N908DA
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.
214 reports on file, 1996-02-09 – 2020-02-25.
Part: FASTENER — MISSING (VERTICAL STAB) · airframe 63,146 hrs · 34,885 cycles
LOOSE AND MISSING FASTENERS ABOVE SPLICE STA ZFS= 52.267 AT VERTICAL STABILIZER LEADING EDGE (EHV) SUMMARY NRC 00491: VERTICAL STABILIZER LEADING EDGE WAS REPAIRED PER MD-90 SRM 55-30-05 VOLUME I PAR. 11, AD 5530-01044-05 AND DWG SG09550004 REV. D. PERFORM DVI (INITIAL 3,000 CYCLES AND REPETITIVE 3,000 CYCLES) PER MD90 SRM 55-30-05 STEP 10 PAR. D. (1) VOL. I LOG-PAGE UPDATED (1505084)
Part: BEAM — CRACKED (NLG DOOR FRAME) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACKED RH DOOR JAMB BEAM ON STA 45 AND X=- 18 AT NLG WHEEL WELL AREA (FYT) ENTR 00983062 W SUMMARY OF NRC 600:RH DOOR JAMB BEAM ON STA 45 AND X=-18 AT NLG WHEEL WELL AREA WAS REPAIRED PER ETI-90-20-020 REV 2 AND ER/A 585590-14 REV. ORIGINAL ASSOCIATED ER/A 14-585590 ADDED FOR AC 9208 (1504497)
Part: SKIN — CRACKED (BS 1437) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA Y=1437 BTW LONG 13-13RH (FUS) SUMMARY OF NRC S/N 00161: FUSELAGE SKIN STA Y=1437 BTW LONG 13- 13RH WAS REPAIRED PER ER/A 585546-14 REV. ORIGINAL AND ETI-90-20 -016 REV. 1 AND PERFORM DETAIL VISUAL INSPECTION WITHIN EVERY 3,000 FLIGHT CYCLES AFTER SECTION I PER ENGINEERING REPAIR/ AUTHORIZATION 585546-14 REVISION ORIGINAL SEC II. UNDER LP 1499631 ASSOCIATED ER/A 14-585546 ADDED FOR AC 9208 (1500807)
Part: FLOOR SUPPORT — CORRODED (BS 720-740) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON L2 LOWER SILL INTERCOSTAL BTW STA 720/740 AND 63 LBL PASSENGER CABIN (W2) LOG-PAGE UPDATED SUMMARY OF NRC 00359 CORROSION LEVEL 2 LOWER SILL BTW STA 720/ 740, 63 LBL WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 AND 7 (1499637)
Part: TORQUE TUBE — CRACKED (VENTRAL STAIRWAY) · airframe 63,141 hrs · 34,883 cycles
CRACKED VENTRAL STAIR WAY TORQUE TUBE BEAM AT AFT ACCESSORY COMPARTMENT (CAT) LOG-PAGE UPDATED SUMMARY OF NRC 00794. VENTRAL STAIR WAY TORQUE TUBE BEAM AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER MD 90 SRM 51-30-02, 51-30 -05 AND 51-30-01 VOL. II ALSO D/DWG 9911992 REV. AK (1499831)
Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: WORN AND BENTED PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN ON L1 DOOR HOLD OPEN ATTACH POINT (FUS) SUMMARY OF NRC 00100. PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN ON L1 DOOR HOLD OPEN ATTACH POINT WAS REPLACED PER MD 90 SRM 51- 30-05 VOL. II AND SRM 53-30-01 PAR.9 FIG. 8 VOL. I (1499838)
Part: DOOR FRAME — CORRODED (BS 1212-1220) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON DOOR JAMB WEB STA 1212-1220 BTW PROJECTION LONGS 29RH-28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 SUMMARY OF NRC 00334: CORROSION LEVEL 2: WEB OF STA. 1204 TO 1276 BTW. LONG. 26 R/H TO LONG. 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 VOL. II SRM 51-30-02 AND 51-30-05 ALSO DWG 5936442 REV. A (1498015)
Part: SKIN — CORRODED (BS 864) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON FUSELAJE SKIN STA=864 AND STR- 28R TO STR- 29R. SUMMARY OF NRC 00198: CORROSION (LEVEL 2) ON FUSELAJE SKIN STA= 864 AND STR- 28R TO STR- 29R WAS REPAIRED PER ETI-90-20-009 REV. ORIGINAL AND ER/A 585513-14 REV. ORIGINAL SECTION I. ACCORDING TO ER/A 585513-14 REV. ORIGINAL SECTION II REPETITIVE INSPECTIONS. PERFORM GVI TO THE SECTION I REPAIR, PER MD90 SRM VOL. II 51-11-01 WITHIN EVERY 8,000 FLIGHT CYCLES AFTER SECTION I LOG PAGE # 1496818. ASSOCIATED ER/A 00-585513 ADDED FOR AC 9208 LOG-PAGE UPDATED (1497885)
Part: DOOR FRAME — CRACKED (NLG DOOR) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACKED LH DOOR JAMB BEAM ON STA 48 AND X=18 AT NLG WHEEL WELL AREA (FYT) LOG-PAGE UPDATED SUMMARY OF NRC 00601: LH DOOR JAMB BEAM ON STA 48 AND X=18 AT NLG WHEEL WELL AREA WAS REPAIRED PER MD-90 VOL. I SRM 53-90-01 PAR.8 LOG-PAGE UPDATED (1495717)
Part: SKIN — CORRODED (BS 886-902) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 883 TO 902 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00887: CORROSION WAS ATTENDED PER MD-90 SRM 51-10-03 PAR 26 (A) VOL. II ETI-90-20-008 REV. 1 AND ER/A 585247 -14 REV; ORIGINAL ASSOCIATED ER/A 00-585247 ADDED FOR AC 9208 LOG-PAGE UPDATED (1494558)
Part: FRAME ANGLE — CORRODED (BS 1379) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1379 BTW LONGS 29RH TO 26RH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00552: FRAME CLIP STA 1379 BTW LONGS 29RH TO 26RH AT AFT CARGO COMPARTMENT (CCT) WAS REPLACED PER MD-90 SRM VOL I 53-10-02 FIG 3.(1494565)
Part: INTERCOSTAL — CORRODED (BS 1205-1210) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON INTERCOSTAL STA 1205-1210 BTW LONGS 30 AND 29RH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00349: CORROSION LEVEL 1: CORROSION ON INTERCOSTAL STA 1205 TO 1210 BTW LONGS 30 TO 29 RH AT AFT CARGO COMPARTMENT WAS REMOVED PER MD90 VOL. LL SRM 51-10-03 PAR. 26 (A ) AND (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR. 5 FIG. 3 SHEET 1 AND 2. ORIGINAL THICKNESS IS 0.040" AND REMAINING THICKNESS IS 0.039" THEREFORE IT'S WITHIN LIMITS PER ERA 511165- 14MA REV. D. EQUIPMENT OLYMPUS 38DL C/N: 1787 S/N:171455902 EXP: 21/FEB/20. TRANSDUCER SONOPEN V26-RM N/S: 947479 ASSOCIATED ER/A 00-511165 ADDED FOR AC 9208 LOG-PAGE UPDATED (1494320)
Part: SKIN — CORRODED (BS 962-984) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 962 TO 984 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF THE NRC 00886: CORROSION WAS ATTENDED PER MD-90 SRM 51-10-03 PAR 26 VOL. II AND ETI-90-20-007 REV. ORIG AND ER/A 585124-14 REV: ORIGINAL ASSOCIATED ER/A 00-585124 ADDED FOR AC 9208 LOG-PAGE UPDATED (1494556)
Part: SKIN — CORRODED (BS 943-962) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 943 TO 962 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ;OF NRC 00890, CORROSION LEVEL 1 : CORROSION ON CENTER WING UPPER SKIN STA 943 TO 962 BTW X=44 TO X=60 AT WING BOX AREA WAS ATTENDED PER MD-90 SRM 51-10-03 PAR (C) VOL. II , ETI-90-20 -008 REV 1 AND ER/A 585247-14 REV. ORIGINAL ASSOCIATED ER/A 14-585247 ADDED FOR AC 9208 LOG-PAGE UPDATED (1494754)
Part: SKIN — CORRODED (BS 902-924) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY. OF NRC 0888. CORROSION LEVEL I. CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=44 TO X=60 AT WING BOX AREA WAS REMOVED PER MD-90 SRM VOL. II 51-10-03 PAR. 26 A ER/A 585247-14 REV; ORIGINAL SECTION I (PERMANENT REPAIR) ETI-90-20- 008 REV. 1 ASSOCIATED ER/A 14-585247 ADDED FOR AC 9208 (1495102)
Part: SKIN — CORRODED (BS 924-943) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00885, CORROSION LEVEL 1; CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=-44 TO X=-60 AT WING BOX AREA WAS REMOVED REMAINING WITHIN LIMITS PER MD-90 SRM 51-10-03 PAR 26 VOL. II AND ETI-90-20-007 REV. ORIG AND ER/A 585124-14 REV: ORIGINAL ASSOCIATED ER/A 14-585124 ADDED FOR AC 9208 LOG-PAGE UPDATED (1494772)
Part: SKIN — CORRODED (BS 924-943) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=44 TO X=60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY ; OF NRC 889, CORROSION LEVEL 1 ; CORROSION ON CENTER WING UPPER SKIN STA 924 TO 943 BTW X=44 TO X=60 AT WING BOX AREA WAS ATTENDED PER MD-90 SRM 51-10-03 PAR 26 (A) VOL. II ETI-90- 20-008 REV. 1 AND ER/A 585247-14 REV; ORIGINAL ASSOCIATED ER/A 14-585247 ADDED FOR AC 9208 LOG-PAGE UPDATED (1494763)
Part: SKIN — CORRODED (BS 943-962) · airframe 63,141 hrs · 34,883 cycles
AWR HIDDEN CORROSION IN REF NRC 895. DURING REMOTION OF VAPOR BARRIER WAS FOUND CORROSION ON CENTER WING UPPER SKIN STA 943- 962 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 01179: CORROSION LEVEL 1; CORROSION ON CENTER WING UPPER SKIN STA 943- 962 BTW X=-44 TO X=-60 AT WING BOX AREA WAS REMOVED REMAINING WITHIN LIMITS PER MD-90 SRM 51-10- 03 PAR 26 VOL. II AND ETI-90-20-007 REV. ORIG AND ER/A 585124-14 REV: ORIGINAL ASSOCIATED ER/A 14-585124 ADDED FOR AC 9208 (1495495)
Part: SKIN — CORRODED (BS 992) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 992 BTW X=44 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY OF NRC 00891. CORROSION LEVEL 1. CORROSION ON CENTER WING UPPER SKIN STA 992 BTW X=44 AT WING BOX AREA WAS REMOVED PER MD-90 SRM 51-10-03 PAR 26 (A) VOL. II, ER/A 585247-14 REV. ORIGINAL SECTION I (PERMANENT REPAIR) AND ETI-90-20-008 REV. 1 ASSOCIATED ER/A 14-585247 ADDED FOR AC 9208 (1495270)
Part: SKIN — CORRODED (BS 902-924) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=-44 TO X=-60 AT WING BOX AREA MRB 57-331-02 (CPAX) SUMMARY; OF NRC 00884, CORROSION LEVEL 1 , CORROSION ON CENTER WING UPPER SKIN STA 902 TO 924 BTW X=-44 TO X=-60 AT WING BOX AREA WAS REMOVED REMAINING WITHIN LIMITS PER MD-90 SRM 51-10-03 PAR 26 VOL. II ETI-90-20-007 REV. ORIG. AND ER/A 585124-14 REV . ORIGINAL ASSOCIATED ER/A 14-585124 ADDED FOR AC 9208 LOG-PAGE UPDATED (1494812)
Part: LONGERON — CRACKED (BS 1475) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACKED LONGERON 2RH ON STA 1475 AT AFT ACCESSORY COMPARTMENT (CAT) SUMMARY OF NRC S/N 00785: LONGERON WAS REPAIRED PER ER/A 564080- 14MA REV. ORIG. SECTION II. PERFORM SECTION III INSPECTION EVERY 3000 CYCLES AFTER THIS REPAIR. PER ER/A 564080-14MA REV. ORIGINAL SECTION II STEP 7. PERFORM A DETAILED VISUAL INSPECTION OF THE L2R SPLICE REPAIR INSTALLED PER THIS ERA LOCATED AT STA 1463 TO ENSURE NO NEW DAMAGE EXISTS. PER ER/A 564080-14MA REV. ORIGINAL SECTION III: REPEAT INSPECTION. ASSOCIATED ER/A 00-564080 ADDED FOR AC 9208 LOG-PAGE UPDATED (1495632)
Part: FRAME ANGLE — CORRODED (BS 1269) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1269 BTW LONGS 29RH TO 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00328: CORROSION LEVEL 2. FRAME CLIP STA 1269 BTW LONG. 29 RH TO 28 WAS REPLACED PER MD 90 SRM VOL.I 53-10-02 PAR . 5 FIG. 3 AND SRM VOL.II 51-30-05 AND 51-30-02 (1491697)
Part: FRAME ANGLE — CORRODED (BS 1364) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON FRAME CLIP STA 1364 BTW LONGS 28RH TO 27LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00303. CORROSION LEVEL 2. FRAME CLIP STA 1364 BTW LONGS 28RH TO 27LH WAS REPLACED PER MD90 SRM 51-30-02 VOL.II AND D/DWG 9912243 REV. JS (1491774)
Part: LONGERON — CORRODED (BS 1395) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON LONGERON END 27RH STA 1395 AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) LOG-PAGE UPDATED RII: N ENTR 00897853 W SUMMARY OF NRC 00558. CORROSION LEVEL 2. LONGERON END 27RH STA 1395 AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM 51-30- 05 AND D /DWG 5936439 REV. CD (1491695)
Part: LONGERON — CORRODED (BS 1395) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON LONGERON END 28RH STA 1395 AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) SUMMARY OF NRC 00557. CORROSION LEVEL 2 LONGERON END 28RH BTW STA 1395 AT AFT CARGO COMPARTMENT WAS REPLACED PER MD90 VOL. LL SRM 51-30-05 AND D/DWG 5936439 REV. CD LOG-PAGE UPDATED (1491693)
Part: SKIN — CRACKED (BS 1494) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA Y=1494 BTW LONG 2 -3 LH (FUS) LOG-PAGE UPDATED SUMMARY OF NRC 00591: SKIN STA Y=1494 BTW LONG 2-3 LH WAS REPAIRED PER ER/A 585379-14 REV. ORIG AND ETI-90-20-002 REV. 1 PERFORM A GENERAL VISUAL INSPECTION PER ER/A 585379-14 REVISION ORIGINAL SECTION II "REPETITIVE INSPECTION", PER MD90 SRM VOL. II 50-11-01 WITHIN EVERY 3000 CYCLES UNDER LOG PAGE 1488717 ASSOCIATED ER/A 14-585379 ADDED FOR AC 9208 LOG-PAGE UPDATED (1491562)
Part: SEAT TRACK — CORRODED (BS 620-735) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON LH SEAT TRACK X=54 STA 620-625, 640-650, 670-675, 690-695, 700-705, 710-715 AND 730-735 MRB 53- 211-02 (CPAX) SUMMARY ; OF NRC 102 ; NEW SECTION SEAT TRACK ON STA Y=598 TO 864 WAS REPLACED PER MD-90 SRM 53-40-01 PAR .10 FIG . 6 VOL.I LOG-PAGE UPDATED (1491352)
Part: SEAT TRACK — CORRODED (BS 745-840) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON LH SEAT TRACK X=54 STA 745-750, 765-770, 775-780, 795,800, 805-810 AND 825-840 MRB 53-211-02 ( CPAX) SUMMARY ; OF NRC 103 ; NEW SECTION SEAT TRACK ON STA Y=598 TO 864 WAS REPLACED PER MD-90 SRM 53-40-01 PAR .10 FIG . 6 VOL. I LOG-PAGE UPDATED (1491379)
Part: DOOR FRAME — CORRODED (BS 360-370) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON DOOR JAMB WEB STA 360-370 BTW LONGS 28RH AND 26RH AT FWD CARGO COMPARTMENT MRB 53-302-07 (CCD) SUMMARY ; OF NRC 00827 ; LEVEL CORROSION 2 . DOOR JAMB WEB STA 360-370 BTW LONGS 28RH AND 26RH AT FWD CARGO COMPARTMENT WAS REPAIRED PER MD-90 SRM 53-00-01 PAR 8 FIG 6 VOL 1 LOG-PAGE UPDATED (1491460)
Part: STRUCTURE — CORRODED (BS 1364) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00555. CORROSION LEVEL 2 PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM VOL.I 53-10-02 PAR. 4 FIG. 2 AND 51-30-02 ALSO 51-40-05 VOL.II LOG-PAGE UPDATED (1491527)
Part: SKIN — CORRODED (BS 1364) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00555. CORROSION LEVEL 2 PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM VOL.I 53-10-02 PAR. 4 FIG. 2 AND 51-30-02 ALSO 51-40-05 VOL.II. UPDATED IN REFERENCE LOG PAGE (1491531)
Part: PAN — CRACKED (EMER DOOR FRAME) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACK ON LH AFT EMERGENCY EXIT DOOR JAMB PAN UPPER AREA (FUS) SUMMARY OF NRC 00162. LH AFT EMERGENCY EXIT DOOR JAMB PAN UPPER AREA (FUS) WAS REPAIRED PER MD 90 SRM 53-60-02 FIG. 4. LOG-PAGE UPDATED (1488821)
Part: FRAME — CRACKED (BS 1364) · airframe 63,141 hrs · 34,883 cycles
CRACK ON CAP STA Y= 1364 LONG 7LH AT PASSENGER CABIN (CPAX) SUMMARY OF NRC S/N 01063: CAP STA Y= 1364 LONG 7LH AT PASSENGER CABIN WAS REPAIRED PER ER/A 585192-14 REV. ORIGINAL AND ETI-90- 20-004 REV, ORIGINAL ASSOCIATED ER/A 00-585192 ADDED FOR AC 9208 (1488707)
Part: DOOR FRAME — CORRODED (BS 695-750) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON MID CARGO COMPT LOWER DOOR JAMB STA 695 TO 750 MRB 53-122-02 (CCC) SUMMARY OF NR 00206. LEVEL CORROSION II. MID CARGO COMPT LOWER DOOR JAMB STA 695 TO 750 WAS REPAIRED PER MD90 SRM VOL I 53-60- 02 FIG 9. SRM VOL II 51-10-03 PAR 21, 14 AND 26. (MRB 53-122-02) (1488715)
Part: FRAME — CORRODED (BS 1364) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT). SUMMARY OF NRC 00554. CORROSION LEVEL 2 PREVIOUS REPAIR FRAME STA 1364 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM VOL. I 53-10-02 PAR. 4 AND 51-30-02, 51- 30-05 VOL. II (1488685)
Part: CHANNEL — CORRODED (BS 1344) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON PREVIOUS REPAIR CHANNEL AND STRAP FRAME STA 1344 BTW LONGS 28RH TO 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 (CCT) NRC 00301. CORROSION LEVEL 2 PREVIOUS REPAIR CHANNEL AND STRAP FRAME STA 1344 BTW LONGS 28RH TO 28LH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM VOL. II 51-30-05 AND VOL. II 53-10-02 PAR 4 FIG. 2 (1487253)
Part: FITTING — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON FWD AND AFT FITTING AT AFT CARGO COMPT LOWER DOOR JAMB STA 1211 AND 1268 (CCT) MRB 53-123- 02 NRC 00202. CORROSION LEVEL 2. FITTING AT AFT CARGO COMPARTMENT LOWER DOOR JAMB STA Y=1211 AND Y=1268 WERE REPLACED PER MD 90 SRM 51-30-05 VOL. I AND D/DWG 5936469 REV. NEW. (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR. 5 FIG 3 SHEET 1-2; ORIGINAL THICKNESS IS 0.125" AND MINIMUM REMAINING THICKNESS IS 0.070" THEREFORE IT'S OUT LIMITS PER MD90 SRM VOL. I 53-00-01 FIG. 3. (1484698)
Part: FRAME — CORRODED (BS 1379) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) NRC 00550. CORROSION LEVEL 2. PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29LH AND 28LH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM VOL I 53-10-02 PAR. 4 FIG. 2 (1484201)
Part: FRAME — CORRODED (BS 1379) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT MRB 53-302-07 ( CCT) SUMMARY OF NRC 00549. CORROSION LEVEL 2.PREVIOUS REPAIR FRAME STA 1379 BTW LONGS 29RH AND 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER MD 90 SRM VOL. I 53-10-02 PAR. 4 FIG. 2 (1484182)
Part: SKIN — DAMAGED (L1 DOOR) · airframe 63,141 hrs · 34,883 cycles
RE-WRITE FROM NRC 0415: INITIAL INSPECTION: BEND EXTERNAL LOWER PREVIOUS REPAIR AT FWD ENTRANCE DOOR (L1) (PTAS)". REASON FOR RE-WRITE: PREVIOUS REPAIR CANT BE CONFORMED.SUMMARY OF NRC 1132: EXTERNAL LOWER SKIN AT FWD ENTRANCE DOOR ( L1) WAS REPAIRED PER MD-90 SRM VOL 1 52-01-01 FIG 16 LOG-PAGE UPDATED @ 10FEB20 (1484442)
Part: CUSP WEB — CORRODED (BS 718-736) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON RH CUSP WEB BTW STA 718-736 BTW X=-44 AND X=-60 MRB 53?211?01 (CPAX) SUMMARY OF NRC 01239: (LEVEL CORROSION 2), SECTION RH CUSP WEB OUT LIMIT BTW STA 718-736 BTW X=-44 AND X=-60 WAS REPAIRED PER MD-90 VOL II SRM 53-20-02 FIG 27 LOG-PAGE UPDATED (1484448)
Part: FRAME ANGLE — CORRODED (BS 1344) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON FRAME CLIP AT AFT CARGO COMPARTMENT STA 1344 AND BETWEEN L27-R AND L26-R. (C3) CORROSION LEVEL 2: FRAME CLIP AT AFT CARGO COMPARTMENT STA 1344 AND BETWEEN L27-R AND L26-R WAS REPAIRED PER MD-90 SRM VOL I 53-10-02 FIG.3. (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR. 5 FIG 3 SHEET 1-2; THICKNESS IS 0.063" AND MINIMUM REMAINING THICKNESS IS 0.034" THEREFORE IS OUT OF LIMITS PER MD90 SRM VOL. I 53-00-01 PAR. 5 FIG. 3 EQUIPMENT (1484056)
Part: WINDOW FRAME — CRACKED · airframe 63,141 hrs · 34,883 cycles
CRACK ON FRAME OF CLEAR VIEW WINDOW LH, UPPER AFT CORNER. (CPIL) INTERNAL DOUBLER WAS REPLACED PER MD90 SRM VOL II 51-30-02 AND 51-30-05 AND DWG 5911356 REV. DJ. (1483970)
Part: WINDOW FRAME — CRACKED · airframe 63,141 hrs · 34,883 cycles
AWR HIDDEN CRACK: IN REF NRC 01010 AFTER DOUBLER WAS REMOVED HIDDEN CRACK WAS FOUND ON UPPER AFT SKIN CORNER OF RH CLEARVIEW WINDOW (CPIL) SUMMARY NRC 01243:UPPER AFT SKIN CORNER OF RH CLEARVIEW WINDOW WAS REPAIRED PER MD 90 SRM VOL.I 56-10-02 FIG. 1 (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON UPPER AFT SKIN CORNER OF RH WINDOW. NO CRACKS WERE FOUND AFTER STOP DRILL PER MD-90 VOL. I SRM 56-10-02 REPAIR NOTE B. 3) & DC-MD/BOEING NDTSPM PART 6, 06- 10-01.001 (1482993)
Part: WINDOW FRAME — CRACKED · airframe 63,141 hrs · 34,883 cycles
CRACK ON FRAME OF CLEAR VIEW WINDOW RH, UPPER AFT CORNER. (CPIL) INTERNAL DOUBLER WAS REPLACED PER DWG: 5911356 REV DJ, MD90 SRM 51-30-01, SRM 51-30-02 AND SRM 51-30-05 VOL. II. (1482734)
Part: DOOR FRAME — CORRODED (BS 200-210) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION DOOR JAMB WEB ON STA 200-210 AND X =54 AT FWD WET AREA MRB 53?211?01 (W1) . CORROSION LEVEL 2. DOOR JAMB WEB ON STA 200-210 AND X=54 AT FWD WAS REPAIR PER MD-90 SRM 53-00-01 PAR.8 FIG.6 VOL.I (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR . 5 FIG 3 SHEET 1-2; NOMINAL THICKNESS ON DOOR JAMB WEB STA 200- 210 AND X=54 AT FWD WET AREA IS 0.055" AND MINIMUM REMAINING THICKNESS IS 0.034" THEREFORE IS OUT OF LIMITS PER MD90 SRM VOL. I 53-00-01 PAR. 5 FIG. 3 EQUIPMENT PANAMETRICS OLYMPUS 38DL PLUS EXP. DATE 14-NOV-20 S/N: 151215011, TRANSDUCER SONOPEN V260 (1480720)
Part: FLOOR PANEL — DELAMINATED · airframe 63,141 hrs · 34,883 cycles
DURING INSPECTION BY DELAMINATION, WERE FOUND FLOOR PANELS 221BF, 221HF, 221JF AND 221LF ARE OUT OF LIMITS IN REF TO NRC 00406.(CPAX) FLOOR PANELS 221BF, 221HF, 221JF AND 221LF WERE FABRICATED REPLACED AND IDENTIFIED PER.MD-90. VOL.1 SRM 53-20- 03 FLOOR PANELS MUST BE INSTALLED WITH CARD 5321-0301 (1481895)
Part: FLOOR PANEL — DAMAGED · airframe 63,141 hrs · 34,883 cycles
PANELS 222BF, 222LG,222UF WITH A MEASURE HIGTHER TO 20 PERCENT OF ALLOWED DAMAGE , THEREFORE THEY ARE OUT OF LIMITS PER MD-90 SRM VOL.1. 53-20-03 PARAGRAPH 5 FIGURE 2 FABRICATED, REPLACED AND IDENTIFIED PER MD-90 SRM VOL.I 53-20-03 PARAGRAPH 5 AND MUST BE INSTALLED WITH CARD 5321-0301 (1481896)
Part: CUSP WEB — CORRODED (BS 670-769) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON LH CUSP WEB STA 670-674, 674- 693, 693-712, 712-731, 731-750, 750-769 BTW X=54 AND X=60 MRB 53 ?211?01 (CPAX) CORROSION LEVEL 2, CUSP WEB ON STA= 655 TO STA =769 WAS REPLACED PER MD-90 SRM VOL II 51-30-02 AND DWG 9930538-9 REV: CF (1481194)
Part: CUSP WEB — CORRODED (BS 256-313) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON LH CUSP WEB STA 256-274, 274- 293 AND 293-313 BTW X=54 AND X=60 MRB 53-211-01 (CPAX) SUMMARY OF NRC 00265: (CORROSION LEVEL 2) NEW CUSP WEB WAS INSTALLED PER MD-90 SRM 51-30-02. VOL II AND SRM 51-30-01 TOOLS USED : TORQUE WRENCH P/N 1501MRMH, S/N 0414022500, D/D 14/MAY/20 (1481747)
Part: SKIN — CRACKED (PAX DOOR) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACK ON OUTER SKIN ABOVE HANDLE HOUSING AT FWD ENTRANCE DOOR (L1)(PTAS) ENTRANCE DOOR WAS REPAIRED PER ER/A 501106-14MA REVISION "C" ASSOCIATED ER/A 00-501106 ADDED FOR AC 9208 (1480715)
Part: PAN — CRACKED (BS 750) · airframe 63,141 hrs · 34,883 cycles
CRACKED OUTER PAN OVER BEAM # 5 STA 750 AT MID CARGO COMPARTMENT DOOR (PTAS) OUTER PAN OVER BEAM # 5 STA 750 AT MID CARGO COMPARTMENT DOOR WAS REPAIRED PER MD-90 SRM VOL. I 52-30- 02 PAR. 6 FIG. 4 (1481765)
Part: FLOORBEAM — CORRODED (BS 522) · airframe 63,141 hrs · 34,883 cycles
CORROSION ON FLOOR SUPPORT STA 522 BTW LONGS 26RH TO 26LH AT FWD CARGO COMPARTMENT MRB 53-302-07 (CCD) CORROSION LEVEL 1. CORROSION WAS REMOVED PER MD-90 SRM 51-10-03 PAR 26 (A) VOL II. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FLOOR SUPPORT STA 522 BTW LONGS 26RH TO 26LH AT FWD CARGO COMPARTMENT. NO CRACKS WERE FOUND ON REWORKED AREA PER ERA 511165-14MA REV. D AND DC-MD/BOEING NDTSPM PART 6, 06- 10-01.001 (EQUIPMENT: MENTOR C/N:1205 EXP: 08-OCT-20). (UT) WAS ACCOMPLISHED NDT SPM 04-00-07 PAR. 5 FIG. 3, SHEET 1-2, NOMINAL THICKNESS: 0.040" MINIMUM REMAINING THICKNESS IS: 0.038", THEREFORE ARE WITHIN LIMITS PER ERA 511165-14MA REV. D. EQUIPMENT: OLYMPUS 38DL PLUS EXP. DATE: 23/AUG/20. C/N: 1298, S/ N: 140938708, TRANSDUCER V260-RM. S/N: 947479 ASSOCIATED ER/A 00-511165 ADDED FOR AC 9208 (1480675)
Part: CUSP WEB — CORRODED (BS 598-655) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON LH CUSP WEB STA 598-605, 610- 617, 617-625 AND 650-655 BTW X=54 AND X=60 MRB 53?211?01 (CPAX) SUMMARY OF NRC 00110. CORROSION LEVEL 2. LH CUSP WEB STA 598-655 , WAS REPLACED PER MD 90 SRM 51-30-02 VOL.II AND 51-30-01 VOL II (1475482)
Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON LAVATORY SERVICE PANEL (FUS) ( AMDS 5300-2264) SUMMARY OF NRC 00033. CORROSION LEVEL 2: LAVATORY SERVICE PANEL WAS REPLACED PER MD-90 SRM 51-30-02 AND 51-30-05 VOL. II (1475820)
Part: CUSP WEB — CORRODED (BS 525) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
AWR IN REF NRC 0118, CORROSION ON RH CUSP WEB STA Y=525 AT PASSENGER COMPARTMENT MRB 53-211-01 ENTR 00983062 W SUMMARY OF NRC 01186, CORROSION LEVEL 2 ; RH CUSP WEB STA Y=525 AT PASSENGER COMPARTMENT WAS REPAIRED PER MD-90 VOL. I SRM 53-20 -02 FIG.16. (1475479)
Part: CUSP WEB — CRACKED (BS 1140) · airframe 63,141 hrs · 34,883 cycles
CRACKED LH CUSP WEB ON STA 1140 BTW X=54 AND X=60 (CPAX) CUSP WEB ON STA 1140 BTW X=54 AND X=60 LH WAS REPAIRED PER MD 90 SRM 53-20-02 PAR. 6 FIG. 6 VOL. I. (1473860)
Part: WEB — CORRODED (BS 120-149) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: SEVERAL CORROSION POINTS ON DIAPHRAGM FROM STA Y=120 TO Y=149 X=-40 TO X=40 IN REF AMDS 5300-2573. (CPIL) CORROSION WAS REMOVED STA Y=120 TO Y=149 X=-40 TO X=40 PER MD 90 VOL. II SRM 51-10-03 PAR.26 (A).(UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR. 5 FIG 3 SHEET 1-2; ORIGINAL THICKNESS IS 0.020" AND MINIMUM REMAINING THICKNESS IS 0.018", THEREFORE IT'S WITHIN LIMITS PER ER/A 511165-14MA REV. D (1474236)
Part: DOOR FRAME — CRACKED (BS 207) · airframe 63,141 hrs · 34,883 cycles
CRACK ON DOOR JAMB WEB STA 207, LONG 15 LH ( L1) CRACK ON DOOR JAMB WEB STA 207, LONG 15 LH WAS REPAIRED PER. MD-90 SRM 53-60-02 FIG. 15 VOL. I. (1472815)
Part: FRAME — WORN (BS 1050) · airframe 63,141 hrs · 34,883 cycles
WEAR ON RING PAN LOWER MID EDGE AT STA Y= 1050 RH SIDE. (CPAX) C/A NRC 00285:RING PAN LOWER MID EDGE AT STA Y= 1050 RH SIDE WAS REPLACED PER MD-90 SRM 51-30-02 AND 51-30-05 VOL. II (1472757)
Part: DOOR FRAME — CRACKED (BS 207) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACK ON DOOR JAMB WEB STA 207, LONG 11 LH ( L1) CRACK ON DOOR JAMB WEB STA 207, LONG 11 LH WAS REPAIRED PER. MD-90 SRM 53-60-02 FIG. 15 VOL. I. (1472823)
Part: SEAT TRACK — CRACKED (BS 1045-1050) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RH SEAT TRACK X=-54 BTW STA= 1045 AND 1050 PASSENGER CABIN C/A SEAT TRACK X=-54 BTW STA= 1045 AND 1050 WAS REPAIRED PER MD-90 SRM 53-40-01 VOL. I PAR. 6. (1469198)
Part: DOOR FRAME — CORRODED (BS 1211-1268) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON PREVIOUS REPAIR SPACER AT AFT CARGO COMPT LOWER DOOR JAMB STA 1211 TO 1268 MRB 53-123-02 CARGO COMPT LOWER DOOR JAMB STA 1211 TO 1268 WAS REPLACED PER MD90 VOL. L SRM 53-60-02 FIG. 9 (1469805)
Part: FRAME — CRACKED (BS 943) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 943 LH SIDE. (CPAX) RING PAN UPPER FWD EDGE AT STA Y= 943 LH WAS REPAIRED PER MD-90 SRM 56-20-02 VOL. I PAR. 3 FIG. 2 (1468779)
Part: FLOORBEAM — CRACKED (BS 1003) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACKED FLOOR SUPPOR ON STA 1003 BTW X=10 AT PAX CABIN AREA (CPAX). SUMMARY OF NRC S/N 00837: CRACKED FLOOR SUPPOR ON STA 1003 BTW X =10 AT PAX CABIN AREA (CPAX) WAS REPLACED PER MD-90 SRM 51-30-05 VOL.II. (LP# 1463142)
Part: FLOORBEAM — CRACKED (BS 1022) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACKED FLOOR SUPPOR ON STA 1022 BTW X=15 AT PAX CABIN AREA (CPAX). SUMMARY OF NRC S/N 00835: CRACKED FLOOR SUPPOR ON STA 1022 BTW X =15 AT PAX CABIN AREA (CPAX) WAS REPLACED PER MD-90 SRM 51-30-05 VOL.II. (LP# 1463137)
Part: FLOORBEAM — CRACKED (BS 1041) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACKED FLOOR SUPPOR ON STA 1041 BTW X=15 AT PAX CABIN AREA (CPAX). SUMMARY OF NRC S/N 00836: CRACKED FLOOR SUPPORT ON STA 1041 BTW X=15 AT PAX CABIN AREA (CPAX) WAS REPLACED PER MD-90 SRM 51-30- 05 VOL.II. (LP#1463134)
Part: FRAME — CRACKED (BS 1003) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 1003 RH SIDE. (CPAX) . SUMMARY OF NRC 00283:RING PAN UPPER FWD EDGE AT STA Y= 1003 RH SIDE WAS REPAIRED PER MD90-SRM VOL I 56-20-02 PAR. 3 FIG. 2. (LP# 1463818)
Part: FRAME — CRACKED (BS 674) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 674 RH SIDE. (CPAX) SUMMARY OF NRC 00281: RING PAN UPPER FWD EDGE AT STA Y= 674 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462880)
Part: FRAME — CRACKED (BS 1288) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1288 LH SIDE. (CPAX) SUMMARY OF NRC 00138:RING PAN UPPER AFT EDGE AT STA Y= 1288 LH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1461939)
Part: FRAME — CRACKED (BS 807) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 807 AND LOWER FWD EDGE STA Y=864 RH SIDE. (CPAX) SUMMARY OF NRC 00292: RING PAN UPPER FWD EDGE AT STA Y= 807 AND LOWER FWD EDGE STA Y=864 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462863)
Part: FRAME — CRACKED (BS 984) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 984 RH SIDE. (CPAX) SUMMARY OF NRC 00293: RING PAN UPPER FWD EDGE AT STA Y= 984 RH SIDE WAS REPAIRED PER MD 90 VOL I SRM 56-20-02 TYPE C FIGURE 3
Part: FRAME — CRACKED (BS 731) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER FWD EDGE AT STA Y= 731 RH SIDE. (CPAX) SUMMARY OF NRC 00282: RING PAN UPPER FWD EDGE AT STA Y= 731 RH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1462766)
Part: FRAME — CRACKED (BS 674) · airframe 63,141 hrs · 34,883 cycles
CRACK ON WINDOW RING PAN, UPPER FORWARD EDGE AT STA Y=984 AND Y=674 LH SIDE. (CPAX) SUMMARY OF NRC 00184:WINDOW RING PAN, UPPER FORWARD EDGE AT STA Y=984 AND Y=674 LH SIDE WAS REPAIRED PER MD-90 SRM-56-20-02 FIGURE2 (1461878)
Part: FRAME — CRACKED (BS 845) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN LOWER AFT EDGE AT STA Y= 943, Y=674 AND Y= 845 LH SIDE. (CPAX) SUMMARY OF NRC 00136:RING PAN LOWER AFT EDGE AT STA Y=943, Y=674 AND Y= 845 LH SIDE. WERE REPAIRED PER MD-90 SRM-56-20-02 FIGURE 2 (1461887)
Part: FRAME — CRACKED (BS 1288) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACK ON RING PAN LOWER FWD EDGE AT STA Y= 1288 LH SIDE. (CPAX) SUMMARY OF NRC 00137:RING PAN LOWER FWD EDGE AT STA Y= 1288 LH SIDE WAS REPAIRED PER MD90 VOL 1 SRM 56-20-02 FIG 2 (1461934)
Part: FRAME — CRACKED (BS 1098) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN LOWER FWD EDGE AT STA Y= 712 AND LOWER AFT EDGE STA Y=1079 AND Y=1098 RH SIDE. (CPAX) RING PAN LOWER FWD EDGE AT STA Y= 712 AND LOWER AFT EDGE STA Y=1079 AND Y=1098 RH WERE REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 (1461639)
Part: FRAME — CRACKED (BS 332) · airframe 63,141 hrs · 34,883 cycles
CRACK ON LOWER AFT RING PAN STA Y= 332 AND 636 AT PAX CABIN SUMMARY OF NRC 00135 LOWER AFT RING PAN STA Y= 332 AND 636 WERE REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 LOG-PAGE UPDATED (1461624)
Part: SEAT TRACK — CORRODED (BS 1095-1160) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON LH SEAT TRACK X=54 STA 1095- 1100, 1110-1115, 1130-1135,1140-1145 AND 1155-1160 MRB 53-211-02 (CPAX) SEAT TRACK X=54 LH ON STA 1095 TO STA 1160 WAS REPLACED PER MD-90 SRM VOL. II 51-30-01 (1460540)
Part: FRAME — CRACKED (BS 1250) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1250 RH SIDE. (CPAX) SUMMARY OF NRC 00294 RING PAN UPPER AFT EDGE AT STA Y= 1250 RH WAS REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2 (1461632)
Part: FRAME — CRACKED (BS 1231) · airframe 63,141 hrs · 34,883 cycles
CRACK ON RING PAN UPPER AFT EDGE AT STA Y= 1231 RH SIDE. (CPAX) SUMMARY OF NRC 00284: RING PAN UPPER AFT EDGE AT STA Y= 1231 RH WAS REPAIRED PER MD90 VOL I SRM 56-20-02 TYPE B FIGURE 2
Part: CUSP WEB — CORRODED (BS 1079-1098) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION LEVEL 2 OUT OF LIMITS ON LH CUSP WEB STA 1079- 1098 AND 1117-1136 BTW X=54 AND X=60 ON REFERENCE AT NRC 269 MRB 53?211?01 (CPAX) : LH CUSP WEB STA 1079-1098 AND 1117-1136 WERE REPAIRED PER MD-90 SRM VOL. I 53-20-02 FIG 18. (1459776)
Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 63,141 hrs · 34,883 cycles
CORROSION ON FLOOR SUPPORT STA 160-200 AND X =-44 AT FWD WET AREA MRB SUMMARY OF NRC S/N 00375 CORROSION LEVEL 2: FLOOR SUPPORT STA 160-200 AND X=-44 AT FWD WET AREA OUT LIMITS WAS REPLACED PER MD -90 SRM 51-30-02 VOL. II (1459079)
Part: CUSP WEB — CORRODED (BS 960-1079) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CORROSION ON LH CUSP WEB STA 960-965, 984- 1003, 1003-1022, 1022-1041, 1041-1060 AND 1060-1079 BTW X=54 AND X=60 MRB 53?211?01 (CPAX) C/A SUMMARY OF NRC S/N 00268: CORROSION LEVEL 1 ON LH CUSP WEB STA 960-965, 984-1003, 1003-1022, 1022-1041, 1041-1060 AND 1060-1079 BTW X=54 AND X=60 WAS REMOVED PER MD-90 SRM 51-10-03 PAR 26(A) VOL II, (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR. 5 FIG 3 SHEET 1-2 ON LH CUSP WEB STA 960-965, 984- 1003, 1003-1022, 1022-1041, 1041-1060 AND 1060-1079 BTW X=54 AND X=60, ORIGINAL THICKNESS ARE .040" MINIMUM REMAINING THICKNESS IS .038" THEREFORE REWORKED AREAS ARE WITHING LIMITS PER MD/90 SRM 53-20-02 PAR 7. C (1) FIG. 30 VOL I AND ERA NO. 511165-14MA (1454888)
Part: CUSP WEB — CRACKED (BS 875) · airframe 63,141 hrs · 34,883 cycles
INITIAL INSPECTION: CRACKED LH CUSP WEB ON STA 875 BTW X=54 AND X=60 (CPAX) C/A LH CUSP WEB ON STA 875 BTW X=54 TO X=60 WAS REPAIRED PER MD 90 SRM 53-20-02 PAR. 6 FIG. 6 VOL. I. (1454253)
Earlier reports · 1996–2019 · 129 reports
2019
Part: BEAM — NOT REPORTED (R1 DOOR) · airframe 63,141 hrs · 34,883 cycles
BEAM NR 4 AT FWD GALLEY SERVICE DOOR (R1) WAS REPLACED IAW SRM, VOL. II 51-30-01, 51-30-02 AND 51-30 -05. THE BEAM NR 4 AT FWD GALLEY SERVICE DOOR (R1) WAS REPLACED IAW SRM, VOL. II 51-30-01, 51-30-02 AND 51-30 -05.
Part: BEAM — CRACKED (GALLEY DOOR) · airframe 63,141 hrs · 34,883 cycles
CRACKED BEAM NR 4 AT THE FWD GALLEY SERVICE DOOR. THE BEAM WAS REPLACED IAW SRM, VOL. II 51-30-01, 51-30-02, AND 51-30 -05.
Part: DOOR — OPEN (NLG) · airframe 62,362 hrs · 34,361 cycles
A/C RETURN TO BLOCKS DUE TO LEFT NOSE GEAR DOOR OPEN. INSPECTED AND VERIFIED LEFT NOSE GEAR DOOR OPEN. VERIFIED PLUMB BOB SECURE IN HOLDER. SECURED GEAR DOOR. ALL CHECKS GOOD. A/C OK FOR SERVICE. (5494472)
Part: BATTERY — DISCHARGED (CABIN) · airframe 61,466 hrs · 33,755 cycles
BATTERY PACK B5-234 WILL NOT PWR FWD LIGHTS. INSP AND FOUND BATTERY BAD. REPLACED. CK NML. REF AMM 33-51. (LP# 5835604)
Part: SEAL — MISSING (LT NACELLE) · airframe 61,217 hrs · 33,586 cycles
LEFT UPPER FWD PYLON APRON SEAL ON LT ENGINE COWLING IS MISSING. REMOVED PANEL & SEPARATED APRON SEAL PER AMM 71-14 -01. INSTALLED NEW APRON SEAL FWD POS, LT ENG. IAW MD 90 AMM 71-14 OK FOR SVC. (LP# 5318774)
2018
Part: LIGHT — MISSING (CABIN) · airframe 60,975 hrs · 33,430 cycles
FLOOR PHOTO STRIP MISSING AT 25B. FOUND & REINSTALLED FLOOR PHOTO STRIP. (LP# 5011964)
Part: UNKNOWN — ODOR (CABIN) · airframe 60,471 hrs · 33,110 cycles
APU AIR ON AT GATE HAZE AND SMOKE IN AFT OF CABIN. BOTH DUCTS WENT UP TO 150 ON THE GROUND. C/W WK'S 2120-2001 & 2120-2002(936244) C/W NO GO ODI PREVENTION 2172. ALSO RMVD INLET DOOR VERIFIED NO CONTAMINATION. CLEANED AS PRECAUTION. VERIFIED NO CONTAMINATION IN CROSSOVER DUCT. C/W FULL DUCT BURNOUT PER AMM 21-53-00-720-801. (LP 4140179)
Part: STRUCTURE — CORRODED (BS 200-218) · corrosion level 2 · airframe 59,306 hrs · 32,375 cycles
FOUND CORROSION IN THE E & E BAY ABOVE AVIONICS RACK UNDER FWD GALLEY, BETWEEN BS 200 - 218.
2017
Part: SWITCH — FAILED (NLG DOWN) · airframe 58,491 hrs · 31,898 cycles
PERFORMED AN ABORTED APPROACH DUE TO AN ABNORMAL NOSE GEAR INDICATION WITH GEAR HANDLE DOWN. RAN QRH AND DECLARED EMERGENCY. HAD AN UNEVENTFUL LANDING AND TAXI TO GATE. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR DOWN SWITCH S1-412 IAW MM. OPERATION AND GEAR SWING CHECKS OK.
Part: CABLE — LACK OF LUBE (TAILCONE RELEASE) · airframe 57,517 hrs · 31,379 cycles
TAILCONE DID NOT RELEASE DURING OPERATIONAL TEST. LUBED, RECHECKED RIGGING OF CABLES. PERFORMED SUCCESSFUL FUNCTIONAL TEST.
2016
Part: COVER — LOOSE (EXIT SIGN) · airframe 57,120 hrs · 31,165 cycles
EMERGENCY EXIT SIGN COVER LOOSE. SECURED. OPERATION CHECKS GOOD.
Part: TERMINAL — SHORTED (READING LIGHT) · airframe 56,283 hrs · 30,645 cycles
READING LIGHT IN ROW 19-20 WENT OUT FOLLOWED BY ALL OF THE READING LIGHTS IN THE MAIN CABIN. WHILE DEPLANING PASSENGERS NOTED ELECTRICAL ODOR AT ROW 18. MAINTENANCE FOUND SHORTED TERMINAL END AT READING LIGHT SEAT 19B. COMPLIED WITH ERA 549193-14, REV O.
2015
Part: ATTACH FITTING — CRACKED (LT WING) · airframe 54,072 hrs · 29,327 cycles
LT WING GROUND SPOILER ACTUATOR FORWARD END ATTACH FITTING IS CRACKED ON INBD SIDE. REPAIRED IAW AMDS 5750-01120-0901.
Part: INTERCOSTAL — CRACKED (BS 971) · airframe 53,969 hrs · 29,257 cycles
CRACKED INTERCOSTAL LT SIDE, BS 971.75. R & R INTERCOSTAL IAW DWG 9911946 AND ERA 538857-14.
Part: INTERCOSTAL — DAMAGED (BS 1549) · airframe 53,934 hrs · 29,233 cycles
FOUND SEVERED INTERCOSTAL, BS 1549.750. COMPLIED WITH ERA 538857-14, REV O.
Part: SKIN — CRACKED (BS 1531) · airframe 53,455 hrs · 28,968 cycles
FOUND CRACK ON FUSELAGE SKIN, LT SIDE, BS 1531. REPAIRED IAW SRM 53-00-01.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,174 hrs · 28,801 cycles
TWO TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD.
Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 52,721 hrs · 28,513 cycles
L1 DOOR DAMAGED LOWER FORWARD CORNER. REPAIRED IAW PRI 534065-14, REV 0,1. COMPLY WITH ERA 534065-14, REV 0.
2014
Part: DUCT — CRACKED (CABIN PRESSURE) · airframe 52,030 hrs · 28,092 cycles
PERFORMED AN AIR TURN BACK. DURING CLIMB, AT 10000 FEET, ACFT DID NOT PRESSURIZE. NO FLOW. STARTED TO PRESSURIZE ON DESCENT. PERFORMED HEATLH CHECKS ON BOTH PACK SYSTEMS IAW AMDS. ALSO, PERFORMED OPS TEST OF PRESSURE SWITCH IAW AMM. ALL CHECKED GOOD. FOUND RAM AIR Y DUCT CRACKED AT FLANGE TO RT HEAT EXCHANGER. REPLACED DUCT, LT AND RT COMPRESSOR DISCHARGE THERMAL SWITCHES S1-119 / S1-120, LT AND RT TURBINE INLET THERMAL SWITCHES S1-121 / S1-122, AND LT AND RT HI LIMIT TEMP ANTICIPATORS D1-75/D1-81. PERFORMED SINGLE PACK OPS TEST. ALL NORMAL.
2013
Part: LANYARD — FRAYED (R1 DOOR SLIDE) · airframe 49,190 hrs · 26,281 cycles
DURING SERVICE CHECK, R1 DOOR SLIDE LANYARD FOUND FRAYED. REMOVED AND REPLACED LANYARD IAW AMM.
Part: VAPOR BARRIER — CORRODED (BS 938) · airframe 49,180 hrs · 26,275 cycles
BS 938, VAPOR BARRIER HAS CORROSION LBL 54. REMOVED CORROSION. RESTORED IAW ERA 516488-14AD, REV O.
Part: SKIN — CORRODED (BS 952) · airframe 49,180 hrs · 26,275 cycles
SKIN CORRODED AT BS 952, LBL 24-44L. REMOVED CORROSION, REWORKED, TREATED, PRIMED AND RESTORED VAPOR BARRIER IAW ERA 516488-MA, REV O.
Part: FUEL CELL — CORRODED (BS 950) · airframe 49,180 hrs · 26,275 cycles
CENTER TANK UPPER SURFACE, BS 950, HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED NEW FILLER, DOUBLER AND SHEAR CLIPS. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW ERA 516488-14AD, REV O.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 49,180 hrs · 26,275 cycles
AFT PRESSURE BULKHEAD LOWER DOOR JAMB HAS CORROSION. CUT OUT DAMAGE. LOCATED, DRILLED, FABRICATED AND INSTALLED REPAIR SPLICE DOUBLER IAW SRM 51-30-02, 53-60-02, FIG 3 AND 51-10-05.
Part: CUSP WEB — CORRODED (BS 950) · airframe 49,180 hrs · 26,275 cycles
CUSP WEB FS 950 CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED CUSP WEB FROM BS 902 TO 962 IAW SRM 53-20-02 AND DWG 69940443.
Part: SEAT TRACK — DAMAGED (BS 845-1155) · airframe 49,180 hrs · 26,275 cycles
MAIN CABIN SEAT TRACK FROM FS 845-1155, LBL 54.5, HOLES FOUND ELONGATED. FABRICATED, TREATED, PRIMED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, 51-10-03, & 51-30-02.
Part: LONGERON — CRACKED (BS 1475) · airframe 49,180 hrs · 26,275 cycles
AFT ACCESSORY COMPARTMENT, BS 1475, LONGERON 2 LT CRACKED. FABRICATED AND INSTALLED NEW LONGERON AND ANGLE SUPPORT IAW SRM 51-30-05 AND ERA 500312-14.
Part: FRAME — CRACKED (BS 962) · airframe 49,180 hrs · 26,275 cycles
BS 962 FRAME HAS A CRACKED. REMOVED DAMAGED FRAME SECTION. LOCATED, DRILLED AND INSTALLED NEW FRAME SECTION IAW DWG SR90530027, REV A.
Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 49,180 hrs · 26,275 cycles
CHAFING IN SKIN ON LT WING OUTBOARD FLAP, UPPER SURFACE, APPROXIMATELY 24 INCHES FROM OUTBOARD END. BLENDED AREA. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED INSTALLED IAW ERA 516489-14.
Part: FRAME — CORRODED (BS 1364) · airframe 49,180 hrs · 26,275 cycles
AFT CARGO BILGE AREA, BS 1364, LOWER FRAME HAS CORROSION LONGERON 28R-28L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. INSTALLED FRAME REPAIR IAW SRM 53-10-02.
Part: DOOR FRAME — DAMAGED (AFT CARGO BAY) · airframe 49,180 hrs · 26,275 cycles
AFT CARGO DOOR FRAME SURROUNDING DOOR STOPS STRUCTURAL HAS DETERIORATED, CHIPPED PAINT. REPAIRED IAW SRM 53-60-02, PARA 14.
Part: SKIN — DENTED (BS 275) · airframe 49,180 hrs · 26,275 cycles
LEFT HAND LOWER FUSELAGE SKIN BS 275 BETWEEN L25-26L FOUND DENTED. EVALUATED DENT, FOUND TO BE OUT OF LIMITS. DRILLED AREA, HFEC, NO CRACKS FOUND. TREATED, PRIMED AND INSTALLED RIVETS IAW SRM 53-31-01, 53-31-02 AND 51-10-03.
Part: SKIN — CORRODED (BS 864) · airframe 49,180 hrs · 26,275 cycles
EXTERIOR SKIN AT FS 864, LONGERON 29R CORRODED. REMOVED CORROSION, FABRICATED, TREATED, PRIMED AND INSTALLED NEW DOUBLER IAW SRM 53-30-01, 51-30-03 AND PL 900-5-1, NR 4.
Part: BULKHEAD — DAMAGED (BS 1395) · airframe 49,180 hrs · 26,275 cycles
FORWARD FACE OF AFT PRESSURE BULKHEAD, BS 1395, HAS BARE METAL EXPOSED. BOTTOM OF LONGERON 30-29R. CLEANED THE AREA'S METAL AND LOCATED HEAVY CORROSION THAT IS OUT OF LIMITS. REPAIRED IAW SRM 51-10-05, 51-30-05 AND DWG 9915561.
Part: SKIN — DAMAGED (BS 351) · airframe 49,180 hrs · 26,275 cycles
FUSELAGE SKIN, BS 351, BETWEEN LONGERONS 26 AND 27R HAVE LIGHTNING STRIKES. BLENDED LIGHTNING STRIKE. FOUND TO BE OUT OF LIMITS. FABRICATED INTERNAL DOUBLER, TREATED, PRIMED, AND INSTALLED DOUBLER REPAIR IAW SRM 51-31-01, 53-31-02 AND 51-30-02.
Part: SEAT TRACK — CORRODED (BS 1193) · airframe 49,180 hrs · 26,275 cycles
MAIN CABIN SEAT TRACK, BS 1193, LBL 44, IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01.
Part: SEAT TRACK — CORRODED (BS 200-256) · airframe 49,180 hrs · 26,275 cycles
SEAT TRACK, BS 200-256 RBL 44 HAS CORROSION ON UPPER SURFACE OF SCALLOPS AND UPPER SURFACE OF FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGED SEAT TRACK. FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW SRM 53-40-01 AND 51-10-03.
Part: CUSP WEB — CORRODED (BS 503) · airframe 49,180 hrs · 26,275 cycles
CUSP WEB, LOWER SURFACE, BS 503 HAS CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-20-02.
Part: SEAT TRACK — DAMAGED (BS 1250) · airframe 49,180 hrs · 26,275 cycles
SEAT TRACK, RBL 24, BS 1250 HAS GROOVES AND SMALL GOUGES. CUT OUT DAMAGE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01.
Part: CUSP WEB — CORRODED (BS 807-826) · airframe 49,180 hrs · 26,275 cycles
MAIN CABIN RT CUSP WEB, BS 807-826 HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-20-02 AND 53-20-00.
Part: CUSP WEB — CORRODED (BS 1079-1096) · airframe 49,180 hrs · 26,275 cycles
MAIN CABIN RIGHT CUSP WEB, BS 1079-1096 CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-20-02.
Part: CUSP WEB — CORRODED (BS 475) · airframe 49,180 hrs · 26,275 cycles
MAIN CABIN, BS 475 LBL 58, HAS CORROSION AT LIGHTNING HOLE CUSP WEB. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02.
Part: CUSP WEB — CORRODED (BS 522-541) · airframe 49,180 hrs · 26,275 cycles
LEFT SIDE OF FUSELAGE INTERIOR FS 541 TO 522 AND LBL 54 - 58 HAS CORRODED CUSP WEB. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-20-02.
Part: SEAT TRACK — CORRODED (BS 995-1025) · airframe 49,180 hrs · 26,275 cycles
CORROSION ON WEB AND ON SCALLOPS, RBL 54.5, SEAT TRACK BS 995 -1025. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01.
Part: CUSP WEB — CORRODED (BS 446-465) · airframe 49,180 hrs · 26,275 cycles
MAIN CABIN, RIGHT CUSP WEB BETWEEN BS 446 -465 HAD CORROSION AT LIGHTNING HOLE. REMOVED CORROSION. FOUND TO BE OUT OF LIMTIS. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-20-02.
Part: CUSP WEB — CORRODED (BS 489-503) · airframe 49,180 hrs · 26,275 cycles
MAIN CABIN, RT CUSP WEB BETWEEN BS 489 -503 HAS CORROSION AT LIGHTNING HOLE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED, TOPCOATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02.
Part: CUSP WEB — CORRODED (BS 541-560) · airframe 49,180 hrs · 26,275 cycles
LT SIDE OF FUSELAGE INTERIOR FS 541 TO 560, LBL 54-58 HAD CORRODED CUSP WEB. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-20-02.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,760 hrs · 26,034 cycles
2 X 2 INCH HOLE IN ACFT. CUT OUT DAMAGE SKIN. INSTALLED REPAIR IAW SRM 53-30-01, PG 68J, FIG 8.
Part: FAIRING — CRACKED (RT AILERONS) · airframe 47,708 hrs · 25,452 cycles
RT ALERON FAIRING BETWEEN T/E TABS CRACKED AT T/E. IAW ERA 512021-14 ACCOMPLISHED ENGINEERING APPROVED TIME LIMITED REPAIR IAW PS 900-5-1, NR 04 ASSOCIATED ER/A 00-512021 REMOVED FOR AC 9208. REPAIRED DAMAGED AILERON FAIRING IAW ERA 512021-14, REV A AND SRM 57-50-02. TAP TEST GOOD OK TO PAINT. INSPECTION TAP TEST GOOD OK TO PAINT. PRIMED AND PAINTED REPAIR AREA. BALANCED AILERON BY CALCULATION METHOD IAW SRM 57-50-01, PAR 9. NEW BALANCE IS WITHIN BALANCE LIMITS IAW SRM 57-50-01. ENGRAVED THE NEW BALANCE CONDITION ON WEIGHT AND BALANCE TAG.
2012
Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 46,308 hrs · 24,670 cycles
ON POWER UP AND RESETTING CIRCUIT BREAKER ARCING NOISE AND ASSOCIATED ELECTRICAL ODOR FOUND CAPT VSI/TCAS INDICATOR INOP PULLED AND RESET CIRCUIT BREAKER INDICATOR STILL INOP. CONFIRMED SOURCE OF ELECTRICAL ODOR WAS FAILED CAPTAINS VSI. REMOVED AND REPLACED VSI. OPERATION CHECKS GOOD.
Part: SWITCH — CONTAMINATED (AC BAY) · airframe 44,843 hrs · 23,866 cycles
SHIP 9208 REPORTED SMELL/FUMES IN CABIN. NO VISIBLE SMOKE. DISSIPATED IN APPROXIMATELY 2 MINUTES. MAINTENANCE TROUBLESHOT AND FOUND GENEROUS AMOUNT OF WATER IN LINES TO SECOND SEGMENT CLIMB SWITCHES. CLEARED LINES AND REPLACED SWITCHES. AIRCRAFT OKAY FOR SERVICE.
Part: SKIN — CRACKED (BS 1494 L2-3R) · airframe 44,830 hrs · 23,862 cycles
DURING PSV, A CRACK WAS DISCOVERED IN THE FUSELAGE SKIN AT BS 1494 BETWEEN L2R AND L3R. ACCOMPLISHED REPAIR PER SRM 53-31-03 FIG 8.
Part: SKIN — CRACKED (BS 1475) · airframe 49,180 hrs · 26,275 cycles
FUSELAGE SKIN BS 1475 L2L CRACKED, REPAIRED IAW ERA 500312-14, REV B.
Part: FRAME — CRACKED (BS 1542) · airframe 44,830 hrs · 23,862 cycles
CANTED FRAME AT BS 1542 WAS FOUND WITH A CRACK APPROX .5". THE CRACK RUNS FROM THE CORNER INBD NEAR ZR=-30. REPAIR IAW ERA 500264-14.
Part: SKIN — CRACKED (BS 1475, L3L) · airframe 44,830 hrs · 23,862 cycles
DURING PSV, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 1475 AND L3L. REPAIRED PER ER/A 500312-14.
Part: SCREW — LOOSE (TAIL CONE) · airframe 44,830 hrs · 23,862 cycles
TAIL CONE JETTISON NOZZLE, MISSING SCREW AND OTHER OTHER SCREWS LOOSE. INSTALLED NEW SCREW AND TIGHTENED REMAINING 3 LOOSE SCREWS.
Part: RELEASE CABLE — FRAYED (TAIL CONE) · airframe 44,830 hrs · 23,862 cycles
TAIL CONE JETTISON BOTTLE CABLE FRAYED. REMOVED AND REPLACED CABLE. INSTALLED ON AIRCRAFT SIDE. CONNECTION TO TAIL CONE ACCOMPLISHED.
Part: RELEASE CABLE — MISINSTALLED (TAIL CONE) · airframe 44,830 hrs · 23,862 cycles
TAIL CONE JETTISON BOTTLE ACTUATION CABLE IMPROPERLY INSTALLED, WRAPPED AROUND BOTTLE. REMOVED AND REPLACED CABLE.
2011
Part: CONNECTOR — DEFECTIVE (CATWALK) · airframe 44,033 hrs · 23,485 cycles
DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY LIGHT OVERAFT CATWALK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CONNECTOR. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.
Part: WIRE — DISCONNECTED (CABIN) · airframe 43,007 hrs · 22,962 cycles
DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD FIRST CLASS CABIN EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE FOUND WIRES DISCONNECTED ABOVE CEILING PANEL AND RECONNECTED THEM. OPERATION CHECKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,007 hrs · 22,962 cycles
DURING LINE CHECK, MAINTENANCE FOUND SEVERAL EMERGENCY CEILING LIGHTS INOPERATIVE IN CABIN. MAINTENANCE REPLACED THE BULBS. OPERATION CHECKS GOOD. AIRCRAFT OKAY FOR SERVICE.
Part: LANYARD — DISCONNECTED (EVAC SLIDE) · airframe 42,446 hrs · 22,719 cycles
OPERATIONS REPORTED L-1 DOOR SLIDE BUSTLE RELEASE LANYARD DISCONNECTED. MAINTENANCE RE-SECURED LANYARD PER MAINTENANCE MANUAL. AIRCRAFT OKAY FOR SERVICE.
Part: CUSP WEB — PUNCTURED (BS 146 RBL 1) · airframe 42,292 hrs · 22,655 cycles
PUNCTURE DAMAGE WAS FOUND ON FLOOR CUSP WEB. PUNCTURES ARE LOCATED AT BS 146, RBL1. REPAIR IAW ERA 490154-14.
Part: BRACKET — DISCONNECTED (L2 DOOR SLIDE) · airframe 42,265 hrs · 22,642 cycles
FLIGHT CREW FOUND SLIDE PACK BRACKET DISCONNECTED AT DOOR 2L. MX RECONNECTED SLIDE PACK LOWER CLIP. ACFT OK FOR SERVICE.
Part: OVEN — ODOR (GALLEY) · airframe 42,082 hrs · 22,576 cycles
ON FLIGHT 1497, CABIN CREW REPORTED A BURNING ODOR ORIGINATING FROM GALLEY OVEN WHEN IN THE ON POSITION. CIRCUIT BREAKER WAS PULLED AND ODOR DISSIPATED. MX CLEANED HEATING ELEMENTS, OPERATED OVEN AND OVEN NOW CHECKS NORMAL.
2010
Part: FRAME — CRACKED (BS 962) · airframe 41,242 hrs · 22,213 cycles
FATIGUE CRACK IN FRAME FS 962 RT. R & R FRAME EO 02-460094-12AD REVA ME03 OPN0301.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 41,241 hrs · 22,212 cycles
OVERWING EXIT FRAME 962 RT WAS FOUND CRACKED AND R & R IAW EA 02-460094-12AD.
Part: LIGHT — DAMAGED (CABIN) · airframe 40,985 hrs · 22,087 cycles
EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE & DAMAGED. MAINTENANCE REPLACED THE LIGHT MODULE ASSEMBLY. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE
Part: WIRE — BROKEN (CABIN) · airframe 40,893 hrs · 22,044 cycles
THE EMERGENCY LIGHT AT SEAT 3C WAS FOUND TO BE INOPERATIVE /DAMAGED. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE TRACK COVER. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0900) (DLM90101964).
Part: DISTRIBUTOR — OVERHEATED (COMM SYSTEM) · airframe 40,616 hrs · 21,922 cycles
ON APPROACH THE CABIN CREW REPORTED THAT THEY HAD A SMELL OF SMOKE/ODOR. NO VISIBLE SMOKE AND THE ODOR DISSIPATED WITHIN A FEW MINUTES. MX FOUND DISTRIBUTION UNIT AT 22E OVERHEATED. UNIT WAS REPLACED UNIT AND NEW UNIT OVER HEATED.(DLM90101581)
Part: LIGHT — INOPERATIVE (SEAT 3C) · airframe 40,413 hrs · 21,811 cycles
ON 18MAY, THE INBOUND FLIGHT PILOT WROTE UP A FLOOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 3C AS INOPERATIVE. MX FORWARDED THE LOG TO MX CONTROL WHO PLACARDED IT DUE TO PARTS NOT AVAILABLE . ON 26MAY, MX REPLACED RECEPTACLE AND LENS. OPS CHECK OF LIGHT, NOW CHECKS GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 40,042 hrs · 21,600 cycles
EMERG FLOOR PROX ESCAPE PATH LIGHTING BY SEAT 03C LOOSE, 2 ADJACENT WHITE LIGHTS INOP. FOUND BOTH BULBS BURNED OUT. RELAMPED SAME. OPS NORMAL AT THIS TIME. MCO AND PLACARD REMOVED.
Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 39,858 hrs · 21,471 cycles
CABIN EMERGENCY PATH LIGHTS INOP. SPLICED BROKEN WIRES LIGHTS TEST GOOD.
2009
Part: SKIN — DENTED (BS 271) · airframe 38,791 hrs · 20,825 cycles
MX FOUND A DENT AT THE FWD LAV DRAIN HOLE AT BS 271 AND BETWEEN L29-30R. REPAIR IAW ERA 477270-14.
Part: FLAP — DENTED (WING) · airframe 38,461 hrs · 20,637 cycles
RE-INSPECTION OF THE DENT FOUND ANOTHER DENT, ON 08/01/09. NO EMERGENCY PROCEDURE REQUIRE, WILL NEED A SRM/ERA REPAIR. UNKNOWN ON WHAT CAUSE THE DENTS. A PERMANENT REPAIR DONE AT ATL.
Part: SKIN — CRACKED (RT STABILIZER) · airframe 37,747 hrs · 20,235 cycles
RIGHT STABILIZER UPPER SKIN INBD FOUND CRACKED 1.2500" LONG. REPAIR IAW 02-460214-12 ME06.
Part: SKIN — CRACKED (LT STABILIZER) · airframe 37,747 hrs · 20,235 cycles
LEFT STABILIZER UPPER SKIN WAS CRACKED 1.2500" LENGTH INBD AFT END. REPAIR IAW 02-460214-12 ME05 (02-460214-12).
2008
Part: SPAR — DENTED (HORIZ STAB) · airframe 37,019 hrs · 19,802 cycles
RT HORZ STAB UPPER SKIN AND REAR SPAR UPPER CHORD FLANGE COMMON TO XFS 165 HAD AN EDGE DENT AND GOUGE. THE DAMAGE WAS TRIMMED OUT, TREATED AND PAINTED.
Part: HEATER — SHORTED (VENT) · airframe 35,722 hrs · 19,022 cycles
WASTE OVBD VENT TEE HEATER SHORTED OUT AND BURNT A 3 INCH HOLE IN THE TEE THEN THE A/C COULD NOT PRESSURIZE WITH 1 PACK.
2007
Part: UPLOCK SENSOR — OUT OF ADJUST (RIGHT) · airframe 34,366 hrs · 18,235 cycles
RT MLG SLOW TO RETRACT. FOUND SENSOR D1-25 OUT OF ADJUSTMENT ADJUSTED SAME CKS OK.
Part: SKIN — CRACKED (FS 1476) · airframe 34,241 hrs · 18,166 cycles
FS 1476 UPPER FUSELAGE RIGHT SKIN IS CRACKED BELOW LOWER FORWARD VERTICAL STABILIZER FAIRING. REPAIRED SKIN AT FS 1476 BELOW VERTICAL STABILIZER FAIRING IAW DELTA EA 464026-14AD. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ERA REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 24 MONTHS FROM REPAIR ACCOMPLISHMENT.
Part: ATTACH ANGLE — CORRODED (BS 1458-1475) · airframe 34,241 hrs · 18,166 cycles
AFT ACCESSORY BETWEEN STA 1458 AND 1475 AIRSTAIR CUTOUT RIGHT OUTBOARD SIDE ATTACH ANGLE IS CORRODED. REMOVED AND REPLACED ANGLE IAW MD90 SRM 51-30-02 AND 51-30-05.
Part: SKIN PANEL — CRACKED (BS 1476 S2R) · airframe 34,241 hrs · 18,166 cycles
DURING HMV AT AAR/OKC, THE FUSELAGE SKIN PANEL WAS FOUND CRACKED AT STA 1476, S-2R. THE DAMAGE WAS REPAIRED PER ER/A 02-464026-14AD.
Part: LONGERON — CORRODED (BS 1385 L29L) · airframe 34,241 hrs · 18,166 cycles
AFT PIT LONGERON 29L CORRODED AROUND FASTENER AT STA 1385. REPAIRED IAW MD90 SRM 53-10-01 FIG 7.
Part: SEAT TRACK — GOUGED (FS 648 TO FS 740) · airframe 34,241 hrs · 18,166 cycles
FOUND CABIN SEAT TRACK RBL 24 IS OUT OF LIMITS AT FS 700. REPAIRED SEAT TRACK RBL 24 FROM FS 648 TO FS 740 IAW MD90 SRM 53-40-01 FIG 6.
Part: SEAT TRACK — GOUGED (BS 1130) · airframe 34,241 hrs · 18,166 cycles
CABIN SEAT TRACK RBL 24 IS OUT OF LIMITS AT FS 1130. REPAIRED CABIN SEAT TRACK RBL 24 FS 973 TO 1184 IAW MD90 SRM 53-40-01 FIG 6.
Part: CUSP WEB — CORRODED (FS 655-769) · airframe 34,241 hrs · 18,166 cycles
FOUND LEFT CUSP WEB CORRODED FS 655 TO FS 769. REMOVED AND REPLACED CUSP WEB, LT IAW MD90 SRM 51-30-2, 51-30-5 AND 51-30-1.
Part: FRAME — CRACKED (BS 1542) · airframe 34,241 hrs · 18,166 cycles
AFT ACC BAY STA 1542 CANT FRAME IS CRACKED RT JUST O/B OF AIRSTAIR CUTOUT. REPAIRED FRAME IAW MD90 SRM 51-70-01 FIG 1.
Part: PAN — GOUGED (CARGO DOOR) · airframe 34,241 hrs · 18,166 cycles
C-1 DOOR PAN GOUGED AT LWR AFT LATCH CAM. REPAIRED DAMAGED AREA ON C-1 DR IAW MD80 SRM 52-05D FIG 26B SH2.
Part: SKIN — DENTED (BS 1379 S28-29L) · airframe 34,241 hrs · 18,166 cycles
FOUND MINOR DENT AT STA 1379 BETWEEN S28L AND 29L WITHIN LIMITS PER SRM 53-30-02 TABLE 3 CONDITION 2 WILL REQUIRE REPAIR WITHIN 3500 FLT HOURS. REPAIRED DAMAGED AREA AT STA 1379 BETWEEN S 28L AND 29L IAW MD90 SRM 53-30-01 FIG 1. INSTALLED ID TAG IAW DAL PS 900-5-1 NR 4.
Part: PAN — CORRODED (CARGO DOOR) · airframe 34,241 hrs · 18,166 cycles
FWD CARGO DOOR FRAME PAN LWR VERT AND HORIZ LEGS CORRODED FS 370 TO 427. REPAIRED FWD CARGO DOOR FRAME PAN IAW MD88 SRM 53-05D FIG 44.
Part: SKIN — DAMAGED (FS 225 L30L) · airframe 34,241 hrs · 18,166 cycles
FWD CARGO COMPT FS 225 L30 DRAIN ATTACHMENT HOLES LARGER THAN ALLOWABLE LIMITS. REPAIRED DAMAGED AREA IN SKIN FS 225 L30 IAW MD80 SRM 53 04D FIG 12B.
Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 34,241 hrs · 18,166 cycles
MID PIT LOWER DOOR JAMB IS CORRODED. REPAIRED MID PIT LWR DOOR JAMB IAW MD80 SRM 53-05D FIG 63.
Part: FLOORBEAM — CORRODED (BS 1364) · airframe 34,241 hrs · 18,166 cycles
FLOORBEAM AT FS 1364 BETWEEN ENG PYLON SUPPORT BLKHDS HAS CORROSION. REPAIRED FLOORBEAM AT FS 1364 BETWEEN ENG PYLON SUPPORT BLKHDS IAW MD90 SRM 53 20 01 FIG 2 AND 51 70 01 FIG 2.
Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 34,241 hrs · 18,166 cycles
MULTIPLE SCRATCHES ON FWD CARGO DOOR OUTER SKIN. REPAIRED FWD CARGO DOOR IAW MD-90 SRM 52-01-01 FIG 3 VOL 1 ON N/R 8000-0054 ON HMV-2 IN OKC.
Part: SKIN — PUNCTURED (LT WING) · airframe 34,241 hrs · 18,166 cycles
LT FIXED WING L/E SKIN STA XRS 105.000 HAS A PUNCTURE. REPAIRED L/E SKIN IAW MD-90 SRM 57-20-01 FIG 11 VOL 1 ON N/R 5200-0043 ON HMV-2 IN OKC.
Part: CUSP WEB — CORRODED (BS 1136-1155) · airframe 34,241 hrs · 18,166 cycles
RT CUSP WEB CORRODED STA 1136-1155. REMOVED AND REPLACED CUSP WEB AT STA 1136-1155 IAW MD-90 SRM 51-30-02, 51-30-05, 51-10-05, 51-30-01 ON N/R 2000-0110 AT HMV-2 IN OKC.
Part: FLOOR SKIN — CORRODED (FS 150 RBL 54) · airframe 34,241 hrs · 18,166 cycles
FLOOR WEB CORRODED AT STATION 150 NAD RBL 54. REPAIRED WEB IAW MD-90 SRM 51-11-01 FIG 2 ON N/R 63278 AT HMV-2 IN OKC.
Part: DRAIN — CORRODED (FS 296 L30) · airframe 34,241 hrs · 18,166 cycles
FWD CARGO COMPARTMENT FS 295 L30 DRAIN ATTACHMENT HOLES LARGER THAN ALLOWABLE LIMITS. REPAIRED DAMAGED AREA AT FS 295 L30 IAW MD-90 FIG 12B SHEET 7ON N/R 63399 AT HMV-2 IN OKC.
Part: STRUCTURE — BENT (L1 DOOR) · airframe 34,241 hrs · 18,166 cycles
L-1 DOOR LOWER LIP IS BENT IN 2 PLACES. REPAIRED LOWER LIP IAW MD-90 SRM VOL 2 51-30-01 AND 52-10-01 FIG 2 VOL 1 ON N/R 62422 AT HMV-2 IN OKC.
Part: SEAT TRACK — CORRODED (BS 1360) · airframe 34,241 hrs · 18,166 cycles
AFT CABIN LBL 44 SEAT TRACK I/B FLANGE IS EXFOLIATED AT FS 1360. REPAIRED SEAT TRACK LBL 44 IAW MD-90 SRM 53-40-FIG 6 ON N/R 63297 AT HMV-2 IN OKC.
Part: SKIN — GOUGED (BS 1310-1330) · airframe 34,241 hrs · 18,166 cycles
RT FUSELAGE SKIN 4 FEET AFT OF C-3 DOOR HAS SCRATCH THAT IS OUT OF LIMITS. REPAIRED SKIN WITH EXTERNAL DOUBLER IAW MD90 SRM 53-04D FIG 12B AT FS 1310 TO 1330 AND L-21R TO L23R.
Part: SEAT TRACK — CORRODED (BS 503) · airframe 34,241 hrs · 18,166 cycles
SEAT TRACK AT LBL54 STA 503 IS CORRODED OUT OF LIMITS. REPAIRED IAW SRM 53-40-01 VOL 1 FIG 6.
Part: SEAT TRACK — CORRODED (BS 655 - 674) · airframe 34,241 hrs · 18,166 cycles
SEAT TRACK AT RBL 54 CORRODED OUT OF LIMITS, STA 655 - 674. REPAIRED SEAT TRACK IAW MD90 SRM53-40-01 VOL 1 FIG 6.
Part: CUSP WEB — CORRODED (BS 558) · airframe 34,241 hrs · 18,166 cycles
RT CUSP WEB CORRODED STA 558. REPLACED CUSP WEB ON WORK ORDER 1002987 2400 0227, DL 63329.
Part: CUSP WEB — CORRODED (BS 541 L18R) · airframe 34,241 hrs · 18,166 cycles
CORROSION AT STA 544 AT LONGERON 18R ON LWR SIDE OF WEB. CUSP WEB REPLACED ON W/O 1002987-2400-0227, DL63329.
Part: CUSP WEB — CORRODED (BS 522 - 541) · airframe 34,241 hrs · 18,166 cycles
RT CUSP WEB CORRODED STA 522-541. CUSP WEB REPLACED ON W/O 1002987 2400 0227. DL 63329
Part: SEAT TRACK — CORRODED (BS 826-845) · airframe 34,241 hrs · 18,166 cycles
SEAT TRACK AT RBL 54 STA 826-845 CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW MD90 SRM 53-40-1 VOL 1 FIG 9.
Part: CUSP WEB — CORRODED (BS 503-522) · airframe 34,241 hrs · 18,166 cycles
RT CUSP WEB CORRODED STA 503 - 522. CUSP WEB REPLACED ON W/O 102897 2400 0227, DL 63329.
Part: SEAT TRACK — CORRODED (BS 1328) · airframe 34,241 hrs · 18,166 cycles
SEAT TRACK AT LBL54 STA 1328 IS CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW MD90 SRM 53-40-01 VOL1 FIG 6.
Part: CUSP WEB — CRACKED (BS 1364) · airframe 34,241 hrs · 18,166 cycles
LT CUSP WEB CRACKED AT LIGHTENING HOLE STA 1364. REPAIRED CUSP WEB IAW MD90 SRM 51-11-01 FIG 2.
Part: SEAT TRACK — CORRODED (BS 588-626 L24) · airframe 34,241 hrs · 18,166 cycles
FOUND CABIN SEAT TRACK CORRODED AT STA 612. REPAIRED SEAT TRACK IAW MD90 SRM 53-40-01 VOL I.
Part: CUSP WEB — CORRODED (BS 924) · airframe 34,241 hrs · 18,166 cycles
FOUND LT CUSP WEB CORRODED AT STA 924. REPAIRED LEFT CUSP WEB IAW MD90 SRM 53-06-05 FIG 827D.
Part: SEAT TRACK — CORRODED (BS 1260-1364) · airframe 34,241 hrs · 18,166 cycles
CABIN SEAT TRACK CORRODED BEYOND LIMITS AT LBL24 STA 1260 - 1364. REPLACED SEAT TRACK SECTION IAW MD90 SRM VII 51-30-01 VOL 1.
Part: CUSP WEB — CORRODED (BS 769-788) · airframe 34,241 hrs · 18,166 cycles
CSP WEB CORRODED OOL AT STA 769 - 788 LT SIDE. REPAIRED IAW ERA 3981911-14MA REV ORIG AND SRM 53-00-011 VOL III.
Part: FRAME — CORRODED (BS 1344 S28-29L) · airframe 34,241 hrs · 18,166 cycles
AFT PIT FWD SIDE OF FRAME CORRODED STA1344 28L-29R. REPAIRED FRAME AT STA 1344 IAW MD90 SRM 53-10-02A VOL I.
Part: CUSP WEB — CORRODED (FS 598-655) · airframe 34,241 hrs · 18,166 cycles
PAX CABIN LT CUSP WEB IS CORRODED AT FS 598-655. REMOVED AND REPLACED WITH NEW WEB IAW MD-90 SRM 51-10-05 AND 51-30-02 ON N/R 63156 AT HMV-2 IN OKC.
Part: BOTTLE — DISCHARGED (EVAC SLIDE) · airframe 32,893 hrs · 17,402 cycles
FLIGHT ATTENDANT WAS ARMING SLIDE AT POSITION 2E WHEN HEARD A LOUD HISSING SOUND (NOT INTENTIONAL). THE BOTTLE DEPLETED BUT THE SLIDE DID NOT INFLATE AT ALL. THE AMT'S OPENED THE PARACHUTE PINS TO INSPECT THE SLIDE PACK AND SUSPECT THAT THE DEFLATION VALVE WAS PARTIALY OPENED, P/N 100505-201 S/N D9A011 ROUTED TO REPAIR SUPPLIER USING REPAIR PO 4800028600. SLIDE WAS REPLACED ON THE A/C.
2005
Part: SLIDE — NO TEST (TAIL) · airframe 29,560 hrs · 15,489 cycles
PERFORMED OPN 6900 AND SLIDE DID NOT DEPLOY. ADJUSTED AFT STRAPS PER FIG 18 AND SLIDE DEPLOYED AS REQUIRED.
2004
Part: ODOR — DETECTED (CABIN) · airframe 26,749 hrs · 14,038 cycles
WHILE AT GATE FLIGHT ATTENDANTS REPORT SMELL AND FUMES IN CABIN. SUSPECT LEFT PACK OVERHEAT. REPLACED COALESCER BAGS AND CHECKED ENGINES AND APU FOR LEAKS. NONE FOUND. RAN PACKS FOR 30 MINUTES, NO MORE ODOR. PACK TEMP CONTROLS ARE BOTH GOOD IN AUTO MANUAL. CHECKS ARE GOOD PER MD90 TROUBLESHOOTING MANUAL.
2001
Part: TIRE — SEPARATED (NLG) · airframe 18,634 hrs · 9,977 cycles
AFTER TAKEOFF AND RAISING LANDING GEAR, UNSAFE NOSE GEAR INDICATION WITH LANDING GEAR HANDLE UP. CONFIRMED BY AIRPORT OPERATIONS RUBBER/GLASS ON THE RUNWAY. AIRCRAFT RECONFIGURED FUEL BURNED DOWN, LANDING ACCOMPLISHED AT 142,200 GROSS WT. RT NOSE TIRE CAP SEPARATED, TIRE NOT BLOWN, TIRE PSI 190 PSI ON ARRIVAL PER TRANS CK LIMITS. REPLACED RT NOSE TIRE, NOSE GEAR SWING CKD OK.
Part: LENS — DAMAGED (CABIN) · airframe 17,935 hrs · 9,600 cycles
PAX SEAT 3C EMERGENCY LIGHT DAMAGED. REPLACED LENS AND LIGHT BULB.
Part: PUMP — FAILED (FUEL BOOST) · airframe 17,126 hrs · 9,166 cycles
BOTH CENTER BOOST PUMP B PHASE C/BS POPPED IN FLIGHT. TRIED RESETTING BUT POPPED AGAIN. TROUBLESHOOTING CNTR BOOST PUMP C/BS POPPING. REPLACED BOTHCNTR BOOST PUMPS. OPS CHECKS NORMAL AND ACCESS PANELS INSTALLED.
2000
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 15,778 hrs · 8,482 cycles
AFT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,899 hrs · 8,030 cycles
THE FS 1520 CANTED BULKHEAD WEB WAS FOUND WITH A 4.5 INCH CRACK ALONG THE WEB SPLICE JOGGLE LINE AT STRINGER 8L. THE WEB WAS CUT TO REMOVE THE DAMAGED SECTION. A NEW SECTION OF WEB WAS SPLICED IN WITH AN ALUMINUM DOUBLER AND TRIPLER PER ER/A 377529-14, REV A.
1999
Part: BULB — FAILED (RT MLG)
ON LANDING DFW PLACED GEAR HANDLE DOWN AND HAD NO GREEN LIGHT ON RIGHT MAIN. FOLLOWED CHECK LIST PER POM. FOUND BOTH BULBS INOP. RELAMPED SAME. SIMULATED GEAR SWING USING SLUGS, ALL CHECK NORMAL.
Part: COALESCER BAG — DIRTY (CABIN)
OILY SMELL FROM AIR CONDITION SYSTEM AFTER TAKEOFF. REMOVED ACCESS PANEL AND INSULATION BARRIER FOR H2O SEPARATOR BAGS. REPLACED H2O SEPARATOR BAGS, RUN LEAK CK AND OPERATIONAL NORMAL. REINSTALLED PANELS. CHECKED A/C AND APU FOR LEAKS, CHECKED OK. CLEANED APU INLET AND DOOR ASSY, PERFORMED DUCT BURN OUT, RAN PACKS AND NO ODORS.
1998
Part: WINDSHIELD — FAILED (COCKPIT)
BURNING SMELL FROM BEHIND TRIM AT CAPT/CENTER WINDSHIELD. FOUND WINDOW HEAT CONNECTION TERMINAL DAMAGED. REPLACED CONNECTOR AND HARNESS. ALSO, REPLACED WINDSHIELD.
1996
Part: FILTER BOWL — CRACKED (RT ENGINE)
RIGHT AC FAULT CAME ON DURING CRUISE, ALONG WITH STATUS MSG RT GEN OIL PRESS. STARTED APU AND PICKED UP RT AC LOAD. THEN RTI GEN OFF ILLUMINATED. FOUND RT VSCF GEN OIL LOW WITH FILTER HOUSING CRACKED AND LEAKING. REPLACED FILTER BOWL. SERVICED, OPERATION NORMAL.