESS PANEL — DELAMINATED (ZONE 300 ELEV) · airframe 64,200 hrs · 38,631 cycles
DELAMINATED ELEVATOR ACCESS PANEL 334GT ON LT ELEVATOR. REPAIRED ACCESS PANEL 334GT ON LT ELEVATOR IAW SRM 55-20-01-2R-4 REPAIR 4 AND SRM 51-70-04-2R-10, REPAIR 10.
Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
DELAMINATED ACCESS PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCES PANEL 194CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-2, REPAIR 2.
Part: FRAME — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK INDICATION ON FRAME WEB SURFACE AROUND FASTENER LOCATED AT BS 328 BETWEEN S-20R TO S-21R IN AVIONIC BAY. REPAIRED WITH THE REPLACEMENT OF FRAME AND STRAP LOCATED AT BS 328 BETWEEN S-19R TO S-27R IN AVIONIC COMPARTMENT IAW EA 26-153-01437-WIP1 AND EA 26-153-01437.
Part: TIE CLIP — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK TIE CLIP LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 500D AND STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DRAWING 143A1221 SHEET 45 REV: -.
Part: WEB — ELONGATED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
ELONGATED HOLES ON SHIELD WEB BTW STA 492.4 TO STA 500A STR 26R AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB BTW STA 492.4 TO STA 500A STR 26R AT FWD CARGO COMPARTMENT I.A.W SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV. -.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACK ON INTERCOSTAL LOCATED BTW BS 685 - 706, STR 14L. REPLACED INTERCOSTAL LOCATED BTW BS 685 TO BS 706 AT LEVEL STR 14L AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 144A7500 SHEET 6 REV. A.
Part: STIFFENER — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACKED ON STIFFENER LOCATED FWD FACE BULKHEAD BS 540 LBL 24.75 AT FWD CARGO BAY. REPLACED STIFFENER LOCATED AT FWD FACE BULKHEAD BS 540 LBL 24.75 AT FWD CARGO COMPARTMENT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02-0G-0, AND DWG 111A6000, SHEET 245, REV- AND DWG 111A2001, SHEET 77, REV-. <
Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CORROSION SUPPORT ZEE LOCATED BTW BS 480 - 500D, STR 26L, WL 157 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BTW BS 480 - 500D, STR 26L, WL 157 IAW SRM 53-00-53-2R-6, REPAIR 6, AND DWG 143A7500, SHEET 58, REV-.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 867 RBL 54 AT AFT CARGO COMPARTMENT. REPLACED ANGLE LINER SUPPORT LOCATED BTW BS847 TO BS 887+13? RBL 54 AT AFT CARGO COMPARTMENT I.A.W SRM 51-40-02 AND DWG 149A9490 SHEET 21 REV. -
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL 52 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL 52 AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0.
Part: SUPPORT ANGLE — ELONGATED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
ELONGATED HOLE ON CARGO LINER SUPPORT ANGLE LOCATED BS 947.5 RBL 41 AT AFT CARGO BAY. REPLACED ANGLE LINER SUPPORT AND FASTENERS LOCATED BTW BS887+13 TO 947.5 RBL 41 AT AFT CARGO BAY IAW SRM 51-40-02 AND DWG 149A9490 SHEET 23 REV. A.
Part: RIB — CRACKED (ZONE 300) · airframe 64,200 hrs · 38,631 cycles
CRACKED INSPAR RIB, STAB STA 120.30 AND 28 INCHES FROM FRONT SPAR, RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB 120.30 AT 28 INCHES FROM FRONT SPAR AT LT HORIZONTAL STAB IAW SRM 55-10-09-2R-5. REPAIR 5.
Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACKED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE AND FASTENERS LOCATED BS 294.5 AT LEVEL STR 13L AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02-0G-0, AND DWG 141A1311, SHEET 1, REV C.
Part: GUSSET — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACKED GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D STR 19L AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 174; REV - .
Part: ANGLE — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACKED GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D AT STR 19R AT FWD CARGO BAY IAW SRM 51-10-01, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 174, REV -.
Part: ANGLE — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 21L AT FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS LOCATED BS 500D AT LEVEL STR 21L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 174, REV-, AND DWG 143A9481, SHEET 2, REV A.
Part: STRINGER — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACKED STRINGER 15L BTW BS 294.5 - BS 303.9 IN FWD GALLEY AREA. PERFORMED PERMANENT REPAIR LOCATED ON STR 15L BETWEEN BS 277 MORE 10 INCHES TO BS 294.5 AT FWD GALLEY AREA IAW SRM 53-00-03-2R-1. REPAIR 1.
Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACK ON SUPPORT ANGLE LOCATED FWD FACE BS 695 BL 0 WL 208.1 REPLACED SUPPORT ANGLE AND FASTENERS LOCATED FWD FACE BS 695 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 273A9110, SHEET 6, REV A.
Part: ANGLE — CRACKED (ZONE 100) · airframe 64,200 hrs · 38,631 cycles
CRACK ON ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS LOCATED FWD FACE BS 500C AT LEVEL STR 26L IAW SRM 51-40-02-0G-0 AND DWG 143A7505; SHEET 82; REV.-.
Part: TIE CLIP — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS, BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0; DWG 141A1110 SHEET: 18 REV: - AND DWG 141A8380, SHEET: 21 REV:-.
Part: STUB FRAME — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BETWEEN S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.250 IN. APPROX.AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED ON BS 296.5 BETWEEN STR 7R AND STR 9R UPPER POSITION AT FWD GALLEY AREA IAW SRM 51-40-02 AND DWG 141A8370 SHEET 9 AND SHEET 11, REV D.
Part: HANDLE — DETERIORATED (ZONE 800) · airframe 64,200 hrs · 38,631 cycles
DETERIORATED WASHER ASSISST HANDLE FWD ENTRY DOOR LINING. REPLACED WASHER ASSIST HANDLE FWD ENTRY DOOR LINING IAW AMM 52-11-31-400-802 STEP 3.G. ITEM (2)(B).
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABI IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A0060; SHEET: 46; REV - .
Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 64,200 hrs · 38,631 cycles
CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN I.A.W B737-700 SRM 53-40-51-2R-2 REPAIR 2; SRM 51-40-02.
Part: ENGINE — FIRE (NR 2) · airframe 64,070 hrs · 38,543 cycles
WHILE TAXING FOR T/O ACFT BEHIND STATED FLAMES COMING OUT OF THE NR 2 ENGINE. ALL ENGINE PARAMETERS NORMAL. CFR FIRE, RESCUE DID NOT OBSERVE ANY FLAMES OR SMOKE. WHILE TAXING FOR T/O AC BEHIND STATED FLAMES COMING OUT OF THE NR 2 ENGINE. ALL ENGINE PARAMETERS NORMAL. CFR FIRE / RESCUE DID NOT OBSERVE ANY FLAMES OR SMOKE. PERFORMED FIM TASK 71-05 TASK 811. NO DEFECTS NOTED. PERFORMED ENGINE RUN. OK TO CONTINUE SERVICE.
Earlier reports · 2008–2025 · 221 reports
2025
Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 62,383 hrs · 37,385 cycles
L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 62,383 hrs · 37,385 cycles
LEFT FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,383 hrs · 37,385 cycles
ENTRY DOOR L-1 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP PER M/M 33-51-04.
Part: BATTERY PACK — FAILED (ZONE 200) · airframe 62,383 hrs · 37,385 cycles
R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
Part: ENGINE — BIRD INGESTION (NR 1) · airframe 60,345 hrs · 36,102 cycles
INGESTED BIRD ON #1 ENGINE ON FINAL APPROACH . IMEDIATELY SMELLED IN CABIN AND COCKPIT. FELT A VIBRATION ON LEFT SIDE BUT ALL ENGINE PARAMETERS NORMAL. REDUCED POWER + UNEVENTFUL LANDING.<[01] C/W BIRD STRIKE CONDITIONAL INSP PER AMM 05-51-18 PREFORMED BIRD STRIKE VISUAL INSPECTION PER MT 772-00-00 AND COMPLIED WITH BORESCOPE INSP PER MT 772-00-02 REF TTG8Q00YKTDS & TTG8Q00YKTZY NO DEFECTS NOTED.
2024
Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 59,930 hrs · 35,828 cycles
FWD CARGO COMPARTMENT AC DISTRIBUTION BAY CABIN FLOOR SUPPORT CRACKED AT FWD AND AFT INBD FASTENERS LOCATED R/H OF BASELINE 0 STATION 540<[01] R&R FWD CARGO COMPARTMENT A/C DISTRIBUTION BAY CABIN FLOOR SUPPORT (INTERCOSTAL) LOCATED R/H OF BASLINE 0 STA 540 IAW SRM 51-40-02.
Part: SLIDE — DISLODGED (ZONE 800) · airframe 59,393 hrs · 35,489 cycles
SLIDE POPPED OUT OF PLACE R1 DOOR<[01] REINSTALLED SLIDE AT R1 DOOR PER MT 725-61-06
Part: TRANSMITTER — INOPERATIVE (ZONE 100) · airframe 58,892 hrs · 35,181 cycles
DURING CONFIGURATION FOR LDG FLAPS INDICATE 25* WITH 30* SELECTED. RAN QRH AND LANDED; AFTER LANDING FLAPS INDICATED 30*<[01] R&R L/H T/E FLAP POSITION TRANSMITTER REFERENCE MM 27-58-01.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,479 hrs · 34,921 cycles
EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672; M1673; AND M1674 ARE INOP. EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672 M1673 AND M1674 ARE INOP.<[01] REMOVED; REPLACED WITH SERVICEABLE UNITS AND PERFORMED GOOD INSTALLATION TEST OF M1672; M1673; M1674 EMERGENCY BATTERY PACKS IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1
Part: FLOOR SUPPORT — CRACKED (BS 295 LBL53) · airframe 58,479 hrs · 34,921 cycles
INTER COSTAL CRACKED ON FED CUTOUT AT BS 294.5 LBL 53 WL 283<[01] UPON INVESTIGATION FOUND INTERCOSTAL CRACKED ON FED CUTOUT AT BS 294.5 LBL 53 WL 216;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED AND REPLACED INTERCOSTAL ON FED CUTOUT AT BS 294.5 TO BS 303 LBL 53 STR 16-L PER SRM 51-40-02-0G-0 AND BOEING DWG 141A8180.;[04] VERIFIED COMPLETION CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
Part: FLOOR SUPPORT — CRACKED (BS 827-847 LBL22) · airframe 58,479 hrs · 34,921 cycles
ACB INTERCOSTAL CRACKED AT BS827-BS847; LBL 22; WL 156.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS827-BS847; LBL 22; WL 156 IAW BOEING DWG 146A7502 AND SRM 51-40-02
Part: DOOR FRAME — CRACKED (BS 312) · airframe 58,479 hrs · 34,921 cycles
FRAME CRACKED ON FED CUTOUT AT BS 312 LBL 53 WL 216 ; BELOW S-5L.<[01] UPON INVESTIGATION FOUND FRAME CRACKED ON FED CUTOUT AT BS 312 LBL 53 WL 283 ; BELOW S-5L.;[02] VERIFIED CORRECTIVE ACTION #1;[03] UPDATED MEASUREMENTS TABLE.;[04] WORK WILL BE COMPLETED ON CUSTOMER CARD NO. TTG8Q00TRGMN.;[05] VERIFIED CORRECTIVE ACTION STEP 4.
Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 58,479 hrs · 34,921 cycles
PANEL 193CL HAS AN ELONGATED FASTENER HOLE.<[01] ELONGATED FASTENER HOLE ON PANEL 193CL HAS BEEN REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
Part: FLOOR SUPPORT — CRACKED (BS 907-927) · airframe 58,479 hrs · 34,921 cycles
CRACKS FOUND AROUND FASTENERS ON 2 INTERCOASTALS ON FLOOR STRUCTURE BETWEEN RBL 13 TO RBL 8; BS 907-927; WL 156.<[01] UPON FURTHER INVESTIGATION NO ALLOWABLE DAMAGE FOUND PER SRM; REPAIR BY REPLACEMENT OF PARTS. REMOVED AND REPLACED 2EA INTERCOSTALS BETWEEN RBL 13 TO RBL 8; BS 907-927 IAW BOEING DWG 147A7221 AND SRM 51-40-02;[02] VERIFIED
Part: SIDEWALL SUPPORT — CORRODED (BS 727D-767) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-767; RBL 21; WL 156.<[01] REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-767; RBL 21; WL 156 PER SRM 51-40-02-0G-0; SRM 53-00-53-1A-2 & BOEING DWG 146A7502; AMM 51-21-72-370-804.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
Part: SHIELD — CORRODED (BS 847) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON AFT CARGO DOOR SHIELD BS 847+8; RBL 21; WL 156<[01] REPLACED AFT CARGO DOOR SHIELD BS 847+8; RBL 21; WL 156 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-00; DWG 146A0081; APPLIED WHITE ENAMEL TOPCOAT AND CIC PER AMM 51-21-73-370-804; AMM 51-21-91-620-802.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
Part: SIDEWALL SUPPORT — CORRODED (BS 727D-787) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-787; LBL 21; WL 156.<[01] REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D-787; LBL 21; WL 156 PER SRM 51-40-02-0G-0; SRM 53-60-53-0I-2; SRM 53-00-53-1A-2; SRM 51-40-05-0G-09; SRM 53-00-53-2R-5; DWG 146A7500; REV A; SOPM 20-43-03; AMM 51-21-72-370-804.;[02] EDITED TABLE;[03] VERIFIED;[04] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
Part: DOUBLER — CRACKED (BS 663 BULKHEAD) · airframe 58,479 hrs · 34,921 cycles
UPON REMOVING L/H VAPOR BARRIER BS 663 FOUND DOUBLER P/N 111A1511-27 CRACKED AT LBL 26 DOUBLER LBL 6 TO LBL 31`FWD SIDE BS 663 CRACKED AT LBL 26<[01] FABRICATED DOUBLER FRON 2024-T3 0.040 LOT; 1564200-1 IAW DWG 111A1511 AND SRM 51-30-01-0G-0 APLIED CHEMICALL CONVERSION AND PRIMER IAW SOPM 20-43-03 AND SRM 51-21-01 <BR>DOUBLER GONIG TO BE INSTALL ON W/C TTG8Q00TLP82 STEP 5
Part: SILL DRAIN — CORRODED (BS 807-827 RBL23) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON AFT CARGO LOWER DOOR SILL BS 807-827; RBL 23; WL 156<[01] REMOVED AFT CARGO LOWER DOOR SILL IAW SRM 51-40-02<BR><BR>LOCATED AND DRILLED NEW AFT CARGO LOWER DOOR SILL IAW SRM 51-40-05 AND DWG 146A8340;[02] REMOVED AND REPLACED ACB LOWER DOOR SILL (SUB-THRESHOLD WEB) IAW SRM 51-40-02 AND DWG 146A8340;[03] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
Part: FORMER — CRACKED (FAIRING) · airframe 58,479 hrs · 34,921 cycles
LEFT WING FAIRING FORMER CRACKED; BS500D; BETWEEN STR 18/19 6-INCH O/B OF FUSELAGE SKIN; I/B UPPER CORNER OF FIXED L/E SKIN (MARKED)<[01] REMOVED CRACKED FAIRING FORMER (FRAME) PER SRM 51-40-02;[02] REMOVED AND REPLACED LEFT WING FAIRING FORMER P/N:116A318- AT BS 500D BETWEEN STR 18 TO STR 19 ; 6 INCH O/B OF FUSELAGE SKIN PER SRM 51-40-2 AND DWG:116A3010;REV:D.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
Part: SEAT TRACK — CORRODED (BS 707) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON SEAT TRACK CROWN BS 707+10; RBL 25; WL 208. CORROSION ON SEAT TRACK CROWN & WELL BS 707+10 LBL 25 WL 208<
Part: SEAT TRACK — CORRODED (BS 827-867) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON SEAT TRACK WELL BS 867-7; BS 827-2 CROWN; RBL 45; WL 208.<[01] COMPLETED STEP 2 AND 4.;[02] REMOVED AND REPLACED CABIN SEAT TRACK SRM PER SRM 53-00-52-1A-A AND DWG:146A5300.;[03] VERIFIED CORRECTIVE ACTION #2
Part: SEAT TRACK — CORRODED (BS 867) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON SEAT TRACK WELL BS 867-7; RBL 45; WL 208.<
Part: WEB — CRACKED (RT WING) · airframe 58,479 hrs · 34,921 cycles
R/W T/E UPPER SURFACE PANEL AT ORSS 280 LOWER TRANSVERSE WEB CRACKED AT O/B UPPER FASTENER<[01] REMOVED AND REPLACED TRANSVERSE WEB AT R/W T/E UPPER SURFACE PANEL AT ORSS 280 IAW SRM 51-40-02 0G-0 PARA. 4.;[02] VERIFIED CORRECTIVE ACTION #1
Part: SILL DRAIN — CORRODED (BS 321-328) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON FSD MOP SILL BS321 - BS328 RBL58 WL208.<[01] REMOVED AND REPLACED FOR CORROSION MOP SILL SRM 53-10-15-1A-2 BS321 - BS328 RBL58 WL208.AND INTALATION MOP SILL FSD IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0 AND DWG #141A8310 REV-;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
Part: FLOOR SUPPORT — CRACKED (BS 349 RBL 11) · airframe 58,479 hrs · 34,921 cycles
CRACKED INTERCOSTAL AT FWD WET AREA BS349 RBL11 WL208.<[01] REMOVED AND REPLACED FWD WET AREA INTERCOSTAL BS349; RBL11;WL208 PER SRM 51-40-02.;[02] CHANGED MEASUREMENT TABLE TO MATCH DAMAGE.; VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
Part: FLOORBEAM — CORRODED (BS 986) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL43 WL208.<[01] UPDATED STEPS;[02] STEP 4 PARTIAL UPDATE.;[03] STEP 9 UPDATE;[04] APPLY CHEMICAL CONVERSION AND PRIMER TO REPAIR PARTS AND STRUCTURE CUTOUT AREA.;[05] STEP 8 COMPLETE.;[06] UPDATED STEPS 8;10;[07] UPDATE STEPS 10;11;[08] JOB SUMMARY: FLOORBEAM 986 AT LBL43 WAS CORRODED AT NUTPLATE AT LBL43 WL208 AND OUT OF LIMITS. IT WAS REPAIRED IAW SRM 53-70-51-2R-6 REPAIR 6 FIG 205; ALTERNATIVE 4 AND FINAL FINISH APPLIED.;[09] FAULT COMPLETE;[10] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
Part: WEB — CORRODED (BS 1020) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON WEB AT AFT WET AREA BS1020 LBL17; BS1026 LBL18; BS1026 LBL20. WL208. MARKED<[01] UPDATED MEASUREMENTS TABLE EXCEPT ITEM ITEMS 20 AND 21.;[02] UPDATED MEASUREMENT TABLE;[03] REPAIRED CORROSION ON WEB AT AFT WET AREA BS1020 LBL17; BS1026 LBL18; BS1026 LBL20. WL208. IAW EA. 24-153-01459;[04] VERIFIED CORRECTIVE ACTION ENTRIES 1-3 WITH STEPS 1-3.
Part: SUPPORT ANGLE — CORRODED (BS 305-324) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON FSD THRESHOLD SUPPORT BS305 - BS324 RBL59 WL208.<[01] VERIFIED CORRECTIVE ACTION ON STEP 1;[02] CORROSION ON FSD THRESHOLD SUPPORT BS 304-324 RBL 59; WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-2 REMOVED AND REPLACED FSD THRESHOLD SUPPORT ANGLE IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 141A8310 REV-. ALL OTHER FASTENERS TO BE INSTALLED UPON FSD MOP SILL INSTALLATION.;[03] UPDATED PARTS.;[04] VERIFIED COMPLETION CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.
Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,479 hrs · 34,921 cycles
FWD FLOOR PANEL 221BF UPPER SKIN HAS AREA OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREA OF PULLED STRANDS WAS REPLACED ON FAULT TTG8Q00TJADR.;[02] JOB COMPLETE.
Part: FLOOR SUPPORT — CRACKED (BS 349 LBL11) · airframe 58,479 hrs · 34,921 cycles
CRACKED INTERCOSTAL AT FWD WET AREA BS349 LBL11 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BS349 LBL11 WL208 IAW DWG 141A5400; SRM 51-40-05 AND SRM 51-40-02;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 58,479 hrs · 34,921 cycles
R/H HORIZONTAL STAB REMOVABLE L/E 341B RIB #3 IS CRACKED<[01] TASK COMPLETE:<BR>REMOVED CRACKED #3 RIB IAW SRM 51-40-02-0G-0. RECEIVED NEW RIB (PN: 186A1303-2 LOT: 1565504-1) AND INSTALLED IAW SRM 51-40-02-0G-0.;[02] VERIFIED;[03] VERIFIED
Part: ATTACH ANGLE — CRACKED (BS 312 RBL54) · airframe 58,479 hrs · 34,921 cycles
CRACKED ATTACH ANGLE AT FWD WET AREA BS312 RBL54 WL208.<[01] UPON FURTHER INVESTIGATION FOUND ANGLE CRACKED AT FWD WET AREA BETWEEN BS 291.5 TO 295.5 RBL254 WL208.;[02] UPON FURTHER INVESTIGATION FOUND ANGLE CRACKED AT FWD WET AREA BETWEEN BS 291.5 TO 295.5 RBL 54 WL208.;[03] REMOVED AND REPLACED ATTACH ANGLE AT FWD WET AREA BETWEEN BS291.5 TO 295.5 RBL 54 WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 1418310.;[04] VERIFIED COMPLETION CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
Part: SILL DRAIN — CORRODED (BS 303-312) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON FED MOP SILL BS303; BS312 LBL57 WL208.<[01] UPDATED STEP 1;[02] REMOVED AND REPLACED FED MOP SILL IAW BOEING DWG 143A5900; 141A8110; 140A9810 AND SRM 51-40-02 AND SRM 51-40-05;[03] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
Part: STRAP — CORRODED (BS 1028) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON TENSION STRAP AT AFT WET AREA BS1028 RBL18 WL208.<[01] CORROSION ON TENSION STRAP BS 1028; RBL 18; WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS GIVEN IN SRM. REMOVED EXISTING STRAP; LOCATED; DRILLED; COUNTERSUNK; DEBURRED; AND INSTALLED NEW STRAP PER SRM 51-40-02; SRM 51-40-05; SRM 51-40-08; AND DWG# 147A5730 REV C.;[02] UPDATED MEASUREMENT TABLE.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1-2 AND MEASUREMENT TABLE.
Part: WEB — CORRODED (BS 1016) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON 1016 WEB AT AFT WET AREA LBL9 - LBL14 WL208.<[01] UPDATED MEASUREMENTS TABLE EXCEPT ITEMS 20 AND 21.;[02] REFER TO FAULT TTG8Q00TJSCF WHERE EA 24-153-01459 WAS ADDED AS A SUBTASK.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.<BR>REFER TO FAULT TTG8Q00TJSCF WHERE EA 24-153-01459
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 58,479 hrs · 34,921 cycles
RIGHT HORIZONTAL STABILIZER RIB AT STAB STA 101.90 IS CRACKED AT 3RD STIFFNER FROM FORWARD<[01] REPAIRED RIGHT HORIZONTAL STABILIZER RIB AT STAB STA 101.90; 3RD STIFFNER IAW SRM 51-40-02-0G-0 AND SRM 55-10-09-2R-4 REPAIR 4; FIG. 202.;[02] VERIFIED CORRECTIVE ACTION AND MEASUREMENT TABLE COMPLETED
Part: FLOORBEAM — CORRODED (BS 986) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL43 WL208.<[01] STEP 4 UPDATE;[02] STEP 9 UPDATE;[03] EDIT TO STEP 10;[04] CERTIFY EDIT TO STEP 10.;[05] UPDATED STEPS 8;10;[06] STEPS 10;11;[07] PARTIAL UPDATE STEP #11;[08] ADDITIONAL EDIT TO STEP #11;[09] CERTIFY ACTIONS 7;8;[10] JOB SUMMARY: 986 FLOOR BEAM AT RBL43 AND RBL40 WERE OUT OF LIMITS. REPAIRED THE FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6. ALL FASTENERS HAVE BEEN INSTALLED AND FINAL FINISHES APPLIED.;[11] CHANGED MEASUREMENT TABLE TO MAJOR REPAIR; UPDATED REMAINING THICKNESS; AND ADDED ORIGINAL THICKNESS TO STEP 2.;[12] VERIFIED COMPLETION CORRECTIVE ACTION 10-11 AND MEASUREMENT TABLE.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 58,479 hrs · 34,921 cycles
FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FORWARD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] JOB COMPLETE.
Part: ATTACH ANGLE — WORN (LT WING FAIRING) · airframe 58,479 hrs · 34,921 cycles
L/W FLAP TRACK AFT FAIRING 542BB AFT ATTACH BEAM AND ADJUST LINK ARE WORN<[01] REMOVED AND REPLACED L/W FLAP TRACK AFT FAIRING 542BB AFT ADJUST LINK AND ATTACH IAW AMM 27-51-18-400-802 STEPS 5.G.(1).<BR>CAL TOOL ID ATS2099 D/D 09/2024
Part: SILL DRAIN — CORRODED (BS 954-993) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON ASD MOP SILL BS954 - BS993 RBL48 WL208.<[01] UPDATED MEASUREMENT TABLE.;[02] REMOVED AND REPLACED ASD MOP SILL FROM BS 893 TO 1006; RBL 48 WL 208 PER SRM 51-40-02 AND DWG 147A8501;[03] VERIFIED COMPLETION CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 58,479 hrs · 34,921 cycles
FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
Part: FLOOR SUPPORT — CRACKED (BS 284 BL 0) · airframe 58,479 hrs · 34,921 cycles
CRACKED INTERCOSTAL AT FWD WET AREA BS284 BL0 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS284; BL0 WL208 PER SRM 51-40-02.;[02] CHANGED MEASUREMENT TABLE TO MATCH DAMAGE.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
Part: SUPPORT ANGLE — CORRODED (BS 313-338) · airframe 58,479 hrs · 34,921 cycles
CORROSION ON FED THRESHOLD SUPPORT ANGLE BS313 - BS338 LBL58 WL208.<[01] UPDATED STEP 1;[02] REMOVED AND REPLACED FED THRESHOLD SUPPORT ANGLE AT BS 312 TO BS 344 LBL 58 WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A8110.;[03] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
Part: FLOOR SUPPORT — CRACKED (BS 318 RBL30) · airframe 58,479 hrs · 34,921 cycles
CRACKED INTERCOSTAL AT FWD WET AREA BS318 RBL30 WL208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS318; RBL30; WL208 PER SRM 51-40-02.;[02] CHANGED MEASUREMENT TABLE TO MATCH DAMAGE.;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
Part: FLOORBOARD — PULLED (ZN 200 FUS TOP) · airframe 58,479 hrs · 34,921 cycles
PASSENGER FLOORBOARD 241AF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] FABRICATION OF NEW 241AF FLOORBOARD HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0. AND BOEING DWG: 144A5810 ID: 0127.;[02] VERIFIED CORRECTIVE ACTION 1
Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 58,479 hrs · 34,921 cycles
PASSENGER FLOORBOARD 241DF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] FABRICATION OF NEW 241DF FLOORBOARD HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0128.;[02] VERIFIED
Part: FLOORBOARD — PULLED (CABIN) · airframe 58,479 hrs · 34,921 cycles
PASSENGER FLOORBOARD 232SF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] FABRICATION OF NEW 232SF FLOORBOARD HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.;[02] VERIFIED JOB COMPLETE
Part: FLOORBOARD — PULLED (ZN 200 FUS TOP) · airframe 58,479 hrs · 34,921 cycles
PASSENGER FLOORBOARD 242AF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] FABRICATION OF NEW 242AF FLOORBOARD HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 58,479 hrs · 34,921 cycles
BS663 VAPOR BARRIER IS CRACKED AT WL 164; RBL 40.<[01] R//H B.S. 663 VAPOR BARRIER CRACKS WILL BE REPAIRED ON FAULT TTG8Q00TGL0Z;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 58,479 hrs · 34,921 cycles
PASSENGER FLOORBOARD 241BF HAS NUMEROUS PULLED FIBERGLASS STRANDS AND WARNING PLACARD P/N BAC27DCA854 IS DAMAGED.<[01] FABRICATION OF NEW 241BF FLOORBOARD HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 58,479 hrs · 34,921 cycles
CRACKS NOTED ON THE R/H B.S. 663 VAPOR BARRIER<[01] REPAIRED CRACK DAMAGE ON R/H B.S. 663 VAPOR BARRIER IAW SRM 51-70-04-2R-10.;[02] VERIFIED JOB COMPLETE
Part: BRACKET — CRACKED (RT WING) · airframe 58,460 hrs · 34,909 cycles
RIGHT WING I/B UPR ACCESS PANEL SUPPORT FWD ATTACH BRACKET CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RIGHT WING I/B UPR ACCESS PANEL SUPPORT FWD ATTACH BRACKET IAW SRM 51-40-02.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 58,323 hrs · 34,824 cycles
FOUND 8 CRACK IN AFT CARGO FLOOR PANEL; AFT PANEL; BIN D.<[01] APPLIED FLOOR FIBER GLASS PATCH TO AFT CARGO; BIN ?D? AFT FLOOR PANEL PER AMM 25-52-01.
Part: ISOLATION MOUNT — CRACKED (SLIDE MOUNT) · airframe 57,949 hrs · 34,605 cycles
AFT GALLEY SERVICE DOOR SLIDE FWD MOUNT ISOLATOR CRACKED.<[01] R&R AFT GALLEY SERVICE DOOR SLIDE FWD MOUNT ISOLATOR IAW SRM 51-40-02.
2023
Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 55,959 hrs · 33,378 cycles
EXTERIOR EMERGENCY LIGHT INOP AFT OF FWD ENTRY DOOR<[01] RELAMPED EMERGENCY LIGHT AFT OF FWD ENTRY DOOR PER AMM 33-51-04.
Part: SIGN — MISSING (ZN 200 FUS TOP) · airframe 55,856 hrs · 33,316 cycles
EXIT SIGN IN AFT GALLEY IS MISSING.<[01] REMOVED AND REPLACED R2 DOOR EMERGENCY LIGHT ASSY IAW AMM 33-51-01.
Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 55,197 hrs · 32,917 cycles
AFT SERVICE DOOR SLIDE PARTIALLY DEPLOYED<[01] REPACKED AFT SERVICE DOOR SLIDE PER SLIDE MT#725-61-06.
Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 54,316 hrs · 32,338 cycles
23CBA AREA EMERGENCY LIGHT INOP<[01] RELAMPED 23CBA AREA EMERGENCY LIGHT IAW AMM 33-51-03. OPS CHECK GOOD @ THIS TIME.
Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 54,249 hrs · 32,299 cycles
R1 GRIT BAR RETAINING CLIP MISSING<[01] INSPECTED GIRT BAR AND FOUND TO BE SERVICEABLE PER SIP;AIRCRAFT OK FOR CONTINUED SERVICE.;[02] EDIT FROM SIP TO PER AMM 25-66-01
2022
Part: COVER — LOOSE (SLIDE GUAGE) · airframe 53,999 hrs · 32,131 cycles
FWD ENTRY DOOR SLIDE COVER PLASTIC GAUGE COVER IS LOOSE. SECURED THE FWD ENTRY DOOR SLIDE CLEAR PLASTIC COVER IAW SIP.
Part: GIRT BAR — OUT OF POSITION (FWD SERVICE DOOR) · airframe 53,109 hrs · 31,538 cycles
FWD SERVICE DOOR GIRT BAR FELL WHILE DOOR BEING OPENED. SLIDE IS OUT OF CONTAINER BUT NOT DEPLOYED. / [01] REINSTALLED FWD SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01 & MT 725-240- 00-00
Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 52,920 hrs · 31,399 cycles
1 EA BULB INOP ON EMERGENCY EXIT SIGN ABOVE FLIGHT DECK DOOR / [01] RELAMPED EMERGENCY EXIT SIGN ABOVE FLIGHT DECK 1 EA BULB AS PER B737 AMM 33-51-01-960-801. TEST OK;[02] VERIFIED STEP 1.
Part: GIRT BAR — OUT OF POSITION (R2 DOOR) · airframe 52,920 hrs · 31,399 cycles
R2 DOOR SLIDE GIRT HITS SCUFF PLATE WHEN DOOR IS CLOSING. / [01] INSTALLED CORRECTLY R2 DOOR SLIDE GIRT IN REF. AMM 25-66-01-400-803.;[02] VERIFIED STEP 1
Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 52,920 hrs · 31,399 cycles
L2 DOOR SLIDE GIRT HITS SCUFF PLATE WHEN DOOR IS CLOSING. / [01] INSTALLED CORRECTLY L2 DOOR SLIDE GIRT IN REF. AMM 25-66-01-400-803.;[02] VERIFIED STEP 1
Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 52,920 hrs · 31,399 cycles
L/H FWD EMERGENCY OVERWING EXIT DOOR LIGHT INOP. / [01] RELAMPED L/H FWD EMERGENCY OVERWING EXIT DOOR LIGHT AS PER REF B737 AMM 33-51-01-960-801. TEST OK.;[02] VERIFIED STEP 1.
Part: LIGHT — BROKEN (PAX CABIN) · airframe 52,920 hrs · 31,399 cycles
RIGHT EMERGENCY EXIT DOOR BOTTOM SIGN INOP. SECURED LIGHT ASSEMBLY CONNECTOR FOR THE RT EMERGENCY EXIT DOOR BOTTOM SIGN IAW AMM 33-51-03-960-802. PERFORMED OPS CHECK AND FOUND NORMAL.
Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 52,920 hrs · 31,399 cycles
EMERGENCY LIGHT BIN 3 FED; 6 FED INOP<[01] RELAMPED EMERGENCY LIGHT BINS 3FED AND 6FED AS PER REF. AMM 33-51-03-960-801. PERFORMED OPS CHECK AND FOUND NORMAL.;[02] VERIFIED STEP 1
Part: SEAT TRACK — OUT OF TOLERANCE (FWD FUSELAGE) · airframe 52,920 hrs · 31,399 cycles
FLIGHT DECK CAPTAIN AFT I/B SEAT TRACK THE HOLES OUT OF LIMIT. / [01] REMOVED FLIGHT DECK CAPTAIN AFT I/B SEAT TRACK IAW B737 AMM 25-11-01-000-801;[02] VERIFIED STEP 1. OK TO INSTALL NEW TRACK.;[03] INSTALLED NEW FLIGHT DECK CAPTAIN AFT I/B SEAT TRACK AS PER B737 AMM 25-11-11-400-801 FIXTURE TRACK SETTING USED B/C 170026;[04] VERIFIED STEP 3.
Part: TRACK — OUT OF TOLERANCE (FWD FUSELAGE) · airframe 52,920 hrs · 31,399 cycles
FLIGHT DECK FIRST OFFICER AFT I/B SEAT TRACK THE HOLES OUT OF LIMIT. / [01] REMOVED FLIGHT DECK FIRST OFFICER AFT I/B TRACK AS PER B737 AMM 25-11-01-000-801;[02] VERIFIED STEP 1. OK TO INSTALL NEW TRACK.;[03] INSTALLED NEW FLIGHT DECK FIRST OFFICER AFT I/B TRACK AS PER B737 AMM 25-11-11-801; USED FIXTURE TRACK SETTING B/C170026;[04] VERIFIED STEP 3.
Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 52,920 hrs · 31,399 cycles
AFTER REMOVING LEFT HORIZONTAL STAB RIB # 5 FOUND 2 POSSIBLE CRACKS ON THE LOWER CHORD FWD OF STIFFENER #1. / [01] RFORMED HFEC INSP ON STIFENER 1 O/B SIDE LWR CHORD; IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166316. CALIB DUE 10-8-22. NO CRACKS FOUND.;[08] FABRICATED REPAIR ANGLE MATERIAL USED P/N:BAC 1490-2738 7075T6 PO#1244016;LOCATED AND DRILLED ALL REPAIR PARTS REF B737-700 SRM 55-10-09-2R-5 REPAIR 5 FIG 203;[22] INSTALLED REPAIR PARTS AT L/H HORIZONTAL STAB RIB #5 ON STIFFENER #1 REF B737-700 SRM 55-10-09-2R-5 REPIR 5 FIG 203;[23] CORRECTION FROM STEP 22:INSTALLED REPAIR PARTS AT L/H HORIZONTAL STAB RIB #5 ON STIFFENER #1 REF B737-700 SRM 55-10-09-2R-5 REPAIR 5 FIG 203;[24] VERIFIED AND INSPECTED STEP#23.;[25] INSPECTED.;[26] VERIFIED
Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 52,920 hrs · 31,399 cycles
FWD CARGO COMP LBL 21' BETWEEN STA 500 AND STA 500A BAFFLE CRACKED / [01] REMOVED & REPLACED BAFFLE P/N: 143A7510-15 AT FWD CARGO COMP LBL 21' BETWEEN STA 500 AND STA 500A; AS PER B737-7 SRM 51-40-02 & DWG. 143A7505.;[02] VERIFIED STEP 1
Part: ANGLE — CRACKED (CENTER WING) · airframe 52,920 hrs · 31,399 cycles
WING CENTER SECTION REAR SPAR LT VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED BS 663 WL 170 APROXIMATELY / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.343'<BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE- 10/22];[02] FORMED 2EA ANGLES (REPLACEMENT ANGLE & SPLICE ANGLE ) MAT: USED: 2024-T3 CLAD .063' & .O71' AS PER B737-700 SRM 57-10-10-2R-5 & 51-30-01;[03] REMOVED FASTENERS AT CENTER FUEL TANK SECTION REAR SPAR L/H VAPOR BARRIER UPPER ATTACH ANGLE BS 663 REF B737-700 SRM 51-40-02-0G-0;[04] PERFORMED FPI PER SOPM 20-20-02; ON FORMED ANGLES. NO CRACKS. TOOL USED B/C 12553;[05] CUT OUT DAMAGE SECTION OF ATTACH ANGLE AT LBL 15.00 AS PER B737-7 SRM 57-10-10-2R-5 REPAIR 5; FIG. 202 DETAIL 'D'.;[08] TRIMMED; LOCATED & DRILLED 2EA. FORMED ANGLES(REPLACEMENT ANGLE & SPLICE ANGLE); AT LT VAPOR BARRIER UPPER ATTACH ANGLE AREA AS PER B737-7 SRM 57-10-10 2R-5; FIG.202; DETAIL: 'D'.;[09] VERIFIED STEP 8;[10] OK TO TREAT AND PRIME;[11] TREATED & PRIMED 2EA. REPAIR ANGLES AS PER B737-7 SRM 51-20-01; & AMM 51-21-72-370-804.;[12] VALIDATED STEP 11<BR><BR>OK TO INSTALL NEW REPAIR PARTS;[13] CORRECTION TO STEP 12.<BR>RII<BR>VALIDATED STEP 11<BR>OK TO INSTALL NEW REPAIR PARTS;[14] LATE ENTRY. VERIFIED STEP 3;[15] PARTIALLY INSTALLED REPAIR ANGLE AND SPLICE AND CAP SEAL APPLIED ON HILOK HEADS REF. B737-700 SRM 57-10-10-2R-5 REPAIR 5 FIGURE 202. JOB ACCOMPLISHED BY JORGE LINDERO EMP. # 34913;
Part: DOUBLER — CRACKED (CENTER WING) · airframe 52,920 hrs · 31,399 cycles
RT VAPOR BARRIER WEB DOUBLER IS CRACKED; BS 663; WL 170; BETWEEN RBL 6.15 & RBL 31.83.(P/N: 111A1511-24). / [01] FABRICATED RT VAPOR BARRIER DOUBLER (P/N: 111A1511-24) AS PER DWG. 111A1511. MAT. USED: 2024-T4 0.040'.;[02] LOCATED & DRILLED NEW DOUBLER AS PER B737-7 SRM 51-40-05.;[03] VERIFIED STEPS 1 AND 2.;[04] OK TO TREAT AND PRIME.;[05] TREATED & PRIME NEW DOUBLER AS PER B737-7 SRM 51-20-01 & AMM 51-21-72-370-804.;[06] VERIFIED STEP 5;[07] TASK C/W;[08] TASK C/W
Part: BRACKET — CRACKED (CENTER WING) · airframe 52,920 hrs · 31,399 cycles
FOUND CRACKED BRACKET AT RT VAPOR BARRIER BS663; BETWEEN RBL 45 & RBL 55.(P/N:276A9183-2) / [01] REMOVED AND REPLACED BRACKET AT RT VAPOR BARRIER BS 663; BETWEEN RBL 45 AND RBL 55 (P/N: 276A9183-2) REF B 737-700 SRM 51-40-02 AND DRAWING 111A1000. WORK WAS ACCOMPLISHED BY TECHNICIAN JORGE L LINDERO EMPL # 34913;[02] VERIFIED STEP 1.
Part: TRACK — CORRODED (AFT CARGO) · airframe 52,920 hrs · 31,399 cycles
AFT CARGO COMP CARGO TRACK STA 947.5-5 RBL 15' UPPER SURFACE CORRECTION FOR ORIGINAL WRITE UP AFT CARGO COMP CARGO TRACK STA 947.5-5 RBL 15' UPPER SURFACE CORROSION / [01] FOUND EXFOLIATING CORROSION THAT IS OUT OF LIMITS; PART REQUIRES REPLACEMENT;[02] VERIFIED CORROSION OUT OF LIMITS;[03] PARTIALLY LOCATED AND DRILLED HOLES ON AFT CARGO TRACK STA 947.5 RBL 15' REF B 737-700 SRM 51-40-05. WORK WAS ACCOMPLISHED BY TECHNICIAN JORGE L LINDERO EMPL # 34913;[04] PARTIALLY LOCATED AND DRILLED HOLES ON AFT CARGO TRACK STA 947.5 RBL 15' REF B 737-700 SRM 51-40-05. WORK WAS ACCOMPLISHED BY TECHNICIAN JORGE L LINDERO EMPL # 34913;[05] FINALIZED LOCATING AND DRILLING HOLESON AFT CARGO TRACK STA 947.5 RBL 15' REF B 737-700 SRM 51-40-05. WORK WAS ACCOMPLISHED BY TECHNICIAN JORGE L LINDERO EMPL # 34913;[06] VERIFIED STEP 5;OK TO INSTALL AFT CARGO TRACK;[07] PARTIALLY INSTALLED AFT CARGO TRACK FROM STA 867 TO STA 947.5 REF B 737-700 SRM 51-40-02-0G-0. WORK WAS ACCOMPLISHED BY TECHNICIAN JORGE L LINDERO EMPL # 34913;[08] FINALIZED INSTALLATION OF AFT CARGO TRACK FROM STA 887 TO STA 947.5 REF B 737-700 RBL 15' SRM 51-40-02-0G-0 AND DWD 147A7501. WORK WAS ACCOMPLISHED BY TECHNICIAN JORGE L LINDERO EMPL # 34913[12] FINALIZED INSTALLATION OF AFT CARGO TRACK FROM STA 867 TO STA 947.5 RBL 15' REF B 737-700 SRM 51-40-02-0G-0 AND DWG 147A7501. WORK WAS ACCOMPLISHED BY TECHNICIAN JORGE L LINDERO EMPL # 34913
Part: ANGLE — CRACKED (CENTER WING) · airframe 52,920 hrs · 31,399 cycles
WING CENTER SECTION REAR SPAR RT VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED; BS 663; WL 170 APPROX. / [01] FORMED 2EA. ANGLES (REPLACEMENT ANGLE & SPLICE ANGLE) MAT. USED 2024-T3 CLAD 0.063' & 0.071'. AS PER B737-7 SRM 57-10-10-2R-5. & 51-30-01.;[28] REMOVED FASTENERS AT CENTER FUEL TANK SECTION REAR SPAR R/H VAPOR BARRIER UPPER ANGLE BS 663 REF B737-700 SRM 51-40-02-0G-0CUT OUT CRACK SECTION OF UPPER ATTACH ANGLE AT CENTER FUEL TANK SECTION REAR SPAR R/H VAPOR BARRIER BS 663 AND WL 170 APPROX. REF B737-700 57-10-10-2R-5 REPAIR 5 FIGURE 202PERFORMED HFEC INSP ON CUT OUT AREA IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23. FORMED 2EA. ANGLES (REPLACEMENT ANGLE & SPLICE ANGLE) MAT. USED 2024-T3 CLAD 0.063' & 0.071'. AS PER B737-7 SRM 57-10-10-2R-5. & 51-30-01.PERFORMED HFEC INSP. ON FORMED 2EA. ANGLES (REPLACEMENT ANGLE & SPLICE ANGLE) IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED TOOL: NORTEC 600 B/C: 166317 DUE: 10/20/22. INSTALLED REPAIR ANGLE AND SPLICE AT CENTER FUEL TANK SECTION REAR SPAR R/H VAPOR APPLIED CAP SEALANT AT RT VAPOR BARRIER UPPER ANGLE REPAIR FASTENER COLLARS INSIDE THE CENTER TANK; AS PER B737-7 SRM 51-80-01.BARRIER BS 663 REF B737-700 SRM 57-10-10-2R-5 REPAIR 5 FIG 202. APPLIED FILLET SEALANT AROUND THE EDGES OF THE REPAIR AS PER B737-7 SRM 51-20-05. APPLIED CIC TO THE REPAIR AREA AS PER B737-7 SRM 51-20-01.
Part: RIB DOUBLER — CRACKED (VERT. STAB.) · airframe 52,920 hrs · 31,399 cycles
DORSAL FIN STRUCTURE. FWD MOST RIB ASSY (STA 867) CRACKED AT TWO LOCATIONS (DOT 25-1). / [01] REMOVED CRACKED FWD RIB ASSY AT DORSAL FIN REF B737-700 ERM 51-40-02-0G-0;[02] VERIFIED STEP 1.;[03] OK TO INSTALL NEW RIB ASSY;[04] INSTALLED NEW DORSAL FIN FWD MOST RIB ASSEMBLY REF B 737-700 SRM 51-40-02-0G-0. WORK WAS ACCOMPLISHED BY TECHNICIAN JESUS HERNANDEZ EMPL # 1709;[05] VERIFIED STEP 4.
Part: BRACKET — CRACKED (AFT CARGO BAY) · airframe 52,920 hrs · 31,399 cycles
AFT CARGO COMP STA 867 LBL 10' BRACKET APPEARED CRACKED / [01] REMOVED AND REPLACED BRACKET AT AFT CARGO COMP STA.867 LBL 10' REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED AND INSPECTED STEP#1.
Part: TRACK — ELONGATED (AFT CARGO) · airframe 52,920 hrs · 31,399 cycles
AFT CARGO COMP STA 727A+9 RBL 13' CARGO TRACK HOLE ELONGATED / [01] RE-INSPECTED AFT CARGO TRACK RBL 13.84 FROM BS 727 TO BS 727D: FOUND 4 EA. ELONGATED FASTENER HOLES: #1 LOCATED BETWEEN BS 727 & 727A; MAX DIAMETER: 0.334'; HOLE #2: LOCATED BETWEEN BS 727A & 727B; MAX. DIA.: 0.297'; HOLE #3: LOCATED BETWEEN BS 727B & 727C; MAX. DIA.: 0.225'; & HOLE #4 : LOCATED BETWEEN BS 727C & 727D; DIA.: 0.234'; FOUND OUT OF LIMITS AS PER B737-7 SRM 53-00-53-1A-2.;[14] INSTALLED AFT CARGO TRACK FROM STA 727 TO STA 887 RBL 13.8' WL 156 REF B 737-700 SRM 51-40-02-0G-0 AND DWD 146A7501. WORK WAS ACCOMPLISHED BY TECHNICIANS MARIO MARTINEZ EMPL # 21787 AND JORGE L LINDERO EMPL # 34913;[15] MEASSUREMENTS INPUT ONLY;[16] JOB COMPLETE . (RII BUYBACK )
Part: RIB DOUBLER — CRACKED (L/H HORIZ. STAB.) · airframe 52,920 hrs · 31,399 cycles
LEFT HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 331B RIB #7 CRACKED / [01] PERFORMED HFEC INSP ON L/H HORIZ STAB L/E ACCESS PANEL RIB#7 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED (LENGTH 0.250?)<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] REMOVED LEFT HORIZONTAL STABILIZER L/E ACCESS PANEL 331B RIB # 7 REF B737-700 SRM 51-40-02. WORK WAS ACCOMPLISHED BY RICARDO SAMANIEGO EMPL # 35463;[03] VERIFIED STEP 2;[04] LOCATED AND DRILLED HOLES ON NEW LEFT HORIZONTAL STABILIZER LEADING EDGE PANEL 331B RIB # 7 REF B 737-700 SRM 51-40-05-0G-0.WORK WAS ACCOMPLISHED BY TECHNICIAN RICARDO SAMANIEGO EMPL # 35463.;[05] VERIFIED STEP 4;OK TO INSTALL NEW RIB # 7;[06] REPLACED RIB #7 PN 186A1307-3 AT L/H HORIZ. STAB. L.E PANEL REF. B737-700 SRM 51-40-02-0G-0;[07] VERIFIED STEP 6;[08] VERIFIED INSTALLATION OF NEW RIB;CARD COMPLETED
Part: RIB DOUBLER — CRACKED (R/H HORIZ. STAB.) · airframe 52,920 hrs · 31,399 cycles
RIGHT HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 341B RIB #4 CRACKED / [01] PERFORMED HFEC INSP ON R/H HORIZ STAB L/E ACCESS PANEL RIB#4 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED (LENGTH 0.450?)<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] REMOVED CRACKED RIB #4 AT R/H HORIZONTAL STAB L/E PANEL #341B REF B737-700 SRM 51-40-02-0G-0;[03] INSTALLED RIB #4 AT AFT CARGO COMP R/H HORIZ. STAB L/E REF SRM 51-40-02-0G-0.;[04] CORRECTION: INSTALLED RIB #4 AT R/H HORIZ. STAB L/E REF SRM 51-40-02-0G-0.;[05] LATE ENTRY: OK TO INSTALL SERVICEABLE RIGHT HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 341B #4 RIB.;[06] INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q0025LG3;[07] CORRECTION OF STEP #5:<BR>LATE ENTRY: OK TO INSTALL LEADING EDGE #4 RIB.;[08] INSTALLATION OF L/E PANEL 341B WILL BE ACCOMPLISHED ON TASK CARD TTG8Q0025LG3
Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,920 hrs · 31,399 cycles
FWD CARGO COMP STR 19L STA 500D GUSSET APPEARED CRACKED / [01] REMOVE & REPLACED GUSSET P/N: 143A9481-6; AT FWD. CARGO COMPT. AFT BULKHEAD STA. 500D; S-19L; AS PER B737-7 SRM 51-40-02 & DWG. 143A9481;[02] VERIFIED STEP 1
Part: BRACKET — ELONGATED (AFT CARGO) · airframe 52,920 hrs · 31,399 cycles
AFT CARGO DOOR CUTOUT STA 787+2 RBL 23' SUPPORT BRACKET FWD HOLE ELONGATED / [01] REMOVED SUPPORT BRACKET FOR ACCESS AT AFT CARGO DOOR CUTOUT STA 787+2 RBL 23' REF B737-700 SRM 51-40-02-0G-0;[02] INSTALLED NEW SUPPORT BRACKET AT AFT CARGO DOOR CUTOUT STA 787+2 RBL 23' REF B737-700 SRM 51-40-02-0G-0;[03] VERIFIED INSTALLATION ON STEP 2
Part: RIB DOUBLER — CRACKED (R/H HORIZ. STAB.) · airframe 52,920 hrs · 31,399 cycles
RIGHT HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 341B RIB #9 CRACKED / [01] PERFORMED HFEC INSP ON R/H HORIZ STAB L/E ACCESS PANEL RIB#9 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED (LENGTH 0.375?)<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] REMOVED RIGHT HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 341B RIB #9 REF B 737-700 SRM 51-40-02-0G-0. WORK WAS ACCOMPLISHED BY TECHNICIAN JUAN VILLELA EMPL # 35611;[03] LOCATED AND DRILLED NEW RIB #9 AT RIGHT HORIZONTAL L/E PANEL 341B REF SRM 51-40-05-0G-0;[04] VERIFIED STEP 3.<BR>VERIFIED PROTECTIVE COATING OF BARE METAL SURFACES.<BR>OK TO INSTALL.;[05] (LATE ENTRY) <BR>VERIFIED STEP 2.;[06] INSTALLED NEW RIB #9 AT RIGHT HORIZONTAL STAB L/E ACCESS PANEL 341B REF B737-700 SRM 51-40-02-0G-0 WORK ACCOMPLISHED BY JUAN VILLELA #35611;[07] VERIFIED STEP 6.
Part: BARRIER — CRACKED (CENTER WING) · airframe 52,920 hrs · 31,399 cycles
L/H VAPOR BARRIER CRACKED / [01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION AT R\H VAPOR BARRIER AND FOUND CRACK OF 12' AND <BR>FOUND CONTAMINATION PER B737 NTM 51-05-01 PART 1 AND B737 SRM 51-70-04-2R-0 PARAGRAPH(4.A);[03] PERFORMED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF CRACK PER B737 SRM<BR>57-10-10-2R-2 PARAGRAPH(6.B);[04] PREPARED DAMAGED AREA ON VAPOR BARRIER FOR 24HR DRY-OUT PROCESS PER B737<BR>SRM 51-70-04-2R-0 PARAGRAPH (4.D);[05] VERIFIED STEPS 1-4. OK TO PERFORM 24HR DRYOUT PROCESS.;[06] ACCOMPLISH DRY OUT PROCESS ON DAMAGE AREA OF L/H VAPOR BARRIER AS PER B737 SRM 51-70-04-2R-10;[07] STEPS 3 AND 4 ARE RII;[08] VERIFIED STEP 6. OK TO APPLY REPAIR.;[09] REPAIRED L/H VAPOR BARRIER ON BOTH SIDES WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10. MATERIALS USED PO#1774613 AND PO#1690463;[10] PERFORMED TAP TEST ON REPAIRED AREA OF VAPOR BARRIER ; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[11] VERIFIED ABOVE STEP #9 & 10 .;[12] APPLIED PRIMER AT FWD SIDE & TOPCOAT AT AFT SIDE OF LT VAPOR BARRIER WEB AS PER B737-7 AMM 51-21-72-370-804 & 51-21-73-370-803.;[13] PERFORMED INSPECTION AND VERIFICATION OF STEPS 9 AND 10.;[14] SEE STEP 13 FOR VERIFICATION OF STEPS 9 AND 10.;[15] VERIFIED STEP #12
Part: BARRIER — CRACKED (CENTER WING) · airframe 52,920 hrs · 31,399 cycles
R/H VAPOR BARRIER CRACKED / [01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION ON R/H VAPOR BARRIER AND FOUND CRACK OF 11' AND FOUND CONTAMINATION PER B737 NDTM 51-05-01;[03] PERFORMED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF CRACK PER B737 SRM 57-10-10-2R-2 STEP 6.B;[04] PREPARED DAMAGED AREA ON VAPOR BARRIER FOR REPAIR PER B737 SRM 51-70-04-2R-10 AND 51-70-04-2R-0 PARAGRAPH 4.E;[05] CORRECTION TO STEP 4: PREPARED VAPOR BARRIER FOR 24HR DRY-OUT PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.D;[06] VERIFIED STEPS 1-5. OK TO APPLY 24HR DRY;[07] APPLIED DRY OUT PROCESS AT R\H VAPOR BARRIER ON REPAIR AREA PER B737 SRM<BR>51-70-04-2R-0 PARAGRAPH(4.D) AND OK TO APPLY REPAIR AREA PER B737SRM<BR>51-70-04-2R-0 PARAGRAPH(4.E);[08] VERIFIED STEP 7. OK TO APPLY REPAIR.;[09] REPAIRED R/H VAPOR BARRIER ON DAMAGE AREA WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10. MATERIALS USED PO#1774613 AND PO#1690463;[10] VERIFIED STEP 9;[11] STEPS 3; 5; 7 AND 8 ARE RII;[12] APPLIED TEFLON PAINT ON R/H VAPOR BARRIER REF B 737 AMM 51-21-81-370-801;[13] VERIFIED STEP 12;[14] TASK C/W;[15] TASK C/W
Part: DOOR — CORRODED (FUSELAGE) · airframe 52,920 hrs · 31,399 cycles
TOILET SERVICE DOOR 145AL INNER UPPER SKIN AND HINGES CORRODED / [01] FOUND DEEP EXFOLIATING CORROSION THAT IS OUT OF LIMITS. DOOR NEEDS REPLACEMENT REF B 737-700 SRM52-40-01-1A-4;[02] REMOVED WASTE TANK SERVICE PANEL IN REF. AMM 52-49-07-000-801.;[03] VERIFIED STEP 2;OK TREAT AND PRIME.;[04] TREATED AND PRIMED WASTE TANK SERVICE PANEL IN REF. AMM 51-21-41-370-803; AMM 51-21-72-370-804.;[05] TREATED AND PRIMED NEW SERVICEABLE WASTE TANK SERVICE PANEL IN REF. AMM 51-21-41-370-803; AMM 51-21-72-370-804.;[06] VERIFIED TREAT AND PRIME;OK TO TOP COAT.;[07] APPLIED TOPCOAT AT NEW SERVICEABLE TOILET SERVICE DOOR REF B 737-700 AMM 51-21-73-370-803. WORK WAS ACCOMPLISHED BY TECHNICIAN ROBERT PERNERAT EMPL # 34877;[08] VERIFIED TOP COAT APPLICATION;OK TO INSTALL;[09] INSTALLED TOILET SERVICE DOOR REF. B737-700 AMM 52-49-07-400-801.;[10] INSTALLED TOILET SERVICE DOOR REF. B737-700 AMM 52-49-07-400-801.<BR>BONDING METER: S/N 17-0018<BR>CALIBRATION DUE 04/2023;[11] VERIFIED STEP 10
Part: SEAL BRACKET — CRACKED (LH WING) · airframe 52,537 hrs · 31,155 cycles
LEFT WING UPPER FIXED TRAILING EDGE PANEL AFT OF #1 ENGINE FAIRING COVE SEAL RETAINER CRACKED. / [01] REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-40-02.;[02] INSPECTED WORK PERFORMED.
Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 52,537 hrs · 31,155 cycles
L/H OVERWING EXIT FWD EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED LAMP PER AMM 33-51-04
2021
Part: SKIRT — DELAMINATED (R1 DOOR SLIDE) · airframe 48,918 hrs · 29,037 cycles
FWD SERVICE DOOR ESCAPE SLIDE SKIRT RUBBER RUB PAD DELAMINATING / FWD SERVICE DOOR- SLIDE WAS REMOVED AND REPLACED ON MOD-7 CARD J11701697. REFER TO J11701697 FOR ALL WORK PERFORMED.
Part: HANDLE — BROKEN (R1 DOOR ASSIST) · airframe 48,849 hrs · 28,998 cycles
FORWARD SERVICE DOOR ASSIST HANDLE BROKEN / R&R FWD SERVICE DOOR ASSUST HANDLE PER AMM 52-41-31.
2020
Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 47,510 hrs · 28,192 cycles
LOWER EGPR STIFFENER HAS DRILL DAMAGE AT THE FORWARD END. / INSTALLED NEW STIFFENER PER SRM 51-40-02
Part: RUB STRIP — DAMAGED (FUSELAGE) · airframe 47,510 hrs · 28,192 cycles
GROUND POWER DOOR CUTOUT LOWER LATCH RUB STRIP ATTACH FASTENER HOLES DO NOT HAVE EDGE MARGIN / REPAIRED PER EA# 20-153-01354 AND SRM 53-10-15-2R-5 AND SRM 53-10-15-2R-4
Part: ANGLE — CRACKED (BS 500A-500D) · airframe 47,510 hrs · 28,192 cycles
FORWARD CARGO PIT RH TRANSITION ANGLE HAS CRACK AT STA 500A+6 (MARKED) . / REMOVED AND REPLACED FWD CARGO RH TRANSITION ANGLE STA 500A TO STA 500D PER SRM 51-40-02.
Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 47,510 hrs · 28,192 cycles
FLIGHT COMPARTMENT FLOOR DENTED UNDER FIRST OBSERVERS SEAT. / REMOVED AND REPLACED PREVIOUS REPAIR PER SRM 51-40-02 AND EA# 20-153-01423
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 47,510 hrs · 28,192 cycles
LEFT HORIZONTAL STABILIZER INSPAR RIB #4 THE #3 STIFFENER IS CRACKED. VERIFIED WITH NDT. / REPAIRED RIB PER SRM 55-10-09-2R-4
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 47,510 hrs · 28,192 cycles
CABIN FLOOR BOARD 241BF HAS EDGE DAMAGE ON FWD EDGE. REMOVED AND REPLACED PER AMM.53-21-00.
Part: SEAT TRACK — CORRODED (BS 714) · airframe 47,510 hrs · 28,192 cycles
SEAT TRACK NO.4 HAS CORROSION (MARKED) AT STA. 714. / REMOVED CORROSION AREA ON # 4 SEAT TRACK PER SRM 51-10-02.FOUND TO BE WITHIN LIMITS PER SM 53-00-52-1A-1.(MATERIAL LOSS 0.008) TREATED THE AREA PER SRM 51-20-01.APPLIED ALUMINIZED EPOXY PRIMER TO THE AREA REFER TO SOPM 20-41-04.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 47,510 hrs · 28,192 cycles
CABIN FLOOR BOARD 241AF HAS FIBER DAMAGE ON TOP/AFT END OF PANEL / REMOVED AND REPLACED PER AMM.53-21-00
Part: DOUBLER — CRACKED (GRND PWR DOOR) · airframe 47,235 hrs · 28,025 cycles
GROUND POWER DOOR HAS CRACKED BROKEN TABS ON THE INTERNAL DOUBLER. MOD FACT AS A RESULT OF POST REPAIR INSPECTION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,894 hrs · 27,811 cycles
EMERGENCY LIGHTS L548 L547 L1065 INOP / REPLACED M1670 BATTERY PACK AND CHARGER IAW AMM 33-51-51
Part: LIGHT — LOOSE (ROW 12DEF) · airframe 46,187 hrs · 27,370 cycles
EMERGENCY EXIT SIGN IS LOOSE AT ROW 12DEF. REPLACED THE LIGHT AT ROW 12DEF PER M/M 33-51-01.
2019
Part: HOLDER — OUT OF ADJUST (R1 DOOR GIRT BAR) · airframe 45,320 hrs · 26,813 cycles
R1 DOOR SLIDE BAR DIFFICULT TO TAKE OUT. / ADJUSTED SLIDE BAR HOLDERS PER SIP.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 44,323 hrs · 26,177 cycles
RT STABILIZER CRACKED RIB, 5TH BAY FROM INBOARD, 3RD RIB FROM FORWARD SPAR. (STA 180.30 RIB). R&R RIB IAW SRM.
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 43,608 hrs · 25,705 cycles
RIGHT HORIZ STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZ STAB FWD UPPER SLIDING SEAL PER AMM. 53-31-31
Part: STRAP — MISSING (FLASHLIGHT) · airframe 42,912 hrs · 25,292 cycles
AFT EMERGENCY FLASHLIGHT STRAP MISSING. R&R FLASHLIGHT STRAP PER MM.
2018
Part: MOUNT BRACKET — MISSING (CABIN) · airframe 41,903 hrs · 24,672 cycles
CENTER CABIN AISLE EXIT LIGHT MOUNTING BRACKET MISSING. INSTALLED BRACKET PER SIP.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 18L. R&R GUSSET PER SRM.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 18R. R&R GUSSET PER SRM.
Part: PANEL — ELONGATED (ELEVATOR LH) · airframe 41,752 hrs · 24,575 cycles
LEFT ELEVATOR LOWER L/E FIXED PANEL HAS 1EA SCREW HOLE ELONGATED 24' FROM FUSELAGE. / REPAIRED PANEL PER SRM 51-70-04-2R-9.
Part: BRACKET — CRACKED (LEFT WING) · airframe 41,752 hrs · 24,575 cycles
L/H WING TRAILING EDGE PANEL 551FB FWD MOUNT BRACKET CRACKED IN RADIUS. / REMOVED AND REPLACED BRACKET PER SRM 51-40-02.
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 41,752 hrs · 24,575 cycles
R/H UPPER LONG SIDING SEAL CRACKED @ HORIZONTAL STABILIZER FWD. ATTACH BOLTS. / R&R SLIDER;OPS CHECKED GOOD PER AMM 53-31-31;WITH REFERENCE TO SRM 51-40-02.
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 41,752 hrs · 24,575 cycles
L/H UPPER LONG SIDING SEAL CRACKED @ HORIZONTAL STABILIZER FWD. ATTACH BOLTS. / INSTALLED NEW SLIDING SEAL AND PERFORMED OPS CHECK ALL WORK PER AMM 53-31-31 SEE ATTACHED WIP FOR ALL WORK PERFORMED
Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 41,752 hrs · 24,575 cycles
RUDDER BALANCE WEIGHT MATING SURFACE ON RUDDER ARM CORRODED. / R&R RUDDER PER AMM 27-21-11.RIG AND OPS CHECKS GOOD PER AMM 27-21-00. TAG NO: 457754 PN ON: 173A0103-10 SN ON: CASA2238 PN OFF: SN OFF: SB1941
Part: DRAIN — CRACKED (MAIN CABIN) · airframe 41,752 hrs · 24,575 cycles
FOUND A CRACK AT THE INBD SIDE OF THE FUSELAGE DRAIN HOLE IN THE LOWER CORD (MARKED) / REPAIRED PER EA 1-757-15481 PART 2
Part: INTERCOSTAL — CRACKED (FWD CARGO LH) · airframe 41,752 hrs · 24,575 cycles
FWD CARGO: STA. 500-500A LBL 25 INTERCOSTAL CRACKED / REMOVED AND REPLACED INTERCOSTAL IN FWD CARGO AT STA. 500-500A AS REQUIRED PER SRM 51-10-02 AND SRM 51-40-02. PLEASE SEE SUBTASKS FOR ADDITIONAL SIGNOFFS.
Part: SUPPORT — BROKEN (CABIN) · airframe 41,752 hrs · 24,575 cycles
FLOOR SUPPORT BROKEN BETWEEN #1 SEAT TRACK AND CREASE BEAM AT STA.540. / INSTALLED NEW FLOOR SUPPORT PER SRM 51-40-02.
Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
FLOOR SUPPORT BROKEN AT BS 540, BETWEEN NR 3 AND NR 4 SEAT TRACK. R&R SUPPORT PER SRM.
Part: SUPPORT — BROKEN (CABIN) · airframe 41,752 hrs · 24,575 cycles
FLOOR SUPPORT BROKEN BETWEEN #1 AND #2 SEAT TRACK AT STA.540. / INSTALLED NEW FLOOR SUPPORT PER SRM 51-40-02.
Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
FLOOR SUPPORT BROKEN AT BS 540, BETWEEN NR 2 SEAT TRACK AND BL 0. R&R SUPPORT PER SRM.
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES; UPPER AND LOWER SURFACE; FROM STA.727E-STA.747. MARKED / REPAIRED R/H TRANSITION ANGLE FROM STA.727C+10' TO STA.767 PER SRM 53-00-53-2R AND SRM 51-40-02.
Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
INTERCOSTAL BROKEN AT BS 540, BETWEEN RBL 24 TO RBL 45. R&R INTERCOSTAL PER SRM.
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES; UPPER AND LOWER SURFACE; FROM STA.747-STA.767. MARKED / REPAIRED R/H TRANSITION ANGLE FROM STA.727C+10' TO STA.767 PER SRM 53-00-53-2R AND SRM 51-40-02.
Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 41,752 hrs · 24,575 cycles
FWD CARGO DOOR CUTOUT OPENING.; LOWER ENTRY WEB HAS SEVERAL AREAS AT FASTENER OPENINGS WITH LIGHT SURFACE CORROSION. / REMOVED & REPLACED FWD CARGO DOOR CUTOUT OPENING; LOWER ENTRY WEB PER SRM 51-40-02-0G-0.
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES; UPPER AND LOWER SURFACE; FROM STA.727D-STA.727E. MARKED / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA.727C+10 TO STA.767 PER SRM 53-00-53-1A AND SRM 51-40-02.
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; LEFT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES FROM STA.727E-STA.747. MARKED / REMOVED AND REPLACED CARGO LH TRANSITION FROM STATION 727 TO STATION 847 PER SRM 51-10-02 AND SRM 51-40-02
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; LEFT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES FROM STA.747-STA.767. MARKED / REMOVED AND REPLACED CARGO LH TRANSITION FROM STATION 727 TO STATION 847 PER SRM 51-10-02 AND SRM 51-40-02
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; LEFT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES FROM STA.727D-STA.727E. MARKED / REMOVED AND REPLACED CARGO LH TRANSITION FROM STATION 727 TO STATION 847 PER SRM 51-10-02 AND SRM 51-40-02
Part: ANGLE — CRACKED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; STA.729 RBL 5 ; ANGLE ADJACENT TO THE APU BLEED DUCT; IS CRACKED. MARKED / REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
AFT CARGO COMPARTMENT FLOOR INTERCOSTAL CORRODED AT BS 771, BETWEEN LBL 21 TO RBL 21. R&R ASSEMBLY PER SRM.
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; LEFT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES FROM STA.727C-STA.727D. MARKED / REMOVED AND REPLACED CARGO LH TRANSITION FROM STATION 727 TO STATION 847 PER SRM 51-10-02 AND SRM 51-40-02
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES; UPPER AND LOWER SURFACE; FROM STA.767-STA.787. MARKED / REMOVED AND REPLACED AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE FROM STA. 767-STA. 787 AS REQUIRED PER SRM 51-10-02 AND SRM 51-40-02. PLEASE SEE SUBTASKS FOR ADDITIONAL SIGN OFFS.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL PER SRM.
Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 41,752 hrs · 24,575 cycles
FWD CARGO R/H TRANSITION ANGLE HAS EVIDENCE OF CORROSION BETWEEN STA 500A TO 500B. / REMOVED FWD CARGO R/H TRANSITION ANGLE BETWEEN STA 500A TO STA 500D PER SRM. 51-10-02
Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
R1 DOOR Z ANGLE CORRODED BETWEEN BS 312-2 TO BS 328+3. R&R Z ANGLE PER SRM.
Part: FITTING — CRACKED (LOWER EXT FUSELA) · airframe 41,752 hrs · 24,575 cycles
FWD LEFT ATTACH 'T' FITTING CRACKED ALL THE WAY THROUGH FOR PANEL 192E. (MARKED) / REPLACED FITTING PER SRM 51-40-02.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
L1 DOOR Z ANGLE CORRODED ATA BS 312-10, LBL 55. R&R Z ANGLE PER SRM.
Part: ANGLE — CORRODED (FWD CARGO LH) · airframe 41,752 hrs · 24,575 cycles
FWD CARGO COMPARTMENT L/H FLOOR TRANSITION ANGLE HAS CORROSION AROUND SEVERAL FASTENER HOLES BETWEEN STA 440-460 . / R/R TRANSITION ANGLE FROM STA. 400 TO STA.500 D ; PER SRM. 51-10-02 AND SPLICE REPAIRED PER SRM. 53-00-53-2R-5
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,751 hrs · 24,575 cycles
INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL PER SRM.
Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 41,752 hrs · 24,575 cycles
FWD CARGO R/H TRANSITION ANGLE HAS EVIDENCE OF CORROSION BETWEEN STA 500 TO 500A. / CORROSION FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2 ; REMOVED TRANSITION ANGLE ; PER SRM 51-40-01 ; LOCATED AND DRILLED NEW ANGLE PER SRM. 51-10-05 ; INSTALLED NEW TRANSITION ANGLE FROM STA. 500 TO 500A PER SRM 51-10-02
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 41,751 hrs · 24,575 cycles
VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 40.5. REPAIRED WEB PER SRM.
Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 41,752 hrs · 24,575 cycles
AFT CARGO DOOR ;AFT CORNER THRESHOLD PLATE CRACKED. / AFT CARGO ;AFT CORNER THRESHOLD PLATE REPAIRED BY VENDOR PER R/O # 7530220-AUR. TO BE INSTALLED PER ROUTINE CARD # 753-140-00-02Y.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 41,751 hrs · 24,575 cycles
VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 33.5. REPAIRED WEB PER SRM.
Part: NONE — CRACKED (LEFT WING) · airframe 41,752 hrs · 24,575 cycles
WAFFLE PLATE JUST O/B OF SWING DOWN PANEL 551DB IS CRACKED. / REPLACED WAFFLE PLATE JUST O/B OF SWING DOWN PANEL 551DB IAW SRM 51-40-02.
Part: DOOR — CRACKED (HORIZONTAL STAB) · airframe 41,752 hrs · 24,575 cycles
RIGHT HORIZONTAL STABILIZER LOGO LIGHT ACCESS DOOR # 343FB CRACKED / REMOVED AND REPLACED ACCESS DOOR PER SRM 51-40-02. RESTORED FINISH PER AMM 51-21-00.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 40,476 hrs · 23,748 cycles
EXTERNAL POWER DOOR CUTOUT FRAME CRACKED. REPAIRED DOOR FRAME IAW SRM.
2017
Part: HANDLE — BROKEN (R1 DOOR) · airframe 39,322 hrs · 23,048 cycles
R1 DOOR ASSIST HANDLE BROKEN. R&R HANDLE PER SIP.
Part: HANDLE — BROKEN (R2 DOOR ASSIST) · airframe 39,298 hrs · 23,032 cycles
R2 DOOR ASSIST HANDLE BROKEN. / R&R HANDLE IAW SIP.
Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 38,766 hrs · 22,698 cycles
L1 DOOR EMERGENCY EVAC SIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER MM.
Part: FITTING — BROKEN (GIRT BAR) · airframe 38,618 hrs · 22,606 cycles
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP RIVET BROKEN. R&R CLIP PER SIP.
Part: FLOORBEAM — CRACKED (BS 540) · airframe 37,149 hrs · 21,724 cycles
CABIN FLOORBEAM CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24. R & R THE FLOORBEAM IAW SRM.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 36,462 hrs · 21,321 cycles
AFT OUTBOARD FLASHLIGHT INOPERATIVE. R & R THE BATTERY IAW CMM.
2016
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 35,031 hrs · 20,518 cycles
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 129.50. REPAIRED THE RIB IAW EA.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 34,139 hrs · 19,996 cycles
R1 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,370 hrs · 19,547 cycles
R2 DOOR EMER EVAC SLIDE EXTERIOR LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,906 hrs · 19,272 cycles
LEFT FWD EMER EXIT LIGHT INOPERATIVE. R & R CHARGER IAW MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,906 hrs · 19,272 cycles
LEFT FWD EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 32,825 hrs · 19,227 cycles
RIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 32,825 hrs · 19,227 cycles
LEFT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
2015
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 29,694 hrs · 17,389 cycles
R2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.
Part: COVER — MISSING (CABIN) · airframe 29,399 hrs · 17,212 cycles
LEFT EMER EXIT LIGHT COVER MISSING AT ROW 11. INSTALLED COVER IAW AMM.
2014
Part: STRAP — CORRODED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FLOOR STRUCTURE STRAP CORRODED AT BS 1010 RBL 5. R & R STRAP IAW SRM.
Part: STRAP — CORRODED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FLOOR STRUCTURE STRAP CORRODED AT BS 1005 LBL 5. R & R STRAP IAW SRM.
Part: STRAP — CORRODED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FLOOR STRUCTURE STRAP CORRODED AT BS 1010 LBL 5. R & R STRAP IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 LBL 45. R & R INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 RBL 29. R & R INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
INTERCOSTAL CRACKED BETWEEN BS 328 TO 344 LBL 45. R & R INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
INTERCOSTAL CRACKED BETWEEN BS 294.5 TO 312 RBL 16. R & R INTERCOSTAL IAW SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
R1 DOOR THRESHOLD ATTACH STRUCTURE ANGLE CORRODED. R & R ANGLE IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
INTERCOSTAL CRACKED BETWEEN BS 344 TO 360 LBL 5. R & R INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
INTERCOSTAL CRACKED BETWEEN BS 277 TO 294.5 BL 0. R & R INTERCOSTAL IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK OTBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK OTBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B LBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK OTBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B LBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B RBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
FORWARD SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: POST — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
LEFT NR 3 FLIGHT DECK WINDOW FRAME E - F POST FASTENER HOLE 2ND FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.
Part: POST — CRACKED (FUSELAGE) · airframe 28,342 hrs · 16,615 cycles
RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST FASTENER HOLE 2ND FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.
Part: SLIDE — UNSECURE (R1 DOOR) · airframe 28,069 hrs · 16,451 cycles
R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE IAW MT.
Part: LENS — BROKEN (CABIN) · airframe 26,737 hrs · 15,667 cycles
R2DOOR EMERGENCY EXIT LENS BROKEN. R & R LENS IAW MM.
2013
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 24,194 hrs · 14,168 cycles
L2 DOOR EMERGENCY EVAC SLIDE FELL FROM CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 24,107 hrs · 14,120 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR IAW MM.
Part: COVER — BROKEN (CABIN) · airframe 23,933 hrs · 14,026 cycles
L1 DOOR EMERGENCY EXIT LIGHT LENS COVER BROKEN. R&R COVER IAW M/M.
Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 23,544 hrs · 13,810 cycles
WITH RT CENTER PUMP DEFERRED, A FUEL IMBALANCE WAS CREATED BY NO FUEL BURNING OUT OF THE NR 1 TANK. FUEL BURNING OUT OF NR 2. LESS FUEL BURN OUT OF CENTER. R & R RT CONTROL LOW PRESSURE SWITCH IAW MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 23,309 hrs · 13,671 cycles
R1 GALLEY DOOR SLIDE FLAP LOOSE. ADJUSTED SLIDE PER M/M.
2012
Part: COVER — MISSING (CABIN) · airframe 21,503 hrs · 12,601 cycles
EEPLS COVER MISSING AT ROW 17. INSTALLED COVER PER M/M.
Part: LENS — BROKEN (CABIN) · airframe 21,335 hrs · 12,500 cycles
LEFT EEPLS LENS BROKEN AT ROW 20. REMOVED AND REPLACED LENS PER AMM.
Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 21,184 hrs · 12,387 cycles
L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.
Part: LENS — DAMAGED (CABIN) · airframe 20,377 hrs · 11,890 cycles
PASSENGER CABIN EEPLS LENS STAINED BETWEEN ROW 22 AND ROW 23. REMOVED AND REPLACED LENS PER M/M.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,688 hrs · 11,502 cycles
EMERGENCY EXIT LIGHT PATHWAY INOP AT ROW 1. RELAMPED LIGHT PER M/M.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,689 hrs · 11,502 cycles
EEPLS INOP AT ROW 7. REPAIRED EEPLS PER WDM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,096 hrs · 11,178 cycles
AFT ENTRY DOOR EMERGENCY EXTERNAL LIGHT INOP. RELAMPED PER M/M.
2011
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,107 hrs · 10,602 cycles
DURING SCHEDULED CV CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
Part: COVER — CRACKED (CABIN) · airframe 18,107 hrs · 10,602 cycles
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
Part: LENS — CRACKED (CABIN) · airframe 18,107 hrs · 10,602 cycles
DURING SCHEDULED CV CHECK, FOUND AFT EEPLS LENS CRACKED. REMOVED AND REPLACED EEPLS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,107 hrs · 10,602 cycles
DURING SCHEDULED CV CHECK, FOUND EEPLS BULB INOP. REMOVED AND REPLACED BULB PER MM.
Part: LIGHT — CRACKED (CABIN) · airframe 16,893 hrs · 9,900 cycles
DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,652 hrs · 9,768 cycles
DURING SCHEDULED MV2 CHECK FOUND, FWD ENTRY EEPLS INOP. RELAMPED PER MM.
Part: COVER — MISSING (CABIN) · airframe 16,318 hrs · 9,568 cycles
F/A REPORTED AFT SERVICE DOOR EMERGENCY EXIT OVER MISSING. REPLACED SERVICE DOOR COVER PER MM.
2010
Part: CAP — MISSING (CABIN) · airframe 14,712 hrs · 8,652 cycles
DURING SCHEDULED MV2 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED END CAP PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,643 hrs · 8,613 cycles
FWD EEPLS INOP. RELAMPED PER MM.
Part: LENS — MISSING (CABIN) · airframe 14,636 hrs · 8,609 cycles
FWD ENTRY EEPLS LENS MISSING. INSTALLED LENS PER MM.
Part: LENS — MISSING (CABIN) · airframe 13,869 hrs · 8,175 cycles
DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: LENS — MISSING (CABIN) · airframe 13,700 hrs · 8,085 cycles
DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 15. INSTALLED LENS PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,898 hrs · 7,593 cycles
DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
Part: LENS — LOOSE (CABIN) · airframe 12,837 hrs · 7,556 cycles
LEFT EEPLS LENS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
Part: COVER — LOOSE (CABIN) · airframe 12,615 hrs · 7,428 cycles
LT EEPLS COVER LOOSE. REMOVED AND REPLACED COVER PER MM.
Part: LENS — MISSING (CABIN) · airframe 12,207 hrs · 7,180 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 16. INSTALLED LENS PER MM.
Part: LIGHT — MISSING (CABIN) · airframe 12,207 hrs · 7,180 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS BULB MISSING AT ROW 16. INSTALLED BULB PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 12,207 hrs · 7,180 cycles
DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
2009
Part: COVER — CRACKED (CABIN) · airframe 11,163 hrs · 6,537 cycles
DURING SCHEDULED CV CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
Part: COVER — MISSING (CABIN) · airframe 10,965 hrs · 6,409 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS COVER MISSING AT ROW 1. REMOVED AND REPLACED COVER PER MM.
Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 9,876 hrs · 3,858 cycles
FLIGHT ATTENDANT REPORTED SMOKE FROM AFT GALLEY COFFEEMAKERS. REMOVED AND REPLACED NR 2 AFT GALLEY COFFEEMAKER PER MM.
2008
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 5,271 hrs · 3,037 cycles
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.