N543US
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 | 2019-08-18 – 2019-08-18 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2019-08-18 – 2019-08-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
SHIP 5643 SLIDE LIGHT AT 2L AND 4L EXTINGUISHED WHILE AIRBORNE. CORRECTIVE ACTION: CLEAN AND LUBE GIRT BAR AND FLUSH FITTING IAW B757 AMM 25-66. 2L DOOR OF FOR SVC. INSPECT 4L DOOR IAW B757 AMM 25-66. FOUND LIFT ASSEMBLY BLOCK WORN. ADJUSTED GIRT BAR MECHANISM PER B757 AMM 52-11. R/R AFT GIRT BAR LIFT ASSY IAW B757 CMM 52-11-25. OPS CK GOOD. (6601219)
SHIP 5643 BOTH PACKS PRODUCE A HEAVY MUSTY SMELL, MOST NOTICABLE WHEN SWITCHING PACKS FROM ENGINE O APU BLEED AIR AND VICEVERSA. CORRECTIVE ACTION: T/S FOUND OIL CONTMINATION AT HEAT EXCHANGER - LT AND RT. REPLACED LT AND RT SIDE ECS BAY PRIMARY AND SECONDARY HEAT EXCHANGERS REF B757 AMM 21-51. REPLACED RECIRC FAN. C/W OIL CONTAMINATION REMOVAL.
SHIP 5643 3L DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT DOES NOT ILLUMINATE. CORRECTIVE ACTION: REMOVED FOD FROM L3/L4 DOOR GIRT BAR FLOOR FITTING. OPS CHECK L3 /L4 DOOR ARMING MECHANISM AND LIGHT PER B757 AMM 25-66-01, OPS CK OK. (0620239)
SHIP 5643 -DIV/DE- TO GSP DUE TO DIRTY SOCK SMELL IN CRUISE. CORRECTIVE ACTION: FOUND OIL IN APU BLEED DUCT, PERFORMED OIL CONTAMINATION REMOVAL. R/R BOTH RECIRC FAN FILTERS. (SUBSEQUENTLY CHANGED APU)
SHIP 5643 -MISC/DE- DUE TO NORMAL AND ALTERNATE ANTISKID FAULT. CORRECTIVE ACTION: REPLACED NUMBER 2 WHEEL SPEED TRANSDUCER.
AIRCRAFT 5643, ON WALKAROUND SAW L4 DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: REPLACED L4 DOOR SLIDE LIGHT LAMP. (LP 5410082)
FA REPORTED ELECTRICAL BURNING SMELL IN AFT GALLEY ON DECENT. R/R AFT GALLEY LIGHT IAW B757 AMM 33-27. OPS CHK NML. NO DEFECTS NOTED.
SHIP 5643 -PRES/DIV- TO CVG DUE TO LT PACK FAIL WITH RT PACK ALREADY ON MEL. CREW DONNED O2 MASKS. CORRECTIVE ACTION: R/R LT PACK REHEATER DUCT DUE TO CRACK. R/R RT PACK LOW FLOW RELAY AND PACK FLOW CONTROL SHUTOFF VALVE. A/C RTS.
SHIP 5643 3L SLIDE LIGHT MISSING. CORRECTIVE ACTION: INSTALLED NEW SLIDE LIGHT CAP.OPS CKS NML IAW B757 AMM 33-51 AND ACCOMPLISHED PERMANENT RESTORATION PER ERA 614982-14 REV IR. (5549376)
SHIP 5643 DENT ON RIGHT WING PANEL 611DB. CORRECTIVE ACTION: REF ERA 614118-14. (5086408)
SHIP 5643 -MISC/DE- CREW DECLARED EMERGENCY DUE TO TE FLAP ASYM ON APPROACH. CORRECTIVE ACTION: SECURED LOOSE CONNECTOR ON FLAP POWER DRIVE UNIT.
SHIP 5643 EXIT SING AT DOOR L2 FELL OFF. CORRECTIVE ACTION: RE SECURED EMERGENCY EXIT LIGHT COVER PER B757 AMM 33-51. NO FAULTS NOTED AT THIS TIME. (4906888)
SHIP 5643 AFTER INSPECTION OF L-1 DOOR, ROTARY SNUBBER FOUND TO BE OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC:00056- REMOVED AND REPLACED L1 DOOR SNUBBER IAW B757 AMM 52-11-10. (2954289)
SHIP 5643 RH ENG DRAG FTG CLAMP-UP HOLE #12 HAS GOUGES AND CORROSION NOTED IN SKIN LOCATED AT 7 AND 9 O'CLOCK POSITION. CORRECTIVE ACTION: REAMED HOLE #12 IN THE SKIN CONCENTRICALLY UP TO 0.06557" AND C/ W HFEC OPEN HOLE INSPECTION NO DEFECTS NOTED, ASSET#'S 21511,17459,23968, FABRICATED INSTALLED, REAMED FREEZE PLUG AND INSTALLED NEW FASTENER AT HOLE IAW ER/A 582596-14AD REV C. (2946345)
SHIP 5643 R-4 PASSENGER DOOR, ROTARY SNUBBER FOUND TO BE OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND INSTALLED R4 DOOR ROTARY SNUBBER IAW B757 AMM 52-11. (2923005)
SHIP 5643 -SMKE/FUME- CREW REPORTED BRIEF AND QUICKLY DISSIPATING SMOKE AND ELECTRICAL ODOR IN FLIGHT DECK AFTER LANDING. CREW OXYGEN MASKS DONNED. NO ODOR OR VISIBLE ACCUMULATION IN PASSENGER CABIN. CORRECTIVE ACTION: T/S NO SMOKE SMELL PRESENT, MTC C/W MCC NO GO LOG. DOOR 2 HEATER DEFERRED.
SHIP 5643 R1 DOOR DIFFICULT TO CLOSE FROM THE OUTSIDE OF THE A/C. CORRECTIVE ACTION: FOUND DOOR TO NOT BE SITTING FLUSH WITH A/C. REMAINS CRACKED OPEN. PER MCC REQUEST, INSPECT DOOR LINKAGES, SEALS ETC. REF B757 AMM 52- 11. REMOVED ESCAPE SLIDE RAFT COVER PER B757 AMM 52-11. ADJUSTED DOOR, R1, AS PER B757 AMM 52-11, OPS CK GOOD. STOWED SLIDE PIN AND INSTALLED SLIDE COVER PER B757 AMM 52-11. (2747115)
SHIP 5643 1 RIGHT DOOR IS BROKEN AND WOULD NOT CLOSE. CORRECTIVE ACTION: PERFORMED OPS CHECK OF 1R DOOR. CHECK OK.REF B757 AMM 52-11. (4193226)
SHIP 5643 -DIV- TO JFK DUE TO WEATHER RADAR WITH STORMY WEATHER ENROUTE. CORRECTIVE ACTION: R/R WEATHER RADAR ANTENNA DRIVE UNIT AND TRANSCEIVER.
SHIP 5643 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS****L3 SLIDE LIGHT INOP. CORRECTIVE ACTION: EXAMINED GIRT BAR LOCK PER B757 AMM 25-66. LIGHT OPS NML. (2676529)
SHIP 5643 DOOR 4L UPPER FORWARD CM FOLLOWER BEARING BROKEN. CORRECTIVE ACTION: REMOVE AND REPLACE THE FWD UPPER LATCH CAM ROLLER B757 AMM 52-11 -00. ADJ. AND OPS CH. GD. (9462370)
SHIP 5643 R FWD ENTRY DOOR WOULD NOT ARM OR CLOSE COMPLETELY. CORRECTIVE ACTION: OPENED & RE-CLOSED R1 DOOR ARMED & OPS CHECK GOOD REF B757 AMM 52-00. (9558990)
SHIP 5643 DURING SVC FOUND MULTIPLE EMERGENCY LIGHTS INOP - EPATH SEATS 43 -45 DEF, 3R UPPER INTERIOR SIGN, 3L LOWER INTERIOR SIGN, 3R EXTERIOR EMER. LIGHT. CORRECTIVE ACTION: T/S PER B757-200 SSM 33-51. FOUND ALL LIGHTS ASSOCIATED WITH BATTERY PACK M736 INOP, INSTALLED POWER SUPPLY PER B757 AMM 33-51. TEST OK. (9558943)
COMPLY WITH ERA 604561-14AD REV. ORIGINAL. COMPLIED WITH ERA 604561-14AD REV ORIGINAL.
SHIP 5643 1R DOOR DOES NOT CLOSE PROPERLY. CORRECTIVE ACTOIN: CYCLED 1R DOOR, DOOR OPS NML. (9171718)
SHIP 5643 EMERGENCY EXIT COVER KNOCKED OFF BY PAX BAG. CORRECTIVE ACTION: REATTACHED COVER. CHECKS OK. (2290539)
SHIP 5643 2L DOOR NOT CLOSING PROPERLY & GUST LOCK RELEASE NOT LATCHING. CORRECTIVE ACTION: FOUND EXTERIOR HANDLE OUT OF SEQUENCE. CYCLED & ALL CKS WELL. EXERCISED GUST LOCK & NOW OPS NORMAL ALSO. OK FOR CONT. SVC. REF B757 AMM 52-11. (9279732)
SHIP 5643 DURING SVC CHK FOUND LAMP INOP AT 16D CEILING PANEL. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHT CAP ASSY BY SEAT 16C/D PER B757 AMM 33-51. CHECKS GOOD. (8768633)
SHIP 5643 ON WAKE UP FOUND - SQUIB TEST 2 - EMERGENCY ESCAPE LEFT BOTTLE PRESS TEST FAIL. CORRECTIVE ACTION: T/S PER FIM TASK 25-65. R/R RELAY K10486 AND NO HELP ALSO SWAPPED SQUIB TEST PANEL - REINSTALLED OLD TEST PANEL. R/R OVER WING EMERGENCY ESCAPE SLIDE INFLATOR PER AMDS CARD# OPS CHECK GOOD LEFT OFF WING SLIDE BOTTLE INSTALLED PER JIC. (7830070)
SHIP 5643 ROW 23-26 EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R BATTERY PACK M10507 IAW B757 AMM 33-51. OPS CHK NML. (7830001)
SHIP 5643 HE #3 SLAT T/E WEDGE LWR SURFACE HAS AN AREA THAT HAS AN INDICATION OF DISBOND NOTED. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON #3 SLAT T/E WEDGE IAW BOEING S.B. 757-57-0066, B757-200 SRM. SLAT REMOVED AND INSTALLED ON AMDS W/C. (1933049)
SHIP 5643 DTA MONITOR INSPECTION LOG REF ERA 593624-14 REV. B. CORRECTIVE ACTION: REF ERA 593624-14 REV B. (1932962)
SHIP 5643 DTA MONITOR INSPECTION LOG REF ERA 593633-14 REV. B. , SEVERAL DENTS (5EA) WERE FOUND ON EXTERNAL SKIN. CORRECTIVE ACTION: REF ERA 593633-14 REV B AND REF 593560-14. (1932028)
SHIP 5643 BS 1640 FUSELAGE FRAME R/H SIDE LOWER I/B FASTENER HOLE AT S-14R HAS CRACK INDICATION AT THE 3 OCLOCK POSITION (I/B SIDE OF FASTENER HOLE VIEWED FROM THE FWD SIDE OF FRAME LOOKING AFT) LAYERS NEED TO BE SEPARATED (INTERCOSTAL TEE CLIP FRAME WEB & LOWER HINGE FITTING FOR FURTHER NDT EVALUATION. CORRECTIVE ACTION: REPAIRED STA 1640 R/H FRAME LOWER I/B HOLE @ S-14R IAW ERA 593495-14AD REV ORIG. (1930783)
SHIP 5643 DENT FOUND AT STA 740-760 S-4L TO S6L AND REQUIRES REPAIR. CORRECTIVE ACTION: REPAIRED UPPER FUSELAGE SKIN STA 740-760 S-4L TO S5L IAW ERA # 593626-14 REV A. (1929545)
SHIP 5643 DENT FOUND AT STA 740-760 S-4R TO S-6R AND REQUIRES REPAIR. CORRECTIVE ACTION: REPAIRED UPPER FUSELAGE SKIN FROM STA 740 - 780 STR 4 R TO STR 6R IAW ERA # 593624-14 REV A. (1929431)
SHIP 5643 FUSELAGE SKIN UPPER CROWN HAS 5 EACH LOCATIONS WITH DENTS AND REQUIRES REPAIRS STA 760-780 S-4R TO S-4L. CORRECTIVE ACTION: REPAIRED UPPER FUSELAGE SKIN FROM STA 760 TO 780 STR 4L TO STR 4R IAW ERA # 593633-14 REV ORIGINAL. (1929442)
SHIP 5643 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 582596-14 REV A. CORRECTIVE ACTION: REF ERA 582596-14AD REV A. (1754150)
SHIP 5643 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 582596-14 REV A. CORRECTIVE ACTION: REF ERA 582596-14AD REV B. (1754160)
SHIP 5643 ON SVC CHK R1 SLIDE D-RING NOT VISIBLE FOR SURVIVAL KIT. CORRECTIVE ACTION:REMOVED SLIDE COVER AND PINNED R-1 SLIDE. FOUND D-RING INCORRECT ROUTING. AS A PRECAUTION REMOVED AND REPLACED R-1 SLIDE PER AMDS WORK CARD. (7192774)
SHIP 5643 -ATB- ON TAKE OFF F/O SIDE AIRSPEED SLOWLY WENT TO ZERO ALTIMETER FROZE AT ABOUT 1100', WENT THROUGH QRH PROCEDURE AND BROUGHT BACK F/O A/S & ALT W/ AIR DATA SWITCH. SEVERAL EICAS MSGS MACH/SPD TRIM AND RUDDER RATIO DID NOT CLEAR. CORRECTIVE ACTION: FOUND RIGHT ADC STATIC LINE COUPLING DISCONNECTED, REINSTALLED PERFORMED ADC TEST PER AMM SYSTEMS CHECKS GOOD.
(AIRCRAFT 5643, L/P 6381424) DOOR 1R WILL NOT ARM. CORRECTIVE ACTION: OPENED DOOR AND CK FOR DEBRIS. NOTED WATER DRAINING FROM DOOR. CLOSED AND ARMED SLIDE. OPS NORMAL.
RT FWD ENTRY DOOR WILL NOT DISARM. DISARM LEVER NOT FULLY TO LEFT. CLEANED DEBRI FROM TRACK AREA.
(AIRCRAFT 5643, L/P 6157781) 2L EMERGENCY EXIT SIGN FELL OFF WHEN DOOR OPENED. CORRECTIVE ACTION: REINSTALLED EXIT ROW SIGN.
EMERGENCY EXIT SIGNS INOPERATIVE, REPLACED THE EXIT SIGN IAW 33-51. OK FOR SERVICE.
ENROUTE NOTICED A BRIGHT ORANGE ELECTRICAL ARC IN CAPTAINS LOWER RIGHT FWD WINDOW. ACCOMPLISHED NNC TURNED L FWD HEAT OFF. R & R 1 LEFT WINDSHIED IAW AMM 56-11-01. THIRD TORQUE COMPLETED.
EMERGENCY SIGN OVER THE L2 DOOR FELL DOWN. ADJUSTED EMERGENCY EXIT SIGN AND RESECURED.
(AIRCRAFT 5643, L/P 6157756) EMERGENCY EXIT LIGHT LENSE OVER L2 DOOR CAME OFF. CORRECTIVE ACTION: RESECURED LENSE.
LEFT AFT ENTRY DOOR LIGHT ILLUMINATED ON THE GROUND. ADJUSTED LEFT AFT ENTRY DOOR SENSOR, PERFORMED OPERATIONAL CHECK, OPS CHECKED GOOD.
SHIP 5643 RIGHT WING HAS FUEL LEAKING OUT OF DRY BAY "WEEP" HOLE. CORRECTIVE ACTION: REPAIRED R/W DRY BAY BETWEEN STA 285 & 313 IAW ER/A 583355-14 REV. ORIG. (1379026)
SHIP 5643 HARD LANDING STA 395 BULKHEAD L/H CHORD REPAIR ESR 006. CORRECTIVE ACTION: REPAIRED L/H CHORD STA 395 IAW DELTA ER/A 582392-14 REV. 0 MONITOR INSPECTION LOG 1371499. (1379032)
(AIRCRAFT 5643, L/P 1379019) LEFT WING INTERNAL DRY BAY IS LEAKING FUEL OUT OF "WEEP" HOLE. CORRECTIVE ACTION: REPAIRED IAW ERA 583350-14.
SHIP 5643 SECTION I REPAIR ERA 583350-14 REV ORIG TO LH WING DRY BAY FUEL BARRIER REQUIRES SECTION II REPAIR. CORRECTIVE ACTION: REF ERA 583350-14. (1377990)
EMERGENCY TRACK LIGHTING INOPERATIVE, BS 388 TO 680 L&R. CONNECTED THE CONNECTORS IAW AMDS CARD 2525-0062.
SHIP 5643 SECTION I REPAIR TO RH WING DRY BAY FUEL BARRIER REQUIRES SECTION II REPAIR WITHIN 24 MONTHS. CORRECTIVE ACTION: REF ERA 583355 REV A. (1377981)
(AIRCRAFT 5643, L/P 1377015) HARD LANDING STA 395 BULKHEAD R/H CHORD REPAIR. CORRECTIVE ACTION: REPAIRED STA 395 BULKHEAD R/H CHORD IAW ERA 582391-14 REV ORIGINAL.
AFT CARGO STRINGER 20R SPLICE AT BS 1620 IS CRACKED. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED NEW AFT CARGO BS 1620 STRINGER 20R SPLICE IAW SRM 51-40-02 AND DWG 146N3821 REV P.
AFT CARGO RT SIDE TUNNEL POSSIBLE CRACK AND HAS CORROSION UNDER STRINGER STA 1620 S20R. CORRECTIVE ACTION: CUT OUT DAMAGED SECTION OF STR 20R AND REPAIRED STRINGER SECTION IAW SRM 53-00-03-2R PROCEDURE 1 REPAIR 1.
(AIRCRAFT 5643, L/P 1371258) 2 DEEP BLEND OUTS AROUND FASTENERS ON EXTERNAL FUSELAGE SKIN BTWN STA 1520-1540 ON STR 27R. CORRECTIVE ACTION: REPAIRED AREA IAW B757 SRM 53-00-01 REPAIR 28 INSPECTION THRESHOLD 25,000 FLIGHT CYCLES. REPEAT INTERVALS 6,000 FLIGHT CYCLES HFEC AND EXTERNAL DETAILED VISUAL NDT PT6 51-00-01.
(AIRCRAFT 5643, L/P 1371985) FWD CARGO BS720 SHEAR TIE CORRODED INB OF S-27L UNDER TRANSITION PANEL. CORRECTIVE ACTION: REMOVED CORROSION AT FWD CARGO BS 770 SHEAR TIE STR 27L IAW B757 SRM 51-10-02. REMOVED, FABRICATED AND INSTALLED NEW SHEAR TIE.
(AIRCRAFT 5643, L/P 1371509) FASTENER #2 HAS CRACK INDICATIONS IN UPPER SKIN 4 OCLOCK AND 10 OCLOCK POSITIONS LOOKING AFT. CORRECTIVE ACTION: REPAIRED RIGHT WING FWD DRAG FITTING #2 HOLE IAW ER/A # 582596-14 AD.
(AIRCRAFT 5643, L/P 1371379) FUSELAGE SKIN STA 395 STR 18R TO 17R PERMANENT REPAIR. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE SKIN STA 395 STR CUT OUT IAW DELTA ERA 582140-14 REV ORIGINAL SECTION 1.
(AIRCRAFT 5643, L/P 1369948) LOCATED DENT AT FUSELAGE SKIN STA 460, STR 22R - 23R. CORRECTIVE ACTION: DENT OUT OF LIMITS PER B757 SRM 53-00-01. REMOVED DAMAGE, FABRICATED FILLER , DOUBLER, TRIPLER, ALODINED AND REPAIR PARTS. INSTALLED REPAIR PARTS. SEALED AFFECTED AREAS, ALL IAW B757-SRM-53-00-01 REPAIR 29, SRM 51-20-01 AND SRM 51-20-05.
(AIRCRAFT 5643, L/P 1368823) LOCATED DENT AT FUSELAGE SKIN STA 690 STR 23L-24L. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED AREA IAW B757 SRM 53-00-01 REPAIR 28 FIGURE 201 THIS IS A CATEGORY B REPAIR AND REQUIRES SUPPLEMENTAL INSPECTIONS AS GIVEN IN B757 SRM 53-00-01 REPAIR 28 TABLE 206 STARTING AT 37,500 FLIGHT CYCLES AND EVERY 6,000 CYCLES THEREAFTER BY HFEC AND DETAILED VISUAL INSPECTION.
(AIRCRAFT 5643, L/P 1368391) MAIN CABIN L/H OUTBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1358 AND STA 1512. CORRECTIVE ACTION: REMOVED FLOOR PNLS IN MAIN CABIN L/H SIDE, O/B SEAT TRACK, I/B AND O/B SIDE BTWN STA 1320-1540 FOR ACCESS TO PERFORM A REPAIR, REMOVED MAIN CABIN L/H SIDE O/B SEAT TRACK, PERFORMED A MATERIAL VERIFICATION FOR REPAIR, FABRICATED NEW PARTS, CUT OUT DAMAGED SEAT TRACK FOR NEW PARTS, LOCATED AND DRILLED NEW PARTS, TREATED AND PRIMED NEW PARTS, APPLIED TOP COAT ON NEW PARTS, INSTALLED PARTS, AND NEW ANGLES, REINSTALLED FLOOR PNLS IN MAIN CABIN L/H SIDE, O/B SEAT TRACK, I/B AND O/B SIDE BTWN STA 1320-1540, IAW B757 SRM 51-40-02 SRM 53-00-52 REPAIR 1, SRM 51-20-01 AND AMM 51-21-00.
(AIRCRAFT 5643, L/P 1368752) LOCATED 3 DENTS ON EXTERNAL SKIN REPAIR BTWN STA 1600-1620 APPROX STR 17L. CORRECTIVE ACTION: REMOVED DAMAGED FUSELAGE SKIN REPAIR DOUBLER STA 1600 TO 1620 STR 17L IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW EA 582946-14 REV O.
(AIRCRAFT 5643, L/P 1363263) HARD LANDING DAMAGE FRAME AND SHEAR TIE STA 377 STR 23L. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED NEW FRAME SECTION AT STA 377 L/H IAW DRW# 141N1220 REV - AND SHEAR TIE AT STA 377 STR 23L IAW DRW# 141N1220 REV - . PARTS HEAT TREATED IAW AMS 2770.
(AIRCRAFT 5643, L/P 1363071) THERE IS CORROSION IN MID CABIN AREA STARTING AT STA 680 ON L/H SIDE OF RBL 24 SEAT TRACK ENDING AT STA 730. CORRECTIVE ACTION: REMOVED FABRICATED AND INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-05 AND B757 SRM 51-40-02.
(AIRCRAFT 5643, L/P 1358095) DENT ON EXTERNAL FUSELAGE SKIN BTWN STA 1320-1340, BTWN STR 29L-30. CORRECTIVE ACTION: FABRICATED REPAIR PARTS. LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR PARTS AS REQ IAW B757 SRM 53-00-01 R.29, SRM 51-40-02, 51-40-05, 51-40-08, INSTALLED ID TAG IAW DPS 900-5-1 NO:04, PERFORM A DECAL CONDITION INSPECTION EVERY C CHECK PER TOPP MANUAL 30-10-70 PAR1 PAGE 14.
(AIRCRAFT 5643, L/P 1358057) MAIN CABIN STA 1175 RH SIDE CREASE BEAM CORRODED. CORRECTIVE ACTION: REMOVED CORROSION AS REQ AT MAIN CABIN STA 1175 R/H INNER CHORD CUSP WEB. FABRICATED, LOCATED, DRILLED AND TRIMMED 3 EA REPAIR PARTS (1) EA STRAP. INSTALLED REPAIR PARTS IAW B757 SRM 53-00-13 REPAIR 2.
(AIRCRAFT 5643, L/P 1358130) LOCATED DENT AT FUSELAGE SKIN STA 500, STR 23R-24R. CORRECTIVE ACTION: FABRICATED REPAIR DOUBLER AND FILLER IAW B757 SRM 53-00-01, REPAIR 29 & NDTM PT 6 51-00-16, INSTALLED ID TAG IAW DPS 900-5-1 NO:04, PERFORM A DECAL CONDITION INSPECTION EVERY C CHECK PER TOPP MANUAL 30-10-70 PAR 1, PAGE 14.
(AIRCRAFT 5643, L/P 1355990) MAIN CABIN R/H OUTBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1325. CORRECTIVE ACTION: CUT OUT DAMAGED SECTION ON MAIN CABIN R/H OUT BOARD SEAT TRACK BETWEEN STA 1510 TO 1560 RBL 54 IAW B757 SRM 53-00-52 REP 1. FABRICATED AND INSTALLED REPAIR PARTS IAW B 757 SRM 53-00-52, REP 1 AND B 757 SRM 51-40-02.
(AIRCRAFT 5643, L/P 1356001) MAIN CABIN R/H INBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1295. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED NEW MAIN CABIN R/H INBOARD SEAT TRACK STA 1295 USING BAC 1520-792 7178 IAW B757 SRM 53-60-52 AND B 757 SRM 51-40-02 BETWEEN STA 1140 TO 1320.
(AIRCRAFT 5643, L/P 1355999) MAIN CABIN L/H INBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1510. CORRECTIVE ACTION: CUT OUT DAMAGED SECTION OF SEAT TRACK ON MAIN CABIN L/H INBOARD SEAT TRACK BETWEEN STA 1510 TO 1560 IAW B 757 SRM 53-00-52, FABRICATED AND INSTALLED REPAIR PARTS IAW B 757 SRM 53-00-52 REP 7 AND B 757 SRM 51-40-02.
(AIRCRAFT 5643, L/P 1339494) AFT CABIN FLOOR STRUCTURE HAS CORROSION ON UPPER SURFACE FROM STA 1681-1718 BL 0 - LBL 54. CORRECTIVE ACTION: REMOVED CORROSION AT FLOOR STRUCTURE AFT DECK FROM STA 1681 - 1718 BL 0 TO LBL 17 AND LBL 25 TO LBL 54 IAW B757 SRM 51-10-02, AREA WITH ORIGINAL THICKNESS .071 MATT LOSS .005 MATT REMAINING .066 TO BE WITHIN LIMITS IAW B757 SRM 53-00-51. AREA BETWEEN STA 1681 - 1718 LBL 18 TO LBL 24 WITH MATT REMAINING .060 TO BE OUT OF LIMITS IAW B757 SRM 53-00-51 CUT OUT DAMAGED AREA FABRICATED AND INSTALLED REPAIR PARTS IAW B757 SRM 53-60-51 REP 17.
(AIRCRAFT 5643, L/P 5894078) HARD LANDING ON NOSE WHEEL AFTER MAINS TOUCHED DOWN. CORRECTIVE ACTION: WHILE PERFORMING HARD LANDING PHASE I INSPECTION FOUND EXTENSIVE DAMAGE. REQUIRES PHASE II INSP. PER B757 AMM 05-51. REF. L/P 1251252 FOR PHASE II INSPECTION COMPLIED WITH. PERFORMED REPAIRS PER ER/A 580761-14 REV A AND ER/A 580760-14 REV A . REQUIRED INSPECTION COMPLIED WITH. REF LOG PAGE 5894099.
DAMAGED STRINGERS. COMPLIED WITH ERA 581455-14, COMPARE ERA 581455-14 REF ORIGINAL WITH PRI 581455-14 REV 0 THUR 5.
CROWN SKIN DAMAGED BS 550 - 661 STR 10L TO 10R. COMPLIED WITH ERA 581456-14, COMPARED ERA 581456-14 REV ORIGINAL WITH PRI 581456-14 REV 0 THUR 4, BOTH MATCH.
DURING ACCOMPLISHMENT OF OPEN HOLE EDDY CURRENT PER AA5311-01207-01B STEP 13, FOUND INBOARD HOLE HAS CRACK INDICATION AT APPROXIMATELY 3 O'CLOCK POSITION AS VIEWED FROM REAR. INDICATION IS IN THE STA 1681 FRAME, NOT THE CLIP ON AFT SIDE OF FRAME. CANNOT DETERMINE LENGTH OF CRACK WITH INSTALLATION STACK UP. COMPLIED WITH ER/A 581570-14AD REV ORIGINAL.
CRACK IN FRAME BS 1640 UNDER STRAP AT STRINGER 14L. UNABLE TO DETERMINE LENGTH. REPAIR MUST BE COMPLETED PRIOR TO FURTHER FLIGHT. COMPLIED WITH ER/A 581573-14AD REV ORIGINAL.
DURING PERMANENT REPAIR OF CROWN SKIN DAMAGE PER ER/A 581456-14, DAMAGE REMOVAL REQUIRED THE REMOVAL ON GPS ANTENNAS AND / MOUNTING STRUCTURE REF ERA 581683-14. CORRECTIVE ACTION: REF ERA 581683-14 REV A.
(AIRCRAFT 5643, L/P 5491190) STRAP HANGING FROM 1R DOOR NEAR BOTTOM OF DOOR SLIDE. RESECURED DITCHING STRAP TO SLIDE BUSSEL PER AMM 52-11.
(AIRCRAFT 5643, L/P 5340812) 3L DOOR SLIDE LIGHT WON'T COME ON & ARM HANDLE WILL NOT "ARM". CLEARED OBSTRUCTION - OPS CHECK GOOD. OK SERVICE - REF B757 AMM 25-66.
SHIP 5643 ON TAKEOFF "L AFT ENT DOOR" EICAS MSG CAME ON FOR A FEW SECONDS AND THEN EXTINGUISHED SEVERAL TIMES. CORRECTIVE ACTION: PSEU BITE SHOWS NO FAULTS AND TARGET POSITION INDICATES NORMAL. CLEANED AND INSPECTED PROX SWITCH AT DOOR 4L. ADJUSTED PROX SWITCH PLUNGER OUT SLIGHTLY TO ELIMINATE NUISANCE INDICATION. (5365382)
(AIRCRAFT 5643, L/P 4216116) DURING DESCENT GOT C HYD SYS PRESS EICAS MSG, COMPLIED W/ QRH AFTER LANDING DURING TAXI LOST R HYD SYSTEM. STOPPED A/C AND TOWED TO GATE. AFTER LANDING DURING TAXI LOST R HYD SYSTEM TRANSFER TO LOG #4216117. TROUBLESHOT CENTER HYD PRESS INDICATION PER B757 FIM 29-11-00-815-831. NO FAULTS FOUND. PERFORMED ENG RUN, TO RUN BOTH CENTER PUMPS. NO FAULTS. R&R CENTER PRESS X-MITTER M342 & C SYSTEM PRESSURE SWITCH S10002 AS PRECAUTION. REF B757 AMM 29-31-01 AND B757 AMM 29-11-19. OPS CHECKS GOOD. CONTACTED MC. OK FOR SVC.
SHIP 5643 DOOR 1R WILL NOT ARM. CORRECTIVE ACTION: RESECURED DOOR LAYNARD. (4396058)
SHIP 5643 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND SECURITY LANYARD LOOSE, RECONNECTED LANYARD REF B757 AMM 52-11. (4396012)
AT DEP, 1R DOOR WONT ARM. REMOVED DEBRIS. SATIS.
DURING A ROUTINE GIRT BAR TEST. THE L4 DOOR SHOWED CLOSED ALL THE TIME. EICAS DOES NOT SEE L4 DOOR OPEN. REPLACED THE DOOR WARNING SENSOR PLUNGER ROD IAW AMM 52-71-00. CHECKED GOOD.
R1 DOOR WONT ARM. INSPECTED THE GIRT BAR FOR SLIDE, CLEARED DEBRIS, CLOSED AND ARMED DOOR. OK FOR SERVICE.
PASSENGER SEATS, TRIPLE SEAT Y/C ROW 40 RIGHT FWD INBOARD SEAT TRACK DAMAGED. COMPLIED WITH ERA 569526-14 REV ORIG SEC II PERMANENT REPAIR, INSTRUCTIONS AND ERA 569675-14 REV ORIGINAL.
DOOR 1R HAS WIRE HANGING OUT OF THE BOTTOM. SECURED SURVIVAL ROPE CHK GOOD.
EMERGENCY LIGHT LENS AT SEAT 27A WAS MISSING. INSTALLED A NEW LENS IAW AMM 33-51.
AIR TURNBACK DUE TO THE CREW REPORTED DURING CLIMB, THERE WAS A HAZE AND ODOR IN THE COCKPIT WITH AN ASSOCIATED EQUIPMENT COOLING FAN OVERHEAT WARNING. REPLACED A SEIZED LEFT ACM. REPLACED LT LOW LIMIT VALVE AND REHEATER AS PRECAUTION. PERFORMED WATER SPRAY NOZZLE CHECK FOR LT PACK, CHECKED GOOD. INSP 2.5 BLEED RING FOR OIL LEAKS, NONE NOTED. PERFORMED SINGLE PACK CONFIDENCE CHECK, ALL WITHIN LIMITS. REPLACED RT TEMP CONTROL VALVE DUE FAULT, LOG 4387226.
DUE TO REPORTS OF R1 DOOR MECHANISM BEING STICKY AND HARD TO ARM. CLEANED, LUBED, AND INSPECTED THE R1 GIRT BAR ATTACH FITTINGS. MANUALLY ENGAGED GIRT BARS AND VERIFIED SLIDE LIGHT AND GIRT BAR ATTACHMENT.
SLIDE INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE L2 GIRT BAR PROXIMITY SENSOR IAW AMM 25-66.
R1 DOOR NOT ARMING. REPACKED A LOOSE STRING SO AS TO NOT INTERFERE WITH SLIDE MECHANISM.
ROW 26DEF HAS ONE RED EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS, OPS CHECKED NORMAL.
HOT ODOR REPORTED BY FLIGHT ATTENDANT COMING FROM VENTS EITHER SIDE OF THE L3 DOOR. VENTS WERE WARM. HOT ODOR. LASTED ABOUT 10 MINUTES. EXAMINED AREA ABOVE AND BELOW L3 DOOR NO SIGNERS OF BURNING OR HOT ODOR. PERFORMED CHECK OF AND EXAMINED COFFEEMAKER AT THE L3 DOOR. COFFEEMAKER INOPERATIVE. PERFORMED DOOR HEATER CHECK IAW AMM 21-45, OPS CHECKED GOOD. PERFORMED NOGO ODI PREVENTION CHECK LIST, NO OTHER CAUSES WERE FOUND.
R1 DOOR SLIDE WOULD NOT ARM. REMOVED DEBRIS FROM THE THRESHOLD. OPS CHECKED GOOD.
DEEP GOUGE AT BOTTOM OF VERTICAL STAB LT SIDE LOWER FWD ATTACH ANGLE. REPAIRED THE ATTACH ANGLE IAW ERA 562481-14, REV 0.
ANGLE HAS A DEEP GOUGE, BOTTOM OF VERTICAL LEFT SIDE LOWER FWD ATTACH ANGLE. COMPLIED WITH ERA 562481-14 REV ORIGINAL.
L4 DOOR SLIDE PACK BULGED AT CORNERS. SLIDE REPLACED.
RIGHT HORIZONTAL STAB, RIGHT SYSTEM ACTUATOR, MOST OUTBOARD UNIT BEARING WORN OUT, CLEVIS LINK SLOPPY, MOVES WHEN SHAKEN BY HAND. VISIBLE FROM BOTTOM, LOOKING UP, HEAVY RUST AROUND WORN BEARING. REPLACED PCU ON CARD 2900-4202-01.
L1 DOOR EMERGENCY POWER TRIGGER MECHANISM DID NOT MEET CABLE TRAVEL MEASUREMENT. THE MECHANISM WAS ADJUSTED IAW AMM 52-11-32.
CORROSION IN THE SKIN JOINT AT THE 6 O CLOCK POSITION ON THE FUSELAGE JUST BELOW THE AFT CARGO DOOR AND JUST IN FRONT OF THE ANTENNA ON THE BELLY. REPAIRED PER SRM 53-00-01 AND RESTORED FINISH PER SRM 51-20-01.
PNEUMATIC DUCT SUPPORT WORN IN WING L/E AT THE NR 6 SLAT. R & R THE SUPPORT BRACKET IAW AMM 36-11-01.
DIV TO OKC DUE TO CREW OXYGEN SLOWLY DECREASING AND DOWN TO 240 PSI. MTC FOUND OBS SEAT O2 MASK IN EMERGENCY, REPLACED OBS O2 STORAGE BOX. FOUND F/O O2 MASK LEAKING AT STORAGE BOX, REPLACED MASK AND STORAGE BOX. REPLACED O2 BOTTLE LEAK CHECKS GOOD.
L2 DOOR EXTERIOR HANDLE NOT SEATED FLUSH AFTER DOOR CLOSURE. ADJUSTED EXTERIOR DOOR HANDLE CATCH IAW AMM 52-11. DOOR HANDLE LATCHED & SECURED FLUSH AFTER CLOSURE. OK FOR SERVICE.
DOOR 3L DOOR ARMING HANDLE JAMMED WON'T MOVE. REMOVED DEBRIS FROM GIRT BAR, PERFORMED OPS CHK PER AMM 52-11, OPS CHKS GOOD. OK FOR SVC.
R1 DOOR SLIDE WILL NOT ARM.FOUND SURVIVAL STRAP ATTACH CHORD CAUGHT IN GIRT BAR MECHANISM. REPOSTIONED CHORD. DOOR SLIDE ARMS AND DISARMS. REF. B757 AMM 25-66.
2R ARM LEVER PART MISSING. SECURED COVERPLATE FOR DOOR HANDLE ATTACH.
R1 MAIN DOOR WOULDN'T ARM. SECURED THE R1 DOOR SLIDE LANYARD. GROUND CHECKED GOOD.
EXIT SIGN OVER 2L DOOR COVER FELL OFF. RESECURED EXIT SIGN.
DOOR 2R EXIT LENS COSMETICALLY DAMAGED. REPLACED LENS ACFT OK FOR SERVICE.
WHILE CONDUNTING AN OPS CHECK OF THE INTERIOR EMERGENCY LIGHTS DURING THE SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE IN MULTIPLE SECTIONS. FOUND BATTERIES DEPLETED AND UNABLE TO HOLD CHARGE AT BATTERY PACK CHARGERS M730, M732, M10568, M10699 AND M736. R & R DEFECTIVE UNITS IAW AMM 33-51. OPS CHECK GOOD.
EXIT SIGNS ON L2 DOOR FALL OFF. FOUND LENS 2 EA RETAINING LEAF SPRINGS BENT. REPOSITIONED SPRINGS. INSTALLED LENS IAW AMM 33-51-10. CKS GOOD. MCC ADVISED. OK FOR SERVICE.
ON TAKEOFF AND ENROUTE CABIN EMERGENCY LIGHTS WOULD ILLUMINATE WITH COCKPIT SWITCH IN ARMED POSITION. FOUND FORWARD EMERGENCY LIGHTS ON WITH COCKPIT SWITCH IN ARMED POSITION. R & R EMERGENCY LIGHT BATTERY CHARGER, M731 AND BATTERY IAW AMM 33-51. INSPECTED NLG EMERGENCY LIGHT TEST SWITCH WIRING. NO FAULTS FOUND. R & R EMERGENCY LIGHT POWER TRANSFER RELAY K10570. SYS OPS CHECKS NORMAL IAW AMM 33-51.
THE EMERGENCY LIGHTS FLICKERED ON AND OFF DURING TAKEOFF AND REMAINED ILLUMINATED UNTIL MID CLIMB. DOORS 1 AND 3 LIGHTS STAYED ILLUMINATED UNTIL CRUIZE. MAINTENANCE FOUND AND REPLACED TWO BAD BATTERY PACKS, 1 IN THE FWD GALLEY AND ONE IN THE AFT GALLEY. BOTH CHARGERS WERE ALSO REPLACED. LIGHTS CHECKED OK.
THE CABIN EMERGENCY LIGHTS ILLUMINATED ON TAKEOFF AND CLIMB OUT AND WERE UNCONTROLLABLE FROM THE F/F PANEL. MAINTENANCE TROUBLESHOT THE EMERGENCY LIGHT SYS AND COULD NOT FIND A PROBLEM. THE ACFT WAS RETURNED TO SERVICE.
EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EMERGENCY EXIT SIGN ABOVE L2 DOOR IAW AMM 25-60.
EMERGENCY LIGHT AT M731 INOPERATIVE. REPLACED CHARGER ASSY IAW AMM 33-50, CHECKED OK FOR SERVICE.
DURING SERVICE CHECK, FOUND LT OUTSIDE EMERGENCY LIGHT OUT. REPLACED THE FUSE. FOUND BETWEEN PIN NR 9, D7764 AND GROUND, 100 OHM MORE. RESEQURED GD2994-DC TERMINAL AND CKS NORMAL IAW MM33-51, WDM 33-51-13.
EXTERIOR EMERGENCY LIGHT AT DOOR 1 RT & EMERGENCY LIGHT AT ROW 1 THRU 3 INOPERATIVE. ISOL & T/S BATTERY PACK INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED OK.
L2 DOOR EMERGENCY EXIT OVERHEAD SIGN FALLS OFF WHEN DOOR IS CLOSED OR OPENED. REPLACED OVERHEAD EXIT SIGN.
L4 DOOR SNUBBER FAILED CHECK ON WC 521-2102-4L, STEP 2. REPLACED L4 DOOR SNUBBER REF N/R CARD 00273.
MSP MAINTENANCE FOUND EMERGENCY EXIT LIGHTING INOPERATIVE ROWS 24-28. EMERGENCY LIGHTS POWER SUPPLY ABOVE ROW 23 DEF WAS REPLACED. LP1941441.
EMERGENCY AISLE SEAT LIGHTS INOPERATIVE FROM ROW 20 TO ROW 28. TROUBLESHOT & REPAIRED WIRING IAW WDM 33-51-22 AND EMERGENCY LIGHTS INSTALLATION DWG 5B33-41158.
DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE ON SEATS ROWS 20 TO 28. R & R EMERGENCY POWER SUPPLY ON ROW 23. OPS CHECKED NORMAL.
ROW 24ABC TO 28ABC SEAT EMERGENCY LIGHTS OUT. R & R BATTERY PACK CHARGER IAW AMM 33-51.
ON S/C FOUND 34C EMERGENCY ESCAPE LIGHT INOPERATIVE. REPLACED SPLICE CONNECTION AT 34C.
AFT AISLE EXIT SIGN AND R4 DOOR EXIT SIGN INOPERATIVE DURING EMERGENCY LIGHT TEST. REPLACED POWER SUPPLY M00737 AND BATTERY PACK IAW AMM 33-51-07. EMERGENCY LIGHT CK OK.
FUSELAGE SKIN BS 570 - 660, S14-19L DAMAGED. SKIN REPLACED IAW ER/A 520601-14AD.
L4 DOOR GIRT BAR LOCK SPRING CHECK FAILED. R & R L4 DOOR GIRT BAR ASSY IAW AMM 25-66-10-402-022, OPS CHECKED GOOD.
DURING REMOVAL OF RT TRANSITION PANEL, DISCOVERED CORROSION ON AFT CARGO LOWER SILL ANGLE BS 1360-1380. R & R SILL ANGLE IAW SRM 51-40-02. PG 1-10.
AFT CABIN FLOOR LOWER SURFACE BS 1681, LBL 3, 39 AND 46 IS CORRODED. BLENDED OUT CORROSION FOUND OUT OF LIMIT. ACCOMPLISHED PERMANENT REPAIR IAW REF SRM 53-60-51 REPAIR.
MAIN CABIN CREASE BEAM HAS CORROSION AT STRINGER 17R, BS 1180-1200. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, PG 102, FIG 101. INSTALLED PERMANENT REPAIR IAW ER/A 520606-14.
FUSELAGE FRAME BS 540, S23-25L, DENTED IN TWO PLACES. FRAME TRIMMED AND REPAIRED IAW ER/A 520603-14.
ON REMOVAL OF FUSELAGE SKIN, LT BS 590-660 DISCOVERED STR 16L DENTED ON LOWER FLANGE AT STA 598-605. DENT ON STR 16L LWR FLANGE STA 598-605 MEASURED A=1.0", Y=.050" A/Y=20. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, ALLOWABLE DAMAGE 1, PG 2, FIGURE 101, DETAIL III. REPAIRED STR 16L FROM STA 570-612 IAW SRM 53-00-03, REPAIR 1, FIG 201 AS PERMANENT.
ON REMOVAL OF SKIN, DISCOVERED STRINGER 18L DENTED ON LOWER FLANGE AT BS 594. REPAIRED IAW SRM 53-00-03, FIG 201, REPAIR 1.
ON REMOVAL OF NUT PLATE STRIP ON FORWARD CARGO DOOR SILL, LOWER ANGLE FOUND CORRODED BS 560 TO 620 ON UPPER SURFACE OF OTBD FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101. R & R IAW SRM 51-40-05 & SRM 51-40-02.
MID CABIN RT INBD CREASEBEAM ANGLE HAS CORROSION BS 780, RBL 62. R & R ANGLE IAW SRM 51-40-02.
MAIN CABIN CREASEBEAM INNER ANGLE HAS AREAS OF CORROSION BETWEEN BS 860 AND 900. REMOVED CORROSION IAW SRM 53-30-13, FIG 101, DETAIL VIII ALLOWABLE DAMAGE-I, PAGE 105. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DET VIII ALLOWABLE DAMAGE -I, PAGE 105. REMOVED DAMAGE CREASEBEAM AND REPLACED IAW SRM 51-40-02.
FORWARD CABIN, FLOORBEAM HAS CORROSION ON UPPER AND LOWER SURFACES BS 377, LBL 12-RBL 8. REMOVED CORROSION TO FOUND OUT OF LIMITS IAW SRM 53-00-51. ALLOWABLE DAMAGE, 1 DETAIL III. INSTALLED PERMANENT REPAIR IN REF SRM 53-00-51, REPAIR 10.
FORWARD CABIN, FLOORBEAM HAS CORROSION, PREVIOUS BLEND, AT BS 365, RBL 5-20. REMOVED CORROSION TO FOUND OUT OF LIMITS. INSTALLED PERMANENT REPAIR IAW SRM 53-00-51.
AFT CARGO BAY, FRAME DENTED AT BS 1480, LBL 28. CUT OUT DAMAGE IAW SRM 53-00-07, REPAIR 5, FIG 2, STEP 1. FABRICATED, REPAIR J SECTION. INSTALLED REPAIR SECTION IAW SRM 51-40-02, PARA 7D AND SRM 53-00-07, REPAIR 5, FIG 201, DETAIL 1.
ON REMOVAL OF SKIN, DISCOVERED STRINGER 15L DENTED ON LOWER FLANGE BS 633-637. REPAIRED IAW SRM 53-00-03 REPAIR I, FIG 201.
AFT CARGO BAY, BILGE FRAME DENTED AT BS 1340, RBL 28. REPAIRED FRAME IAW SRM 53-00-07, REPAIR 5, FIG 201.
MAIN CABIN RT CREASEBEAM HAS AREAS OF CORROSION BETWEEN BS 1020 AND 1040, REMOVED CORROSION & FOUND OUT OF LIMITS. R & R CREASEBEAM ANGLE IAW SRM 51-10-02.
AFT CARGO, LT BILGE FRAME HAS DENT AT BS 1520, LBL 27. TRIMMED OUT DAMAGE ON FRAME AND REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5.
FWD CARGO FRAME DENTED AT BS 660, LONGERON 24L. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 5.
AFT CARGO BILGE FRAME DENTED AT BS 1500, RBL 24, REPAIRED IAW SRM 53-00-07, REPAIR 5, FIG 201.
AFT CARGO, RT FRAME SPLICE HAS GOUGES BS 1480, STRINGER 23- 25R. R & R FRAME SPLICE IAW SRM 51-40-02.
BROKEN STABILIZER STRAP BETWEEN CABIN FLOORBEAMS AT BS 365 AND 377, LBL 24. R & R BROKEN STABILIZER STRAP IAW ER/A 384483-14MA, REV D.
DURING LINE CHECK MAINTENANCE FOUND EXIT SIGN AT 3R INOP. MAINTENANCE RECONNECTED LOSE CONNECTOR. EXIT SIGN NOW WORKS OK PER AMM 33-51.
DURING LINE CHECK MAINTENANCE FOUND DOOR EMERGENCY SLIDE AT DOOR R2 INOP. MAINTENANCE REPLACED BATTERY PACK M736. CHECK OF LIGHT NOW OK PER AMM 33-51.
DURING CHECK, CORROSION WAS FOUND COMMON TO BS 1380 FRAME WEB AT STRINGER 25R. CORRODED FRAME WEB WAS REPAIRED IAW SECTION I OF ER/A 499039-14.
MX FOUND EMERGENCY LIGHT HSG AT 2L BROKEN. REPLACED EMERGENCY LIGHT ASSY. OPS CHECKED OK.
DURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT 1-4AB INOPERATIVE. MX REPLACED THE LIGHTS. OPS CHECK WAS GOOD.
DOOR 1 LEFT, EMERGENCY SLIDE LIGHTS INOP. REPLACED M731 POWER SUPPLY, OPS OK.
FIRST CLASS EMERGENCY EGRESS SEAT MOUNTED LIGHTS INOP (LOG PAGES 0161082, 0161883). REPLACED POWER SUPPLIES M730 AND M732, TESTS OK.
DOOR 1L AND L629 EXIT LIGHT INOPERATIVE. REPLACED M731 BATTERY PACK. LIGHT CHECKED OK.
DURING LINE CHECK FOUND SEAT-MOUNTED EMERGENCY LIGHTS AT ROWS 34-38 AND OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 27-37 INOPERATIVE. MAINTENANCE REPLACED BATTERY ON M735 POWER SUPPLY.
DURING OVERNIGHT LINE CHECK, FOUND DOOR 2 RIGHT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED DOOR 2 RIGHT POWER SUPPLY, REF FIM NR 33-51-00, FIG NR 103. OPS CHECK NORMAL. AIRCRAFT OK FOR SERVICE.
During "H" check found crack in outboard side of pylon lower torque box upper aft corner at access panel 433AL. Repaired per EA 56-189401.
DURING SCHEDULED CHECK, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY WITH A SERVICEABLE UNIT, OPERATIONAL CHECK WAS SATISFACTORY.