N3737C
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 | 2025-02-05 – 2025-02-05 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2025-02-05 – 2025-02-05 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
ATB/DE- DUE TO RIGHT ENGINE FAN VIBRATION 4.2 AND HAD TO REDUCE THROTTLE TO KEEP VIB BELOW LIMITS. PERFORMED FAN TRIM BALANCE VIB NOW AT 1.8. (LOG 8365005 - AIRCRAFT WAS GROUNDED).
(LOG 0855497) VERTICAL STAB MOUNTING POINTS CORROSION PRI 624280 ISSUED. C/W VERTICAL STAB/MOUNTING POINTS/CORROSION FINDINGS ERA 624280-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. VERIFIED ERA 624280-14 HAS BEEN COMPLETED.
(LOG 0855976) A/C HIT IN RUDDER BY JAL 787. C/W ERA 624172-14 SECTION 1 PERMANENT REPAIR. R/R RUDDER ASSY, REF LOG 0853320. REPAIRED VERTICAL STAB ASSY IAW ERA 624172-14,624294-14,624280-14,624522-14,624701-14 ALL REV ORIGINAL.
(LOG 0853320) DAMAGED RUDDER BY TAIL STRIKE. REMOVED RUDDER PER AMDS #2721-4912 STEPS 1-3. C/W RUDDER REPLACEMENT IAW AMDS 2721-4912 (R.GROSS 436426) ALL RII ITEMS C/W.
AIRCRAFT 3737, WHILE PARKED ON DE-ICE PAD IN SEA, AIRCRAFT WAS STRUCK BY THE RIGHT WINGTIP OF A TAXIING JAL B787. AIRCRAFT VERTICAL STABILIZER WAS STRUCK ON THE RIGHT SIDE CAUSING SUBSTANTIAL DAMAGE. IN ORDER TO ACCESS THE BOLTS FOR THE REAR SPAR PRIMARY FITTINGS FOR INSPECTIONS AN ACCESS HOLE WAS REQUIRED IN THE LWR CLOSURE RIB WEB (P/N 172A3104-1). REFERENCE ER/A 624172-14 FOR INSPECTIONS INSTRUCTIONS. THE CLOSURE RIB WEB IS ORIGINALLY MANUFACTURE FROM 0.200" BARE 7075-T6 SHEET PER QQ-A-250/12, LOCALLY CHEM MILLED TO 0.090" THICK. CORRECTIVE ACTION: REPAIRED PER ER/A 624294-14 AND DEFERRED PER MONITOR. (LP 0831792)
AIRCRAFT 3737, ON VERTICAL STAB AFT MOUNT OUTBOARD LT FITTING LUG CORROSION ON FACE OF BUSHING. CORRECTIVE ACTION: REPLACED VERTICAL STAB AFT MOUNT OUTBOARD LT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS. REF ERA 624280-14 REV 0 PRI REV5. (LP 0829461)
(LOG 0829464) ALL 8 BUSHINGS ON AFT PRIMARY AND FAIL SAFE FITTING MUST BE REPLACED. R/R ALL 8 BUSHINGS ON AFT PRIMARY AND FAILSAFE FITTINGS PER PRI 624280-14, C/W ALL RII ITEMS, REF ERA 624280 REV 0, PRI REV 5.
(LOG 0828481) ACCESS HOLE CUTOUT IN LWR CLOSURE RIB WEB (P/N 172A3104-1) IS MADE FOR REAR SPAR PRIMARY FITTING BOLTS INSPECTION. HOLE CUTOUT IS REPAIRED BY DOUBLER IAW PRI 624294-14 REV 1.
(LOG 0829460) ON VERTICAL STAB AFT MOUNT OUTBOARD RT FITTING LUG CORROSION ON FACE OF BUSHING. R/R VERT STAB AFT MOUNT OUTBOARD RT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS, REF ERA 624280-14 REV 0, PRI REV 5.
(LOG 0824717) ON FWD MOUNT OF VERTICAL STAB, FOUND CORROSION ON RIGHT BOLT ATTACH BUSHING AND FRAME. REMOVED AND REPLACED R/H FWD ATTACH BUSHING REF PRI 624280-14.
(LOG 0824702) FOUND CORROSION ON FWD MOUNT OF VERTICAL STAB ON LH FWD BUSHING AND FRAME AROUND BUSHING ATTACH BOLT. REMOVED AND REPLACED L/H FWD MOUNT BUSHING REF PRI 624280-14.
SHIP 3737 -MISC- DECLARED EMERGENCY INTO ATL DUE TO ABNORMAL FLIGHT CONTROL FEEL DURING ROLL MANEUVERS. CHECKED AILERON SPRING CARTRIDGE, RATIO CHANGER INPUT ROD, VERIFIED CABLE TENSIONS, GREASED AILERON POWER LEVER. FOUND UPPER AILERON POWER CONTROL UNIT B SYSTEM SEAL BLOWN OUT AND LEAKING. REPLACED AILERON PCU B SYSTEM AND CHECKED AILERON POSITION SENSORS. (LP 0725113, 6650092)
SHIP 3737 -UFC/DE- DECLARED EMERGENCY INTO ATL DUE TO FLAP LOCKOUT. CORRECTIVE ACTION: MAINTENANCE REPLACED TEE ANGLE GEARBOX PER B737 AMM 27-51.
(LOG 0610929) CRACK ON UPPER/FWD CUTOUT JAMB OF AFT ENTRY DOOR AT PAX CABIN. UPPER STUB FRAME ON FWD CUTOUT JAMB OF AFT ENTRY DOOR AT PAX CABIN WAS REPAIRED PER ER/A 620875-14.
(LOG 0604725) CORROSION ON FLOOR SUPPORTS BTW STA=727 D TO 727 E, LBL=8.1 AND STA= 767 TO 787 RBL= 3.0, RBL=8.1 AT AFT CARGO COMPARTMENT. FLOOR SUPPORTS BTW STA=727 D TO 727 E, LBL=8.1 AND STA= 767 TO 787 RBL= 3.0, RBL=8.1 AT AFT CARGO COMPARTMENT WERE REPAIRED PER B737-800 SRM 53- 00-53-2R.
(LOG 0602237) CORROSION ON SIDE PLATES FROM STA 727 TO STA 727G ALSO FROM STA 727G TO STA 787 LH SIDE AT AFT CARGO COMPARTMENT. SIDE PLATES STA 727G TO STA 787 LH SIDE AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0600722) CORROSION ON SIDE PLATES FROM STA 727 TO 727G+10 AND FROM STA 727G+10 TO STA 787 ALSO FROM STA 887 TO STA 947.5 RH SIDE AT AFT CARGO COMPARTMENT. SIDEPLATE RH BTW STA 727 AND STA 767 WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0599360) CORROSION ON LH SIDE PLATE BTW STA 510 TO STA 500H AT FWD CARGO COMPARTMENT. LH SIDE PLATE BTW STA 510 TO STA 500H AT FWD CARGO COMPARTMENT WAS REPLACED PER PER B737-800 SRM 51-40-02-0G.
(LOG 0600655) CORROSION ON STRINGER 26LBL & FROM STA 802 TO STA 827 AT AFT CARGO COMPARTMENT. STRINGER 26LBL & FROM STA 777 TO STA 887 AT AFT CARGO COMPARTMENT WAS REPAIRED PER 53-00-03-2R PROCEDURE 1 REPAIR 1.
(LOG 0598896) GOUGES IN HOLES WERE FOUND ON VERTICAL PRESSURE DECK WEB, VERTICAL STIFFENERS, ATTACH ANGLE AND UPPER COMPRESSION CHORD. VERTICAL PRESSURE DECK WEB, VERTICAL STIFFENERS, ATTACH ANGLE AND UPPER COMPRESSION CHORD BTW BS 663 RBL 30-40 WERE REPAIRED PER ER/A 621040-14 REV.ORIGINAL. ASSOCIATED AA 5714-01004 ADDED FOR AC 3737.
(LOG 0597577) CORROSION ON RH/LH FITTING SUPPORT STA=951- 972, RBL=50 AND LBL=50 AT CPAX. RH/LH FITTING SUPPORT STA=951-972, RBL=50 AND LBL=50 AT CPAX (W2) WERE REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0598552) CORROSION ON RH SIDE PLATE BTW 500B +10 TO 500H AT FWD CARGO COMPARTMENT. RH SIDE PLATE BTW 500B + 10 TO 500H AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-05-0G AND SRM 51-40-02-0G.
(LOG 0598818) CORROSION ON LH SIDE PLATE BTW STA 400 TO STA 510 ATFWD CARGO COMPARTMENT. LH SIDE PLATE BTW STA 400 TO STA 510 ATFWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR. 4. AND SRM.51-40-05-0G.
CORROSION ON FLOOR SUPPORTS 294.5-344 AT FLOOR SRTUCTURE OF PASSERNGER CABIN. LEVEL 2-FLOOR SUPPORTS BTW STA 312 TO 328 LBL 11, STA 328 TO 344 LBL 11 AND INTERCOSTAL BTW STA 312 TO 294.5 LBL 11 WERE REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0597233) CORROSION ON SHIELD BTW STA767 TO STA 790 AFT CARGO COMPARTMENT. SHIELD BTW STA767 TO STA 790 AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR 4 , SRM 51-40-02-0G PAR 7 AND SRM 51-40-02-0G PAR 5 AND DWG: 146A8127.
(LOG 0591035) CORROSION ON FLOOR BEAM STA=977-981, LBL=17. STA= 951-961, RBL=26 AND STA 951 RBL 19, STA 951 RBL 40. AND ANGLES STA=992.8, LBL/RBL=41, AT PAX CABIN. FLOOR BEAM STA=977-981, LBL=17. STA= 951-961, RBL=26 AND STA 951 RBL 19, STA 951 RBL 40 AND ANGLES STA=992.8, LBL/RBL=41 WERE REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0591048) CORROSION ON FLOOR SUPPORT STA 887 BTW STRINGERS 25RH-25LH AT AFT CARGO COMPARTMENT. FLOOR SUPPORT STA 887 BTW STRINGERS 25RH-25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0586565) CORROSION ON RH SIDE PLATE BTW STA 500 TO STA 500A AT FWD CARG COMPARTMENT. RH SIDE PLATE BTW STA 500 TO STA 500A AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0585465) WEAR RH INB/OUTBD SEAT TRACKS STA520 AT CPAX. RH INB/OUTBD SEAT TRACKS STA 520 WERE REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 4. REPAIR 4.
(LOG 0584614) CRACK ON INTERCOSTAL BTW STA 345 AND STA 360 AT FLOOR STRUCTURE OF PASSERNGER CABIN. INTERCOSTAL BTW STA 345 AND STA 360 AT FLOOR STRUCTURE OF PASSERNGER CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0579458) WEAR ON LH IN'BD & OUT'BD SEAT TRACKS AT STA 500I TO 520. SEAT TRACK SECTION PREVIOUS REPAIR LH IN'BD & OUT'BD AT STA 500I TO 520 WERE REPLACED PER B737-800 SRM 53-00-52-2R PROCEDURE. 4.
(LOG 0577624) CORROSION ON RH INBOARD SEAT TRACKS STA462 AT CPAX. RH INBOARD SEAT TRACKS STA462 AT CPAX WAS REPLACED PER B737-800 SRM 51-40-02-0G.
(LOG 0576156) " A.A IN REF AMDS 5732-01015-01A-01: OBTAIN VA FROM FLEET ENGINEERING". SUMMARY OF NRC:00598 VA 90996 REV C WAS ACCOMPLISHED IN CONJUNCTION WITH AA 5732-01015-01A-01.
(LOG 0576123) "A.A IN REF AMDS 5732-01015-01B-01: OBTAIN VA FROM FLEET ENGINEERING". SUMMARY OF NRC: 00599 VA 90996 REV C WAS ACCOMPLISHED IN CONJUNCTION WITH AA 5732-01015-01B-01.
(LOG 0576124) CRACK WAS FOUND OF 0.15IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0576118) CRACK WAS FOUND OF 0.12IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8R & S-9R.RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0575896) CRACK WAS FOUND OF 0.14IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0575887) CRACK WAS FOUND OF 0.11IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0575883) CRACK WAS FOUND OF 0.28 IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0575872) CRACK WAS FOUND OF 0.26IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 480. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 480. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0576096) CRACK WAS FOUND OF 0.19IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0575891) CRACK WAS FOUND OF 0.310IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500F BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500F BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.
(LOG 0575884) CRACK WAS FOUND OF 0.1IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.
(LOG 0575882) CRACK WAS FOUND OF 0.22IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500D. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500D. BTW S-8L & S-9L WAS REPIARED UNDER CARD 2526-01236-02A.
(LOG 0575871) CRACK WAS FOUND OF 0.21IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.
(LOG 0575867) CRACK WAS FOUND OF 0.12IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.
(LOG 0575863) CRACK WAS FOUND OF 0.200IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867 BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867 BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.
(LOG 0575860) CRACK WAS FOUND OF 0.8IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 440. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 440. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.
(LOG 0575492) CORROSION ON FLOOR BEAM STA=986.5, LBL=11 TO LBL 44 AT CPAX. FLOOR BEAM STA=986.5, LBL=11 TO LBL 44 WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 4 REPAIR 4.
(LOG 0575820) CRACK WAS FOUND OF 0.7IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8L & S-9L. LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 380. BTW S-8L & S-9L WAS REPAIRED UNDER CARD 2526-01236-02A.
(LOG 0572433) CORROSION ON FLOOR BEAM STA=986.5, RBL= 33 TO RBL 34 AT CPAX (W2). CORROSION ON FLOOR BEAM STA=986.5, RBL= 33 TO RBL 34 AT CPAX WAS REMOVED UNDER NRC 0375 AND WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 6 REPAIR 6.
(LOG 0515226) EMERGENCY EXIT LIGHTS OVER LEFT FWD OVERWING DOOR INOP. R/R EMERGENCY LIGHT BATTERY PACK M1694 IAW B737 AMM 33-51.
(LOG 0452706) DURING OVERNIGHT IN CVG ON 11-JULY-2024, MTC DISCOVERED DAMAGE CONSISTING OF A CRACK RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (E-F POST) THROUGH A FASTENER LOCATION COMMON TO THE WINDOW FRAME ASSEMBLY OF THE LH NO. 3 FLIGHT COMPARTMENT WINDOW. MAINTENANCE REPAIRED CRACK PER ERA 619441-14.
(LOG 5794376) DURING CAPTAIN #1 WINDSHIELD REMOVAL FOUND / SUSPECT LT #3 WINDOW FRAME CRACK AT BOTTOM SIDE. REPAIRED PER ERA 619441-14.
(LOG 5794374) ON SVC CHK WHILE CLEANING WINDSHIELD FOUND CRACK ON CAPTAINS #1 WINDOW FRAME. REPAIRED CRACK PER ERA 619423-14.
(LOG 0444041) B737-800 FUSELAGE NOSE CAPTAINS WINDSHIELD NO. 1 WINDOW FRAME UPPER OTBD CORNER CRACK. REPAIRED PER ERA 619423-14.
(LOG 0265216) 1R EMERGENCY EXIT LIGHTS ILLUMINATED DURING TAKEOFF ROLL. T/S PER WDM 33-51-12. R/R BATTERY PACK AND POWER SUPPLY AND INSTALL TEST OK IAW B737 AMM 33-51. A/C OK FOR SVC.
(LOG 5747769) DURING SVC CK, FOUND DOOR 1L EMER LIGHT INOP. FOUND CONNECTOR D11072 DISCONNECTED. RE-CONNECTED CONNECTOR AND CHECKS GOOD.
(LOG 5747744) DURING SERVICE CHECK FOUND CABIN EMERGENCY EXIT SIGN LIGHT AT MID AISLE OVERHEAD INOP. REMOVED AND REPLACED THE POWER SUPPLY FUSE AT M1670 IAW B737 AMM 33-51-06. OPS CHECK GOOD.
(LOG 4340449) SECTION OF SEAT MOUNTED EMERGENCY LIGHTS INOP AFT OF OVERWING EXITS. RPLD BATTERY PACK FOR PWR SUPPLY M1671 PER B737 AMM 33-51. OPS CKS GOOD.
(LOG 4340448) FIRST CLASS SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP. RPLD BATTERY PACK FOR PWRSUPPLY M1674 PER B737 AMM 33-51. OPS CKS GOOD.
SHIP 3737 -ATB/UFC- RETURNED TO LAX DUE TO AILERON CONTROL ISSUES. CORRECTIVE ACTION: FOUND #9 FLIGHT SPOILER FLUTTERING. REPLACED FLIGHT SPOILER ACTUATOR. OPS CHECKS GOOD.
(LOG 0013059) WHILE ACCOMPLISHING WINGLET MODIFICATION PER EA 12-468783-03, JUST IB OF RIB 19 ON STRINGER 8 ON THE LH WING, MTC DRILLED A HOLE IN THE WRONG LOCATION. REPAIRED PER ERA 474401-14.
SHIP 3737 -DIV- DISPATCHED IAD WITH RT IDG ON MEL. ENROUTE LOST APU, DOWN TO SINGLE ELECTRICAL SOURCE, DIVERTED TO MSP. CORRECTIVE ACTION: REPLACED RT IDG. APU AUTO SHUTDOWN DUE TO LOW OIL PRESSURE. CLEANED OIL COOLER, CHANGED OIL AND FILTER. REPLACED LOP SWITCH.
SHIP 3737 -SMOKE/ODOR- RETURN TO BLOCK DUE TO REPORT OF SMOKE COMING FROM THE AFT GALLEY DRAIN. CORRECTIVE ACTION: PERFORMED ALL REQUIRED INSPECTIONS WITH NO TROUBLE FOUND.
(LOG 8059233)DURING INSPECTION FOUND NO 2 FLAP OUTBOARD FLAP TRACK FAIRING TAIL CONE MISSING. IRO NBR 3 INBOARD FLAP TAIL CONE FAIRING FWD TO CDL 57-10-04. PLAC INSTALLED. "SUPPLEMENTAL INFORMATION" 01/13/22, STATION LAX. AFTER FURTHER INVESTIGATION IT WAS DETERMINED THAT THE TAIL CONE DID NOT FALL OFF THE AIRCRAFT. IT WAS REMOVED BY MAINTENANCE TO FACILITATE A REPAIR. THEREFORE, THIS DOES NO LONGER QUALIFY AS AN SDR/PDA FOR PARTS DEPARTING AIRCRAFT.
(LOG 1985053) DURING INSPECTION FOUND SCRATCHES ALONG PREVIOUS REPAIR LOWER SKIN AND GOUGE AT LOWER SKIN SURFACE BTW STAB STA 129.5 AND 157.1 APROX OF RH HOR STAB. SCRATCHES ALONG PREVIOUS REPAIR WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11.
(LOG 1984317) DURING INSPECTION FOUND WORN SETTLEMET AREA OF NUTPLATES ON SUPPORT STRUCTURE. PERMANENT REPAIR ON SETTLEMET AREA OF NUTPLATES ON SUPPORT STRUCTURE STA BS 727+2.7. WAS PERFORMED PER STEP NO.1 UNTIL STEP NO.17 OF ETI-37-21-500 REVISION. 2 AND ER/A NO.594819-14A.
(LOG 1984534) DURING INSPECTION FOUND ELONGATED HOLE AT AFT WING-TO-BODY FAIRING PANEL 193D SUPPORT STRUCTURE BTW STA BS 725. PERMANENT REPAIR ON ELONGATED HOLE AT AFT WING-TO-BODY FAIRING PANEL 193D SUPPORT STRUCTURE BTW STATION BS 725 WAS PERFORMED PER ETI-37-21-500 REVISION. 2 FROM STEP 18 TO STEP 25. AND ER/A NO.594819-14AD.
(LOG 1981318) DURING INSPECTION FOUND ELONGATED HOLES (7 EA) AT AFT WING-TO-BODY FAIRING PANEL 193D. ELONGATED HOLES (7 EA) AT AFT WING-TO-BODY FAIRING PANEL 193D WERE REPAIRED PER B737-800 S.R.M 51-70-05-2R PROCEDURE 8 PAR. 4. AND B737-800 S.R.M. 51-70-05-2R REPAIR GENERAL.
(LOG 1977363) DURING INSPECTION FOUND CRACK ON LH HOR STAB LWR SKIN SURFACE STATION 101.90. LH HOR STAB LWR SKIN SURFACE STA 101.90 WAS REPAIRED PER B737-800 SRM 55-10-01-2R REPAIR 11.
(LOG 7865108) DURING INSPECTION FOUND EMERGENCY LIGHT SIGNS AT ROWS 17-18ABC INOP. REMOVED AND REPLACED BATTERY PACK AT POWER SLED M1694 IAW B737 AMM 33-51. EMERGENCY LIGHT SIGNS CK GOOD.
SHIP 3737 -ATB- DUE TO AUTOPILOT MCP (MODE CONTROL PANEL) ALTITUDE SELECTOR INOPERATIVE. CORRECTIVE ACTION: REPLACED AUTOPILOT MODE CONTROL PANEL. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
DURING INSPECTION FOUND DAMAGE BEHIND 2L DOOR. REPAIR REF SRM 53-70-01-2R PROCEDURE 1 REPAIR 1.
(LOG 1534109) RIGHT HORIZONTAL STABILIZER AFT LOWER ATTACH POINT, EXCESSIVE PLAY BETWEEN BOLT AND BUSHINGS. MAINTENANCE REPAIRED DAMAGE PER ERA 586226-14.
(LOG 1534104) LEFT HORIZONTAL STABILIZER: AFT LOWER ATTACH POINT, BUSHING HAS TOOLING DAMAGE. MAINTENANCE REPAIRED DAMAGE PER ERA 586222-14.
(LOG 1534110) LEFT HORIZONTAL STABILIZER FWD ATTACH POINT, ON AIRCRAFT FWD LOWER BUSHING HAS EXCESSIVE PLAY WITH ITS ATTACH BOLT. MAINTENANCE REPAIRED DAMAGE PER ERA 586096-14.
(LOG 5538096) DURING INSPECTION FOUND RIGHT AFT OVERWING EXTERIOR EMERGENCY EVACUATION LIGHT INOPERATIVE. FOUND DEFECTIVE FUSE IN M1671 BATTERY CHARGER . REPLACED SAME PER AMM 33-51-06. OPS CHECK GOOD.
(LOG 5367134) ABOUT 25 MILES FROM LANDING AUTOBRAKE DISARM & "ANTI SKID INOP" LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE AND DECLARED EMERGENCY. LANDING 40 DEG FLAP, EASY ON BRAKES, CONTINUED TO GATE WITHOUT INCIDENT. FOUND HIGH RESISTANCE ON PIN 1 AND PIN 2 ON CONNECTOR D2574 FOR SERVO VALVE. R/R PRESSURE CONTROL MODULE IAW AMM 32-42-81 ALL OPS LEAK CKS GOOD.
DURING INSPECTION FOUND EMER EXIT LIGHT SWITCH COVER HAS LOST SPRING TENSION AND IS HANGING DOWN. R&R SWITCH COVER IAW SWPM 20-84-13, OPS CHECK GOOD.
DURING INSPECTION FOUND EMERGENCY LIGHTS AT SEAT ROW 11-15 INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER EIN M1676 PER AMM 33-51. OPS CK GOOD.
(LOG 0793117) DURING INSPECTION FOUND CRACK ON STRINGER 28R ON STATION 325 E/E. STRINGER 28R BS 312-323.7 WAS REPAIRED PER ETI-37-18-541 REVISION ORIGINAL AND ER/A 572452-14.
(LOG 0793354) DURING INSPECTION FOUND FUSELAGE FRAME FREE FLANGE IS DENTED STATION 500A BETWEEN STR 25L AND 26L AT FWD CARGO COMPARTMENT. DENTED FUSELAGE FRAME FREE FLANGE AT STATION 500A BETWEEN STRINGER 25L & 26L AT FORWARD CARGO COMPARTMENT WAS REPAIRED PER ETI-37-18-529 REVISION 1 AND ER/A 572472-14.
(LOG 0793183) DURING INSPECTION FOUND FUSELAGE FRAME FREE FLANGE IS DENTED STATION 727C STR 24L AT AFT CARGO COMPARTMENT. DENTED FUSELAGE FRAME FREE FLANGE AT STATION 727C STRINGER 24L AT AFTER CARGO COMPARTMENT WAS REPAIRED PER ETI-37-18-533 REVISION 2 AND ER/A 572486-14.
(LOG 0793173) DURING INSPECTION FOUND FUSELAGE FRAME FREE FLANGE IS DENTED IN TWO PLACES STATION 727H BETWEEN STR 23L AND 25L AT AFT CARGO COMPARTMENT. DENTED FUSELAGE FRAME FREE FLANGE AT STATION 727H BETWEEN STRINGER 23L AND 25L WAS REPAIRED PER ETI-37-18-534 REVISION 2 AND ER/A 572492-14.
(LOG 0793132) DURING INSPECTION FOUND FUSELAGE FRAME FREE FLANGE IS DENTED STATION 420 BETWEEN STR 25L AND 26L AT FWD CARGO COMPARTMENT. DENTED FUSELAGE FRAME FREE FLANGE AT STATION 420 BETWEEN STRINGER 25L & 26L AT FORWARD CARGO COMPARTMENT WAS REPAIRED PER ETI-37-18-528 REVISION 3 AND ERA 572474-14.
(LOG 0791298) DURING INSPECTION FOUND CORROSION ON SIDEPLATE LT STATION 500A TO 500I. LT SIDEPLATE STATION 500A TO 500I WAS REPLACED PER SRM 53-30-53.
(LOG 0791294) DURING INSPECTION FOUND FUSELAGE FRAME FREE FLANGE IS DENTED STATION 500C ABOVE STR 24L AT FWD CARGO COMPARTMENT. DENTED FUSELAGE FRAME FREE FLANGE AT STATION 500C ABOVE STRINGER 24L AT FORWARD CARGO COMPARTMENT WAS REPAIRED PER ETI-37-18-530 REVISION 1 AND ERA 572460-14.
(LOG 0792103) DURING INSPECTION FOUND DENT ON EXTERNAL FUSELAGE SKIN BTW STATION 318, BTW STR 28R AND PROYECTION 29. DAMAGE ON EXTERNAL FUSELAGE SKIN BTW STATION 318, BTW STR 28R AND PROYECTION 29 WAS REPAIRED PER ETI-37-18-525 REV. 5 AND ERA 572505-14.
(LOG 0791423) DURING INSPECTION FOUND FUSELAGE FRAME FREE FLANGE IS DENTED STATION 727E BETWEEN STR 23L AND 24L. AT AFT CARGO COMPARTMENT. DENTED FUSELAGE FRAME FREE FLANGE AT STATION 727E, BETWEEN STRINGER 23L & 24L AT AFTER CARGO COMPARTMENT WAS REPAIRED PER ETI-37-18-532 REVISION 2 AND ERA 572482-14.
(LOG 0790398) DURING INSPECTION FOUND CORROSION ON BEAM STATION = 986 BTW RBL 54 TO LBL 54 AT CABIN PAX. CORROSION ON BEAM STA = 986 BTW RBL 54 TO LBL 54 AT CABIN PAX. FLOOR STRUCTURE BEAM AT STATION 986.5 (PASSENGER COMPARTMENT) WAS REPAIRED PER ETI-37-18-524 REV. 1 AND ER/A 572468-14.
(LOG 0790339) DURING INSPECTION FOUND FUSELAGE FRAME FREE FLANGE IS DENTED STATION 767 BETWEEN STR 22 LT AND 23 LT AT AFT CARGO COMPARTMENT. DENTED FUSELAGE FRAME FLANGE AT STATION 767 BETWEEN STR 22L AND 23L AT AFTER CARGO COMPARTMENT WAS REPAIRED PER ETI-37-18-535 REV. 1 AND ERA 572459-14.
(LOG 0790312) DURING INSPECTION FOUND CORROSION ON STRINGER 28L BTW STA 500F+10 AND 500G+8 AT FWD CARGO COMPARTMENT. CORROSION ON STRINGER 28L BTW STATION 500F+10 AND 500G+8 AT FWD CARGO WAS REPAIRED PER SRM 53-00-03.
(LOG 0790044) DURING INSPECTION FOUND CRACK ON LT HORIZONTAL STABILIZER LOWER CHORD STA SS 285.9 FRONT SPAR AREA. LT HORIZONTAL STABILIZER LOWER CHORD STATION SS 285.9 FRONT SPAR WAS REPAIRED PER ER/A 572326-14 REV ORIG AND ETI -37-18-522 REV 2.
(LOG 0790266) DURING HCK AT QRO ONE DENT WAS FOUND AFFECTING THE BS 727E FRAME 146A1225-7 BETWEEN S-23L AND S-24L. MAINTENANCE REPAIRED DAMAGE PER ERA 572482-14.
(LOG 0788206) DURING INSPECTION FOUND CORROSION OUT OF LIMITS ON LT ZEE SIDEPLATE FROM STATION 727G TO STA 807. LEVEL CORROSION 2 SIDE PLATE LT STATION 727G TO 807 WAS REPLACED PER SRM 51-40-02.
(LOG 0788117) DURING INSPECTION FOUND CRACKS ON LT ZEE SIDEPLATE FROM STATION 727A TO STATION 727B (3EA) AND STA 727F. SIDE PLATE LT ON STATION 727A TO STA 727F WAS REPLACED PER SRM 51-40-02.
(LOG 0788841) DURING INSPECTION FOUND CRACK ON INTERCOSTALS BTW STATION 500A-500B, BTW 500B-500C, BTW 500C-500D,BTW 500E-500F, BTW 500F-500G, BTW 500G-500H, 500H-500I. DAMAGED INTERCOSTALS WERE REPLACED PER SRM 51-40-02.
(LOG 0785222) DURING INSPECTION FOUND CRACK ON FRAME STATION 727B BTW S9R TO S8R. FRAME STATION 727B BTW S9R TO S8R WAS REPAIRED PER ERA 571918-14AD REV. ORIGINAL.
(LOG 0785810) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL AT LONG 27 BTW 727A TO 727B. LEVEL CORROSION 2 INTERCOSTAL WAS REPLACED PER SRM 51-40-02.
(LOG 0782606) DURING INSPECTION FOUND CORROSION ON FRAME CLIPS STATION 500G BTW STGR 27L TO 25L. FRAME CLIPS STATION 500G BETWEEN STRINGERS 27L & 25L WERE REPLACED PER SRM 51-40-02.
(LOG 0783160) DURING INSPECTION FOUND OIL CANNING ON DOME WEB (AFT BULKHEAD) BTW 11:00-12:00 HRS. POSITION AT AFT ACCESORY COMPARTMENT. AREA WAS REPAIRED PER SRM 53-80-08 REPAIR 7.
(LOG 0783168) DURING INSPECTION FOUND OIL CANNING ON DOME WEB (AFT BULKHEAD) BTW 11:00-12:00 HRS. POSITION AT AFT ACCESORY COMPARTMENT. AREA WAS REPAIRED PER SRM 53-80-08 REPAIR 7.
(LOG 0780461) DURING INSPECTION FOUND CORROSION ON FRAME CLIPS STATION 500H BTW STR 27R TO 25L. THESE CLIPS STA 500H BTW STR 27R TO 25L WERE REPLACED PER SRM 51-40-02.
DURING INSPECTION FOUND CORROSION UPPER AND LOWER AREA ON RT ZEE SIDEPLATE FROM STA 727 TO STA 727F+11'. SIDE PLATE WAS REPLACED PER SRM 51-40-02.
DURING INSPECTION FOUND CORROSION ON UPPER AND LOWER AREA AT RT ZEE SIDEPLATE FROM STA 727F+11 TO STA 767. SIDE PLATE WAS REPLACED PER SRM 51-40-02.
DURING INSPECTION, FOUND THE EMERGENCY LIGHT AT THE L1 DOOR INOPERATIVE. MAINTENANCE INSPECTED AND FOUND A WIRE INTERMITTENTLY SHORTED, REPLACED THE WIRE W4142-0112-20, D10750 & D3662 IAW WDM 33-51-21 & 20-25. SYS OPS CHECKED NORMAL IAW 33-51-00.
DURING INSPECTION, FOUND A SEAT TRACK GOUGED AT BS 520 LBL 22. REPAIRED THE SEAT TRACK IAW SRM 53-00-52 REPAIR 4. DWG 143A5300 REV A, AND ERA 553105-14.
DURING INSPECTION, FOUND SEAT TRACK GOUGED AT BS 520, RBL 45. REPAIRED THE SEAT TRACK IAW SRM 53-00-52 REPAIR 4, DWG 143A5300 REV A AND ER/A 553105-14.
DURING INSPECTION FOUND A SEAT TRACK GOUGED AT BS 520 RBL 22. REPAIRED THE SEAT TRACK IAW SRM 53-00 -52 REPAIR 4, DWG 143A5300 REV A, AND ERA 553105-14.
DURING INSPECTION, FOUND A SEAT TRACK GOUGED BS 520 LBL 45. REPAIRED THE SEAT TRACK IAW SRM 53-00-52 REPAIR 4, DWG 143A5300 REV A, AND ERA 553105-14.
DURING TEST FOUND PER WORK CARD 3350-7413, EMERGENCY LIGHTING BATTERY PACK AT ROW 23 D,E,F. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK AT ROW 23 D ,E,F PER AMM 33-51-06.
DURING INSPECTION FOUND AFT CARGO FORWARD FLOOR SUPPORT CRACKED. MAINTENANCE REPAIRED THE FLOOR SUPPORT IAW SRM 51-70. OK FOR SERVICE.
DURING INSPECTION FOUND FUSELAGE FRAME, BS 907 S23-24L SHEAR TIE CORRODED. MAINTENANCE REPAIRED IAW ERA 508430-14.
DURING INSPECTION CORROSION, FOUND ON THE INNER SURFACE OF THE REF A KIN DOUBLER AT BS 869 JUST ABOVE S-25L. MAINTENANCE REPAIRED IAW ERA 508435-14.
DURING INSPECTION, CORROSION WAS FOUND ON THE INNER SURFACE OF SKIN DOUBLER AT BS 869 JUST ABOVE S-25L. MAINTENANCE REPAIRED IAW ERA 508435-14.
DURING TESTING, FOUND SERVERAL BATTERYS WOULD NOT HOLD CHARGE AT FIRST CLASS SEATS, OVERWING AND ROWS 19-21. REPLACED FOUR BATTERIES.
CABIN FRAME AT BS 727B IS CRACKED LOCATED AT STRINGER 8L. REPAIRED IAW ERA 507346-14 AD ORIG.
CABIN FRAME AT BS 400 IS CRACKED AT STRINGER 8L. REPAIRED IAW ERA 507346-14 AD ORIG.
CABIN FRAME AT BS 440 IS CRACKED AT STRINGER 8R. REPAIRED IAW ERA 507346-14 AD ORIG.
AFT GALLEY FLOORBEAM BS 967, LBL 6 FASTENER HOLES CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1.
UPPER CABIN FWD GALLEY FLOORBEAM, BS 344, BL 0 CORRODED AT F/A FASTENER HOLE. REPAIRED IAW SRM 53-10-51.
CABIN SEAT TRACK AT BS 521, LBL 45 HAS WORN CROWN. REPAIRED IAW SRM 53-00-52. REPAIR 4.
CABIN SEAT TRACK AT BS 521 RBL 25 HAS WORN CROWN. REPAIRED IAW SRM 53-00-52. REPAIR 4.
CABIN SEAT TRACK AT BS 521 LBL 25 HAS WORN CROWN. REPAIRED IAW SRM 53-00-52 REPAIR 4.
DURING EMERGENCY LIGHT TEST BATTERY PACKS M1671, M1672, M167AND M1695 FAILED CAPACITY TEST. REPLACED BATTERY PACKS AND TESTS OK.
SMOKE COMING FROM FL BUTTON ON TRANSPONDER. TURNED TRANSPONDER TO STBY AND SMOKE BEGAN TO DISSIPATE. PULLED CORRESPONDING ATC CBS AND NO SMOKE WAS NOTED. DURING INSP NOTED THAT FO LIGHTING CB ON PEDESTAL POPPED. REPLACED TRANSPONDER PANEL. AFTER CONFIRMING PANEL SMOKED. TRANSPONDER TEST GOOD CB RESET LIGHTS TEST GOOD. NO FURTHER INCIDENCE OF SMOKE.
WINGLET MOD RT WINGTIP. MAINTENANCE MISDRILLED OF THE HOLE LOCATIONS AT APPROX OF SS725 COMMON TO THE UPPER FRONT SPAT CHORD, THE SPAR WEB AND THE SLAT TRACK SUPPORT FITTING FOR THE SLAT TRACK AT OFSS 730.
OIL CANNING FOUND IN THE BS 1016 AFT PRESSURE BULKHEAD AT APPROX RBL 10 & WL 290. DAMAGE CUT OUT AND REPAIR DOUBLER INSTALLED.
AFTER PUSHBACK, F/O SPD AND ALT TAPES WERE LOST, CAME BACK INTERMITTENTLY. SWITCHING FMC NAV SWITCH TO BOTH ON L SEEM TO WORK FOR ABOUT 2 SEC ON T/O, A/T ARM SWITCH WENT TO OFF. AIRBORNE, CAPT LOST F/D AUTO PILOT WOULD ENGAGE IN CWS ONLY HAD FAINT ODOR OF SMOLDERING WIRE. REPLACED AIR DATA MODULE PER FIM, ALL CHECKS GOOD.