N214UP
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.
91 reports on file, 1995-06-08 – 2001-12-20.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:PFLT CREW ENTRANCE EMERGENCY EXIT LIGHT DOES NOT TEST. REPLACED BATTERIES, OPS CHECKED GOOD.
Part: BULKHEAD — CORRODED (FUSELAGE)
INSPECTION TYPE:IN FWD SIDE OF BS 1342 NR 2 ENGINE BULKHEAD IS CORRODED AT APPROX LBL TO LBL 40 AS VIEWED LOOKING AFT STANDING ON AIRSTAIRS JUST O/B OF NR 2 ENGINE GENERATOR FEEDER CABLES NUMEROUS FASTENERS ARE CORRODED AS IS A STIFFENER. CLEANED AND TREATED AREA AND REMOVED CORROSION PER SRM.
Part: WINDOW — CRACKED (COCKPIT)
INSPECTION TYPE:PFLT CAPTAIN'S L1 WINDOW INNER PANE CRACKED AND ARCHING. REPLACED L1 WINDOW PER MM 56-11-11.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES.
Part: TERMINAL — DAMAGED (CARGO DOOR)
AMBER MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURES PER AOM CH 2. DIVERTED FLIGHT TO FWA. DEFERED PER MEL 52-4 AND COMPLIED WITH DMP VERIFYING THAT MAIN CARGO DOOR CLOSED AND LOCKED PRIOR TO DEPARTURE. ITEM DEFERRED M211761 PLACARD INSTLD T/S FOUND 1 EA BROKEN WIRE TERMINAL ON SWITCH S909 REPLACED WIRE TERMINAL AS REQUIRED. PRESSURIZED A/C AND OPS CHECKED CARGO DOOR SYSTEM IAW M/M 55-34-00. OPS CHECKED GOOD. CLEARED DEF LP 492291
Part: SKIN — CRACKED (LT FLAP) · airframe 29,085 hrs · 27,894 cycles
INSPECTION TYPE:C, LEFT WING I/B AFT FLAP LOWER SURFACE L/E CRACKED AT O/B CENTER ECCENTRIC ROLLER FITTING CUTOUT. REPAIRED PER SRM 57-50-4.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,085 hrs · 27,894 cycles
INSPECTION TYPE:C CORROSION (C53-100-01.00-04) UNDER STRINGER 29L BETWEEN BS 1166- BS 1183 AND T-CLIP AT 1183. REMOVED CORROSION ON STRINGER 29L IN AN AREA OF 1.0 X.5 X.020 INCH FROM ORIG THICKNESS OF .090 INCH OUT OF LIMITS PER SRM 53-10-1, SRM 53-10-2 SRM 51-10-7. REMOVED STRINGER, FABRICATED REPAIR PARTS. FOUND CORROSION ON SKIN. REMOVED CORROSION, FOUND ALL TO BE WITHIN LIMITS. REINSTALLED ALL NEW REPAIRS PARTS PER SRM 51-30-2.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 29,085 hrs · 27,894 cycles
INSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON FRAME SHEAR TIE, BS 600 BETWEEN STR 28R AND STR 28L. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-151.
Earlier reports · 1995–1999 · 83 reports
1999
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (COCKPIT)
INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.
Part: SKIN — CORRODED (BS 1005)
INSPECTION TYPE:C WHILE WORKING CARD 973519, FOUND CORROSION ON INNER SKIN AT BS 1005, RBL 7, WL 148. REMOVED CORRODED SECTION OF SKIN AT BS 1005, RBL 7, WL 148 AND REPAIRED IAW ER NR 99-5802 AND SRM 53-30-03 FIG 3A.
Part: KEEL BEAM — CORRODED (BS 982)
INSPECTION TYPE:C CORROSION (C53-113-01.06-02) BS 982 RT KEEL BEAM. REMOVED CORRODED KEEL BEAM SEGMENT AND REPLACED WITH NEW SEGMENT IAW ER 99-5790.
Part: STRINGER — CORRODED (BS 1153)
INSPECTION TYPE:C WHILE WORKING CUST CARD NR 973522 FOUND CORROSION ON STR 20R STA 1153. REMOVED CORRODED STRINGER BS 1153 AND REPLACED WITH NEW STRINGER IAW SRM 51-40-03, 51-10-1, 51-30-02, DRW NR 65-16349.
Part: CLIP — CORRODED (BS 990)
INSPECTION TYPE:C CORROSION ON SHEAR TIE T-CLIP AT BS 990, RBL 8, WL 148 BETWEEN STR 29-29 R (WHILE WORKING CARD 973519). REMOVED CORRODED T-CLIP AND REPLACED WITH NEW T-CLIP IAW 51-10-1 AND 51-30-02.
Part: SHEAR TIE — CORRODED (BS 970)
INSPECTION TYPE:C WHILE WORKING 973519, FOUND CORROSION ON SHEAR TIE AT BS 970 RBL 8, WL 148 BETWEEN STRINGER 28, 29R. REPAIRED SHEAR TIE AT BS 970 RBL 8 WL 148 PER SRM 53-10-1, 51-30-2, 53-10-4, 51-10-2.
Part: CREASE BEAM — CRACKED (BS 1166)
INSPECTION TYPE:C, LEFT I/B CREASE BEAM IS CUT AT BS 116, WL 209, LBL 64. FOUND CREASE BEAM TO BE CRACKED AT BS 1166, WL 209, LBL 64 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF CREASE BEAM FROM BS 1157 TO BS 1177, FABRICATED NEW CREASE BEAM, REPAIR ANGLE AND SPLICE AND FILLER AND INSTALLED REPAIR PARTS AND CREASE BEAM IAW SRM 51-40-3, SRM 51-30-2 SRM 51-30-8 FIG 8.
Part: SEAT TRACK — CORRODED (BS 950)
INSPECTION TYPE:C CORROSION ON SEAT TRACK UPPER SURFACE O/B SIDE BS 950, LBL 45. REMOVED AND REPLACED SEAT TRACK FROM BS 870 TO BS 960.
Part: SHEAR TIE — CORRODED (BS 990)
INSPECTION TYPE:C CORROSION ON FRAME SHEAR TIE BS 990, RBL 4, WL 148 BETWEEN STR 29-30R. REMOVED DAMAGE SHEAR TIE AND REPAIRED IAW SRM 53-10-04 FIG 15.
Part: SPLICE — CORRODED (BS 1000)
INSPECTION TYPE:C, WHILE WORKING CARD 973519, FOUND CORROSION AND GOUGE ON STRINGER SPLICE BS 1000, STR 29R, RBL 6, WL 148. REMOVED AND REPLACED STR SPLICE BS 1000 STR 29R, RBL 6, WL148, WITH NEW STR SPLICE.
Part: CREASE BEAM — CORRODED (BS 1166)
INSPECTION TYPE:C CORROSION ON CREASE BEAM I/B BS 1166, WL 209 RBL 64. CORROSION OUT OF LIMITS REPAIR WILL BE ACCOMPLISHED ON NRC 973389 DO TO OTHER DEFECTS REPAIR WILL COVER FROM 1138-1176.*
Part: CREASE BEAM — CORRODED (BS 1170)
INSPECTION TYPE:C CORROSION ON I/B CREASE BEAM BS 1170 WL 208 LBL 64. CORROSION OUT OF LIMITS REPAIRS WILL BE ACCOMPLISHED ON NRC 973397, WHICH ENCOMPASS THIS AREA. REPAIR GOES FROM BS 1159-1176.
Part: FRAME — CRACKED (BS 1183)
INSPECTION TYPE:C, CRACKS NOTED IN BS 1183, LBL 18 DOOR FRAME. ONE CRACK AT NR 7L DOOR STOP CUTOUT AND THE OTHER CRACK AT 2 FWD OF NR 7L DOOR STOP CUTOUT. ACCESSED AREA AT 1183 FRAME AND REPAIRED FRAME IAW SB B727-53-0210.
Part: WINDOW — SHATTERED (FLIGHT DECK)
INSPECTION TYPE:N/A, AIRCRAFT DIVERTED INTO TUL DUE TO L-2 WINDOW SHATTERED IN FLIGHT. *S/D* REMOVED AND REPLACED L-2 WINDOW WITH NEW PER MM 56-12-11 (P/N 5-71762-39) (S/N 1429) OFF. (P/N 5-71762-39) (S/N 84-H -3-5-116) ON. HEAT CONTROL (P/N 1231-2) (S/N 978) OFF. HEAT CONTROL (P/N 231-2) (S/N 4764) ON.
1998
Part: SKIN — CORRODED (BS 720)
INSPECTION TYPE:SI CORROSION (C53-224-01.00-02) ON INTERIOR OF SKIN AROUND PERIMETER OF SIDELIGHT BETWEEN BS 720B PLUS 5 AND 720C LBL 73 WL 218-228 BETWEEN STR 14L AND 16L. CORROSION OUT OF LIMITS IAW SRM 53-30-3. REPAIRED SKIN AROUND PERIF OF LT SIDELIGHT IAW BFG/TRAMCO EO 98-2051 UPS FILE NR 727-53-1995.
Part: RIB — CORRODED (VERT STAB)
INSPECTION TYPE-SI, FRETTING CORROSION ON VERTICAL STAB L/E FAIRING RIB, FWD LIP AT FIN STA 55.9. RECEIVED NEW TEE-EXTRUDED RIB AND INSTALLED WEB TO NEW RIB PER 727 SRM 51-30-2.
Part: REAR SPAR — CRACKED (WS 686.5)
INSPECTION TYPE-SI, L/W STRINGER 2ND FROM REAR SPAR ON UPPER SKIN AT WING STATION 686.5 IS CRACKED AT STRINGER 5 TO 10. REPAIRED L/W STRINGER 2ND FROM REAR SPAR (STR 10) AT STA 686.5 IAW UPS EO B727-5710-0314.
Part: BOTTLE PIN — CORRODED (RT WING)
INSPECTION TYPE-SI, R/W REAR BOTTLE PIN IS CORRODED. ALSO, FWD AND AFT BUSHINGS ARE MISSING SECTION OF MICARTA INNER SLEEVE CORROSION (C53-100-05.00-04). REMOVED AND REPLACED R/W AFT BOTTLE PIN ON NRC 657574 IAW MM 57-41-01, BUSHING REPLACED ON AOG (BOEING) AGREEMENT 6-1171-TA-883.
Part: SUPPORT — CORRODED (TE FLAP)
INSPECTION TYPE-SI, NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT AFT BOLT HOLES FLAP TRACK FWD ATTACH POINT BUSHING HAS MIGRATED. ALSO, FWD HARDWARE REQUIRES REPLACEMENT I/B AND O/B AT RADIUS BLOCKS. REPLACED NR 7 FLAP TRACK FITTING IAW SRM 51-10-1 WILL BE INSTALLED ON TC C57-581-04-4D.
Part: SUPPORT — CORRODED (TE FLAP)
INSPECTION TYPE-SI, NR 4 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT FLAP TRACK FWD ATTACH LUG I/B SIDE. REMOVED AND REPLACED NR 4 FLAP TRACK FWD FITTING IAW MM 32-11-51.
Part: SILL — CRACKED (BS 294-304)
INSPECTION TYPE-SI, MOPSILL CRACKED LBL 54 STA 294 TO 304 WL 208. REPLACED MOPSILL AT LBL 54 STA 294 TO 304 WL 208 IAW SRM 51-30-2.
Part: BEAM — CORRODED (BS 760-848)
INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON LONGITUDINAL BEAM ST 760 TO 848 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED LONGITUDINAL BEAM IAW SRM 51-10-1, 51-30-2.
Part: STRINGER — CRACKED (BS 720)
INSPECTION TYPE-SI, DISCOVERED END OF STR 15L TO BE CRACKED AT BS 720+5. AREA OF DAMAGE REMOVED AND STRINGER END REPAIRED PER SRM 53-10-3 AND SRM 51-30-2.
Part: SKIN — CORRODED (BS 1090)
INSPECTION TYPE-SI, WHILE CLOSING FLOOR ON CARD 656802 FOUND CORROSION ON SKIN AT BS 1090 AT STR 28R. REMOVED CORROSION IAW SRM 51-10-6 REWORK OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1090 STR 28R IAW SRM 53-30-3.
Part: CHORD — CORRODED (BS 1166)
INSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON NUT PLATE AND FLOORBEAM AT STA 1166, LBL 10, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPAIRED FLOORBEAM PER SRM 53-10-8.
Part: ANGLE — CORRODED (BS 380-410)
INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT MOP SILL AT BOTTOM OF RT ENTRY DOOR BS 380 TO 410 RBL 63 WL 208 TOP AND BOTTOM SURFACES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON LWR SUPPORT ANGLE IAW 51-10-06, 53-10-1. REMOVED AND REPLACED ANGLE IAW SRM 51-30-02.
Part: SEAT TRACK — CORRODED (BS 980)
INSPECTION TYPE-SI, CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK WELL AND TOOTH BETWEEN BS 980 TO 1010 LBL 25. CORROSION REWORK OUT OF LIMTS IAW SRM 53-10-1. MECHANICAL DAMAGE WITHIN LIMITS IAW SRM 53-10-1. SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-02, 53-10-05.
Part: FLOORBEAM — CORRODED (BS 950)
INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON TOP OF FLOORBEAM 950 RBL 25 TO 65. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPAIRED 950 FLOORBEAM RBL 25 TO 65 IAW TRAMCO/BFG EWO 98-2012 (UPS FILE 727-53-1983).
Part: FRAME — CRACKED (BS 783.95)
INSPECTION TYPE-SI, CRACK INDICATION NOTED AT FASTENER HOLE IN FRAME AT BS 783.95 APPROX WL 207 APPROX LBL 65. REPAIRED CRACK IN FRAME STA 783.95 LBL 65 WL 207 IAW UPS EO B727-5310-5474.
Part: SEAT TRACK — CORRODED (BS 720)
INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK FLANGE BETWEEN BS 720D TO 720F LBL 25. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 720D TO BS 720F LBL 25 IAW SRM 53-10-5.
Part: FLOORBEAM — CORRODED (BS 380)
INSPECTION TYPE-SI, CORROSION AT BS 380 RBL 45 TO 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AND BOTTOM SURFACE AT FASTENER HOLES (C53-224-01.05-01). CORROSION REMOVED IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8.
Part: SEAT TRACK — CORRODED (BS 720)
INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 720C TO BS 745 RBL 25, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED SEAT TRACK, FABRICATED, INSTALLED REPAIR SEAT TRACK IAW SRM 53-10-5.
Part: SEAT TRACK — CORRODED (BS 520/610)
INSPECTION TYPE-SI, CORROSION (2-224-01) GOUGES AND BARE METAL ON SEAT TRACK AT BS 520 BS 610, LBL 60, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-05, 51-30-08, MM 51-20-31, OHM 20-50-01.
Part: LINK — CORRODED (BS 740)
INSPECTION TYPE-SI, CORROSION (C53-224-01.00-02) ON EXPANSION LINK AT BS 740 TO 755 LBL 45. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED LINK PER SRM 51-20-1, 51-10-1, 51-30-2.
Part: LUG — CORRODED (NR 4 LE FLAP)
INSPECTION TYPE-SI, NR 4 K-FLAP HAS CORROSION ON O/B UPPER LUG WHERE BONDING JUMPER ATTACHES. REMOVED AND REPLACED NR 4 K-FLAP IAW OHM 57-51-21 AND MM 27-81-01.
Part: FLOORBEAM — CORRODED (BS 1070)
INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE UNDER NUT PLATES BS 1070, BL 0 TO LBL 10 WL 200. REMOVED DAMAGED SECTION AND REPAIRED LOWER FLANGE IAW SRM 53-10-8.
Part: FRAME — CORRODED (BS 720)
INSPECTION TYPE-SI, CORROSION ON FRAME BS 720D STR 10 TO 13 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.
Part: SEAT TRACK — DENTED (BS 448-570)
INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 484 TO BS 570 BL 0 WL 208. CORROSION ON SEAT TRACK WAS FOUND TO BE WITHIN LIMITS AFTER CLEAN UP. HOWEVER, DENTS WERE FOUND ON BS 490 AND BS 571 WHICH WERE OUT OF LIMITS. SEAT TRACK WAS REPLACED FROM BS 470 TO BS 600 IN ACCORDANCE WITH SRM 53-10-5, SRM 51-30-5, SRM 51-30-8, SRM 51-10-2.
Part: FLOORBEAM — CORRODED (BS 480)
INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT BS 480 LBL 45 RBL 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AS MARKED. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.
Part: FLOORBEAM — CORRODED (BS 950)
INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE AT NUT PLATE BS 950F, LBL 12, WL 200. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND TRIPLER ANGLE AND FILLER IAW SRM 53-10-8.
Part: FRAME — DENTED (BS 1130)
INSPECTION TYPE-SI, AFT CARGO BAY BS 1130 AT STR 26L FRAME IS DENTED. DENT FOUND OUT OF LIMITS PER SRM 51-30-1. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-3 AND SRM 51-30-2.
Part: FLOORBEAM — CORRODED (BS 620)
INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON TOP CHORD OF FLOORBEAM AT BS 620 RBL 10 WL 208. CORROSION ON CHORD FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS PER SRM 53-10-8.
Part: SILL — CORRODED (BS 950)
INSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON MOPSILL BETWEEN BS 950 TO 950A, LBL 65 AROUND NUT PLATE HOLES. MOPSILL BS 950 TO 950A FOUND TO BE OUT OF LIMITS SRM 51-40-4. REMOVED CORRODED AREA IAW SRM 53-10-1, FABRICATED AND INSTALLED REPAIR PARTS SRM 51-40-2.
Part: FITTING — CORRODED (NR 5 TE FLAP)
INSPECTION TYPE-SI, RIGHT WING NR 5 FLAP TRACK FWD ATTACH FITTING I/B SIDE CORRODED (CORROSION C57-581-07.00-04). CORROSION FOUND TO BE OUT OF LIMITS PER SRM 57-40-01. REPLACED WITH NEW FITTING IAW MM 32-11-51 AND OHM 20-50-03.
Part: BEAM BLOCK — CORRODED (NR 3 TE FLAP)
INSPECTION TYPE:SI NR 3 FLAP TRACK REAR SPAR ATTACH POINT HAS CORROSION, ALSO BOTH FAIL/SAFE ATTACH HOLES. FLAP TRACK BEAM BLOCK REMOVED, FOUND OUT OF LIMITS AND REPLACED WITH NEW ITEM PER SRM 57-30-5, 51-10-2 AND 51-30-2.
Part: BONDING JUMPER — CORRODED (NR 5 LE FLAP)
INSPECTION TYPE-SI, NR 5 K-FLAP O/B LOWER BONDING JUMPER HAS CORROSOION WHERE JUMPER ATTACHES. CORROSION FOUND OUT OF LIMITS PER SRM 57-50-01. CORROSION DAMAGE REMOVED AND STANDARD REPAIR COMPLETED PER SRM 57-50-3, SRM 51-20-2 AND SRM 51-30-00.
Part: FITTING — CORRODED (NR 8 TE FLAP)
INSPECTION TYPE:SI NR 8 FLAP TRACK FWD ATTACH FITTING IS CORRODED AROUND FLAP TRACK FWD ATTACH POINT BUSHING, AND BUSHING MIGRATED AND CORROSION IN FAIL/SAFE STRAP ATTACH POINT BOLT HOLES FWD ATTACH HARDWARE REQUIRES REPLACEMENT OUTBOARD AND INBOARD. REWORKED AND INSTALLED FLAP TRACK SUPPORT FITTING PER ENGINEERING REPAIR NO 98-2085 AND MM 25-51-31.
1997
Part: FLOORBEAM — CORRODED (BS 1130)
INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) AFT CARGO BAY ON FLOORBEAM, FWD LOWER UNDER NUT PLATES BS 1130, LBL 6 TO LBL 25, WL 200. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIR BY ADDITION OF REPAIR ANGLES PER BOEING TELEX TCO-PAN-98-07175RR AND ER 98-2032.
Part: BATTERIES — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE WHEN SELECTED ON. REPLACED 4 EA DEAD BATTERIES S106 EMERGENCY EXIT LIGHTS, OPS CK GOOD.
Part: SKIN — CRACKED (BS 1130)
F/S 1130 LBL 20 AFT BELLY SKIN CRACK 1.0 INCH LONG WITH BULGE. VERIFIED CRACK WITH EDDY CURRENT, FOUND TO BE FWD AND AFT BETWEEN TWO RIVETS. REMOVED CORROSION AS REQUIRED, CLEANED STRINGER FOR INSPECTION (3) REMAINING STEPS TO BE COMPLETED ON A WIP FORM ACCOMP REPAIR PER SRM 53-30-3.
Part: SKIN — CRACKED (NR 2 LE FLAP)
INSPECTION TYPE:W/E, 3 CRACKS FOUND ON NR 2 K-FLAP ANTI-ICE SKIN. COMPLIED WITH UPS EO 9650. D 137034.
1996
Part: BATTERIES — DISCHARGED (CABIN)
INSPECTION TYPE: FOUND BOTH EMERGENCY EXIT LIGHTS INOP. REPLACED NI-CAD BATTERIES. OPS CHECK GOOD.
Part: STIFFENER — CORRODED (RT WING FWD SPAR)
INSPECTION TYPE: C. CORROSION AT RWS 245.0 FRONT SPAR STIFFENER ON UPPER O/B END. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 57-10-01, REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM'S 51-30-5, 51-30-2, MM 28-11-00.
Part: FITTING — CORRODED (LT AILERON)
INSPECTION TYPE: C. L/W I/B AILERON TAB HINGE FITTINGS ARE CORRODED AILERON SIDE. REMOVED AND REPLACED L/W I/B AILERON TAB HINGE FITTINGS PER SRM 51-30-2.
Part: CHORD — CORRODED (BS 296)
INSPECTION TYPE: C. CORROSION ON NOSE LANDING GEAR WHEELWELL MID-CHORD AT BS 296 LBL 15 WL 169. CORROSION FOUND TO BE THROUGH 100 PERCENT OF TOTAL THICKNESS, REMOVED AND REPLACED LT MID-CHORD IAW SRM'S 51-10-1, 51-30-5, AND MM 51-30-00-51-20-13 AND 51-20-01.
Part: FRAME — CORRODED (BS 1166)
INSPECTION TYPE: C. CORROSION ON SHEAR TIE AND FRAME AT STA 1166 LBL 2 WL 150. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 51-40-3.
Part: FRAME — CRACKED (BS 321)
INSPECTION TYPE: C. LEFT HAND INBOARD DOGHOUSE FRAME CRACKED AT STA 321 WL 169 LBL 25. STOP DRILLED CRACK AND REPAIRED PER SRM 51-40-02.
Part: RIB — CORRODED (NR 9 SPOILER)
INSPECTION TYPE: C. NR 9 SPOILER OUTBOARD CLOSURE RIB IS CORRODED. FOUND DAMAGE TO BE BEYOND ECONOMICAL REPAIR. PART WAS REPLACED IAW- MM 27-620.
Part: FITTING — CORRODED (BS 622)
INSPECTION TYPE: C. CORROSION ON CARGO TIE-DOWN SUPPORT UNDER WEB STA 622 RBL 20-22 WL 155. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1, REPLACED TIE-DOWN FITTING AT STATION 622 RBL 21 IAW SRM 51-30-2.
Part: FITTING — CORRODED (BS 540)
INSPECTION TYPE: C. CORROSION ON CARGO TIE DOWN AT STATION 540 RBL 23 WL 156. REMOVED CORRODED CARGO TIE-DOWN FITTING AND INSTALLED NEW CARGO TIE-DOWN FITTING. ALL WORK DONE IAW SRM'S 53-10-1, 51-30-2.
Part: STIFFENER — CORRODED (BS 257.85)
INSPECTION TYPE: C. CORROSION ON RIGHT WING STATION 257.85. FRONT SPAR STIFFENER IS CORRODED ON I/B UPPER END. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-10-1, REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-30-2.
Part: FITTING — CORRODED (BS 588)
INSPECTION TYPE: C. CORROSION ON FITTING AT STA 558 RBL 23 WL 155. REMOVED CORRODED FITTING AND INSTALLED NEW FITTING. ALL WORK DONE IAW SRM'S 53-10-1, 51-10-6, AND SRM 51-30-2.
Part: FITTING — CORRODED (FWD CARGO PIT)
INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN AT STA 720C RBL 23 WL 156. REMOVED CARGO TIE DOWN AND REPLACED WITH NEW PART PER SRM 51-30-2, 51-10-1, 51-20-4, 51-30-5.
Part: FRAME — CORRODED (BS 1148)
INSPECTION TYPE-C, CORROSION ON FAIL-SAFE ANGLE ON FRAME AT BS 1148 RBL 1 AFT SIDE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUTOUT DAMAGE AREA AND REPAIRED PER SRM 51-40-3.
Part: FRAME — CORRODED (BS 681)
INSPECTION TYPE: C. CORROSION OF AFT SIDE LOWER FLOOR BEAM FLANGE AT STA 681 LBL 5 TO RBL 5 WL 149. REMOVED CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGE AND REPAIRED PER SRM'S 53-10-4, 51-30-2, 51-10-4.
Part: SKIN — DELAMINATION (LT TE AFT FLAP)
INSPECTION TYPE: C. AREA OF DELAMINATION ON LEFT WING I/B AFT FLAP UPPER SKIN 64 INCHES I/B OF OUTBOARD END OF FLAP AND 14 INCHES FORWARD OF TRAILING EDGE. REPAIRED LT WING I/B AFT FLAP UPPER SKIN. ALL WORK DONE IAW SRM 51-40-6.
Part: STIFFENER — CORRODED (WS 257.85)
INSPECTION TYPE: C. CORROSION, RIGHT WING STATION 257.85. FRONT SPAR STIFFENER IS CORRODED ON I/B UPPER END. REMOVED CORRODED STIFFENER AND INSTALLED NEW STIFFENER. ALL WORK DONE IAW SRM 51-30-2, SRM 57-10-1, AND MM 28-11-00.
Part: FITTING — CORRODED (BS 720)
INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN STA 720C LBL 23 WL 156. REPLACED CARGO TIE DOWN WITH NEW PART PER SRM 51-30-2, 51-20-4.
Part: FITTING — CORRODED (BS 720)
INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN AT STA 720B RBL 23 WL 156. REPLACED CARGO TIE DOWN WITH NEW PART PER SRM 51-10-1, 51-20-4, 51-30-2, 51-30-5.
Part: FRAME — CRACKED (BS 1273/1263)
INSPECTION TYPE: C. CRACKED FRAME AT BS 1273 RBL 21 WL 194. REPAIRED IN ACCORDANCE WITH B727-5310-1239-E. NOTE: ADDITIONAL CRACKED FRAME AT BS 1263 RBL 21 WL 194 WAS ALSO REPAIRED ON THIS NRC.
Part: FITTING — CORRODED (BS 560)
INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN STA 560 LBL 23 WL 156. CORROSION REWORK REVEALED TIE DOWN TO BE CRACKED. REPLACED TIE DOWN AT STA 560 LBL 23 IAW SRM 51-30-2.
Part: RIB — CRACKED (NR 5 LE FLAP)
INSPECTION TYPE-C, NR 5 SLAT I/B RIB AT ACTUATOR MOUNT CRACKED AT SMALL TAB FLANGE. REPAIRED NR 5 SLAT I/B RIB AT ACTUATOR MOUNT IAW SRM 57-50-3.
Part: FITTING — CORRODED (BS 500)
INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN AT STA 500 RBL 23 WL 156. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED TIE DOWN AT STA 500 RBL 23 IAW SRM 51-30-2, 51-30-5.
Part: SHEAR WEB — CORRODED (BS 1175)
INSPECTION TYPE-C, CORROSION FOUND ON SHEAR WEB AT BS 1175 LBL 32 WL 208. CORROSION REMOVAL FOUND WEB TO BE CRACKED, REPAIRED IAW SRM 51-40-2.
Part: FRAME — CORRODED (BS 1030)
INSPECTION TYPE-C, CORROSION AT BS 1030 ON THE AFT SIDE OF FRAME AND UNDER THE LEVELING COMPOUND RBL 5, WL 145. REMOVED LEVELING COMPOUND AND FOUND CORROSION UNDER SHEAR TIE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED ANTENNA AND CUTOUT DAMAGE, FABED DOUBLER AND REPAIR PARTS. REINSTALLED ALL PARTS WITH FASTENERS, INSTALLED ANTENNA, SEALED, IAW SRM 51-30-2, 53-30-3, 53-30-1.
1995
Part: BATTERY — DISCHARGED (FLIGHT DECK)
WHILE ON THE GROUND, MAINTENANCE FOUND FLIGHT DECK DOOR AND MAIN ENTRY DOOR EMERGENCY EXIT LIGHTS INOP DURING DAILY CHECK. MAINTENANCE REMOVED AND REPLACED THE FLIGHT DECK DOOR AND MAIN ENTRY DOOR EMERGENCY EXIT LIGHT BATTERIES PER MM 30-50-101. OPS CHECKED GOOD PER MM 33-50-01.
Part: BULLNOSE — CORRODED (NR 2 LE FLAP)
WHILE IN C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP BULLNOSE AROUND LOWER ATTACH POINT HAS CORROSION. REPLACED K-FLAP IAW SRM 57-50-1, 51-30-2, OHM 57-51-11, 20-20-00, M/M 27-81-00.
Part: SKIN — DAMAGED (BS 1097)
WHILE IN C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN GOUGED 1.5 WIDE AND .065 DEEP AT BS 1097, RBL 70, WL 200. INSTALLED FABRICATED PARTS IAW SRM 51-20-1, 53-30-3, M/M 51-20-151.
Part: BULLNOSE — CORRODED (NR 3 LE FLAP)
WHILE IN C-CHECK, MAINTENANCE FOUND NR 3 K-FLAP BULLNOSE I/B LOWER ADJUSTMENT ROD ATTACH POIINT CORRODED. REPLACED K-FLAP IAW SRM 57-50-1, 51-30-2, OHM 57-51-11.
Part: SHEAR TIE — CRACKED (FS 1268)
WHILE IN C-CHECK, MAINTENANCE FOUND TWO CRACKS IN SHEAR TIE AT BS 1268, BETWEEN STR 11 AND 12, 13 AND 14. INSTALLED FABRICATED PARTS IAW SRM 53-10-04.
Part: RIB — CRACKED (RT ELEVATOR)
WHILE IN C-CHECK, MAINTENANCE FOUND RT NR 4 BALANCE BAY I/B RIB CRACKED. REPLACED RIB IAW SRM 51-30-2, 51-30-5.
Part: SKIN — CRACKED (RT WING LE)
WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED SKIN ON RT L/E PANEL NR 9203 AT SECOND TO LAST RIB UPPER SIDE. INSTALLED FABRICATED PARTS IAW SRM 55-10-03.