N788AX
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.
76 reports on file, 2000-09-13 – 2018-10-23.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 58,397 hrs · 43,223 cycles
CORROSION ON LOWER FLANGE ON RIGHT HORIZONTAL STABILIZER CHORD 17. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON THE #4 SLAT OUTBOARD AUX TRACK INBOARD LOWER STRUT. THE AIRLOAD RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: ATTACH FITTING — CORRODED (LT WING TE) · airframe 58,397 hrs · 43,223 cycles
CORROSION ON LEFT WING TRAILING EDGE LOWER PANEL ATTACH CHORD. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: STIFFENER — CRACKED (BS 266.5) · airframe 58,397 hrs · 43,223 cycles
CRACK IN THE MAIN DECK CARGO FLOOR BEAM VERTICAL STIFFENER AT FUSELAGE STATION 266.5. THE STIFFENER WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON THE LEFT WING LEADING EDGE FRONT SPAR AT LEADING EDGE STATION 867. THE FRONT SPAR'S WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
Part: ATTACH FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH CHORD AT WING STATION 433. THE CHORD WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: SKIN — DENTED (RT WING SLAT) · airframe 58,397 hrs · 43,223 cycles
DENT ON #12 SLAT ON TOP SKIN. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
Part: DOOR FRAME — CRACKED (BS 295-330) · airframe 58,397 hrs · 43,223 cycles
CRACK IN THE FRAME OF THE LOWER AFT CORNER OF THE L1 DOOR. THE FRAME WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: DOUBLER — CORRODED (LT AILERON) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON DOUBLER FORWARD OF THE OUTBOARD AILERON ON THE LEFT WING. THE DOUBLER WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: STRUT — CORRODED (RT WING) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON LOWER STRUT ON AIRLOAD RIB ON RIGHT WING. THE STRUT WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 58,397 hrs · 43,223 cycles
CHAFE AND CRACK ON #1 PYLON INBOARD HYDRAULIC BAY LOWER BEAM ZEE ANGLE. THE ZEE ANGLE WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: ATTACH FITTING — CORRODED (LT WING LE) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON LEFT WING LEADING EDGE LOWER PANEL ATTACH STRUCTURE. REPLACED WEB. THE AIRPLANE WAS GROUNDED.
Part: CIRCUIT BREAKER — FAILED (BUSS POWER) · airframe 58,397 hrs · 43,223 cycles
EXCESSIVE HEAT AT C10 CIRCUIT BREAKER "C BUS PWR" INSIDE P6-2 PANEL. REPLACED CIRCUIT BREAKER C884 AND WIRE W1032-004-6. THE AIRPLANE WAS GROUNDED. THE CAUSE OF THE EXCESSIVE HEAT IS UNKNOWN.
Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON #2 SLAT OUTBOARD AUX TRACK INBOARD LOWER STRUT. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: BEAM — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON THE RIGHT HORIZONTAL STABILIZER FIXED TRAILING EDGE BEAM UPPER CHORD BETWEEN ELEVATOR STATIONS 237 AND 261. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
Part: FITTING — CHAFED (NR 1 NACELLE) · airframe 58,397 hrs · 43,223 cycles
CHAFE ON #1 PYLON INBOARD SIDE LOAD FITTING AT NACELLE STATION 302. THE WEAR AREA MEASURED 3.60â LONG X 0.150â WIDE X 0.043â DEEP (ENTIRE LENGTH). THE FITTING WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
Part: FAILSAFE — CORRODED (BS 539) · airframe 58,397 hrs · 43,223 cycles
CORROSION ON FORWARD LOWER CARGO DOOR INNER SILL FAIL SAFE STRAP. REPLACED FAIL SAFE STRAP. THE AIRPLANE WAS GROUNDED.
Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD BETWEEN REAR SPAR STATIONS 200 AND 226.6. THE CHORD WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 58,397 hrs · 43,223 cycles
CORROSION ON #1 SLAT INBOARD AUX TRACK INBOARD LOWER STRUT. THE RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
Part: SKIN — DENTED (RT WING SLAT) · airframe 58,397 hrs · 43,223 cycles
DENT ON #12 SLAT (RIGHT WING) UPPER SKIN AT OUTBOARD SLAT STATION 992. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
Part: SKIN PANEL — CHAFED (LT WING) · airframe 58,298 hrs · 43,163 cycles
CHAFE DAMAGE TO THE LOWER WING SKIN PANEL # 1 (P/N: 111T4015-4) AND LOWER CENTER WING BEAM (LBL 62.05) WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21), & LOWER CHORD (P/N: 111T5012-17). THE CHAFE AREA COMMON TO THE LOWER CENTER WING SKIN PANEL # 1 MEASURED WERE APPROXIMATELY 1.25" (CHORDWISE) X 0.049 (DEPTH). THE SKIN, WING BEAM WEB, DOUBLER, AND LOWER CHORD WERE REPAIRED. THE AIRPLANE WAS GROUNDED.
Part: BEAM — CHAFED (LT WING) · airframe 58,298 hrs · 43,163 cycles
CHAFING AT BODY STATION 900, LBL 57 ON THE LOWER WING SKIN PANEL (P/N: 111T4015-4) AND LOWER CENTER WING BEAM WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21), & LOWER CHORD (P/N: 111T5012-17). THE SKIN PANEL, WEB, DOUBLER, AND CHORD WERE REPAIRED. THE AIRPLANE WAS GROUNDED.
Earlier reports · 2000–2017 · 54 reports
2017
Part: ESCAPE REEL — MISSING (CABIN) · airframe 57,564 hrs · 42,778 cycles
ONE EMERGENCY DESCENT SAFETY HARNESS WAS MISSING FROM ITS STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), A NEW SAFETY HARNESS WAS INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING HARNESS IS UNKNOWN.
Part: UNKNOWN — ODOR (CABIN) · airframe 57,055 hrs · 42,484 cycles
WHILE THE LEFT ENGINE WAS IN OPERATION, THE LEFT PRESSURE REGULATING SHUTOFF VALVE WAS CLOSED. A STRONG ODOR WAS ASSOCIATED WITH IT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE LEFT ENGINE WAS OPERATED WITH NO DEFECT FOUND. THE CAUSE OF THE ODOR WAS NOT FOUND.
2016
Part: COUPLING — FAILED (AC BAY) · airframe 55,236 hrs · 41,618 cycles
WITH THE EQUIPMENT COOLING SWITCH IN OVRD POSITION & BOTH PACKS OPERATING AT 39,000 FEET, THE CABIN ALTITUDE CLIMBED TO 11,000 FEET. THE FLIGHT CREW DESCENDED TO 10,000 FEET TO REGAIN PRESSURIZATION. REPLACED THE COUPLING & SEAL THAT JOINS THE CONDITIONED AIR GND CONNECTOR TO THE ADJACENT T DUCT. THE CAUSE OF THE CABIN ALTITUDE CLIMB WAS THE FAILED COUPLING ABOVE THE CONDITIONED AIR GND CONNECTOR.
2015
Part: MEC — FAULTY (LT ENGINE) · airframe 54,008 hrs · 40,923 cycles
ADVANCED THRUST LEVER APPROX HALF WAY FOR TAKEOFF ON LT ENG & ENG WOULD NOT ACCELERATE. REPLACED LT ENG MAIN ENG CONTROL.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 53,755 hrs · 40,801 cycles
LAVATORY SMOKE ALARM SOUNDED, NO SMOKE OBSERVED. REPLACED LAVATORY SMOKE DETECTOR.
Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 53,754 hrs · 40,800 cycles
VERTICAL STABILIZER TO SKIN ANGLE LT OTBD END CRACKED, ACCESS THROUGH PANEL 324AL. REMOVED ANGLE, FABRICATED NEW ANGLE IAW DWG 173T1302 FROM 2024-T3 .040. PERFORMED HFEC INSPECTION. INSTALLED NEW ANGLE IAW SRM 5140-02. SDR INFO, CRACKED 1.900", PN 173T1302-1, SN N/A, PART NAME ANGLE, FS LOCATION ON ACFT FS 1725.5 TO 1746.5, STRINGER & WS LOCATION ON ACFT, STRINGER 2L TO 2R. ACFT WAS GNDED.
Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
DURING OK TO CLOSE OF LE PANELS FOUND CORROSION ON NUT STRIP ON FIXED LE AT APPROX LES 590. FOUND CORROSION TO BE ON NOSE BEAM WEB COMMON TO NUTPLATES. REMOVED WEB & FABRICATED NEW ONE FROM 7075-76-050 PO 0056503. INSTALLED NEW WEB & REMOVED ASSEMBLY IAW SRM 51-40-02, 51-30-01 & DWG 114T2300. SDR INFO, CORRODED L2, PN 114T2300-19, SN NSN, PART NAME, NOSE BEAM WEB, STRINGER & WS LOCATION ON ACFT, OSS 585 TO OSS 607. ACFT WAS GNDED.
Part: BEAM — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
LEFT HORIZONTAL STABILIZER UPPER REAR BEAM HAS AREAS OF CORROSION FROM ELEVATOR STATION 49 - 302. OUT OF LIMITS AREA ELEVATOR STATION 146 - 150.5. REPAIRED IAW REA B655-61427. THREE BLEND LOCATIONS FOUND TO BE WITHIN ACCEPTABLE LIMITS WHEN COMBINING SRM 55-10-13 FIG 101 & DWG TOLERANCES IAW ENGINEERING. REMAINING CORROSION ON BEAM BLENDED WITHIN LIMITS IAW SRM 55-10-13 FIG 101. SDR INFO, PN 183T1701, PART NAME AFT UPPER BEAM, SN NSN, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT ELEVATOR STATION 49.5 TO 302. ACFT WAS GNDED.
Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
RIGHT WING TE LOWER CHORD OF SUPPORT RIB AT WS 1080 IS CORRODED & SPLIT. R & R RT WING TE LOWER CHORD OF SUPPORT RIB WS 1080 IAW SRM 51-40-02 & DOC 113T1521 REV 6. FABRICATED ON REA B657-61431. SDR INFO, PN 113T1521-16, PART NAME CHORD, SN NSN, CORRODED LEVEL 2, EXACT STRINGER & WS LOCATION ON ACFT 1080 TO 1080. ACFT WAS GNDED.
Part: SPAR — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
LEFT HORIZONTAL STABILIZER REAR SPAR & TE BEAM ARE CORRODED AT ELEVATOR STATION 325. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD ELEVATOR STATION 321.5 - 337.5 IAW REA B655-61425-MR. TE BEAM AT ELEVATOR STATION 325 FOUND TO BE ACCEPTABLE FOR CONTINUED SERVICE WHEN COMBINING SRM 55-10-13 FIG 101 LIMITS & STANDARD DWG TOLERANCES IAW ENGINEERING. SDR INFO, PN 182T1100-1, PART NAME REAR SPAR UPPER CHORD, SN NSN, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT ELEVATOR STATION 321.5 TO 337.5. ACFT WAS GNDED.
Part: SPAR — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
LEFT HORIZONTAL STABILIZER REAR SPAR IS CORRODED AT ELEVATOR STATION 139 - 143. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR UPPER CHORD ELEVATOR STATION 139 - 143 IAW REA B655-61435-MR. SDR INFO, PN 182T1100-1, PART NAME REAR SPAR UPPER CHORD, SN NSN, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT ELEVATOR STATION 139 - 143. ACFT WAS GNDED.
Part: RIB — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 91 UPPER CHORD OF THE TE RIB IS CORRODED. R & R CHORD PN 183T1400-5 IAW SRM 51-40-02. SDR INFO, PN 183T1400-5, PART NAME UPPER CHORD, SN NSN, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT ELEVATOR STATION 91. ACFT WAS GNDED.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,754 hrs · 40,800 cycles
EA 53500009-001 NEEDS ACCOMPLISHED. REPAIRED DAMAGED CHORD RT STATION 883.5 STRINGER 18R IAW SRM 53-50-07 REPAIR 1. SDR INFO CRACKED 0.250", PN 145T8000-1, SN N/A, PART NAME CHORD, FS LOCATION ON ACFT, FS 883.5, STRINGER LOCATION ON ACFT, STRINGER 18R. ACFT WAS GNDED.
Part: RIB — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD OF THE TE RIB IS CORRODED. INSTALLED NEW LT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD OF THE TE RIB IAW REA B657-61411-MR & SRM 51-40-02. SDR INFO, CORRODED LEVEL 2, PN 183T1340-29, PART NAME UPPER CHORD, SN NSN, EXACT FS & BS ELEV STATION 215. ACFT WAS GNDED.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
RIGHT KEEL BEAM LOWER INBD FLANGE LOWER SURFACE CORROSION FS 998 - 1007. REPAIRED RT KEEL BEAM IAW REA B653-61424-MR. SDR INFO, CRACKED, CORRODED L2, PN 145T8611, SN NSN, PART NAME KEEL BEAM, FS & BS LOCATION ON ACFT RT 998 TO 1007. ACFT WAS GNDED.
Part: RIB — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
LEFT HORIZONTAL STABILIZER, ELEVATOR STATION 325 UPPER CHORD OF THE TE RIB IS CORRODED. REPLACED UPPER T CHORD FITTING ON LT HORIZONTAL STATION 325. PN 183T1530-5AX IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 183T1530-5AX, SN NSN, PART NAME UPPER CHORD, FS & BS LOCATION ON ACFT ELEV STATION 325. ACFT WAS GNDED.
Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
CORROSION FOUND ON FIXED LE STRUCTURE AT APPROX LE STATION 894 AT SCREW HOLE. REMOVED NOSE BEAM WEB ASSEMBLY, FABRICATED NEW WEB & REINSTALLED ASSEMBLY WITH NEW WEB IAW SRM 51-40-02 & DWG 114T2300. SDR INFO, CORRODED L2, PN 114T2300-39, SN NSN, PART NAME NOSE BEAM WEB, FFS & BS LOCATION ON ACFT RT WING LE, STRINGER & WS LOCATION ON ACFT STATION 894. ACFT WAS GNDED.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
LEFT FWD KEEL BEAM FWD STATION 977, LBL 2 CORROSION FOUND, MARKED WITH NR. FOUND ANGLE AT STATION 977, LBL 2 TO BE CORRODED BEYOND LIMITS IAW SRM 53-50-12 FIG 101. R & R ANGLE IAW SRM 51-40-02. SDR INFO, CORRODED LEVEL 2, PN 145T8604-2, PART NAME ANGLE, SN N/A, EXACT FS FROM LBL 2, EXACT STRINGER & WS STATION 977. ACFT WAS GNDED.
Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
HYDRAULIC LINE SUPPORT CLIP OTBD & AFT OF TOP OF LG CORRODED ON TE SUPPORT. REMOVED CLIP, FOUND BEAM TO BE CORRODED. REPLACED BEAM, REINSTALLED CLIP IAW SRM 51-40-02 & DWG 113T1633. SDR INFO, CORRODED LEVEL 2, PN 113T1633-217, PART NAME BEAM, SN NSN, STRINGER & WS LOCATION WS 410. ACFT WAS GNDED.
Part: BEAM — CORRODED (RT WING) · airframe 53,754 hrs · 40,800 cycles
CORROSION AROUND NUTPLATE AT APPROX LES 620. R & R WEB IAW SRM 51-40-02. SDR INFO, CORRODED, PN 114T2300-225, SN N/A, PART NAME NOSE BEAM. ACFT WAS GNDED.
Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 53,754 hrs · 40,800 cycles
CORROSION AROUND NUTPLATES ON REAR SPAR TO TE BEAM UPPER CHORD AT WS 433 NEAR TE. R & R UPPER CHORD WS 433 REAR SPAR TO TE IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 113T1510-33, SN NSN, PART NAME CHORD, AILERON SUPP STRINGER & WS LOCATION ON ACFT WS 433. ACFT WAS GNDED.
2014
Part: UNKNOWN — FUMES (COCKPIT) · airframe 52,522 hrs · 40,210 cycles
ON TOP OF DESCENT, THE FLIGHT CREW COULD SMELL ELEC FUMES. COMPLIED WITH SMOKE, FIRE, & FUMES CHECKLIST & FUMES CEASED. INSPECTED THE MAIN EQUIPMENT CTR, FWD EQUIPMENT COMPARTMENT, GALLEY AREA, HOT CUP, LAVATORY & RT AIR PACK, NO DEFECTS WERE FOUND. OPERATED BOTH PACKS IAW AMM 21-51-03-4, NO ODORS WERE NOTED.
2013
Part: ANGLE — DAMAGED (ZONE 200) · airframe 51,500 hrs · 39,616 cycles
FUSELAGE SKIN AT LT HORIZONTAL ANGLE, BS 1809, S12L HAS DEFECT INDICATION IN LOWER FWD FASTENER OF INSPECTED AREA 1 IAW NDTM PART 6, FIG 1. FASTENER OBLONG, REAMED TO .341" ON EXTERIOR RUB STRIP CUT OUT LOCATION. FASTENER DOUBLER REPAIRED IAW ENGINEERING REA B60522MR, ACFT WAS GROUNDED.
Part: SKIN — CORRODED (ZONE 200) · airframe 51,500 hrs · 39,616 cycles
RIGHT SIDE EMERGENCY EXIT DOOR CUTOUT FOUND WITH CORROSION IN THE FORWARD LOWER CORNER AREA APPROX. 2" LONG. REMOVED CORROSION IN RT SIDE EMERENCY EXIT CUTOUT FORWARD LOWER CORNER AREA. IAW REAB653-60542, ACFT WAS GROUNDED.
Part: MOUNT — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 51,500 hrs · 39,616 cycles
NR 2 ENGINE AFT MOUNT HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED ENGINE MOUNT IAW B767 MM CH 71-21-02-4, ACFT WAS GROUNDED.
Part: STIFFENER — CORRODED (ZONE 100) · airframe 51,500 hrs · 39,616 cycles
STIFFENER BETWEEN KEELBEAM PANELS CORRODED ON BOTH ENDS, STIFFENER CORRODED BEYOND LIMITS, R & R IAW SRM 51-40-02, PARA 4B AND 51-40-0, ACFT WAS GROUNDED.
Part: MOUNT — CORRODED (NR 1 ENGINE) · corrosion level 2 · airframe 51,500 hrs · 39,616 cycles
NR 1 ENGINE AFT ENGINE MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED AFT ENGINE MOUNT IAW B767 AMM 71-21-02-4, ACFT WAS GROUNDED.
2012
Part: INERTIA REEL — UNSECURE (COCKPIT) · airframe 51,009 hrs · 39,352 cycles
EMERGENCY ESCAPE DEVICE (INTERTIAL REEL) FELL OUT OF HOLDER DURING FLIGHT. REPLACED DESCENT DEVICES IN SUPERNUMERARY COMPARTMENT CONTAINER AT POS 7 IAW AMM 25-61-03-04, ACFT WAS GROUNDED.
Part: INERTIA REEL — UNSECURE (COCKPIT) · airframe 51,009 hrs · 39,352 cycles
EMERGENCY ESCAPE DEVICE (INTERTIAL) FELL OUT OF HOLDER DURING FLIGHT. REPLACED DESCENT DEVICES IN SUPERNUMERARY COMPT CONTAINER AT POS NR 5 IAW AMM 25-61-03-04, ACFT WAS GROUNDED.
Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 50,678 hrs · 39,153 cycles
AFTER LEVEL OFF AT CRUISE ALT, THE EMERGENCY EXIT LIGHT ILLUMINATED. INSPECTED P6-2 DC BUSES FOUND CB RIGHT DC BUS POS G-9 SECT 1 POPPED OUT. INSPECTED EMERGENCY LIGHT, FOUND OK IAW WIRING DIAGRAM 34-54-21 CHECK OPS GOOD AT THIS TIME, ACFT WAS GROUNDED.
2011
Part: RIB — CORRODED (LT WING) · airframe 68,978 hrs · 32,085 cycles
BOTH LT WING LEADING EDGE RIBS I/B AND O/B OF NR 2 SLAT I/B AUX TRACK HAVE CORROSION AROUND NUT PLATES. REPLACED BOTH I/B AND O/B RIBS IAW B767 SRM 51-40-02.
Part: RIB — CRACKED (LE SLAT) · airframe 68,978 hrs · 32,085 cycles
NR 9 SLAT INBOARD TRACK CUTOUT INBOARD L/E RIB IS CRACKED. CRACK IS .5 INCH LONG. REMOVED AND REPLACED RIB IAW B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
Part: RIB — CORRODED (LE SLAT) · airframe 68,978 hrs · 32,085 cycles
NR 11 SLAT OUTBOARD AUX TRACK OUTBOARD RIB IS CORRODED. REPLACED STRUT 114T2224-16 IAW 767-200 SRM 51-40-02.
Part: RIB — CORRODED (LT WING) · airframe 49,655 hrs · 38,568 cycles
LEADING EDGE RIB I/B OF NR 3 SLAT O/B AUX TRACK HAS CORROSION AROUND NUT PLATES. REMOVED AND REPLACED L/E RIB I/B OF NR 3 SLAT O/B AUX TRACK IAW B767 SRM 51-40-02.
Part: RIB — CORRODED (LT WING) · airframe 49,655 hrs · 38,568 cycles
CORROSION BETWEEN LT WING LEADING EDGE SKIN AND LEADING EDGE RIB AT APPROX STA 455. REMOVED AND REPLACED RIB AT APPROX WING STA 455 IAW SRM 51-40-02.
Part: SKIN — GOUGED (WING) · airframe 49,655 hrs · 38,568 cycles
LOWER WING SURFACE AT APPROX 975 IS GOUGED. DAMAGE WAS REPAIRED IAW REA B657-59239-MR.
Part: RIB — CRACKED (LE SLAT) · airframe 68,978 hrs · 32,085 cycles
INBOARD RIB OF NR 4 SLAT INBOARD DRIVE ROD AT STA 561 HAS CRACKED CLOSE OUT PAN IN NOSE RIB AREA. REMOVED AND REPLACED RIB P/N 114T2512-9AX IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
Part: RIB — CRACKED (LT WING) · airframe 68,978 hrs · 32,085 cycles
RIB CRACKED ON LT WING LEADING EDGE AT APPROX WS 528 WHERE RIB ATTACHES TO FRONT SPAR. REPAIRED WING L/E INNER CHORD ON WING RIB AT STA 528 IAW B767-200 SRM 57-41-09. AIRCRAFT WAS GROUNDED.
Part: RIB — CRACKED (LE SLAT) · airframe 68,978 hrs · 32,085 cycles
NR 8 SLAT OUTBOARD TRACK CUTOUT OUTBOARD L/E RIB IS CRACKED. CRACK IS .7 INCH LONG. REMOVED AND INSTALLED NEW RIB IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
Part: RIB — CORRODED (LE SLAT) · airframe 68,978 hrs · 32,085 cycles
LEADING EDGE RIB I/B OF NR 4 SLAT I/B AUX TRACK HAS CORROSION AROUND NUT PLATES. REMOVED AND REPLACED STRUT P/N 114T2208-15AX IAW B767-200 SRM 51-40-02.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 49,655 hrs · 38,568 cycles
CRACK IN LEFT SIDE NOSE WHEEL WELL CHORD STA 287. CRACK IS 1.250 INCH LONG AND IS LOCATED 12 INCHES BELOW TOP OF CHORD. REMOVED DAMAGED AREA IN CHORD STA 287 PART NUMBER 141T2938-16 AND REPAIRED CHORD IAW B767-200 SRM 51-70-12.
Part: RIB — CORRODED (LT WING) · airframe 68,978 hrs · 32,085 cycles
LT WING LEADING EDGE RIB O/B OF NR 2 SLAT O/B TRACK HAS CORROSION AROUND NUT PLATES. REMOVED AND REPLACED L/E RIB P/N 114T2224-15 IAW B767 SRM 51-40-02. AIRCRAFT WAS NOT GROUNDED.
Part: RIB — CORRODED (LE SLAT) · airframe 68,978 hrs · 32,085 cycles
NR 10 SLAT OUTBOARD AUX TRACK INBOARD RIB IS CORRODED. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-02. AIRCRAFT WAS GROUNDED.
2008
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 48,593 hrs · 37,726 cycles
EMERGENCY LIGHTS WERE DIM AND THEN WENT OUT AFTER 2 SECONDS. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW B767 AMM 33-50-00. OPS CHECK GOOD.
Part: ATTACH ANGLE — CRACKED (NR 1 NACELLE) · airframe 47,275 hrs · 37,198 cycles
INBOARD ATTACH ANGLE FOR PANEL 437DB HAD APPROXIMATELY 3 INCH CRACK NEAR BOTTOM. REMOVED AND REPLACED CRACKED ATTACH PART IAW B767 SRM 51-40-2.
2006
Part: BULKHEAD — DENTED (FUSELAGE) · airframe 45,904 hrs · 36,422 cycles
2 DENTS/GOUGES IN AFT PRESSURE BULKHEAD, AFT SIDE, BETWEEN RS7 AND 8, AND BETWEEN TS6 AND INNER RING. REPAIRED DAMAGE AREA IAW SRM 53-80-08.
2005
Part: FITTING — CRACKED (FUSELAGE) · airframe 43,282 hrs · 35,473 cycles
LEFT FORWARD OUTER CHORD FITTING CRACKED PER DETAILED VISUAL INSPECTION IAW JC NEA53800004-001 AND AD 2001-09-13. REPAIRED LEFT FORWARD OUTER CHORD FITTING IAW S/B 767-53A-0078.
2004
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,751 hrs · 34,975 cycles
EMERGENCY EXIT LIGHTS GO OUT AFTER 10 SECONDS. SWAPPED TO SPARE BATTERY. SYSTEM CHECKED GOOD. DEFERRED SPARE BATTERY PER MEL 33-51-1, CAT-C, CODE 11, MBCB 03-11-04. PLACARD INSTALLED. REPLACED SPARE BATTERY PER B767 AMM 33-51-07-2. PLACARD REMOVED.
2002
Part: SENSOR — DEFECTIVE (LEFT HAND) · airframe 38,641 hrs · 33,931 cycles
Lt eng hi stage displayed. Lt hi stage light illuminated. Per non-normal check list the left pneumatic switch was cycled on/off with oily fumes coming into the cabin. Note: The remainder of the flight was operated with left engine bleed and left A/C pack off. Fumes cleared. Left pneumatic pressure read 14 psi with left side switch off. Replaced fan air temp sensor. Leak and ops checked good IAW B767 MM 36-11-17-4.
2001
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,776 hrs · 33,324 cycles
RIGHT GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE NOT DISPLAYED. DOOR AND GEAR AMBER LIGHTS WERE EXTINGUISHED. CREW ELECTED TO DO A GO-AROUND AND A GEAR RECYCLE. RELAMPED RIGHT GEAR DOWN AND LOCKED. INDICATION OPS CHECKED GOOD.
2000
Part: RIB — CRACKED (LT WING) · airframe 35,240 hrs · 32,830 cycles
CRACKS ON WING LEADING EDGE. REPAIRED IAW ABX REA 657-37420MR.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 35,240 hrs · 32,021 cycles
CORROSION FOUND ON CHANNEL FUSELAGE STATION 266.5 AND 287 RBL 15.90. REPAIRED IAW ABX REA 653-37419MR.
Part: SUPPORT BRACKET — CORRODED (RT WING SPOILER) · airframe 35,240 hrs · 32,830 cycles
CORROSION ON SPOILER SUPPORT UPPER CHORD FLANGE. REPAIRED IAW ABX REA 657-37483MR.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 35,240 hrs · 32,830 cycles
CORROSION ON INNER CHORD OF NR THREE AFT CARGO BEAM. REPAIRED CORROSION IAW ABX REA 652-37474MR. (X)