N794AX
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.
93 reports on file, 2002-08-26 – 2017-11-27.
Part: SENSOR — MALFUNCTIONED (RT ENGINE) · airframe 57,538 hrs · 44,649 cycles
PASSING THROUGH FLIGHT LEVEL 230, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. THE CREW COULD NOT RESTORE NORMAL ENGINE OPERATION VIA THE QUICK REFERENCE HANDBOOK PROCEDURES. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE RIGHT ENGINE'S MAIN ENGINE CONTROL (MEC), HYDROMECHANICAL FAN INLET TEMPERATURE (T2) SENSOR, AND THE COMPRESSOR INLET TEMPERATURE (CIT) SENSOR WERE REPLACED. THE CAUSE OF THE COMPRESSOR STALLS WAS A FAULTY MEC, T2 SENSOR, AND/OR CIT SENSOR.
Part: STATOR VANE — OUT OF ADJUST (LEFT ENGINE) · airframe 57,537 hrs · 44,648 cycles
DURING CLIMB THROUGH FLIGHT LEVEL 200, THREE LOUD BANGS OCCURRED THAT JOLTED THE AIRCRAFT. THE AIRPLANE SEEMED TO YAW EACH TIME. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE LEFT ENGINE'S VARIABLE STATOR VANE SYSTEM WAS OUT OF ADJUSTMENT. THE VARIABLE STATOR VANE CABLE WAS REPLACED AND THE VARIABLE STATOR VANE SYSTEM WAS ADJUSTED.
Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 57,537 hrs · 44,647 cycles
RIGHT ENGINE HAD A COMPRESSOR STALL. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE FAULT ISOLATION MANUAL DIAGRAM 71-05, FAULT TREE 808 WAS ACCOMPLISHED. ALL FINDINGS WERE WITHIN LIMITS. THE CAUSE OF THE COMPRESSOR STALL IS UNKNOWN.
Part: FLOORBEAM — CORRODED (BS 1109) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORROSION ON THE FORWARD SIDE OF THE FLOOR BEAM CHORD AT FUSELAGE STATION 1109, LBL 46, IN THE AFT LOWER CARGO COMPARTMENT. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: RIB — CRACKED (RT WING) · airframe 57,536 hrs · 44,646 cycles
CRACK IN RIGHT WING NOSE RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: TEE FITTING — CORRODED (BS 1541-1562) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, RBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: TEE FITTING — CORRODED (BS 1541-1562) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORROSION ON THE LOWER SURFACE OF UPPER CABIN FLOOR SUPPORT TEE FROM FUSELAGE STATION 1541 TO STATION 1562, LBL 80. THE SUPPORT TEE WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: STRINGER — CORRODED (BS 434) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORROSION ON STRINGER 32L AT FUSELAGE STATION 434. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.
Part: TEE FITTING — CORRODED (HORIOZNTAL STAB) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORROSION ON THE ATTACH TEE AT THE REAR SPAR/UPPER RIB INTERSECTION OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE TEE WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORRODED NUT PLATES ON THE RIGHT WING LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: STRINGER — CRACKED (BS 676) · airframe 57,536 hrs · 44,646 cycles
CRACK IN STRINGER 5L AT SPLICE. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.
Part: FITTING — CRACKED (FUSELAGE) · airframe 57,536 hrs · 44,646 cycles
CRACK IN FRAME TO STRINGER ATTACH CLIP AT STA 1702. THE ATTACH CLIP WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: RIB — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORROSION ON UPPER RIB CHORD OF THE LEFT HORIZONTAL STABILIZER AT HORIZONTAL STABILIZER BUTT LINE 357.442 LEFT. THE CHORD WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 57,536 hrs · 44,646 cycles
CORROSION IN RIGHT LOWER AIR LOAD RIB. THE RIB WAS REPLACED. AIRPLANE WAS GROUNDED.
Part: CARABINER — MISSING (FORWARD CABIN) · airframe 57,429 hrs · 44,586 cycles
TWO EMERGENCY DESCENT SAFETY HARNESS CARABINERS WERE MISSING FROM THEIR STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), TWO NEW SAFETY HARNESS CARABINERS WERE INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINERS IS UNKNOWN.
Part: WIRE — SHORTED · airframe 56,978 hrs · 44,368 cycles
DURING TAXI, EICAS MESSAGE FOR THE LT REVERSER ISOLATION VALVE DISPLAYED AND THE THRUST REVERSER INDICATION CIRCUIT BREAKER TRIPPED OPEN. THE AIRPLANE WAS REMOVED FROM SERVICE. THE CAUSE OF THE EICAS MESSAGE AND TRIPPED CIRCUIT BREAKER WAS WIRE W756-503-24 WAS SHORTED TO GROUND AND BURNED AT BS 303. THE WIRE WAS REPAIRED.
Earlier reports · 2002–2016 · 77 reports
2016
Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 55,554 hrs · 43,688 cycles
LOWER FASTENER HOLE IN RT FAILSAFE COMMON TO T FITTING IS CRACKED, VERIFIED BY HFEC HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IAW DOCUMENT 47008ORD04, THAT IS ATTACHED TO JC EA 53500014-003 FOR WORK STEPS TAKEN. CRACKED LENGTH .125", PN 145T2524-22, PART NAME FAILSAFE STRAP, SN NSN, EXACT FS & BS LOCATION ON ACFT AT STATION 955, EXACT STRINGER & WS LOCATION ON ACFT AT WL 178. ACFT WAS GNDED.
Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 55,554 hrs · 43,688 cycles
LEFT FAILSAFE LOWER HOLE COMMON TO T FITTING HAS CRACK INDICATION, VERIFIED BY HFEC ROTARY HOLE SCAN. TRIMMED OUT CRACK ON FAILSAFE STRAP COMMON TO T FITTING IAW DOCUMENT 47008ORD03, THAT IS ATTACHED TO JC EA 53500013-003 FOR WORK STEPS TAKEN. CRACKED LENGTH 125", PN 145T2524-21, PART NAME FAILSAFE STRAP, SN NSN, EXACT FS & BS LOCATION ON ACFT AT STATION 955, EXACT STRINGER & WS LOCATION ON ACFT AT WL 178. ACFT WAS GNDED.
2015
Part: FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
NUMBER 9, COUNTED FROM FRONT, MAIN DECK CARGO DOOR LATCH CAM PIN FITTING HAS CORROSION IN THE BORE. REMOVED, REPAIRED & RE-INSTALLED NR 9 LATCH PIN & LATCH PIN FITTING IAW REA B652-61882-MR & AMM SUPP 52-32-00. SDR INFO, CORRODED LEVEL 2, PN 368-53-00-95347-203, PART NAME LATCH FITTING, SN NSN, FS & BS LOCATION L588 TO L588, STRINGER & WS LOCATION LBL 89. ACFT WAS GNDED.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
LEFT WING SURFACE CORRODED AFT OF OVERWING EXIT AT WING TO BODY FAIRING AT APPROX STATION 938. REMOVED CORROSION & REPAIRED AREA IAW REA B657-61841-MR. SDR INFORMATION, CORRODED LEVEL 2, PN 112T3229-11, SN N/A, PART NAME RIB CHORD, EXACT FS & BS LOCATION ON ACFT FROM FS 938, EXACT STRINGER & WS LOCATION ON ACFT FROM WBL 97.5 UPPER WING SKIN. ACFT WAS GNDED.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
SUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 1025. REPAIRED CORRODED AREA ON RT WING AT REAR SPAR & WS 1030 IAW REA B657-61825-MR. REINSTALLED FIXED PANELS IAW SRM 51-40-02 & REA 657-61825. REPAIR AREA TO BE PAINTED ON NR 1241. FUEL PANEL 652BB TO BE LEAK CHECKED ON NR 1239. SDR INFORMATION, CORRODED, LEVEL 2, PN 112T3101-6, SN NSN, PART NAME UPPER WING SKIN. ACFT WAS GNDED.
Part: SKIN — CORRODED (RT WING) · airframe 55,039 hrs · 43,448 cycles
SUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 912. REMOVED PANELS, REMOVED CORROSION & NDT INSPECTED. PERFORMED REPAIR ON REA B657-61824-MR. REINSTALLED PANELS IAW SRM 51-40-02 & REA B657-61824-MR. TOUCH UP PAINT TO BE DONE ON NR 1241. DANGER TAG REMOVED. SDR INFORMATION, CORRODED, PN 112T3101-6, PART NAME SKIN, SN NSN, EXACT FS & BS LOCATION ON ACFT FROM RT WING TO TE. EXACT STRINGER & WS LOCATION ON ACFT FROM WS 908 TO WS 914. ACFT WAS GNDED.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
MID FREQUENT EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
MID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER TS4 & TS5, RS23, INBD OF APU SHROUD. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS23. ACFT WAS GNDED.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
MID FREQUENCY EDDY CURRENT DEFECT INDICATION 1 EACH FASTENER MIDWAY, BETWEEN TS4 & TS5, RS17 INBD ROW. REPAIRED ON REA B653-61835-MR. CRACKED LENGTH .100, PN 148T2610, PART NAME AFT PRESS BULKHEAD, FS & BS LOCATION TS4 - 5, RS17. ACFT WAS GNDED.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
LEFT 1809 FWD OUTER CHORD INBD FLANGE AT OTBD FASTENER BELOW SPLICE FITTING CRACKED APPROX 1.5". HFEC VERIFIED IAW NDTM PART 6 51-00-19. REMOVED & REINSTALLED ANGLES & ATTACH BRACKETS TO FACILITATE REPLACEMENT OF LT 1809 OUTER CHORD IAW SRM 51-40-02 PARA 7D & 9B. THE 1809 LT OUTER WILL BE REPLACED ON EA 53800001-003. CRACKED 1.5", PN 148T2740-0, SN N/A, PART NAME LT OUTER CHORD, ACFT WAS GNDED.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
CORROSION SUSPECTED AT LT WING REAR SPAR WS 854. BLEND OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA 657-61837-MR, WS 810-815. BLEND OUT & TRIM OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA B657-61838-MR, WS 850 - 859. SDR INFORMATION CORRODED LEVEL 2, PN 112T3101-5, PART NAME SKIN, SN N/A. EXACT FS & BS LOCATION ON ACFT FROM WS 810 TO WS 854 UPPER SKIN TE. ACFT WAS GNDED.
Part: SUPPORT BEAM — CORRODED (TR WING) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
RIGHT WING TE UPPER PANEL SUPPORT AT WS 1052 IS CORRODED. REMOVED CORRODED PANEL SUPPORT BEAM & INSTALLED NEW FABRICATED BEAM REV NO 61536-0000-0005 & REA NO B657-61840 IAW SRM 51-40-02 GENERAL PG 7 PARA 70. CORRODED LEVEL 2, PN 113T1913024, PART NAME PANEL SUPPORT BEAM, SN NSN, EXACT STRINGER & WS LOCATION ON ACFT, FROM WS 1031 TO WS 1079 RT WING TE UPPER PANEL SUPPORT. ACFT WAS GNDED.
Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
RIGHT WING SKIN UPPER TE IS CORRODED UNDER PANEL 113T1651 AT WS 512 - 521. CORROSION UNDER UPPER WING TRAILING EDGE PANEL WAS REPAIRED ON REA B657-61823-M. PANEL WAS REPAIRED ON NR-0468 & REINSTALLED ON NR-0682. CORRODED LEVEL 2, PN 112T3101-6, PART NAME SKIN PLANK, SN N/A, FS & BS LOCATION FROM WS 512 TO WS 521, UPPER TE OF SKIN. ACFT WAS GNDED.
Part: SUPPORT — CORRODED (RT AILERON) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
RIGHT WING TE OTBD AILERON, HINGE SUPPORT RIB AT WS 1079.95 HAS CORROSION ON THE UPPER CHORD OF THE SUPPORT ASSEMBLY. REMOVED CORRODED CHORD & REPLACED WITH NEW FABRICATED UPPER CHORD REF REA B657-51827, IAW SRM 51-40-02 PG 2 PARA 4B & 51-40-02 PG 7 PARA 7D. CORRODED LEVEL 2, PN 113T1521-84, SN NSN, PART NAME CHORD, EXACT STRINGER & WS LOCATION ON ACFT FROM RT WS 1079.95. ACFT WAS GNDED.
Part: BRACKET — CRACKED (LE SLAT) · airframe 55,039 hrs · 43,448 cycles
NUMBER 6 SLAT LOWER TE ATTACH ANGLE, OUTBOARD OF CTR AUX TRACK, IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION, CRACKED, LENGTH .250, PN 14T3166Y111, SN N/A, PART NAME BRACKET, EXACT FS & BS LOCATION ACFT, FROM ISS 274, EXACT STRINGER & WS LOCATION ON ACFT NR 6 SLAT. ACFT WAS GNDED.
Part: ATTACH ANGLE — CRACKED (LE SLAT) · airframe 55,039 hrs · 43,448 cycles
NUMBER 6 SLAT LOWER TE ATTACH ANGLE, LOCATED OUTBOARD OF OUTBOARD AUX TRACK IS CRACKED. R & R ATTACH ANGLE, INSTALLED FASTENERS IAW SRM 51-40-02 PARAGRAPH 7D & 9B. SDR INFORMATION CRACKED LENGTH .250, PN 114T3166-71, SN N/A, PART NAME ANGLE, EXACT FS & BS LOCATION ON ACFT FROM ISS 327, EXACT STRINGER & WS LOCATION ON ACFT NR 6 SLAT. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
UPPER CARGO STRINGER 19L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 19L, STATION 698 - 720 IAW ENGINEERING SKETCH NO ESO2821 REV A & 767 - 200 SRM 53-00-03 REPAIR 1 DETAIL II. CRACKED 0.5", SN N/A, PART NAME STRINGER, EXACT FS & BS LOCATION ON ACFT FROM FS 676, EXACT STRINGER & WS LOCATION ON ACFT FROM STRINGER 1L. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
UPPER CARGO STRINGER 7L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED CRACKED LONGERON STRINGER 7L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES 02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, PART NAME STRINGER, SN N/A, EXACT FS & BS LOCATION ON ACFT FROM FS 676 - 708. EXACT STRINGER & WS LOCATION ON ACFT FROM STRINGER 7L. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
UPPER CARGO STRINGER 17L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. CONTACT ENGINEERING FOR REPAIR. REPAIRED CRACKED LONGERON STRINGER 17L, FS 676 - 708 IAW ENGINEERING SKETCH NR ES02821 REV A & SRM 53-00-03 REPAIR 1. CRACKED 0.5", PN 143T3001, SN N/A, PART NAME STRINGER, EXACT FS & BS LOCATION ON ACFT FROM FS 676 - 708, EXACT STRINGER & WS LOCATION ON ACFT STRINGER 17L. ACFT WAS GNDED.
Part: CHANNEL — CORRODED (LT WING) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
WING TE PANEL ATTACH LOWER CHANNEL SPLIT ON EDGE AT TE WS 936. REMOVED DAMAGED CHANNEL, NEW CHANNEL FABRICATED REA B657-61805 & INSTALLED NEW CHANNEL IAW SRM 51-40-02 & REA B657-61805. CORRODED LEVEL 2, PN 113T1912-3, PART NAME CHORD CHANNEL, SN NSN, FS & BS LOCATION FROM LT WING LOWER TO TE STRINGER & WS LOCATION FROM WS 1079 - 936. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
FORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE. REPAIRED STRINGER 21L AT FS. 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED 4.75", EXACT FS & BS LOC ON ACFT 676 - 707, EXACT STRINGER & WS LOC ON ACFT STRINGER 21L. ACFT WAS GNDED.
Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
AT OPENING ABOVE LT LG, AFT WING PANEL ATTACH BEAM CORRODED AROUND NUTPLATE. REMOVED CORRODED PANEL ATTACH BEAM, DRILLED FOR LOCATION & INSTALLED IAW SRM 51-40-05 TABLE 3 & 51-40-02-7. CORRODED LEVEL 2, PN 113T1632-197, SN N/A, PART NAME RIB TE PANEL SUPPORT, WS 197.4 UPPER AFT TE. ACFT WAS GNDED.
Part: STRUCTURE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
HORIZONTAL STABILIZER S10 UPPER AFT FLANGE AT RIB 2R OUTBOARD CORROSION. BLENDED AREA WITHIN LIMITS TO REMOVE CORROSION IAW SRM 51-10-02. SDR INFO, CORRODED LEVEL 2, STRINGER & WS LOCATION, FROM STRINGER 10 TO RIB 2R. ACFT WAS GNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,039 hrs · 43,448 cycles
FORWARD LOWER CARGO STRINGER 21L IS CRACKED, AT STATION 676, AFT OF FRAME AT SPLICE, CONTACT ENGINEERING FOR REPAIR. REPAIRED STRINGER 21L AT FS 676 - 707 IAW SRM 53-00-03 FIG 201 REPAIR 2 & NEA 53100137-201. PN 143T3001, PART NAME STRINGER, SN NSN, CRACKED 4.75", EXACT FS & BS LOCATION ON ACFT 676 - 707, EXACT STRINGER & WS LOCATION ON ACFT STRINGER 21L. ACFT WAS GNDED.
Part: BEAM — CRACKED (NR 2 PYLON) · airframe 55,039 hrs · 43,448 cycles
NUMBER TWO STRUT INTERIOR STRUCTURE IS CRACKED WHERE PANEL 447ERX ATTACHES AT LOWER EDGE. R & R NR 2 PYLON HYD BAY OTBD BEAM WHERE PANEL 447ERX ATTACHES IAW SRM 51-40-02. CRACKED 1.0", PN 313T1380-242, PART NAME BEAM, AFT FAIRING OTBD, SN NSN, STRINGER & WS LOCATION FROM 344.3 TO 345.3. ACFT WAS GNDED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,039 hrs · 43,448 cycles
CORROSION FOUND ON LT LOWER KEEL CHORD STATION 952. CLEANED UP CORROSION ON LT LOWER KEEL CORD AT FS 952 IAW SRM 53-50-12 ALLOWABLE DAMAGE 1 FIG 101. CORROSION IS WITHIN ALLOWABLE LIMITS. SDR INFO, CORRODED LEVEL 2, PN 145T8610-5005, PART NAME KEEL CORD, SN NSN, FS & BS LOCATION FS 952, STRINGER & WS LOCATION LBL 9.5. ACFT WAS GNDED.
Part: SWITCH — OUT OF TOLERANCE (CARGO DOOR) · airframe 54,240 hrs · 42,950 cycles
MAIN CARGO DOOR LIGHT & SIREN ILLUMINATED DURING CLIMB OUT AT APPROXIMATELY 2.0 TO 2.1 PSID. INDICATION SWITCHES GAP ADJUSTED TO TOLERANCE & E1-1 BURNDY BLOCK CLEANED. WORN DOOR MECHANISM CAUSING SWITCH GAP TO FALL OUT OF TOLERANCE.
2014
Part: SUPPORT — CORRODED (RT WING) · airframe 53,140 hrs · 42,315 cycles
HINGED PANEL 651TB OTBD LOWER PANEL ATTACH CHANNEL SPLIT ON EDGE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED BEAM, REPAIRED IAW REA B657-60865, PN 113T1623-40, SN N/A, PART NAME UPPER SUPPORT, LOCATION RTW WS 358 AFT OF REAR SPAR. ACFT WAS GROUNDED.
Part: STRUCTURE — CORRODED (RT WING) · airframe 53,140 hrs · 42,315 cycles
TRAILING EDGE PANEL 652HB AFT ATTACH BEAM LOWER CHORD SPLIT ON EDGE. REPLACED LOWER CORD AT PANEL 652HB AFT ATTACH IAW SRM 51-40-02 PER 4 & 7. SDR INFO CORRODED, PN 113T1407-2, SN N/A, PART NAME CHORD LOWER, FUSELAGE & BODY STATION, LOCATION FROM WS 412 TO WS 431 AFT OR REAR SPAR. ACFT WAS GROUNDED.
Part: BEAM — CORRODED (RT WING) · airframe 53,140 hrs · 42,315 cycles
REAR SPAR TO TE PANEL ATTACH BEAM SPLIT ON INBD SIDE LOWER CHORD AT STATION 257, 20 INCHES FROM REAR SPAR. REPLACED REAR SPAR TO TE PANEL ATTACH BEAM IAW SRM 51-40-02. SDR INFO CORRODED, PN 113T1622-9, SN N/A, PART NAME CHORD, BEAM LOWER, STRINGER & WING STATION, LOCATION WS 257. ACFT WAS GROUNDED.
Part: SKIN — CORRODED (RT WING) · airframe 53,140 hrs · 42,315 cycles
RIGHT WING TRAILING UPPER WING SKIN IS CORRODED 40 INCHES OTBD OF FUSE AT FWD EDGE OF PANEL 651 FT. BLENDED CORROSION AS DESCRIBED IAW SRM 51-20-01, AREA BLENDED IS WITHIN LIMITS IAW ENGINEERING DISPOSITION ON ENTRY NR 8. UPSIZED TWO FASTENER HOLES COMMON TO BLENDED AREA. SEE REA B657-60853-MR FOR HOLE PREPARATION & FASTENER INSTALLATION. SDR INFO PN 112T3101-6, PART NAME UPPER WING SKIN, CORRODED, WS LOCATION ON ACFT FROM 156 T0 193 WING UPPER SKIN ABOVE SPAR. ACFT WAS GROUNDED.
Part: FORMER — CRACKED (RT WING) · airframe 53,140 hrs · 42,315 cycles
RIGHT WING LE NOSE BEAM FORMER IS CRACKED AT THE NR 8 SLAT INBD AUXILIARY TRACK INBD SIDE. REMOVED DAMAGED NOSE FORMER & INSTALLED NON-NOSE FORMER IAW SRM 51-40-02. SDR INFO CRACKED .750 INCHES, PN 114T2200-6, SN NSN, PART NAME FORMER, NOSE BEAM, LOCATION OSS 437 RT. ACFT WAS GROUNDED.
Part: SUPPORT BEAM — CORRODED (SPOILER) · corrosion level 2 · airframe 53,140 hrs · 42,315 cycles
LEFT WING UPPER SURFACE, BULGE IN PANEL JUST FWD OF NR 5 SPOILER CTR OTBD FITTING. FOUND SPOILER SUPPORT BEAM TO BE CORRODED BEYOND LIMITS. FABRICATED NEW BEAN PN 654T0391-3 IAW REA B657-60857-MR & REPAIRED NEW BEAM IAW REA B657-60862-MR. INSTALLED BEAM IAW SRM 51-40-02 PAR 4 & 7. SDR INFO CORRODED LEVEL 2, PN 654T0391-3, SN N/A, PART NAME CHORD UPPER, LOCATION FROM LWB L355 TO LWBL 247. ACFT WAS GROUNDED.
Part: ANGLE — CORRODED (LT MLG WW) · airframe 53,140 hrs · 42,315 cycles
CORROSION FOUND BETWEEN STATION 999 & STATION 1021 IN LT WW BEHIND MAIN GEAR DOOR ACTUATOR ON CTR BEAM. CLEANED LT WW BEHIND MLG DOOR ACTUATOR FS 999 - 1021, FOUND ANGLE PN 145T8601Y37 CORRODED. REPLACED IT WITH A NEW PART IAW SRM 51-40-02 PARA 7. SDR INFO PN 145T8601Y37, SN N/A, PART NAME ANGLE, LOCATION FS 1021, LBL 0-8, CORROSION. ACFT WAS GROUNDED.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,140 hrs · 42,315 cycles
CORROSION ON KEEL WEB FLANGE LBL 12 AT STATION 959 & 993. BLENDED CORROSION ON LT KEEL BEAM STATION 965 - 969 & STATION 981 - 999 AREAS BLENDED OUT OF LIMITS IAW SRM 53-50-12. SEE REA B653-60852-MR FOR COMPLETION OF REPAIRS. SDR INFORMATION CORRODED, PN 145T8611-5, SN N/A, PART NAME KEEL BEAM, FUSELAGE STATION FROM 959 TO 970, LBL FUSELAGE STATION 981 - 999 LBL. ACFT WAS GROUNDED.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,140 hrs · 42,315 cycles
CORROSION FOUND AFT OF STATION 977 IN LT WW CTR BEAM. BLENDED CORROSION ON LT KEEL BEAM OTBD FLANGE STATION 958 - 977 AREA BLENDED FOUND TO BE OUT OF LIMITS IAW SRM 53-50-12. SEE REA B653-60856-MR FOR COMPLETION OF REPAIR. SDR INFORMATION CORRODED, PN 145T8611-5, SN, PART NAME KEEL BEAM, FUSELAGE STATION FROM 958 TO 977. ACFT WAS GROUNDED.
Part: BRACKET — CORRODED (APU BAY) · airframe 53,140 hrs · 42,315 cycles
APU COMPARTMENT FWD FIREWALL NYLON DOOR STOP BRACKET & HARDWARE ARE CORRODED. FABRICATED NEW BRACKET ON REA B653-60850 & INSTALLED FABRICATED BRACKET IAW SRM 51-40-02. SDR INFO PN 148T6513-1, SN NA, PART NAME BRACKET, LOC STATION 1832, CORRODED. ACFT WAS GROUNDED.
Part: SUPPORT BRACKET — CHAFED (LT WING) · airframe 53,140 hrs · 42,315 cycles
SUPPORT BRACKET FOR OVERWING PANEL IS CHAFED ON TOP INBD SIDE BY INBD FWD SIDE OF LT INBD AILERON. R & R INBD UPPER PANEL SUPPORT BEAM FWD SIDE OF LT INBD AILERON IAW SRM 51-40-02. SDR INFO PN 113T1944-49, SN NA, PART NAME BEAM, LOCATION WS 437 TO WS 447, CHAFE DAMAGE BEYOND LIMITS. ACFT WAS GROUNDED.
Part: STRUCTURE — CORRODED (RT WING) · airframe 53,140 hrs · 42,315 cycles
REAR SPAR TO TE PANEL ATTACH BEAM UPPER CHORD SPLIT ON EDGE AT STATION 285, 50 INCHES FROM REAR SPAR. REMOVED OLD UPPER CORD & INSTALLED NEW UPPER CORD FROM REAR SPAR TO TE PANEL ATTACH BEAM AT STATION 285, IAW SRM 51-40-02. SDR INFO CORRODED, PN 113T1623-158, SN NA, PART NAME CHORD, UPPER LOCATION 50 INCHES FROM RT WING TE AT STATION 285. ACFT WAS GROUNDED.
Part: RIB — CORRODED (RT WING) · airframe 53,140 hrs · 42,315 cycles
JUST OTBD OF TELESCOPING DUCT INBD SIDE THE INBD SUPPORTING BRACKET AT TE CORRODED. INSTALLED A NEW LE BRACKET AT R/W TAI DUCT LOCATION & INSTALLED TELESCOPING DUCT FROM LE & DUCT AT OFSS 446.00 IAW SRM 51¬40-02 & AMM 30-11-05-4. LEAK CHECK PERFORMED, CHECKED GOOD, NO LEAKS NOTED. SDR INFO CORRODED, PN 114T2202-8, PART NAME 2 E RIB STRINGER & WING STATION LOC RW WS 456. ACFT WAS GROUNDED.
Part: FORMER — CORRODED (RT WING) · airframe 53,140 hrs · 42,315 cycles
RIGHT WING NR 8 SLAT TAI DUCT CURTAIN INBD ATTACH BRACKET COMMON TO THE LE NOSE BEAM IS CORRODED. R & R NOSE FORMER & AIR LOAD RIB IAW SRM 51-40-02 PARA 4 B & 51-20-02 PARA 5 B. SDR INFO PN 114T2202-20, SN N/A, PART NAME FORMER, LOC AT 0SS 456 CORROSION. ACFT WAS GROUNDED.
Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 53,140 hrs · 42,315 cycles
NUMBER 1 PYLON STRINGER HAS CRACKED INTERNAL Z ANGLE M PANEL. NR 1 PYLON STRINGER Z ANGLE ON PANEL 437BB IAW SRM 51-40-02 PARA 6B & DWG 015T0322. SDR INFO PN 015T0322-11, PART NAME Z ANGLE, SN NSN, CRACKED LENGTH 1 INCH, STRINGER & WING STATION LOC ON ACFT NAC WL 137.58 TO NAC WL 158.00. ACFT WAS GROUNDED.
2013
Part: UNKNOWN — ODOR (CABIN) · airframe 52,904 hrs · 41,614 cycles
A STRONG BURNING ODOR COMING THROUGH THE A/C POSSIBLY THE RT PACK. RAN THE LT & RT PACKS FOR ONE HOUR THROUGH HOT AND COLD RANGE PER AMM 21-00-00-2, ACFT WAS GROUNDED. FOUND NO EVIDENCE OF ANY BURNING SMELLS. NOTE - JUST PRIOR TO TAKEOFF FROM CVG AIRCRAFT HAD BEEN DE-ICED.
2012
Part: SEAL — CORRODED (FUSELAGE) · airframe 51,479 hrs · 41,247 cycles
LEFT WING EMERGENCY EXIT SEAL CORRODED AT BOTTOM OF OPENING. REPAIRED BLENDED AREA IAW REA NO B653-59852-M. ACFT WAS GROUNDED.
Part: FILLER — LOOSE (FUSELAGE) · airframe 51,479 hrs · 41,247 cycles
LEFT EMERGENCY OVERWING EXIT HAS COMPOUND DETACHED AT THE LOWER AFT CORNER. FILLING COMPOUND REPLACED ON REA 653-59852-MR REF BOEING DWG 140T4500. ACFT WAS GROUNDED.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,479 hrs · 41,247 cycles
UPPER S-7L CRACKED ON LEFT SIDE O/B OF RIB 2L. REPLACED SECTION OF CRACKED STRINGER IAW B767 SRM 51-40-02, 51-10-03, AND DWG 182T3100, ACFT WAS GROUNDED.
Part: STRUCTURE — CORRODED (STAB) · airframe 51,479 hrs · 41,247 cycles
CORROSION UPPER 10 L STR 12 O/B OF RIB 2L FWD FLANGE UPPER SURFACE IN HORZ STAB BOX. CLEANED AREA OF CORROSION EXCEEDING LIMITS IAW B767 SRM 55-10-03 FIG 101. AREA REPAIR COMPLETED IAW ABX REA B655-59861-MR AT LOCATION UPPER LEFT STRINGER 10 AT LS STA 12.0, ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,479 hrs · 41,247 cycles
CORROSION UPPER SL-11L I/B SIDE OF RIB 2L FWD FLANGE UPPER SURFACE. REMOVED AND REPLACED S-11L ON UPPER SIDE OF RIB 2L IAW B767 SRM 51-40-02. ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,479 hrs · 41,247 cycles
CORROSION UPPER NR 11R STR O/B OF RIB 2R AFT FLANGE UPPER SURFACE. REMOVED AND REPLACED NR 11R STRINGER ON O/B SIDE OF RIB 2R IAW B767 SRM 51-40-02. ACFT WAS GROUNDED.
Part: STRINGER — CORRODED (ZONE 400) · airframe 51,479 hrs · 41,247 cycles
CORROSION LWR 10 L STRINGER 4" O/B RIB 2 L UPPER FWD FLANGE LWR SURFACE 2 AREAS IN HORZ STAB BOX. CHECKED AREA OF CORROSION EXCEEDING LIMITS IAW B767 SRM 55-10-03 FIG 101 AREA REPAIR COMPLETED IAW ABX REA B655-59861-MR, LOCATION HORZ STAB, LOWER LEFT STRINGER #10 AT STA 4, ACFT WAS GROUNDED.
Part: CLOSEOUT PANEL — CORRODED (LT WING) · airframe 51,479 hrs · 41,247 cycles
LEFT WING, LEADING EDGE CLOSE OUT PANEL BETWEEN SLAT AND AUX TRACKS CORRODED WS 775. REMOVED AND REPLACED CLOSE OUT PANEL, INSTALLED HI-LOKS & RIVETS IAW 767 SRM 51-40-02. ACFT WAS GROUNDED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,479 hrs · 41,247 cycles
UPPER CARGO FLOORBEAM CORRODED JUST I/B OF L1 ENTRY DOOR. REPAIRED FLOORBEAM IAW B767 SRM 53-00-51-REPAIR, AT STA 303, LBL 11.0". ACFT WAS GROUNDED.
Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 51,479 hrs · 41,247 cycles
SHEAR TIE CORRODED AFT SIDE OF FRAME FS 566, S37R - 38R. REMOVED AND REPLACED DAMAGE SHEAR TIE IAW BAC DWG 143T1206 AND B767 SRM 51-40-02, ACFT WAS GROUNDED.
Part: PANEL — DAMAGED (RT WING) · airframe 51,479 hrs · 41,247 cycles
FASTENER PULLED THROUGH RT WING TRAILING EDGE PANEL AT WS 798.2 FWD SAFETY LINE ATTACH POINT PLACARD. REPAIRED IAW REA# B657 54841-MR. ACFT WAS GROUNDED.
2011
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,831 hrs · 40,953 cycles
DURING SCRIBE LINE INSP AD2010-06-16 INSP FOUND 3 INDIVIDUAL SCRIBE LINES LOCATED BETWEEN STA 338-338.5 SL17L WITH DAMAGE MEASURING .5X.063X.0140 (2) .5X.2X.006 (3) .5X.100X.002. REPAIRED AREA IAW REA B653-59527, USING 2024T3 .160 AND .190, AWG.
Part: PBE — DEFECTIVE (COCKPIT) · airframe 49,922 hrs · 40,243 cycles
COCKPIT PBE INDICATOR EXTENDING PAST FLUSH. REPLACED PBE IAW AMM 25-60-00.
2010
Part: BRACKET — OUT OF POSITION (CARGO DOOR) · airframe 48,443 hrs · 39,339 cycles
DURING CLIMB "MAIN CARGO DOOR" LIGHT ILLUMINATED AT FL350. INSPECTED MAIN CARGO DOOR NO DEFECTS NOTED. PLACED DOOR INDICATION SYSTEM ON DI 65443 PER B767 MEL 52-71-1-2 AND COMPLIED WITH MAINTENANCE PROCEDURES. DOOR VERIFIED CLOSED AND LOCKED. PERFORM MAIN CARGO DOOR RIG. SWITCH BRACKET INTERFERING WITH TORQUE TUBE. RIGGED HOOKS AND LATCH MECHANISM. ADJUSTED SWITCHES FOR LIGHTS. REPLACED SPRING. PRESSURIZED AIRCRAFT. NO DEFECTS NOTED, OPS CHECKS GOOD. DI CLEARED.
Part: WARNING SYSTEM — MALFUNCTIONED (CARGO DOOR) · airframe 48,440 hrs · 39,336 cycles
ON DESCENT MN CARGO DOOR ILLUM. PRESS REMAINED NORMAL. INSPECTED MAIN CARGO DOOR SWITCHES. NO DEFECTS NOTED. OPENED AND CLOSED DOOR SEVERAL TIMES AND DOOR WARNING INDICATES NORMAL PER AMM 52-32-00-5.
2009
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 48,125 hrs · 39,146 cycles
GALLEY AREA CENTER EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY, OPS CHECKS OK.
2007
Part: PRESSURE PANEL — CORRODED (BS 1350) · airframe 46,244 hrs · 38,064 cycles
PRESSURE PANEL AT FS 1350, RIGHT BUTT LINE 40 WAS CORRODED. REMOVED, REPLACED AND REINSTALLED PRESSURE PANEL AT FS 1350, RIGHT BUTT LINE 40.
Part: BEAM — CORRODED (CARGO DOOR) · airframe 46,244 hrs · 38,064 cycles
FORWARD LOWER CARGO DOOR BEAM WAS CORRODED AT THE INSULATION BLANKET NUT PLATES. REPAIRED FORWARD LOWER CARGO DOOR BEAM IAW B767 MM.
2006
Part: ACTUATOR — OVERHEATED (RAM AIR DOOR) · airframe 44,292 hrs · 37,318 cycles
SMOKE IN COCKPIT AT AROUND 30,000 FT. RAM AIR DOOR ACTUATOR OVERHEATED (BEARINGS). REPLACED ACTUATOR.
2004
Part: BEARING — MISINSTALLED (RT MLG STRUT) · airframe 41,737 hrs · 36,259 cycles
EN ROUTE TO SJC, RIGHT MAIN LANDING GEAR FAILED DOWN AND LOCK WITH GEAR DOOR OPEN. OBSERVED BY ATC TOWER, HELICOPTER. ACCOMPLISHED NON NORMAL, DID NOT SOLVE PROBLEM. SEVERAL NEGATIVE AND POSITIVE G'S MANEUVERS AND GEAR CAME DOWN. AIRCRAFT WAS RE-ROUTED TO MHR WHERE IT LANDED WITHOUT FURTHER INCIDENT. UPON LANDING, GEAR WAS PINNED AND AIRCRAFT TOWED TO GATE. OPENED WORK PACK W/O 600196580. STRUT REPACKED IAW B767 AMM 32-11-25-2. ACCOMPLISHED LANDING GEAR ALTERNATE EXTEND CONDITION. ACCOMPLISHED SEVERE OR UNUSUAL TURBULANCE INSPECTION. NO DEFECTS NOTED. REWORKED AREA ON RIGHT MAIN LANDING GEAR UPLOCK FITTING. ROTOPEEN IAW REA B 632-49613, REF ABX PROCESS STANDARDS MANUAL 900-4, NUMBER 10.
2002
Part: COVER — BINDING (EVAC SLIDE) · airframe 39,451 hrs · 35,521 cycles
EMERGENCY SLIDE WOULD NOT ARM WHEN MAIN ENTRY DOOR CLOSED. FOUND COVER FOR SLIDE BINDING. ADJUSTED DOOR COVER, SLIDE ARMS NORMAL.
Part: WEB — CRACKED (#1 ENGINE) · airframe 39,430 hrs · 35,515 cycles
#1 ENGINE STRUT AFT FAIRING SPAR WEB, FOUND ONE CRACK ON STIFFENER (P/N 313T1380-15), AND FOUR CRACKS ON WEB (P/N 313T1380-9). REPAIRED STRUT AFT FAIRING IAW REA B654-44936-MR.
Part: CAP — CORRODED (FWD CARGO) · corrosion level 2 · airframe 39,430 hrs · 35,515 cycles
FORWARD CARGO LOWER LOBE, STATION 676, DEEP CORROSION ON UPPER CAP AT LEFT BUTT LINE 20. REPLACED CAP IAW SRM 51-40-02.
Part: STRUT — CORRODED (LEFT WING L/E) · corrosion level 2 · airframe 39,430 hrs · 35,575 cycles
LEFT WING FIXED LEADING EDGE RIB, W.S. 456.98, HAD CORROSION IN ANTI-ICE TAIL DUCT TO LEADING EDGE SLAT AT WING FIXED LEADING EDGE RIB. REMOVED CORRODED RIB AND INSTALLED NEW STRUT IAW BOEING SRM 51-40-02, 57-41-09, AND BAC DWG 114T2202.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,430 hrs · 35,515 cycles
FORWARD CARGO LOWER LOBE, STATION 742, BETWEEN STRINGERS 37 - 39 RIGHT, AND STRINGER 38 LEFT, CORRODED SHEAR TIES. REPLACED SHEAR TIES IAW SRM 51-40-02.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,430 hrs · 35,515 cycles
FORWARD CARGO LOWER LOBE, STATION 720, LEFT BUTT LINE 45, CORRODED UPPER CHORD. REPLACED CHORD IAW SRM 51-40-02.
Part: FRAME — CRACKED (LT WING TE FLAP) · airframe 39,430 hrs · 35,575 cycles
LEFT WING NR 6 INBOARD TRAILING EDGE FLAP AFT FAIRING FORWARD FRAME, FOUND CRACK. NO, THIS PART HAS BEEN PREVIOUSLY ACCOMPLISHED ON A/C SB 767-57-0014. THE COMPONENT THE PART IS INSTALLED ON, IS FLAP LINKAGE FAIRING NR 3. REPAIRED AREA IAW REA B657-44390.
Part: FITTING — CORRODED (TE FLAP) · airframe 39,430 hrs · 35,515 cycles
LT WING INBOARD TRAILING EDGE FLAP OUTBOARD HINGE FITTING ASSEMBLY BEARING BORE, HAD SURFACE CORROSION. THE CORROSION WAS FOUND ON THE SURFACE OF THE BORE, WHERE BEARING INSTALLS. REPAIRED AREA IAW REA B657-44910MR.
Part: CAP — CORRODED (FWD CARGO) · corrosion level 2 · airframe 39,430 hrs · 35,515 cycles
FORWARD CARGO LOWER LOBE, STATION 522, RIGHT BUTT LINE 25, DEEP CORROSION ON UPPER CAP. REPLACED CAP IAW SRM 51-40-02.
Part: SPAR — CORRODED (LT WING) · airframe 39,430 hrs · 35,575 cycles
LT WING INBOARD TRAILING EDGE MAIN FLAP FRONT SPAR LOWER CHORD VERTICAL FLANGE BETWEEN FS 286 - 290, FOUND CORROSION. REPAIRED AREA IAW REA B657-44906MR.
Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 39,430 hrs · 35,575 cycles
RT WING INBOARD TRAILING EDGE MAIN FLAP MID SPAR UPPER FORWARD CHORD HAD CORROSION, WS 177 - 186 AND BETWEEN WS 252 - 261. REPAIRED AREA IAW REA B756-44900MR.
Part: FLOOR PANEL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 39,430 hrs · 35,515 cycles
FORWARD CARGO LOWER LOBE, STATIONS BETWEEN 544 - 610, FROM RIGHT BUTT LINE 10, LEFT BUTT LINE 10, CORRODED SHEAR FLOOR PANEL. REPLACED PANEL IAW N.R.C. LT 135 AND SRM.
Part: ANGLE — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 39,430 hrs · 35,515 cycles
LEFT WING, NR 1 PYLON SKIRT, LOWER CHORD MID SECTION, HAD INTERGRANULAR CORROSION. ALSO FROM MID TO AFT END FOUND SPOTS OF CORROSION. REPLACED CHORD (ANGLE) IAW SRM 54-51-71.
Part: HINGE FITTING — CORRODED (LEFT WING) · corrosion level 2 · airframe 39,430 hrs · 35,575 cycles
CORROSION UNDER JUMPER BONDING BOLT, LEFT OUTBOARD AILERON, OUTBOARD HINGE FITTING, W.S. 1127.45. REPLACED FITTING IAW BOEING SRM 57-51-02, IPC 57-51-51-A01, AND DWG 113T1521.