N377DA
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 | 2017-08-15 – 2017-08-15 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2017-08-15 – 2017-08-15 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FA AND JET BRIDGE OPERATOR UNABLE TO OPEN L1 DOOR. FOUND HANDLE MECH CONNECTION ROD DISCONNECTED. RECONNECTED ROD. OPS CHK GOOD.
(LOG 1465698) CRACK LOWER AREA ON INBOARD SKIN OF FWD GALLEY SERVICE DOOR AT PASSENGER CABIN. REPAIRED PER ER/A NO. 632463-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI REV. 2 AND PRI REV 3.
CRACK ON INTERNAL CUT OUT SKIN OF DOOR EXTERNAL POWER RECEPTACLE SETTLEMENT AREA AT FUSELAGE. INTERNAL CUT OUT SKIN DOUBLER OF DOOR EXTERNAL POWER RECEPTACLE SETTLEMENT AREA AT FUSELAGE WAS REPAIRED PER ER/A 585248-14 REV. B SECTION II: PERMANENT REPAIR AND PRI 585248-14 REV. 1.
ACCOMPLISH AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR. ACCOMPLISHED AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. SHIM WAS INSTALLED.
(LOG 1456145) LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR. ACCOMPLISHED AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. SHIM WAS INSTALLED.
SHIP 3707 -ATB- RETURNED TO JFK DUE TO PRESSURIZATION ISSUES AND NO LT DUCT PRESSURE. CORRECTIVE ACTION: REPLACED LT PRSOV SENSE LINE AND LT HPV MUSCLE AIR LINE FOR LT ENGINE BLEED ISSUE. REPLACED RT BLEED AIR REGULATOR, RT SECONDARY HEAT EXCHANGER AND RT TCV SENSE LINE FOR RT BLEED SYSTEM ISSUES. OPS NORMAL.
SHIP 3707 -DIV- DIVERTED TO JFK DUE TO IAS DISAGREE. CORRECTIVE ACTION: FOUND FIRST OFFICER'S PITOT TUBE INLET DAMAGED. REPLACED PITOT TUBE AND ADM. OPS CHECKS GOOD.
(LOG 6795742) RIGHT SIDE EMERGENCY LIGHTS L7 OVERWING AND L548 GROUND ILLUMINATION INOP. REMOVED AND REPLACED M1671 BATTERY PACK CHARGING ASSY PER B737 AMM 33-51. OPS CHECK GOOD.
(LOG 7247662) SEAT 20D EMERGENCY LIGHT INOP. FOUND CONNECTOR AT 20E UNDER IFE COVER DISCONNECTED. RECONNECTED , OPS CHECKS GOOD PER B737 AMM 33-51.
(LOG 6725316) ON S/C FOUND E-LIGHT OUT AT ROW 11. FOUND CONNECTOR LOOSE AT SIDEWALL. NOW CKS GOOD.
(LOG 5723198) DURING 3A CK, EMERGENCY LIGHT BATTERY PACK CK WORK CARD 3350-7413, FOUND BATTERY M1672 NOT HOLDING CHARGE. REPLACED BATTERY PACK M1672 PER B737 AMM 33-51, OPS CK GOOD.
(LOG 5752318) AFTER LANDING AND CLEARING RUNWAYS A PUFF OF SMOKE (HAZE) AND SMELL CAME FROM CAPT RIGHT YOKE. DONNED O2 MASKS AND RAN QRH CLEARED W/IN SECONDS WHEN COCKPIT LIGHTS TURNED OFF. REMOVED CAPT YOKE MEMORY DEVICE REF B737 AMM 33-11. REPLACED YOKE DEVICE PER B737 AMM 33-11-00. OPS CHK NML.
(LOG 5755582) ROW 11 CDE SEATS NOT IN TRACK AND LOOSE. SECURED SEAT ROW PER B737 AMM 25-22.
(LOG 0088890) EMER LIGHT SEAT 24D INOP. FOUND PIN ON ELECTRICAL CONNECTOR WIRE HARNESS LOOSE. RESECURED PIN INTO PLACE. IAW B737 AMM 33-51. OPS TEST GOOD.
(LOG 4764308) AFT RIGHT SERVICE DOOR UPPER EMERGENCY LIGHT WILL NOT ILLUMINATE DURING TEST. REF B737 WDM 33-51 FOUND CONNECTOR D40046P LOOSE IN CEILING. RESECURED SAME. NOW OPS NML.
(LOG 9413428) DURING SVC CHK FOUND LT AND RT SIDE FWD OVERWING LOWER INDICATORS INOP. FOUND L1207 EXIT INDICATOR LIGHT SHORTED. R/R L1207 EXIT INDICATOR ASSY IAW B737 AMM 33-51 AND POWER SUPPLY FUSE IAW B737 AMM 33-51. OPS CHK GOOD.
(LOG 9413431) ON SVC CK FOUND RED ISLE FWD GALLEY EMERGENCY LIGHT INOP. FOUND GALLEY PLUG DISCONNECTED. CONNECTED RED ISLE FWD GALLEY EMERGENCY LIGHT AIRFRAME SIDE CONNECTOR. OPS CHK GOOD IAW B737 AMM 33-51.
(LOG 9413421) DURING INSPECTION FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. R/R DOOR EXIT LIGHT ASSY PER B737 AMM 33-51.
(LOG 2735300) DURING INSPECTION FOUND L2 DOOR INNER SKIN IS CRACKED. REPAIRED L2 DOOR INNER SKIN IAW ER/A 607752-14 REV ORIG.
(LOG 2724295) DURING INSPECTION FOUND E&E BAY RH DOOR CUTOUT WEB GOUGED. FABRICATED REPLACEMENT WEB IAW BOEING 737-800 SRM 51-40-05. INSTALLED REPLACEMENT WEB IAW BOEING 737-800 SRM 51-40-02.
(LOG 2721314) DURING INSPECTION FOUND FLOOR SUPPORT ANGLE STA 500D-500E CHAFED. REPAIRED FLOOR BEAM (SUPPORT) AT STA 500D-500E LH IAW BOEING 737-800 SRM 53-00-53-2R-2.
(LOG 2719923) DURING INSPECTION FOUND FUSELAGE / STA 500C FRAME OVERSIZED HOLE AT LBL 25. REPAIRED FRAME PER ERA 607791-14.
(LOG 2719807) DURING INSPECTION FOUND FWD CARGO L/H FLOOR TRANSITION PLATE STA 480 - STA 500 HAS EVIDENCE OF CORROSION AT UPPER SIDE. FABRICATED & INSTALLED NEW REPLACEMENT TRANSITION PLATE STA480-500 L/H IAW BOEING 737-800 SRM 51-4-05, 51-40-02, 51-20-01 & SOPM 20-41-02.
(LOG 2719796) DURING INSPECTION FOUND FWD CARGO R/H FLOOR TRANSITION PLATE STA 500F- STA 500I HAS EVIDENCE OF CORROSION AT UPPER SIDE. FABRICATED REPLACEMENT SECTION OF AND INSTALLED R/H TRANSITION PLATE STA 500F - 500I IAW BOEING 737-800 SRM 51-40-05, 51-40-02.
(LOG 2719779) DURING INSPECTION FOUND BAFFLE AT STA LH 500A-500B IS DAMAGED. REMOVED AND REPLACED BAFFLE IAW B737-800 SRM 51-40-02-0G.
(LOG 2719264) LH FWD CARGO SIDEWALL BEAM STA 500C ANGLE SUPPORT BARCKETS BETWEEN BEAM AND BELOW FLOOR TRANSITION PLATE UPPER FWD MOUNTING FASTENER NOT INSTALLED CORRECTLY. REPAIRED FRAME AT STA 500C LBL25 IAW DELTA ER/A 607791-14 REV ORIG.
(LOG 2719815) DURING INSPECTION FOUND FWD CARGO STA 500C L/H INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW B737-800 SRM 51-4-002-0G.
(LOG 2719799) DURING INSPECTION FOUND FWD CARGO R/H FLOOR TRANSITION PLATE STA 500A-STA 500F HAS EVIDENCE OF CORROSION AT UPPER SIDE. FABRICATED REPLACEMENT SECTION AND INSTALLED FOR R/H TRANSITION PLATE STA 500A - 500F IAW BOEING 737-800 SRM 51-40-05, 51-40-02.
(LOG 2719793) DURING INSPECTION FOUND FWD CARGO L/H FLOOR TRANSITION PLATE STA 500- STA 500 I HAS EVIDENCE OF CORROSION AT UPPER SIDE. REMOVED, FABRICATED & INSTALLED NEW REPLACEMENT TRANSITION PLATE STA 500-500I L/H IAW BOEING 737-800 SRM 51-40-05, 51-40-02, 51-20-01 & SOPM 20-41-02.
(LOG 2719776) DURING INSPECTION FOUND FWD CARGO STA 500D L/H INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW B737-800 SRM 51-40-02-0G.
DURING INSPECTION FOUND AFT CARGO LH FLOOR TRANSITION STRIP STA 790-807 HAS EVIDENCE OF CORROSION AT UPPER SIDE. REMOVED & REPLACED LH AFT PIT TRANSITION PANEL STA 790-807 IAW BOEING 737-800 SRM 51-40-02.
(LOG 2712694) DURING INSPECTION FOUND AFT CARGO LH FLOOR TRANSITION STRIP STA 727G-790 HAS EVIDENCE OF CORROSION IN MULTIPLE SPOTS AT UPPER SIDE. REMOVED & REPLACED LH AFT PIT TRANSITION PANEL STA 727G-790 IAW BOEING 737-800-SRM 51-40-02.
(LOG 2709991) DURING INSPECTION FOUND BREAK PANEL AT STA 540 BL0 TO RBL 22 IS CRACKED. REMOVED & REPLACED BREAK PANEL ASSY IAW BOEING 737-800 SRM 51-40-02.
(LOG 2708748) DURING INSPECTION FOUND AFT CARGO L/H TRANSITION STRIP STA 727B - 727G HAS EVIDENCE OF CORROSION IN MULTIPLE SPOTS AT UPPER SIDE. REMOVED AND REPLACED AFT PIT L/H TRANSITION PANEL STA 727B-727G IAW BOEING 737-800 SRM 51-40-02.
(LOG 2705414) DURING INSPECTION FOUND HORZ STAB MANUAL CHAIN DISCONNECTED AT SPROCKET ON FWD MECHANISM. RECONNECTED HORZ STAB MANUAL CHAIN AT SPROCKET ON FWD MECHANISM IAW B737-800 AMM 27-41-41-400-801. OPS TEST STABILIZER MANUAL TRIM & TRIM INDICATOR GOOD IAW B737-800 AMM 27-41-00.
(LOG 2705243) DURING INSPECTION FOUND AFT CARGO RH TRASITION PLATE STA 727G-767 IS CORRODED. REMOVED AND REPLACED RH AFT CARGO TRANSITION PLATE STA 727G-767 IAW BOEING 737-800 SRM 51-40-02.
(LOG 2705232) DURING INSPECTION FOUND AFT CARGO RH TRANSITION PLATE STA 727B-727G IS CORRODED. REMOVED AND REPLACED TRANSITION PLATE STA 727B-727G IAW BOEING 737-800 SRM 51-40-02.
(LOG 2703573) DURING INSPECTION FOUND FUSELAGE / STA 559 FRAME CRACKED AT S-8L. REPAIRED DAMAGE PER ERA 607302-14AD.
(LOG 2701689) DURING INSPECTION FOUND WEB AT STA 420-440 STR 26R HAS ELONGATED FASTENER HOLES. REMOVED AND REPLACED WEB IAW BOEING 737-800 SRM 51-40-02.
(LOG 2701778) DURING INSPECTION FOUND FLOOR BEAM STA 328 IS CORRODED AROUND NUTPLATE HOLES RBL 15 TO RBL 55. REPAIRED FLOOR BEAM STA328 RBL15 TO RBL55 IAW DELTA ERA 606989-14.
(LOG 2701748) DURING INSPECTION FOUND STA 540 STR 27L IS CORRODED. REPAIRD STR 27L AT STA 540 IAW BOEING 737-800 53-00-03-2R-1.
(LOG 2701665) DURING INSPECTION FOUND R-1 MOP SEAL CORRODED IN NUMEROUS AREAS AT PREVIOUS BLENDOUTS. REMOVED AND REPLACED MOP SILL CHORD IAW BOEING 737-800 SRM 51-40-02.
(LOG 2701649) DURING INSPECTION FOUND FLOOR INTERCOSTAL CORRODED AROUND FASTENER HOLES STA 294.5 TO 312 LBL 12. REMOVED AND REPLACED FLOOR INTERCOSTAL STA 294.5 TO 312 IAW BOEING 737-800 SRM 51-40-02.
(LOG 2696999) DURING INSPECTION FOUND LH FUSELAGE FRAME AT STA 559 IS CRACKED AT AC RAIL BRACKET BETWEEN STR 8-9. REPAIRED LH FRAME AT STA 559 BETWEEN STR 8-9 FOR AC RAIL BRACKET SUPPORT IAW ER/A 607302-14 & DELTA WORK CARD 2526-01236-02A.
(LOG 2696095) DURING INSPECTION FOUND L-1 DOOR AFT GIRT BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR MOUNT TIEDOWN ATTACH FITTING IAW BOEING 737-800 SRM 51-40-02.
(LOG 2695677) DURING INSPECTION FOUND FWD CARGO PIT RH TRANSITION PLATE STA 420-440 UPPER SIDE IS CORRODED. REMOVED AND REPLACE TRANSITION PLATE RH STA 420-440 IAW BOEING 737-800 SRM 51-40-02.
(LOG 2694208) DURING INSPECTION FOUND L-1 DOOR LOWER JAMB MOP SEAL CHORD EXFOILATED. REMOVED AND REPLACED L-1 MOP SEAL CHORD IAW BOEING 737-800 SRM 54-40-02.
(LOG 2694208) DURING INSPECTION FOUND L-1 DOOR LOWER JAMB MOP SEAL CHORD EXFOILATED. REMOVED AND REPLACED L-1 MOP SEAL CHORD IAW BOEING 737-800 SRM 54-40-02.
DURING INSPECTION FOUND CABIN AFT WET STA 986 FLOOR FRAME UPPER CAP CORRODED LBL0-LBL45. REPAIRED STA 986 FLOORBEAM BETWEEN LBL0-LBL45. REPAIRED STA 986 FLOORBEAM BETWEEN LBL0-LBL45. "SUPPLEMENTAL INFO 10/10/24 OKC REPAIRED PER SRM 53-70-51-2R6 REF WORKCARD 5300-2303 1021117-2000/0229".
LOG (2684766) DURING INSPECTION FOUND LH SEAT TRACK 44.5 O/B LANDING IS DAMAGED. REPAIRED SEAT TRACK IAW BOEING 737-800 SRM 53-00-52-2R-4.
(LOG 2681437) DURING INSPECTION FOUND RH FRAME STA 727B IS CRACKED AT I/B HOLE FOR BIN SUPPORT BRACKET. REPAIRED RH FRAME AT STA 727B AT BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.
(LOG 2681477) DURING INSPECTION FOUND RH FRAME STA 867 IS CRACKED AT I/B FASTENER HOLE FOR BIN SUPPORT BRACKET. REPAIRED FRAME AT STA 867 BETWEEN STR 8 & 9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.
(LOG 2681513) DURING INSPECTION FOUND R/H FRAME STA 727D IS CRACKED AT I/B FASTENER HOLE FOR BIN SUPPORT BRACKET. REPAIRED RH FRAME STA 727D BETWEEN STR 8-9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.
(LOG 2681714) DURING INSPECTION FOUND L/H FRAME STA 727D IS CRACKED AT BIN SUPPORT BRACKET. REPAIRED FRAME STA 727D BETWEEN STR 8-9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02A.
(LOG 2681754) DURING INSPECTION FOUND LH STA 907 FRAME IS CRACKED AT BIN SUPPORT. REPAIRED LH FRAME STA 907 BETWEEN STR 8-9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-03A.
(LOG 2681490) DURING INSPECTION FOUND RH FRAME STA 827 IS CRACKED AT I/B FASTENER HOLE FOR BIN SUPPORT BRACKET. REPAIRED RH FRAME AT STA 827 BETWEEN STR 8 - 9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.
(LOG 2678420) DURING INSPECTION FOUND FLOOR PANEL 241ABF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 241ABF AND REPLACED INSERTS IAW B737-800 SRM 53-0050-2R -9 REPAIR 9 AND SRM 53-0050-2E-0 REP GEN PARA 5.
(LOG 2678332) DURING INSPECTION FOUND FLOOR PANEL 221EF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221EF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678349) DURING INSPECTION FOUND FLOOR PANEL 222DF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 222DF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678371) DURING INSPECTION FOUND FLOOR PANEL 221 GF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221 GF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678384) DURING INSPECTION FOUND FLOOR PANEL 241YZ/ZF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 241YF/ZF AND REPLACED INSERTS IAW B737-800 SRM 53-00-50 -2R-9 REPAIR 9 AND SRM 53-00-50-2R-6 PARA 3.
(LOG 2678394) DURING INSPECTION FOUND FLOOR PANEL 241ADF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 241ADF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678396) DURING INSPECTION FOUND FLOOR PANEL 242UF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 242UF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678404) DURING INSPECTION FOUND FLOOR PANEL 241AAF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 241AAF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678408) DURING INSPECTION FOUND FLOOR PANEL 221CF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221CF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678415) DURING INSPECTION FOUND FLOOR PANEL 221BF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221BF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678316) DURING INSPECTION FOUND FLOOR PANEL 221EF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221EF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678424) DURING INSPECTION FOUND FLOOR PANEL 221DF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221DF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678426) DURING INSPECTION FOUND FLOOR PANEL 221FF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221FF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678439) DURING INSPECTION FOUND FLOOR PANEL 241AEF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 241AEF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-80-50-2R-0 REP GEN PARA 5.
(LOG 2678449) DURING INSPECTION FOUND CORROSION 231AF PANELS. REPAIRED 231AF AND REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9 & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678458) DURING INSPECTION FOUND FLOOR PANEL 222CF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 222CF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678499) DURING INSPECTION FOUND FLOOR PANEL 242VF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 242VF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678508) DURING INSPECTION FOUND FLOOR PANEL 242TF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 242TF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678432) DURING INSPECTION FOUND FLOOR PANEL 222BF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 222BF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678432) DURING INSPECTION FOUND FLOOR PANEL 222BF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 222BF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678475) DURING INSPECTION FOUND FLOOR PANEL 241XF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 241XF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9, & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678516) FLOOR PANEL 241YF & REPLACED INSERTS IAW B737-800SRM 53-00-50-2R-9 REPAIR 9 & SRM 53-00-50-2R-0.
(LOG 2678504) DURING INSPECTION FOUND FLOOR PANEL 221AF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 221AF AND REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9 AND SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678491) DURING INSPECTION FOUND FLOOR PANEL 242SF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 242SF & REPLACED INSERTS IAW B737-800SRM 53-00-50-2R-9 REPAIR 9 & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678487) DURING INSPECTION FOUND FLOOR PANEL 242VF FWD HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 242CF & REPLACED INSERTS IAW B737-800SRM 53-00-50-2R-9 REPAIR 9 & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678481) DURING INSPECTION FOUND FLOOR PANEL 222AF HAS CORRODED INSERTS AND DELAMINATION. REPAIRED 222AF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9 & SRM 53-00-50-2R-0.
(LOG 2678465) DURING INSPECTION FOUND FLOOR PANEL 241ZF HAS CORRODED INSERTS AND DELAMANITION. REPAIRED 241ZF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9 & SRM 53-00-50-2R-0 REP GEN PARA 5.
(LOG 2678479) DURING INSPECTION FOUND CABIN FLOOR PANEL 231ACF HAS 2 BROKEN INSERTS AND FASTNER HOLE DAMAGE. REPAIRED 231ACF & REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-9 REPAIR 9 & SRM 53-00-50-2E-0 REP GEN PARA 5.
(LOG 2676977) DURING INSPECTION FOUND FLOOR BEAM STA 344 CORRODE LBL 10. REPAIRED FLOOR BEAM STA 344 IAW BOEING 737-800 SRM 53-10-51-2R-8.
(LOG 2675365) DURING INSPECTION FOUND AFT CARGO R/H FLOOR TRANSITION STRIP STA 676-787 HAS BLOWN HOLES AND CORROSION. REMOVED AND REPLACED AFT CARGO R/H SHIELD ( TRANSITION STRIP) AT STA 767-787 IAW BOEING 737-800 SRM 51-40-02.
(LOG 2672245) DURING INSPECTION FOUND CABIN AFT WET STA 947 FLOOR FRAME UPPER CAP CORRODED AT LBL 48-LBL 54. REMOVED DAMAGE AND REPLACED T CHORD IAW BOEING 737-800 SRM 53-70-51-2R-5.
DURING INSPECTION FOUND CORROSION ON LAV EXHAUST VENT. STARTED FABRICATION OF REPAIR PARTS AND LAYUP. DOUBLER AND TRIPLER TO FINAL SIZE PER B737 SRM 53-70-01-2R-3-3 491375. TREATED AND PRIMED REPAIR PARTS INSTALLED FILLER WASHERS. OK TO INSTALL REPAIR REF B737 SRM 53-70-01-2R-3. INSTALLED DOUBLER/TRIPLER REPAIR IAW B737 SRM 53-70-01-2R REPAIR 3 SECTION 47 . PRIMED AND PAINTED. ACCOMPLISHED SEC II PERMANENT REPAIR OF ERA 605112-14 REV"B" PER B737 SRM 57-70-01-2R PROCEDURE 3 REPAIR 3.
(LOG 9881261) DURING INSPECTION FOUND EMERGENCY LIGHTS AFT OF L/H O/W EXIT NOT WORKING. REPLACED EMERGENCY LIGHTS BATTERY AT L/H STA 727C PER B737 AMM 33-51.
DURING INSPECTION FOUND LT INTERIOR OVERWING EXIT EMERGENCY LIGHTS INOP. FOUND BATTERY PACK INOP. R&R LT BATTERY PACK FOR LT OVERWING EXIT. OPS CHECK OK.
(LOG 9712318) CREW NOTICED OILY FUMES, SLIGHT ODOR, WHEN OPERATING PACKS OFF APU. FOUND APU COMBUSTOR DRAIN CLOGGED. CLEANED DRAIN ORIFICE PER B737 AMM 49-55. R/R BOTH RECIRC FAN FILTERS PER B737 AMM 21-25.
(LOG 2435784) REPORTS OF OIL SMELL IN CABIN FROM UNKNOWN SOURCE AT DEPARTURE. FOUND APU OIL COOLER CONTAMINATED. R/R SAME PER B737 AMM 49-91. LK CK OK. R/R RECIRCULATION FILTERS PER B737 AMM 21-25.
(LOG 9271896) ON SVC FOUND BURNING SMELL IN FLT DECK WITH APU BLEED ON. FOUND DEBRI IN PLENUM. R/R RECIRC FAN FILTERS IAW B737 AMM 21-25. RAN ENGINES WITH PACKS AND NO ODOR WAS DETECTED. AIR CONDITIONING OPS CHECK GOOD IAW B737 AMM 21-00.
(LOG 8863496) DURING INSPECTION FOUND 2 EMERGENCY LIGHT BATTERY PACKS AT FWD CEILING PANEL PER B737 AMM 33-51. OPS CHECK GOOD.
SHIP 3707 -DE/MISC- AFTER LANDING CREW ADVISED BOTH ENGINES AND APU FIRE WARNINGS ILLUMINATED. AIRCRAFT WAS MET BY FIRE DEPARTMENT WITH NO SIGNS OF FIRE OR SMOKE. AIRCRAFT GATED UNDER ITS OWN POWER. CORRECTIVE ACTION: REPLACED ENGINE AND APU FIRE DETECTION UNIT AND FIRE CONTROL PANEL. OPS CHECKS GOOD.
(LOG 7443008) DURING INSPECTION FOUND CABIN EMERGENCY LIGHT AT SEAT CD 4 FLOOR LIGHTING INOPERATIVE. FOUND DISCONNECTED WIRES ON CONNECTOR UNDER SEAT 4CD. RESECURED WIRES INTO CONNECTOR PER BOEING CHAP 20 SWPM, LIGHT OPS CK NORMAL.
SHIP 3707 - DIV- TO PHL FOR A SMOKE EVENT. FLIGHT ATTENDANTS REPORTED A SMOKE SMELL IN THE CABIN. CORRECTIVE ACTION: C/W NO-GO TASKS - FOUND AFT DOOR HEATER FAILED - FORWARD TO MEL. REPLACED AFT DOOR HEATER PER AMM.
(LOG 1486395) DURING INSPECTION FOUND CRACK ON DENTED AREA OF LEFT AFT INBD FLAP LOWER SURFACE 11 FROM OUTBD EDGE AND 5.5 FROM TRAILING EDGE. REPAIR PARTS WERE BONDED ON LEFT AFT INBD FLAP LOWER SURFACE 11 FROM OUTBD EDGE AND 5.5 FROM TRAILING EDGE PER B737-800 S.R.M. 51-70-10-2R AND B737-800 S.R.M. 57-53-01-2R-4.
(LOG 1486450) DURING INSPECTION FOUND GOUGE WAS FOUND IN DENT # 32 ON LOWER SKIN OF INBOARD AFT FLAP AT LH WING. LOWER SKIN OF INBOARD AFT FLAP AT LH WING WAS REPAIRED PER B737-800 S.R.M. 51-70-10-2R AND B737-800 S.R.M. 57-53-01-2R-4.
(LOG 1486388) DURING INSPECTION FOUND CRACK FOUND ON DENT NO 35 WITH 0.600 OF LENGTH ON LOWER SKIN OF INBOARD AFT FLAP AT LH WING. LOWER SKIN OF INBOARD AFT FLAP AT LH WING WAS REPAIRED PER B737-800 S.R.M. 51-70-10-2R AND B737-800 S.R.M. 57-53-01-2R-4.
(LOG 1485967) DURING INSPECTION FOUND CRACKS ON INTERNAL PRODUCTION DOUBLER AT EXTERNAL PWR RECEPTACLE CUT OUT. CRACKS ON INTERNAL PRODUCTION DOUBLER AT EXTERNAL PWR RECEPTACLE CUT OUT WAS REPAIRED PER ETI-37-20-310 REV.1 AND ER/A 585248-14.
(LOG 1477712) DURING INSPECTION FOUND WEAR ON INTERCOSTAL WEB LH SIDE CUT OUT FRAME ACCESS DOOR E/E COMPARTMENT. WEB LH WAS REPLACED PER B737-800 SRM 53-10-15 AND 51-40-02.
SHIP 3707 PROTUDING FASTENER ON EXTERNAL FUSELAGE SKIN ON STA 727I+2" AND S-8LH . CORRECTIVE ACTION: REPLACED THE BLIND FASTENERS WITH SOLID RIVET AS FOLLOWS PER B737-800 SRM 53- 00-01-2R-41 PAR 6 B (3) AND DEFERRED. (1478798).
SHIP 3707 INITIAL INSPECTION: WEAR ON INTERCOSTAL WEB RH SIDE CUT OUT FRAME ACCESS DOOR E/E COMPARTMENT . CORRECTIVE ACTION: E/E COMPARTMENT WAS REPLACED PER B737-800 SRM 53-10-15- FIG 3 AND B737-800 SRM 51-40-02-0G PAR 4 AND 7. (1479023).
DURING INSPECTION FOUND LEFT OVERWING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51. OPS TEST OK.
SHIP 3707 - ATO - UPON ADVANCEMENT OF THROTTLES, RIGHT ENGINE ROLLED BACK & SHUT DOWN. CORRECTIVE ACTION: MAINTENANCE REPLACED THE N2 SPEED SENSOR & EEC. AIRCRAFT RETURNED TO SERVICE.
(LOG 5452485) DURING INSPECTION FOUND AFT EMERGENCY LIGHT NOT WORKING. R+R AFT LEFT EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.
(LOG 5452472) DURING INSPECTION FOUND SEAT MOUNTED EMERGENCY LIGHTS AT ROW 16DE TO 18DE INOPERATIVE. REPLACED POWER SUPPLY BATTERY, REF. AMM 33-51. OPS CHECKS GOOD.
(LOG 5452443) FND BATTERY PACK AND POWER SUPPLY BAD AT AFT RIGHT ABOVE GALLEY. R/R PER AMM 33-51 OPS CHKS GOOD.
FWD LEFT EMERGENCY FLASHLIGHT BATTERY FOUND DEAD DURING PREFLIGHT. REPLACED FWD LEFT EMERGENCY FLASHLIGHT BATTERY PACK PER AMM 25-64. OPS CHECK GOOD.
DURING INSPECTION, FOUND FORWARD CARGO BAY LEFT ZEE ANGLE FROM BS 500 - 500I HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW SRM 53-00-53 AND SRM 51-40-02.
DURING INSPECTION, FOUND FORWARD CARGO BAY LEFT ZEE ANGLE AT BS 480 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW SRM 53-00-53 AND SRM 51-40-02.
DURING INSPECTION, FOUND THE FORWARD CARGO BAY CARGO TRACK AT BS 500I, LBL 19 CORRODED. CUT AND REMOVED THE CARGO TRACK. FABRICATED AND INSTALLED A NEW CARGO TRACK AND SPLICE IAW SRM 51-10-02, 57-00-53 AND 53-00-53, REPAIR 3.
DURING INSPECTION, FOUND PASSENGER CABIN FLOORBEAM BS 986, RBL 35 - 45 CORRODED. MAINTENANCE REPAIRED THE FLOORBEAM IAW ERA 464736-14MA.
DURING INSPECTION, FOUND FWD CARGO BAFFLE ANGLE CRACKED AT BS 500H FWD SIDE ABOVE STRINGER 26L. MAINTENANCE REMOVED AND REPLACED BAFFLE ANGLE IAW DWG 143A2505 AND IAW SRM 51-40-02.
DURING INSPECTION, FOUND PASSENGER CABIN FLOOR SUPPORT BS 986+2, RBL 45 SHEAR WEB UPPER SURFACE CORRODED. MAINTENANCE REMOVED AND REPLACED IAW DWG 147A5700 AND SRM 51-40-02.
DURING INSPECTION, FOUND PASSENGER CABIN BS 986+2, RBL 45 SHEAR WEB UPPER SURFACE CORRODED. REMOVED AND REPLACED THE SHEAR WEB IAW DWG 147A5700 AND SRM 51-40-02.
DURING INSPECTION, FOUND THE PASSENER CABIN FLOORBEAM BS 986, RBL 45 - 35 CORRODED. REPAIRED THE FLOORBEAM IAW ERA 464736-14MA.
DURING INSPECTION, FOUND FORWARD CARGO BAY AFT BULKHEAD LT SIDE PANEL SUPPORT ANGLE CORRODED. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW SUPPORT ANGLE IAW SRM 51-10-02, 51-40-02, AND 53-00-53.
DURING INSPECTION, FOUND AFT PASSENGER CABIN FLOOR STRUCTURE RIGHT SIDE BS 947 TO 992 R2 DOOR CREASE BEAM CORRODED.
DURING INSPECTION, FOUND AFT PASSENGER CABIN CREASE BEAM BS 947 TO 992 CORRODED. REMOVED AND REPLACED THE CREASE BEAM IAW DWG 147A8501 REV C, AND SRM 51-40-02.
DURING INSPECTION, FOUND FORWARD CARGO BAY RT ZEE ANGLE FROM BS 500G - 500I CORRODED. REPAIRED THE ANGLE IAW SRM 53-00-53, REPAIR 5.
DURING INSPECTION, FOUND THE RIGHT HORIZONTAL STAB LOWER RIB AT HSS 92.7 AND 21 INCHES AFT OF FORWARD SPAR CRACKED. REPAIRED THE RIB IAW PRI 553125-14, REV O, AND ER/A 553125-14.
DURING INSPECTION, FOUND THE FORWARD CARGO BAY RIGHT ZEE ANGLE FROM BS 500A - 500F CORRODED. REPAIRED THE ANGLE IAW SRM 53-00-53, REPAIR 5.
DURING INSPECTION, FOUND FUSELAGE FRAME BS 500A BELOW STRINGER 8R CRACKED. REPAIRED THE FRAME IAW PRI 553124-14AD.
DURING INSPECTION, FOUND THE L2 DOOR CREASE BEAM IS CORRODED. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM IAW SRM 51-40-02 AND DWG 147A8540 REV C.
DURING INSPECTION, FOUND FUSELAGE FRAME, BS 480 BELOW STRINGER 8L CRACKED AT STOWBIN LOWER RAIL TO FRAME ATTACHMENT. MAINTENANCE REPAIRED THE FRAME IAW PRI 553120-14AD.
DURING INSPECTION, FOUND FUSELAGE FRAME BS 440 BELOW STRINGER 8R CRACKED. REPAIRED THE FRAME IAW PRI 553120-14AD.
DURING INSPECTION, BS 986, LBL 44 FLOORBEAM CORRODED. REPAIRED THE FLOORBEAM IAW ERA 464736-14MA.
DURING INSPECTION, FOUND FUSELAGE FRAME BS 380 BELOW STRINGER 8L CRACKED. REPAIRED THE FRAME IAW PRI 553120-14AD.
DURING INSPECTION, FOUND FUSELAGE FRAME BS 400 BELOW STRINGER 8R CRACKED. REPAIRED THE FRAME IAW PRI 553120-14AD.
DURING INSPECTION FOUND FWD CARGO BAFFLE CRACKED STATION 500F-500G STRINGER 26R. MAINTENANCE REMOVED AND REPLACED BAFFLE AT STATION 500F-500G STRINGER 26R IAW SRM 51-40-02 AND DWG 143A7505.
DURING INSPECTION FOUND FORWARD CARGO COMPARTMENT AT RT RAIL AT STATION 500I RBL 15 HAS AREAS OF CORROSION. MAINTENANCE REPLACED NEW RAIL STATION 410-500I RBL 15 IAW DWG 143A7501 AND IAW SRM 51-40-02.
DURING INSPECTION, FOUND FUSELAGE FRAME BS 480 BELOW STRINGER 8R CRACKED AT STOWBIN LOWER RAIL TO FRAME ATTACHMENT. MAINTENANCE REPAIRED THE FRAME IAW ERA 553119-14AD.
DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK RBL 45, BS 727A PLUS 7 TO 727A PLUS 14 WORN ON CROWN. REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 2.
DURING INSPECTION, FOUND THE RT HORIZONTAL STAB LOWER RIB AT HSS 92,7 AND 30 INCHES AFT OF FORWARD SPAR CRACKED. REPAIRED IAW SRM 55-10-04, REPAIR 4.
DURING INSPECTION FOUND FWD CARGO COMPARTMENT AT RT RAIL STATION 500I RBL 15 HAS AREAS OF CORROSION. MAINTENANCE REPLACED NEW RAIL STATION 410-500I RBL 15 IAW DWG 143A7501 IAW SRM 51-40-02.
DURING INSPECTION, FOUND EXTERNAL FUSELAGE SKIN HAS PULLED RIVETS AND BULGING SKIN AT BS 360+8 TO +13 STRINGER 26L. MAINTENANCE REPAIRED THE SKIN IAW ERA 553117-14 REV O.
DURING INSPECTION, FOUND FUSELAGE FRAME BS 400 BELOW STRINGER 8L CRACKED AT STOWBIN LOWER RAIL TO FRAME ATTACHMENT. MAINTENANCE REPAIRED THE FRAME IAW ERA 553119-14AD.
DURING INSPECTION, FOUND FUSELAGE FRAME BS 440 BELOW STRINGER 8L CRACKED AT STOWBIN LOWER RAIL TO FRAME ATTACHMENT. MAINTENANCE REPAIRED THE FRAME IAW ERA 553119-14AD.
DURING INSPECTION, FOUND AFT PASSENGER CABIN BS 947 LBL 52 FLOORBEAM CORRODED AROUND LAVATORY MOUNT FITTING. MAINTENANCE REPAIRED THE FLOORBEAM FROM LBL 7 - 60 IAW SRM 53-70-51 REPAIR 5.
DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK RBL 24 STATION TO STAB 727B PLUS 9 TO STATION 727B PLUS 15 HAS CORROSION ON BASE AND CROWN. MAINTENANCE FABRICATED, LOCATED, AND DRILL REPAIR SEAT TRACK SECTION, ANGLES AND STRAPS TREAT, PRIME AND INSTALLED THEM IAW SRM 53-00-52 REPAIR 5.
DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK RBL 24 BS 727B + 9 TO BS 727B + 15 HAS CORROSION ON THE BASE AND CROWN. MAINTENANCE FABRICATED , LOCATED, AND DRILL A REPAIR. INSTALLED IAW SRM 53-00-52, REPAIR 5.
DURING INSPECTION FOUND FWD CARGO COMPARTMENT STATION 500B TO 500C STRINGER 26R BAFFLE CRACKED AT AFT SIDE ATTACH ANGLE. MAINTENANCE INSTALLED NEW BAFFLE IAW DWG 193A7505 SHEET 16 REV B.
DURING INSPECTION FOUND UPPER FUSELAGE VERTICAL STABILIZER ACCESS PANEL TO FUSELAGE SKATE ANGLE CORRODED O/B OF VERTICAL STAB FWD ATTACH BOLT BS 1016. MAINTENANCE REMOVED AND REPLACED UPPER FUSELAGE VERTICAL STABILIZER ACCESS PANEL TO FUSELAGE SKATE ANGLE O/B OF VERTICAL STAB FWD ATTACH BOLT BS 1016 TO 1016-10" RBL 13" IAW SRM 51-40-02.
DURING INSPECTION, FOUND THE NR 2 ENGINE SAIL TAIL LOWER ATTACH SURFACE FOR HEAT DEFLECTOR CORRODED. MAINTENANCE REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 313A2700.
DURING INSPECTION FOUND AFT CARGO PIT LOWER DOOR SILL WEB HAS AREAS OF CORROSION BS 794 TO BS 874 RBL 28. MAINTENANCE REMOVED AND REPLACED AFT CARGO LOWER SILL WEB BS 794-874 RBL 28 IAW DWG 146A8123 REV C & SRM 51-40-02.
DURING INSPECTION, FOUND PASSNEGER CABIN FLOOR SUPPORT BS 307 LBL 11 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SECTION 7 AND DWG 141A5600, REV N.
DURING INSPECTION FOUND FWD PIT THRESHOLD TIE DOWN CLOSE OUT PLATE CORRODED. MAINTENANCE RECEIVED NEW 453A1611-26 PLATE , IAW DWG 453A1600 REV- TO BE INSTALLED ON WORK ORDER 35178/1400/0033 AN+MDS 5320-0455.
DURING INSPECTION FOUND AFT CARGO PT SIDEWALL ATTACH ANGLE IS DAMAGED AT BS 727I AT S25R TO S24R. MAINTENANCE FABRICATED NEW SIDEWALL ATTACH ANGLE IAW W/O 35181-1600-0001. LOCATED AND DRILLED IAW 51-40-05. TREATED PRIMED IAW 51-20-01 INSTALLED SIDEWALL ATTACH ANGLE IAW DWG 146A1243.
DURING INSPECTION FOUND AFT CARGO PIT FLOOR SPLICE T CORRODED AT FASTENER HOLES BS 887. MAINTENANCE REPLACED NEW "T" SPLICE ON AFT CARGO IAW SRM 51-40-05-0G-0.
DURING INSPECTION FOUND CRACK IN FUSELAGE SKIN AT BS 540, 2ND FROM TOP AFT, OPENED FASTENER HOLE BETWEEN STRINGER 22R AND STRINGER 23R. MAINTENANCE REPAIRED IAW AND WORK ACCOMPLISHED ON WORK CARD 5331-01257-10.
DURING INSPECTION FOUND AFT CARGO COMPARTMENT FWD BULKHEAD STATION 727 LBL 25 BULKHEAD PANEL SUPPORT ANGLE IS BENT AT FLOOR. MAINTENANCE REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE IAW SRM 51-40-05 & SRM 51-40-02.
DURING INSPECTION, FOUND PASSENGER CABIN FLOOR SUPPORT BS 307, LBL 11 HAS CORROSION AROUND TWO FASTENER HOLES. MAINTENANCE REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 SECTION 7 & DWG 141A5600 REV N.
DURING INSPECTION, FOUND AFT CARGO BAY FLOOR SUPPORT HAS AREAS OF CORROSION BS 827 TO 794, RBL 14. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 3.
DURING INSPECTION FOUND AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767 TO 794 . REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 5.
DURING INSPECTION FOUND AFT CARGO PIT FLOORBOARD Z ANGLE HAS CORROSION AT BS 737 TO BS 794 AT S25R. MAINTENANCE REMOVED AND REPLACED NED Z ANGLE ON AFT CARGO RT FRM STA 727G-767 IAW SRM 53-00-53 REPAIR 5 .
DURING INSPECTION FOUND FWD CARGO COMPARTMENT AFT BULKHEAD LOWER ANGLE HAS MULTIPLE AREAS OF CORROSION. MAINTENANCE INSTALLED NEW BULKHEAD LOWER ANGLE ON FWD CARGO IAW SRM 51-40-02-0G PAGE 2 PARA 4.
DURING INSPECTION,M FOUND THE AFT CARGO BAY FLOOR SUPPORT HAS AREAS OF CORROSION AT BS 727G-1 - 787+10 AT STRINGER 25L. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION, FOUND PASSENGER CABIN FLOOR SUPPORT AT LBL 45 BS 320 CRACKED. MAINTENANCE REPLACED THE FLOOR SUPPORT BS 320-300 IAW SRM 51-40-02 AND DWG 141A5400, REV 0.
DURING INSPECTION, FOUND THE FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM BS 420 - 440 AFT END HAS A CRACK. MAINTENANCE REPLACED THE SIDEWALL SUPPORT IAW SRM 51-40-02-0G & DWG 143A0080 REV. A.
DURING INSPECTION FOUND AFT CARGO PIT LOWER FLOOR BOARD TO FWD BLKD U CHANNEL DAMAGED AT BS 727+4" 0BL. MAINTENANCE REPLACED AFT CARGO FWD FLOOR BOARD CHANNEL IAW DWG 453A2611 REV F P/N 453A2611-25 INSTALLED ON CARD 5320-0150.
DURING INSPECTION, FOUND AFT CARGO BAY FLOOR SUPPORT HAS CORROSION AT BS 767 TO 794 AT AT STRINGER 25R. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 5.
DURING INSPECTION, FOUND AFT CARGO BAY FLOOR SUPPORT HAS NUMEROUS AREAS OF CORROSION FROM BS 727 TO 727G, STRINGER 25L. MAINTENANCE REPLACEDTHE FLOOR SUPPORT IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION, FOUND AFT CARGO BAY FLOOR SUPPORT HAS AREAS OF CORROSION AT BS 847 - 787+10 AT STRINGER 25L. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION FOUND FWD CARGO COMPARTMENT AFT OF THE DOOR RT FLOOR TO CEILING ANGLE AT STATION 5000+13 HAS CRACK. MAINTENANCE INSTALLED NEW ANGLE IAW DWG 143A0080 REV AND SRM 51-40-02.
DURING INSPECTION FOUND FWD CARGO COMPARTMENT DOOR SILL WEB IS CORRODED. MAINTENANCE REMOVED AND REPLACED SILL WEB IAW DWG 143A8330 REV A AND SRM 51-40-02 SECTION 5.
DURING INSPECTION FOUND AFT CARGO PIT FLOOR Z ANGLE HAS NUMEROUS AREAS OF CORROSION LT SIDE FROM BS 727 TO BS 727G+1" S25L. MAINTENANCE REMOVED AND REPLACED Z CHANNEL IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION FOUND AFT CARGO PIT FLOORBOARD Z ANGLE HAS AREAS OF CORROSION AT BS 847 TO787+10 AT S25L. MAINTENANCE REMOVED AND REPLACED Z CHANNEL IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION FOUND AFT CARGO PIT FLOOR BOARD Z ANGLE HAS AREAS OF CORROSION AT BS 727G-1 TO BS 787+10 AT S25L. MAINTENANCE REMOVED AND REPLACED Z CHANNEL IAW SRM 53-00-53 REPAIR 5.
DURING INSPECTION FOUND L2 DOOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE FOUND BATTERY POWER PACK M1673 AT FAULT. R&R BATTERY POWER PACK FUSE PER AMM 33-51-06. OPS CKS OK.
DURING INSPECTION, FOUND EMERGENCY ESCAPE LIGHTS INOPERATIVE AT 2D, 11D, AND 18D. MAINTENANCE REPLACED THE LAMP AT 2D AND 18D IAW AMM 33-51 CHECKED AND REPLACED SEAT HARNESS AT SEAT 11D IAW AMM 33-51. CHECKED GOOD.
DURING FLIGHT, WHILE AT FL380, RECEIVED CABIN ALT WARNING LIGHT AND WARNING HORN. LT BLEED DUCT PRESSURE 40 PSI. RT BLEED DUCT PRESSURE 0 PSI. DESCENDED AND MASKS DID NOT DEPLOY. ACFT DIVERTED. MAINTENANCE FOUND CIRCUIT BREAKER B7 ON THE P6-4 PANEL OUT. INSPECTED NR 2 PRSOV AND PERFORMED TASK AMM 36-00-00-860-804. OPS CHECKS OK, ACFT RETURNED TO SERVICE.
AFTER TAKEOFF THE PILOT MOVED THE GEAR HANDLE PAST THE OFF POSITION. THE GEAR DOOR WAS HEARD TO ACTUATE. MAINTENANCE PERFORMED SPEED CONDITION INSPECTION IAW AMM 05-51-47. FOUND WHEEL WELL AFT BODY FAIRING PANEL DAMAGED. REMOVED PANEL AND UNDERLYING DAMAGE REQUIRES BRACE ASSY REPLACEMENT MAIN GEAR DOOR INNER ADDED TO CDL, REF LOG 7807799. REMOVED AND INSTALLED BRACE ASSY WING TO BODY FAIRING SUPPORT STRUCTURE LT SIDE IAW SRM 53-40-71 ABD AMM 53-51-21, OK FOR SVC.
MAINTENANCE COMPLIED WITH VA 90146 FOR ASSOCIATED AA 2500-01777.
MAINTENANCE COMPLIED WITH VA 90134MA, REV A FOR ASSOCIATED AA 2520-01919.
MAINTENANCE COMPLIED WITH VA REV IR FOR AA 2340-01075.
MAINTENANCE COMPLIED WITH VA 90138MA, REV IR ASSOCIATED AA 2520-01937.
MAINTENANCE COMPLIED WITH VA90132 MA, REV A FOR ASSOCIATED AA 2330-01337.
DURING INSPECTION, FOUND LT MLG WHEEL WELL FORWARD BULKHEAD STA 663 HAS 2" CRACK AT LBL 40", 6" DOWN FROM PRESSURE DECK. MAINTENANCE REMOVED DAMAGED WEB IAW SRM 57-10-10-10, REPAIR 3, FIG 204, MACHINED REPAIR DOUBLER AND FABRICATED REPAIR PARTS IAW SRM 57-10-10, REPAIR 3. INSTALLED AND COMPLETED REPAIR IAW SRM 57-10-10, REPAIR 3. ACCOMPLISHED PRESSURIZATION CHECK. CHECK GOOD IAW AMM 31-31-00.
DURING INSPECTION, FOUND RT MLG WHEEL WELL FORWARD BULKHEAD STA 663 HAS 1" CRACK AT RBL 40", 6" DOWN FROM PRESSURE DECK. MAINTENANCE REMOVED DAMAGED WEB IAW SRM 57-10-10, REPAIR 3, FIG 204. MACHINED REPAIR DOUBLER AND FABRICATED REPAIR PARTS IAW SRM 57-10-10, REPAIR 3. INSTALLED AND COMPLETED REPAIR IAW SRM 57-10-10, REPAIR 3. ACCOMPLISHED PRESSURIZATION CHECK IAW AMM 21-31-00.
MAINTENANCE COMPLIED WITH VA 90132MA, REV B FOR ASSOCIATED AA 2330-01337.
MAINTENANCE COMPLIED WITH VA 90135MA, REV IR ASSOCIATED AA 2520-01938.
DURING INSPECTION FOUND AFT LT F/A SEAT UPPER ATTACH FRAME CRACKED. MAINTENANCE REPAIRED AFT LT F/A SEAT UPPER ATTACH FRAME IAW SRM 51-70-11.
DURING INSPECTION, FOUND LT HORIZONTAL STABILIZER LOWER SKIN HAS TWO CRACKS ON LOWER SKIN STAB STA 129.5 17" AND 25" FROM FRONT SPAR. MAINTENANCE REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN IAW SRM 55-10-01 REPAIR II.
DURING INSPECTION FOUND RT WING T/E CAVITY BETWEEN NR 7 AND NR 8 SPOILERS LOWER SURFACE SEAL RETAINER CHANNEL IS CRACKED AT CUTOUT. MAINTENANCE REMOVED RT WING T/E SEAL RETAINER CHANNEL BETWEEN NR 7 & NR 8 SPOILERS LOWER SURFACE. REPLACED WITH NEW PART IAW DWG 115A3700, REV B, SHEET 6.
DURING INSPECTION, FOUND THE CABIN SEAT TRACK CROWN CORRODED BS 520, RBL 45. MAINTENANCE R & R THE SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND THE CABIN SEAT TRACK CROWN CORRODED BS 520, LBL 25. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND CABIN SEAT TRACK CROWN IS CORRODED BS 520, RBL 25. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK CROWN IS CORRODED BS 520, LBL 45. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK AT BS 500A +2 RBL 25 IS GOUGED. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION FOUND CABIN SEAT TRACK CROWN IS FRETTED AND GOUGED, BS 538. LBL 45. MAINTENANCE R & R SEAT TRACK BETWEEN BS 537 - 563 IAW SRM 53-00-52, REPAIR 3.
DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK AT BS 540, RBL 45 IS GOUGED. MAINTENANCE R & R SEAT TRACK BETWEEN BS 537 - 563 IAW SRM 53-00-52, REPAIR 3.
DURING INSPECTION, FOUND R1 DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY IAW AMM 33-51. OPS TEST OK.
DURING INSPECTION, FOUND EMERGENCY EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY IAW AMM 33-51. OPS TEST OK.
DURING TEST, FOUND BATTERY PACK, M1675, FAILED FUNCTIONAL TEST. MAINTENANCE R & R M1675 BATTERY PACK WITH SERVICEABLE UNIT IAW AMM 33-51-06. OPS TEST OK.
DURING ACCOMPLISHMENT OF EA 12-488843-03AD, FOUND DAMAGED FASTENER HOLES AT FS 737B AT LBL45.50, RBL 24.75 & RBL 45.50. DAMAGED HAS BEEN REPAIRED IAW ERA 513776-14.
DURING EMERGENCY LIGHT TEST FOUND LIGHTS AT R1 DOOR AND FIRST CLASS SEATS INOPERATIVE. REPLACED BATTERY PACK AND TEST OK.
DURING EMERGENCY LIGHT FUNCTION CHECK FOUR PACKS FAILED TEST. REPLACED BATTERIES M1670, M1671, M16702, M1673, M1674, M1676, M1694, M1695 AND TESTS OK.
PSV-14 AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB CORRODED. REPLACED WEB IAW SRM 51-40-02 AND BOEING DWG 146A8340, N/R 632619.
AFT CARGO COMPT STA 787 TO 887 RBL 14 TIEDOWN TRACK CORRODED. REMOVED AND REPLACED TRACK WITH NEW SECTION IAW 51-40-05 AND 51-40-02.
FWD CABINS FLOORBEAM HAS CORROSION STA 274 RBL 13. REPAIRED IAW ER/A 491215-14.
AFT CARGO PIT FLOOR SUPPORT AT STA 727D+6 RBL 3 HAS LIGHT CORROSION NEAR FASTENER HOLES. REPAIRED FLOOR SUPPORT BS 727D+6 RBL 3 IAW ER/A 492942-14 REV ORIG.
FUSELAGE DENTS (3) AT STATION 388 ABOVE STR 17L AND 390 ABOVE 17L. REPAIRED DENTS IAW ERA 491218-14 ORIGINAL.
AFT CARGO COMPARTMENT FLOOR PANEL 140 AF HAS MULTIPLE CORROSION SPOTS. REPLACED PANEL.
R-1 DOOR CREASE BEAM CORRODED FROM STA 294 TO 332. REPLACED CREASE BEAM AT R-1.
PS-14 AFT CARGO COMPARTMENT FLOOR STRUCTURE BS 887 PANEL SPLICE STRAP CORRODED. FABRICATED AND INSTALLED NEW SPLICE STRAP IAW SRF 53-00-53 FIG 103 SRM 51-40-02 AND SRM 53-60-53 PG 5.
AFT FLOORBEAM STA 986.5 RBL 30-38, CORROSION AROUND FASTENER HOLE. REPAIRED FLOORBEAM STA 986.5 IAW ERA 491216 AND 464736-14MA NR 632611.
THE L-1 WINDOW CRACKED DUE TO WINDOW HEAT OVERHEATING. MX REPLACED THE NR1 WINDSHIELD IAW AMM TASK 56-11-11 000-801 AND ACCOMPANING WINDOW HEAT CONTROL UNIT IAW 30-41-11-401. PERFORMED TEST OF WINDSHIELD AND WINDSHIELD HEAT CONTROL UNIT AND ALL CHECKS GOOD. ACFT IS OK FOR SERVICE.
NBR 2 ENG INFLT SHUTDOWN DUE TO OIL BYPASS AND HIGH VIBS. DIVERTED AND DECLARED EMERGENCY. ONCE ON GRD FOUND METAL ON MID AND AFT CHIP DET AND FAN SEIZED. REQ ENG CHG. ETOPS CATEGORY 'C': UNCOMMANDED PWR CHANGES, SURGES,OR STALLS.
AT FL350 LOST BOTH A/PS AND BOTH F/AS ; NO VNAV INFO IN FMS; A/THROTTLES INOP. REPLACED TAT PROBE. TAT PROBE INDICATION NORMAL. PERFORMED DFCS OPS TEST AND LAND VERIFY TEST. ALL TEST GOOD. PERFORMED ADIRU TEST. ADIRU TEST GOOD. PERFORMED FMC OPS TEST. FMC OPS TEST GOOD. AUTOTHROTTLE BITE TEST GOOD.
UPON APPLICATION OF T/O THRUST LOST NOSE WHEEL STEERING. REGAINED CONTROL AFTER THROTTLES RETARDED. INSPECTED ALL GEAR AND HARDWARE. PERFORMED OPN CK OF NOSE GEAR STEERING. PERFORMED HIGH SPEED TAXI CK. ALL CKS OK.
AFT CARGO DOOR LIGHT AND MASTER CAUTION LIGHT CAME ON DURING TAKEOFF ROLL. DISCONTINUED TAKEOFF AT 105 KTS. INSPECTED SENSORS AND DOOR.