N950UP
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.
220 reports on file, 1995-01-05 – 2004-12-16.
Part: LIGHT — MALFUNCTIONED (EMERGENCY EXIT)
EMERGENCY EXIT LIGHT IN COCKPIT FLICKERS VERY DIM WHEN SWITCH PLACED TO ON. REMOVED AND REPLACED EMERGENCY LIGHT PER 33-50-1, TEST OK.
Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)
EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERIES IN FWD & AFT EXIT LIGHTS, ALL CHECK GOOD IAW MM 33-50.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE:N/A ON INSPECTION SEAT TRACK SECTION FOUND CORRODED AT BS 730 AT RBBL 625 APPROX. NEW SEAT TRACK SECTION FABRICATED IAW SRM 51-20-1 AND ALODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW EO B727-5310-7477 STEP 28.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, SUSPECT CRACK IN NLG WW LOCATED ON PRESSURE WEB B STA 240 RBL 24. AREA REPAIRED IAW SRM 51-40-02.
Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING IS CRACKED AT MID AFT END. REPLACED FAIRING IAW MM 78-30-43.
Part: FITTING — CRACKED (NACELLE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, AREA ABOVE NR 2 HORIZONTAL FIREWALL, UPPER LEFT FITTING AT STA 1470. 5 AND WL 300.15 IS CRACKED. FITTING REMOVED IAW SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02 AND BOEING DRAWING 65-17553.
Part: BULKHEAD — CRACKED (NLG WW) · airframe 67,038 hrs · 19,303 cycles
INSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL WALL AT LBL 24, BS 285 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2, 51-40-07 & MM 32-33-51.
Part: WEB — CRACKED (LT I/B AILERON) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, LEFT I/B AILERON, O/B WEB CRACKED AT AFT UPPER FASTENER, AND FASTENER MISSING FROM WEB. REPAIR CARRIED OUT IAW 51-30-02.
Part: PANEL — CRACKED (LT WING) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, CRACK ON LT WING T/E PANEL UPPER SURFACE FWD OF NR 5 SPOILER. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30-02 & 51-10-02.
Part: WEB — CRACKED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, NOSE WHEEL WELL STRUCTURE HAS EVIDENCE OF CRACK AT BSTA 240 LBL. REPAIR CARRIED IAW SRM 51-40-02. LEAK CHECKED SATISFACTORY.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, ATTACH FITTING AT THE BASE OF THE BS 950 STRUCTURAL FITTING HAS EVIDENCE OF INTERGRANULAR CORROSION. FITTING REPLACED IAW SRM 51-30-02 & DRAWING 65-16338.
Part: SKIN — CRACKED (NR 6 LE FLAP) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, NR 6 L/E FLAP CRACKED I/B OF LANDING LIGHT & JUST ABOVE BULLNOSE. FLAP REPLACED IAW MM 27-81-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, DUE TO BELOW MIN EDGE DISTANCE & CORROSION ON SKIN DURING RT 740 FITTING REPLACEMENT, SKIN REPAIR REQUIRED BETWEEN S17 & S18 RT TO BETWEEN S24 & 25 RT. REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING EO 2004-054-005 & SRM 51-30-2 7 51-20-04 UPS ENGINEERING FILE 727-53-20144.
Part: SKIN — CORRODED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, FASTENER HEAD POPPED & BULGE IN SKIN. SUSPECT CORROSION BETWEEN SKIN & STR AT BS 1065 S29L. SKIN CUTOUT BETWEEN BS 1061 AND BS 1072 AT S29L, CORROSION REMOVED IAW SRM 51-10-6. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR COMPLETED IAW AAAE EO 2004-054-001 AND UPS EO 727-53-20148.
Part: SKIN — CRACKED (LT WING) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE:C SUSPECT CRACK IN SKIN AT LT WING ICE LIGHT CUTOUT (UPPER FWD). REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING 2004-054-004 & SRM 51-30-02 & 51-00-00.
Part: SKIN — CORRODED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, BULGING IN SKIN AT BS 1183 BETWEEN S6R AND S10R. CUT OUT INTERNAL BONDED DOUBLER BETWEEN S6R TO S10R BS 1183 TO BS 1177 REFERENCE SRM 53-30-3. HFEC CARRIED OUT, NO DEFECTS FOUND. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3. REPAIR DOUBLER AND FILLER INSTALLED WITH SEALANT IAW SRM 53-30-3 FIG 1 AND 5.
Part: ANGLE — CORRODED (NLG WW) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, CORROSION AT BS 312L VIEW IN 3RD LIGHTENING HOLE FROM FRONT OM INBOARD ANGLE MIDWAY BETWEEN UPPER AND LOWER NWW CHORDS. CORRODED ANGLE FABRICATED AND INSTALLED IAW DWG 65-18415.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
CRACK IN SKIN AT FWD ENTRY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460 & SRM 51-30-02.
Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, NR 5 LEFT BALANCE BAY PANEL HAS VERY LITE SURFACE CORROSION. UPON INVESTIGATION, CORROSION FOUND TO BE BEYOND LIMITS. BALANCE PANEL PLATE REPLACED IAW MM 27-30-27.
Part: SKIN — CORRODED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, SKIN CORRODED AT BS 1263 S9R. CORROSION REMOVED IAW SRM 53-30-3 FIG 4. HFEC CARRIED OUT AROUND CUTOUT, NO DEFECTS FOUND. COMPLETED REPAIR IAW AAAE EO 2004-054-003.
Part: TEE FITTING — CRACKED · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, TEE FITTING CRACKED ON UPPER I/B T-EDGE PANEL FOR APU EXHAUST 70.5 WBL. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-10-2.
Part: SUPPORT — CRACKED (CENTER ENGINE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, CENTER ENGINE LEFT AND RIGHT SUPPORT WEBS AT BS 1387 ARE CRACKED. WEBS REMOVED IAW SRM 51-30-02. NEW WEBS FABRICATED IAW BOEING DRAWING 65-17553, NEW WEBS INSTALLED IAW SRM 51-30-02.
Part: SKIN — CORRODED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, FASTENERS POPPED AT S25R BETWEEN BS 290 & BS 300 SUSPECT CORROSION BETWEEN SKIN & STRINGER. REPAIR CARRIED OUT IAW SRM 51-20-01, 51-30-02, 51-10-1, 53-30-01, 51-20-04 & 51-80-01.
Part: FITTING — CRACKED (FUSELAGE) · airframe 67,038 hrs · 49,303 cycles
INSPECTION TYPE: C, RIGHT BS 740 FITTING CRACKED BEYOND LIMITS OUTBOARD FLANGE. FITTING REPLACEMENT & REPAIR CARRIED OUT IAW AAAE EO 2004-054-005 UPS ENG FILE 727-53-20144 & UPS EO B727-5310-7477, DRG 65C13724 & SRM 51-30-2.
Earlier reports · 1995–2003 · 196 reports
2003
Part: LIGHT — INOPERATIVE (DOOR)
L-1 DOOR EMERGENCY LIGHT TEST INOPERABLE. REMOVED AND REPLACED AND CKD OK USED AMERICAN AIRLINES BORROWED PART MM 33-50-01 P/N ON OFF 10-0067-9, S/N OFF 7012 S/N ON 22921.
2002
Part: BUTT JOINT — CORRODED (FUSELAGE)
C CHECK FUSELAGE AT SKIN BUTT JOINT BS 260 AND BETWEEN STR 12 RT & 13 RT IS BULGING CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER AS PER BOEING DRAW ING 69-62161 AND UPS E.O. B727-5310-1371-F APPENDIX E
2001
Part: WINDOW — CRACKED (COCKPIT)
INSPECTION TYPE:N/A, F/O SLIDING WINDOW CRACKED. REMOVED AND REPLACED NR 2 WINDOW ASSY PER MM 56-12-11. OPS CHECKS NORMAL P/N OFF/ON 5-71762-42 SN OFF 56WIN1244 ON UP01358.
Part: STRINGER — CORRODED (BS1183 STR 18L)
INSPECTION TYPE:C STRINGER TERMINAL FITTING CORRODED AT BS 1183 STR 18L REMOVED CORRODED STRINGER BS 1183, STR18L. PER SRM 51-30-2, FABRICATED STRINGER TERMINAL FITTING PER BOEING DRAWING 65-242276 AND B727 SRM 51-10-2 TREATED AND PRIMED. INSTALLED STRINGER TERMINAL FITTING ON AIRCRAFT.
Part: SKIN — CRACKED (NLGWW BS 294 R/H)
INSPECTION TYPE:C NOSE WHEEL WELL R/H SIDE WALL SHOW CRACK AT BS 294 WL165 CRACK ABOUT 10" LONG LOOKING GROM INSIDE REMOVED VERTICAL ANGLE FOR ACCESS REPAIR PER B727 SRM 51-30-2 CUT OUT DAMAGE AREA PER B727 SRM 51-40-2 APP.4 SIDE CUT OUT 6"X1" PERFORMED HFEC INSP AT CUT OUT DAMAGE. INSTALL DOUBLER REPAIR AS PER B727 SRM 51-30-2 REPAIR SIZE APPROX 10"X4".
Part: BULKHEAD — CRACKED (NWW BS 294.5)
INSPECTION TYPE:C CRACKS AT BULKHEAD STA 294.5 RBL 12, NOSE LANDING GEAR WHEEL WELL, INSPECTED. INSPECTED NLG WHEEL WELL BULKHEAD AND VERIFY CRACK AS PER B727 NAT MANUAL PART 6 51-00-00 FIG 4. REMOVED VERTICAL ANGLE TO ACCESS REPAIR AND CUT OUT CRACK AREA AS PER B727 SRM 51-30-2 REPAIR IN ACCORDING PER UPS EFILE# B72753-200-18 AND AUITAS EREPAIR ORDER# AUH M223RO-1 REV IR
Part: SPAR — CRACKED (LT WING)
INSPECTION TYPE:C, LEFT WING REAR SPAR UPPER CHORD AT WING STATION APPROX CRACK INDICATION IS ABOUT 2 INCHES LONG OUTBOARD OF NR 1 FUEL SOV. REMOVE CRACK AT REAR SPAR UPPER CHORD AT WS 190 AND INSTALL FILLER AND DOUBLER REPAIR AS PER BOEING DRAWING 65C196447, REMOVED AND REPLACED STIFFENER AT WS 192 AS PER BOEING DWG 65C19647 AND B727 SRM 51-30-2, INSTALLED WEB REPAIR ON LT WING RIB AFT AT WBL 928 PER B727- SRM 51-40-2.
Part: KEELBEAM — CRACKED (FUSELAGE)
INSPECTION TYPE:C KEEL BEAM BS 900 APPROX APU COMPARTMENT ACCESS PANEL SHOWS A HOLE AND CRACKED AREA. CUT DAMAGED AREA AT KEEL BEAM ACCESS PANEL BS 900 APU COMPARTMENT AS PER B727 SRM 51-10-1, INSTALLED DOUBLER ON KEEL BEAM ACCESS PANEL AS PER B727 SRM 51-40-2 FIG 1.
Part: SKIN — CORRODED (FUSELAGE)
INSPECTION TYPE:C, INDICATION OF MATERIAL LOSS GREATER THAN 10 8/0 IN THE SKIN AT CIRCUMFERENTIAL JOINT BS 441 BETWEEN S 17R AND S 20R FORWARD PANEL. CUT DAMAGED AREA ON STA 441 BETWEEN STA 17R AND STA 20R PER DRAWING 69-62161. INSTALLED DOUBLER REPAIR IN CUT OUT AREA PER UPS EO B727 5310-1371E APPENDIX 8.5 AND DRAWING 69-62161.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:IN, EMERGENCY EXIT LIGHTS INOP ON LT OVERWING LIGHTS AND LT REAR EMERGENCY EXIT LIGHT NEXT TO LAV DOOR. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, RIGHT FWD OVERWING FLOOR EMERGENCY LIGHT FAILED TO TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:IN, LEFT LOWER FLOOR EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:IN ROW 9 LEFT SEAT EMERGENCY LIGHT TEST. REMOVED AND REPLACED ROW 9 SEAT EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:IN, FWD BULKHEAD EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:IN RT FWD OVERWING EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:IN, FWD PAY DOOR LOWER FLOOR EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, AFT LEFT LAV LOWER EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, RT CEILING OVERWING EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, FORWARD ENTRY WAY CEILING EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED FWD ENTRY WAY CEILING EMERGENCY EXIT LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:IN ROW 4 SEAT 4 EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 4 EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, REAR EXIT CEILING EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED REAR EXIT CEILING EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, ROW 19 LEFT SEAT EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED ROW 19 EMERGENCY LIGHT BATTERY ASSY PER MM 33-50-22. OPS CHECKS GOOD.
Part: BATTERY — DISCHARGED (OVERWING)
INSPECTION TYPE:IN REF M208478 RT OVERWING DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY, OPS GOOD.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, EMERGENCY INTERIOR OVERWING LIGHT INOP ACFT IN CARGO MODE. *S.D* REMOVED AND REPLACED BATTERY, OPS GOOD. THIS CLEARS M208478.
2000
Part: INDICATOR — FAILED (COCKPIT)
INSPECTION TYPE:N/A ATB - NB 2 FUEL QTY WENT TO ZERO. SUMPED NR 2 FUEL TANK. PERFORMED ADJ/TEST OF NR 2 FUEL QTY INDICATION SYSTEM PER REF 28-41-00. SYS OPS CKS NORMAL. THIS CLEARS M206491. PLACARD REMOVED.
Part: BATTERY PACK — FAILED (COCKPIT)
INSPECTION TYPE:N/A AFT LEFT OVERWING EMERGENCY LIGHT INOP RNR'D BATTERY PACK, OPS GOOD
Part: BATTERY PACK — FAILED (COCKPIT)
INSPECTION TYPE:N/A FWD ENTRY DOOR EMERGENCY LIGHT INOP RNR'D BATTERY PACK, OPS GOOD.
Part: BATTERY PACK — FAILED (COCKPIT)
INSPECTION TYPE:N/A AFT RIGHT OVERWING EMERGENCY LIGHT INOP. RNR'D BATTERY PACK, OPS GOOD.
Part: LIGHT — INOPERATIVE (GALLEY)
INSPECTION TYPE:N/A, AFT OVERHEAD EXIT LIGHT IN GALLEY INOP. REMOVED AND REPLACED BATTERY. OPS GOOD.
Part: LIGHT — INOPERATIVE (OVERWING)
INSPECTION TYPE:N/A, RIGHT AFT SIDEWALL OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS GOOD.
Part: LIGHT — INOPERATIVE (OVERWING)
INSPECTION TYPE:N/A, RIGHT FWD SIDEWALL OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS GOOD.
Part: LIGHT — INOPERATIVE (OVERWING)
INSPECTION TYPE:N/A, LEFT FWD SIDEWALL OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS GOOD.
Part: LIGHT — INOPERATIVE (OVERWING)
INSPECTION TYPE:N/A, LEFT AFT SIDEWALL OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OP CHECKS GOOD.
Part: BATTERY PACK — INOPERATIVE (ROW 19)
INSPECTION TYPE:N/A, EMERGENCY LIGHT IN ROW 19L INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, EMERGENCY LIGHT AT FWD ENTRY, GALLEY ENTRY AND ROW 17L INOP. REMOVED AND REPLACED BATTERY PACK, SYSTEM OPS GOOD.
Part: BATTERY PACK — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, EMERGENCY LIGHT ABOVE F/A FWD SEAT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, EMERGENCY LIGHT FOR MAIN ENTRY DOOR INOP. REMOVED AND REPLACED LIGHT BATTERY PACK, OPS CHECK NORMAL.
Part: BATTERY PACK — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, RIGHT AFT OVERWING EMERGENCY LIGHT FOR INSIDE DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD.
Part: PRESSURE PANEL — CRACKED (NLG WW)
INSPECTION TYPE:N/A, CRACK IN TOP OF NOSE W/W APPROX 4 INCHES LONG. REPAIRED AREA IAW SRM 53-10-9. 7-11-2K.
Part: LIGHT — INOPERATIVE (CABIN)
EMERGENCY EXIT LIGHT INOP AT GALLEY DOOR. REMOVED AND REPLACED EMERG BATTERY PACK TESTED OK.
Part: LIGHT — INOPERATIVE (CABIN)
EMERG EXIT LIGHT INOPERATIVE AT FWD L1 DOOR. REMOVED AND REPLACED EMERG BATTERY PACK.
Part: BATTERY PACK — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, ALL EMERGENCY LIGHTS INOP (INTERIOR). REPLACED ALL EMERGENCY LIGHT BATTERY ASSY.
Part: BATTERY PACK — INOPERATIVE (OVERWING)
INSPECTION TYPE:N/A, RT AFT OVERWING EMERGENCY EXIT LIGHT ON SIDEWALL INOP. REMOVED AND REPLACED BATTERY PACK, LIGHT OPS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT OVER RIGHT FWD OVERWING DOOR WAS INOP. REPLACED BATTERY PACK, OPS CHECKS OK.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A EMERGNECY EXIT LIGHT OVERHEAD THAT POINTSTO LEFT OVERWING DOORS IS INOP. REPLACED BATTERY PACK OPS OK
Part: LIGHT — INTERMITTENT (CABIN)
INSPECTION TYPE:A/SE, EMERGENCY EXIT LIGHT LOWER RIGHT SIDE OF MAIN ENTRY DOOR FLICKERING, WILL NOT GO OUT. TESTED EMERGENCY LIGHTS WHICH RESET SYSTEM, NORMAL OPERATION AFTERWARD.
Part: BATTERY PACK — DISCHARGED (CABIN)
PAX EMERGENCY LIGHT AT FWD BULKHEAD ABOVE F/A JUMPSEAT IS INOP. REMOVED AND REPLACED EMERGENCY AREA LIGHT AND PANEL ASSY AND BATTERY PACK IAW MM 33-50-10. OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY LIGHT AT FWD PAX DOOR INOP. REMOVED AND REPLACED LIGHT BATTERY PACK AT FWD PAX DOOR IAW MM 33-50 -00, OPS CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
FWD EMERGENCY LIGHT IS INOP AND AFT LIGHT IS DIM AT SEAT 13C. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT 13C IAW MM 33-50-00, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
FWD EMERGENCY LIGHT IN INOP AND AFT LIGHT IS DIM AT SEAT 2C. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT 2C IAW MM 33-5 0-10, OPS CHECKS NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY LIGHT INOP AT LEFT MID GALLEY BULKHEAD. REMOVED AND REPLACED LIGHT BATTERY PACK AT LEFT MID GALLEY BULKHEAD IAW MM 33-50-00. OPS CHECK NORMAL.
1999
Part: BATTERY — DISCHARGED (COCKPIT)
INSPECTION TYPE:N/A, EMERENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS OK.
Part: SKIN — CORRODED (WS 867)
INSPECTION TYPE:SI DISCOVERED CORROSION ON LOWER SURFACE OF UPPER WING CENTER SECTION SKIN AT BS 867 RBL 66 AND LBL 66. REPAIRED IAW BFG ER 99-6346 (UPS FILE NR B727-5710-12093).
Part: STRINGER — CORRODED (BS 463)
INSPECTION TYPE:SI CORROSION ON STRINGER AT BS 463 STR 21R. REPAIRED STRINGER PER SRM 53-10-3 FIG 1.
Part: SKIN — CORRODED (BS 355)
INSPECTION TYPE:SI BULGING SKIN AT BS 355, STR 27R, WL 156. REPAIRED BULGING SKIN AT BS 355, STR 27R, WL 156 IAW ER 99-6374 AND SRM 53-30-03 FIG 3A AND ER 99-6412.
Part: SHEAR TIE — CORRODED (BS 480)
INSPECTION TYPE:SI SHEAR TIE AT BS 480 STR 20-21 RT IS CRACKED AND CORRODED. FABRICATED AND REPLACE SHEAR TIE PER SRM 53-10-4 AND SRM 51-30-2.
Part: STRINGER — CORRODED (12-1)
INSPECTION TYPE:SI CORROSION ON STRINGER BS 360 TO 380, STR 26L. REMOVED AND REPLACED STRINGER SEGMENT PER SRM 53-10-3 FIG 1.
Part: ANGLES — CORROSION (13-1)
INSPECTION TYPE:SI CORROSION (C53-111-01.03-02) ON FWD CARGO BAY CEILING BEAM AROUND 2 EACH FASTENER HOLES BS 580-BS 600, BL 0, WL 200. REMOVED DAMAGE AND REPAIRED PER ERO 99-6278.
Part: BEAM — CRACK (24-2)
INSPECTION TYPE:SI CRACK IN VERTICAL BEAM AT BS 1183, LB 18.5, WL 275. REMOVED DAMAGE AND REPAIRED PER UPS EO B727-5310-7267 APPX B.
Part: ANGLE — CORROSION (23-2)
INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) CORROSION ON AFT EDGE OF L-ANGLE AT BS 297, RBL 12-RBL 54, WL 208. REMOVED L-ANGLE AND REPLACED.
Part: FITTING — CORRODED (35-1)
INSPECTION TYPE:SI WHILE WORKING TASK CARD NR 1249 FOUND THE NR 4 FLAP TRACK FITTING THAT ATTACHES TO FWD LANDING GEAR TRUNION BEARING TO BE CORRODED. REPLACED FITTING PER SRM 51-30-4.
Part: L-ANGLE — CORROSION (23-2)
INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) CORROSION ON FLOOR STRUCTURE L-ANGLE AND WEB AT STA 298 RBL 13, WL 208. REMOVED DAMAGED AND REPAIRED PER SRM.
Part: STRINGER — CORROSION (12-1)
INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STRINGER AT BS 360 TO BS 400 STR 27L. REMOVED CORRODED SECTION AND REPLACED PER SRM.
Part: SUPPORT — CORROSION (13-1)
INSPECTION TYPE:SI CORROSION (C53-111-01.00-02) ON SIDEWALL/BULKHEAD SUPPORT AT BS 680 LBL 31-45 WL 159-166. REMOVED SUPPORT AND REPLACED PER SRM.
Part: STIFFNER — CORRODED (31-1)
INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON SIDES OF E/E DOOR WARNING SWITCH COVER HOUSING. REPLACED STIFFENER BS 450-452 LBL 10 TO RBL 13 AND DOOR SWITCH HOUSING SAME BS LBL 2 TO RBL 6 PER 727 SRM 51-30-2, 51-20-1, 51-30-5, 51-20-151 AMD MM 52-40-11.
Part: AILERON — DELAMINATED (81-5)
INSPECTION TYPE:SI LT O/B AILERON T/E WEDGE IS DELAMINATED AND SATURATED WITH OIL ON THE O/B AFT END. REMOVED A 1 HALF INCH AREA OF DELAMINATED SKIN AT O/B AFT CORNER UPPER AND LOWER SURFACES AND REMOVED CONTAMINATED POTTING COMPOUND. FABRICATED REPAIR PLUGS AND INSTALLED WITH REPAIR PLUGS SANDED AND APPLIED FINISH COAT REBALANCE OF AILERON NOT REQUIRED.
Part: STRINGER — CORRODED (BS 445)
INSPECTION TYPE:SI, CORROSION ON STRINGER SPLICE AT BS 445, STR 20R. DAMAGE BEYOND LIMITS. REMOVED AND REPLACED STRINGER SPLICE PER BAC DWG 65-18215.
Part: CHANNEL — CORRODED (BS 236)
INSPECTION TYPE:SI, CORROSION (C53-221-01.01-01) ON FLOOR STRUCTURE AT BS 236 WL 208, LBL 32. REMOVED DAMAGE AND REPLACED PER SRM.
Part: SKIN — CORROSION (BS 295-312)
INSPECTION TYPE:SI CORROSION (C53-100-01.07-04) BULGING SKIN AND ONE SHEARED RIVET BELOW THE FORWARD LAV SERVICE PANEL BS 295 TO BS 312 STR 20R. REMOVED DAMAGE AND REPAIRED PER SRM 53-30-3.
Part: SEAT TRACK — CORRODED (BS 379)
INSPECTION TYPE:SI, CORROSION ON SEAT TRACK AT BS 379, LBL 1, WL 208. REMOVED CORROSION ON SEAT TRACK, FOUND TO BE OUT OF LIMITS PER SRM 51-10-6 AND SRM 53-10-1. REMOVED CORRODED SEAT TRACK FROM BS 360 TO 545, BL 0 AND INSTALLED NEW SEAT TRACK PER SRM 51-30-2.
Part: FRAME — CORRODED (E/E DOORWAY)
INSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) ON AFT E & E DOOR FRAME AFT SIDE AT BS 451. REMOVED FRAME AND REPLACED WITH NEW FRAME.
Part: SEAT TRACK — CORRODED (BS 740)
INSPECTION TYPE:SI, SEAT TRACK CORRODED AT BS 740, RBL 45, WL 208. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK FROM BS 660 TO 745, RBL 45, PER SRM 53-10-5 AND 51-30-2.
Part: FRAME — PUNCTURED (BS 680)
INSPECTION TYPE:SI, FWD CARGO BAY FRAME UPPER FLANGE PUNCTURED BS 680 LBL 23 WL 148.5. CUT OUT DAMAGED AREA 1 X 3 ON FRAME CROWN AT BS 680 LBL 23 WL 148.5, FABRICATED REPAIR DOUBLER, HEAT TREATED & INSTALLED ALL WORK ACCOMPLISHED IAW SRM 53-10-1, SRM 51-30-2, MM 51-20-21 AND MM 50-21-151 AND SRM 51-40-3.
Part: SKIN — CORRODED (WING)
INSPECTION TYPE:SI, CORROSION ON INNER SURFACE OF BOOST PUMP CAVITY 7302 AT THE 3 O'CLOCK POSITION. REPAIRED PER ER NR 99-6318.
Part: SKIN — CORRODED (WING)
INSPECTION TYPE:SI, CORROSION ON INNER SURFACE OF BOOST PUMP CAVITY 7302 AT THE 6 O'CLOCK POSITION. REPAIRED PER ER 99-6318.
Part: SEAT TRACK — CORRODED (BS 739)
INSPECTION TYPE:SI CORROSION ON LOWER SURFACE OF SEAT TRACK BS 739 LBL 63 WL 208 REPLACED SEAT TRACK SEGMENT FROM BS 660 TO BS 740 LBL 65 PER 727 SRM 53-10-5 AND 51-30-2 ***CPCP***
Part: CHORD — CRACKED (BS 870)
INSPECTION TYPE:SI WHILE WORKING NRC 010078 FUSE 157, 870 LOWER CHORD IS CRACKED LBL 10 WL 138 (870 BULKHEAD AIR COND BAY SIDE). CUT OUT DAMAGED SECTION OF CHORD AND REPAIRED PER SRM 51-40-4 BY SPLICING IN A NEW SECTION.
Part: SEAT TRACK — CORRODED (BS 882)
INSPECTION TYPE:SI, CORROSION ON SEAT TRACK AT BS 882, LBL 1, WL 208. CORROSION WAS FOUND TO BE OUT OF LIMITS AND REPLACED THE SEAT TRACK FROM BS 870 - BS 958, BL 0, WL 208, ON CUSTOMER ID 010795 PER SRM 51-30-2.
Part: SKIN — CORRODED (BS 344)
INSPECTION TYPE:SI CORROSION (C53-111-03.00-01) BULGE IN FUSELAGE SKIN BS 344, LBL 16, LWL 148 AND LEVELING COMPOUND SEPARATED FROM INTERIOR STRUCTURE HORIZ WALKWAY BEAM FROM BS 335-BS 351, LBL 16, WL 152. REMOVED DAMAGE AND REPAIRED PER SRM 53-30-3.
Part: TRACK — CORRODED (TE FLAPS)
INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 4 FLAP TRACK UPPER SURFACE AT MOUNT PADS. REPLACED FLAP TRACK PER 727 MM.
Part: FRAME — PUNCTURE (BS 680)
INSPECTION TYPE:SI, FWD BAY FRAME UPPER FLANGE PUNCTURED BS 680 RBL 23 (BELOW RT FLOOR TO SIDEWALL SUPPORT NUTPLATE). REMOVED DAMAGE AND REPAIRED PER SRM.
Part: SEAT TRACK — CORRODED (BS 362&369)
INSPECTION TYPE:SI CORROSION ON SEAT TRACK AT BS 362 AND 369 RBL 45, WL 208 OUT OF LIMITS. REPLACED SEAT TRACK FROM BS 340 TO 390 PER SRM 53-10-5.
Part: SEAT TRACK — CORRODED (BS 940)
INSPECTION TYPE:SI CORROSION ON SEAT TRACK AT BS 940 RBL 45 WL 208. REPLACED SEAT TRACK SEGMENT FROM BS 870 TO 960 RBL 45 PER 727 SRM 51-30-5, 51-10-2 AND 51-30-2.
Part: FRAME — DENTED (BS 1030)
INSPECTION TYPE:SI AFT BAY FRAME DENTED BS 1030 LBL 25 WL 150. REMOVED DAMAGE AND REPAIRED PER SRM 51-40-3.
Part: SUPPORT — CRACKED (WING)
INSPECTION TYPE:SI CRACKED, T/E UPPER PANEL SUPPORT L CHANNEL JUST ABOVE THE VERTICAL BULB, APPROX 1 FT FROM THE OB END OF THE I/B AILERON. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-20-1.
Part: SHEAR TIE — DAMAGED (BS 344)
INSPECTION TYPE:SI WHILE WORKING CARD NR 010022 FOUND SHEAR TIE WITH 2 EA EXISTING HOLES WITH EXCESSIVE DIAMETER AT BS 344 ABOVE RT NOSE CHORD WL 156. REMOVED DAMAGED SHEAR TIE AND REPLACED WITH FABRICATED SHEAR TIE.
Part: CARRIAGE — CORRODED (TE FLAPS)
INSPECTION TYPE:SI CORROSION ON NR 4 FLAP CARRIAGE SPINDLE FWD SHIM MATING SURFACE ORDERED AND RECEIVED NEW NR 4 FLAP CARRIAGE AND INSTALLED PER MM 27-51-03.
Part: FLOORBEAM — CORRODED (BS 680)
INSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) FLOORBEAM TOP CHORD BS 680 RBL 51, WL 208. REMOVED AND REPLACED TOP CHORD PER SRM 53-10-1, SRM 53-10-8, OHM 20-41-02, SRM 51-30-2.
Part: BEAM — CORROSION (24-2)
INSPECTION TYPE:SI CORROSION ON UPPER FLANGE OF LONGITUDINAL BEAM BS 825 AND BS 845 LBL WL 208. REMOVED CORRODED UPPER FLANGE ON LONGITUDINAL BEAM. FABRICATED NEW UPPER BEAM AND INSTALL NEW REPLACEMENT PART AND SPLICE PER SRM 51-30-2, 51-30-.
Part: SEAT TRACK — CORRODED (BS 780/825)
INSPECTION TYPE:SI, CORROSION ON SEAT TRACK AT BS 780 AND BS 825 TO BS 840, LBL 63 WL 208. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-1, SRM 51-30-5, SRM 51-20-151, SRM 51-40-3, SRM 51-30-2.
Part: FITTING — CORRODED (LT AILERON)
INSPECTION TYPE:SI, WHILE WORKING CARD 010635 (WINGS 277) FOUND LT WING O/B, AILERON O/B AND O/B CENTER HINGE SUPPORT FITTINGS CORRODED, AILERON SIDE. REMOVED AND REPLACED HINGE FITTINGS PER SRM 51-30-2.
Part: WEB — CRACKED (BS 758)
INSPECTION TYPE:SI UPPER WEB CRACKED ON INTERCOSTAL, BS 758, LBL 35, WL 208. REMOVED AND REPLACED UPPER WEB SKIN ON INTERCOSTAL PER SRM 53-10-1 SRM 51-10-2, SRM 51-30-2.
Part: TRACK — CORRODED (LT TE FLAP)
INSPECTION TYPE:SI L/W I/B AFT FLAP I/B TRACK ON MID-FLAP IS CORRODED. REMOVED CORRODED TRACK, INSTALLED NEW TRACK PER SRM 51-30-2.
Part: CLIP — CORRODED (BS 460)
INSPECTION TYPE:SI STRINGER CLIP CORRODED AT STR 28R, BS 460 REPLACED STRINGER CLIP PER SRM 51-30-2 ***CPCP***
Part: STRINGER — CORRODED (BS 450)
INSPECTION TYPE:SI, CORROSION ON RT STRINGER BS 450, STR 28R, E & E COMPL. REMOVED CORRODED SECTION OF STRINGER, INSTALLED NEW STRINGER AND SPLICE PER SRM 51-30-6, 51-30-5 AND 53-10-3.
Part: FRAME — CORRODED (E/E DOORWAY)
INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON FWD E/E DOOR FRAME LT AND RT SIDE OF FWD LATCH. REMOVED AND REPLACED FRAME PER SRM 51-30-2, SRM 51-10-1, SRM 51-10-3, SRM 51-10-02, MM 51-20-151, SRM 51-20-4 AND SRM 51-20-4 MM 51-20-00.
Part: TRACK — CORRODED (LT TE AFT FLAP)
INSPECTION TYPE:SI L/W I/B AFT FLAP, CENTER I/B TRACK ON MID FLAP IS CORRODED. CORRODED TRACK REMOVED AND NEW TRACK INSTALLED PER SRM 51-30-2.
Part: STRINGER — CORRODED (BS 450)
INSPECTION TYPE:SI, CORRODED STRINGER 28L BS 450, E & E COMPL. REMOVED CORRODED SECTION OF STRINGER AND INSTALLED NEW SECTION W STRINGER SPLICE PER SRM 53-10-3.
Part: STIFFNER — CORROSION (35-1)
INSPECTION TYPE:SI CORROSION AT TOP OF STA 870 STIFFENER AT LBL 25 WL 198. REMOVED CORRODED STIFFENER AT STA 870 FABRICATED NEW REPLACEMENT PART AND INSTALLED IAW SRM 51-30-2, 51-30-6.
Part: SEAT TRACK — CORRODED (BS 326/329)
INSPECTION TYPE:SI, CORROSION ON SEAT TRACK UNDER NUTPLATE AT BS 326 AND 329 RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 340 - 390 PER SRM 51-30-2.
Part: TRACK — CORRODED (TE FLAPS)
INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 3 FLAP TRACK LOWER SURFACE AROUND SPOILER BEAM MOUNT HOLES. REMOVED AND REPLACED NR 3 FLAP TRACK.
Part: BATTERY PACK — DISCHARGED (ROW 11 ABC)
EMERGENCY LIGHT AT SEAT 11 ABC OUT. REMOVED AND REPLACED BATTTERY PACK AT SEAT 11 ABC. OPS CHECK GOOD PER MM 33-50-00.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY EXIT SIGN ILLUMINATED AND REMAINED ON. NO CABIN EMERGENCY LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY PACK AT COCKPIT DOOR PER MM 33-50-00, OPS CHECK GOOD.
Part: LIGHT — INOP (COCKPIT)
INSPECTION TYPE:N/A, EMERGENCY LIGHT SYSTEM NOT OPERATING PROPERLY. PERFORMED EMERGENCY LIGHTING ADJ/TEST IAW MM 33-50-01. RESET EMERG LIGHT SWITCH CARGO POSITION, SYS OPS CHECKS NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, EMER LIGHT AT 17ABC INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)
INSPECTION TYPE:N/A, LEFT AFT EMER OVERWING EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, UPPER RIGHT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATT PACK, CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (VENTRAL STAIRS)
INSPECTION TYPE:N/A,VENTRAL STAIRS EMER LIGHT INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, CTR LEFT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, CTR RIGHT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OP CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, LOWER RIGHT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATT PACK, OPS CHECKS OK.
Part: BATTERY PACK — DISCHARGED (ROW 3)
INSPECTION TYPE:N/A, EMERG FLOOR LIGHT ROW 3 INOP. REMOVED AND REPLACED BATT PACK, OP CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, UPPER LEFT EXT EMERG LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, LOWER LEFT EXT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (PAX DOOR)
INSPECTION TYPE:N/A, EMERG LIGHTS INOP LWR MAIN DOOR. REMOVED AND REPLACED BATT PACK, CKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY LIGHT INOP ABOVE FLT ATTENDANT FWD SEAT. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD, P/N 96-2-1015.
Part: LIGHT — INOP (PAX DOOR)
EMERGENCY EXIT LIGHT INOP AT ENTRY DOOR. REMOVED AND REPLACED LIGHT ASSY.
Part: LIGHT — INOP (CREW ENTRY)
EMERGENCY EXIT LIGHT AT CREW ENTRY FAIL. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (FLIGHT DECK)
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP ON FLIGHT DECK. REMOVED AND REPLACED BATTERY PACK, LIGHT CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (FLIGHT DECK)
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT ON FLIGHT DECK INOP. REMOVED AND REPLACED BATT PACK, LIGHT CHECKS GOOD.
Part: BULB — FAILED (CABIN)
TWO AFT AIRSTAIR EMERGENCY LIGHTS INOP. RELAMPED, OPS CHECKS GOOD FROM SWITCH AT FLIGHT ATTENDANTS STATION.
Part: LIGHT — INOP (CABIN)
MAIN CABIN EMERGENCY EXIT LIGHT ABOVE REAR DOOR, AND MAIN CABIN OVERWING EMERGENCY LIGHT (LT SIDE AFT LOWER) INOP. REMOVED AND REPLACED BOTH LIGHTS. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (R1 DOOR)
INSPECTION TYPE-N/A, R-1 DOOR EMERGENCY EXIT LIGHT ON CEILING FWD POSTION INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, RT AFT CEILING EMERGENCY LIGHT AT GALLEY INOP. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, RT FLOOR LEVEL FWD EEL INOP. REMOVED AND REPLACED EEL BATTERY, OPS CHECK GOOD.
Part: BULB — FAILED (AFT AIRSTAIRS)
INSPECTION TYPE-N/A, AFT 3 AIRSTAIR EMER LIGHTS INOP. RELAMPED.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY LIGHTS INOP AT LT LAV LOWER LIGHT, AT SEAT 2 C AT BOTTOM OF SEAT, VENTRAL STAIRS AND ALL EXTERIOR LIGHTS OVERWING. REPLACED NECESSARY BATTERY PACKS FOR EMERGENCY LIGHTING TO ENSURE PROPER OPS PER MM 33-50-01. ALL EMERGENCY LIGHTS EXCEPT THE LEFT OVERWING ARE FUNCTIONAL LEFT WING EGRESS LIGHTS INOP, REFER TO NON ROUTINE.
Part: BATTERY PACK — DISCHARGED (ROW 14)
LEFT WING EGRESS LIGHTS (EXTERIOR) DO NOT OPERATE. BATTERY PACKS NEED REPLACED 3 TOTAL, P/N 96-2-1015, THEY ARE LOCATED ABOVE ROW 14 RIGHT SIDE OF A/C. REMOVED AND REPLACED LEFT OVERWING EXTERIOR EMERGENCY LIGHT BATTERIES IAW MM 33-50-01.
Part: BATTERY — DISCHARGED (ROW 2ABC)
EMERGENCY EXIT LIGHTS INOP AT SEAT 2ABC. REPLACED EMERGENCY EXIT LIGHT BATTERIES PER 33-50-101, OPS CKECK OK.
Part: BATTERY — DISCHARGED (CABIN)
EMERGENCY LIGHTS OUT AT CEILING AT ROW 11, LT AFT OVERWING EXIT LIGHT OUT. LOWER EXIT LIGHT OUT IN GALLEY AT SERVICE DOOR. REMOVED AND REPLACED BATTERIES IN ALL SAID LOCATIONS.
1998
Part: BATTERY PACK — DISCHARGED (MAIN ENTRY)
INSPECTION TYPE-N/A, FWD MAIN ENTRY EEL INOP. REMOVED AND REPLACED EEL ASSY, OPS CHECK GOOD (P/N 96-3-1030-1).
Part: OXYGEN MASK — FAILED TEST (CABIN)
EMERGENCY 02 MASKS DEPLOYMENT FAILED DROP TEST AT THE FOLLOWING STATIONS 5RT, 6LT, 9RT, 10LT, 11RT, 12LT, 16RT, 17RT, 18LT, 18RT, 19RT AND AFT LAV. ADJUSTED MASKS AND RECOILED, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
EEL RT SIDE AFT DOOR INOP. REPLACED BATT PACK P/N ON 96-2-1033. OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
EEL OVER GALLEY DOOR INOP. REPLACED BATT PACK, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT OUT AT GALLEY EXIT. REMOVED AND REPLACED BATTERY PACK AT GALLEY EXIT FOR EMERGENCY LIGHTS.
Part: FIRE LOOP — MALFUNCTIONED (WHEEL WELL)
FALSE WHEEL WELL FIRE WARNING WENT OUT ON GEAR EXTENTION. INSPECTED LOOPS AND DEFERRED FOR LOOP PER 26-8.
Part: CONNECTOR — CORRODED (NLG WW)
AT APPROXIMETLY 3500 FT MSL WHEEL WEEL FIRE LIGHT ILLUMINATED WITH HORN (BELL) HOT BRAKES SHOULD NOT BE A FACTOR BRAKE COOLING CHECKS WERE REFERENCED IN ROANOKE VA ALL APPROPRIATE CHECKLISTS ACCOMPLISHED. INSPECTED ALL LOOPS FOUND CONNECTORS AT NOSE FIRE LOOP CORRODED, CLE ANED SAME, OPS CHECKS GOOD
Part: OVERHEAT DET — MALFUNCTIONED (E/E COMPT)
PASSING 10,000 FT ON CLIMB-OUT, WHEEL WELL LIGHT FLASHED AND BELL RANG MOMENTARILY. PASSING 7,000 FT ON DESCENT, CAME ON AND STAYED ON UNTIL GEAR WAS EXTENDED. MEASURED BRAKE TEMPERATURE AT BLOCK-IN AND NO HOT BRAKE WAS NOTED. INSPECTED ALL WHEEL WELLS WITH NO DEFECTS NOTED. RAN ENGINES AND NO LEAKS WERE NOTED IN WHEEL WELL DUCTS. WILL REMOVED AND REPLACED FIRE AND OVERHEAT DETECTOR ACCESSORY UNIT, PRECAUTIONARY.
Part: AILERON — CORRODED (RT WING)
INSPECTION TYPE:C, R/W O/B AILERON I/B FITTING ON AILERON CORRODED AT ACTUATOR MOUNT ATTACHMENT. REMOVED AND REPLACED AILERON IAW MM 27-10-31.
Part: HINGE FITTING — CORRODED (RT AILERON)
INSPECTION TYPE:C, CORROSION ON RIGHT WING OUTBD AILERON CENTER OUTBD FIXED TRAILING EDGE HINGE FITTING. REMOVED AND REPLACED HINGE FITTING IAW SRM 51-30-2.
Part: FLAP — CORRODED (NR 5 LE FLAP)
INSPECTION TYPE:C, NR 5 K-FLAP NOSE FLAP TO K-FLAP BONDING JUMPER BOLTS HOLES ARE CORRODED. REMOVED AND REPLACED K-FLAP ASSEMBLY DUE TO NO FLAP NOSE ASSEMBLY AVAILABLE PER MM 27-81-01.
Part: FITTING — CORRODED (RT AILERON)
INSPECTION TYPE:C, CORROSION ON RIGHT WING OUTBD AILERON CENTER INBD FIXED TRAILING EDGE HINGE FITTING. REMOVED AND REPLACED HINGE FITTING IAW SRM 51-30-2.
Part: SPAR CHORD — CRACKED (WS 462-464)
INSPECTION TYPE:C, CRACK INDICATION NOTED ON RT WING UPPER REAR CHORD FROM WS 462 TO WS 464 (APPROX). CRACK INDICATION WAS CORROSION WS 457-470. REPAIRED PER SRM 57-10-6 FIG 3 AND DWG 65C19647 CAT II REPAIR.
Part: FLOORBEAM — CORRODED (BS 312)
INSPECTION TYPE:C WHILE WORKING INTERIOR 119 CUSTOMER NR 717462 DISCOVERED BS 312 FLOORBEAM TOP FLANGE CORRODED RBL 35-55 WL 208. CORROSION FOUND OUT OF LIMITS PER SRM 51-10-6 COMPLETED REMOVAL OF CORRODED SECTION AND INSTALLATION OF STANDARD T CHORD SPLICE PER SRM 53-10-8, 51-30-2, 51-10-2, AND MM 51-20-10
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERY PACK, CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EEL AT 6 ABC TO 9 ABC, 11 ABC, 13 ABC AND GALLEY INOP. REMOVED AND REPLACED BATT PACKS FOR ALL LOCATIONS AS ABOVE, OPS CHECK OK FOR SERVICE.
1997
Part: OVERHEAT LOOP — OUT OF POSITION (NR 1 STRUT)
INSPECTION TYPE-N/A, ENG NR 1 STRUT OVHT LIGHT ILLUMINATED. IN CRUISE AT FL 290 ENG PARS EPR 1.620 ENG TAT ON AND THRUST STABLE FOR APPX 15 MIN. CHKLIST WAS FOLLWED AND THRUST WAS REDUCED AND ENG 1 BLEED CB WAS PULLED. AFTER WAITING 3 MINS THE LIGHT STAYED ON SO THE NR 1 ENG WAS SHUTDOWN. THE LIGHT STAYED ON FOR ANOTHER 4 TO 5 MINS, THEN WENT OUT. RAN ENGS TO 1.7EPR FOR 20 MINS ON GROUND. OPENED ALL ACCESS PANELS, CHKED FOR AIR LEAKS AND FOR SENSING LOOP GNDING OUT, FOUND ALL OK. COULDN'T FIND ANY FAULTS. REPOSITIONED SEVERAL GROMMENTS AT SENSING LOOP. OPS CHK OK ON GROUND.
Part: OVERHEAT LIGHT — INTERMITTENT (NR 1 ENGINE)
INSPECTION TYPE-N/A, DURING FLIGHT ENG NR 1 STRUT OVERHEAT LIGHT INTERMITTENTLY BEGIN FLUCTUATING ON AND OFF. INSPECTED NR 1 ENG STRUT FOUND OVERHEAT DETECTOR LOOP INSULATION MISSING. REINSTALLED SAME AND TIGHTEND LOOSE CONNECTOR, RUN NR 1 ENG AND FOUND NO FAULT.
Part: OVERHEAT SENSOR — MALFUNCTIONED (NR 1 STRUT)
INSPECTION TYPE-N/A, NR 1 STRUT OVERHEAT IN CLIMB. ACCOMP ENG SHUTDOWN. *S/D* REMOVED AND REPLACED BOTH NR 1 PYLON SENSING ELEMENTS, RAN ENGINE, NO AIR LEAKS NOTED. NO OVERHEAT NOTED, OPS CK SYS IAW MM 26-14-00.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EMER LIGHT AT MAIN ENTRY DOOR INOP. REMOVED AND REPLACED EMER LIGHT BATTERY, OPS OK.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EMERGENCY LIGHT ASSY AT GALLEY SERVICE DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY, OPS OK.
Part: FIRE WIRE — CONTAMINATED (NR 1 ENGINE)
SYSTEM FAULT LIGHTS FOR NR 1 ENGINE FIRE DETECTION SYSTEM ILLUMINATED INTERMITTENTLY AFTER TAKEOFF. RAN CHECK LIST. FIRE TEST PRODUCED ABNORMAL INDICATIONS FOR ENGINE NR 1. SHUT DOWN ENGINE NR 1 AS A PRECAUTION. RETURNED TO RDU. CLEARED WATER FROM D4180J AT PYLON AND REINSULATED WIRES LAYING IN THE WATER IN BO OF D4180J. TEST NORMAL PER M/M 26-11-02.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, CENTER OVERHEAD AISLE EMER EXIT LIGHT AT ROW 12 ABC INOP. REMOVED AND REPLACED BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (LT GALLEY)
INSPECTION TYPE-N/A, LEFT SIDE GALLEY BULKHEAD EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, LEFT OVERWING AFT EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.
Part: LGHT — INOPERATIVE (CABIN)
INSPECTION TYPE-N/A, AFT LOWER EXIT LIGHT INOP AT ROW NR 13 LT SIDE. REPLACED BATTERY PACK AND OPS CKD NORMAL.
1996
Part: STRINGER — CRACKED (BS 87)
INSPECTION TYPE: C. VERT STAB STRINGER 11 CRACKED BETWEEN TORQUE BOX LOWER CHORD AND FIN STA 87. REPAIR VERT STAB STRINGER IAW SRM 55-30-4 FIG 1.
Part: ANGLE — CRACKED (BS 1342)
INSPECTION TYPE: C. B/S 1342 RT SKIN ATTACH ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 51-40-3.
Part: T CHORD — CORRODED (BS 1342)
INSPECTION TYPE: C. B/S 1342 LBL 15, RBL15 WL 280 UPPER T-CHORD CORRODED BEYOND LIMITS. REMOVED AND REPLACED T-CHORD IAW SRM 51-30-2 AND BAC DWG 65-17508.
Part: STRAP — OUT OF LIMITS (BS 1342)
INSPECTION TYPE: C. B/S 1342 LT OTBD UPPER T-CHORD STRAP OUT OF LIMITS. CUT OUT DAMAGED STRAP AT STA 1342. FABRICATED STRAP DOUBLER AND INSTALLED PER SRM 51-40-4 AND SRM 51-30-2.
Part: STRINGER — CORRODED (BS 1243-1342)
INSPECTION TYPE-C, STRINGER 12L CORRODED BS 1342 TO 1243. REMOVED, FABRICATED AND REPLACED STR 12 BS 1243 TO 1342 PER SRM 53-10-2 AND 51-30-2.
Part: SHEAR TIE — CORRODED (BS 1303)
INSPECTION TYPE: C. SHEAR TIE CORRODED AT B/S 1303 BETWEEN STR'S 12R AND 13R. REMOVED SHEAR TIE, FAB'D SHEAR TIE PER BAC DWG 65-17500 AND INSTALLED PER SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 1303)
INSPECTION TYPE: C. SHEAR TIE CORRODED B/S 1303 BETWEEN STR'S 13R - 14R. REMOVED SHEAR TIE AT B/S 1303, FAB'D SHEAR TIE PER BAC DWG 65-17500 AND INSTALLED PER SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 1283)
INSPECTION TYPE: C. SHEAR TIE CORRODED AT B/S 1283 BETWEEN STR'S 13R AND 14R. REMOVED SHEAR TIE AT B/S 1283, FAB'D SHEAR TIE PER DWG 65-17500 AND INSTALLED SHEAR TIE PER SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 1303)
INSPECTION TYPE: C. SHEAR TIE CORRODED AT BS 1303 BETWEEN STRINGERS 13L AND 14L. REMOVED SHEAR TIE AND FAB'D SHEAR TIE PER BAC DWG 65-17500 AND INSTALLED SHEAR TIE PER SRM 51-30-2.
Part: SHEAR TIE — CORRODED (BS 1283)
INSPECTION TYPE: C. SHEAR TIE CORRODED AT B/S 1283 BETWEEN STRINGER 13L AND 14L. SHEAR TIE, FABRICATED SHEAR TIE PER BAC DWG 65-17500 AND INSTALLED SHEAR TIE PER SRM 51-30-2.
Part: STRINGER — CORRODED (BS 1243-1342)
INSPECTION TYPE-C, STR 13L CORRODED BS 1243 TO 1342. REMOVED CORRODED STR FABRICATED AND INSTALLED STR 13L PER SRM 53-10-2, BS 1243 TO 1342.
Part: STRINGER — CORRODED (BS 1243-1342)
INSPECTION TYPE-C, STRINGR 12R CORRODED BS 1243 TO 1342. REMOVED, FABRICATED AND REPLACED STRINGER BS 1243 TO 1342 IAW SRM 53-10-2 AND 51-30-2.
Part: STRINGER — CORRODED (BS 1243-1342)
INSPECTION TYPE-C, STRINGER 13R CORRODED BS 1243 TO 1342. REMOVED, FABRICATED AND INSTALLED STR 13R BS 1243 TO 1342 PER SRM 53-10-2 AND 51-30-2.
Part: SHEAR TIE — CORRODED (BS 1303)
INSPECTION TYPE: C. SHEAR TIE CORRODED AT BS B/S 1303 BETWEEN STR 12L AND 13L. REMOVED SHEAR TIE, FAB'D SHEAR TIE PER BAC DWG 6517500 AND INSTALLED PER SRM 51-30-2.
Part: SKIN — CORRODED (BS 1330)
INSPECTION TYPE: C. FUSELAGE SKIN CORRODED B/S 1330 BETWEEN STRINGER 7R AND 10R. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIRED IAW SRM 53-30-3 FIG 12 AND SRM 51-30-2.
Part: CHORD — CORRODED (BS 1342)
INSPECTION TYPE-C, VERT FIN TORQUE BOX LT HORIZ CHORD FS 1342 FIN STA 0 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPLACED CHORD AT STA 1342 FIN STA 0 PER DHC SK 950-435.
Part: RIB — CRACKED (VERT STAB)
INSPECTION TYPE: C. B/S 1367, FIN STA 22.5 RT RIB IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED AN INSTALLED REPAIR PARTS IAW SRM 51-40-3 AND 51-30-2.
Part: FRAME — CORRODED (BS 1342)
INSPECTION TYPE: C. B/S 1342 RT LOWER FRAME CHORD SEVERELY CORRODED. REMOVED AND REPLACED FRAME CHORD IAW SRM 51-30-02.
Part: CHORD — CORRODED (BS 1342)
INSPECTION TYPE: C. B/S 1342 RT OTBD CHORD RBL 30 WL 250 SEVERELY CORRODED. REMOVED AND REPLACED CHORD PER SRM 51-30-2.
Part: CHANNEL — CORRODED (BS 1342)
INSPECTION TYPE: C. B/S 1342 CENTER CHANNEL SEVERELY CORRODED. REMOVED AND REPLACED CENTER CHANNEL IAW SRM 51-30-2.
Part: CHANNEL — CORRODED (BS 1342)
INSPECTION TYPE: C. B/S 1342 LT CHANNEL LBL 18 WL 247 SEVERELY CORRODED. REMOVED AND REPLACED LT CHANNEL IAW SRM 51-30-2.
Part: FRAME — CORRODED (BS 1342)
INSPECTION TYPE: C. B/S 1342 LT LOWER FRAME CHORD LBL 24 IS SEVERELY RUSTED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2.
Part: CHANNEL — CORRODED (BS 1342)
INSPECTION TYPE: C. B/S 1342 RT CHANNEL RBL 18 WL 247 SEVERELY CORRODED. REMOVED AND REPAIRED RT CHANNEL IAW SRM 51-30-2.
Part: SKIN — CORRODED (BS 1243-1342)
INSPECTION TYPE-C, FUSELAGE SKIN IS CORRODED STA 1243 TO 1342 STR 10L TO 14L. REMOVED, FABRICATED AND REPLACED SKIN PER SRM 53-30-2 AND 51-30-2.
Part: FRAME — CORRODED (BS 1342)
INSPECTION TYPE-C, BS 1342 RT FRAME CHORD RBL 20 IS SEVERELY RUSTED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2 AND EO B727-5530-4601.
Part: FRAME — CORRODED (BS 1342)
INSPECTION TYPE-C, BS 1342 LT FRAME CHORD, LBL 20 IS SEVERELY RUSTED. REMOVED AND REPLACED LT FRAME CHORD IAW SRM 51-30-2 AND EO B727-5530-4601.
Part: CHORD — CORRODED (BS1342)
INSPECTION TYPE: C. B/S 1342 LT OTBD CHORD LBL 30 WL 250 SEVERELY CORRODED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2.
Part: ENGINE — FAILED (NR 2 ENGINE)
NR 2 ENGINE FAILED INFLIGHT. REMOVED AND REPLACED NR 2 ENG PER T/C 1202 (P/N JT8D-7B) (S/N 68500). REMOVED MAIN ENGINE OIL STRAINER, FOUND LARGE AMOUNTS OF METAL.
1995
Part: BULKHEAD — CRACKED (BS 178)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACK ON BULKHEAD BS 178, RBL 1 WL 197. REAPIRED IAW SRM 53-10-9, 53-10-2.
Part: DOOR — CORRODED (AFT CARGO)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON MAIN CARGO DOOR AFT LIFT ACTUATOR LOWER CUTOUT. REPAIRED IAW EO B727-52-0153.
Part: SPAR — CORRODED (WS 198)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON UPPER CHORD OF LEFT WING REAR SPAR AT WS 198.0. REPAIRED IAW SRM 57-10-6, 51-30-2, M/M 28-11-0.
Part: RIB — CRACKED (HORIZ STAB)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACKED SUPPORT RIB ON RT HORIZ STAB T/E AT STA 99.79. REPLACED RIB IAW SRM 51-20-4, 51-20-5, 57-30-2, M/M 27-30-5.
Part: TAB — CORROSION (AILERON)
WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON L/W O/B AILERON TAB, I/B TAB CORRODED. INSTALLED TAB IAW SRM 51-10-1, M/M 27-10-4.
Part: SKIN — DELAMINATED (RT TE AFT FLAP)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND DELAMINATION ON R/W O/B AFT FLAP ON UPPER SKIN 14 INCHES FROM I/B SIDE. REPAIRED IAW SRM 51-40-06.
Part: SHEAR WEB — CORRODED (BS 1173)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON SHEAR WEB AND HAT CHANNEL AT BS 1173, LBL 23 TO 28 WL 208. REPLACED HAT CHANNEL AND WEB IAW SRM 57-10-2, 51-30-2, 51-30-8, 51-40-2, 53-10-1.
Part: SKIN — LIGHTNING STRIKE (BS 400)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND DAMAGE TO SKIN DUE TO LIGHTNING AT STA 400, STR 4 LT. REPAIRED IAW SRM 53-30-3, 51-10-2, 51-30-2, 51-20-4.
Part: SKIN — CRACKED (BS 1228)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACK ON EXTERNAL SKIN AT BS 1228, RBL 9 WL 148. REPAIRED IAW SRM 53-30-3.
Part: SKIN — DELAMINATED (LT TE FLAP)
WHILE IN FOR C-CHECK MAINTENANCE, FOUND DELAMINATION ON L/W I/B FLAP. REPAIRED IAW SRM 51-40-6, M/M 51-20-0.
Part: FIBERGLASS — DELAMINATED (LT TE MID FLAP)
MAINTENANCE FOUND LEFT WING I/B FLAP FIBERGLASS DELAMINATED FROM T/E OF MID FLAP. REPAIRED IAW B727-5750-6197B.
Part: CONNECTOR — LOOSE (NR 2 ENGINE)
PILOT REPORTED NR 2 ENGINE FIRE DETECTION (GRD FAULT LIGHT) FLICKERS ENROUTE, LIGHT REMAINED OUT ON LANDING. CLEANED AND RESECURED LOOP CONNECTOR. GROUND CHECKS GOOD.