N386DA
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 | 2025-09-10 – 2025-09-10 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2025-09-10 – 2025-09-10 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
(LOG 1414279) DURING B-4 CHECK, FOUND L1 WINDOW FRAME C-D POST CRACKED AT UPPER OTBD CORNER. REPAIRED THE CRACKS IAW ERA 620146-14.
(LOG 8092530) ON B4 CHECK, FOUND R1 & L1 OUTER DOOR FRAMES CRACKED, UPPER OTBD CORNERS. ALL WORK AND RII'S PERFORMED ARE TRANSFERRED TO WORKPAGE 7543424 AND NON-ROUTINES NR 1 AND NR 2 IAW ER/A 620146-14TR, REV ORIG, & 620147-14TR, REV ORIG.
(LOG 1414305) DURING B-4 CHECK, FOUND R1 WINDOW FRAME C-D POST CRACKED AT UPPER OTBD CORNER. REPAIRED THE CRACKS IAW ERA 620147-14.
FOUND EMERGENCY EXIT SIGN AT CENTER AISLE CEILING PANEL IN. REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M1670 IAW B737 AMM 33-51. OPS CHECK GOOD.
ROW 17 EMERGENCY EXIT COVER MISSING. INSTALLED EMERGENCY LIGHT COVER REF B737 AMM 33-51. (LP 7371785)
ON SERVICE CHECK R1 DOOR EMERGENCY EXIT SIGN LIGHTS AND FIRST CLASS EMERGENCY AISLE LIGHTS INOP. R & R FWD EMERGENCY BATTERY PACK (M1674) IAW B737 AMM 33-52.OPS CHECK GOOD.
ROW 18-22 EMERGENCY LIGHTNING INOP. R & R EMERGENCY LIGHT BATTERY PACK AS PER B737 AMM 33-51. OPS TEST PASSED ALL LIGHTS COME ON. OK FOR SVC.
DIV DE- DUE TO RIGHT ENGINE COMPRESSOR STALL AND FAILURE TO ADVANCE BEYOND 50% N2 DURING CRUISE. ENGINE WAS NOT SHUT DOWN AND DIVERTED TO BZE. CONTRACT MAINTENANCE FOUND FAN VERY HARD TO TURN AND METAL ON AFT SUMP CHIP DETECTOR. REPLACED RIGHT ENGINE ON LOG PAGE 1193731.
(LOG 7469168) SEATS LOOSE IN TRACK 17ABC, 21DEF, 26ABC. SECURED SEATS IN TRACK REF B737 AMM 25-22.
(LOG 0925496) SEAT TRACK DAMAGE AT ROW 13ABC. FABRICATED REPAIR PER B 737 SRM 53-00-52-2R REPAIR 4 (457268). OK TO TREAT AND PAINT. APPLIED ONE LAYER OF ALUMINIZED PRIMER PER SOPM 20-41-04. PROTECTIVE COATING APPLIED ON SHOP ORDER VP5356. INSTALLED FWD SPLICE PER B 737 SRM 53-00-52-2R REPAIR 4. COMPLETED PERM REPAIR PER ERA 625711-14 REG ORIG SEC 2(457268).
(LOG 0656303) WHILE INSTALLING SEAT ROW 27ABC SEAT TRACK TANG BROKE, AT SEAT TRACK LOCATION STA. 727I 14" LBL 45.50". REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 5 REPAIR 5 - SECTION 46 SEAT TRACK REPAIR FOR BAC1520-2789 ALUMINUM EXTRUSION BETWEEN FLOOR BEAMS PERMANENT REPAIR INSTRUCTIONS.
(LOG 0652516) DAMAGE TO A SEAT TRACK, P/N 146A5350-39, AT ROW 28ABC. THE DAMAGE CONSISTS OF A WORN OFF SEAT TANG OF THE SEAT TRACK LOCATED AT STA 747 LBL 45.50. SEAT ROW 28ABC / SEAT TRACK / DAMAGE REPAIRED PER E/RA 622069-14 REV. ORIG.
SHIP 3716 -UFC- PERFORMED GO AROUND DUE TO TRAILING EDGE FLAP LOCKOUT ON APPROACH SEA. FSEU BITE FAULT 27-52260 (TE FLAPS SNSR DIS) RECORDED. REPLACED LEFT-RIGHT FLAP POSITION TRANSMITTERS. REPLACED FLAP POSITION INDICATOR PRECAUTIONARY. OPS CHECKS OK.
SHIP 3716 -UFC- PERFORMED GO AROUND DUE TO TRAILING EDGE FLAP LOCK OUT ON APPROACH MCI. CORRECTIVE ACTION: RECORDED FSEU FLAP FAULT 27-52261 (TE FLAPS SNSR DIS). REPLACED LEFT FLAP POSITION TRANSMITTER. OPS CHECKS GOOD.
(LOG 4575075) ESCAPE PATHLIGHT INOP AT SEAT 1CD. FOUND WALL CONNECTION DISCONNECTED. CONNECTED & SECURED PLUGS. PERFORMED OPS CHK, ALL OPS OK.
SHIP 3716 -ATB/PRESS- RETURNED TO ATL DUE TO CABIN ALTITUDE ALERT. UNABLE TO PRESSURIZE CABIN. CORRECTIVE ACTION: R2 SERVICE DOOR AJAR. DOOR INDICATION CLOSED. REPLACED DOOR SNUBBER. PERFORMED R2 DOOR RIG AND ADJUSTMENT. OPS CHECKS GOOD.
(LOG 0180347) LH WING UPPER SKIN BTWN RIB 22 / RIB 24 AND STGR U-13.5 / MISDRILLED HOLES. REPAIRED PER ERA 614975-14.
(LOG 0180822) MISDRILLED HOLES ON THE LH WING UPPER SKIN RIB 22 / RIB 24 AND U-13.5, REAPIR AS REQUIRED. AT LH WING UPPER SKIN RIB 22/ RIB 24 AND U-13.5 THE MISDRILLED HOLES WERE REPAIRED I.A.W B737-800, ER/A 614975-14 REV. 1.
(LOG 0180817) LEFT WING, TWO OPEN HOLE WITH CRACK INDICATION ON FRONT REAR SPAR TENSION FITTING AT RIB 27 AND ONE OPEN HOLE WITH CRACK INDICATION ON REAR SPAR TENSION FITTING AT RIB 27. LEFT WING, CRACK IN HOLES WERE REPAIRED I.A.W. ER/A 614787.
(LOG 0178882) LH WING / RIB 27 / FRONT & REAR SPAR TENSION FITTINGS / CRACKS. REPAIRED PER ERA 614787-14.
(LOG 0177620) CRACKS INDICATION ON STA 440 FRAME LH SIDE UP TO 1.400" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 440, FRAME WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02A SECTION 02.
(LOG 0177755) CRACKS INDICATION ON STA 480 FRAME LH SIDE UP TO 1.300" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 480, FRAME WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02A SECTION 02.
(LOG 0175949) AFT RH ENTRANCE DOOR ON STA 987 FLOOR STRUCTURE WITH CORROSION. AFT RH ENTRANCE DOOR ON STA 987 UPPER T-CHORD FLOOR STRUCTURE WAS REPLACED I.A.W. B 737-800 SRM 51-40-02-0G.
(LOG 0165391) CRACKS INDICATION ON STA 500F FRAME LH SIDE UP TO 0.300" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 500F, FRAME WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-04A.
(LOG 0162337) CRACKS INDICATION ON STA 500C FRAME RH SIDE UP TO 0.162" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 500C, FRAME RH SIDE WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02B.
(LOG 0162325) CRACKS INDICATION ON STA 500A FRAME RH SIDE UP TO 0.280" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 500A, FRAME RH SIDE WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02B.
(LOG 0162321) CRACKS INDICATION ON BS 480 FRAME RH SIDE UP TO 0.541" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON BS 480, FRAME RH SIDE WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02B.
(LOG 0162318) CRACKS INDICATION ON STA 440 FRAME RH SIDE UP TO 0.300" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 440, FRAME RH SIDE WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02B.
(LOG 0160527) CRACKS INDICATION ON STA 400 FRAME LH SIDE UP TO 0.800" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 400, FRAME LH WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02A.
(LOG 0160614) CRACKS INDICATION ON STA 867 FRAME LH SIDE UP TO 0.300" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 867, FRAME WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02A SECTION 02.
(LOG 0160599) CRACKS INDICATION ON STA 727B FRAME LH SIDE UP TO 0.200" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRAKS INDICATION ON STA 727B, FRAME WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02A.
(LOG 0160581) CRACKS INDICATION ON STA 500C FRAME LH SIDE UP TO 0.150" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 500C, FRAME WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02A SECTION 02.
(LOG 0160556) CRACKS INDICATION ON STA 500A FRAME LH SIDE UP TO 0.150" LONG AT A/C RAIL BRACKET INBOARD FASTENER HOLE. CRACKS INDICATION ON STA 500A, FRAME WAS REPAIRED I.A.W. B737-800 CARD 2526-01236-02A SECTION 02.
(LOG 0154644) AFT CARGO COMPARTMENT RH SIDE, FLOOR SUPPORT STRUCTURE BETWEEN STA 727J AND STA 787 WITH CORROSION. AFT CARGO COMPARTMENT RH SIDE, FLOOR SUPPORT BETWEEN STA 727J AND STA 787 WAS REPLACED IAW B737-800 SRM 51-10-02-0G PAR. 9 AND SRM 51-40-02-0G.
(LOG 9667870) EMERGENCY LIGHTS INOP FROM ROWS 23 ALL THE WAY AFT. T/S PER B737 FRMFIM 33-50. FOUND BATTERY AT POWER SUPPLY M1672 INOP. REMOVED AND REPLACED M1672 BATTERY PER B737 AMM 33-51. OPS CKS GOOD, OK FOR SVC.
(LOG 4054240) DURING INSPECTION FOUND EMERGENCY LIGHTS AT ROWS 10-15 AND R1 DOOR LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS FOR ROWS 10-15 AND R1 DOOR PER AMM 33-51. OPS NML.
SHIP 3716 - ATB - DUE TO BIRDSTRIKES AND SUBSEQUENT #2 ENGINE DAMAGE. CORRECTIVE ACTION: FOUND DAMAGE TO FAN BLADES AND PLATFORMS. REPLACED FULL FAN BLADE SET AND PLATFORMS. PERFORMED BORESCOPE WITH NO DAMAGE NOTED.
SHIP 3716 -ATO- DUE TO TAKEOFF CONFIG WARNING. CORRECTIVE ACTION: PERFORMED FSEU BITE CHECK. FAULTED 'SL4 PROX INBOARD'. REPLACED SLAT #4 INBOARD SENSOR (S1001). OPS CHECKS GOOD.
(LOG 8695719) INBOUND F/A UNABLE TO OPEN 1L DOOR. FOUND DOOR 1L GUIDE ARM HOLD-OPEN MECHANISM GUST LOCK BROKEN, AND PIN THAT HOLDS UPPER AND LOWER RADIUS LINK'S MISSING. INSTALLED NEW PIN X2 NEW WASHERS NEW KEYWASHER, AND NEW SCREW. REF B737 AMM 52-11-21. DOOR OPS CHECK GOOD.
(LOG 1911505) DURING INSPECTION FOUND CORROSION AND ELONGATED HOLES ON FAIRING PANEL SUPPORT STRUCTURE STA 727+2.7. CORROSION AND ELONGATED HOLES ON FAIRING PANEL SUPPORT STRUCTURE STA 727+2.7 WAS REPAIRED PER ERA 593431-14 AD REV ORIGINAL SECTION 1 PERMANENT REPAIR AND ETI-37-21-453 REV 1.
DURING INSPECTION, FOUND TWENTY THREE (23EA) HOLES OF IDTV ANTENNA RADOME WERE FOUND WITH CRACKS (17EAS) , ELONGATED. TWENTY THREE (23EA) HOLES OF IDTV ANTENNA RADOME WERE REPAIRED PER ETI-37-21-451 REV. 15 AND ERA 593428-14AD REV. A.
DURING INSPECTION FOUND CRACK AND BENT ON FWD FUSELAGE CUTOUT OF EXTERNAL POWER RECEPTACLE ACCESS DOOR NBR 114AR. CRACK ON FWD FUSELAGE CUTOUT OF EXTERNAL POWER RECEPTACLE ACCESS DOOR NBR 114AR (FUS) WAS REPAIRED PER ER/A 593393-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR AND ETI-37-21-450 REV 3.
(LOG 1910888) DURING HORIZONTAL STABILIZER TRIM BALLSCREW INSPECT ,WAS FOUND METALLIC PARTICLES IN GREASE. HORIZONTAL STABILIZER TRIM BALLSCREW WAS REPLACED PER AMDS 2740-01077-0301 AND AMDS 2740-01077-0101 STEP 11.
(LOG 1907567) DURING INSPECTION FOUND CORROSION ON EXTERNAL FUSELAGE SKIN BTW S-20LH AND S-21LH, STA 917. ORROSION ON EXTERNAL FUSELAGE SKIN BTW S-20LH AND S-21LH, STA 917 WAS REPAIRED PER B737-800 SRM 53-70-01-2R-3.
DURING INSPECTION FOUND 1L EMERGENCY LIGHT CIRCUIT BOARD IS INOPERABLE. REPLACE 1L EMERGENCY LIGHT CIRCUIT BOARD, PER B737 AMM 33-51.
DURING INSPECTION FOUND LEFT SIDE EMERGENCY EXIT LIGHT SIGNS INOPERATIVE. R & R BATTERY AND CHARGER AT ROW 17A IAW AMM 33-51. OPS CHECKED GOOD.
DURING INSPECTION, FOUND THE LT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS FOUND TO BE BAD, REPLACED THE BATTERY IAW AMM 33-51. OPS CHECKED NORMAL.
(LOG 6335378) DURING INSPECTION FOUND EXIT PLACARD BY 1R DOOR MISSING. R/R EMERGENCY LT COVER AT 1R PER B737 AMM 33-51. OPS CHECK NORMAL.
(LOG 6335352) DURING INSPECTION FOUND EMERGENCY LIGHT SIGN INOPERATIVE NEAR FLOOR AT 17 A&F. REMOVED AND REPLACED BATTERY PACK AT SEAT 17A IAW B737 AMM 33-51. OPS CK GOOD.
DURING INSPECTION, FOUND THE LEFT OVERWING EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.
(LOG 5956387) DURING INSPECTION FOUND CEILING EMER. LIGHTS OUT ROW 22. REMOVED AND REPLACED BATTERY PACK M1670, REF B737 AMM 33-51. OPS CK'S GOOD. OK FOR SVC.
(LOG 6060170) DURING INSPECTION FOUND EMERGENCY LIGHTS INOP AT L1 DOOR COCKPIT DOOR AND DOME LIGHT. REMOVED AND REPLACED EMER LIGHT BATTERY PACK BATTERY M1675 AND TESTED PER AMM 33-51.
(LOG 5341700) SEAT 11 ABC DISCONNECTED FROM FLOOR. MAINTENANCE REPAIRED DAMAGE PER ERA 577436-14 AND OBTAINED AND DRILLED NEW SEAT TRACK AND SPLICE PER B737 SRM 53-00-52, REPAIR 4 PG. 201. (889397) STEP 4F. COMPLETED SEAT TRACK INSTALLATION PER B737 SRM 53-00-52, REPAIR NUMBER 4.
DURING INSPECTION FOUND EXIT SIGN ABOVE & OUTSIDE FLIGHT DECK DOOR IS MISSING. REATTACHED EXIT SIGN COVER LENS.
(LOG 3748315) DURING INSPECTION FOUND DENT ON LEFT HORIZONTAL STABILIZER APPROXIMATELY 1.5 FEET OUTBOARD OF FUSELAGE. DENT WAS REPAIRED PER B737-800 SRM 55-10-01-2R-1.
DURING INSPECTION FOUND EMERGENCY LIGHTS OUT ON FIRST CLASS ROWS 1-4, AND R1 OVERHEAD LIGHT, GALLEY SIDEWALL LIGHT AND LIGHT OUTSIDE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK REF AMM 33-51. OPS CHECK GOOD.
DURING INSPECTION, FOUND A CRACKED FRAME AT BS 727B, BETWEEN STRINGERS 8R AND 9R IN THE PASSENGER COMPARTMENT. MAINTENANCE REPAIRED THE FRAME IAW ERA 566042-14AD, REV ORIG, AND ETI-37-18-344.
DURING INSPECTION, FOUND CORROSION ON THE ATTACH BRACKET IN NR 2 GALLEY. MAINTENANCE REPLACED THE BRACKET IAW ER/A 562424-14 REV. ORIGINAL AND ETI-37-17-349 REV. ORIGINAL.
DURING INSPECTION, FOUND CORROSION ON THE LT SIDE PLATE FROM BS 480 TO 500I IN THE FWD CARGO BAY. MAINTENANCE REPLACED THE PLATE IAW SRM 51-40-02.
DURING INSPECTION, FOUND CORROSION ON THE ATTACH BRACKETS OF THE NR 4 GALLEY. MAINTENANCE REPLACED THE BRACKETS IAW ER/A 562425-14, REV ORIGINAL, AND ETI-37-17-350, REV ORIGINAL.
DURING INSPECTION, FOUND CORROSION OUT OF LIMITS ON THE ANGLE OF STRINGER 23L BETWEEN BS 313 & 318. MAINTENANCE REPAIRED THE ANGLE ERA 564686-14, REV ORIG, AND ETI-37-17-357, REV 5.
DURING INSPECTION, FOUND A CRACK ON THE AFT EDGE OF THE INNER SKIN BS 343, STRINGER 13L. MAINTENANCE REPAIRED THE SKIN IAW ERA 562430-14, REV ORIG, AND ETI-37-17-355 REV 4.
DURING INSPECTION, FOUND CORROSION ON THE SIDE PLATE BS 727 - 767, RBL 20 IN THE CARGO BAY. MAINTENANCE REPLACED SIDE PLATE IAW SRM 51-40-02.
DURING INSPECTION, FOUND CORROSION ON SIDE PLATE BS 727 TO 847, LBL 20, IN THE AT AFT CARGO BAY. MAINTENANCE REPLACED THE SIDE PLATE IAW SRM 51-40-02, AND 51-40-05.
DURING INSPECTION, FOUND CORROSION ON SHIELD BS 767 - 790, RBL 20 IN THE AFT CARGO BAY. MAINTENANCE REPLACED SHIELD IAW DWG 146A8127, REV C, AND SRM 51-40-02.
DURING INSPECTION, FOUND CORROSION ON THE FLOORBEAM REPAIR ON THE UPPER TEE BS 986.5 BETWEEN LBL 44 TO RBL 44. MAINTENANCE REPAIRED THE FLOORBEAM IAW ERA 562429-14, REV ORIGINAL, AND ETI-37-17-354, REV 3.
DURING INSPECTION, FOUND CORROSION ON THE FLOORBEAM BS 947, RBL 53. MAINTENANCE REPAIRED IAW ERA 562427 -14, REV ORIGINAL, AND ETI-37-17-352, REV 4.
DURING INSPECTION, FOUND A CRACKED SEAT TRACK, RBL 45, BS 727J + 5. MAINTENANCE REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 5.
DURING INSPECTION, FOUND CORROSION ON THE LOWER WEB AND FRAME UNDER HEAT SHIELD FAIRING AREA AT THE LT ENGINE STRUT. MAINTENANCE REPLACED THE FRAMES IAW SRM 51-40-02 PAR 7.
DURING INSPECTION, FOUND CORROSION ON THE FLOORBEAM REPAIR FILLER AT BS 967, LBL 5. MAINTENANCE REPAIRED THE FLOORBEAM IAW ER/A 562428-14, REV ORIG, AND ETI 3717-353, REV 1.
DURING INSPECTION, FOUND CORROSION ON LOWER WEB AND FRAME UNDER HEAT SHIELD FAIRINGS, RT ENGINE STRUT AFT FAIRING STRUCTURE. MAINTENANCE REPLACED LOWER WEB AND FRAMES IAW SRM 51-40-02.
DURING INSPECTION, FOUND A CRACKED REPAIR DOUBLER ON THE BS 303, RBL 54 FLOOR STRUCTURE. MAINTENANCE REPAIRED IAW ERA 562426-14 REV ORIG AND ETI-37-17-351 REV 2.
DURING INSPECTION, FOUND CRACKED ON THE BS 663 BULKHEAD. MAINTENANCE REPAIRED THE BULKHEAD IAW SRM 57-10-10, REPAIR 2.
DURING INSPECTION, FOUND A CRACK ON LOWER SKIN OF THE RT MLG INTERIOR DOOR. REPAIRED IAW SRM 52-80-02.
DURING INSPECTION FOUND THREE DENTS ON THE LOWER SKIN AT THE LT INBOARD AFT FLAP. MAINTENANCE REPAIRED THE FLAP IAW SRM 57-53-01, REPAIR 4, AND CARD 2000-8149-02.
DURING INSPECTION, FOUND A CRACKED BULKHEAD UPPER WEB AT BS 663 BETWEEN RBL 31.83 TO 45.64 AND Z -6.
DURING INSPECTION, FOUND CORROSION ON THE WEB FROM BS 440 TO 500, STRINGER 25R IN THE FWD CARGO COMPARTMENT. MAINTENANCE REMOVED AND INSTALLED A NEW WEB IAW SRM 51-40-02.
DURING INSPECTION, FOUND THE BULKHEAD WEB CRACKED AT BS 663 BETWEEN LBL 31.83 TO 45.64 AND Z -6. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, REPAIR 3.
DURING INSPECTION, FOUND CRACKED BULKHEAD UPPER WEB AT BS 663 BETWEEN RBL 31.83 TO 45.64 AND Z -6. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, REPAIR 3.
DURING INSPECTION, FOUND THE BULKHEAD WEB CRACKED AT BS 663 BETWEEN LBL 31.83 TO 45.64 AND Z -6. MAINTENANCE REPAIRED THE BULKHEAD IAW SRM 57-10-10, REPAIR 3.
DURING INSPECTION, FOUND CRACKED ON THE BULKHEAD UPPER WEB AT BS 663 BETWEEN LBL 31.83 TO 45.64. MAINTENANCE REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, REPAIR 3.
DURING INSPECTION, FOUND A CRACKED UPPER WEB ON THE BS 663 BULKHEAD BETWEEN RBL 31.83 TO 45.64, Z -6. MAINTENANCE REPAIRED THE BULKHEAD IAW SRM 57-10-10, REPAIR 3.
(LOG 03388120) DURING INSPECTION FOUND CRACKED LOWER RIGHT WEB ON WING CENTER SECTION (BULKHEAD) OF STA 663 BTW RBL 40.0 TO 54.21. MAINTENANCE REPAIRED PER B737-800 SRM 57-10-10 REPAIR 2.
DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BTW STATION -312 TO STATION -328, S-29 TO S-27L, E&E COMPARTMENT. MAINTENANCE REPLACED INTERCOSTAL PER DWG 141A3504 REV A AND SRM 51-40-02 GENERAL.
DURING INSPECTION FOUND CRACK ON INTERCOSTAL FROM STA 312 TO 328 AND STA LBL 45 AT FLOOR STRUCTURE. MAINTENANCE REPLACED INTERCOSTAL PER SRM 53-10-51 AND 51-40-02.
DURING INSPECTION FOUND CRACK ON INTERCOSTAL FROM STATION 312 TO 328 AND STATION LBL 45 AT FLOOR STRUCTURE. MAINTENANCE REPLACED INTERCOSTAL PER SRM 53-10-51 AND 51-40-02.
DURING INSPECTION FOUND CRACK ON INTERCOSTAL FROM STATION 328 TO 344 AND STATION LBL 45 AT FLOOR STRUCTURE. MAINTENANCE REPLACED INTERCOSTAL PER SRM 53-10-51 AND 51-40-02.
DURING FLIGHT CREW REPORTED THEY HAD AN OVEN SMOKING, VISIBLE SMOKE WITH A PLASTIC SMELL WHEN TURNED ON. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY OVEN PER AMM 25-31. INSPECTED CONNECTOR AND WIRING, ALL OPS OK.
DURING INSPECTION, FOUND PASSENGER SEAT ROW 32 DEF, SEAT TRACK UPPER CROWN LUG BROKE OFF AT SEAT ATTACH POINT BS 857, RBL 24. MAINTENANCE R & R SEAT TRACK FROM BS 837 TO BS 887, RBL 24 IAW SRM 53-00-52, REPAIR 5.
DURING INSPECTION FOUND LOWER VHF ANTENNA DOUBLER HAS TWO STUCK FASTENERS AND EVIDENCE OF LIGHT SURFACE CORROSION ON DOUBLER AND EXTERNAL SKIN. MAINTENANCE REMOVED CORROSION FROM SKIN UNDER LOWER VHF ANTENNA IAW ERA 537918-14 REV ORIGINAL AND PRI ER/A 537918-14 REV ORIGINAL. RESTORED FINISH IAW MM 51-21-72. FABRICATED AND INSTALLED ADAPTOR PLATE (DOUBLER) IAW DWG 143A3281.
DURING INSPECTION, FOUND RT HORIZONTAL, L/E, STABILIZER STATION 212.3+5", HAS DENT ON L/E. MAINTENANCE REPAIRED IAW SRM 55-10-01, REPAIR 1.
DURING INSPECTION, FOUND BS 519, LBL 24 HAS AREA OF WEAR. MAINTENANCE REPAIRED SEAT TRACK AT BS 519, LBL 24 IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION FOUND BS 519, RBL 24 HAS AREA OF WEAR. MAINTENANCE REPAIRED SEAT TRACK AT BS 519, RBL 24 IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND BS 519, RBL 45 SEAT TRACK HAS AREA OF WEAR. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-52, REPAIR 4.
DURING INSPECTION, FOUND SEAT TRACK BS 519, LBL 45 HAS AREA OF WEAR. MAINTENANCE FABRICATED AND INSTALLED SEAT TRACK REPAIR IAW SRM 53-00-52, REPAIR 4.
DURING TEST, FOUND EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECKS. MAINTENANCE REPLACED THE BATTERY PACKS IAW AMM 33-51-06. OPS CHECKED GOOD.
DURING INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 32 ABC, BULLNOSE PANEL. FOUND CONNECTOR D12882, DISCONNECTED. CONNECTED. OPS CHECKED NORMAL.
DURING DEPLOYMENT TEST, THE R1 ESCAPE SLIDE FAILED TO DEPLOY. MAINTENANCE REPLACED DOOR R1 ESCAPE SLIDE ASSY IAW AMDS 2560-44-25.
FUSELAGE SEAT TRACKS FASTENERS, REPAIRED IAW AA 5321-01065.
FUSELAGE CABIN FLOOR STRUCTURE LONGITUDINAL FLOORBEAM S LBL 45.50 RBL 24.75 AND RBL 45.5 AT FS 727 REPAIRED IAW ERA 519620-14.
DURING INSPECTION, FOUND EMERGENCY LIGHTS AT SEAT ROWS 16DEF, 17DEF, AND 18DEF ARE INOPERATIVE. MX REPLACED SEAT HARNESS AT SEAT 18DEF IAW WDM 33-51-22. OPS TEST OK.
DURING TEST, EMERGENCY ESCAPE PATH LIGHT BATTERY PACK M1671 FAILED TEST. MX REPLACED BATTERY PACK M1671 IAW AMM33-51-06. OPS CHECK OK.
PSV14 AIRCRAFT DAMAGE RT SIDE OF FUSELAGE STA 1068 STGR 20R. REPAIR PER ERA 498050-14 REV ORIGINAL.
PSV 14 FWD CARGO STA 500C FRAME STGR 26L HAS DENT. REPAIR PER ERA 498053-14 REV ORIG.
PSV14 CABIN FLOORBEAM 312 LBL 12 AND 13 UPPER SURFACE CORRODED. REPAIRED PER ERA 497355-14 REV ORIG.
PSV14 CABIN FLOORBEAM STA 986.5 RBL 43 CORRODED. REPAIR PER B737-800 SRM 53-70-51 REPAIR 4.
F/O R1 WINDOW INNER PANE CRACKED. FLIGHT DIVERTED AND LANDED UNEVENTFULLY. R1 WINDOW WAS REPLACED AND WINDOW HEAT SYS TESTED SUCESSFULLY.
LT AFT OVERWING EXIT LIGHT INOP DUE TO BAD POWER SUPPLY. M1695 REPLACED LT AFT EMERGENCY LIGHT CHARGER. OPS CK GOOD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.
THE FUSELAGE SKIN HAD LIGHTNING STRIKE DAMAGE AT THE S-14L LAP SPLICE AT STA 400. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.
NR 1 ENGINE SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT ON AND WOULD NOT EXTINGUISH WITH THROTTLE AT IDLE. T/S LT ENG OIL FILTER BYPASS LITE IAW FIM FOUND NO FILTER DEB. REMOVED CHIP DETECTOR AND FOUND METAL ON FWD DETECTOR 537332005. REMOVED AGB IAW ESM 72-00-63 940757 INSTALLED AGB IAW ESM 72--00-63 RAN NBR 1 ENG IAW M/M ENG TEST 3B CKS GOOD AND LEAK CKS GOOD.
WHEN FLAPS EXTENDED TO 1 AT 210 KTS AIRCRAFT ROLLED LEFT, BEYOND 1, ROLL MOMENT REMAINED. FOUND LT OUTBOARD AFT FLAP CONTROL BELLCRANK BROKEN. REPLACED SAME.
EMERGENCY LIGHT ABOVE 14C INOP. RELAMPED, OPS NORMAL.
REAR GALLEY CENTER OVERHEAD EMERGENCY SIGN LOOSE. SECURED EMERGENCY EXIT SIGN. CKS OK.
WHILE ACCOMPLISHING INSPECTIONS OF THE LT ELEVATOR TAB PER AD 2001-08-09 & 2001-14-05, A SMALL AREA OF EROSION WAS FOUND ON THE UPPER SKIN OF TRAILING EDGE. THE DAMAGE WAS REPAIRED WITH A SEALING REPAIR PER THE B737-800 SRM AND APPROVED/DOCUMENTED PER ER/A 382205-14AD.
COCKPIT HALON FIRE EXTINGUISHER FOUND EMPTY, SEAL WAS NOT BROKEN AND GREEN DISCHARGE BUTTON WAS INTACT ALONG WITH HEAT SHRINK ON PULL PIN. MECHANIC NOTICED CONTROL HEAD WAS LOOSE. REPLACED EXTINGUISHER.