N527UP

No registry detail on file · not in current registry

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.

44 reports on file, 2001-02-05 – 2003-01-16.

OTHER · 2003-01-16 Matched by certificate designator
ATA 1430

Part: BOLT — BROKEN (BULKHEAD) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE: C, CENTER TANK RIGHT FS 1241 AFT BULKHEAD FITTING ATT BOLT FOUND LEAKAGE AS MK. A 1.125 INCH DIAMETER BROKEN BOLT REPLACED AS PER MM 20-51-01 AND REFER CWS FOR WORK DETAIL.

Source: SDR UPS03440023
OTHER · 2003-01-07 Matched by certificate designator
ATA 5310

Part: CLIP — CRACKED (BS 2200 STG 25R) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C M/D - BS 2200 STRINGER S25R TIE CLIP FOUND CRACK. BS 2200 STRINGER 25R TIE CLIP REPLACED AS PER SRM 51-10-01 P.8.

Source: SDR UPS03440040
OTHER · 2003-01-06 Matched by certificate designator
ATA 5210

Part: BEAM — CRACKED (PAX DOOR) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE: C, NR 2L DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED AS PER SRM 52-10-02 FIG 10.

Source: SDR UPS03440014
OTHER · 2003-01-06 Matched by certificate designator
ATA 5210

Part: BEAM — CRACKED (NO.2R DR) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C NO.2R DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED & INSTALLED AS PER SRM 52-10-02 FIG.10.

Source: SDR UPS03440015
OTHER · 2003-01-06 Matched by certificate designator
ATA 5210

Part: BEAM — CRACKED (1R DOOR) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C NO.1R DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED AND INSTALLED AS PER SRM 52-10-02 FIG.10.

Source: SDR UPS03440016
OTHER · 2003-01-05 Matched by certificate designator
ATA 5730

Part: PANEL — CORRODED (LH WLG BAY) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C LH WLG BAY AREA MOST I/B SKIN PNL (TRIANGLE SHAPE) EDGE SHOCK STRUT DOOR CUTOUT EDGE SEAL RETAINER EDGE CORROSION FOUND AT 3 LOCATIONS. SEAL RETAINER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG.2.

Source: SDR UPS03440012
OTHER · 2003-01-04 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE: C M/D - AFTER FLOOR PANEL REMOVED, FLOOR SUPPORT FOUND CORROSION AT BS 2280-2300 LBL 60. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8. DEPTH 0.035 INCH, WIDTH 1 INCH, LENGTH 3 INCHES.

Source: SDR UPS03440010
OTHER · 2003-01-03 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C, RIGHT BS 1480 BULKHEAD NR 11 HOLE FOUND CRACK AT BULKHEAD FRAME RUNNING FWD AND AFT APPROX .0625 INCH AND THROUGH THICKNESS RESPECTIVELY. CRACKED FASTENER HOLE REWORKED AS PER RS NR R534334957 DUE TO DIMENSION OF HOLE EXCEEDED S/B REPAIR LIMIT.

Source: SDR UPS03440045
OTHER · 2003-01-03 Matched by certificate designator
ATA 5310

Part: FITTING — CRACKED (LH BS 1480 B/H) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C LH BS 1480 B/H NO.24 HOLE CRACK AT OUTER CHORD SPLICE FITTING RUNNING O/B APPROX 5/32". REFER ATTACH SKETCH FOR DETAILS. DEFECTIVE HOLE REWORKED AS PER RS-53-43-34957 ISSUE 'B' AND EO B747-5310-18127-A

Source: SDR UPS03440060
OTHER · 2003-01-03 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (LH BS 1480 B/H) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C LH BS 1480 B/H NO.11 HOLE CRACK AT FX SKIN RUNNING FWD AD AFT AND THRU THICKNESS. REER ATTACH SKETCH FOR DETAILS. CRACKED FASTENER HOLE REWORK AS PER RS NO.R53-43-34957 DUE TO HOLE DIMENSION EXCEEDED SB REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTIONS).

Source: SDR UPS03440046
OTHER · 2003-01-03 Matched by certificate designator
ATA 5310

Part: SKIN — CRACKED (RH BS 1480) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C B/H BS 1480 BULKHEAD NO.11 HOLE CRACK AT FX SKIN RUNNING FWD AND AFT THROUGH THICKNESS. REFER ATTACH SKETCH FOR DETAILS. HOLE REWORKED AS PER RS-53-43-43957 DUE EXCEEDED SB 747-53A2390 REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTION).

Source: SDR UPS03440043
OTHER · 2003-01-03 Matched by certificate designator
ATA 5310

Part: FITTING — CRACKED (LH BS 1480 B/H) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:N/A LH BS 1480 B/H NO.7 HOLE CRACK AT EXTENSION FTG RUNNING AFT UPWARD DIRECTION APPROX 1/16" LONG. REFER ATT SKETCH FOR DETAILS. HOLE REWORKED AS PER RS-53-43-34957 DUE EXCEEDED SB 747-53A2390 REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTIONS).

Source: SDR UPS03440044
OTHER · 2003-01-03 Matched by certificate designator
ATA 5310

Part: FITTING — CRACKED (RH BS 1480 B/H) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C RH BS 1480 B/H NO.17 HOLE CRACK AT OUTER CHORD SPLICE FITTING RUNNING O/B AND I/B APPROX 3/16" AND 0.040" RESPECTIVELY. REFER G ATTACH SKETCH FOR DETAILS. DEFECTIVE HOLE REWORKED AS PER RS 53-43-34957 ISSUE B AND EO B747-5310-18127-A.

Source: SDR UPS03440059
OTHER · 2003-01-03 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (BS 1480 FX SKIN) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C RH BS 1480 FX SKIN AT EXTENSION FTG AREA HOLE #12 TWO CRACKS FOUND THROUGH FOR DETAIL, PLS REF ATTACHED SKETCH. HOLE REWORKED AS PER RS R-53-43-34957 DUE EXCEEDED SB B747-53A2390 LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTIONS).

Source: SDR UPS03440047
OTHER · 2003-01-03 Matched by certificate designator
ATA 5310

Part: FITTING — CRACKED (BS 1480 B/H) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C LH BS 1480 B/H NO.24 HOLE AT OUTER CHORD SPLICE FITTING RUNNING O/B APPROX 5/32" REFER ATTACH SKETCH FOR DETAILS. CRACKED FASTENER HOLE REAMED TO 0.530" AND BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-5310-10732-H WITHIH PLAN 'A' LIMIT CRACK F REE CONFIRMED BY NDT AS PER BTM PART 6 51-00-00 FIG.16 (REF EO B747-5310-1827-A)

Source: SDR UPS03440042
OTHER · 2003-01-02 Matched by certificate designator
ATA 5310

Part: BULKHEAD — CORRODED (LH WLG W/W) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C LH WLG W/W FWD BULKHEAD WEB UPPER AREA BS 1241 LBL 60-100 CORROSION REVEALED. CORROSION REMOVED AND C/OUT REPAIR AS PER RS R57-12-34959. DEPTH 0.038, WIDTH 1", LENGTH 2".

Source: SDR UPS03440070
OTHER · 2003-01-02 Matched by certificate designator
ATA 5310

Part: WEB — CORRODED (LH WLG W/W) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C L/H WLG W/W FWD BULKHEAD WEB UPPER AREA BS 1241 LBL 60-100 CORROSION REVEALED. CORROSION REMOVED IAW SRM51-10-01, CORROSION DEPTH 0.038", WIDTH 1", LENGTH 2".

Source: SDR UPS03440041
Earlier reports · 2001–2002 · 27 reports

2002

OTHER · 2002-12-31 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (LWR FUSE) · airframe 63,410 hrs · 17,788 cycles

INSPECTION TYPE:C FX LOWER FUSELAGE, EXTERNAL SKIN EDGE FOUND HEAVY CORROSION AT STA 983 LH SIDE STG 41L TO STG 42L(2 LOCATIONS). SKIN REPAIRED AS PER SRM 53-30-03 FIG.1. (DEPTH 0.063", WIDTH 2", LENGTH 4")

Source: SDR UPS03440011
NO TEST · 2002-11-16 Matched by certificate designator
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:PFLT 1 EMERGENCY LT INOP UPPER DECK JUST FWD OF JUMPSEATS ON CEILING. RELAMPED. OPS CK OK.

Source: SDR UPS02439916
FLT CONT AFFECTED · 2002-08-06 Matched by certificate designator
ATA 2750

Part: TERMINAL — LOOSE (T/E FLAP)

INSPECTION TYPE:N/A OUTBOARD FLAPS WOULD NOT EXTEND. SECURED TERMINALS 6 & 7 OF TB 258 AND TERMINAL 11 OF TB 259 IN J42, REPLACED S1404 GL 51752, S329, S339, PER MM 27-51-07. CYCLED FLAPS, NO MALFUNCTIONS FOUND.

Source: SDR UPS02439008
OTHER · 2002-06-18 Matched by certificate designator
ATA 3240

Part: BRAKE — MALFUNCTIONED (LANDING GEAR)

INSPECTION TYPE:N/A AUTOBRAKES DISENGAGED IMMEDIATELY AFTER TOUCHDOWN. PERFORMED AUTO BRAKES ADJUSTMENT TEST AS PER MM 34-43-00 NO DEFECTS NOTED.

Source: SDR UPS02438644
OTHER · 2002-06-10 Matched by certificate designator
ATA 3350

Part: LENS — CRACKED (CABIN)

INSPECTION TYPE:N/A LENS CRACKED ON DOME LIGHT AT UPPER DECK EMERGENCY EXIT. REMOVED AND REPLACED LIGHT ASSY.

Source: SDR UPS02438575
OTHER · 2002-06-01 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — SHEARED (COCKPIT)

INSPECTION TYPE:N/A CAPT SEAT TRACK STOP SHEARED OFF REF D238709 AND M238705 AND REQ A238705. CAPTS SEAT ELECTRICAL CHORD ISNTALLED AND ELECTRIC OPERATION NORMAL AT THIS TIME, THIS CLEARS M238705 R&R LT SEAT TRACK ASSY. (CAPT'S) (AFT OTBD) OPS NORMAL AT THIS TIME. THIS CLEARS D238709

Source: SDR UPS02438509
NO TEST · 2002-05-16 Matched by certificate designator
ATA 3350

Part: FUSE — NOT SEATED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT INOP ON UPPER DECK. RESEATED FUSES IN PS, OPS NORMAL.

Source: SDR UPS02438280
OTHER · 2002-05-11 Matched by certificate designator
ATA 3350

Part: FUSE — NOT SEATED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT AT FWD PART OF UPPER DECK IS INOP. RESEATED FUSES IN POWER SUPPLY. OPS NORMAL PER MM 33-51-00.

Source: SDR UPS02438229

2001

NO TEST · 2001-12-05 Matched by certificate designator
ATA 3350

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A TWO EMERGENCY LIGHTS INOP. (CAPTS/CENTER) RELAMPED LIGHTS IAW MM 33-10-00 CK OK.

Source: SDR UPS01437353
FLUID LOSS · 2001-09-25 Matched by certificate designator
ATA 7310

Part: FUEL LINE — CHAFED (NR 4 ENGINE)

INSPECTION TYPE:N/A NR 4 ENGINE HAS FUEL LEAK - TUBES TAGGED - CHAFED WITH ANOTHER TUBE. REMOVED TWO CHAFED LINES KLS 82050 INSTALLED SERVICEABLE FUEL SIGNAL TUBE ASSY AND INSTALLED SERVICEABLE DRAIN TUBE ASSY PER AMM 30-10-10 LEAK CHECK GOOD.

Source: SDR UPS01436854
NO TEST · 2001-06-08 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT INOP IN UPPER DECK MOST AFT LIGHT. RELAMPED, NO HELP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND CKS GOOD.

Source: SDR UPS01436030
OTHER · 2001-03-26 Matched by certificate designator
ATA 5512

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT HORIZONTAL STAB L/E. IS CRACKED AT L/E. STA. 360 REPAIRED SKIN I.A.W. SRM. 55-10-03 FIG. 1

Source: SDR UPS01435450
OTHER · 2001-02-12 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C HFEC INSP REVEALED TWO CRACKS AT 3RD INSULATION BLANKET STANDOFF HOLE FROM TOP AT STA 300 ON VERTICAL WEB OF NOSE WHEEL WELL INSIDE CABIN RT SIDE. REMOVED AND REPLACED WEB IAW DWG 65B07942 AND SRM 51-30-02.

Source: SDR UPS01435152
OTHER · 2001-02-12 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C2,3, HFEC INSP REVEALED TWO CRACKS EXTENDING FROM 3RD INSULATION BLANKET STANDOFF HOLE FROM TOP AT LT SIDE STA 320 ON VERTICAL WEB OF NOSE WHEEL WELL IN CABIN. REMOVED AND REPLACED WEB IAW DWG 65B07942, AND SRM 51-30-02.

Source: SDR UPS01435153
OTHER · 2001-02-12 Matched by certificate designator
ATA 5754

Part: STRUCTURE — CORRODED (RT WING LE FLAP) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, RIGHT WING I/B FOREFLAP IS CORRODED BEYOND LIMITS WBL 128.4675 TO WBL 445. REMOVED AND REPLACED RIGHT I/B FOREFLAP.

Source: SDR UPS01435351
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1112 BETWEEN LBL 25 TO LBL 40. REPAIRED SUPPORT IAW SRM 53-50-04.

Source: SDR UPS01435160
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT WING LOWER BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1170 BETWEEN BL 0 AND LBL 60. REPAIRED SUPPORT IAW SRM 53-50-04.

Source: SDR UPS01435159
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT AT STA 940 LBL 14 TO LBL 20 IS CORRODED BEYOND LIMITS. REPAIRED SUPPORT IAW SRM 53-50-04 FIG 1.

Source: SDR UPS01435163
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C2, 3, STA 1306 LOWER SUPPORT FRAME BETWEEN BODY DOORS IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT FRAME IAW DWG 65B14056, AND SRM 51-30-02.

Source: SDR UPS01435342
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1064 LBL 23 TO LBL 50. REPAIRED SUPPORT IAW SRM 53-50-04 FIG 2.

Source: SDR UPS01435161
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: CLIP — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT HANGER CLIPS ARE CORRODED BEYOND LIMITS AT STA 860 LBL 31 FWD AND AFT CLIP. REMOVED, FABRICATED, AND REPLACED CLIPS IAW DWG 65B01834, AND SRM 51-30-02.

Source: SDR UPS01435164
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1000 LBL 43. REPAIRED SUPPORT IAW SRM 53-50-04.

Source: SDR UPS01435162
OTHER · 2001-02-11 Matched by certificate designator
ATA 5711

Part: SPAR CAP — CORRODED (RT WING) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, RIGHT WING FRONT SPAR LOWER CAP LOWER LEG IS CORRODED BEYOND LIMITS, 15 INCHES I/B OF STA FSSO, WS 1322. REPAIRED LOWER SPAR CAP IAW SRM 57-30-03 FIG 4.

Source: SDR UPS01435350
OTHER · 2001-02-11 Matched by certificate designator
ATA 5320

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C STA 1329 LOWER FUSELAGE SUPPORT BETWEEN BODY GEAR DOORS IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT IAW DWG 65B14056, AND SRM 51-10-02.

Source: SDR UPS01435341
OTHER · 2001-02-08 Matched by certificate designator
ATA 5512

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, LEFT HORIZONTAL STAB L/E IS CRACKED AT STA 400 ON UPPER SKIN OF L/E. REPAIRED SKIN IAW SRM 55-10-03.

Source: SDR UPS01435026
OTHER · 2001-02-07 Matched by certificate designator
ATA 5754

Part: SKIN — CRACKED (RT WING) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, RIGHT WING NR 12 K-FLAP BULLNOSE INNER SKIN IS CRACKED AT INBOARD END. REPAIRED SKIN IAW SRM 57-50-03 FIG 8.

Source: SDR UPS01435027
OTHER · 2001-02-05 Matched by certificate designator
ATA 5280

Part: SKIN — CORRODED (RT STRUT DOOR) · airframe 59,290 hrs · 16,920 cycles

INSPECTION TYPE:C, RT BODY GEAR I/B STRUT DOOR INNER SKIN IS CORRODED BEYOND LIMITS. REPAIRED SKIN IAW SRM 51-40-2 FIG 1.

Source: SDR UPS01435157