ATLAS AIR INC

Operated by ATLAS AIR INC (per NTSB report)

Operated by Atlas Air Inc. (per NTSB report)

Operated by Atlas Air (per NTSB report)

Operated by Atlas Air (per NTSB report)

Operated by ATLAS AIR INC (per NTSB report)

Maintenance personnel’s improper installation and inspection of the port M borescope plug, which resulted in an engine fire.

Operated by Atlas Air (per NTSB report)

Operated by Atlas Air (per NTSB report)

The inappropriate response by the first officer as the pilot flying to an inadvertent activation of the go-around mode, which led to his spatial disorientation and nose-down control inputs that placed the airplane in a steep descent from which the crew did not recover. Contributing to the accident was the captain's failure to adequately monitor the airplane's flightpath and assume positive control of the airplane to effectively intervene. Also contributing were systemic deficiencies in the aviation industry's selection and performance measurement practices, which failed to address the first officer's aptitude-related deficiencies and maladaptive stress response. Also contributing to the accident was the Federal Aviation Administration's failure to implement the pilot records database in a sufficiently robust and timely manner.

Operated by Atlas Air (per NTSB report)

Operated by Atlas Air Inc (per NTSB report)

an improper landing flare technique and the lack of the appropriate bounced landing recovery procedure.

Operated by Atlas Air (per NTSB report)

Operated by Atlas Air , Inc. (per NTSB report)

the flight crew's failure to properly identify the airport and runway of intended landing. Contributing to the incident was the flight crew's failure to follow company procedures for crosschecking navigational information and visual cues to verify the airport and runway of intended landing.

Operated by ATLAS AIR INC (per NTSB report)

Operated by ATLAS AIR INC (per NTSB report)

The Boeing 747 first officer’s failure to maintain clearance from another airplane while taxiing due to his inadequate judgment of the distance between the airplanes.

Operated by ATLAS AIR INC (per NTSB report)

impact of the fore flap with the aft fuselage after fatigue failure of the right wing fore flap carriage assembly attachment fitting at position 6.

Operated by ATLAS AIR INC (per NTSB report)

Operated by ATLAS AIR INC (per NTSB report)

Operated by ATLAS AIR INC (per NTSB report)

Operated by ATLAS AIR INC (per NTSB report)

Operated by ATLAS AIR (per NTSB report)

disbonding and separation of the right inboard wing fixed trailing edge panel during cruise flight, which resulted in damage to the inboard fore flap and inboard mid flap, and a subsequent precautionary landing at the departure airport.

Sanction: $80,000 · case closed 2016-04-18

Sanction not stated · case closed 2010-12-17

Sanction: $165,000 · case closed 2010-12-17

Sanction: $120,000 · case closed 2007-05-30

Sanction: $7,500 · case closed 2006-04-10

Sanction: 14,000 · case closed 2005-11-14

Sanction: $10,000 · case closed 2004-12-17

Sanction: $10,000 · case closed 2005-02-25

Sanction: $16,000 · case closed 2001-04-24

Sanction not stated · case closed 2000-06-30

Sanction not stated · case closed 2000-06-30

Sanction not stated · case closed 2000-06-30

Sanction not stated · case closed 2000-06-30

Sanction not stated · case closed 2000-06-30

Sanction not stated · case closed 2000-06-30

Sanction: $90,000 · case closed 2000-06-30

Sanction not stated · case closed 2000-06-30

Sanction: $3,500 · case closed 1999-09-03

Sanction: $5,000 · case closed 1999-04-02

Sanction: $15,000 · case closed 1999-05-03

Part: FIRE WARNING — FALSE ACTIVATION · airframe 124,019 hrs · 22,411 cycles

ON LANDING EICAS WARNING MESSAGE "FIRE MAIN DECK AFT". (EMERGENCY WAS DECLARED BY THE FLIGHT CREW) FOLLOWED FIM 26-16 TASK 899-905. MDC AFT ZONE AREA INSPECTED, NO ABNORMALITIES NOTED. PERFORMED CARGO SMOKE DET A & B SYS RESET AND HUMIDITY REDUCED, FIRE SYS GND TEST RESULT PASS. NIL EXISITING FAULT MSG NOTED IAW AMM 26-14-00.

Part: ELEVATOR — CRACKED (ZONE 300) · airframe 15,759 hrs · 2,396 cycles

LEFT OTBD ELEVATOR TRAILING EDGE CRACKED (DIMENSION 11" X 1.5). PERFORMED REPAIR ON THE LT OTBD ELEVATOR T/E IAW SRM 51-70-05-2R, REPAIR 2, AND AMM 51-24-22. PERFORMED LT OTBD ELEVATOR BALANCING IAW SRM 51-60-00 AND SRM 51-60-02 AFTER REPAIR. NO OTHER DEFECTS NOTED.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 62,487 hrs · 10,232 cycles

CAPTAIN FLASHLIGHT INOPERATIVE. TRANSFER TO MDDR 257506 PER MEL 25-64-02C CAT C. R/R CAPT FLASHLIGHT AND HOLDER IAW AMM 25-64-01. OPS CHK AND FUNCTIONAL CHK GOOD. THIS CLEARS DMI 257506. PLACARDS REMOVED.

Part: WIRE — DAMAGED (ZONE 200) · airframe 114,034 hrs · 18,365 cycles

CENTER SECTION ROW 26 AND AFT DID NOT DEPLOY O2 MASKS, REPAIRED WIRE W0720-01-14 BTWN PANEL P19 AND CONNECTOR D6000. OPS CHECKED GOOD IAW SWPM 20-10-11, WDM 35-21-14, AND AMM 35-21-00.

Part: BUCKLE — FAULTED (SEAT BELT) · airframe 110,348 hrs · 21,458 cycles

CAPTAIN`S SEAT BELT BUCKLE WILL NOT RELEASE. REMOVED ROTARY PART OF SEAT BELT FROM CAPT SEAT AND SWITCHED ROTARY PART OF SEAT BELT WITH THE SECOND OBSV ROTARY SEAT BELT PART AND DEFERRED SECOND OBSV SEAT PN 1101550-03. TRANSFER TO DMI 257490 PER MEL 25-11-02-02 CAT D DUE 12DEC26.</P>)

Part: CONTROL MODULE — FAULTED (ZONE 700) · airframe 104,509 hrs · 17,617 cycles

GEAR DISAGREE MESSAGE. LANDING GEAR LEVER WOULD NOT GO UP AFTER T/O. LANDING GEAR STAYED IN DOWN POSITION. RETURNED TO AIRPORT. COMPLETED FIM TASK 34-61-00-745-222. FMC-L FMC-R BOTH PASSED. PERFORMED TASK 23-27-00-715-001-004. TEST PASSED. MAINT NOTED THAT ACARS NETWORK IS DOWN. LP 2045769 M1: TRANSFER TO DMI 257550 PER MEL 32-30-01 CAT C. LP 2136974 M6: LANDING GEAR CONTROL MODULE WAS REPLACED. OPS CHECK PERFORMED. OPS CHECKED GOOD IAW AMM 32-31-01. THIS CLEARS DMI 257550, PLACARD REMOVED.

Part: LANDING GEAR — WARNING MESSAGE (ZONE 700) · airframe 67,852 hrs · 11,937 cycles

EICAS MSG GEAR TILT WHEN AIRBORNE AND ATTEMPTED TO RETRACT THE LANDING GEAR AFTER TAKE-OFF. MX IN WORK WHILE IN AOGM FOR GEAR TILT MSG AND LANDING GEAR DID NOT RETRACT. AOGM ETR: 15AUG26.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 35,411 hrs · 6,203 cycles

CPTS FLASHLIGHT INOPERATIVE. TRANSFER TO DMI 257381 PER MEL 25-60-03-01 CAT C DUE DATE 22AUG26.

Part: EEC — FAULTED (NR 2 ENGINE) · airframe 105,360 hrs · 17,680 cycles

ENGINE 2 OIL TEMP INFLIGHT. ENG 2 IFS. PERFORMED WINDMILLING INSPECTION AND NO TROUBLE FOUND AS PER AMM 72-00-00/601. PERFORMED ENGINE MAG CHIP INSPECTION AND NO TROUBLE FOUND PER AMM 79-00-00/601. REMOVED AND REPLACED #2 ENG'S EEC AND THEN OPS CHECKED OK PER AMM 73-21-15/401, AMM 79-34-00/501 &AMP; IPC 73-21-15-01. REPLACED #2 ENG'S EEC WITH THE ORIGINAL PART AT MCC'S REQUEST AS PER AMM 73-21-15/401. MX IN WORK WHILE IN AOGM FOR UER / FUEL SYS HEALTH. AOGM ETR: 15AUG26.</P>)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 114,032 hrs · 18,364 cycles

R4 DOOR HAS 2 EACH EMERGENCY SIGNS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY M1210 IAW AMM 33-51-09-002-006 AND AMM 33-51-07-402-010. OPS CHECKS GOOD. POWER SUPPLY P/N:&NBSP; BPS7-3, S/N: 26392.</P>)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 114,032 hrs · 18,364 cycles

LEFT EXTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED POWER SUPPLY M736 AND M738 IAW AMM 33-51-07-002-006. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 54,350 hrs · 7,048 cycles

L5 DOOR; SQUARE EMERGENCY LIGHT FAILS TO ILLUMINATE. REPLACED THE LAMPS FOR EMERGENCY LIGHT AT L5 DOOR IAW AMM 33-24-02. OPS CHKD GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 54,350 hrs · 7,048 cycles

L1 DOOR FWD EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED L1 EMERGENCY LIGHT ASSY IAW AMM 33-51-05-402-013. OPS CHECKED GOOD.

Part: SLIDE — FAULTED (ZONE 800) · airframe 114,032 hrs · 18,364 cycles

DURING CONNECTION OF LT OVERWING EXIT DOOR BATTERY CONNECTOR, SLIDE DOOR DEPLOYED CAUSING SLIDE LANYARD TO DISENGAGE FROM SLIDE BAR. DURING TROUBLESHOOTING, FOUND L/H AFT AUTO ARM/FIRE SWITCH PANEL AFT EYE BOLT BRACKET CORRODED, CAUSING THE STRAIGHT PIN CONTACTING AND MOVING THE ARM AND AUTO FIRE SWITCHES IN ARMED CONDITION, CAUSING THE SLIDE DEPLOYMENT. REMOVED AND REPLACED LT AFT AUTO ARM/FIRE SWITCH PANEL ASSEMBLY IAW AMM 25-65-15-904-073-001. REMOVED AND REPLACED L/H OFF-WING SLIDE ASSY IAW AMM 26-65-01-024-001-001 AND AMM 25-65-01-424-060-001. NO FURTHER DEFECTS NOTED.</P>)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 114,032 hrs · 18,364 cycles

L/H EXTERIOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED POWER SUPPLY M736 AND M738 IAW AMM 33-51-07-002-006. OPS CHKD GOOD.

Part: BEARING — LOOSE (ZONE 400) · airframe 114,032 hrs · 18,364 cycles

RIGHT PYLON SIDE LINK FITTING, ATTACHED ON RIGHT WING WS 400 FORWARD SPAR LOWER PANEL HAS 1EA LOOSE BEARING. REMOVED AND REPLACED FITTING ASSEMBLY ON RT WING FORWARD SPAR LOWER PANEL WS 400 PER DRAWING 112T7001-2 AND SERVICE BULLETIN 757-54-0081 REV 2 ON BOEING AIRCRAFT REPAIR ORDER TLS-RE-BGS-2600720. FIELD REPAIR RECORD FRR-1 HAS BEEN CATEGORIZED AS MAJOR REPAIR CATEGORY A WITH AN AMOC. REFERENCE ENGINEERING COORDINATION SHEET 767-CSE-26-039 AND FAA 8100-9 DATED JULY 28, 2026. ALL WORK ACCOMPLISHED BY THE BOEING COMPANY AT STE SAA. REF NON-ROUTINE 00700. NO FURTHER DEFECTS NOTED.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 114,032 hrs · 18,364 cycles

CORROSION ON LOWER FUSELAGE SKIN AROUND DRAIN VALVE BETWEEN STA.1540 - 1562 AND BETWEEN S-39L AND S-39R. REMOVED CORROSION L = 5.290" X W = 2.215" AND ACCOMPLISHED PERMANENT CATEGORY A CORROSION DAMAGE BLEND REPAIR ON EXTERNAL SIDE OF FUSELAGE SKIN P/N 146T3241-12 AROUND DRAIN VALVE BETWEEN FS1540 AND FS1562 AND BETWEEN S-39L AND S-39R IAW STE SAA EA# 767-5360-28-B0756 REV I/R DATED JUNE 25, 2026, AND ATLAS AIR EA-6753A316 REV. 0 DATED 11JUL 26. CLASSIFIED AS MAJOR REPAIR, APPROVED 8100-9 ISSUED. NO FURTHER DEFECTS NOTED.

Part: SKIN — DENTED (ZONE 100) · airframe 114,032 hrs · 18,364 cycles

DENT ON FUSELAGE SKIN AT STA 364 BETWEEN S-38L AND S-39L. ACCOMPLISHED PERMANENT CATEGORY B EXTERNAL REPAIR ON FUSELAGE SKIN ON ZONE-A AT STA 364 BETWEEN S-38L AND 39L, IAW SRM 53-00-01-2R-1 REPAIR 1. REPAIR REQUIRES REPEAT INSPECTIONS WITH THRESHOLD TO BEGIN 6000 FC AFTER REPAIR AND REPEAT INSPECTIONS THEREAFTER PER SRM 53-00-01-2R-1 REPAIR 1 TABLE V ALTERNATIVES. (CLASSIFIED AS MAJOR REPAIR). NO FURTHER DEFECTS NOTED.

Part: TRU — FAULTED · airframe 105,375 hrs · 16,995 cycles

EICAS MSG "ELEC GEN 3". COMPLIED QRH PROCEDURE(<P>AS A PRECAUTIONARY, R/R TRANSFORMER ASSY T4006 PER AMM 24-23-03/401 &AMP; IPC 24-23-03-034. PERF IDLE RUN UP OF #2 &AMP; #3 ENGINE IAW AMM 71-00-00/501. OPS CHK OK, ALL INDICATIONS NORMAL AND WITHIN LIMITS. FOUND WIRE W6056-306-184 CHAFING AGAINST BRAIDED LINE. REPAIRED WIRE PER WDM 24-21-32-4 &AMP; SWPM 20-10-11. PERFORMED HIGH POWER ENG RUN IAW AMM 71-00-00/501, OPS CHECK OK, UNABLE TO RECREATE FAULT.</P>)

Part: UNKNOWN — ODOR (CABIN) · airframe 16,774 hrs · 2,242 cycles

ON START AND SHUTDOWN, OIL BURN ODOR IN COCKPIT. PERFORMED GVI IAW FIM 21-00 TASK 808, NO OIL CONTAMINATION DETECTED AT THIS TIME.

Part: FITTING — CRACKED (ZONE 100) · airframe 100,749 hrs · 16,513 cycles

FOUND LUG FITTING CRACK AT FWD CARGO, BS 1000, LBL 11.33. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0, REV 107. INSTALLED NEW PART IAW SRM 51-40-02-0G-0, REV 107 AND REF EO 4453C024, PART 3, REV 4. CONDITION CHKD NORMAL.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 100,749 hrs · 16,513 cycles

FOUND SHEAR TIE CRACK AT STA 1000 RBL 33, FWD CGO. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 107. PERFORMED EI T2026A53M-1419, REV 0, AND REF EO 4453C024, PART 8, REV 4. ACCOMPLISHED EI T2026A53M-1419, REV 1. CONDITION CHKD NORMAL.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 100,749 hrs · 16,513 cycles

FOUND SUBSTITUTE SEAT TRACK SURFACE CRACKED AT M/D BS 1000, LBL 75.92. REMOVED DAMAGED TRACK IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 64525, SRM 53-00-52-2R-13, REV 107. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0, REV 107, AND DWG 65B8250, SHEET 9, REV B, AND DWG 65B16004, SHEET 4, REV A. CONDITION CHKD NORMAL.

Part: CARGO TRACK — BROKEN (ZONE 100) · airframe 100,749 hrs · 16,513 cycles

FOUND FWD CARGO TRACK BROKEN BS 560, LBL 24.75. REMOVED DAMAGED IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 60524, SRM 53-00-52-2R-10 REV 107, & EI T2026A53M-1614, REV 0. INSTALL FASTENERS IAW SRM 51-40-02-0G-0, REV 107, AND DWG 65B12300, SH 6, REV A, AND DWG 65B06051, SH 39, REV -. CHKD NORMAL.

Part: SPAR WEB — NONE (ZONE 300) · airframe 100,749 hrs · 16,513 cycles

FOUND EXISTING REPAIR ON VERTICLE STAB REAR SPAR WEB BETWEEN VSS 205 - VSS 220. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0, REV 107. REPAIRED DAMAGED AREA IAW W/S 60564 SRM 55-30-10-2R-2 REV 107. CHKD NORMAL.

Part: BULKHEAD — MODIFICATION (ZONE 100) · airframe 100,749 hrs · 16,513 cycles

PERFORMED BS 2598 BULKHEAD MODIFICATION, FOUND DEVIATION AT DOUBLER. ACCOMPLISHED EI T2026A53M-1528, REV 1, AND EI T2026A53M-1439, REV 1. CHECKED NORMAL.

Part: REPAIR — NONE (ZONE 600 FLAP) · airframe 100,749 hrs · 16,513 cycles

EXISTING REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE. PERFORMED PERMANENT REPAIR ON RT WING OTBD MID FLAP LOWER SURFACE, WBL 563 IAW SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-0, REV 107. CONDITION CHECK IS SATISFACTORY. REPAIR PROCESS REFER TO J/C ATTACHING SHEET 0511205.

Part: SPLICE ANGLE — CRACKED (ZONE 200) · airframe 100,749 hrs · 16,513 cycles

CRACK, PERFORMED SB 4453B761, PART 1-2. FOUND A CRACK AT BS 2598, S11R, RT FWD LWR FITTING AREA. ACCOMPLISHED EI 2026A53M-1510, REV 2, AND DWG 65B02706, SH 24, REV A, AND DWG 65B02597, SH 2 REV H, AND DWG 65B02509, SHT 3, REV R. CHECKED NORMAL.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 100,749 hrs · 16,513 cycles

FOUND CORROSION ON THE UPPER ANGLE BS 1030, LBL 11.33. ACCOMPLISHED W/S 60551 IAW SRM 53-40-52-2R-3, REV 107. & EI T2026A53M-1522, REV 1. CHECKED NORMAL.

Part: REPAIR — NONE (ZONE 100) · airframe 100,749 hrs · 16,513 cycles

PERFORMED UPGRADE TIME-LIMITED REPAIR ON SEC 48 FUSELAGE SKIN AT BS 2600, S51R. ACCOMPLISHED EI T2026A53M-1409, REV 1, AND DWG 65B02509, SH 9, REV C, AND DWG 65B02700, SH 2, REV G, SH 6, REV -. CHECKED NORMAL.

Part: SMOKE DETECTOR — ACTIVATED (CREW REST) · airframe 105,571 hrs · 17,762 cycles

SMOKE IN CREW REST EICAS AT 1955Z FOR ABOUT 5 MINS. SMOKE DISSIPATED AND EICAS DID NOT RETURN. REPLACED ALL PACK WATER SEPERATOR COALESCER BAGS IAW AMM 05-51-56 AND FIM 21-00 TASK 810. REPLACED CREW REST AREA SMOKE DETECTOR IAW AMM 26-14-51 AND 21-51-05. NO SMOKE, FUMES, OR ELECTRICAL FAULT IN THE CABIN NOTED.</P>)

Part: HEAT EXCHANGER — FAULTED (FUEL/OIL SYS) · airframe 105,346 hrs · 17,677 cycles

ENG 2 OIL TEMP EICAS MSG. FL 380 MAX OIL TEMP APPROX 194. ENG 2 SHUT DOWN. PERFORMED FIM 79-00, FT FIG 109. R & R FUEL/OIL HEAT EXCHANGER IAW AMM 79-21-01-404-014-J00, OPS CHECK & LEAK CHECKED GOOD. RUN ENG NR 2 AT DIFFERENT POWER SETTINGS AND OIL TEMP NORMAL PARAMETERSIAW AMM 71-00-00 & IPC 79-21-09-05.

Part: ENGINE — VIBRATION · airframe 124,229 hrs · 19,232 cycles

AIRCRAFT VIBRATION INCREASED WITH POWER ADVANCED. MX IN WORK WHILE IN AOGM FOR RTO AIRFRAME VIBRATION.

Part: HOOK AND LOOP — DETACHED (ZONE 200) · airframe 74,861 hrs · 11,489 cycles

CAPTAIN SIDE EVAS VELCRO PARTIALLY DETACHED(<P>RESECURED GLARESHIELD LOOP FASTENER IAW B777 AMM 25-60-99. NO FURTHER DEFECTS NOTED</P>)

Part: CLAMP — MISSING (ZONE 700) · airframe 30,243 hrs · 5,319 cycles

MISSING CLAMP ON #1 TORQUE ROD. REINSTALLED BAND CLAMP PER AMM 20-51-01 & IPC 654/6625-2441. OK FOR SERVICE.

Part: HMU — FAULTED (LT ENGINE) · airframe 116,597 hrs · 23,973 cycles

LEFT ENG INDICATIONS ERRATIC, STABLE AT IDLE, FOLLOWED BY A HIGH SURGE TO OVER 100N, THEN WE SHUT THE LT ENGINE DOWN. REMOVED AND REPLACED LT ENG EEC IAW AMM 73-21-15, P/N OFF 1870M33P14 & S/N OFF EC007065. REMOVED AND REPLACED THE LT ENG HMU IAW B767 73-21-14. OPS & LEAK CHKD OK.

Part: CABLE — DAMAGED (O2 MASK MIC) · airframe 16,697 hrs · 2,233 cycles

FO OXYGEN MASK MICROPHONE CABLE DAMAGED(<P>REMOVED AND REPLACED THE FO'S O2 MASK PER AMM 35-11-18-400-801 AND AIPC 35-11-18-03. OPS CHECK NML, NO LEAKS NOTED. MIC OPS NML</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles

M/D BS 1180 LHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>INTERCOSTAL WEB REPAIRED AS PER RI-53-40-18379 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: WEB — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles

M/D BS 1180 RHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER SRM 51-10-02 AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles

M/D BS 1220 LHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18378 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles

M/D BS 1220 RHS O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18381 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles

M/D STA 1200 RBL 105" BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED(<P>WEB CRACK AREA REPAIRED AS PER RI-53-40-18382 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 113,499 hrs · 20,012 cycles

M/D STA 1200 LBL 105 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED(<P>WEB REPAIRED AS PER RI-53-40-18377 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles

M/D BS 1020 TO 1070 LBL 11 SEAT TRACK RHS FLANGE BOTTOM SIDE FOUND CORROSION(<P>SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW SEAT TRACK INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles

RHW L/E UPPER FIXED PANEL O/B EDGE NEAR #3 PYLON O/B FOUND CORROSION(<P>CHORD REPLACED AND INSTALLED AS PER RI-57-41-18383 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: STRUCTURE — CORRODED (ZONE 500) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles

LHW STA 1241 CETNER LH O/J PUMP CUTOUT FOUND CORROSION(<P>WEB CORROSION AREA REPAIRED AS PER RI-57-10-18352 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: STRUCTURE — CORRODED (ZONE 600) · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles

RHW STA 1241 RH CENTER O/J PUMP CUTOUT FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-10-18355 REV A. NO DEFECTS NOTED</P>)

Part: SPAR — CRACKED (ZONE 500) · airframe 113,499 hrs · 20,012 cycles

LHW - UPPER WING T/E MOST I/B FIXED PNL SUPPORT P/N 65B11532-41 CRACK(<P>SUPPORT P/N 65B11532-41 REPLACED AS PER RI-57-20-18384 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: FITTING — CRACKED (ZONE 100) · airframe 113,499 hrs · 20,012 cycles

RH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA FOUND 1EA CRACK(<P>LONGERON EXTENSION FITTING REPLACED AS PER ATLAS AIR EO 4453A818 REV 20 PART 4. NO FURTHER DEFECTS NOTED</P>)

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 113,499 hrs · 20,012 cycles

NR 3 FUEL AFT BOOST PUMP FOUND CUTOUT DOUBLER CORROSION. DOUBLER FABRICATED AS PER BOEING DWG 65B19560 AND PL, NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)