N374DA
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2012-02-18 – 2012-02-18 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2012-02-18 – 2012-02-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
ON WALK AROUND FOUND CORROSION DAMAGE ON WASTE BLOWER OVERBOARD VENT. REPAIRED PER SRM 53-70-01-2R PROCEDURE 3 AND ERA 635375-14. (LOG 1673121 - AIRCRAFT WAS GROUNDED).
CORROSION TO STRINGER 23L AT BS 907. REMOVED DAMAGED STRINGER SECTION IAW SRM 53-00-03-2R-1, REPAIR 1. LOCATED AND DRILLED NEW STRINGER, 2 NEW STRINGER SPLICES, AND 2 NEW STRINGER CLIPS PER SRM 53-00-03-2R-1, REPAIR 1. TREATED AND PRIMED REPAIR PARTS IAW SRM 53-00-03-2R-1, REPAIR 1. INSTALLED REPAIR PARTS, 2 STRINGER CLIPS AND NEW STINGER SECTION IAW SRM 53-00-03-2R-2. (LOG 1673169 - AIRCRAFT WAS GROUNDED).
ON WALK AROUND FOUND CORROSION DAMAGE ON WASTE BLOWER OVERBOARD VENT. REPAIRED PER SRM 53-70-01-2R PROCEDURE 3. (LOG 1667229 - AIRCRAFT WAS GROUNDED).
DECLARED AN EMERGENCY, RETURNED PHX DUE TO FLAP ASYMMETRY. FSEU BITE FAULT 27-53255 (FLAP 6 SKEW) AND 27-53414 (FLAP 6 SKEW CON) RECORDED. REPLACED #6 SKEW SENSOR T530. OPS CHECK GOOD. (LOG 7604600 - AIRCRAFT WAS GROUNDED).
(LOG 1444087) HANDLE MISSNG AND HAS BEEN REMOVED WITH THE HOLES FILLED THERE IS NO FA EMERGENCY ASSIST HANDLE LOCATED FORWARD A/C LEFT OF DOOR 1L. THIS MAKES 1L AN UNUSABLE EXIT IN AN EMERGENCY BECAUSE THERE IS NO WHERE TO HOLD ON IN AN EMERGENCY EVACUATION. SWAPPED HANDLE FROM INSIDE RT LAV TO FWD GALLEY WALL LT OF FA SEATS PER B737 AMM 25-40. EMER EXIT SIGNS PRESENT AND OPS CHECK GOOD.
(LOG 7189724) L1 DOOR ESCAPE SLIDE PACK BELOW NORMAL PSI RANGE FOR SERVICE. REMOVED/INSTALLED L1 DOOR SLIDE PER WC 2560-4425.
(LOG 7484406) ON SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS ABOVE AISLE AT ROWS 2C AND 4C INOP. FOUND F4 FUSE BAD AT POWER SUPPLY M1674. REPLACED F4 FUSE PER B737 AMM 33-51. OPS CHECK GOOD.
(LOG 0953755) DENT FROM A BIRD STRIKE AT STA 178 4 INCHES ABOVE STR 21. MEASURING 1INCH WIDE BY 4INCHES LONG WITH A MAX DEPTH OF 0.090 INCHES. REPAIRED PER ERA 626141-14.
(LOG 0953506) UPON ARRIVAL INTO AMES (TPA), MTC REPORTED A DENT BY BIRD STRIKE LOCATED IN STA 178.4 AND ABOVE STR 21R. ADDITIONALLY, THAT THERE IS A PREVIOUS REPAIR WITH DISTANCE OF 12.8 INCHES BETWEEN DENT LAND UPPER EDGE OF THE PREVIOUS REPAIR. REPAIRED PER ERA 626141-14.
(LOG 0941672) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE LEFT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGERS S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING, AND PERFORMING APPLICABLE ON-CONDITION ACTIONS PER BOEING SERVICE BULLETIN 737-53A1402 REVISION 01. COMPLIED WITH TASK CARD 5311-01251-02A FORECAST NUMBER 38-0553-8-0154 AD RELATED/ RII ON LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR
(LOG 0941692) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE RIGHT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGER S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING, AND PERFORMING APPLICABLE ON CONDITION ACTIONS PER BOEING SERVICE BULLETIN 737-53A1402 REVISION 01. COMPLIED WITH TASK CARD 5311-01251-02B FORECAST NUMBER 38-0553-5-0156 AD RELATED/RII ON RIGHT HAND STA 727 FRAME INNER CHRD, 737 REPAIR.
(LOG 5634931) ROWS 11-15 EEPLS INOP. REMOVED AND REPLACED ASSOCIATED BATTERY IN REF B737 AMM 33-51. OPS CHECK GOOD AT THIS TIME.
(LOG 5041154) L1 DOOR WILL NOT CLOSE. REMOVED, REPLACED & ADJUSTED L1 ENTRY DOOR GUIDE ARM & ROLLER PER B737 AMM 52-11. REINSTALLED LINER PER AMM 52-11.
SHIP 3704 -PRESS- DUE TO LOSS OF PRESSURIZATION CONTROL. CORRECTIVE ACTION: C/W PNEUMATIC HEALTH CHECKS AND PRESSURIZATION TROUBLE SHOOTING TASKS. REPLACED FAULTING #2 CABIN PRESSURE CONTROLLER, #2 ENGINE HSR AND CABIN OUTFLOW VALVE. OPS CHECKED GOOD.
(LOG 4166388) DURING INSPECTION FOUND CRACK AT LEFT WHEEL WELL VAPOR BARRIER O/B OF RBL 10.54, 10 IN LONG AND RIGHT WHEEL WELL VAPOR BARRIER O/B OF RBL 6.15, 9IN LONG. CRACKS ON VAPOR BARRIER REPAIRED IAW B737 SRM 57-10-10-1A PROCEDURE 2.C.4. REPAIR ID TOPP 40-20-66 PS 900-5-1 NO. 04. PER B737 SRM 57-10-10-1A.
(LOG 8970094) UPON ENTERING COCKPIT SMELLED ELECTRICAL BURNING SMELL. FOUND CAPTS MASTER CAUTION LIGHT SWITCH BURNING SMELL. REMOVED AND REPLACED CAPTS MASTER CAUTION LIGHT SWITCH IAW B737 SWPM 20-84. OPS CHECKS GOOD.
(LOG 8970070) ON ARRIVAL AFT LAV SERVICE DOOR MISSING. INSTALLED NEW SERVICE DOOR IAW B737 IPC 52-49.
(LOG 2445892) DURING INSPECTION FOUND COCKPIT NUMBER 1 WINDOW RH WAS FOUND CRACK ON COCKPIT NUMBER 1 WINDOW FRAME ASSEMBLY RH ON OUTBOARD UPPER CORNER INNER STRUCTURE FACE. NUMBER 1 WINDOW FRAME ASSEMBLY RH WAS REPAIRED PER ER/A 602485-14AD REV ORIGINAL.
(LOG 2445830) DURING INSPECTION FOUND COCKPIT WINDOW FRAME ASSEMBLY", WAS FOUND CRACK 1.250" LONG ON COCKPIT NUMBER 1 WINDOW FRAME ASSEMBLY ON OUTBOAR UPPER CORNER EXTERIOR FACE. COCKPIT NUMBER 1 WINDOW FRAME ASSEMBLY ON OUTBOARD UPPER CORNER EXTERIOR FACE WAS REPAIRED PER ER/A 602277-14AD REV:ORIG.
(LOG 2442239) DURING INSPECTION FOUND CRACK ON CUTOUT OF TRAY ON EXTERNAL POWER RECEPTACLE, MID FWD EDGE. CRACK ON CUTOUT OF TRAY ON EXTERNAL POWER RECEPTACLE, MID FWD EDGE WAS REPAIRED PER B737-800 SRM 53-10-15-2R REPAIR 5.
(LOG 2438878) DURING INSPECTION FOUND CORROSION ON WEATHER ANTENNA RADAR AT NOSE RADOME. WEATHER ANTENNA RADAR FLAT PLATE WAS REMOVED AND NEW WEATHER ANTENNA RADAR FLAT PLATE WAS INSTALLED. OPERATIONAL TEST WAS PERFORMED PER B737-800 AMM 34-43-11.
(LOG 2435676) DURING INSPECTION FOUND FLIGHT COMPARTMENT FIXED LH NO. 1 WINDOW FRAME UPPER CORNER WITH CRACK & WEAR. REPAIRED DAMAGE PER ERA 602277-14.
(LOG 2427860) DURING INSPECTION FOUND CORROSION AT EMERGENCY SLIDE ANCHORS (4 EA) OF L2/R2 DOORS. SLIDE ANCHOR L2,R2 WAS VERIFIED AND REPLACED PER B737-800 IPC 25-66-02-01 ITEM 050.
(LOG 2424750) DURING INSPECTION PREVIOUS REPAIR WAS FOUND ON SUPPORT STRUCTURE STA 727+2.7. FRAME SUPPORT STRUCTURE STA 727+2.7 WAS REPAIRED PER PRI 601909-14 REV.0 AND ER/A NO.601909-14 REV. ORIGINAL.
(LOG 2418179) DURING INSPECTION FOUND CORROSION ON PEVIOUS REPAIR RAIL RBL 3.0 FROM STA 727I+3 TO 727I+6 AND STA 767+2 TO 767+5 AT AFT CARGO COMPARTMENT. RAIL RBL 3.0 FROM STA 727I+3 TO 727I+6 AND STA 767+2 TO 767+5 AT AFT CARGO COMPARTMENT WERE REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 2.
(LOG 2416347) DURING INSPECTION FOUND CORROSION ON SEVERAL POINT AT FLOOR BEAM ON STA 986.5 BTW RBL 41 TO LBL41, AT PASSENGER COMPARTMENT W2. FLOOR BEAM ON STA 986.5 BTW RBL 50 TO LBL 50, AT PASSENGER COMPARTMENT W2 WAS REPAIRED PER. ERA 601683-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 601683-14 REV. 2.
(LOG 2416275) DURING INSPECTION FOUND CORROSION ON RAIL RBL3.0 FROM STA 787+3 TO 787+4.5 AT AFT CARGO COMPARTMENT. CORROSION ON RAIL RBL3.0 FROM STA 787+3 TO 787+4.5 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-53-2R.
(LOG 2414837) DURING INSPECTION FOUND CORROSION ON LH 2 DOOR SILL FROM STA 947 TO 996.5 AND LBL 51, AT PASSENGER COMPARTMENT W2. SILL FROM STA 947 TO 996.5 AND LBL 51, AT PASSENGER COMPARTMENT W2 (CPAX) WAS REPAIRED PER ER/A NO.601860-14 REV.ORIGINAL. SECTION I: PERMANENT REPAIR AND PRI 601860-14 REV 0.
(LOG 2414214) DURING INSPECTION FOUND CORROSION ON LH 2 DOOR SILL FROM STA 947 TO 996.5 AND LBL 51, AT PASSENGER COMPARTMENT W2. SILL FROM STA 947 TO 996.5 AND LBL 51, AT PASSENGER COMPARTMENT W2 (CPAX) WAS REPAIRED PER ER/A NO.601860-14 REV.ORIGINAL. SECTION I: PERMANENT REPAIR AND PRI 601860-14 REV 0.
(LOG 2415131) DURING INSPECTION FOUND CORROSION AT LH SIDEPLATE-SUPPORT ZEE BETWEEN STA 747 TO 727J -10, AFT CARGO COMPARTMENT. CORROSION ON SECTION SIDEPLATE LH BETWEEN STA 727H+10 TO STA 847 WAS REPAIRED PER B737-800 SRM 53-00-53-2R REPAIR 5.
(LOG 2411011) DURING INSPECTION FOUND CORROSION ON RAIL LBL 8.1 STA 767+2" TO 767+5" AND ON RBL 8.1 STA 727I+3" TO STA 727I+6", STA 767+3" TO 767+6" WITH PREVIOUS REPAIR. REPAIRS ON RAIL LBL 8.1 STA 767+2" TO 767+5" AND ON RBL 8.1 STA 727I+3" TO STA 727I+6", STA 767+3" TO 767+6" WERE REPLACED PER B 737-800 SRM 51-40-02-0G.
(LOG 2406885) DURING HCK AT QRO, WHILE PERFORMING AN UNDERAFTER GALLEY AND LAVATORIES WET AREAS INTERNAL INSPECTION PER WC 5300-2103, CORRODED AREAS WERE FOUND AFFECTING THE L2 DOOR LOWER MAIN SILL INNER CHORD, BETWEEN STA 951.07 & STA 992.8. CORROSION REPAIRED PER ERA 601860-14.
(LOG 2404925) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT AT STA 951 BTW RBL 15 TO RBL 47, AT PASSENGER COMPARTMENT W2. FLOOR SUPPORT AT STA 951 BTW RBL 15 TO RBL 47, AT PASSENGER COMPARTMENT W2 WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 2405982) DURING INSPECTION FOUND CORROSION ON SETTLEMENT AREA OF RUBBER SEAL AT RIGHT FUEL ACCESS PANELS 632EB AND 632HB. FUEL ACCESS PANELS 632EB AND 632HB WERE REPLACED AND PART NUMBER VERIFIED PER B737-800 IPC 28-11-11.
(LOG 2404922) DURING INSPECTION FOUND CORROSION ON WEB ON STA 988 AND LBL 37, AT PASSENGER COMPARTMENT W2. WEB ON STA 988 AND LBL 37, AT PASSENGER COMPARTMENT W2 WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 2404918) DURING INSPECTION FOUND CORROSION ON WEB BTW STA 986.5 TO STA 992 AND RBL 43 TO RBL 36, AT PASSENGER COMPARTMENT W2. WEB BTW STA 986.5 TO STA 992 AND RBL 43 TO RBL 36, AT PASSENGER COMPARTMENT W2 WAS REPLACED PER B737-800 B737-800 SRM 51-40-02-0G.
(LOG 2404547) DURING INSPECTION FOUND CORROSION ON WEB AT STA 1016+10 BTW LBL 30 AND LBL 34, AT PASSENGER COMPARTMENT. CORROSION LEVEL 2 ON WEB AT STA 1016+10 BTW LBL 30 AND LBL 34, AT PASSENGER COMPARTMENT WAS REPAIRED PER ER/A 601789-14 REV. ORIGINAL. SECTION I; PERMANENT REPAIR AND PRI 601789-14 REV. 0.
(LOG 2401995) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BTW STA 986.5 AND 967 LBL 16, AT PASSENGER COMPARTMENT W2. FLOOR SUPPORT BTW STA 986.5 AND 967 LBL 16, AT PASSENGER COMPARTMENT W2 WAS REPLACED AT NRC 00708.
(LOG 2398926) DURING INSPECTION FOUND CRACK OF 0.400IN LENGHT AT 7 CLOCK POSITION WAS FOUND ON RH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA 907. RH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA 907 WAS REPAIRED PER AMDS 2526-01236-03B.
(LOG 2398830) DURING INSPECTION FOUND CRACK OF 0.400IN LENGHT AT 9 CLOCK POSITION WAS FOUND ON RH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA 500D.
(LOG 2395966) DURING INSPECTION FOUND CORROSION IN THE COUNTER FRAME OF THE GARBAGE DOOR ACCESS A423 AT GALLEY 4. COUNTER FRAME OF THE GARBAGE DOOR ACCESS A423 AT GALLEY 4 REPLACED PER ERA 601874-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 601874-14 REV 0. AND C&D ZODIAC CMM 25-32-27 REPAIR SECTION PAR 2 C TO G.
(LOG 2391430) DURING INSPECTION FOUND CORROSION ON ACCESS PLATE AT GALLEY 4. ACCESS PLATE (2 EA S) AT GALLEY 4 WERE REPLACED PER ER/A 12-486041-14MA REV. G.
(LOG 2388035) DURING INSPECTION FOUND CRACK OF 0.560IN LENGHT AT 3 CLOCK POSITION WAS FOUND ON LH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA 867. LH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA. 867 WAS REPAIRED PER. CARD 2526-01236-02A.
(LOG 2388032) DURING INSPECTION FOUND CRACK OF 0.560IN LENGHT AT 3 CLOCK POSITION WAS FOUND ON LH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA 867. LH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA. 867 WAS REPAIRED PER. CARD 2526-01236-02A.
(LOG 2388031) DURING INSPECTION FOUND CRACK OF 0.400IN LENGHT AT 3 CLOCK POSITION WAS FOUND ON LH FUSELAGE FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA 827. FRAME AT A/C RAIL BRACKET AT THE INBOARD FASTENER HOLE STA 827 WAS REPAIRED PER. CARD 2526-01236-02A.
(LOG 2386610) DURING INSPECTION FOUND CORROSION AT FLOOR BEAM STA 328 RBL 10 TO RBL 51 CABIN PAX. CABIN PAX WAS REPAIRED PER. B737-800 SRM. 53-10-51-2R PROCEDURE 7 REPAIR 7.
(LOG 2384527) DURING INSPECTION FOUND ELONGATED FASTENER HOLES AT CENTER WHEEL-WELL PANEL 193D. PANEL 193D WAS REPAIRED PER B737-800 S.R.M. 51-70-05-2R REPAIR GENERAL. PAR. 4. IN REFERENCE PER B737-800 S.R.M. 51-70-05-2R PROCEDURE 6 REPAIR 6.
(LOG 2384015) DURING INSPECTION FOUND CORROSION AT FLOOR STRUCTURE SUPPORT FROM STA 312 TO STA 328 RBL 10 CABIN PAX. FLOOR STRUCTURE SUPPORT FROM STA 312 TO STA 328 RBL 10 CABIN PAX WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 2381839) DURING INSPECTION FOUND CORROSION LEVEL 2 ON FLOOR BEAM STA 947.5 AT RBL 50 AND RBL 52, AT PASSENGER COMPARTMENT W2. FLOOR BEAM STA. 947.5 AT RBL 50 AND RBL 52 WAS REPAIRED PER. B-737-800 SRM 53-70-51-2R REPAIR 5.
(LOG 2374477) DURING INSPECTION FOUND CORROSION AT FWD/AFT SLIDE ANCHOR BRACKET (2 EA) OF L1 DOOR WET AREA. FWD/AFT SLIDE ANCHOR BRACKETS (2 EA) OF L1 DOOR WET AREA WERE REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 8848535) DURING CHECK FOUND FWD EXIT SIGN, L1 DOOR EXIT SIGN AND L1 EXT. EMERGENCY LIGHT INOP. REPLACED BATTERY PACK M01675 PER B737-AMM-33-51-06. LIGHTS OPS CHECK GOOD.
ON T/O ROLL, STRONG CHEMICAL ODOR. ROLLED TEMP SELECTOR BACK, ALL 3 LOOKED A/S INDICATOR, 100 KT. CONTINUED TAKEOFF SMELL DISSIPATED. C/W B737 FIM TASK 21-00-00-810-806 AND EVERYTHING CHECKS NORMAL. NO ODORS OR ABNORMAL READINGS USING PTRAK TOOL.
ON SHUT DOWN A STRONG ODOR WAS PRESENT. SMELLED ACCURATE AND SLOWLY DISSIPATED. FOUND COKING ON RIGHT ENGINE BLEED DUCT BEHIND INBOARD SLATS, SUSPECT TO BE SOURCE OF FUMES. REMOVED AND REPLACED BOTH RESEARCH AIR FILTERS, PER A 373 AMM 21-25. NO ABNORMAL DEFECTS NOTED. TIGHTEN THE HYDRAULIC LINE SURROUNDING DUCT, NO LEAKS NOTED AT THIS TIME.
DURING INSPECTION FOUND LEFT FORWARD OVERWING EMERGENCY LIGHT OUT. RELAMPED LH FWD OVERWING EMERGENCY LIGHT PER B737 AMM 33-51. OPS CHECK GOOD.
DURING INSPECTION FOUND PANEL MISSING FROM UNDER FUSELAGE. MAINTENANCE REPAIRED MISSING PANEL, PER ERA 587883-14.
(LOG 1258732) DURING INSPECTION FOUND SEVERAL DENTS ON AFT CARGO DOOR OUTER SKIN. AFT CARGO DOOR EXTERNAL SKIN WAS REPLACED PER B737-800 SRM 52-30-01-2R PROCEDURE 3, REPAIR 3.
(LOG 5745473) DURING INSPECTION FOUND ROW 1 OVERHEAD, BOTH L1 DOOR LIGHTS & SLIDE LIGHT INOPERATIVE. R/R M01675 BATTERY PACK PER B737 AMM 33-51. OPS GOOD.
(LOG 5745421) DURING INSPECTION FOUND EMERGENCY LIGHT COVER MISSING FROM STA 260 FWD GALLEY A/C RIGHT FLOOR AREA. REPLACED LIGHT ASSY P/N 0201924-1007, CKS OK.
(LOG 5745420) DURING INSPECTION FOUND EMERGENCY LIGHTS FROM ROW 22 AFT NOT COMING ON. REPLACED POWER SUPPLY AND BATTERY PACK, CKS OK.
L1 DOOR WILL NOT OPEN. MAINTENANCE FOUND THE LINK TO GUIDE ARM PIN BROKEN. REPLACED THE PIN AND ATTACHING HARDWARE.
DURING INSPECTION, FOUND THE LT MLG FWD TRUNNION SUPPORT FITTING CORRODED ON ALL INSIDE FACES AT BORES. REPAIRED IAW ERA 568016-14.
DURING INSPECTION, FOUND CORROSION ON THE FUSELAGE SKIN AT BS 1016, STRINGER 22L. REPAIRED IAW ERA 567371-14.
DURING INSPECTION, FOUND THE EMERGENCY LIGHT CHARGER M1671 INOPERATIVE. MAINTENANCE REMOVED & REPLACED THE CHARGER IAW AMM 33-51.
DURING INSPECTION FOUND BS 520 BL0 INTERCOSTAL ATTACH ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 (4)(B) AND (7)(D) AND DWG'S 143A5400 REV-AND 149A5510 REV A.
DURING INSPECTION FOUND AFT CARGO COMP FLOOR PANEL 140BF HAS CORROSION AROUND FASTENER HOLES. MAINTENANCE FABRICATED NEW PANEL 140BF AFT CARGO FLOOR, CORROSION OUT OF LIMITS IAW SRM 53-00-53.
DURING INSPECTION FOUND AFT CARGO PIT LT Z ANGLE LBL 22 CORRODED BS 767-9" TS BS 847. MAINTENANCE REPAIRED IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION FOUND AFT CARGO PIT, LT Z ANGLE LBL 21 HEAVILY CORRODED FROM BS 727 TO BS 747+11. MAINTENANCE REPAIRED IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION FOUND AFT CARGO COMP FLOOR PANEL 140CF HAS CORROSION AROUND FASTENER HOLES. MAINTENANCE REPLACED FLOOR PANEL IAW SRM 51-40-05 AND 53-60-53.
DURING INSPECTION FOUND AFT CARGO PIT RT FLOOR SUPPORT RAIL CORRODED AT RBL 14 AREAS MARKED BETWEEN BS 727F AND 747. MAINTENANCE REPLACED DAMAGED SECTION IAW SRM 53-00-53 REPAIR 3.
DURING INSPECTION FOUND AFT CARGO PIT, FLOOR BOARD SUPPORT CHANNEL HAS AREAS OF CORROSION FROM BS 727 TO BS 727B+3 RBL 8. MAINTENANCE REPLACED DAMAGED SECTION IAW SRM 53-00-53 REPAIR 3.
DURING INSPECTION FOUND AFT CARGO LT FLOOR SUPPORT RAIL HAS DAMAGE AT TIE DOWN BS 787 + 3" LBL 17. MAINTENANCE REMOVED DAMAGED SECTION OF AFT CARGO FLOOR SUPPORT RAIL STATION 787 + 3 LBL 17 AND REPAIRED IAW SRM 53-00-53 REPAIR 3.
DURING INSPECTION FOUND AFT CARGO FLOOR SUPPORT CHANNEL REPAIR CORRODED AT NUT PLATE LOWER SURFACE BS767+5 RBL 8. MAINTENANCE REMOVED AND INSTALLED NEW REPAIR TO AFT CARGO FLOOR SUPPORT STATION 767 +5 RBL 8" IAW SRM 53-00-53 REPAIR 2 AND ERA 492969-14MA.
DURING INSPECTION FOUND AFT CARGO PIT, FLOOR BOARD SUPPORT CHANNEL HAS AREAS OF CORROSION FROM BS 727 TO BS 727F LBL 3". MAINTENANCE REPLACED DAMAGED SECTION IAW SRM 53-00-53 REPAIR 3.
DURING INSPECTION FOUND AFT CARGO PIT RT FLOOR SUPPORT CHANNEL CORRODED AT RBL 3 AREAS MARKED BETWEEN BS 727F AND 747. MAINTENANCE REPAIRED 2 EACH AREAS IAW SRM 53-00-53 REPAIR 2.
DURING INSPECTION FOUND LT FRAME BS 807 FRAME DENTED BETWEEN S25L AND S24L. MAINTENANCE REMOVED DAMAGE ON STATION 807 FRAME BETWEEN STRINGER 25L-24L AND REPAIRED IAW PRI 551660-14 REV 0 & ERA 551660-14.
DURING INSPECTION FOUND HIDDEN DAMAGE IN AFT CARGO COMPARTMENT LEFT SIDE UNDER WASTE TANK. BS 907 STRINGER 907 STRINGER 23L TO 24L FORWARD SIDE OF FRAME CORRODED. MAINTENANCE REPAIRED FRAME IAW PRI 551665-14 REV 0 AND ERA 551665-
DURING INSPECTION FOUND CABIN RT SIDE STATION 400 BELOW STRINGER 8R FRAME CRACKED AT RAIL SUPPORT BRACKET FASTENERS. MAINTENANCE REPAIRED PER ERA C/W PRI 551669-14AD REV ORIGINAL AND 551659-14AD REV ORIGINAL.
DURING INSPECTION FOUND THE BS 727D FRAME CRACKED AT STRINGER 8R. MAINTENANCE REPAIRED THE FRAME IAW PRI 551666-14AD REV 0 AND ER/A 551666-14AD.
DURING INSPECTION, FOUND THE BS 400 STRINGER 8L FRAME CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 551668-14AD REV 0 AND ERA 551668-14AD.
DURING INSPECTION, FOUND THE BS 480 FRAME BELOW STRINGER 8R CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV 0 AND ERA 551659-14AD.
DURING INSPECTION, FOUND DAMAGE IN AFT CARGO BAY LEFT SIDE UNDER WASTE TANK BS 887 STRINGER 24L BUTT SPLICE STRAP CORRODED. MAINTENANCE REMOVED AND REPLACED BUTT SPLICE STRAP IAW SRM 51-40-02 AND DWG 147A0060 SHT 26.
DURING INSPECTION, FOUND HIDDEN DAMAGE IN AFT CARGO BAY LEFT SIDE UNDER WASTE TANK, BS 807 TO 907, STRINGER 24L FORWARD END OF STRINGER CORRODED. MAINTENANCE REPAIRED THE STRINGER IAW SRM 53-00-03 REPAIR 1.
DURING INSPECTION, FOUND AFT CARGO BAY UNDER WASTE TANK, CORROSION AT STRINGER SPLICE 24L AT BS 887. MAINTENANCE REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-40-02 AND DWG 147A3287 SHT 32 REV A.
DURING INSPECTION, FOUND CABIN RT SIDE BS 500 BELOW STRINGER 8R, FRAME CRACKED. MAINTENANCE REMOVED DAMAGE AND INSTALLED A REPAIR IAW PRI ERA 551569-14AD AND ERA 551659-14AD.
DURING INSPECTION FOUND MAIN CABIN BS 727B FRAME CRACKED AT STRINGER 8L. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A REPAIR IAW PRI ERA 551659AD REV ORIGINAL AND ER/A 551659-14AD.
DURING INSPECTION, FOUND CABIN RT SIDE BS 380 STRINGER 8R, FRAME CRACKED. MAINTENANCE REMOVED THE DAMAGED AND INSTALLED A REPAIR IAW PRI ERA 551659-14AD REV 0 AND ERA 551659-14AD.
DURING INSPECTION, FOUND BS 663 LBL 25 TO 45 VERTICAL PRESSURE WEB WITH THREE CRACKS. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10 REPAIR 3.
DURING INSPECTION, FOUND LT SIDE UNDER FLOOR AT BS 663 RBL 25 TO RBL 45 VERTICAL PRESSURE WEB HAS THREE CRACKS. MAINTENANCE REPAIRED THE VERTICAL WEB IAW SRM 57-10-10 REPAIR 3.
DURING INSPECTION, FOUND BS 727B FRAME CRACKED AT STRINGER 8R. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV ORIGINAL AND ERA 551659-14AD.
DURING INSPECTION, FOUND THE BS 480 BELOW STRINGER 8L FRAME CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV ORIGINAL AND ER/A 551659-14AD.
DURING INSPECTION, FOUND BS 440 BELOW STRINGER 8L FRAME CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV ORIGINAL AND ERA 551659-14AD.
DURING INSPECTION, FOUND BS 500F BELOW STRINGER 8R FRAME CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV ORIGINAL AND ERA 551659-14AD.
DURING INSPECTION, FOUND THE BS 747 FRAME CRACKED AT STRINGER 8L. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV. ORIGINAL AND ER/A 551659-14AD
DURING INSPECTION, FOUND THE BS 867 FRAME CRACKED AT STRINGER 8R. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV ORIGINAL AND ER/A 551659-14AD.
DURING INSPECTION, FOUND CABIN LEFT BS 440 FRAME BELOW STRINGER 8L CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV ORIGINAL AND ER/A 551659-14AD.
DURING INSPECTION, FOUND THE BS 440 FRAME, STRINGER 8R CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI ERA 551659-14AD REV O AND ERA 551659-14AD.
DURING INSPECTION, FOUND THE BS 500C FRAME, STRINGER 8R CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI 551659-14AD REV ORIGINAL AND ERA 551659-14AD.
DURING INSPECTION, FOUND THE BS 380 STRINGER 8L FRAME CRACKED. MAINTENANCE REPAIRED THE FRAME IAW PRI ERA 551659-14AD REVO AND ERA 551659-14AD.
DURING INSPECTION FOUND : AFT CARGO COMPARTMENT STATION 727G, UPPER FREE FLANGE OF FRAME, IS DENTED AT STRINGER 22L. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFT CARGO COMPARTMENT, STRINGER 22L, STATION 727G FRAME IAW PRI ERA 551663-14.
DURING INSPECTION FOUND MAIN CABIN SEAT TRACK LBL 45 HAS WEAR MARKS STA 520. MAINTENANCE REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 4.
DURING INSPECTION FOUND AFT CARGO PIT RIGHT FLOOR SUPPORT CHANNEL CORRODED AT RBL 8" AREAS MARKED BETWEEN BS 727F AND 747. MAINTENANCE REPAIRED PER ERA 492969-14MA.
DURING INSPECTION FOUND CABIN LT SIDE STATION 380 STRINGER -8L CLIP IS CRACKED. MAINTENANCE REMOVED CRACKED CLIP AT STATION 380 LT STRINGER-8L AND INSTALLED NEW CLIP AS REQUIRED REF SRM 51-40-02 STEP 4B AND BWG DWG 143A1110 REV B.
DURING INSPECTION FOUND AFT CARGO PIT FLOOR SUPPORT RAIL RBL 14 CORRODED BS 794 TO 847. MAINTENANCE REMOVED AND REPLACED RAIL FROM STATION 758-887 RBL 14 IAW DWG 146A7500 REV A.
DURING INSPECTION, FOUND THE L1 DOOR SILL MIDDLE SILL ATTACH ANGLE CORRODED. MAINTENANCE FABRICATED A NEW ANGLE AND INSTALLED IAW SRM 53-10-51, SRM 51-40-02, DWG 141A8112, SRM 51-40-05, SRM 51-20-01, AND AMM 51-21-91.
DURING INSPECTION FOUND AFT CARGO COMPARTMENT STATION 727C, UPPER FREE FLANGE IS DENTED BETWEEN STRINGERS 22L&23L. MAINTENANCE REPAIRED DAMAGED FRAME AT STATION 727C BETWEEN S22L&23L IAW ERA 551664-14.
DURING INSPECTION FOUND FLIGHT DECK FLOOR UPPER SURFACE CORRODED AFT OF CENTER PEDESTAL FORWARD OF ACCESS PANEL. MAINTENANCE FABRICATED REPAIR PARTS, TREATED AND PRIME PART AND INSTALLED IAW SRM 51-40-02, SRM 53-10-51, PG 14, AMM 51-21-73-370-808, AMM 51-21-370-804, SRM 51-70-13, AMM 20-60-07.
DURING INSPECTION FOUND LEFT FRAME BS 727J FRAME DENTED BETWEEN S23L AND S24L. MAINTENANCE REMOVED AREA DAMAGE AND REPAIR AREA PER ERA 551661-14.
DURING INSPECTION FOUND CABIN RT SIDE STATION 500B STRINGER 10R CLIP IS CRACKED. MAINTENANCE REMOVED AND INSTALLED NEW CLIP P/N 143A1010U1 REF DWG 143A1123 REV B.
DURING INSPECTION, FOUND CABIN LEFT SIDE BS 500A STRINGER CLIP S9L IS CRACKED. MAINTENANCE REMOVED AND INSTALLED A NEW STRINGER CLIP IAW DWG 143A1122 REV B.
DURING INSPECTION, FOUND L2 DOOR SURROUND CREASE BEAM ANGLE CORRODED. MAINTENANCE REMOVED AND REPLACED CORRODED CREASE BEAM IAW SRM 51-40-02 & DRAWING 147A8501 SHT 39 REV C.
DURING INSPECTION FOUND MAIN CABIN STRINGER 9L STRINGER CLIP IS CRACKED AT STATION 767. MAINTENANCE REMOVED AND REPLACED CRACKED STRINGER CLIP STRINGER 9L STATION 767 IAW DWG 146A1132 REV B AND SRM 51-40-02 PARA 4.
DURING INSPECTION FOUND FLIGHT DECK FLOOR AFT OF CENTER PEDESTAL ACCESS PANEL HAS SPOTS OF CORROSION ON UPPER SURFACE. MAINTENANCE REMOVED AND REPLACED PANEL IAW SRM 51-40-05 & SRM 51-40-02.
DURING INSPECTION, FOUND FLIGHT DECK FLOOR CAPTAIN'S SIDE UPPER SURFACE CORRODED AT RIGHT SIDE OF FORWARD INBOARD SEAT TRACK. MAINTENANCE REPAIRED IAW SRM 53-10-51 FIG 203 REPAIR 2 PG 203.
DURING INSPECTION FOUND L1 DOOR SILL INNER CREASE SILL ATTACH ANGLE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED L-1 DOOR SILL INNER CREASE CHORD SILL ATTACH ANGLE IAW SRM 51-40-02 DWG # 141A8110 REV A.
DURING INSPECTION, FOUND MAIN CABIN FLOOR SUPPORT UPPER FLANGE CRACKED BS 323 LBL 26. MAINTENANCE REPAIRED IAW SRM 53-10-51 REP. 6.
DURING INSPECTION FOUND AFT CABIN WET AREA BS 947 FLOORBEAM LBL 54" CORRODED. MAINTENANCE REPAIRED T-CAP STATION 947 LBL 54" IAW SRM 53-70-51 REPAIR 5.
DURING INSPECTION FOUND AFT CABIN WET AREA BS 986 FLOORBEAM LBL 44 FORWARD SIDE HOLE AT DOMENUT CORRODED. MAINTENANCE REPAIRED FLOOR BEAM IAW ERA 464736-14MA REV A.
DURING INSPECTION FOUND FORWARD RT NOSE EXTERNAL POWER RECEPTACLE CUT OUT AFT FLANGE IS CRACKED AT 2 EACH LOCATIONS. MAINTENANCE REPAIRED 2EA CRACKS IN FORWARD RIGHT NOSE EXT POWER RECEPTACLE CUT OUT AFT FLANGE AS REQ'D REF SRM 53-10-15 REP 4.
DURING INSPECTION FOUND AFT CABIN WET AREA BS 947 FLOORBEAM LOWER FLANGE LBL 8" TO RBL 12" AT PREVIOUS REPAIR CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND REPLACED FLOORBEAM SECTION FROM STATION 947 LBL 8 TO RBL 58.6 IAW SRM 53-70-51 REPAIR 5.
DURING INSPECTION FOUND AFT CABIN WET AREA BS 986+6" Z STIFFENER RBL 39" FORWARD SIDE HOLE AT NUTPLATE CORRODED. MAINTENANCE REMOVED AND REPLACED Z STIFFENER AT AFT CABIN WET AREA BS 986+6" RBL 39" IAW SRM 51-40-02.
DURING INSPECTION FOUND AFT CARGO PIT, FLOOR BOARD SUPPORT CHANNEL HAS AREAS OF CORROSION FROM BS 727 TO BS 727F RBL 3. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS, IDENTIFIED REPAIR AS PER ENGINEERING APPROVED PERMANENT REPAIR. ALL WORK ACCOMPLISHED IAW ENGINEERING REPAIR/AUTHORIZATION 492969-14MA; SRM 53-00-53 REPAIR 2, AMM 51-21-41 , 51-21-72 AND NDT PT6 51-00-00 PROC 23.
DURING INSPECTION FOUND AFT CARGO FLOOR SUPPORT CHANNEL REPAIR CORRODED AT NUT PLATE LOWER SURFACE BS767+5" LBL 12". MAINTENANCE REMOVED CORRODED FLOOR SUPPORT, LOCATED AND DRILLED REPAIR SPLICE, TREATED, PRIMED AND CIC'D. IDENTIFIED REPAIR PART IAW ERA 492969-14MA, SRM 51-10-02, 53-00-53, AMM 51-21-72-320-804 AND 51-21-41-370-803, 51-21-91-701.
DURING INSPECTION FOUND FORWARD PIT, AC DISTRIBUTION BAY STRINGER 28 LT CORRODED BS 540-3. MAINTENANCE REPAIRED PER ERA 14-551662.
DURING INSPECTION FOUND MAIN CABIN INTERCOSTAL UPPER FLANGE CRACKED STA 284 BL 0. MAINTENANCE REMOVED AND REPLACED MAIN CABIN INTERCOSTAL STATION 284 BL 0 IAW DWG 141A5400.
DURING INSPECTION FOUND AFT CARGO FLOOR SUPPORT CHANNEL REPAIR CORRODED AT NUT PLATE LOWER SURFACE BS 767+5" RBL 3. MAINTENANCE FABRICATED NEW REPAIR, LOCATED, DRILLED PRIMED AND INSTALLED IAW ER/A 492969-14MA, SRM 53-00-53, 51-10-02 AND AMM 51-21-72-370-804, 51-21-41-370-802 AND APPLIED CIC IAW SRM 51-21-91-620-802.
DURING INSPECTION FOUND AFT CARGO PIT LEFT FLOOR SUPPORT CHANNEL CORRODED AT LBL 3" AREAS BETWEEN BS 727F AND 747. MAINTENANCE FABRICATED NEW REPAIR CHANNEL SPLICE, LOCATED DRILLED, TREATED AND PRIMED AND INSTALLED NEW REPAIR CHANNEL SPLICE IAW SRM 53-00-53, ERA NR 492969-14MA, B737-800 AMM 51-21-41-370-802, AMM 51-21-41-370-804, AMM 51-21-91-620-802, PS 900-5-1 NR 4.
DURING INSPECTION FOUND MAIN CABIN LT CREASE BEAM WEB UPPER SURFACE CORRODED AT STATION 500H. MAINTENANCE REMOVED AND REPLACED WEB PER BAC DWG 143A5913 REV AND SRM 51-40-02.
DURING INSPECTION FOUND AFT CABIN WET AREA BS 986 FLOORBEAM RBL 44 FORWARD SIDE HOLE AT DOMENUT CORRODED. MAINTENANCE REPAIRED FLOORBEAM AT FS 986 AND REMOVED AND REPLACED DOME N/P IAW ERA 464736-14MA.
DURING INSPECTION FOUND L1 DOOR INNER CHORD CORRODED IN SEVERAL AREAS STATION 312 TO 344. MAINTENANCE INSTALLED NEW INNER CREASE CHORD P/N 654A0004-1073 ISSUE A15679, IAW SRM 51-40-05, SRM 51-40-02 & DWG 141A8110 REV E.
DURING INSPECTION FOUND R-1 DOOR CREASE CHORD CORRODED IN SEVERAL AREAS STATION 291 TO 328. MAINTENANCE REMOVED R1 INNER CHORD, INSTALLED EWIS PROTECTION, VERIFIED NEW PART IAW DWG 141A8315 REV - & A TAG A15680. LOCATED & DRILLED R1 INNER CHORD, INSTALLED R1 INNER CHORD IAW DWG# 141A8310 REV-, SRM 51-40-02.
DURING INSPECTION FOUND AFT CARGO BAY LOWER SILL WEB CORRODED BS 794 TO 847. MAINTENANCE REMOVED AND REPLACED THE WEB IAW SRM 41-40-02 AND SRM 51-40-05 AND DWG 146A8340 REV. E.
DURING INSPECTION FOUND MAIN CABIN SEAT TRACK RBL 45 GOUGED AT STATION 520. MAINTENANCE REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 4.
DURING INSPECTION, FOUND MAIN CABIN INTERCOSTAL UPPER FLANGE CRACKED BS 317 RBL 31. MAINTENANCE REMOVED CRACKED INTERCOSTAL & REPLACED IAW SRM 51-40-02 PARAGRAPH 7, 51-40-05 PARAGRAPH 4 AND DWG 141A5400 REV. - SHEETS 1-2.
DURING INSPECTION FOUND MAIN CABIN SEAT TRACK LBL24 HAS WEAR MARKS STATION 520. MAINTENANCE REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 4.
DURING INSPECTION FOUND MAIN CABIN SEAT TRACK RBL 24 GOUGED AT STATION 520. MAINTENANCE REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 4.
DURING INSPECTION FOUND RT HORIZ STAB, STAB STATION 129.5 STIFFENER FROM FORWARD EDGE, HAS CRACK AT THE BOTTOM EDGE APPROX .75" FROM BOTTOM. MAINTENANCE REPAIRED RT HORIZ STAB STIFFENER AT STAB STATION 129.5 IAW SRM 55-10-09 REPAIR 4 AND INSTALLED LOWER HORIZ STAB SKIN ACCESS DOUBLER IAW SRM 55-10-01 REPAIR 11.
DURING INSPECTION, FOUND FORWARD CARGO DOOR AFT SURROUND, SURROUND OUTER SKIN BENT OUTBD AND INBD EDGE WORN 21" ABOVE AFT BOTTOM CORNER. MAINTENANCE CUT AND REMOVED DAMAGED AREA ON FORWARD CARGO DOOR AFT SURROUND OUTER SKIN. FABRICATED REPAIR PARTS. ALODINED AND PRIMED REPAIR PARTS. INSTALLED & PAINTED REPAIR PARTS IAW SRM 53-00-01 REPAIR 24.
DURING INSPECTION FOUND EMERGENCY LIGHTS ROW 1-10 INOPERATIVE. MAINTENANCE FOUND POWER SUPPLY BAD. REPLACED POWER SUPPLY. EMERGENCY LIGHTS TEST GOOD.
DURING INSPECTION, FOUND AFT RT LAVATORY EXIT SIGN MISSING. MAINTENANCE REPLACED THE SIGN. OK FOR SERVICE.
DURING INSPECTION FOUND EMERGENCY SEAT LIGHTS OUT FROM 17 AFT. MAINTENANCE FOUND BATTERY CHARGER BREAKERS B9 AND B10 TRIPPED. RESET BREAKERS, OPS CK GOOD.
DURING TAKEOFF ROLL AT APPROXIMATELY 100 KIAS, THE TAKEOFF CONFIGURATION LIGHT AND WARNING HORN SOUNDED. CREW ABORTED TAKEOFF. MAINTENANCE FOUND PSEU FAULT T/O WARNING INHIBIT 31-550008 AND SPEEDBRAKE DN FAULT 27-62008 RECORDED. REPLACED C/B FOR TAKEOFF WARNING PRECAUTIONARY. T/S IAW FIM 31-51-00-810-809 NO DEFECT FOUND. REPLACED S651. WHILE TESTING FOUND SPEED BRAKE HANDLE BINDING AND NOT DROPPING INTO STOW DETENT. LUBED HANDLE IAW FIM 27-62-00-810-807, STEP D. PERFORMED TAKEOFF WARNING CHECKOUT IAW AMM 31-51 CHECKS OK. ACFT RETURNED TO SERVICE.
DURING FLIGHT, WHEN MOVING GEAR HANDLE TO OFF POSITION, NOSE WHEEL DROPPED FROM WHEELWELL. HAD RED & GREEN LIGHT GEAR INDICATION. ACFT RETURNED TO DEPARTURE. MAINTENANCE PERFORMED PSEU BITE, NO FAULTS NOTED. GEAR VISUAL INSPECTION, NO DAMAGE OR LEAKS NOTED. FOUND LOCK VALVE MANIFOLD AND RETRACT ACTUATOR BYPASSING. REPLACED BOTH. OPS TESTS OK, ACFT RETURNED TO SERVICE.
DURING INSPECTION, FOUND CORROSION ON ANGLE JUST INBD OF R2 DOOR AT BS 980. MAINTENANCE REPAIRED.
DURING INSPECTION, FOUND CORROSION FLOOR BULGING, RIGHT AFT LAV, JUST FORWARD OF R-2 DOOR. MAINTENANCE REPAIRED.
DURING INSPECTION FOUND WING LEADING EDGE EXTERNAL WINGLET BALLAST WEIGHT HAS CORROSION. MAINTENANCE REPAIRED PER ERA 502048-14MA.
DURING INSPECTION FOUND LT WINGLET BALLAST WEIGHT CORRODED. MAINTENANCE REPAIRED PER ERA 502048-14MA.
DURING INSPECTION FOUND RIGHT WINGLET BALLAST WEIGHT CORRODED. MAINTENANCE REPAIRED PER ERA 502048-14MA.
DURING TEST OF BATTERY PACKS FOR EMERGENCY LIGHTS, FAILED FUNCTIONAL CHECK. REPLACED BATTERY PACK IAW AMM 33-51.
DURING INPECTION, FOUND EMERGENCY EXIT SIGN AT SEAT 22 CENTER AISLE MISSING. MX INSTALLED SIGN.
WHILE ACCOMPLISHING EA12-488843-03AD, DURING PSV AD16, THE NDT INSPECTION DETECTED CRACK INDICATIONS IN A SPLICE STRAP AT BS 727B AT LBL 24.75 THE INBD AFT HOLE. NO OTHER CRACKS FOUND AN ERA ISSUED TO PREFORM TERMINATION ACTION IAW SB 737-53-1296.
FUSELAGE CABIN FLOOR STRUCTURE BS 727B SPLICE STRAP LBL 24.75 CRACKED.
DURING CHECK, FOUND EMERGENCY EGRESS LIGHTING INOP IN FIRST CLASS AISLE AND AT FORWARD EXIT SIGN. REPLACED BATTERY PACK IN POWER SUPPLY M1674.
MAIN CABIN GALLEY TIEDOWN STA 284 RBL42 INTERCOSTAL CORRODED, OUT OF LIMITS. REPLACED INTERCOSTAL. (DL738103052)
CABIN SEAT TRACK WORN AT STATION 520 LBL 45. REPAIRED PER SRM 53-00-52, ERA 486461-14, AND ERA 486466-14. (DL738103086)
CABIN SEAT TRACK AT STATION 520 LBL 24 WORN BEYOND LIMITS. REPAIRED PER SRM 53-00-52, ERA 486461-14, AND ERA 486466-14. (DL738103083)
SEAT TRACK AT STATION 520 RBL 45 WORN BEYOND LIMIT. REPAIRED PER SRM 53-00-52, ERA 486461-14, AND ERA 486466-14. (DL738103085)
CABIN SEAT TRACK AT STA 520 RBL 24 WORN BEYOND LIMITS. REPAIRED PER SRM 53-00-52, ERA 486461-14, AND ERA 486466-14. (DL738103084)
CABIN FLOOR SUPPORT AT STATION 316 LBL 6 CORRODED. REPLACED PER ERA 486463-14. (DL738103090)
RETURNED TO DEPARTURE FOR CRACKED L1 WINDOW CAPTS SLIDING. R & R CAPT`S SLIDING WINDOW IAW AMM. FUNCTIONAL AND OPS CK GOOD. R & R HEAT CONTROLLER AS PRECAUTION.
LT HORIZ STAB SKIN CONTACTED TAILDOCK. SKIN PUNCTURE AND UNDER LYING RIB BUCKLED. REPAIRED SKIN WITH DOUBLER AND RIB WITH FITTINGS AND ANGLES.
APPROX 2.5 HRS INTO FLT, FLIGHT ATTENDANT REPORTED STRONG ELEC FUMES AFT OF OVERWING EXITS. AT SAME TIME VIDEO SCREENS RETRACTED/EXTENDED ON THEIR OWN AFT OF ROW 23. VIDEO 3 C/B WAS POPPED. FLT CREW PULLED REMAINING VIDEO C/B`S AND ENTERTAINMENT C/BS. FUMES IMMEDIATELY DISSIPATED. REPLACED VIDEO DISTRIBUTION UNIT AT SEAT 20ABC.
AFT EMERGENCY FLASHLIGHT INOP. REPLACED AFT JUMPSEAT FLASHLIGHT ASSY AND BATTERY.