N122UP
Registered owner: UNITED PARCEL SERVICE CO, KY (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
SMALL EMERGENCY EXIT LIGHT IN LAV INOP IN THE ALWAYS ON LOW POSITION. SMALL RECTANGLE LIGHT. RELAMPED LAV AUX/MIRROR LIGHT PER 33-51-21. OPS CHECK GOOD
WHEN I OPENED THE MAIN ENTRY DOOR THE PRESS WARNING LT UNIT FELL OUT. REMOVED AND REPLACED ESCAPE SLIDE LIGHT AND RECESSED PANEL ASSY. IAW AMM 57-73-11 AND 52-10-13 OPS CHECK GOOD
*** MAJOR REPAIR *** TO LINK AND ACCOMPLISH EO-97088-REQ1 (N122UP: FUSELAGE SKIN LEFT AND RIGHT SIDE EXTERNAL DOUBLER REPAIRS AT FR7 AND FR8) REVIEWED
IN ORDER TO COMPLETE STEP 142 OF EA 300-5311-27-A4409, PRELIMINARY 5. ACCOMPLISHED PER STEP 142 OF EA 300-5311-27-A4409 PRELIMINARY 5. ACCOMPLISHED PER STEP 142 OF E.A.#: 300-5311-27-A4409 PRELIMINARY 5 AS A REQUIREMENT OF THE T3F18E008CUAT REPAIR.
DURING OK TO INSTALL PANEL 623BB, FOUND CRACK AT THE FWD UPPER RADIUS OF PANEL CUTOUT, DOT 55-006. INSTALLED REFORCING PLATE IAW SRM 57-41-12-227.
FWD CARGO- PANEL 132LC HAS CORROSION AROUND 16EA HOLES. SH91148554. REMOVED CEILING STRUCTURE AT CROSS BEAM 54 STA Y-450 BTW Y+450 IAW SRM 51-40-21-001. INSTALLED NEW CEILING SUPPORT AT FRAME 54 IAW SRM 51-40-21-001.
THE R/H SIDE MIDDLE FASTENER HOLE INSIDE FR40 LWR JUNCTION, HAS ABRASION DAMAGE TO ALL LAYERS. INSTALLED PANELS (4 E/A) AT RH WING FRAME 40 LWR JUNTION IAW A300-600 SRM 51-40-21
THE RT SIDE TOP FASTENER HOLE INSIDE FR40 LWR JUNCTION, HAS PITTING CORROSION TO ALL LAYERS. INSTALLED PANELS (4 E/A) AT RH WING FRAME 40 LWR JUNTION IAW A300-600 SRM 51-40-21. THIS TASK CARD WAS WORKED IN CONJUNCTION WITH TASK CARD T3F18E008KY8Y. PRELIMINARY #1 STEPS 5-8 AND PRELIMINARY #4 STEP 21 WERE DOCUMENTED ON TASK CARD T3F18E008KY8Y.
ENG #1, I/B T/R UPPER AFT BRACKET HAS A CRACK. INSTALLED NEW BRAKET IN ENG #1, I/B T/R UPPER AFT PER SRM 51-40-21-001.
MDC SEAT TRACK ON -Y1221.2 AT FR 80 RH SIDE, CORRODED DOT 31-039. REMOVED CORROSION BY TOOL FROM SEAT TRACK -Y1221.2 AT FR 80 RH SIDE AND AFTER MESUARED FOUND WITHIN LIMITS. IAW A300-600 SRM 53-10-16. RESTORED SURFACE PROTECTION AT MDC SEAT TRACK ON -Y1221.2 AT FR 80 RH SIDE. IAW A300-600 SRM 51-21-10 AND SRM 51-75-10. REVIEWED
MDC Z PROFILE BROKEN AT FR80 RH SIDE DOT 31-044 INSTALLED NEW Z PROFILE (PROFILE-T) I.A.W. SRM 51-40-21
EMPENNAGE TAIL SECTION, INSIDE OF ACCESS DOOR 312AR R/SIDE LOWER AREA BTWN FR 85/86 INTERCOSTAL UPPER CHORD IS CRACKED AND BENTED. DOT 34-002 INSTALLED NEW INTERCOSTAL UPPER CHORD I.A.W A300-600 SRM 51-40-21
MDC Z PROFILE BROKEN AT FR80 LH SIDE. INSTALLED NEW PROFILE AT FR80 LH SIDE IAW SRM 51-40-21-001.
MDC Z PROFILE AT FR74 LH SIDE HAS A CRACK. VERIFIED INSTALLATION OF Z-PROFILE AT MDC LH FR 74-75 IAW SRM 51-40-21-001.
ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER MIDDLE BRACKET DAMAGED. DOT 90-25. INSTALLED MIDDLE BRACKET IN ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER. IAW P&W SRM 54-30-00, PAGE 98.138, ITEM 52 AND SRM 51-40-21.
NR 1 ENG AFT FAIRING LOWER SURFACE HAS A CRACK AND ELONGATED HOLE. INSTALLED NEW FAIRING LOWER, IAW SRM 51-40-21-001.
NR 1 ENG, INBD THRUST REVERSER, INTERNAL STRUCTURE UPPER MIDDLE BRACKET DAMAGED.
NR 1 PYLON, OTBD SIDE RIB 3, BRACKET HAS A CRACK. NEW FISHPLATE (BRACKET) AT PYLON #1, O/B SIDE RIB 3, INSTALLED IAW A300-600 SRM 51-40-21, JOB COMPLETED. REVIEWED
RIGHT WING, KRUEGER BOX AREA, AFT STR, BTW RIB 1 AND 2, STRUCTURE WITH 4 GOUGE AND 4 RIVETS HEADS DAMAGE. INSTALLED NEW STRAP AT R/H WING, KRUEGER BOX AREA, AFT STR, BTW RIB 1 AND 2 IAW A300-600 SRM 51-40-21.
RIGHT WING, KRUEGER BOX AREA, FWD STR AT RIB 1, ATTACH BRACKET WITH CRACK. DOT 73-004 INSTALLED NEW BRACKET AT R/H WING, KRUEGER BOX AREA, FWD STR AT RIB 1:I.A.W. A300-600 SRM 51-40-21:
FAULT - STR Z400 - ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER STRIP HAS GOUGES. DOT 90-24. REMOVED STRIP AT ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER IAW A300-600 SRM 51-40-21-001 WIL BE REPLACE (BROKEN PART). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97062-REQ1 AND VT-MAE EA 300-5430-27-A4413, REV. _.
NR 1 PYLON, INBD SIDE RIB 3, BRACKET HAS A CRACK. REMOVED 1EA BRACKET AT NR 1 PYLON, INBD SIDE RIB 3 IAW SRM 51-40-21. INSTALLED NEW FISHPLATE AT NR 1 PYLON, INBD SIDE RIB 3 IAW SRM 51-40-21.
*** MAJOR REPAIR *** FAULT: 1EA CRACKS FOUND AT R/H RIB 15 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. MARKED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96975-REQ1 AND VT-MAE EA 300-5753-27-A4410, REV. -.
LEFT WING I/B FLAP UPPER SURFACE I/B RUB STRIP HAS A CRACK AND ARROUN IT SKIN TOO, ALSO NEEDS A INPECTION UNDER IT TO RULE OUT DAMAGE TO THE RIB DOT 31-015 ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97032-REQ1 AND VT-MAE EA 300-5752-27-A4416, REV. _.
MAJOR RPAIR, 1EA CRACKS FOUND AT RT RIB 26 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. ACCOMPLISHED PERMANTENT REPAIR IN ACCORDANCE WITH EO-96969-REQ1 AND VT-MAE EA 300-5753-27-A4408, REV. -.
TWO CRACKS FOUND AT LT RIB 26 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. PERFORMED CUTOUT OF CRACKED FLANGE ON RIB 26 STR 2.2 - 2.3 IAW SRM 57-50-00. INSTALLED REPAIR DOUBLER AT RIB 26 TO RIB 27 STR 2.1 TO STR 2.3 IAW SRM 51-40-21.
MAJOR REPAIR, DURING JACKING OF AIRCRAFT, AIRCRAFT FELL OFF ALL THREE JACKS. ACCOMPLISH THE CATEGORY C MAJOR REPAIR PER EO-96552-REQ1.
UNCOMMANDED FUEL MIGRATION RIGHT OUTER TANK
UNCOMMANDED FUEL MIGRATION RIGHT OUTER TANK REMOVED AND REPLACED RT INBD FILL VALVE . REF AMM 28-25-12 LEAK CK AND OPS CK GOOD. NO MIGRATION OF NOTED. OK FOR SERVICE.
*** ATB *** FAULT: PILOT REPORT AP 1 WOULD NOT COUPLE IN FLIGHT PERFORMED OPS CHECK OF YAW DAMPER ACTUATOR. OPS CHECK GOOD IAW AMM 22-26-00/501. PERFORMED AFS TEST. AFS TEST GOOD. IAW AMM 22-40-00/501 AC STILL CAT DOWNGRADED
FAULT: PILOT REPORT EMERGENCY CANCEL BUTTON SAFETY WIRE BROKEN. SAFETY WIRE INSTALLED ON EMERGENCY CANCEL BUTTON IAW AMM 20-11-11/001.
O/B L/H CLS ADAPTER AT FR37 IS BROKEN REMOVED SIDEWALL PANEL 131PW AND CEILING PANELS 131UC AND 131WC FOR ACCESS IAW A300-600 SRM 51-41-21
O/B L/H CLS ADAPTER AT FR37 IS BROKEN REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM 51-40-21. INSTALLED SIDEWALL PANEL 131PW AND CEILING PANELS 131UC AND 131WC IAW A300-600 SRM 51-40-21
FRAME 38.1 R/H SIDE HAS DOGBONE CRACKED O/B EDGE OF FLOOR PANEL. REMOVED AND REPLACED DOGBONE ON FRAME 38.1 RH SIDE O/B EDGE OF FLOOR PANEL IAW A300 SRM 51-40-21 REVIEWED
ALL FASTENER HOLES IN THE LWR SIDE OUTER WING SKIN, FOR FUEL TANK ACCESS PANEL 550MB (NEAR RIB 24), HAVE CORROSION INDICATIONS INSIDE THE HOLES AND SURROUNDING OUTER SURFACE. REMOVED LIGHT CORROSION BY HAND IN HOLE AND SURROUNDING OUTER SURFACE IN PANEL 550MB, IAW A300-600, SRM 51-74-10, CHECKED LIMIT AFTER REWORK, MATERIAL LOSS 0.003", FOUND TO BE NEGLIGIBLE DAMAGE IN IAW A300-600, 51-73-11. TR 09848.
13EA FASTENER HOLES IN THE LWR SIDE OUTER WING SKIN, FOR FUEL TANK ACCESS PNL 650LB (NEAR RIB 23), HAVE CORROSION INDICATIONS INSIDE THE HOLES AND 1EA OUT OF ROUND. ROTO PERFORMED ON FASTENER HOLES. NO DEFECTS FOUND IAW 51-10-01.
RH WING CENTER FLAP OTBD END DEFLECTOR PLATE BROKEN REMOVED AND REPLACED DEFLECTOR PLATE ANGLE P/N A5796040221500 BATCH # 0004185041 IAW SRM 57-53-11 FIG 2.
AFT CARGO COMP FR54 Y -1959 BRACKET CRACKED INSTALLED AFT. CARGO COMP BRACKET AT FR54 -Y 1959 P/N A5341076521900 BATCH #0004158669 AND MS20470AD5-6 IAW SRM 51-40-21.
*MAJOR REPAIR* FAULT-FLOOR PANEL 151NG CRACKED FABBED PNL 151NG FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
FOUND WATER INTRUSION ON THE UPPER SURFACE OF THE R/H ELEVATOR. AREA MARKED IN RED VERIFIED INSTALLED R/H ELEVATOR I.A.W A300 AMM 27-31-24/401 REVIEWED
*SDR FILED OPEN* FAULT: FOUND WATER INTRUSION ON THE UPPER SURFACE OF THE R/H ELEVATOR. AREA MARKED IN RED VERIFIED SAFETY LOCK WASHERS INSTALLED
FAULT AT FRAME 75-76 HAS A CRACKED ON WEB ON R/H SIDE INSTALLED NEW SHEER WEB AT FRAME 67 TO FRAME 77 R/H IAW SRM 51-40-21 (P/N HL18PB6-3).
FWD CARGO FLOOR PNL 131RG CRACKED DOT 146-165 FABBED PNL 131RG FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
FWD CARGO FLOOR PNL 131DE CRACKED DOT 146-160 VERIFIED FABBED PNL 131DE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
FWD CARGO FLOOR PNL 132MG CRACKED DOT 146-163 VERIFIED. FABBED PNL 132MG FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
FWD CARGO FLOOR PNL 131GE CRACKED DOT 146-162 FABBED PNL 131GE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
*OPEN* FWD CARGO FLOOR PNL 131RG CRACKED.
FWD CARGO FLOOR PANEL 132DE CRACKED DOT 146-161 FABBED PNL 132DE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
FWD CARGO FLOOR PNL 131FE CRACKED DOT 146-164 FABBED PNL 131FE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
AFT CARGO FLOOR PNL 151SF CRACKED DOT 146-181 FABBED PNL 151SF FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
*SDR FILED OPEN* FAULT-FWD CARGO FLOOR PNL 131GE CRACKED DOT 146-162 VERIFIED
AFT CARGO FLOOR PANEL 152VF CRACKED. FABBED PNL 152VF FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED
*** SDR FILED OPEN *** FAULT - VERTICAL STABILIZER L/E PANEL322 AL EXTERNAL MIDDLE CTR COMPOSITE DAMAGED . 89-168
DAMAGE ON HOLE E NEAR TOP OF THE HOLE ON LH FRAME 47 HORIZONTAL JUNCTIONAREA OF THE CWB LOWER ANGLE FITTING. ACCOMPLISH EO-89300-REQ1 AND EO 300-5710-27-A3498 REV. -. REVIEWED
VERTICAL STABILIZER L/E PANEL322 AL EXTERNAL MIDDLE CTR COMPOSITE DAMAGED . 89-168 PANEL WAS DOCUMENTED FOR REMOVAL ON TWO NRC'S. PANEL WILL BE REINSTALLED ON NRC T#F18E003S5ZL / 6100408536.
VERTICAL STABILIZER LE PANEL 322AL , 322BL ,ALLUMINIUM BONDED COVER AT LE HAS APPEAR TO HAVE DENTS AT SEVERAL PLACECS . 89-171 INSTALLED VERTICAL STAB LEADING EDGE PANELS 322AL, 322BL, IAW A300 AMM 53-32-11/401 VERIFIED.
*** SDR FILED OPEN *** FAULT: DAMAGE ON HOLE E NEAR TOP OF THE HOLE ON LH FRAME 47 HORIZONTAL JUNCTIONAREA OF THE CWB LOWER ANGLE FITTING.
*** SDR FILED OPEN *** FAULT - VERTICAL STABILIZER LE PANEL 322AL , 322BL ,ALLUMINIUM BONDED COVER AT LE HAS APPEAR TO HAVE DENTS AT SEVERAL PLACECS . 89-171
FAULT-ACCESS PANEL 672LB ANGLE CONDUCTOR CRACKED DOT 146-121 REMOVED AND REPLACED ANGLE CONDUCTOR. IAW A300-600 SRM 51-40-21.
-CARGO MAIN DECK, FLOOR PANEL 221EG HAS DELAMINATION 1. FABRICATED PANEL 221EG FROM 5024N40000155-G BATCH# 4055277 PER SREO-A300-5320-16407-E
ACCESS PANEL 672CB ANGLE CONDUCTOR CRACKED DOT 146-111 REMOVED AND REPLACED ANGLE CONDUCTOR IAW SRM 51-40-21
FAULT-ACCESS PANEL 672GB ANGLE CONDUCTOR CRACKED DOT 146-119 REMOVED AND REPLACED ANGLE CONDUCTOR IAW SRM 51-40-21
ACCESS PANEL 672AB ANGLE CONDUCTOR CRAKED DOT 146-120 REMOVED AND REPLACED ANGLE CONDUCTOR. IAW A300-600 SRM 51-40-21.
FAULT-ACCESS PANEL 672AB ANGLE CONDUCTOR CRAKED DOT 146-120 VERIFIED FABRICATED
SEAT TRACK AT FRAME 80 RBL -450 IS EXFOLIATED INSTALLED 1EA. SEAT TRACK REPAIR SECTION AND 2 EA. SPLICE ANGLES AT FRAME 78.10 TO 80 AT -Y450 IAW SRM 51-10-16 REPAIR 201 AND SRM 51-40-23 (P/N HL10VF8-5 AND HL10VF6-5) REVIEWED
R/H FRAME 40 LOWER JUNCTION HAS TWO FASTENER HOLES WITH DAMAGE. (TOP HOLE AND BOTTOM HOLES) ROTO PERFORMED ON RH FRAME 40 LOWER FASTENER HOLES. BOTTOM HOLE IS GOOD, TOP HOLE HAS DAMAGE. IAW 51-10-01. T96525 T91779. PER E0-61305-JIC0004-REV 1 TOP HOLE NOT TO BE INSPECTED UNTIL 2028 REVIEWED
CRACK FOUND IN FASTENER HOLE ON LEFT WING FRAME 40 LOWER RADIUS. ROTO PERFORMED ON LEFT WING FRAME 40 LOWER RADIUS FASTENER HOLE. DAMAGE STILL PRESENT IN HOLE, IAW 51-10-01. T96525 T91779. ROTO PERFORMED ON LH FRAME 40 LOWER RADIUS FASTENER HOLE. NO DEFECTS FOUND IAW 51-10-01. T96525 T91779.
*** SDR FILED OPEN *** FAULT: L/H FRAME 40 LOWER JUNCTION FASTENERS HAVE TWO HOLES WITH DAMAGE/CRACK INDICATIONS. MIDDLE HOLE (DAMAGE) BOTTOM HOLE (CRACK). STEP #7 VERIFIED
*** SDR FILED OPEN *** FAULT: CRACK FOUND IN FASTENER HOLE ON LEFT WING FRAME 40 LOWER RADIUS. VERIFIED
DAMAGE FOUND IN MIDDLE HOLE ON RIGHT WING FRAME 40 LOWER JUNCTION. ROTO PERFORMED ON RIGHT WING MIDDLE HOLE FASTENER FRAME 40 LOWER JUNCTION. DAMAGE STILL PRESENT IN HOLE, IAW 51-10-01. T96525 T91779. ROTO PERFORMED ON FRAME 40 LOWER JUNCTION RH MIDDLE HOLE. NO DEFECTS FOUND, IAW 51-10-01. T96525 T91779.
L/H FRAME 40 LOWER JUNCTION FASTENERS HAVE TWO HOLES WITH DAMAGE/CRACK INDICATIONS. MIDDLE HOLE (DAMAGE) BOTTOM HOLE (CRACK). ROTO PERFORMED ON LH FRAME 40 LOWER JUNCTION. MIDDLE HOLE IS FREE OF DEFECTS. BOTTOM HOLE STILL WITH DAMAGE, IAW 51-10-01. T96525 T91779. CLEANED HOLE IAW-SRM-51-40-44
44 DAMAGE HOLES ON PIANO HINGE FITTINGS. INSTALLED HINGES AT 3 LOCATIONS IAW SRM 51-40-21 AND IPC 52-36-12-14
CARGO MAIN DECK FLOOR, SKIN UNDER PANEL 231VG HAS CORROSION.DOT119-013 INSTALLED THRUST BRACKET IAW A300-600 SRM 51-40-21 CIC APPLIED IAW EO NO: M-5100-2780-L REVIEWED
TAIL APU RH ACCESS DOOR SKIN BENT AND CRACKED AFT END DOT 146-080APPLIED TREAT AND PRIME IN AREA CUT, DOUBLER AND FILLER. IAW A300-600 SRM 51-21-10. INSTALLED DOUBLER AND FILLER. IAW A300-600 SRM 52-41-11, FIGURE 202 AND SRM 51-40-21
CARGO MAIN DECK, FLOOR PANEL 231VG HAS PUNCTURE.DOT119-012 1. FABRICATED PANEL 231VG FROM 5024N4D000155-G BATCH# 4055277 PER SREO A300-5320-40552-B.
CARGO MAIN DECK FLOOR , SKIN UNDER FLOOR PANELS 231MJ-231LG-231RG-231WG-231BH HAS CORROSION BETWEEN FR16A AND FR31.DOT119-011. REMOVED CORROSION AT MCD UNDER FLOOR PANELS 231MJ, 231LG, 231RG, 231WG AND 231BH BETWEEN FR16A TO FR31. IAW A300-600 SRM 51-74-10. MAJOR REPAIR.
RH MAIN DECK SEAT TRACK ADAPTER WITH SURFACE CORROSION AT FR31 AND Y0 DOT 146-077 INSTALLED SEAT TRACK ADAPTER AT FR 31, Y O. P/N EN6114V4-15, BATCH # 0004191764. P/N HL70-8, BATCH # 0004212587. IAW SRM 51-40-21.
*SDR FILED OPEN* FAULT-CARGO MAIN DECK FLOOR, SKIN UNDER PANEL 231VG HAS CORROSION.DOT119-013 AUDIT COMPLETED
MIDDLE HOLE ON FRAME 40 LH UPPER TENSION BOLTS HAS DAMAGE AT THE BACK OF THE HOLE. CLEANED HOLE IAW-SRM-51-40-44. ROTO PERFORMED ON FRAME 40 L/H UPPER TENSION MIDDLE HOLE. NO DEFECTS FOUND IAW 51-10-01 T96525 T91779
RH MAIN DECK SEAT TRACK ADAPTER WITH SURFACE CORROSION AT FR38.1 AND Y0 DOT 146-074 ACCOMPLISH PERMANENT REPAIR PER UPS EO-89244-REQ1. REVIEWED
*** SDR FILED OPEN *** FAULT: MIDDLE HOLE ON FRAME 40 LH UPPER TENSION BOLTS HAS DAMAGE AT THE BACK OF THE HOLE. VERIFIED
*** SDR FILED OPEN *** FAULT: TOP HOLE ON FRAME 40 RH UPPER TENSION BOLT HAS DAMAGE AT THE BACK OF THE HOLE. VERIFIED
TOP HOLE ON FRAME 40 RH UPPER TENSION BOLT HAS DAMAGE AT THE BACK OF THE HOLE. ROTO PERFORMED ON FRAME 40 RH UPPER TOP HOLE WITH DAMAGE. NO DEFECTS FOUND IAW 51-10-01. T96525 T91779. WOR COMPLETED ON EO MXP-571039-01-1-138-JIC
*** SUPPLEMENTAL SDR *** AFT CARGO DOOR CUTOUT PLATE CRACKED (AFT ZONE ) DOT 041 INSTALLED NEW CUTOUT PLATE P/N: F5347537320600 AND NEW SUPPORT ASSY P/N: F5397134701000 AT AFT. CARGO DOOR (AFT. ZONE) I.A.W. A300-600 S.R.M. 51-40-21.
R/H FWD CARGO FLOOR RBL 0 STA.2029/FR31 - STA.2082/FR32 HAS CORROSION. DOT 33-003 CLEANED AREA FWD CARGO DOOR FLOOR BOTTOM RBL-0, FR31- FR32. AFTER EVALUATION IN THE AREA NOT DAMAGE FOUND IAW SRM 51-78-00.
FUS STRUCTURE FR86 TO FR87 LH WEB ( INTERCOSTAL) BENT DOT 146-052 REPAIRED INTERNAL STRUCTURE FR 86 TO FR 87 INTERCOSTAL BENT IAW E.O.: M-5100-41097-C. APPLIED C.I.C. AT FUS. LH INTERNAL STRUCTURE FR86 TO FR87 INTERCOSTAL I.A.W. E.O. M-5100-278-L.
*SDR FILED OPEN* FAULT-FUS STRUCTURE FR86 TO FR87 LH WEB ( INTERCOSTAL) BENT DOT 146-052 APPROVED
THE R/H CENTER FLAP HAS 1 EA CRACK AT RIB 27 AFT SIDE ON STR 2.1. ACCOMPLISH PERMANENT REPAIR PER EA 300-5750-27-A3483 REV. - AND EO-89185-REQ1.
LT WING #1 SLAT INBD SLAT DRIVE RETRACTABLE DOOR IS CRACK. PERFORMED SURFACE HFEC INSP OF THE L/H WING #1 SLAT INBD DRIVE RETRACTABLE DOOR IAW A300 NTM PART 6 51-10-08. THE SURFACE AREA OF THE DOOR IS CRACK / DEFECT FREE AT THIS TIME. NDT COMPLETE. INSP ONLY. T89170
LOWER FR 91 TO 92 SECTION C68 LOWER RIB SIDEWALL BETWEEN C67 AND C68 CRACKED ON TOP AT MIDDLE SECTION DOT 101- 120 INSTALLED WEB STIFFENER IAW A300-600 SRM 51-40-21 REVIEWED
*SDR FILED OPEN* FAULT: R/H FWD CARGO FLOOR RBL 0 STA.2029/FR31 - STA.2082/FR32 HAS CORROSION. DOT 33-003
*SDR FILED OPEN* FAULT: LOWER FR 91 TO 92 SECTION C68 LOWER RIB SIDEWALL BETWEEN C67 AND C68 CRACKED ON TOP AT MIDDLE SECTION DOT 101- 120
*SDR FILED OPEN* AFT CARGO DOOR CUTOUT PLATE CRACKED (AFT ZONE ) DOT 041 APPROVED
*SDR FILED OPEN* FAULT:AA014 -LT WING #1 SLAT INBD SLAT DRIVE RETRACTABLE DOOR IS CRACK. APPROVED
FAULT: UNDER FLIGHT DECK IN AVIONICS BAY, R/H CORNER ABOVE O2 BOTTLES, CORNER BRACKET TO DECK SUPPORT IS CRACKED. DOT 60-001 INSTALLED NEW BRACKET USING FASTENER P/N: HL18PB5-3, BATCH NO: 0004146161 IAW SRM 51-40-21
ENG#2 T/R O/B SLEEVE FWD, EDGE DISBONDING. DOT 641/11 INSTALLED 02 TRANSLATING SLEEVE EDGE PROTECTOR ON ENGINE #2 T/R, O/B, IAW SRM 51-40-21.
FAULT, ENG#2 T/R I/B FWD BOTTOM IN THE CORNER, DENT DOT 641/07 INSTALLED ANGLE AT #2 ENG. T/R I/B FWD FRAME. IAW A300-600 PW4000 SRM 54-04-01.
4 DAMAGED HOLES (2 L/H) (2 R/H) AT SPLICING AT FRAME 17 AND MAIN DECK FLOOR BEAM ATTACHMENT. AREAS MARKED IN RED. ROTO PERFORMED ON FRAME 17 HOLES. ALL HOLES ARE FREE OF DEFECTS, IAW 51-10-01. T96525 T91779
FR 47 RH SPLICE FITTING HAS 2 HOLES DAMAGED AT THE BACK OF HOLE. AREAS MARKED IN RED. ROTO PERFORMED ON FRAME 47 RH SPLICE FITTINGS. BOTH HOLES A & E ARE FREE OF DEFECTS, IAW 51-10-01. T96525 T91779. T96515 T91779. FASTENERS WILL BE INSTALLED ON THE EO-18288-JIC002
FR 47 RH SPLICE FITTING HAS 2 HOLES DAMAGED AT THE BACK OF HOLE. AREAS MARKED IN RED. ROTO PERFORMED ON FRAME 47 RH SPLICE FITTINGS. BOTH HOLES A & E ARE FREE OF DEFECTS, IAW 51-10-01. T96525 T91779. T96515 T91779
*SDR FILED OPEN* FAULT: 4 DAMAGED HOLES (2 L/H) (2 R/H) AT SPLICING AT FRAME 17 AND MAIN DECK FLOOR BEAM ATTACHMENT. AREAS MARKED IN RED. ROTO PERFORMED ON FRAME 17 HOLES. ALL HOLES ARE FREE OF DEFECTS, IAW 51-10-01. T96525 T91779
FLOOR PANEL 251YJ IS BROKEN
*** SUPPLEMENTAL SDR *** FAULT: MAIN DECK FLOOR PANEL 232SG IS BROKEN FABRICATED PANEL 232SG FROM 5024N40001SS-G BATCH # 4055277 PER SREO A300-5320-40552-B
WING RIGHT I/B FLAP HAS SOME DENTS AT LOWER SURFACE.DOT119-008 APPLY AERODYNAMIC FILLER ON LOWER SURFACE IAW SRM 57-50-00. TREATED AND PRIMED AREA IAW SRM 51-21-10. APPLIED TOP COAT ON AREA IAW SRM 51-75-10, CUP PAINT # 02-012-176
LH WING INBD FLAP LWR SURFACE SHOWS SOME DENT EVALUATE DOT 146-031 APPLY AERODYNAMIC FILLER ON LOWER SURFACE IAW SRM 57-50-00. TREATED AND PRIMED AREA IAW SRM 51-21-10. APPLIED TOP COAT ON AREA IAW SRM 51-75-10, CUP PAINT #02-012-176.
MAIN DECK FLOOR PANEL 232SG IS BROKEN
FAULT - # 1 ENGINE OBD FAN COWL LEADING EDGE INTERNAL SURFACE HAS MISSING SEVERAL FINGER SEAL . 89-139. INSTALLED 02 TRANSLATING SLEEVE EDGE PROTECTOR ON ENGINE #2 T/R, O/B IAW SRM51-40-21. REVIEWED
*SDR FILED OPEN* FAULT-LH WING INBD FLAP LWR SURFACE SHOWS SOME DENT EVALUATE DOT 146-031
-WING RIGHT I/B FLAP HAS SOME DENTS AT LOWER SURFACE.DOT119-008
FLOOR PANEL 251YJ IS BROKEN FABRICATED PANEL 251YJ FROM 5024N400001SS-G BATCH # 4055277 PER SREO A300-5320-40552-B
RH WHEEL WELL AT FRAME 47 , STATION 2983 DRAIN TUBE HAS DENT . 89-130 INSTALLED NEW RH W/W AT FR47 ST2983 DRAIN TUBE IAW A300 AMM 20-23-12/001
RH WHEEL WELL AT FRAME 47 , STATION 2983 DRAIN TUBE HAS DENT . 89-130
*SDR FILED OPEN* FAULT - NLG RH WHEEL WELL FWD DOOR HAS 1 EA FRAYED BONDING WIRE . 89-120
NLG RH WHEEL WELL FWD DOOR HAS 1 EA FRAYED BONDING WIRE . 89-120 REMOVED AND REPLACED NLG RH WHEEL WELL FWD DOOR HAS 1 EA FRAYED BONDING WIRE IAW AMM 20-28-11-0001. BINDING METER CHECK OK TR-4949
FORWARD ENTRY DOOR RED WARNING LIGHT INOPERATIVE. PERFORMED TSM 52-73-00 FIG 105 AND FOUND LOOSE CONNECTION ON WARNING LIGHT, RECONNECTED PER AMM 52-73-11, OPS CHK GOOD AT THIS TIME, DEFERRAL CLEARED, PLACARD REMOVED.
INSPECTION TYPE:N/ASTRONG BURNING SMELLR&R (CALESCERS PER MM 21-51-00 SERVICED USING APU PNEMATIC PROCEDURE OPS CHECK GOOD NO SMELL NOTED AT THIS TIME. ESR: IPC 24-54-01
INSPECTION TYPE:SEGRH OVER WING IN AREA OF FR 47 S26R WTB PANEL SUPPORT BRACKET FOUND CRACKED.REMOVED AND REPLACED FITTING PER SRM 51-40-21.
INSPECTION TYPE:A300CENTER FUSELAGE RH BASE FRAME FITTING HAS CRACKED LOCATED FR44 AT AREA 1 BETWEEN STR 35 AND STR 36REPAIRED BASE FRAME FITTING FR44 RH SIDE PER EO A300-5310-46789-G APPENDIX-K
INSPECTION TYPE:A300LT WING #3 FLAP I/B END ANGLE BRACKET BROKEN/MISSING.REMOVED AND REPLACED ANGLE BRACKET SUPPORT IAW A300 SRM 51-40-21.
INSPECTION TYPE:A300LH WING #5 SLAT TRACK HAS BROKEN SHUTTER STOP PLATE.REMOVED AND REPLACED PLATE IAW A300 SRM 51-40-21.
INSPECTION TYPE:A300RH WING SUPPORT BRACKET INSIDE OF PANEL 612DB BROKENREMOVED AND REPLACED BRACKET IAW A300 SRM 51-40-21
INSPECTION TYPE:A300FRAE 72-1459 FLOOR BEAM SUPPORT BRACKET P/N A3617032720000 IS CRACKED.REMOVED AND REPLACED BRACKET P/N A3617032720000 BATCH 0003824942 IAW A300 SRM 51-40-21.
INSPECTION TYPE:NAATB - AFTER TAKEOFF ALL 3 LANDING GEAR WOULD NOT RETRACTREPLACED LANDING GEAR CONTROL MICROSWITCH UNIT (2GA) PER AMM 32-31-11-401. OPS GOOD. SN OF 895, SN ON 870. ALSO REPLACED PSEU (54GB) PRECAUTIONARY PER AMM 32-31-71-401. SN OFF 751, SN ON 23
INSPECTION TYPE:N/A RT WING INBD L/E NOSE SKIN MULTIPLE DENTS/GOUGES. REPAIRED IAW EO A300-5750-72544-C.
EMERGENCY LIGHT TEST INOPERATIVE. REPLACED THE LIGHT, OPSTESTED SYS MUPTIPLE TIMES IAW AMM 33-51-00. NO DEFECTS NOTED.
INSPECTION TYPE:N/A LAV EMER LIGHT INOP. RELAMPED OPS TEST GOOD PER AMM 33-51-21-4.
INSPECTION TYPE:SDR RT INBD FLAP LEADING EDGE DAMAGE (DENTED). ACCOMPLISHED INTERIM MINOR REPAIR PER EO A300-5750-92544A 05577896 5-9-19/ AS PER EO A300-5750-72544A, ACCOMPLISHED HFEC PER NDTM / PART 6,51-00-08 AND HFEC ILLEG SCAN PER NDSM PART 6, 51-10-01 NO CRACKS NOTED. ACCOMPLISHED ULTRASOUND THICKNESS CHECK. AIRCRAFT OK FOR SERVICE.
INSPECTION TYPE:124C AFT CARGO DOOR L/H LOWER SEAL RETAINER AND CORNER SEE CRACKED.REMOVED AND REPLACED IAW A300-600 SRM 51-40-21.
MAIN CABIN SEAT TRACK BETWEEN FRA 26 AND FRA 27 Y=0 HAS CORROSION ON UPPER SURFACE REMOVED CORROSION, APPLIED ALUMINUM FILLER, AND RESTORED PROTECTIVE COATING IAW A300-600 SRM 53-10-16
INSPECTION TYPE:12Y MAIN CABIN AFT SIDE OF LT FR 79 CLIP CRACKED. REMOVED AND REPLACED CLIP (P/N A53951939202) IAW SRM 51-40-21 AND DRAWING A53981939 REV C.
INSPECTION TYPE:12Y FLOOR SUPPORT AT FR 80 IS CRACKED AT THE SCREW ATTACHMENT HOLE.REMOVED AND REPLACED FLOOR SUPPORT IAW A300-600 SRM 51-40-21.
INSPECTION TYPE:12Y BELOW FLOORBOARD AT FR 19.22, RBL 50 THE FLOORBOARD IS BROKEN. FABRICATED NEW FLOOR PANEL IAW SREO A300-5320-42722-F.
INSPECTION TYPE:12Y NUMBER 2 PYLON PRECOOLER SUPPORT STRUCTURE INBOARD SIDE UPPER PYLON AREA IS CRACKED. REMOVED AND REPLACED EXTRUSION IAW SRM 51-40-21 AND DWG A54611629 ISSUE D.
NUMBER 1 PYLON SPIGOT RETAINER IS CORRODED. REMOVED AND REPLACED FLANGE IAW A300-600 AMM 54-51-78-0401
INSPECTION TYPE:12YR/W I/B LEADING EDGE KRUEGER FLAP UP STOP FITTING RIB AFT CORNER IS CRACKEDREMOVED AND REPLACED IAW A300-600 SRM 51-40-21, AB DWG A535-10144
INSPECTION TYPE:12YRR/W I/B LEADING EDGE KRUEGER FLAP UP STOP FITTING CLOSEOUT CRACKEDREMOVED AND REPLACED IAW A300-600 SRM 51-40-21, AB DWG A53510147
INSPECTION TYPE:12YRSUPERNUMERARY AREA, L/H SIDE, FWD FACE OF L-SHAPED SOLID BARRIER HAS CORROSION ALONG LOWER SURFACECUTOUT CORRODED MATERIAL, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW REO G21869
INSPECTION TYPE:12Y E AND E COMPARTMENT CEILING FR LBL37 INTERCOSTAL CLIP CRACKED. REMOVED AND REPLACED INTERCOSTAL CLIP IAW SRM 51-40-21.
INSPECTION TYPE:12YRW IB LEADING EDGE KRUGER FLAP OUTBD RIB AFT CLIP CRACKEDREMOVED AND REPLACED CLIP PER A300-600 SRM 51-40-21.
INSPECTION TYPE:124C AFT PIT, BULK CARGO, LOWER STEP UP WALL, FRAME 69 RIGHT VERTICAL WEB IS DENTED NUMEROUS SPOTS. REMOVED AND REPLACED VERTICAL WEB IAW SRM 51-40-21.
INSPECTION TYPE:124C AFT PIT, BULK CARGO, LOWER STEP UP WALL, FRAME 69 LEFT VERTICAL WEB IS DENTED NUMEROUS SPOTS. REMOVED AND REPLACED VERTICAL WEB IAW SRM 51-40-21.
INSPECTION TYPE:12YR RIGHT WING PANEL 613AB LAND AREA OB FWD FASTENER HOLE CRACKED. REPAIRED PER SRM 53-15-63.
INSPECTION TYPE:12Y NR 1 PYLON O/B I/B SHACKLE PITTED. REMOVED AND REPLACED SHACKLE PER AMM 54-51-72-0401.
RUDDER - TRAILING EDGE IS SEPARATED IN SEVERAL AREAS.REMOVED AND REPLACED APEX STRIP IAW A300-600 SRM 51-40-44.
INSPECTION TYPE:12Y AVIONICS COMPARTMENT UNDER FLOOR PANEL 121TF WIRE BUNDLE SUPPORT CRACKED FR18-FR19. REMOVED AND REPLACED WIRE BUNDLE SUPPORT IAW 51-40-21.
INSPECTION TYPE:12YFWD PIT, UNDER FLOOR, RIGHT SIDE, FR 33 ATTACH BRACKET FOR WIRE BENT. REPAIRED PER DWG A92496354
INSPECTION TYPE:12Y LT LOWER TRAILING EDGE BELOW NR 3 SPOILER PANEL SUPPORT STRUCTURE CRACKED. REMOVED AND REPLACED IAW SRM 57-51-11, 51-40-21 DWG #A572-46551.
INSPECTION TYPE:12Y RT SHEAR PLATE AFT OF FRA 79 STR 26 IS CRACKED. REMOVED CRACKED SHEAR PLATE AND REPLACED WITH ANGLE IAW EO #A300-5310-58168-A.
INSPECTION TYPE:12Y LT FR 79 FWD ATTACH ANGLE IS CRACKED. REMOVED CRACKED ANGLE AND REPLACE WITH NEW ANGLE IAW SRM 51-40-21 AND DRAWING A53275449 REV C.
INSPECTION TYPE:12Y LT SHEAR PLATE AFT OF FR 79 STR 26L IS CRACKED. REMOVED CRACKED SHEAR PLATE AND REPLACED WITH ANGLE IAW EO A300-5310-58168-A.
FUSELAGE EXTERIOR REPAIR AT TAIL JACK PAD HAS SEVERAL DENTS AND GOUGES IN THE REPAIRREPAIRED IAW UPS EO #A300-5330-72174-A
FUSELAGE EXTERIOR REPAIR AT TAIL JACK PAD HAS SEVERAL DETNS AND GOUGES IN THE REPAIRREPAIRED IAW UPS EO A300-5330-72158-A
INSPECTION TYPE:12Y AFT. SKIN O/B SIDE CRACKED NR 2 PYLON AFT. LOWER FAIRINGREPAIRED PER EO A300-5450-21297-1 APPENDIX B.
INSPECTION TYPE:12Y AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRAKET FR54 @ RBL36 CRACKED. REMOVED AND REPLACED PER SRM 51-40-21.
INSPECTION TYPE:12YR REMOVED AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT FR54 @ RBL40 CRACKED. REMOVED AND REPLACED NEW PANEL SUPPORT CPN5826 IAW SRM 51-40-21.
INSPECTION TYPE:12YAFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR54 @BL0 CRACKED. REMOVED AND REPLACED BRACKET PER SRM 51-40-21.
INSPECTION TYPE:12Y FWD CARGO COMPARTMENT DOOR FRAME UPPER RT FR20 WIRE HARNESS BRACKET DAMAGED. REMOVED AND REPLACED WIRE HARNESS BRACKET FR20 IAW SRM 51-40-21.
INSPECTION TYPE:12Y FWD CARGO COMPARTMENT AFT BULKHEAD UPPER SUPPORT STA 38.2 @ LBL 22 BRACKET CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.
FWD CARGO COMPARTMENT RT UPPER SEAL DEPRESSOR @FR20 GOUGED. REMOVED AND REPLACED CARGO DOOR SEAL DEPRESSOR IAW A300-600 SRM 51-40-21
INSPECTION TYPE:12Y AVIONICS COMPARTMENT FLOOR SUPPORT ANGLE FR10 AND RBL 37 CRACKED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-40-21.
INSPECTION TYPE:12Y FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 AND LBL 41. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.
INSPECTION TYPE:12Y FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 AND LBL 60. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.
INSPECTION TYPE:12Y FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 @ RBL60 BRACKET CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.
INSPECTION TYPE:12Y FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2@ LBL 22 BRACKET CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.
BULK CARGO COMPARTMENT FLOOR PANEL JUST INSIDE BULK DOOR DAMAGED. MARKED WITH TAPE. DAMAGE LOCATED INBOARD OF LONGITUDINAL NET FLOOR ANCHOR.REPAIRED DAMAGE IAW EO NO A300-5320-42722-F.
EMERGENCY ESCAPE SLIDE WARNING LIGHT DOES NOT ILLUMINATE. R & R THE PSU IAW MM 52-73-18-0401. OPS CHECKED GOOD.
INSPECTION TYPE: 1C, DAMAGE FOUND AT BACK SIDE OF FRAME 47, HOLE M, AT 6 TO 9 O'CLOCK POS. ON BACK SIDE OF FRAME. REPAIRED IAW EO A300-5310-62121-A.
INSPECTION TYPE: 1C, DAMAGE FOUND AT BACK SIDE OF FRAME 47 LT SIDE, HOLE "A", AT 12 TO 1 O'CLOCK POS. ON BACK SIDE. REPAIRED IAW EO A300-5310-62122-A
INSPECTION TYPE: 1C, FRAME 40 MIDDLE FASTENER HOLE NR 2 HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION. REAMED THE FRAME AND INSTALLED A SECOND OVERSIZE FASTENER WITH WASHERS AND NUT IAW EO A300-5710-62125-B AND REO G20300, REV "D".
LT LANDING GEAR FORWARD LUG BORE DIAMETER "Y" IS 5.193. BORED HOLE TO FINAL DIA OF 5.284 IAW HAECO REO G19579 AND DWG R57240425, REV "A". PRIMED AND INSTALLED REPAIR BUSHINGS, 2 EACH, IAW REO G19579 AND DWG R57240425, REV "A".
INSPECTION TYPE:SPV, AFT CARGO PIT DOOR FRAME 61, FORK FITTING BETWEEN BEAM 4 AND 5 IS CRACKED. R & R FRAME 61 FORK FITTING.
RIGHT WHEEL WELL CEILING FOUND EVIDENCE OF BURNED WIRES AT FRAME 51, BS 2840. WIRES DAMAGED WING TO TRANSITION AREAS FOR LANDING GEAR EXT AND RETRACTION SYS 1 WIRE 3231-0092, 3231-0093, 3231-0094, 3231-0095, WDM 32-31-01. REPAIRED WIRES 3231-0092, 3231-0093, 3231-0094, 3231-0095, WDM 32-31-01, W/REF TO ESPM 20-43-11 FOR THE LANDING GEAR EXT RETRACTION SYS 1. OPS CHECKED LANDING GEAR SELECTOR VALVE. CK GOOD W/REF TO MM32-31-12-0501. REF LP'S 724989 THRU 724995.
INSPECTION TYPE: 5YR, FLOOR PANEL 231RG IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREO.
INSPECTION TYPE: 5YR, FLOORBOARD 251PG IS BROKEN. FABRICATED A NEW FLOORBOARD SREO.
INSPECTION TYPE: 5YR, FLOOR PANEL 231WG IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREO.
INSPECTION TYPE: 5YR, FLOOR PANEL 232XG BROKEN. FABRICATED NEW FLOOR PANEL IAW EO.
INSPECTION TYPE: 5YR, FLOORBOARD NR 231-SG IS BROKEN. FABRICATED NEW FLOORBOARD IAW SREO.
INSPECTION TYPE: 5YR, MAIN CABIN FLOORBOARD 222DG DAMAGED. FABRICATED NEW FLOORBOARD IAW REO 5320-16407.
INSPECTION TYPE: 5YR, MAIN CARGO FLOORBOARD 242LM DAMAGED. FABRICATED A NEW FLOORBOARD IAW EA 5320-16407.
INSPECTION TYPE: 5YR, FLOOR PANEL 242SH BROKEN. FABRICATED NEW FLOOR PANEL IAW SREO 5320-16407-E.
INSPECTION TYPE: 5 YR, FLOOR PANEL 231NJ IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW SREO.
INSPECTION TYPE: 5YR, FLOOR PANEL 231HG IS BROKEN. FABRICATED NEW IAW SREO.
INSPECTION TYPE: 5YR, CABIN FLOOR PANEL 231MJ FWD END DAMAGED FR20-FR21, LBL 78 LBL95. FABRICATED NEW FLOOR BOARD IAW SREO A300-5320-16407-E.
INSPECTION TYPE: 5YR, CABIN FLOOR PANEL CRACKED 221EG FROM 18-FR19 LBL 36-LBL 45. FABRICATED NEW FLOOR PANEL IAW SREO.
INSPECTION TYPE: 5YR, FLOOR PANEL NR 241-QJ IS BROKEN FABRICATED A NEW FLOORBOARD IAW SREO.
INSPECTION TYPE:5YR, FWD CABIN, LAVATORY WET AREA, CORROSION FOUND TOP SIDE OF FLOORBEAM AROUND FASTENER HOLE AT APPROXIMATELY FR 13A AND LBL 60. ACCOMPLISHED REPAIR IAW EO A3005310-56702-A.
CABIN SEAT TRACK CORRODED FROM FRAMES 79-80, LBL 31. REPAIRED SEAT TRACK IAW SRM 53-10-16.
INSPECTION TYPE: 5YR, MAIN DECK FLOOR SEAT TRACK HAS CORROSION FRAMES 79 - 80 RBL 45. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201
INSPECTION TYPE:5YR, MAIN DECK FLOOR SEAT TRACK HAS CORROSION FR 79-FR 80, BL0. ACCOMPLISHED REPAIR IAW SRM 53-10-16, FIG 201.
INSPECTION TYPE:5YR, CABIN SEAT TRACK CORRODED, FR 79-FR80, LBL 45. REPAIRED BY SPLICING NEW SECTION OF SEAT TRACK WITH REPAIR SPLICES IAW SRM 53-10-16, FIG 201.
INSPECTION TYPE:5YR, AFT CABIN UNDER FLOOR FRAME 79 BEAM RT SIDE APPROXIMATELY, Y1580 THERE IS SUSPECTED INDICATION OF CRACKING ACCOMPLISHED IAW EO A300-5310-56629-A.
INSPECTION TYPE: PDC, FOUND L1 DOOR EVAC SLIDE RELEASE WARNING SYS LIGHT INOPERATIVE. INSPECTED AND CLEANED CONNECTOR ON AUTONOMOUS STANDBY POWER SUPPLY UNIT. REINSTALLED CONNECTOR IAW AMM 52-73-18-0401. OPS CK GOOD.
MLG SLOW TO RETRACT, DISPATCHED GEAR DOWN AND LOCKED REF M530375. INSPECTED RT MAIN GEAR AND FOUND DOOR SEQUENCE VALVE OUT OF RIG, AD ADJUSTED IAW 32-31-00-501, PERFORMED RE-TRACK TEST IAW 32-31-00-501 WITH GROUND POWER CARTS. SYS OPS NORMAL THIS CLEARS M-530375.
CAPTAIN'S GLARESHIELD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM 33-12-11-0401. OPS CHECKED NORMAL.
AFTER TAKE OFF AND GEAR RETRACTED, AFTER A MINUTE RECEIVED AN AMBER DOOR LIGHT AND RED UNIT LIGHT ON LEAR LIGHT PANEL. ACCOMPLISHED NLG RETRACTION IAW MM 32-31-00-0501. ALL INDICATIONS NORMAL IN BOTH SYS 1 AND 2. NO DEFECTS NOTED. ACCOMPLISHED GVI OF NOSE GEAR COMPONENTS. NO DEFECTS NOTED.
3C INSPECTION, ACFT BAY FUSELAGE FRAME 46 BASE FITTING CRACKED. REPAIRED FITTING IAW EO A300-5310-46789-A, APPENDIX F.
3C INSPECTION, ACFT BAY FUSELAGE RT FRAME 45 BASE FITTING CRACKED. REPAIRED FITTING IAW EO 5310-46789-A, APPENDIX G.
3C INSPECTION, ACFT BAY FUSELAGE RT FRAME 46 BASE FITTING CRACKED. REPAIRED FITTING IAW EO A300-5310-46789-A, APPENDIX G.
DURING 3C INSPECTION, RT WING OTBD FLAP UPPER SKIN HAS CORROSION AT OTBD STATIC WICK ACCOMPLISHED REPAIR ON RT OTBD FLAP UPPER SKIN AT OTBD STATIC WICK IAW STA EA 300-5750-01-A5251 IR AND EO A300-5750-54197-A.
EVACUATION SLIDE RELEASE RED WARNING LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM 52-73-18-0401 TESTED IAW AMM 52-73-00-0501. OPS CHECKED OK.
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231PH IS CRACKED AT LOWER SKIN. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.
INSPECTION TYPE: SV, MAIN CABIN FLOORBEAM IS CORRODED AT UPPER SURFACE AFT OF FR 15A Y45 AND Y953. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBEAM AT FR 15A Y450 AND Y953 IAW EO A300-5310-46814-A, PARA 6A.
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231MJ IS CRACKED AT FWD INBD CORNER. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232NJ IS CRACKED AT AFT INBD CORNER. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.
CREW ENTRY DOOR EMERGENCY EXIT SIGN INOPERATIVE. R & R EMERGENCY EXIT SIGN IAW 33-51-13-04. CHECKED GOOD.
INSPECTION TYPE:1C, MAIN CABIN FLOORBOARD NR231LJ HAS A CRACK AT LT FWD SCREW. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 231LJ IAW EO A300-5320-40552-A, APPENDIX B.
INSPECTION TYPE:1C, RT WING INBD FLAP INBD BULLNOSE CHAFED. REPAIRED RT WING INBD FLAP INBD BULLNOSE BETWEEN RIBS 1 AND 2 REF STA, SA, EA 300-5750-01-A3511 AND EO A300-5750-44656-A.
MAIN DECK SEAT TRACK AT FR 32-33 DAMAGED AT -Y953. REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201 AND EO A300-5310-42 579-B.
CREW REPORTED EVACUATION SLIDE WARNING SYS LIGHT DID NOT TEST, BUZZER IS GOOD. TS IAW FIM 52-73-00, FIG 102. R & R ESCAPE SLIDE IND LIGHT IAW AMM 52-73 -11-04. OPS CK GOOD. C/W WAN NR1703356. THIS CLEARS DEFERRAL M442679.
ATB - AFTER TAKEOFF "ECAM FLT CTL BLUE SERVO LOW PRESSURE" STATUS. BLUE SERVO INOP. HYD PAGE "BLUE" SYS WAS DISPLAYED IN AMBER PRESSURE 3450 BLUE SYS. R & R SW 17CB IAW MM 27-14-18-04 REF TSM 27-14-00, FAULT ISO, PG 101, FIG 102.
AFTER TAKEOFF "ECAM FLT CONTROL BLUE SERVO LOW PRESSURE" STATUS. BLUE SERVO INOPERATIVE HYD PAGE "BLUE" SYS WAS DISPLAYED IN AMBER PRESSURE, 3450 BLUE SYS. OPEN
INSPECTION TYPE:10YR, L-1 DOOR FWD GIRTBAR FLOORBOARD SEPARATED. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX B.
INSPECTION TYPE: 10YR AFT CARGO FLOOR PANEL 151UF IS DELAMINATED, CRACKED IN NUMEROUS AREAS. FABRICATED FLOOR PANEL 151UF IAW EO A300-5320-16407-D APP C.
INSPECTION TYPE:10YR, AFT CARGO FLOOR PANEL NR 151VF CRACKED IN HALF FOUND AFTER RECHECKING OF ACFT PARTS FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX. C.
INSP TYPE:10YR BULK PIT FLOOR PANEL 161HF REQUIRES REPLACEMENT IAW EO A300-5320-16407-D (EFN15220071007 FABRICATED NEW BULK PIT FLOOR PANEL 161HF IAW EO A300-5320-16407, APPENDIX D.
INSPECTION TYPE:10YR BULK PIT FLOOR PANEL 161GF REQUIRES REPLACEMENT IAW EO A300-5320-16407-D. FABRICATED NEW BULK PIT FLOOR PANEL 161GF IAW EO A300-5320-16407, APPENDIX D.
INSPECTION TYPE:10YR, MAIN COMPARTMENT FLOOR PANEL 222EG IS DAMAGED FABRICATED FLOOR PANEL 222EG IAW EO A300-5320-16407-D, APPENDIX B.
INSP TYPE:10YR, MAIN CARGO COMPARTMENT FLOOR PANEL 231NJ IS DAMAGED. REPAIRED FLOOR PANEL 231NJ IAW EO A300-5310-37761-A.
INSPECTION TYPE:10YR, MAIN CARGO COMP FLOOR PANEL 231GH IS DELAMINATED. REPAIRED IAW EO A300-5310-37749-A, REF RCD 337266.
INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOOR PANEL 231QH IS DELAMINATED. REPAIRED IAW EO A300-5310-37749-A, REF RCD 337266.
INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOOR PANEL 232XG IS CRACKED AT FWD EDGE. REPAIRED FLOOR PANEL 232XG IAW EO A300-5310-37759-A.
INSPECTION TYPE:10YR, MAIN COMPARTMENT FLOOR PANEL 231KJ IS PUNCTURED ON SEVERAL AREAS. FABRICTED FLOOR PANEL 231KJ IAW EO A300-5320-16407-D, APPENDIX B.
INSPECTION TYPE:10YR, SEAT TRACK ELONGATED FOUND AT MAIN CARGO COMPT. STA FRAME 33 BL 37RT. REPAIRED IAW EO A300-2550-37794-A, AND SAA EA 300-5310-01-A2293 REV I/R.
INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOOR PANEL 241LJ IS DELAMINATED. REPAIRED FLOOR PANEL 241LJ IAW EO A300-5310-37752-A.
INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOORBOARD 251 WG BROKEN AFT CORNER. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203 SHT. 1 REF RCD 337200.
INSPECTION TYPE:10YR, MAIN CABIN CARGO COMPARTMENT FLOORBOARD 252UJ IS DELAMINATED AT CTR SECTION LT SIDE. REPAIRED FLOORBOARD 252UJ IAW EO A300-5310-37770-A.
INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241AJ IS CRACKED OTBD CTR EDGE. REPAIRED BY FABRICATING PANEL IAW EO A300-5320-16407-A, APPX B.
INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOOR PANEL 251JM IS PUNCTURED. FABBED IAW 53-10-20, PARA. 8A, FIG 201 REF RCD 337183.
INSPECTION TYPE:10YR, MAIN CARGO COMP FLOOR PANEL 251RG BETWEEN FR 57.1 TO FR 58 IS CRACKED ACCOMPLISHED REPAIR IAW SRM 53-10-20, PARA 8B REF RCD 337186.
INSPECTION TYPE:10YR, MAIN CARGO COMP. FLOOR PANEL 261 CM IS DELAMINATED ACCOMPLISHED REPAIR IAW SRM 53-10-20, PARA. 8B REF RCD NR 3 37144.
INSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT FLOOR PANEL 262AM IS CRACKED AT AFT EDGE. REPAIRED FLOOR PANEL 262AM IAW PER EO .
INSPECTION TYPE:10YR NR 2 PYLON RIB 18 AFT ATTACH FITTING BORE PITTED AND CORRODED. R & R RIB 18 ATTACH FITTING IAW AMM 54-51--75-04.
INSPECTION TYPE:10YR MAIN CARGO COMP. FLOOR ACESS PANEL 262 CM IS CRACKED AT AFT EDGE ACCOMPLISHED REPAIR IAW SRN 53-10-20, PARA 8B REF RCD NR 3371 42.
INSPECTION TYPE:10YR LT INBD FLAP L/E DENTED 4 PLACES APPROX 52 TO 64 IN'S FROM INBD END. REPAIRED IAW SRM 57-50-00, FIG 208, PARA 4H.
INSPECTION TYPE:10YR LT INBD FLAP UPPER SKIN REPAIR DOUBLER GOUGED REPAIRED IAW EP NR A300-5750-37801-A AND SAA EA 300-5750-01-A2278 REV. I/R
INSPECTION TYPE:10YR, LT CTR FLAP UPPER SKIN REPAIR DOUBLER GOUGED. REPAIRED IAW EO A300-5750-37795-A AND EA 300-5750-01-A2276, REV. I/R.
INSPECTION TYPE:10YR, MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 79 AND 80 CORRODED AT Y 17.75 FWD SIDE. R & R SEAT SECTION BETWEEN FRAME 79 AND 80 AT Y 17.75 FWD SIDE IN MAIN CARGO COMPT REF EO A300-5310-37842-A.
INSPECTION TYPE:10YR, DEFERRED ITEM D422787 MAIN DECK CARGO COMPT. RIGID BARRIER AFT REPAIR. REPAIRED MAIN DECK CARGO COMPT. RIGID BARRIER REF EO A300-5310-37297-B AND EA 300-5310-01-A2263 REV I/R.
D419148 SKIN DENTED 4 PLACES ON PREVIOUS REPAIR FRAME 84/85 STRINGERS 44L-44R. REMOVED DAMAGED DOUBLER AND INSTALLED NEW REPAIR IAW EO A300-5330-36645-B, REF NRC 346597 AND LOG PAGE.
EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW MM 33-51-14-04. OPS TEST GOOD.
INSPECTION TYPE:N/A ATB - IN FLIGHT PASSING FL 250 BOTH PACKS FAILED RETURNED TO SJU. PERFORMED CABIN PRESSURE CONTROL AND BITE TEST IAW A300-600 TSM 21-30-00. TESTED GOOD AT THIS TIME. PERFORMED CABIN PRESSURIZATION IAW A300-600 AMM 21-31-00-05. OPERATION WAS GOOD AT THIS TIME. OK FOR SERVICE.
ATB - WHILE CLIMBING THROUGH 12,000 FEET, THE CREW RECEIVED A SPOILER FAULT MESSAGE ON THE NUMBER 1, 4 AND 7 SPOILERS AND THE NR 1 YAW DAMPER. RETURNED TO PHL WITHOUT INCIDENT. REPLACED FAC. PERFORMED OPERATIONAL TEST PER 27-61-00. DEFERRAL CLEARED. PLACARD REMOVED.
ATB DUE TO SUSPECTED COMPRESSOR STALL ON TAKEOFF. HEARD LOUD BANG AND A LARGE SHUDDER DURING ROTATION. THE F/O THOUGHT HE SAW A FLASH OF LIGHT ON THE RT SIDE. ALSO HAD AUTO THROTTLE ANOMALIES. FOUND EVIDENCE OF BIRD STRIKE TRAILING SIDE OF FAN AND COMPRESSOR AT 2:30 POS AND REMNANTS FOUND AT 2.5 BLEED SCREENS AT THE 10:00 POS. NR 2 ENG RAN PER TSM 72-00-40 T/S PER 72-00-40, OK FOR SERVICE.
INSPECTION TYPE:N/A MCD FLOOR PANEL POS 6/7LT DAMAGED. REPAIRED PER EO A300-5320-16407.
INSPECTION TYPE:N/A MAIN ENTRY DOOR HARD TO OPEN AND CLOSE FROM INSIDE AND OUTSIDE. ESCAPE SLIDE REMOVED PER MM 25-61-21-04. PLACARD PER MEL 52-11-01-3 LUBED ALL DOOR LINKAGES. OPS CHECK NORMAL OPENING AND CLOSING INSIDE AND OUTSIDE OF DOOR. AIRCRAFT OK FOR SERVICE.
INSPECTION TYPE:4C REPAIR NR EFN 122LGPG1023 WAS FOUND ON LOWER BULK PIT PANEL 161LF. FABBED FLOOR PANEL 161 LF IAW EO NR A300-5320-16407-C APPX D.
INSPECTION TYPE:4C SURVEY NR 122-W3-02 LW CENTER FLAP UPPER SKIN BETWEEN STR 2.6-2.8 AND RIBS 13-15 DOUBLER GOUGED. REMOVED FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00, PG 218, 57-50-00, FIG 205.
INSPECTION TYPE:4C SURVEY SEQ NR 122-W4-02 R/W INBD FLAP UPPER SKIN BETWEEN RIBS 11-12 AND STR 2.1-2.4 DOUBLER GOUGED. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00 PG 218, 57-50-00 FIG 205.
INSPECTION TYPE:4C SURVEY SEQ NR 122 L/WD INBD FLAP UPPER SKIN BETWEEN RIBS 11-12 AND STR 2.1-2.2 REPAIR DOUBLER GOUGED. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00, FIG 205 AND 51-21-10, PG 1.
INSPECTION TYPE:4C BULK CARGO FLOOR PANEL NR 161 HF IS DENTED AND HAS FIELD REPAIRS. FABRICATED NEW FLOOR PANEL IAW EO NR A300-5320-16407-C APPX D.
INSPECTION TYPE:4C BULK CARGO FLOOR PANEL NR 161GFI HEAVILY DENTED. FABRICATED NEW FLOOR PANEL IAW EO NR A300-5320-16407-C, APPX D.
INSPECTION TYPE:4C BULK CARGO FLOOR PANEL NR 162HF IS HEAVILY DENTED AND HAS FIELD REPAIRS. FABRICATED NEW FLOOR PANEL IAW EO NR A300-5320-16407-C, APPX D.
INSPECTION TYPE:4C TRANSFERRED FROM LOG PAGE NR 230041 ITEM 1 FUSELAGE SKIN LIGHTNING DAMAGE FWD OF FRAME 11 (TOP OF FUSE NOSE SECT) REF EO A300-5330-31036-A. REMOVED TEMP REPAIR AND FABBED AND INSTALLED REPAIR DOUBLER IAW SRM A 300 51-31-00, TABLE 3 PAGE 21, 51-21-10, TABLE 1, 53-10-12, PG 367, FIG 215.
INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PER 33-51-0, OPS CHECKS OK.
INSPECTION TYPE:N/A LIGHTNING STRIKE TO FASTENER 1 INCH FWD OF FRAME 11. REPAIRED PER EO A300-5330-31036-A.
INSPECTION TYPE:N/A FUSELAGE DENT FWD OF LOWER AFT CARGO DOOR OUT OF LIMITS. ENGINEERING EVALUATING. INSPECTED AREAS JUST FWD OF FRAME 58, BETWEEN STR 33 AND STR 29. CHECKED MATERIAL REMAINING WITH ULTRA SOUND AND FOUND TO BE WITHIN REWORK LIMITS PER A300 SRM 53-10-13 DIA 101 PERM ALLOWABLE REWORK.
INSPECTION TYPE:SV LEFT LANDING GEAR FWD TRUNNION BEARING HOUSING HAS A DEEP GOUGE ON LWR SIDE. ACCOMPLISHED REPAIR OF LT LANDING GEAR FWD TRUNNION BEARING HOUSING LWR SIDE IAW SAA EA 300-5751-01-A1425, UPS EO A300-5740-29719-A, AND AIRBUS RAS/BAE/1007667/2008.
INSPECTION TYPE:SV RIGHT LANDING GEAR FWD TRUNNION BEARING HOUSING HAS A DEEP GOUGE ON LWR SIDE. ACCOMPLISHED REPAIR OF RT LANDING GEAR FWD TRUNNION BEARING HOUSING LWR SIDE IAW SAA EA 300-5751-01-A1426, UPS EO A300-5740-29720-A, AND AIRBUS RAS/BAE/1007668/2008.
INSPECTION TYPE:N/A UNABLE TO UNLATCH OR OPEN LIFE RAFT BIN. LUBED LATCH, OPS CHECKS GOOD.
INSPECTION TYPE:N/A ESCAPE SLIDE INOP. M342678 D/D 1/26/07. INSTALLED SERVICEABLE ESCAPE SLIDE WITH REF TO MM 25-61-21-04. THIS CLEARS M342678.
EMERG LIGHTS INOP ON MAINT CHECK. REPLACED BATTERY PACK.
SUPERNUMARY AREA EMERGENCY LIGHTS WON'T TEST CORRECTLY PER 33-51-00- 5 (2) PLACED LIGHTS ON DEFERRAL M-332471 PER MEL 33-51-05-1 PLACARD INSTALLED. REF. L/P 641546; PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING ALL LIGHTS OPS CK GOOD, SYS CK GOOD IAW AMM 33-51-00. THIS CLEARS M332471. OK FOR FLIGHT
INSPECTION TYPE:N/A EMERGENCY LIGHTING SYSTEM INOP. PERFORMED ADJ/TEST OF EMERGENCY LIGHTS PER MM 33-51-00-05. OPS CHECK NORMAL AT THIS TIME.
EXIT LIGHT OVER ENTRY DOOR DIM. REPLACED BULBS IN EXIT LIGHT, CHECKS OK.
FO'S WINDSHIELD CRACKED. R&R'D F/O WINDSHIELD WITH REF TO MM 56-11-11-4. OPS CKS OK.
NR 2 AFT LOWER PYLON AT RIB 18 HAS CRACK APPROX .75 L AT RIB SECTION MEMBER INBD. MEMBER 2 PLACES ABOVE AND BELOW NUTPLATE. REMOVED AND REPLACED L-ANGLE ON THE NR 2 PYLON IAW A300 SRM 51-40-00.
NR 1 AFT LOWER PYLON AT RIB 18 BOTH INBD AND OTBD SECTION MEMBERS ARE CRACKED ABOVE AND BELOW CNTR NUTPLATE. REMOVED AND REPLACED L-ANGLE MEMBERS IAW A300 SRM 51-40-00 AND 51-40-21.
THE DOOR SLIDE ARMED AURAL WARNING AT THE DOOR DID NOT TEST PROPERLY PRIOR TO OPENING THE ENTRY DOOR AFTER LANDING. EVACUATION SLIDE WARNING BUZZER DEFERRED PER A300 MEL 52-73-01-2 M 295473 ASSIGNED. RESET C/B'S 2WN & 1WN PERFORMED TEST IAW AMM 25-63-00-5 THIS CLEARS M 295473 PLACARD REMOVED.
INSPECTION TYPE:N/A WHEN OPENING DOOR, TESTED CREW ENTRY DOOR SLIDE WARNING BUZZER DID NOT SOUND. WARNING LIGHT STILL ILLUMINATES. WORKED FINE WHEN DEPARTED. PERFORMED OPERATION TEST OF DOOR PER 52-10-11-6, OPS CHECK OK.
F/O OXYGEN MASK WILL NOT TEST. INSTALLED SERVICEABLE CREW QUICK DOWNING OXYGEN MASK AND STOWAGE BOX ASSY IAW MM 35-12-51-4.
F/O 02 MASK WILL NOT TEST PROPERLY. REINSTALLED F/O 02 MASK. TEST OKAY.
BOTH THRUST REVERSERS LOCKED OUT DUE TO LT CASCADE VANE AND TRANSLATING COWL DAMAGE. REMOVED NR 1 ENGINE RT TAIL ROTOR COWL ASSY IAW MM 71-13-03-4. RB 04126. INSTALLED REVERSER HALF, THROUGH 71-13-03-4 C. 1-19, 21 AND 22,32,33. JDS 81085. C/W STEP 31 OF 71-13-03 & REMOVED AND REPLACED NR1 T/R 78-31-00. 51783 COMPLIED W/REMAINING STEPS IAW MM 71-13-03-4.
INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. R&R NR 1 AND NR 2 BATTERIES AND PERFORMED CAPACITY TEST M AUTO. STANDBY POWER SUPPLY UNIT PER MTC 52-300-03-1-4 PASS TEST.
INSPECTION TYPE:N/A CAPTAINS & FIRST OFFICERS SHOULDERS HARNESS RETRACT INTO SEATBACK.