N396DA
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 | 2015-06-30 – 2015-06-30 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2015-06-30 – 2015-06-30 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
SEAT 1 A,B AISLE AREA EMERGENCY LIGHT INOP UNDER OVERHEAD BIN INOP. FOUND PLUG D11088 AND D11344 DISCONNECTED. RECONNECTED PLUG, EMER LIGHTS TEST GOOD PER B737 AMM 33-51. (LOG 8925502 - AIRCRAFT WAS GROUNDED).
SEAT 10D,E,F EMERGENCY LIGHT INOP. R/R HARNESS PER B737 AMM 33-51. OPS NORMAL. (LOG 8925503 - AIRCRAFT WAS GROUNDED).
SHIP 3726 -SMK/DE- DECLARED EMERGENCY DUE TO REPORTED SMOKE ODOR IN COCKPIT. CORRECTIVE ACTION: ODOR FROM L2 WINDOW TERMINAL AREA LOWER AFT CORNER OF WINDOW. TURNED WINDOW HEAT OFF AND FORWARD WINDOW HEAT TO MEL AND PLACARD.
(LOG 7005415) EXTERIOR SLIDE ILLUMINATION EMERGENCY LIGHTS INOP AT RT AFT OVER WING DOOR AND RT SIDE OF FUSELAGE AFT OF WING ROOT. REMOVED AND REPLACED BATTERY PACK AT M1671 PER SAME AMM. LIGHTS CAME ON FULL BRIGHT, OPS CHECK GOOD.
(LOG 6144034) GREY SMOKE FROM THE FORWARD GALLEY OVEN. OVEN UNPLUGGED AND CIRCUIT BREAKER PULLED. SMOKE DISIPATED. R+R FWD OVEN IAW B737 25-31. OPS CHECK GOOD.
(LOG 0498845) CHECK FOR CORRECT CONFIGURATION OF THE OVERWING EXIT DOORS LOWER EXIT SIGNS. T/S PER B737 WDM 33-51-21. FOUND SIDEWALL PANELS SWAPPED OVER. SWAPPED PANELS TO CORRECT POSITION AND VERIFIED ALL CONNECTIONS IN PROPER POSITIONS. PERFORMED OPS CHK EMERGENCY LTS. AS PER B737 AMM 33-51.OPS NML.
(LOG 6190858) EMERGENCY EXIT FLOOR LEVEL SIGN MISSING AT ROW 18 FAA FOUND IT. CEILING MOUNTED EMERGENCY EXIT SIGN INSTALLATION NORMAL PER B737 IPC 33-51-01-17 SHEET 1 ITEM B. OK FOR SVC.
SHIP 3726 -ATO- APPROX. 120KTS DUE TO LEFT AFT DOOR INDICATION DURING TAKEOFF. CORRECTIVE ACTION: CHECKED DOOR RIG, NO TROUBLE FOUND. ADJUSTED L2 DOOR INDICATION SENSOR. OPS CHECKS GOOD.
(LOG 9587657) FA'S OBSERVED BURNING SMELL IN FIRST CLASS UPON ARRIVAL. PERFORMED GENERAL INSP OF FIRST CLASS AREA GALLEY AREA NO UNSUAL ODOR NOTED. INPS'D ADV MASTER CONTROL UNIT. POWERED & ALL INDICATION GREEN. SUSPECT DOOR HEATER. REPLACED DOOR HEATER ON LOG PAGE 9587660 PER B737 AMM 21-45. RMD& RPLCD RECIRC FILTER PER B737 AMM 21-45.
(LOG 0388392) DURING INSPECTION OF THE BS 706 UPPER FRAME PER DELTA WORK CARD # 2526-01236-01A (AD 2009-01-02 / SB 737-25-1544, REV 3), CRACK WAS FOUND ON THE FRAME WEB (PN 144A1128-1) AT THE AIR CONDITIONING SUPPORT BRACKET ATTACHMENT HOLES, BETWEEN STR 8L AND STR 9L. MAINTENANCE REPAIRED CRACK PER ERA 618232-14AD.
(LOG 0388637) FUSELAGE FRAME CRACKED AT BS 706, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. C/W ER/A 618232-14AD.
(LOG 0388439) FOUND SKIN TO BE BLENDED AROUND REMOVED FASTNER AND OVER STR 1 FASTENER AT STA500C. C/W ER/A 618414-14.
(LOG 0388434) FOUND TOOLING DAMAGE ON EXTERNAL SKIN AROUND REMOVED FASTNER HOLE AT STA344, LBL5.5.
(LOG 0386609) CORROSION AT FLOOR BEAM STA 986.5 RBL45 TO LBL45 WL 208 MULTILE AREAS. C/W ER/A 618227-14 REV ORIGINAL.
(LOG 0386826) DURING HCK AT ATS-MCI, MULTIPLE LIGHTNING STRIKES SRM 53-00-01 REPAIR 38 CATEGORY C REPAIRS WERE LOCATED. REPAIRS WE ACCOMPLISHED PER ER/A 618414-14.
(LOG 0385898) DENT ON SLAT #7 UPPER SURFACE LOCATED 33" FROM I/B SIDE AND 1.5" FROM T/E. REPAIRED DENT ON #7 SLAT UPPER SURFACE LOCATED 33" FROM I/B EDGE AND 1.5 FROM T/E PER B737 SRM 51-70-10-2R-4.
(LOG 0381721) FLOOR BEAM HAS TOOL MARKS AT STA 380 RBL 24 TO LBL 24 WL 208. C/W ER/A 618163-14 REV ORIGINAL.
(LOG 0379822) RH MIDDLE SLIDE EMERGENCY LIGHT INOP. REPLACED LIGHT ON THE R/H MIDDLE SLIDE EMERGENCY I.A.W B737 AMM 33-51-04-960-801. OPS CHECK GOOD.
(LOG 0381513) FUSELAGE FRAME CRACKED AT BS 827, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381696) FRAME @ STA 500A AT STG 8R A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-02B.
(LOG 0381546) FRAME @ STA 400 AT STG 8R A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-02B.
(LOG 0381515) FUSELAGE FRAME CRACKED AT BS 727B, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381531) FUSELAGE FRAME CRACKED AT BS 400, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381521) FUSELAGE FRAME CRACKED AT BS 500A, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381519) FUSELAGE FRAME CRACKED AT BS 500D, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381518) FUSELAGE FRAME CRACKED AT BS 500F, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381714) FRAME @ STA 480 AT STG 8R A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-04B.
(LOG 0381500) FRAME @ STA 380 AT STG 8L A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381494) FRAME @ STA 440 AT STG 8L A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381709) FRAME @ STA 440 AT STG 8R A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-04B.
(LOG 0381705) FRAME AT R/H STA 380 A/C RAIL BRACKET CRACKED. REPAIRED PER WORK CARD 2526-01236-02B.
(LOG 0381699) FRAME @ STA 867 AT STR 8R A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-02B.
(LOG 0381507) FUSELAGE FRAME CRACKED AT BS 867, S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER. REPAIRED PER WORK CARD 2526-01236-02A.
(LOG 0381698) FRAME @ STA 727B AT STG 8R A/C RAIL BRACKET IS CRACKED. REPAIRED PER WORK CARD 2526-01236-02B.
(LOG 0375213) AFT CARGO DOOR THRESHOLD WEB HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED DAMAGED AFT CARGO THRESHOLD WEB WITH NEW PART IAW B737-800 SRM 51-40-02-0G AND DWG 146A8340.
(LOG 0376530) DENT ON AFT CARGO COMPARTMENT LOWER SILL WEB STA 794-847 RBL 21 WL 156. REMOVED AND REPLACED AFT CARGO COMPARTMENT LOWER SILL WEB STA 794-847 RBL 21 WL 156 WITH NEW ITEM# 146A8123Y10 IAW B737 SRM 51-40-02-0G AND DRAWING# 146A8121.
(LOG 0368846) R/H STAB LOWER SKIN IS CRACKED AT SS101. REMOVED CRACK DAMAGE AND REPAIRED RH STAB LOWER SKIN PER B737 SRM 55-10-01-2R PROCEDURE 11 REPAIR 11.
(LOG 0383478) AFT CARGO R/H ZEE CORRODED BS 727 TO 747. REMOVED AND REPLACED R/H ZEE CHANNEL DAMAGED STA. 727-747 IAW B737-800 SRM 51-40-02-OG, AND BOEING DWG. 146A7500.
(LOG 0374970) AFT CARGO DOOR FWD SHIELD IS CORRODED IN SEVERAL PLACES. REMOVED AND INSTALLED NEW AFT CARGO DOOR FWD SHIELD IAW B737-800 SRM 51-40-02-0G AND DWG 146A8127.
(LOG 0368278) FWD CARGO COMPARTMENT R/H FLOOR BAFFLE STA 500G-500F CRACKED. R/H FLOOR BAFFLE STA 500G WAS REMOVED, LATER A NEW ONE WAS INSTALLED PER B737 SRM 51-40-02-OG.
(LOG 0375009) CORROSION AT FORWARD CARGO BAY L/H ZEE CHANNEL FROM STA 500D-500G STR 26L. REMOVED AND REPLACED L/H ZEE CHANNEL STA 400-500I STR 26L IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG 143A7500.
(LOG 0375054) CORROSION ON UNDERSIDE OF AFT CARGO COMPARTMENT AFT SHIELD STA 847-867. REMOVED AND REPLACED AFT CARGO CORMPARMENT AFT SHIELD STA 847 TO 867 RBL 21 WL 165 IAW B737-800 SRM 51-40-02-0G AND DWG 146A0081 REV A.
(LOG 0374986) AFT CARGO FLOOR SUPPORT STRAP FROM BS 787 TO BS 855, RBL 20, WL 160 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED AFT CARGO STRAP TO STA 767+4 TO 847+14 RBL 20 WL 160 IAW B737-800 SRM 51-40-02-0G AND DWG 146A8120 REV B.
(LOG 0364518) CORROSION AFT CARGO FLOOR RAIL AT BS 787 + 6" TO BS 827 +12, RBL 14, WL 163. WEB REMOVED AND REPLACED AFT CARGO FLOOR RAIL AT BS 787+6" TO BS 827+12", WL 163 IAW B737 SRM 51-40-02-0G AND FINALLY APPLIED CIC IAW B737 AMM 51-21-91-620-802.
AIRCRAFT 3726, CORROSION LEVEL 2 MOP SILL AT STA 326 TO STA 331 RBL 56 WL 208 MULTIPLE AREAS. CPRRECTIVE ACTION: EVALUATED DAMAGE ON MOP SILL AT STA 326 TO STA 331 RBL 56 WL 208 FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-10-15-01-02 AND 53-10-15-1A-2 REMOVED AND REMPLACED MOP SILL AT STA 270 TO STA 360 RBL 56 WL 208 IAW B737 SRM 51-40-02-0G AND DWG 141A8310 REV D. (LP 0361418)
AIRCRAFT 3726, CRACK AT L/H WING FUEL TANK STR-9U REINFORCEMENT END, WSTA-617+21.5. CORRECTIVE ACTION: PERFORMED REPAIR OF L/H WING FUEL TANK STR-9 @WSTA 617+21 PER ER/A 618214-14 REV. ORIGINAL DECAL MONITOR CREATED ASSOCIATED ER/A 14-618214. (LP 0360027)
(LOG 0363236) OVERSIZED HOLE INTERCOSTAL AT STA 312 TO 328 LBL 45 WL 208. REMOVED AND REPLACED INTERCOSTAL AT STA 312 TO 328 LBL 45 WL 208 PER B737 SRM 51-40-02-0G AND DWG# 141A5400.
(LOG 0363230) FORWARD CARGO BAY BAFFLE DAMAGED AT STA 500H STR 26R FWD SIDE. REMOVED AND REPLACED FWD CARGO BAY BAFFLE AT STA 500H - 500G STR 26R ITEM# 143A7510-22 IAW B737 SRM 51-40-02-0G DRAWING# 143A7505 REV B.
(LOG 0363216) CORROSION ON AFT CARGO COMPARTMENT LOWER SILL WEB STA 767-787 RBL 21 WL 156. REMOVED AND REPLACED AFT CARGO COMPARTMENT LOWER SILL WEB STA 767-787 RBL 21 WL 156 ITEM# 146A8123U19 IAW B737 B737 SRM 51-40-02-0G DRAWING# 146A0081 REV A.
(LOG 0363209) AFT CARGO L/H ZEE CORRODED BS 727 TO BS 827. REMOVED AND REPLACED AFT CARGO LH ZEE CHANNEL STA 727 TO 847 WITH ITEM# BAC1496-377#7075T62 IAW B737 SRM 51-40-02-0G-0, DRAWING# 146A7500 REV C.
(LOG 0363170) MULTIPLE TOOL MARKS AT FLOOR BEAM STA 328 RBL10 TO RBL 49 WL 208. PERFORMED REPAIR ON FLOOR BEAM UPPER CHORD FROM RBL 1 TO RBL 60 PER B737 SRM 53-10-51-2R.
(LOG 0363180) CORROSION AT MOP SILL AT STA 947 TO STA 986 LBL 56 WL 208 MULTIPLE AREAS. REMOVED AND REPLACED MOP SILL DAMAGED AT STA 947 TO 986 LBL 56 WL 208 PER B737-800 SRM 51-40-02- AND DWG 147A8501.
(LOG 0363266) CORROSION AT FLOOR SUPPORT STA 294.5 TO STA 312 RBL 11 WL 208. REMOVED AND REPLACED FLOOR SUPPORT FROM STA 294.5 TO STA 312 RBL 11, WL 208 PER B737 SRM 51-40-02-0G DWG# 141A5400.
(LOG 0363242) WASTE TANK ENCLOUSE BULKHEAD CLIP CRACKED STA 867 LBL 17 WL 156. REMOVED AND REPLACED AFT CARGO WASTE TANK ENCLOSURE BULKHEAD CLIP ITEM# 149A8109U114 IAW B737 SRM 51-40-02-0G DRAWING# 149A8102.
(LOG 0364521) GOUGE DAMAGE ON SEAT TRACK FROM STA 520 LBL 25 LH. REMOVED AND REPLACED EXISTING REPAIR SECTION SEAT TRACK BTW STA 490-520 LBL 25 IAW B737-800 SRM 53-00-52-2R. REPAIR 4.
(LOG 0363206) CORROSION MOP SILL AT STA 947 TO STA 986 RBL 56 WL 208 MULTIPLE AREAS. MOVED AND REPLACED MOP SILL DAMAGED AT STA 947 TO 986 RBL 56 WL 208 PER B737-800 SRM 51-40-02-0G AND DWG 147A8501.
(LOG 0362885) GOUGE DAMAGE ON SEAT TRACK FROM STA 520 LBL 45 LH. REMOVED AND REPLACED EXISTING REPAIR SECTION SEAT TRACK BTW STA 490-520 LBL 45 IAW B737-800 SRM 53-00-52-2R REPAIR 4.
AIRCRAFT 3726, FWD CARGO COMPARTMENT L/H FLOOR BAFFLE STA 500F-500G CRACKED. CORRECTIVE ACTION: REMOVE AND REPLACE FWD CARGO COMPARTMENT L/H FLOOR BAFFLE STA 500F-500G IAW B737 BOEING DWG# 143A7505 AND B737 SRM 53-30-53-2R. (LP 0361453)
(LOG 0363187) FWD CARGO COMPARTMENT L/H FLOOR BAFFLE STA 500E-500F CRACKED. REMOVED & REPLACED FWD CARGO L/H FLOOR BAFFLE @ STA 500E - STA 500F IAW BOEING DWG# 143A7505 REV: - & B737 SRM 51-40-05-0G & 51-40-02-0G.
(LOG 0363273) CORROSION*** FLOOR SUPPORT STA 312 TO STA 328 LBL 11 WL 208. REMOVED AND REPLACED FLOOR SUPPORT FROM STA 312 TO STA 328 LBL 11 WL 208 PER B737 SRM 51-40-02-0G AND DWG# 141A5400.
(LOG 0363191) FWD CARGO COMPARTMENT L/H FLOOR BAFFLE STA 500D-500E CRACKED. REMOVED & REPLACED FWD CARGO L/H FLOOR BAFFLE @ STA 500D - STA 500E IAW BOEING DWG# 143A7505 REV: A & B737 SRM 51-40-05-0G & 51-40-02-0G.
(LOG 0363276) CORROSION AT FLOOR SUPPORT STA 328 TO STA 344 LBL 11 WL 208. REMOVED AND REPLACED FLOOR SUPPORT FROM STA 328 TO STA 344 LBL 11, WL 208 PER B737 SRM 51-40-02-0G AND DWG# 141A5400.
AIRCRAFT 3726, INTERCOSTAL STA 947-967 RBL 50 WL 208 EXISTING MIS-DRILLED FASTENER HOLE. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL AND ANGLE CLIPS DAMAGED AT STA 947-967 REBL 50 WL 208 PER B737-800 SRM 51-40-02-0G AND DWG 147A5650 REV. A J. (LP 0361352)
AIRCRAFT 3726, CORROSION LEVEL 2 AT FORWARD CARGO BAY DOOR THRESHOLD WEB. CORRECTIVE ACTION: REPLACED FWD CARGO BAY DOOR THRESHOLD WEB IAW B737 SRM 51-40-02-0G, 51-40-05-0G AND BOEING DRAWING# 143A8330 REV: A. (LP 0356992)
AIRCRAFT 3726, CORROSION AT INTERCOSTAL STA 947.5+4 RBL36 WL 208 MULTILE AREAS. CORRECTIVE ACTION: REPLACED DAMAGED SUPPORT INTERCOSTAL STA 947.5+4 RBL 36 WL 208 PER B737-800 SRM 51-40-02-0G AND DWG 147A5650 REV. A. (LP 0355434)
AIRCRAFT 3726, CORROSION LEVEL2 AT FLOOR SUPPORT STA 312 TO STA 328 RBL 11 WL 208. CORRECTIVE ACTION: REPLACED FLOOR SUPPORT FROM STA 312 TO STA 328 RBL 11, WL 208 PER B737 SRM 51-40-02-0G AND DWG# 141A5410. (LP 0356980)
AIRCRAFT 3726, CORROSION LEVEL 2 FOUND ON FLOOR BEAM UPPER CHORD @STA. 947.5, RBL 45. CORRECTIVE ACTION: REMOVED DAMAGED SECTION OF FLOOR BEAM STA 947.5 RBL 38- RBL 63 ON UPPER CHORD, REPAIRED FLOOR BEAM PER B7373-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5 ALTERATIVE 2. (LP 0361361)
AIRCRAFT 3726, CORROSION LEVEL 2 AT FLOOR SUPPORT STA 947.5 TO STA 967 LBL50 WL 208 MULTIPLE AREAS. CORRECTIVE ACTION: EVALUATED DAMAGE FOUND CORROSION ON MULTIPLE AREAS FLOOR SUPPORT STA 947.5 TO STA 967 LBL 50 WL 208 FOUND TO BE OUT OF LIMITS IAW B737 SRM 51-10-02-0G STEP 9 REPLACED FLOOR SUPPORT IAW B737-SRM 51-40-02-0G AND DWG 147A5650 REV- E. (LP 0356976)
AIRCRAFT 3726, CORROSION LEVEL 2 AT INTERCOSTALL STA 947.5+4 LBL34 WL 208 MULTIPLE AREAS. CORRECTIVE ACTION: EVALUATED DAMAGE FOUND CORROSION ON MULTIPLES AREAS INTERCOSTAL STA 947.5+4 LBL 34 WL 208 FOUND TO BE OUT OF LIMITS IAW B737 SRM 51-10-02-0G STEP REPLACED INTERCOSTAL IAW B737 SRM 51-40-02-0G AND DWG 147A5650. (LP 0356968)
AIRCRAFT 3726, CORROSION ON STA 947 FLOOR BEAM UPPER CHORD AT LBL 50 WL 208. CORRECTIVE ACTION: EVALUATED DAMAGE CORROSION FOUND ARROUND HOLES AT STA 947.5 LBL 50 WL 208 UPER CHORD OUT OF LIMITS, REPAIRED DAMAGE ON STA 947.5 LB 40.5 TO LBL 50 WL 208 IAW B737 SRM 53-70-51-2R REPAIR 5 STEP 4 "C" FIG 206 ALTERNATIVE 2, E. (LP 0358237)
(LOG 0368246) CRACK IN VAPOR BARRIER ATTACH ANGLE THRU FUEL TANK AT STA 663 WL 176 RBL 11. REPAIRED CRACK IN VAPOR BARRIER ATTACH ANGLE THRU FUEL TANK AT STA 663 WL 176 RBL 11 IAW B737 SRM 57-10-10-2R-5.
AIRCRAFT 3726, CORROSION LEVEL 2 AT MOP SILL AT STA 312 TO STA 350 LBL 56 WL 208 MULTIPLE AREAS. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW MOP SILL ON STA 312 TO STA 350 LBL 56 WL 208 IAW B737-800 SRM 51-40-02-0G AND DWG 141A8110 REV- O. (LP 0352067)
(LOG 4926952) ON DEPT OUT OF MCO FA'S SMELED A BURNING SMELL, THEN DISIPATED. REMOVED AND REPLACED FWD DOOR AREA HEATER AS PER B737-800 AMM 21-45. OPS CHECK OK.
(LOG 4686158) SEAT 10F IFE SCREEN SMOKE W/EXTENDED. SCREEN STOWED ASAP END OF EVENT. PANASONIC FOUND THE WIRE HARNESS IN THE VIDEO SCREEN AT 10F CHAFFED AND SHORTED. REPLACED SAME.
(LOG 2811760) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. RE-CONNECTED LIGHT ASSY, CK GOOD PER B737 AMM 33-51.
(LOG 4681067) EMERGENCY LIGHT OUT SEAT 20D INOPERATIVE. FOUND LAMP OF EMERGENCY AREA LIGHT AT SEAT 20D DETACHED FROM LIGHT ASSEMBLY. REINSTALLED LAMP PER B737 AMM 33-51. OPERATIONAL TEST NORMAL.
(LOG 2610348) DURING CCK AT QRO, WHILE PERFORMING STEPS 17 & 18 OF WORK CARD 2330-01337-1001, FOUR (4) CRACKED HOLES AND TWO (2) ELONGATED HOLES WERE FOUND ON FUSELAGE SKIN BETWEEN STA. 727E & 727H, STRINGER S-3R & STRINGER S-3L AT LOCATIONS SHOWN IN FIGURE 1 AND DETAILED BELOW. ADDITIONALLY, A DENT ON FUSELAGE SKIN APPROX. 6# FORWARD OF STA. 727H INBD. OF S-2L LOCATION WAS FOUND. MAINTENANCE REPAIRED DAMAGE PER ERA 593033-14AD REV A,B,C.
(LOG 2607114) DURING GOGO 2KU INTERNET, RADOME AND ANTENNA DEMOD ON 737-800 RADOME PER WC 2330-01334-21D AND 2330-01337- 42, MTC NOTED TWO HOLES WITHOUT A MINIMUM FASTENER SPACING. MAINTENANCE REPAIRED DAMAGE PER ERA 605622-14.
(LOG 8106498) DURING INSPECTION FOUND EMERGENCY LIGHT ON ROW 13 MISSING COVER. R/R SEAT 13D EMERGENCY LIGHT ASSY ON SEAT 33-51-11. OPS CHECK GOOD.
(LOG 1889082) DURING INSPECTION FOUND CRACKS ON FOUR HOLES ON SKIN TO ATTACH THE ADAPTER RING AND ELONGATED HOLE BTW STRG 2 LH STA 727F. AREA WAS REPAIR PER ETI-37-21-434 REV 12 AND ERA 593033-14.
(LOG 1886918)DURING CCK AT QRO, WHILE PERFORMING STEPS 17 & 18 OF WORK CARD 2330-01337-1001, FOUR (4) CRACKED HOLES AND TWO (2) ELONGATED HOLES WERE FOUND ON FUSELAGE SKIN BETWEEN STA. 727E & 727H, STRINGER S-3R & STRINGER S-3L. ADDITIONALLY, A DENT ON FUSELAGE SKIN APPROX. 6# FORWARD OF STA. 727H INBD. OF S-2L. MAINTENANCE REPAIRED DAMAGE PER ERA 593033-14.
(LOG 1885424) AA 5352-01035 FOUND WORN AND ELONGATED FASTENERS HOLES (7/EAS) OF PANEL SUPPORT STRUCTURE AT BS 727+2.7 BTW LBL 10" AND RBL 23". WORN AND ELONGATED FASTENERS HOLES (7/EACH) OF PANEL SUPPORT STRUCTURE AT BS 727+2.7 BTW LBL 10" AND RBL 23" WERE REPAIRED PER ETI-37-21-426 REV 1 AND ER/A 592967-14AD
(LOG 1882481) DURING INSPECTION FOUND CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 114AC AND 113AC. CORROSION ON SETTLEMENT AREA OF ACCESS PANELS 114AC AND 113AC WAS REPAIRED PER ERA 592905-14 REV. ORIGINAL. SECTION I PERMANENT REPAIR AND ETI-37-21-428 REV. ORIGINAL.
(LOG 7643446) DURING INSPECTION FOUND MID EXIT SIGN AFT FACEPLATE IS MISSING. INSTALLED LENS COVER ON EXIT SIGN REF B737 AMM 33-51. CHECKED OK FOR SVC.
(LOG 1792544) COMPLY WITH CARD 5710-01125-0301 MLG-TRUNNION FTG FUSE PIN BORES CORROSION.
(LOG 1792553) COMPLY WITH CARD 5710-01125-0301 MLG-TRUNNION FTG FUSE PIN BORES CORROSION.
(LOG 1788578) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING: HOLE A PITTED ON INBD FACE. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788579) DURNG INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING: HOLE A PITTED ON OTBD SPOTFACE. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1858599) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING: HOLE A PITTED INSIDE BORE. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788600) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING HOLE 7D INNER FACE OF LUG CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788601) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING: HOLE C PITTED INSIDE BORE. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788606) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING: HOLE D PITTED INSIDE BORE. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788603) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING: HOLE C PITTED AT SPOTFACE. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788605) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING: HOLE D PITTED AT SPOTFACE. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788602) DURING INSPECTION FOUND RMLG FWD TRUNNION SUPPORT FITTING HOLE 5C INNER FACE OF LUG CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788228) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 1A OUTER FACE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788215) DURING INSPECTION FOUND LMLG FWD UPPER I/B TRUNION LUG MARKED 2C, INNER FACE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2
(LOG 1788218) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 4D BORE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788219) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 4D INNER FACE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788224) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 1A BORE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788229) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 3B BORE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788231) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 3B OUTER FACE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788233) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 3B INNER FACE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1788236) DURING INSPECTION FOUND LMLG FWD TRUNNION LUG MARKED 4D OUTER FACE CORRODED. REPAIRED PER B737 SRM 57-20-90 REP 2.
(LOG 1743361) EMERGENCY BATTERIES FAILED OPS CHECK. R/R EMERGENCY BATTERIES @ EMERGENCY BATTERY CHARGERS AT M10673 AND M10671 PN D717-02-030 AND PN D717-02-001 RESPECTIVELY. OPS CHECK GOOD.
DURING INSPECTION FOUND SEAT EMERGENCY LIGHT INOP BETWEEN ROW 19-23. REMOVED AND REPLACED BATTERY FOR ROW 19-23. OPS CK GOOD.
(LOG 6719867) DURING INSPECTION FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE THROUGHOUT CABIN. REPLACED BATTERY PACK @ M1671 LOCATION, LIGHTS OPS NML PER B 737 AMM 33-51.
(LOG 6398356) REPLACED BATTERY AT BATTERY CHARGER M1674 PER B737 AMM 35-51. OPS CKS GOOD.
(LOG 5953102) DURING INSPECTION FOUND EXIT SIGN (LENS) MISSING AT 18A. INSTALLED NEW EXIT SIGN LENS PER AMM 33-51.
(LOG 5439370) DURING INSPECTION FOUND AFT GALLEY EMERGENCY EXIT LIGHT SIGN IS DAMAGED. R/R EXIT LIGHT ASSEMBLY IAW B737-800 AMM 33-51. OPS NML.
(LOG 5527914) DURING TEST FOUND EMERGENCY EXIT LIGHTS INOP ROWS 18-23. RESEATED CONNECTOR ON M1695 BATTERY PACK OPERATION OK B737 AMM 33-51.
DURING INSPECTION FOUND FLIGHT ATT FLASHLIGHT INOP. AT AFT LEFT OUTBOARD POSITION. R&R FLASHLIGHT BATTERY IAW AMM 25-64-00-900-806. OPS CHECK GOOD.
(LOG 5235926) DURING INSPECTION FOUND LEFT WING AFT EXTERIOR EMERGENCY LIGHT AND ROW 22 OVERHEAD EXIT SIGN INOPERATIVE. FOUND BATTERY PACK M1670 BAD. R+R BATTERY PACK IAW B737 MM 33-5. LIGHT CKS OK.
DURING INSPECTION FOUND OIL CAN CONDITION ON AFT PRESSURE BULKHEAD AT 9, 11, 12 AND 1 OâCLOCK POSITION AT AFT ACC COMPARTMENT. MAINTENANCE REPAIRED PER ETI-37-18-422 REV 2 AND ER/A 569931-14 REV ORIGINAL.
DURING INSPECTION FOUND CORROSION ON FUSELAGE SKIN AREA UNDER DORSAL FIN AND VERTICAL STABILIZER FROM STA 1016 TO STA 1156. AREA WAS REPAIRED PER ETI-37-18-427 REV 2 AND ER/A 569932-14 REV ORIG.
DURING INSPECTION FOUND ANGLE LT STA 1075-1099 IS OUT LIMITS WITH MINIMUM REMAINING 0.034. PER B737-800 SRM ALLOWABLE DAMAGE 1 53-80-13. AREA OUT LIMITS WAS REPAIRED PER SRM 53-80-71 REPAIR 6.
DURING INSPECTION FOUND CRACK ON RIB BTW FRONT SPAR AND REAR SPAR LT HORIZONTAL STABILIZER LE STA 95.96. AREA WAS REPAIRED PER SRM 55-10-09 REPAIR 4 FIGURE 202 AND ER/A 569674-14 REV ORIGINAL.
DURING INSPECTION FOUND EXPOSED MATERIAL ON ACCESS PANEL NR 441EL OF ENGINE 2. ACCESS PANEL 441EL WAS REPAIRED PER SRM 51-70-05 REPAIR 10 AND SRM 51-70-05 REPAIR GENERAL.
DURING INSPECTION FOUND WEAR IN COMPOSITE MATERIAL OF ACCESS PANEL 193D. ACCESS PANEL WAS REPAIRED PER SRM 51-70-05-2R-6 PAR 4 STEP E F AND G AND SRM 51-70-05-2R-0.
DURING INSPECTION FOUND CRACK AT LT MLG WHEEL WELL FWD BULKHEAD LOWER AREA. BULKHEAD LOWER AREA WAS REPAIRED PER SRM 51-40-05 PAR 7D AND 57-10-10 REPAIR 2.
DURING INSPECTION FOUND EXPOSED MATERIAL ON ACCESS PANELS NBR 431ER AND 431EL OF ENGINE NR 1. ACCESS PANELS 431ER AND 431EL WERE REPAIRED PER SRM 51-70-05 REPAIR 10 AND SRM 51-70-05 REPAIR GENERAL PAR 4.
DURING INSPECTION FOUND CRACK AT LT MLG WHEEL WELL FWD BULKHEAD LOWER AREA. BULKHEAD LOWER AREA WAS REPAIRED PER SRM 51-40-05 PAR 7D AND 57-10-10 REPAIR 2.
DURING INSPECTION FOUND HOLGED HOLE ON ACCESS PANEL 193AL. ACCESS PANEL 193AL WAS REPAIRED PER SRM 53-40-70 REPAIR 1 PAR 4B (2). TABLE 202, SRM 51-70-05 REPAIR 8 PAR 4 F G AND SRM 51-70-05 REPAIR GENERAL PAR 4.
DURING INSPECTION FOUND WEAR ON SLAT 3 LOWER SKIN, WEDGE AREA. MAINTENANCE REPAIRED PER SRM 57-42-01 REP 6.
DURING INSPECTION FOUND CORROSION ON FLOOR STRUCTURE BTWN STA 951-968 AND RBL 52 AT W2 AREA. FLOOR SUPPORT BTW STA 951-968 & RBL 52 WAS REPLACED PER SRM 51-40-02.
DURING INSPECTION FOUND CRACK ON RIB BTW FRONT SPAR AND REAR SPAR RT HORIZONTAL STABILIZER LE STA 95.96. SPAR RT HORIZONTAL STABILIZER LE STA 95.96 (EHV) WAS REPAIRED PER SRM 55-10-09 REPAIR 4.
DURING INSPECTION FOUND CRACK ON LT SIDE PLATE BTW STA 500B TO STATION 500C FWD CARGO COMPARTMENT. MAINTENANCE REPAIRED SIDE PLATE PER SRM 53-00-53 REPAIR 5.
DURING INSPECTION, FOUND WEAR ON THE NR 3 SLAT LOWER SKIN WEDGE AREA. MAINTENANCE REPAIRED THE DAMAGE IAW SRM 57-42-01, REPAIR 6.
DURING INSPECTION, FOUND WEAR ON THE NR 2 SLAT LOWER SKIN WEDGE AREA. THE DAMAGE WAS REPAIRED IAW SRM 57-42-01, REPAIR 6.
DURING INSPECTION, FOUND AN OIL CANNING CONDITION ON THE AFT PRESSURE BULKHEAD, AT THE 9 HRS POSITION. MAINTENANCE REPAIRED THE BULKHEAD IAW SRM 53-80-08, REP 1.
DURING INSPECTION, FOUND CORROSION ON THE FLOORBEAM ANGLE, BS 887 BETWEEN STRINGERS 25R AND 27L. MAINTENANCE REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02, PAR 4.
DURING INSPECTION, FOUND CORROSION ON THE RT ZEE CHANNEL SIDEPLATE BETWEEN BS 727 - 947.5, RBL 21. MAINTENANCE REPLACED THE CHANNEL IAW SRM 51-40-02.
DURING INSPECTION FOUND OIL CANNING AT LT MLG WHEEL WELL FWD BULKHEAD LOWER AREA. WHEEL WELL FWD BULKHEAD LOWER AREA WAS REPAIRED SRM 51-40-05 PAR 7D AND 57-10-10 REPAIR 2.
DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 328 - 312, RBL 31. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.
)DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 328 - 344, LBL 44. REPLACED IAW SRM 51-40-02.
DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 312 - 328, LBL 44. REPLACED IAW SRM 51-40-02.
DURING INSPECTION FOUND OIL CANNING AT RT MLG WHEEL WELL FWD BULKHEAD LOWER AREA. RT MLG WHEEL WELL FWD BULKHEAD LOWER AREA WAS REPAIRED PER SRM 51-40-05 PAR 7D AND 57-10-10 REPAIR 2.
DURING INSPECTION FOUND CORROSION ON FLOOR STRUCTURE AREA STA 344. LEVEL CORROSION 2 IN REF NRC 00488 SUPPORT WAS REPLACED PER SRM 51-40-02.
DURING INSPECTION FOUND CORROSION ON FLOOR STRUCTURE ON STA 986 BTW RBL 52 AND RBL 28 AT W2 AREA. AREA WAS REPAIRED PER ERA 569903-14 REV ORIG AND ETI -37-18-423 REV 2.
CREW DECLARED AN EMERGENCY AFTER A MOMENTARY, CABIN ALTITUDE, WARNING HORN SOUNDED ON DESCENT. MAINTENANCE FOUND THE SUPPLY PRESSURE SENSE LINE BETWEEN THE PCCV AND BAR BROKEN AND REPLACED IT. PERFORMED PNEUMATIC HEALTH CHECK IAW W/C 3610-7956 AND THE OPS CHECK WAS GOOD. PERFORMED BITE CHECK CPC-1 AND FOUND RATE HI, LO INFL, HI LEAKAGE. BITE OF CPC-2 SHOWED NO FAULTS. PERFORMED PHASE 1 SINGLE PACK CHECK IAW AMM 21-00 CHECKS OK. PERFORMED PHASE 3 SINGLE PACK CONFIDENCE CHECK LEAK RATE OUT OF LIMITS. FOUND APU BLEED DUCT CLAMP AT P-DOME NOT SECURE. RESECURED SAME. TIGHTENED KEEL BEAM DUCT CLAMPS. PERFORMED AMM 21-00-05-780-801, PHASE 1, 2, 3 TESTS. ALL NORMAL. SINGLE PACK AND LEAKAGE RATE WITHIN LIMITS. ACFT RETURNED TO SERVICE.
DURING SCHEDULED MAINTENANCE VISIT, TWO EXISTING LIGHTNING STRIKE MONITORS WERE FOUND IN THE FOOTPRINT OF THE SAT TV ANTENNA MOD BEING INSTALLED AT CURRENT CHECK. MAINTENANCE REPAIRED IAW ERA 540735-14AD.
DURING INSPECTION, FOUND AFT PIT RT FLOOR TO SIDEWALL ATTACHING FLOOR SHIELD HAS SURFACE CORROSION AT FASTENER LOCATIONS BS 787-727J. MAINTENANCE R & R SHIELD ASSY IAW DWG 146A8127 ID 001, REV C, 7 DWG 146A0081 ID 0001, REV B.
DURING INSPECTION FOUND AFT PIT LT SIDEWALL PANEL LOWER FLOOR Z-ANGLE ATTACH CORRODED FROM BS 767 TO 727H. MAINTENANCE R & R AFT PIT LTSIDEWALL PANEL LOWER FLOOR Z-ANGLE FROM BS 767 TO 727H, DUE TO BEING OUT OF LIMITS.
DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK BS 520, LBL 45 IS WORN. MAINTENANCE REMOVED AND INSTALLED NEW PASSENGER CABIN SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK BS 520, LBL 24 IS WORN. MAINTENANCE REMOVED AND INSTALLED NEW PASSENGER CABIN SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK BS 520, RBL 24 IS WORN. MAINTENANCE REMOVED AND INSTALLED NEW PASSENGER CABIN SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND PASSENGER CABIN SEAT TRACK BS 520, RBL 45 IS WORN. MAINTENANCE REMOVED AND INSTALLED NEW PASSENGER CABIN SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND DAMAGE TO MAIN ELECTRONICS AND EQUIPMENT DOOR BEYOND SRM ALLOWABLE LIMITS. MAINTENANCE REPLACED ELECTRONICS AND EQUIPMENT DOOR IAW AMM. LEAK CHECK OK.
DURING INSPECTION, FOUND EMERGENCY LIGHT ASSY ON SEAT 16B MISSING. MAINTENANCE INSTALLED LIGHT. OPS TEST OK.
DURING INSPECTION, FOUND CRACKS IN FLOORBEAM AT BS 727B, LBL 24.75. MAINTENANCE REPAIRED IAW ERA 522094-14AD.
DURING INSPECTION FOUND CABIN FLOORBEAM BS 727B, SPLICE STRAP, LBL 24.75, RBL 24.75, LBL 45.5, AND RBL 45.5 CRACKED. REPAIRED IAW ER/A 522094-14, REV ORIGINAL.
DURING INSPECTION, FOUND LARGE DENT IN LT HORIZONTAL STABLIZER ROUGHLY 6 X 2 INCHES DEEP. MX REPAIRED DAMAGE IAW ERA 517221-14.
FWD ENTRY DOOR WOULD NOT OPEN. MX REPLACED GUST LOCK ARM PIN LOWER RETENTION SCREW. OPS CHECKED OK.
DURING INSPECTION, FOUND EMERGENCY LIGHT AT SEAT 15 DEF INOPERATIVE. MX R & R EMERGENCY LIGHT ASSY IAW MM 33-51. OPS CHECKED OK.
PASSENGER SEAT TRACK AT BS 520 LBL 25 WORN BEYOND LIMITS. REPAIRED IAW SRM 53-00-52.
PASSENGER CABIN SEAT TRACK WORN AT BS 520 LBL 45. REPAIRED IAW SRM 53-00-52.
DURING CRUISE FLIGHT THE NR 2 ENGINE FLAMED OUT AT FL330. FLIGHT CREW SECURED THE NR 2 ENGINE AND RETURNED TO DEPARTURE AIRPORT. MX FOUND FUEL LEAKING AT THE HMU FUEL OUTLET LINE/PLATE GASKET. MX REPLACED THE GASKET. THE NR 2 ENGINE GROUND RUN UP TO POWER WAS SUCCESSFUL WITH NO LEAKS NOTED.
DURING CRUISE FLIGHT THE NR 2 ENGINE FLAMED OUT AT FL330. FLIGHT CREW SECURED THE NR 2 ENGINE AND RETURNED TO DEPARTURE AIRPORT. MX FOUND FUEL LEAKING AT THE HMU FUEL OUTLET LINE/PLATE GASKET. MX REPLACED THE GASKET. THE NR 2 ENGINE GROUND RUN UP TO POWER WAS SUCCESSFUL WITH NO LEAKS NOTED.
SMOKE CAME FROM CEILING ABOVE CAPTAINS HEAD, STRONG SMELL OF ELECTRICAL FIRE AT GATE IN THUNDERSTORM. SHUT DOWN ALL POWER AND SMOKE DISSIPATED. A/C STRUCK BY LIGHTNING, REPORTED BY ANOTHER FLT CREW. PERFORMED LIGHTNING STRIKE INSP REF AMM, NO EVIDENT OF LIGHTNING DAMAGE FOUND. CHECKED BEHIND OVERHEAD INSTR PANEL AND CB PNLS. CHECKED HUD SYS, GALLEYS, LAVS, CABIN LIGHTING, IFE SYS - NO DISCREPANCIES FOUND. POWERED A/C WITH GND PWR APU AND BOTH ENGINES, ALL CHECKS GOOD. RAN PACKS WITH PNEU FROM APU AND BOTH ENGS, CHECKS GOOD NO TROUBLE FOUND. CONFERRED WITH MCC. A/C OK FOR SERVICE.
HOLES COMMON TO MINOR REPAIR WERE MIS-COUNTERSUNK, REQUIRING SKIN CUTOUT AND DOUBLER/TRIPLER SKIN REPAIR. REFERENCE ERA 473452-14.
SEVERAL TIMES DURING FLIGHT AFTER AIRBORNE THE RED FWD CARGO LIGHT AND FIRE BELL FLASHED AND RANG. THIS WAS INTERMITTENT AND LASTED BARELY A SECOND OR TWO THEN WENT AWAY. HAPPENED IN A LOOP, B LOOP, AND BOTH LOOPS. NO DETECTOR FAULT ILLUMINATED. REPLACED CARGO FIRE CONTROL PANEL AND FWD CARGO ELECTRONICS UNIT PER M/M. TESTED PER M/M. TEST OK. SYSTEM CHECKS OK.
TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF. PERFORMED TAKEOFF WARNING SYSTEM TEST PER MM 31-51-00-5. NO MALFUNCTIONS NOTED. TAKEOFF WARNING SYSTEM CKS GOOD.