N438UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
206 reports on file, 2001-12-11 – 2026-08-03.
Part: SPLICE PLATE — CORRODED (ZONE 300) · airframe 31,943 hrs · 20,896 cycles
UPON REMOVAL OF RT ELEVATOR TIP TRAILING EDGE WEDGE FOUND CORROSION ON UPPER SPLICE PLATE AND UPPER CONDUCTIVE FRAME. VERIFIED STEPS 4, 5 AND 6
Part: BEARING RACE — CORRODED (ZONE 700) · airframe 31,943 hrs · 20,896 cycles
LEFT MLG AFT TRUNNION BEARING RACE HAS PITTING CORROSION ON THE INSIDE.
Part: FLOOR PANEL — GOUGED (ZONE 200) · airframe 31,943 hrs · 20,896 cycles
ACCOMPLISH A PERMANENT REPAIR PER SREO-3220-REQ002 AFT CARGO FLOOR PANEL. CUT OUT DAMAGE ON PANEL 153AF AFT CARGO FLOOR PANEL CUT OUT DIMENSIONS LENGTH 2.9" WIDTH 1.6" WITH A .500" RADIUS REF SREO-3220-REQ002 REV 1. INSTALLED REPAIR DOUBLER ON AFT CARGO COMPT FLOOR PANEL REF SREO-3220-REQ002 REV 1 (APPX B) STEP 1 AND SRM 51-70-13-0G-0 REV 125.
Part: RETAINER — CRACKED (ZONE 100) · airframe 31,943 hrs · 20,896 cycles
LEFT MLG FWD TRUNNION FAIRING DOOR ASSY HAS A CRACKED SEAL RETAINER. LOCATED AND DRILLED NEW SEAL RETAINER AT LT MLG FWD TRUNNION FAIRING DOOR ASSY IAW SRM 51-40-05-0G-0.
Part: STRAP — CORRODED (ZONE 100) · airframe 31,943 hrs · 20,896 cycles
WHILE EVALUATING APU INLET SURROUND STRUCTURE FOUND CORROSION AT AFT STRAP STA 1825 BETWEEN S-3R TO S-6R. COMPLETED PER DOCUMENTS AND GMM RII 04-02
Part: CAM — GOUGED (DOOR LATCH) · airframe 31,943 hrs · 20,896 cycles
CREW ENTRY DOOR UPPER AND LOWER LATCH CAM HAS GOUGE DAMAGE VERIFIED STEP 11.
Part: STIFFENER — CORRODED (ZONE 200) · airframe 31,943 hrs · 20,896 cycles
MAIN CARGO AFT DECK PLATE LOWER SURFACE STIFFENER EXFOLIATED RH SIDE BS 1720,
Part: SPLICE PLATE — CORRODED (ZONE 600 ELEV) · airframe 31,943 hrs · 20,896 cycles
RIGHT ELEVATOR OTBD END SPLICE PLATE BETWEEN TIP AND CONDUCTIVE FRAME HAD CORROSION. OPEN
Part: ANGLE — CORRODED (ZONE 200) · airframe 31,943 hrs · 20,896 cycles
MAIN CABIN FLOOR DECK PLATE LOWER SURFACE NUTPLATE RETAINERS CORRODED THROUGHOUT LT & RT AND CENTER SECTION BS 1680 TO 1720.
Part: SUPPORT BRACKET — CRACKED (ZONE 400) · airframe 31,943 hrs · 20,896 cycles
NR 1 ENG COOLING AIR MANIFOLD INLET AT 9 OCLOCK POS. HAS A CRACKED SUPPORT BRACKET. INSTALLED NEW SERVICIABLE BRACKET KIT IAW SRM 51-40-02.
Part: SUPPORT BRACKET — NICKED (ZONE 300) · airframe 31,943 hrs · 20,896 cycles
HORZ STAB COMPT, STA. 1787.45 FWD FACE BILGE AREA SUPPORT BRACKET HAS NICK DAMAGE JUST ABOVE OF THE APU BLEED DUCT (059-09). REMOVED DAMAGED SUPPORT BRACKET AT HORZ STAB COMPT, STA. 1787.45 FWD FACE BILGE AREA PER 757-200PF-SRM 51-40-02-0G-0. INSTALLED SUPPORT BRACKET AT HORZ STAB COMPT, STA 1787.45 FWD FACE BILGE AREA I.A.W B757-200PF SRM 51-40-02-OG-0 AND DWG 212N3089.
Part: FITTING — CORRODED (ZONE 300) · airframe 31,943 hrs · 20,896 cycles
AFT HORIZONAL STAB STA. 1885 FWD FACE 311AL SERVICE DOOR TWO LATCH FITTINGS HAD EVIDENCE OF CORROSION. OUT OF LIMITS.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 31,943 hrs · 20,896 cycles
FWD CARGO COMP CEILING AT FWD UPPER CUTOUT MAIN CABIN FLOOR BEAM FRAME ANGLE IS CRACKED STR ATA 53-00 GM013 VERIFIED STEP 3.
Part: BONDING WIRE — CORRODED (ZONE 300) · airframe 31,943 hrs · 20,896 cycles
LEFT HORIZONTAL STAB REAR SPAR TO ELEVATOR FRONT SPAR BONDING WIRE AND ATTACH BRACKETS HAVE CORROSION AT OTBD SIDE OF OTBD HINGE. RL001 VERIFIED STEP 11
Part: SUPPORT BRACKET — CRACKED (ZONE 400) · airframe 31,943 hrs · 20,896 cycles
NR 1 ENG COOLING AIR MANIFOLD INLET AT 3 OCLOCK POS. HAS A CRACKED SUPPORT BRACKET. INSTALLED NEW SUPPORT BRACKET AT NR 1 ENGINE COOLING AIR MANIFOLD INLET AT 3 OCLOCK POSITION IAW SRM 51-40-02-0G-0 PAR. 4 AND 9. AND AMM 70-51-00-912-001-R00, PAR.2
Part: STRAP — CORRODED (ZONE 100) · airframe 31,943 hrs · 20,896 cycles
APU INLET SORROUND STRUCTURE FWD STRAP HAS CORROSION ,
Part: DUCT — LOOSE (ZONE 100) · airframe 31,811 hrs · 20,823 cycles
CABIN ALTITUDE WARNING CLIMBING THROUGH FL 225. AIR TURN BACK. SECURED LOOSE DUCT AND LOOSE SUPPORT RODS AT RH PACK PLENUM MAIN DUCT. REF IPC 21-51-15-01 ITEM 215 AND 203. WILL REQUIRE ACFT PRESSURIZATION CHECK WITH BOTH PACK OPERATING. ACCOMPLISHED SATISFACTORY ACFT PRESSURIZATION CHECK PER AMM 05-51-24.
Part: DUCT — LOOSE (ZONE 100) · airframe 31,807 hrs · 20,820 cycles
CABIN ALTITUDE WARNING CLIMBING THROUGH FL 225. AIR TURN BACK SECURED LOOSE DUCT AND LOOSE SUPPORT RODS AT RH PACK PLENUM MAIN DUCT. REF IPC 21-51-15-01 ITEM 215 AND 203. WILL REQUIRE ACFT PRESSURIZATION CHECK WITH BOTH PACK OPERATING.
Part: FUEL SYS — INOPERATIVE (ZONE 100) · airframe 31,807 hrs · 20,820 cycles
FUEL MIGRATION FL 350. TOP OF DESCENT 0.0. START DESCENT 300. IN DESCENT 600. ON LANDING 1600. AT PARKING 1400. NOTE! LEFT TANK TO CENTER. REMOVED AND REPLACED BOTH CENTER TANK REFUELING VALVES (VALVE, ASSY, FUEL CONTROL), 2 EACH DRAIN CHECK VALVES (VALVE PRESSURE FUEL DRAIN), AND LEFT DEFUEL VALVE (VALVE FUEL SHUTOFF) IAW AMM 28-21-02, 28-21-05, AND 28-26-01. OPS CHECK DUE LEAK CHECK ACCOMPLISHED ON REFUELING VALVES, NO LEAKS NOTED IAW AMM 28-21-02
Earlier reports · 2001–2025 · 187 reports
2025
Part: FUEL SYS — MALFUNCTIONED · airframe 31,301 hrs · 20,496 cycles
APPEARS TO BE MIGRATING FROM THE RIGHT TO LEFT TANK. STARTED WITH 7.2 IN LEFT TANK 7.5 IN RIGHT, 0.3 IN CENTER. AT TOP OF CLIMB LH TANK 5.8 RIGHT FUEL TANK AT 5.3 CENTER AT 0.5.
Part: FUEL SYS — OUT OF BALANCE (ZONE 500) · airframe 31,307 hrs · 20,502 cycles
APPEARS TO BE MIGRATING FROM THE RIGHT TO LEFT TANK. STARTED WITH 7.2 IN LEFT TANK 7.5 IN RIGHT, 0.3 IN CENTER. AT TOP OF CLIMB LH TANK 5.8 RIGHT FUEL TANK AT 5.3 CENTER AT 0.5. SEE LOG PG PICTURE. INSTALLED L/H AFT X FEED VALVE ACTUATOR IAW AMM TASK 28-22-12-404-288. ACCOMPLISHED TEST OF THE FORWARD AND AFT ENGINE FUEL CROSSFEED VALVES OPERATION REF AMM TASK 28-22-02-714-055 ALL INDICATIONS NORMAL
Part: FUEL SYS — OUT OF BALANCE (ZONE 100) · airframe 31,297 hrs · 20,491 cycles
IN FLIGHT RIGHT FUEL TANK WENT 3000 LBS LESS THAN LEFT. INITIALLY WHEN BALANCED RIGHT TANK DROPPED 500 LBS IN TEN MINS THEN 1200 IN 30 MINS. LANDED WITH 3800 LBS LESS IN RIGHT TANK.
Part: FUEL TANK — OUT OF BALANCE (ZONE 600) · airframe 31,298 hrs · 20,492 cycles
IN FLIGHT RIGHT FUEL TANK WENT 3000 LBS LESS THAN LEFT. INITIALLY WHEN BALANCED RIGHT TANK DROPPED 500 LBS IN TEN MINS THEN 1200 IN 30 MINS. LANDED WITH 3800 LBS LESS IN RIGHT TANK. REMOVED AND REPLACED LEFT WING FUELING SHUTOFF VALVE I.A.W. UPS B757 AMM 28-21-02-004-017 AND AMM 28-21-02-404-019 THROUGH STEP H-24 MINUS STEP H-23.REMOVED AND REPLACED RIGHT WING DEFUEL VALVE I.A.W. UPS B757 AMM 28-26-01-004-144 AND AMM 28-26-01-404-145 THROUGH STEP E-10. PERFORMED OPS/LEAK CHECK OF REFUEL/DEFUEL VALVES. OPS CHECK GOOD.
Part: FUEL SYS — OUT OF BALANCE · airframe 31,298 hrs · 20,492 cycles
FUEL CONFIG MESSAGE IN CRUISE. RIGHT TANK 2000LBS LESS THAN LEFT. RAN QRH REBALANCING L&R. AFTER REBALANCING, ON DECENT 12.8 AS RH TANK WAS 1000 LESS THAN LEFT TANK.
Part: FUEL — OUT OF BALANCE · airframe 31,300 hrs · 20,495 cycles
FUEL CONFIG MESSAGE IN CRUISE. RIGHT TANK 2000LBS LESS THAN LEFT. RAN QRH REBALANCING L&R. AFTER REBALANCING, ON DECENT 12.8 AS RH TANK WAS 1000 LESS THAN LEFT TANK. PERFORMED OPS CHECK OF LH AND RH DEFUEL VALVES IAW AMM 28-26-01-404-145. OPS CHECK GOOD.
Part: STRINGER — PUNCTURED (ZONE 100) · airframe 30,787 hrs · 20,165 cycles
**SDR FILED OPEN** AIRCRAFT FUSELAGE PUNCTURED APPROXIMATELY 9FT AFT OF LOWER AFT CARGO DOOR MATERIAL IDENTIFICATION: DOUBLER P/N 2024T3 .063", PO# SP2772414, SNR LOT# 5696144. FILLER P/N 2024T39 .056", PO# SP1818420, SNR LOT# 5995. STRINGER SPLICE P/N BAC1498-203, PO# SP2283532, SN 668328A.
2024
Part: FUEL SYS — OUT OF BALANCE (ZONE 100) · airframe 30,536 hrs · 20,024 cycles
WE DEP DTW WITH 10.1 IN L AND 10.2 IN R TANK 1 HOUR INTO THE FLIGHT WE HAVE A 1000LBS DIFF BETWEEN TANKS 7.1 IN L AND 6.0 IN R. @ THE GATE AFTER BLOCK IN L 6.2 R 4.6 FUEL IMBALANCE AFTER 1:26 MIN IN A REMOVED AND REPLACED RIGHT DEFUEL VAVLE IAW UPS B757 AMM 28-26-01-401. OPS CHECK GOOD IAW UPS B757 AMM 28-26-01-790-801. REMOVED AND REPLACED L/W MAIN TANK FUEL SHUTOFF VALE IAW UPS B757 AMM 28-21-02-401. OPS CHECK GOOD. VALVE LEAK CHECK GOOD.
Part: FUEL SYS — OUT OF BALANCE (ZONE 100) · airframe 30,534 hrs · 20,022 cycles
WE DEP DTW WITH 10.1 IN L AND 10.2 IN R TANK 1 HOUR INTO THE FLIGHT WE HAVE A 1000LBS DIFF BETWEEN TANKS 7.1 IN L AND 6.0 IN R. @ THE GATE AFTER BLOCK IN L 6.2 R 4.6 FUEL IMBALANCE AFTER 1:26 MIN IN A FUEL IMBALANCE WITHIN AMM 28-21-00-702-001 LIMITS BASED ON BLOCK TO BLOCK TIME OF 1115Z OUT AND 1255Z IN. NO EXTERNAL LEAKS NOTED.<BR>DEFERRED PER AMM 28-21-00-702-001 FOR MAXIMUM OF FOUR FLIGHTS. OPEN
Part: SWITCH — FAILED (EVAS UNIT) · airframe 30,057 hrs · 19,731 cycles
CAPT`S EVAS UNIT BLOWER WILL NOT STOP ( SWITCH FAILED) C/W DMP 25-60-01 BY REMOVING CAPTS EVAS UNIT IAW AMM 25-69-00-401
Part: EVAS UNIT — INOPERATIVE (COKCPIT) · airframe 30,059 hrs · 19,733 cycles
CAPTS EVAS UNIT BLOWER WILL NOT STOP ( SWITCH FAILED) INSTALLED NEW CAPTAINS EVAS IAW 757 AMM 25-69-00. OPS GOOD, THIS CLEARS DEFERRAL.
2023
Part: UNKNOWN — UNKNOWN (NOT REPORTED) · airframe 29,735 hrs · 19,548 cycles
SUSPECTED FUEL LEAK ON R/H MAIN TANK/ENGINE! IT BEGAN AT APPROX 10,000 TO 6000 FT. SUSPECT RH DEFUEL VALVE LEAKING. REMOVED AND REPLACED RH DEFUEL VALVE ACTUATOR IAW AMM 28-26-02, OPS CHECK GOOD.
Part: FUEL TANK — LEAKING (RIGHT) · airframe 29,775 hrs · 19,566 cycles
SUSPECTED FUEL LEAK ON R/H MAIN TANK/ENGINE! IT BEGAN AT APPROX 10,000 TO 6000 FT. SUSPECT RH DEFUEL VALVE LEAKING. REMOVED AND REPLACED RH DEFUEL VALVE ACTUATOR IAW AMM 28-26-02, OPS CHECK GOOD.
Part: SKIN PANEL — DAMAGED (STA 384-440 LH) · airframe 29,337 hrs · 19,279 cycles
INSPECTION TYPE:DI*MAJOR REPAIR* MULTIPLE DENTS AND DAMAGE AT STA 382-440 STR 16L-22LREPAIRED FUSELAGE SKIN STA 382-440 STR 16L-22L PER UPS EO B757-5330-86623-A AND VTMAE EA 757-5310-27-A3198 REV-
Part: STRINGER — DAMAGED (STA 404-440 20L) · airframe 29,337 hrs · 19,279 cycles
INSPECTION TYPE:SPVINCOMING DAMAGE TO STRINGER 20L STA 404-440REMOVED, FABRICATED AND INSTALLED STRINGER IAW SRM 51-40-02
Part: STRINGER CLIP — BROKEN (STA 418 18L) · airframe 29,337 hrs · 19,279 cycles
INSPECTION TYPE:SPVSTRINGER CLIP AT 18L STA 418 LOWER LEG BROKENREMOVED, FABRICATED AND INSTALLED STRINGER CLIP IAW SRM 51-40-02
Part: STRINGER — DAMAGED (STA 418-440 18L) · airframe 29,337 hrs · 19,279 cycles
INSPECTION TYPE:SPVINCOMING DAMAGE TO STRINGER 18 L STA 418-440REMOVED, FABRICATED AND INSTALLED STRINGER IAW SRM 51-40-02
Part: SKIN PANEL — DAMAGED (STA340-355STR11-) · airframe 29,337 hrs · 19,279 cycles
INSPECTION TYPE:SV*MAJOR REPAIR* SKIN DAMAGE STA 340 TO 355 BETWEEN STR 11L AND 12LREPAIRED PER VTMAE EA 757-5310-27-A3202 AND UPS EO B757-5330-86624-A
2022
Part: SHEAR WEB — CORRODED (FS 275 LBL 40) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:SEG3MAIN CABIN FLOOR SHEAR WEB AT FS 275 HAS SURFACE CORROSIONREMOVED CORROSION FOUND SHEAR WEB TO BE WITHIN LIMITS PER SRM 53-10-51-1A-1
Part: STRINGER — DENTED (FR1500 26RH) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:SEG1AFT LOWER CARGO PIT AT FRAME 1500 RH SIDE AT STRINGER 26R HAS A DENT ON THE UPPER FLANGE OF FRAMEREPAIRED FRAME PER RCD AND SRM 53-00-07-2R-5 DETAIL I
Part: FLOOR PANEL — NONE (MCD FLOOR) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:CMCD FLOOR PANEL 232XHF IS DELAMINATINGFABRICATED FLOOR PANEL 232XHF FROM 5024N4000001SS-G BAT: 0003855547 PER SREO B757-5320-9692-K
Part: PANEL — CORRODED (FS455 RBL30) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:CAFT CARGO PIT DOOR SILL AT FS 1455 RBL 30 HAS EXFOLIATION CORROSIONREMOVED SIDE PANEL AND ISNTALLED REPLACEMENT 146N5391-2 SIDE PANEL PER SRM 51-40-02
Part: DOUBLER — CORRODED (#2 PYLON I/B) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:C17#2 ENGINE STRUT OB SKIN I/B SIDE AT NAC 149 TO NAC 156 HAS CORROSIONREPAIRED PYLON SKIN PER EA# 757-5450-27-A2955
Part: PANEL — CORRODED (FS 1445) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:CAFT LOWER CARGO PIT AT FS 1445 RH SIDE TRANSITION PANEL HAS EXFOLIATION ON FWD RH ENDSPLICED A REPAIR SIDE PANEL SEGMENT PER SRM 51-70-11-0G
Part: SKIN — CRACKED (FS 1956.7) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:SEG1AFT APU RH DOOR AFT LATCH AT FS 1956.7 ON SKIN P/N 148N6660-6 HAD A .216" LONG CRACK IN LOWER HOLE CUT OUTREPAIRED SKIN PER EO # 757-5240-27-A2954
Part: DOUBLER — CORRODED (#2 PYLON I/B) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:C17#2 ENGINE STRUT IB SKIN I/B SIDE AT NAC 153 TO NAC 174 HAS CORROSIONREPAIRED PYLON SKIN PER EA# 757-5450-27-A2952
Part: DOUBLER — CORRODED (#1 PYLON I/B) · airframe 28,542 hrs · 18,803 cycles
INSPECTION TYPE:C17#1 ENGINE STRUT OB SKIN I/B SIDE AT NAC 153 TO NAC 157 HAS CORROSIONREPAIRED PYLON SKIN PER EA# 757-5450-27-A2951
2020
Part: BRACKET — BROKEN (ENTRY DOOR) · airframe 26,194 hrs · 17,355 cycles
MAIN ENTRY DOOR TARGET HAS BROKEN BRACKET. PERFORMED INTERM REPAIR AS PER EO 757-5210-76804-A CAP AND STOWED ILLEG AS REQ. REPLACED L1 ENTRY DOOR PROXIMITY SENSOR SUPPORT BRACKET IAW SRM 51-40-02.
Part: SENSOR — DIRTY (ENTRY DOOR) · airframe 26,069 hrs · 17,294 cycles
INSPECTION TYPE:NAON SHORT FINAL RECEIVED "L FWD ENTRY DOOR: ON EICAS. DOOR REMAINED CLOSED AND LATCH REMAINED IN PROPER POSITION AFTER BLOCK INNO HISTORY NOTED PERFORMED CREW ENTRY DOOR OPS CHK GOOD I/A/W AMM 52-12-00-001, CLEANED SENSOR. OK FOR SVC
Part: SENSOR — OUT OF ADJUST (L1 DOOR) · airframe 25,736 hrs · 17,076 cycles
INSPECTION TYPE:N/ARECEIVED MOMENTARY EICAS ON LANDING ''L FWD ENT DOOR''ADJUSTED DOOR WARNING SENSOR IAW FIM 52-74-00-815-802 & AMM 52-71-00
2019
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 24,893 hrs · 16,519 cycles
INSPECTION TYPE:SDR EMERGENCY LIGHT HAS THREE INOP BULBS. INSTALLED THREE BULBS IN EMERGENCY LIGHT PER AMM 33-51-01.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 24,833 hrs · 16,479 cycles
LEFT I/B MAIN FLAP LWR SKIN DENT AND DISBOND REPAIR. LINKED TO D-663694REPAIRED IAW E.O. B757-5750-71256-D
2018
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,018 hrs · 15,959 cycles
EMERGENCY LIGHT HAD THREE BULBS INOPERATIVE. REPLACED THE BULBS IAW AMM 33-51-01-2.
2017
Part: LINKAGE — BROKEN (MLG DOOR) · airframe 23,498 hrs · 15,634 cycles
INSPECTION TYPE:N/AAFTER TAKEOFF ON GEAR RETRACTION GOT GEAR DOORS EICAS MSG AND GEAR DOOR LIGHTFOUND LINKAGE FOR GEAR OPERATED SEQUENCE VALVE BROKEN.REPLACED LINKAGE WITH REF TO 757 AMM 32-34-07-404-010 OPERATIONAL CHECK GOOD.
Part: LINKAGE — BROKEN (MLG DOOR) · airframe 23,496 hrs · 15,631 cycles
INSPECTION TYPE:N/AAFTER TAKEOFF ON GEAR RETRACT HOT GEAR DOORS EICAS MESSAGE AND GEAR DOOR LIGHTFOUND LINKAGE FOR GEAR OPERATED SEQUENCE VALVE BROKEN. REPLACED LINKAGE WITH REF TO 757 AMM 32-34-07-404-010. OPS CHECKS GOOD.
Part: LINKAGE — BROKEN (MLG DOORS) · airframe 23,496 hrs · 15,631 cycles
INSPECTION TYPE:N/AATB - AFTER DEPARTURE THE NOSE GEAR DOORS DID NOT CLOSE. THE CREW PERFORMED AN ATB TO RFD. EMERGENCY DECLARED. FOUND LINKAGE FOR GEAR OPERATED SEQ VLV BROKEN. REPLACED LINKAGE WITH REF TO AMM 32-34-07-404-010; OPS CK GOOD.
2016
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 22,389 hrs · 14,887 cycles
INSPECTION TYPE: SEG4, MCD FLOOR PANEL 241XGF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 22,389 hrs · 14,887 cycles
INSPECTION TYPE: SEG4, MCD FLOOR PANEL 242XGF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: SKIN — CORRODED (BS 1401) · airframe 22,040 hrs · 14,627 cycles
FUSELAGE SKIN CORROSION BS 1401, STR 30, APPLIED DOUBLER. REPAIRED IAW EO B757-5330-60001.
2015
Part: BULKHEAD WEB — DAMAGED · airframe 21,750 hrs · 14,439 cycles
INSPECTION TYPE:SV, DENT BEHIND RADOME ON FWD BULKHEAD AT APPROX 3:30 POS DENT .275 5.2" X 4.3. REQUIRE HI FREQUENCY HFEC AREA, NO CRACKS NOTED IAW REF NDTM PART 6-51-00-19. C/W EO B757-5310-58824A. DEFERRED DAMAGE TO FWD PRESS BULKHEAD. MUST FLY. INSTALLED PERM REPAIR IAW REF G19217, REV B. DEFERRAL CLOSED.
Part: FLOORBEAM — CORRODED (BS 1020) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, UPPER LOBE INTERIORS BS 1020, LBL 24.75 FLOORBEAM TEE ANGLE CORRODED. REMOVED CORROSION BETWEEN BL 0 - LBL 24.75 IAW SRM 51-10-02-0G. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A-1, FIG 101, DETAIL III USING TR. 17-809 3. REMOVED DAMAGE FLOORBEAM ANGLE IAW SRM 51-40-02-0G. FABRICATED NEW FLOORBEAM TEE ANGLE.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 232XAF DAMAGED HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 231XRF HAS EDGE DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — BROKEN (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 232XSF IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 232XVF HAS DAMAGED HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 232XGF CRACKED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 232XQF DAMAGED HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 231XDF DETERIORATED HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 232XDF DENTED AT THE EDGE AND MISSING HONEY COMB. FABRICATED A NEW FLOOR PANEL IAW SREO 5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 232XEF DENTED AND SCRATCHED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 232XCF DETERIORATED HONEYCOMB AT EDGE 143-491. FABBED PANEL 232XCF, PN 143N5457-82 FROM A402H-48X144, BATCH 2613192 IAW SERO 5320-9692-H. 2. STEP OUT REQUIRED IAW SREO 5320-9692-H3. SCUFF SAND AROUND THE STEP CUT AREA IAW SREO B757-5320-9692-H4. CLEAN THE AREA IAW SREO B757-5320-9692-H5 OK TO BOND. ACCOMPLISHED SDR IAW GMM 03.16.01.01
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 231XPF HAS DETERIORATED HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP 11, MAIN DECK FLOOR PANEL 232XBF MISSING HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 221XCF DENTED AND TOOL DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 222XCF HAS DETERIORATED HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO 5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 231XTF DETERIORATED HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 231XKF MISSING HONEYCOMB AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 232XRF DETERIORATED HONEYCOMB. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 232XTF WITH TOOL DAMAGE. FABRICATED FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DENTED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOOR PANEL 221XBF DENTED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 232XNF MISSING, AND DAMAGED HONEYCOMB. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 231XBF DETERIORATED AT THE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 231XMF WITH DENT & TOOL DAMAGE. FABRICATED A NEW FLOOR PANEL IAW REO B757-5320-9692-H.
Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, FLOOR PANEL 232XFF IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DENTED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, FLOOR PANEL 232XWF HAS A DENT AT THE CORNER. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE:CP11, FLOOR PANEL 231XWF MISSING AN INSERT. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H .
Part: FLOOR PANEL — DENTED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, FLOOR PANEL 231XYF HAS DENT. FABRICATEDED A NEW FLOOR PANEL IAW SREO 5320-9692-W.
Part: FLOOR PANEL — DENTED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE:CP11, FLOOR PANEL 232XXF HAS A DENT. FABRICATED A NEW FLOOR PANEL IAW SREO 5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, FLOOR PANEL 232XYF HAS DAMAGE INSERT. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: CMCD, FLOOR PANEL 231XAF HAS SEVERAL DENTS AND HONEYCOMB MATERIAL MISSING AT FWD AND AFT EDGES. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
FLOOR PANEL 231XNF, HONEYCOMB MATERIAL IS RIPPED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: CMCD, FLOOR PANEL 231XLF DAMAGE TO THE HONEYCOMB ON ONE EDGE. FABRICATED A NEW FLOOR PANEL IAW SREO 5320-9692-H.
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE:CP11, MCD FLOOR PANEL 231XFF RT SIDE EDGE IS DELAMINATED THE ENTIRE LENGTH OF THE PANEL. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: CMCD, FLOOR PANEL 231XSF HONEYCOMB IS DAMAGED AT SEVERAL SPOTS AROUND THE EDGES. FABRICATED A NEW FLOOR PANELIAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MCD FLOOR PANEL 231XMF BOTTOM HONEYCOMB PROTECTIVE LAYER IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H2.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE:CMCD, FLOOR PANEL 232XUF HAS DAMAGED HONEYCOMB. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOORBOARD 242XMF DAMAGED ON UNDERNEATH SIDE. FABRICATED FLOORBOARD IAW SREO 5320-9692-H.
Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOORBOARD 252XEF HAS PUNCTURE. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H.
Part: FLOORBOARD — PUNCTURED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOORBOARD 241XGF PUNCTURED. FABRICATED A NEW FLOORBOARD IAW SREO 5320-9692-H.
Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 241XKF DAMAGED AT INSERT. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOOR PANEL 242XAF DELAMINATED IN CORNER. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-H.
Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP11, MAIN DECK FLOORBOARD 252XUF DAMAGED IN CORNER 122-0141. FABRICATED A NEW FLOORBOARD IAW SREO B757-5320-9692-H, PN 146N5361-45.
Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 21,346 hrs · 14,171 cycles
INSPECTION TYPE: C, MAIN DECK FLOORBOARD 241XMF DAMAGED. FABRICATED A NEW FLOORBOARD IAW SREO 5320-9692-H.
Part: FLOOR PANEL — DELAMINATED (MAIN DECK) · airframe 213,468 hrs · 14,171 cycles
INSPECTION TYPE: CP 11, PANEL RACK MAIN DECK FLOOR PANEL 251XQF HAS A AREA OF DELAMINATION AT PREVIOUS. FABBED PANEL 251XQF, PN 146N5361-15 FROM A402H-48X144 IAW SREO B757-5320-9692-H2. STEP B2 OF SREO B757-5320-9692-H REQUIRED. SCUFF SAND AROUND THE STEP CUT AREA IAW SREO B757-5320-9692-H. CLEAN THE AREA IAW SREO B757-5320-9692-H. OK TO BOND. ACCOMPLISHED SDR IAW GMM 03.16.01.01.
2014
Part: TRANSMITTER — FAILED (HYD PRESSURE)
RT HYD SYS EICAS MESSAGE DURING DESCENT. EMERGENCY DECLARED, RAN QRH PROCEDURE. NO OTHER PROBLEMS NOTED. RT HYD QTY STAYED AT .94. DIDN'T OBSERVE ANY OVERHEAD HYD PRESSURE LIGHTS. HYD MAINT PAGE SHOWS RT HYD SYS PRESSURE AUTO EVENT. CREW REPORTED NO OTHER INDICATIONS OF RT HYDRAULIC PRESSURE LOSS AND RT HYD SYS PRESSURE OK AFTER BLOCK IN. R & R RT HYD SYS PRESSURE TRANSMITTER IAW FIM 29-11-00, AMM 29-31-01-401.
Part: GUARD — BROKEN (EMERGENCY LIGHT)
EMERGENCY EXIT LIGHT SWITCH, A PIECE OF PLASTIC PART OF THE SPRING FELL OUT WHILE TURNING IT OFF. REPLACED SWITCH GUARD. OPS CHECKED NORMAL.
2013
Part: SKIN — DENTED (NR 6 SLAT) · airframe 20,223 hrs · 13,347 cycles
INSPECTION TYPE:C10, RT WING NR 6 SLAT UPPER AREA COMPOSITE DENTED. FABRICATED AND INSTALLED A REPAIR IAW SRM 57-41-02-2R-1, MAJOR REPAIR.
Part: SKIN — DAMAGED (NR 6 SLAT) · airframe 20,223 hrs · 13,347 cycles
INSPECTION TYPE:C10, RT WING NR 6 SLAT WEDGE UPPER SURFACE 19" FROM OTBD EDGE. FABRICATED AND INSTALLED A REPAIR IAW SRM 57-43-02-2R-1, MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 1055) · airframe 20,223 hrs · 13,347 cycles
INSPECTION TYPE: C10, MAIN CABIN UNDER FLOORBEAM TEE CORRODED BS 1055, RBL 0-25, CORRODED OUT OF LIMITS. R & R FLOORBEAM TEE IAW DWG 144N5005.
Part: FLOORBEAM — CORRODED (BS 1040 RBL 0-25) · airframe 20,223 hrs · 13,347 cycles
INSPECTION TYPE: C10, MAIN CABIN UNDER FLOORBEAM CORRODED BS 1040, RBL 0-25 CORRODED OUT OF LIMITS. R & R TEE IAW DWG 144N5005. MINOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 1055) · airframe 20,223 hrs · 13,347 cycles
INSPECTION TYPE:C10, MAIN CABIN UNDER FLOORBEAM TEE CORRODED BS 1055, RBL 25- RBL-50 CORROSION OUT OF LIMITS. R & R FLOORBEAM TEE IAW BAC DWG 144N5005, MINOR REPAIR.
2012
Part: WEDGE — DENTED (NR 4 SLAT)
NR 4 SLAT T/E WEDGE DENTED AND DEBONDED. REPAIRED REF EOB757-5750-48728-B.
Part: WINDOW — BINDING (L2)
CAPTAIN`S L2 SLIDING WINDOW LOCK IS BINDING BADLY AFTER PRESSURIZING THE ACFT. ADJUSTED NR 2 WINDOW IAW AMM 56-11-02-5. OPS CHECKED NORMAL.
2011
Part: SKIN — DAMAGED (BS 263 S20R)
CONVERT LIGHTNING STRIKE TEMP REPAIR AT FS 263 S-20R TO PERM ACCOMPLISH REPAIR IAW APP A, PREPAIRED IAW EO B757-5330-34712-B.
Part: SKIN — DAMAGED (BS 231 S20R)
DAMAGE TO FUSELAGE STA 231 BELOW STR 20R. REPAIRED IAW EO B757-5330-34712-B.
Part: SKIN — DAMAGED (BS 247 S20R)
CONVERT LIGHTNING STRIKE TEMP REPAIR AT FS 247 BELOW S20R TO PERM ACCOMPLISH PERM REPAIR IAW APP A. REPAIRED IAW EO B757-5330-34705B.
Part: SKIN — DAMAGED (BS 231 S20R)
SKIN DAMAGED STA 231 BELOW S20R. REPAIRED REF EOB757-5330-34704-B.
Part: SKIN — DAMAGED (BS 418 S23R)
LIGHTNING STRIKE REPAIR AT STA 418 JUST BELOW STR 23 RT. REPLACE TEMP FASTENERS IN REPAIR WITH SOLIDS IAW EO B757-5330-34715-B.
Part: BRACKET — CRACKED (NR 1 NACELLE) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR1 PYLON UPPER AFT INBD BRACKET ASSY IS CRACKED IN RADIUS, PPS 187, RBL 10, PN 312N5817-36. REPLACED BRACKET IAW SRM 51-40-02-0G.
Part: SUPPORT BRACKET — CRACKED (BS 520) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, CRACKED CEILING SUPPORT BRACKET BS 520, BL 0, WL 202, IN FWD CARGO BAY. R & R BRACKET IAW SRM.
Part: ACCESS PANEL — DAMAGED (NR 2 PANEL) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR 2 PYLON UNDERWING FAIRING STRUCTURE, OTBD AFT ACCESS PANEL NR 443ER HAS A DAMAGED FASTENER HOLE, LOCATED AT THE FWD LWR CORNER P/N 313N5004-4. FABRICATED NEW ACCESS PANEL NR 443ER IAW SRM 51-40-05-0G, SRM 51-40-08-0G, DWG 313N5004, AMM 51-21-10-7 AND AMM 51-21-04-7.
Part: SILL — DAMAGED (BS 297-321) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FWD ENTRY DOOR SILL WEB ASSY HAS SEVERAL SCREW STRIKES AT BS 297-321. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB, IAW SRM 53-10-15-1A.
Part: FLOOR PANEL — DAMAGED (BS 1320-1420) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, MAIN CARGO FLOOR PANEL MISSING INSERTS BS 1320-1420, LBL 25-45. FABRICATED NEW BOARD IAW EO 757-5320-9692-G.
Part: FLOOR PANEL — DELAMINATED (BS 338-440) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL BS 338-440 RBL 25 IS DELAMINATED AND HAS MISSING INSERTS. REPAIRED IAW EO B757-5320-9692-G, DATED: 04/15/2009.
Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD NR1 PYLON AFT FAIRING STRUCTURE INBD AND OTBD NUT PLATE. SUPPORT BRACKETS ABOVE DRAIN LINES ARE CRACKED. R & R INBD AND OTBD SUPPORT BRACKETS IAW SRM 51-40-02-0G.
Part: SUPPORT BRACKET — CRACKED (NR 2 NACELLE) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR2 PYLON AFT FAIRING STRUCTURE INBD AND OTBD NUTPLATE SUPPORT BRACKETS ABOVE DRAIN LINES ARE CRACKED AND WORN. R & R BOTH INBD AND OTBD NUTPLATE SUPPORT BRACKETS IAW SRM 51-40-02-0G.
Part: FLOOR PANEL — DELAMINATED (BS 333-440) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOOR PANEL, BS 333-440 LBL 25, HAS DELAMINATION ON LOWER SURFACE AND A MISSING INSERT. REPAIRED IAW EO B757-5320-9692-G, DATED 04/15/2009.
Part: FLOORBOARD — DAMAGED (BS 560-620) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, MAIN CARGO FLOORBOARD. BS 560-620, LBL 45-65 HAS MISSING INSERT. REPLACED FLOORBOARD ASSY IAW EO B757-5320-9692-G, SRM 53-00-50-1A1.
Part: FITTING — GOUGED (NR 1 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR 1 PYLON INBD MID SPAR FITTING ON ACFT INBD AND OTBD SURFACE AROUND THE BUSHING ARE WORN AND GOUGED. REPAIRED FITTING IAW EO B757-5440-41606-A AND ER 11-01495.
Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR1 PYLON AFT FAIRING STRUCTURE LOWER T/E SKIN PANEL IS CRACKED ABOVE DRAIN LINES. R & R SKIN PANEL IAW SRM 51-40-02-0G.
Part: SKIN — CHAFED (LT WING) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, LT WING LOWER SKIN IS CHAFED AT FSS 295, FROM 2-14 INCHES AFT OF THE SKIN L/E. REPAIRED IAW SRM 57-20-01-1A1, ATS ER 11-01575, DATED 23, FEB 2011, EO B757-5730-41559-A DATED 23, FEB 2011.
Part: SUPPORT — WORN (NR 2 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR 2 PYLON AFT FAIRING STRUCTURE FWD INBD UPPER NUT PLATE SUPPORT WORN AROUND LOWER NUT PLATE. FABRICATED NEW FWD INBD UPPER NUT PLATE SUPPORT IAW SRM 54-50-71-1A1, SRM 51-30-01-0G, SRM 51-40-05-0G, AMM 51-21-11-7, AMM 51-21-10-7.
Part: SKIN PANEL — CRACKED (NR 2 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE: MOD, NR2 PYLON AFT FAIRING STRUCTURE LOWER AFT CLOSE-OUT SKIN CRACKED ABOVE DRAIN LINE. R & R LOWER AFT CLOSE-OUT SKIN IAW SRM 51-40-02-0G.
Part: FAIRING — GOUGED (NR 1 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR1 PYLON AFT FAIRING STRUCTURE FWD INBD UPPER NUTPLATE SUPPORT IS WORN AROUND NUTPLATES. REMOVED, FABRICATED, AND INSTALLED IAW DWG NR313N5033, AND SRM 51-40-02.
Part: FITTING — CORRODED (NR 1 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR 1 PYLON MID SPAR FITTING ON THE ACFT INBD SURFACE AROUND THE BUSHING IS PITTED AND WORN. REPAIRED FITTING IAW EO B757-5440-41606-A, DATED 24 FEB 2011 AND ATS ER 11-01495, DATED 23 FEB 11.
Part: SKIN — CHAFED (RT WING) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, RT WING LOWER SKIN AT FSS 295 IS CHAFED FROM 7-14 INCHES AFT OF THE SKIN L/E. REPAIRED IAW SRM 57-20-01-1A1, EO B757-5730-41559-A, DATED 23 FEB 2011, AND ATS ER 11-01575 DATED 23 FEB, 2011.
Part: SUPPORT — WORN (NR 2 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR 2 PYLON AFT FAIRING STRUCTURE FWD OTBD UPPER NUTPLATE SUPPORT WORN AROUND NUTPLATES. REMOVED, FABRICATED AND INSTALLED NEW NUTPLATE SUPPORT IAW SRM 54-50-70-1A1, SRM 51-40-02-0G, SRM 51-40-05-0G, AMM 51-21-10-7, AMM 51-21-11-7.
Part: FLOORBOARD — DAMAGED (BS 879-900) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOORBOARD AT STA 879 TO 900 RBL 45-60, DAMAGED AT FWD END. R & R FLOORBOARD IAW EO 757-5320-9692G.
Part: FLOORBEAM — CORRODED (BS 900) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOORBOARD SUPPORT AT STA 900, RBL 0-25, IS CORRODED. R & R IAW SRM 51-40-02 AND DWG PL 144N5005.
Part: FLOORBEAM — CORRODED (BS 324) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C, CORROSION ON T-CHORD INBD FLANGE AT BS 324, LBL 60, WL 208. REPAIRED CHORD IAW EO 757-5310-41500-A AND ER 11-01476.
Part: FLOORBEAM — DAMAGED (BS 900) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOORBEAM STA 900, RBL 25-45 HAS MECH DAMAGE. R & R FLOORBEAM IAW SRM.
Part: FLOORBOARD — DAMAGED (BS 480-560) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOORBOARD DAMAGED MID OTBD SIDE BS 480 TO 560, LBL 25-45. FABRICATED REPLACEMENT FLOORBOARD IAW EO NR B757-5320-9692.
Part: FLOORBEAM — CORRODED (BS 1681) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, CORROSION ON BS 1681 FLOORBEAM, LBL 40 ON THE UNDERSIDE OF THE J FLANGE. REPAIRED IAW ATS ER 11-01477, DATED 2/24/11.
Part: FLOORBOARD — DAMAGED (BS 720-820) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOORBOARD AT STA 720-820, LBL 45-60, DAMAGE AT AFT END STA 800 MARKED. REPLACED FLOOR PANEL IAW SRM 53-00-50-1A1, TABLE I AND EO B757-5320-9692-G.
Part: SHEAR WEB — CORRODED (BS 440-660) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, SEVERAL AREAS OF CORROSION ON SHEAR WEB (MARKED) AT BS 440-BS 660, LBL 45-LBL 60, WL 208. REPAIRED IAW SRM 51-10-02-0G, SRM 53-30-15-0I1, SRM 51-40-02-0G, ATS ER NO 11-01491 DATED 2/24/2011, AND EO B757-5310-41615-A, DATED 02/24/11.
Part: INTERCOSTAL — CRACKED (BS 857) · airframe 18,978 hrs · 12,461 cycles
INSP TYPE:C1, INTERCOSTAL CRACKED AT BS 857, LBL 16, WL 208. FABRICATED INTERCOSTAL AND INSTALLED IAW SRM 51-40-05-0G.
Part: FLOORBEAM — GOUGED (BS 900) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOORBOARD SUPPORT AT STA 900, LBL 25-45, HAS MECHANICAL DAMAGE. R & R IAW SRM 51-40-02 AND DWG PL 144N5005.
Part: FLOORBOARD — DAMAGED (BS 440-480) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FLOORBOARD AT STA 440 TO 480 LBL 45-60, DAMAGE FWD END OTBD SIDE MARKED. REPLACED FLOORBOARD IAW EO B757-5320-9692-9 AND SRM 53-00-50-2R1, SRM 53-00-50-1A1.
Part: FLOORBOARD — DAMAGED (BS 900-1120) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FOUND FLOORBOARD AT STA 900-1120, RBL 25-45, FWD CORNER DAMAGED (MARKED). R & R WITH FABRICATED NEW FLOORBOARD IAW SRM 53-00-50-1A, AND EO B757-5320-9692-G.
Part: FLOORBOARD — DAMAGED (BS 1100-1200) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FOUND FLOORBOARD STA 1100 TO 1200, BL0 TO RBL 25, FWD END AND OTBD AFT END DAMAGED AND MARKED. REPLACED FLOORBOARD IAW EO B757-5320-9692-G, SRM 53-00-50-1A1.
Part: FLOORBOARD — DAMAGED (BS 900-1020) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FOUND FLOORBOARD AT STA 900-1020, LBL 45-60, OTBD SIDE DAMAGED (MARKED). R & R WITH FABRICATED NEW FLOORBOARD IAW SRM 53-00-50-1A, AND EO B757-5820-9692-G.
Part: FLOORBOARD — DAMAGED (BS 900-1020) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FOUND FLOORBOARD AT STA 900-1020, BL 0- LBL 25, FWD CORNER DAMAGED (MARKED). R & R WITH FABRICATED NEW FLOORBOARD IAW SRM 53-00-50-1A, AND EO B757-5320-9692-G.
Part: FLOORBOARD — DAMAGED (BS 1020-1055) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FOUND FLOORBOARD AT STA 1020-1055, RBL 45-60, AFT END DAMAGED (MARKED). R & R WITH FABRICATED NEW FLOORBOARD ANEL IAW SRM 53-00-50-1A, AND EO B757-5320-9692-G.
Part: FLOORBOARD — DAMAGED (BS 1540-1600) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, MISSING INSERT IN FLOORBOARD AT STA 1590, RBL44. REPLACED MCB FLOORBOARD AT BS 1540-1600, RBL 44, IAW EO B757-5320-96 92-G.
Part: FLOORBOARD — DAMAGED (BS 1100-1200) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FOUND FLOORBOARD STA 1100 TO 1200, RBL 25 TO 45, FWD AND AFT ENDS DAMAGED AND MARKED. REPAIRED IAW EO B757-5320-9692-G.
Part: FLOORBOARD — DAMAGED (BS 1055-1100) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1 FOUND FLOORBOARD AT STA 1055-1100, RBL 25-45, OTBD SIDE DAMAGED (MARKED) AND MISSING INSERT. R & R WITH FABRICATED NEW FLOORBOARD IAW SRM 53-00-50-1A, AND EO B757-5320-9692-G.
Part: FLOORBOARD — DAMAGED (BS 1610) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, MISSING INSERT IN FLOORBOARD AT STA 1610, RBL44. FABRICATED REPLACEMENT FLOORBOARD IAW EO B757-5320-9692-G.
Part: SUPPORT ANGLE — WORN (NR 1 NACELLE) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:MOD, NR1 PYLON, CROSS OVER BRACE, UPPER SUPPORT ANGLE FWD FACE IS WORN ALONG ENTIRE LENGTH. R & R NR1 PYLON CROSS OVER BRACE IAW SRM 51-40-02-0G.
Part: SUPPORT — CORRODED (BS 1320-1360) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, CORROSION ON FLOOR TO SIDEWALL SUPPORT RT BS 1320-1360. R & R IAW SRM 51-40-02.
Part: CHANNEL — WORN (NR 2 PYLON) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C, NR 2 PYLON CROSSOVER BRACE UPPER CHANNEL FWD FACE IS WORN ALONG ENTIRE LENGTH. R & R CHANNEL IAW SRM 51-40-02-0G.
Part: SILL — DAMAGED (BS 297) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, FWD ENTRY DOOR SILL HAS A DOUBLE HOLE DRILLED AT BS 297, WL 215. FABRICATED REPLACEMENT PART IAW SRM 51-40-05, SRM 51-30-1.
Part: SKIN — GOUGED (BS 1861 S17L) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, LT FUSELAGE SKIN GOUGED FROM LOWER STAB SEAL AT BS 1861 JUST ABOVE STRINGER 17. REPAIRED IAW ATS ER 11-01526, DATED 2/21/11.
Part: SUPPORT — CORRODED (BS 1540-1620) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, CORROSION ON FLOOR TO SIDEWALL SUPPORT RT BS 1540-1620. R & R IAW SRM 51-40-02.
Part: BRACKET — CRACKED (A:130 Z:100) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, BRACKET IS CRACKED AT BS 912, LBL 8, WL 148. R & R IAW SRM 51-10-02-0G, SRM 51-40-02-0G.
Part: FRAME — GOUGED (BS 660 S15-16R) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, SCREW STRIKE ON FRAME INNER FLANGE AT BS 660 BETWEEN 15R AND 16R. REPAIR IAW ATS ER NR 11-01428.
Part: CLOSEOUT PANEL — CORRODED (ZONE 200) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, 9G WALL LOWER CLOSE OUT TRIM PANEL HAS CORROSION AROUND FASTENER HOLES. FABRICATED NEW CLOSE OUT TRIM PANEL IAW DWG 141N6007, AMM 25-00-00-7, SRM 51-20-01-0G, AM 51-21-00-7, SRM 51-40-02-0G.
Part: FLOOR PANEL — DENTED (FUSELAGE) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, UPPER FLOOR PANEL IN THE CONTROL CABIN HAS NUMEROUS BROKEN AND CORRODED INSERTS, DENTS AND PUNCTURES. REPLACED CONTROL CABIN UPPER FLOOR PANEL IAW EO B757-5320-9692-G, SRM 53-00-50-2R1, AND SRM 53-00-50-1A1, FIG 101, TABLE I.
Part: FRAME — DAMAGED (BS 520) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, SCREW STRIKE ON FRAME INNER FLANGE AT BS 520 BETWEEN STRNGER 15R AND 16R REPAIRED IAW ER NR 11-01420, DATED 21FEB11.
Part: WEB — DENTED (BS 607 S3L) · airframe 18,978 hrs · 12,461 cycles
INSPECTION TYPE:C1, MAIN CARGO DOOR CUT-OUT UPPER WEB IS DENTED BS 607, BELOW AFT DOOR ACTUATOR, (APPROX STR 3L). REPAIRED IAW SRM 51-70-11-0G.
2010
Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)
MAIN CARGO DECK FLOOR PANEL ZONE 131 OTBD HAS DAMAGE TO EDGE. MFG AND INSTALLED NEW FLOOR PANEL IAW EO B757-5320-9692-G AND AMM-53-01-01.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)
MAIN CARGO DECK ZONE 131 INBD FLOOR PANEL HAS DAMAGE TO EDGE, CRUSHED. MFG AND REPLACED FLOOR PANEL IAW EOB757-5320-9692-G AND AMM-53-01-01.
2009
Part: WINDOW — STUCK (COCKPIT)
R2 SLIDING WINDOW DIFFICULT TO OPEN. CLEANED AND LUBRICATED SEAL IN UPPER AFT CORNER REF AMM 56-11-53-4. OK TO CONTINUE.
Part: SKIN PANEL — DAMAGED (FUSELAGE)
INSPECTION TYPE:N/A PREVIOUSLY BLENDED AREA DAMAGE WAS FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER REPAIR PER EO B757-5330-34715-A.
Part: SKIN — DAMAGED (FUSELAGE)
INSPECTION TYPE:N/A DAMAGE TO FUSELAGE SKIN RT SIDE STA 345 STRINGER 19R - 20R. REPAIRED IAW EO B757-5330-34722-A.
Part: SKIN — DAMAGED (FUSELAGE)
INSPECTION TYPE:N/A DAMAGE TO FUSELAGE SKIN AT STA 263 BELOW STRINGER 20R. INTERIM REPAIR INSTALLED IAW EO B757-5330-34712. REFERENCE NRC 345563.
Part: SKIN — DAMAGED (FUSELAGE)
INSPECTION TYPE:N/A DAMAGE TO FUSELAGE SKIN STA 247 BELOW STRINGER 20R. INSTALLED INTERIM REPAIR IAW EO B757-5330-34705-A.
Part: SKIN PANEL — DAMAGED (FUSELAGE)
INSPECTION TYPE:N/A PREVIOUS BLENDS ARE OUT OF LIMITS AT STA 231 BELOW STR 20R. INSTALLED TEMP REPAIR PER EO B757-5330-34704-A.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS CHARGE INDICATOR RIGHT BULB INOP. RELAMPED IAW AMM 33-16-02-2. OPS CHECKS GOOD.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 CORROSION MAIN CABIN SEAT TRACK BS 1184, LBL 61, WL 208. REPAIRED PER ATS ENGINEERING ORDER 09-1601.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 APU LIGHT HAS CORROSION AROUND THE AFT LWR NUT PLATE, 3RD NUT PLATE GOING FROM THE AFT LWR END OF CUTOUT. REQUIRES REMOVAL OF APU DUCTING AND APU INLET HOUSING. REMOVED, FABRICATED AND INSTALLED REPLACEMENT APU DOOR HOUSING MOUNT ANGLES PER SRM 51-40-02, SRM 53-00-03-1A1.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 CORROSION MAIN CABIN FLOORBEAM BS 1200 LBL 5 WL 209. REPAIRED PER ATS ER 09-1641 DATED 26FEB09 AND UPS EO B757-5310-32484A.
Part: SILL — CORRODED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 NR 2 CARGO DOOR LWR SILL UPPER SURFACE CORRODED AROUND FASTENER HOLES. REPAIRED PER ATS ER 09-1599 DATED 26FEB09 AND UPS EO B757-5310-32479-A.
Part: SEAL DEPRESSOR — PUNCTURED (CARGO DOOR) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 AFT CARGO DOOR FWD LWR CORNER SEAL DEPRESSOR IS PUNCTURED. REMOVED AND REPLACED DEPRESSOR PER SRM 51-40-02.
Part: STAND OFF — CRACKED (THRUST REVERSER) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 NR 2 ENGINE OUTBOARD T/R LOWER ACTUATOR TELEFLEX CABLE STAND OFF IS CRACKED 12 INCHES ABOVE ACTUATORS. REMOVED, FABRICATED, INSTALLED REPLACEMENT STANDOFF PER SRM 51-30-01-0G, SRM 51-40-02.
Part: CHANNEL — CHAFED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 FIRE LOOP RAIL CHAFED 8 INCHES FROM AFT END OF RT APU DOOR. REMOVED, FABRICATED AND INSTALLED PER SRM 51-40-02 M/M 26-15-02-4.
Part: SKIN — DEBONDED (LE SLAT) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 VERIFY STRUCTURAL SOUNDNESS OF PREVIOUS REPAIR ON NR 3 SLAT T/E WEDGE UPPER SURFACE AT OSS 519.55-528.55 EVALUATION REQUIRED PER EO B757-5100-30760 (438-W3-04). REMOVED DISBONDED REPAIR AND REPAIRED PER ATS ER09-1688 DATED 26FEB09 UPS EO B757-5740-32475-A.
Part: SKIN — DENTED (CARGO DOOR) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 FWD CARGO DOOR EXTERNAL SKIN IS DENTED AT LOWER EDGE 12-18 INCHES AFT OF THE FWD EDGE. REPAIRED PER ER 09-0065.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 CORROSION MAIN CABIN FLOORBEAM BS 1200 LBL 48-55 WL 208. REPAIRED PER ATS ER 09-1641 DATED 26FEB09 UPS EO B757-5310-32484A.
Part: SKIN — CHAFED (ACCESS DOOR) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 REMOVED CHAFING DAMAGE ON INNER SURFACE OF OUTER SKIN ON ACCESS DOOR 311AL IN AN AREA OF 6.3"X.5"X.007". ORIGINAL THICKNESS IS .056", FOUND BLENDED AREA TO BE OUT OF LIMITS PER SRM 52-40-01-1A FIG 101. ALODINED, PRIMED AND PAINTED PER ENGINEERING ER 09-1631 AND CUSTOMER AUTHORIZATION B757-5240-32462-A.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 MAIN CABIN FLOOR PANEL CRACKED BS 900-1020 RBL 45-62 WL 208. FABRICATED REPLACEMENT PANEL PER EO B757-5320-9692-F.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 FUSELAGE EXTERIOR SKIN CROWN AREA LIGHTNING STRIKE BETWEEN ST 2L AND ST 3L AT BS 359. REPAIRED LIGHTNING STRIKE PER IAW SRM 53-10-01.0I, SRM 53-10-01-0A AND SRM 53-10-01-2R.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 FUSELAGE EXTERIOR SKIN - CROWN AREA LIGHTNING STRIKE BETWEEN STR 1 AND STR 2R BS 451.5. REPAIRED PER SRM 53-00-01-2R6.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,391 hrs · 11,352 cycles
INSPECTION TYPE:C4 LIGHTNING STRIKE BETWEEN STR 1 AND STR 2R BS 386.5. REPAIRED PER ER 09-1603 DATED 26FEB09 AND UPS B757-5310-32480-A.
2008
Part: ENGINE — FAULTY (NR 2)
INSPECTION TYPE:N/A RT PACK EXTREME ODOR/FUMES WHEN OPERATING SHUT DOWN RT PACK & FUMES EXTINGUISHED. ACCOMPLISHED NR 2 ENG PWR RUN PER MM 71-00-00-5. OIL FUMES EMITTED FROM NR 2 ENG WITH EITHER PACK L OR R SELECTED AND ENG ABOVE GRD IDLE. FUMES DISSIPATED WITH NR 2 ENG BLEED OFF. REF L/P 160663 I3 NR 2 ENG REMOVED AND REPLACED, NO FUMES NOTED DURING ENG RUN AFTER INSTALLATION.
Part: UNKNOWN — ODOR (COCKPIT)
INSPECTION TYPE:N/A AIR TURNBACK AT 1020Z DURING CLIMBOUT AT APPROX 15,000FT, NOTICED AN ODOR IN THE COCKPIT FOLLOWED A MINUTE OR TWO LATER BY THE PRESENCE OF A LIGHT HAZE. DURING THE SMOKE/FUMES CHECKLIST NOTICED THE RIGHT ENGINE OIL PRESSURE IN THE AMBER BAND (OIL QUANTITY WAS GOOD). MAINTAINED PRESS IN THE NORMAL. *SDR FILED OPEN*
Part: UNKNOWN — ODOR (COCKPIT)
INSPECTION TYPE:N/A NOTICED ODOR AND LIGHT HAZE IN COCKPIT DURING CLIMB. FOUND FUEL IN NR 2 ENGINE OIL SYSTEM. PER FIM CHANGED NR 2 ENGINE LOW PRESSURE AND HIGH PRESSURE FUEL PUMPS, FFG, FCOC AND FCOC BYPASS VALVE. ALSO PERFORMED DUCT BURNOUT OF PNEUMATIC DUCT SYSTEM.
2007
Part: WINDOW — BINDING (COCKPIT)
R2 WINDOW BINDING DURING OPERATION. COMPLETED REMOVAL OF RT WINDOW CRANK AND INSTALLED NEW SERVICEABLE GEARBOX AND (4) MOUNT BOLTS. REFERENCE MM 56-11-04-4. INSTALLED NR 2R WINDOW SHROUD AND CRANK HANDLE PANEL. OPENED & CLOSED WINDOW SEVERAL TIMES. CHECKS GOOD W/REF TO MM 56-11-04-4.
Part: COMPRESSOR — STALLED (LT ENGINE)
INSPECTION TYPE:N/A ATB - SEVERAL COMPRESSOR STALLS NOTED ON CLIMBOUT LEFT ENG. *SUPPLEMENTAL SDR* REMOVED AND REPLACED NR 1 ENGINE WITH REFERENCE TO MAINTENANCE FUNCTION TASK CARD TC 5001 (RR), ENGINE GROUND RAN NORMAL. A/C OK FOR SERVICE.
Part: FRAME — DENTED (FUSELAGE) · airframe 23,170 hrs · 6,707 cycles
INSPECTION TYPE:C3 FWD CARGO BAY FRAME DENTED AT STA 700 STR 24R. REMOVED DAMAGE ON FRAME AND REPAIRED PER SRM 51-70-11.
Part: FRAME — DENTED (FUSELAGE) · airframe 23,170 hrs · 6,707 cycles
INSPECTION TYPE:C3 FWD CARGO BAY FRAME DENTED AT STA 680 STR 23R. REMOVED DAMAGE ON FRAME AND REPAIRED PER SRM 51-70-11.
Part: SKIN — DENTED (FUSELAGE) · airframe 23,170 hrs · 6,707 cycles
INSPECTION TYPE:C3 EXTERIOR FUSELAGE SKIN HAS A DENT AT STR 7R, BS 751. REPAIRED DENT IN EXTERIOR FUSE SKIN BS 751, STR 7R, IAW SRM 53-00-01-2 -2R.
2006
Part: ANTI-ICE VALVE — INOPERATIVE (RT ENGINE)
DIVERSION, RT ENGINE ICE MESSAGE DISPLAYED WITH SWITCH ON. REMOVED AND REPLACED RT ENGINE INLET THERMAL ANTI-ICE VALVE IAW MM 30-21-03-4. OPS CHECK NORMAL.
Part: WINDOW — STIFF (COCKPIT)
L2 WINDOW HARD TO OPEN. UNLATCH LEVER DOES NOT WORK PROPERLY. REPLACED CAPT NR 2 WINDOW PER MM 56-11-02-4 STEPS 1, 2, 3, 4D TASKS 1-14. INSTALLED INTERIOR LINER AND PERFORMED WINDOW HEAT, OPS CK IAW 30-41-00-5.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
INSPECTION TYPE:N/A EMERGENCY LIGHTS DO NOT TEST PROPERLY. REMOVED AND REPLACED EMERGENCY LIGHTT BATTERY PACK IAW MM CHT 33-51-07-02, OPS CHECK GOOD.
2005
Part: ENGINE — POWER LOSS (LEFT)
LOSS OF POWER LT ENGINE. LT ENG HIGH EGT AND EPR INDICATION.
2004
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)
INSPECTION TYPE:N/A EMERGENCY LIGHT POWER SUPPLY DEAD. REPLACED EMERGENCY LIGHT POWER SUPPLY, OPS CHECK GOOD.
2001
Part: POWER SUPPLY — DISCHARGED (CABIN)
INSPECTION TYPE:IN AFTER REPLACING SEVERAL LAMPS, EMERGENCY EXIT LIGHT CAME ON, THEN WENT OUT. UNABLE TO GET IT BACK ON. R&R EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY ASSY IAW 33-51-07-2. OPS CHECKS GOOD.