N3203Y
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| EVERGREEN INTERNATIONAL AIRLINES INC | Operator | on 2001-12-28 | Operator named in NTSB report |
Accident & incident history
Operated by EVERGREEN INTERNATIONAL AIRLINES 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.
336 reports on file, 1996-06-24 – 2001-05-20.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
REPAIR OF CANTED PRESSURE DECK AND ANGLE, STA1238 - 1265, LBL 41 - RBL 53. REPAIR OF THE CORROSION DAMAGE TO 65B07992-1 (CANTED) PRESSURE DECK BETWEEN STA 1238 AND 1265 LBL 41 TO BL 0 AND SHORT E/D COMMON TO THE 65B10670 FLOORBEAM LOWER CHORD. CONSIST OF TRIMMING OUT THE CORROSION DAMAGE AND INSTALLING NET FIT FILLERS, EXTERNAL AND INTERNAL DOUBLERS. TRIMMING OUT THE DISCREPANT SHORT E/D HOLES, AND INSTALLATION OF A REPAIR STRAP, TEE AND FILLERS, COMMON TO THE 65B10670 FLOORBEAM LOWER CHORD PER ECRA 3203-53-046-2 REV A.
Part: SUMP — LEAKING (RT FUEL TANK)
KSEA - AFTER TAKEOFF, STRONG ODOR OF FUEL NOTICED IN COCKPIT FOR SEVERAL MINUTES AFTER FIRST AC PACK NR 1 TURNED ON. RESEALED LEAKING RIGHT SUMP DRAIN. (M)
Part: FITTING — CORRODED (WING) · airframe 85,973 hrs · 19,030 cycles
ADDITIONAL WING REAR SPAR TO WING CENTER SECTION UPPER SPLICE FITTING REWORK. A DEVIATION TO AND ADDITIONAL REWORK FOR S/B 747-57-2110 TERMINATING ACTION PER FIG 4. THE DEVIATION CONSISTS OF USING A FILLER BETWEEN THE REPLACEMENT (NEW) 65B17223-5 SPLICE FITTING AND THE UPPER WING SKIN. THE ADDITIONAL REWORK CONSISTS OF MATCHING THE O/B LOWER EDGE OF THE EXISTING EXTERNAL LONGERON SPLICE & USE OF OVERSIZE FASTENERS IN ADJACENT STRUCTURE. THE FILLER IS REQUIRED TO ACCOUNT FOR A CONFIGURATION MISMATCH BETWEEN THE REPLACEMENT (NEW) 65B17223-5 SPLICE FITTING AND THE REPLACED 65B12071-1 SPLICE FITTING.
Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 85,973 hrs · 19,030 cycles
ALTERNATE FASTENERS FOR NR 1 PYLON FWD INBOARD HANGER FITTING REWORK. A DEVIATION TO THE SERVICE BULLETIN 747-54A2203 WHICH CONSISTS OF USING LARGER FASTENER SIZES OF THE SAME TYPE AS LISTED IN THE SERVICE BULLETIN PER ECRA 3203-54-034-2.
Part: SKIN — CRACKED (ELEVATOR) · airframe 85,973 hrs · 19,030 cycles
REPAIR- RIGHT INBD ELEVATOR LEADING EDGE, UPPER SURFACE ELEV STA 77-86. AN EXISTING REPAIR WAS FOUND OUTBOARD OF THE CRACK LOCATION. THE EXISTING REPAIR WAS REMOVED TO INCORPORATE THE NEW CRACK INTO THE REPAIR. UPON DISASSEMBLY IT WAS FOUND THAT THE PRIOR REPAIR AREA WAS A RESULT OF DEFORMATION AND CRACK DAMAGE (CRACK WAS STOPPED DRILLED). REPAIR OF THIS AREA AND THE NEW CRACK IS ACCOMPLISHED BY TRIMMING OUT THE DAMAGED AREA AND INSTALLING A NEW INTERNAL DOUBLER. THIS DOUBLER REPLACES THE OLD REPAIR DOUBLER AND THE ORIGINAL PRODUCTION DOUBLER (65B05771-17) PER ECRA 3203-55-035-2.
Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 85,973 hrs · 19,030 cycles
NR 2 ENGINE PYLON, FORWARD MOUNT, OVERSIZE HOLES. DURING SCHEDULED MAINTENANCE INSPECTION OF THE AIRPLANE CRACKS WERE FOUND IN THE INBOARD AND OUTBOARD HANGER FITTING UPPER ATTACHMENT HOLES. THE CRACKS WERE REMOVED BY OVERSIZING, AND NDT INSPECTED TO ASSURE A CRACK AND CORROSION FREE CONDITION. OVERSIZE DIA BOLTS WERE INSTALLED PER BOEING RECOMMENDATIONS PER ECRA 3203-54-049-2.
Part: SKIN — DAMAGED (NACELLE) · airframe 85,973 hrs · 19,030 cycles
REPAIR- ENGINE STRUT NR 4, RIGHT SKIN DAMAGE-NAC STA 236.5. THIS DAMAGE IS IN A PREVIOUSLY REPAIRED AREA AT NAC STA 236.5 AND COMMON AND TO THE LOWER EDGE OF THE SKIN. THE PREVIOUSLY INSTALLED REPAIR DOUBLER WAS DAMAGED. THIS REPAIR REPLACES THE DAMAGED REPAIR DOUBLER WITH A NEW LARGER DOUBLER TO ADDRESS THE INCREASED DAMAGE SIZE PER ECRA 3203-54-024-2.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
REPAIR OF DAMAGED FRAME OUTER CHORD, STA 440, S-9R TO S-14R. THIS CONSISTS OF CUTTING AND SPLICING THE EXISTING 65B01715-170 FRAME BETWEEN STRINGERS 9 AND 10 AND REMOVING AND REPLACING THE FRAME SEGMENT LOCATED BELOW THE CUT TO THE EXISTING SPLICE LOCATED AT STRINGER 13A. REPAIR OF SHORT EDGE CONDITION EXISTING ON SKIN DOUBLER SPLICE PLATE LOCATED BETWEEN S-12R AND S-13R CONSISTS OF FABRICATING AND INSTALLING A NEW ONE IN PLACE OF THE ORIGINAL PER ECRA 3203-53-041-2.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
REPAIR- FUSELAGE SKIN - FWD AND ABOVE NR 1 MAIN ENTRY DOOR. THIS REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE AND INSTALLING A MODIFIED SRM REPAIR, EXTERNAL SKIN DOUBLER, TRIPLER AND A SPLICE ARE FABRICATED AND FIT TO CORRECT THE DISCREPANT CONDITION PER ECRA 3203-53-39-2.
Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
REPAIR OF INTERCOSTAL CHORD FWD AND AFT ENDS STA 1265, RBL 101 AND WL 199. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR THE DISPOSITION OF THE USE OF TWO LARGER FASTENERS IN LIEU OF TWO DRAWING FASTENERS COMMON TO THE FOWARD AND AFT INTERCOSTAL CHORD ENDS. THE CHORDS WILL BE TRIMMED TO ALLOW THE LOWER ADJACENT FASTENER TO BE INSTALLED PER ECRA 3203-53-36-2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
REPAIR OF CRACKED OUTBOARD FLANGE OF UPPER PARTIAL FRAME, STA 806 S-18L. REPAIR OF CRACKED OUTBOARD FLANGE OF 65B05002-185 UPPER PARTIAL FRAME AT STA 806 (FWD EDGE OF L2 DOOR FRAME), STRINGER 18L. CONSISTS OF REMOVING AND DISCARDING 65B05002-4 RADIUS FILLER, TRIMMING OUT THE CRACK, INSTALLING A NET FIT FILLER AND AN INTERNAL DOUBLER PER ECRA 3203-53-038-2.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT FROM STA 1080 TO 1100 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01, AND FOUND WINDOW FORGING TO BE WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW AT STA 990 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW CASTING PER 747 SRM 51-10-01, FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED WINDOW CASTING PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK LT FROM STA 1040 TO 1060 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01, AND FOUND WINDOW FORGING TO BE WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT FROM STA 1160 TO 1180 AND BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT SIDE FROM STA 1460 TO 1480 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE BETWEEN STA 1372 AND STA 1394 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT CORNER. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE AT STA 1350 TO STA 1372 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT CORNER. REMOVED MAIN CABIN WINDOW FORGING PER 747 SRM 51-30-02 AND FOUND WINDOW FORGING OUT OF LIMITS PER 747 SRM 56-20-01. REPLACED WINDOW FORGING PER 747 SRM 51-30-02 AND ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW AT STA 1130 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW CASTING PER 747 SRM 51-10-01 AND FOUND IT WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 52-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
L-12 WINDOW STA 370 HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOVED CORROSION ON CASTING PER 747 SRM 51-10-01 AND FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
RIGHT WINDOW AT STA 1210 HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION PER 747 SRM 51-10-01 AND FOUND WINDOW FORGING TO BE WITHIN ALLOWABLE LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
SURFACE CORROSION INTERIOR SIDE OF R-4 WINDOW FRAME UPPER AFT CORNER AT STA 230. REMOVED WINDOW FRAME PER 747 SRM 51-20-02. REMOVED CORROSION FROM WINDOW FRAME, FOUND WINDOW FRAME WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED PER 747 SRM 51-10-01, PRIMED PER SOPM 20-41-02. INSTALLED WINDOW FRAME PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
SURFACE CORROSION ON R-5 WINDOW FRAME INTERIOR, AFT LOWER CORNER AT STA 250. REMOVED WINDOW FRAME PER 747 SRM 51-10-01. REMOVED CORROSION PER 747 SRM 56-20-01. FOUND WINDOW FRAME WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FRAME PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW FRAME PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW FORGING BETWEEN STA 1020-1040 HAS CORROSION COMING OUT FROM UNDER THE SEALANT IN MAIN CABIN ON THE RIGHT SIDE. REMOVED WINDOW FORGING PER 747 SRM 51-30-02, WINDOW FORGING FOUND IT WITHIN LIMITS PER ECRA 3203-53-047-2. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02 AND SEALED PER 747 SRM 51-10-06.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW AT STA 1210 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOVED CORROSION PER 747 SRM 51-10-01, AND FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN STA 1040-1060 RIGHT HAND WINDOW FORGING HAS CORROSION COMING OUT FROM UNDER SEALANT. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW FORGING PER 747 SRM 51-10-01, WINDOW CASTING FOUND TO BE WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED WINDOW CASTING PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE BETWEEN STA 1416 AND STA 1438 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION ON WINDOW FORGING PER 747 SRM 51-10-01, FOUND WINDOW FORGING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
UPPER DECK WINDOW FORGING 1R HAS CORROSION PROTRUDING AROUND EDGES STA 560 TO STA 580 RIGHT SIDE S-8R TO S-10R. REMOVED UPPER DECK WINDOW FORGING FOUND IT WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW FORGING PER 747 SRM 51-10-02 AND PRIMED WINDOW FORGING PER 747 SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE BETWEEN STA 1438 AND STA 1460 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT SIDE. REMOVED WINDOW FORGING PER 747 SRM 51-30-05. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER 747 SRM 51-10-01. REPLACED WINDOW FORGING PER 747 SRM 51-30-05. ALODINED WINDOW FORGING PER 747 SRM 51-10-01 AND PRIMED PER 747 SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE BETWEEN STA 1394 AND STA 1416 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02 AND REMOVED CORROSION PER 747 SRM 51-10-01 AND FOUND TO BE WITHIN ALLOWABLE LIMITS PER 747 SRM 56-20-01. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
UPPER DECK WINDOW FORGING 2R HAS CORROSION PROTRUDING AROUND TOP EDGE STA 620 TO 640 RIGHT SIDE AT S-8R BOTTOM SIDE. REMOVED WINDOW FORGING PER 747 SRM 51-30-02, REMOVED CORROSION ON FORGING PER 747 SRM 51-10-01. FORGING IS WITHIN LIMITS PER ECRA 3203-53-047-2. REINSTALLED WINDOW FORGING PER 747 SRM 51-30-02 AND ECRA 3203-53-047-2.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK LT FROM STA 1160 TO 1180 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02 AND REMOVED CORROSION PER 747 SRM 51-10-01. MINIMUM MATERIAL REMOVED. ALODINED AND PRIMED PER 747 SRM 51-10-02 AND SOPM 20-41-02. REINSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE BETWEEN STA 1580 AND STA 1600 S-20L AND S-22L HAS CORROSION AT WINDOW FORGING LOWER AFT SIDE. REMOVED LIGHT SURFACE CORROSION MINIMUM MATERIAL LOSS PER 747 SRM 51-10-01. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
UPPER DECK WINDOW FORGING 2L HAS CORROSION PROTRUDING BOTTOM EDGE STA 620 TO STA 640 LEFT SIDE AT S-10L TOP SIDE. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION ON FORGING PER 747 SRM 51-10-01. FORGING IS WITHIN LIMITS PER ECRA 3203-53-047-2. REINSTALLED WINDOW FORGING PER 747 SRM 51-30-02 AND ECRA 3203-53-047-2.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK LT SIDE FROM STA 320 TO 340 BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING, CLEANED SURFACE CORROSION, FOUND TO BE WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED AND PRIMED PER 747 SRM 51-10-03 AND SOPM 20-41-02 AND INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK LT SIDE FROM STA 380 TO 400 BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED LIGHT SURFACE CORROSION PER 747 SRM 51-10-01 AND FOUND TO BE WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED AND PRIMED PER 747 SRM 51-10-02 AND SOPM 20-41-02. INSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW AT STA 1010 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION PER 747 SRM 51-10-01 OUT OF LIMITS PER 747 SRM 56-10-02. REPLACED WINDOW FORGING AND SEALED PER 747 SRM 51-30-02 AND 51-10-06.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW AT STA 670 LEFT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02. REMOVED CORROSION FROM PITTED AREAS OF FRAME OUTER SURFACE PER 747 SRM 55-20-01, OUT OF LIMITS PER 747 SRM 56-20-01. REPLACED WINDOW FORGING PER 747 SRM 51-30-02 AND 51-10-01 AND SOPM 20-41-02 AND PER ECRA 3203-53-47-2.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE BETWEEN STA 200 TO 220 AND BETWEEN S-20L AND S-22L WINDOW HAS CORROSION UNDER FORGING ON AFT SIDE. REMOVED SEALANT AND REMOVED LIGHT SURFACE CORROSION PER 747 SRM 51-10-01. TREATED AND PRIMED AND SEALED PER 747 SRM 51-10-02 AND SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK LT BETWEEN STA 1060 AND 1080 BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION FWD BOTTOM CORNER. REMOVED WINDOW FORGING PER 747 SRM 51-30-02, REMOVED CORROSION ON WINDOW FORGING FOUND TO BE OUT OF LIMITS PER 747 SRM 56-20-01. INSTALLED NEW WINDOW FORGING PER 747 SRM 51-30-05 AND 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
CORROSION BETWEEN S-20L AND WINDOW FORGING AT STA 530 MAIN CABIN LT SIDE. REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02.
Part: SKIN — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
SURFACE CORROSION ON SKIN AROUND PAX WINDOW FORGING STA 500 TO 520 AND S-20L TO S-22L. ALSO ON UNDER SIDE OF S-22L AND UPPERSIDE OF S-20L MAIN CABIN LT SIDE. REMOVED WINDOW AND FORGING PER 747 SOPM 20-50-01. REMOVED CORROSION ON FORGING AND FUSELAGE SURFACE PER 747 SRM 51-10-01 FOUND TO BE WITHIN LIMITS PER 747 SRM 56-20-01. REPLACED WINDOW FORGING PER 747 SRM 51-30-01.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN AT STA 986 LT SIDE WINDOW FORGING HAS 2 AREAS OF CORROSION JUST ABOVE S-22L. BLENDED OUT CORROSION PER 747 SRM 51-10-01, MINIMUM MATERIAL REMOVED. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02 AND SEALED PER 747 SRM 51-10-06.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN WINDOW FORGING AT STA 660 - 680 LEFT HAND HAS CORROSION IN SEVERAL SPOTS COMING OUT FROM UNDER SEALANT. REMOVED SEALANT AND REMOVED CORROSION PER 747 SRM 51-10-01, WITHIN LIMITS PER 747 SRM 56-20-01. ALODINED PER 747 SRM 51-10-02 AND PRIMED PER 747 SOPM 20-41-02 AND RESEALED PER 747 SRM 51-10-06.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT SIDE FROM STA 400 TO 420 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING, REMOVED CORROSION FOUND IT IN LIMITS PER SRM 51-10-01 & SRM 56-20-01. ALODINED AND PRIMED PER SRM 51-10-02. INSTALLED WINDOW FORGING AND SEALED PER SRM 51-30-02 & SOPM 20-050-01.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW FORGING BETWEEN STA 1080 - 1100 HAS CORROSION COMING OUT FROM UNDER THE SEALANT IN THE MAIN CABIN ON THE RIGHT SIDE. REMOVED WINDOW FORGING PER 747 SRM 56-20-01, REMOVED CORROSION WITHIN LIMITS PER 747 SRM 56-20-01. REINSTALLED WINDOW FORGING PER 747 SRM 51-30-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT SIDE FROM STA 1438 TO 1460 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING PER 747 SRM 51-10-01. REMOVED CORROSION ON FORGING AND FOUND TO BE OUT OF LIMITS PER 747 SRM 56-20-01. INSTALLED NEW WINDOW FORGING AND SEALED PER 747 SRM 51-10-01, SRM 51-30-05 & SRM 51-30-06.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN LT SIDE BETWEEN STA 180 TO 200 AND BETWEEN S-20L AND S-22L WINDOW FORGING HAS CORROSION ON UPPER FASTENERS. REMOVED UPPER FASTENERS AND REMOVED LIGHT SURFACE CORROSION FROM FORGING PER 747 SRM 51-10-01. INSTALLED NEW FASTENERS PER 747 SRM 51-30-02 AND SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN CABIN WINDOW FORGING AT STA 560 TO 580 RT HAS CORROSION ON UPPER FRD CORNER COMING OUT FROM UNDER SEALANT. REMOVED SEALANT AND LIGHT CORROSION WITHIN LIMITS. ALODINED AND PRIMED, RESEALED WITH BMS 5-95 SEALANT PER 747 SRM 51-10-01, 51-10-02, 56-20-01, AND 747 SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
RIGHT WINDOW AT STA 1070 HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW FORGING PER 747 SRM 51-30-02 WINDOW FORGING FOUND TO BE OUT OF LIMITS PER 747 SRM 56-20-02. REMOVED WINDOW FORGING AND REPLACED WITH NEW FORGING PER 747 SRM 51-30-02, 51-10-02, SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
CORROSION ON WINDOW FRAME AT STA 950 RIGHT AFT LOWER CORNER. REMOVED WINDOW FORGING, REMOVED CORROSION FROM WINDOW FRAME PER SRM 51-10-01. FOUND WINDOW FRAME TO BE OUT OF LIMITS PER SRM 56-20-01. REMOVED AND REPLACED WINDOW FRAME PER SRM 51-10-01, SRM 51-30-05, SRM 51-30-02 & SOPM 20-41-02.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW AT STA 1427 RIGHT HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED WINDOW CASTING PER 747 SRM 51-30-02. REMOVED CORROSION FROM WINDOW CASTING PER 747 SRM 51-10-01 AND FOUND WINDOW CASTING WITHIN LIMITS PER ECRA 3203-53-047-2. ALODINED WINDOW CASTING PER 747 SRM 51-10-02 AND PRIMED WINDOW CASTING PER SOPM 20-41-02. INSTALLED WINDOW CASTING PER 747 SRM 51-30-02.
Part: FORGING — CORRODED (FUSELAGE)
FOUND LEFT STATION 1040-1060 STRINGER 20L TO STRINGER 22L CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 560-580)
MZJ-EAC - FOUND RIGHT STATION 560-580 STRINGER 8R TO STRINGER 10R CORROSION AROUND EDGES OF 1R WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FUSELAGE)
MZJ-EAC - FOUND RIGHT STATION 1160-1180, STRINGER 20R TO STRINGER 22R CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 1080-1100)
MZJ-EAC - LEFT STATION 1080-1100 STRINGER 20L TO STRINGER 22L CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 620)
MZJ-EAC - LEFT STATION 620-640 STRINGER 10L CORROSION ON 2L WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FASTENER — FAILED (NR 2 PYLON)
MZJ-EAC - NR 2 PYLON FORWARD ENGINE MOUNT HANGAR FITTING FASTENERS FAILED TORQUE CHECK, PRIMARY FAST INBOARD NR 1 AND NR 4, OUTBOARD NR 4, SECONDARY FAST INBOARD NR 2, AND OUTBOARD NR 3. COMPLIED WITH SB 54-747-1611-00 REV E AND ECRA 3203-54-049-2. (M)
Part: FORGING — CORRODED (FS 1416-1438)
MZJ-EAC - FOUND MAIN CABIN LEFT STATION 1416-1438 STRINGER 20L TO STRINGER 22L CORROSION AT WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 1210)
MZJ-EAC - FOUND RIGHT STATION 1210 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 1040-1060)
MZJ-EAC - FOUND RIGHT STATION 1040-1010 CORROSION EXTENDING OUT FROM UNDER WINDOW FORGING SEALANT. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 1427)
MZJ-EAC - FOUND RIGHT STATION 1427 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 250)
MZJ-EAC - FOUND STATION 250 SURFACE CORROSION ON R-5 WINDOW FRAME INTERIOR AFT LOWER CORNER. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: WEB — CRACKED (BS 1265)
MZJ-EAC - FOUND MED NR 3 BS 1265 FRAME CRACKS. REPAIRED AND MODIFIED PER EO 53-747-1580-00 REV D. (M)
Part: DOUBLER — BULGED (FS 440-460)
MZJ-EAC - FOUND LEFT STATION 440-460 STRINGER 14L TO STRINGER 14EL, SKIN UNDER REPAIR DOUBLER BULGED. REPAIRED PER ECRA 3203-53-039-2. (M)
Part: FORGING — CORRODED (FS 1130)
MZJ-EAC - FOUND LEFT STATION 1130 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 370)
MZJ-EAC - FOUND STATION 370 CORROSION ON AND AROUND L-12 WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FS 230)
MZJ-EAC - FOUND STATION 230 SURFACE CORROSION ON R-4 WINDOW FRAME INTERIOR AFT UPPER CORNER. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FUSELAGE)
MZJ-EAC - FOUND RIGHT STATION 1020-1040 CORROSION ON WINDOW FORGING AND UNDER SEALANT. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT SIDE FROM STA 380 TO STA 400 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED WINDOW FORGING, REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS, INSTALLED WINDOW FORGING AND SEALED PER SRM 51-30-02, SOPM 20-50-01, SRM 51-10-06, SOPM 20-10-03.
Part: FORGING — CORRODED (FUSELAGE)
MZJ-EAC - FOUND RIGHT STATION 620-640 STRINGER 8R, CORROSION ON AND AROUND 2R WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FUSELAGE)
MZJ-EAC - FOUND LEFT STATION 990 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
WINDOW AT STATION 210 RIGHT HAND SIDE HAS CORROSION ON AND AROUND WINDOW CASTING. REMOVED LIGHT SURFACE CORROSION PER B747 56-20-01, ALODINED PER B747 SRM 51-10-02, PRIMED PER B747 SOPM 20-41-02, RESEALED PER B747 SOPM 20-50-19.
Part: FORGING — CORRODED (FUSELAGE)
MZJ-EAC - FOUND LEFT STATION 1372-1394 STRINGER 10L TO STRINGER 22L, CORROSION AT WINDOW FORGING LOWER AFT CORNER. REPAIRED PER ECRA 3203-53-047-2. (M)
Part: FORGING — CORRODED (FUSELAGE)
MZJ-EAC - FOUND RIGHT STATION 1460-1480 STRINGER 20R TO STRINGER 22R CORROSION UNDER WINDOW FORGING. REPAIRED PER ECRA 3203-053-047-2. (M)
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT STATION 300 TO 320 AND BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. CLEANED AND TREATED CORROSION PER SRM 51-10-01, SRM 56-20-01, 51-10-01, SRM 51-30-02, SOPM 20-10-03 PG 1-24, SOPM 20-41-02 PG 1.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT SIDE BETWEEN STATION 320 TO 340 WINDOW FORGING BETWEEN S-20R AND S-22R HAS CORROSION UNDER FORGING. REMOVED LIGHT SURFACE CORROSION PER B747 SRM 51-10-01. WINDOW FORGING IS FOUND TO BE WITHIN LIMITS PER B747 SRM 56-20-01.
Part: WINDOW FRAME — CORRODED (FUSELAGE) · airframe 85,973 hrs · 19,030 cycles
MAIN DECK RT FROM STA 360 TO 380 BETWEEN S-20R AND S-22R WINDOW FORGING HAS CORROSION UNDER FORGING. REMOVED, CLEANED CORROSION CHECKED LIMITS AND REINSTALLED WINDOW FORGING PER 747 SRM 51-10-01, SRM 56-20-01, SRM 51-10-02, 51-30-02, SOPM 20-10-03, SOPM 20-41-02, MM 56-21-01.
Part: PAN — CRACKED (FS 807)
MZJ-EAC - FOUND STATION 807 FORWARD UPPER EDGE L2 DOOR CUTOUT, DOOR FRAME PAN CRACKED. REPAIRED PER ECRA 3203-53-038-2. (M)
Part: SKIN — DAMAGED (RT WING)
MZJ-EAC - FOUND RIGHT WING L/W BULLNOSE DAMAGED AND LOOSE FASTENERS AT AFT WEB ANGLE. REMOVED DAMAGED BULLNOSE AND AFT ANGLE WEB LOOSE FASTENERS. FABRICATED NEW SPLICE ANGLE AND REPAIR DOUBLERS. INSTALLED NEW BULLNOSE, SPLICE ANGLES, AND REPAIR DOUBLERS PER SRM 51-30-02, 57-20-02, 51-40-02, 51-10-02 AND SOPM 20-41-02. (M)
Part: STRUCTURE — CORRODED (VERTICAL STAB)
MZJ-EAC - FOUND VERTICAL STAB INTERIOR CORROSION ON FORWARD FLANGE OF T-CHORD AT FIN STATION 570 RIGHT. FABRICATED AND INSTALLED CHORD PER B747 SRM 51-30-02 AND 51-10-02. (M)
Part: FLOORBEAM — MISDRILLED (FUSELAGE)
MZJ-EAC - FOUND FS 460 RBL 19 DOUBLE DRILLED HOLE IN FLOORBEAM AFT FLANGE. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD FROM BL 0 TO RBL 45, FABRICATED NEW UPPER CHORD SECTION 1 AND 2 SPLICE ANGLES, 3 STRAPS, 6 AND 7 FILLERS, AND INSTALLED PER SRM 53-10-07 FIG 8 AND 51-30-02. (M)
Part: STRUCTURE — CHAFED (NR 4 PYLON)
MZJ-EAC - FOUND NR 4 PYLON LOWER EDGE CHAFED BELOW REPAIR DOUBLER AT RIGHT OUTBOARD SIDE, AFT OF AFT ENGINE MOUNT. REPAIRED NR 4 PYLON PER ECRA 3203-54-024-2. (M)
Part: SPAR — CORRODED (FUSELAGE)
MZJ-EAC - FOUND WEB AT FINS STATION 570, 39 INCHES FROM LE, AND WEB FORWARD SPAR AT FIN STATION 570 CORRODED. INSTALLED FRONT SPAR WEB REPAIR AT STATION 570 PER B747 SRM 55-30-05 FIG 1. REPLACED INBOARD L-CHORD AND WEB ON LE RIB AT STATION 570 PER B747 SRM 51-20-01 AND 51-30-02. (M)
Part: FLOORBEAM — MISDRILLED (FUSELAGE)
MZJ-EAC - FOUND FS 474 RIGHT OUTBOARD FLOORBEAM NUTPLATE HOLE DOUBLE DRILLED AT RBL 90. REPAIRED BEAM PER B747 SRM 51-20-01 AND ECRA 3203-53-33-2. (M)
Part: FITTING — CRACKED (FUSELAGE)
MZJ-EAC - FOUND FS 660 RBL 117 WL 199 FLOORBEAM FITTING HAS .250 DIAMETER HOLE BROKEN OUT OF EDGE OF UPT T-CAP AFT FLANGE. REPAIRED FITTING PER ECRA 3203-53-20-2. (M)
Part: STRUCTURE — CRACKED (RT ELEVATOR)
MZJ-EAC - FOUND RIGHT INBOARD ELEVATOR, UPPER SURFACE LE CRACK AT RIVET HEAD, 24 INCHES OUTBOARD OF INBOARD EDGE. REPAIRED RIGHT INBOARD ELEVATOR PER ECRA 3203-55-035-2. (M)
Part: PANEL — CORRODED (KEELBEAM)
MZJ-EAC - FOUND SURFACE CORROSION EXT SURFACE 191JJ KEEL BEAM PNL AND CRACK AT ONE SCREW HOLE. FABRICATED AND INSTALLED NEW PANEL PER B747 SRM 51-20-01 FIG 7. (M)
Part: FORGING — CORRODED (FUSELAGE)
MZJ-EAC - FOUND LEFT STATION 1210 CORROSION ON AND AROUND WINDOW FORGING. REPAIRED PER ECRA 3203-53-047-2. (M)
Earlier reports · 1996–2000 · 247 reports
2000
Part: INDICATOR — FAILED (NR 4 ENG EPR)
PANC - FLT 1302 - NR 4 ENGINE EPR INDICATOR FAIL FLAG APPEARED AND AIRCRAFT LOST DIRECTIONAL STEERING DUE TO UNRELIABLE EPR INDICATION. ALL OTHER ENGINE PARAMETERS NORMAL. NR 4 ENGINE INSPECTED FOR FOD, NO ABNORMALITIES FOUND. (M)
Part: PDU — MALFUNCTIONED (TE FLAPS)
FLT 328 - VHHH - AFTER TAKEOFF, FLAPS 1 DEGREE NR 1 RT LED WOULD NOT RETRACT. ACCOMP ALT RETRACTION PROCEDURE NR 1 RT LED WENT TRANSIT BUT WOULD NOT RETRACT. ALT LED FLAP DRIVE C/B ON P6 PANEL TRIPPED WHEN ATTEMPT TO EXTEND LED FOR LANDING. GROUND CHECK OK. COULD NOT DUPLICATE PNEU MALFUNCTION. NR 1 RT LED ELECT ACTUATOR INOPERATIVE, DEACTIVATED. REPLACED NR 1 RT LED PER MM 27-81-03. RII ACCOMPLISHED. (M)
Part: SKIN — CRACKED (FUSELAGE)
HKG-HAECO - FOUND ON B-CHECK, AFT FUSELAGE SKIN BS 2733.89 LEFT WL 310-319 CRACKED. TRIMMED OFF CRACKED AREA, NDT INSPECTED PER NTM PT6, REPAIRED SKIN PER SRM 53-30-03. (M)
Part: SKIN — CRACKED (FWD CARGO DOOR)
HKG-HAECO - FOUND ON B-CHECK, FORWARD CARGO DOOR EXTERNAL SKIN LOWER EDGE CRACKED AND REPAIR DOUBLER PLATE BROKEN. CRACKED AREA TRIMMED OFF, NDT INSPECTED AND DOUBLER PLATE REPAIRED PER SRM 2-00-03. (M)
Part: BULKHEAD — CRACKED (FUSELAGE)
HKG-HAECO - FOUND ON B-CHECK, STATION 2460 LEFT B/H WEB CRACKED STRINGER 16 TO STRINGER 17. TRIMMED OFF DAMAGED AREA. NDT INSPECTED, CRACK FREE. BS 2460 LEFT FRAME WEB REPAIRED PER SRM 51-40-03 FIG 1 AND SRWS NR 917284. (M)
Part: FITTING — CRACKED (L1 DOOR)
HKG-HAECO - FOUND ON B-CHECK, L1 DOOR AFT FRAME NR 1 STOP FITTING CRACKED. HFEC INSPECTION COMPLIED WITH. FOUND CRACK, CONFIRMED APPROX 1 INCH IN LENGTH. STOP FITTING REPLACED PER SRM 51-10-01. (M)
Part: SKIN — CRACKED (L1 DOOR)
HKG-HAECO - FOUND ON B-CHECK, DR L1 MED UPPER HINGE CUTOUT LOWER CORNER CRACKED APPROX .875 INCH LONG. STOP DRILLED, HFEC INSPECTED PER NTM PT6-CRACK FREE. REPAIRED HINGE CUTOUT SKIN PER BSB 747-52-2144 FIG 3. (M)
Part: INVERTER — INOPERATIVE (ELECTRICAL)
KDAY - ON PREFLIGHT, FOUND STATIC INVERTER INOP. REPLACED STATIC INVERTER. (M)
Part: INVERTER — INOPERATIVE (ELECTRICAL)
KDAY - ON PREFLIGHT, FOUND STATIC INVERTER INOPERATIVE. REPLACED STATIC INVERTER. (M)
Part: O-RING — FAILED (APU)
KCLT - APU OIL QUANTITY FELL TO ZERO, ACCOMPANIED BY APU AUTO SHUTDOWN. REPLACED NR 1 GENERATOR SHAFT O-RING AND RESEATED SHAFT SEAL. OPS AND LEAK CHECKS NORMAL. (M)
1999
Part: ENGINE — STALLED (NR 1)
KCLT - NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT NORMAL CLIBM POWER THROUGH FL260. EGT OVER 1,000 FOR FIVE SECONDS. PRIOR TO STALL, ALL PARAMETERS NORMAL. ATTEMPTED ONE RESTART AND FOUND ENGINE DID NOT NORMALIZE, BUT WAS STABLE WITH HIGH EGT WITHIN LIMITS, AND OIL AND FUEL CONDITIONS NORMAL. SHUT DOWN ENGINE. WINDMILLING OIL PRESSURE 21 PSI. NO VIBRATION NOTED AT ANYTIME. FOUND HEAVY METAL DEPOSITS IN TAILPIPE UPON INSPECTION AT KCLT. (M)
Part: FRAME — CRACKED (BS 1265)
TLV - FOUND CRACK IN FRAME WEB AT STATION 1265 RIGHT JUST ABOVE FLOOR LINE. WEB REPLACEMENT PERFORMED AND INSTRUCTION OF THIS WORK NOTED IN JOB CARD NR 366-53-035M REF IAI SB 366-53-035. DRAWING R05366-53-15-15196-006. (M)
Part: SKIN — CORRODED (BS 660-700)
TLV - SWELLING ON EXTERNAL FUSELAGE WITH SHEARED RIVET BETWEEN STATION 660-700 BETWEEN STRINGER 41-43R. REPAIR DOUBLER INSTALLED IAW EO MF-MAN-B47-53-00-88832 REF, BOEING FAX MESSAGE M-7200-99-06866 DATED 8/5/99 AND SRM 53-30-03 FIG 1. (M)
Part: FRAME — CRACKED (BS 1265)
TLV - FOUND CRACK IN FRAME INNER CHORD AT STATION 1265 LEFT BELOW FLOOR LINE. WEB REPAIR PERFORMED AND INSTRUCTION DETAILED OF THIS WORK ARE NOTED IN EO MF-MAN-B47-53-88847 NEW REF BOEING SERVICE ENG MESSAGE M-7200-99-02111 8/12/99 AND M7200-99-07861 8/30/99. (M)
Part: CHORD — CRACKED (LT WING)
TLV - FOUND CRACK IN THE RADIUS OF THE UPPER CHORD OF LEFT WING STATION 669.5 INTERIOR FUEL TANK. CRACKED UPPER CHORD REMOVED. INSTALLED NEW UPPER CHORD IAW SB 57-2273-R2. (M)
Part: SKIN — CORRODED (WS 1360)
TLV - SWELLING ON RIGHT WING UPPER SKIN, UPPER SURFACE ABOVE FRONT SPAR AT WS 1360. PERFORMED REPAIR PER EO MF-MAN-B47-57-88838 NEW REF BOEING SERVICE ENGINEERING MESSAGE M-7200-99-07260 DATED AUGUST 16, 1999. INSTALLED DOUBLER. (M)
Part: SPAR WEB — CRACKED (LT WING)
TLV - DURING THE ACCOMPLISHMENT OF THE TERMINATING OF THE SB 747-57A2266 REV 6 CRACK FOUND AT FASTENER HOLES IN THE FRONT SPAR WEB STATION 660, COMMON TO THE LOWER CHORD. PERFORMED REPAIR IAW IAI EO MF MAN B47-57-88849 AND AS APPROVED BY FAA REPAIR 8110-3 ATTACHED. WEB REPAIR ACCOMPLISHED. (M)
Part: SUPPORT — CORRODED (BS 880)
TLV - SWELLING AND OPEN HOLES ON FAIRING SUPPORT AT LOWER FUSELAGE STATION 880 BETWEEN AREA RBL 15 TO RBL 27. SWOLLEN AREA TRIMMED OUT AND DEBURRED. REINFORCED AREA WITH 2 SUPPORTS(7075 T60 .080 THK) PER SRM 53-50-04, FIG 1. ALODINED AND EP PRIMER PROTECTED PER SRM 51-10-01. INSTALLED REPAIR WITH RIVETS PER SRM 51-30-02. (M)
Part: BULKHEAD — CRACKED (BS 140)
TLV - FOUND CRACKS ON PRESSURE BULKHEAD STATION 140 FORWARD SIDE, WL 305 APPROX L AND R BL 33. CRACKED AREA TRIMMED OUT. REINFORCED AREA WITH DOUBLERS AND FILLER 2024-T3 .050 PLUS .032 THK PER SRM 53-10-04 FIG 8D ALODINED AND EP PRIMER PROTECTED PER SRM 51-10-02 AND RIVETED PER SRM 51-30-00. (M)
Part: FITTING — CORRODED (BS 1480)
TLV - FOUND CORROSION ON THE OUTER CHORD SPLICE FITTING AT STATION 1480 LEFT SIDE. REPAIR STRAP INSTALLED IAW IAI EO MF-MAN-B47-53-88841 REV A DATED 9-9-99. (M)
1998
Part: WHEEL — DEPARTED (LT MLG)
DURING LANDING ROLL-OUT, LEFT BODY GEAR ANTI-SKID LIGHT CAME ON, AFTER FURTHER INVESTIGATION THE NR 5 TIRE ASSEMBLY WAS FOUND MISSING, AND THOUGHT TO HAVE DEPARTED AIRCRAFT UPON LANDING. (M)
Part: SKIN — CORROSION (RT WING)
RT WING LOWER SKIN NR 4 MAIN TANK AFT BOOST PUMP HOUSING CUTOUT FOUND HEAVY CORROSION. CORROSION REMOVED BLEND OUT NOT WITHIN SRM LIMIT 57-30-03. REPAIRED PER PAO HKG 98-0068TE AND 0070RE AND SRM 57-30-03 FIG 3.
Part: WEB — CORROSION (BS 1341-1349)
LEVEL 1 CORROSION LT WING GEAR W/W STA 1341-1349 UPPER BEAM WEB UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02 BLENDED OUT WITHIN SRM LIMITS 53-30-01.
Part: SKIN — CORROSION (BS 1350-1380)
LT BODY GEAR W/W STAT 1350-1380 LOWER FIXED PANEL FOUND CORROSION AT SKIN AND ANGLES. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-10-01.
Part: DOOR — CORROSION (LT MLG STRUT)
LT BODY GEAR STRUT DOOR INNER SKIN FOUND SURFACE CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 52-00-02.
Part: KEEL BEAM — CORROSION (LT MLG WW)
LEVEL 1 CORROSION AT LT BODY GEAR WHEEL WELL KEEL BEAM UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS 53-30-01.
Part: SUPPORT — CORROSION (BS 1346)
LT WING GEAR BEAM FWD SIDE WING FAIRING SUPPORT AFT FACE FOUND CORROSION AT STA 1346 WBL 148. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 BLENDED OUT WITHIN SRM LIMITS PER 53-10-01.
Part: SKIN — CORROSION (RT MLG WW)
RT WING GEAR W/W CEILING SKIN AT STA 1320 O/B FOUND CORROSION. REMOVED AND TREATED AS PER SRM 51-10-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-30-01.
Part: PANEL — DELAMINATION (HORIZ STAB)
LT HORIZ STAB LOWER T/E FIXED PANEL 334GBL FOUND DELAMINATION. HOT BOND REPAIRED PER SRM 51-40-06 PARA 3.
Part: BONDING JUMPER — CORROSION (NR 2 TANK)
LT WING REAR SPAR WEB HEAVY CORROSION AT ATTACHMENT OF BONDING JUMPER OF NR 2 TANK I/B JETTISON PUMP AREA. REMOVED CORROSION PER SRM 51-10-01 BLEND OUT NOT WITHIN LIMIT 57-10-01. REPAIRED PER BOEING PAO-HKG-98-0073RE-INSTALL FILLERS DOUBLERS AND TREAT AREA.
Part: ANGLE — CORRODED (BS 1370-1400)
FUSELAGE UPPER BODY FAIRING NR 294FR LOWER SUPPORT ANGLE BETWEEN BS 1370-1400 FOUND CORROSION AROUND FLOAT NUTS. CORROSION REMOVED PER SRM 51-01-01, BLEND OUT NOT WITHIN SRM LIMITS 53-10-01. REPAIRED PER SRM 51-40-04 FIG 3 AND TREATED PER SRM 51-10-02.
Part: SPLICE — CORROSION (BS 1438)
LEVEL 1 CORROSION FOUND AT LT BODY GEAR O/B SPLICE CHORD AT STA 1438. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-10-01.
Part: BRACE — WORN (NR 2 PYLON)
NR 2 ENG DIAGONAL BRACE WORN ON AFT END ON LT SIDE. AREA SMOOTHED OUT AND SHOT PEENED. NO CRACKS NOTED PER SRM 51-10-02, OHM 20-10-03, NDT PT 6 51-00-00 FIG 4.
Part: SUPPORT — CORROSION (BS 1130)
LEVEL 1 CORROSION, FOUND ON NUTPLATE SUPPORT RT STA 1130 AT UPPER WING TO BODY FILLET FAIRING AREA. CORROSION REMOVED AS PER SRM 51-10-01 AND TREATED AS PER 51-10-02.
Part: SUPPORT — CORROSION (BS 1620)
LEVEL 1 CORROSION, FOUND AT FUSELAGE BODY FAIRING SUPPORT AT BS 1620 LBL O THROUGH 60. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT AND REPAIRED PER 53-50-04.
Part: SKIN — CORROSION (WS 614-642)
LEVEL 1 CORROSION LT/W MIDSPAR W/S 614-642 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.
Part: SKIN — CORROSION (WS 660-680)
LEVEL 1 CORROSION FRONT SPAR AREA WS 660-680 UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.
Part: SKIN — CORROSION (BS 880)
LEVEL 1 CORROSION AT BS 880-900 ST 38L. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 51-10-02. BLEND OUT NOT WITHIN LIMITS PER SRM 53-110-01. STRINGER REPAIRED PER SRM 53-10-03 FIG 1.
Part: SKIN — CORROSION (WS 382-411)
LEVEL 1 CORROSION, FOUND LT WING MID SPAR AREA WS 382-411 AND WBL 150-235 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.
Part: SKIN — CORROSION (BS 2355)
LEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 2355 TO 2365 STR 46L TO 46R. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02 BLEND OUT WITHIN SRM LIMIT 53-30-01.
Part: SKIN — CORROSION (BS 942)
LEVEL 1 CORROSION FOUND AT RT STA 942 STR 44R. CORROSION REMOVED AND TREATES PER SRM 51-10-01, 51-10-02. BLEND OUT NOT WITHIN SRM LIMIT 53-10-01. REPAIRED PER SRM 53-10-03 FIG 1.
Part: ANGLE — CRACKED (BS 2598)
APU BATTERY COMPARTMENT BS 2598 STR 22-STR 23, LT SIDE FITTING FRAME CHORD ATTACH ANGLE FOUND CRACKED. ANGLE REPLACED PER SRM 51-10-01.
Part: SKIN — CORROSION (WS 440-455)
LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 440-455 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT WITHIN SRM LIMIT 57-30-01.
Part: SUPPORT — CORROSION (BS 1540)
FUSELAGE BODY FAIRING SUPPORT FOUND SLIGHT CORROSION AT BS 1540 LBL 60 - RBL 40. CORROSION REMOVED PER SRM 51-01-01. BLEND OUT NOT WITHING SRM LIMITS 53-10-01 FIG 1, BODY FAIRING SUPPORT REPAIRED PER SRM 53-50-01 AND TREATED PER SRM 51-10-02.
Part: DOOR — CRACK (LT MLG STRUT)
LT W/G I/B STRUT DOOR, FWD END FAIRING FWD EDGE FOUND FABRIC CRACK. FIBERGLASS REPAIRED AS PER SRM 51-40-06 APRA 2E.
Part: SUPPORT — CRACKED (NR 4 NOSE COWL)
NR 4 ENG NOSE COWL ANTI-ICE DUCT SUPPORT CRACKED AT STA 180. WELDING CARRIED OUT PER BAC 5975.
Part: ANGLE — CORROSION (FUSELAGE)
FUSELAGE ACCESS DOOR PANEL NR 192ER MID HINGE LOWER HALF ATTACH ANGLE FOUND CORROSION. ATTACH ANGLE REPLACED AS PER MM 20-50-01.
Part: PANEL — DELAMINATED (LT WING)
LT WING TOP T/E FIXED PANEL DEBONDED AND A PUNCH HOLD FOUND AT I/B AILERON I/B. FIBERGLASS REPAIRED AS PER SRM 51-40-15.
Part: BEAM — CORROSION (BS 1260)
LEVEL 1 CORROSION FOUND AT RT WING W/W O/B UPPER LONGITUDINAL BEAM WEB UPPER SURFACE AT STA 1260 WL 180. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-30-01.
Part: SKIN — DELAMINATION (RT TE MIDFLAP)
RT WING O/B MID FLAP I/B TOP ACCESS PANEL NR 687LT FOUND LOWER MID AREA SKIN CORROSION AND DELAMINATED. HOT BOND REPAIRS PER SRM 51-40-06 FIG 17.
Part: FRAME — CRACKED (BS 540)
UPPER DECK FRAME 540 FOUND CRACKED AT STR 7R AND 7AR AND 8R CUTOUT AREA. FRAME REPAIR AT U/D BS 540 STR 7R, 7AR AND 8R PER SRM 53-10-04 FIG 54.
Part: STATIC WICK — CORROSION (RUDDER)
UPPER RUDDER STATIC DISCHARGER 2ND AND 3RD FROM TOP FOUND WITH CORROSION ON ATTACH STRIP. STATIC CHARGE BASE 2ND AND 3RD REPLACED PER SRM 51-01-01.
Part: CABLE COVER — CRACKED (BS 1250)
MAIN DECK LT STA 1250 SIDEWALL UPPER CONTROL CABLE PULLEY METAL COVER FOUND MOUNTING BRACKET CRACK AND DEFORMED. MOUNTING BRACKET REPLACED AS PER SRM 51-10-01 AND SPEED BRAKE CABLE RIGGING CHECKED PER MM 27-62-02.
Part: FRAME — CRACKED (BS 640)
UPPER DECK FRAME 660 STR 7AL CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D BS 640 STR 7AL PER SRM 53-10-04 FIG 54.
Part: SKIN — DAMAGED (BS 500)
FUSELAGE SKIN DEEP LIGHTNING STRIKE MARK REVEALED AT STA 500 STR 36L. SKIN REPAIRED PER SRM 53-30-03 FIG 1.
Part: STABILIZER — CRACKED (RT HORIZ STAB)
RT HORIZONTAL STABILIZER SLOT SEAL CRACKED AT FWD LOWER AREA. FIBERGLASS REPAIR CARRIED OUT PER SRM 51-40-15.
Part: SUPPORT — CORRODED (BS 1620)
FUSELAGE BODY FAIRING SUPPORT FOUND SLIGHT CORROSION AT BS 1620 LBL 0 TO 60. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. REPAIRED PER SRM 53-50-04.
Part: SKIN — CORRODED (BS 1736)
LEVEL 1 CORROSION, FOUND BS 1736 STR 46R-49R FUSELAGE SKIN. CORROSION REMOVED PER SRM 51-10-01 AND TREATED PER SRM 51-10-02. BLEND OUT WITHIN SRM LIMIT 53-30-01.
Part: SKIN — CORROSION (WS 350-380)
LEVEL 1 CORROSION FOUND LEFT WING SPANWISE BEAM NR 3 AREA WS 350 - 380 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-70-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.
Part: SKIN — CORROSION (WS 520-530)
LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 520-530 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02. BLENDED OUT PER SRM 57-30-01.
Part: SKIN — CORROSION (WS 557-586)
LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 557-586 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT PER 57-30-01.
Part: FOREFLAP — DAMAGED (RT WING)
RT WING O/B FLAP NOSE AREA NR 8 FLAP TRACK I/B FOUND SPONGED AS MARKED APPROX 4 BY 6 INCHES. FIBERGLASS REPAIRED AS PER SRM 51-40-14.
Part: COWL — DISBONDED (NR 2 ENGINE)
NR 2 LEFT FAN COWL INTERNAL MIDDLE AREA HONEY COMB DISBONDED. HOT BOND REPAIRED AS PER SRM 51-40-06 FIG 17A. HOT BOND REPAIRED AS PER SRM 51-40-06 FIG 17A.
Part: FLAP — CRACKED (NR 3 LE FLAP)
LT WING NR 3 L/E FLAP INBD ACTUATING ARM NOSE AREA L/E NOSE BEAM RIB CHORD FLANGE AT LOWER END FOUND CRACK. NOSE BEAM RIB CHORD REPAIRED PER SRM 57-20-03.
Part: FOREFLAP — CORROSION (LT TE FOREFLAP)
LT WING INBD FORE FLAP I/B TOP SURFACE PANEL FOUND SURFACE CORROSION AT 3 LOCATIONS. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORROSION (LT WING)
LEVEL 1 CORROSION FOUND LT WING LOWER SKIN O/B SURFACE AT MID SPAR BETWEEN PANEL 554GB AND 555 AB. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS PER 57-30-01.
Part: SUPPORT — CORROSION (BS 1580)
LEVEL 1 CORRSOION, FOUND FUSELAGE BODY FAIRING SUPPORT AT BS 1580 LBL LEFT 0 THROUGH 245. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS 53-30-01.
Part: STRINGER — CORROSION (BS 910-920)
FWD CARGO COMPARTMENT BS 910-920 STRINGER FOUND CORROSION. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 REFSRWS 912817.
Part: STIFFENER — CRACKED (BS 1000)
FUSELAGE KEEL BOX ATTACH VERTICAL STIFFENER FOUND CRACKED AT BS 1000. STIFFENER REPAIRED AS PER SRM 51-10-01.
Part: BULKHEAD — CRACKED (BS 140)
FUSELAGE BS140 B/H FWD FACE FOUND CRACKED AT RBL 38 2 PLACES. WEB REPAIRED AS PER SRM 53-10-04 FIG 89.
Part: DOOR — DEBONDED (LT MLG STRUT)
LT W/G I/B STRUT DOOR AFT EXTERIOR SKIN FOUNDED DEBONDED AT I/B EDGE. FIBERGLASS REPAIRED PER SRM 51-40-06 PARA 2E.
Part: SKIN — CRACKED (BS 785)
ONE EACH CRACK FOUND ON THE FASTENER HOLE OF SKIN LONGITUDINAL LAP SPLICE AT BS 785 STR 392 OUTER SKIN AREA RUNNING FORWARD APPROX 0.51 LONG. RT STR 382 LAP REPAIRED AS PER SRM 53-30-03 FIG 17.
Part: COWL — DELAMINATED (NR 3 ENGINE)
NR 3 ENGINE INLET COWL LT SIDE PANEL AFT DELAMINATED. REPAIRED PER SRM 51-40-06.
Part: STRINGER — CORROSION (BS 1670-1682)
LEVEL 1 CORROSION, FOUND AFT CARGO COMPARTMENT BS 1670-1682 ST 44R. STRINGER REPAIRED IAW RS R-53-11-33645.
Part: SKIN — CORROSION (NR 3 FUEL TANK)
RT WING NR 3 MAIN FUEL TANK JETTISON PUMP CUTOUT AREA OF REAR SPAR BONDING ATTACH POINT CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 51-10-02. BLEND OUT WITHIN SRM LIMIT 57-10-01.
Part: TR SLEEVE — DAMAGED (NR 1 ENGINE)
NR 1 ENG FAN T/R TRANSLATING SLEEVE AT 9 O'CLOCK POSITION NEEDS REPAIR INSIDE AND OUTSIDE. FILLER REPAIRS CARRIED OUT PER SRM 51-40-06 PARA 2B.
Part: FAIRING — SPONGY (NR 2 CANOE)
LEFT WING NR 2 CANOE FAIRING MIDDLE LOWER AREA FOUND SPONGY. FIBERGLASS REPAIRED PER SRM 51-40-14.
Part: CHORD — CRACKED (BS 2598)
FUSELAGE BS 2598 B/H ATTACH CHORD FOUND CRACKED AT RT STR 11R - STR 12R RIVET HOLES. BULKHEAD CHORD REPAIRED PER SRM 51-40-04.
Part: FAIRING — SPONGED (RT WING)
RT WING #7 FIXED FAIRING MARKED AREA FOUND SPONGED. FIBERGLASS REPAIR AS PER SRM 51-40-15.
Part: WEB — CORROSION (BS 1241)
LEVEL 1 CORROSION FOUND LT W/G W/W INBD WEB AT STA 1241 WL 155. REMOVED AND TREATED AS PER SRM 5110-01, 51-10-02. BLEND OUT AND REPAIRED PER SRM 51-40-04.
Part: SKIN — CORROSION (LT WING)
LEVEL 1 CORROSION FOUND AT LT WING O/B LOWER SKIN T/E AREA PREVIOUS REWORK AREA O/B AILERON MID AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 BLEND OUT WITHIN SRM LIMIT 57-30-01.
Part: ANGLE — CORROSION (ACCESS DOOR)
FUSELAGE ACCESS DOOR 192M MID AND AFT HINGE LOWER HALF ATTACH ANGLE FOUND CORROSION. ANGLE REPLACED PER MM 20-50-01.
Part: FRAME — CRACKED (BS 600)
UPPER DECK FRAME 600 STR 8L CUTOUT AREA FOUND CRACKED. U/D BS 600 FRAME REPAIR AT STR 8L PER SRM 53-10-04 FIG 54.
Part: COWL — DENTED (NR 2 ENGINE)
NR 2 T/R FAN TRANSLATING COWL AT 9 O'CLOCK POSITION RT SIDE DENTED. REPAIRED AS PER SRM 51-40-00 PARA 2E.
Part: SKIN — CORROSION (WS 1112-1155)
LEVEL 1 CORROSION LT WING FRONT SPAR WS 1112-1155 UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01.
Part: FRAME — CRACKED (BS 680)
UPPER DECK FRAME 680 STR 7AL CUTOUT AREA FOUND CRACKED. DENT SMOOTHED OUT AND TREATED PER SRM 51-10-01 AND 51-10-02.
Part: FRAME — CRACKED (BS 720)
UPPER DECK FRAME 720 FOUND CRACKED AT STR 9R CUTOUT. FRAME REPAIRED AT UD BS 720 STR 9 R PER SRM 53-10-04.
Part: STRINGER — CORRODED (BS 884)
LEVEL 1 CORROSION FOUND AT RT STA 884 STR 44R. CORRSOION REMOVED PER SRM 51-10-01 BLEND OUT NOT WITHIN SRM LIMIT 53-10-03. STRINGER REPAIRED PER SRM 53-10-03 FIG 1 AND TREATED IAW SRM 51-10-02.
Part: SKIN — CORROSION (RT MLG WW)
RT WING W/W FWD RT CENTER TANK JETTISON PUMP BONDING JUMPER ATTACH POINT FOUND SKIN CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02 BLENDED OUT PER SRM 57-10-01.
Part: FRAME — CRACKED (BS 720)
STA 720 FRAME FOUND CRACKED AT STR 9L CUTOUT. FRAME REPAIRED AT U/D BS 720 STR 9L PER SRM 53-10-04 FIG 54.
Part: SKIN — DENTED (BS 2618)
DENT FOUND IN SKIN AND SUSPECT SKIN CRACK AT 6 O'CLOCK POSITION AT STA 2618. DENT AREA DRESSED PER SRM 51-10-01 AND TREATED PER SRM 51-01-02 AND CONDITION CHECK FOUND WITHIN SRM 53-30-01 LIMITS.
Part: FAIRING — SPONGY (LT WING)
LT WING I/B T/E FLAP INBD NR 4 CANOE FAIRING SEVEAL AREAS SPONGY DISBONDING AND PUNCHED HOLE FOUND. FIBERGLASS REPAIR PER SRM 51-40-14.
Part: SPLICE — CRACKED (BS 1350)
BS 1350 R/H/S OVERWING LONGERON SPLICE FITTING FOUND CRACKED. LONGERON SPLICE FITTING REPLACED IAW SRM 51-01-01.
Part: SKIN — DENTED (BS 2598)
DENT FOUND IN RT BODY SKIN AT 6 O'CLOCK POSITION ON SKIN AFT OF STA 2598 WL 212. DENT AREA PATCH REPAIRED AS PER SRM 53-50-03 FIG 4 AND SRWS 912822.
Part: FAIRING — DELAMINATION (FUSELAGE)
FUSELAGE BODY FAIRING EXTERIOR MID AREA FOUND DELAMINATION FAIRING 192KR. BODY FAIRING FIBERGLASS REPAIRED PER SRM 51-40-14.
Part: SKIN — CORROSION (WS 469-499)
LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREAS WS 469-499 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT PER 57-30-01.
Part: SPAR — CORROSION (HORIZ STAB)
LEVEL 1 CORROSION, FOUND INSIDE HORIZONTAL STAB REAR SPAR UPPER CHORD AND SKIN AREA AT RBL 43.5. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT PER SRM LIMIT 55-10-01.
Part: DOOR — DENTED (FUSELAGE)
DOOR 315AL AFT AREA AT RIB FOUND DENTED 12 INCHES LONG. DOOR 315 AL DRESSED PER SRM 51-10-01.
Part: SKIN — CORROSION (BS 1620-1680)
LEVEL 1 CORROSION FUSELAGE SKIN AT BS 1620 TO 1680 STR 40L STR 43R. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02 BLEND OUT WITHIN SRM LIMIT PER SRM 53-30-01.
Part: PANEL — CHIPPED (WS 890-917)
RT WING L/E UPPER FIXED PNL WS 890-917 T/E FABRIC PATCH FOUND CHIPPED AND GLASS REPAIRED AS PER SRM 51-40-15.
Part: COWL — DELAMINATION (NR 1 ENGINE)
NR 1 ENG NOSE COWL AT THE 5 O'CLOCK POSITION DELAMINATION. NR 1 ENG NOSE COWL ACCOUSTIC PANEL REPAIRED AS PER SRM 54-30-03 FIG 7 AND SRM 54-30-03 FIG 29A.
Part: FITTING — CORROSION (BS 1350)
LEVEL 1 CORROSION FOUND FUSELAGE RT OVERWING LONGERON SPLICE FITTING AT BS 1350, TAPER FILLER. TAPER FILLER REPLACED PER SRM 51-10-01.
Part: STIFFENER — CORRODED (BS 1050)
LEVEL 1 CORROSION, FOUND FUSELAGE BS 1050 RBL 10 KEEL BEAM O/B FACE ATTACH VERTICAL STIFFENER. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT WITHIN SRM LIMITS 53-10-01.
Part: FRAME — CRACKED (BS 620)
UPPER DECK FRAME 620 STR 7R CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D BS 620 STR 7R PER SRM 53-10-04 FIG 54.
Part: DOOR — DELAMINATED (RT MLG STRUT)
RT WING GEAR I/B STRUT DOOR AFT EDGE FOUND DISBONDED. FIBERGLASS REPAIRED PER SRM 51-40-06 PARAGRAPH 2.
Part: SKIN — DAMAGED (NR 3 ENG COWL)
NR 3 ENG NOSE COWL RT AFT LOWER ACOUSTIC PANEL OUTER SKIN DAMAGED, ACOUSTIC PANEL REPAIRED FIBERGLASS REPAIR PER SRM 51-30-02.
Part: SKIN — DENTED (RT TE FLAP)
RT /W INBD T/E FLAP AFT FLAP FOUND DENT MARK AT MID SECTION BOTTOM NR 5 AND NR 6 FLAP TRACK. FIBERGLASS REPAIRED PER SRM 51-40-15.
Part: SIDEWALL — CORROSION (RT MLG WW)
RT BODY GEAR W/W O/B SIDEWALL AT BS 1475 APPROX SPLICE PLATE LOWER ATTACH CHORD CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.
Part: BULKHEAD — CORROSION (NR 3 ENGINE)
LEVEL 1 CORROSION, FOUND ON NR 3 ENG BULKHEAD TO FIREWALL FWD LT CORNER AREA IN STRUCTURE (FWD ING MOUNT BULKHEAD STRUCTURE). SURFACE CORROSION REMOVED ON FWD BULKHEAD AT FIREWALL FWD LWR LT CORNER PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — CRACKED (SERVICE DOOR)
UD R/H/S CREW SERVICE DOOR FWD AND AFT CORNER CRACKED. SKIN REPAIR PER SRM 52-00-03 FIG 3.
Part: FLAP — SPONGED (RT TE AFT FLAP)
RT WIN O/B AFT FLAP FOUND ONE LOCATION SPONGED JUST O/B T/E LWR SURFACE. FIBERGLASS REPAIRED PER SRM 51-40-15.
Part: FAIRING — DELAMINATED (FUSELAGE)
FUSELAGE BODY FAIRING 193G AND 194G EXTERIOR LAYER FOUND CRACKED AND DELAMINATED. AREA REPAIRED PER SRM 51-24-11.
Part: FRAME — CRACKED (BS 640)
UPPER DECK FRAME 640 8R CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D STA 640 STR 84 SRM 53-10-04 FIG 54.
Part: SKIN — CORRODED (RT TE FOREFLAP)
RT WING I/B T/E FOREFLAP L/E LOWER SURFACE BETWEEN NR 5 AND NR 6 FLAP TRACKS HAS LIGHT SURFACE CORROSION ON SKIN PANEL. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 AND FILLER REPAIRED PER SRM 51-40-06.
Part: SILL — CRACKED (SERVICE DOOR)
U/D R/H/S CREW SERVICE DOOR LOWER DOOR SILL AREA FWD CORNER REVEAL FOUND CRACKED. FWD CORNER REVEAL REPLACED PER SRM 51-10-10 P 18.
Part: FAIRING — SPONGED (LT WING)
LT WING NR 2 FIXED FAIRING MARKED AREA FOUND SPONGED. NR 2 FIXED FAIRING FIBERGLASS REPAIRED AS PER SRM 51-40-15.
Part: SKIN — CORROSION (LT MLG STRUT DR)
LT WING GEAR O/B STRUT DOOR INNER SKIN LOWER EDGE FOUND CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — DISBONDED (LT TE FOREFLAP)
LT WING I/B FOREFLAP I/B PANEL FOUND SKIN DISBONDED AT CORROSION REWORK LOCATION 2 BY 10 INCHES. HOT BOND REPAIRED PER SRM 51-40-06 FIG 17 AND FIG 17A.
Part: FRAME — CRACKED (BS 600)
UPPER DECK FRAME 600 STR 7R AND 8R CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 600 STR 7R AND STR 8R PER SRM 53-10-04 FIG 54.
Part: FRAME — CRACKED (BS 700)
UPPER DECK STA 700 FRAME FOUND CRACKED AT STR 7AR AND 9R CUTOUT. FRAME REPAIRED AT U/D BS700 STR 7AR AND 9R PER SRM 53-10-01 FIG 54.
Part: SKIN — DENTED (BS 2000-2020)
BS 2000-2020 STR 33L -34L FUSELAGE SKIN FOUND DENT. AREA SMOOTHED OUT PER SRM 51-01-01, TREATED PER SRM 51-10-02, NO CRACK EVIDENT.
Part: FRAME — CRACKED (BS 540)
UPPER DECK FRAME 540 STR 7AL CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 540 STR 7AL PER SRM 53-10-04 FIG 54.
Part: DOOR — DISBONDED (RT MLG STRUT)
RT WING GEAR STRUT DOOR AFT EDGE FOUND DEBONDED. HOT BOND REPAIR PER SRM 51-40-06 FIG 17A.
Part: FRAME — CRACKED (BS 680)
UPPER DECK FRAME 680 STR 7AR AND 8R CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 680 STR 8R PER SRM 53-10-04 FIG 54.
Part: FRAME — CRACKED (BS 720)
UPPER DECK STA 720 FRAME FOUND CRACKED AT STR 8R CUTOUT. FRAME REPAIRED AT U/D BS 720 STR 8R PER SRM 53-10-04 FIG 54.
Part: FRAME — CRACKED (BS 580)
UPPER DECK FRAME 580 STR 6AL-7AL CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 580 STR 6AL AND 7AL PER SRM 53-10-04 FIG 54.
Part: SKIN — CORRODED (BS 1350)
LEVEL 1 CORROSION ON UPPER SURFACE PANEL IN RIGHT WING GEAR WHEEL WELL AT BS 1350, RBL 15 TO 90. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SPLICE — CORRODED (BS 1372)
LEVEL 1 CORROSION ON SPLICE PLATE IN RIGHT BODY GEAR WHEEL WELL AT BS 1372, WL 150. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01, 51-10-02.
Part: BRACKET — CORRODED (VENTRAL FIN)
LEVEL 1 CORROSION ON TWO L SHAPED BRACKETS ON THE HORIZONAL STABILIZER VENTRAL FIN TRAILING EDGE. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SPLICE — CORRODED (RT MLG WW)
LEVEL 1 CORROSION ON SPLICE PLATE OF OUTBOARD SIDEWALL IN RIGHT BODY GEAR WHEEL WELL AT S1475, WL 150. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: STRUT — CORRODED (LT MLG)
LEVEL 1 CORROSION ON LEFT WING GEAR SHOCK STRUT INNER CYLINDER LOWER PORTION. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SPLICE — CORRODED (BS 1438)
LEVEL 1 CORROSION ON THE SPLICE PLATE IN THE RIGHT BODY GEAR WHEEL WELL AT BS 1438, WL 150. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02.
Part: SKIN — CORRODED (RT MLG WW)
LEVEL 1 CORROSION ON UPPER SURFACE SKIN IN THE RIGHT BODY GEAR WHEEL WELL OUT BOARD OF GEAR RETRACT ACTUATOR FITTING. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — DEBONDED (LT TE FOREFLAP)
DEBONDED AREA ON UPPER SKIN OF INBOARD FOREFLAP INBOARD TRAILING EDGE. MADE FIBERGLASS REPAIR PER BAC SRM 51-40-14.
Part: SKIN — CORROSION (RT MLG WW)
LEVEL 1 CORROSION IN RIGHT BODY GEAR OUTBOARD WHEEL WELL INTERIOR SKIN. REMOVED CORROSION AND TREATED AS PER BAC SRM 51-10-01 AND 51-10-02.
Part: PANEL — CORRODED (NR 13 LE FLAP)
LEVEL 1 CORROSION ON NUMBER 13 LEADING EDGE FLAP INBOARD CORNER INTERNAL PANEL. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (RT ELEVATOR)
DELAMINATION OF FIVE AREAS ON UPPER SURFACE OF THE RIGHT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.
Part: SKIN — CORRODED (WS 724-752)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 724 TO 752. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (BS 440-586)
LEVEL 1 CORROSION, ON UPPER SKIN OF RIGHT WING REAR SPAR AREA AT WS 440 TO 586. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 1516-1548)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN FROM WS 1516 TO 1548 FROM MID SPAR TO REAR SPAR. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 1308-1336)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 1308 TO 1336. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1105-1115)
LEVEL 1 CORROSION ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1105 TO 1115. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 1364-1392)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 1364 TO 1392. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: BULKHEAD — CORRODED (BS 2658)
LEVEL 1 CORROSION, ON THE FORWARD SIDE OF THE APU BULKHEAD AT STATION 2658, RIGHT BODY LINE 512. CORROSION REMOVED AND AREA TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (WS 382-420)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 382 TO 420. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS PER SRM 57-30-01.
Part: SKIN — DELAMINATED (HORIZ STAB)
DELAMINATION IN SEVERAL OUTBOARD AREAS ON RIGHT HORIZONTAL STABILIZER TRAILING EDGE FIXED PANEL. TRIMMED DAMAGE PER BAC SRM 51-10-01 AND MADE FIBERGLASS REPAIR PER SRM 51-40-06.
Part: SKIN — CORRODED (WS 1010-1050)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1010 TO 1050. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 889-917)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 889 TO 917. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1392-1482)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1392 TO 1482. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1210-1240)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1210 TO 1240. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 1270)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 1270 TO 1290. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1265-1285)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 1265 TO 1285. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1224-1252)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1224 TO 1252. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: PANEL — CORRODED (HORIZ STAB)
LEVEL 1 CORROSION, ON THE UPPER SURFACE OF ALL TRAILING EDGE FIXED PANELS ON THE RIGHT HORIZONTAL STABILIZER. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (WS 1168-1224)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN WBL 834 FROM MID TO REAR SPAR AT WS 1168 TO 1224. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1252-1280)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1252 TO 1280. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1336-1392)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1336 TO 1392. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (RT WING)
LEVEL 1 CORROSION OF THE UPPER WING SKIN AT WBL 834 FROM MID SPAR TO REAR SPAR. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN THE LIMITS OF SRM 57-30-01.
Part: SKIN — DENTED (BS 1760/1780)
DENT ON FUSELAGE SKIN AT BS 1760 TO 1780, STR 41R AND 42R. BLENDED DAMAGED AREA PER BAC SRM 51-40-01 AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION, NO CRACKS FOUND.
Part: SKIN — CORRODED (WS 917-944)
LEVEL 1 CORROSION, ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 917 TO 944. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1252-1282)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 1252 TO 1282. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 807-834)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 807 TO 834. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS PER SRM 57-30-01.
Part: SKIN — DELAMINATED (LT ELEVATOR)
DELAMINATION ON SEVERAL AREAS OF LEFT OUTBOARD ELEVATOR UPPER SURFACE. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.
Part: BULKHEAD — CRACKED (BS 140)
CRACKED ON BODY STATION 140 BULKHEAD AT LBL 38. REPAIRED AREA WEB PER BAC SRM 53-10-06.
Part: SKIN — CORRODED (WS 469-499)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 469 TO 499. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 353-411)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 353 TO 411. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (HORIZ STAB)
LEVEL 1 CORROSION, DELAMINATION AND CRACK ON LEFT HORIZONTAL STABLIZER INBOARD TRAILING EDGE FIXED PANEL. DAMAGED AREA TRIMMED PER BAC SRM 51-10-01 AND FIBERGLASS REPAIR MADE PER SRM 51-40-06.
Part: SKIN — CRACKED (HORIZ STAB)
CRACK ON RIGHT HORIZONTAL STABILIZER TRAILING EDGE FIXED PANEL INBOARD AREA. TRIMMED DAMAGE PER BAC SRM 51-10-01 AND MADE FIBERGLASS REPAIR PER SRM 51-40-06.
Part: SKIN — DELAMINATED (RT ELEVATOR)
DELAMINATION ON SEVERAL AREAS OF THE RIGHT OUTBOARD ELEVATOR UPPER SURFACE. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.
Part: SKIN — CORROSION (RT WING)
LEVEL 1 CORROSION, ON UPPER SURFACE OF LOWER WING SKIN IN LEADING EDGE CAVITY FORWARD OF FRONT SPAR. CORROSION REMOVED AND AREA TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (HORIZ STAB)
CORROSION INSIDE CENTER SECTION OF THE HORIZONTAL STABILIZER BETWEEN STRINGERS 54 AND 55, STAB RIGHT BODY LINE 15 TO 43.5. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (WS 411-469)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 411 TO 469. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 499-557)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 499 TO 557. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1320-1485)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1320 TO 1485. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (RT WING)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 1336)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1336 TO 1485. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 1485-1548)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1485 TO 1548. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — DELAMINATED (LT ELEVATOR)
DELAMINATION ON UPPER SURFACE OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.
Part: SKIN — CORRODED (WS 1175-1190)
LEVEL 1 CORROSION, ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 1175 TO 1190. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1224-1252)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 1224 TO 1252. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1280-1336)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1280 TO 1336. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CORRODED (WS 1423-1485)
LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 1423 TO 1485. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: PANEL — CORRODED (HORIZ STAB)
LEVEL 1 CORROSION, ON UPPER SURFACES OF ALL TRAILING EDGE FIXED PANELS ON LEFT HORIZONTAL STABIBLIZER. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: BULKHEAD — DEFORMED (BS 2658)
DEFORMATION AT 6 O'CLOCK POSITION ON APU FIRE BULKHEAD AT STATION 2658. DRESSED OUT DEFORMED AREA PER BAC SRM 51-10-01.
Part: SKIN — CORRODED (WS 1240-1270)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1240 TO 1270. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: SKIN — CORRODED (WS 1130-1252)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1130- TO 1252. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SKIN — CRACKED (LT ELEVATOR)
CRACK ON UPPER SURFACE OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15.
Part: SKIN — CORRODED (WS 900-920)
LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE REFUEL AREA AT WS 900 TO 920. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS.
Part: FAIRING SUPPORT — CORRODED (BS 1175)
LEVEL 1 CORROSION ON AIR CONDITIONING ACCESS PANEL SUPPORT AT BS 1175 TO 1235, LBL 60. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (WS 1056-1110)
LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1056 TO 1110. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01.
Part: SUPPORT — CORRODED (BS 1175 - 1235)
LEVEL 1 CORROSION ON FUSELAGE AIR CONDITIONING BAY ACCESS PANEL SUPPORT AT BS 1175 TO BS 1235. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: ANGLE — CORRODED (BS 920 - 950)
LEVEL 1 CORROSION ON BODY FAIRING LONGITUDINAL SUPPORT ANGLES AT BS 920 TO 950, LBL 5 TO RBL 5. REPLACED SUPPORT ANGLES PER BAC SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 1350 - 1480)
LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL SUPPORT AT BS 1350 TO BS 1480. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (LAV SERVICE DOOR)
LEVEL 1 CORROSION ON MID LAVATORY SERVICE DOOR CUTOUT SKIN. CORROSION REMOVED AND TREATED PER BAC SRM 51-10-01, 51-10-02.
Part: SKIN — DENTED (BS 1730 - 1740)
DENT ON FUSELAGE SKIN AT FROM BS 1730 TO 1740, S38R TO 39R. SMOOTHED OUT DAMAGED AREA AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN LIMITS OF SRM 53-30-01.
Part: SKIN — DEFORMED (BS 1460 - 1480)
DEFORMATION IN FUSELAGE SKIN AT BS 1460 TO 1480, S32L TO S34L. DAMAGED AREA SMOOTHED AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 53-30-01 LIMITS.
Part: ANGLES — CORRODED (BS 880 - 910)
LEVEL 1 CORROSION ON FUSELAGE BODY FAIRING LONGITUDINAL SUPPORT ANGLES AT BS 880 TO 910, LBL 5 TO RBL 5. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1215 - 1235)
LEVEL 1 CORROSION ON FUSELAGE ACCESS PANEL 191KL UPPER SUPPORT CHANNEL AT S 1215 TO BS 1235. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1235)
LEVEL 1 CORROSION ON FUSELAGE AIR CONDITIONING BAY ACCESS PANEL SUPPORT AT BS 1235, LBL 100 TO RBL 60. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1235 - 1255)
DENT ON ON FUSELAGE SKIN FORWARD OF ACCESS PANEL 192NR FROM BS 1235 TO 1255. CORROSION REMOVED AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: ACCESS PANEL — CORRODED (BS 1160 - 1175)
LEVEL 1 CORROSION ON AIR CONDITIONING BAY ACCESS PANEL AT BS 1160 TO 1175, LBL 60. CORROSION REMOVED AND TREATED PER BAC SRM 51-10-01, 51-10-02.
Part: ANGLE — CORRODED (FUSELAGE)
LEVEL 1 CORROSION ON FUSELAGE ACCESS DOOR 191AL FORWARD HINGE ATTACH ANGLE. REPLACED ATTACH ANGLE PER BAC MM 20-51-01.
Part: SUPPORT — CORRODED (BS 880)
LEVEL 1 CORROSION ON BODY FAIRING SUPPORT AT S 880, BL 0 TO RBL 12. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — DEBONDED (LT TE FLAP)
DEBONDED AREA ON LEFT INBOARD TRAILING EDGE FORE FLAP SKIN. REPAIRED PER BAC SRM 51-40-15.
Part: WEB — CORROSION (LT ELEVATOR)
LEVEL 1 CORROSION ON LEFT OUTBOARD ELEVATOR OUTBOARD WEB. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (BS 840)
LEVEL 1 CORROSION ON FUSELAGE SKIN AT BS 840, LBL 4 TO RBL 4. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02.
Part: SKIN — DENTED (NR 11 FLAP)
DENT ON NUMBER 11 LEADING EDGE FLAP BULL NOSE SKIN. REPAIRED PER BAC SRM 51-40-01 AND TREATED PER SRM 51-10-02.
Part: SKIN — CORROSION (LT ELEVATOR)
LEVEL 1 CORROSION ON THE LEFT OUTBOARD ELEVATOR UPPER SURFACE. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02.
Part: ACCESS PANEL — CORRODED (KEEL BEAM)
LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL191GG. CORROSION REMOVED AND TREATED PER BAC SRM 51-10-01, 51-10-02.
Part: FAIRING — DELAMINATED (FUSELAGE)
FUSELAGE BODY FAIRING 1920 FOUND PUNCTURE HOLE AND DELAMINATION. BODY FAIRING FIBERGLASS REPAIRED PER SRM 51-40-15.
1997
Part: ENGINE — STALLED (NR 4)
DURING CLIMB, NUMBER 4 ENGINE INDICATED LOW THRUST AND APPEARED TO BE STALLED. RESTARTED ENGINE. ENGINE OPERATED NORMAL FOR REMAINDER OF FLIGHT. PERFORMED CHECKS PER M/M 71-00-42 AND FOUND ALL NORMAL. REPLACED MAIN ENGINE FUEL FILTER PRECAUTIONARY, LEAK CHECK OK.
Part: HINGE — BROKEN (NR 1 PACK DOOR)
LEVEL 2 CORROSION NR 1 PACK EXIT DOOR PANEL 2ND HINGE FOUND BROKEN. REPLACED HINGE ASSY ON DOOR AS PER SRM 51-30-02. ACCOMPLISHED REPAIR ON NR 1 AND NR 3 HINGE MOUNT AS PER POLAR MA NR 531210.
Part: HINGE — BROKEN (NR 2 PACK ACCESS)
LEVEL 2 CORROSION NR 2 PACK ACCESS PANEL NR 3 HINGE BROKEN. REPLACED NR 1, NR 2 AND NR 3 HINGE ASSYS AS PER SRM 51-30-02.
Part: STRAP — BROKEN (NR 3 PACK ACCESS)
LEVEL 2 CORROSION NR 3 PACK ACCESS PANEL STRAP BROKEN. FABRICATED AND INSTALLED NEW STRAP AS PER SRM 51-10-01.
Part: TORQUE TUBE — BROKEN (LT LE FLAP)
ON POST FLIGHT WALKAROUND, FOUND NR 4 LEFT WING LEADING EDGE FLAP HANGING DOWN. REPLACED BROKEN TORQUE TUBE ASSEMBLY FROM DRIVE ACTUATOR TO SCREW JACK PER BOEING M/M 27-81-05 PAGE 401 TO 407. OPERATIONAL CHECK GOOD.
Part: LIGHT — BROKEN (RT TAIL LIGHT)
BROKEN RT TAIL (STABILIZER) LIGHT HOUSING. FABRICATED LIGHT ASSY SHROUD AND INSTALLED AS PER SRM 51-10-01.
Part: SELECTOR VALVE — CRACKED (LT MLG)
NR 1 HYDRAULIC QUANTITY WENT TO 0 DURING TAXI IN. FOUND LEFT LANDING GEAR SELECTOR VALVE HOUSING CRACKED. REPLACED LEFT LANDING GEAR SELECTOR VALVE PER M/M 32-31-03.
Part: HYDRAULIC TUBE — CRACKED (HORIZ STAB)
NR 1 HYDRAULIC SYSTEM LOST QUANTITY AFTER LANDING. FOUND DAMAGED TUBE ON LEFT OUTBOARD ELEVATOR POWER PACKAGE. REPLACED TUBE OPERATIONAL AND LEAK CHECK PER MM 27-31-08.
Part: RELAY — LOOSE (E/E COMPT)
EMERGENCY LIGHTS SHOW UNARMED WHEN ON OR ARMED. RESEATED K1 AND K2 RELAYS OPERATIONAL CHECK NORMAL PER M/M 33-51-00.
Part: BRG VENT DUCT — SHEARED (NR 4 ENGINE)
NR 4 ENGINE NR 3 BEARING VENT DUCT RIGHT SIDE SHEARED AT CLAMP LOCATION. REPLACED VENT DUCT PER M/M 75-22-01.
Part: CHIP DETECTOR — MISSING (NR 3 ENGINE)
NR 3 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE, OIL QUANTITY LOW AND INCREASING OIL TEMPERATURE. ENGINE SHUT DOWN AT 23:30 LANDED 22:48 UTC 5 PSI OIL PRESSURE UNTIL LANDING. DURING INSPECTION OF ENGINE FOUND CHIP DETECTOR PLUG FOR ANGLE GEAR BOX IN BOTTOM OF COWLING. INSPECTED CHIP DETECTOR NO DEFECTS NOTED. REPLACED PACKINGS INSTALLED DETECTOR AND SERVICED OIL. COMPLETED WINDMILL INSPECTION PER MAINTENANCE MANUAL 72-00-00, NO DEFECTS NOTED.
Part: SKIN — DELAMINATED (LT ELEV TE)
LEFT HAND INBD ELEVATOR INBD TRAILING EDGE AT CORNER IS SEPARATED. CLEANED DAMAGED AREA, APPLIED FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09. PAINTED REPAIRED AREA IAW MM 57-24-11.
Part: SKIN — DENTED (RT LE FLAP)
DENT ON RIGHT WING LEADING EDGE FLAP PANEL 16. REPAIRED PER BAC SRM 51-30-02.
Part: SKIN — DELAMINATED (LT ELEV TE)
LEFT HAND OUTBD ELEVATOR TRAILING EDGE IN CENTER IS SEPARATED. CLEANED DAMAGED AREA, APPLIED FIBERGLASS OVERLAYS, PER BOEING SRM 51-40-09. PAINTED REPAIRED AREA IAW MM 57-24-11.
Part: BRACKET — BROKEN (NR 2 PYLON)
NR 2 PYLON ATTACH BRACKET BROKEN, I/B INTERNAL RIB, BY ACCESS PANEL 462BL. REMOVED AND REPLACED BRACKET PER BOEING SRM 51-30-02 AND FABRICATED PER SRM 51-10-01.
Part: SKIN — DELAMINATED (RT ELEV TE)
RIGHT HAND INBD ELEVATOR INBD TRAILING EDGE IS SEPARATED. REMOVED DAMAGE APPLIED FIBERGLASS OVERLAYS PER BOEING SRM 51-40-09. PAINTED AREA IAW MM 57-24-11.
Part: CADC — MALFUNCTIONED (NR 1)
CAPTAINS ALTIMETER 900 FT LOW AT FL 370, STANDBY MODE NO HELP, MACH NR'S .4 LOW, TRUE AIRSPEED LOW 30 KNOTS, ALTERNATE STATIC SOURCE NO HELP. REMOVED AND REPLACED NR 1 CADC PER MAINTENANCE MANUAL 34-12-01 PAGE 401. OPERATIONAL CHECKED PER MAINTENANCE MANUAL 34-12-00 PAGE 501. LEAK CHECKED PER MAINTENANCE MANUAL 34-11-00 PAGE 501.
Part: PANEL — DELAMINATED (LT WING)
DELAMINATION ON LEFT WING UPPER PANEL 521AT. REPAIRED PER BAC SRM 51-40-15.
Part: CADC — FAILED (RT COCKPIT)
FIRST OFFICER'S ALTIMETER READS 300 FT HIGH AT 31,000 FEET, MACH METER READS .03 HIGH, AND IAS READS NORMAL. REPLACED CADC IAW MAINTENANCE MANUAL 34-12-01 PG 401, OPERATIONAL CHECK PER 34-12-00 PG 508-5.
Part: FAIRING — CRACKED (NR 3 ENGINE)
CRACK NR 3 ENGINE DOGHOUSE JUST AFT OF LEADING EDGE 2 INCHES LONG. REPAIRED PER BOEING SRM 54-50-03.
Part: NOSE COWL — DELAMINATED (NR 4 ENGINE)
NR 4 ENGINE NOSE COWL INLET AT 2 O'CLOCK POSITION OLD REPAIR DELAMINATED 12 BY 12 AREA. REPLACED NOSE COWL PER WORK CARD M7111-001.
Part: EXHAUST SLEEVE — CRACKED (NR 3 ENGINE)
NR 3 ENGINE EXHAUST SLEEVE CRACKED WITH LOOSE AND MISSING RIVETS. REPAIRED PER BOEING SRM 54-30-03 FIGURE 11.
Part: FAN BLADES — WORN (NR 4 ENGINE)
NR 4 ENGINE FAN BLADES ARE SHINGLING (EXCESSIVE AXIAL MOVEMENT AT BLADE ROOT). REPLACED COMPLETE SET OF 46 BLADES PER WORK CARD M7220-001.
Part: SEAL DEPRESSOR — CHAFED (NR 2 PYLON)
NR 2 PYLON SAILBOAT INBOARD SIDE CHAFING DIAGONAL BRACE ON FORWARD END OF THE BRACE AND DOOR LIP. TRIMMED 1 RADIUS IN SEAL DEPRESSOR, CHECKED CHAFING OK PER BOEING SRM 51-40-01, EDDY CURRENT CHECKED PER NDT MANUAL 51-00-00 RESTORED FINISH.
Part: TIRE — FAILED (NR 9)
FOUND NR 9 TIRE RECAP HAD COME OFF AND THE TIRE FLAT. CHANGED NR 9 AND NR 10 TIRES PER BOEING M/M 32-45-01. PERFORMED INSPECTION PER MAINTENANCE MANUAL 5-51-25. FOUND BODY GEAR DOOR STRUT BENT. REPLACED PER BOEING M/M 32-14-00.
Part: FAIRING — DELAMINATED (FUSELAGE)
DELAMINATED BODY FAIRING PANEL, 2ND PANEL BEHIND ADF PANEL RT SIDE NR 194CR. REPAIRED PANEL PER BOEING SRM 51-40-07.
Part: PANEL — DAMAGE (FUSELAGE)
DAMAGED PANEL AT 1650 4TH PANEL BEHIND ADF PANEL RT SIDE NR 194FR. REPAIRED PANEL PER BOEING SRM 51-40-07.
Part: HINGE — FAILED (RT MLG DOOR)
ON PREFLIGHT, FOUND RT BODY GEAR OUTBOARD STRUT DOOR MISSING. FOUND MIDDLE AND AFT HINGE SHEARED AT HINGE POINT FORWARD IN TACT. REPLACED DOOR, HINGES, AND ACTUATOR ROD PER BOEING MAINTENANCE MANUAL 32-14-06 ADJUSTED PER 32-14-00.
Part: PANEL — DAMAGED (FUSELAGE)
DAMAGED NR 2 ADF PANEL. REMOVED AND REPLACED PANEL PER BOEING SRM 51-10-01.
Part: FAIRING — DAMAGED (FUSELAGE)
DAMAGED 2 EACH BODY FAIRING PANELS AFT OF NR 2 ADF PANEL RIGHT SIDE. REPAIRED PANELS PER BOEING SRM 51-40-07.
Part: ENGINE — FAILED (NR 2)
IN CRUISE, NR 2 ENGINE OIL FILTER BYPASS LIGHT CAME ON. ENGINE PULLED BACK TO IDLE, OIL TEMP BEGAN TO RISE, SHUTDOWN ENGINE AT 148 DEGREES. INSPECTED, FOUND OIL BLACK AND GUMMY. ACCOMPLISHED BOEING M/M PROCEDURE 71-00-44. ON ENGINE RUN UP, OIL COMING FROM TAIL PIPE AND DIFFUSER SEAMS. REPLACED ENGINE PER POLAR AIR CARGO FORM M 7100-002.
Part: TURBINE — FAILED (NR 3 ENGINE)
NR 3 ENGINE COMPRESSOR STALLED ON TAKEOFF AT NAN 140 KTS, EGT PEGGED OUT HIGH. REPLACED ENGINE PER POLAR AIR ENGINE CHANGE WORK CARDS.
Part: BREATHER — CRACKED (RT ENGINE)
NR 2 ENGINE BREATHER EXHAUST IS CRACKED. CRACK WELDED, REPAIRED PER P AND W 70-42-1 OVERHAUL MANUAL CHPT 4. ALUM. INSP REPAIR PER NDT PART 6, 54-10-01. NO CRACK FOUND.
Part: SKIN — CORRODED (WS 411.42)
DURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION IN THE RIGHT WING TRAILING EDGE UPPER SKIN PANEL NR 1, AT WS 411.42. BLENDED AWAY THE CORROSION, ROTOPEENED THE AFFECTED AREA, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER. ACCOMPLISHED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N3203Y-57-009-EAC.
Part: BRACE — CHAFED (NR 4 PYLON)
DURING C-CHECK INSPECTION, DISCOVERED CHAFING MARKS ON THE NR 4 POSITION DIAGIONAL BRACE. REMOVED WEAR MARKS BY BLENDING PER SRM 54-40-01, FIG 3, AND SHOTPEENED AFFECTED AREA. RESTORED FINISH. ACCOMPLISHED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N3202Y-54-006-EAC. (M)
Part: SLOPING PRESS DK — CORRODED (BS 1253.68)
DURING C-CHECK INSPECTION DISCOVERED CORROSION ON THE SLOPING DECK AT STATION 1253.68 AND LBL 11.3. THE CORROSION AFFECTED THE BONDED PRESSURE WEB ASSEMBLY 65B07992-111 OUTER AND INNER MEMBERS AND THE HORIZONTAL MOST OUTBOARD FLANGE OF A 'T' MEMBER AT LBL 11.33. TRIMMED OUT AFFECTED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS, ANGLES AND FILLERS. ACCOMPLISHED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N3203Y-53-007-EAC. (M)
1996
Part: CHIP DETECTOR — LEAKING (NR 1ENG GB)
FLT NR VR966 - GRU-MEX - NR 1 ENGINE HIGH OILCONSUMPTION AT TOP OF DESCENT QTY SHOWED 2 GALLONS PRESSURE DROPPED TO 30PSI AND WAS FLUCTUATING, SHUTDOWN ENGINE, TOTAL WINDMILLING TIME 28 MINUTES. PERFORMED WINDMILL INSPECTION. NO DAMAGE NOTED. SERVICED ENGINE OIL.ENGINE RUN REVEALED ACCESSORY GEAR BOX CHIP DETECTOR LEAKING. REPLACED AGBCLIP DETECTOR. ENGINE RUN OPS CHECKS OK. (M)