N3730B
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 | on 2010-06-19 | Operator named in NTSB report |
Accident & incident history
Operated by Delta Air Lines Inc (per NTSB report)
Operated by Delta Air Lines, Inc. (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
107 reports on file, 2002-10-28 – 2024-10-25.
Part: WINDOW POST — CRACKED (ZONE 200) · airframe 70,213 hrs · 32,164 cycles
(LOG 0627768) SUSPECTED CRACKS ON R/H (CO-PILOTS) WINDOW POST BETWEEN SLIDING WINDOW AND FWD WINDSCREEN IN 2 AREAS MARKED. C/W ER/A 619132-14 ADTR REV ORIGINAL.
Part: STANCHION — CRACKED (ZONE 200) · airframe 70,213 hrs · 32,164 cycles
(LOG 0627494) DURING INSPECTION, A CRACK WAS FOUND RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAMES OF THE LH 9P/N 141A8811-3) AND/OR RH (P/N 141A8811-4) NO. 1 DECK WINDOWS. REPAIRED CRACK PER ERA 619132-14.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0625569) PASSENGER COMPARTMENT FLOOR STRUCTURE, FLOOR BEAM STA 328 RBL 12 WL 208 CORRODED. C/W ER/A 621498-14 REV ORIGINAL.
Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 70,207 hrs · 32,161 cycles
PASSENGER COMPARTMENT FLOOR STRUCTURE LAV ATTACH POIN SUPPORT STA 277-STA 294.5 LBL 12 WL 208 SCRATCHED. REMOVED AND REPLACED INTERCOSTAL AT STA277 TO 294.5 LBL 12 IAW B737-800 SRM 51-40-02.
Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0620580) CORROSION AT AFT CARGO COMPARTMENT DOOR FWD SHIELD. REMOVED AND REPLACED AFT CARGO COMPARMENT DOOR FWD SHIELD I.A.W. B737 SRM 51-40-02-0G AND DWG 146A0081.
Part: CHANNEL — DAMAGED (ZONE 100) · airframe 70,207 hrs · 32,161 cycles
(LOG 0608482) FORWARD CARGO BAY R/H ZEE CHANNEL HAS DAMAGE AT STA 500A+18 STR 25R WL 168. REMOVED AND REPLACED ZEE CHANNEL R/H FROM STA 500A TO 500I, WL 168 PER B737 SRM 53-00-53-2R-6, PARA. 4. TABLE 201, FIG 202 AND SRM 53-00-53-1A-2.
Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 70,207 hrs · 32,161 cycles
(LOG 0603673) R/H HORIZONTAL PRESSURE DECK CRACKED 2" AFT OF 663 VERTICAL PRESSURE WEB, 6" INBOARD OF RBL 45.50. REPAIRED R/H HORIZONTAL PRESSURE DECK AFT OF 663 VERTICAL PRESSURE WEB 6" INBOARD OF RBL 45.50 IAW B737-800 SRM 53-40-51-2R-2 O.
Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0600705) CORROSION ON FORWARD CARGO BAY L/H ZEE CHANNEL AT STA 400 - STA 500I STR 25L WL 168. REMOVED & REPLACED FWD CARGO BAY L/H ZEE CHANNEL @ STA 400- STA 500I STR 25 WL 168 IAW B737 SRM 51-40-02-0G & BOEING DWG# 142A7500.
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0602093) CORROSION ON FORWARD CARGO BAY AFT BULKHEAD SUPPORT AT STA 500I STR 18R - STR 25R. REMOVED AND REPLACED RIGHT RAIL (SUPPORT) AT STA 500I STR 18 TO STR 25R IAW B737 SRM 51-40-02-0G AND DWG 143A9485-36.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0598532) PASSENGER COMPARTMENT FLOOR STRUCTURE, FLOOR SUPPORT STA 298 RBL 12 WL 208 CORRODED. REMOVED, REPLACED AND INSTALLED FLOOR SUPPORT BTW STA 298 TO 312, RBL 12 WL 208 IAW B737-800 SRM 51-40-02-0G AND DWG 141A5400.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0600227) STA 986 LBL 43 STR 21L HAS CORROSION AROUD TERMINAL BLOCK. REMOVED AND REMPLACED INTERCOSTAL PN: 147A8801U85 IAW B737 SRM 51-40-02-0G AND DWG 147A8801.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0598730) PASSENER SEAT TRACK HAS EVIDENCE OF CORROSION FROM STA 767 TO STA 887 RBL 25. ACCOMPLISHED REPAIR ON SEAT TRACK FROM STA 767 TO 887 RBL 25 PER B737 SRM 53-00-52-2R, REPAIR 5 AND DWG# 146A5300 REV. C.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0598521) FLOOR SUPPORT AT STA 947+5 RBL 46 HAS CORROSION . REMOVED, REPLACED AND INSTALLED FLOOR SUPPORT STA 947.5 + 5" AND RBL 30 TO RBL 50 IAW B737-800 SRM 51-40-02-0G AND DWG 147A5650 REV: A.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 70,207 hrs · 32,161 cycles
(LOG 0598757) PASSENER SEAT TRACK HAS EVIDENCE OF CORROSION FROM STA 767 TO STA 887 LBL 25. ACCOMPLISHED SEAT TRACK REPAIR AND SECTION REPLACEMENT FROM STA 767 TO STA 887 LBL 25 IAW B737 SRM 53-00-52-2R-5 AND BOEING DWG# 146A5300.
Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 70,207 hrs · 32,161 cycles
(LOG 0598334) VAPOR BARRIER LH UPPER ANGLE TO FUEL TANK HAS CRACK AT LBL 8 STA 663. REMOVED, FABRICATED AND INSTALLED VAPOR BARRIER L/H UPPER ANGLE AT STA 663 BETWEEN LBL 6.13 TO LBL 19 IAW B737-800 SRM 57-10-10-2R-5.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0598505) FLOOR SUPPORT AT STA 947-967 RBL 50 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02-0G AND BOEING DWG# 147A5650.
Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 70,207 hrs · 32,161 cycles
(LOG 0598314) VAPOR BARRIER LH UPPER ANGLE TO FUEL TANK HAS CRACK AT LBL 8 STA 663. REMOVED, FABRICATED AND INSTALLED VAPOR BARRIER L/H UPPER ANGLE AT STA 663 BETWEEN LBL 6.13 TO LBL 19 IAW B737-800 SRM 57-10-10-2R-5.
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0597072) WEB AT STA 986-1016 HAS CORROSION ON CORNER AT RBL 34. REMOVED AND REPLACED WEB AT STA 986-1016 RBL 34 IAW B737 SRM 51-40-02-0G DRAWING# 147A5700 REV-ASSOCIATED ER/A 14-618756 ADDED FOR AC 3730.
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0596987) CORROSION ON AFT CARGO DOOR THRESHOLD WEB. REPLACED AFT CARGO DOOR THRESHOLD WEB IAW B737-800 SRM 51-40-02-0G, SRM 51-40-05 DWG 146A8340 REV A.
Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0596696) MOP SEAL STA 947-986 RBL 56 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALLED MOP SEAL IAW B737 SRM 51-40-02-0G AND DWG 147A8501.
Part: BAFFLE — DAMAGED (ZONE 100) · airframe 70,207 hrs · 32,161 cycles
(LOG 0597146) FWD CARGO LH BAFFLE STA 440-460 DAMAGED. INSTALLED NEW BAFFLE ON FWD CARGO LH STA 440-460 IAW B737 SRM 51-40-02-0G.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0597107) PASSENGER COMPARTMENT FLOOR STRUCTURE, FLOOR BEAM STA 312 RBL 12 WL 208 CORRODED. REPAIRED FLOOR BEAM STA 312, RBL 12 WL 208 IAW B737-800 SRM 53-10-51-2R PROCEDURE 15, ALTERNATIVE.
Part: BAFFLE — DAMAGED (ZONE 100) · airframe 70,207 hrs · 32,161 cycles
(LOG 0597114) FWD CARGO RH BAFFLE STA 500A TO 500B DAMAGED. INSTALLED NEW BAFFLE ON FWD CARGO RH STA 500A TO 500B IAW B737 SRM 51-40-02-0G.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0597059) FLOOR BEAM AT STA 947 RBL 53 HAS CORROSION. PERFORMED REPAIR ON T-CHORD STA 947 FLOOR BEAM FROM RBL 36 TO RBL 60 PER B737 SRM 53-70-51-2R-5.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 70,207 hrs · 32,161 cycles
(LOG 0600365) CABIN SEAT TRACK GOUGED AT STA 520 LBL 25 WL 208. REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 510H TO BS 520 LBL 25 WL 208 AND REPAIRED PER B737 SRM 53-00-52-2R-4.
Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0597097) CORROSION ON AFT CARGO BAY FWD SHIELD STA 767 TO STA 797 STR 24R. REMOVED AND REPLACED SHIELD DAMAGED AT AFT CARGO BAY FWD SIDE STA 767 TO 797 STR 24R PER B737-800 SRM 51-40-02 AND DWG 146A0081 REV. A.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 70,207 hrs · 32,161 cycles
(LOG 0600374) CABIN SEAT TRACK GOUGED AT STA 520 RBL 25 WL 208. REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 510H TO BS 520 RBL 25 WL 208 AND REPAIRED PER B737 SRM 53-00-52-2R-4.
Part: ATTACH FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0592108) PASSENGER COMPARTMENT FLOOR STRUCTURE L1 DOOR FWD AND AFT GIRT BAR LATCH ATTACH FITTINGS ARE CORRODED. REMOVED AND REPLACED PASSENGER COMPARTMENT FLOOR STRUCTURE L1 DOOR FWD AND AFT GIRT BAR LATCH ATTACH FITTING I.A.W B737 SRM 51-40-02-0G AND DWG# 141A5220.
Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
PASSENGER COMPARTMENT FLOOR STRUCTURE, R/H MOPSILL STA 297-STA 360 WL 208 CORRODED. REMOVED AND REPLACED PASSENGER COMPARTMENT FLOOR STRUCTURE R/H MOPSILL STA. 297- STA 360 WL 208 I.A.W B737 SRM 51-40-02-0G AND DWG# 141A8310.
Part: SILL DRAIN — SCRATCHED (ZONE 200) · airframe 70,207 hrs · 32,161 cycles
(LOG 0597132) PASSENGER COMPARTMENT FLOOR STRUCTURE L/H MOPSIL STA 270-STA 290 WL 208 SCRATCHED. REMOVED AND REPLACED FWD ENTRY DOOR LOWER SILL INNER CHORD (MOP SILL) STA 270-360 WL 208 IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG 142A0050 REV - DUE TO SCRATCHES EXCEEDING MAX ALLOWABLE OF 10% MATERIAL LOSS PER B737 SRM 53-10-15-1A-1 AT STA 270-290.
Part: WEB — DAMAGED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0592124) AFT CARGO LOWER SILL WEB STA 767 TO STA 787 RBL 20 DAMAGED. REMOVED AND REPLACED LOWER SILL WEB AT AFT CARGO STA 767 TO 787 RBL 20 PER B737-800 SRM 51-40-02-0G AND DWG 146A0081.
Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0595307) Z CHANNEL HAS MULTIPLE SPOTS OF CORROSION FROM STA 727-STA 727F+10 STR 24L. REMOVED AND REPLACED Z CHANNEL AT STA 727 TO STA 847 STR 24L IAW B737 SRM 57-40-02-0G AND DWG 146A7500.
Part: FRAME — CRACKED (ZONE 200) · airframe 70,207 hrs · 32,161 cycles
(LOG 0592097) FOUND CRACK IN FRAME AT BS 440 STR 8L INBD FASTENER HOLE. REPAIRED PER WORK CARD 2526-01236-04A INSTRUCTIONS, REF SUPPORTING AA 2526-01236.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
PASSENGER COMPARTMENT FLOOR STRUCTURE, FLOOR SUPPORT STA 328-STA 344 LBL 13 WL 208 CORRODED. REPLACED PART IAW B737-800 SRM 51-40-02-0G.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
LOG (0592131) 986 FLOOR BEAM HAS MULTIPLE SPOTS OF CORROSION AT RBL 33-43. REMOVED AND REPLACED FLOOR BEAM T-CHORD SECTION STA 986 FROM LBL 7 TO RBL 50 PER B737 SRM 53-70-51-2R-4.
Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,207 hrs · 32,161 cycles
(LOG 0595301) Z CHANNEL HAS MULTIPLE SPOTS OF CORROSION FROM STA 727E-STA 767 STR 24R. REMOVED AND REPLACED ZCHANNEL FROM STA 727 TO 767 STR 24R I.A.W B737-800 SRM 51-40-02-0G AND DWG 146A7500 REV C.
Part: BAFFLE — DAMAGED (ZONE 100) · airframe 70,207 hrs · 32,161 cycles
(LOG 0586889) FWD CARGO LH BAFFLE STA 500B-500C DAMAGED. REMOVED AND REPLACED FWD CARGO LH BAFFLE STA 500B-500C IAW B737 SRM 51-10-02-0G PAR 9 AND BOEING DWG NO. 143A7505 REV B.
Part: POWER SUPPLY — MALFUNCTIONED (ZONE 200) · airframe 69,996 hrs · 32,086 cycles
(LOG 6169664) DURING SVC CHECK THE FWD GALLEY LEFT SIDE CABIN EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. REMOVED AND REPLACED THE FWD GALLEY LEFT SIDE EMERGENCY EXIT POWER PACK ASSY IAW B737 AMM 33-51 AND REPLACED THE BATTERY PACK AS WELL WITH THE SAME REFERENCE. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 69,996 hrs · 32,086 cycles
(LOG 6169653) MULTIPLE EMER LIGHTS OUT AT FWD GALLEY + ROWS 19-24. REPLACED POWER SUPPLIES (M1670) OPS CHECK NML LK 054303. R/R POWER SUPPLY (M01675), R/R BATTERY @(M1675). OPS CHECKED GOOD IAW B737 AMM 33-51.
Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 69,075 hrs · 31,687 cycles
(LOG 4543534) FOUND EMERG LIGHTS BATTERY PACK AT 23F DOES NOT OPERATE CORRECTLY. R/R BATTERY PACK AT 23F PER B737 AMM 33-51. OPS CHECK GOOD.
Earlier reports · 2002–2023 · 67 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,695 hrs · 31,055 cycles
SHIP 3730 -HYD/DE- DECLARED EMERGENCY DUE TO 'A' HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. MANUALLY EXTENDED LANDING GEAR. CORRECTIVE ACTION: FOUND LEFT HYDRAULIC MODULAR PACKAGE O-RING LEAKING. REPLACED SAME. REPLACED LEFT ENGINE EDP AND CASE DRAIN FILTER. OPS AND LEAK CHECKS GOOD.
Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 67,361 hrs · 30,908 cycles
(LOG 5364399) EMERGENCY LIGHTS FROM ROW 16-18 INOP. REMOVED AND REPLACED BATTERY PACK IN REF B737 AMM 33-51. OPS CHECK GOOD AT THIS TIME.
Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 66,641 hrs · 30,626 cycles
(LOG 4905245) 1L DOOR, 1L F/A SEAT, AND COCKPIT ENTRY EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER B737-800 AMM 33-51. TEST OK.
2022
Part: BATTERY PACK — INOPERATIVE · airframe 64,643 hrs · 29,722 cycles
(LOG 9589560) DURING INSPECTION FOUND AFT GALLEY EMER LIGHT BATTERIES M1672 & M1673 ARE INOP. REMOVED & REPLACED AFT EMER LIGHT BATTERIES PER B737 AMM 33-51. OPS CHECK GOOD.
2021
Part: MODULE — LEAKING (HYD SYSTEM) · airframe 61,503 hrs · 28,385 cycles
SHIP 3730 -HYD- DUE TO LOSS OF 'A' SYSTEM HYDRAULICS. MANUALLY EXTENDED LANDING GEAR PRIOR TO LANDING. CORRECTIVE ACTION: FOUND 'A' SYSTEM HYDRAULIC MODULE LEAKING. REPLACED O-RING. REPLACED #1 ENGINE EDP. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PANEL — CHAFED (WNG-BDY FAIRING) · airframe 61,271 hrs · 28,292 cycles
(LOG 1893985) AA5352-01035 WING TO BODY PANEL 193D CENTER WHEEL WELL PANEL IS CHAFED ON T/E. REPAIRED THE DAMAGED IN 193D CENTER WHEEL WELL PANEL PER SRM 53-60-70.
2020
Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,354 hrs · 27,019 cycles
DURING INSPECTION FOUND EMERGENCY FLOOR LIGHT AT 30DEF INOPERATIVE. R/R LIGHT ASSY PER AMM 33-51. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (SEAT 30) · airframe 57,766 hrs · 26,752 cycles
(LOG 6337388) DURING INSPECTION FOUND AISLE SEAT 30 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. OPS TEST EMERGENCY ESCAPE PATH LIGHT AT LIGHT SEAT 30 PER B737 AMM 33-51. OPS TEST GOOD.
2019
Part: SENSOR — MALFUNCTIONED (TE FLAP) · airframe 54,561 hrs · 25,439 cycles
ON APPROACH FOR 24 R FLAP HANDLE AT 1-INDICATIOR SHOWED SPLIT. COMPLIED WITH QRH PROCEDURE FOR ASSYM. CONFIGURED AND LANDED ON 24L. R&R SENSOR PER AMM 27-59. OPS CHECK GOOD.
2018
Part: TRANSMITTER — FALSE INDICATION (TE FLAPS) · airframe 53,889 hrs · 25,160 cycles
(LOG 4867486) UPON LANDING, FLAPS INDICATED 2 AND STUCK THERE. WE USED THE ALT FLAP SWITCH TO MOVE THE FLAPS TO 15. NORMAL LANDING. REPLACED RT FLAP POSITION TRANSMITTER IAW B737 AMM 27-58. PER MCC ALSO REPLACED FLUID IN ALL 8 FLAP TRANSMISSIONS IAW B737 AMM 12-22. FLAPS OPS CKS NML.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
CORROSION ON ZEE SUPPORT RT BTW STA 727 TO 767 AT AFT CARGO COMPARTMENT. (LEVEL CORROSION 2) ZEE SUPPORT RT BTW STA 727 TO 767 WAS REPLACED PER SRM 51-40-02.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
SEVERAL POINTS OF CORROSION ON ZEE SUPPORT LT BTW STA 727 TO 847 AT AFT CARGO COMPARTMENT 5300-2190. ZEE SUPPORT LT BTW STA 727 TO 847 WAS REPLACED PER SRM 51-40-02.
Part: STRUT — CORRODED (RT MLG) · airframe 53,342 hrs · 24,937 cycles
DUE TO THE REMOVAL OF RT MLG. CORROSION ON RT MLG LOWER SIDE STRUT LOWER/FWD SPOT FACE. R&R LOWER SIDE STRUT AT RT MLG PER AMM 32-11-61.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
HIDDEN CRACK ON EXTERNAL POWER RECEPTACLE FWD CUTOUT AREA. REPAIR WAS ACCOMPLISHED WITH ETI-37-18- 490 REV 2 AND ER/A 571431-14 REV ORIG.
Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
CORROSION ON LH SIDEPLATE BTW STA 460 TO STA 500 I AT FWD CARGO COMPT. (LEVEL CORROSION 2) SIDE PLATE WAS REPLACED PER SRM 53-00-53 REPAIR 5 PAR 4B AND SRM 51-40-02.
Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
OUT OF LIMITS CORROSION ON RT TIE TRACK BTW STA 787 AND STA 847. LEVEL CORROSION 2, TIE TRACK BTW STA 787 AND STA 847 WAS REPLACED PER SRM 51-40-02.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
CORROSION AT BEAM STA 986 FROM 30/48 LBL. BEAM WAS REPAIRED PER ETI-37-18-504 REV 2 AND ER/A 571457-14 REV ORIGINAL ASSOCIATED ER/A 00-571457.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
CORROSION AT BEAM STA 986 FROM 30/48 RBL. BEAM WAS REPAIRED PER ETI-37-18-504 REV 2 AND ER/A 571457-14 REV ORIGINAL ASSOCIATED ER/A 00-571457.
Part: SKIN — DENTED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
REVALUATED DENT APPROX 12 IN AFT OF L1 DOOR THERSHOLD, OUT OF LIMITS PER SRM 53-00-01. DENT WAS REPAIRED PER ETI-37-18-506 REV 2 AND ER/A 571433-14 REV ORIGINAL.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,342 hrs · 24,937 cycles
INITIAL INSPECTION: CRACK RIB OF LT HORIZONTAL STABILIZER STA SS 92.70 (EHV). RIB OF LT HORIZONTAL STABILIZER STA SS 92.70 WAS REPAIRED PER SRM 55-10-09, FIG 202 REPAIR 4.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,342 hrs · 24,937 cycles
INITIAL INSPECTION: CRACK RIB OF RT HORIZONTAL STABILIZER STA SS 92.- 70 (EHV). RIB OF RT HORIZONTAL STABILIZER STA SS 92.70 WAS REPAIRED PER SRM 55-10-09, FIG 202 REPAIR 4.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CORROSION AT DOOR SILL AFTER ENTRY DOOR FROM STA 927/1000 LT. DOOR SILL AFTER ENTRY DOOR FROM STA 927/1000 LT (CPAX) WAS REPLACED PER SRM 51-40-02 PAR 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
CRACK STUB FRAME AT STA 294 RBL 60 FWD WET AREA (W1). STUB FRAME AT STA 294 RBL 60 WAS REPAIRED PER ETI-37-08-492 REV ORIGINAL AND ER/A 571317-14 REV ORIGINAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 727B BTW S9R TO S8R. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ER/A 571063-14 REV ORIGINAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 727B BTW S9L TO S8L. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ERA 571063-14 REV ORIGINAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 500A BTW S9L TO S8L. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ER/A 571063-14 REV ORIGINAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 480 BTW S9L TO S8L. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ER/A 571063-14 REV ORIGINAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 480 BTW S9R TO S8R. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ERA 571063-14 REV ORIGINAL.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CORROSION ON ZEE SUPPORT RT, AFTER ENTRY DOOR. ZEE SUPPORT RT, AFTER ENTRY DOOR (CPAX) WAS REPLACED PER SRM 51-40-02 PAR 4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 500D BTW S9L TO S8L. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ERA 571063-14 REV ORIGINAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 500D BTW S9L TO S8L. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ER/A 571063-14 REV ORIGINAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CRACK ON FRAME STA 500A BTW S9R TO S8R. FRAME WAS REPAIRED PER ETI-37-18-498 REV ORIGINAL AND ER/A 571063-14 REV ORIGINAL.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CORROSION ON ZEE SUPPORT AFTER SERVICE DOOR RT. ZEE SUPPORT AFTER SERVICE DOOR RT (CPAX) WAS REPLACED PER SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CORROSION AT INTERCOSTAL BTW STA 951/967 48 LBL. INTERCOSTAL REPLACED PER SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CORROSION AT INTERCOSTAL BTW STA 951/967 48 RBL. INTERCOSTAL BTW STA 951/967 48 RBL WAS REPLACED PER SRM 51-40-02 PAR 4.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND CORROSION AT DOOR SILL, AFTER SERVICE DOOR FROM STA 927 TO 1000 (CPAX). DOOR SILL WAS REPLACED PER SRM 51-40-02 PAR 4 AND PAR 7.
Part: INTERCOSTAL — WORN (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION FOUND WEAR ON INTERCOSTAL WEBS OF E&E DOOR CUTOUT E&E. WEB WAS REPLACED PER SRM 53-10-15 FIG 3 AND TABLE 3 (8) AND 51-40-02 PAR 4 AND 7.
Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 53,342 hrs · 24,937 cycles
(LOG 0721231) DURING INSPECTION FOUND CRACK ON LWR MAIN SILL WEB OF THE FWD SERVICE DOOR AT RBL 54 AND STA 296. WEB WAS REPAIRED PER SRM 51-70-13 REPAIR 4.
Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION, FOUND A CRACKED FLOOR SUPPORT, BS 277 TO 294, BL 0. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-70-11, FIG 201.
Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION, FOUND A CRACKED FLOOR SUPPORT, BS 328 - 344, LBL 46. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-70-11, FIG 201.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT, BS 312 - 328, LBL 46. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 53,342 hrs · 24,937 cycles
DURING INSPECTION, FOUND A CRACK ON THE FLOOR SUPPORT BETWEEN BS 312 TO 328, RBL 31. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02, PAR 4, AND 7.
Part: ENGINE — FIRE (TAIL PIPE) · airframe 52,150 hrs · 24,486 cycles
WHILE TAXIING, TOLD THAT A FLAME WAS COMING OUT OF THE NR 2 ENGINE. DECLARED AN EMERGENCY AND RETURNED TO THE GATE AFTER SECURING THE ENG. MAINTENANCE VISUALLY EXAMINED THE NR 2 ENGINE EXHAUST AREA AND FOUND OIL PUDDLE AND HEAVY SOOT INSIDE EXHAUST PLUG. IAW AMM 71-00 THIS CONDITION IS DESCRIBED AS A KIND OF CANDLE FIRE PHENOMENA. INSPECTED FLAME ARRESTOR WITH NTF, RAN ENG AT IDLE FOR 20 WITH NO FLAMES NOTED.
Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 51,382 hrs · 24,219 cycles
L1 GIRT BAR HOLDER RIGHT SIDE STICKING AND VERY DIFFICULT TO RELEASE. REMOVED DEBRIS, GIRT BAR HOLDER OPS CHECKED NORMAL.
2016
Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 46,602 hrs · 22,615 cycles
DURING FLIGHT AT FL 360, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED. BOTH BLEEDS AND PACKS ON. CABIN DESCENDED 1200 FPM. SELECTED ALT MODE. CABIN STABILIZED AT FL 230. AIRCRAFT DIVERTED. COMPLETED QRH GOING TO MANUAL MODE ON APPROACH. MAINTENANCE FOUND BOTH CABIN PRESSURE CONTROLLERS BITE TEST FAULT FOR THE CABIN OUTFLOW VALVE. REPLACED THE OUTFLOW VALVE IAW AMM 21-31-03-000-801. OPS CHECKED NORMAL, AIRCRAFT RETURNED TO SERVICE.
Part: SEAT TRACK — WORN (BS 520) · airframe 45,788 hrs · 22,341 cycles
DURING INSPECTION, FOUND PASSENGER CABIN BS 520, RBL 45 SEAT TRACK HAS WEAR FROM SEAT. MAINTENANCE REMOVED WORN SEAT TRACK. FABRICATED AND REPLACED -1 SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
Part: SEAT TRACK — WORN (BS 520) · airframe 45,788 hrs · 22,341 cycles
DURING INSPECTION FOUND PASSENGER CABIN BS 520, LBL 45, SEAT TRACK HAS WEAR FROM SEAT. MAINTENANCE REMOVED WORN SEAT TRACK. FABRICATED AND REPLACED SEAT TRACK AT BS 520, LBL 45 IAW SRM 53-00-52, REPAIR 4.
Part: SEAT TRACK — WORN (BS 520) · airframe 45,788 hrs · 22,341 cycles
DURING INSPECTION, FOUND PASSENGER CABIN BS 520, RBL 24 SEAT TRACK HAS WEAR FROM SEAT. MAINTENANCE REMOVED WORN SEAT TRACK. FABRICATED AND REPLACED -1 SEAT TRACK IAW SRM 53-00-52, REPAIR 4.
Part: SEAT TRACK — WORN (BS 520) · airframe 45,788 hrs · 22,341 cycles
DURING INSPECTION FOUND PASSENGER CABIN BS 520, LBL 24 SEAT TRACK HAS WEAR FROM SEAT. MAINTENANCE REMOVED WORN SEAT TRACK. FABRICATED AND REPLACED-1 SEAT TRACK, LBL 24 BS 520 IAW SRM 53-00-52, REPAIR 4.
2015
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 42,925 hrs · 21,332 cycles
DURING INSPECTION FOUND SEAT 32 DEF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND CONNECTOR LOOSE. SECURED THE CONNECTOR. EMERGENCY LIGHT OPS CHECKED NORMAL IAW AMM 33-51.
2014
Part: OVEN — FAILED (GALLEY) · airframe 39,958 hrs · 20,331 cycles
DURING FLIGHT, FORWARD GALLEY OVEN HAD SMOKE COMING FROM BOTH VENTS WITH DISTINCT ODOR OF ELECTRIC FIRE. OVEN WAS ON BUT NOT HEATING AT THE TIME THEN SHUT ITSELF OFF. REMOVED AND REPLACED THE OVEN .
Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,689 hrs · 20,248 cycles
DURING INSPECTION FOUND CABIN SEAT TRACKS AT BS 727B LBL 24.75, RBL 27.75, LBL 45.5, RBL 45.5 HAS CRACK DAMAGE. MAINTENANCE REPAIRED SEAT TRACKS IAW ERA 528495-14AD, REV ORIG.
2013
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,400 hrs · 19,011 cycles
DURING INSPECTION, FOUND BATTERY PACK FAILED. MX R & R BATTERY PACK. OPS CHECKED GOOD.
2012
Part: FRAME — CRACKED (BS 440 S8R) · airframe 32,861 hrs · 17,726 cycles
FUSELAGE FRAME CRACKED AT STATION 440 STRINGER 8R. REPAIRED IAW ERA 504544-14AD.
Part: FRAME — CRACKED (BS 380 S8R) · airframe 32,861 hrs · 17,726 cycles
FUSELAGE FRAME CRACKED AT BS 380 STR 8R. REPAIRED IAW ER/A 504544-14AD.
Part: FRAME — CRACKED (BS 400 S8L) · airframe 32,861 hrs · 17,726 cycles
FUSELAGE FRAME CRACKED AT BS 400 STRINGER 8L. REPAIRED IAW ERA 504544-14AD.
Part: FRAME — CRACKED (BS 400 S8R) · airframe 32,861 hrs · 17,726 cycles
FUSELAGE FRAME CRACKED AT BS 400 STRINGER 8R. REPAIRED IAW ERA 504544-14AD.
Part: SPAR — DAMAGED (HORIZONTAL STAB) · airframe 32,162 hrs · 17,472 cycles
DURING PSV 12 SCHEDULE MAINTENANCE, MAINTENANCE REPORTED WEAR DAMAGE ON THE HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR FITTING ADJACENT TO THE LT LOWER AFT LUG. REPAIRED PER ERA 493419-14.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 32,155 hrs · 17,469 cycles
DURING EMERGENCY LIGHT FUNCTION CHECK, TWO PACKS FAILED TEST. REPLACED BATTERIES M1671 M1675 AND TESTS OK.
2010
Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,838 hrs · 14,974 cycles
AIRCRAFT WAS STRUCK BY BAGGAGE CART AT STA 887 BY STRINGERS 22L AND 23L (DL738101733).
Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,838 hrs · 14,974 cycles
AIRCRAFT WAS STRUCK BY BAGGAGE CART AT STA 887 BY STRINGER 22L AND 23L.
2008
Part: OVERHEAT LOOP — INOPERATIVE (CARGO BAY) · airframe 18,870 hrs · 12,229 cycles
AFTER TAKEOFF CLIMBING THROUGH 300 FT AGL LT WING-BODY OVERHEAT LIGHT ILLUM. DID QRH PROCEDURE. LIGHT STILL ILLUM, RETURNED TO LAND SLC. LANDED OVERWEIGHT. AT GATE, LIGHT STILL ILLUM. REPLACED DETECTORS M347 AND M1147. TESTS OK.
2007
Part: SENSOR — OPEN (NR 1 NACELLE) · airframe 17,414 hrs · 11,749 cycles
AT FL 390 AND .77M ATC REQUESTED TO SLOW TO .75M. ALMOST IMMEDIATELY GOT NR 1 LEFT BLEED TRIP. LOST CABIN PRESS CABIN WENT UP TO 12'000 TO 12'200. BEFORE BLEED RESET WORKED AT APPROX 29'000. LEVELED AT FLT 250 AND KEPT AS STABLE AS POSSIBLE. NO FURTHER TRIPS OCCURRED. MTC IN PROGRESS DNTC. REPLACED 390 DEG TEMP SENSOR ON NR 1 ENG PYLON. REPLACED 390 DEG TEMP SENSOR NR 2 ENG PYLON. CKS GOOD PER M/M.
2005
Part: WARNING LIGHT — FALSE INDICATION (L1 DOOR) · airframe 11,182 hrs · 9,299 cycles
REJECTED TAKEOFF AT 100 KIAS FOR L1 DOOR INDICATED OPEN ON TAKEOFF. CLEANED DOOR PROX SENSOR.
2004
Part: BEARING — FAILED (NR 1 ENGINE) · airframe 5,872 hrs · 6,160 cycles
NR 1 ENG INFLIGHT SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT. FOUND METAL IN TAILPIPE AND FAN WOULD NOT SPIN. REPLACED ENGINE.
2003
Part: FITTING — DAMAGED (NR 2 ENGINE) · airframe 3,801 hrs · 4,493 cycles
NR 2 ENG HYD QTY DECREASING ON CLIMBOUT. REPLACED NR 2 ENG HYD PUMP PRESSURE HOSE AND QUICK DISCONNECT FITTING AND CASE DRAIN HOSE AT ENG PUMP.
2002
Part: BULB — BURNED OUT (LT AFT OVRWG EXI) · airframe 3,239 hrs · 3,885 cycles
LT AFT OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. RELMAPED SAME. OPS CHECKS NORMAL.