N931UP
Registered owner: BOEING CO, WA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
131 reports on file, 1995-04-13 – 2001-12-07.
Part: LIGHT — INOPERATIVE (COCKPIT)
INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT IN COCKPIT INOP HGT SPARE PREFLIGHT. EMERGENCY EXIT LIGHT IN COCKPIT CHARGED AND OPERATIONAL PER 33-50, OPS CHECK GOOD OK FOR SERVICE.
Part: FIRE LOOP — CONTAMINATED (NLG WW)
INSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT AND BELL CAME ON ON APPROACH AT APPROX 3000 FT MSL WHEN GEAR EXTENDED, LIGHT EXTINGUISHED. NO APPARENT DAMAGE OR PROBLEMS ON LANDING. INSPECTED ALL WHEEL WELL FIRE LOOPS FOR GROUNDS. FOUND CONTAMINATION IN THE NOSE WHEEL WELL FIRE LOOP CONNECTOR CAUSING LOOP TO SHORT TO GROUND. CLEANED AND RE-SECURED CONNECTOR. R/I FIRE DETECTION UNIT AS PRECAUTIONARY. OP'S CHECKS GOOD AS PER M/M 26-12-00 ADJ/TEST. OK FOR SERVICE.
Part: DOOR SEAL — TORN (PAX DOOR)
INSPECTION TYPE:N/A PILOT REPORT-AT 5000 FT LOST CABIN PRESSURIZATION REPAIRED MAIN ENTRY DOOR SEAL
Part: CONTACTOR — CORRODED (BATTERY PACK)
INSPECTION TYPE:PFLT PRE FLT - EMER EXIT LIGHT FWD ENTRY W/N STAY ILLUM. REMOVED LIGHT ASSY AFTER INSPECTION FOUND BATTERY CONTACTS TO HAVE LIGHT CORROSION. CLEANED CONTACTS, AND RE-LAMPED LIGHT ASSY, RE-INSTALLED OPS GOOD REF M/M 33-50-101.
Part: BULB — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE:N/A COCKPIT DOOR EMERGENCY EXIT LIGHT HAS ONE DIM BULB RELAMPED EMER. LIGHT OVER FLIGHT DECK ENTRY DOOR, OPS CHECK GOOD
Earlier reports · 1995–2000 · 126 reports
2000
Part: STRINGER — CORRODED (FUSELAGE)
INSPECTION TYPE:C, STRINGER END 22L CORRODED BETWEEN BS 348.2 AND BS 360. INSTALLED NEW STRINGER SECTION, (P/N 65-18420-269) AND TIE FITTING (P/N 65-29876-7), IAW SRM 51-30-2.
Part: SEAT TRACK — BROKEN (FUSELAGE)
INSPECTION TYPE:C, AFT CARGO COMPARTMENT SEAT TRACK TONGUE BROKEN BETWEEN BS 1148 AND BS 1166 NEAR STRINGER 28 LEFT. REPLACED SECTION OF SEAT TRACK FROM STA 1063L TO STA 1166L. MATERIAL USED, P/N BAC 1520-843, SPLICE MAT 7075-T6, 0.250, .75 X 24 7 075-T6, 1.25 X 8.5 7075-T6, 0.125, 18 X .75, 24 X 2.5. ACCOMPLISHED IAW SRM 53-10-5.
Part: SEAT TRACK — BROKEN (FUSELAGE)
INSPECTION TYPE:C, FUSELAGE STATION 517, RBL 0.5 SEAT TRACK IS BROKEN (BROKEN TONGUE). REPLACED SECTION OF SEAT TRACK FROM STA 490 TO STA 550, RBL 0.5, MATERIAL USED, P/N BAC 1520-1331, 5 IAW SRM 53-10-5.
Part: SEAT TRACK — DEFORMED (FUSELAGE)
INSPECTION TYPE:C, FUSELAGE STATION 940, RBL 45.5, SEAT TRACK HAS 1 ELONGATED HOLE, DEFORMED TONGUE. REPLACED SECTION OF SEAT TRACK FROM BS 870 - BS 1000. MATERIAL USED, P/N BAC1520-1434, SIZE 12'' IAW B727 SRM 53-10-5 FIG 7.
Part: SEAT TRACK — BROKEN (FUSELAGE)
INSPECTION TYPE:C, FUSELAGE STATION 541, LBL 62.75, CARGO TRACK HAS 1 BROKEN TONGUE. REPLACED SECTION OF SEAT TRACK FROM BS 445 - 550, LBL 62.75 IAW SRM 53-10-5 FIG 7 MATERIAL USED P/N BAC 1520-1433.
Part: DRAG BRACE — INOPERATIVE (NLG)
INSPECTION TYPE:N/A, NOSE GEAR DID NOT EXTEND ON INITIAL TRY. FERRY PERMIT (9137) ISSUED AND SENT TO PRF, DURING INSP MX FOUND DURING GEAR EXTENSION, NOSE GEAR DELAYED SEVERAL SECONDS AND SOUNDED LIKE IT FREE FELL OR HUNG UP ON NOSE GEAR DOORS WITH A RESOUNDING CLUCK. *S/D* REMOVED AND REPLACED NLG DRAG BRACE ASSY IAW B727 MM 32-21-11. OPS CKD MLG-EXTENSION AND RETRACTION NORMAL IAW B 727 MM 32-32-00.
1999
Part: FITTING — CORRODED (NR 4 FLAP TRACK)
INSPECTION TYPE-C, NR 4 FLAP TRACK FORWARD MOUNT FITTING HAS CORROSION IN MOUNT HOLE BORES. NR 4 FLAP TRACK FITTING WAS REPLACED IAW OHM 20-50-01 PG 1 PARA 2 AND TABLE 1 AND M/M 27-51-31 PARA D8, ON NRC 879844.
Part: STRINGER — CRACKED (BS 850)
INSPECTION TYPE:C WHILE WORKING (EO B727-5310-5474) DISCOVERED CRACK IN STRINGER 17 LT BS 850 BL 70.5 WL 208. INSTALLED RADIUS FILLERS BS 848-TO BS 856 AND FABRICATED AND INSTALLED INTERCOSTAL BS 848 TO 870 PER 727 SRM 51-30-2, 51-40-4 AND 51-20-4.
Part: FITTING — CRACKED (LT MLG)
INSPECTION TYPE-C, LT MLG FWD TRUNNION AFT SPAR SUPPORT CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING PER SRM 51-30-1, AND DWG 65-19297.
Part: TRUNNION — CRACKED (LT MLG)
INSPECTION TYPE-C, LT MLG FORWARD TRUNNION FITTING CRACKED. REMOVED AND REPLACED LT MLG FORWARD TRUNNION FITTING IAW MM 32-11-51.
Part: TRUNNION — CRACKED (LT MLG)
INSPECTION TYPE-C, LT MLG FORWARD TRUNNION FITTING CRACKED. REMOVED AND REPLACED LT MLG FORWARD TRUNNION FITTING IAW MM 32-11-51.
Part: FITTING — CORRODED (LT TE FLAP)
INSPECTION TYPE:C, TORQUE TUBE SUPPORT FITTING JUST O/B OF MAIN LANDING GEAR BEAM CORRODED AT INBD AND OTBD LOWER FASTENERS HOLES. REMOVED AND REPLACED L/WING O/B FLAP TORQUE TUBE SUPPORT FITTING IAW MM 27-51-131.
1998
Part: LIGHT — INOPERATIVE (COCKPIT)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT IN COCKPIT INTERMITTENTLY FLASHES ON AND OFF WITH SWITCH IN ARM POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CK NORMAL.
Part: BATTERY — DISCHARGED (PAX DOOR)
ENTRY DOOR EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OP'S CHK'S GOOD.
Part: LIGHT — INOPERATIVE (CABIN)
FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY OPS IS INTERMINT AND BACK COVER IS MISSING. REMOVED AND REPLACED FWD ENTRY DOOR EMERG EXIT LIGHT ASSY PER M/M 33-50-01. OPS CHECK GOOD. OK FOR SERVICE. P/N : 10-0067-9,S/N OFF UNKNOWN S/N :ON 13697.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY OPERATION IS INTERMITTENT AND BACK COVER IS MISSING. REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT ASSEMBLY AS PER M/M 33-50-01, OP'S CHECKS GOOD.
Part: LIGHT — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE-N/A, COCKPIT EXIT LIGHT CAME ON AFTER LANDING WITH SWITCH IN OFF. SECURED COCKPIT EMER EXIT LIGHT, OPERATION OK.
1997
Part: LIGHT — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR ON WITH SWITCH IN ARMED POSITION. CYCLED SWITCH, OPS CKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A ON DEPARTURE CHECK, FOUND EMERGENCY EXIT LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT, OPS GOOD.
Part: LIGHT — INOPERATIVE (COCKPIT)
COCKPIT EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WHEN TESTED. RESEATED EMERGENCY LIGHT ASSEMBLY OPS CK NML.
Part: FITTING — CRACKED (RT MLG DOOR)
INSPECTION TYPE:C RT MLG WING DOOR ATTACH FITTING CRACKED. FITTING REPLACED IAW EO B727-3210-2583F APP D.
Part: PRESSURE WEB — CRACKED (NLG WW)
INSPECTION TYPE:C CRACK CONFIRMED AT BS 282 WL 172 RT NOSE WHEEL WELL PRESSURE WEB PRESSURE WEB REPLACED IAW DRG 65-18414.
Part: PRESSURE WEB — CRACKED (NLG WW)
INSPECTION TYPE:C CRACKS CONFIRMED AT BS 242 WL 168 AND BS 282 WL 172 LT NOSE WHEEL WELL PRESSURE WEB. PRESSURE WEB REPLACED IAW DRG 65-18414.
Part: EYE END — WORN (LT MLG)
INSPECTION TYPE:C LT MLG MANUAL EXTENSION UPLOCK RELEASE SHAFT PUSHROD EYE ENDS WORN EYE ENDS REPLACED IAW MM 32-34-0.
Part: CHORD — CORRODED (BS 1080)
INSPECTION TYPE:C LOWER AFT CARGO COMPARTMENT AT BS 1080 EYE BEAM HAS SOME SURFACE CORROSION. LOWER AFT CARGO COMPARTMENT CHORD REPLACED IAW SRM 53-10-2 FIG 7 AN D 51-10-5.
Part: CHORD — CORRODED (BS 594)
INSPECTION TYPE:C SURFACE CORROSION ON LOWER CHORD OF LONGITUDINAL I MEMBEER FWD CARGO COMPT CEILING BS 594 BBL 0. REPAIR CARRIED OUT IAW SRS EO 97-20-003 UPS ENG FILE NUMBER 727-53-1 957.
Part: BRACKET — CRACKED (BS 1260)
INSPECTION TYPE:C PULLEY BRACKET FOR NR 2 ENG START CABLES BS 1260 CRACKED. PULLEY BRACKET REPLACED IAW MM 20-80-01.
Part: HINGE BRACKET — CRACKED (LT MLG DOOR)
INSPECTION TYPE-C, LT I/B FLAP TRACK- AFT HINGE BRACKET ON FLAP TRACK FOR LT MLG WING DOOR IS CRACKED. REPLACED HINGE BRACKET IAW SRM 51-30-2.
Part: SKIN — CRACKED (CARGO DOOR)
INSPECTION TYPE:C SKIN ON LOWER AFT CARGO DOOR AREA BLENDED OUT AT BS 1060 LOWER EDGE SIX INCHES IN FROM REAR EDGE HAS A CRACK. REPAIR CARRIED OUT IAW SRM 52-00-3 FIG 4.
Part: FITTING — CRACKED (BS 740)
INSPECTION TYPE-C, CRACK FOUND ON FUSELAGE FRAME FITTING BS 740 LT BETWEEN S19L AND S2 0L. REPAIRED IAW UPS EO B727-5310-7497.
Part: PRESSURE PANEL — CORRODED (NLG WW)
INSPECTION TYPE-C, SURFACE CORROSION ON LT PRESSURE PANEL NLG WHEEL WELL CEILING. REPLACED DOME PANEL IAW SRM 51-10-1.
Part: BRACKET — CORRODED (BS 304)
INSPECTION TYPE-C, CORROSION ON FLOOR BRACKET BETWEEN STN 294.5 AND STN 312 LBL 14.00. CORRODED BRACKET REMOVED AND FOUND TO BE OUTSIDE LIMITS OF SRM 51-10 -6. NEW BRACKET FABRICATED FROM 7075 T0 0.040 INCH AND HT TO T6 REF HT NR 97-20-03 AND SRM 51-20-1. BRACKET REPROTECTED IAW SRM 51-10-2 AND FITTED REF SRM 51-30-2.
Part: CHANNEL — CRACKED (BS 520-540)
INSPECTION TYPE-C, CHANNEL SECTION BETWEEN BS 520 AND BS 540 RBL 17 IN FWD CARGO IS CRACKED. REPLACED CHANNEL SECTION IAW SRM 51-30-2 AND SRM 51-10-1.
Part: DOOR — DENTED (CARGO COMPT)
INSPECTION TYPE-C, DAMAGE TO FWD LOWER CARGO DOOR BOTTOM EDGE FIVE INCHES FWD FROM AFT EDGE STA 570 RT. REPAIR CARRIED OUT IAW SRM 52-00-3 FIG 4.
Part: FITTING — CRACKED (BS 740)
INSPECTION TYPE-C, CRACKS FOUND ON FUSELAGE FRAME FITTING BS 740 RT BETWEEN S18R AND 19R, S19R AND S20R, S23R AND S24R. FRAME REPAIRED IAW UPS EO B727-5310-7497.
Part: SKIN — DENTED (CARGO DOOR)
INSPECTION TYPE:C LOWER AFT CARGO DOOR, AREA DRESSED OUT AT BS 1057 S24R OUTSIDE LIMITS AS PER SRM 52-00-2. REPAIR CARRIED OUT IAW SRM 52-00-3 FIG 4.
Part: SKIN — DENTED (CARGO DOOR)
INSPECTION TYPE:C LOWER AFT CARGO DOOR, AREA DRESSED OUT AT BS 1083 S19R OUTSIDE LIMITS AS PER SRM 52-00-2. CARRIED OUT REPAIR IAW SRM 52-00-3 FIG 4.
1996
Part: CIRCUIT BREAKER — TRIPPED (COCKPIT)
INSPECTION TYPE-N/A, AFTER TAKEOFF ENTIRE CREW NOTED A STRONG ODOR IN COCKPIT RESEMBLING ELECTRICAL SMOKE. FOUND STBY ALT/AS CB POPPED, ODOR STOPPED. DID NOT ATTEMPT TO RESET CB. PERFORMED OPS CHK ON STBY ALT/AS IND PER MM 34-12-06 PG 501, SYS OPS CHK GOOD COULD NOT DUPLICATE.
Part: SENSE WIRES — CHAFED (LT AIRSTAIR WALL)
NR 1 ENGINE STRUT OVERHEAT FLICKERED TWICE DURING CRUISE. FOUND STRUT DETECTOR WIRES WITH MINOR SIGNS OF CHAFING. CORRECTED ALL CHAFING AREAS. SYSTEM CHECKS NORMAL. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (COCKPIT)
MAINTENANCE REPORTED EMERGENCY LIGHT IN COCKPIT FAILED. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL.
Part: FORGING — CRACKED (BS 870)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT AFT 870 TERMINAL FORGING IS CRACKED AT BS 870 WL 188 LBL 67. REMOVED CRACKED AREA AND NDT VERIFIED CRACK CONTAINMENT, REPAIRED IAW EO 96-2060.
Part: FLOORBEAM — CORRODED (BS 1110)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOORBEAM UPPER FLANGE BS 1110 RBL 50 TO 56 LBL 3 TO 20 AND 40 TO 44. REMOVED CORROSION, OUT OF LIMITS REPAIRED PER EWO 96-2087.
Part: SKIN — CORRODED (BS 640-660)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INNER SKIN BS 640 TO 660 BETWEEN STR 2 TO 3 LT. REMOVED CORROSION, OUT OF LIMITS PER SRM 53-30-2 FABRICATED REPAIR PARTS AND INSTALLED IAW 96-2089.
Part: FORGING — CRACKED (BS 950)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED WHILE WORKING FUSELAGE CUST NR 433165, FOUND A CRACK ON THE BS 950 FORGING AT THE FWD SIDE OF PRESSURE WEB ATTACH FITTING. DRILLED CRACK AND VERIFIED CRACK CONTAINMENT, INSTALLED NEW FITTING AND REPAIRED IAW EO 96-2098.
Part: STRINGER — CORRODED (BS 940)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STRINGER 18A LT HAS NO EDGE DISTANCE AT STA 940, DUE TO CORROSION IN FASTENER HOLES. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EWO 96-2090.
Part: FORGING — CRACKED (BS 940)
DURING 'C' CHECK MAINTENANCE REPORTED, BS 940 FORGING CRACKED AT STRINGER 18A, WL 208. REPLACED FORGING IAW EO B727-5310-4501C.
Part: GATE — CORROSION (BS 328)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR LOWER GATE EXTERNAL SURFACE CORRODED CORROSION (C53-224-01.06-01). REMOVED AND REPLACED FWD ENTRY DOOR LOWER GATE IAW UPS SRM 51-30-2, 51-10-1, 51-10-2 AND UPS MM 52-11-00.
Part: GATE — CORROSION (BS 328)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD ENTRY DOOR UPPER GATE CORRODED AROUND LOWER RIV-NUTS AND EXTERNAL EDGES CORROSION (C53-224-01.06-01). REMOVED AND REPLACED FWD ENTRY DOOR UPPER GATE IAW UPS SRM 51-10-1, 51-10-2, 51-10-3 AND UPS MM 52-11-00.
Part: FLOORBEAM — CORROSION (BS 312)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01), ON FLOORBEAM STA 312 LBL 48 TO LBL 0 WL 208 AROUND NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM IAW UPS SRM 53-10-8, 51-10-6, 53-10-1.
Part: BONDING JUMPER — CORROSION (NR 5 LE FLAP)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 5 K-FLAP I/B UPPER LUG CORRODED AT BONDING JUMPER. REMOVED AND REPLACED NR 5 K-FLAP NRC 432723.
Part: SEAT TRACK — CORROSION (BS 870-1000)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK AT STA 870 TO 1000 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK FROM STA 870 TO 1060 LBL 45 IAW UPS SRM 51-30-2.
Part: FRAME — CRACKED (BS 930)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT 930 FRAME CRACKED AT TOP OF FORGED SECTION STR 14 BETWEEN RIVETS ON FACE OF FRAME. REPAIRED RT 930 FRAME AT STR 14R PER UPS EO NR B727-5310-2580-B APPENDIX 8.1 AND 8.2.
Part: FLOORBEAM — CORROSION (BS 640)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01), ON FLOORBEAM UPPER CHORD STA 640, LBL 60 TO RBL 60, WL 208 AROUND NUTPLATE HOLES. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED PER TRAMCO EWO 96-2071, EO 727-53-1727.
Part: FLOORBEAM — CORROSION (BS 1030)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01-05-03), ON FLOORBEAM UPPER FLANGE BS 1030, RBL 10 AND LBL 0 TO 58, WL 208. CORROSION REMOVAL ON FLOORBEAM UPPER FLANGE WAS OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED PER TRAMCO EWO NR 96-2079, EO NR 727-53-1729.
Part: FLOORBEAM — CORROSION (BS 600)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01) ON FLOORBEAM UPPER CHORD STA 600 RBL 45 TO RBL 65 WL 208, AROUND NUTPLATE HOLES. CORROSION REMOVAL ON UPPER CHORD OF FLOORBEAM WAS OUT OF LIMITS. BLENDED AREA, FABRICATED AND INSTALLED REPAIR PARTS, ALL WORK DONE PER TRAMCO EWO 96-2080, EO NR 727-53-1730.
Part: FLOORBEAM — CORROSION (BS 680)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES STA 680 LBL 60 TO RBL 60, WL 208. CORROSION REMOVAL ON FLOORBEAM UPPER CHORD WAS OUT OF LIMITS PER SRM 53-10-1. BLENDED AREA, FABRICATED REPAIR ANGLES, REPAIR PARTS AND INSTALLED PER TRAMCO EWO 96-2086 AND EO NR 727-53-1731.
Part: FLOORBEAM — CORROSION (BS 660)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01) ON FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES STA 660 RBL 10 TO RBL 55. MECHANICALLY REMOVED CORROSION FROM 660 FLOORBEAM UPPER CHORD RBL 10 TO 58. FOUND REWORK FROM RBL 54 TO 58 TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED AREA IAW UPS EO NR 727-53-1726.
Part: MID CHORD — CORROSION (BS 302)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT MID CHORD BETWEEN DOGHOUSE FLOOR AND BS 302 LBL 15 WL 170. CORROSION REMOVED OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED LT MID CHORD IAW SRM 51-30-2, 51-30-4 AND MM 51-20-151.
Part: HANDLE CASTING — CORROSION (LT EMER EXIT)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT AFT OVERWING EXIT EXTERNAL HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01.
Part: HANDLE CASTING — CORROSION (RT EMER EXIT)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON RT FWD OVERWING EXIT EXTERIOR HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01.
Part: ATTACH LUG — CORRODED (NR 1 LE FLAP)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 1 K-FLAP BULLNOSE I/B ROD ATTACH LUG IS CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW UPS OHM 57-51-01.
Part: HANDLE CASTING — CORROSION (LT EMER EXIT)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT FWD OVERWING EXIT EXTERIOR HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01.
Part: STIFFENER — CORROSION (BS 357)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER BS 357 LBL 16 AND WL 1498. CORROSION OUT OF LIMITS, REMOVED DAMAGED STIFFENER, FABRICATED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-1 AND DWG-18417.
Part: STIFFENER — CORROSION (BS 358)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER BS 358 LBL 6 AND WL 149. CORROSION OUT OF LIMITS, REMOVED DAMAGED STIFFENER, FABRICATED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-1 AND DWG-18417.
Part: FRAME — GOUGED (CARGO DOOR)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR HAS TOOLING MARKS/GOUGES IN Z-FRAME STA 590 WL 302. GOUGE OUT OF LIMITS, FABRICATED REPAIR ANGLE AND HEAT TREATED. INSTALLED PART IAW SRM 51-40-3, 51-10-2, 51-30-2, AND 53-10-1.
Part: UPPER LUG — CORRODED (NR 5 K-FLAP)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 K-FLAP O/B UPPER LUG CORRODED AT BONDING POINT. REMOVED AND REPLACED NR 5 K-FLAP IAW UPS MM 27-81-01.
Part: FITTING — CORRODED (RT INBD AILERON)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON I/B CENTER HINGE FITTING AILERON SIDE IS CORRODED AND BEARING BLOCK HAS BLOWN DUST COVER. REPLACED CENTER HINGE FITTING IAW UPS OHM 57-50-111 AND MM 27-10-41.
Part: WEB — CORRODED (BS 203-219)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON WEB AND ANGLES AT STA 203 TO 219 LBL 15 WL 159. REPLACED WEB IAW SRM 51-40-2, 51-30-2, 51-10-6, 51-10-2, 51-10-1, 53-10-1, 51-20-4, AND 51-20-1.
Part: CHORD — CORRODED (BS 330-346)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON MID CHORD BETWEEN DOG HOUSE FLOOR AND CHORD BS 330 AND 346 RBL 15 WL 170. REMOVED AND REPLACED MID CHORD IAW SRM 51-30-2 AND 51-20-4.
Part: STIFFENER — CORRODED (BS 344)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON VERT STIFFENER AT BS 344 LBL 14 WL 180. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2 AND 51-20-4.
Part: STIFFENER — CORRODED (BS 344)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON NOSE GEAR W/W VERT STIFFENER AT BS 344 LBL 14 WL 173 AND 180. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2 AND 51-20-4.
Part: SKIN — DELAMINATION (NR 5 SPOILER)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SPOILER NR 5 HAS DELAMINATION AT THE ACTUATOR FITTING AT FWD EDGE CENTER OF SPOILER BOTH UPPER AND LOWER SURFACE. REPAIRED SPOILER IAW SRM 51-40-6 AND 57-50-6.
Part: SKIN — DELAMINATED (NR 4 SPOILER)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 4 SPOILER HAS AN AREA OF DELAMINATION AROUND CENTER DOUBLER ON THE LOWER SURFACE. REPAIRED NR 4 SPOILER AROUND CENTER DOUBLER IAW SRM 51-40-6 AND 57-50-6.
Part: SEAT TRACK — DAMAGED (BS 550-650)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, SEAT TRACK STA 480 TO 650 RBL 45 WL 208 HAS MECHANICAL DAMAGE AND CORROSION. REPLACED SECTION OF SEAT TRACK FROM BS 550 TO 650 RBL 45 WL 208. WORK DONE PER SRM 53-10-5 AND 51-30-8.
Part: WEB — CORRODED (BS 227)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, VERTICAL WEB FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10-2 AT STA 227 LBL 41 TO 44 WL 209 TO 218, CORROSION (C53-221-01,03, 01). REMOVED DAMAGED AREA OF VERTICAL WEB, FABRICATED REPAIR PARTS AND INSTALLED PER 53-10-2 AND 51-20-4.
Part: SEAT TRACK — CORRODED (BS 650-740)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION IN WELL OF SEAT TRACK AT STA 680 TO 730, LBL 45, WL 208. REMOVED CORRODED SEAT TRACK FROM BS 650 TO 740, WL 208, LBL 45, FABRICATED NEW SECTION AND INSTALLED. ALL WORK DONE PER SRM 53-10-1 AND 53-10-5.
Part: BULLNOSE — CORRODED (NR 2 K-FLAP)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, L/W NR 2 K-FLAP BULLNOSE IS CORRODED AT O/B HINGE LOWER ATTACH POINT. REMOVED AND REPLACED BULLNOSE IAW MM 27-81-01 AND SRM 57-50-1.
Part: CENTER HINGE — CORRODED (LT INBD AILERON)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE IS CORRODED AT PANEL ATTACH POINT. REPLACED HINGE FITTING IAW MM 27-10-01.
Part: UPPER GATE — CORRODED (MID GALLEY DOOR)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MID GALLEY DOOR UPPER GATE HAS AREAS OF CORROSION. REMOVED AND REPLACED MID GALLEY DOOR GATE IAW SRM 51-10-1, 51-20-4, 51-30-8 AND MM 52-12-11.
Part: SPOILER — WATER ENTRAPED (LT WING)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS POSSIBLE WATER ENTRAPMENT IN VIEW 6 OF X-RAY. REPAIRED NR 1 SPOILER IAW SRM 51-40-6.
Part: SPOILER — WATER ENTRAPED (LT WING)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS POSSIBLE WATER ENTRAPMENT IN VIEW 4 OF X-RAY. REPAIRED NR 1 SPOILER IAW SRM 51-40-6.
Part: FITTING — CORRODED (NR 3 SPOILER)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, I/B CENTER HINGE BOLT HOLE CORRODED, NR 3 SPOILER. REMOVED AND REPLACED NR 3 SPOILER ACT HINGE FITTING IAW MM 27-61-81.
Part: SKIN — DELAMINATION (NR 1 SPOILER)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS AN AREA OF DELAMINATION AT HINGE AREA FWD EDGE CENTER OF SPOILER UPPER SURFACE. REPAIRED NR 1 SPOILER IAW SRM 51-40-6.
Part: SKIN — CORRODED (BS 300)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON INSIDE OF FUSELAGE SKIN BELOW FWD TOILET SERVICE PANEL AT BS 300 RBL 54 WL 182. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-30-3 AND 53-30-2.
Part: FRAME — CRACKED (CARGO DOOR)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED WHILE WORKING NRC 432263 DOOR 74, FOUND THE UPPER FLANGE ON THE LOWER AFT FRAME TO BE CRACKED. REPAIRED UPPER FLANGE ON THE LOWER AFT FRAME ON AFT CARGO DOOR IAW SRM 51-40-3.
Part: BULKHEAD — CRACKED (BS 178)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SUSPECTED CRACK AT FASTENER HOLE ON BS 178 BULKHEAD LBL 9, WL 236. REMOVED 2 FASTENERS, CLEANED AREA, NDT INSPECTED FOUND CRACK. TRIMMED OUT AREA THAT WAS CRACKED. NDT VERIFIED CRACK CONTAINMENT FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED ON AIRCRAFT IAW SRM 53-10-9, SRM 51-30-2.
Part: SEAT TRACK — CORRODED (BS 360-520)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 360-520, RBL 60, WL 208. REPLACED SEAT TRACK PER SRM 51-10-6, 53-10-5, AND 51-30-2.
Part: SKIN — CORRODED (BS 310)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON FUSELAGE SKIN AFT OF FWD TOILET SERVICE PANEL BS 310 RBL 68 WL 186. CORROSION OUT OF LIMITS, REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. ALL WORK DONE PER SRM 53-30-3 AND 53-30-2.
Part: SEAT TRACK — CORRODED (BS 344-360)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK FLANGE AROUND NUTPLATE HOLES AT STA 344-360, LBL 65, WL 208. REPAIRED PER SRM 53-10-1, 51-10-6, 51-30-2, 51-10-2, AND OHM 20-41-02.
Part: STIFFENER — CORRODED (BS 295)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION REINFORCING ANGLE AT BS 295, WL 181, RBL 12. REPLACED ANGLE PER SRM 51-10-6, 53-10-6, 53-10-2, 53-10-1, 51-30-5.
Part: FRAME — CRACKED (BS 320)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CRACKED FRAME BS 320, LBL 45. INSTALLED DOUBLER IAW SRM 51-30-2 AND 51-40-3.
Part: FITTING — CORRODED (LT AILERON)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2.
Part: HINGE ARM — CORRODED (RT AILERON)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION R/W I/B AILERON HINGE ARM. REPLACED HINGE PER UPS MM 27-10-01.
Part: HAT CHANNEL — CORRODED (BS 324-340)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL AT STA 324-340, RBL 20, WL 208. REPLACED HAT CHANNEL PER SRM 51-20-1, 51-10-2, 51-30-2.
Part: INTERCOSTAL — CORRODED (FS 211-219)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 211-219, RBL 25, WL 174. REPLACED INTERCOSTAL PER SRM 53-10-1, 51- 20-1, AND 51-10-22.
Part: FITTING — CORRODED (LT AILERON)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2.
Part: FLOOR BEAM — CORRODED (BS 312)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM STA 312, LBL 48, BL ZERO, WL 208, AROUND NUTPLATE HOLES. REPLACED FLOORBEAM PER SRM 53-10-8.
Part: STIFFENERS — CORRODED (BS 203)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON STIFFENERS AT STA 203, LBL 18 AND 22, WL 180. REPLACED STIFFENERS PER SRM 51-40-4.
Part: FITTING — CORRODED (LT AILERON)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2.
Part: FITTING — CORRODED (LT AILERON TAB)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON TAB FITTINGS, TAB SIDE. REPLACED FITTINGS PER SRM 51-30-2.
Part: STIFFENER — CORRODED (BS 308)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON HOR. STIFFENER TOP NOSE WW AROUND FASTENER HEADS BS 308, WL 181, LBL 10, RBL 10. REPAIRED PER SRM 53-10-1, 53-10-2, 51-10-6.
Part: FITTING — CORRODED (AILERON)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION R/W AILERON O/B HINGE FITTING. REPLACED FITTING PER SRM 51-30-2 AND 51-10-1.
Part: FRAME — CRACKED (BS 284.5)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED FRAME CRACKED AT BS 284.5 AT STR 24R, RBL 20. REPAIRED PER SRM 51-30-2 AND 53-10-2.
Part: SEAT TRACK — CORRODED (BS 760-848)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 760-848, RBL 60, WL 208. REPLACED SEAT TRACK PER SRM 51-10-6, 53-10-5, AND 51-30-2.
Part: HINGE FITTING — CORRODED (AILERON TAB)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE LT I/B AILERON TAB HINGE FITTINGS, AILERON SIDE. REPLACED IAW 727 SRM 51-30-2.
Part: HINGE — CORRODED (RT AILERON)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE RT WING O/B AILERON CENTER O/B HINGE AILERON SIDE. REPLACED PER SRM 51-30-2.
Part: BULLNOSE — CORRODED (NR 3 LE FLAP)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON THE L/W NR 3 K-FLAP BULLNOSE CENTER HINGE LOWER ATTACH POINT. REPLACED NR 3 K-FLAP PER MM 27-81-00.
Part: HANDLE — CORRODED (OVERWING EXIT)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION OF RT AFT EXTERNAL HANDLE SEAL CASTING ON OVERWING EXIT. REMOVED AND REPLACED CASTING IAW SRM 51-30-02, 51-10-05 AND 51-10-08.
Part: HINGE FITTING — CORRODED (RT AILERON)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE RT WING I/B AILERON HINGE FITTINGS O/B AND CENTER FITTINGS. REPLACED FITTINGS PER SRM 51-30-2.
Part: HINGE FITTING — CRACKED (RT AILERON)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON O/B HINGE FITTING IS CORRODED. REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-30-2.
Part: HINGE FITTING — CORRODED (RT AILERON)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER O/B HINGE FITTING IS CORRODED. REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-30-2.
Part: ANGLE — CRACKED (FS 804)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK ON WEB TIE ANGLE AT STA 804 STR 10 RT. REPAIRED WEB AND FABRICATED TIE ANGLE.
Part: THRUST SHAFT — CORRODED (TE FLAP)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON THE NR 7 FLAP CARRIAGE LOCATER ON THE THRUST SHAFT FWD OF THE THRUST NUT. RECEIVED NEW FLAP CARRIAGE.
Part: SPOILER — WATER ENTRAPMENT (NR 3 SPOILER)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW X-RAY NR 3 SPOILER. REPAIRED PER SRM 51-40-6.
Part: SUPPORT FITTING — CORRODED (NR 11 SPOILER)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FLUORESCENT PENETRANT INSPECTION OF THE NR 11 O/B FLT SPOILER ACT SUPPORT FITTING, EXHIBITS CORROSION INDICATIONS AROUND THE HOLE ON BOTH THE I/B AND O/B LOWER LUGS. REMOVED AND INSTALLED NEW FITTING. WORK DONE PER SRM 51-30-2, MM 27-51-131, AND 27-61-81.
Part: SHEAR TIE — CRACKED (BS 277)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED UPPER SHEAR TIE CRACKED AT BS 277, STR 16 RT, ACCESSING REQ. REPAIRED IAW 51-40-02 FIG 1.
Part: SPOILER — WATER ENTRAPMENT (NR 14 SPOILER)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 4 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6.
Part: SPOILER — WATER ENTRAPMENT (NR 14 SPOILER)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 6 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6.
Part: SPOILER — WATER ENTRAPMENT (NR 14 SPOILER)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 5 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6.
Part: SPOILER — WATER ENTRAPMENT (NR 9 SPOILER)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 8 OF X-RAY OF SPOILER NR 9. REPAIRED PER SRM 57-50-6.
Part: SPOILER — WATER ENTRAPMENT (NR 7 SPOILER)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 5 X-RAY NR 7 SPOILER. REPAIRED PER SRM 51-40-6.
Part: SEAT TRACK — DAMAGED (BS 680-700)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MECHANICAL DAMAGE ON SEAT TRACK AT STATION 680 TO 700 LBL 65 WL 208. FOUND DAMAGE TO BE OUT OF LIMITS, REMOVED DAMAGED SEAT TRACK AND REINSTALLED FABRICATED SEAT TRACK WITH FASTENERS AT STA 683 TO 740 IAW SRM 51-30-02, 51-10-02, AND 53-10-1.
Part: FRAME — CRACKED (BS 930)
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT STA 930 FRAME CRACKED ON ZEE FRAME T-FORGED FRAME AT SPLICE ON STRINGER NR 14. REMOVED CRACKED FRAME, POSITIONED AND INSTALLED NEW FRAME, LOCATED ALL HOLES AND SECURED WITH FASTENERS IAW EO B747-5310-2580-B ER 020596JM1, ER 0214964D1 SRM 51-40-04, 53-10-3.
Part: FLOOR BEAM — CORRODED (BS 344)
WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM AT STA 344, RBL 17-20, WL 208. REPAIRED FLOOR BEAM PER SRM 53-10-8, FIG. 7 AND E.R. NR 020696CD3, 53-10-10.
1995
Part: TE SKIN — DELAMINATED (NR 6 SPOILER)
WHILE ON GROUND, MAINTENANCE FOUND NR 6 SPOILER LT WING DELAMINATED ON TRAILING EDGE. REMOVED AND REPLACED NR 6 GROUND SPOILER (P/N 65-17348-108A) (S/N 5758) ON, (P/N 65-17348-55) (S/N 6307) OFF.
Part: EEL BULB — FAILED (FLIGHT DECK)
MAINTENANCE REPORTED EMERGENCY EXIT LIGHT (UNARMED) ON PILOT'S OVERHEAD INOP. RELAMPED EMER EXIT LIGHTS. OPS CHECK GOOD PER MM 33-50.